N641GT

Boeing 767 None injury Part 121 — ATLAS AIR INC

ATA 5210

L1 SLIDE RELEASE BUTTON NOT COME OUT. PERFORMED HANDLE MECHANISM ADJUSTMENT IAW AMM 52-11-25/201 & AMM 52-11-00/501. L1 DOOR OPS CHECKED GOOD.

ATA 3350

RIGHT AFT EXTERNAL EMERGENCY SLIDE LIGHT FWD OF AFT LWR CARGO DOOR INOP(<P>RELAMPED IAW B767 33-51-06. OPS CHECK GOOD. OK FOR SERVICE</P>)

ATA 3510

1ST OBS O2 MASK INOP CAUSING FEEDBACK(<P>R/R 1ST OBSERVER'S O2 MASK IAW AMM 35-11-51. OPS CHECKS GOOD</P>)

ATA 2562

ELT REQ REPLACEMENT. REMOVED AND REPLACED FIXED ELT REF AMM 23-24-01, OPS CHECK GOOD. PER MCC REQ, R/R FIXED ELT CRADLE BOX PER AMM 23-24-01. & IPC SMM CEIS MODEL AD6U2 PN: 9506076. OPS CHK GOOD.

ATA 2612

ALL AFT LAVS FIRE EXTINGUISHER TRASH CANS DO NOT HAVE WAX. FOUND ALL HEAT AND FIRE INDICATORS STRIPE WITH NO FIRE OR HEAT INDICATING IAW AMM 26-24-00/001. NO FURTHER DEFECTS NOTED.

ATA 2565

R4 ENTRY DOOR SLIDE ACTIVATED DUE TO FLT ATTENDANT INADVERTENT OPENING, DOOR ARMED. R & R DOOR SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED.

ATA 2560

L4 JUMPSEAT FLASHLIGHT OR BATTERY NOT CHARGING. REMOVED AND REPLACED FLASHLIGHT BATTERY REF AMM 25-64-00. OPS CHECK GOOD.

ATA 2565

R1 DOOR ESCAPE SLIDE PRESSURE LOW. REPLACED ESCAPE SLIDE PER AMM 25-66-01. NO FURTHER DEFECTS NOTED.

ATA 3397

R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE.(<P>FOUND R1 EMERGENCY EXIT SIGN LIGHT PLATE DISCONNECTED IAW WDM 33-51-14. RESECURED CONNECTOR AND LIGHT OPS CHECK GOOD IAW B767 AMM 33-51-09.</P>)

ATA 2560

PBE AT R4 DOOR MISSING TAMPER SEAL.(<P>R/R PBE IAW AMM 25-64-00-01. NO FURTHER DEFECTS NOTED. DMI 224468 CLOSED. REF IPC 25-64-54-19. OSD: 1/23/2025

ATA 2761

LH OVERWING EXIT INOP (MAIN ENTRY DOORS/SLIDES/EMERGENCY).(<P>R/R LEFT WING SPOILER BLOW DOWN ACTUATOR PER AMM 25-65-20. OPS CHECK GOOD. DMI 224324 CLOSED</P>)

ATA 2560

R1 RIGHT FORWARD ENTRY DOOR SLIDE WILL NOT ARM. INSTALLED SHIM ON GIRT BAR FITTING AND BEARING ASSY IAW AMM 52-11-00/501 AND IPC 52-11-41-01. OPS CHECK GOOD. DOOR ARMS PROPERLY.</P>)

ATA 3350

EMERGENCY LIGHTS TEST, EMERGENCY LIGHT OF CEILING PANELS ROWS 16 LH AND 19 RH INOP(<P>EMERGENCY LIGHTS OF CEILING PANELS ROWS 16 LH AND 19 RH BULBS WERE REPLACED IAW AMM 33-51-04-002-001. OPS CHK GOOD</P>)

ATA 5414

CORROSION AT ENG 1 INLET COWL, INBD SIDE (INSIDE ACCESS PANEL) AT 8:00 O'CLOCK.(<P>ENG 1 INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED.</P>)

ATA 2565

REMOVAL AND INSTALATION OF SLIDE ON LEFT WING FOR ACCESS LOOSE BOLT(<P>THE LOOSE BOLT OF SLIDE ON LEFT WING WAS INSTALLED CORRECTLY IAW AMM 20-11-00-910-802. NO FURTHER DEFECTS NOTED</P>)

ATA 3445

CORROSION ON BASE ANTENNA TCAS UPPER FUSELAGE(<P>TCAS ANTENNA WAS REPLACED WITH SATISFACTORY TEST IAW AMM 34-45-02-344-158. TORQUE APPLIED 20-LB-IN S/N 924401137 DATE 30/SEP/25 BONDING METTER 0.8 MILLI OHM S/N 80005870</P>)

ATA 5511

LEFT HORIZONTAL STABILIZER TIP UPPER SURFACE WITH LIGHT CORROSION AT 4.5'' FROM TRAILING EDGE.(<P>STABILIZER TIP UPPER SURFACE AT 4.5'' FROM TRAILING EDGE BASE DISCHARGER WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED.</P>)

ATA 5410

ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD WITH SEALANT DAMAGE.(<P>ENGINE 2 LH CORE COWL (427AL), ZONE CC5, FIRE SHIELD SEALANT WAS RESTORED IAW AMM 78-31-00-308-072-H00. NO FURTHER DEFECTS NOTED</P>)

ATA 5220

BROKEN LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR.(<P>LINING DOOR COVER AT RH AFT EMERGENCY EXIT DOOR. WAS REPAIRED IAW AMM 25-00-00-308-166. NO FURTHER DEFECTS NOTED</P>)

ATA 5410

ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WITH WEAR.(<P>ENGINE #1 NACELLE STRUT FIRE SEAL ON NAC STA 256 INBOARD AND OUTBOARD SIDE WAS REPLACED IAW SRM 51-10-02-0G-0. NO FURTHER DEFECTS NOTED</P>)

ATA 2720

RUDDER, LOWER PCA WITH HYDRAULIC LEAK.(<P>RUDDER, LOWER PCA WAS ADJUSTED PER AMM 27-21-02-422-038. LEAK CHK GOOD. NO FURTHER DEFECTS NOTED.</P>)

ATA 5730

LH WING, UPPER SURFACE, BETWEEN REAR SPAR AND STGR L-10, WBL 97.9566 WITH CORROSION(<P>THE CORROSION AREA WAS REPAIRED BY INSTALLING 2 REPAIR DOUBLERS, 1 SKIN FILLER AND STRINGER SEGMENTS. THIS REPAIR INSTRUCTION WERE PROVIDED ON BOEING MESSAGE CMA-TLS-24 0218 &AMP; TRE 6757272. NO FURTHER DEFECTS NOTED</P>)

ATA 2810

RIGHT WING, DRY BAY WITH FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9(<P>FUEL LEAK ON LOWER AFT PART BETWEEN RIB 7 AND RIB9 RIGHT WING, RIGHT WING, DRY BAY WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED</P>)

ATA 2810

FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITTING.(<P>FUEL LEAK ON LH WING LOWER SURFACE WBL310.0 AT WING DIAGONAL BRACE WING FITTING WAS REPAIRED IAW AMM 28-11-00-308-013. LEAK CHECK GOOD. NO FURTHER DEFECTS NOTED.</P>)

ATA 2822

RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION(<P>RH WING, OUTBOARD HOUSING UNIT OF BOOST PUMP WITH CORROSION WAS REPLACED PER AMM 28-22-03-004-001. OPS CHK GOOD</P>)

ATA 3497

UPPER HALF OF FUSELAGE, TOP TCAS ANTENNA, FOUR CONNECTORS, WITH CORROSION.(<P>CONNECTORS WERE CLEANED AS CLIENT REQUIREMENT, CORROSION INHIBITING COMPOUND AV25 WAS USED AS PROTECION AGENT IAW SWPM 20-60-03. NO FURTHER DEFECTS NOTED</P>)

ATA 5330

MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD BETWEEN BSTA 933 TO BSTA 938.5 AND WL185.2 AT BBL 97.42.(<P>MISDRILLED ON LH FUSELAGE SKIN AND BODY RIB CHORD BETWEEN BSTA 933 TO BSTA 938.5 AND WL185.2 AT BBL 97.42. WAS REPAIRED IAW TRE 6753710 &AMP; FAA FORM 8100-9. NO FURTHER DEFECTS NOTED</P>)

ATA 5753

LEFT WING, INBOARD FLAP LOWER AREA BTW WS 314 AND WS404 WITH DELAMINATION.(<P>LEFT WING INBOARD FLAP LOWER AREA WAS REPAIRED IAW SRM 57-53-01-2R-1. NO FURTHER DEFECTS NOTED</P>)

ATA 5754

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 45'' FROM INBD EDGE AND 11'' FROM TE.(<P>LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE AT 45'' FROM INBD EDGE AND 11'' FROM TE WAS REPAIRED SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED</P>)

ATA 5754

LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE WITH BUCKLING AT 28'' FROM INBD EDGE AND 11'' FROM TE.(<P>LEFT WING, SLAT #3, TRAILING EDGE WEDGE UPPER SURFACE AT 28'' FROM INBD EDGE AND 11'' FROM TE WAS REPAIRED IAW SRM 57-43-02-2R-1. NO FURTHER DEFECTS NOTED.</P>)

ATA 5330

SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(<P>SERVICE DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW SRM 53-10-01-2R-1. NO FURTHER DEFECTS NOTED.

ATA 5330

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP.(<P>FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER FUSELAGE SKIN AND BEAR STRAP, CRACK WAS REPAIRED IAW SRM 53-10-01-2R-1. NO FURTHER DEFECTS NOTED.</P>)

ATA 5414

ENG 1, INLET COWL, ZONE 411, WITH POINTS OF CORROSION INNER ACCESS 412, AT INNER BARREL SKIN SURFACE, AT 12 HRS POSITION.(<P>&NBSP;ENG 1, INLET COWL WAS REPLACED IAW AMM 71-11-01-004-002-H00. NO FURTHER DEFECTS NOTED</P>)

ATA 5220

RIGHT OVERWING ESCAPE STEP MISALIGNED(<P><SPAN>REMOVED RIGHT AFT EMERGENCY ESCAPE HATCH. REALIGNED ESCAPE STEP, REINSTALLED RIGHT AFT EMERGENCY HATCH PER AMM 52-21-01</SPAN></P>)

ATA 3350

1 EA OVERHEAD EMER LT INOP NEAR 30AC(<P>RELAMPED 1 EA EMER LT 30AC &AMP; OPS CHK OK IAW AMM 33-51-07</P>)

ATA 5410

ENGINE # 1 AFT NACELLE O/B ACCESS DOOR REAR HINGE FITTING WITH BOLT LOOSE(<P>REMOVED DAMAGE ANGLE AT ENG 1, AFT NACCELLE O/B ACCESS DOOR REAR HINGE FITTING AREA, LOCATED, CLEANED, PREPARED, DRILLED, SECURED AND INSTALLED NEW ANGLE, COMPLETED ASSEMBLY, NO FURTHER DISCREPANCIES NOTED, AT ENG #1, AFT NACCELE O/B ACCESS DOOR REAR HINGE, PER BOEING 767 SRM&NBSP;</P> / <P>51-40-02-0G-0</P>)

ATA 7830

ENGINE #2 INB T/R VALVE TO OPEN AND CLOSE C/DUCT INOP.(<P>REMOVED AND REPLACED OPENING VALVE AT #2 REVERSER INBOARD HALF IAW AMM 78-31-03. INSTALLED REVERSER COWLING OPENING FITTING DUST CAP &AMP; OPS CHECK OK&NBSP;</P>)

ATA 3500

FWD CLOSET PORTABLE OXYGEN BOTTLE MFG LABEL DAMAGE P/N 9700C1A-BF23A(<P>REMOVED AND REPLACED PORTABLE OXYGEN CYLINDER LOCATED IN CABIN FWD CLOSET AS REQUIRED IAW AMM&NBSP;</P> / <P>35-11-01. OPS &AMP; LEAK CHECK GOOD</P>)

ATA 5340

AFT MEGAPHONE BRACKET DAMAGE LH AFT CLOSET(<P>REMOVED DAMAGED BRACKET ASSY AT AFT MEGAPHONE BY LH AFT CLOSET, MD. LOCATED, CLEARED, PREPARED, SECURED AND INSTALLED NEW BRACKET ASSY, PER BOEING 767 SRM 51-40-02-06-0</P>)

ATA 5410

ENG #2 NACELLE STRUT INBOARD DOOR WITH LATCH LOOSE(<P>LOCATED, CLEANED, PREPARED &AMP; REMOVED ADJUSTABLE BOLT &AMP; SAFETY WIRE, PROCEED TO PERFORM ADJUSTMENT, RIGGING AS REQUIRE, RESECURED AND RE-INSTALL BOLT AFTER VERIFIED. NO FURTHER DISCREPANCIES. PERFORM SAFETY WIRE AS PER B767-300 SRM 51-40-02-0G-0 &AMP; AMM 20-10-23-964-001.</P>)

ATA 2620

FIRE BOTTLE LEAKED(<P>REMOVED AND REPLACED FIRE BOTTLE IAW EO 6725A252. OK FOR SERVICE</P>)

ATA 3397

R1 LOWER EMERGENCY EXIT SIGN WILL NOT ILLUMINATE. FOUND R1 EMERGENCY EXIT SIGN PLATE DISCONNECTED. RECONNECTED PER WDM 33-51-14. OPS CHECK GOOD PER AMM 33-51-09.

ATA 3350

DURING OPERATIONAL CHECK OF EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS FOUND WITH FAIL(<P>EMERGENCY LIGHTS ATTENDANT´S SWITCH WAS REPLACED PER AMM 33-51-00. NO FURTHER DEFECTS NOTED.</P>)

ATA 3350

DURING OPERATIONAL TEST EXTERIOR EMERGENCY LIGHTS, THREE RIGHT REAR LIGHTS DO NOT OPERATE IN STA 1197, STA 1219, AND 1562.(<P>THE M733 POWER SUPPLY BATTERY PACK WAS CHANGED PER AMM 24-54-00. OPS CHK GOOD.</P>)

ATA 3350

LEFT OVERWING EMERGENCY EXIT SIGN FOUND LOOSE(<P>RE-SECURED LEFT WING EMERGENCY EXIT SIGN. SECURED IAW AMM 33-51-01</P>)

ATA 2600

LI-ION EXTINGUSHING AGENT P/N LKFD IN RH SIDE LAST OVERHEAD BIN FOUND LEAKING NEEDS REPLACMENT(<P>REMOVED AND REPLACED LI-ION EXTINGUISHING AGENT REFERENCE ATLAS AIR EMERGENCY EQUIPMENT CONFIGURATION - 641GT&NBSP;</P>)

ATA 2560

L1 PBE INDICATOR STRIP SHOWS RED(<P><SPAN>REMOVED AND REPLACED PBE AT L1 DOOR IAW AMM 25-64-00</SPAN></P>)

ATA 2560

CAPT & F/O EVAS INOP(<P>INSTALLED NEW EVAS SECURITY SEAL STICKERS IAW EO6725A222. NO FURTHER DEFECTS NOTED</P>)

ATA 3520

FLIGHT ATTENDANT SEAT L4A PSU INOP.(<P>TRANSFER TO MDDR 189255 PER MEL 35-21-01-01A CAT B, DUE DATE 7/17/2023</P>)

ATA 5310

FUSELAGE SKIN BETWEEN STA 157 AND STRINGER S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5310

LH FUSELAGE SKIN BETWEEN STA 158.2 AND BELOW WL220 WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS</P>)

ATA 5310

FUSELAGE SKIN BETWEEN STA 143 / STA 157 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5310

FUSELAGE SKIN BETWEEN STA 132 / STA 143 AND S-21 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5320

UPPER FUSELAGE SKIN BETWEEN STA 566 / STA 588 AND S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5320

UPPER FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5320

UPPER FUSELAGE SKIN BETWEEN STA 456 / STA 478 AND S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5310

UPPER FUSELAGE SKIN BETWEEN STA 266.5 / STA 276 AND S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 2560

RH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH AFT SERVICE DOOR (843) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 2560

RH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, BOTH SPRINGS LOOSE(<P>RH FWD SERVICE DOOR (841) BOTTOM GIRT BAR CARRIER, WAS REPLACED PER AMM 25-66-03-404-098 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5320

UPPER HALF FUSELAGE SKIN BETWEEN STA 544 / STA 566 AND STRINGER S-1 RH WITH LIGHTNING STRIKE DAMAGE(<P>&NBSP;LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 2800

FUEL LEAK ON PORT OF DRY BAY AT LH WING TANK(<P>FUEL LEAK WAS REPAIRED ON PORT OF DRY BAY AT LH WING TANK THE FUEL LEAK TEST WAS SATISFACTORY PER AMM 28-11-00-30-8-013</P>)

ATA 5310

UPPER HALF FUSELAGE SKIN BETWEEN STA 412 / STA 434 AND STRINGER S-1 RH / S-2 RH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS</P>)

ATA 5310

UPPER HALF FUSELAGE SKIN AT STA 287 AND STRINGER S-1 LH / S-2 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5310

UPPER HALF FUSELAGE SKIN AT STA 266.5 AND STRINGER S-3 LH / S-4 LH WITH LIGHTNING STRIKE DAMAGE(<P>LIGHTNING STRIKE DAMAGE WAS REPAIRED PER SRM 53-00-01-2R-8, REPAIR 8, FIG 201 REQUIREMENTS. NO FURTHER DEFECTS NOTED</P>)

ATA 5310

CORROSION ON KEEL BEAM HORIZONTAL WEB BETWEEN STA 785.9 / STA 880(<P>REPAIR WAS ATTENDED BY SR 3-5696704793 (MXA EO TRE6753615) APPROVED BY FAA FORM 8100-9</P>)

ATA 3350

L1 DOOR LOWER EXIT LIGHT HA BURNT OUT BULBS(<P>DURING REPLACEMENT FOUND EXIT SIGN HAS DAMAGED CLIP REMOVED AND REPLACED LENS COVER IAW 33-51-8. OK FOR SERVICE.</P>)

ATA 3350

L1 EXIT SIGN LOOSE.(<P>SECURED L1 EXIT SIGN IAW AMM 33-51-01. NO FURTHER DEFECTS NOTED</P>)

ATA 3300

EXIT LIGHT ASSY AT L4 BROKEN.(<P>REMOVED AND REPLACED EXIT LIGHT ASSY AT L4 PER B767 AMM 33-51-01</P>)

ATA 2500

AFT CARGO DOOR, REAR UPPER STOP LOOSE .(<P>RETORQUED AFT CARGO DOOR REAR UPPER STOP PER AMM 20-11-00.</P>)

ATA 3510

RIGHT OFF WING SLIDE INFLATION BOTTLE PIN WARNING STREAMER DAMAGED .(<P>REPLACED INFLATION CYLINDER SAFETY PIN WITH DAMAGED STREAMER ON RH WING AS REQUIRED IAW AMM 25-65-00-442-410 STEP 10.</P>)

ATA 4920

L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 OUT OF SERVICE DATE(<P>REMOVED AND REPLACED L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 AS REQUIRED IAW B767 AMM 35-21-04.</P>)

ATA 2500

AFT CARGO DOOR CUT OUT AFT UPPER STOP IS LOOSE(<P>SECURED STOP AT AFT CARGO DOOR CUT OUT AFT FRAME IAW B767 SRM 51-40-02</P>)

ATA 3050

LOWER FUSELAGE, DME ANTENNA WITH PAINT DAMAGED AT L/E.(<P>REPLACED DME #1 SYS ANTENNA &AMP; OPS CHECK DME SYS OK PER AMM 34-55-02.</P>)

ATA 5100

L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 OUT OF SERVICE DATE(<P>REMOVED&NBSP; AND REPLACED&NBSP; L-1 AFT FA SEAT OXYGEN GENERATOR S/N 69366 AS REQUIRED IAW B767 AMM 35-21-04.</P>)

ATA 5100

PASSENGER CABIN NUMEROUS BIO-HAZARD KITS OUT OF SERVICE DATE P/N 500094 .(<P>REMOVED &AMP; REPLACED NUMEROUS BIO HAZARD KITS AS REQUIRED IN PAX CABIN PER 767 AMM 25-64-00. OPS CHECK OK.</P>)

ATA 5410

ENG #2 NACELLE STRUT EXTERNAL ACCESS DOOR REAR LATCH BROKEN(<P>REMOVED DAMAGED 4EA LATCH LOCATED AND INSTALLED NEW LATCHES AT #2 ENG. NACELLE STRUT AFT ACCESS DOOR PER B767-300 SRM 51-40-02-0G-0.</P>)

ATA 2500

COCKPIT LIFE VEST STORAGE COMPARTMENT ABOVE 2ND OBS SEAT HAS LOOSE VELCRO.(<P>REMOVED &AMP; REPLACED DAMAGED VELCRO AT COCKPIT LIFE VEST STORAGE COMPARTMENT ABOVE SECOND OBS SEAT IAW B767 AMM 20-30-01.</P>)

ATA 2565

LEFT OFF WING SLIDE INFLATION BOTTLE, P/N WARNING STREAMER DAMAGED .(<P>REPLACED PIN WITH STREAMER IAW 767 AMM 25-65-00-442-410 STEP 10</P>)

ATA 2612

2 HRS INTO FLIGHT RECEIVED "RT ENG FIRE" EICAS MESSAGE. RAN ALL ASSOCIATED CHECKLISTS AND SHUT RT ENG DOWN. REMOVED AND REPLACED RH ENG ASSY PER AMM 71-00-02 & W/C A-71-989-04. PRE-COOLER REPLACED AS PRECAUTION. RH & LH CORE COWLS & THRUST REVERSERS REPLACED.

ATA 3300

NUMEROUS EMERGENCY LIGHTS INOP.(<P>REMOVED AND REPLACED POSITION M1210 BATTERY PACK PER B767 AMM 33-51-07-422-012. OPS CHECKED GOOD.</P>)

ATA 3300

NUMEROUS EMERGENCY LIGHTS INOP.(<P>REPLACED M736 EMERGENCY POWER SUPPLY PER B767 AMM 33-51-07-002-006. OPS CHECK GOOD.</P>)

ATA 3300

NUMEROUS EMERGENCY LIGHTS INOP.(<P>RE-LAMPED EMERGENCY LIGHTS AT SEAT LOCATION16L, 28L AND 31L PER767 AMM 33-51-05-002-039. OPS CHECKED GOOD.</P>)

ATA 3350

L1 DOOR OVERHEAD LIGHT INOP.(TRANSFERRED TO MDDR 168798 PER MEL 33-21-01-02. LP 1533523: T/S L1 DOOR OVERHEAD LIGHT INOP AND FOUND MISSING PACK AT M735. INSTALLED A NEW BATTERY PACK IAW AMM 33-51-07. OPS CHECK GOOD. DMI 168798 CLOSED.</P>)

ATA 4950

APU SURGE VALVE WITH DUCT DAMAGED(<P>REMOVED AND REPLACED APU SURGE&NBSP; BLEED VALVE&NBSP; DUCT ASSY&NBSP; IAW B767-300 AMM 49-53-01. OPS CHK&NBSP; NORMAL . NO&NBSP; LEAKS FOUND .</P>)

ATA 5280

RIGHT MLG EXTENSION HANDLE ACCESS DOOR # 198BR HAS THE INTERNAL EDGES SEAL COMING APART. REAPPLIED BLACK VINYL TAPE TO RMLG EXT HANDLE ACCESS DOOR #198BR IAW B767-300, AMM&NBSP; 20-30-01

ATA 5200

LEFT MLG EXTENSION HANDLE ACCESS DOOR # 197BL HAS THE AFT HINGE BONDING JUMPER BROKEN. REMOVED & REPLACED BONDING JUMPER&NBSP; AT LEFT EXTENSION HANDLE; ACCESS DOOR; 197BL. AFT; HINGE AND PERFORMED RESISTANCE;CHECK AND FOUND WITHIN ALLOWABLE LIMITS AS PER BOEING SWPM 20-20-00 20-20-10

ATA 3250

N/L/G STEERING CABLES, TURN BUCKELS HAVE SPEED TAPE ON SAFETY CLIPS ( REMOVE SPEED TAPE & REPLACE SAFETY CLIPS IF REQUIRED REMOVED & INSTALLED LOCKING CLIPS ON TURN BUCKRLS FOR NLG STEERING PER AMM 20-10-05.

ATA 2340

R4 CALL LIGHT / SOUND / CHIME REPEATLY GOING OFF-GITOST LIGHT PERFORMED PASSENGER SERVICE SYSTEM OPS CHECK. ALL CALL LIGHTS/ SOUND WORK NORMAL AS PER B767-300 AMM 23-34-00

ATA 2320

RECIEVING A DOUBLE AURAL DING WHEN REQ ACARS DATA ON RECEIVING AN ACARS/ FLIGHT PLAN MESSAGE. SHOULD ONLY BE ONE AURAL NOTIFICATION . NOT TWO. ACARS OPERATIONAL TEST OK PER B767-300 AMM 23-22-00 TLS D633T1C9

ATA 2741

STAB TRIM ADVISORY EICAS MESSAGE UPON LANDING. T/S FIM 27-48- F/T 809 FOUND SYSTEM OK PER AMM 27-41-00/715 E/O 6722A008CS

ATA 3340

L/H OUTBOARD WHITE POSITION INOP. RELAMPED LH WING REAR POSITION LT OPS CHECK OK AMM 33-43-02.</P>)

ATA 4990

DUE TO EXTENDED GROUND TIME-VISUAL INSP.OF APU OIL SERVICE IS REQUIRED. CHECK APU OIL IAW MM 12-13-04-200-801, NO OIL NEEDED

ATA 5410

NACELLE STRUT #2 INBOARD SIDE, THE PROSV ACCESS DOOR IS LIFTED IN CLOSE POSITION. SECURED #2 ENG I/B PROSOV ACCESS DOOR IAW B767-300 SRM 51-40-02</P>)

ATA 3510

E&E COMPARTMENT SERVICE CREW OXYGEN CYLINDER TO FULL. SERVICED CREW OXY CILINDER; AT LOWER; E&E AS PER; B767;AMM 12-15-08-603-001,35-00-00-412-005,35-11-00-206-228; 35-11-00-206-233.;ADVISORY CIRCULAR AC 43.13-1B; PAR 9-46 THRU; 9-51;PGS9-448THRU 9-459

ATA 2821

WHEN FUELING - AT THE REFILL PANEL, THE RESET BUTTON MUST BE HELD. - ITEM SHORT SIGNED BY FLIGHT MX - T/S PER AMM 28-55-00, FOUND ALL INDICATING POINTING TO LEFT TANK AUTO SW ASSY. REMOVED LEFT WING SURGE TANK ACCESS PANEL 542AB; IAW; REF B767 AMM 28-11-03, REMOVED AND REPLACED LT TANK FUEL LEVEL SENSOR UNIT IAW REF B767; AMM 28-21-03; OK TO CLOSE ACCESS PANEL # 542AB CLOSED LT/WING SURGE TANK ACCESS PANEL # 542AB IAW REF B767 AMM 28-11-03 3519177/KR42314M ;5/3/22 ERTS PENDING FOR OPS LEAK CHECK. CHECK LEVEL FUEL SENSOR OK AMM 28-21-04 PERFORMED LEAK CHECK NO LEAKS

ATA 7100

#2 ESN 704757 HAS 1EA HPT VANE AT 5 O'CLOCK POSITION WITH CONVEX SIDE MISSING AND LIFTING MATERIAL. CONDITION IS NOT PERMITTED. REPLACED ENGINE. REMOVED #2 ENG PER B767-300 AMM 71-00-02. OK TO INSTALL SERVICIABLE ENG. / INSTALLED NEW&NBSP; SERVICIABLE ENG PER B767-300 AMM 71-00-02. OPS&NBSP; CHECK&NBSP; GOOD&NBSP; &AMP;&NBSP; NO LEAKS&NBSP;</P>)

ATA 3300

LEFT AND RIGHT LANDING GEAR LIGHTS INDICATIONS NOT FLUSH WITH EACH OTHER, RIGHT GEAR DOWN LIGHT HARD TO SEE ILUMINATED FROM CAPT SEAT(<P>REMOVED &AMP; REPLACED L &AMP; R L/G DIODE SUSE CARD SW. LTS &AMP; OPS&NBSP; CHECK OK AMM 33-13-00/902.</P>)

ATA 3451

CAP VOR/DME TUNER CRS KNOB IS SKIPPING NUMBERS ON DISPLAY GOING FROM 120 TO 247 TO 132 AS EXAMPLES. REMOVED & REPLACED CAPT VOR CTL PANEL M91 OPS CHECK OK AMM 34-51-02.

ATA 2340

BOTH CAPT AND FO I/C , INT SWITCH ON YOKES ARE ON A DELAY WHEN COMMUNICATING, PUSH SWITCH TO TALK CANT HEAR OTHER PILOT FOR 3-5 SECOND UNTIL MIC BECOME HOT. REMOVED/REPLACED AUDIO ACCESSORY UNIT M108. TEST OK PER AMM 23-42-01

ATA 4920

ENG. # 2 AFT FIRE SEAL WORN OUT .(<P>REMOVED &AMP; REPLACED FIRE SEAL AT ENG. # 2 AT AFT AREANBSP; AS PER&NBSP; 767-300 SRM 51-40-02-0G-0.</P>)

ATA 4920

ENG. # 2 AFT NOZZLE FOUND SEVERAL FINGER SEAL BROKEN .(<P><SPAN>REMOVED &AMP; REPLACED&NBSP; BROKEN FINGER SEAL&NBSP; AT ENG. # 2&NBSP; AFT NOZZLE AS PER 767-300 SRM 51-40-02-0G-0.</SPAN></P>)

ATA 3510

E&;E COMPARTMENT CREW OXYGEN CYLINDER IS OUT OF DATE ,P/N 801307-00 S/N ST352350 MFG DATE 30 APR 97(REMOVED & REPLACED CREW OXYGEN BOTTLE AS PER B767-300 AMM 12-15-08. LEAK CHK GOOD AS PER&NBSP; B767-30 AMM 35-11-00-206-228..</P> / <P>&NBSP;</P>)

ATA 4920

ENGINE #1, DURING PNEUMATIC LEAK CHECK, FOUND POINT L WITH LEAK REMOVED AND REPLACED PACKING &INBSP; ON LOCATION "K"&NBSP; IAW&NBSP; B767&NBSP; &NBSP;AMM&NBSP; &NBSP;20-11-00.&NBSP; &NBSP; &NBSP;NO LEAKS NOTED</SPAN></P>)

ATA 4920

ENGINE #1, DURING PNEUMATIC LEAK CHECK FOUND POINT E WITH LEAK(<P>REMOVED AND REPLACED PACKING AT LOCATION&NBSP; "E"&NBSP; IAW B767 AMM&NBSP; 20-11-00. NO LEAKS NOTED.</P>)

ATA 3350

EXTERIOR EMERGENCY LIGHT BY STATION 1600 L/H RELAMPED OVERWING ESCAPE LT. L645&NBSP; REPLACED COVER LENS, ENG&NBSP; LT. OPS CHECK OK PER&NBSP;</P> / <P>AMM 33-51-06</P>)

ATA 3510

2ND OBSERVER O2 MASK TEST LEVER DOES NOT RETURN TO RESET PROPERLY.(<P>REMOVED AND REPLACED 2ND OBSERVERS O2 MASK STOWAGE BOX IAW 767 AMM 35-11-51, LEAK CHECK GOOD.</P>)

ATA 3300

FUSELAGE LEFT AFT OF WINDOW 3E EMERGENCY EXTERIOR LIGHT OUT(<P>REMOVED AND REPLACED BATTERY PACK ASSY AT M738. OPS CKS GOOD IAW AMM 33-51-07.</P>)

ATA 2561

L1 DOOR SLIDE UNSECURE (DOOR SLIDE REMOVED LEFT IN BIF(<P>TRANSFERRED TO MDD 159678 IAW MEL CAT C, DUE DATE 20JAN22</P> / <P>12JAN22 - LP 1420099 - ITEM #19 - BWI - INSTALLED L1 DOOR LIFE RAFE ASSY PER AMM 25-66-01. OPS CHECK GOOD. THIS CLEAR DMI.</P>)

ATA 3250

LEAK EVIDENCE OF VALVE MODULE - NLG STEERING P/N 3790037-108(<P>VALVE WAS REPLACED IN ACCORDANCE WITH AMM 32-51-04-401-013</P>)

ATA 2800

FUEL LEAK EVIDENCE ON CENTER WING AT RBL 97.42 AND STRINGER L-6(<P>FUEL LEAK WAS REPAIRED PER AMM</P>)

ATA 5200

IT WAS FOUND BROKEN THE SUPPORT ASSY - CARRIER P/N 141T6591-10 FROM FWD SERVICE DOOR AT CABIN PAX(<P>BROKEN PART WAS REPLACED AND TORQUE APPLIED IN ACCORDANCE WITH B767 AMM 20-11-00-910-802</P>)

ATA 5300

DENT PLUS REWORK ON FUSELAGE SKIN BETWEEN STA 1540 / STA 1562 AND STGR 17 / 19LH(<P>EVALUATED AREA PER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL II AND III, HOWEVER IT WAS FOUND OUT</P> / <P>OF LIMITS AND FOR SUCH REASON MXA CONTACTED TO BOEING PER SR# 3-5175816448 (LEAVE IN "AS IS"</P> / <P>CONDITION EACH AFFECTED AREA AND RESTORE THE SURFACE FINISH)</P>)

ATA 5310

DENT PLUS REWORK ON FUSELAGE SKIN BETWEEN STA 282 AND STGR 19 / 20LH(<P>EVALUATED AREA PER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL III, HOWEVER IT WAS FOUND OUT OF LIMITS AND FOR SUCH REASON MXA CONTACTED TO BOEING PER SR# 3-5178994812 (LEAVE IN "AS IS" CONDITION EACH AFFECTED AREA AND RESTORE THE SURFACE FINISH)</P>)

ATA 5700

CORROSION ON THE RH WING TRAILING EDGE FLAP, WEDGE SKIN, AND WEDGE SPAR AT OTEF STA 105.7548(<P>REPAIRED AREA IN ACCORDANCE WITH BOEING SR#3-5164623900</P> / <P>RH WING OUTBD FLAP P/N 113T3100-78 AND S/N 000889</P>)

ATA 5300

CORROSION ON STRINGER S-38LH BETWEEN STA 1562 TO STA 1582 IN BULK CARGO / AREA.(<P>IT WAS REPAIRED PER B767 SRM 53-00-03-2R-2 REPAIR 2 (FUSELAGE STRINGER REPAIR)</P>)

ATA 5315

CORROSION ON PASSENGER CABIN CROSS FLOOR BEAM UPPER CHORD AT STA 287 BETWEEN RBL 20.0 / RBL 54.0(<P>IT WAS REPAIRED PER B767 SRM 53-00-51-2R-1 REPAIR 1 (FLOOR BEAM REPAIR)</P>)

ATA 5300

CORROSION ON PASSENGER CABIN CROSS FLOOR BEAM UPPER CHORD AT STA 347 AND BETWEEN RBL 20.0 TO RBL 48.0(<P>IT WAS REPAIRED PER B767 SRM 53-00-51-2R-1 REPAIR 1 (FLOOR BEAM REPAIR)</P>)

ATA 5300

CORROSION ON STRINGER S-38RH AND ADJACENT AREA BETWEEN STA 1562 TO STA 1582 IN BULK CARGO AREA.(<P>IT WAS REPAIRED PER B767 SRM 53-00-03-2R-2 FIGURE 201 (FLOOR BEAM REPAIR)</P> / <P>AND IT WAS REPLACED / MANUFACTURED THE END-FITTING P/N 146T0203-1 IAW MXA ENGINEERING TASK CARD NO. M6753287 (SMAL REQUEST)</P>)

ATA 2100

AFTER A " PACK OFF" DEPARTURE: "FWD EQPT OVHT" EICAS. QRH COMPLETED. EQUIP COOLING PLACED IN STBY(<P>MAINTENANCE RETURNED SWITCH TO AUTO, SYSTEM OPERATES NORMAL PER B767 AMM 21-58-00.</P>)

ATA 2822

EICAS MSG "L FWD FUEL PRESS"(<P>PERFORMED OPS CHECK OF L FWD FUEL PUMP PER B767 AMM 28-21-00. SYSTEM GOOD. LIGHT EXTINGUISHED</P>)

ATA 2821

L FWD FUEL PRESS(<P>PERFORMED OPS TEST OF L FWD FUEL PUMP. ALL CHECK OK IAW AMM 28-21-00. OK FOR SERVICE.</P>)

ATA 3000

LEFT ENGINE ANTI-ICE VALVE DISAGREEMENT LIGHT. CYCLE TO CLEAR.(<P>REMOVED &AMP; REPLACED LEFT ENGINE INLET TAI VALVE IAW AMM 30-21-03. OPS CHECKED &AMP; LEAK CHECKED GOOD.</P>)

ATA 2822

LEFT FORWARD FUEL PUMP(<P>LEFT FWD FUEL PUMP OPS CK NORMAL PER AMM 28-42-00. ACFT OK FOR SERVICE.</P>)

ATA 7300

ON INITIAL ROTATION AND CLIMBOUT AND DURING CRUISE CLIMB FL330 TO FL350 WE RECEIVED EICAS MESSAGE R ENG FUEL FILT(<P>REMOVED AND REPLACED RH ENG FUEL FILTER ASSY IAW PER MM 73-11-03. OPS &AMP; LEAK CHK OK.</P>)

ATA 4900

APU FAULT UPON ENGINE SHUTDOWN. RESTART NOT SUCCESSFUL.(<P>PERFORMED BITE ON APU ECU-FAULTED, RESET ECU, APU STARTED NORMALLY PER AMM 49-61-05.</P>)

ATA 2822

"R AFT FUEL PUMP" EICAS MESSAGE IN CRUISE FLIGHT.(<P>R AFT FUEL PUMP C/B RESET IAW AMM 20-60-01. NO FAULS NOTED &AMP; R AFT PUMP OPS CHECK SATISFACTORY IAW AMM 28-22-03.</P>)

ATA 2822

L FWD FUEL PUMP EICAS MSG ON FINAL APPROACH L FWD FUEL PUMP CK NORMAL PER AMM 28-42-00. A/C OK FOR SERVICE.

ATA 4940

APU FAULT, 3 ATTEMPTS TO START UNSUCCESSFUL APU ECU INTERROGATED AND NO FAULTS. APU SUCCESSFULLY STARTED IAW AMM 49-11-00. OK FOR SERVICE.

ATA 2500

FIXED ELT FAILS GPS TEST. TRANSFERRED TO MDDR 154060, DDG 25-23-10-02C, CAT D. MAINT ACTIONS COMPLETED. DUE 22 JAN 22 PLACARD INSTALLED.&NBSP; 30SEP21 - LP 1314601 - ITEM 8 -&NBSP; IAH - REMOVED AND REPLACED FIX ELT. IAW AMM 25-63-03. OPS CHECK NORMAL. THIS CLEARS MDDR #154060. PLACARD REMOVED. LC@0050Z

ATA 2842

LEFT FWD FUEL PUMP EICAS.(<P>PERFORMED OPS CK OF LT FWD FUEL PUMP ALL CHECKS OK NO MSG OR FAULTS PER AMM 28-42-01</P>)

ATA 2150

STATUS MSG AFT EQ EXH FAN 1(<P>CLEARED MSG PER AMM 21-58-00.</P>)

ATA 4940

APU FAULT, 3 ATTEMPTS ON GROUND.(<P>STARTED APU ON FIRST TRY - OIL QTY READING 0.50 - APU OPS CKS OK PER AMM 49-41-00</P>)

ATA 3442

RADAR RETURNS VERY WEAK. NEED MAX GAIN TO SEE WX RETURNS.(<P>PERFORMED FIM TASK 34-43 FAULT TREE 805 AND WEATHER RADAR OPS CHECK IAW AMM 34-43-00. OPERATIONAL CHECK OK AT THIS TIME.</P>)

ATA 4990

APU LEAKING OIL FROM THE MAGNETIC CHIP DETECTOR FOR THE GEAR BOX. REMOVED AND REPLACED DRAIN PLUG MAGNETIC DRAIN PLUG,TORQUED TO SPECS AS PER AMM 20-11-00 & LEAK CHECKED GOOD.

ATA 1100

COCKPIT L/H AND R/H WINDOW PLACARD " WINDOW NOT CLOSED " DAMAGED. REMOVED AND REPLACED THE DAMAGED PLACARD IAW AMM 20-10-12-004-001 AND 20-10-12-404-004.

ATA 2560

COCKPIT CAPTAIN SMOKE GOOGLES LENS DAMAGED P/N MXP210-00. REMOVED & REPLACED THE CAPT. SMOKE GOOGLES IAW LOPA AND AMM 25-64-00.

ATA 2700

INSTR SOURCE SELECTOR FLT DIR CAPT "C" FD "C" FOR BOTH FLT DIR PITCH UP. PERFORMED OPERATIONAL TEST OK PER AMM 22-10-00/715 REV 101/133. PERFORMED MCDP GND TEST L/O AUTO LAND OK PER AMM 72-03 F/T 820.

ATA 3150

APU FAULT 3 FAILED ATTEMPTS(<P>PERFORMED OPERATIONAL CHECK OF APU ALL CHECKS OK. NO FAULT NOTED B767 AMM 49-11-00.</P>)

ATA 3150

STATUS MSG R ENG ANALOG N2(<P>PERFORMED FIM 73-21 FAULT TREE 901. NO DEFECTS FOUND.</P>)

ATA 4990

UNABLE TO START APU, "APU FAULT". SERVICED APU TO CORRECT LIMITS IAW AMM 12-13-04 AND OPS CK OF APU GOOD AT THIS TIME IAW AMM 49-11-00.

ATA 7714

STATUS MSG R ENG ANALOG N2(<P>T/S PER FIM 77-12 TREE 809, MSG CLEARS. NO FAULTS NOTED. SYS OK FOR SVC.</P>)

ATA 4920

APU FAULT - 3 ATTEMPTS(<P>APU STARTS NORMAL AFTER 30 MIN ON AND PER MM 49-11-01</P>)

ATA 4900

AFTER LANDING, APU FAULT EICAS MESSAGE DURING APU START ATTEMPT. ATTEMPTED 3 STARTS; APU ACCELERATED TO 23% AND THEN SHUTDOWN ON EACH ATTEMPT.(<P>PERFORMED BITE ON ECU, NO FAULTS. STARTED APU FIRST TRY PER AMM 49-50-00. APU OK FOR SERVICE.</P>)

ATA 2120

LT BLD DUCT LEAK(ON GND APU PWR &AMP; AIR).(<P>FOUND COUPLING TO ACM LOOSE, ADJUSTED SAME PER AMM 21-51-00, LEAK CKS GOOD.</P> / <P>16JUL21 - 1476169 - ITEM# 3 - BWI - ADJUSTED LOWER REAR COUPLING TO ACM PER 767 AMM 21-51-00. LEAK CHECK GOOD AT THIS TIME. NO MSGS. DUCT PRESSURE RISE IS OK.</P>)

ATA 3450

FWD EQPT OVHT ON T/O. RAN QRH, COOLED DOWN. EICAS CLEARED.(<P>T/S PER FIM 21-58 TREE 909, NO FAULTS NOTED. SYSTEM CHECK OK. AMM 21-58-00.</P>)

ATA 3350

12H OVHD EMERGENCY LIGHT LENS WILL NOT STAY ON.(<P>RESCURED 12H OVHD EMERGENCY LIGHT LENS IAW 33-51-00. OPS CKS GOOD.</P>)

ATA 3350

2 BATTERY PACKS &AMP; 2 BATTERY CHARGERS REMOVED FROM LEFT OVERWING TO ACFT 480(<P>FWD TO MDDR 149803 PER MEL 33-51-01C, CAT C, DUE 17JUL21, PLACARD INSTALLED.</P> / <P>09JUL21 - LP 1476142 - ITEM 14 - IAH - REMOVED AND REPLACED 1EA BATTERY CHARGER AND BATTERY IAW AMM 33-51-00. BOTH BATTERY AND CHARGER CHANGED ONLY. OPS CHECKS OK. THIS CLOSES MDDR 149803.</P> / <P>LP1484180 ITEM# 9 - REMOVED AND REPLACED 1EA BATTERY CHARGER AND BATTERY IAW AMM 33-51-00. BOTH BATTERY AND CHARGER CHANGED ONLY. OPS CHECKS OK.&NBSP;</P>)

ATA 2150

BURNING SMELL COMING FROM PACKS, INSP RAM AIR INTAKE TO HEAT EXCHANGERS.(<P>INSPECTED LEFT AND RIGHT RAM AIR INTAKE TO HEAT EXCHANGER, NO DEBRIS FOUND. NO BLOCKAGE REF AMM 36-11-00.</P>)

ATA 3150

"R ENG PRV" STATUS MSG(<P>C/W FIM 36-10 TREE 847, INSP OF PRV AND BITE OF AIR SUPPLY MODULE NO FAULTS FOUND, A/C OK FOR SERVICE.</P>)

ATA 4990

LOW APU DUCT PRESSURE DURING START DUE TO HIGH EGT.(<P>APU PNEUM. PLACED ON MEL 49-11-01-01 CAT C DEFRRAL # 149299. RS 1437.</P> / <P>27JUN21 LP 1402166 ITEM 3: REMOVED AND REPLACED APU AIR/OIL COOLER IAW B767 AMM 49-27-00. PERFORMED LEAK AND OPS CHECKS/LEAK CHECK WITH NO DEFECTS NOTED IAW B767 AMM 49-00-00. THIS CLEARS DEFERRAL 149299. MCC NOTIFIED.</P>)

ATA 2150

RT PACK INOP. FWD TO MDDR 148438 PER MEL 21-51-01-01. CAT C, DUE 22JUN21, PLACARD INSTALLED. DISP: RS @ 13:19Z. OPS CHK. REACTIVATED RT PACK FOR MTC CONVENIENCE OF TROUBLEHOOTING PER AMM 21-48-00. THIS CLEARS MDDR 148438. PLACARD REMOVED. DISP: RKB @ 1533Z</P>)

ATA 2120

BURNING SMELL IN CABIN ON DEPARTURE.(<P>ACCOMPLISHED FUMES IN CABIN CONDITIONAL INSPECTION AMM 05-51-56-202-001, NO FAULTS FOUND. OK FOR FURTHER SERVICE.</P>)

ATA 3442

AT FL 410 WEATHER RADAR DID NOT PAINT WEATHER ON L/R(<P>PERFORMED WX RADAR BITE FOR LEFT AND RIGHT SYSTEM PER FIM 34-43 FLT 805, NO FAULTS, TEST GOOD BOTH LT AND RT WX RADAR<BR /></P>)

ATA 4950

APU AIR DROPS TO 5 PSI DURING ENGINE START/ SLOWLY RECOVERS. TESTED NEW ENG VALVE, AMM 49-53-07, NO HELP, REINSTALLED ORIGINAL VALVE ASSY. INSTALLED APU SURGE CONTROLER VALVE HOSE CLAMP IAW AMM 49-53-01. PERFORMED OPS CHECK ON THE APU SURGE VALVE PER AMM 49-11-00. MAX PRESSURE 12 PSI ORIGINAL SURGE VALVE RE-INSTALLED.

ATA 2150

BOTH PACK CONTROLLERS ARE FAULTING THE ALTITUDE SW(<P>REMOVED AND REPLACED PACK CONTROL ALTITUDE SWITCH IAW AMM 21-51-17, PERFORMED BITE TEST ON PACK TEMP CONTROLLER PER TASK 21-51-14-705-035, OPS TEST GGOD. NO OTHER DEFECTS NOTED AT THIS TIME<BR /></P>)

ATA 4950

APU BLEED AIR MAX 12 PSI, TOO LOW FOR ENGINE START(<P>FWD TO MDDR #148250 PER MEL 49-11-01-01, CAT C, DUE 18 JUN 21. PLACARD INSTALLED. REMOVED AND REPLACED ECU, NO HELP. REMOVED AND REPLACED SURGE VLV. NO HELP. INSPECTED SURGE VLV SENSE LINE AND IGV FREE PLAY PER FIM 49-11 TREE 980 IGV CONNECTOR STILL LOOSE. REMOVED AND REPLACED IGV ACTUATOR REF AMM 49-52-02, OPS CK FAIL. REMAINS OPEN FOR FURTHER T/S.</P><P>LP 1484183: INSPECTED AND FOUND INLET CLOGGED WITH CICADAS. CLEANED CICADAS AND OPS CK APU. APU AND ALL INDICATIONS GOOD AT THIS TIME IAW AMM 49-11-00. THIS CLEARS DMI 148250. PLAC REMOVED.</P>)

ATA 7200

L ENG SPAR VALVE CHECK FAILED ON START(<P>NOTED BY MAINTENANCE. ENGINE SHUTDOWN AFTER COOL DOWN, L ENG RESTARTED IAW AMM 71-00-00. ALL IND NORMAL, OK FOR SERVICE.

ATA 8012

R/H START VALVE TRANSIT LIGHT DOES NOT EXTINGUISH IN OPEN POSITION.(<P>REMOVED AND REPLACED&NBSP;#2 ENGINE VALVE ENGINE STARTER IAW 767 AMM 80-11-02-404-017-H00. REQUIRES OPS CHECK ON ITEM 13. LP 1476181.</P><P>LP 1476181, ITEM M13: C/W ENG STARTER OPS CK. OK PER AMM 80-11-02</P>)

ATA 2822

L FWD FUEL PUMP EICAS MESSAGE ON TAXI.(<P>MSG SELF CLEARED AFTER PARKING AT THE GATE. SYSTEM CK GOOD. ACFT OK FOR SVC PER AMM 28-42-01</P>)

ATA 2913

ITEM#1 - L HYD QTY EICAS MSG IN FLIGHT. ITEM# 2 - L HYD PRIME PUMP EICAS MSG IN FLIGHT. TURNED PUMP OFF PER QRH. ITEM# 3 - L HYD SYS PRESSURE EICAS/ ALL LEFT HYD PUMPS OFF.(<P>ITEM #1 &AMP; #3 CORRECTIVE ACTION - LOG# 1092013 - ITEM# 6 - SOF - 31MAY21 - POPPET INDICATOR REMOVED, INSPECTED AND RESEATED IAW AMM 29-11-15. LEAK CHK CARRIED OUT. NO LEAKS EVIDENT.</P><P>ITEM# 2 CORRECTIVE ACTION - LOG# 1092013 - ITEM# 2 - SOF - 31MAY21 - AFTER ENGINE RUN LEAK CHECK, FOUND HYD LEAK AT L/H ENG EDP. REMOVED &AMP; REPLACED EDP IAW AMM 29-11-05 OPN CHK SATIS. NO FURTHER LEAKS EVIDENT.</P>)

ATA 7830

LEFT ENG. LH REV. MESH 9-11 O' CLOCK MISSING IAW EO6778A019 PART 1 C/W PART 2 DUE NEXT A CHECK .(<P>REMOVED #1 ENG OUTBD TRANSLATING COWL TO ACCESS AND RETAIN&NBSP; IAW&NBSP; AMM&NBSP; 78-31-10-004-001-H00</P><P>REV 101.</P><P>ACCOMPLISHED PERMANENT REPAIR&NBSP; AT&NBSP; L/H ENG I/B&NBSP; T/R&NBSP; PER&NBSP; ATLAS&NBSP; AIR&NBSP; &NBSP;EO&NBSP; 6778A019&NBSP; REV 4&NBSP;</P><P>REPAIR&NBSP; ACCOMPLISHED PER AVENIR AVIATION&NBSP; &NBSP;FAA&NBSP; # 8AVR479B&NBSP; &NBSP; R.O 5002563&NBSP; &NBSP;AND&NBSP; WO&NBSP; W15623</P><P>CMM&NBSP; 78-32-02&NBSP; REV 61&NBSP; &NBSP;8130&NBSP; ATTACHED FOR TRANSLATING&NBSP; COWL&NBSP; INSTALLATION&NBSP; SEE&NBSP;&NBSP;</P><P>NON ROUTINE #49</P>)

ATA 5340

MAIN CABIN AFT R/H PBE SUPPORT BRACKET DAMAGED. P/N AC4036-1(<P>REMOVED AND REPLACED DAMAGED BRACKET AT MAIN CABIN AFT R/H&NBSP; PBE PER&NBSP; &NBSP;B767-300</P><P>AMM&NBSP; &NBSP;20-11-00-910-802 .</P>)

ATA 7330

#2 ENG FUEL TRANSMITTER LEAKING DURING WET MOTORING(<P>REMOVED AND REPLACED ENGINE FUEL PUMP INTERSTAGE&NBSP; PRESSURE TRANSMITTER IN ACCORDANCE&NBSP; WITH&NBSP;B767&NBSP; AMM&NBSP; REMOVAL-&NBSP; &NBSP;73-33-01-002-001-H00 INSTALLATION- 73-33-01-402-007-H00.</P><P>REQUIRES LEAK&NBSP; AND OPS CHECK ACCOMPLISHED&NBSP; P.P&NBSP; TEST&NBSP; #2&NBSP; ( DRY MOTOR) REF MM&NBSP;&NBSP;</P><P>71-00-00-712-168-H05&NBSP; NO LEAKS&NBSP; NOTED</P>)

ATA 7314

#2 ENG. FUEL PUMP LEAKING DURING WET MOTORING. REMOVED & REPLACED #2 ENG FUEL PUMP GASKET IAW AMM 79-21-01 REV&NBSP; 132&NBSP; PENDING FOR LEAK CHECK. LEAK CHECK ACCOMPLISHED PER 71-00-00-712-168-M03-N0, NO LEAKS NOTED.

ATA 2560

FWD OVHD BIN AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN . P/N AS-002-1(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AT&NBSP; FWD&NBSP; OVHD BIN&NBSP; AS PER&NBSP; B767-300</P><P>AMM&NBSP; &NBSP;25-60-00</P>)

ATA 2560

AFT R/H OVHD BIN AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN P/N AS-002-1.(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AFT R/H BIN AS PER&NBSP; B767-300&NBSP; AMM 25-60-00<BR /></P>)

ATA 5410

# 1 ENGINE O/B CORE COWL OPEN HOLD ROD IS DAMAGED .(<P>REMOVED &AMP; REPLACED #1 ENG O/B CORE COWL HOLD OPEN ROD PER AMM 70-50-00.</P><P>OPS CHECK GOOD</P>)

ATA 5410

# 1 ENGINE STRUT DOOR PANELS LATCHES FOUND LOOSE(<P>REMOVED AND REPLACED&NBSP; DAMAGED LATCHES AT # 1 ENG STRUT DOOR PANELS I/B&NBSP; AND O/B&NBSP; PER&NBSP; B767-300</P><P>AMM&NBSP; &NBSP;20-11-00-910-802</P>)

ATA 5410

# 2 ENG. CORE COWL RUB STRIP 9 O' CLOCK POSITION 1EA RIVET MISSING IAW 78-11-00.(<P>REMOVED AND REPLACED WORN RUB STRIP AND DAMAGED SCREW AT #2 ENG CORE COWL BY 9 O'CLOCK POSITION PER AMM 20-11-00-910-802.

ATA 3150

FWD EQPT OVHT EICAS MESSAGE ON INITIAL CLIMB OUT FOLLOWED QRH, CONTINUED FLIGHT WITH EICAS MESSAGE EXTINGUISHED AFTER HAVING TO GO BACK TO AUTO AFTER 30 MIN(<P>OPS TEST OF EQUIPMENT COOLING SYSTEM CARRIED OUT IAW AMM 21-58-00. ALL TEST PASS, OK FOR SERVICE</P>)

ATA 3150

L FWD FUEL PUMP EICAS MESSAGE ON DESCENT FOLLOW QRH, CONTINUED FLIGHT(<P>L FWD FUEL PUMP MSGS ERASED AFTER PARKING AT GATE. ALL INDICATION NORMAL OK FOR SERVICE, AMM 28-42-01</P>)

ATA 2822

"L FWR FUEL PUMP" EICAS ADVISORY. REPEAT WRITE UP.(<P>REMOVED AND REPLACED&NBSP;LT FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01, OPS CHECK AND LEAK TEST GOOD.</P>)

ATA 2822

L FWD FUEL INOP EICAS ADVISORY.(<P>L FWD FUEL PUMP OPS CHECK GOOD PER M/M 28-22-00, SYSTEM CHECK OK FOR CONTINUED SERVICE.</P>)

ATA 2822

LEFT FWD FUEL PUMP EICAS MSG ON DESCENT W ASSOCIATED PRESS LIGHT(<P>LEFT FWD FUEL PUMP - OPS CK OK PER AMM 28-22-00 SYS OK FOR SERVICE.</P>)

ATA 2421

L IDG VALVE STATUS MSG. T/S PER FIM 24-20 FT 802 - FOUND L IDG VALVE FAILURE RELAY 9K468 BAD, REMOVED AND REPLACED PER WDM 24-11-11. OPS TEST GOOD IAW AMM 24-11-00</P>)

ATA 3150

STATUS MESSAGE " L IDG VALVE" DISPLAYED. PERFORMED BITE TEST OF THE BPCU IAW FIM 24-20FT807 NO FAULTS REMAIN AT THIS TIME.

ATA 3150

L IDG VALVE MESSAGE. PERFORM BITE TEST OF THE BPCU AND NO FAULT AT THIS TIME, FAULT MSG CLEARED.

ATA 2822

L FWD FUEL PUMP CAUTION ILLUMINATED AFTER LANDING(<P>R&AMP;R L FWD FUEL BOOST PUMP IAW AMM 28-22-03, OPS TEST GOOD<BR /></P>)

ATA 2822

RIGHT AFT FUEL PUMP EICAS ADVISORY MSG(<P>OPS CHECK OF RIGHT AFT FUEL PUMP CARRIED OUT IAW AMM 28-22-01. OPS CHECK SATIS. OK FOR SERVICE<BR /></P>)

ATA 2150

FWD EQUIP VAL EICAS ADVISORY REPEAT WRITE UP.(<P>TRANSFERRED TO DMI 145549 IAW DDG 21-58-07-02-01 PROCEDURE 2 CARRIED OUT, CAT C, STR 0346Z</P><P>BWI MX, LP 1335298, ITEM M3: REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05, OPS TEST GOOD. DMI CLEARED. PLACARDS REMOVED. DISP TJ @ 1028Z</P>)

ATA 3150

FWD EQUIP EICAS ADVISORY(<P>FIM 21-58 TASK 805 CARRIED OUT. MSG ERASED. OK FOR SERVICE.</P>)

ATA 2822

LEFT FWD FUEL PUMP EICAS MSG ON FINAL(<P>TRANSFERRED TO MDDR 145506 IAW MEL 28-22-01, CAT C.</P><P>REMOVED AND REPLACED FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS AND LEAK CHECKS GOOD. THIS CLEARS MDDR 145506. MCC NOTIFIED. PLACARDS REMOVED. CW 23:54Z</P>)

ATA 2822

EICAS MSG L FWD FUEL PUMP.(<P>CONTROL ALL BREAKERS ARE CLOSED AND NO CURRENT EICAS MSG. NO DEFECTS NOTED AT THIS TIME IAW AMM 28-22-00.<BR /></P>)

ATA 2421

L GEN OFF EICAS MESSAGE AFTER START.(<P>TRANSFERRED TO MDDR 145429, CAT B, DUE DATE 19APR21. MEL 24-00-01-01.</P><P>19APR21 - LP 1335294 - ITEM# M8 - BWI - REPLACED L/H GEN IAW AMM 24-11-01. OPS CHECK AND LEAK CHECK GOOD. THIS CLEARS MDDR # 145429. MCC NOTIFIED. PLACARD REMOVED.</P>)

ATA 2421

STATUS MSG L IDG VALVE(<P>INSPECTED L IDG OIL LEVEL AND DELTA "P" IAW B767AMM 12-13-03. NO DEFECTS NOTED. MESSAGE CLEARED.</P>)

ATA 7510

STATUS MESSAGE: L ENG TAI VALVE(<P>R/R ENG INLET TAI VALVE LH IAW AMM 30-21-03. PERFORMED OPS CHECK, OPS CHECK GOOD.</P>)

ATA 7510

STATUS MESSAGE: L ENG TAI VALVE(<P>R/R ENG INLET TAI VALVE LH IAW AMM 30-21-03. PERFORMED OPS CHECK. OPS CHECKS GOOD</P>)

ATA 2150

NO EICAS MSG WHEN RT PACK SW OFF(<P>REMOVED AND REPLACED RT PACK FLOW CIRCUIT CARD PER AMM 21-51-09 TASK 401. OPS CKS GOOD AND THIS CLEARS MDDR 144783.</P>)

ATA 2822

L FWD FUEL PUMP FAIL AFTER LANDING(<P>L FWD FUEL PUMP OPS CHK SATIS. NO ACTIVE MSGS. OK FOR SERVICE. IAW AMM 28-22-00.</P>)

ATA 5410

LEFT ENGINE HOLD ROD INOP. REMOVED AND REPLACED NR 1 ENG INBD AFT HOLD OPEN FAN COWL ROD IAW B767 AMM 71-11-11. OPS CHECK NORMAL.

ATA 3350

EMERGENCY (AISLE) LIGHTS OUT FROM SEAT # 1AC-10AC DURING TEST. REMOVED AND REPLACED BATTERY POWER SUPPLY M735, OPS CHECKS GOOD IAW AMM 33-51-07.

ATA 3350

AISLE EMERGENCY LIGHT OUT AT SEAT # 25HK - REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP, OPS CHECKS GOOD IAW AMM 33-51-05.

ATA 2822

LEFT FWD FUEL PUMP EICAS. TRANSFER TO DDG CONTROL MEL 28-22-01, MDDR 142605, CAT "C", DUE 28FEB21 20FEB21 - LP 1273119 - ITEM NR 3 - BWI. REMOVED AND REPLACED K10703 IAW AMM 28-22-18. THIS CLEARS MDDR 142605. 1955 JT

ATA 2510

EVAS GLARESHIELD VELCRO UNSERVICEABLE (LEFT) CAPT. SIDE(<P>TRANSFERRED TO MDDR #142055 PER MEL 25-63-06, CAT D, DUE 06 JUN 21.</P><P>LP&NBSP;1273095: INSTALLED CAPTAIN'S CSVS VELCRO IAW SMM 25-60-99. THIS CLEARS MDDR 142055.</P>)

ATA 4940

APU FAILED TO START UPON ARRIVAL, 3 ATTEMPTS. DOOR ACTUATOR CB FOUND POPPED, CB RESET IAW AMM 20-60-01. OPS CHK SATISFACTORY. APU START FIRST ATTEMPT.

ATA 4990

STATUS MESSAGE APU OIL QTY, VISUALLY VERIFIED APU OIL QT. SERVICED WITH 1/4 OF A QUART. APU OIL LVL OK PER AMM 12-13-04.

ATA 2160

FORWARD ZONE CABIN TEMP TRIM AIR VALVE INOPERATIVE. FWD CABIN AIR CONDITIONING ZONE INOP LIGHT. TRANSFERRED TO DMI 141569, IAW MEL 21-61-04-01B CAT C DUE 07FEB21. MCC NOTIFIED, PLACARDS INSTALLED. LOG PAGE 1273154: REPLACED TRIM VALVE MODULATING IAW AMM 21-61-07. OPS AND LEAK CHECK GOOD. THIS CLEARS DMI 141569. MCC NOTIFIED.

ATA 4950

APU BLEED AIR S/O VALVE OPERATIONS INTERMITTENTLY. REMOVED AND REPLACED APU BLEED AIR S/O VALVE, IAW AMM 36-11-10, OPERATIONS CHECK OK.

ATA 2565

LEFT OFF WING ESCPAE INFLATION CYLINDER WHITE INDICATOR NOT VISIBLE AND INFLATION TRIGGER CABLE NOT INSTALLED CORRECTLY. REMOVED AND REPLACED LEFT OFF WING ESCAPE INFLATION CYLINDER, AS PER B767 AMM 25-65-02.

ATA 7510

RT ENGINE A/I VALVE INTERMITTENTLY STICKS WHEN OPERATING. REMOVED AND REPLACED RT ENGINE COWL ANTI ICE VALVE, IAW AMM 30-21-03. PERFORMED OPERATIONS TEST AND LEAK CHECK, FOUND GOOD.

ATA 3350

SEAT NR 8HC AISLE EMERGENCY LIGHT LENS MISSING. INSTALLED AISLE EMERGENCY LIGHT LENS, IAW AMM 33-51-05.

ATA 2160

FWD CABIN TEMP CONTROLLER INOPERABLE. CABIN COMPARTMENT TEMP CONTROL SYSTEMS, PASSENGERS, -200/300/-400. PERFORMED BITE CHECK ON CABIN TEMP CONTROLLER, RESET CB INOPERABLE, CLEARED. OPERATIONS CHECK GOOD, PER 767 FIM 31-61-FT 803.

ATA 4990

APU OIL QTY IND. INTERMITTENT/ERRATIC. REMOVED AND REPLACED APU OIL TRANSMITTER, PER AMM 49-94-04. OPERATIONS CHECK OK.

ATA 2822

LT FWD FUEL PRESSURE LIGHT. REMOVED AND REPLACED LEFT FWD BOOST PUMP 28-22-03. OPERATIONS AND LEAK CHECK NORMAL.

ATA 2822

LEFT FWD BOOST PUMP HAS INTERMITTENT PRESSURE LIGHT WHEN OPERATING. REMOVED AND REPLACED LEFT FWD BOOST PUMP PRESSURE SWITCH, IAW AMM 28-42-01. OPERATIONS AND LEAK CHECKS OK.

ATA 7510

RIGHT ENGINE ANTI-ICE VALVE LIGHT ILLUMINATED. OPERATIONS CHECK, IAW 30-21-03, NO DEFECTS NOTED AT THIS TIME.

ATA 2560

AFT GALLEY EMERGENCY FLASHLIGHT ASSEMBLY RED LIGHT NOT FLASHING. REMOVED AND REPLACED AFT GALLLEY EMERGENCY FLASHLIGHT, IAW AMM 25-60-00.

ATA 2160

FWD CABIN TEMP EICAS MESSAGE ILLUMINATED PRIOR TO BLOCKOUT(<P>TRANSFERRED TO MDDR #137963 IAW DDG MEL# 21-61-01-01, CAT C, DUE ON 27NOV20. DISPATCH: C.W. @ 0050Z.<BR /></P><P>22NOV20, LP 1272907 M4 - BWI - REMOVED AND REPLACED FWD ZONE TRIM AIR MODULATING VALVE. IAW AMM 21-61-07. OPS CHECK GOOD. THIS CLEARS MDDR #137963. MCC NOTIFIED. PLACARD REMOVED.</P>)

ATA 2822

LEFT FWD FUEL PUMP INOPERABLE. TRANSFERRED TO MDDR 137978, IAW MEL 28-42-01-01 CAT "C" DUE 27NOV20. VERIFIED OPERATION OF FUEL SYSTEM, PER DDG 28-42-01-01. OPERATIONS CHECK GOOD AT THIS TIME, NEXT INSPECTION DUE EVERY FLIGHT DAY. 18NOV20/1272892/ITEM-M2/RMS. REMOVED AND REINSTALLED AFTER CLEANING PRESS SWITCH, IAW B767 28-42-01, THIS CLEARS MDDR 137978.

ATA 3150

LT ENGINE TAI STATUS MESSAGE. T/S IAW B767 FIM 30-21 FAULT TREE 805. NO FAULTS FOUND AT THIS TIME. STATUS MESSAGE CLEARED. MCC NOTIFIED.

ATA 2822

LEFT FWD FUEL PUMP EICAS ON SHORT FINAL. CHECKED PRESSURE SWITCH AND CONNECTOR. OPERATIONS AND INDICATION OF FWD FUEL PUMP OK, PER MM 28-42-01 AND FIM 28-22 FAULT TREE 827.

ATA 3610

AFTER LEVEL OFF LT ENGINE HPSOV EICAS STATUS. COMPLETED CHECK LIST. RAN BITE CHECK ON AIR SUPPLY MODULE, PER AMM 36-23-00, NO FAULTS NOTED. RAN ENGINE, PER AMM 71-00-00. HPSOV OPERATIONS CHECK OK.

ATA 2160

FWD CAB TEMP EICAS MESSAGE, COMPT TEMP INOPERABLE LIGHTS, PASSENGER, -200/-300, TRIM AIR MODULATING VALVE CLOSED. TRANSFERRED TO MDDR 136025, IAW MEL 21-61-06-01-01A, CAT C. REMOVED AND REPLACED FWD CABIN TRIM AIR VALVE ASSEMBLY, PER AMM 21-67-07. OPERATIONS CHECKS GOOD. THIS CLEARS MDDR 136025. DISP SP AT 2017.

ATA 2822

CENTER LT FUEL PUMP EICAS MESSAGE ON TAXI OUT. FWD TO MDDR 135952, PER MEL 28-22-02A, CAT C, DUE 22OCT20. PLACARD INSTALLED. PERFORMED OPERATIONS CHECK OF LT CENTER BOOST PUMP, PER AMM 28-22-03. OPERATIONS CHECKS OK. THIS CLEARS MDDR 135952, PLACARD REMOVED. DISP LUC @ 01:44Z.

ATA 2160

FWD CABIN TRIM LIGHT INOPERABLE IS ON. TRANSFERRED TO MDDR 135921, PER MEL 21-61-06-01-01A, CAT C. DUE 22 OCT 2020. 3 SUCESSFUL LEGS WHEN TEMP CONTROL. OPERATIONS OK, NO FAULTS NOTED. PERFORMED SYSTEM OPERATIONS CHECK, PER AMM 21-61-05. THIS CLEARS MDDR 135921. PLACARD REMOVED. DISP CD AT 2303.

ATA 7510

RT ENGINE ANTI ICE. OPERATIONS TEST OF RT ENGINE TAI CARRIED OUT, IAW AMM 30-21-03. ALL INDICATIONS NORMAL. OK FOR SERVICE.

ATA 3610

AFTER T/O AT APPROX 9000' EICAS MSG "LT ENGINE PRV" DISPLAYED AND WENT AWAY TWICE. NOW "LT ENGINE PRV" STATUS MESSAGE DISPLAYED. REMOVED AND REPLACED LT ENGINE PRV CONTROLLER, IAW AMM REF 36-11-19. OPERATIONS CHECK OK, LEAK CHECK OK. MESSAGE CLEARED. S/N OFF: MTH00887, P/N OFF: 792755-15. REMOVED AND REPLACED AIR SUPPLY BITE MODULE, IAW AMM REF 36-23-01, BITE TEST OK.

ATA 3610

LT ENG HPSOV STATUS MSG. LT ENG HPSOV BITE TEST CARRIED OUT, IAW AMM 36-23-00. NO ACTIVE MSG, SELF ERASED.

ATA 4950

APU NO PNEUMATIC OUTPUT. APU RESTARTED, ALL PNEU DUCT PRESSURE NORMAL, IAW AMM 49-11-00. OK FOR SERVICE.

ATA 3097

RIGHT ENGINE ANTI ICE VALVE LIGHT INOP. TRANSFERRED TO MDDR 134644, IAW MEL 30-21-02-01A, CAT C. FOUND AND SECURED LOOSE PIN WIRE AT SWITCH, PER AMM 33-13-00. OPS CHECKED NORMAL. THIS CLEARS MDDR 134644. PLACARD REMOVED.

ATA 2170

LEFT PACK WATER EXTRACTOR HAS A CRACK AT THE INBOARD TEMP PROBE. REMOVED AND INSTALLED LEFT WATER EXTRACTOR ASSY AND PERFORMED INSTALLATION AND TEST OK, PER AMM 21-51-04.

ATA 3020

AFTER TURNING OFF RT ENGINE ANTI ICE DURING DESCENT VALVE LIGHT INTERMITTENT BETWEEN OFF/ON. FOUND KORRY SWITCH FAULTY PER FIM 30-21-803. SWITCH ON ORDER, REQUIRES RELAY REPLACEMENT. REPLACED K2 RELAY, IAW WD 30-21-11, SYS OPS OK.

ATA 3150

LT ENG PRV MESSAGE, CLEARED MESSAGE PER FIM 36-10-00. PERFORMED ENGINE RUN, PER AMM 71-00-00, NO FAULTS NOTED. AIRCRAFT OK FOR SERVICE.

ATA 2822

ON SHORT FINAL, LEFT FWD FUEL PUMP EICAS. FWD FUEL PUMP OPERATIONS CHECK CARRIED OUT IAW AMM 28-22-03. ALL SATISFACTORY AND INDICATE NORMAL.

ATA 3610

LT ENG PRV STATUS MESSAGE ON TAXI IN. ENG NR 1 RAN; OPERATIONS CHECK SATISFACTORY IAW AMM 71-00-00. ALL IND NORMAL NO ACTIVE MESSAGES.

ATA 2150

R PACK TEMP EICAS MSG (PACK TEMPERATURE CONTROL SYSTEMS (-200/-300), AUTO MODE) TRANSFERRED ITEM TO MDDR 133072 PER MEL 21-03-01, CAT C, DUE 28 AUG 20 MCC ALEY DISP SP 2222Z. REMOVED AND REPLACED RH PACK TEMP CONTROLLER BOX REF AMM 21-51-14. OPS CHECKS OK. THIS CLEARS MDDR 133072. NOTIFIED MCC.

ATA 2150

LEFT PACK OVER HEAT ILLUMINATED HISTORY REMOVED, INSPECTED, AND REINSTALLED THE LH PACK OVERHEAT SWITCH REF B767 AMM 21-51-18. NO DEFECTS NOTED AT THIS TIME.

ATA 2822

FWD BOOST PUMP EICAS MSG ON RECENT HISTORY REMOVED AND REPLACED ;L FWD FUEL PUMP PRESS SWITCH IAW B767 FIM 28-25-00T815. OPS CKS GOOD.

ATA 2150

RIGHT PACK TEMP EICAS DURING CRUISE AT FL 340 1716Z(<P>ACCOMPLISHED FIM 21-51-00-810-877-001. RESET R PACK TEMP CONTROLLER AND OPS CHECKS GOOD PER MM 22-51-00. NO FAULTS.<BR /></P>)

ATA 2822

"L FWD FUEL PUMP" EICAS MSG DISPLAYED. COMPLETED QRH.(<P>ACCOMPLISHED F.M 28-22 TREE 819 AND L FWD BOOST PUMP OPERATES NORMAL AS PER AMM 28-42-01. OK FOR SERVICE, NO FAULTS FOUND.</P>)

ATA 2761

C HYD SYS PRESS EICAS AND LOSS C HYD FLUID. NUMBER 8 INBD SPOILER PCA FAILED. REMOVED AND REPLACED NUMBER 8 INBD SPOILER PCA RIGHT WING IAW MM 27-61-02. CHECKS GOOD. C HYD SYSTEM SERVICED PER MM 12-12-01.

ATA 3610

LEFT PRV MESSAGE AFTER TAKE OFF. REMOVED AND REPLACED LEFT ENG PRV IAW AMM 36-11-18. LEAK AND OPS CHECK GOOD. NO MESSAGE DISPLAYED.

ATA 3610

STATUS MSG L ENG PRV PERFORMED BITE OF AIR SUPPLY SYSTEM IAW AMM 36-23-00. FAULTED L ENGINE HPSOV. REMOVED AND REPLACED L ENG HPSOV IAW 36-11-07. OPS CHECKED GOOD.

ATA 2150

DUE TO +38 DEGREES C TEMPS OUTSIDE, LT DUCT LEAK LIGHT ON LEFT PACK. NO LEAKS NOTED IAW AMM 21-48-00. OPENED LEFT PACK DOORS TO FACILITATE COOLING, CLOSED PACK BAY DOORS PER AMM 21-51-00.

ATA 3150

LEFT ENG PRV STATUS MSG ENG RUN C/W ON #1 ENG IAW AMM 71-00-00. ALL INDICATIONS NORMAL. NO ACTIVE MSG. OK FOR SERVICE. OPS CHECK OF PRV IAW AMM 36-11-07. OPS CHECK OK.

ATA 2822

ON APPROACH EICAS MESSAGE FOR LT FWD FUEL PUMP. PERFORMED CIRCUIT BREAKER RESET IAW AMM 28-25-00, TEST OK.

ATA 3610

LEFT ENGINE PRV STATUS MESSAGE. PERFORMED AIR SUPPLY MODULE BITE TEST IAW AMM 36-00-30, NO FAULTS.

ATA 4950

NO APU AIR PRESSURE AFTER ENG SHUTDOWN. SHUTDOWN APU AND RESTARTED IAW AMM 49-11-00. OPS CHECKED GOOD.

ATA 4950

APU AIR RIGHT DUCT PRESSURE INDICATING 0 ON DUCT PRESSURE GAUGE AND ECS. REMOVED AND REPLACED THE RT BLEED PRESSURE TRANSDUCER IAW AMM 36-21-01, OPS CHECK GOOD.

ATA 2421

APU GENERATOR OFF EICAS MESSAGE AFTER APU START ON LANDING. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01. OPS CHECKED GOOD.

ATA 3350

LEFT SIDE, ONE EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-00, OPS CHECKED OK.

ATA 5210

L1 DOOR POPS WHEN OPEN. FOUND L1 DOOR FWD CARTRIDGE LIMITING OVERHEAD DOOR BROKEN. REMOVED AND REPLACED CARTRIDGE. AMM 52-11-21 AND COUNTER BALANCE SYSTEM AMM 52-11-16 OPS TEST AND CHECK OK.

ATA 2562

MAIN DECK LH AFT STORAGE COMPARTMENT ELT DAMAGED. REMOVED AND REPLACED ELT AT AFT STORAGE COMPARTMENT. AMM 25-63-00.

ATA 2562

MAIN DECK FWD CLOSET ELT DAMAGED. REMOVED AND REPLACED ELT AT FWD CLOSET PER AMM 25-63-00.

ATA 2120

LT PACK DUCT P/N 2202317-1 HAS LEAK AT TEMP PROBE. REMOVED &AMP; REPLACED LT PACK DUCT AS PER AMM 20-11-00. LEAK CHECK PERFORMED, NO LEAKS NOTED.

ATA 2150

FWD EQUIPMENT OVERHEAT EICAS MESSGAE ILLUMINATED AFTER DEPARTURE. IAW QRH SELECTED EQUIPMENT COOLING SWITCH TO STANDBY THEN OVRD, CLEARING THE PROBLEM. OAT WAS 117ºF, EXTENDED GROUND TIME, TAXI AND HOLD FOR TAKE OFF. OAT STILL AT 10C AT 30K FT. AFTER REACHING COOL. SPS OPS NORMAL, C/W FIM 21-58 F/T 910. OAT ABOVE 110C WITH NO DEFECTS NOTED. SYSTEM OPS CHECKED AND BITE CHECKED GOOD.

ATA 2130

STATUS MSG CABIN ALT AUTO 2 ILLUMINATED. C/W FIM 21-31 F/T 803. NO FAULTS FOUND. CABIN ALT 2 OPS CKS GOOD AT THIS TIME.

ATA 2820

LT FWD FUEL PUMP EICAS BLED PRESSURE SWITCH SENSE LINE FOR LT BOOST PUMP, RE-SECURED SWITCH AND LINE. LT FWD BOOST PUMP AND PRESS LIGHTS OPS CK NORMAL IAW AMM 28-42-01.

ATA 2150

LEFT PACK TEMP MSG ON ECS PLUS PREVIOUS HISTORY. REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHK GOOD.

ATA 2131

CABIN ALT AUTO 2, REMOVED AND REPLACED NR 2 AUTO PRESSURE CONTROLLER IAW AMM 21-31-02. OPS CHK GOOD.

ATA 7510

LEFT ENG TAI VALVE EICAS MESSAGE. REMOVED AND REPLACED TAI VALVE ON LEFT ENGINE IAW AMM 30-21-03. OPS CHECK NORMAL.

ATA 2130

CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED CABIN PRESSURE CONTROLLER BITE PROCEDURE IAW FIM 21-31-00/101, NO FAULTS NOTED. MESSAGE CLEARED. OPS OK.<BR /></P>)

ATA 2822

L FWD FUEL PUMP EICAS MESSAGE. PERFORMED OPS CHECK PER AMM 28-22-00. OPS NORMAL.

ATA 2150

LEFT A/C PACK TEMP EICAS IN FLIGHT. PERFORMED FIM 21-51 TASK / 877. LEFT PACK CONTROLLER BITES SHOWS TEMP VALVE FAULT. PERFORMED A RESET OF THE LEFT PACK CONTROLLER. NO FAULTS DISPLAYED. OPS TESTED GOOD IAW AMM 21-51-00.

ATA 2131

CAB ALT 2 AUTO EICAS MSG. RESET CABIN PRESSURE / CONTROLLER, IAW AMM 21-31-02. SYS TEST, SAT IS NO FAULTS ACTIVE, DMI 130049 / CLEARED, MCC INFORMED.

ATA 2131

CABIN ALTITUDE 2 STATUS MESSAGE. PERFORMED BITE IAW FIM 21-31-00, FAULTED AC MOTOR, RESET FAULTS. PERFORMED ANOTHER BITE. NO FAULTS NOTED. AC OK FOR SERVICE.

ATA 2130

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. BITE ON CONTROLLER FAULTS A/C MOTOR. REMOVED AND REPLACED THE CABIN ALTITUDE NR 2 AC MOTOR IAW AMM 21-31-05, OPS CHECKED NORMAL.

ATA 2822

LT FWD FUEL PUMP EICAS MESSAGE ON TAXI-IN. LT FWD FUEL PUMP WORKING IAW AMM 28-42-00, ALL SATISFACTORY.

ATA 4950

APU AIR SURGES WHILE TRYING TO OPERATE BOTH PACKS ON THE GROUND. VISUAL INSPECTION CARRIED OUT IN APU COMPARTMENT AREA. HOLE FOUND IN DUCT CONNECTED TO SURGE CONTROL VALVE. OLD BROKEN DUCT REMOVED AND NEW ONE FITTED. OPS CHECK GOOD. REF AMM 49-53-01-004-001.

ATA 2612

L ENG FIRE LOOP 2 MESSAGE WILL NOT RESET. FOUND UPPER AFT AND LOWER AFT LOOPS NR 2 BAD. REMOVED AND REPLACED THE NR 1 ENGINE AFT LOWER FIRE DETECTOR IAW AMM 26-11-02. OPS CHECKED GOOD. FAULTING UPPER AFT DETECTOR. REMOVED AND REPLACED AFT UPPER FIRE LOOP NR 1 IAW AMM: 26-11-02. OPS CHECK PERFORMED, NO FAULTS FOUND.

ATA 2150

RT PACK INOPERATIVE. REMOVED AND REPLACED THE RT FLOW CONTROL VALVE ASSY IAW AMM 21-51-01, OPS CHECK OF RIGHT PACK WAS GOOD.

ATA 4920

APU DRAIN PLUG FOUND DAMAGED. REMOVED DRAIN PLUG FROM APU AND INSTALLED ON NEW APU. OPERATIONAL AND LEAK CHECK OK IAW AMM 49-27-01, MCC NOTIFIED.

ATA 4900

V BAND CLAMP LEAKING ON DUCT ON APU. REMOVED AND REPLACED V BAND CLAMP. OPERATIONAL CHECK NORMAL. LEAK CHECK NORMAL IAW AMM 49-11-00.

ATA 5330

GOUGE ON FUSELAGE SKIN CROWN AREA, BETWEEN STA 236.50 AND STRINGER S-2R. REPAIRED IN ACCORDANCE WITH MRO TRE6753356.

ATA 5330

BULGE DAMAGE ON THE FUSELAGE SKIN BETWEEN STA 1654.50 / STA 1725.50 AND STRINGER S-32L / S-34L. DAMAGE REPAIRED PER SRM 53-00-01-2R-29 REPAIR 29.

ATA 5330

DENT + GOUGE ON FUSELAGE SKIN BETWEEN STA 390 / STA 412 AND STRINGERS S-22L / S-23L. DAMAGES REPAIRED IN ACCORDANCE WITH SRM 53-00-01-2R-1 REPAIR 1.

ATA 4920

APU FAILED TO START SEVERAL TIMES. REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECK GOOD.

ATA 5330

SCRATCH AND GOUGE ON FUSELAGE SKIN BETWEEN STA 764 AND S-1L / S-1R. DAMAGES REPAIRED IN / ACCORDANCE WITH TRE6753353.

ATA 5330

GOUGE DAMAGE ON FUSELAGE SKIN BETWEEN STA 982 AND STRINGER S-3L. REPAIRED IN ACCORDANCE WITH MRO TRE6753355.

ATA 5330

SCRIBE LINE DAMAGES WERE FOUND AROUND ADF ANTENNA NR 1, BETWEEN STA 1109 / STA 1131 AND ADF ANTENNA NR 2, BETWEEN STA 1153 / STA 1175. BOTH OF THEM ON THE CROWN AREA BETWEEN STRINGERS S-1L AND S-1R.DAMAGES WERE REPAIRED IN ACCORDANCE WITH MRO TRE6753358 R1.

ATA 2564

DURING MAINTENANCE VISIT AT MRO, THE CABIN PAX LIFE RAFT WAS FOUND WITH COVER DISJOINTED P/N R0202A211. THE PART WAS REQUESTED FOR / REPLACEMENT, HOWEVER THE LEAD TIME OF THE PART IS OUT OF THE AIRCRAFT RETURN TO / SERVICE DUE DATE AND THE NRC IS DEFERRED IAW MEL;25-62-01, MDDR 128702, CAT 'D'. REMOVED AND REPLACED CABIN PAX LIFE RAFT IAW AMM 25-62-00. THIS CLEARS DMI 128702, MCC NOTIFIED AMM 1600Z.

ATA 3520

FWD CABIN AFT LAVATORY INOP TRANSFERRED TO DMI 128701 IAW MEL 38-30-01B, CAT 'C'. REMOVED AND REPLACED FWD CABIN AFT LAV LT SIDE O2 GENERATOR PER AMM 35-21-13. NO FURTHER DEFECTS NOTED. MMC NOTIFIED. PLACARDS REMOVED. THIS CLEARS DMI 128701.

ATA 4990

APU OIL QUANTITY INOP, FLUCTUATES FROM ADD TO FULL AND ALL POINTS IN BETWEEN. VERIFIED OIL QTY IS FULL BY VISUAL SIGHT GLASS. APU OIL QTY TRANSMITTER WAS REPLACED IAW AMM 49-94-04-404-004.

ATA 4990

APU OIL QUANTITY INDICATOR FLUCTUATES IN FLIGHT.(<P>REMOVED AND REPLACED OIL QUANTITY TRANSMITTER IAW AMM 49-94-04, OPS CHECKS GOOD.</P>)

ATA 2822

L/H CTR OVERRIDE PUMP DOESN'T PUT OUT ENOUGH PRESSURE.(<P>REMOVED AND REPLACED L/H CTR OVERRIDE PUMP, REF 28-22-05. OPS AND LEAK CHECK OK.</P>)

ATA 2822

L FWD FUEL PUMP CAUTION MSG APPEARED AFTER LANDING (INTERMITTENT).(<P>REMOVED PRESSURE SWITCH, PURGED, CLEAN AND INSPECTED FUEL PRESSURE LINE. REINSTALLED PRESSURE SWITCH AND CLEAN CONNECTOR IAW AMM 28-42-01. OPS CHECK GOOD. LEAK CHECK GOOD.</P>)

ATA 2560

FORWARD CABIN EMERGENCY MEDICAL KIT MISSING.(<P>INSTALLED&NBSP;MISSING FORWARD CABIN MEDICAL KIT IAW WORK CARD NUMBER A-25-099-20-01.</P>)

ATA 2897

LT FWD FUEL PUMP PRESS EICAS ON FINAL APPROACH.(<P>LH FWD FUEL PUMP PRESSURE SWITCH CONNECTOR CLEANED AND RESET I.A.W AMM 28-42-01. OPS CHECK SATISFACTORY, ALL INDICATIONS NORMAL.</P>)

ATA 2820

L FWD FUEL PUMP EICAS, QRH COMPLETE.(<P>L FWD PUMP OPS CHECK NORMAL PER FIM 28-22 TREE 819.</P>)

ATA 2820

LEFT FWD FUEL PUMP CAUTION.(<P>REMOVED AND REPLACED LEFT FWD PRESSURE SWITCH (LEFT FUEL PRESSURE). OPS CHECKED NORMAL IAW B767 AMM 28-42-01.&NBSP;</P>)

ATA 3040

LEFT SIDE WINDOW HEAT SWITCH WILL NOT STAY IN.(<P>REMOVED AND REPLACED WINDOW HEAT PANEL ASSY IAW B767 AMM 30-41-02. OPS CHECK NORMAL.</P>)

ATA 2897

LEFT FUEL PUMP PRESS LIGHT ILLUMINATED W/ EICAS ON LANDING.(<P>CLEANED C/P ON LT FWD BOOST PUMP PRESSURE SW, OPS CHK NORMAL PER AMM 28-42-02.</P>)

ATA 2822

L FWD FUEL PUMP EICAS MESSAGE DISPLAYED AFTER TOUCHDOWN.(<P>ITEM TRANSFERRED TO MDDR 125004 PER MEL 28-22-01. ITEM IS CAT C, DUE 04MAR20. MX ACTION C/W. ALL PLACARDS INSTALLED. MCC NOTIFIED.</P><P>LP 1048618 - ITEM M3: AS PER WD 28-22-11, REPLACED K10703 GFI RELAY. OPS TESTED LEFT FWD BOOST PUMP IAW AMM 28-22-00, TESTED OK. THIS CLEARS MDDR 125004. PLACARD REMOVED.</P>)

ATA 4900

APU FAULT EICAS MSG.(<P>A/C IS IN MAINTENANCE.</P><P>INSPECTED APU FOR FAULTS, APU CONTROLLER SHOWED NO FAULTS, NO MESSAGE ON EICAS, OPERATED APU THRU SEVERAL CYCLES, NO FAULTS NOTED PER AMM 49-11-00.</P>)

ATA 2822

L FWD FUEL PUMP EICAS MESSAGE.(<P>TRANSFERRED TO MDDR #124856 IAW MEL 28-22-01, CAT C, DUE 29FEB20. PLACARD INSTALLED. MCC NOTIFIED AND MX PROCEDURE C/W.</P>)

ATA 2822

DURING APPROACH LH FWD FUEL PUMP MESSAGE APPEARED. RAN QRH.(<P>NO EICAS MSG PRESENT. ACCOMPLISHED OPS CHECK FOR THE LH FWD FUEL PUMP PER AMM 28-22-00. OPS CHECK GOOD. MCC NOTIFIED.</P>)

ATA 2822

L FWD FUEL PUMP.(<P>OPS CHECKED L/H FWD FUEL BOOST PUMP IAW B767 AMM 28-22-00, OPS CHECK GOOD. NO EICAS MESSAGES DISPLAYED.</P>)

ATA 2822

L FWD FUEL PUMP EICAS MSG ON LANDING.(<P>TRANSFERRED TO MDDR 124422 PER MEL 28-22-01, CAT 'C', DUE 18FEB20.</P><P>REF LOG PAGE 1226141: REMOVED AND REPLACED L/H FWD BOOST PUMP PER AMM 28-22-03. OPS AND LEAK CHECKS GOOD. THIS CLEARS MDDR 124422. PLACARD REMOVED.</P>)

ATA 2150

R PACK TEMP EICAS IN FLIGHT FL 390 LEVEL FLIGHT. QRH COMPLIED WITH. R PACK CONTROL SELECTOR REMAINS AT STBY N.(<P>REMOVED AND REPLACED RH RAM AIR INLET DOOR ACTUATOR IAW B767 AMM 21-53-03. BITE RH TEMP CONTROLLER TEST GOOD. REFER TO ITEM M19 LP 1226188 FOR OPERATIONAL CHECK OF THE PACK OUTLET TEMP CONTROLLER IAW B767 AMM 21-51-14.</P><P>LP 1226188 - ITEM M19: PERFORMED OPS CHECK OF THE R PACK IAW B767 AMM 21-53-03, OPS CHECK GOOD AT THIS TIME.</P>)

ATA 2560

CA SIDE SMOKE GOGGLES HEADSTRAP NEEDS REPLACEMENT. STRAP IS LOOSE AT TIGHTEST ADJUSTMENT. STRAP LOOSENS ON ITS OWN FROM TIGHTEST ADJUSTMENT.(<P>REMOVED AND REPLACED&NBSP;CA SIDE SMOKE GOGGLES IAW B67 AMM 25-64-00.<BR /></P>)

ATA 3510

F/O O2 MASK HARNESS INOP.(<P><SPAN>O2 MASK REMOVED FROM 2ND OBS POSITION AND USED AT F/O POSITION.</SPAN><SPAN>&NBSP;</SPAN>OPS CHK SATISFACTORY, NO LEAKS NOTED. NOW 2ND OBS O2 MASK INOP.</P><P>LP 1226171 - ITEM 5: 2ND OBS O2 MASK INOP TRANSFERRED TO DMI 124232 IAW DDG 25-11-02-02, CAT 'D'.</P><P>LP&NBSP;1226172 - ITEM 3: REMOVED AND REPLACED 2ND OBS O2 MASK. LEAK AND OPS CHECKED OK PER AMM 35-11-51. THIS CLEARS MDDR 124232. PLACARD REMOVED.</P>)

ATA 3610

L ISLN VALVE STICKING AND SLOW TO OPEN.(<P>L ISLN VALVE REMOVED AND REPLACED IAW AMM 36-11-04. OPS CHECK SATISFACTORY, ALL INDICATIONS NORMAL.</P>)

ATA 7300

L ENG FUEL FILTER STATUS MSG.(<P>REMOVED AND REPLACED L ENG FUEL FILTER IAW AMM 73-11-02, NO LEAKS NOTED.</P>)

ATA 7497

RIGHT ENGINE IGNITOR 1 WAS INOPERATIVE. REMOVED AND REPLACED THE IGNITER PLUG NR 1 IAW AMM 74-21-02, NO HELP. REMOVED AND REPLACED RH ENGINE IGNITION EXCITER IAW AMM 74-11-01, NO HELP. FOUND BAD WIRE ON P37 AT RELAY K1231 (WDM 74-31-21). REPAIRED WIRE IAW SWPM 20-81-12. RT ENGINE IGNITION 1 & 2 TESTED GOOD IAW AMM 74-00-00. DMI 123685 CLEARED.

ATA 7261

NR 1 ENGINE HAS HIGH OIL CONSUMPTION. FOUND IDG GARLOCK SEAL LEAKING. DRAIN LINE CAPPED IAW AMM 71-71-00. REMOVED LEFT IDG, REMOVED AND REPLACED LH IDG DRIVE CARBON SEAL IAW AMM 72-64-02. INSTALLED LT IDG IAW AMM 24-11-01. RUN AND LEAK CHECKED OK IAW AMM 71-00-00. DRAIN LINE RESTORED.

ATA 2121

AFT EQ EXH FAN 1 STATUS MESSAGE. PERFORMED FIM TASK 21-26 FT 805. SYSTEM OK, MESSAGE CLEARED.

ATA 2421

APU GENERATOR INOPERATIVE. PERFORMED A BITE ON BPCU, FAULTS GENERATOR DIODE. REMOVED AND REPLACED THE APU GENERATOR IAW AMM 24-21-01. OPS CHECKED GOOD, LEAK CHECKED GOOD.

ATA 2822

EICAS "LH FWD FUEL PUMP"(<P>PERFORMED OPERATIONAL CHECK PER AMM 28-22-00. NO FAULTS NOTED. SYSTEM OK FOR SERVICE.</P>)

ATA 2150

L PACK TEMP EICAS, PERFORMED BITE ON LT PACK CONTROLLER IAW FIM 21-51-00. FAULT LT PACK TEMP CONTROL VALVE. REMOVED AND REPLACED THE TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECKED NORMAL,

ATA 2897

LEFT ENGINE FWD FUEL PUMP LOW PRESS LIGHT WILL NOT SHUT OFF. CONFIRMED LH FWD FUEL PUMP OPERATING OK. LOW PRESSURE LIGHT DOES NOT TURNOFF. FOUND THE CONNECTOR TO THE LEFT FWD PRESSURE SWITCH NOT INSTALLED ON SWITCH. CONNECTED THE CONNECTOR TO THE SWITCH. LEFT FWD PRESSURE SWITCH CHECKED OK IAW AMM 28-42-01.

ATA 2150

LEFT PACK INOPERATIVE IN AUTO. OPS CHECKED OK IN STBY. REMOVED AND REPLACED LEFT RAM DOOR ACTUATOR IAW AMM 21-53-02. OPS CHECK OK .

ATA 2150

LEFT PACK TEMP EICAS, RAN THE QRH/NNL AND REMAINED IN STBY.(<P>PREFORMED BITE ON PACK TEMP CONTROLLER, FAULT FOR RAM ACTUATOR - CLEARED FAULTS, RAN BITE AGAIN. NO MX FAULTS. SYS OK FOR SERVICE PER FIM 21-51-00.</P>)

ATA 2822

L FWD FUEL PUMP EICAS MESSAGE ON DESCENT. TROUBLESHOOTING PERFORMED FIM 28-22 FAULT TREE 819 TO STEP 50, BLED THE PRESSURE SENSE LINE. INSPECTED SENSE LINE IAW FIM 28-22 FT 819. NO WATER OR DEBRIS FOUND. REMOVED AND REPLACED THE LT FWD FUEL PUMP IAW AMM 28-22-03. OPS AND LEAK CHECKED GOOD.

ATA 2150

LEFT PACK TEMP EICAS MESSAGE, PER QRH PACK SELECTOR TO STBY N, MESSAGE WENT OUT. PERFORMED OPS TEST IAW AMM 21-51-00. OPS CHECKED GOOD.

ATA 2150

FWD EQPT VALVE EICAS MESSAGE. REMOVED AND REPLACED PSEU IAW AMM 32-09-04. OPS CHECKED GOOD. PERFORMED AUTO SPEED BRAKE SYS TEST AND OPS TEST IAW AMM 27-62-00. OPS CHECKED GOOD.PERFORMED OPS TEST IAW AMM 21-23-08, OPS TESTED GOOD.

ATA 2820

DURING START LEFT ENGINE SPAR VALVE LIGHT DID NOT ILLUMINATE. ENGINE STABILIZED AND SHUT DOWN BY ITSELF. REMOVED AND REPLACED LEFT SPAR VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED GOOD.

ATA 3610

LEFT BLEED ISOLATION VALVE EICAS MESSAGE.(<P>REMOVED AND REPLACED LEFT BLEED ISOLATION VALVE IAW AMM 36-11-05-404-013. OPS CHECK GOOD.</P>)

ATA 2150

L PACK TEMP EICAS CAUTION, PERFORMED QRH 2.51. MESSAGE EXTINGUISHED. PERFORMED AN OPS TEST IAW AMM 21-51-00, OPS CHECKED GOOD.

ATA 3443

CAPTAIN'S RADAR ALT PROVIDING/DISPLAYING ERRONEOUS INDICATIONS ON DESCENT BELOW 8000.&NBSP;(<P>PERFORMED OPS TEST IAW AMM 34-43-00. OPS CHECK GOOD.</P>)

ATA 3610

L ISLN VALVE EICAS BLEED.(<P>PERFORMED GROUND TEST I.A.W AMM 36-11-04. OPS CHECK GOOD.</P>)

ATA 7330

FUEL LEAKING FROM LEFT ENGINE.(<P>UPON INSPECTION FOUND FUEL TRANSMITTER DRAIN LINE CAP LOOSE. TIGHTENED I.A.W AMM 70-50-00. WET MOTORED ENGINE FOR LEAK CHECK I.A.W AMM 71-00-00. NO LEAKS. OPS CHECK GOOD.&NBSP;</P>)

ATA 3350

EMERGENCY LIGHTS AT RIGHT AISLE CEILING INOP (ROW 22JL).(<P>REMOVED AND REPLACED BATTERY PACK ASSY IAW B767 AMM 33-51-07, OPS CHECK OK.</P>)

ATA 7310

RIGHT ENGINE FUEL FILTER STATUS/EICAS MESSAGE.&NBSP;(<P>REMOVED AND REPLACED RIGHT ENGINE FILTER REF AMM 73-11-02-004-001-H00, NO LEAKS NOTED. PERFORMED FUEL FILTER INSPECTION, NO DAMAGE FOUND IN REF 73-11-03-202-001-H00. PERFORMED ENGINE RUN, NO MESSAGES, ALL NORMAL REF AMM 71-00-00.</P>)

ATA 2150

FWD EQUIPMENT VALVE EICAS MESSAGE. REMOVED AND REPLACED EQUIPMENT COOLING INDICATION CARD IAW AMM 21-58-24, NO HELP. REMOVED AND REPLACED THE MANIFOLD INTERCONNECT VALVE IAW AMM 21-58-01. OPERATIONAL CHECKS PERFORMED IAW AMM 21-58-01-005. CHECKED GOOD.

ATA 3610

AFTER ENG START, "RH ENG BLEED" MSG. NO DUCT PRESSURE.&NBSP;(<P>PER CUSTOMER REQUEST, REMOVED AND REPLACED R/H PRSOV IAW B767 AMM 36-11-09, OPS CHECK REQUIRED.</P><P>LP 1112969 - ITEM M22: PERFORMED OPERATIONAL CHECK OF&NBSP;R/H PRSOV IAW AMM 36-11-09, NO FAULTS OR DEFECTS NOTED.&NBSP;</P>)

ATA 3610

RT ENGINE BLEED FAILED TO PRESSURIZE.(<P>PERFORMED AIR CONTROL MODULE BITE TEST, MSG PRSOV ON RIGHT ENG. AFTER BITE, RESET, AND PERFORMED ENG RUN. OPS CHECK OK IN REF AMM 36-23-00 AND AMM 71-00-00.</P>)

ATA 7997

LEFT ENGINE OIL PRESSURE NOT SHOWING ON EICAS.(<P>TEMPORARILY REPAIRED WIRE W5322-301R-18 IAW SWPM 20-10-13. LEFT ENGINE OIL PRESSURE INDICATION OPS CHK GOOD IAW AMM 79-32-00.<BR /></P>)

ATA 2897

LEFT FWD FUEL PUMP DISPLAYED EICAS ON FINAL APPROACH, WENT AWAY SHORT FINAL.(<P>CLEANED CONNECTOR FOR THE LEFT FORWARD FUEL PUMP PRESSURE SWITCH. PUMP OPS CHECK GOOD IAW AMM 28-22-03.</P>)

ATA 2822

L FWD FUEL PUMP INOP AFTER LANDING.(<P>PERFORMED OPS CHECK OF THE LEFT FORWARD FUEL PUMP IAW AMM 28-22-03, OPS CHECK GOOD AT THIS TIME.</P>)

ATA 2822

EICAS MESSAGE FOR LT FWD FUEL PUMP. CYCLED LT FWD FUEL PUMP CIRCUIT BREAKER IAW AMM 28-22-01, OPS CHECKED OK. MESSAGE CLEARED IAW AMM 28-22-01.

ATA 2822

ON APPROACH, LEFT FORWARD FUEL PUMP EICAS MESSAGE.&NBSP;(<P>PERFORMED OPS TEST IAW AMM 28-22-00, OPS CHECK GOOD.&NBSP;</P>)

ATA 3610

"LEFT ENGINE HPSOV" EICAS MSG, QRH COMPLETED.(<P>TRANSFERRED TO MDDR #119459 IAW MEL 36-11-02-02, CAT C, DUE: 31-OCT-19. MCC NOTIFIED AND PLACARD INSTALLED.&NBSP;</P><P>LP 1112974 - M10: REMOVED AND REPLACED FAN AIR TEMP SENSOR PER B767 AMM 36-11-17. PERFORMED TUMB CHECK OF THE HPSOV AND CONTINUITY CHECK OF SWITCHES PER WDM 36-11-61. LEAK AND OPS CHECK FOUND NORMAL PER AMM 36-11-17 AND AMM 71-00-00. THIS CLEARS MDDR 119459. PLACARD REMOVED AND MCC NOTIFIED.</P>)

ATA 2822

L FWD FUEL PUMP PRESS, QRH COMPLETED.(<P>PERFORMED OPS TEST IAW AMM 28-22-00, OPS CHECK GOOD.</P>)

ATA 7530

L ENG HPSOV EICAS MESSAGE, QRH COMPLETED.&NBSP;(<P>TRANSFERRED TO MDDR #119359 IAW AMM 36-11-02-02, CAT C, DUE DATE: 29-OCT-19. MCC NOTIFIED AND PLACARD INSTALLED.</P><P>LP 1210888 - M4: REMOVED AND REPLACED L/H BLEED AIR CONTROL CARD IAW AMM TASK 36-11-12-404-026. RAN ENGINE IAW AMM 71-00-00, OPS CHECK NORMAL. THIS CLEARS MDDR #119359. PLACARD REMOVED AND MCC NOTIFIED.</P>)

ATA 3610

IN-FLIGHT L ENG HPSOV. CHECKLIST COMPLETED, 3RD WRITE UP.&NBSP;(<P>REMOVED AND REPLACED HPSOV PER AMM 36-11-07. LEAK CHECKS OK AND OPS CHECKS NORMAL.</P>)

ATA 3520

DURING LANDING, THE ONBOARD MX REP REPORTED AN O2 MASK DEPLOYED. REPACKED MASK @ 1 JL IAW AMM 35-21-14, OPS CHECK GOOD.</P>)

ATA 3610

L ENG HPSOV EICAS. ALL MAINTENANCE PROCEDURES COMPLIED WITH. REMOVED AND REPLACED HIGH PRESSURE CONTROLLER IAW AMM 36-11-08, OPS CHECK NORMAL.

ATA 3610

LEFT ENG HPSOV EICAS MESSAGE DISPLAYED AND ASSOCIATED STATUS MESSAGE. ACCOMPLISHED QRH CHECKLIST. PERFORMED AIR SUPPLY CONTROL SYSTEM BITE IAW AMM 36-23-00, STATUS CLEARED. COMPLIED WITH HPSOV TEST IAW AMM 36-11-07, NO DEFECTS FOUND AT THIS TIME.

ATA 7421

RIGHT ENGINE DID NOT LIGHT OFF ON FIRST ATTEMPT, SECOND ATTEMPT SUCCESSFUL. STATUS MSG R ENG IGNITER 1. REMOVED AND REPLACED RIGHT ENGINE IGNITER NR 1 PER AMM 74-21-02. PERFORMED RIGHT ENGINE AUDIBLE CHECK PER AMM 74-00-00-730-803-H03. OPS CHECK GOOD AT THIS TIME.

ATA 7400

RT ENG IGNITION STATUS MESSAGE. RH ENG NO IGNITION WITH SINGLE IGN SELECTED ON FIRST START ATTEMPT. START SUCCESSFUL IN BOTH. PERFORMED RT ENGINE START AT THE GATE. ALL INDICATIONS NORMAL IN SINGLE SOURCE IGNITION START IAW AMM 71-00-00.

ATA 3610

EICAS RT ENG BLEED OFF. REF DMI # 118236, RT ENGINE HPSOV LOCKED CLOSED PER 36-11-02-02. DISP: YK @ 13:13Z. LP1210839 - M2: REMOVED AND REPLACED RIGHT ENGINE HPSOV. OPS CHECK AND ALL INDICATIONS NORMAL. ENGINE RUN PER AMM 71-00-00 AND 36-11-07. OFF PART (PN: 790270-14, SN: 880311) LP 1210839 - M3: REMOVED AND REPLACED RIGHT ENGINE HP CONTROLLER PER AMM 36-11-08. OPS AND INDICATIONS NORMAL. ENGINE RUN IAW AMM 71-00-00. THIS CLOSED MDDR 118236.

ATA 8012

LT ENGINE VALVE LIGHT CAME ON. PERFORMED ENGINE RUNS IAW AMM 71-00-00, TEST 3. OPERATIONAL TEST NORMAL. AIRCRAFT RELEASED TO CONTINUE ETOPS SERVICE.

ATA 2150

HI FLOW INHIBIT MESSAGE. PERFORMED FIM 21-51 FAULT TREE 813. CYCLED LT & RT PACK CONTROL SWITCHES, SYSTEM OPERATIONAL CHECK SATISFACTORY.

ATA 7797

4.3 UNITS FAN VIBRATION ON LEFT ENGINE INDICATED ON CLIMB OUT. ACCOMPLISHED FIM 71-05 FT 853. SECURED WIRING HARNESS IAW AMM 70-24-05. SECURED HOLD OPEN ROD IAW AMM 71-11-00. NO ISSUES NOTED ON ENGINE RUN, VIBE AT 1.8 UNITS.

ATA 3097

LEFT SIDE WINDOW HEAT INOP. TRANSFERRED TO MDDR # 117627 AS PER MEL 30-40-01-02 CAT C LP 1076367: REPAIRED BROKEN WIRE AT L2 WINDOW C/P IAW SWPM 20-10-11. OPS CHECK NORMAL. MDDR 117627 CLEARED. PLACARD REMOVED AND MCC NOTIFIED.

ATA 3610

#1 ENG PRV VALVE HAS FAILED HEALTH CHECK. REMOVED & REPLACED #1 ENG PRV VALVE IAW AMM 36-11-18. OPS CHECK GOOD, NO LEAK NOTED.

ATA 7334

#2 ENGINE FUEL PRESSURE SWITCH IS LEAKING FROM FWD FITTING LOCATED ABOVE FUEL FILTER. REMOVED AND REPLACED #2 ENGINE FUEL PRESSURE SWITCH PACKING, AND RE-INSTALLED #2 ENG FUEL PRESSURE SWITCH IAW AMM 73-34-01. PENDING LEAK CHECK. PERFORMED LEAK CHECK IAW AMM 71-00-00, NO LEAKS NOTED.

ATA 2613

AFTER TAKEOFF, "FWD EQPT OVHT" EICAS MESSAGE ILLUMINATED. RAN QRH WHICH CALLED FOR PUTTING EQUIP COOLING SELECTOR TO STBY. EICAS MSG EXTINGUISHED. LEFT EQUIPMENT COOLING SELECTOR IN STANDBY PER QRH.&NBSP;(<P>TROUBLESHOT PER FIM 21-58 FAULT TREE 912. NO MESSAGES SHOWN. CLEANED SUPPLY EXHAUST FAN SCREEN PER AMM 21-58-22.<BR /></P>)

ATA 3150

EICAS MSG OF "FWD EQPT OVHT" RCVD DURING INITIAL CLIMB. EICAS MSG CLEARED AFTER COMPLETING STEP 6 OF NNC. PERFORMED OPS CHECK OF FWD EQPT COOLING SYSTEM GRILL INLET, SUPPLY AIR INLET, EXHAUST FAN, AND SCREEN. OPS CHECKED GOOD AT THIS TIME PER AMM 21-58-00/201.

ATA 2121

#1 EQUPIMENT COOLING FAN EICAS MESSAGE DISPLAYED &AMP; CB POPPED. (<P>REMOVED AND REPLACED&NBSP;#1 EQUIPMENT COOLING FAN IAW AMM 21-26-01-004-001/404-024, OPS CHECK GOOD.<BR /></P>)

ATA 2150

LT PACK TEMP&NBSP; DISPLAYED ON APPROACH LIGHT EXTINGUISHED&NBSP; AND CAME BACK ON&NBSP;(<P>PERFORMED&NBSP; LEFT PACK TEMP CONTROLLER PER AMM 21-51-14 OPS CHECK OK</P>)

ATA 3442

WX RADAR REQUIRES -6 TILT TO SEE T-STORMS 40 NM AWAY. (<P>PERFORMED OPS CHECK OF WEATHER RADAR AS PER AMM 34-43-00. OPS CHECKED GOOD AT THIS TIME.&NBSP;</P>)

ATA 2613

ON CLIMBOUT @ APPROX 2000' AGL, EICAS MSG FWD EQPT OVHT, FOLLOWED QRH AND MESSAGE CLEARED. OPS TEST C/W IAW AMM 21-58-00, ALL TEST PASS. NO ACTIVE MSG AT THIS TIME.

ATA 2121

EQUIPMENT COOLING EICAS DID NOT RESOLVE. OPERATED IN STANDBY MODE PER QRH, MESSAGE STAYED CLEAR W STDBY MODE. PERFORMED OPERATIONAL TEST IAW AMM 21-58-00. OPS CHECKS GOOD.

ATA 5610

L3 WINDOW HAS BUBBLES. REMOVED AND REPLACED L3 WINDOW IAW AMM 56-11-00-404. ACCOMPLISHED L3 WINDOW HEAT SYSTEM CHECK PER AMM 30-41-00, TEST GOOD.

ATA 2150

AFTER T/O, CLIMBING 1000 FT, EICAS MSG "FWD EQUIPMENT OVHT". IAW QRH UP TO STEP 7, EICAS MSG CLEARED. NO STATUS MSG. OPS TEST CARRIED OUT IAW AMM 21-58-00. ALL TEST PASS, NO ACTIVE MSGS. OK FOR SERVICE.

ATA 3350

ON INSPECTION, FOUND LEFT EXT EMERGENCY 2 AFT LIGHTS INOP.(<P>REPLACED BULBS FOR LEFT AFT EXT EMERGENCY LIGHTS IAW B767 AMM 33-51-01. OPS CHECK NORMAL.</P>)

ATA 3350

ON INSPECTION, FOUND FLT DECK EMERGENCY EXIT LIGHT INOP. OPERATIONAL CHECK OK IAW B767 AMM 33-51-00-715-200.

ATA 3350

ON INSPECTION, FOUND LEFT &AMP; RIGHT OVER WING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK IAW B767 AMM 33-51-07. EMERGENCY EXIT LIGHTS OPS CHECK NORMAL IAW B767 AMM 33-51-00.

ATA 2822

CENTER LEFT FUEL PUMP MESSAGE ON CLIMB OUT.(<P>TRANSFERRED CENTER LEFT FUEL PUMP TO MDDR #111904 PER MEL 28-22-02A CAT C DUE 29MAY19 PLACARD INSTALLED.</P><P>LP 1081508 - M10: REMOVED AND REPLACED LEFT CENTER BOOST PUMP IAW AMM 28-22-02.</P>)

ATA 2162

FLIGHT DECK TEMP EICAS AFTER ENGINE SHUTDOWN(<P>PERFORMED BITE TEST AND FIM TASK PER 21-64. OPS CHECKED GOOD.<BR /></P>)

ATA 4950

APU SURGE VALVE FILTER THREADS DAMAGED INTERNALLY.(<P>REMOVED AND REPLACED&NBSP;APU SURGE VALVE REF B767 AMM 49-53-01.</P>)

ATA 2121

STATUS MESSAGE AFT EQ EX FAN 2.(<P>REMOVED AND REPLACED #2 AFT EQ EXHAUST FAN ASSY PER AMM 21-26-01.<BR /></P>)

ATA 8012

EICAS MESSAGES R STARTER CUTOUT AND R ENG STARTER DISPLAYED AFTER TAKEOFF(<P>REMOVED AND REPLACED R ENGINE STARTER VALVE I.A.W 80-11-02. OPS CHECKS GOOD.&NBSP;<BR /></P>)

ATA 2121

AFT EQUIPMENT EXHAUST FAN INOP. RESET THE C/B. FLEW 2 LEGS, NO ISSUES IAW 21-58-001.

ATA 2797

DURING DISARM OF OFF WING ESCAPE SYSTEM FOR MAINT. FOUND LH SPOILER OVERRIDE ACTUATOR SQUIB PINS PUNCHED AND BENT. REMOVED AND REPLACED LH SPOILER OVERRIDE ACTUATOR SQUIB IAW AMM 25-65-10. OPS CHECKED GOOD IAW AMM 25-65-00.

ATA 4950

DURING MAINT TASK ON APU, FOUND SURGE CONTROL VALVE RUBBER DUCT WITH HOLE IN IT.(<P>REMOVED AND REPLACED SURGE VALVE DUCT PER AMM 49-53-01. LEAK AND OPS CHECK GOOD.

ATA 4990

APU HAS OIL LEAK IN THE VICINITY OF THE FILL CAP. FOUND OIL CAP PACKINGS WORN. REMOVED AND REPLACED APU OIL TANK CAP PACHINGS PER AMM 12-13-01-613-001. OPERATED APU &AMP; NO LEAKS NOTED.<BR /></P>)

ATA 3610

LEFT ISLN CHECK VALVE. CHECK VALVE PN 732-11750-03(<P>R/R ISOLATION BYPASS CHECK VALVES IAW AMM 36-11-05/401. OP PNEUMATIC LEAK NORMAL AT THIS TIME.</P>)

ATA 2612

LEFT ENGINE LP 1 INOP&NBSP;(<P>TRANSFERRED TO MDDR 108667</P><P>LP 0971739-M6: REPLACED TERMINAL END LEFT ENG UPPER AFT LOOP RIGHT SIDE IAW SWPM 20-10-11. LEFT ENGINE FIRE WARNING CHECKS OK PER AMM 26-11-00. CLOSED MDDR 108667.</P><P><BR /></P>)

ATA 7740

PER TASK CARD A-77-304-01 TALLY 8027 STANDBY ENGINE INDICATIOR (ETOPS) BITE TEST FAILED(<P>REMOVED AND REPLACED STANDBY ENGINE INDICATOR IAW AMM 77-41-01. BITE TEST SATISFACTORY IAW 77-41-01.</P>)

ATA 7230

DURING INSPECTION ON NR 1 ENGINE ACCUSTICAL LINER SEGMENT FROM 4 O CLOCK TO 6 O CLOCK POSITION WAS FOUND WITH DELAMINATION.(<P>REMOVED AND REPLACED ACOUSTICAL LINER SEGMENT IAW AMM 72-33-01-004-001-H00 AND 72-33-01-404-011-H00.</P>)

ATA 7230

ENG #2 DURING ACCOMPLISHMENT OF LP COMPRESSOR ROTOR BLADES INSPECTION WERE FOUND SEVERAL BLADES WITH NICKS AND DENTS WITHIN LIMITS THAT WILL NEED BLEND. REPAIRED BLADES ON #2 ENGINE IAW AMM 72-31-02-308-055-H00.

ATA 2564

O/H BIN WITH EXTRA LIFE RAFT WONT STAY SHUT(<DIV>REPOSITIONED LIFE RAFT IN OVRHEAD BIN. NOW CLOSES BETTER AND STAYS LOCKED</DIV>)

ATA 2150

LT PACK INOP IN AUTO(<DIV>R/R LT PACK TEMP CONTROL VALVE PER AMM 21-51-12 OPS CHECKS GOOD. DISPATCH AA@0655Z</DIV>)

ATA 2612

LEFT ENGINE LOOP 1 INOP.&NBSP;(<P>DEFERRED IAW MEL 26-11-01-0 CNTRL 18 MAR 19, MDDR #108360.<BR /></P><P>LP 0971727-M20 REMOVED AND REPLACED&NBSP; FIRE DETECTION CARD ASSY IAW AMM 26-10-01, OPS CHECK OK. CLEARED MDDR # 108360.&NBSP;</P>)

ATA 2150

LEFT PACK OFF EICAS MESSAGE AFTER ENGINE START.(<DIV>CYCLE PACK SWITCH, CYCLE LEFT ISOLATION VALVE. OPS CHECK GOOD. REF FIM 21-51 FT 876. SYSTEM OK FOR SERVICE.&NBSP;</DIV>)

ATA 2612

LEFT FIRE LOOP STATUS MESSAGE.&NBSP;(<P>ENGINE FIRE DETECTION SYSTEM TEST CARRIED OUT IAW AMM 26-11-00 TEST PASS MESSAGE SELF ERASED.&NBSP;</P>)

ATA 2897

L FWD FUEL PUMP EICAS AND PRESS LIGHT ON RADAR DOWNWIND(<P>TRANSFER TO MDDR 107885 IAW DDG 28-22-01</P><P>LP 0975817-M7: REMOVED AND CLEANED PRESSURE SWITCH CONNECTOR. RESET C/B, PERFORMED OPS CHECK IAW AMM 28-22-01. OPS CHECK GOOD AND PLACARDS REMOVED. MDDR 107885 CLOSED. DISPATCH @ST10131.&NBSP;</P>)

ATA 2133

OUTFLOW VALVE INDICATION. REMOVED AND REPLACED THE OUTFLOW VALVE ACTUATOR IAW AMM 21-31-04, OPS CHECKED GOOD.

ATA 2822

L FWD FUEL PUMP INOP(<P>TRANSFER TO MDDR # 107464 IAW DDG 28-22-01 CAT C DUE DATE 02-27-2019</P><P>LP 1054875: REMOVED AND REPLACED LEFT FWD FUEL PUMP IAW AMM 28-22-03, OPS CHECKED GOOD. THIS CLEARS MDDR 107464. PLACARD REMOVED.<BR /></P>)

ATA 2822

ON FINAL APP, L FWD FUEL PUMP EICAS WITH 11.0 IN L FUEL TANK&NBSP;(<P>OPERATED LT FWD FUEL PUMP SW, ALL EICAS AND LOW PRESSURE LIGHTS FUNCTION NORMAL PER AMM 28-42-01</P>)

ATA 2820

"RT AFT FUEL PUMP LOW PRESS SWITCH INOP / ( FUEL PUMP LOW PRESS LIGHTS, -200/-300 )"(<P>R/R RIGHT AFT FUEL PRESS SWITCH PER AMM 28-42-01,THIS CLEARS MDDR 107124.</P>)

ATA 2820

"L FWD FUEL PUMP INOP / ( MAIN TANK FUEL PUMPS (NOTIFY DISPATCH)."(<P>REMOVE AND REPLACED PRESSURE SWITCH IAW 28-42-01,THIS CLEARS MDDR 107070.</P>)

ATA 2822

L FORWARD FUEL PUMP EICAS MSG&NBSP;(<P>PERFORMED OPS TEST OF LEFT FORWARD FUEL PUMP, ALL CHECKS OK NO FAULTS OR EICAS MSG AS PER AMM 28-22-00</P>)

ATA 3697

R ENG PRV EICAS RECEIVED IN FLIGHT&NBSP;(<P>TRANSFERRED TO MDDR # 106721 AS PER MEL 36-11-08-01-01A CAT C&NBSP;</P><P>FOUND OPEN BETWEEN AIR SUPPLY BITE MODULE D2378A-B13 AND PIN 1 OF PRV CONTROLLER CAUSED BY BROKEN WIRE AT TB320 YA19 AT P37 PANEL , RESECURED WIRE AT TB320 YA19 PER SWPM 20-90-11 RAN ENG AND OPS CHECK OK, MDDR CLOSED&NBSP;<BR /></P>)

ATA 3610

RT ENG PRV EICAS AFTER ENG START(<P>TRANSFERRED TO MDDR 106393 IAW DDG 36-11-08-01-01A</P><P>REF LOG PAGE 1025719 ITEM M3; REMOVED AND REPLACED RIGHT ENGINE PRV IAW AMM 36-11-18. OPS CHECK NORMAL. NO LEAKS NOTED. LOG PAGE 1025720 ITEM M4; REMOVED AND REPALCED PRESSURE REGULATING CONTROLLER ASSY IAW AMM 36-11-19/401, OPS CHECK OK, NO LEAKS FOUND, NO EICAS MESSAGE AFTER ENGINE RUN LEAK CHECK. THIS CLEARS MDDR 106393.&NBSP;<BR DATA-MCE-BOGUS="1" /></P><P>PRV P/N 802170-12&NBSP; S/N 200103159</P><P><BR DATA-MCE-BOGUS="1" /></P>)

ATA 3020

AFTER ENG SHUTDOWN LEFT ENGINE ANTI ICE VALVE FAILED TO CLOSE&NBSP;(<P>REMOVED AND REPLACED LEFT ENGINE&NBSP; NOSE ANTI ICE VALVE IAW AMM 30-21-03 OPERATIONAL TEST OK</P>)

ATA 2820

RIGHT FWD FUEL PUMP SWITCH WHEN TURNED OFF, NO PRESS LIGHT AND NO R FWD FUEL PUMP EICAS MSG.(<P>REPLACED THE RIGHT FWD FUEL PUMP PRESSURE SWITCH, REF AMM 28-42-01 MDF 2668639 OPS AND LEAK NORMAL.<BR /></P>)

ATA 2842

LEFT FWD FUEL PRESSURE LIGHT WILL NOT EXTINGUISH WITH APU RUNNING.(<P>FWD TO MDDR 105784 PER MEL 28-42-01-01 CAT C. DUE DATE 21JAN19. ORANGE PLACARD INSTALLED. DISPATCH: @ 1309Z.LOG PAGE&NBSP; 0978492-M11 REMOVED AND REPLACED LEFT FWD FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01 OPS CHECK AND LEAKS NORMAL THIS CLEARED DMI 105784&NBSP;</P>)

ATA 2612

L ENG FIRE LP 2 STATUS MSG. (<P>R/R L ENG FIRE UPPER AFT DETECTOR&NBSP; REF AMM 26-11-01<BR /></P>)

ATA 3442

RIGHT SIDE WX RADAR SYS DISPLAYS MSG WXR WEAK. (<P>R/R WEATHER RADAR RT SIDE REF AMM 34-43-01 OPS CK OK<BR /></P>)

ATA 5347

CAPT. SIDE I/B AFT SEAT TRACK HAS GOUGE.(<P>REMOVED AND REPLACED SEAT TRACK.</P>)

ATA 5321

FWD CARGO BALLMAT HAS CORROSION IN BOTTOM SIDE OF PNL 124BXF.(<P>FABRICATED AND INSTALLED 1EA FILLER AND 1EA DOUBLER REPAIR.</P>)

ATA 7230

#2 ENGINE SPINNER REQ REPAINT AS PER CUSTOMER REQ.(<P>REMOVED,PAINTED &AMP; REINSTALLED #2 ENGINE SPINNER IAW B767 AMM 72-31-01 &AMP; ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)

ATA 2897

CUSTOMER REQUEST:RIGHT WING FUEL QUANTITY WIRE HARNESS SHOWS SIGNS OF ARCING.(<P>REMOVED AND REPLACED R/H FQIS WIRE HARNESS,LEAK CHECK &AMP; BITE CHECK GOOD NO LEAKS NOTED IAW B-767 AMM 28-41-01.</P>)

ATA 5697

FLIGHT DECK R-1 WINDSHIELD UPPER AND LOWER ELECTRICAL WIRE STRIPS ARE BROWN FROM ARCING.(<P>REMOVED AND REPLACED FLIGHT DECK R-1 WINDOW WITH SERVICEABLE UNIT IAW B767-3 AMM 56-11-01</P>)

ATA 5710

RIGHT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18207 RIR.</P>)

ATA 5220

L/H FWD OVERWING-EMERGENCY HATCH BOTTOM AFT STOP FTG HAS MISSING STOP PIN RETAINER.(<P>INSTALLED MISSING STOP PIN RETAINER ON L/H FWD OVERWING EMERGENCY HATCH BOTTOM AFT STOP FTG,IAW B-767 AMM 52-21-01,PERFORMED TOLERANCE CHECK OF EMERGENCY HATCH IAW B-767 AMM 52-21-01</P>)

ATA 3610

ASM HEALTH TEST FAILURE RIGHT PRV DOES NOT OPEN.(<P>REMOVED AND REPLACED #2 ENG. PRV IAW B767 AMM 36-11-18.PERFORMED SATISFACTORY LEAK CHECK AND NO LEAKS NOTED IAW B767 AMM 36-11-18.</P>)

ATA 3610

ASM HEALTH TEST FAILURE R/H FAV OPEN AND CLOSE DISAGREE.(<P>REMOVED AND REPLACED #2 ENG FAV IAW B767 AMM 36-11-16.PERFORMED SATISFACTORY OP/LK CHECK IAW B767 AMM 36-11-16.(NO DEFECTS NOTED).</P>)

ATA 3610

#1 ENG. PRV IS STICKING MANUALLY OPEN OR CLOSE.(<P>REMOVED AND REPLACED #1 ENG PRV IAW B767 AMM 36-11-18.ACCOMPLISHED OP/LK CHECK ON WORKSHEET T/C T2031 AND W/C 6736A013PT1.</P>)

ATA 2150

R/H E&AMP;E COOLING EXHAUST FAN HAS A BROKEN IMPELLER BLADE.(<P>REMOVED AND REPLACED R/H E&AMP;E BAY EXHAUST FAN IAW B767 AMM 21-58-06.OP/LK CHECK C/W AND NO DEFECTS NOTED IAW B767 AMM 21-58-06.</P>)

ATA 3610

#1 ENG PRV SENSE LINE/ELBOW @PRV IS LEAKING DAMAGED/LEAKS.(<P>REMOVED AND REPLACED #1 ENG SENSE LINE AND ELBOW @ PRV IAW N767 AMM 36-11-18. ELBOW P/N AS4138J0608.</P>)

ATA 3610

ASM HEALTH TEST FAILURE L/H F.A.T.S. DOES NOT COMMAND FAV TO CLOSE.(<P>REMOVED AND REPLACED L/H FAN AIR TEMPERATURE SENSOR IAW B767 AMM 36-11-17 OP/LK CHECK ACCOMPLISHED ON WORK T/C 6736A013PT1.</P>)

ATA 7220

#1 ENG SPINNER NEEDS REPAINT AS PER CUSTOMER.(<P>REMOVED,PAINTED &AMP; REINSTALLED #1 ENG SPINNER IAW B767 AMM 72-31-01 &AMP; ENGINE MANUAL (GEK 92451) TASK 72-21-10-300-802-0.</P>)

ATA 3610

ASM HEALTH TEST FAILURE R/H PRESSURE SENSOR OUTPUT IS TO HIGH.(<P>REMOVED AND REPLACED #2 ENG F.A.M.V. TEMP SENSOR IAW B767 AMM 36-11-17.PERFORMED SATISFACTORY LEAK CHECK (NO LEAKS NOTED)IAW B767 AMM 36-11-17.</P>)

ATA 2150

STANDBY PACK TEMP CONTROLLER FAIL AT POSITION 7.(<P>REMOVED AND REPLACED R/H PACK COMPRESSOR OULET SENSOR T55135 IAW B767 AMM 21-51-14.PERFORMED SATISFACTORY PACK STANDBY CONTROLLER BITE TEST IAW B767 AMM 21-51-14.</P>)

ATA 5710

LEFT WING UPPER FILL PORT HAS CORROSION AROUND FLANGE.(<P>COMPLIED WITH FEA 18210 IR.</P>)

ATA 5347

F/O SIDE I/B AFT SEAT TRACK HAS GOUGE.(<P>REMOVED AND REPLACED SEAT TRACK.</P>)

ATA 2432

MAIN SHIPS BATTERY IS DEAD. REMOVED AND REPLACED BATTERY IAW AMM 24-31-01 OPS CHECK GOOD.

ATA 2613

"FWD EQPT OVHT" EICAS. RAN QRH, EQUIPMENT COOLING OPERATIONAL TEST CARRIED OUT IAW AMM 21-58-00. OPS CHK SATIS. NO FAULTS MSGS.

ATA 7421

RT ENG IGNITION 1 INOP. REMOVED AND REPLACED RT ENG IGNITOR PLUG 1 AS PER AMM 74-21-02, RAN ENG OPS CHECK OK.

ATA 4960

APU AUTO SHUTDOWN SEVERAL TIMES, TROUBLESHOOT. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. OPS AND BITE TEST GOOD.

ATA 4960

APU AUTO SHUT DOWN. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05 OPS AND BITE TEST GOOD.

ATA 3350

EMERGENCY FLOOR LIGHT FWD OF 20F INOP. R&R LT FLOOR LIGHT BATTERY PACK. OPS CHECK GOOD PER AMM 33-51-07.

ATA 3350

EMERGENCY FLOOR LIGHT FWD OF 20F INOP. REMOVED AND REPLACED EMERGENCY LIGHT ASSY, OPS CHECK OK IAW AMM 33-51-05.

ATA 3350

FLOOR EMERGENCY LIGHT AFT OF SEAT 19H WAS FOUND INOPERATIVE. REPLACED THE LAMP, AND OPS CHECKED GOOD IAW AMM 33-11-10-962-064.

ATA 2565

AFT SERVICE DOOR EMERGENCY SLIDE BUSTLE COVER HAS A LATCH WITH DISBOUNDED INSERTS AT THE FWD BOTTOM LATCH. REPAIRED THE SLIDE BUSTLE COVER LATCH INSERTS IAW AMM 25-00-00.

ATA 3350

FLOOR EMERGENCY LIGHT FORWARD OF SEAT 4J INOPERATIVE. REPLACED THE LAMP, OPS CHECKED GOOD IAW AMM 33-51-10- 912-064.

ATA 3350

EMERGENCY LIGHT INOPERATIVE ABOVE SEAT 33C. REPLACED THE LAMPS, OPS CHECKED GOOD IAW AMM 33-51-05-002-039.

ATA 3350

FLOOR EMERGENCY LIGHTS INOPERATIVE FROM SEATS 31C TO 38C. REPLACED THE LAMPS IAW AMM 33-51-05-002-034, OPS CHECKED GOOD.

ATA 3450

AFT RIGHT EXTERNAL ESCAPE HATCH EMERGENCY SLIDE LIGHT INOPERATIVE. TROUBLESHOT IAW FIM 33-51, FOUND THE BATTERY PACK M733 INOPERATIVE. REPLACED THE BATTERY IAW AMM 33-51-07-201. OPS CHECKED GOOD IAW AMM 33-51-07-422-012.

ATA 3350

FLOOR EMERGENCY LIGHT, AFT RIGHT SIDE OF FWD COAT CLOSET WAS FOUND INOPERATIVE. RELAMPED THE EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-10-962-054.

ATA 3442

RIGHT WEATHER RADAR SYSTEM INOPERATIVE. R & R THE RIGHT WEATHER RADAR R/T, OPS NORMAL IAW AMM 34-43-00.

ATA 7300

EICAS IDLE DISAGREE.

ATA 2150

FWD EQUIPMENT COOLING EICAS MESSAGE, SWITCH REMAINED IN STBY FOR REMAINDER OF CHECK FLIGHT. PERFORMED EQUIPMENT COOLING TEST IAW AMM 21-58-00, TESTED OK, NO FUTHER ISSUES.

ATA 3350

EMERGENCY LIGHT LENS MISSING AT SEAT 20J. INSTALLED A NEW LENS IAW AMM 38-51-10, CHECKED NORMAL.

ATA 7200

AFTER ENGINE START RECEIVED AN EICAS MESSAGE FOR IDLE DISAGREE. REMOVED AND REPLACED THE M644 CARD IAW AMM 73-21-11. OPS CHECKED OK.

ATA 7320

AFTER LANDING, AN IDLE DISAGREE MESSAGE ILLUMINATED. THE RT ADC WAS REPLACED, NO DEFECT NOTED AFTER PERFORMED 30 TEST.

ATA 7510

RIGHT ENGINE NOSE ANTI-ICE VALVE SLOW TO CLOSE. REMOVED AND REPLACED THE RT INLET ANTI-ICE VALVE IAWAMM 30-21-03, RAN ENGINE, OPS AND LEAK CHECKED GOOD.

ATA 3350

EMERGENCY LIGHT FOUND BROKEN, LENS WILL NOT STAY ON. SECURED THE LENS AT SEAT 19L IAW AMM 20-60-00, OPS CHECKED GOOD.

ATA 2822

LEFT FWD BOOST PUMP PRESSURE LIGHT WILL NOT GO OUT. : R & R THE LEFT FWD BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-01, LEAK AND OPS CHECKED GOOD,

ATA 7510

RT ENGINE ANTI-ICE VALVE SLOW TO CYCLE. PERFORMED OPS CHECKED THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED GOOD IAW AMM 30-21-03.

ATA 7510

EICAS MESSAGE FOR THE ENGINE ANTI-ICE SYSTEM. PERFORMED OPS CHECK OF THE RT ENGINE ANTI-ICE VALVE, OPS CHECKED OK IAW AMM 30-21-03.

ATA 2822

LEFT FWD BOOST PUMP PRESSURE LIGHT WILL NOT GO OUT. OPEN

ATA 3417

IDLE DISAGREE MESSAGE AT DEPARTURE. REMOVED AND REPLACED THE LT ADC IAW AMM 34-12-01, OPS CHECK GOOD IAW AMM 34-12-01

ATA 7830

IDLE DISAGREE AFTER THRUST REVERSER STOWED. R & R THE RT ENG INBD THRUST REVERSER CDU POSITION TRANSDUCER IAW AMM 78-31-24, OPS CHECKED GOOD

ATA 7200

IDLE DISAGREE DURING DEPARTURE.

ATA 7230

RIGHT ENGINE SHOWED A FAN VIBRATION UP TO 5 DURING TAKEOFF. REMOVED AND REPLACED THE NR 2 ENGINE 5 AND 6 BLADES IAW AMM 72-31-02.

ATA 7200

NR 2 ENGINE BLADES 5 AND 6 ARE DAMAGED. R & R THE BLADES. OPS CHECKED NORMAL IAW AMM 72-31-02.

ATA 7230

DURING TAKEOFF, A 4.9 VIBRATION ON FAN. REMOVED AND REPLACED THE NR 3 FAN BLADE IAW AMM 72-31-02 , TRIMMED VIBRATION IAW AMM 72-31-00, TRIM NOW 1.0 AT TAKEOFF, FAN LUBE COMPLIED WITH.

ATA 4920

APU BLEED SURGES, VALVE FILTER SPRING IS DAMAGED. R & R APU BLEED SURGE VALVE SPRING. OPS CHECKED NORMAL AND NO LEAKS IAW AMM 49-53-06.

ATA 7320

IDLE DISAGREE MESSAGE, AT FLT IDLE AFTER STOWING THE THRUST REVERSER. R & R THE HMU IAW AMM 73-21-14. OPS CHECKED NORMAL IAW AMM 71-00-00.

ATA 7230

NR 2 ENGINE, ONE HPC STAGE 1 BLADE WITH A L/E DENT AND CRACK. BORO BLENDED REPAIR TO THE BLADE IAW AMM 72-00-00.

ATA 5410

NR 1 ENGINE INBD LOCKOUT PLATE HAS A SHEARED BOLT. R & R THE BOLT IAW AMM 51-40-02.

ATA 7320

IDLE DISAGREE EICAS MESSAGE ON LANDING. RT PIMU HAS A DISAGREE MESSAGE ON BOTH A & B CHANNELS. REMOVED AND REPLACED THE HMU. TESTED 3,2,6 AND 7 IAW AMM 71-00-00, CHECKED OK.

ATA 7321

CAUTION MSG IDLE DISAGREE AFTER LANDED RIGHT ENGINE 34.7 N1 LEFT ENGINE 25.5 N1. REMOVED AND REPLACED EEC DISCRETE PRINTED CIRCUIT CARD IAW AMM 73-21-12.

ATA 7200

LEFT ENGINE VIBRATION, 5.0 DURING CLIMB. ADJUSTED THE NR 1 ENGINE FAN TRIM BALANCE USING EXTERNAL ANALYZER IAW AMM 72-31-00/501.

ATA 7320

RIGHT ENGINE IDLE DISAGREE ILLUMINATED AFTER LANDING. REMOVED AND REPLACED THE RT ENGINE REVERSE RELAYS IAW WDM 73-21-19 & 77-35-11 , OPERATED THE ENGINE IAW AMM 71-00-00, OPS CHECKED GOOD, AIRCRAFT OK FOR SERVICE.

ATA 3350

SEATS 37J, 32C, FWD OF 19D, EMERGENCY LIGHT LENSES ARE MISSING. REPLACED EMERGENCY LIGHTS LENSES IAW MM 33-53-00.

ATA 3350

FLOOR EMERGENCY LIGHT INOPERATIVE. PINNED THE LIGHTS IAW AMM 33-51-10, OPS CHECKED OK.

ATA 2822

LEFT ENGINE SPAR LIGHT VALVE VERY SLOW TO EXTINGUISH IN START AND SHUTDOWN. REMOVED AND REPLACED FUEL SHUTOFF VALVE ACTUATOR IAW MM 28-22-11, OPS CHECKED OK.

ATA 7300

IDLE DISAGREE ON LANDING AFTER REVERSER DEPLOYMENT. REVERSER STOWED NORMALLY. NR 1 IDLE N1 AT 25.5%, NR 2 IDLE 34.8%. REMOVED AND REPLACED THE AIR GROUND RELAY K207 IAW AMM 32-09-02, AND THE RT IDLE SOLENOID RELAY K433 IAW AMM 20-81-00 , RAN ENGINE, OPS CHECKED OK IAW AMM 71-00-00.

ATA 7830

IDLE DISAGREE EICAS CAUTION DURING LANDING. REPLACED THE RIGHT ENGINE THRUST REVERSER INBD ELECTRO MECHANICAL BREAK LOCK IAW AMM 78-34-07. OPS CHECKED NORMAL.

ATA 2823

LEFT ENGINE SPAR LIGHT VALVE VERY SLOW TO EXTINGUISH IN START OR SHUTDOWN. REMOVED AND REPLACED THE LEFT ENGINE FUEL SHUTOFF VALVE ACTUATOR IAW AMM 28-22-11. OPS CHECKED OK.

ATA 8012

LEFT STARTER CUTOUT CAUTION MESSAGE AT 18,000 FT DURING CLIMB. COMPLIED WITH THE QRH, THE MESSAGE REMAINED. REMOVED AND REPLACED THE LEFT ENGINE START VALVE IAW AMM 80-11-02. OPS AND LEAK CHECKED GOOD.

ATA 3350

LT FUSELAGE AFT OF LEFT WING EMERG LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-51-16.

ATA 3350

L4 EXT EMERGENCY LIGHT INOP. REMOVED AND REPLACED EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-16 OPS CHECK OK.

ATA 2822

EICAS MESSAGE FOR THE LT FWD FUEL PUMP. PERFORMED A PUMP TEST IAW AMM 28-22-00-215-018. TESTED OK. NO OTHER FAULTS NOTED.

ATA 2841

EICAS MESSAGE FOR INTERMITTANT FUEL CONFIGURATION LEFT FUEL GAUGE BLANKED, THEN READ 3000 LBS HIGH BEFORE RETURNS TO NORMAL STATUS MESSAGE. FUEL QTY CHANNEL. PERFORMED TASK 24-41 TREE 837, TESTED OK. PERFORMED QUANTITY TEST IAW AMM 28-41-00-715-031-001. TESTED OK. NO OTHER FAULTS.

ATA 3350

LEFT SIDE EXTERIOR EMERGENCY LIGHT, LEFT WING SLIDE INOPERATIVE. PERFORMED A CHECK OF EXTERIOR EMERGENCY LIGHTS. OPS CHECKED OK. IAW AMM 33-51-06.

ATA 5610

R2 SLIDING WINDOW ARCING, IN THE AFT LOWER CORNER. REMOVED AND REPLACED THE R2 SLIDING WINDOW IAW AMM 56-11-03.

ATA 3350

RT ISLE OVERHEAD EMERGENCY LIGHT LENS MISSING AT ROW 12. INSTALLED THE LENS IAW AMM 33-21-00.

ATA 3610

AFTER LANDING, A LT ENGINE BLEED OFF MESSAGE ACTIVATED. PERFORMED AN AIR SUPPLY BITE IAW 36-20-00, NO FAULTS. OPERATED LEFT ENGINE IAW 71-01-02, BLEEDS OPS CHECKED GOOD.

ATA 7200

AFTER ENGINE START , IDLE DISAGREE EICAS MESSAGE. REMOVED AND REPLACED ECU. OPS CHECKED NORMAL IAW AMM 73-21-15.

ATA 7320

RT ENGINE GOING TO FLT IDLE AFTER START. REMOVED AND REPLACED THE IDLE RELAY K433 IAW WDM 20-60-04. ENGINE RUNS CARRIED OUT IAW AMM 71-01-02, OPS CHECKED NORMAL.

ATA 2822

AFTER FUEL XFEED L - R , RE-SELECTED R PUMPS ON, XFEED ON , EICAS R AFT FUEL PUMP W/ PRESS LT IN SWITCH&NBSP;(<P>REMOVED AND REPLACED RH AFT MAIN BOOST PUMP AS PER AMM 28-22-03 OPS CHECK GOOD, NO FURTHER DEFECTS NOTED&NBSP;</P>)

ATA 7320

AFTER TOUCH DOWN, THE RT ENGINE REMAINED IN HIGH IDLE, N1 34%, N2 75% AND RECEIVED IDLE DISAGREE MESSAGE, INSPECTED ,CLEANED AND INSTALLED THE RELAY K433 IAW AMM 20-60-04. ENGINE RUNS IAW AMM 71-01-02. CHECKED NORMAL.

ATA 7200

DURING THE NR 2 ENGINE START, THE ENGINE ADVANCED TO 35 PERCENT N1 AND 74 PERCENT N2 ON ITS OWN AND RECEIVED IDLE DISAGREE EICAS. TROUBLESHOT IAW FIM 71-05 F/T 844. PERFORMED ENGINE RUNS IAW AMM 71-01-02. INDICATIONS NORMAL, OK FOR SERVICE.

ATA 3442

WEATHER RADAR TILT NOT WORKING CORRECTLY. PERFORMED A WEATHER RADAR SYSTEM TEST IAW AMM 34-43-00, OPS CHECKED NORMAL.

ATA 3442

TILT IS OFF ON RADAR. AT 7000 FT, ZERO TILT, GOOD WEATHER PICTURE. AT FL 380, -1 TILT NO WEATHER RADAR PRINTED. PERFORMED A WEATHER RADAR ADJUSTMENT TEST IAW AMM 34-43-00-501, OPS NORMAL, CHECKED GOOD.

ATA 3350

EMERGENCY LIGHTS INOPERATIVE AT ROW 1. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM 33-51-10, OPS CHECKED GOOD. OK FOR SERVICE.

ATA 2421

RT GENERATOR CONTROL TRIPPED AFTER ENGINE START, RESET IAW QRH OPS NORMAL. PERFORMED AN OPS TEST FOR RIGHT IDG IAW AMM 24-11-00-715-006, OPS CHECKED GOOD.

ATA 3150

IDLE DISAGREE EICAS CAME ON DURING LANDING. SELF EXTINGUISH DURING TAXI. OPS CHECKED NORMAL IAW FIM 71-05-844.

ATA 3030

FIRST OFFICER`S PITOT HEAT INOPERATIVE. REMOVED AND REPLACED THE PITOT TUBE IAW AMM 34011-01, OPS AND LEAK CHECKED GOOD IAW 34-11-00-501, NO LEAKS NOTED.

ATA 3150

IDLE DISAGREE EICAS MESSAGE ON LANDING. IAW AMM 77-12-00 NO FAULTS NOTED.

ATA 3442

LEFT WEATHER RADAR DURING DESCENT, PAINTED A 15 MILE ARC DURING NUMEROUS HEADING CHANGES , DID NOT TRY THE RT RADAR. PERFORMED A WEATHER RADAR TEST IAW AMM 34-43-00, OPS CHECKED GOOD ON GROUND.

ATA 2822

RT AFT FUEL PUMP EICAS MESSAGE. REMOVED AND REPLACED RIGHT AFT FUEL PUMP PRESSURE SWITCH IAW AMM 28-42-01. OPS CHECKED GOOD, NO LEAKS NOTED.

ATA 2565

OVERWING SQUIBS WILL NOT TEST. DISARMED AND REARMED THE OVERWING ESCAPE SYSTEM IAW AMM 25-65-00. OPS CHECKED GOOD.

ATA 3610

RIGHT ENGINE IDG OUT TEMP MAINTENANCE MESSAGE. REMOVED AND REPLACED THE NR 2 ENGINE AIR SHUTOFF VALVE IAW AMM 24-11-07, OPS CHECKED GOOD.

ATA 7200

IDLE DISAGREE EICAS MESSAGE ON LANDING. RAN FIM 22-03 F/T'S 803 & 810, TESTS 2 & 10 ON MCDP. OPS CHECKED NORMAL.

ATA 2150

LEFT DUCT LEAK AFTER LANDING. REMOVED AND REPLACED THE SECONDARY HEAT EXCHANGER. LEFT SIDE IAW AMM 21-51-02. NO LEAKS, OPS CHECKED NORMAL.

ATA 2421

RIGHT ENGINE IDG OUT TEMP. RT ENG READING HIGH. PERFORMED 24-26 FAULT TREE 807, OUT TEMP DISPLAY. NO FAULT ON WIRING NOTED. RESISTANCE CHECKED WITHIN LIMITS. OPS CHECKED NORMAL.

ATA 2421

IDG OUT TEMP MTC MESSAGE, RT ENGINE READING HIGH. CONFIRMED IDG SERVICING IAW AMM 12-13-03, COMPLIED WITH FIM 24-20 FT 807, NO FAULTS NOTED, IDG OK FOR SERVICE.

ATA 2160

FWD CARGO HEAT OV/HEAT INOP. R&R SWITCH ASSY FOR FWD CARGO HEAT, OPS CKD GOOD PER AMM 33-13-00.

ATA 4990

APU HAS AN OIL LEAK, FOUND ON POST ACFT POSITIONING WALK AROUND. R & R THE OIL PRESSURE SWITCH IAW AMM 49-94-02, LEAK CHECKED GOOD.

ATA 4990

OIL LEAK FROM THE APU. R & R THE OIL PRESSURE SWITCH, OPS CHECKED GOOD, LEAK CHECKED GOOD IAW AMM 49-94-02.

ATA 2150

RIGHT PACK OFF LIGHT WITH ALL OTHER PARAMETERS NORMAL AND PACK RUNNING. REPLACED THE RIGHT PACK FLOW CONTROL VALVE IAW AMM 21-51-01. OPS CHECKED NORMAL.

ATA 2421

RIGHT GENERATOR DRIVE EICAS MESSAGE ILLUMINATED AFTER RIGHT ENGINE START AND STAYS ON FOR 2 TO 3 MINUTES. REMOVED AND REPLACED THE RIGHT IDG IAW AMM 24-11-01, ENGINE RUN AND GENERATOR GROUND OPERATIONS NORMAL.

ATA 2150

RIGHT PACK OFF LIGHT ILLUMINATED. REMOVED AND REPLACED THE RT PACK FLOW CONTROL CARD IAW AMM 21-51-09. OPS CHECKED GOOD.

ATA 2150

RIGHT A/C PACK OFF MESSAGE. A/C PACK RESET & BITE TEST CARRIED OUT IAW AMM 21-51-00. NO ACTIVE MESSAGES, OK FOR SERVICE.

ATA 4900

APU FAILED ON START FIRST ATTEMPT, APU DOOR STATUS MESSAGE. REMOVED AND REPLACED THE AIR INTAKE DOOR ACTUATOR IAW AMM 49-15-06. OPS CHECKED GOOD. NO DEFECTS NOTED.

ATA 3610

RIGHT DUCT LEAK AND ASSOCIATED EICAS MESSAGE DISPLAYED WHEN PARKED ON RAMP , QRH PROCEDURE COMPLIED WITH. FOUND LOOSE CLAMP ON THE RT ISOLATION VALVE , TIGHTEN THE CLAMP IAW AMM 36-11-04, OPS CHECKED SATISFACTORY, NO FURTHER MESSAGES.

ATA 3150

APU DOOR MESSAGE SELF ERASED AFTER RESET OF CIRCUIT BREAKER AND BITE TEST OF ECU IAW AMM 49-61-05. OPS CHECKED GOOD.

ATA 4920

APU FAILED TO START, 2 ATTEMPTS. APU DOOR STATUS MESSAGE. RESET DOOR INLET CIRCUIT BREAKER & BITE TESTED THE APU ECU IAW AMM 49-61-05. OPS CHECKED SATISFACTORY.

ATA 4997

APU WOULD NOT START AFTER FLIGHT , APU DOOR STATUS MESSAGE. FOUND APU DOOR CIRCUIT BREAKER TRIPPED, RESET, STARTED APU SEVERAL TIMES AND CHECKED GOOD IAW AMM 49-41-00</P>)

ATA 5247

WHILE ATTEMPTING TO START APU. APU DOOR ACTUATOR CIRCUIT BREAKER TRIPPED. R & R APU DOOR ACTUATOR IAW AMM 49-15-06, OPS CHECKED GOOD.

ATA 2150

RIGHT PACK OFF MESSAGE. RT PACK RESET & A BITE TEST WAS CARRIED OUT IAW AMM 21-51-01. NO ACTIVE MESSAGES, OK FOR SERVICE.

ATA 3610

RIGHT BLEED ISLN VAL EICAS CAUTION MSG WHILE STILL ON THE BLOCK. REMOVED AND REPLACED RIGHT ISOLATION VALVE IAW AMM 36-11-04. OPS AND LEAK CHECK GOOD.

ATA 3040

EICAS MESSAGE FOR THE L2 SIDE WINDOW. QRH PROCEDURES ACCOMPLISHED. REMOVED AND REPLACED LT WINDOW HEAT CONTROLLER IAW AMM 30-41-01, OPS CHECKED GOOD.

ATA 3040

EICAS MESSAGE FOR THE LT SIDE WINDOW DISPLAYED. ACCOMPLISHED QRH. PERFORMED FIM 30-41 FT 804 AND BITE TEST. HEAT CONTROLLES. NO FAULTS NOTED. WINDOW HEAT OK.

ATA 2421

RIGHT GENERATOR DRIVE LIGHT AND EICAS MESSAGE ILLUMINATED AND SHOWN APPROX FOR 90 SECONDS AFTER ENGINE START. SERVICED THE RT IDG OIL IAW AMM 12-13-03, NO DISCREPANCIES NOTED.

ATA 4900

APU SHUTDOWN UNCOMMANDED ON RAMP. PERFORMED BITE TEST OF APU CONTROL UNIT IAW AMM 49-61-05, 49-61-05-742-027. NO FAULTS FOUND.

ATA 2820

LEFT ENGINE SPAR VALVE LIGHT INOPERATIVE.

ATA 3040

LEFT SIDE WINDOW EICAS. PERFORMED FIM 30-41 FT 804 &. CHECKED WINDOW HEAT CONTROLLER, NO FAULT NOTED. OPS CHECKED OK.

ATA 2421

REMOVED AND REPLACED RT GENERATOR CONTROL UNIT IAW AMM 24-22-02 OPS CHECK GOOD IAW AMM 71-00-00 NO FUTHER DEFECT NOTED AT THIS TIME.

ATA 3040

LEFT SIDE WINDOW EICAS MESSAGE DISPLAYED. ACCOMPLISHED QRH, PERFORMED FIM 30-41 FT 804, TASK 802, SWAPPED LT WINDOW NR 3 TO SPARE SENSOR IAW AMM 30-41-00, OPS CHECKED NORMAL AT THIS TIME.

ATA 3040

LEFT SIDE WINDOW EICAS MESSAGE. ACCOMPLISHED QRH. PERFORMED BITE ON THE WINDOW HEAT CONTROLLER, NO FAULTS. WINDOW HEAT CHECKED NORMAL IAW AMM 30-41-01.

ATA 3040

LEFT SIDE WINDOW CAUTION MESSAGE ON EICAS DURING FLIGHT. WINDOW HEAT CONTROL UNIT BITE TEST CARRIED OUT IAW AMM 30-41-01, NO FAULTS, OK FOR SERVICE.

ATA 2421

RIGHT GENERATOR DRIVE EICAS MESSAGE, AFTER START. EXTINGUISHED IN 60 SECONDS. PERFORMED A RT IDG OIL SERVICING IAW AMM TASK 12-13-03-613-027.

ATA 2822

RT AFT FUEL PUMP MESSAGE DURING FLIGHT, COMPLIED WITH QRH. PERFORMED SYSTEM TEST IAW FIM 28-22-820. NO FAULTS NOTED. OK FOR SERVICE.

ATA 2822

R AFT FUEL PUMP MSG INFLIGHT C/W QRH, PERFORMED SYSTEM TEST & IAW AMM 28-22-820. NO FAULTS NOTED OK FOR SERVICES.

ATA 4920

APU SHUTDOWN WITH A FAULT INDICATION AFTER BLOCK IN. RESTART NORMAL. PERFORMED APU BITE IAW AMM 49-61-05, NO FAULTS INDICATED. PERFORMED START IAW AMM 49-11-00.

ATA 2613

DURING CLIMB OUT, THE FWD EQUIPMENT OVERHEAT EICAS MESSAGE ACTIVATED. COMPLETED QRH, MESSAGE DID NOT ILLUMINATE AGAIN. RETURNED EQUIPMENT COOLING SWITCH TO AUTO AND COMPLIED WITH SYSTEM OPS CHECK IAW AMM 21-58-00, NO FAULTS INDICATED.

ATA 2421

RIGHT ENGINE IDG OUT TEMP MAINTENANCE MESSAGE. PERFORMED FIM 24-20 FAULT TREE 807, FOUND IDG AIR/OIL COOLER VALVE TO BE FAULTY, REMOVED AND REPLACED AIR/OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24-11-07. OPS CHECKED NORMAL

ATA 4950

APU SURGE VALVE FILTER ELEMENT SPRING MISSING. INSTALLED THE SPRING IAW AMM 49-53-06.

ATA 2421

MESSAGE FOR THE IDG OUT TEMP RT ENG. REMOVED AND REPLACED THE IDG IAW AMM 24-11-01. OPS CHECKED NORMAL.

ATA 3610

RIGHT ISOLATION VALVE INOPERATIVE. REMOVED AND REPLACED THE ISOLATION VALVE. OPS CHECKED NORMAL, NO LEAKS IAW AMM 36-11-04.

ATA 3350

RIGHT UPPER CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-05.

ATA 3397

LEFT ROW 4-9 EMERGENCY LIGHT INOPERATIVE. INSTALLED THE CONNECTORS IAW AMM 33-51-10. OPS CHECKED NORMAL.

ATA 2150

MESSAGE FOR THE LT PACK BITE. REMOVED AND REPLACED THE LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECKED NORMAL.

ATA 2421

MAINTENANCE MESSAGE FOR RT IDG OUT TEMP. CHECKED SERVICING OF IDG IAW AMM 12-12-03. CHECKED GOOD. CLEARED MAINTENANCE MESSAGE, NO FILTER BYPASS BUTTON POPPED.

ATA 3610

RIGHT ISOLATION VALVE FAILED. R&R RT ISOLATION VALVE, OPS CHECK NORMAL, NO LEAKS IAW AMM 36-11-04.

ATA 5410

DURING PRE-FLIGHT, MULTIPLE ENGINE COWL RIVETS LOOSE IN THE NR 1 ENGINE. REMOVED AND REPLACED THE RIVETS IAW SRM 51-40-02-0G-0, AND CMM 71-11-16, FIG 1. LT NOSE COWL RIVETS SMOOTH AND SECURE ACFT RELEASE TO CONTINUE SERVICE.

ATA 3350

EMERGENCY LIGHT INOPERATIVE AT THE RT EMERGENCY ESCAPE HATCH AND AT SEAT 1J. REMOVED AND REPLACED EMERGENCY LIGHT ASSY IAW AMM 33-51-05, OPS CHECKED GOOD.

ATA 5210

FOUND THE L4 DOOR OPEN HANDLE LOOSE AND CANNOT OPEN DOOR. SECURED THE DOOR HANDLE MECHANISM IAW AMM 52-11-25-402-012. OPS CHECKED GOOD.

ATA 8012

LEFT ENGINE START VALVE DID NOT OPEN R & R THE LT ENGINE START VALVE ASSY IAW AMM 80-11-02. OPS CHECKED GOOD.

ATA 2150

FWD EQUIPMENT OVERHEAT EICAS MESSAGE AND DISCRETE MESSAGE. COMPLIED WITH EQUIPMENT COOLING OPERATIONAL CHECK IAW AMM 21-58-00. EQUIPMENT COOLING CHECKED NORMAL.

ATA 2841

STATUS MESSAGE FOR FUEL QTY CHANNEL. COMPLIED WITH FQIS BITE IAW AMM 28-41-00, NO FAULTS, SYS OK FOR SERVICE.

ATA 2421

INTERMITTENT RT IDG OUT TEMP. REMOVED AND REPLACED THE RT ENG IDG FILTER ASSY IAWAMM 24-11-02, OPS CHECKED & LEAK CHECKED GOOD IAW AMM 24-11-02.

ATA 7932

RIGHT ENGINE OIL LEVEL READING OFF SCALE. REMOVED AND REPLACED OIL LEVEL TRANSMITTER IAW AMM 79-31-01/401. OPS AND LEAK CHECKED OK.

ATA 3610

RT ENGINE BLEED AIR SWITCH DOES NOT POP OUT COMPLETELY WHEN TURNED OFF. REMOVED AND REPLACED THE SWITCH IAW SWPM 20-84-14. OPS CHECKED GOOD.

ATA 2913

RIGHT PRIMARY HYD PUMP EICAS MESSAGE CAME ON IN FLIGHT. TROUBLESHOT IAW FIM 29-11. ALL OPS CHECKS NORMAL. INSPECTED PRESSURE SWITCH CONNECTOR IAW AMM 29-11-17, CONNECTOR IS CLEAN NO CORROSION PRESENT. ACFT OK FOR SERVICE.

ATA 7731

ON CLIMB OUT LT ENG VIBRATION INDICATOR FAN 4.1. INSTALLED ALT ACCELEROMETER IAW AMM 77-31-01. ACCOMPLISHED FAN LUBE IAW AMM 72-31-02. ENG RUN IAW AMM 71-00-00 FAN VIBRATION CHECKED GOOD.

ATA 2421

ATER LANDING, STATUS MESSAGE FOR RT IDG OUT TEMP. TROUBLESHOT IAW FIM 24-20, FOUND RT IDG OVERSERVICED. CORRECTED IAW AMM 12-13-03.

ATA 4990

APU OIL PRESSURE SWITCH LEAKING. REMOVED AND REPLACED APU OIL PRESSURE SWITCH IAW AMM 49-94-02. RAN APU, NO LEAKS DETECTED.

ATA 4990

APU LOW OIL PRESSURE SWITCH LEAKING. REMOVED & REPLACED THE OIL PRESSURE SWITCH ASSY IAW AMM 49-94-02, OPS & LEAK CHECKED GOOD.

ATA 3350

RIGHT SLIDE GROUND LIGHTS INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW 33-51-06902-082. OPS CHECKED GOOD.

ATA 3350

L1 EXTERIOR DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE FUSE ON THE BATTERY PACK M736 AT BS 467 IAW WPM 33-51-25. OP CHECKED GOOD IAW AMM 33-51-07-422-012.

ATA 3397

PASSENGER CABIN FLOOR EMERGENCY LIGHTING INOPERATIVE AT SEAT ROW 1 LT AND RT. CLEANED AND SECURED EMERGENCY POWER SUPPLY UNIT ELECTRICAL CONNECTOR IAW SWPM 20-60-01 SECURED OPEN CONTACT FOUND AT SEAT 2JL IAW WDM 33-51-16. OPS CHECKED GOOD.

ATA 3350

PASSENGER CABIN DOOR EMERGENCY LIGHT INOPERATIVE AT DOOR 2L, 2R, AND 39JL. TROUBLESHOT, AND REPLACED THE LAMPS. OPS CHECKED GOOD IAW WDM 33-51-12.

ATA 3397

PASSENGER CABIN FLOOR EMERGENCY LIGHTING INOPERATIVE AT SEAT ROWS 4 THRU 10 LT AND RT. CLEANED AND SECURED EMERGENCY POWER SUPPLY UNIT NR 1 ELECTRICAL CONNECTOR, SECURED OPEN CONTACT AT SEAT 4, OPS CHECKED GOOD IAW SWPM 20-60-01, AND WDM 33-51-18.

ATA 2160

PER CREW REPORT COCKPIT TRIM AIR VALVE HAS FAILED MULIPLE TIMES AND THEN STARTED WORKING AGAIN ON LAST FEW LEGS. REMOVED AND REPLACED FLT DECK ZONE TRIM AIR MODULATING VALVE IAW AMM 21-61-07 OPS CHECKED NORMAL.

ATA 3442

LEFT WX RADAR SYSTEM FAILED. LEFT WX RADAR SYSTEM TEST & CARRIED OUT IAW AMM 34-43-00. TEST PASSED, OK FOR SERVICES.

ATA 2820

ON STARTING THE RT ENGINE SPAR VALVE FAILED OPS CHECK IAW AMM 28-21-02.

ATA 3150

RIGHT PIMU MAINTENANCE MESSAGE. TROUBLESHOOTING SHOWS CODE 353-224. PERFORMED FIM 71-01-43. SYSTEM CHECKED NORMAL.

ATA 7510

RIGHT ENGINE NACELLE ANTI-ICE VALVE IS VERY SLOW TO INDICATE OPEN IN COLD WEATHER. REMOVED AND REPLACED THE ANTI-ICE VALVE. OPS CHECKED GOOD IAW AMM 30-21-03.

ATA 3150

RIGHT PIMU MAINTENANCE MESSAGE. TROUBLESHOOTING SHOWS CODE 353-224. PERFORMED FIM 71-01-43 & SYSTEM OPS NORMAL.

ATA 7320

STATUS MESSAGE EICAS DISAGREE DISPLAYED. DURING TROUBLESHOOTING, FOUND CODE 514 N1 LEFT, CODE 516 N2 LEFT, LT ENGINE HIGH OIL TEMP, SUSPECT LT ENGINE EEC FAILED. REMOVED & REPLACED THE EEC.

ATA 3610

RIGHT ENGINE BLEED AIR SWITCH, MECHANICAL FLOW BAR INDICATOR STICKS IN THE ON POSITION. VERIFIED THE RT ENGINE BLEED SWITCH OPS NORMAL IAW AMM 36-11-26.

ATA 3000

RT ENGINE ANTI-ICE VALVE LIGHT INOPERATIVE. REMOVED AND REPLACED THE ANTI-ICE LIGHT ASSY. IAW AMM 33-11-00. OPS CHECKED NORMAL.

ATA 3020

RT ENG ANTI-ICE VALVE ILLUMINATED AFTER ENGINE START WITH SWITCH ON. OPERATED SEVERAL TIMES DURING FLIGHT OPS, CHECKED OK. PERFORMED GROUND TEST IAW AMM 30-21-03. CHECKED GOOD.

ATA 3610

AIR LEAK IN LEFT MLG WW. FOUND DUCT BELOW CENTERT ISOLATION VALVE CRACKED. REMOVED AND REPLACED THE DUCT ASSY IAW AMM 36-11-01. NO LEAKS NOTED.

ATA 2150

MTC MESSAGE RT PACK BITE. CONTROLLER FAULTED RT PACK LOW CONTROL VALVE, REPLACED LOW LIMIT VALVE REF AMM 21-51-11, OPS CHECK OK.

ATA 2820

LEFT SPAR VALVE FAILED ON ENGINE SHUT DOWN. TROUBLESHOT IAW FIM 28-22 14, R & R THE LT SPAR VALVE LIGHT DIODE, FUSE CARD IAW AMM 33-16-02. OPS CHECKED OK.

ATA 3010

EICAS MESSAGE FOR RT ENGINE ANTI-ICE, QRH PROCEDURE PERFORMED. CONFIRMED VALVE OPERATION IAW AMM 30-21-03. REMOVED AND REPLACED THE RT ENGINE TAI VALVE IAW AMM 30-21-03. LEAK AND OPS CHECKED, NDICATIONS NORMAL.

ATA 4990

ON POST FLIGHT WALK AROUND, FOUND OIL DRIPPING FROM APU COWLING. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH IAW AMM 49-94-02. NO LEAKS NOTED.

ATA 2131

LEFT PACK TEMP CONTROL FAULT. R & R THE A/C PACK CONTROLLER. OPS CHECKED GOOD IAW AMM 21-51-14.

ATA 2131

RIGHT PACK TEMP CONTROL FAULT. REMOVED AND REPLACED THE RIGHT A/C PACK CONTROLLER ASSY IAW AMM 21-51-14. OPS CHECKED NORMAL.

ATA 2150

ECS MESSAGE LT PACK. REMOVED AND REPLACED LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS & BITE CHECKED GOOD .

ATA 2150

LEFT PACK TEMP EICAS MESSAGE. PERFORMED BITE ON LT PACK CONTROLLER IAW FIM 21-51 FT 803. FAULTED LT PACK TEMP CONTROL VALVE. RESET LT PACK CONTROLLER PERFORMED BITE PREOCEDURE A SECOND TIME. NO CURRENT FAULTS NOTED. NO EICAS MSGE PRESENT. ACFT OK FOR SERVICE.

ATA 2120

UNABLE TO CLEAR AIR SUPPLY BITE MODULE FAULTS. REMOVED AND REPLACED AIR SUPPLY BITE MODULE.

ATA 3350

LEFT AND RIGHT OVERWING EMERGENCY LIGHTS FOUND INOPERATIVE. REPLACED THE LAMPS, CLEANED AND REPLACED THE POWER SUPPLY. OPS CHECKED GOOD.

ATA 3350

EMERGENCY LIGHTS INOPERATIVE. REPLACED THE LAMPS, CONNECTED THE CONNECTOR FOR SEATS 4-9CA, REMOVED AND REPLACED THE INVERTER, REMOVED AND REPLACED AFT GALLEY EMERGENCY LIGHT ASSY.

ATA 2897

RIGHT FUEL JETTISON PUMP CIRCUIT BREAKER (C376) ON P37 BROKEN. REMOVED AN REPLACED THE CIRCUIT BREAKER.

ATA 2822

RIGHT FWD BOOST PUMP PRESS LIGHT INDICATION ON PUSH BUTTON SWITCH FAILED TO COME ON WITH GFI TRIPPED. REMOVED AND REPLACED TIME DELAY RELAY (K-5) ON FUEL CONTROL PANEL FOR RIGHT FWD BOOST PUMP PRESS LIGHT INDICATION.

ATA 5280

ON POST FLIGHT INSPECTION FOUND PANEL 651VB BROKEN, MLG STRUT DOOR BOLT MISSING & MLG TRUNNION DOOR & LEADING EDGE DAMAGED. PERFORMED TEMP REPAIRS PER EO 6757A120 & EO 6752A038. REMOVED STRUT DOOR PER CDL 32-12-01.

ATA 2841

AFTER TAKE OFF FUEL QTY WAS ERRATIC THEN SETTLED AFTER LEVEL OUT. TROUBLESHOT IAW FIM. FAULTED PROCESSOR REMOVED AND REPLACED IAW AMM 28-41-08 OPS CHECK AND BITE CHECKED NORMAL.

ATA 3350

EMERGENCY LIGHT COVER AT SEAT 38J IS MISSING. REPLACED THE EMERGENCY LIGHT COVERS IAW MM 25-27-09.

ATA 4900

APU SHUTDOWN. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. OPS CHECKED NORMAL.

ATA 2150

RIGHT PACK COMPRESSOR OUTLET TEMP INDICATION BLANK. R & R RT PACK COMPRESSOR OUTLET TEMP BULB. OPS CHECK GOOD IAW AMM 21-52-01.

ATA 4920

APU OIL QTY MESSAGE ON STATUS PAGE. OIL FOUND IN TAIL PIPE. TRANSFERRED TO DMI; MDDR 69791 IAW MEL 49-11-01B, CAT B. REMOVED AND REPLACED APU IAW WORK CARD T1071 AMM 49-11-01.

ATA 7200

LEFT ENGINE COMPRESSOR STALLS WITH HEAVY YAW APPROX 13000-14000. REDUCED THRUST TO IDLE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED THE ENGINE, OPS CHECKED OK. ACFT RELEASED FOR SERVICE.

ATA 5210

L4 DOOR OPENING HANDLE LOOSE WHEN CLOSED. REPLACED THE HANDLE WORN BUSHING IAW AMM 52-11-25. NO RIGGING WAS REQUIRED. DOOR HANDLE OPERATED NORMAL.

ATA 2560

MAIN CABIN R4 PBE DAMAGED. REMOVED AND REPLACED PBE MASK IAW AMM 25-60-00.

ATA 2562

MAIN CABIN ROW 20 LIFE RAFT PRESSURE GAUGE READS LOW. REMOVED THE RAFT ASSY. ROUTED TO VENDER FOR SERVICE IAW AMM 25-05-03. REINSTALLED RAFT ASSY.

ATA 3350

MAIN CABIN ROW 32 FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-00, OPS CHECKED OK.

ATA 3350

MAIN CABIN LEFT EMERGENCY LIGHT BETWEEN ROW 39 AND AFT GALLEY FLOOR LIGHT INOPERATIVE. REMOVED AND REPLACED THE LIGHTS IAW AMM 33-53-00 OPS CHECKED OK.

ATA 3397

RIGHT ROW 40 FLOOR EMERGENCY LIGHTS INOPERATIVE. FOUND LOOSE CONNECTOR ROW 40. CLEANED AND RESET CONNECTOR. EMERGENCY LIGHTS OPS OK. IAW SSM 33-51-01.

ATA 3350

MAIN CABIN ROW 9 RIGHT FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT IAW AMM 33-53-00. OPS CHECKED OK.

ATA 3350

MAIN CABIN ROW 31 FLOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-53-00. OPS CHECKED OK.

ATA 3350

MAIN CABIN EMERGENCY LIGHT ROW 5 LT AISLE CEILING INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT.

ATA 2840

AFTER LANDING STATUS MESSAGE FUEL QTY CHANNEL. FQIS PROCESSOR BITE TEST CARRIED OUT IAW AMM 28-41-00, ALL TESTS PASSED, MESSAGE ERASED.

ATA 2150

RIGHT PACK BAY AIR LEAK ABOVE RE-HEATER CONTROLLER. REPLACED THE SEALS. LEAK CHECKED OK IAW MM 21-51-00.

ATA 2421

ON POST FLIGHT WALK AROUND, FOUND RT ENG IDG FILTER DP BUTTOM POPPED. REPLACED THE FILTER IAW MM 24-11-02.

ATA 3610

RIGHT BLEED DUCT LEAKING. PERFORMED OPS CHECK OF AIR SUPPLY SYSTEM. SYSTEM CHECKED NORMAL IAW MM 36-21-00.

ATA 2121

FWD EQUIP OVERHEAT MESSAGE. REMOVED AND REPLACED THE FWD EQUIPMENT SUPPLY FAN IAW AMM 21-58-06, OPS NORMAL.

ATA 2613

EQUIPMENT OVERHEAT MESSAGE. ACCOMPLISHED QRH SELECRTOR TO STBY FOR 5 MIN THEN OVRD FOR 30 MIN. SELECTOR BACK TO AUTO . OVERHEAT LIGHT EXTINGUISHED . CONT FLIGHT NORMAL. PERFORMED EQUIPMENT COOLING TEST IAW AMM 21-58-00. NO FAULTS FOUND AT THIS STATION.

ATA 2822

LT SPAR VALVE NO INDICATION ON ENGINE START. REMOVED AND REPLACED FUEL SHUTOFF ACTUATOR IAW AMM 28-22-11.

ATA 7321

STATUS MESSAGE LT ENGINE, ELECTRONIC ENGINE CONTROL T/S IAW FIM 71-00, TASK A17. R & R LT ENGINE, ENGINE CONTROL UNIT IAW AMM 73-21-13, RAN ENGINES. OPS CHECK NORMAL.

ATA 7330

STATUS MSG, LT ENGINE, ELECTRONIC ENGINE CONTROL, C1 CLEARED MSG IAW AMM 31-35-00, TEST OF THE LT PIMU IAW FIM 71-01, TR 811, FAULT CLEARED. OK FOR SERVICE.

ATA 7330

LEFT ENGINE ELECTRONIC ENGINE CONTROL C1, PERFORMED ELECTRONIC ENGINE CONTROL LT PIMU BITE, CK 350-18A LATCHED RESET CLEARED, CHECKED CONNECTOR PLUG CONNECTORS ON ENGINE. ELECTRONIC ENGINE CONTROL UNIT, CHECKED CONNECTOR PLUG AT PYLON CONNECTOR, NO DEFECTS FIM 71-01, FT810, MM 71-00-00.

ATA 7330

STATUS MESSAGE, LT ENGINE ELECTRONIC ENGINE CONTROL C1. CLEARED MESSAGE IAW AMM 31-35-00, PERFORMED TEST OF LT PIMU, DATA MODE DISAGREE, FOLLOWED FIM 71-01 F, TREE 811, CLEARED FAULTS SYS, CKS NORMAL.

ATA 7497

RIGHT ENG IGNITOR 1 STATUS MSG. PLACED ON MEL 74-00-01B, MDDR 67109. SECURED CONNECTOR SOCKETS AT AW0325 CONNECTION SYS TEST IAW AMM CH 74-00-00. RT ENG IGNITOR OPERATES NORMAL MDDR 97109 CLOSED.

ATA 7412

RIGHT ENG IGNITER 1 R & R RT ECU AMM 73-21-13 & RT ENG NR 1 IGNITER EXCITER IAW AMM 74-11-01. OPERATIONS CHECKED NORMAL.

ATA 7421

RIGHT ENG IGNITOR 1 STATUS MSG. MSG CLEARED USING MCDP EICAS ERASE PROCEDURES IAW AMM 31-41-02. SYS CHECKED OK FOR SERVICE.

ATA 7497

RIGHT ENG IGNITER 1 STATUS MSG. PLACED DEFERRAL 74-00-01B MDDR 66953. FOUND CONNECTOR ON EXCITER BOX LOOSE, TIGHTENED SAME OPS CHECKS GOOD THIS CLEARS MDDR 66953 AMM 74-11-01.

ATA 3610

RIGHT ENG HPSOV STATUS MSG. PLACED ON DDG 36-11-02-02 & MDDR 66954. RT HP CONTROLLER REPLACED ON LP 764074 , M3. REACTIVATED HP VALVE, SYSTEM TESTED NORMAL DURING ENG RUN PER MM CH 36-11-07. MDDR CLEARED.

ATA 7200

DURING POWER RUN POST WALK, FOUND NR 2 ENG WITH OIL LEAK FROM AFT BEARING LINE. R & R RT ENG ASSEMBLY IAW WO 15415. LEAK & OPERATIONS CHECKED GOOD.

ATA 3610

RT STRUT DUCT LEAK EICAS MSG. FOUND PRE COOLER EXHAUST FITTING DISCONNECTED BETWEEN PRE COOLER & PRSOV. REPOSITIONED FLANGE & SEAL ASSEMBLY IAW AMM 36-11-15, RAN HIGH POWER IAW AMM 71-00-00, ALL OPERATIONS CHECKED GOOD.

ATA 2150

LEFT PACK INOPERATIVE LIGHT. REPLACED LT PACK ACM IAW AMM 21-51-03. OPERATIONS & LEAK CHECKS GOOD.

ATA 3697

RIGHT ENG BLEED OFF & RT PACK OFF, EICAS MSG INTERMITTENT DURING CLIMB. RAN BITE ON PNEUMATIC CONTROLLER FAULTED FAN AIR MOD VLV. INSPECTED VLV, CLEANED CONNECTOR & CYCLED VLV IAW AMM 36-11-16. PERFORMED BITE AGAIN, ALL CHECKED NORMAL.

ATA 2150

AT DEPARTURE LT PACK INOPERATIVE LIGHT. FOUND LT PACK OVERTEMP ON BITE BOX. RESET BOX, OPENED PACK BAY DOORS, NO PROBLEMS NOTED, SYS OK IAW AMM 21-51-03.

ATA 3610

RIGHT ENG BLEED OVERHEAT ADVISORY MSG AFTER TAKEOFF, CLEARED IAW QRH PROCEDURE. TROUBLE SHOT IAW FIM 36-10 TREE 835, FOUND HPSOV BAD. R & R HPSOV IAW AMM 36-11-07. DRY MOTORED ENG LEAK CHECKS GOOD.

ATA 3620

RIGHT ENG HPSOV ADVISORY MSG. QRH COMPLETED. COMPLIED WITH FIM 36-10 TREE 832 BITE CHECK ON PNEUMATIC CONTROLLER, NO FAULTS. CLEARED MSG & SYS CHECKED OK.

ATA 3620

RIGHT ENG HPSOV STATUS MSG DISPLAY. COMPLIED WITH FIM 36-10 TREE 832 BITE CHECK. PNEUMATIC CONTROLLER NO FAULT CLEARED HPSOV & STATUS MSG USING AUTO ERASE FUNCTION SYS CHECK OK AT THIS TIME.

ATA 3610

RIGHT DUCT PRESS FLUCTUATES ON TAKEOFF. R & R NR 2 ENG HPSOV IAW AMM 36-11-07-024-001-001 & AMM 36-11-07-424-016-00. ACCOMPLISHED BLAST FENCE RUN & BLEED OPERATION IS NORMAL IAW AMM 71-00-00.

ATA 7230

NUMBER 2 ENG HAS VARIOUS OF FAN BLADES NEED DRESSING UP. BLENDED OUT SMALL NICKS AT NR 2 ENG FAN BLADES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLUORESCENT PENETRANT INSPECTION. FOUND NICKS REMOVED, NO CRACKS IAW AMM 70-11-06 PB 201.

ATA 7321

LEFT ENG 353 24-B LOW PRESSURE TURBINE CASING T/M W/A FAIL. R & R NR 1 ENG ECU IAW MM 73-21-15-404-068-HOO. PERFORMED NR 3 GND TEST OK 71-00-00.

ATA 8010

NUMBER 2 ENG PNEUMATIC DUCT ATTACHMENT ROD, AT APPROX 10 O'CLOCK POSITION, HAS ONE ROD END BAD BEARING, ATTACHED TO ENG FLANGE. R & R THE ROD END BEARING ON THE UPPER SUPPORT LINK. FOR THE PNEUMATIC DUCT IAW AMM 80-11-05-004-016-H00 & 80-11-05-404-006-H00.

ATA 7321

LEFT ENG 353 21-B HPTC T/M W/A FAIL. R & R NR 1 ENG ECU IAW AMM 73-21-15. PERFORMED TEST 3 GND TEST OK AMM 71-00-00.

ATA 3350

MAIN CABIN RT 21 FLOOR EMER LIGHTS TRACK COVER, TAPED IN PLACE. REPLACED EMER LIGHT TRACK COVER ON RT ROW 21 IAW AMM 33-53-00. OPERATIONS CHECK NORMAL AT THIS TIME.

ATA 3350

MAIN CABIN LT ROW 19 FLOOR EMER LIGHTS TRACK COVER DAMAGED. REPLACED EMER LIGHT TRACK COVER ON LT ROW 19 IAW AMM 33-53-00. OPERATIONS CHECKED NORMAL AT THIS TIME.

ATA 3610

NUMBER 2 ENG PRE-COOLER RAM AIR DUCT ON COWLING HAS A CRACK. R & R AIR SUPPLY DUCT IAW AMM 36-11-01.

ATA 7110

NUMBER 2 ENG PRE-COOLER RAM INLET, SQUARE ENTRANCE ON INBD COWL SIDE HAS CRACK. REMOVED CRACKED PRE-COOLER RAM INLET SQUARE ENTRANCE ON INBD REVERSER IAW SRM 51-40-02-06. PREPARED, CLEANED & REPAIR AREA'S WITH CRACKS IAW SRM 51-70-07-00-0 & 250 DEG F CURE PERMANENT HOT BOND REPAIR ACCOMPLISHED. LOCATED & INSTALLED REPAIRED PRE-COOLER RAM INLET, SQUARE ENTRANCE MASKED & SEALED IAW SRM 51-40-02-06 & 51-20-05-00-0.

ATA 4950

APU RUBBER DUCT FROM ENG, OUT TO SURGE VLV, HAS A HOLE. REMOVED & INSTALLED AIR SURGE DUCT, PN 3884292-2, IAW AMM 49-53-01-404-010. OPERATED APU NO LEAKS NOTED IAW AMM 49-00-00.

ATA 7230

NUMBER 1 ENG HAS SOME FAN COMPRESSOR BLADES THAT NEED DRESSING UP. BLENDED OUT ALL NICKS AT NR 1 ENG FAN BLADES IAW AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLUORESCENT & PENETRANT INSPECTION. FOUND NICKS REMOVED & NO CRACKS FOUND IAW AMM 70-11-06 PB 201.

ATA 2400

LEFT ENG 350 27-NO 28VDC DETECTED. R & R RELAY XLD4N009 K1036. OPERATIONS CHECKED OK IAW 31-41-00.

ATA 3620

STATUS MSG RT ENG HPSOV. PERFORMED HPSOV TEST ON AIR SUPPLY BITE MODULE IAW AMM 36-11-07-714-031-001, RT ENG HPSOV NO FAULTS, CLEARED MSG. ACFT CLEARED TO CONTINUE NORMAL OPERATIONS.

ATA 2612

LEFT ENG FIRE LOOP 1 STATUS MSG. NO ACTIVE MSGS FOUND FIRE TEST CARRIED OUT IAW AMM 26-11-00. ALL TEST SATISFY.

ATA 3350

EMERGENCY LT LENS MISSING AT RT WING EMER DOOR, BELOW DOOR. LOCATED & INSTALLED MISSING LENS IAW AMM 33-57-00.

ATA 4940

APU DID NOT LIGHT AFTER TOUCH DOWN. TROUBLE SHOT APU IAW AMM 49-61-05. PERFORMED APU ECU BITE TEST. NOTED FAULT, ABORTED START, STARTED APU SEVERAL TIMES ON GND. OPERATIONS CHECKED GOOD.

ATA 2612

LEFT ENG FIRE LOOP 2 EICAS MSG. TRANSFERRED TO MDDR 66104 IAW DDG 26-11-01-01 CAT C. ACFT LIMITED TO 120 MIN ETOPS. R & R LT ENG LOWER AFT FIRE LOOP IAW AM 26-11-02. OPERATIONS CHECKED GOOD, CLEARED MDDR 66104. REMOVED PLACARD & NOTIFIED MCC.

ATA 2612

STATUS MSG LT ENG FIRE LP1. TRANSFERRED TO MEL 26-11-01-01 23 MAR, LP 727420, ITEM M3. R & R ENG 1 UPPER AFT DETECTION LOOP IAW MM 26-11-02, TEST 26-11-00 OK & CLEARS MDDR.

ATA 2612

LEFT ENG FIRE LP 1 STATUS, FWD TO MDDR 65184 IAW MEL 26-11-01-01-CAT C DUE 31 MAR 16, PLACARD INSTALLED. PERFORMED ENG FIRE LOOP TEST IAW AMM 26-11-00. ALL CHS NORMAL, PLACARD REMOVED. MCC NOTIFIED & CLEARED MDDR 65184.

ATA 3350

RIGHT EXTERIOR EMER LIGHT FWD OF AFT CARGO DOOR INOPERATIVE. RELAMPED RT EXTERIOR EMER LIGHT FWD OF AFT RT CARGO DOOR IAW MM 33-51-16. OPERATIONS CHECKED OK.

ATA 5620

SEAT LOCATED 2L WINDOW SEAL LEAKING. R & R WINDOW SEAL LOCATED AT 2L SEAT POSITION IAW AMM 56-21-01.

ATA 5610

BAD SEAL ON NR 2 LT MAIN WINDOW, CAPTAINS SIDE MAKING NOISE. R & R NR 2 WINDOW LT PRESS SEAL IAW AMM 56-11-11.

ATA 4990

SWITCH 8TJ99GGE1 WITH OIL LEAK IN GEAR BOX OF APU. R & R OIL TRANSMITTER IAW 49-94-04 & SERVICED APU OIL. ACCOMPLISHED OPERATIONS CHECK & LEAK CHECK NORMAL, NO LEAKS. R & R CONNECTOR IAW AMM 49-94-03 & 49-94-04.

ATA 3350

MAIN DECK AFT CEILING EMER LIGHT INOPERATIVE. RELAMPED MAIN DECK AFT CEILING EMER LIGHT IAW AMM 33-51-04. SYS CHECKED NORMAL.

ATA 4950

VENTILATION DUCT OF APU DAMAGED. R & R VENTILATION DUCT COOLING AT APU COMPARTMENT LT SIDE IAW & MM 49-51-01.

ATA 2822

FORWARD RT FUEL PUMP, WHEN TURNED OFF, NO PRESS LIGHT & NO EICAS MSG. CYCLED FWD RT FUEL PUMP SWITCH. OPERATIONS CHECK SATISFACTORY, UNABLE TO FAULT IAW AMM 28-22-00.

ATA 2150

AFT EQUIP COOLING 2 INOPERATIVE. MEL 21-58-05 CAT C DUE 25 FEB, PLACARD INSTALLED. INSTALLED & SECURED BOLT IAW SMP 20-11-00. PERFORMED AFT EQUIP COOLING FAN & PERFORMED AFT EQUIP COOLING FAN TEST IAW AMM 21-58-41, OPERATIONS OK.

ATA 3397

FLOOR EMER LIGHTING HAS A SPOT NOT WORKING. FOUND LOOSE CONNECTION AT ROW 16F. CONNECTED WIRE, OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

ATA 3350

VARIOUS EMER FLOOR LIGHTS INOPERATIVE. R & R LAMPS AT R40 & R8, R13, L26, L16, L13. OPERATIONS CHECKED NORMAL IAW AMM 33-51-10 & PN 3071BPEGPL 6 EA.

ATA 2150

DUE TO REPORTS OF LT AC PACK TRIP OFF, FOUND LT PACK COMPRESSOR OUTLET, TEMP BULB FAULTING ON PACK CONTROLLER. TROUBLE SHOT IAW AMM 21-51-14. FOUND LT COMPRESSOR OUTLET TEMP BULB BAD. REPLACED SAME IAW AMM 21-51-06. OPERATIONS & LEAK CHECKED GOOD.

ATA 3497

WEATHER SYS LT RADAR INDICATED, WXR FAIL. REMOVED THE LT WX RADAR TRANSCEIVER, CLEANED CONNECTORS. PERFORMED OPERATIONS CHECK, SYS OK IAW AMM 34-43-00 501.

ATA 2150

ON DEPT PACK TEMP MSG. PERFORMED QRH EICAS PROCEDURE. PERFORMED BITE ON LT PACK CONTROLLER, FAULTED COMPRESSOR SENSOR. COMPLETED RESET & VERIFICATION ALL CHECKED GOOD IAW AMM 21-61-00.

ATA 3610

ON WALK AROUND FOUND RT ENG PRSOV LEAKING AIR FROM VLV DIAPHRAGM HOUSING. R & R RT ENG PRSOV. LEAK CHECK OK IAW AMM 36-11-02. ENG RUN OPERATIONS GOOD IAW AMM 72-00-00.

ATA 2897

ON PUSHBACK & LT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. PERFORMED TROUBLESHOOTING WDM 28-22-12, FOUND A BROKEN WIRE W176-90H-24 AT TERMINAL BLOCK TB218 YA5. REPAIRED WIRE & REPLACED TD RELAY K10693 AS PRECAUTION. OPERATED LT CENTER BOOST PUMP IAW MM 28-22-00. OPERATIONS CHECKED NORMAL.

ATA 2150

LEFT ACM TURBINE INLET COUPLING LEAKING AIR. R & R LT ACM TURBINE INLET COUPLING SEALS IAW AMM 21-51-03. LEAK & OPERATIONS CHECKED GOOD.

ATA 3610

ENG 2 PART 3 OF EO6736A005 STEP 6 FAILED & PRV DID NOT CLOSE WEN BLEED SWITCH WAS TURNED TO OFF. R & R PRV CONTROLLER. OPERATIONS & LEAK CHECKED GOOD. REF AMM 36-11-19.

ATA 3610

NUMBER 2 HP CONTROLLER FAILED HEALTH CHECK. R & R NR 2 HP CONTROLLER IAW AMM 36-11-08.

ATA 3097

RIGHT WING THERMAL WING ANTI-ICE VLV AT TOP OF PYLON, HAS FRAYED BONDING WIRE. REPLACED RT WING THERMAL WING ANTI-ICE VLV BONDING WIRE IAW SWPM 20-20-10.

ATA 3610

LEFT WW APU PNEUMATIC DUCT SUPPORT CLAMP JUST DOWNSTREAM OF CTR ISOLATION VLV HAS AIR LEAKING FROM UNDERNEATH. R & R CLAMP DOWNSTREAM OF CTR ISOLATION VLV IAW AMM 36-11-01. NO DEFECTS NOTED & LEAK CHECKED GOOD.

ATA 2150

RIGHT PACK, COMP OUT, TEMP SENSOR INOPERATIVE. RT PACK PRIM HX IN TEMP SENSOR INTERMITTENT. R & R RT PACK COMP OUT TEMP SENSOR IAW AMM 21-52-01. R & R RT PACK HX IN TEMP SENSOR IAW MM 21-52-08. ALL OPERATIONS CHECKED GOOD. LOG BOOK ITEM CLEARED.

ATA 2197

LEFT PACK RAM AIR DOOR ACTUATOR GND DISCONNECTED. CONNECTED LT PACK RAM AIR EXHAUST ACTUATOR BONDING JUMPER IAW AMM 21-53-04. RESISTANCE CHECKED GOOD.

ATA 2120

LOWER FWD CARGO BILGE AREA STATION 400, AVIONICS OVERBOARD EXHAUST DUCT HAS CLAMP NOT SECURED AT FLOOR & AROUND DUCT. SECURED STRINGER CLIP IAW SWPM 20-10-12.

ATA 2197

GROUND WIRE FRAYED ON LT HEAT EXCHANGER FWD DUCT. REPLACED BONDING WIRE ON LT HEAT EXCHANGER IAW SWPM 20-20-10. GND BOND CHECKED GOOD.

ATA 2197

CONNECTOR D1338 TO LT PACK COMPRESSOR INLET TEMP BULB TS290 HAS A LOOSE BACK SHELL & POSSIBLE DAMAGED WIRING. REMOVED & INSTALLED NEW CONNECTOR & BACK SHELL AT TEMP BULB TS290 IAW SWPM 20-61-19. OPERATIONS CHECKED GOOD.

ATA 3020

RIGHT ENG INLET, TAI PRESS SWITCH CONNECTOR IS NOT CONNECTED. PLUG & SWITCH SHOW SIGNS OF CORROSION. CLEANED CONNECTOR IAW SWPM 20-60-01. R & R TAI PRESS SWITCH IAW AMM 30-21-01. OPERATIONS CHECK ACCOMPLISHED ON WC A-30-003-02-2.

ATA 2520

LEFT FWD OVERWING EXIT DOOR HAS DAMAGE TO DOOR LINER COVERING. CLEANED AREA, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

ATA 2520

LEFT AFT OVERWING EXIT DOOR HAS DAMAGE TO DOOR LINER COVERING. CLEANED AREA, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

ATA 2520

RIGHT FWD OVERWING EXIT DOOR HAS DAMAGE TO DOOR LINER COVERING. CLEANED AREA, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

ATA 2520

RIGHT AFT OVERWING EXIT DOOR HAS DAMAGE TO DOOR LINER COVERING. CLEANED AREA, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

ATA 3350

LEFT AISLE AFT EXIT SIGN HAS TRIM SEPARATED. RE-ATTACHED TRIM AT LT AISLE, AFT EXIT SIGN IAW AMM 20-30-01-992-001.

ATA 3350

EXIT SIGN AT 19JL IS LOOSE FROM PANEL, REATTACHED EXIT SIGN ON PANEL AT SEAT 19JL IAW SOPM 20-50-12.

ATA 3350

EXIT SIGN AT 21JL IS LOOSE FROM PANEL. REATTACHED EXIT SIGN ON PANEL AT SEAT 21JL IAW SOPM 20-50-12.

ATA 2560

R1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R R1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM GAS SPRING IAW AMM 25-66-03.

ATA 2560

L2 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R L2 DOOR GAS SPRING IAW AMM 25-66-03.

ATA 2560

R2 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R R2 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM GAS SPRING IAW AMM 25-66-03.

ATA 3350

OVERHEAD EXIT SIGNS AT AFT & FWD LAVATORY CRACKED & NEEDS PAINT. REPAIRED EXIT SIGNS AT AFT & FWD LOCATIONS IAW AMM 25-00-00-308-166. INSTALLED PLACARDS IAW AMM 20-10-12-404-004, NO PAINT NEEDED.

ATA 2520

LEFT AFT OVERWING ESCAPE HATCH, UPPER LATCH HANDLE TRIM IS GOUGED. CLEANED & PREPARED DAMAGE AS REQUIRED FOR LT AFT OVERWING ESCAPE HATCH LATCH HANDLE. APPLIED REPAIR IAW AMM 25-00-00. APPLIED TOPCOAT AS REQUIRED IAW AMM 25-00-00.

ATA 3350

CABIN FLOOR EMER LIGHTS AT RT SIDE 31, 32 & 40, AFT & LAST LIGHT ON LT SIDE ARE INOPERATIVE. TRACK LIGHTING IS REPLACED IAW AMM 33-51-10. OPERATIONS CHECKED GOOD.

ATA 3350

REPLACE EMER LIGHT TRACK COVERS AS REQUIRED WITH NEW. R & R EMER LIGHT TRACK COVERS IAW AMM 33-51-10.

ATA 3350

MULTIPLE EMER LIGHTS INOPERATIVE AT FLOOR & CEILING IN ZONES C & D. REPLACED 2 LENSES & LIGHT ASSEMBLIES JUST FWD & AFT OF SEAT 36CA FLOOR IAW AMM 33-51-06. OPERATIONS CHECKED GOOD.

ATA 3350

LEFT SIDE FLOOR & AISLE EMER LIGHTS INOPERATIVE A ZONE. TROUBLE SHOT RT SIDE EMER FLOOR LIGHTS ZONE A IAW WDM 33-51-16, BATTERY M730 FOUND UNSERVICEABLE. REPLACED BATTERY & OPERATIONS CHECKED IAW AMM 33-51-07.

ATA 2560

RIGHT AFT OVERWING SLIDE HAS DAMAGE TO THE COVER OF DEPLOY HANDLE. CLEANED, PREPARED, APPLIED REPAIR & TOP COAT IAW AMM 25-00-00-308-166. INSTALLED HANDLE IAW SRM 51-40-02.

ATA 3350

R2 DOOR EXTERIOR EMER LIGHT INOPERATIVE. RELAMPED R2 DOOR EXTERIOR EMER LIGHT IAW AMM 33-51-06. OPERATIONS CHECKED GOOD.

ATA 2520

RIGHT AFT OVERWING ESCAPE HATCH WINDOW TRIM & HANDLE LATCH TRIM IS GOUGED. REMOVED DAMAGE, PREPARED FOR & APPLIED REPAIR IAW AMM 25-00-00 801.

ATA 3397

WIRE BUNDLE AT RT STATION 396 - 412 IS LOOSE. EMER TRACK LIGHTING. SECURED WIRE HARNESS IAW SWPM 20-10-11.

ATA 2565

L1 DOOR ESCAPE SLIDE DEPLOYMENT MECHANISM HAS AN INEFFECTIVE GAS SPRING. R & R L2 DOOR ESCAPE SLIDE GAS SPRING IAW AMM 25-66-03.

ATA 3610

NUMBER 1 & ENG PRSOV FAILS HEALTH CHECK. R & R NR 1 ENG PRSOV, OPERATIONS CHECK & LEAK CHECKED GOOD IAW AMM 36-11-09.

ATA 3697

RIGHT PNEUMATIC ISOLATION VLV INOPERATIVE. TROUBLE SHOT RT PNEUMATIC ISOLATION VLV IAW WDM 36-11-21. CLEANED CONNECTOR IAW SWPM 20-60-01. OPERATIONS CHECKED GOOD IAW AMM 36-11-04.

ATA 3610

ENG 2 PRSOV FAILED HEALTH CHECK. R & R ENG 2 PRSOV. LEAK & OPERATIONS CHECK GOOD IAW AMM 36-11-09.

ATA 7334

LEFT ENG FUEL FILTER BYPASS FAILED STEP B OF TASK CARD 73-306-01-1. R & R , OPERATIONS CHECKED & LEAK CHECKED NR 1 ENG FUEL FILTER BYPASS IAW AMM 73-34-01-424-008 & 73-34-00-715-001-H00 & 71-00-00 001. OPERATIONS CHECKED GOOD, NO LEAKS NOTED AT THIS TIME.

ATA 7532

ENG 1 HAS FUEL LEAKING FROM DRAIN MAST AT A RATE OF 2 - 3 DROPS PER MINUTE. TROUBLE SHOT ENG 1 FUEL LEAK FROM DRAIN MAST, REF AMM 71-71-00. R & R VSV IAW AMM 75-31-02. R & R RT & LT VBV'S IAW AMM 75-32-01. OPERATIONS CHECKED GOOD.

ATA 7921

ENG 2 HAS A FUEL LEAK, LOCATED BETWEEN MAIN FUEL PUMP & FUEL & OIL HEAT EXCHANGER. R & R GASKET ON ENG 2 IAW AMM 79-21-01. OPERATIONS CHECKED GOOD. NO LEAKS NOTED AT THIS TIME.

ATA 7230

CORE MODULE, VAR STATOR VANE LEVER ASSEMBLY AFT MODULATING STUD ON ENG 1, INBD SIDE IS BROKEN. R & R CORE MODULE VAR STATOR VANE LEVER AFT MOUNTING STUD ON ENG 1 IAW AMM 72-36-00.

ATA 3610

ENG 1 PRECOOLER HAS A CRACK ON THE LOWER FWD OTBD CORNER. R & R NR 1 ENG PRECOOLER. OPERATIONS LEAK CHECKED NORMAL IAW MM 36-11-15.

ATA 7933

RIGHT ENG OIL TEMP BLANKED OUT IN FLIGHT. TROUBLE SHOT IAW FIM 79-34TR807. FOUND RT ENG TEMP TX BROKEN OFF, R & R. PERFORMED LEAK CHECK & OPERATIONS CHECK TEST 3 IAW AMM 79-34-001 & 71-00-00. OK FOR SERVICE.

ATA 2121

STATUS MSG FWD EQUIP EXHAUST FAN, DEFERRED FWD EQUIP EXHAUST FAN INOPERATIVE IAW MEL 21-58-04-02-01 CAT C. REPLACED EXHAUST FAN PN 732591D.

ATA 2130

STATUS MESSAGE, CABIN ALTITUDE AUTO 1. PERFORMED FIM 21-31 TREE 803 & BIT CABIN PRESSURE CONTROLLER & RESET, NO FAULTS NOTED.

ATA 2560

PASSENGER CABIN MEGA PHONE LT AFT STORAGE COMPARTMENT SUPPORT CLAMP DAMAGED. REMOVED DAMAGED BRACKET LOCATED & INSTALLED NEW MEGA PHONE BRACKET AT PAX CABIN LT AFT STORAGE COMPARTMENT IAW SRM 51-40-02-06-0.

ATA 2560

PASSENGER CABIN MEGA PHONE FWD OVERHEAD BIN SUPPORT CLAMP DAMAGED. REMOVED DAMAGED MEGA PHONE HOLDER BRACKET. LOCATED & INSTALLED NEW BRACKET AT PAX CABIN FWD OVERHEAD LT BIN IAW SRM 51-40-02-06-0.

ATA 2560

COCKPIT CAPTAIN SMOKE GOGGLES DAMAGED. R & R DAMAGED CAPTAINS SMOKE GOGGLES IAW AMM 25-60-00.

ATA 3530

PASSENGER CABIN, FOUR EACH PORTABLE OXYGEN BOTTLE MASKS ARE DAMAGED. R & R DAMAGED PORTABLE OXYGEN BOTTLE MASK IN PAX CABIN AS NEEDED IAW AMM 35-31-00.

ATA 2150

LEFT PACK HAS AIR LEAKS AT THE TWO COUPLINGS COMING FROM THE ACM OUTLET & THE COUPLING AT THE ACM INLET. R & R TWO EACH COUPLING SEALS AT LT PACK DUCTS IAW AMM 21-51-23.

ATA 3350

EXTERNAL EMER EXIT LIGHT INOPERATIVE NEAR AFT CARGO DOOR. RELAMPED IAW AMM 33-51-16.

ATA 3350

LEFT FUSELAGE EXTERNAL EMER EXIT LIGHT INOPERATIVE, STATION 1250 WING TO BODY FAIRING, STATION 1540 AFT ENTRY DOOR. R & R BATTERY POWER SUPPLY IAW AMM 33-51-07.

ATA 3350

LEFT FUSELAGE EXTERNAL EMER EXIT LIGHT INOPERATIVE, STATION 1250 WING TO BODY FAIRING, STATION 1540 AFT ENTRY DOOR. RELAMPED IAW AMM 33-51-16.

ATA 3350

LEFT FUSELAGE EXTERNAL EMER EXIT LIGHT INOPERATIVE, STATION 1250 WING TO BODY FAIRING, STATION 1540 AFT ENTRY DOOR. R & R LAMP HOLDER ASSEMBLY IAW AMM 33-51-16.

ATA 3620

LEFT ENG BLEED VLV IS NOT OPENING & REQUIRES 60% N1 TO UNSTICK & CARRY DEMAND. INSPECTED PRSOV, FOUND SENSE LINE LOOSE, TIGHTENED. PERFORMED BITE CHECK ON BLEED CONTROL BOX IAW 36-23-00 & FIM 36-10. FAULT TREE 829, NO FAULTS INDICATED AT THIS TIME.

ATA 3620

LEFT BLEED VLV LIGHT ILLUMINATED AFTER ENG START WITH ZERO DUCT PRESS. ENG RUN TO 70% N1 CORRECTED SITUATION. RAN LT ENG IAW AMM 36-11-00 501. OPERATIONS CHECKED NORMAL.

ATA 7830

LEFT ENG OTBD THRUST REVERSER, INTERIOR LINER MISSING AT 10 O CLOCK POSITION. IAW EO 6778A019 COMPLIED WITH PART 1 INTERIM REPAIR. PART 2 DVI REQUIRED EVERY 5 FC. PART 3 PERMANENT REPAIR DUE AT NEXT A CHECK. PLACED ON NON-MEL 59424.

ATA 3610

LEFT BLEED DUCT LEAK EICAS, PERFORMED AIR SUPPLY BITE CHECK IAW AMM 36-23-00. RE-RACKED M859 CARD FILE IAW AMM 36-11-12 & ADJUSTED BALL JOINTS IAW MM 36-11-01. SYSTEM NORMAL AT THIS TIME.

ATA 2841

FUEL QUANTITY INDICATOR SYSTEM BITE INTERMITTENT. R & R FUEL QUANTITY INDICATOR SYSTEM PROCESSOR UNIT IAW AMM 28-41-08. BITE TEST COMPLIED WITH, NO FAULTS NOTED.

ATA 2150

DURING TROUBLESHOOTING LEFT PACK, FOUND LEFT PACK CONTROLLER NOT TESTING OR BITE TESTING. R & R A/C PACK CONTROLLER IAW AMM 21-62-00. OPS CHECKED NORMAL.

ATA 2150

EICAS MESSAGE, LEFT PACK TEMP & LEFT PACK OFF. TROUBLESHOT IAW MM 21-62-00. FOUND MAIN DUCT MANIFOLD CRACKED. R & R DUCT NEAR LEFT PACK HEAT EXCHANGER. OPS CHECKED GOOD IAW MM 21-62-00.

ATA 3620

EICAS MESSAGE, INTERMITTENT LEFT ENGINE BLEED OFF. ACCOMPLISHED AIR SUPPLY PRESSURE INDICATION SYSTEM OPEN TEST. TESTED OK IAW AMM 36-21-00.

ATA 3442

WEATHER RADAR NOT PAINTING KNOWN WEATHER. COMPLIED WITH FIM 34-43 FT 805 RADAR SYS BITE CHECK, NO DEFECT NOTED. PERFORMED RADAR SYS OPERATIONS CHECK ON LT & RT SYS IAW AMM 34-43-00. BOTH SYS OPERATES NORMAL, NO FAULTS NOTED.

ATA 2612

APU FIRE LOOP 1 STATUS MSG. R & R CCA IAW AMM 26-10-01. OPERATIONS CHECKED SATISFACTORY.

ATA 3350

EMERGENCY LIGHT INOPERATIVE, FWD AFT CARGO DOOR. SECURED LAMP EMER LIGHT FWD OF AFT CARGO DOOR IAW AMM 33-51-16.

ATA 7200

MAX THRUST AT TAKEOFF N1 109.1, LT ENG WOULD ONLY GENERATE 106.6 N1 WITH THROTTLE TO STOP. ASSUMED TEMP REQUIREMENT 106.1, TROUBLESHOOTING ENGINE. R & R NR 1 ENG FUEL PUMP, R & R NR 1 ENG HMU, R & R NR 1 ENGINE EEC, R & R NR 1 ENGINE N1 SPEED SENSOR, R & R THRUST MANAGEMENT COMPUTER. COMPLIED WITH GROUND TEST 5 & 10, MAX POWER ASSURANCE IAW AMM 71-00-00, NO FAULTS NOTED. ENGINE OPS & PARAMETERS WITHIN LIMITS.

ATA 2432

AIRCRAFT MAIN BATTERY HAS LOW VOLTAGE. MAIN BATTERY REPLACED IAW MM 24-31-00. OPERATIONS CHECKED NORMAL.

ATA 2612

STATUS MESSAGE RT ENGINE FIRE LP1. R & R LOWER AFT LOOP IAW AMM 26-11-00. OPERATIONS CHECKED OK.

ATA 2841

LEFT FUEL QTY & TOTAL QTY INTERMITTENT IN CRUISE. STATUS MESSAGE FUEL QTY INDICATOR. R & R LT MAIN FQIS WIRE HARNESS, LT MAIN FQIS COMPENSATOR, LT DENSITOMETER ELECTRONIC UNIT, 14, 5, 6, 4 TANK UNITS CAUSE OUT OF LIMITS, ALL IAW AMM 28-11-01, 28-41-09, 28-41-02, 28-41-03, & 24-41-01. OPS CHECKED NORMAL.

ATA 2841

LEFT FUEL QTY & TOTAL FUEL QTY INTERMITTENT IN CRUISE. FUEL QTY IND STATUS MSG. PERFORMED FIM 28-41 FT 861 & BITE CHECKED FQIS PROCESSOR IAW 28-41-00. MSG ERASED SYS OK FOR SERVICE.

ATA 2150

LEFT PACK EICAS MSG ON CLIMB OUT. PERFORMED FIM TASK 21-51 TASK 803 & REST OK. PERFORMED LT PACK COOLING TEST IAW AMM 21-51-00 & OK FOR SERVICE.

ATA 7321

STATUS MSG L ENG EEC C1. REMOVED AND REPLACED L ENG EEC IAW AMM 73-21-15, EEC TESTS 11 &AMP; 12&NBSP;CARRIED OUT IAW IAW AMM 71-00-00 CONFIG 3 ALL NORMAL MDDR CLEARED.

ATA 2612

RIGHT ENG FIRE LOOP 1 EICAS STATUS MSG, PLACED ON DEFERRAL 26-11-01-01. REPLACED UPPER AFT LOOP TS681. CKS GOOD & NBSP.

ATA 2697

STATUS MESSAGE IN FLIGHT, RT ENGINE FIRE LOOP 1. INSPECTED RT ENG LOOP & FOUND LOOSE CONNECTION AT UPPER LT COWLING. SECURED CONNECTOR, OPERATIONS CHECKED GOOD IAW AMM 26-11-00.

ATA 2565

R4 SLIDE DETACHED FROM DOOR WHILE GND HANDLING. INSTALLED SLIDE PACK IAW AMM 25-66-00. RETURNED ACFT TO ORIGINAL CONFIG & INSPECTED GIRT BAR IAW AMM 25-66-05. OK FOR SERVICE.

ATA 7321

STATUS MSG, L ENG EEC C1. ACCOMPLISHED PIMU BITE PROCEDURES IAW FIM 71-01-00 101, MSG ERASED. OK FOR SERVICE.

ATA 3442

LEFT WEATHER RADAR FAILED MESSAGE ON HSI. SWITCHED TO RT RADAR , RT OPS NORMAL. TRANSCEIVER REMOVED AND REPLACED IAW AMM 34-43-01, OPS CHECK GOOD.

ATA 3350

EXTERIOR EMER LIGHTS INOPERATIVE. REPLACED EXTERIOR EMER LIGHTS LT & RT SIDE. OPERATIONS CHECKED NORMAL AMM 33-51-06.

ATA 2841

LEFT WING TANK QTY DISPLAY BLANKS OUT INTERMITTENTLY. R & R FUEL QTY PROCESSOR IAW AMM 28-41-08. OPS CHECKED GOOD.

ATA 2840

INTERMITTENT LOSS OF OVERHEAD FUEL QTY LEFT TOTAL, RESULTING IN EICAS MSG, LOW FUEL, & FUEL CONFIG MASTER CAUTION. FOUND FUEL QTY CHECKED GOOD. COMPLIED WITH FIM PROCEDURES IAW 28-41-02. NO FAULTS INDICATED.

ATA 2150

BOTH PACKS RUNNING, UNABLE TO MAINTAIN CABIN TEMP BELOW OAT. DURING INSP FOUND RT PACK LOW LIMIT VLV FAULTY. R & R IAW AMM 21-51-11 201. OPERATIONS CHECKED OK.

ATA 8011

NUMBER 2 STARTER INOPERATIVE ON DEPARTURE START-UP. R & R IAW AMM 80-11-01. OPERATIONS CHECKED SATISFACTORY.

ATA 3350

RIGHT ROW SEAT & FLOOR EMER LIGHT BROKEN. REPLACED TRACK BOTTOM & LIGHT ASSEMBLY IAW 33-51-16 & AMM 33-51-06-201. OPERATIONS CHECKED OK.

ATA 7420

NUMBER 1 ENG IGNITOR LEAD CERAMIC TIP BROKEN. R & R NR 1 RT IGNITION LEAD IAW AMM 74-21-01. OPERATIONS CHECKED NORMAL.

ATA 2150

LEFT PACK EXHAUST DOOR CUT OUT IS DAMAGED. R & R LT RAM AIR EXHAUST DOOR IAW AMM 21-53-02. OPERATIONS CHECKED NORMAL.

ATA 2421

LEFT ENG GENERATOR CLAMP DETERIORATED & MISALIGNED. FOUND CLAMP INSULATION MISALIGNED. REALIGNED INSULATION & SECURED CLAMP IAW AMM 20-10-12.

ATA 4950

APU AIR SUPPLY DUCT HAS A HOLE IN IT. R & R APU SUPPLY DUCT. LEAK CHECK OK IAW AMM 49-53-01.

ATA 2150

RIGHT PACK EXHAUST DOOR CUT OUT MISSING 3/8 PIECE. R & R IAW AMM 21-53-02. OPERATIONS CHECKED NORMAL.

ATA 3350

RIGHT ENTRY DOOR UPPER FWD EMER LIGHT SOCKET IS BROKEN. R & R RT ENTRY DOOR UPPER FWD EMER LIGHT ASSEMBLY IAW AMM 33-51-03. OPERATIONS CHECKED NORMAL.

ATA 3350

SEVERAL CEILING EMER LIGHTS BURNED OUT. RELAMPED SEVERAL EMER CEILING LIGHTS IAW AMM 33-51-04. OPERATIONS CHECKED NORMAL.

ATA 3350

AT SEAT ROW 5 CEILING EMER LIGHT LENS IS FALLING APART. SECURED EMER LIGHT LENS AT SEAT ROW 5 RT SIDE IAW AMM 33-51-01.

ATA 3350

RIGHT ROW SEAT POSITION 29 LT IS TORN. REPLACED TRACK BOTTOM & LIGHT ASSEMBLY IAW DM 33-51-06 & AMM 33-51-06-201. OPERATIONAL TESTED OK.

ATA 3350

RIGHT ROW SEAT 30 FLOOR EMER LIGHT BROKEN. REPLACED EMER LIGHT ASSEMBLY IAW WDM 33-51-16 & AMM 33-51-06-201. OPERATIONS CHECKED OK.

ATA 3350

RIGHT ROW SEAT 36 FLOOR EMER LIGHT BROKEN. REPLACED EMER LIGHT ASSEMBLY IAW WDM 33-51-16 & AMM 33-51-06-201. OPERATIONS CHECKED OK.

ATA 3350

RIGHT ROW SEAT 37 FLOOR EMER LIGHT BROKEN. REPLACED EMER LIGHT ASSEMBLY IAW WDM 33-51-16 & AMM 33-51-06-201. OPERATIONS CHECKED OK.

ATA 3397

EMERGENCY WINDOW CTR EMER LIGHTS INOPERATIVE. SECURED EMER LIGHTS PIN AT CTR SEGMENT IAW AMM 33-53-03. OPERATIONS CHECKED NORMAL.

ATA 3350

RIGHT ROW SEAT 7 EMER LIGHT INOPERATIVE. RELAMPED RT ROW SEAT 7 FLOOR LIGHT IAW AMM 33-51-06-201. OPERATIONS CHECKED OK.

ATA 3350

RIGHT OVERWING AFT EMER LIGHT BURNED OUT. CLEANED FWD SOCKET OF RT WING LIGHT ASSEMBLY. ALSO RELAMPED BULB IAW AMM 33-51-06 201. OPERATIONAL TESTED OK.

ATA 8012

LEFT ENG, NO RPM DURING START, MANUAL START SUCCESSFUL. LT ENG START VLV LIGHT OPERATES NORMAL. R & R START VLV. OPERATIONS CHECKED GOOD IAW AMM 80-11-02.

ATA 2822

DURING CRUISE FLIGHT, ENG CONFIG, EICAS MSG CAME ON TWICE DUE TO FUEL IMBALANCE BUT IMBALANCE RETURNED. LT TANK WOULD GO LOW & RT TANK HIGH. EACH TIME, FUEL CONFIG, MSG WOULD COME ON. R & R LT AUX TANK OVERRIDE FUEL BOOST PUMP IAW AMM 28-22-06. OPERATIONS CHECKED LT AUX OVERRIDE PUMP IAW AMM 28-22-05, NO LEAKS OR DEFECTS NOTED.

ATA 3442

RIGHT WX RADAR INOPERATIVE. R & R RT WEATHER TRANSCEIVER IAW AMM 34-43-01. OPERATIONS CHECKED GOOD.

ATA 2840

FUEL APPEARS TO TRANSFER FROM LT MAIN TO RT MAIN IN FLIGHT. COMPLY FIM 28-41-TR824, FUEL CONFIG LIGHT OPERATIONS CHECKED GOOD & OPERATIONS CHECKED FUEL TRANSFER IAW FIM 28-41-TR842, NO DISCREPANCIES FOUND.

ATA 4930

APU INOPERATIVE FOUND FUEL LEAK AT APU FUEL FILTER. R & R FILTER ELEMENT & ORING IAW AMM 49-31-04. OPERATIONS & LEAKS CHECKED OK.

ATA 2800

DURING CRUISE, FUEL CONFIGURATION, EICAS MESSAGE CAME ON TWICE DUE TO FUEL IMBALANCE. CORRECTED BUT RETURNED. LT TANK WOULD GO LOW & RT TANK HIGH. WHEN CTR TANK EMPTY FUEL IMBALANCE DISCONTINUED. APPEARS CENTER TANK PUMP DOES NOT OVERRIDE FWD & AFT LT PUMPS FUEL CROSSFEED. COMPLIED WITH FQS BIT IAW 28-41 FT847 & FT842, NO FAULTS NOTED.

ATA 3350

AFT RT DOOR EXTERIOR & BOTH OVERWING EXTERIOR EMER LIGHTS INOPERATIVE, RELAMPED.

ATA 3350

EMERGENCY FLOOR LIGHTS LT FRONT, CREW AREA, SECTION DO NOT ILLUMINATE. RECONNECTED LT FRONT CREW AREA SECTION FLOOR PROX LIGHT IAW AMM 33-51-10. OPERATIONS CHECKED OK.

ATA 3350

LEFT SIDE ADJACENT TO THE LAVATORY A3L FLOOR, ONE EMER LIGHT IS INOPERATIVE IN THE STRIP SECTION. RECONNECTED LAVATORY A3L FLOOR PATH LAMP IAW AMM 33-51-10. OPERATIONS CHECKED ON.

ATA 3442

WX FAIL MSG ON MFD. WX RADAR WAS ON RT SIDE WHEN WE GOT THIS MSG, PERFORMED FIM 34-43 FAULT TREE 805 & SYS CHECKED OK LT & RT. NO FAULTS NOTED IN BITE PROCEDURE. OK FOR SERVICE.

ATA 2841

RIGHT WING QTY INDICATOR FLUCTUATES SLOWLY IN FLIGHT +/- 600. ACCOMPLISHED FIM 28-41 FT 840 & FQIS BITE 28-41-00 501 & NO FAULTS FOUND, OK FOR SERVICE.

ATA 3442

LEFT WEATHER RADAR IN NUMEROUS POSITIONS DISPLAYED ARE IN SOLID LINES. LT WEATHER RADAR SYS TEST CARRIED OUT IAW AMM 34-43-00 CONFIG 2 PAGE 501. ALL TEST PASSED, UNABLE TO DUPLICATE FAULT. OK FOR SERVICE.

ATA 3442

RIGHT SYS WEATHER RADAR DISPLAY WXR FAILED IN ALL MODES. R & R RT WEATHER RADAR TRANSCEIVER IAW AMM 34-43-00-001. THIS CLEARS MDDR 51264, PLACARD REMOVED.

ATA 2150

AIR CONDITIONING RT PACK INOPERATIVE LIGHT ILLUMINATED. FOUND RT ACM SEIZED, R & R IAW AMM.

ATA 2613

DURING INITIAL CLIMB OUT FWD EQPT OVT EICAS MSG CAME ON WITH OVERHEAD LIGHT. USED QRH PROCEDURE & MSG & LIGHT CLEARED AFTER 30 MINUTES. ACCOMPLISHED EQUIPMENT COOLING. OPERATIONS TESTED OK IAW AMM 21-58-00.

ATA 7321

ENGINE NR 1 EEC SWITCHES TO ALTERNATE ON START. WILL NOT OPERATE IN NORMAL SETTING. R & R NR 1 ENG EEC IAW AMM 73-21-15.

ATA 2613

FORWARD EQUIPMENT & OVERHEAT EICAS CAUTION ON CLIMB OUT. COMPLETED QRH P 2.22 THRU STEP 7 FINISHED FLIGHT IN EQUIP COOLING SELECTOR IN AUTO. PERFORMED FIM 21-58-31-00 NO FAULTS INDICATED. OPERATIONS CHECKED IAW AMM 21-58-00. NO PROBLEMS FOUND, OPERATIONS CHECKED OK.

ATA 4920

APU FAULT EICAS MSG ON APU START. APU WILL NOT START DURING TAXI. NO CURRENT NO LAST LEG FAULTS ON ECU BITE. ACCOMPLISHED NORMAL START IAW AMM 49-11-00 201, NO FAULTS.

ATA 3000

RIGHT PACK FOUND ACM COMPRESSOR TO CONDENSER WARM. AIR ANTI-ICE LINE BOOT RUPTURED. NO PACK INDICATIONS OR FAULTS NOTED. TEMPS NORMAL NO OVERHEATS. TRANSFERRED TO DMI DDG 21-51-01-01.

ATA 5270

FORWARD CARGO DOOR EICAS MSG & CARGO DOORS ANNUNCIATOR LIGHT ILLUMINATED ON CLIMB THROUGH 10,000 FT. CARGO DOORS QRH NON-NORMAL PROCEDURE COMPLIED WITH. TRANSFERRED TO DMI MDDR 49862, IAW DDG 52-71-01-01. DOOR IS CLOSED FAIRED, LATCHED, LOCKED, HANDLE STOWED & VENT DOORS CLOSED.

ATA 4920

APU FAILED TO START 3 TIMES AFTER LANDING. TROUBLE SHOT IAW 49-11-00 FAULT TREE 958. APU STARTED NORMAL ON 3 ATTEMPTS.

ATA 3350

EMERGENCY DOOR EXIT LIGHT INOPERATIVE. REPLACED BATTERY CHARGER M1209 IAW AMM 33-51-07.

ATA 4920

APU FAULT MSG, APU NO START. GND TAXI ACCOMPLISHED APU MX PRACTICES PART 3, APU STARTING OPERATIONS IAW AMM 49-11-00. START SAT APU OPERATIONS NORMAL, ALL INDICATIONS NORMAL, NO ECU FAULTS, NO LEAKS, APU OIL FULL.

ATA 4950

APU COLD START, OAT - 44C, FL350, START UNSUCCESSFUL. R & R ECU OPS CHECKED GOOD IAW AMM 49-11-00.

ATA 5240

POST FLT EXTERNAL HYD MULE GND POWER CONNECTIONS ACCESS DOOR MISSING. NO ACFT STRUCTURE & COMMON TO DOOR. EO 6753A159 INTERIM REPAIRED TO MISSING PANEL 149BL PART 1 COMPLETED.

ATA 3442

WEATHER RADAR LT SYS INOPERATIVE, WXR FAIL MSG FOUND LWXR CB OPEN, RESET CB NO RECURRENCE. RESET IN COMPLIANCE WITH THE GMM 3.10.2. ACCOMPLISHED WXR OPERATIONS TEST IAW AMM 34-35-00, OPERATIONS & IND NORMAL.

ATA 3350

ALL EIGHT OVERWING ESCAPE HATCH EXIT SIGNS WILL NOT ILLUMINATE WHEN TESTED. REPLACED EMER LIGHT SIGNS POWER SUPPLY IAW WDM 33-51-14 P 14 & AMM 33-51-07/201. EMER LIGHTS TESTED OK IAW AMM 33-51-00/501.

ATA 2560

LEFT SLIDE SIDE COMPARTMENT DISCONNECT HOUSING ARM IS BROKEN. R & R LT SLIDE COMPARTMENT DISCONNECT HOUSING ARM IAW AMM 25-65-04.

ATA 2820

APU SHROUD DRAIN LINE FAILED SYS LEAK TEST IAW AMM 28-25-00. PRESS DECREASES MORE THAN 0.1 PSIG FOR 5 MIN. R & R O RING FROM CONNECTION IN FWD COMPARTMENT OF OFF WING ESCAPE SLIDE BOTTLE IAW AMM 20-10-19. PERFORMED APU SHROUD DRAIN LEAK TEST. LEAK TESTED GOOD.

ATA 2120

RIGHT PACK AREA TUBING CLAMP IS DETERIORATED. REPLACED RT PACK AREA DETERIORATED TUBING CLAMP IAW SRM 51-40-02.

ATA 2140

STEP E 1 F FAILED OF THE CARGO FIRE EXIT ARMED SWITCHES ROUTINE CARD FWD CARGO HEAT MX MSG FAILED TO SHOW THE LOWER EICAS DISPLAY. REMOVED & INSTALLED NEW FWD CARGO HEAT CONTROL VLV IAW AMM 21-43-00-705-047-003.

ATA 3610

NUMBER 1 ENG PRE COOLER HAS BENT FINS & MISSING FINS ON OTBD SIDE. R & R NR 1 ENG PRE COOLER IAW AMM 36-11-15.

ATA 3610

NUMBER 2 ENG PRE COOLER HAS BENT FINS & IS CLOGGED ON THE INBD SIDE. R & R NR 2 ENG PRE COOLER IAW AMM 36-11-15. OPERATIONS & LEAK CHECKED GOOD.

ATA 2530

AFT GALLEY RT WASTE LID WILL NOT CLOSE. CLEANED AFT GALLEY RT WASTE LID SO IT CLOSES PROPERLY AMM 25-00-00.

ATA 2560

R2 DOOR GAS SPRING FOR SLIDE DEPLOY BAR ON RT FWD DOOR WON`T HOLD THE BAR UP. R & R R2 GAS SPRING IAW AMM 25-66 -03.

ATA 2560

R1 DOOR GAS SPRING FOR SLIDE DEPLOY BAR ON RT FWD DOOR WON’T HOLD BAR UP. R & R GAS SPRING FOR SLIDE DEPLOY BAR ON RT FWD DOOR IAW AMM 25-66 -03.

ATA 2612

LEFT MLG WW FIRE LOOP IS BROKEN. R & R RIVET ON LT MLG WW LOOP IAW SRM 51-40-02.

ATA 3350

ALL OF THE FLOOR EMER ESCAPE PATH LIGHTING TRACK COVER IS SCRATCHED, GOUGED, DISCOLORED & DIRTY. R & R ALL FLOOR EMER ESCAPE PATH LIGHTING TRACK COVERS IAW AMM 33-51-00.

ATA 2197

EE COOLING SYS DIFFERENTIAL PRESS SWITCH S613 FAILED STEP B 4 A OF ROUTINE CARD. PERFORMED SATISFACTORY OPERATIONS CHECK OF EE COOLING SYS DIFFERENTIAL PRESS SWITCH IAW AMM 21-58-00 WITH NO DISCREPANCIES FOUND AFTER PIN 2 INSERTED ON DIFFERENTIAL PRESS SWITCH CONNECTOR IAW SWPM 20-61-00.

ATA 3350

FLOOR EMER ESCAPE PATHWAY LIGHTING COVER CRACKED AT 2J, 4J & 5J MID CABIN CROSS AISLE 17J, 22J, 31J, 33J, 40J LAV F2, 7A, 8A, 29A, 30A, 33A, 35A & LT AFT LAVATORY A3 & ALONG LT AFT OTBD CLOSET. R & R CRACKED LIGHTING COVERS OF FLOOR EMER ESCAPE PATHWAY LIGHTING IAW AMM 33-51-10-10-022-074.

ATA 3350

FORWARD MAST LT FLOOR EMER ESCAPE PATHWAY PROX LIGHT, RED ARROW, INOPERATIVE. RE LAMPED LT FWD EMER PATH PROX LIGHT, RED ARROW, IAW AMM 33-51-10. OPERATIONS CHECKED SATISFACTORY AT THIS TIME.

ATA 2823

LEFT ENG FUEL SOV TEST FAILED. SPAR VLV LIGHT DOES NOT COME ON WHEN LT FUEL CONTROL SWITCH IS ACTIVATED. R & R LT FUEL SOV ACTUATOR IAW AMM 28-22-11-404-008. OPERATIONS CHECKED GOOD.

ATA 2150

LEFT PACK FLOW SENSOR HAS AIR LEAK. REPLACED LT PACK SENSOR IAW AMM 21-52-03. OPERATIONS CHECKED OK.

ATA 2560

LEFT OFF WING ESCAPE SLIDE INTERROGATOR CONNECTION TO AFT DOOR ACTUATOR BROKEN. R & R PAWL FABRICATED FROM 15-5PH CRES 180-200KSI, AMM 26-65-12.

ATA 2560

LEFT SIDE OF WING ESCAPE SLIDE COMP DOOR LATCHES & LINKAGE FAIL TO RETURN TO LOCKED POSITION, FWD AFTER CHECKING OPENING TORQUE FORCE. R & R MFG PANEL ON INTERROGATOR. R & R LATCH ACTUATOR AS REQUIRED IAW AMM 26-65-11 & 25-65-12.

ATA 3350

FLOOR EMER ESCAPE PATHWAY PRX LIGHT ASSEMBLY IS BROKEN AT 37J, THE LENS IS ALSO MISSING. REMOVED & INSTALLED NEW LIGHT ASSEMBLY & COVER. RELAMPED EMER TRACK LIGHTS. OPERATIONS TESTED GOOD IAW AMM 33-51-10.

ATA 8012

V BAND COUPLING BETWEEN NR 1 ENG START VLV & STARTER BROKE. R & R V BAND CLAMP ON NR 1 ENG START VLV IAW AMM 80-11-02.

ATA 2150

LOW FLOW DETECTOR TS 104 FWD CARGO BENEATH FLOOR, LT SIDE FWD END HAS BENT CONNECTOR. R & R LOW FLOW DETECTOR TS 104 FOR THE FWD RACK & EQUIPMENT COOLING IAW AMM 21-58-17.

ATA 3610

ENGINE 1 PRV MANUAL LOCK OUT WITH WRENCH HAS EXCESSIVE PLAY. R & R NR 1 ENG PRESS REGULATING VLV IAW AMM 36-11-18, LEAK CHECKED GOOD.

ATA 3610

LEFT ENG HPSOV WILL NOT CLOSE, STICKS WEAK RETURN SPRING. R & R NR 1 ENG HPSOV IAW AMM 36-11-07, OPERATIONS & LEAK CHECKED GOOD.

ATA 7520

ENG 2 TURBINE CASE COOLING HIGH PRESS AIR SUPPLY TUBE DENTED. R & R NR 2 ENG TURBINE CASE COOLING HIGH PRESS AIR SUPPLY TUBE IAW AMM 70-00-00.

ATA 3397

MULTIPLE AREAS OF EMER PATHWAY LIGHTING WIRES DAMAGES. REPAIRED EMER FLOOR PATH LIGHTING IN ACFT CABIN AREA AS REQUIRED IAW AMM 33-51-00 & SWPM 20-10-13. PERFORMED SATISFACTORY OPERATIONS TEST IAW AMM 33-51-07-612-035.

ATA 3610

LEFT WING BLEED AIR DUCT IN LE JUST INBD OF NR 1 ENG IS LEAKING AT CLAMP. REPOSITIONED DUCT & ADJUSTED CLAMPS IAW AMM 36-11-01, NO LEAKS.

ATA 3610

LEFT ENG HPSOV FWD CLAMP NUT HAS NO RUN ON TORQUE. R & R COUPLING ON HPSOV NR 1 ENG FWD LOCATION IAW AMM 36-11-07 PAR E 11 A - E, LEAK CHECKED GOOD.

ATA 3350

EMERGENCY FLOOR PATH LIGHTING AT ROW 1C & 40J MISSING LIGHT ASSEMBLY & COVER. INSTALLED LIGHT ASSEMBLY & COVER AT SEATS 1C & 40J FOR EMER PATH LIGHTING IAW AMM 33-51-10. OPERATIONS CHECKED GOOD.

ATA 3350

FLOOR EMER ESCAPE PATHWAY LIGHTING FLOOR TRACK IS LIFTING & PULLED FROM FLOOR 28J & 40J LOG BOOK PG 598850 M2. SECURED PATHWAY LIGHTING TRACK TO FLOOR PANEL AT SEAT AREAS 28J & 40J IAW AMM 25-27-09 ITEM M2 OF LOG BOOK PAGE 598850 CLEARED.

ATA 3350

EMERGENCY LIGHTING BATTERY M737 STATION 988 LT SIDE & M1209 STATION 916 RT SIDE WILL NOT HOLD A CHARGE. R & R EMER LIGHTING BATTERY M737 STATION 988 LT & M1209 STATION 916 RT IAW AMM 33-51-07-022-001. PERFORMED SATISFACTORY BATTERY PACK CAPACITY TEST IAW AMM 33-51-07-612-035.

ATA 2560

AFT CARGO COMPARTMENT FWD LT WALL LOWER SMOKE BARRIER MISSING. REMOVED FLOORBOARD & CARGO TAPE. REATTACHED SMOKE BARRIER & REINSTALLED CARGO TAPE FT CARGO COMP FWD WALL LOWER LT & INSTALLED FLOOR PANEL IAW AMM 20-11-00, 25-52-01 & SOPM 20-50-12.

ATA 2550

AFT CARGO COMP FWD CTR LT WALL BOTTOM VELCRO WORN, MISSING IN AREAS DISBONDED. REPLACED ALL WORN VELCRO & REGLUED DISBONDED AREA IAW SOPM 20-50-12.

ATA 2560

AFT CARGO COMP FWD RT WALL LOWER SMOKE BARRIER VELCRO WORN & DISBONDING. REMOVED FLOORBOARD & REATTACHED LOWER SMOKE BARRIER & VELCRO. REINSTALLED FLOORBOARD IN AFT CARGO COMP FWD RT ALL IAW AMM 20-11-00 & 25-52-01 SOPM 20-50-12.

ATA 4910

TWO BROKEN STUDS IN ANCHOR NUTS IN FLANGE THAT MOUNTS APU AIR INTAKE TO FUSELAGE LOWER ROW. R & R TWO ANCHOR NUTPLATES CONTAINING BROKEN STUDS AT APU AIR INTAKE TO FUSELAGE LOWER ROW ATTACHMENT IAW SRM 51-40-02.

ATA 5330

PUNCTURE IN FUSELAGE SKIN AT STATION 699 LT JUST BELOW STRINGER 24L. REPAIRED PUNCTURE IN FUSELAGE SKIN AT STATION 699 LT JUST BELOW STRINGER 24L IAW SRM 53-00-01 FIG 201.

ATA 3610

NUMBER 1 ENG PRE COOLER LINK SUPPORT ASSEMBLY RACEWAY & BUSHING WORN. REPLACED NR 1 ENG PRE COOLER LINK SUPPORT ASSEMBLY RACEWAY & BUSHING IAW AMM 36-11-15.

ATA 3350

EMERGENCY LIGHTING STRIP HAS WIRES PULLED FREE FROM CTR SEATING AT ROW 19. REPLACED BROKEN SOCKETS IAW SWMP 20-64-17. REFORMED OPERATIONS CHECK GOOD IAW AMM 33-51-00-715-200.

ATA 2560

RT SLIDE COMPARTMENT DOOR LATCH NR 3 IS WORN. REPLACED RT SLIDE COMPARTMENT DOOR LATCH NR 3 IAW AMM 25-65-09.

ATA 3350

FLOOR EMER ESCAPE PATHWAY FLOOR TRACK IS BROKEN AT 1J, 8J, 17J, 40J, 5A, 7A, 8A, 9A, 17A & 22A, REPLACEMENT REQUIRED CANNOT BE REPAIRED. R & R EMER ESCAPE PATHWAY FLOOR TRACK IAW B767-300 AMM 25-27- 09. )

ATA 3350

FLOOR EMER ESCAPE PATHWAY LIGHTING FLOOR TRACK END CAPS MISSING AT MID CABIN CROSS AISLE F4 GALLEY LT END LAVATORY F2 ALL 3 END CAPS 1A,10A & LAVATORY 3A. REPLACED FLOOR EMER ESCAPE PATHWAY LIGHTING FLOOR TRACK END CAPS AT MID CABIN CROSS AISLE F4 GALLEY LT END LAVATORY F2 ALL 3 END CAPS 1A,10A & LAVATORY 3A IAW AMM 33-51-00)

ATA 3097

RIGHT ENG ANTI-ICE VLV LIGHT INOPERATIVE. FOUND RT ENG ANTI- ICE VLV LIGHT BULBS GOOD. FOUND WIRING CONNECTOR LOOSE ON BACK OF LIGHT & BUTTON ASSEMBLY, SECURED WIRE. OPERATIONS CHECKED IAW AMM 30-21-03.

ATA 7200

NR 2 ENG FAILED BORESCOPE IAW JOB CARD A-72-307-C1-2. R & R NR 2 ENG.

ATA 2421

STATUS MESSAGE ILLUMINATED ON RT IDG VALVE . REPLACED IDG AIR OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24-11-07.

ATA 2121

FWD EQUIPMENT COOLING FAN VIBRATING CAN BE HEARD FROM SEAT 1C. R & R FWD EQUIP COOLING FAN, OPERATIONS CHECKED NORMAL.

ATA 3020

RT ENG ANTI-ICE VLV LIGHT INOPERATIVE. PLACED ON MEL DDG 30-21-02-01A, VLV OPERATIONS VERIFIED, MDDR 47124.

ATA 3350

FLIGHT DECK EMERGENCY EXIT, PORTABLE, LIGHT BATTERY IS DISCHARGED & WILL NOT RECHARGE. REPLACED & TESTED OK IAW AMM 33-51-01 207 & 208 OFF SN NSN & PN 10-0067-9.

ATA 7520

LT ENG DRAIN MAST DRIPPING FUEL, FOLLOWED LINE TO TCC VLV. R & R LPTCC VLV IAW AMM 75-24-01 206. COMPLIED WITH TEST 12, EEC, ECU ACTUATORS IAW AMM 71-00-00 PP 593, NO LEAKS, LPTCCV FULL TRAVEL OBSERVED.

ATA 2612

PRIOR TO DEPARTURE RT ENG FIRE LOOP 2 STATUS MESSAGE DISPLAYED. OIL CONTAMINATION FOUND AT FWD LOWER FIRE LOOP AREA, CLEANED & INSPECTED. FIRE TEST CARRIED OUT IAW AMM 26-11-01, TEST SATISFACTORY, MDDR 46629 CLOSED.

ATA 2840

EICAS MESSAGE FUEL QTY BITE MESSAGE. REPLACED FUEL QTY LOAD SELECT CONTROL PANEL IAW AMM 28-21-13 401. TESTED IAW AMM 28-21-13 EDSD MX PRACTICES OBSERVED IAW AMM 20-41-01 201.

ATA 3350

EMERGENCY LIGHTING FLOOR PROXIMITY LIGHTING, LIGHT LENS IS MISSING, RT SIDE FWD OVERWING ESCAPE DOOR. INSTALLED A SERVICEABLE LENS & LAMP COVER IAW AMM 33-51-10, OPERATIONS CHECKED OK.

ATA 7700

LEFT & RT PIMU MAINT MESSAGE. ACCOMPLISHED FIM71-01 FAULT TREE 810 CLEARED FAULT 155.15 A/B T25 SENSE DISAGREE & RT PIMU FAULT 352-15 A/B T25SENSOR DISAGREE FAULT ISOL PERFORMED, PIMU GND TEST IAW AMM 77-35-00 201NO FAULTS PRESENT OR RECORDED.

ATA 3350

R1 & L2 EXTERIOR EMERGENCY EXIT LIGHTS INOPERATIVE. RELAMPED, TESTED EXTERIOR EMERGENCY LIGHTING AT R1 & L2, PASSED IAW AMM 33-51-06 201.

ATA 2150

LEFT PACK INOPERATIVE LIGHT ON IN AUTO. PERFORMED BITE TEST ON PACK CONTROLLER PE AMM 21-25-00 NO FAULTS. MANUALLY CYCLED PACK CONTROL VLV OPERATIONS CHECKED NORMAL.

ATA 2150

LEFT PACK INOPERATIVE. R & R LT PACK CONTROL VLV IAW AMM 21-51-01 401. OPERATIONS CHECKED OK. PN OFF 396462, SN OFF 7100.

ATA 2150

RIGHT PACK TEMP CONTROL INOPERATIVE AUTO, STBY OK. R & R RT PACK TEMP CONTROL VLV IAW AMM 21-51-12. OPERATIONS & LEAK CHECKED GOOD.

ATA 3530

PORTABLE OXYGEN BOTTLE AT POSITION R4 UPPER READS 1600 PSI. R & R O2 BOTTLE IAW AMM 25-31-01.

ATA 2420

HMG CONTROL VLV LEAKING. R & R HMG CONTROL SHUT OFF VLV IAW AMM 24-25-03.

ATA 2422

STATUS MESSAGE STANDBY INVERTER DISPLAY. R & R STATIC INVERTER IAW AMM 24-33-05 TESTED OK.

ATA 2421

30 MIN AFTER TAKEOFF, EICAS MESSAGE RT GEN OFF, UNABLE TO RESET. DISCONNECTED FOLLOWED BY RT GEN OFF. R & R RT ENG IDG IAW AMM 24-11-01, OPERATIONS & LEAK CHECKED NORMAL.

ATA 7310

RIGHT ENG FUEL FILTER MESSAGE. R & R FUEL FILTER ELEMENT & LEAK CHECKED IAW AMM 73-11-02 OK.

ATA 3443

LEFT RADAR INOPERATIVE. PLACED ON MEL 34-43-01, MDDR 44939, PLACARD INSTALLED. DISPATCH NOTIFIED YK AT 18:31.

ATA 7310

FUEL DRIPPING FROM NR 1 ENG DRAIN MAST, FUEL DIRECT TUBE AFTER STATIC AIRCRAFT ENG RUN UP AT A RATE OF 7 DROPS PER MINUTE. DEFERRED TO MDDR 44901, FOUND FUEL TO BE COMING FROM THE TCC PORT OF THE LPT ACC VLV. LEAK RATE IS ACCEPTABLE FOR DISPATCH IAW AMM 71-71-00 PG 607. LEAK RATE OF 7 DROPS PER MIN LIMIT 35 DROPS PER MINUTE, TRANSFERRED TO NON-MEL.

ATA 3350

SEAT 22 - 23 JL HAS EMERGENCY FLOOR LIGHTING COVER MISSING. REPLACED SEAT JL EMERGENCY FLOOR LIGHTING COVER IAW AMM 33-51-10.

ATA 3350

RIGHT ROW 28 EMERGENCY FLOOR LIGHT ASSEMBLY BROKEN. REPLACED ROW 28 LIGHT ASSEMBLY & SECURED COVER. OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

ATA 3350

RIGHT ROW 29 EMERGENCY FLOOR LIGHT ASSEMBLY BROKEN. REPLACED LIGHT ASSEMBLY IAW WDM 33-51-17. SECURED WIRE BUNDLE & COVER, OPERATIONS CHECKED NORMAL IAW AMM 33-51-00.

ATA 3350

LEFT ROW SEAT NR 1 EMERGENCY FLOOR LIGHT ASSEMBLY INOPERATIVE. REPLACED LT ROW SEAT NR 1 EMERGENCY & NBSP FLOOR LIGHT ASSEMBLY IAW AMM 33-51-00, OPERATIONS CHECKED NORMAL.

ATA 3350

LEFT ROW SEAT NR 1 EMERGENCY FLOOR LIGHT LENS MISSING. REPLACED LT ROW SEAT NR 1 FLOOR LIGHT ASSEMBLY IAW AMM 33-51-00, OPERATIONS CHECKED NORMAL.

ATA 3350

RIGHT WING EMERGENCY LIGHT INOPERATIVE. CLEANED RT OVERWING EMERGENCY LIGHT SOCKET & RELAMPED IAW AMM 33-51-16, OPERATIONS CHECKED OK.

ATA 3350

LEFT AFT EMERGENCY EXTERIOR LIGHT INOPERATIVE. CLEANED LT AFT EXTERIOR EMERGENCY LIGHT SOCKET & RELAMPED IAW AMM 33-51-16, OPERATIONS CHECK OK.

ATA 3350

LEFT FWD EMERGENCY LIGHT BATTERY HAS A FUSE BLOWN. R & R LT FWD EMERGENCY POWER SUPPLY IAW AMM 33-51-07 OPERATIONS CHECKED GOOD.

ATA 3397

LEFT ROW SEAT 37 & 38 EMERGENCY LIGHT WIRE HARNESS PLASTIC COVER DAMAGED. REPLACE HARNESS & SEAT 37C LIGHT ASSEMBLY & PLASTIC COVER IAW WDM 33-51-17 & AMM 33-51-00.

ATA 3140

CABIN ALT AUTO NR 2 EICAS STATUS MESSAGE. PERFORMED FIM IAW 21 - 31 FAULT TREE 803, MESSAGE CLEARED ALL INDICATION NORMAL.

ATA 3442

LEFT WEATHER RADAR INOPERATIVE. R & R WAVE GUIDE X BAND ROTARY SWITCH IAW MM 34-43-04, OPS CHECKED GOOD.

ATA 3442

LT WEATHER RADAR SYSTEM INOPERATIVE. PERFORMED OPS TEST IAW AMM 34-43-00, WX RADAR SYS OPERATED NORMALLY.

ATA 4900

APU INOPERATIVE. R & R APU IAW 49-11-01-404--085, ADJUSTED AND TESTED IAW 49-11-725-001.

ATA 2612

RIGHT ENGINE FIRE LOOP NR 2 STATUS MESSAGE. ACCOMPLISHED FAULT ISOLATION MANUAL 26-11-806, OPS CHECKED AND INDICATION CHECKED NORMAL. OK FOR SERVICE.

ATA 4920

APU WOULD NOT START.

ATA 4940

APU NO START ON LANDING. CHECKED OIL LEVEL, CHECK OK, NO OIL ADDED. BITE TEST IAW AMM 49-61-05-742, APU ECU FOUND MULTIPLE FAULTS. CLEARED FAULTS. OPS CHECKED APU. APU CHECKED NORMAL ON GROUND. NO DEFECTS NOTED.

ATA 3442

RT WEATHER RADAR SYS WILL NOT TEST.

ATA 4920

APU WILL NOT START, THREE ATTEMPTS. APU FAULT LIGHT.

ATA 3350

FWD RT BATTERY CHARGER FOR EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY CHARGER ASSY IAW AMM 33-51-00, OPS CHECKED GOOD.

ATA 3442

RT RADAR INOPERATIVE, INSPECTED RT & LT WXR RADAR, FOUND OPS CHECK GOOD, FOUND RT WXR RADAR "ON BUTTON" LIGHT OUT, R & R BULB, OPS CHECKED WXR SYS GOOD IAW AMM 34-43-00/501, & 33-13-00/201.

ATA 3397

LEFT RED FWD GALLEY EMERGECNY LIGHT INOPERATIVE. SECURED WIRE IAW AMM 33-51-00, CHECKED NORMAL IAW AMM 33-51-00.

ATA 3350

RIGHT BODY SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD ;AMM 33-51-00 WDM 33-51-14.

ATA 2822

ON PRE-DEPARTURE, FOUND LT SPAR VALVE LIGHT ILLUMINATED, CIRCUIT BREAKER TRIPPED. R & R LT ACTUATOR IAW AMM 28-22-01, OPS CHECK NORMAL.

ATA 3350

AFT GALLEY ELECTRO LUMINESCENT CROSS AISLE EMERGENCY LIGHT INOPERATIVE. REPLACED ELECTRO LUMINESCENT CROSS AISLE EMERGENCY LIGHT, BS 1527 IAW SWPM 20-30-12. OPS TEST OK IAW; AMM 33-51-00.

ATA 3350

RIGHT EMERGENCY LIGHTS 1, 29, 31, 32 AND 39 ARE INOPERATIVE. REPLACED LAMPS IAW WDM 33-51-14. OPS CHECK NORMAL AMM 33-51-00.

ATA 3040

L3 WINDOW ARCING & INOPERATIVE.

ATA 3040

L3 WINDOW HEAT EICAS MESSAGE. TROUBLE SHOT IAW FIM 31-41-00, FAULT TREE 804, CHECKED SENSOR WIRES 217B-24, 217R-24 AT TERMINAL BLOCK 324. CHECKED WINDOW HEAT AT MAIN & SPARE PINS. CHECKED OK, REPOSITIONED TO MAIN POSITION IAW SPWM 28-86-00 SYS CHECKS OK IAW AMM 30-41-00, THIS CLEARS MDDR 41957.

ATA 5610

"LEFT SIDE WINDOW" EICAS MESSAGE ON LANDING.

ATA 3040

LT SIDE WINDOW HEAT EICAS IN FLT.

ATA 3040

LEFT SIDE WINDOW EICAS MESSAGE, QRH PROCEDURE ACCOMPLISHED. BITE PROCEDURE CARRIED OUT IAW FIM 30-41 FAULT TREE 804. BITE TEST GOOD, PERFORMED 30-41-00/201, TASK 802 AND FOUND OK. OPS TEST C/W IAW AMM 30-41-00. OPS CHECK GOOD, OK FOR SERVICE.

ATA 4940

APU FAULT ON START, ACCOMPLISHED QRH PROCEDURE, BOTH START ATTEMPTS UNSUCCESSFUL. APU BITE PROCEDURE PERFORMED IAW FIM 49-11 FAULT TREE 958 FIG 105. APU STARTED ON GROUND. AT FIRST ATTEMPT, OPS CHECKED GOOD. APU OK FOR FURTHER SERVICE.

ATA 2120

ELECTRICAL ODOR IN COCKPIT, CYCLED COCKPIT DOOR MASTER AND ODOR CEASED. VISUAL INSPECTION CARRIED OUT IAW AMM 05-51-56/201, NO EVIDENCE FOUND. FLIGHT COMPARTMENT DOOR INSPECTION CHECK CARRIED OUT IAW AMM 52-51-05/601, OPS CHECKED GOOD. OK FOR SERVICE.

ATA 4940

APU WOULD NOT START AFTER THREE ATTEMPTS, AFTER LANDING. FAULT LIGHT WAS ILLUMINATED. APU BITE PROCEDURE PERFORMED IAW FIM 49-11 FAULT TREE 958, FIG 103. APU STARTED ON GROUND AT FIRST ATTEMPT AND OPS CHECKED GOOD. APU OK FOR FURTHER SERVICE.

ATA 2150

LEFT PACK TEMP EICAS MESSAGE IN AUTOMATIC. STANDBY MODE WORKS OK. R & R COMPRESSOR OUTLET SENSOR ASSY, IAW AMM 21-51-06/401. OPS CHECKS GOOD, THIS CLEARS MDDR 41645, PLACARDS REMOVED.

ATA 2421

NR 2 ENGINE IDG, INTEGRATED DRIVE GENERATOR, OIL LEAK, R & R NR 2 ENGINE IDG, IAW AMM 24-11-01. LEAK CHECKS GOOD. DISCONNECT FUNCTION CHECKS GOOD.

ATA 3040

LEFT SIDE WINDOW EICAS MESSAGE ON APPROACH AND LANDING. TROUBLESHOOTING CARRIED OUT IAW FIM 30-41-FAULT TREE 804. GROUND OPS CHECKED GOOD. WINDOW ANTI-ICE BITE TEST PERFORMED, IAW AMM 30-41-00. TEST PASS, EICAS MESSAGE AND INOPERATIVE SWITCH LIGHT EXTINGUISHED, OK FOR SERVICE.

ATA 4900

APU ISOLATION VALVE STATUS MESSAGE. TESTED SYS IAW FIM 28-25 FAULT TREE 804 & TEST PASSED.

ATA 2560

FLASHLIGHT AT JUMPSEAT 2R INOPERATIVE.

ATA 2421

NR 2 IDG INOPERATIVE. R & R 2 IDG OIL COOLING TUBE ASSY IAW AMM 24-11-04, LEAK CHECKS GOOD. THIS CLEARS MDDR 41184.

ATA 2421

IN CRUISE FLT, RT GENERATOR DRIVE MESSAGE, ACCOMPLISHED QRH CHECKLIST. FOUND LOOSE LINE, TIGHTENED LINE IAW AMM 20-11-00, NR 2 GENERATOR RECONNECTED IAW AMM 24-11-01. LEAK CHECK AND OPS CHECKED FAILED IAW AMM 24-11-01.

ATA 3040

LT SIDE WINDOW HEAT INOPERATIVE IN FLIGHT. BITE TESTED WINDOW HEAT BOX IAW AMM 30-41-00. BITE TESTED GOOD.

ATA 3350

MID CROSSOVER ISLE EMERGENCY LIGHT MISSING. REPLACED EMERGENCY LIGHT ASSY IAW WDM 33-51-12. OPS CHECK SATISFACTORY.

ATA 3350

FWD RT ISLE EMERGENCY LIGHTING DIM. TROUBLESHOT IAW WDM 33-51-12 AND REPLACED RT SIDE EMERGENCY LTS POWER SUPPLY OPS TEST OK.

ATA 2421

GENERATOR DRIVE EICAS DURING CLIMB, CW QRH REF DDG. R & R NR 2 IDG REF MM 24-11-01-4, OPS LK CK GOOD.

ATA 4950

APU FAILED AFTER SELECTING APU BLEED TO OFF. R & R SURGE VALVE IAW AMM 49-53-01. OPS AND LEAK CHECKED OK.

ATA 2841

1200 POUNDS FUEL IMBALANCE AT TOP OF CLIMB BETWEEN LT & RT MAINS AFTER BURNING CTR TANK. REMAINS EQUAL AFTER BALANCING, RT MAIN TANK HAD 1200 MORE, PERFORMED FIM PROCD 28-41& NBSP; TASK 802 & FUEL QTY BITE TEST 28-41 TASK 852, NO FAULTS FOUND, NO LEAKS FOUND, NO FUEL MIGRATION NOTED UNABLE TO DUPLICATE.

ATA 2820

DEPARTED WITH FUEL IN ALL THREE TANKS AND ALL PUMPS ON. AT TOP OF CLIMB NOTED THAT FUEL WAS BEING USED FROM LT MAIN TANK AS WELL AS CENTER TANK. THIS LED TO A FUEL CONFIG EICAS MESSAGE. COMPLIED WITH QRH PROCEDURE, FUEL TRANSFER FEED ON, LEFT PUMP OFF WHICH STOPPED FUEL USED FROM LT TANK. FOUND LT WING FUELING SHUTOFF VALVE LIGHT ON. CYCLED SHUTOFF VALVE & CYCLED DEFUEL VALVE, OPS CHECKED GOOD, IAW AMM 28-21-12.

ATA 2613

RIGHT DUCT LEAK LIGHT ON. REPLACED RT PACK BAY OVERHEAT SENSOR IAW AMM 26-18-01-024-005-001 AND TESTED IAW AMM 26-18-00-715-001-002. ALL NOW GOOD, OK FOR SERVICE.

ATA 2621

CARGO FIRE BOTTLE ONE LIGHT ILLUMINATED DURING CRUISE, EICAS DISPLAYED. R & R NR 1 CARGO FIRE BOTTLE IAW AMM 26-33-02-40-131, TESTED IAW 26-23-00 ALL PASSED OK FOR SERVICE.

ATA 3020

RIGHT ENGINE ANTI-ICE VALVE TRANSIT LIGHT INOPERATIVE. OPS CHECKED RIGHT ENGINE ANTI-ICE VALVE IAW AMM 30-21-00. OPS CHECKED NORMAL.

ATA 3350

PAGE 7 OF 13, STEP 3 E. REVEALED FORWARD SEGMENT RT FROM SEAT LT TO SEAT 9 FLOOR MOUNTED AISLE PATH LIGHTTING SYS INOP. ALL OTHER EMERGENCY LIGHTING OPS CHECK NORMAL, IAW AMM 33-51-00/501. ACCOMPLISHED FIM 33-51 FAULT TREE 803, BLOCK 46. REPLACED POWER SUPPLY INVERTER FUSES IAW AMM 33-51-10/201, SYS FUNCTIONAL TEST OK IAW AMM 33-51-00.

ATA 3350

R1 DOORWAY EMERGENCY LIGHT IS NOT WORKING. R & R LAMP IAW AMM 33-51-10 -962-077.

ATA 3350

OVERHEAD EMERGENCY LIGHTS INOPERATIVE, AND MISSING LENS BETWEEN A3-A4 LAVS. R & R LAMPS ON IAW AMM 33-51-11 AND INSTALLED NEW LENS BETWEEN A3-A4 LAVS IAW .

ATA 3350

EMERGENCY LIGHTS INOP AT SEATS 19JL AND 28JL. R & R LAMPS ON EMERGENCY LIGHTS IAW AMM 33-51-11-002-001.

ATA 3350

EMERGENCY LIGHT IS OUT AT 20D,23AC,31JL,. R & R LAMPS IAW AMM 33-51-10-962-077.

ATA 2121

EICAS MESSAGE "AFT EQ EXHAUST FAN 1, ACCOMPLISHED EQUIPMENT COOLING SYS ADJ/TEST IAW AMM 21-58-00/501. CHECKS GOOD MESSAGE CLEARED.

ATA 4940

APU NO START, IGNITION NOT ENERGIZED DURING START SEQUENCE, FUEL OK. TROUBLESHOT IAW FIM 49-11, FAULT TREE 958, FIG 107.

ATA 2150

RT PACK UNABLE TO CONTROL TEMP IN AUTO. R & R PACK FLOW CONTROL; SHUTOFF VALVE IAW AMM 21-51-01, OPS CHECK GOOD.

ATA 2150

RT PACK UNABLE TO CONTROL TEMP IN AUTO MODE STANDBY.

ATA 3350

R4 DOOR EMERGENCY EXIT SIGN LENS COVER MISSING. REPLACED LENS COVER IAW AMM 33-51-01.

ATA 8011

NR 1 ENGINE STARTER DRIVE PAD LEAKING. R & R NR 1 ENGINE STARTER DRIVE PAD NO LEAKS NOTED.

ATA 2130

STATUS MESSAGE "CABIN ALT AUTO 1", BIT CABIN ALT AUTO CONTROLLER NO FAULTS FOUND MESSAGE CLEARED IAW AMM 21-31-00.

ATA 2560

FOUND L-1 DOOR AFT F/A EMERGENCY FLASHLIGHT NOT FLASHING. R & R L-1 DOOR AFT F/A EMERGENCY FLASHLIGHT BATTERY IAW AMM 25-64-00.

ATA 2740

ON CLIMBOUT EICAS MESSAGE STAB TRIM APPEARED AND REMAINED FOR DURATION OF FLT. R & R STAB TRIM POSITION TRANSMITTER/MODULE IAW AMM 21-48-01/401. OPS CHECK, LEAK CHECK GOOD. THIS CLEARS MDDR 37897. PLACARD REMOVED.

ATA 3442

RT WEATHER RADAR SYS INOPERATIVE. R & R RT WEATHER RADAR TRANCEIVER IAW AMM 34-43-01/401. OPS CHECKED GOOD. GROUND CHECKED GOOD.

ATA 2150

FWD EQUIPMENT COOLING EXHAUST FAN STATUS MESSAGE. R & R COOLING FAN IAW AMM 21-58-06/401. OPS CHECKED GOOD.

ATA 2197

AT 41000 FT AND START OF DESCENT RT PACK; RT PACK TEMP EICAS MESSAGE, RAN QRH AND PLACED PACK IN STBY MODE. FOUND CONNECTOR PLUG FOR THE COMPRESSOR OUTLET OVERHEAT TEMP SENSOR VERY LOOSE, RE-SECURED CONNECTOR PLUG IAW AMM 21-51-06, OPS CHECK NORMAL.

ATA 3350

DIM EXIT LIGHT BULB AT FWD OVERWING EXIT DOOR ON RT SIDE. BULB CHANGED.

ATA 5330

GAUGE NOTED ON LT FUSELAGE SKIN AT STA 1809.5 S-17L EXCEEDS ALLOWED LIMITS IAW SRM 53-00-01, FIG 101. REPAIR ACCOMLISHED IAW SRM 53-80-01, REPAIR 3, DETAIL V AND SRI-2910010860.

ATA 5315

CORROSION NOTED AT BS 347, RBL 45, FLOORBEAM EXCEEDS ALLOWED LIMITS IAW SRM 53-00-51. DAMAGE REPAIRED IAW SRM 53-00-51, REPAIR 1. REMOVED CORROSION SECTION OF BEAM CAP AND INSTALLED REPAIR CAP.

ATA 5315

CORROSION NOTED ON BS 266.5 LBL 15 FLOORBEAM EXCEEDS ALLOWED LIMITS IAW SRM 53-00-51. DAMAGE REPAIRED IAW SRM 53-00-51, REPAIR 1. REMOVING CORROSION SECTION OF BEAM CAP AND INSTALLING REPAIR/ REPLACEMENT CAP.

ATA 5315

CORROSION NOTED ON BS 325, LBL20, FLOORBEAM CAP EXCEEDS ALLOWED LIMITS IAW SRM 53-00-51. DAMAGE REPARIED IAW SRM 53-00-51. REPAIR 1. REMOVING CORROSION SECTION OF BEAM CAP AND INSTALLING REPAIR /REPLACEMENT CAP.

ATA 7261

STATUS MESSAGE " RT OIL FILTER" DISPLAYED. R & R RT ENGINE OIL FILTER ELEMENT IAW 79-21-04. PERFORMED ENGINE RUN, NO LEAKS NOTED, MESSAGE CLEARED.

ATA 4990

APU FAULT NO START AFTER LANDING. APU OIL LEVEL SHOWING 0.50, SERVICED APU OIL TO FULL, IAW AMM 12-13-04. OPS CHECKED GOOD. APU STARTED SUCCESSFULLY.

ATA 2612

LEFT ENGINE FIRE LOOP NR 1 INOPERATIVE. R & R LT ENG NR 1 UPPER AFT FIREWALL FIRE LOOP IAW AMM 26-11-02-401, OPS CHECKED GOOD.

ATA 7332

EVIDENCE OF FUEL LEAK ON LT ENGINE DURING WALK AROUND. R & R LT ENGINE FUEL PRESSURE TRANSMITTER, AMM 73-33-01, LEAK CHECKED NORMAL.

ATA 4990

APU RELIABILITY COLD START ACCOMPLISHED DURING FLT FL 400, FAILED ON ATTEMPT THREE, EGT 850 DEG, RPM 30 PERCENT, OIL QTY .25. SERVICED APU OIL TO FULL, CLEANED AND RESATED APU OIL QTY. TRANSMITTER CONNECTOR, APU STARTS AND OPERATES NORMALLY, QTY READS FULL, REF AMM 49-11-00.

ATA 4990

APU RELIABILITY COLD SOAK START, UNSUCESSFUL START ATTEMPTS. APU OIL QTY FOUND BELOW FULL (.25), SERVICED AS REQUIRED. SYSTEM STARTS/OPERATES GOOD IAW AMM 49-11-00/12-13-04.

ATA 2120

RT ACFT PACK HAS A DUCT LEAK. FOUND DUCT SEAL AT SLIP COUPLING BAD, DUCT DAMAGED, INSTALLED SERVICABLE LOANER DUCT. OPS & LEAK CHECK GOOD, IAW AMM 21-51-03; 21-51-00.

ATA 2913

RT ENGINE EDP IS LEAKING. R & R RT ENGINE DRIVEN PUMP IAW AMM 29-11-05. OPS & LEAK CHECKED OK.

ATA 5280

RT REAR NOSE DOOR SHOWS SIGNS OF DELAMINATION. REPAIRED IAW EO 6752A007 PART 1.

ATA 2841

RT WING FUEL QUANITY INDICATOR INOPERATIVE.

ATA 2612

STATUS MESSAGE FOR LT ENGINE FIRE LP1.

ATA 7320

STATUS MESSAGE FOR LT ENG FUEL FILTER. R & R LT ENG FUEL FILTER ELEMENT WITH NEW UNIT IAW AMM 73-11-02. LEAK, OPS AND GROUND CHECKED GOOD.

ATA 2612

STATUS MESSAGE "LT ENGINE FIRE LOOP 1". OPEN

ATA 2697

EICAS MESSAGE FOR LT ENGINE FIRE LOOP ONE, DISPLAYED. FOUND LOWER AFT ENGINE FIRE DETECTOR TERMINAL LOOSE. CLEANED & AMP; INSTALLED IAW AMM 26-11-02/406. OPS CKS GOOD.

ATA 3610

FOUND LEFT ENGINE PRSOV FAILING TO FULLY CLOSE DURING ENGINE RUNS. R & R NR 1 ENGINE PRSOV IAW AMM 36-11-09/212. OPS CHECKED GOOD.

ATA 3610

RT ENGINE BLEED OFF EICAS MESSAGE IN FLIGHT. SWAPPED PRV CONTROLLERS BETWEEN NR1 AND NR2 ENGINES. VERIFIED BAD PRV CONTROLLER. CURRENTLY INSTALLED ON NR1 ENGINE. R & R NR 1 ENG PRV CONTROLLER IAW AMM 36-11-19/401. OPS CHECKED GOOD.

ATA 7500

RT ENGINE BLEED OFF EICAS MESSAGE IN FLIGHT.

ATA 7500

RT ENG BLEED OFF EICAS MESSAGE.

ATA 7500

RIGHT ENGINE BLEED PRESSURE INOPERATIVE WITH ENGINE PRESSURE. REMOVED RIGHT ENGINE PRSOV, OPS CHECKED NORMAL.

ATA 3350

R4 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. R & R4 DOOR EMERGENCY LIGHT IAW AMM 33-51-16.

ATA 2565

ON WALK AROUND INSPECTION, MX FOUND L1 SLIDE PARTIALLY SEPARATED FROM SLIDE COVER (R & R L1 DOOR SLIDE. PLACARD REMOVED. REF MM 25-66-01)

ATA 2611

SMOKE LIGHT FAILED TO ILLUMINATE DURING EQUIPMENT COOLING TEST. REPLACED SMOKE DETECTOR LAW AMM 21-56-17.

ATA 2450

LEFT AC BUSS INTERMITTENT ON ENGINE SHUTDOWN. FOUND LT GENERATOR CONTROL CIRCUIT BREAKER T-1 CONTACT OPEN DURING FAULT. R & R LT GENERATOR CONTROL CIRCUIT BREAKER IAW AMM 24-22-03, SYS OPS CHECKED GOOD.

ATA 2780

LEADING EDGE SLAT ASYM EICAS MESSAGE. FOUND TORQUE TUBE COUPLING BACKED OFF AT NR 8 SLAT ROTARY ACTUATOR. RESECURED COUPLING IAW AMM 27-81-24/417, STOP CLEARANCES CHECKED GOOD.

ATA 2497

LEFT BUSS TIE AND LEFT GENERATOR FIELD TRIP OFF ON ENGINE SHUTDOWN. REPLACED RT BTB WITH SERVICABLE UNIT IAW AMM 23-22-03. OPS CHECKED GOOD. ENGINE GROUND TESTED OK IAW AMM 71-00-00/201.

ATA 4940

APU FAULT ON GROUND - IAW MCC. REPLACED APU BATTERY WITH REPAIRED UNIT IAW AMM 34-31-04. OPS /GND CHECK - GOOD. OK FOR CONTINUE SERVICE.

ATA 2120

LEFT PACK DUCT LEAK ILLUMINATED ON GROUND WITH PACK ON. FOUND AIR LEAK SECONDARY HEAT EXCHANGER DUCT COUPLING. REPLACED SEAL WITH NEW UNIT IAW AMM 21-51-02 LEAK AND OPS CHECKED GOOD.

ATA 4940

APU DIDN'T START ON TAXI-IN. THREE ATTEMPTS. PERFORMED OPS CHECK OF APU START SYS. IAW FIM 49-11-00. APU STARTED

ATA 2841

LEFT WING FUEL PANEL, RT MAIN FUEL QTY INDICATOR , DIGITS NOT LEGIBLE AND INTERMITTENT. REPLACED LT WING, RT MAIN FUEL QTY INDICATOR WITH REPAIRED UNIT IAW AMM 28-21-13.

ATA 4940

APU FAULT EICAS AFTER LANDING THREE ATTEMPTS. PERFORMED OPS CHECK OF APU IAW FIM 49-11-00, FIG 106A. NO FAULTS NOTED - GROUND CHECK OK.

ATA 2841

DURING REFUEL, NR 1 MAIN FUEL QUANTITY INDICATION BLANKED OUT. R & R FUEL PROCESSOR GROUND OP'S CHECKED NORMAL IAW MM 28-41-0.

ATA 3350

ISLE PATH LIGHT AT ROW 30R MISSING SEAT TRACK COVER LIGHT. LIGHT OPS OK.

ATA 7310

STATUS MESSAGE "RT ENG FUEL FILTER". R & R RT ENGINE FUEL FILTER IAW AMM 73-11-02. LEAK CHECKED GOOD.

ATA 2400

LEFT AC BUSS FAILED AFTER SHUTDOWN. PERFORMED BITE TEST OF BPCU, NO FAULTS LISTED. PEFORMED ENGINE RUN FOR BUS PICK UP VERIFICATION, SYS OPS CHECKED GOOD. FIM 24-20-00/104.

ATA 4940

APU WILL NOT START. REMOVED & REPLACED APU STARTER PER AMM 49-41-01, SYSTEM OPS CHECKED GOOD.

ATA 5297

FWR CARGO DOOR CAUTION LIGHT WHILE LEVELING OFF AT 34,000. QRH PROCEDURE COMPLETED AND AT APPROX 16,000 CAUTION LIGHT WENT OUT. PRESSURIZATION GAUGES INDICATED NORMAL. VISUALLY INSPECTED DOOR ON LANDING, ALL INDICATION CLOSED AND LATCHED. INSPECTED DOOR AND LATCHES NO DEFECT NOTED. WIGGLED WIRE CONDUIT TO CARGO DOOR AND CARGO DOOR LIGHT FLICKERED. DOOR VISUALLY CHECK CLOSED AND LATCH FWR CARGO DOOR.

ATA 2130

EICAS STATUS MESSAGE " CABIN ALT AUTO 2" DISPLAYED. PERFORMED FAULT ISOLATION IAW AMM 21-31-00/101, FIG 110, STEP 23 REF TO FIG 103 THRU STEP 5, SYS IS OK.

ATA 3350

EMERGENCY EXIT FLOOR LIGHT BETWEEN ROW 10-29 RT INOPERATIVE. REPLACED BATTERY CHARGER ASSY IAW AMM 33-51-10, OPS CHECKED GOOD.

ATA 2160

LEFT PACK TEMPERATURE EICAS MESSAGE. R & R PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-12. OPS CHECKED NORMAL.

ATA 2150

EICAS "LT PACK TEMP". OPERATES NORMAL IN STANDBY MODE.

ATA 2150

EICAS MESSAGE "LT PACK TEMP", COMPLIED WITH QRH AND SET AUTO SWITCH TO "N" MESSAGE WENT AWAY. PERFORMED FIM 21-51-00, FIG 103 AND TABLE B TEMP CONT VALVE STEP 1, SYS CHECKED NORMAL.

ATA 3411

AFTER ENGINE START, RT AUX PITOT EICAS MESSAGE DISPLAYED, RETURN TO BLOCKS. R & R RT LOWER PITOT PROBE, OPS AND LEAK CHECKED OK. OK FOR SERVICE IAW MM 34-11-01.

ATA 2420

LEFT GCU FAILED BPCU BITE TEST. R & R LT GCU, OPS CHECKED OK, OK FOR SERVICE IAW MM 24-11-00.

ATA 7313

NR 5 FUEL NOZZLE SEAL BROKEN. NR 2 ENG OTBD FUEL RAIL NR 5 NOZZLE. R & R NR 5 FUEL NOZZLE SEAL AT NR2 ENG O/B FUEL RAIL IAW BAMM 767 73-11-05 THRU STEP 5D(5). PERFORMED OPS AND LEAK CK IAW AMM 73-11-05, CHECKS GOOD.

ATA 8011

STARTER DUCT LINK ROD END BEARINGS WORN NR 2 ENGINE SIDE 10:00. REPLACED ROD ENDS IAW AMM 70-00-00. REINSTALLED STARTER DUCT LINK IAW AMM 80-11-05.

ATA 2697

FIRE LOOP ELECTRICAL HARNESS DAMAGED. NR 1 ENG AT 6 O'CLOCK POSITION NEAR DRAIN TUBE. REPAIRED FIRE LOOP WIRE HARNESS IAW WDM 20-10-13.

ATA 7700

STANDBY ENGINE INDICATOR FAILED TEST. REPLACED INDICATOR, BITE TESTED GOOD IAW AMM 77-41-01.

ATA 4950

GASKET DAMAGED ON FLOW SENSOR MODULE ON APU. REPLACED GASKET ON FLOW SENSER MODULE/ASSY IAW AMM 49-53-08.

ATA 2150

RT PACK TEMPERATURE CONTROL INOPERATIVE IN AUTO. R & R RT PACK TEMPERATURE CONTROL VALVE IAW AMM 21-51-12.

ATA 2421

AT ENGINE SHUTDOWN, LT A/C BUSS FAILURE, LT GENERATOR FIELD TRIPPED ALSO. RESET GENERATOR FIELD LIGHT IAW AMM 24-11-00, RAN ENGS IAW AMM 71-00-00, CYCLED POWER BETWEEN ALL BUSSES. OPS GOOD, NO FURTHER FAULTS NOTED.

ATA 3411

ON LANDING, RT AUX PITOT EICAS MESSAGE APPEARED. FOUND CIRCUIT BREAKER TRIPPED, RESET IAW SWPM 20-60-05. PERFORMED SYS TEST IAW AMM 30-31-00. OPS CHECKED GOOD.

ATA 2150

RIGHT PACK TEMP EICAS MESSAGE. IN STANDBY MODE, OPERATED NORMALLY. AFTER QRH PROCEDURE, MESSAGE CLEARED. OPEN

ATA 2150

RIGHT PACK TEMP EICAS MESSAGE. RT PACK SELECTOR POSITIONED TO "N" IAW QRH PROCEDURES, MESSAGE CLEARED. PERFORMED RT PACK TEMP CONTROLLER BIT IAW FIM 21-51-00. NO FAULTS NOTED & RELEASED OK FOR SERVICE.

ATA 2133

OUTFLOW VALVE INDICATOR INDICATES .5 OPEN IN CRUISE. PERFORMED BITE ONE BOTH CPC'S, NO FAULT FOUND IAW AMM 21-31-00, SYS. CHECKED NORMAL IN BOTH AUTO AND MANUAL MODES. OK FOR SERVICE.

ATA 2130

CABIN ALTIMETER AUTO 1 STATUS MESSAGE, BITE CHECK COMPLIED WITH IAW AMM 21-31-00, NO FAULTS FOUND.

ATA 2130

CABIN ALTITUDE AUTO 1. PERFORMED CABIN CABIN PRESSURE CONTROLLER BITE TEST IAW FIM 21-31-00/105. NO FAULTS NOTED MESSAGE CLEARED.

ATA 4940

APU FAULT ON START. PERFORMED APU BITE PROCEDURE IAW FIM 49-11-00/103, NO FAULTS NOTED. RESET ECU, APU START NORMAL ON SECOND ATTEMPT.

ATA 2565

L1 DOOR SLIDE INADVERTENTLY DEPLOYED. R & R L-1 DOOR SLIDE IAW AMM 25-66-00, PG 201 &AMP; AMM 25-66-01, 401 & NBSP; INSTALL CHECKED GOOD.

ATA 2565

L1 DOOR SLIDE WAS ACCIDENTALLY DEPLOYED AT GATE. REMOVED DEPLOYED SLIDE AND TRANSFERRED TO MDDR 29960, MEL 52-11-04-01 CAT. "A" ONE DAY.

ATA 4990

APU GENERATOR DIFFERENTIAL PRESSURE INDICATOR CHECK. ACCOMPLISHED W/C A-49-024-C1 APU/GEN DIFFERENTIAL PRESSURE INDICATOR CHECK. R & R SCAVENGE FILTER IAW AMM 49-27-03/401, LEAK CHECKED GOOD.

ATA 4940

APU IGNITOR PLUG TO BE REPLACED AS PRECAUTION DUE TO SLOW START. R & R APU IGNITOR PLUG IAW AMM 49-41-02 & NBSP; OPS CHECKED GOOD.

ATA 3150

RT OIL FILTER STATUS MESSAGE. STATUS MESSAGE ON ENGINE START SUSPECT EXTREME COLD CONDITIONS CAUSED MESSAGE. ALL TEMPS AND PRESSURES NORMAL, NON BY-PASS CONDITION. MESSAGE CLEARED AFTER NORMAL TEMPERTURE RANGE ACHIEVED REF AMM 79-35-00. CHIP DETECTOR CLEAN. LEAK CHECKED GOOD.

ATA 2130

STATUS " CAB ALT AUTO 1", PERFORMED FIM 21-31-00 FIG 103, NO FAULTS FOUND. OK FOR CONTINUED SERVICE, GROUND CHECKS GOOD IAW AMM 21-31-00)

ATA 2560

SQUIB TEST PANEL ON TEST 1 "EMERGENCY ESCAPE" RT DOES NOT ILLUMINATE DURING TEST. TROUBLESHOT IAW WDM 25-65-12, FOUND TIME DELAY RELAY FAULTY. R & R, REF AMM 20-00-00.

ATA 2560

CENTER OBSERVERS SEAT SMOKE GOGGLES LENS CRACKED (TRANSFERRED TO MDDR 28903. MEL 25-11-02-01B; OBSERVERS SEAT BLOCKED OUT FOR USE.)

ATA 3040

RIGHT SIDE WINDOW HEAT INOPERATIVE, NR 2 WINDOW. MX R & R HEAT CONTROLLER IAW AMM 30-41-01. OPS CHECKED GOOD.

ATA 7700

RT ENGINE CONTROL MESSAGE. PEFORMED "PIMU" RESET PROCEDURES IAW FIM 73-21-00. NO FAULTS NOTED. MESSAGE CLEARED.

ATA 3150

EICAS MESSAGE "RT SIDE WINDOW". PERFORMED FIM 30-41-00, FIG 103, ALL COMPONENTS CHECKED GOOD, OK FOR SERVICE.

ATA 2840

FUEL QUANTITY CHANNEL MESSAGE, RT DISPLAYED STATUS MESSAGE. RESET FUEL QTY PROCESSOR IAW FIM 28-41-00/101, FIG 106. FAULT CLEARED NO FURTHER ISSUES.

ATA 7700

STATUS MESSAGE RT ENGINE CONTROL. PEFORMED FIM TABLES IAW FIM 73-21-00/71-PIMU. FAULT CLEARED, MESSAGE CLEARED PERFORMED GROUND TEST IAW FIM 71-PIMU. NO DEFECTS NOTED.

ATA 2560

AFT RT F/A SEAT EMERGENCY FLASHLIGHT INOPERATIVE. ITEM TRANSFERRED TO MDDR 28497. MEL 25-63-04.

ATA 3040

LT WINDOW ARCING. R & R WINDOW HEAT CONTROL WITH REPAIRED UNIT IAW AMM 30-41-01, OPS CHECKED GOOD.

ATA 5610

LT WINDOW CRACKED. REMOVED & INSTALLED NEW WINDOW AMM 56-11-01, INSTALLATION CHECKED GOOD, AND OPS CHECKED AMM 30-41-01.

ATA 2133

CABIN AUTO INOPERATIVE MESSAGE, FOUND INSULATION BLOCKING PRESSURE RELIEF VALVE. REMOVED INSULATION. CLEARED FAULT ON PRESSURE CONTROLLER. GROUND CHECKS GOOD IAW AMM 21-31-00, 21-32-00.

ATA 2612

APU FIRE WARNING TEST HAS NO SPEAKER AURAL WARNING. REPLACED WARNING MODULE "M1000" IAW AMM 31-51-04. OPS CHECKED GOOD. REPLACED PRINTED CIRCUIT CARD "M618" IAW AMM 31-51-04. OPS CHECKED GOOD.

ATA 2612

APU FIRE WARNING TEST HAS NO SPEAKER AURAL WARNING FOR T/S, WITH DOM'S APPROVAL IAW ETOPS MX MANUAL 5.1.5., SWAPPED M616 AND M621 POWER SUPPLY UNITS FOR TROUBLESHOOTING. NO HELP. RETURNED TO ORIGINAL POSITIONS. NG.)

ATA 2820

FUEL MIGRATION FROM RT TO LT TANK. LT 18.2, CTR 0.2, RIGHT 3.8. FOUND DURING MX CHECK. (REPLACED RT TANK INBD FUELING SHUT-OFF VALVE IAW AMM 28-21-02, REF:W/O 7507, REPLACED RT MAIN TANK DEFUEL VALVE IAW AMM 28-26-01, REF W/O 7507, R & R FUEL PANEL DOORS 631BB, 632BB, 632DB IAW AMM 28-11-02; 28-11-01 LEAK CK GOOD. LEAK CHECK GOOD-NO FUEL MIGRATION OVER 18 HRS - NO LEAKS C/T FUEL PANELS AND VALVES. REF W/O 7507 PARTS - R & R SHUTOFF VALVE OFF PN 60160-5, OFF SN 6834, ON PN 60160-5, ON SN 5693 PARTS - R & R DEFUEL VALVE.

ATA 2820

FUEL MIGRATION FROM RT TO LT TANK.; LT 18.2,; CENTER 0.2, RT 3.8. FOUND DURING MX CHECK. OPEN

ATA 3350

EXTERNAL EMERGENCY LIGHT BURNED OUT AT R2 DOOR, RT ABOVE FLAP, LT AFT OF FLAP. R & R BULB.

ATA 4940

APU WILL NOT START. R & R APU STARTER IAW MM 49-41-01. OPS CHECK OK. NO LEAK NOTED

ATA 4990

APU FAILED TO START TWICE AFTER LANDING, OIL QTY SHOWS .25 (SERVICED APU ENGINE OIL WITH 1.5 QTS IAW AMM 49-90-00. NO LEAKS NOTED IN APU COMPARTMENT APU OPERATES NORMAL. BITE CHECK SHOWS NO FAULTS.)

ATA 5330

PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS WERE REMOVED AND THE DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED AT EACH AREA. FASTENERS INSTALLED. ALL WORK WAS ACCOMPLISHED IAW INSTRUCTIONS SR 1-1993034429.

ATA 5315

DURING ROUTINE C4/A4 CHECK MX, DISCOVERED CORROSION ON THE FLOORBEAM UPPER TEE FORWARD FLANGE AT BS 1518 BETWEEN LBL 25.5 AND LBL 35.5. DAMAGED SECTION OF THE FLOORBEAM TEE WAS REPAIRED IAW SRM 53-10-51, FIG 201, REPAIR 4. THE REPAIR IS CLASSIFIED AS A CATAGORY A PERMANENT REPAIR IAW SRM 51-00-06.

ATA 5330

DURING C-CHECK, FUSELAGE SKIN WAS FOUND WITH A SMALL PUNCTURE AT BS 1881-1890, S6-8L. DAMAGED AREA TRIMMED OUT AND A REPAIR DOUBLER INSTALLED IAW SR 1- 2006471601.

ATA 5330

PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC WAS PERFORMED. REPLACEMENT FASTENERS INSTALLED. WORK ACCOMPLISHED IAW SR 1-1993034429.

ATA 5330

PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED. REPLACEMENT FASTENERS INSTALLED. ALL WORK WAS ACCOMPLISHED IAW INSTRUCTIONS SR 1-1993034429.

ATA 5330

PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS 307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED, HFEC WAS PERFORMED, REPLACEMENT FASTENERS WERE INSTALLED. ALL WORK WAS ACCOMPLISHED IAW INSTRUCTIONS SR 1-1993034429.

ATA 5330

PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. THE BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS BECAUSE THEY WERE LOCATED AT FASTENER LOCATIONS. REPAIR ACCOMPLISHED.

ATA 5320

CORROSION ON KEELBEAM SUPPORT PANEL BRACE, BELOW PANEL 139E2. REMOVED CORROSION ON SUPPORT PANEL BRACE. FOUND CORROSION OUT OF LIMITS. R & R SUPPORT IAW SRM 51-10-02, 51-40-02. 53-30-12.

ATA 5743

LT MLG AFT TRUNNION BEARING, AFT ACCESS CAVITY EDGE HAS SEVERAL GOUGES. REPAIRED LT MLG AFT TRUNNION BEARING AFT ACCESS CAVITY IAW SRM 51-70-13.

ATA 5220

THE STEP PORTION OF THE RT AFT OVERWING ESCAPE HATCH ASSY WAS FOUND MISSING. A REPLACEMENT STEP WAS FABRICATED.

ATA 5330

DURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S33-35R AND FROM BS 307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC PERFORMED. REPLACEMENT FASTENERS INSTALLED. WORK ACCOMPLISHED IAW SR 1-1993034429.

ATA 5330

DURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC PERFORMED. REPLACEMENT FASTENERS INSTALLED. WORK ACCOMPLISHED IAW SR 1-1993034429.

ATA 5330

DURING C-CHECK, PREVIOUSLY BLENDED AREAS WERE FOUND ON THE RT FWD FUSELAGE SKIN BETWEEN S-33R TO S-35R AND FROM BS307-384. BLENDS DID NOT MEET SRM ALLOWABLE DAMAGE LIMITS. FASTENERS REMOVED AND DISCREPANT AREAS REWORKED. HFEC WAS PERFORMED. REPLACEMENT FASTENERS INSTALLED. WORK ACCOMPLISHED IAW SR 1-1993034429.

ATA 5315

DURING ROUTINE C4/A4 CHECK MX DISCOVERED CORROSION ON THE UPPER TEE OF FLOORBEAM BS 1480 BETWEEN LBL 34 AND 60.5. THE DAMAGED SECTION OF THE FLOORBEAM TEE WAS REMOVED AND A NEW SECTION SPLICED IAW SRM 53, FIG 201, REPAIR 1. THE REPAIR IS CLASSIFIED AS A CATAGORY A PERMANENT REPAIR IAW SRM 51-00-06.

ATA 5315

DURING THE C4 PLUS A4 CHECKS, CORROSION WAS DETECTED AT EXISTING NUT PLATES (10 PLACES) ON THE UPPER SURFACE OF THE LOWER TEE OF FLOORBEAM 146T5119-1 AT BS 1502. NUT PLATES WERE LOCATED AROUND CUTOUTS IN THE LOWER TEE OF FLOORBEAM AT LBL 2, LBL 7, LBL 14, LBL 21.5, LBL 28, LBL 36, LBL 42, LBL 50, AND LBL 52. THERE WAS ALSO CORROSION AT THE NUT PLATE AT RBL 31 BUT THERE IS NO CUTOUT AT THIS AREA. CORRODED AREAS AROUND THE CUTOUT AREAS WERE BLENDED AND THEN THE CUTOUTS (9 PLACES) WERE INCREASED WHILE MAINTAINING PRODUCTION PROFILE TO BRING MATERIAL THICKNESS BACK TO FULL THICKNESS.

ATA 5711

CORROSION ON SPAR CAP STA 176.000. REMOVED LIGHT CORROSION BETWEEN FASTENERS PERFORMED LT THICKNESS INSPECTION FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED AREA.

ATA 5310

STRUCTURE CRACKED AT BS 1081 WHERE HYDRAULIC LINE PASSES THROUGH OTBD OF LT OVERWING SLIDE CYLINDER FWD END. CUTOUT DAMAGED AREA AND INSTALLED REPAIR DOUBLER.

ATA 5347

THE AFT F/A STATION TIE DOWN FITTING INSTALLED AT BS 1519.2, LBL 18.50 FOUND CORRODED. FABRICATED AND INSTALLED REPLACEMENT FITTING IAW EO IH-53-0460, REV 01, DWG 6-1041-00-000, REV 1 AND DWG 6-1041-00-001, REV 0.

ATA 5755

NR 1 SPOILER LOWER SKIN DENTED 1.115 DIA, 0.045" DEEP. REPARIED DAMAGE.

ATA 5315

CORROSION ON FLOORBEAM, BS 1518, LBL 30. REMOVED CORROSION, FOUND OUT OF LIMITS. CUT OUT DAMAGE AND ACCOMPLISHED REPAIR.

ATA 5340

AFT GALLEY MOUNT FITTINGS SHOWED SIGN OF SURFACE CORROSION. R & R GALLERY MOUNT FITTINGS.

ATA 2530

THE FWD GALLEY WAS FOUND WITH HONEYCOMB PANEL DAMAGE. CORROSION WAS FOUND ON THE FWD U-CHANNEL AND THE COUNTERTOP SURFACE WAS FOUND DAMAGED. REMOVAL OF THE BONDED COUNTERTOP SURFACE RESULTED IN MINOR DAMAGE TO THE UNDERLYING COMPOSITE PANEL. CORROSION WAS ALSO FOUND ON THE VERTICAL ANGLES OF THE GALLEY. (A NEW U-CHANNEL AND COUNTERTOP WORK SURFACE WAS FABRICATED FROM THE SAME MATERIAL AS THE OEM CHANNEL AND INSTALLED IAW THE CMM. THE VERTICAL ANGLES (FACE TRIM) WERE TRIMMED TO REMOVE ALL CORROSION AND NEW SECTIONS WERE FABRICATED, BONDED INTO PLACE. THE COMPOSITE STRUCTURE WAS REPAIRED USING CMM REPAIR MATERIALS AND TECHNIQUES.)

ATA 2530

DURING C-CHECK, REAR GALLEY FOUND CORRODED. FACE TRIM WAS REPLACED, ANY REMAINING DAMAGE WAS REPAIRED IAW CMM 25-38-386, REV 2.

ATA 5410

NR 2 ENG OTBD STRUCTURE FWD LOWER CORNER OF THE ACCESS CUTOUT FOR FIRE BOTTLE WITH A CRACKED LOWER CORNER. REMOVED PANEL, STOPPED DRILL THE CRACK, PERFORMED NDT INSP. REPAIRED THE DAMAGE AREA AND INSTALLED THE PANEL.

ATA 5330

DURING THE C4/A4 CHECK, A 3.5 INCHES WIDE (A) WITH A DEPTH (Y) OF 0.030" DENT WAS FOUND ON THE FUSELAGE SKIN AT BS 1197+132, BETWEEN S39L AND S39R. DENT WAS DETERMINED TO BE WITHIN LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. HFEC INSPECTION DETECTED A CRACK AT THE DENT AREA.

ATA 5730

DURING ROUTINE C-CHECK, DISCOVERED DENTS/GOUGES ON THE LOWER SKIN PANEL AT MULTIPLE LOCATIONS, BETWEEN STRINGERS 5 AND 12, AND BETWEEN WS 250 AND WS 720. DAMAGED AREAS WERE BLENDED OUT. THE MAXIMUM BLEND DEPTH WAS 0.016" WHICH IS AT THE AREA COMMON TO STRINGER 5, AT APPROX WS 250. THE BLENDED AREAS AND EFFECTED FASTENER HOLES WERE HFEC INSPECTED. ROTO PEENED AND REFINISHED IAW THE SRM. REPAIRED IAW SRM 51-00-06.

ATA 5321

FWD CARGO FOUND SMALL CRACK AT FLOOR PANEL. REMOVED DAMAGED CRACKED FLOOR PANEL, FABRICATED IAW SRM 53-30-53 AND INSTALLED.

ATA 5315

CORROSION FOUND ON FLOORBEAM. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. TREATED AND PRIMED.

ATA 5315

CORROSION ON FLOORBEAM BS 1480 LBL 32. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW REF SRM 53-00-51, REPAIRED IAW SRM 53-00-51.

ATA 5755

DURING THE PRESENT C-CHECK, INSPECTION REVEALED A DENT ON THE UPPER SURFACE OF NR 3 SPOILER NEAR CENTER HINGE (FIG 1). DENT MEASURED 0.002" DEEP, 0.495" IN WIDTH AND WAS LOCATED 30" FROM THE INBD EDGE AND 19.75" FROM THE T/E. MX PERFORMED BOND TEST IAW NDTM 51-00-01 AND FOUND NO DELAMINATION. REPAIR WAS PERFORMED IAW SRM 51-70-17 AS STATED IN SRM 57-70-01, FIG 201.

ATA 5315

FOUND CORROSION ON FLOORBEAM. REMOVED CORROSION ON FLOORBEAM IAW SRM 51-10-02. FOUND TO BE IN LIMITS IAW 53-00-51.

ATA 5315

FOUND CORROSION ON FLOORBEAM BS 1502 LOWER FWD FLANGE FROM LBL 7 TO LBL 45. REPAIRED FLOORBEAM IAW RES -WI 2003850-22.

ATA 5315

FOUND CORROSION ON FLOORBEAM BS 1502 LBL 29. REMOVED CORROSION IAW SRM 51-11-00.

ATA 5720

LT WING ACCESS PANEL SUPPORT AT WBL 289.45 HAS CORROSION. REMOVED CORROSION. FOUND TO BE WITHIN LIMITS. TREATED AND PRIME.

ATA 5730

DENTS FOUND ON LOWER SKIN AT WS 210 WS 546, WS 616, WS 694 WS 720 AND WS 864. ALL DENTS WITHIN LIMITS IAW SRM 57-20-01. REWORKED AREAS IAW RES NR 2003862-27, REV 12 AND REV B PERFORMED. LEAK CHECKED.

ATA 5314

CORROSION ON KEELBEAM. REMOVED CORROSION ON KEELBEAM IAW SRM 53-50-12 AND FOUND TO BE IN LIMITS AND SHOT PEENING AT KEELBEAM AREA REF SOPM 20-10-03. TREAT AND PRIMER, TOP COAT IAW SRM 51-20-01.