N649GT

Part: LANYARD — UNSECURE (ELT) · airframe 99,489 hrs · 25,598 cycles

ELT BY LAVATORY HAS STRING HANGING. SECURED THE ELT STRING IAW AMM 25-63-03. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED.

Part: SKIN — DAMAGED (ZONE 400) · airframe 99,372 hrs · 25,560 cycles

AIRCRAFT STRUCK BY LIGHTNING. LIGHTNING STRIKE DAMAGE FOUND ON R/H INLET COWL 3:00 POSITION(<P>PERFORMED PHASE 1 LIGHTNING STRIKE INSPECTION IAW B767 AMM 05-51. R/H ENGINE COWL DAMAGE FOUND WITHIN LIMITS IAW SRM 54-15-01-1A-1. NO FURTHER DEFECTS NOTED</P>)

Part: HF COMM — ABNORMAL · airframe 99,278 hrs · 25,532 cycles

BOTH HF COMM RADIO INOP AND SELCAL INOP(<P>T/S WITH FIM 23-11 FT 804. RESECURED CONNECTIONS AT HF ANTENNA. OPS CHK GOOD PER AMM 23-11-00</P>)

Part: COVER — DETACHED (ZONE 200) · airframe 99,270 hrs · 25,529 cycles

EMERGENCY EXIT LIGHT COVER FELL OFF L1 DOOR. INSTALLED EMERGENCY EXIT LIGHT COVER IAW AMM 33-51-03. NO FURTHER DEFECTS NOTED.

Part: BRACKET — DAMAGED (ZONE 200) · airframe 98,865 hrs · 25,391 cycles

FLIGHT DECK FIRE EXTINGUISHER HOLDING BRACKET INOPERATIVE. RE-ADJUSTED FLIGHT DECK FIRE EXTINGUISHING BRACKET IAW B767 AMM 26-26-02. OPS CHECK GOOD. NO FURTHER DEFECTS NOTED AT THIS TIME.

Part: LATCH — OUT OF ADJUST (ZONE 200) · airframe 98,755 hrs · 25,353 cycles

ON LANDING, FO WINDOW NR 2 EXTERNAL EMERGENCY ESCAPE HANDLE UNLATCHING. ADJUSTED FO WINDOW #2 EMERGENCY ESCAPE HANDLE LATCH & PERFORMED SYSTEM OPS CHECK OF EXTERNAL ESCAPE HANDLE IAW AMM 56-11-04. OPS CHECK GOOD AT THIS TIME. NO OTHER DEFECTS NOTED.

Part: WEDGE — DAMAGED (ZONE 500 SLAT) · airframe 98,667 hrs · 25,324 cycles

LH WING, SLAT# 4, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 4, TRAILING WEDGE, UPPER SURFACE WITH DENTS (11 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG.201 SHEET 1 AND SEVEN DENTS FOUND WITHIN LIMITS IAW SRM 57-43-02-1A-2 NOTE K DETAIL VI REV.52. NO FURTHER DEFECTS NOTED. (SN: 000460 &AMP; PN 114T4104-41).</P>)

Part: WEDGE — DAMAGED (ZONE 500 SLAT) · airframe 98,667 hrs · 25,324 cycles

LH WING, SLAT# 3, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 3, TRAILING WEDGE, UPPER SURFACE WITH DENTS (7 EAS) WERE EVALUATED AND TWO DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEET 1 AND FIVE DENTS FOUND WITHIN LIMITS IAW SRM 57-43-02-1A-1 NOTE K DETAIL VI. NO FURTHER DEFECTS NOTED. (SN 000460 &AMP; PN 767-3602-411).</P>)

Part: WEDGE — DAMAGED (ZONE 500 SLAT) · airframe 98,667 hrs · 25,324 cycles

LH WING, SLAT# 1, UPPER SIDE, WEDGE WITH HAIL DAMAGE.(<P>LH WING, SLAT# 1, TRAILING WEDGE, UPPER SURFACE WITH DENTS (9 EAS) WERE EVALUATED AND FOUR DENTS WERE REPAIRED IAW SRM 57-43-02-2R-1 FIG.201 SHEET 2 PAG.2-3 AND SRM 51-70-10-2R-4 PAG.1,3,7 FIG- .201 SHEET 1 AND FIVE DENTS FOUND WITHIN LIMITS IAW SRM 57-43-02-1A-2 NOTE K DETAIL VI. NO FURTHER DEFECTS NOTED. (SN: 000468 &AMP; PN 767-3600-353).</P>)

Part: BUSHING — CORRODED (ENGINE MOUNT) · airframe 98,667 hrs · 25,324 cycles

FRETTING CORROSION ON BUSHING P/N BACB28X20E085 INSTALLED IN THE FWD SHEAR PIN HOLE OF THE FWD ENGINE MOUNT (P/N 311T2211-7), RH SIDE.(<P>BUSHING WAS REPLACED (P/N BACB28X20E085) PER DWG 311T2211-7 ID SHEET 1. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — DENTED (SONE 500 SPOILER) · airframe 98,667 hrs · 25,324 cycles

LH WING, SPOILER #3, LOWER SURFACE, DENT AT 10.5" FROM AFT EDGE AND 6" FROM OUTBD EDGE.(<P>AFFECTED AREA WAS REPAIRED IN ACCORDANCE WITH B767 SRM 57-70-01-2R-1 PAG 2-5 FIG 201 SHEET 4 AND SRM 51-70-03-0G-0 PAR 5. L FIG 16. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CRACKED (ZONE 100) · airframe 98,667 hrs · 25,324 cycles

SERVICE DOOR CUTOUT, AFT LOWER CORNER FUSELAGE FOUND CRACKS INDICATION, ON OPEN HOLES: #4, POSITION 8 O'CLOCK (SKIN AND BEAR STRAP) APPROX AND HOLE #5, POSITION 8 O'CLOCK (SKIN) AND 2 O'CLOCK (BEAR STRAP) APPROX.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 REPAIR 1 DETAIL I AND TRE6753723 (CMA-TLS-25-0042). NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 98,667 hrs · 25,324 cycles

RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION AROUND FASTENERS. L= 6.0 IN W=1.5 IN.(<P>RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT FRONT SPAR FROM STA 0.0 TO STA 107.927, CORROSION LEVEL 2 AROUND FASTENERS. L= 6.0 IN W=1.5 IN, WAS REPAIRED IAW CMA-TLS-25-0045. NO FURTHER DEFECTS NOTED.</P>)

Part: BEAR STRAP — CRACKED (ZONE 100) · airframe 98,667 hrs · 25,324 cycles

FORWARD ENTRY DOOR CUTOUT AFT LOWER CORNER WITH TWO CRACK INDICATIONS AT HOLE #5: 1. ON SKIN AT 3 O´CLOCK POSITION. 2. ON BEAR STRAP AT 9 O´CLOCK POSITION.(<P>CRACKS WERE REPAIRED PER SRM 53-10-01-2R-1 FIGURE 201 DETAIL III. NO FURTHER DEFECTS NOTED.</P>)

Part: FUEL TANK — LEAKING (CENTER) · airframe 98,667 hrs · 25,324 cycles

FUEL LEAK AT CENTER TANK BETWEEN STGR L-6 AND LBL 97.5.(<P>THE SEALANT IN THE FUEL TANK STRUCTURE WAS REPAIRED PER AMM 28-11-00-308-013. NO FURTHER DEFECTS NOTED.</P>)

Part: SKIN — CORRODED (ZONE 300) · corrosion level 2 · airframe 98,667 hrs · 25,324 cycles

RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION.(<P>RH OUTBD HORIZONTAL STABILIZER, UPPER SURFACE, AT REAR SPAR WITH CORROSION LEVEL 2 WAS REPAIRED IAW CMA-TLS-25-0045. NO FURTHER DEFECTS NOTED.</P>)

Part: EVAS UNIT — INOPERATIVE (ZONE 200) · airframe 98,424 hrs · 25,242 cycles

DURING EVAS OPS CHECK, FOUND CAPTAINS EVAS INOP (BLOWER INOP)(<P>REMOVED &AMP; REPLACED EVAS CAPTAINS SIDE AS PER B-767-300 AMM 25-60-99. OPS CHECK GOOD.</P>)

Part: SKIN — NO DISCREPANCY (ZONE 100) · airframe 98,383 hrs · 25,228 cycles

LIGHTNING STRIKE AT 17000 FT. SUSPECT STRIKE IMPACT ON CAPTAIN'S SIDE IN THE VICINITY OF THE NOSE.(<P>PERFORMED LIGHTNING STRIKE DAMAGE PHASE INSPECTION IAW B767 AMM 05-51-19. FOUND LIGHTNING IMPACT AND POSSIBLE EXIT POINT AT 2 TO 3 O'CLOCK POSITION BETWEEN STA 92.5 TO 100.25. DAMAGE WITHIN LIMITS PER SRM 53-10-72-1A-1. NO FURTHER DEFECTS NOTED AT THIS TIME.</P>)

Part: WIRE HARNESS — DAMAGED (APU) · airframe 98,235 hrs · 25,176 cycles

AIR TURN BACK DUE TO APU SHUTDOWN IN FLIGHT. LEFT GENERATOR ON MEL SO APU IS REQUIRED. APU RESTARTED ON 3RD ATTEMPT.(<P>PER ENGINEERING AND MANAGEMENT REQUEST, R/R APU HARNESS WIRE PN: W020-212R-24 IAW WDM 49-14-11-1 AND SWPM 20-25-00 AND SWPM 20-60-00. DUE TO APU BITE FLAG FOR OVERSPEED AFTER WIRE REPLACEMENT PERFORMED MULTIPLE STARTS OF APU W/ 1+ HOUR OF RUN TIME IN BETWEEN, NO SHUTDOWNS OF OVERSPEED FLAG. OPS CHECK GOOD.

Part: TRANSCOWL — DAMAGED (ZONE 400) · airframe 98,041 hrs · 25,113 cycles

LH ENG T/REV WIRE MESH DAMAGED AT 0700 O'CLOCK POSITION. C/W EO 6778A019 REV 5 PART 1 INTERIM REPAIR. C/W PART 2 PERMANENT REPAIR AT NEXT A-CHECK.(<P>REMOVED TRANSLATING COWL FROM L/H THRUST REVERSER OUTBOARD HALF IAW AMM 78-31-10. OK TO INSTALL TRANSLATING COWL. INSTALLED TRANSLATING COWL AT L/H ENGINE THRUST REVERSER OUTBOARD HALF IAW AMM 78-31-10. TRANSLATING SLEEVE OPERATION IS NORMAL IAW AMM 78-31-00-725-005-H00.</P>)

Part: OXYGEN MASK — CONTAMINATED (ZONE 200) · airframe 98,041 hrs · 25,113 cycles

LAV PORTABLE OXYGEN MASK CONTAMINATED.(<P>REMOVED AND REPLACED LAV PORTABLE OXYGEN MASK AS REQUIRED PER 767 AMM 35-31-01. OPS CHK GOOD.</P>)

Part: CDU — INOPERATIVE (THRUST REVERSERS) · airframe 98,041 hrs · 25,113 cycles

LEFT T/R INOP.(<P>REMOVED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OK TO INSTALL. INSTALLED CENTER DRIVE UNIT AT LEFT ENGINE INBOARD SIDE AS PER REF B747 AMM 78-31-21. OPS CHECK GOOD.</P>)

Part: PANEL — LOOSE (ZONE 400) · airframe 98,041 hrs · 25,113 cycles

#2 ENGINE I/B CORECOWL HINGES DAMAGED, DIFFICULT TO OPEN AND CLOSE. REQUIRES EVALUATION.(<P>EVALUATED AND FOUND SKIRT PANEL WITH LOOSE AND MISSING FASTENERS. LOCATED AND INSTALLED NEW FASTENERS IAW SRM 51-40-02-06. OPS CHECK GOOD.</P>)

Part: RADOME — ERODED (ZONE 100) · airframe 98,041 hrs · 25,113 cycles

FWD FUSELAGE RADOME SURFACE, FOUND SEVERAL AREAS OF EROSION.(<P>INSPECTED SURFACE DEFECT AT NOSE RADOME. FOUND EVIDENCE OF PEELING PAINT IAW B767 AMM 53-12-01 CLEANED AND PAINTED AREA IAW B767 AMM 53-12-01</P>)

Part: SWITCH — FAULTED (STAB TRIM) · airframe 97,861 hrs · 25,061 cycles

UNSCHEDULED STAB TRIM MSG ON DECENT. CLEARED SHORTLY AFTER.(<P>R/R STAB TRIM LIMIT SWITCH MODULE ASSY IAW AMM 27-48-01. OPS CHECK GOOD NO DEFECTS NOTED. PERFORMED MCDP GROUND TEST 40, 65 AND 66. ALL TEST GOOD, NO DEFECTS NOTED. PARTS EFECTIVE PER IPC 27-48-01-01.</P>)

Part: ELT — INOPERATIVE · airframe 97,655 hrs · 25,012 cycles

REF W/O 138840, DURING OPS CHECK OF FIXED ELT FOUND TO BE INOPERATIVE.(<P>R/R FIXED ELT PER EO OT-23-0084. OPS CHECK GOOD. DMI 220446 CLOSED</P>)

Part: SKIN — DAMAGED (RT AILERON) · airframe 97,212 hrs · 24,850 cycles

RH OTBD AILERON TRAILING EDGE LIGHTNING STRIKE(<P>TRANSFER TO NON-MEL DMI 215328 DUE DATE 27AUG24.</P> / <P>LP 1872886 M1: C/W PART 3 PERMANENT REPAIR PER ATLAS EA 6757A156- CS REV 0. NON-MEL DMI 215328 CLOSED

Part: INDICATION SYS — FAULTED (OXYGEN BOTTLE) · airframe 97,087 hrs · 24,805 cycles

AFTER LANDING O2 BOTTLE INDICATES 40 PSI. CONFIRMED EICAS IND INOP. REF DMI 213995 PER MEL 35-11-02-01 CAT B DUE DATE 8AUG24. MMP PERFORMED. BOTTLE #1 1400 PSI, BOTTLE #2 1300 PSI, AVERAGE 1600 PSI. R/R VOLT AVG UNIT PER AMM 35-11-06. OPS CHECK GOOD.

Part: AVERAGING UNIT — FAULTED (OXYGEN SYSTEM) · airframe 97,032 hrs · 24,787 cycles

ON GROUND OXYGEN PRESSURE SHOWS 40 PSI.(<P>R/R AVERAGING UNIT IAW AMM 35-11-06. OPS &AMP; LEAK CHECK GOOD. DMI 213524 CLOSED.</P>)

Part: SHROUD — DAMAGED (ESCAPE ROPE) · airframe 96,588 hrs · 24,636 cycles

L1 DOOR EMERGENCY ESCAPE ROPE SHROUD DAMAGED.(<P>PERFORMED TIME LIMITED REPAIR ON L1 DOOR ESCAPE ROPE RETAINER SHROUD IAW EA 6725A0025. TRANSFER TO NON-MEL DMI 206255 &AMP; 206256 DUE DATE 8APR2024. LP 1807206 M2: R/R SHROUD IAW AMM 52-09-01. NO FURTHER DEFECTS NOTED. DMI 206255 &AMP; 206256 CLOSED.</P>)

Part: ELT — UNKNOWN (UNKNOWN) · airframe 96,294 hrs · 24,533 cycles

DURING OPS CHECK OF FIXED ELT PER W/C # A-23--339-01(<P>TRANSFERRED TO MDDR 203168 PER DDG 25-63-10-02C CAT D DUE 16JUM24. MX ACTIONS C/W, PLACARDS INSTALLED. PRFORMED ELT OPS CHECK PER CAD A-23-999-01, TEST NORMAL. THIS CLEARS DMI 203168, PLACARD REMOVED.&NBSP;</P>)

Part: SENSOR — OUT OF TOLERANCE (CARGO DOOR) · airframe 96,147 hrs · 24,477 cycles

MAIN CARGO DOOR SHOWS OPEN DURING CRUISE. INDICATION WENT OUT DURING DESCENT AT FL 340. "MAIN CARGO DOOR" EICAS MSG.(<P>FOUND MAIN CARGO DOOR LOCKED WARNING SENSOR S892 OUT OF TOLERANCE. RESHIMMED &AMP; ADJUSTMENTED SENSOR TO WITHIN LIMITS, DOOR OPS CHECK NORMAL IAW AMM 52-71-09.</P>)

Part: COMPUTER — UNKNOWN (UNKNOWN) · airframe 96,028 hrs · 24,442 cycles

RETURN TO BLOCK AFTER LOW SPEED RTO DUE MASTER CAUTION LIGHT AND BEEPER. "AUTOTHROTTLE DISCONNECT" EICAS MSG. SPED WAS AROUND 40KTS.(<P>DEFERRED IAW MEL 22-30-01 DMI 199674 CONDITION INSP IAW AMM 05-51-14 NOT REQUIRED AS RTO WAS BELOW 40 KNOTS.R/R TMC COMPUTER OPS CHECK NORMAL IAW AMM 22-31-01</P>)

Part: BATTERY — INOPERATIVE · airframe 95,270 hrs · 24,263 cycles

L1 F/A FLASHLIGHT CHARGING INDICATOR NOT BLINKING.(<P>REMOVED AND REPLACED L1 FLASHLIGHT BATTERY AND OPS CHECKED GOOD IAW AMM 25-64-54</P>)

Part: LIFE VEST — MISSING (SEAT 34G) · airframe 95,214 hrs · 24,249 cycles

SEAT 34G MISSING LIFE VEST. INSTALLED LIFE VEST PER AMM 25-64-00 REV. 137.

Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 95,214 hrs · 24,249 cycles

EMERGENCY LIGHT AT LEFT ROW 36 CEILING IS MISSING LENS. INSTALLED MISSING LENS, OPS CHECKS NORMAL IAW AMM 33-51-05.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 95,214 hrs · 24,249 cycles

EMERGENCY LIGHT AT RIGHT ROW 25 CEILING IS INOP(<P>RE-LAMPED LIGHT AND OPS CHECKS GOOD IAW AMM 33-51-05</P>)

Part: LIGHT — INOPERATIVE (ROW 40) · airframe 95,214 hrs · 24,249 cycles

EMERGENCY LIGHT AT RIGHT ROW 40 CEILING INOP. REMOVED AND REPLACED LIGHT ASSY. OPS CHECKS NORMAL IAW AMM 33-51-05.

Part: BATTERY — INOPERATIVE · airframe 94,828 hrs · 24,167 cycles

EXTERIOR EMEG LIGHTS AFT WING MIDDLE A/C 2 AND 1 AFT L2 DOOR(<P>REMOVED AND REPLACED CABIN LH AFT EMERG BATTERY PACK PER AMM 33-51-07, OPS CHECK GOOD</P>)

Part: NONE — NONE · airframe 94,763 hrs

R1 DOOR SLIDE PRESSURE INDICATOR IN THE RED.(<P>R1 DOOR ESCAPE SLIDE CYLINDER IN GREEN BAND PER AMM 25-66-01. OK FOR SERVICE.&NBSP;</P>)

Part: DISPLAY — INOPERATIVE · airframe 94,496 hrs · 24,095 cycles

COCKPIT, PANEL BACKGROUND LIGHT INOP.(REMOVED & REPLACED EICAS DISPLAY SELECT PANEL M10195 &; OPS CHECK OK AMM 31-41-03.</P>)

Part: CARTRIDGE — OUT OF DATE · airframe 94,496 hrs · 24,095 cycles

ENG 2 OB SQUIB OUT OF DATE(<P>IN ACCORDANCE WITH W/O 94430 WAS REMOVED AND REPLACED CARTRIDGE OUTBOARD B767 AMM 26-21-03</P>)

Part: WINDOW — NOISY · airframe 94,496 hrs · 24,095 cycles

INTERMITTENT WHISTLING NOISE FROM R2 WINDOW CLEANED & REPAIRED R2 WINDOW PER MM 56-11-00-368-059 PRESSURIZED CABIN & ACCOMPLISHED CABIN PRESSURE LEAK CHECK PER B767 -300 MM 05-51-24-782-001. NO LEAKAGE NOTED

Part: BLADE — DENTED · airframe 94,496 hrs · 24,095 cycles

FAN BLADE MARKED # 11 HAS A DENT AT L/E AREA D .BLENDED OUT ENG. # 1; FAN BLADE # 11 AT LEADING EDGE; AREA FOUND WITHIN LIMITS PER B767-300 & AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION IN AREA NO CRACK OR INDICATION NOTED REF. AMM 70-11-06.

Part: ENGINE — INSTALLED · airframe 94,496 hrs · 24,095 cycles

REINSTALL ALL REMOVED HYDRAULIC, PNEMAUTIC AND ELECTRIAL CONNECTORS AND LINKS DUE TO #1 ENGINE CHANGE CANCELATION. REINSTALLED ALL; HYDRAULIC; PNEUMATIC AND ELECTRICAL CONNECTORS AS PER 71-00-02. PENDING ENGINE RUN UP LEAK CHECK .PERFORMED IDLE ;LEAK CHECK PER B767-300 AMM 71-00-00.NO LEAKS NOTED , ENG OPS CHECK GOOD

Part: SQUIB — INSTALLED · airframe 94,496 hrs · 24,095 cycles

CARGO FIRE EXTINGUISHER BOTTLE SQUIB P/N 30903889 S/N 03608 DUE FOR REPLACEMENT IN ACCORDANCE WITH W/O 94430 WAS REMOVED AND REPLACED CARTRIDGE CARGO FIRE AS PER B767 26-011-00

Part: SEAT BELT — DAMAGED · airframe 94,496 hrs · 24,095 cycles

COCKPIT CAPTAIN'S LEFT AND RIGHT LAP BELTS DAMAGED. REMOVED AND REPLACED CAPT. L & R LAP BELT ASSY PER B767-300 AMM 20-11-00.OPS CHECK GOOD.

Part: BLADE — NICKED · airframe 94,496 hrs · 24,095 cycles

FAN BLADE MARKED # 31 HAS A NICK AT L/E AREA D . BLENDED OUT # 1 ENG. FAN BLADE # 31 AT LEADING EDGE; AREA FOUND WITHIN; LIMITS PER B767-300; AMM 72-31-02-308-045-H00. PERFORMED NDT; SPOT &;FLOURESCENT PENETRANT INSPECTION NO NICK; ON CRACK IND NOTED REF. AMM 70-11-06.)

Part: SQUIB — OUT OF DATE · airframe 94,496 hrs · 24,095 cycles

ENG 2 IB SQUIB OUT OF DATE IN ACCORDING WITH W/O 94430 WAS REMOVED AND REPLACED CARTRIDGE INBOARD AS PER B767 AMM 26-21-3</P>)

Part: BLADE — NICKED · airframe 94,496 hrs · 24,095 cycles

FAN BLADE MARKED # 10 HAS A NICK AT L/E AREA D .BLENDED OUT # 1 ENG. FAN BLADE # 10 AT LEADING EDGE AREA FOUND WITHIN LIMITS PER B767-300&; AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED. REF. AMM 70-11-06.</P>)

Part: ROD — UNSERVICEABLE · airframe 94,496 hrs · 24,095 cycles

#2 ENGINE I/B CORE COWL HOLD OPEN STRUT DOES NOT LOCK IN OPEN POSITION. REMOVED AND REPLACED #2 ENG I/B CORE COWL HOLD OPEN ROD STRUT IAW B763 AMM 20-11-00

Part: BLADE — NICKED · airframe 94,496 hrs · 24,095 cycles

FAN BLADE MARKED # 8 HAS A NICK AT L/E AREA D .BLENDED OUT # 1 ENG. FAN BLADE # 8 AT L/E AREA; FOUND WITHIN LIMITS PER B767-300 SRM 72-31-02-308-045-H000. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSP OF THE AREA NO NICK ON CRACK IND NOTED REF. AMM 70-11-06.</P>)

Part: BLADE — NICKED · airframe 94,496 hrs · 24,095 cycles

FAN BLADE MARKED # 1 HAS A NICK AT L/E AREA D. BLENDED OUT #1 ENG. FAN BLADE #1 AT L/E; AREA; FOUND WITHIN LIMITS PER B767-300 AMM 72-31-02-308-045-H00. PERFORMED NDT SPOT FLOURESCENT PENETRANT INSPECTION. NO NICK ON CRACK IND NOTED AT THIS TIME. AMM 70-11-06.</P>)

Part: COWLING — INSTALLED · airframe 94,496 hrs · 24,095 cycles

ENGINE #1 REINSTALL ALL ENGINE COWLS DUE TO ENGINE CHANGE CANCELATION. INSTALL INLET COWL ON ENGINE #1 AS PER B767-300 AMM 71-11-01. INSTALLED FAN COWL ( LEFT RIGHT ) ON ENGINE # AS PER B767-300 AMM 71-11-04. INSTALLED LEFT AND RIGHT CORE COWLS ON ENGINE #1 AS PER B767-300 AMM 71-11-06

Part: COVER — TORN · airframe 94,496 hrs · 24,095 cycles

COCKPIT 1ST OBS LIFE VEST COVER TORN. INSTALLED SERVICEABLE COVER FROM INTERIOR BY MILLY AT COCKPIT 1ST OBS LIFE REST AND INSTALLED ; PER AMM 25-11-00-001.

Part: LAMP — INOPERATIVE · airframe 94,454 hrs

R/H AFT EXTERIOR EMERGENCY LIGHT INOP(<P><SPAN>RELAMPED R/H AFT EXT EMERGENCY LIGHT IAW AMM 33-51-16. OPS CHECK GOOD.</SPAN></P>)

Part: SIGN — BROKEN · airframe 94,312 hrs

EMERGENCY EXIT SIGN AT L1 DOOR BROKEN(<P><SPAN>R&AMP;R EMERGENCY EXIT SIGN AT L1 DOOR PER AMM 33-51-01</SPAN></P>)

Part: SMOKE DETECTOR — NONE · airframe 94,241 hrs · 24,039 cycles

R4 LAV SMOKE DETECTOR INOP.(<P>R4 LAV SMOKE DETECTOR HAS BEEN R/R IAW AMM 26-13-01, OPS CHECK OK.</P>)

Part: SIGN — DAMAGED · airframe 94,189 hrs

L1 AND R4 DOOR EMERGENCY EXIT SIGN DAMAGED(<P><SPAN>REMOVED AND REPLACED EMERGENCY EXIT SIGN ASSY IAW AMM 33-51-07 OPS CHECK GOOD</SPAN></P>)

Part: BRACKET — FAILED · airframe 94,117 hrs · 24,015 cycles

REFERENCE W/O 92373 ELT TEST PER W/0 A-25-099-20-01 FAILED. FOUND BAD BRACKET P/N: 95N6089(<P>PLACED ON MEL 25-63-10-02C, CAT D, EXPIRES 23JUN22, MDDR# 161702, PLACARDS INSTALLED, "M" ACTION C/W.</P>)

Part: LIGHT — NONE · airframe 94,074 hrs · 24,004 cycles

RT WING EXTERIOR EMER OVERWING LIGHT INOP(<P>RELAMPED RH WING EXT EMERGENCY OVERWING LIGHT IAW 767 AMM 33-51-06. OPS CHECK GOOD.</P>)

Part: LIGHT — NONE · airframe 94,036 hrs

EMERGENCY LIGHT AT SEATS 1H 44 19F 33H 35C INOP(<P>RELAMPED LIGHTS AT SEATS 1H, 44, 19F, 33H, 35C REF AMM 33-51-05 OPS CHECK GOOD.</P>)

Part: LIGHT — NONE · airframe 94,038 hrs · 23,997 cycles

COCKPIT PORTABLE EMERGENCY EXIT LIGHT INOP NEEDS REPLACED(<P><SPAN>R+R COCPIT EMERG. EXIT LIGHT OPS CHECK WORK DONE IAW AMM 33-51-01</SPAN></P>)

Part: SHIELD — NONE · airframe 94,036 hrs

DAMAGED METALLIC SHIELD OF THE ELECTRICAL WIRING OF BRAKE TEMPERATURE SENSOR FROM RH MLG BRAKE #3 AND #4.(<P ><SPAN>METALLIC SHIELDS OF ELECTRICAL WIRING OF BRAKE TEMPERATURE SENSOR WERE REPLACED</SPAN></P> / <P>&NBSP;</P>)

Part: NONE — NONE · airframe 94,035 hrs · 23,995 cycles

INCORRECT INSTALLATION OF THE ELECTRICAL WIRING OF THE BRAKE TEMPERATURE SENSOR FROM LH MLG BRAKE #5. FOR SUCH REASON, IT WAS FOUND CHAFFING BETWEEN ELECTRICAL WIRING OF BRAKE TEMPERATURE SENSOR AND STRUCTURE.(<P ><SPAN>ELECTRICAL WIRING OF THE BRAKE TEMPERATURE SENSOR FROM LH MLG BRAKE #5 WAS INSTALLED CORRECTLY.</SPAN></P>)

Part: NONE — NONE · airframe 94,036 hrs

COUNTERBALANCE LOAD LIMITER FROM L1 DOOR WAS FOUND OUT OF LIMITS(<P ><SPAN>COUNTERBALANCE LOAD LIMITER FROM L1 DOOR WAS REMOVED AND INSTALLED CORRECTLY</SPAN></P> / <P>&NBSP;</P>)

Part: HOUSING — NONE · airframe 94,036 hrs

BROKEN DISCONNECT HOUSINGS IN THE LH/RH OFF WING SLIDE COMPARTMENT(<P>DISCONNECT HOUSINGS IN THE LH/RH OFF WING SLIDE COMPARTMENT WERE REPLACED PER AMM TASK&NBSP;<SPAN>25-65-04-414-154-001.</SPAN></P>)

Part: BATTERY — NONE · airframe 93,970 hrs

L4/R4 THRESHOLD EMERGENCY LIGHTS INOP(<P><SPAN>R/R EMERGENCY BATTERY PACK ASSY POWER SUPPLY REF AMM 33-51-07</SPAN></P>)

Part: NONE — NONE · airframe 93,889 hrs

WX RADAR FAULT WHEN TAXIING TO RUNWAY.(<P>PERFORMED OPS TEST OF WX RADAR SYSTEM IAW AMM 34-43-00. OPS CHECK GOOD.</P>)

Part: LIFE VEST — NONE · airframe 93,839 hrs · 23,946 cycles

PASSENGER CABIN SEAT 17G LIFE VEST COMPARTMENT DOOR LOOSE(<P><SPAN>INSTALLED&NBSP; NEW LIFE VEST&NBSP; COMPARTMENT&NBSP; IAW&NBSP; CMM 25-27-32 CK FOR SERVICE .</SPAN></P>)

Part: NONE — NONE · airframe 93,839 hrs · 23,946 cycles

#2 ENG. #4 BRG. OUTER INTERNAL SCAVENGE TUBE IS NOT SECURED &AMP; OUT OF PLACE(<P><SPAN>REMOVED #2&NBSP; ENG&NBSP; TURBINE&NBSP; EXHAUST&NBSP; PLG&NBSP; IAW&NBSP; &NBSP;B767-300&NBSP; &NBSP;AMM&NBSP; &NBSP;78-11-02</SPAN></P> / <P><SPAN>REPOSITIONED&NBSP; AND&NBSP; SECURED&NBSP; INTERNAL&NBSP; SCAVENGE&NBSP; TUBE&NBSP; CLAMP&NBSP; AS&NBSP; REQUIRED&NBSP; &NBSP;IAW&NBSP; AMM&NBSP; 70-00-00</SPAN></P> / <P><SPAN>NO DEFECTS&NBSP; NOTED</SPAN></P> / <P><SPAN>INSTALLED&NBSP; EXHAUST&NBSP; PLUG&NBSP; AS PER&NBSP; 767&NBSP; AMM&NBSP; &NBSP;78-11-02</SPAN></P>)

Part: NONE — NONE · airframe 93,839 hrs · 23,946 cycles

PASSENGER CABIN SEAT 25H LIFE VEST COMPARTMENT LOOSE(<P><SPAN>RESECURED LOOSE LIFE VEST COMPARTMENT AT MAIN CABIN&NBSP; BY SEAT&NBSP; 25H&NBSP; PER B767-300&NBSP; AMM 20-11-00-910-802.</SPAN></P>)

Part: NONE — NONE · airframe 93,839 hrs · 23,946 cycles

#1 ENG O/B T/REV LATCH CAM IS BENT(<P><SPAN>REMOVED AND REPLACED&NBSP; 31&NBSP; ENG&NBSP; O/B&NBSP; &NBSP;T/REV&NBSP; &NBSP;LATCH&NBSP; CAM&NBSP; IAW&NBSP; &NBSP;AMM&NBSP; &NBSP;78-31-01&NBSP; &NBSP; OPS&NBSP; CHECK&NBSP; OK</SPAN></P>)

Part: PBE — NONE · airframe 93,839 hrs · 23,946 cycles

PASSENGER CABIN FWD B/C CLOSET PBE SECURITY SEAL MISSING P/N 15-40F-80 S/N 94703002(<P><SPAN>REMOVED &AMP;&NBSP; REPLACED&NBSP; PBE&NBSP; AT&NBSP; FWD&NBSP; &NBSP;B/C&NBSP; CLOSET&NBSP; &NBSP; AS&NBSP; REQUIRED&NBSP; PER AMM 35-31-02&NBSP; &NBSP;CK'D&NBSP; OK .</SPAN></P>)

Part: ACTUATOR — FIRE (LT WING SLIDE) · airframe 93,839 hrs · 23,946 cycles

LEFT WING SLIDER (2) BOTH DOOR ACTUATORS AND LATCH ACTUATOR WAS FIRE. REMOVED & REPLACED SLIDE COMP DOOR LATCH ACTUATOR PER AMM 25-65-11. REMOVED & REPLACED LT SLIDE COMP SPOILER ACTUATOR PER AMM 25-65-20. REMOVED & REPLACED LT SLIDE COMP AFT DOOR OPENING ACTUATOR PER AMM 25-65-10.

Part: JUMPER — NONE · airframe 93,839 hrs · 23,946 cycles

R/WING VARIABLE CAMBER LEADING EDGE # 17 ,18,20 AND 23 WITH BROKEN BONDING WIRES(<P><SPAN>REMOVED AND&NBSP; REPLACED&NBSP; R/W VARIABLE&NBSP; CAMBER JUMPER PER&NBSP; SWPM 20-20-10 .</SPAN></P>)

Part: NONE — NONE · airframe 93,759 hrs

LEFT ENGINE IDG SERVICE REQUIRED.(<P>LEFT ENGINE IDG SERVICED IAW B767 AMM 12-13-03.</P>)

Part: SWITCH — INTERMITTENT

APU FAULT 3 ATTEMPTS WILL NOT START. CYCLED BATTERY SWITCH. APU STARTED FIRST ATTEMP. NO DEFECTS NOTED IAW B767AMM 49-11-00. OPS CKS GOOD.&NBSP

Part: FUEL FILTER — CLOGGED (LT ENGINE)

L ENG FUEL FILTER STATUS MESSAGE. REMOVED AND REPLACED LH ENG FUEL FILTER PER M767 AMM 73-11-02, LEAK CHECK GOOD, NO LEAKS.</P>)

Part: STOWAGE BOX — NO TEST (OXYGEN MASK)

CAPT FLOW INDICATOR ON O2 MASK STOWAGE BOX DOES NOT TURN ON IN TEST MODE(<P>REMOVED AND REPLACED CAPT O2 MASK STOWAGE BOX IAW 767 AMM 35-11-51, OPS TEST GOOD, NO LEAKS NOTED</P>)

Part: BLADE — DAMAGED (NR 2 COMPRESSOR) · airframe 93,171 hrs · 23,802 cycles

#2 ENG LP COMPRESSOR ROTOR BLADES - SEVERAL REQUIRE BLENDING / NDT DUE TO NICKS(<P>BLENDED OUT NICKS ON SEVERAL FAN ROTOR BLADES AT #2 ENG. PER&NBSP; B767-300 AMM 72-31-02-308-045-H00 PERFORMED SPOT FLOURESCENT PENETRANT INSPECTION OR ALL BLENDED AREA&NBSP; NO NICK INDICATION NOTED REF. AMM 70-11-06</P>)

Part: WASHER — DAMAGED (BOROSCOPE PLUG) · airframe 93,171 hrs · 23,802 cycles

# 1 ENGINE BOROSCOPE PLUG SAFETY WASHER "POSITION" B2-5 DAMAGED.(<P>REMOVED &AMP; REPLACED #1 BORESCOPE PLUG B2-5 WASHER &AMP; INSTALLED B2-5 PER AMM 72-00-00 &AMP; WORK CARD A-72-307-00-01.</P>)

Part: SLEEVE — DAMAGED (THRUST REVERSER) · airframe 93,171 hrs · 23,802 cycles

IN REFERENCE TO A CHECK NON ROUTINE NR-02 REMOVE ENG #1 OUTBOARD THRUST REVERSER SLEEVE TO FACILITATE THE ACCOMPLISHMENT OF PART 2- PERMANENT REPAIR AT NEXT A CHECK(<P>REMOVED ENG. # 1 OUTBOARD THRUST REVERSER SLEEVE TO FACILITATE REPAIR IAW B767 78-31-10-004.</P> / <P>REINSTALLED ENG. # 1 TR SLEEVE AS PER 78-31-10.</P> / <P>PENDING OPS TEST.</P> / <P>PERFORMED T/R OPS CHK PER AMM 748-31-00.</P> / <P>OPS CHECK GOOD.</P>)

Part: SEAT BELT — DAMAGED (COCKPIT) · airframe 93,171 hrs · 23,802 cycles

COCKPIT F/O R/H SEAT BELT TSO TAG DAMAGE(<P>REMOVED AND REPLACED LAP BELT @ FIRST OFFICER SEAT IAW 767 AMM 25-11-00.</P> / <P>OPERATIONAL CHECK IS NORMAL&NBSP; PER AMM 25-11-01.</P>)

Part: MESH — DAMAGED (THRUST REVERSER) · airframe 93,171 hrs · 23,802 cycles

C/W PART 1 OF INTERM REPAIR OF EO 6778A019 TO THE # 1 ENG T/R MESH ON LEFT HALF T/R 11 O'CLOCK POSITION-PART 2 PERMANENT REPAIR REQUIRED NEXT "A" CHECK(<P>ACCOMPLISHED PERMANENT REPAIR AT # 1 ENGINE O/B T/R SLEEVE PER EO6778A019 REV 4 PART 2 AND CMM 78-32-32 PER REPAIR 024.

Part: WIRE HARNESS — DAMAGED (APU) · airframe 93,201 hrs

APU RELIABILITY COLD SOAK START UNSUCCESSFUL, 1ST ATTEMPT - SAT - 53 - FL400 MAX RPM 45% / 2ND ATTEMPT - SAT - 52 - FL400 MAX RPM 20% / 3RD ATTEMPT - SAT - 52 - FL400 MAX RPM 22%.(<P>NOTED BY MX. APU COLD SOAK CLEARED DUE TO APU INOP.&NBSP;</P> / <P>13JUL21 - LP 1354874 - ITEM#6 - ANC - TRANSFER TO DMI 150117, CAT B, IAW ATLAS DDG 49-11-01B, DUE 16JUL21.</P> / <P>BWI - LP 148942 ITEM 7: FOUND SHORT BETWEEN #2 THERMOCOUPLE WIRES T56 .REMOVED AND REPLACED APU WIRING HARNESS ASSY IAW WDM 49-14-11 AND SWPM 20-10-11. PERFORMED SUCESFULL APU STARTS IN GRND AND BATT POWER IAW AMM 49-11-00. PUT ACFT IN SIMULATED AIR MODE IAW AMM 32-09-02 AND PERFORMED 3 SUCCESFUL APU STARTS. PERFORMED APU BIT IAW 49-61-05, OK ON MINI FLAGS AND NO ISSUES. SEE ECM 2021P-225 FOR COMPLETE WIRING CHECKS PRIOR BETWEEN APU AND ECU AND APU FIREWALL . APU OPS CKS GOOD AT THIS TIME IAW 49-11-00. THIS CLEARS DMI 150117. MCC NOTIFIED, PLACARDS REMOVED.

Part: BLADE — NICKED (LT ENGINE FAN) · airframe 93,171 hrs · 23,802 cycles

ON LEFT ENG FOUND NICKS ON SEVERAL FAN ROTOR BLADES AT L/E AREAS(<P>BLENDED OUT SEVERAL ROTOR BLADES WITH NICKS AT L/H ENG BY LEADING EDGE PER B767-300 AMM 72-31-02-308-045-H00. PERFORMED SPOT FLOURESCENT PENETRANT INSPECTION OR ALL BLENDED AREA NO NICK IND. NOTED REF. AMM 70-11-06</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (APU DOOR)

STATUS MSG APU DOOR(<P>PERFORM APU OPERATION PER AMM 49-11-00. APU DOOR OPERATED&NBSP; NORMAL. NO MSG.</P>)

Part: DRAIN VALVE — DAMAGED (NR 1 STARTER) · airframe 93,171 hrs · 23,802 cycles

# 1 ENGINE STARTER DRAIN VALVE FOUND DAMAGED(<P>REMOVED &AMP; REPLACED # 1 ENGINE STARTER DRAIN PLUG IAW AMM 80-11-01. SERVICED STARTER AS REQUIRED IAW AMM 12-13-02. NO LEAK FOUND</P>)

Part: OIL COOLER — FAULTED (APU) · airframe 93,171 hrs · 23,802 cycles

APU INOPERATIVE ( AUXILIARY POWER UNIT ) (APU), ER OERATIONS NOT ALLOWED REMOVED & REPLACED APU OIL COOLER PER AMM 49-27-09. NO LEAKS&NBSP; .</P> / <P>REMOVED &AMP; REPLACED APU COOLING FAN PER AMM 49-51-03. PERFORMED APU OPS CHK PER AMM 49-11-00. APU OPERATED NORMAL.

Part: APU — NOT REPORTED · airframe 93,171 hrs · 23,802 cycles

C/W APU REMOVAL AND REPLACED(<P>REMOVED APU PER B767 AMM 49-11-01. INSPECTED PER B767 AMM 49-05-03. NO DEFECT NOTED ON MOUNTS / FIRE WALL INLET / EXHAUST&NBSP; / FIRE WALL. INSTALLED APU ASSY IAW AMM 49-11-01. OPS CHK OK&NBSP; REMOVED AND INSTALLED&NBSP; MODULE FLOW SENS. IAW 49-53-01. OPS CHK OK. REMOVED &AMP; REPLACED SENSOR VALVE IAW AMM 49-53-06.</P> / <P>OPS CHK OK .</P>)

Part: CONTAINMENT BAG — OPEN (MAIN DECK) · airframe 93,171 hrs · 23,802 cycles

MAIN DECK FIRE CONTAINMENT BAG AT AFT L/H CLOSET VACUUM SEAL BROKE P/N AS-002-1(<P>REMOVED &AMP; REPLACED AVSAX CONTAINMENT BAG AT AFT L/H CLOSET AS REQUIRED PER AMM 25-64-00. CK'D OK .</P>)

Part: APU — MALFUNCTIONED · airframe 93,169 hrs · 23,803 cycles

APU FAIL TO START. REMOVED AND REPLACED APU IAW AMM 49-11-01. OPS CHECK OK, NO LEAKS NOTED

Part: ECU — INOPERATIVE (APU)

APU INOP.(<P>TRANSFER TO MDDR 149250 CAT "B" IAW DDG 49-11-01B</P> / <P>28JUN21 - 1484416 - ITEM# 3 - BWI - R/R ECU IAW B767 AMM 49-61-05 OPS CK GD. NO FAULTS, THIS CLEARS MDDR 149250. MCC NOTIFIED AND PLACARD REMOVED.</P>)

Part: PITOT TUBE — FAULTED (CAPTAIN'S) · airframe 93,148 hrs · 23,797 cycles

CAPT PITOT EICAS MESSAGE.(<P>REMOVED AND REPLACED CAPT PITOT PROBE B767 AMM 34-11-01. LEAK CHECK IAW B767 AMM 34-11-00</P>)

Part: APU — MALFUNCTIONED · airframe 93,159 hrs

APU COLD START UNSUCCESSFUL 3 START ATTEMPTS -16C / FL 360(<P>NOTED BY MX PERFORMED FIM 49-11 FLT 958 MINI FLAG 141 LRU"START ABORT" RESET CLEARED&NBSP;</P>)

Part: APU — MALFUNCTIONED · airframe 93,159 hrs

APU STARTS UNSUCCESSFUL / 3 START ATTEMPTS (COLD SOAK) / -23 DEGREES CELCIUS / FL 390 / MAX RPM 33% 815 DEGREE(<P>NOTED BY MX&NBSP;BITE PERFORMED ON ECU IAW B767 FIM 49-11 FT 858</P>)

Part: HMU — FAULTED (RT ENGINE) · airframe 93,112 hrs

R/H ENGINE EEC C1 STATUS MESSAGE ( ELECTRONIC ENGINE CONTROL (EEC) SYSTEMS, EEC C1 FAULTS (CF6 FADEC))(<P>TRANSFER TO MDDR# 149029, CAT A, IAW DDG 73-21-01-05 DUE 29JUL21 / 300 HRS. REMOVED AND REPLACED R/H ENGINE HMU IAW AMM 73-21-14. OPS CK GOOD, NO FAULTS AT THIS TIME, THIS CLEARS DMI 149029, PLACARDS REMOVED.

Part: PUMP — INOPERATIVE (MAIN TANK) · airframe 93,075 hrs · 23,785 cycles

LEFT FWD FUEL PUMP, INOP IN AUTO ( MAIN TANK FUEL PUMPS, AUTOMATIC FUNCTION OF LEFT FWD PUMP )(<P>DEFER TO MEL 28-22-01-01, REF MDDR 148745, CAT C, DUE 27JUN21.</P>)

Part: PITOT TUBE — FAILED (CAPTAIN'S) · airframe 93,035 hrs · 23,775 cycles

CAPT PITOT EICAS ILLUMINATED ON CLIMBOUT(<P>PERFORMED FIM 30-31 FT 803, SYSTEM FAILED THE PITOT PROBE, REMOVED AND REPLACED CAPTAIN PITOT PROBE IAW B767 M/M 34-11-01, LEAK CHECK IAW B767 M/M 34-11-00-730-811, NO DEFECT NOTED-300 KTS-298 KNTS 1 MINUTE 2 KNTS DROP, TEST SET - TE21363/TL4799.</P>)

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 93,022 hrs · 23,773 cycles

R ENG EEC C1 STATUS MESSAGE(<P>TRANSFER TO MDDR # 148314 IAW ATLAS DDG 73-21-01-05 CAT "A" DUE DATE/TIME (300HR) 933322.2HRS PLACAR INSTALLED.</P> / <P>LOG 1484976 ITEM #21: REMOVED AND REPLACED #2 EEC IAW AMM 73-21-15. PERFORMED TEST #12 GROUND TEST EEC AMM 71-00-00. OPS CHECK GOOD AT THIS TIME. PERFORMED #2 ENG IDLE RUN IAW AMM 71-00-00, NO FAULTS NOTED AT THIS TIME. THIS CLEARS DMI #148314. MCC NOTIFIED. PLACARD REMOVED.

Part: APU — INOPERATIVE · airframe 93,052 hrs · 23,779 cycles

APU INOP. REPLACED APU IAW AMM 49-81-01 AND WO 81871 WORK CARD A-49-999-00-01. APU OPS AND LEAK CHECKED OK. APU MOUNTS SECURED.

Part: RELAY — FAULTED (APU FUEL) · airframe 93,019 hrs · 23,372 cycles

APU START UNSUCESSFUL AT FL 400 AT -45 DEG C AFTER 3 ATTEMPTS AT ALTITUDE. UNSUCCESSFUL ON THE GROUND AS WELL.(<P>NOTED BY MX. REMOVED AND REPLACED DC FUEL PUMP CONTROL RELAY K191. NO HELP PER FIM 28-25 FT. 806. MDDR 147790 REMAIN OPEN. PERFORMED APU BITE PER AMM 49-61-05 NO FAULTS. PERFORMED OPS CHECK OF APU PER AMM 49-11-00. OPS CHECK GOOD.</P>)

Part: APU — FAULTED · airframe 93,019 hrs · 23,772 cycles

INFO ONLY APU START UNSUCCESSFUL AT FL410 AT -61 DEGREES C AND FL260 AT -27 DEGREES C, APU START SUCCESSFUL ON GROUND.(<P>NOTED BY MX. PERFORMED BITE CHECK OF APU ECU, NO FAULTS NOTED; MEL # 147790 REMAINS OPEN.</P>)

Part: APU — FAULTED · airframe 93,019 hrs · 23,772 cycles

APU RELIABILITY COLD START ATTEMPTED. SAT -49DEGREES C, FL 340. START UNSUCCESSFUL AFTER THREE ATTEMPTS. APU FAULT EICAS MESSAGE.(<P>NOTED BY MX.&NBSP;MEL # 147790 FOR COLD SOAK REMAINS OPEN.</P>)

Part: APU — MALFUNCTIONED · airframe 93,002 hrs · 23,770 cycles

APU RELIABILITY COLD SOAK START ATTEMPTED. SAT -60 DEGREES C, FL 400. START UNSUCCESSFUL AFTER THREE ATTEMPTS.(<P>NOTED BY MX.&NBSP;MEL # 147790 FOR COLD SOAK REMAINS OPEN.</P>)

Part: WARNING MESSAGE — FALSE INDICATION (RT EEC) · airframe 92,951 hrs · 23,762 cycles

R ENG EEC C1 STATUS MESSAGE AFTER LANDING.(<P>CLEARED MESSAGE AS REQUIRED PER FIM 71-01 SHEET 1 - SHEET 4.

Part: CONTROL VALVE — FAULTED (LT A/C PACK) · airframe 92,936 hrs · 23,757 cycles

L/H PACK DID NOT TURN OFF WHEN SELECTED(<P>PERFORMED PACK TEMPERATURE CONTROL OPERATIONAL TEST IAW AMM 21-51-00-705-161. TEST PASS, NO DEFECT NOTED AT THIS TIME.</P><P>LOG PAGE 1484388: REMOVED AND REPLACED LH PACK FLOW CONTROL VALVE PER AMM 21-51-01. OPS CHK GOOD AT THIS TIME.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · corrosion level 2 · airframe 59,504 hrs · 56,339 cycles

DURING SCHEDULED INSPECTION AT HAECO LAKE CITY, FLORIDA FOUND AFT CARGO COMPARTMENT FLOOR PANEL 1336X HAS MULTIPLE AREAS OF PITTING CORROSION. S/O 660006 N/R 38252

Part: APU — FAULTED · airframe 92,908 hrs · 23,751 cycles

APU FAULT- NO START @ FL 380- 3 ATTEMPTS- RPMS STOPPED @ 25- THEN FAULT MSG. COLD SOAK START UNSUCCESSFUL.(<P>NOTED BY MX, PERFORMED ECU BITE IAW B767 FIM 49-11 FT 958, MINI FLAGS "OK". LRU FAULTS LAST ATTEMPT "NORMAL STOP" 2,3,4 "NO LIGHT OFF", RESET CLEARED, NORMAL START.&NBSP;</P>)

Part: ECU — FAULTED (APU) · airframe 92,899 hrs · 23,750 cycles

APU FAULT NO START 3 ATTEMPTS.(<P>PERFORMED APU BITE CHECK ON ECU IAW B767 FIM 49-11 FT 958. MINI FLAG- "OK" LRU FAULTS- "NO LIGHT OFF". RESET CLEARED.</P>)

Part: TRANSCEIVER — INTERMITTENT · airframe 92,822 hrs · 23,732 cycles

FO RA INTERMITTENT (NO LAND 3) REMOVED AND REPLACED RT RA XCEIVER, OPS CK OK. THIS CLEARS MDDR 146046.</P><P><SPAN></SPAN></P>)

Part: WARNING MESSAGE — FALSE INDICATION (WX RADAR) · airframe 92,815 hrs · 23,731 cycles

PRIOR TO T/O WXR FAIL MESSAGE ON ADI(<P>PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM PER B767 AMM 34-43-00. OPS CHECK GOOD.</P>)

Part: ECU — MALFUNCTIONED (APU) · airframe 92,723 hrs · 23,713 cycles

APU AUTO SHUTDOWN. REMOVED & REPLACED ECU PER AMM 49-61-05. OPS CHECK IS NORMAL.

Part: EXCITER — INOPERATIVE (APU) · airframe 92,665 hrs · 23,704 cycles

APU INOP ( AUXILIARY POWER UNIT (APU), EXCEPT ER OPERATIONS BEYOND 120 MINUTES (NOTIFY DISPATCH) R120 )(<P>TRANSFERRED TO MDDR 144881 PER MEL 49-11-01B CAT B DUE 08 APR 21</P><P>07 APR 21 LP 1335073 ITEM 2 - HHN-&NBSP;R AND R APU ECU BITE OK&NBSP; APU STILL FAILS TO START MDDR REMAINS OPEN.</P><P><SPAN>REMOVED AND REPLACED EXCITER IAW 49-41-03</SPAN><BR DATA-MCE-BOGUS="1" /></P>)

Part: APU — SHUTDOWN · airframe 92,614 hrs · 23,693 cycles

APU AUTO SHUTDOWN(<P>PERFORMED APU BITE PROCEDURE. NO FAULTS. OPS CHECK GOOD. REF FIM 49-11-00-815-958-003.<BR /></P>)

Part: MODULE — MALFUNCTIONED (CONFIGURATION) · airframe 92,614 hrs · 23,693 cycles

HAD A TAKE OFF CONFIG WARNING WHEN T/O. LOW SPEED REJECT. WE NOTIFIED ON L PT ADI, SPD LIMIT LOWER LEFT CORNER CAPT ADI ONLY.(<P>REMOVED AND REPLACED FSEU PER B767 AMM 27-51-01, OPS CHECK GOOD, NO FAULTS NOTED AT THIS TIME, S/N OFF: D01215, P/N OFF: 285T0049-63. REMOVED AND REPLACED FLAP/STAB POSITION MODULE PER B767 AMM 27-58-01. PERFORMED MCDP GROUND TEST # 65 &AMP; 64 PER FIM 22-04 FT 810 AND 22-04 FT 811. NO FAULTS NOTED AT THIS TIME.</P>)

Part: CONTAINER — BROKEN (CONTAMINATE BAG) · airframe 92,542 hrs · 23,674 cycles

AVSAX CONTAINMENT BAG VACUUM SEAL BROKEN AFT L/H CLOSET(<P>REMOVED &AMP; REPLACED AVSAX CONTAINMENT BAG AS REQUIRED PER AMM 25-64-00. CK'D OK.</P>)

Part: LIFE RAFT — LOW PRESSURE (MAIN DECK) · airframe 92,542 hrs · 23,674 cycles

M/D RAFT R/H ROW 20 OVHD BIN LOW PRESS FWD IND.(<P>REMOVED AND REPLACED M/D RAFT PER M/M 25-62-00-001 R/H</P>)

Part: SEAT BELT — WORN (COCKPIT) · airframe 92,542 hrs · 23,674 cycles

COCKPIT F/O L/H SEAT BELT TSO MARKING ILLEGIBLE(<P>REMOVED &AMP; REPLACED F/D F/O LA BELT AS PER AMM 20-11-00. PERFORMED OPS CHECK PER AMM&NBSP;&NBSP;</P><P>25-11-01. OPS CHECK GOOD.</P>)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,542 hrs · 23,674 cycles

AFT UPPER RIGHT FUESELAGE FOUND E EMERG. LIGHT INOP (OUT)(<P>RELAMPED AFT RH UPPER FUSELAGE EMG. LT. &AMP; OPS CHECK OK AMM 33-51-00</P>)

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 92,542 hrs · 23,674 cycles

FLIGHT DECK EMERG. LIGHT INOP(<P>REMOVED/REPLACED LT. ASY.&NBSP; M744 F/D EMG. PER AMM 33-51-02 &AMP; OPS CHECK EMG. LT SYS OK&NBSP;</P><P>AMM 33-51-00</P>)

Part: SWITCH — OUT OF ADJUST (SPEED BRAKE) · airframe 92,542 hrs · 23,674 cycles

AUTO SPEED BRAKE INOP (AUTO SPEED BRAKE SYST WITH SPEED BRAKE LOAD ALLEVIATION SYST INSTALLED - NOTIFY DISPATCH)(<P>T/S FIM 27-62-00/815; ADJUSTED ARMING SW.S371 &AMP; S493 PER AMM 27-62-06-212. AUTO S/B OPS TEST OK AMM 27-62-00/715. MDDR 143256 CLEARED UP / PLACARD REMOVED</P>)

Part: CLAMP — BROKEN (MEGAPHONE) · airframe 92,542 hrs · 23,674 cycles

R/H AFT CLOSET MEGAPHONE CLAMP DAMAGE(<P>REMOVED AND REPLACED DAMAGED MEGAPHONE BRACKET ASSY AT R/H AFT CLOSET PER B767-300&NBSP;&NBSP;</P><P>AMM 20-11-00-910-802</P>)

Part: LEAD — CRACKED (IGNITER) · airframe 92,542 hrs · 23,674 cycles

#2 ENGINE LOWER IGNITER LEAD END SHIELD IS CRACKED(<P>REMOVED AND REPLACED #2 ENGINE LOWER IGNITION LEAD IAW AMM 74-21-01. PENDING OPS CHECK.</P><P>PERFORMED&NBSP;OPS CHECK, GOOD.</P>)

Part: ACTUATOR — INOPERATIVE (APU INTAKE) · airframe 92,496 hrs · 23,665 cycles

APU INTAKE DOOR WILL NOT OPEN(<P>REMOVED AND REPLACED APU INTAKE&NBSP; DOOR ACTUATOR IAW B767 AMM 49-15-06. ACTUATOR OPS CHECK NORMAL

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 92,486 hrs · 23,664 cycles

EICAS L PACK TEMP MOMENTARILY FLASH ON RUNWAY PRIOR TO DEPARTURE(<P>REMOVED AND REPLACED L TEMP CONTROL VALVE. OPS CHECK GOOD AND NO DEFECTS FOUND. IAW AMM 21-51-12.</P>)

Part: APU — MALFUNCTIONED · airframe 92,486 hrs · 23,664 cycles

APU COLD START ATTEMPT -47C, FL 380, 3 START ATTEMPTS, 3 START FAILS, EGT 0 22 RPM(<P>PERFORMED APU BITE PER FIM 49-11 FT 958, MINI FLAG 34; LRU - "NO LIGHT OFF".&NBSP;RESET CLEARED, PERFORMED SUCCESSFUL GROUND START PER AMM 49-11-00. ECU SUMMARY- A/C START CIRCUIT.</P>)

Part: BATTERY PACK — INOPERATIVE (FWD FLASHLIGHT) · airframe 92,486 hrs · 23,664 cycles

FA POSITION L1 EMER FLASHLIGHT INOP. (REMOVED AND REPLACED L1 EMER FLASHLIGHT BATT IAW B767 MM 25-64-00. OPS CHECK NORMAL.)

Part: CONTROL VALVE — INOPERATIVE (LT A/C PACK) · airframe 92,486 hrs · 23,664 cycles

NO PACK OFF LIGHT ON OVERHEAD PANEL & NO L PACK OFF EICAS WHEN PACK SELECTED OFF. REMOVED AND REPLACED LEFT PACK FLOW CONTROL VALVE IAW B767 M/M 21-51-01, OPS CHECK NORMAL.

Part: A/C PACK — CONTAMINATED · airframe 92,486 hrs · 23,664 cycles

RUNWAY TREATMENT INGESTED IN PACK SYSTEM CAUSING SMOKE &AMP; EVACUATION BLOWERS TO GO OFF, NO INDICATION OR ACTUAL FIRE.(<P>OPERATIONAL CHECK OF A/C PACK SYSTEM/INSPECTIONS IAW B767 M/M 05-51-56. SYSTEM OPERATIONAL. CHECK NORMAL.</P>)

Part: BATTERY — INOPERATIVE (APU STARTER) · airframe 92,452 hrs · 23,656 cycles

APU WILL NOT START. REMOVED AND REPLACED APU BATTERY REF AMM 24-31-04. OPS CKS GOOD.

Part: APU — MALFUNCTIONED · airframe 92,443 hrs · 23,654 cycles

APU COLD SOAK START UNSUCCESSFUL AFTER 3 ATTEMPTS FL330 SAT -61 00.15Z RIV-HHN(<P>PERFORMED APU BITE IAW FIM 49-11-FT958. NO MINI FLAGS LRU NO LIGHT SUMMARY. NO DATA RESET. CLEARED, OPS CHECKED NORMAL ON GRD IAW MM 49-11-00.<BR /></P>)

Part: STOWAGE BOX — LEAKING (COCKPIT) · airframe 92,368 hrs · 23,642 cycles

LEAK IN O2 CREW SYSTEM. REMOVED AND REPLACED CREW O2 MASK STOWAGE BOX, IAW AMM 35-11-51. OPERATIONS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENG FIRE LOOP) · airframe 92,360 hrs · 23,640 cycles

LT ENGINE OH LP 1 STATUS MESSAGE. ON POWER TRANSFER STATUS MESSAGE APPEARED. PERFORMED AFOLT TEST, IAW B767 M/M 26-10-00 CLEARED. NO FAULTS NOTED.

Part: FAULT MESSAGE — FALSE ACTIVATION (APU) · airframe 92,305 hrs · 23,630 cycles

APU FAULT ON GROUND AFTER BLOCK IN. PERFORMED APU BITE, IAW FIM 49-11-00 FT 958, MINI FLAG 130. PERFORMED OPERATIONS CHECK OF APU SYSTEM, IAW B767 M/M 49-11-00, OPERATIONAL CHECK NORMAL. AIRCRAFT CLEARED TO CONTINUE ETOPS SERVICE.

Part: INDICATION SYS — NO INDICATION (LT A/C PACK) · airframe 92,301 hrs · 23,628 cycles

WITH LT PACK IN OFF POSITION PACK OFF LIGHT DOES NOT ILLUMINATE. ALSO EICAS DID NOT INDICATE LT PACK OFF. PERFORMED FIM TASK 21-51-00 BITE SYSTEM FAULT TEMP CONTROL VALVE. RESET SYSTEM. OPERATIONS CHECK NORMAL.

Part: CONTROLLER — FAILED (A/C PACKS) · airframe 92,197 hrs · 23,604 cycles

EICAS MESSAGE "L PACK" AT POWER UP. PERFORMED BITE TEST, IAW B767 AMM 21-51-14. TEST FAILED. HARD FAULT. REMOVED AND REPLACED LT CONTROLLER ASSMBLY PACK, IAW B767 AMM 21-51-14. OPERATIONS CHECK GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 92,158 hrs · 23,595 cycles

AISLE EMERGENCY LIGHT LENS MISSING ABOVE SEAT NR 1-2AC. INSTALLED AISLE EMERGENCY LIGHT LENS, IAW AMM 33-51-05. OPERATIONS CHECK GOOD.

Part: BLOWER — FAULTED (CARGO FIRE DETEC) · airframe 92,158 hrs · 23,595 cycles

STATUS MESSAGE FWD DET FAN. REMOVED AND REPLACED FWD CARGO SMOKE DETECTION BLOWER NR 1. OPERATIONS CHECKS GOOD, IAW AMM 26-16-02.

Part: GCU — INOPERATIVE (RIGHT) · airframe 92,158 hrs · 23,594 cycles

FOUND RESISTANCE ON CONN D10966P ON R IDG. R IDG DISCONNECT, PER DDG 24-00-01-01. TRANSFERRED TO MDDR 139461, CAT B DUE 16DEC20. PLACARD INSTALLED. ER RESTRICTED, DISPATCH NOTIFIED. PERFORMED T/S FIM 24-20 TASK 804 FOR MESSAGE ON BPCU CT LOOP GROUND, FOUND POINT A AT D2568 PIN D13 SHORT TO GROUND THRU IDG TO D2568 PIN D13. MDDR REMAINS OPEN. PLEASE REF LP 1262464 ITEM M10 AND 1262466 ITEM 18 FOR PREVIOUS BUT PVS P/S. FOUND R GCU INOPERABLE. R & R PER AMM 24-22-02. OPERATIONS CHECK NORMAL. MCC NOTIFIED PLACARD REMOVED THIS CLEARS MDDR 139461.

Part: CIRCUIT BREAKER — TRIPPED (FUEL PUMP) · airframe 92,158 hrs · 23,594 cycles

LT FWD FUEL PUMP EICAS COMPLIED WITH QRH. FOUND C/B POPPED LT FWD FUEL PUMP, RESET C/B, CLEARED MESSAGE. RAN BOOST PUMP MULTIPLE TIMES, NO DEFECT FOUND, IAW 28-22-00.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 92,148 hrs · 23,591 cycles

SEAT 22K AISLE EMERGENCY LIGHT INOPERABLE. REMOVED AND REPLACED AISLE EMERGENCY LIGHT LAMP. OPERATIONS CHECKS GOOD, IAW AMM 33-51-05.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 92,154 hrs · 23,592 cycles

L1 AND R1 DOOR INTERIOR EMERGENCY LIGHTS INOPERABLE. REMOVED AND REPLACED FWD CABIN EMERGENCY BATTERY POWER SUPPLY, OPERATIONS NORMAL.

Part: STATUS MESSAGE — FALSE ACTIVATION (RT ENGINE N2) · airframe 92,107 hrs · 23,584 cycles

RT ENGINE N2 ANALOG STATUS MESSAGE. PERFORMED PIMU BITE TEST, IAW 71-01 FT 810, NO FAULTS NOTED. OPERATIONS CHECK OK.

Part: ELT — NO TEST (CABIN) · airframe 92,107 hrs · 23,584 cycles

WHILE PREFORMING ELT TEST, AS PER WO 73334 FOUND ELT TO BE INOPERABLE. REMOVED AND REPLACED ELT 25-63-03. FURTHER TS REVEALED COAX CABLE DAMAGE. RECONNECTED THE COAX AT ELT ANT M9003 AND REPLACED DG 224-1478-00 SWMP 20-57-15. PERFORMED CONTINUITY CHECKS, OPERATIONS GOOD.

Part: START VALVE — SLOW (LEFT) · airframe 92,083 hrs · 23,578 cycles

LT STARTER VALVE VERY SLOW TO OPEN DURING START. IT TOOK OVER 10-15 SECONDS TO OPEN WHEN PLACED IN GROUND. MANUALLY CYCLED LT START VALVE SEVERAL TIMES. OPERATIONS OF START VALVE AND IND IS NORMAL, AS PER AMM 80-11-02.

Part: DUCT — LEAKING · airframe 92,017 hrs · 23,563 cycles

PNUEMATIC DUCT IN LEFT WHEEL WELL FWD CLAMP LEAKING AIR. UPON INSPECTION FOUND DUCT CRACKED AND LEAKING. REMOVED AND REPLACED APU PNUEMATIC DUCT, IAW AMM 36-11-01 AND LEAK CHECKED FOUND OK.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,986 hrs · 23,557 cycles

EMERGENCY AISLE LIGHT INOPERATIVE AT SEAT NR 1AC. REMOVED AND REPLACED AISLE LIGHT LAMP, IAW AMM 33-51-05. CHECKED GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,956 hrs · 23,550 cycles

EMERGENCY AISLE LIGHT INOPERATIVE AT SEAT NR 1 A/C. REMOVED AND REPLACED AISLE LIGHT LAMP, IAW AMM 33-51-05, CHECKS GOOD.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 91,826 hrs · 23,525 cycles

L-1 EXTERIOR EMERGENCY LIGHT INOPERABLE. RELAMPED L-1 DOOR EMERGENCY LIGHT. OPS TEST EMERGERGENCY LIGHT OK, AMM 33-51-00/715.

Part: GENERATOR — MALFUNCTIONED (APU) · airframe 91,826 hrs · 23,525 cycles

INSTALL GENERATOR ON REPLACEMENT APU (A/N P-367C). INSTALLED NEW GENERATOR, AS PER B767-300 AMM 24-21-01. PENDING APU GENERATOR SYSTEM TEST. APU GENERATOR OPS GOOD, REF AMM 49-11-00. P/N ON 727810C S/N 0175.

Part: ANTENNA — DAMAGED (VHF COMMS) · airframe 91,826 hrs · 23,525 cycles

RT VHF COMM COAX CABLE SYSTEM INSP "VSWR FAIL". REMOVED AND REPLACED RT VHF COMM ANTENNA M246, PER AMM 23-12-03. VHF COMM SYSTEM TEST PASS, PER AMM 23-12-00/705. P/N OFF DMC50-17 S/N 22521 S/N ON 11626.

Part: ANTENNA — FAILED (DME) · airframe 91,826 hrs · 23,525 cycles

LEFT AND RIGHT DME INOPERABLE P/N DM 1601354-001. REMOVED AND REPLACED DME RT INTERROGATOR M124, OPS CHECK OK AMM 34-55-01. REMOVED AND REPLACED DME LT ANTENNA M263, OPS CHECK OK AMM 34-55-02. MDDR 133403 CLEARED UP, PLACARD REMOVED. P/N OFF 622-4540-122, S/N 6506, S/N ON 5818.

Part: ROLLER — LACK OF LUBE (L1 DOOR) · airframe 91,826 hrs · 23,525 cycles

L-1 DOOR IS HARD TO OPEN/CLOSE DUE TO TRACKS. REQUIRE CLEAN AND LUBRICATE BOTH DOOR ROLLER TRACKS. CLEANED AND LUBED BOTH TRACKS AND ROLLERS AS REQUESTED, PER AMM 12-21-18-603-006.

Part: BUSHING — FAILED (COMPRESSOR) · airframe 91,892 hrs · 23,536 cycles

DURING EO 1972A763 ENGINE HIGH PRESSURE COMPRESSOR (HPC) STAGE 5 VSV'S LEVER ARMS INSPECTION, SEVERAL VSV'S WERE FOUND WITH EVIDENCE OF METAL TO METAL CONTACT WITH HIGH PRESSURE COMPRESSOR CASE. ACCOMPLISHED (CF6-80C2) HIGH PRESSURE COMPRESSURE (HPC) STAGE 5 VSV'S BUSHING AND LEVER ARM REPLACEMENT, IAW EO 1972A630 PAGE 1 OF 13 WITH REVISION DATE 27/MAR/20 BY MTUD ENGINE SHOP UNDER WO 20114.

Part: ENGINE — STALLED (RIGHT) · airframe 91,713 hrs · 23,498 cycles

DURING CLIMBOUT AT APPROX PASSING 1300 FEET, RIGHT ENGINE COMPRESSOR STALLED SEVERAL TIMES. ENGINE DAMAGE INDICATOR, MAX EGT 995. REMOVED AND REPLACED NR 2 ENGINE, IAW ATLAS WC A-71-999-04-02, OPS CHECKED NORMAL.

Part: INTAKE — CORRODED (LT ENGINE) · airframe 91,645 hrs · 23,485 cycles

ON WALKAROUND FOUND LEFT ENGINE INLET COWL INSIDE AFT 12 O'CLOCK POSITION HAS CORROSION(<P>ACCOMPLISHED PERMANENT HOT BOND COMPOSITE REPAIR ON LEFT ENGINE IAW SRM 51-21-01, 54-12-01-1A-1 AND 54-12-01 REPAIR 6, BY AVENIR FAA CRS #8AVR479B W.O # W14997 FEAM R.O 5002234. FAA FORM 8130-3 ATTACHED</P>)

Part: PUMP — MALFUNCTIONED (LT FUEL CELL) · airframe 91,570 hrs · 23,467 cycles

L FUEL CTR TANK PUMP INOP (CENTER TANK FUEL PUMPS, ONE INOPERATIVE, CENTER TANK FUEL USED. REMOVED AND REPLACED L/H CENTER OVERRIDE PUMP IAW AMM 28-25-05.

Part: HEATER — INOPERATIVE (PITOT PROBE) · airframe 91,479 hrs · 23,451 cycles

CAPTAIN`S PITOT STATIC PROBE HEATER INOPERATIVE. REMOVED AND REPLACED THE CAPTAIN`S PITOT PROBE IAW AMM 34-11-01-004-309. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 91,222 hrs · 23,397 cycles

CENTER MAIN CABIN EMERGENCY CEILING LIGHTS AND PROXIMITY LIGHTS AT ROW 19 & 13 ARE INOP. REMOVED AND REPLACED BATTERY PACK AT M9711 IAW AMM 33-51-07. PERFORMED GOOD OPS CHECK IAW AMM 33-51-07. NO DEFECTS NOTED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,190 hrs · 23,389 cycles

FORWARD EQUIP COOLING MSG COMPLIED WITH QRH MSG CLEARED. PERFORMED OPERATIONS CHECK OF EQUIP COOLING IAW AMM 21-58-00. OPERATIONAL CHECK GOOD.

Part: GCU — MALFUNCTIONED (RIGHT) · airframe 91,174 hrs · 23,385 cycles

RIGHT IDG INOPERATIVE. TRANSFER TO MDDR #128942 IAW MEL 24-00-01-01 CAT B DUE DATE 31-MAY-2020 LOG PAGE 1138658. REMOVED AND REPLACED RT GCU IAW AMM 24-22-02. OPERATIONAL CHECK GOOD. THIS CLEARS MDDR 128942.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 91,174 hrs · 23,385 cycles

APU FAULT DURING APU START. PERFORMED APU BITE TEST IAW FIM 49-11 FT 958, FOUND FAULT 34, CLEARED. PERFORMED OPERATIONAL TEST, OK IAW AMM 49-11-00.

Part: FUEL FILTER — DIRTY (APU) · airframe 91,051 hrs · 23,356 cycles

UPON APU OIL SERVICE INSPECTION, FOUND FUEL FILTER DPI POPPED.(<P>REMOVED AND REPLACED&NBSP;APU FUEL FILTER IAW B767 AMM 49-31-04. LEAK AND OPS CK GOOD WITH APU RUNNING.</P>)

Part: TRANSDUCER — MALFUNCTIONED (OXYGEN SYSTEM) · airframe 90,980 hrs · 23,342 cycles

PER MCC CREW O2 REGULATOR ERRATIC PSI READING.(<P>REMOVED AND REPLACED&NBSP;CREW 02 REGULATOR &AMP; TRANSDUCER ASSY. IAW AMM 35-11-03.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,890 hrs · 23,324 cycles

STATUS LH ENG. HPSOV(<P>PERFORMED AIR SUPPLY CONTROL BITE PER B767 AMM 36-23-00 FAULTED LH HPC, PUSHED VERIFY, NO FAULTS AT THIS TIME.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,839 hrs · 23,315 cycles

STATUS MESSAGE "CABIN ALT AUTO 1"(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE PER FIM 21-31 FT 809, FAULT A/C MOTOR, PUSH VERIFY, NO FAULTS. SYSTEM OK.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,839 hrs · 23,315 cycles

STATUS MESSAGE "L ENG HPSOV".(<P>PERFORMED AIR SUPPLY CONTROL BITE PER 767 AMM 36-23-00. FAULT LH HPC. PUSHED VERIFY, NO FAULTS. SYSTEM OK.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 90,819 hrs · 23,311 cycles

CABIN ALT AUTO 1 STATUS MESSAGE.(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE. A/C MOTOR FAULT. PUSH VERIFY NO FAULTS, SYSTEM OK IAW AMM 21-31-00-705-001 (CPC BITE).</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,736 hrs · 23,295 cycles

CABIN ALTITUDE AUTO 1 STATUS MESSAGE.(<P>TRANSFERRED TO MDDR #125793 IAW MEL 21-31-01A, CAT "C", DUE DATE 25MAR20.</P><P>LP 1171509: PERFORMED FIM TASK 21-31 FAULT TREE 809 BITE TEST. NO FAULTS NOTED. MESSAGE CLEARED. THIS CLEARS MDDR 125793.<BR DATA-MCE-BOGUS="1" /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 90,750 hrs · 23,299 cycles

WXR FAIL ON BOTH RADAR SYSTEMS LEFT AND RIGHT.(<P>PERFORMED BITE OF WX RADAR SYSTEM IAW AMM / FIM 34-43 FAULT TREE 805 BLOCK 1 WX-1 AND WX-2. OPS CHECK GOOD AT THIS TIME.<BR /></P>)

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 90,699 hrs · 23,288 cycles

L2 DOOR EMERGENCY LIGHT INOP (EXTERNAL).(<P>RELAMPED L2 DOOR EMERGENCY LIGHT. OPS CHECK OK IAW AMM 33-51-00/705.</P>)

Part: BUSTLE — DAMAGED (EVAC SLIDE) · airframe 90,699 hrs · 23,288 cycles

DURING L1 DOOR SLIDE CHANGE BUSTLE M/D LATCHES DE-BONDED L&AMP;R SIDE.(<P>REMOVED BUSTLE AS PER AMM 25-66-01 AND SENT FOR REPAIR AVENIR AVIATION. AVENIR REPAIRED BUSTLE PER SRM 51-70-06-0G-0. REINSTALLED BUSTLE AS PER AMM 25-66-01.</P>)

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 90,632 hrs · 23,276 cycles

CABIN ALT AUTO 1 DISPLAYED (STATUS MESSAGE) ON BLOCK IN.(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE PER FIM 21-31 FT 803. AC MOTOR A CH FAULT FOUND. PUSHED VERIFY SWITCH, FAULT CLEARED. SYSTEM OK.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,613 hrs · 23,273 cycles

CABIN ALT AUTO 1 STATUS MSG.(<P>PERFORMED CABIN PRESSURE BITE PER FIM 21-31 FT 803, NO FAULTS. SYSTEM OK.<BR /></P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,592 hrs · 23,269 cycles

DURING DESCENT, CABIN AUTO INOP CAUTION EICAS MESSAGE STATUS PAGE SHOWED CABIN ALT AUTO 2. QRH PROCEDURES COMPLIED WITH.(<P>PERFORMED FIM 21-31 FT 804 CABIN AUTO INOP WITH MANUAL OPERATION NORMAL. PERFORMED CABIN PRESSURE BITE PER FIM 21-31 FT 803. SYSTEM OK.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,592 hrs · 23,269 cycles

CABIN ALT AUTO 1 STATUS MESSAGE DURING CRUISE.(<P>PERFORMED CABIN PRESSURE BITE PER FIM 21-31 FT 803. SYSTEM OK.</P>)

Part: SELECTOR PANEL — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,604 hrs · 23,271 cycles

CABIN ALT AUTO 1 STATUS MESSAGE DISPLAYED.(<P>TRANSFERRED TO MDDR 125070 PER MEL 21-31-01A, CAT C, DUE 06MAR20. JJT 0707Z.</P><P>LOG PAGE 1171654: REMOVED AND REPLACED CABIN PRESS SELECTOR PNL. OPS CK GOOD IAW AMM 21-31-01. THIS CLEARS MDDR 125070.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 90,453 hrs · 23,246 cycles

L ENG ANALOG N2 EICAS STATUS MESSAGE DISPLAYED IN FLIGHT.(<P>CLEARED STATUS MESSAGES. PERFORMED IDLE RUN IN ACCORDANCE WITH AMM 71-00-00. NO DEFECTS NOTED. ALL INDICATIONS OK.<BR /></P>)

Part: SWITCH — FAULTED (CABIN PRESURE) · airframe 90,438 hrs · 23,242 cycles

STATUS MESSAGE CABIN ALT AUTO 2(<P>PERFORMED BITE TEST OF CABIN PRESSURE&NBSP;CONT 2, FAULT ALT SW. CLEARED MESSAGE. BITE CHECK OK IAW MM 21-31-00.</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 90,429 hrs · 23,239 cycles

L ENG ANALOG N2 STATUS MSG(<P>PERFORMED STANDBY ENGINE INDICATOR BITE, REF&NBSP;AMM 77-41-00. PERFORMED ENG IDLE RUN IAW AMM 71-00-00. NO FAULTS NOTED.<BR /></P>)

Part: PRESSURE SWITCH — FAILED (OIL SYSTEM) · airframe 90,298 hrs · 23,213 cycles

RIGHT ENGINE OIL PRESSURE LIGHT WONT ILLUMINATE. REMOVED AND REPLACED LOW OIL PRESSURE SWITCH ON NR 2 ENGINE, IAW AMM 79-33-01. OPS CHECK DURING ENGINE TEST NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (CARGO DETECTOR) · airframe 90,215 hrs · 23,192 cycles

AFT CARGO DET 1 INOPERATIVE. LOWER CARGO COMPARTMENT FIRE DETECTION SYSTEMS, FWD AND AFT, DETECTORS. PERFORMED OPS TESTED IAW TASK 25-16-00-715-001. SMOKE DETECTION SYS TESTED NORMAL. MESSAGE CLEARED.

Part: CONTROL VALVE — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,215 hrs · 23,192 cycles

STATUS MESSAGE FOR CABIN ALT AUTO 1. FOLLOWED BITE PROCEDURE OF CABIN PRESSURE CONTROLLER IAW FIM 21-31-803. NO FAULTS NOTED. OK FOR CONTINUED SERVICE. REMOVED AND REPLACED THE LT FLOW CONTROL VALVE IAW AMM 21-51-01-404-012. PERFORMED OPS CHECK, OPS SATISFACTORY.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,164 hrs · 23,181 cycles

CABIN ALT AUTO 1 STATUS MESSAGE.(<P>PERFORMED BITE CHECK ON CABIN ALT 1 PRESS, NO FAULTS FOUND. CLEARED STATUS MESSAGE CABIN ALT 1 PRESS CTL, OPS CHECK GOOD IAW B767 AMM 21-31-00.</P>)

Part: OXYGEN BOTTLE — LOW PRESSURE · airframe 90,164 hrs · 23,181 cycles

ON PRE-FLIGHT INSPECTION, OXYGEN PRESSURE NOTED AT 617 PSI. ALL FLT DECK MASKS OPS CHECK NOT LEAKING. SUSPECT OXYGEN SYSTEM LEAK, OUTSIDE AIR TEMP 01 C.(<P>REMOVED AND REPLACED&NBSP;CREW O2 BOTTLE IAW B767 AMM 12-15-08 &AMP; GMM 3.28.2.&NBSP; NO LEAKS NOTED ON&NBSP; ENTIRE SYSTEM.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENG HPSOV) · airframe 90,153 hrs · 23,179 cycles

LEFT ENGINE HPSOV STATUS MESSAGE.&NBSP;(<P>PERFORMED AIR SUPPLY BITE IAW 36-23-00/501 HPC FAULT. RESET FAULT, AND CLEARED LEFT ENGINE HPSOV STATUS MESSAGE.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,125 hrs · 23,173 cycles

STATUS MESSAGE AFTER LANDING:CABIN ALT AUTO 1.&NBSP;(<P>PERFORMED BITE CHECK ON CABIN PRESSURE CONTROL 1, NO FAULTS FOUND. STATUS MESSAGE CLEARED IAW 21-31-00.</P>)

Part: CONTROLLER — FAULTED (TEMP) · airframe 90,108 hrs · 23,169 cycles

AUX ZONE TEMP CONTROLLER FAULTS CONTROLLER. REMOVED AND REPLACED AUX ZONE TEMP CONTROLLER PER AMM 21-61-12, OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION · airframe 90,106 hrs · 23,168 cycles

L ENG HPSOV STATUS MESSAGE.(<P>PERFORMED AIR SUPPLY BITE PER FIM 36-20 FT 804, FOUND L/H ENG HPSOV WIRING. PUSHED VERIFY BUTTON, NO FAULT LIGHT CAME ON. OK FOR SERVICE.</P>)

Part: MONITOR — FAULTED · airframe 90,065 hrs · 23,159 cycles

CABIN ALT AUTO 2 STATUS MESSAGE.&NBSP;(<P>PERFORMED BITE, FOUND AC MONITOR FAULT. CLEARED FAULT IAW B767 FIM 21-31. CLEARED STATUS MESSAGE.</P>)

Part: STATUS MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 90,057 hrs · 23,158 cycles

REPEAT WRITE-UP: CABIN ALT AUTO 2 STATUS MESSAGE.(<P>PERFORMED BITE CHECK, FOUND AC MONITOR FAULT. RESET FAULT IAW B767 AMM 21-31-00, FAULT CLEARED.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 90,046 hrs · 23,155 cycles

CABIN ALT AUTO 2 STATUS MESSAGE.&NBSP;(<P>RESET CABIN PRESSURE 2 IAW AMM 21-31-00, OPS CHECK OK. NO STATUS MESSAGE AT THIS TIME.&NBSP;</P>)

Part: SCREEN — LEAKING (MOTIVE FLOW) · airframe 90,023 hrs · 23,151 cycles

BEFORE PUSH BACK, NOTICED FUEL LEAK COMING FROM L WING INB CENTER TANK BOOST PUMP ACCESS PANEL.(<P>AFTER INSPECTION, FOUND OVERRIDE JETTISON PUMP MOTIVE FLOW SCREEN LEAKING. REMOVED AND REPLACED MOTIVE FLOW SCREEN ASSY IAW B767 28-22-05, NO LEAK NOTED AT THIS TIME.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,993 hrs · 23,146 cycles

STATUS MESSAGE: CABIN ALT AUTO 2.(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE PER FIM 21-31 FT 810, NO FAULTS AT THIS TIME.<BR /></P>)

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 90,002 hrs · 23,147 cycles

CABIN AUTO INOP: CABIN ALT AUTO CONTROLLERS 1 &AMP; 2 FAILED DURING DESCENT.(<P>PERFORMED CABIN PRESSURE CONTROLLER BITE, FAULTED A/C MOTOR. VERIFIED NO FAULT AT THIS TIME PER FIM 21-31 FT 810.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 89,966 hrs · 23,140 cycles

CABIN ALT AUTO 2 STATUS.&NBSP;(<P>ACCOMPLISHED BITE TEST FOR CABIN ALT AUTO 2 PER AMM 21-31-00. TEST PASSED, NO FAULTS NOTED. STATUS MESSAGE CLEARED.</P>)

Part: MOTOR — FAULTED (CABIN PRESSURE) · airframe 89,911 hrs · 23,130 cycles

CABIN ALT AUTO 2.&NBSP;(<P>PERFORMED FIM 21-31-00 FAULT TREE 810, FIG 110. FOUND FAULT AC MOTOR, MSG CLEARED. NO FURTHER FAULTS FOUND, OPS TEST NORMAL.&NBSP;</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 89,829 hrs · 23,113 cycles

CABIN ALT 1 STATUS MESSAGE.(<P>PERFORMED BITE CHECK ON CABIN PRESS CONTROLLER NR 1, NO FAULTS FOUND. RESET CONTROLLER, NO MSG AT THIS TIME. CABIN PRESS CTRL OPS CHECK GOOD IAW B767 AMM 21-31-00.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 89,720 hrs · 23,090 cycles

CABIN ALT AUTO 2 STATUS MESSAGE.(<P>PERFORMED BITE ON CABIN ALT CONTROLLER 2 PER B767 AMM 21-31-00. OPS CHECK NORMAL, NO FAULTS FOUND.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,666 hrs · 23,080 cycles

CABIN ALT AUTO 2 STATUS MESSAGE.(<P>PERFORMED BITE FUNCTION ON CABIN ALT AUTO 2 IAW AMM 21-31-00. NO FAULTS FOUND, AND OPS CHECK GOOD.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (CABIN PRESSURE) · airframe 89,643 hrs · 23,076 cycles

"CABIN ALT AUTO 2" STATUS MESSAGE AFTER LANDING. PERFORMED CABIN PRESSURE BITE PER FIM 21-31 FT 803. SYSTEM CHECKS OK.

Part: OXYGEN MASK — BROKEN (COCKPIT) · airframe 89,631 hrs · 23,071 cycles

CAPT OXYGEN MASK NORM/100% TAB AFT TIP IS BROKEN OFF. TAB IS STILL FUNCTIONAL. REMOVED AND REPLACED OXYGEN MASK AT CAPT POSITION IAW AMM 35-11-04, OPS CHECK GOOD.

Part: STARTER — FAULTY (APU) · airframe 89,603 hrs · 23,066 cycles

APU "NO START". ECU FAULTED "APU STARTER". REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. OPS CHECK GOOD.

Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 89,597 hrs · 23,065 cycles

FROM SELECTING TERRAIN TO WX, WXR FAIL ON BOTH SCREENS. PERFORMED OPERATIONAL CHECK OF THE WEATHER RADAR IAW AMM 34-43-00. SYSTEM OPS CHECK NORMAL.

Part: RELAY — FAILED (FUEL SYSTEM) · airframe 89,595 hrs · 23,064 cycles

L FWD FUEL PUMP EICAS IN FLIGHT. REFERENCE LP 1049220 - ITEM 1: FOUND TERMINALS A-1, A-3, AND C1 LOOSE INSIDE K102 GROUND SERVICE TRANSFER RELAY. REMOVED AND REPLACED K102 IAW AMM 24-51-03. PERFORMED INSTALLATION TEST IAW AMM 24-51-03, NO DEFECTS NOTED. ITEM 2 - PERFORMED OPS CHECK IAW AMM 28-00-00, NO DEFECTS NOTED.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,597 hrs · 23,065 cycles

EMERGENCY LIGHTS INOP AT SEATS 3AC, 13AC, 21AC, 27AC, AND 30AC. REMOVED AND REPLACED 1317 LAMP AT SEATS 3AC, 13AC, 21AC, 27AC, AND 30 AC IAW AMM 33-50-00.<

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,571 hrs · 23,060 cycles

CABIN ALT AUTO 2 STATUS MSG. PERF BITE CHK PER MM 21-31-00 TEST OK.

Part: CONNECTOR — LOOSE (BLEED AIR SYS) · airframe 89,368 hrs · 23,010 cycles

AFTER ENGINE START, NO ENGINE BLEED AIR ON RIGHT ENGINE. (<P>FOUND LOOSE CONNECTOR ON PRV CONTROL WIRES. RE-TIGHTENED IAW AMM 36-11-18. ENGINE WAS IDLE RUN IAW AMM 71-00-00. MESSAGE CLEARED.&NBSP;</P>)

Part: CONNECTOR — DAMAGED (AC BAY) · airframe 89,368 hrs · 23,010 cycles

LOWER FUSELAGE A/C BAY L COMP OUTLET TEMP BULB CONNECTOR DAMAGED.(<P>RE-ASSEMBLED FRONT RELEASE CONNECTOR D688 AND PACK OUTLET COMP. TEMP SENSOR PER SWPM 20-61-00 AND WD 21-51-12.</P>)

Part: WIRE — DISCONNECTED (CABIN) · airframe 89,368 hrs · 23,010 cycles

R1 DOOR EMERGENCY EXTERIOR LAMP INOP.(<P>FOUND WIRE BETWEEN LIGHT ASSY, L393 AND CONNECTOR D01122 OPEN. REMOVED CEILING AND WALL PANELS AT R/H STA: 425. FOUND WIRES DISCONNECTED AT CONNECTOR D06324J, SECURED AND CONNECTED CONNECTOR D06324J. INSTALLED CEILING AND WALL PANELS AT R/H STA: 425 IAW AMM 25-14-01, AND 25-15 01, WDM 33-51-21, AND SWPM 20-60-00. PERFORMED OPS CHECK IAW AMM 33-51-06, OPS CHECK NORMAL.</P>)

Part: ROD — DAMAGED (NR 1 COWLING) · airframe 89,368 hrs · 23,010 cycles

#1 ENGINE INBD FAN COWLING FWD HOLD OPEN ROD DAMAGED. (<P>REMOVED AND REPLACED ENGINE #1 INBD FAN COWLING HOLD OPEN ROD AS PER AMM 70-10-00.</P>)

Part: VALVE — FAULTY (AC BAY) · airframe 89,362 hrs · 23,008 cycles

EICAS RIGHT PACK TEMP, RIGHT PACK OFF. ACCOMPLISHED QRH PROCEDURES.&NBSP;(<P>PERFORMED PACK CONTROL SYSTEM BITE TEST IAW FIM 21-51-00, NO FAULTS NOTED, PACK OPS CHECK NORMAL.</P><P>LP 823381 - M5:&NBSP;RIGHT PACK&NBSP;FAILED ON GROUND.&NBSP;TRANSFERRED TO MDDR 115034 AS PER DDG 21-51-03, CAT "C". PACK TEMP CONTROL AUTO MODE INOP.&NBSP;&NBSP;&NBSP;&NBSP;&NBSP;</P><P>LP 823385 - M9: PREFORMED PACK TEMP CONTROLLER BITE TEST, FOUND LOW LIMIT VALVE FAULTY. REMOVED AND REPLACED LOW LIMIT VALVE, OPS AND LEAK CHECK GOOD. ALL WORK DONE PER AMM 21-51-14 AND 21-51-11. THIS CLEARS DMI 115034.</P><P><BR DATA-MCE-BOGUS="1" /></P><P>NOTE: ACCOMPLISHED DURING A-CHECK (MIA), REF NRC 00011.</P>)

Part: SENSOR — FAULTY (AC BAY) · airframe 89,318 hrs · 22,999 cycles

R PACK TEMP EICAS MSG DISPLAYED DURING DECENT, AROUND FL180 WENT AWAY, AND CAME BACK DURING LANDING.(<P>PERFORMED R PACK CTL BITE IAW FIM 21-51 FT 803, COMPRESSOR SENSOR FAULT. WAS ABLE TO RESET AND R PACK OPS CK NORMAL.<BR /></P>)

Part: COVER — NOT SEATED (EXIT SIGN) · airframe 89,335 hrs · 23,003 cycles

L1 EXIT SIGN LOOSE (<P>RE-SEATED L1 EXIT SIGN COVER, OPS CKS GOOD IAW AMM 33-51-00.<BR /></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 89,262 hrs · 22,987 cycles

ON INITIAL CLIMB RCVD EICAS MESSAGE "FWD EQUIP OVHT" EICAS MSG EXTINGUISHES AND RETURNED, THEN BACK ON COMPLETE FLIGHT WITH EQUIP COOLING SELECTOR IN STBY.(<P>PERFORMED FIM 21-58 FT 873 EQUIP COOL SYS BITE NO FAULT FOUND OVHT DUE TO EXTERNAL TEMP ON GROUND IN KWI SYSTEM OPS CK NORMAL.</P>)

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 89,243 hrs · 22,983 cycles

MASTER CAUTION CABIN AUTO INOP WHILE ON DESCENT&NBSP;(<P>RESET AND TESTED PX CONTROLLER IAW AMM 21-31-02-864-008. OPS CHECK NORMAL.</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 89,229 hrs · 22,981 cycles

L ENG CONTROL STATUS MESSAGE(<P>PERFORMED PIMU BITE IAW B767 FIM 71-01-00 FAULTED 354-20-B EEC CPU FAIL. CLEARED MSG &AMP; FAULTS, PERFORMED FIM 73-21 FT 878 ENG RUNS GOOD, NO FAULTS SYSTEM CHECK OK&NBSP;</P>)

Part: PLUG — DEFECTIVE (APU) · airframe 89,175 hrs · 22,971 cycles

APU FAILED TO START AFTER 3 ATTEMPTS, AFTER LANDING(<P>TRANSFERRED TO MDDR 113916 PER MEL 49-11-01, CAT C, DUE 08 JUL 19.</P><P>LP&NBSP;818865 - M11: REMOVED AND REPLACED EXCITER BOX ON APU REF AMM 49-41-03. DMI REMAINS OPEN AT THIS TIME. OFF PART(P/N: 10-617075-6, S/N 16030516)</P><P>LP&NBSP;818865 - M12: REMOVED AND REPLACED APU IGNITION LEAD IAW 49-41-04. REF LP 818867 ITEM 16 FOR IGNITER. OFF PART (P/N: 3888076-3, NSN)&NBSP;</P><P>LP 818867 - M16: REMOVED AND REPLACED APU IGNITION PLUG IAW AMM 49-41-02. OPS CHECK GOOD. THIS CLEARS MDDR 113916. PLACARD REMOVED.</P>)

Part: EXHAUST VALVE — MALFUNCTIONED (E&E BAY) · airframe 89,125 hrs · 22,963 cycles

RECEIVED FWD EQUIP OVHT ADVISORY MESSAGE ON CLIMB OUT. FOLLOWED QRH PROCEDURES.(<P>TRANSFERRED TO MDDR 113748 PER MEL 21-58-01-01, CAT "C", DUE 06-JUL-19.</P><P>LP 818862 - 2: REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05. OPS CHECK GOOD. MCC WAS NOTIFIED AND PLACARD REMOVED.</P><P>LP 818862 - 3: REF LP 818862 ITEM #2. THIS CLEARS MDDR 113748.</P><P><BR DATA-MCE-BOGUS="1" /></P>)

Part: MOTOR — FAULTED (CABIN PRESSURE) · airframe 89,125 hrs · 22,963 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. PERFORMED CABIN PRESSURE BITE, FOUND AC MOTOR FAULT. PERFORMED VERIFY MODE, NO FAULT. ALL WORK DONE PER FIM 21-31 FT 803.

Part: MOTOR — NOT REPORTED (CABIN ALTITUDE) · airframe 89,099 hrs · 22,956 cycles

CABIN ALT AUTO 2 STATUS MESSAGE IN FLIGHT. PERFORMED CABIN PRESSURE BITE, FOUND AC MOTOR. PERFORMED VERIFY MODE, NO FAULTS. ALL WORK DONE IAW FIM 21-31 FT 803.

Part: CONNECTOR — MALFUNCTIONED (ECU) · airframe 89,034 hrs · 22,938 cycles

DURING HOT PRE-FLIGHT, "R ENG CONT" STATUS MSG. REMOVED AND REPLACED ECU RATING/IDENT PLUG AT THE ECU J15 IAW AMM 73-21-19-007. R ENG, OPS CHECKED GOOD.

Part: CHARGER — MALFUNCTIONED (APU BATTERY) · airframe 89,034 hrs · 22,938 cycles

APU FAILED TO START (X3 ATTEMPTS). APU FAULT MSG ON EICAS.(<P>TRANSFER TO DMI 112857 IAW DDG 49-11-01A CAT 'C'.</P><P>LP 818924 - M6: REMOVED AND REPLACED APU BATTERY IAW AMM 24-31-04. OFF PART (SN: 062010, PN: 018550-000)</P><P>LP 818925 - M7: REMOVED AND REPLACED APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 112857. PLACARD REMOVED.</P>)

Part: EEC — MALFUNCTIONED (RT ENGINE) · airframe 89,020 hrs · 22,934 cycles

R ENG CONTROL EICAS MESSAGE. REMOVED AND REPLACED RT ENGINE EEC IAW AMM 73-21-15. OPS CHECK GOOD.

Part: START VALVE — MALFUNCTIONED (RIGHT) · airframe 89,020 hrs · 22,934 cycles

DURING CRUISE, AT FLT 350, MASTER CAUTION. R STARTER CUTOUT FOLLOWED BY R ENG STARTER ADVISORY MESSAGE DISPLAYED. REMOVED AND REPLACED R ENGINE START VALVE IAW AMM 80-11-02. OPS CHECK NORMAL.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 89,020 hrs · 22,934 cycles

CABIN ALT AUTO 1 STATUS MESSAGE. RESET CABIN PRESSURE CONTROLLER. TEST OK IAW AMM 21-31-00.

Part: HSI — MALFUNCTIONED · airframe 88,963 hrs · 22,921 cycles

WXR DISPLAY MSG ON HSI, REMOVED AND REPLACED LEFT HSI IAW AMM 34-22-04, LOADED SOFTWARE IAW AMM 34-22-00-472139. OPS CHECK GOOD. REMOVED AND REPLACED LEFT SYMBOL GENERATOR IAW AMM 34-22-01, LOADED SOFTWARE IAW AMM 34-22-00-472139. OPS CHECK GOOD.

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 88,971 hrs · 22,922 cycles

CABIN ALT AUTO 1 STATUS MSG. PERFORMED CABIN PRESSURE BITE PER FIM 21-31 FT 803 FAULT A/C MOTOR VERIFIED NO FAULTS. CLEARED, OK FOR SERVICE.

Part: CONTROL VALVE — DIRTY (LT A./C PACK) · airframe 88,971 hrs · 22,922 cycles

LEFT PACK OFF LIGHT AND L PACK OFF EICAS MESSAGE DO NOT INDICATE WHEN PACK IS OFF. CLEANED FLOW CONTROL AND SHUTOFF VALVE PER B767 AMM 21-51-01. OPS CHECK OF LEFT PACK OPS CHECK GOOD PER B767 AMM 21-00-00.

Part: TRANSCEIVER — DEFECTIVE (WEATHER RADAR) · airframe 88,961 hrs · 22,920 cycles

CA "WXR DSPY" MSG ON HSI AFTER TAKE OFF. (<P>REMOVED AND REPLACED RECEIVER/TRANSMITTER IAW AMM 34-43-01. OPS CHECK GOOD.<BR /></P>)

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,963 hrs · 22,921 cycles

L-1 PASS DOOR AFT GIRT BAR FITTING ON FUSE CORRODED 2 SQ IN AT ATTACH FASTENERS. (<P>REMOVED AND REPLACED L-1 PASS DOOR AFT GIRT BAR FITTING PLATE IAW SRM 51-40-02. ACCESS GAINED ON NR-00609.</P>)

Part: SKIN — DENTED (LE SLAT) · airframe 88,963 hrs · 22,921 cycles

CR - REPAIR DENT ON EXTERNAL SURFACE OF #10 SLAT ON O/B SIDE. (SEE NR 00233)(<P>CUT OUT DENT AT SLAT #10, FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS (2EA DOUBLER, AND STRAPS AND 1EA REPAIR PLATE). INSTALLED NEW REPAIR PARTS AT #10 SLAT O/B SIDE IAW SRM 57-30-01.&NBSP;</P>)

Part: GASKET — NOT REPORTED (LT WING) · airframe 88,963 hrs · 22,921 cycles

LEFT WING FUEL TANK ACCESS PANELS REQUIRE ALL NEW GASKETS. (<P>REMOVED AND REPLACED L/W ALL FUEL TANK ACCESS PANEL GASKETS IAW AMM 28-11-01. LEAK CHECK COMPLETE ON T/C T2031.&NBSP;</P>)

Part: DOOR FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,963 hrs · 22,921 cycles

L-1 DOOR CUTOUT FWD FRAME ON FUSE AT GIRT BAR FTG HAS 10 SQ IN EXFOLIATION CORROSION. (<P>REPAIRED L-1 DOOR CUTOUT FWD FRAME IAW DWG 691T0022 REV D AND FAS EA 19008 REV 1R.&NBSP;</P>)

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,963 hrs · 22,921 cycles

L-1 PASS DOOR FWD GIRT BAR FTG ON FUSE ATTACH PLATE BENEATH CORRODED 8 SQ IN. (<P>REMOVED AND REPLACED L1 PASS DOOR FWD GIRT BAR FITTING ATTACH PLATE IAW SRM 51-40-02. ACCESS GAINED ON NR-00609.</P>)

Part: SWITCH — MALFUNCTIONED (FIRE WARNING) · airframe 88,963 hrs · 22,921 cycles

RIGHT ENGINE FIRE HANDLE LIGHT ILLUMINATES WHEN HANDLE IS PULLED UP. (<P>REMOVED AND REPLACED RT ENGINE FIRE HANDLE FIRE SWITCH IAW AMM 26-21-02. OPS CHECKED SATISFACTORY.</P>)

Part: EXHAUST VALVE — FAULTY (E&&E BAY) · airframe 88,963 hrs · 22,921 cycles

LOGBOOK PAGE 1058162 ITEM #M8- AFTER L ENG SHUT DOWN FWD EQUIPMENT VALVE EICAS MESSAGE.&NBSP;(<P>REMOVED AND REPLACED OVERBOARD EXHAUST VALVE IAW AMM 21-58-05. PERFORMED SATISFACTORY OPERATIONAL CHECK OF OVERBOARD EXHAUST VALVE IAW AMM 21-58-05.&NBSP;</P>)

Part: POST — DETACHED (NR 2 IDG) · airframe 88,963 hrs · 22,921 cycles

IDG #2: UPON REMOVAL OF T2 TERMINAL, NOTICED T2 &AMP; T3 TERMINAL POSTS ARE DETACHED. (<P>REMOVED AND REPLACED #2 IDG TERMINAL BLOCK IAW AMM 24-11-20. OPERATION CHECK TO BE COMPLETED ON T/C T2031.</P>)

Part: BLADE — DAMAGED (EXHAUST FAN) · airframe 88,963 hrs · 22,921 cycles

UPON REMOVAL, FOUND FWD E/E COOLING EXHAUST FAN ROTOR TO HAVE CRACKED BLADE.&NBSP;(<P>REMOVED AND REPLACED FWD E/E COOLING EXHAUST FAN IAW AMM 21-58-06. INSTALLATION CK GOOD.&NBSP;</P>)

Part: WIRE — BROKEN (CARGO BAY) · airframe 88,963 hrs · 22,921 cycles

DAMAGED WIRES @ LT OF FWD CARGO STA. 390 &AMP; 632(<P>REPAIRED TWO BROKEN WIRES AT LT OF THE FWD CARGO COMP AT STA 390 AND STA 632 IAW SWPM 20-10-13. PERFORMED SATISFACTORY OPS CHECK OF HEATER TAPE IAW AMM 30-71-00 AND PERFORMED SATISFACTORY OPS CHECK OF FWD RACK SUPPLY FAN IAW AMM 21-58-06.</P>)

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 88,963 hrs · 22,921 cycles

BS 390 RBL 54.75 SEAT TRACK IS CRACKED. (<P>REMOVED AND REPLACED SEAT TRACK SECTION STA 390 RBL 54.75 IAW SRM 51-40-02 AND DWG 141T5120 REV. C, E.&NBSP;</P>)

Part: SENSOR — MISSING (AC BAY) · airframe 88,963 hrs · 22,921 cycles

LT PRIMARY HEAT EXCHANGER INLET TEMP IND IS MISSING. &NBSP;(<P>UPON TROUBLESHOOT, REMOVED AND REPLACED LT PRIMARY HEAT EXCHANGER INLET TEMPERATURE BULB IAW AMM 21-52-08-404-010. PERFORMED GOOD OPS CHECK WITH NO DEFECTS NOTED AND INDICATION IS BACK ON EICAS IAW AMM 21-52-08-404-010.</P>)

Part: FITTING — CORRODED (FUSELAGE) · airframe 88,963 hrs · 22,921 cycles

L-1 PASS DOOR FWD GIRT BAR FTG ON FUSE CORRODED 4 SQ IN. (<P>REMOVED AND REPLACED L-1 PASS DOOR FWD GIRT BAR FITTING IAW SRM 51-40-02. ACCESS GAINED ON TASK NR-00609.</P>)

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 88,963 hrs · 22,921 cycles

CORROSION FOUND ON MAIN CABIN FLOOR SUPPORT FRAME T CAP AT BS 325 RBL 25. (<P>REPAIRED MAIN CABIN FLOOR SUPPORT BEAM AT STA 325 RBL 25 IAW SRM 53-00-51-2R-1.</P>)

Part: CONNECTOR — BROKEN (AC BAY) · airframe 88,963 hrs · 22,921 cycles

LT PACK BAY CONNECTOR D1344 IS BROKEN. (<P>REMOVED AND REPLACED CONNECTOR D1344 IAW WDM 21-52-31 AND SWPM 20-61-19. PERFORMED SATISFACTORY OPS CHECK OF DISTURBED SYSTEMS IAW AMM 21-52-01 STEP F, NO DEFECTS NOTED.&NBSP;</P>)

Part: GENERATOR — LEAKING (LEFT) · airframe 88,963 hrs · 22,921 cycles

LT MLG WHEEL WELL I/B BULKHEAD, HMG HAS EVIDENCE OF HYDRAULIC LEAK. (<P>REMOVED AND REPLACED HYD. MOTOR GENERATOR FOR LEAKAGE IAW AMM 24-25-01. PERFORMED INSTALL TEST SATISFACTORY, NO LEAK.&NBSP;</P>)

Part: GASKET — NOT REPORTED (RT WING) · airframe 88,963 hrs · 22,921 cycles

RIGHT WING FUEL TANK ACCESS PANELS REQUIRE ALL NEW GASKETS. &NBSP;(<P>REMOVED AND REPLACED ALL GASKETS ON R/W FUEL PANELS IAW AMM 28-11-01. LEAK CHECK COMPLETED ON T/C T2031.</P>)

Part: SKIN — DENTED (LE SLAT) · airframe 88,963 hrs · 22,921 cycles

LT WING #6 L/E SLAT UPPER SURFACE HAS DENTED REPAIR DOUBLER ON T/E WEDGE 8 INCHES FROM I/B END OF SLAT.&NBSP;(<P>REPAIRED # 6 L/E SLAT UPPER SURFACE ON T/E WEDGE, 8 INCHES FROM I/B END IAW SRM 51-70-10.</P>)

Part: ECU — FAULTY (APU) · airframe 88,963 hrs · 22,921 cycles

APU FAULT MSG SHOWS ON LOWER EICAS.(<P>REMOVED AND REPLACED APU ECU IAW B767 AMM 49-61-05.&NBSP;</P>)

Part: GCU — FAILED (RIGHT) · airframe 88,963 hrs · 22,921 cycles

RT GCU FAILS DURING ENGINE RUNS. (<P>REMOVED AND REPLACED RT GCU IAW AMM 24-22-02.</P>)

Part: WARNING MESSAGE — ILLUMINATED (EQUIPMENT VALVE) · airframe 88,953 hrs · 22,920 cycles

AFTER LANDING ON TAXI IN AFTER L ENG SHUT DOWN, FWD EQUIP VALVE EICAS MESSAGE COMPLIED WITH QRH.(<P>TRANSFERRED TO MDDR 109469<BR /></P>)

Part: RADAR — INOPERATIVE · airframe 88,831 hrs · 22,897 cycles

LEFT WEATHER RADAR INOP.&NBSP;(<P>TRANSFERRED TO MDDR&NBSP;109090 AS PER DDG 34-43-01 CAT "D".</P><P>REF LOGPAGE 1026869:&NBSP;<SPAN>REMOVED AND REPLACED LEFT RADAR IAW AMM 34-43-01 OPS CHECK GOOD THIS CLEARS MDDR 109090&NBSP;</SPAN></P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,791 hrs · 22,887 cycles

STATUS MESSAGE CABIN ALTITUDE AUTO 2&NBSP;(<P>PERFORMED FIM 21-31 FT 803, FAULTED AC MOTOR. RESET, CLEARED, AND VERIFIED NO REPEAT.&NBSP;</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,774 hrs · 22,881 cycles

AFTER START " RIGHT ENGINE CONTROL" CAUTION MESSAGE&NBSP;(<P>PERFORM FIM 73-21 FT 878 SYSTEM TEST OK NO FAULTS ON PIMU AIRCRAFT RELEASE TO SERVICE&NBSP;</P>)

Part: ECU — MALFUNCTIONED (RT ENGINE) · airframe 88,726 hrs · 22,873 cycles

AFTER ENGINE START, NR 2 ENGINE R ENG CONTROL EICAS MESSAGE.&NBSP;(<P>REMOVED AND REPLACED RT ENG ECU PER AMM 73-21-15. OPS CHECK GOOD. (P/N OFF: 1820M33P14 S/N OFF: LMDD8086). LP 1062326-M2: REMOVED AND REPLACED RT PIMU IAW AMM 77-35-02, OPS CHECK GOOD.</P>)

Part: CONNECTOR — DIRTY (AC BAY) · airframe 88,705 hrs · 22,869 cycles

UNABLE TO SHUT OFF LEFT PACK.&NBSP;(<P>CLEANED CONNECTORS ON LEFT PACK FLOW CONTROL VALVE. OPS CHECK GOOD IAW AMM 21-51-00.</P>)

Part: STARTER — FAULTY (RT ENGINE) · airframe 88,705 hrs · 22,869 cycles

UNABLE TO START RIGHT ENGINE START VALVE DOESN'T OPEN&NBSP;(<P>REMOVED AND REPLACED RIGHT ENGINE STARTER IAW AMM 80-11-01, OPS CHECK GOOD IAW AMM 80-11-00.&NBSP;</P>)

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 88,692 hrs · 22,866 cycles

NR 2 ENGINE STARTER FAIL(<P>REMOVED AND REPLACED NR 2 ENGINE STARTER ASSEMBLY IAW AMM 80-11-01. OPS CHECK AND LEAK CHECK GOOD. NO DEFECTS NOTED.&NBSP;</P>)

Part: CHECK VALVE — FAULTY (FUEL SYSTEM) · airframe 88,692 hrs · 22,866 cycles

LOGBOOK ITEM: FUEL MIGRATION TO CENTER TANK 2000 LBS ON DESCENT.(<P>REMOVED AND REPLACED R/W AUX MANIFOLD DRAIN CHECK VALVE. PERFORMED LEAK CHECK, LEAK CHECK GOOD. NO LEAKS NOTED IAW AMM 28-21-05 AND 28-11-02.</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,699 hrs · 22,868 cycles

R ENG CONTROL DISPLAYED ON EICAS AND STATUS MESSAGE(<P>PERFORMED RIGHT PIMV BITE RESET PIMV TO MAKE SURE THAT MSG WAS NOT CAUSED BY EEC NOT BEING SUPPLIED WITH POWER. NO FAULTS SHOWN. GROUND TEST DONE PER 71-01 FT 810, SYSTEM CHECKS OK.</P>)

Part: WARNING MESSAGE — ILLUMINATED (CABIN PRESSURE) · airframe 88,654 hrs · 22,857 cycles

IN CRUISE FLT EICAS MSG CABIN AUTO INOPERATIVE. FOLLOWED QRH.(<P>PERFORMED CABIN PRESS BITE, FOUND A/C MOTOR PUSHED VERIFY NO FAULTS IAW FIM 21-31 FT 803.

Part: SHUTOFF VALVE — MALFUNCTIONED (LEFT) · airframe 88,666 hrs · 22,860 cycles

LEFT BLEED VALVE REMAINED CLOSED AFTER START. REPLACED THE LEFT HPSOV IAW AMM 36-11-07. OPS CHECKED GOOD.

Part: BULB — BURNED OUT (AUTO PRESSURE) · airframe 88,569 hrs · 22,839 cycles

#1 AUTO PRESSURE ASSY AC POWER OFF BULB BURNED OUT.(<P>R&AMP;R AUTO PRESSURE UNIT ASSY IAW AMM 21-31-02.<BR /></P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 88,450 hrs · 22,812 cycles

CABIN ALT AUTO 2 STATUS MSG&NBSP;(<P>BITE CHECK CABIN PRESSURE CONTROLLER # 2 NO FAULTS CLEARED STATUS MSG I.A.W AMM 21-31-00</P>)

Part: FAN — FAULTY (E&E BAY) · airframe 88,367 hrs · 22,796 cycles

FWD EQPT VAL MESSAGE AND EQPT COOLING VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED EXHAUST FAN 21-58-05. OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,343 hrs · 22,790 cycles

"L ENG CONTROL" EICAS MSG AFTER ENG START(<P>PERFORMED BITE CHECK IAW FIM 71-01 FT 811. CLEARED PREVIOUS FAULT DUE TO MAINT. PERFORMED. NO DEFECTS NOTED, AIRCRAFT CLEARED TO CONTINUE "ETOPS" SERVICE&NBSP;<BR /></P>)

Part: SENSOR — FAULTY (LT ENGINE) · airframe 88,356 hrs · 22,794 cycles

OIL TEMP BLANKED ON LT ENGINE.(<P>REPLACED LT ENGINE OIL TEMP SENSOR IAW AMM 79-34-01. OPS CHECK GOOD.<BR /></P>)

Part: CONNECTOR — DIRTY (LT ENGINE) · airframe 88,330 hrs · 22,787 cycles

LEFT ENGINE OIL TEMP INDICATION ERRATIC IN FLIGHT, ALL OTHER EICAS INDICATIONS OK&NBSP;(<P>CLEANED, INSPECTED AND RETORQUED OIL TEMP SENSOR PLUG IAW AMM 79-34-00, NO DEFECT NOTED, ENGINE RUN IAW AMM 71-00-00 OIL TEMP STABLE @ 53C DURING IDLE FOR 5 MINUTES SYSTEM OPERATES NORMAL&NBSP;</P>)

Part: BULB — DEFECTIVE (LT ENGINE) · airframe 88,324 hrs · 22,786 cycles

LEFT ENGINE OIL TEMP INDICATED 35 DEGREES @ FL 360, OIL PRESSURE INDICATED 45, RIGHT ENGINE INDICATING 100 DEGREES&NBSP;(<P>REMOVED AND REPLACED LT ENGINE OIL TEMP BULB REF AMM 79-34-01 OPS CHECK GOOD , NO FAULTS NOTED&NBSP;</P>)

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 88,176 hrs · 22,749 cycles

CABIN AU AUB STATUS MSG DECENDING THROUGH FL 200. PERFORMED CK ON CABIN PRESS AMM 21-32-00 AC MOTOR FAULT RESET, NO FAULT. STATUS MSG CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 88,124 hrs · 22,738 cycles

CABIN ALT AUTO 2 STATUS MESSAGE. PERFORMED BITE TEST OF AUTO CABIN PRESSURE CONTROLLERS IAW AMM 21-31-00. BITE TEST GOOD, NO FURTHER DEFECTS NOTED. MSG CLEARED.

Part: WIRE HARNESS — DAMAGED (RT ENGINE) · airframe 88,007 hrs · 22,713 cycles

RIGHT ENGINE "OIL TEMP" INDICATOR BLANK(<P>REMOVED &AMP; REPLACED P13 HARNESS &AMP; TEMP SENSOR PER AMM 79-34-01 SWPM 20-60-00 OPS CKD OK PER AMM 71-00-00 RT ENG</P><P><BR /></P><P>SENSOR OFF S/N LEW80211 P/N 3100130</P>)

Part: CONTROLLER — MALFUNCTIONED (NR 2) · airframe 87,986 hrs · 22,705 cycles

CABIN AUTO ALTITUDE 2 STATUS MESSAGE. REMOVED AND REPLACED THE NR 2 CABIN PRESSURE CONTROLLER IAW AMM 21-31-02. OPS OK.

Part: FILTER — WARNING MESSAGE (LT ENGINE FUEL) · airframe 87,986 hrs · 22,705 cycles

L ENGINE FUEL FILTER EICAS MESSAGE. REMOVED AND REPLACED THE FUEL FILTER IAW AMM 73-11-03. OPS CHECKED GOOD, NO LEAKS NOTED.

Part: VALVE — FAILED (CABIN TEMP) · airframe 87,968 hrs · 22,702 cycles

MID CABIN ZONE TEMP CONTROL VALVE INOPERATIVE. REMOVED AND REPLACED THE LT MID CABIN AUX TRIM VALVE V135 IAW AMM 21-61-07, OPS CHECKED OK.

Part: IGNITION SYS — INOPERATIVE (RT ENGINE) · airframe 87,960 hrs · 22,700 cycles

RT ENGINE IGNITION SYS WAS INOPERATIVE. OPEN

Part: IGNITER — FAULTY (RT ENGINE) · airframe 87,930 hrs · 22,691 cycles

RIGHT ENGINE NO LIGHTOFF, ABORTED START. PLACED IGNITION TO BOTH ENGINE STARTED NORMALLY ON SECOND ATTEMPT. REMOVED AND REPLACED RT ENGINE IGNITER NR 2 IAW AMM 74-21-02. OPS CHECK GOOD.

Part: CLAMP — BROKEN (APU SURGE VALVE) · airframe 87,937 hrs · 22,694 cycles

FOUND APU SURGE VALVE CLAMP WAS BROKEN ON THE DUCT. REMOVED AND REPLACED THE CLAMP, LEAK CHECKED GOOD IAW AMM 49-53-01.

Part: VALVE — MALFUNCTIONED · airframe 87,937 hrs · 22,694 cycles

EICAS MESSAGE FOR MID CABIN TEMP. FOUND A FAULT IN THE AUX MID TRIM VALVE. PERFORMED AUX ZONE TEMP BITE IAW FIM 21-61 FT 804, FAULT CLEARED.

Part: CONTROLLER — MALFUNCTIONED (WINDOW HEAT) · airframe 87,918 hrs · 22,688 cycles

WINDOW HEAT SWITCH BACKGROUND LIGHT INOP. REMOVED AND REPLACED WINDOW HEAT CONTROLLER IAW AMM 30-41-02, OPS CK OK.

Part: MODULATING VALVE — FAULTY (CABIN TEMP) · airframe 87,912 hrs · 22,684 cycles

MID CABIN TEMP BEFORE ENGINE START. REMOVED AND REPLACED MID ZONE TRIM AIR MODULATION VALVE IAW AMM 21-61-07. OPS CK OK. REMOVED AND REPLACED AUX ZONE TEMP CONTROL IAW AMM 21-51-12. TEMP CONTROLLER S/N OFF 029C-116 P/N OFF 115C406-1.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,898 hrs · 22,682 cycles

EICAS MSG FUEL DISAGREE PAGE 2 IAW QRH FL 35 TOTALIZAR 51.6 CALCULATE 55.0 FIFFERENCE 3.4 TOTALIZER 48.6 CALCULATED 50.1 DIFERENCES 1.5, NO FUEL LEAKS. SYSTEM WITHIN LIMITS IAW SERVICE LETTER 767-SL- 28-1 AND SERVICE LETTER 767-SL-28-035-A.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,871 hrs · 22,677 cycles

MID CABIN TEMP CAUTION LIGHT DURING CRUISE. FOUND AUX MID TRIM VALVE. PERFORMED AUX ZONE TEMP BITE PER FIM 21-61-FT 804 FAULT CLEARED AND RESET OPS CHECK OK GOOD.

Part: CONNECTOR — DIRTY (OIL SYSTEM) · airframe 87,781 hrs · 22,657 cycles

RIGHT ENGINE OILTEMP INDICATOR BLANK IN CRUISE. INSPECTED CLEANED AND RE-SECURED C/P TO RIGHT ENGINE OIL TEMP INDICATOR IAW AMM 79-34-01. NO DEFECTS NOTED ENGINE RUN IAW AMM 71-00-00, ALL ENGINE PARAMETERS NORMAL.

Part: START VALVE — FAULTY (NR 2 ENGINE) · airframe 87,690 hrs · 22,640 cycles

NR 2 ENG START VALVE NEED REPL'D. REPL'D NR 2 ENG START VALVE, NORMAL OPERATION MM 80-11-02.

Part: CONNECTOR — DIRTY (START VALVE) · airframe 87,618 hrs · 22,624 cycles

AFTER SUCCESSFUL ENGINE START T STARTER CUTOUT AND RT ENG STARTER EICAS MESSAGE DISPLAYED. COMPLIED WITH QRH PROCEDURE. BOTH MESSAGES DISAPPEARED ABOUT 3 MINUTES LATER VALVE LIGHT EXTINGUISHED AT ALL TIMES. REMOVED START VALVE CONNECTOR AND CLEANED PER AMM 20-60-03. PERFORMED OPS CHECK OF START VALVE PER AMM 80-11-00 & 71-00-00. OPS CHECK GOOD.

Part: BULB — DIRTY (OIL TEMP) · airframe 87,597 hrs · 22,620 cycles

LEFT ENG OIL TEMP SHOWS 40C DURING CRUISE. RIGHT ENG SHOWS 105C. INSPECTED CLEANED AND RETORQUE OIL TEMPERATURE BULB AND CONNECTOR, IAW MM 79-34-00. OPS CHECK NORMAL IAW MM 71-00-00.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 87,435 hrs · 22,590 cycles

LEFT PACK BITE STATUS MSG. PERFORMED LEFT PACK BITE IAW AMM 21-51 FT 803. AC MOTOR FAULT RESET PACK CONTROLLER NO FAULTS, STAUS MESSAGE CLEARED.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 87,435 hrs · 22,590 cycles

CABIN ALT 2 STATUS MESSAGE. PERFORMED BITE ON CABIN ALT 2 CONTROLLER, RESET CONTROLLER PERFORMED BITE NO FAULTS STATUS MESSAGE IAW AMM 21-31 FT 803.

Part: CONNECTOR — DIRTY (OIL TEMPERATURE) · airframe 87,429 hrs · 22,585 cycles

LT ENGINE OIL TEMP INDICATOR (INOP) BLANK INDICATION. ALL OTHER ENGINE INDICATIONS NORMAL. INSPECTED, CLEANED AND RE-TORQUE OIL TEMPERATURE SENSOR CONNECTOR IAW MM 79-34-00. OPS CHECK NORMAL IAW MM 71-00-00.

Part: ACOUSTIC LINER — MISSING (LT ENGINE) · airframe 87,378 hrs · 22,578 cycles

POST FLIGHT, LEFT ENGINE AFT INBOARD CASE FAN ACUSTIC LINER SEGMENT PANEL AT 5 O'CLOCK POSITION MISSING. (FAN STATOR LINER) REPLACED LEFT ENGINE AFT INBOARD FAN STATOR LINER AT 5 O'CLOCK POSITION IAW AMM 72-33-01. PERFORMED REPAIR TO LEFT ENGINE INBOARD THRUST REVERSE HALF IAW EO 1978A221 REV DATE 18AUG18.

Part: SWITCH — MALFUNCTIONED (FUEL SYSTEM) · airframe 87,378 hrs · 22,578 cycles

BEFORE ENGINE START WITH CENTER FUEL, DURING PRE START FLOW, CENTER WING PUMPS INDICATED ON (NO PRESSURE LIGHT) AND NO CENTER WING PUMP EICAS. MECHANIC RESET FUEL SWITCH AND INDICATIONS APPEARED NORMAL. CLEANED AND ADJUSTED FUELING DOOR PROX SWITCH IAW AMM 28-21-09. SYSTEM OPERATES NORMAL.

Part: EXTENSION — DAMAGED (LT ENGINE) · airframe 87,396 hrs · 22,581 cycles

LEFT ENGINE FAN ACUSTIC LINER SEGMENT MISSING. REMOVED AND REPLACED FLOW PATH EXTENSION POSITION 4 O' CLOCK AS PER AMM 72-33-00-308-104-H00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,298 hrs · 22,559 cycles

FWD EQPT OVHT MSG ON EICAS DURING INITIAL CLIMB. ACCOMPLISHED OPERATIONAL CHECK OF FWD EQPT OVHT SYS. NO DISCREPANCIES NOTED IAW AMM 21-58-00.

Part: LENS — MISSING (CABIN) · airframe 87,279 hrs · 22,555 cycles

MISSING EMERGENCY LIGHT LENS, LEFT AISLE LOWER CEILING BY AFT ENTRY DOOR. INSTALLED EMERGENCY LIGHT LENS AT LEFT AISLE LOWER CEILING BY AFT ENTRY DOOR. OPS CHECK GOOD IAW WDM 33-51-13.

Part: CIRCUIT BREAKER — NOT SEATED (CABIN) · airframe 87,279 hrs · 22,555 cycles

LEFT AISLE EMERGENCY LIGHT INOP BY ROW 21. RE-SEATED CIRCUIT BREAKER, OPS CHECK NORMAL IAW AMM 33-10-00.

Part: CONTROL PANEL — MALFUNCTIONED (COCKPIT) · airframe 87,139 hrs · 22,530 cycles

BOTH ( LEFT & RIGHT ) RADARS FAILED PRIOR TAKE OFF. RE-RACK WX CONTROL PANEL PERFORMED WX OPS CHECK IAW AMM 34-43-00 SYSTEM CHECK NORMAL. CLEANED CONNECTOR.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 87,092 hrs · 22,520 cycles

WEATHER RADAR FAIL LEFT AND RIGHT ON INITIAL CLIMB OUT. REPLACED WEATHER RADAR PANEL ASSY. OPERATIONAL CHECK GOOD PER AMM 34-43-02.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 87,077 hrs · 22,518 cycles

APU FAULT. PERFORMED APU BITE PER FIM 49-11 FT 958. NO FAULTS NOTED.

Part: ECU — FAULTY (APU) · airframe 87,024 hrs · 22,506 cycles

APU AUTO SHUT DOWN MULTIPLE TIMES. REMOVED AND REPLACED ECU IAW AMM 49-61-05. OPS CHECK SATISFACTORY.

Part: CONTROL PANEL — FAULTY (COCKPIT) · airframe 86,993 hrs · 22,494 cycles

F/O WX ON TERRAIN DISPLAY INOP. REMOVED AND REPLACED EFIS CONTROL ON F/O`S IAW AMM 34-22-02. OPS CHECK GOOD IAW AMM 34-43-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 86,975 hrs · 22,491 cycles

APU FAULT EICAS ANNUNCIATED. PERFORMED APU BITE PROCEDURES IAW FIM 49-11FT 958 THERE ARE NO DIAGNOSTIC MINIFLAGS, CODE OR FAULT ACTIVE DURING APU OPERATION AT THIS TIME.

Part: SENSOR — FAILED (NR 1 ENGINE) · airframe 86,975 hrs · 22,491 cycles

L ENGINE OIL TEMP WENT BLANK. U- FLIGHT. REMOVED AND REPLACED NR 1 ENG OIL TEMP SENSOR IAW AMM 79-34-01. RAN ENGINE OPS CHECK OK, NO OIL LEAKS.

Part: ANNUNCIATOR — FAULTY (COCKPIT) · airframe 86,843 hrs · 22,460 cycles

F/O WX RADAR INOP MUST BE SELECTED ON TWICE BEFORE WILL WORK REPEAT ITEM. REMOVED AND REPLACED ANNUNCIATOR ASSY IAW SWPM 20-42-01.

Part: STATUS MESSAGE — FALSE ACTIVATION (RT IDG) · airframe 86,732 hrs · 22,435 cycles

RIGHT IDG VALVE STATUS MESSAGE. PERFORMED A BPCU BITE TEST IAW FIM 24-20 FT 802 , IDG HIGH DELAT TEMP FAULT. SERVICED THE RT IDG, .5 QT IAW AMM 12-13-03. RAN ENGINE IAW AMM 71-00-00, NO FAULTS NOTED.

Part: BATTERY — DISCHARGED (APU) · airframe 86,730 hrs · 22,434 cycles

APU FAULT EICAS AFTER LANDING. FOUND LOW VOLTAGE ON THE APU BATTERY. REMOVED AND REPLACED THE APU BATTERY ASSY IAW AMM 24-31-04. OPS CHECKED GOOD.

Part: CHARGER — LOW VOLTAGE (APU) · airframe 86,730 hrs · 22,434 cycles

APU BATTERRY CHARGER HAD LOW OUTPUT. REMOVED AND REPLACED THE APU BATTERY CHARGER IAW AMM 24-31-05. OPS CHECKED OK.

Part: LIGHT — LOOSE (CABIN) · airframe 86,741 hrs · 22,437 cycles

FWD GALLEY AISLE EMERGENCY STRIP LOOSE. RESECURED AISLE EMERGENCY STRIP REF AMM 33-51-05.

Part: FILTER — NOT REPORTED (RT IDG) · airframe 86,712 hrs · 22,428 cycles

STATUS MESSAGE FOR THE RT IDG VALVE. REMOVED AND REPLACED THE IDG AIR SHUTOFF VALVE FILTER IAW MM 24-11-07, OPS CHECKED OK.

Part: EXCITER — FAILED (APU) · airframe 86,706 hrs · 22,427 cycles

APU FAULT EICAS MESSAGE AFTER LANDING. BITE CHECKED THE ECU, FOUND OK, NO MINI-FLAGS, LAST RUN-NO LIGHT OFF. AUTO EVENT EGT 25-RPM-19 IAW MM 49-61-05. REMOVED AND REPLACED EXITER PLUG IAW MM 49-41-02, SYSTEM CHECKED NORMAL.

Part: EXCITER — DIRTY (APU) · airframe 86,695 hrs · 22,424 cycles

APU FAULT ON STARTUP AFTER LANDING, APU DID NOT START AFTER 3 ATTEMPTS. REMOVED, INSPECTED AND CLEANED CARBON DEPOSIT FROM APU EXCITER PLUG REINSTALLED OPS CHECKS IAW B767 AMM 49-41-02-107-016 OPS CHECKS NORMAL.</P>)

Part: EXCITER — FAILED (APU) · airframe 86,672 hrs · 22,421 cycles

APU FAULT, APU WILL NOT START. REMOVED AND REPLACED THE APU EXCITER IAW AMM 49-41-03, SYSTEM CHECKED NORMAL.

Part: ACTUATOR — MALFUNCTIONED (LT A/C PACK) · airframe 86,684 hrs · 22,423 cycles

DURING CRUISE LEFT PACK TEMP EICAS MESSAGE. COMPLIED WITH QRH, CONTINUED OPERATION IN STBY-N. REMOVED AND REPLACED THE LT PACK EXHAUST RAM AIR ACTUATOR IAW AMM 21-53-04. OPS CHECKED GOOD. NO FAULTS NOTED.

Part: ECU — FAILED (APU) · airframe 86,664 hrs · 22,420 cycles

DURING PRE-FLT, THE APU AUTO SHUTDOWN WITH APU FAULT MESSAGE. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05, SYSTEM CHECKED NORMAL.

Part: CIRCUIT CARD — MALFUNCTIONED (NR 1 FIRE LOOP) · airframe 86,664 hrs · 22,420 cycles

STATUS MESSAGE FOR THE LT ENGINE FIRE LOOP 1. REMOVED AND REPLACED THE ENGINE FIRE DETECTOR LOOP CARD IAW AMM 26-10-01/401, PERFORMED FIM 26-11 FT 804, AND PERFORMEDTHE FIRE /OVERHEAT TEST, NO STATUS MESSAGES.

Part: IGNITION SYS — FAULTED (APU) · airframe 86,625 hrs · 22,411 cycles

APU FAULT ON GROUND. R & R THE APU IGNITION UNIT IAW AMM 49-41-03. OPS CHECKED GOOD.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 86,613 hrs · 22,409 cycles

PHOTOLUMINESCENT FLOOR PATH LIGHTING MISSING 6.5" PIECE, FORWARD GALLEY AREA, INBOARD OF THE GALLEY CART CHILLER. INSTALLED MISSING FLOOR PATH LIGHTING STRIP.

Part: WIRE HARNESS — DAMAGED (NR 1 ENGINE) · airframe 86,613 hrs · 22,409 cycles

NR 1 ENGINE STARTER CONTROL VALVE, AFT CONNECTOR PLUG THREADS WERE STRIPPED. REMOVED AND REPLACED THE WIRE HARNESS HARNESS IAW AMM 73-21-18-024-100-H00 AND 73-21-18-424-107-H00.

Part: CHIP DETECTOR — DAMAGED (NR 1 ENGINE) · airframe 86,613 hrs · 22,409 cycles

NR 1 ENGINE STARTER MAGNETIC CHIP DETECTOR PLUG SHEARED RETAINING PINS. REPLACED NR 1 ENGINE STARTER CHIP DETECTOR.

Part: SHUTOFF VALVE — INOPERATIVE (NR 1 ENGINE) · airframe 86,613 hrs · 22,409 cycles

NR 1 ENGINE HPSOV DOES NOT CLOSE, EICAS DISPLAYS CAUTION, REMOVED AND REPLACED THE NR 1 ENGINE HPSOV IAW AMM 36-11-07-024-001-001 AND 36-11-07-424-016-001.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 86,637 hrs · 22,413 cycles

AISLE EMERGENCY OVERHEAD LIGHT INOPERATIVE AT SEAT 19L. FOUND THE BATTERY PACK CONNECTOR DISCONNECTED, CONNECTED THE CONNECTOR IAW AMM 33-51-00, OPS CHECKED NORMAL,

Part: IGNITION UNIT — FAULTY (APU) · airframe 86,613 hrs · 22,409 cycles

APU WILL NOT LIGHT OFF. REPLACED APU IGNITION UNIT.

Part: IGNITION LEAD — DIRTY (NR 2 ENGINE) · airframe 86,613 hrs · 22,409 cycles

NR 2 ENGINE IGNITER LEADS HAVE PITTING. CLEANED NR 2 ENGINE IGNITER LEADS.

Part: GLOWSTRIP — MISSING (CABIN) · airframe 86,613 hrs · 22,409 cycles

PHOTOLUMINESCENT FLOOR PATH LIGHTING MISSING 6.5" PIECE, FORWARD GALLEY AREA, INBOARD OF THE GALLEY CART CHILLER. INSTALLED MISSING FLOOR PATH LIGHTING STRIP.

Part: HMU — MALFUNCTIONED (LT ENGINE) · airframe 86,522 hrs · 22,386 cycles

LEFT FUEL CONTROL, ENGINE VALVE INDICATION INOPERATIVE. REMOVED AND REPLACED THE LT ENGINE HMU IAW AMM 73-21-14. OPS & LEAK CHECKED OK.

Part: RADAR — MALFUNCTIONED · airframe 86,443 hrs · 22,368 cycles

FIRST OFFICER`S WEATHER/TERRAIN INOPERATIVE. OPS CHECKED AWD RAW BITE CHECK IAW AMM 34-43-00, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE) · airframe 86,377 hrs · 22,358 cycles

LEFT ENGINE CONTROL STATUS MESSAGE. PERFORMED FIM 73-21 F/T 878, NO FAULTS. PERFORMED PIMU BITE IAW FIM 71-01-00, NO FAULTS.

Part: INDICATION SYS — MALFUNCTIONED (OIL TEMP) · airframe 86,377 hrs · 22,358 cycles

LEFT OIL TEMP INDICATION LOST. PERFORMED AN OPS TEST OF THE OIL TEMP INDICATION SYSTEM IAW IAW AMM 79-34-00. SYSTEM TESTED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 86,348 hrs · 22,352 cycles

RT SIDE WINDOW EICAS MESSAGE AFTER LANDING. PERFORMED A BITE TEST IAW FIM 30-41, FT 803, NO FAULTS NOTED. PERFORMED A GROUND TEST IAW AMM 30-41-00. NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (VALVE) · airframe 86,309 hrs · 22,344 cycles

FWD EQUIPMENT VALVE EICAS AFTER START. PERFORMED OPS CHECK OF THE VALVE IAW AMM 21-23-08, OPS CHECKED GOOD , NO FURTHER DEFECTS NOTED.

Part: WARNING MESSAGE — INTERMITTENT (LT ENGINE) · airframe 86,302 hrs · 22,342 cycles

EICAS MESSAGE FOR THE LEFT ENGINE FUEL VALVE DURING ENGINE SHUTDOWN. PERFORMED FIM FAULT TREE 808 BLOCK 11. PERFORMED WET MOTOR FOR LEFT ENGINE IAW AMM 71-00-00-H01, NO EICAS ADVISORY MESSAGE AT THIS TIME, BLOCK 21 STATES THIS WAS AN INTERMITTENT FAULT, OPS CHECKED GOOD. NO EICAS MESSAGE.

Part: FAN — FAILED (E/E BAY) · airframe 86,268 hrs · 22,334 cycles

STATUS MESSAGE FWD EQUIPMENT EXHAUST FAN. REMOVED AND REPLACED FWD EQUIPMENT EXHAUST FAN IAW AMM 21-58-06, OPS CHECKED GOOD.

Part: IGNITION UNIT — MALFUNCTIONED (APU) · airframe 86,169 hrs · 22,318 cycles

APU FAULT EICAS MESSAGE, ACCOMPLISHED QRH. R&R APU IGNITION UNIT AS PER AMM 49-41-03, OPS CHECKS GOOD, NO FAULTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (CABIN PRESSURE) · airframe 86,169 hrs · 22,318 cycles

CABIN ALT AUTO NR 2 INOP. TS PER FIM 21-31 FT 810 BLOCK 1, NO FAULTS, BLOCK 21 SYSTEM OK. C/W AUTO CABIN PRESS CONT 2 BITE TEST PASS, REF MM 21-31-00.

Part: APU — FAULTED · airframe 86,088 hrs · 22,299 cycles

APU FAULT, APU FAILED TO START. PERFORMED A BITE TEST ON ECU, NO LIGHT. FAULT CLEARED. IAW FIM 49-11, APU OPS NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN PRESSURE) · airframe 86,054 hrs · 22,291 cycles

EICAS MESSAGE FOR CABIN ALTITUDE AUTO 2. PERFORMED A BITE ON CABIN ALTITUDE CONTROLLER, NO FAULTS NOTED. RESET AND VERIFY COMPLETED, NO FAULTS NOTED. SYSTEM NORMAL IAW FIM 21-31, FT 803.

Part: BATTERY — DEFECTIVE · airframe 85,964 hrs · 22,274 cycles

APU FAULT ON APU START. REMOVED AND REPLACED BATTERY CHARGER & BATTERY IAW AMM 24-31-05 / 24-31-04. OPS CKD GOOD.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 85,993 hrs · 22,281 cycles

EMERGENCY OVERHEAD ISLE LIGHTS AT SEAT 3A AND 25A ARE INOP LEFT SIDE. REMOVED AND REPLACED BATTERY PACK CHARGER IAW AMM 33-51-07.

Part: VALVE — DEFECTIVE (BLEED AIR SYS) · airframe 85,993 hrs · 22,281 cycles

RIGHT ENGINE FAN AIR VALVE OPEN/CLOSES SWITCHES DISAGREE. REMOVED AND REPLACED FAN AIR VALVE IAW AMM 36-11-04.

Part: COVER — MISSING (CABIN) · airframe 85,993 hrs · 22,281 cycles

BETWEEN SEAT ROWS 16 AND 17 CABIN ZONE TEMP SENSOR FILTER COVER MISSING. INSTALLED NEW SENSOR FILTER COVER IAW AMM 21-61-06.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 85,993 hrs · 22,281 cycles

RIGHT OVERWING EMERGENCY EGRESS LIGHTS INOP. REMOVED AND REPLACED BATTERY CHARGER, OPS CHECK NORMAL IAW AMM 33-51-07.

Part: SHUTOFF VALVE — STUCK (BLEED AIR SYS) · airframe 85,993 hrs · 22,281 cycles

RIGHT ENGINE HPSOV STUCK PARTIALLY OPEN. REMOVED AND REPLACED RIGHT ENGINE HPSOV IAW AMM 36-11-07.

Part: DENSITOMETER — FAULTY (FUEL SYSTEM) · airframe 85,993 hrs · 22,281 cycles

EICAS MAINT MESSAGE "FUEL QTY BITE" WILL NOT CLEAR DG CODE. REMOVED AND REPLACED RT MAIN TANK DENSITOMETER IAW AMM 28-4-03. OPS CHECK NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 85,993 hrs · 22,281 cycles

L1 AND R1 EMERGENCY DOOR SLIDE LIGHTS INOP. REMOVED AND REPLACED BATTERY ASSY CHARGER AMM 33-51-07.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,993 hrs · 22,281 cycles

L4 AFT DOOR SLIDE EMERGENCY LIGHT INOP. CLEANED CONTRACT AND RELAMPED OPS CHECK NORMAL AS PER AMM 33-51-06.

Part: POWER SUPPLY — INOPERATIVE (EXTERIOR) · airframe 85,993 hrs · 22,281 cycles

EXTERIOR LEFT OVERWING EMERGENCY LIGHT EGRESS L389, L395 INOP. REMOVED AND REPLACED POWER SUPPLY M736 IAW AMM 33-51-07.

Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 85,941 hrs · 22,270 cycles

RIGHT ENGINE HPSOV EICAS MESSAGE IN CRUISE. REMOVED AND REPLACED RT ENG HPSOV.

Part: PRESSURE SWITCH — DIRTY (FUEL TANK) · airframe 85,926 hrs · 22,266 cycles

DURING CLIMB, HAD A CENTER RT FUEL PUMP EICAS MESSAGE WITH FUEL IN TANK. CLEANED THE OVERRIDE PUMP PRESSURE SWITCH IAW AMM 28-42-00, SYSTEM TESTED NORMAL.

Part: RADAR — MALFUNCTIONED (WEATHER SYSTEM) · airframe 85,909 hrs · 22,263 cycles

WEATHER RADAR FAULTED AT TOT 5 HOURS. PERFORMED A WEATHER RADAR BITE IAW FIM 34-43 FT 808, NO FAULTS NOTES, WEATHER RADAR OPS NORMAL IAW AMM 34-43-00.

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 85,868 hrs · 22,255 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. ACCOMPLISHED A CABIN ALTITUDE BITE TEST IAW FIM 21-31 FT 803, FAULTED THE MOTOR, ABLE TO CLEAR FAULT & EICAS MESSAGE CLEARED.

Part: RELAY — FAILED · airframe 85,803 hrs · 22,243 cycles

FWD EQUIPMENT VALVE EICAS MESSAGE. REMOVED AND REPLACED RELAY K340, OPS CHECKED NORMAL IAW AMM 21-58-00/001.

Part: WARNING MESSAGE — FALSE ACTIVATION (CABIN ALTITUDE) · airframe 85,625 hrs · 22,213 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. PERFORM A BITE CHECK IAW MM 21-31-00. ACFT MOTOR FAULT. RESET, CLEANED, NO REPEAT. SYSTEM NORMAL.

Part: CONNECTOR — DAMAGED (RAM AIR ACTUATOR) · airframe 85,618 hrs · 22,212 cycles

WHILE PERFORMING FIM 21-51, FOUND THE LT PACK RAM AIR EXHAUST DOOR ACTUATOR TO BE FAULTY, DAMAGED PIN NR 6 IN THE CONNECTOR D4288P. R & R THE LT RAM EXHAUST DOOR ACTUATOR IAW AMM 21-53-04, OPS CHECKED GOOD. NO DEFECTS NOTED.

Part: CONTROL VALVE — MALFUNCTIONED (NR 1 A/C PACK) · airframe 85,559 hrs · 22,198 cycles

NR 1 PACK WILL NOT TURN OFF. REMOVED AND REPLACED THE FLOW CONTROL VALVE IAW AMM 78-31-00. CHECKED NORMAL.

Part: CONNECTOR — DAMAGED (PACK CONTROLLER) · airframe 85,559 hrs · 22,198 cycles

LEFT PACK TEMP EICAS MESSAGE ILLUMINATED IN FLIGHT. PINNED THE NR 6 LEFT PACK CONTROL CONNECTOR D4288P IAW SWPM 20-60-00, OPS CHECKED NORMAL IAW AMM 21-53-04.

Part: ACTUATOR — FAILED (LT PACK EXHAUST) · airframe 85,547 hrs · 22,193 cycles

LEFT A/C PACK TEMP EICAS IN FLIGHT. REMOVED AND REPLACED THE LEFT PACK EXHAUST DOOR ACTUATOR, OPS CHECKED GOOD IAW AMM 21-53-04.

Part: CONTROLLER — FAILED (RT A/C PACK) · airframe 85,547 hrs · 22,193 cycles

RIGHT A/C PACK TEMP EICAS IN FLIGHT. REMOVED AND REPLACED THE RT PACK TEMP CONTROLLER, OPS CHECKED GOOD IAW AMM 21-61-03.

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK) · airframe 85,545 hrs · 22,192 cycles

FIVE MINUTES AFTER TOP OF DESCENT, AN EICAS FOR THE LT PACK HIGH TEMP. COMPLIED WITH QRH 2.33. OPS NORMAL IN STANDBY "N". BITE TESTED AND RESET THE PACK CONTROLLERS LEFT AND RIGHT IAW AMM 21-51-00, NO FURTHER DEFECTS NOTED.

Part: APU — FAILED · airframe 85,545 hrs · 22,192 cycles

APU PRESSURE LOW. REPLACED APU CONTROL UNIT IAW AMM 49-61-05, BITE TEST PASSED.

Part: SENSOR — FAILED (LT A/C PACK) · airframe 85,545 hrs · 22,192 cycles

LEFT PACK TEMP CONTROL BITE TEST FAILED. REMOVED AND REPLACED THE PACK AIR TEMP SENSOR ASSY IAW AMM 21-51-04, OPS CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 85,530 hrs · 22,187 cycles

RIGHT SIDE WINDOW EICAS MESSAGE. PERFORMED FIM 30-41 FT 803 AND AMM 30-41-00 NO FAULTS NOTED, SYSTEM OPERATES NORMAL.

Part: WARNING LIGHT — FALSE ACTIVATION (RT CONTROLLER) · airframe 85,515 hrs · 22,183 cycles

RIGHT PACK CONTROLLER FAULT, AFTER SELECTING STBY, INOPERATIVE LIGHT EXTINGUISHED. PERFORMED A PACK CONTROLLER BITE, SYSTEM FAULTED CONTROLLER, RESET, CLEARED AND VERIFIED NO REPEAT IAW AMM 21-51-00.

Part: CIRCUIT CARD — FAILED (LT A/C PACK) · airframe 85,498 hrs · 22,178 cycles

LEFT PACK TEMP EICAS MESSAGE DURING DESCENT, RAN QRH, LT PACK OPERATED IN NORMAL STANDBY MODE. R & R COMP OUTLET SWITCH S555, OVERHEAT SWITCH, AND FUEL CONTROL PC CARD IAW AMM 21-51-09.

Part: MOTOR — FAILED (OUTFLOW VALVE) · airframe 85,490 hrs · 22,175 cycles

STATUS MESSAGE FOR CABIN ALTITUDE AUTO 2. REMOVED AND REPLACED THE OUTFLOW VALVE ACTUATOR AC MOTOR IAW AMM 21-31-05. OPS CHECKED OK. NO STATUS MESSAGE.

Part: A/C PACK — WARNING MESSAGE (LEFT) · airframe 85,470 hrs · 22,171 cycles

LEFT PACK TEMPERATURE EICAS MESSAGE IN FLIGHT. PERFORMED FIM 21-51 FT 803. PACK OPS NORMAL.

Part: SWITCH — INOPERATIVE (RT EEC) · airframe 85,454 hrs · 22,167 cycles

R/H EEC GRD TEST SWITCH INOP.(<P>REMOVED AND REPLACED R/H EEC IAW AMM 73-21-15 OPS NORMAL<BR /></P>)

Part: CONTROLLER — MALFUNCTIONED (COCKPIT TEMP) · airframe 85,423 hrs · 22,161 cycles

DURING CRUISE LEFT PACK EICAS MSG AFTER MID CABIN TEMP SELECTED TO LOWER TEMP, C/W QRH CONTINUED IN STBY MODE. REMOVED AND REPLACED LT PACK TEMP CONTROLLER IAW AMM 31-51-14.

Part: WARNING LIGHT — FALSE ACTIVATION (LT A/C PACK) · airframe 85,423 hrs · 22,161 cycles

DURING CRUISE FLIGHT, THE LEFT PACK TEMP EICAS MESSAGE ILLUMINATED. PERFORMED A LT PACK BITE IAW FIM 21-51 FT 803, NO FAULT NOTED.

Part: SWITCH — MALFUNCTIONED (LT A/C PACK) · airframe 85,391 hrs · 22,155 cycles

RECEIVED AN EICAS MESSAGE FOR THE LT PACK TEMP, FOLLOWED QRH, RAN PACK, FOUND NORMAL. REMOVED AND REPLACED THE PACK ALTITUDE SWITCH IAW AMM 21-51-17, PERFORMED BITE TEST IAW AMM 21-51-14, TEST PASSED, NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 85,386 hrs · 22,154 cycles

LEFT PACK TEMP EICAS MESSAGE INFLIGHT. PERFORMED A LT PACK BITE IAW FIM 21-51 FT 803, NO FAULTS NOTED.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 85,370 hrs · 22,151 cycles

EMERGENCY LIGHT AT ROW 20AC INOP. REMOVED AND REPLACED BATTERY CHARGER REF AMM 33-51-01, OPS CHECK OK.

Part: MODULE — FAULTY (AC BAY) · airframe 85,370 hrs · 22,151 cycles

LEFT PACK FAILS IN AUTO BITE TEST REFLECTS APC BITE MODULE FAULT. REPLACED AIR SUPPLY BITE BITE MODULE. OPS CHECK GOOD PER AMM 36-23-01.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 85,370 hrs · 22,151 cycles

"L PACK TEMP" EICAS MSG DISPLAYED OCCURRED AT FL 340 APPROX 2 MIN AFTER "R PACK TEMP", ACCOMPLISHED QRH. REMOVED AND REPLACED LT PACK TEMP CONTROLLER REF AMM21-51-14, OPS CHECK NORMAL. NO FAULTS NOTED.

Part: CONTROLLER — MALFUNCTIONED (AC BAY) · airframe 85,370 hrs · 22,151 cycles

"R PACK TEMP" EICAS MSG DISPLAYED OCCURRED AT FL 340. ACCOMLISHED QRH. REMOVED AND REPLACED PACK TEMP CONTROLLER UNIT IAW AMM 21-51-14, OPS CHECK GOOD. NO FAULTS NOTED.

Part: ENGINE — MALFUNCTIONED (LEFT) · airframe 85,360 hrs · 22,148 cycles

LT ENGINE CONTROL STATUS MESSAGE. TROUBLESHOT IAW FIM 73-21 805 & FAULT TREE MESSAGE CLEARED. ENGINE RESTART. NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (A/C PACKS) · airframe 85,356 hrs · 22,147 cycles

LT & RT PACK TEMP MESSAGE DURING FLT AT FL38000. PERFORMED A BITE CHECK OF THE PACK SUPPLY MODULE, NO FAULTS IAW AMM 21-62-01, OPS CHECKED PACKS IAW AMM 21-63-01 OPS CHECKED GOOD.

Part: MODULE — UNSECURE (A/C PACKS) · airframe 85,338 hrs · 22,142 cycles

LEFT & RIGHT PACK TEMP EICAS , RT & LT PACK CONTROLLER FAULTS. FOUND AIR CONTROL MODULE LOOSE IN E/E RACK, SECURED THE MODULE , OPS CHECKED IAW AMM 36-11-01, NO FAULTS NOTED, OPERATED THE PACK IAW AMM 21-63-00, OPS CHECKED GOOD.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 85,326 hrs · 22,139 cycles

CABIN ALTITUDE AUTO 2 STATUS MESSAGE. REMOVED AND REPLACED THE RT AUTO PRESSURE UNIT ASSY CONTROLLER IAW AMM 21-31-02. OPS CHECKED NORMAL.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 85,326 hrs · 22,139 cycles

LEFT PACK TEMP EICAS DURING CLIMB OUT. R & R THE PACK TEMP CONTROLLER, OPS CHECKED GOOD IAW AMM 21-51-14.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 85,299 hrs · 22,134 cycles

LEFT PACK TEMP ILLUMINATED. PERFORMED A LT PACK TEMP CONTROLLER BITE TEST IAW FIM 21-51, FT 803, NO FAULT NOTED.

Part: WARNING LIGHT — FALSE ACTIVATION (LT A/C PACK) · airframe 85,271 hrs · 22,129 cycles

LEFT PACK TEMP EICAS WITH SWITCH IN AUTO , ACCOMPLISHED QRH WITH THE SWITCH IN N. PERFORMED LT PACK BITE IAW FIM 21-51 FT 803, NO FAULTS NOTED.

Part: FIRE LOOP — WARNING MESSAGE (RT ENGINE) · airframe 85,253 hrs · 22,124 cycles

COCKPIT EICAS HAS A STATUS MESSAGE, DISPLAYED RT ENGINE FIRE LOOP 1. REMOVED AND REPLACED THE RT ENGINE AFT UPPER FIRE LOOP IAW AMM 26-11-02. OPS CHECKED OK.

Part: STRINGER — CRACKED (BS 1809) · airframe 85,253 hrs · 22,124 cycles

CRACKED STRINGER 36R, BS 1809. FABRICATED AND INSTALLED A NEW STRINGER IAW SRM 53-80-03-01-1, FIG 1 ITEM 7.

Part: FRAME — CORRODED (BS 1809) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

TAIL BS 1809, BETWEEN STRINGERS 36R AND 36L, LOWER FRAME HAS CORROSION. REMOVED AND REPLACED THE FRAME IAW SRM 53-80-08-01-1.

Part: REGULATOR VALVE — NO TEST (NR 2 ENGINE) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE PRESSURE REGULATOR VALVE CONTROLLER FAILED EO6736A005. REMOVED AND REPLACED THE VALVE IAW AMM 36-11-19, OPS CHECKED GOOD.

Part: INDICATOR — INOPERATIVE (BOTTLE DISCHARGE) · airframe 85,253 hrs · 22,124 cycles

APU DISCHARGE LIGHT AT P40 DOES NOT COME ON DURING APU FIRE BOTTLE PRESSURE SWITCH TEST. REMOVED AND REPLACED THE BOTTLE DISCHARGE INDICATOR LIGHT ASSY IAW AMM 26-15-01, OPS CHECKED GOOD.

Part: EEC — FAILED (NR 2 ENGINE) · airframe 85,253 hrs · 22,124 cycles

DURING NR 2 ENGINE START, RIGHT IGNITION NR 2 BREAKER ON PS PANEL TRIPPED AND WILL NOT RESET. REMOVED AND REPLACED THE NR 2 ENG EEC IAW AMM 73-21-15-404-068-H00. COMPLIED WITH #2 ENG. MOTOR AND GROUND RUN IAW AMM 71-00-00-735-195-H03, AND 71-00-00-00. OPS CHECKED GOOD.

Part: COLLAR — CRACKED (FASTENER) · airframe 85,253 hrs · 22,124 cycles

LEFT WING REAR SPAR BULKHEAD FITTING AT FWD OTBD SIDE OF LT WHEEL WELL HAS A CRACKED FASTENER COLLAR. ACCOMPLISHED EA 767-5350-28-A7024 I/R</P>)

Part: FEEDER CABLE — DAMAGED (NR 2 IDG) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE FEEDER CABLES AT IDG HAVE TORN PROTECTIVE COVERINGS. REMOVED THE PROTECTIVE SLEEVES AND REPLACED. OPS CHECKED GOOD IAW AMM 24-11-00-715-006.

Part: DUCT — LEAKING (A/C BAY) · airframe 82,553 hrs · 22,124 cycles

RIGHT A/C BAY DUCT HAS A LEAK AT CONNECTION. REMOVED AND REPLACED THE DUCTS IAW AMM 21-51-01-004-001, 21-51-01-404, 21-51-11-002-001, AND 21-51-11-002-016. LEAK CHECKED IAW AMM 21-51-01-404-012 AND 21-51-11-002-016.

Part: WIRE — BROKEN · airframe 85,253 hrs · 22,124 cycles

RIGHT AIR DATA COMPUTER DOES NOT PASS FUNCTIONAL TEST. FAULT CODES 8 AND 7 SHOW IN THE EXTERIOR SENSOR FAULT DISPLAY VICE A DASH. REPAIRED ONE BROKEN WIRE BEHIND E2-3 SHELF IAW SWPM 20-30-12 AND WDM 34-12-21. BITE TESTED GOOD.

Part: LAMP — INOPERATIVE (INDICATOR) · airframe 85,253 hrs · 22,124 cycles

LT & RT SQUIB LIGHTS INOPERATIVE ON PGI PANEL. REPLACED THE LAMPS, PERFORMED TEST, TEST PASSED IAW AMM 26-21-04-136-001.

Part: RIB — CORRODED (APU DOOR) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

LEFT APU DOOR 5TH RIB FROM FWD, CORRODED. REPAIRED IAW DWG 148T6557 AND IAW SRM 52-40-01.

Part: OUTFLOW VALVE — DAMAGED (CABIN PRESSURE) · airframe 85,253 hrs · 22,124 cycles

CABIN PRESSURE OUTFLOW VALVE, AC MOTOR HAS FOUR BROKEN ELECTRICAL RECEPTACLES REMOVED AND REPLACED THE OUTFLOW VALVE IAW AMM 21-31-03-402-006, OPS CHECKED GOOD.

Part: SENSOR — CRACKED (SHUTOFF VALVE) · airframe 85,253 hrs · 22,124 cycles

NR 1 ENG. PRSOV AIR TEMP SENSOR PRESSURE SWITCH PLASTIC WIRE HOUSING CRACKED AND HAS EXPOSED WIRES. REMOVED AND REPLACED THE NR 1 ENG PRSOV FAN AIR TEMP SENSOR IAW AMM 36-11-17-004-001 AND 36-11-17-404-017. LEAK CHECKED GOOD IAW AMM 36-11-17-404-017 AND BITE TESTED GOOD IAW AMM 36-23-00.

Part: BLADE — NICKED (NR 2 ENGINE FAN) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE FAN BLADE NR 3, HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI OF THE FAN BLADE IAW AMM 72-31-02-308-045-H00. NO CRACKS NOTED.

Part: BLADE — NICKED (NR 2 ENGINE FAN) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE FAN BLADE NR 19 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE FAN BLADE IAW AMM 72-31-02-308-045-H00. FPI INSP OF THE BLADE IAW AMM 70-11-06-232-010-G00. NO CRACKS NOTED.

Part: VANE — CHAFED (RT LE FLAP) · airframe 85,253 hrs · 22,124 cycles

RIGHT INBD AFT FLAP L/E HAS A CHAFE AT THE OTBD AFT FAIRING. ACCOMPLISHED A PERMANENT REPAIR IAW EA 767-5753-28-A7031, REV IR, AND EO 1927A248.

Part: BLADE — NICKED (NR 1 ENGINE) · airframe 85,253 hrs · 22,124 cycles

NR 1 ENGINE FAN BLADE NR 3 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI THE FAN BLADE IAW AMM 72-31-02-308-045-H00. NO CRACKS NOTED.

Part: TEE FITTING — CORRODED (BS 869) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

KEEL BEAM TEE SUPPORT ANGLE HAS CORROSION, BS 869. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-40-02-0G-0.

Part: TUBE — DIRTY (SMOKE DETECTOR) · airframe 85,253 hrs · 22,124 cycles

SMOKE TEST FAILED FOR TWO NOZZLES FRONT OF FWD CARGO DOOR. CLEANED THE TWO SMOKE DETECTOR TUBES. PERFORMED A TEST AND PASSED.

Part: BLOWER — FAILED · airframe 85,253 hrs · 22,124 cycles

FWD DET FAN MESSAGE ON EICAS DOES NOT CLEAR. REMOVED AND REPLACED FWD BLOWER IAW AMM 26-16-02-024-043. EICAS MESSAGE CLEARED.

Part: SKIN — CRACKED (BS 1832) · airframe 85,253 hrs · 22,124 cycles

LOWER SKIN BS 1832, STRINGERS 39-40. HAS THREE CRACKS. REMOVED AND REPLACED THE SKIN IAW DWG148T3280 AND SRM 51-40-02-0G-0.

Part: CLAMP — OUT OF POSITION (IGNITION LEAD) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE LT UPPER IGNITION LEAD CLAMP OUT OF POSITION. POSITIONED THE IGNITION LEAD CLAMP.

Part: COVER — TORN (ENGINE DRAIN) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE DRAIN LINE COVER TORN OFF 11 O'CLOCK POSITION ON THE COMPRESSOR CASE. REMOVED AND REPLACED DRAIN LINE COVER IAW AMM 20-11-00.

Part: CONNECTOR — BROKEN (OVERHEAD PANEL) · airframe 85,253 hrs · 22,124 cycles

CONNECTOR D10216 ON THE PILOTS OVERHEAD PANEL HAS BROKEN LOCK AT PIN 5. REMOVED AND REPLACED THE CONNECTOR. OPS CHECKED GOOD.

Part: START VALVE — DAMAGED (NR 2 ENGINE) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE STARTER OIL PLUG DRAIN HELI-COIL DAMAGED. REMOVED AND REPLACED THE START VALVE IAW AMM 80-11-01-434-031-H00. OPS AND LEAK CHECKED GOOD.

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 85,253 hrs · 22,124 cycles

NR 1 ENGINE FAN BLADE NR 14 HAS A SMALL NICK AT THE TIP OF THE BLADE. BLENDED THE BLADE IAW AMM 72-31-02-308-405-H00. FPI OF THE BLADE IAW AMM 70-31-06-232-010-045-H00. NO CRACKS NOTED.

Part: REGULATOR VALVE — NO TEST (NR 1 ENGINE) · airframe 85,253 hrs · 22,124 cycles

NR 1 ENGINE PRESSURE REGULATOR VALVE FAILED EO6736A005-CS. REMOVED AND REPLACED THE NR 1 ENG PRV IAW AMM 36-11-18-404-018-001, OPS AND LEAK CHECKED GOOD.

Part: TEE FITTING — CORRODED (BS 916) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

KEEL BEAM TEE SUPPORT ANGLE HAS CORROSION BS 916. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-40-02-0G-0.

Part: GIRT BAR — LOOSE (DOOR SLIDE) · airframe 85,253 hrs · 22,124 cycles

LEFT AFT ENTRY ESCAPE SLIDE DEPLOYMENT BAR AFT BRACKET HARDWARE MISSING. INSTALLED THE HARDWARE IAW AMM 20-11-00-910-807.

Part: STRUCTURE — CORRODED (BS 1832) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

TAIL BS 1832, BETWEEN STRINGERS 37L AND 37R LOWER AREA HAS CORROSION. FABRICATED AND INSTALLED TEE FITTINGS IAW DWG 148T8402 AND SRM 51-40-05-0G-0.

Part: BOLT — DAMAGED (DUCT CLAMP) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE PRECOOLER AFT INLET DUCT CLAMP BOLT, THREADS ARE DAMAGED. REMOVED AND REPLACED THE CLAMP IAW AMM 36-11-15.

Part: LENS — BROKEN (INDICATOR) · airframe 85,253 hrs · 22,124 cycles

INDICATOR FOR RT AUX PITOT LIGHT LENS CAP BROKEN. REMOVED AND REPLACED THE LENS IAW AMM 33-16-02-402-018.

Part: SUPPORT ANGLE — CORRODED (BS 785.9) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

KEEL BEAM SUPPORT ANGLE HAS CORROSION, BS 786. REPAIRED THE SUPPORT ANGLE BETWEEN STRINGERS 39L & 39R IAW EA 767-5300-28-A7021.

Part: VALVE — NOISY (RT A/C PACK) · airframe 85,253 hrs · 22,124 cycles

RIGHT PACK AFT END ISOLATION AIR SUPPLY VALVE MAKES A LOUD METALIC NOISE. REMOVED AND REPLACED THE RT PACK ISOLATION AIR SUPPLY VALVE IAW AMM 36-11-04-404-013. OPS CHECKED GOOD.

Part: BRACKET — CORRODED (BS 1809) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

GENERATOR FEEDER CABLE ATTACH BRACKET HAS CORROSION, BS 1809.5, RBL 29. REMOVED. FABRICATED AND INSTALLED A NEW BRACKET IAW DWG 287T0015, AND SRM 51-40-02-0G-0.

Part: BEARING — MISSING (ROD END) · airframe 85,253 hrs · 22,124 cycles

DURING REMOVAL OF THE NR 1 ENGINE PRSOV, FOUND STRUT PNEUMATIC DUCT ABOVE THE PRSOV, FWD SUPPORT ROD HAS MISSING ROD END BEARING. REMOVED AND REPLACED THE ROD END IAW AMM 36-11-01-404-046-001.

Part: TEE FITTING — CORRODED (BS 962) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

KEEL BEAM TEE SUPPORT ANGLE HAS CORROSION AROUND FASTENERS AT BS 962. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-40-02-0G-0.

Part: BLADE — NICKED (NR 1 ENGINE FAN) · airframe 85,253 hrs · 22,124 cycles

NR 1 ENGINE FAN BLADE NR 12 HAS A SMALL NICK AT THE TIP. BLENDED THE BLADE IAW AMM 72-31-02-308-045-H00. FPI THE FAN BLADE IAW AMM 70-11-06-232-010-600. NO CRACKS NOTED.

Part: TEE FITTING — CORRODED (BS 815) · corrosion level 2 · airframe 85,253 hrs · 22,124 cycles

KEEL BEAM TEE SUPPORT ANGLE HAS CORROSION, BS 815. REMOVED AND REPLACED THE TEE FITTING IAW SRM 51-40-02-0G-0.

Part: CLAMP — BROKEN (SENSE LINE) · airframe 85,253 hrs · 22,124 cycles

NR 2 ENGINE PNEUMATIC SENSE LINE ADEL CLAMP ABOVE OIL COOLER IS BROKEN. REMOVED AND REPLACED THE CLAMP IAW AMM 70-50-00-912-001-H00.

Part: BATTERY — DISCHARGED (CABIN) · airframe 85,370 hrs · 22,151 cycles

LEFT OVER WING EMERGENCY EXIT LIGHT INOP. R&R BATTERY ASSEMBLY IAW AMM 33-51-07. OPS CHECK GOOD.

Part: SHUTOFF VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 85,222 hrs · 22,117 cycles

PRIOR TO ENGINE START, LT PACK SWITCH OFF FOR ENGINE START, LT PACK OFF LIGHT REMAINED EXTINGUISHED AND LT PACK OFF EICAS MESSAGE. REMOVED AND REPLACED THE LT PRSOV IAW AMM 36-11-09, OPS CHECKED GOOD, PERFORMED ENG RUN IAW AMM 71-00-00, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT ENGINE BLEED) · airframe 85,220 hrs · 22,116 cycles

LEFT ENGINE BLEED EICAS MESSAGE ILLUMINATED AFTER ENGINE START, WOULD NOT GO AWAY. PERFORMED BITE PROCEDURE IAW FIM 36-30-20 FAULT TREE 804. NO CURRENT FAULTS NOTED.

Part: IGNITER — DAMAGED (APU) · airframe 85,182 hrs · 22,109 cycles

APU FAULT EICAS. REMOVED AND REPLACED THE IGNITOR PLUG AND CHECKED GOOD IAW AMM 49-41-01.

Part: CLAMP — UNSECURE (COOLING DUCT) · airframe 85,155 hrs · 22,101 cycles

FAN VIBRATION INDICATED HIGHER THAN 3.5 THROUGHTOUT CLIMB , PEAK INDICATION 4.2 AT FL 270. PERFORMED FIM 71-05 FT 852, NO DEFECTS NOTED, ENGINE RAN OK. TROUBLESHOOTING THE ENGINE VIBRATION FOUND COOLING DUCT CLAMP LOOSE AT 10 O CLOCK POSITION. TIGHTENED THE CLAMP AND RAN THE ENGINE. OPS NORMAL IAW AMM 71-00-00.

Part: ENGINE — VIBRATION (RIGHT) · airframe 85,116 hrs · 22,090 cycles

DURING CLIMB OUT, THE RIGHT ENGINE HAD A VIBRATION. THE FAN WAS 4.2. PERFORMED FIM 71-05 FT 852, SHEET 1, BLOCKS 1-3, NO DEFECTS NOTED.

Part: ECU — FAULTY (APU) · airframe 85,090 hrs · 22,085 cycles

APU AUTO SHUTDOWN. REMOVED AND REPLACED APU ECU IAW AMM 49-61-05. PERFORMED BITE TEST NO FAULT NOTED.

Part: APU — MALFUNCTIONED · airframe 85,052 hrs · 22,079 cycles

APU DID NOT START ON GROUND. PERFORMED ECU BITE TEST & NO FAULT NOTED. OPS CHECKED GOOD IAW AMM 49-11-00.

Part: APU — MALFUNCTIONED · airframe 84,972 hrs · 22,062 cycles

APU FAILED TO START AFTER LANDING, TWO ATTEMPTS, APU FAULT ON BOTH, BITE CHECKED APU ECU, NO HARD FAULTS. OPS CHECKED APU IAW 49-00-00 CHECKS GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION (BLEED LEAK) · airframe 84,955 hrs · 22,059 cycles

EICAS L BLEED DUCT LEAK. INSPECTED THE LT BLEED DUCTS IAW AMM 36-00-00, NO LEAKS OR FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT IDG) · airframe 84,961 hrs · 22,060 cycles

STATUS MESSAGE FOR RT IDG VALVE. INSPECTED THE RT IDG IAW AMM 24-11-01, AND 24-11-04, NO FAULTS NOTED. MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIPMENT BAY) · airframe 84,961 hrs · 22,060 cycles

FWD EQUIPMENT OVERHEAT EICAS LIGHT ILLUMINATED. PERFORMED QRH PROCEDURES. OAT WAS 46 C. MESSAGE EXT IAW QRH PROCEDURES, OPS CHECKED EQUIPMENT COOLING SYSTEM IAW 21-58-00/501. NO FAULTS FOUND.

Part: SHUTOFF VALVE — FAILED (HYD SYSTEM) · airframe 84,882 hrs · 22,041 cycles

DURING DEPARTURE, STATUS MESSAGE FOR HYD GEN VALVE. REMOVED AND REPLACED THE HYD MOTOR GEN SHUTOFF VALVE IAW MM 24-25-03. TESTED GOOD.

Part: WARNING LIGHT — FALSE ACTIVATION · airframe 84,848 hrs · 22,035 cycles

AFTER TAKEOFF, THE FWD EQUIPMENT OVERHEAT ILLUMINATED. ACCOMPLISHED QRH NON NORMAL PROCEDURE. EICAS MESSAGE OUT AFTER PROCEDURE COMPLETE. PERFORMED FIM 21-58 FT 815, NO DEFECTS NOTED. SYS OPS NORMAL.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,852 hrs · 22,036 cycles

APU FAULT. APU WOULD NOT START AFTER LANDING. REMOVED AND REPLACED APU ECU APU OPS CHECKED OK IAW AMM 49-61-05.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT IDG VALVE) · airframe 84,848 hrs · 22,035 cycles

STATUS MESSAGE FOR THE LT IDG VALVE. PERFORMED BUSS POWER CONTROL UNIT BIT IAW FIM 24-20 FT 802. NO FAULTS NOTED. RESET UNIT, EICAS MESSAGE CLEARED.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,822 hrs · 22,029 cycles

APU RELIABILITY COLD START FAILED ON 3 ATTEMPTS DURING FLT. PERFORMED BITE PROCEDURE ON APU ECU IAW FIM 49-11. RESET APU ECU APU START NORMAL.

Part: PRIORITY VALVE — FAILED (RT ENGINE) · airframe 74,665 hrs · 9,451 cycles

CREW REPORTED A RIGHT ENGINE PRV EICAS MESSAGE IN FLT. PERFORMED FIM 36-10, FT 847. REMOVED AND REPLACED THE RIGHT ENGINE PRV IAW AMM 36-11-18/401. LEAK CHECKED GOOD. PERFORMED AIR SUPPLY BITE MODUAL TEST IAW FIM 36-20-00/101. ALL FAULTS CLEARED. NO ADDITIONAL FAULTS NOTED. EICAS MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 84,813 hrs · 22,026 cycles

EQUIPMENT COOLING OVERHEAT EICAS MESSAGE DURING CLIMB . COMPLIED WITH QRH, MESSAGE EXTINGUISHED AFTER OVER RIDE SELECTION FOR 30 MIN , MESSAGE REMAINED . EXTINGUISHED DURING THE REMAINDER OF THE FLIGHT. PERFORMED FIM 21-58 FT 815, NO DEFECTS NOTED, SYSTEM OPS NORMAL.

Part: FILTER — DIRTY · airframe 84,783 hrs · 22,021 cycles

RIGHT ENGINE BLEED OFF EICAS MESSAGE. PERFORMED FIM 36-10 F/T 838, CLEANED PRSOV FILTERS IAW AMM 36-11-09-002 PRSOV OPS CHECKED TEST NORMAL.ON ENGINE RUN UP.

Part: FILTER — NOT REPORTED (RT IDG) · airframe 84,813 hrs · 22,026 cycles

RIGHT IDG VALVE STATUS MSG. REMOVED AND REPLACED IDG AIR SHUTOFF VALVE PNEUMATIC FILTER AS PER AMM 24-11-07 OPS TEST NORMAL ON ENG RUN UP, STATUS MSG CLEARED.

Part: SHUTOFF VALVE — MALFUNCTIONED · airframe 84,791 hrs · 22,023 cycles

SIGNIFICANT DUCT PRESSURE DIFFERENCE BETWEEN LEFT AND RIGHT. AT 91% N1 DURING CRUISE FLT. LEFT DUCT AT 37 AND RIGHT 9. PERFORMED FIM 36-10 FT 838, REMOVED AND REPLACED PRSOV IAW AMM 36-11-09/501, AND PRVC IAW AMM 36-11-18/501, BOTH OPS TEST NORMAL ON ENGINE RUN UPS.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 84,822 hrs · 22,029 cycles

AFTER LANDING, APU FAULT EICAS MESSAGE. PERFORMED QRH NON NORMAL PROCEDURE, WITH SAME RESULT. PERFORMED BITE ON APU ECU IAW FIM 49-11, TASK 958. NO FAULTS NOTED. RESET APU ECU. APU STARTED NORMALLY.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,813 hrs · 22,026 cycles

INFO ONLY APU COLD SOAK START UNSUCCESSFUL APU FAULT MSG ON THREE ATTEMPTS FL 380 SAT -45. PERFORMED BITE PROCEDURE ON APU ECU IAW FIM 49-11 FT 958 NO FAULTS NOTED, RESET APU ECU, APU START NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (EQUIP COOLING) · airframe 84,813 hrs · 22,026 cycles

EQUIPMENT COOLING OVERHEAT DURING CLIMB. COMPLIED WITH QRH & SELECTED OVER RIDE, MESSAGE WENT OUT, PERFORMED FIM 21-58 F/T 815, NO DEFECTS NOTED.

Part: APU — MALFUNCTIONED · airframe 84,791 hrs · 22,023 cycles

APU FAILED TO START AFTER LANDING. PERFORMED A BITE ON APU ECU IAW FIM 49-11 FT 958. NO FAULTS NOTED. RESET APU ECU, APU START NORMAL.

Part: ECU — MALFUNCTIONED (APU) · airframe 84,813 hrs · 22,026 cycles

APU RELIABILITY, COLD START COMPLIED WITH. UNSUCCESFUL AFTER 3 ATTEMPTS. APU FAULTS ALL 3 ATTEMPTS. PERFORMED BITE PROCEDURE ON APU ECU IAW FIM 49-11F/T 958. NO FAULTS NOTED. RESET APU ECU, STARTED NORMAL.

Part: DUCT — DAMAGED (APU BLEED AIR) · airframe 84,782 hrs · 22,020 cycles

APU AIR SURGE RUBBER BLEED DUCT HAS A HOLE. REPLACED APU SURGE BLEED RUBBER DUCT IAW AMM 49-10-00 OPS CHECKED OK, NO LEAKS.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 84,782 hrs · 22,020 cycles

L4 CABIN ENTRY EXTERIOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-51-06.

Part: DETECTOR — FAILED (NR 1) · airframe 84,782 hrs · 22,020 cycles

EICAS MESSAGE FWD DETECTOR FAN DISPLA. REMOVED AND REPLACED FORWARD DETECTOR 1 IAW AMM 26-16-02 OPS CHECK NORMAL</P>)

Part: WARNING MESSAGE — FALSE ACTIVATION (RT IDG) · airframe 84,768 hrs · 22,016 cycles

RIGHT IDG VALVE STATUS MESSAGE. PERFORMED BITE TEST ON BUSS POWER CONTROL UNIT. NO FAULTS NOTED. RIGHT IDG VALVE STATUS MESSAGE CLEARED IAW FIM 24-20 FT 802.

Part: BLADE — DAMAGED (LT ENGINE) · airframe 84,768 hrs · 22,016 cycles

ON POST FLIGHT INSPECTION. FOUND A SMALL DENT ON FAN BLADE, LEFT ENGINE. PERFORMED INSPECTION OF LEFT ENGINE FAN BLADES, FOUND DENT ON 9 BLADE IN THE B AREA TO BE WITHIN LIMITS ( 0.035 INCH IN DEPTH) PERFORMED A REPAIR IAW IAW AMM 72-31-02-226-012.

Part: WARNING LIGHT — FALSE ACTIVATION (EQUIP OVERHEAT) · airframe 84,757 hrs · 22,014 cycles

FWD EQUIPMENT OVERHEAT EICAS ON TAKEOFF RAN QRH CHECKLIST AFTER 35 MINUTES LIGHT EXTINGUISHED, GROUND TEMP 47C EQUIPMENT COOLING SYS OPS TESTED NORMAL IAW AMM 21-58-00/705-120-006.

Part: CONTROL VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 84,750 hrs · 22,011 cycles

LEFT PACK WILL NOT TURN OFF. REMOVED, CLEANED AND INSPECTED D 748 FROM THE LT PACK FLOW CONTROL VALVE. REINSTALLED OPS TESTED GOOD IAW FIM 21-51 FT 810.

Part: ECU — FAILED (APU) · airframe 84,743 hrs · 22,009 cycles

APU FAILED TO START. FOUND APU ECU FAILED. REMOVED AND REPLACED ECU IAW AMM 49-61-05-1401.

Part: CONTROL PANEL — BROKEN · airframe 84,649 hrs · 21,986 cycles

R4 FA EVAC PANEL BROKEN. REMOVED AND REPLACED EVAC CONTROL PANEL IAW AMM 25-63-01, OPS CHECKED SATISFACTORY.

Part: ACTUATOR — MALFUNCTIONED (APU DOOR) · airframe 84,619 hrs · 21,979 cycles

APU DOOR ACTUATOR CIRCUIT BREAKER FOUND OPEN. REMOVED AND REPLACED APU DOOR ACTUATOR IAW AMM 49-15-06, OPS CHECKED GOOD.

Part: CIRCUIT BREAKER — TRIPPED (APU DOOR) · airframe 84,619 hrs · 21,979 cycles

APU INOPERATIVE, FOUND APU DOOR CIRCUIT BREAKER OPEN, RESET THE CIRCUIT BREAKER IAW AMM 20-60-01. PERFORMED APU BITE TEST IAW AMM 49-61-05, NO FAULTS FOUND. OPS CHECKED GOOD IAW AMM 49-11-01.

Part: INDICATION SYS — FAULTED (OIL TEMP) · airframe 84,373 hrs · 21,936 cycles

RIGHT OIL TEMPERATURE GAUGE INOPERATIVE. PERFORMED FIM 79-34, FAULT TREE 815, PIMU BITE, TEMP SENSOR FAULTED, IAW PIMU TABLE 71-01-00/201. PERFORMED TASK 71-01-00-810 A4S-H01. NO DEFECTS NOTED. RIGHT OIL TEMPERATURE INDICATION NORMAL.

Part: NUT — SEIZED (THERMOCOUPLE) · airframe 84,366 hrs · 21,934 cycles

NR 2 ENGINE, NR 2 THERMOCOUPLE PROBE, FOUND NUT ON TERMINAL END SEIZED. REMOVED AND REPLACED THE THERMOCOUPLE PROBE IAW AMM 77-21-01.

Part: BLOWER — DEFECTIVE (SMOKE DETECTOR) · airframe 84,346 hrs · 21,932 cycles

CARGO DET AIR STA MESSAGE ON DURING FLIGHT. REMOVED AND REPLACED FWD NR 2 SMOKE DETECTOR BLOWER, OPS TEST GOOD. EICAS STAT MESSAGE CLEARED IAW AMM 26-16-02.

Part: FUEL CONTROL — FAULTED (LT ENGINE) · airframe 84,284 hrs · 21,921 cycles

LT ENG CONTROL FAULT. REPLACE HYD FUEL CONTROL UNIT PER COMPANY REQUEST. REMOVED AND REPLACED HYDRO MECHANICAL FUEL CONTROL UNIT AND LEFT ENG EEC PART 1519M89P29 SERIAL LMDD7973 IAW AMM 73-21-14 AND SUBTASK 73-21-15-714-020-H00. PERFORMED TEST AND LEAK CHECK OF HMU ALL TESTS CHECK GOOD.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,272 hrs · 21,919 cycles

LEFT ENGINE CONTROL EICAS MSG AFTER LANDING DURING TAXI IN. MESSAGE WAS NOT LATCHED FAULT REF AMM 71-00-00-726-268-H03 FFC STATIC TEST PERFORMED CHECKS/TEST NO FAULTS PRESENT.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 84,272 hrs · 21,919 cycles

LEFT ENGINE CONTROL EICAS MSG AFTER LANDING DURING TAXI IN. MESSAGE WAS NOT A LATCHED FAULT REF AMM 71-00-00-725-268-H03, EEC STATIC TEST PERFORMED. CHECKS/TEST GOOD. NO FAULT PRESENT.

Part: EEC — MALFUNCTIONED (LEFT) · airframe 84,277 hrs · 21,920 cycles

LEFT ENGINE CONTROL STATUS MESSAGE. POWERED LEFT EEC, PERFORMED BITE TEST OF LEFT PIMU, FAV SENS DISAGREE FAULT PRESET, REMOVED POWER FROM L EEC, INSPECTED SECURITY OF CONNECTORS OF EWIS TO L ECC , SUPPLIED POWER TO LEFT EEC, PERFORMED VERIFY ERASE OF FAULT, PERFORMED NEW BITE TEST OF LT PIMU NO FAULTS PRESENT , SYSTEM CHECKS TEST NORMAL POSITION IAW AMM 77-35-00-722.

Part: WINDOW — FAILED (COCKPIT) · airframe 84,170 hrs · 21,897 cycles

RT SIDE WINDOW EICAS DURING CRUISE FLT. R & R WINDOW ASSEMBLY AND RIGGED IAW 56-11-02 OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW HEAT) · airframe 84,189 hrs · 21,902 cycles

RT WINDOW HEAT EICAS, PERFORMED LEFT FWD OR RIGHT WINDOW ANTI ICING BITE PROCEDURE IAW FIM TASK 30-41-00-815 AND RIGHT FWD OR LEFT SIDE WINDOW ANTI ICING PROCEDURE 30-41-00-815. BITE TEST GOOD. NO FAULTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (WINDOW) · airframe 84,148 hrs · 21,893 cycles

DURING DESCENT AT 5000FT, RT WINDOW EICAS. PERFORMED TROUBLESHOOTING IAW FIM 30-41 TR 803, BITE TEST, SYSTEM OK, NO FAULTS PRESENT.

Part: FAN — MALFUNCTIONED · airframe 84,109 hrs · 21,885 cycles

STATUS MESSAGE FOR THE AFT EQUIPMENT EXHAUST FAN 1. REMOVED AND REPLACED THE EXHAUST FAN IAW AMM 21-58-00. OP CHECKED GOOD.

Part: IGNITER — FAILED (APU) · airframe 84,055 hrs · 21,874 cycles

APU COLD SOAK START ATTEMPT UNSUCCESSFUL TWICE. ATTEMPTED APU COLD SOAK START AFTER TWO HOURS AT FL 410. APU SHUT DOWN TWICE AFTER REACHING APPROXIMATELY 750 EGT. FAULT LIGHT ILLUMINATED. REMOVED AND REPLACED THE APU IGNITER PLUG, OPS CHECKED OK IAW AMM 49-41-02.

Part: SELECTOR SWITCH — STUCK (WX RADAR) · airframe 84,055 hrs · 21,874 cycles

WEATHER RADAR FAILED MESSAGE, FOUND THE WEATHER RADAR PANEL SELECTOR SWITCH STUCK , CLEANED AND OPS CHECKED GOOD.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT STARTER) · airframe 83,947 hrs · 21,853 cycles

RT STARTER CUTOUT ON FINAL APPROACH WITH RT ENG STARTER MESSAGE LATER ON GROUND. REMOVED, CLEANED, AND INSPECTED THE CONNECTOR PLUGS AT START VALVE. PERFORMED START VALVE TEST IAW AMM 71-0000-995-229-403. OPS TESTED NORMAL.

Part: BLADES — LACK OF LUBE · airframe 83,870 hrs · 21,837 cycles

LEFT ENGINE FAN VIBRATION INDICATES 3.8 - 4.2 WITH STEADY CLIMB POWER. IAW MAINTENANCE ENGINEERING, COMPLETED FAN BLADE LUBRICATION IAW AMM 72-31-00. REMOVED FAN BLADES AND LUBRICATED. REINSTALLED. OPERATIONAL CHECKS AND VIBRATION OK ON ENGINE RUNS IAW MM 72-31-02.

Part: BLADE — LACK OF LUBE (ENGINE FAN) · airframe 83,870 hrs · 21,837 cycles

LEFT ENGINE FAN VIBRATION INDICATES 3.8-4.2 WITH STEADY CLIMB POWER. COMPLETED FAN BLADE LUBRICATION IAW AMM 72-31-00. REMOVED FAN BLADES LUBRICATED REINSTALLED .

Part: SHUTOFF VALVE — LEAKING (APU FUEL) · airframe 83,870 hrs · 21,837 cycles

DURING POST FLIGHT, DISCOVERED A FUEL LEAK FROM THE LT MAIN WHEEL WELL. FOUND APU FUEL SHUTOFF VALVE LEAKING.

Part: SENSOR — FAILED (RT ENGINE) · airframe 83,814 hrs · 21,827 cycles

RT ENGINE OIL TEMP INDICATION BLANKS OUT. REMOVED AND REPLACED RT ENGINE OIL TEMP SENSOR IAW AMM 79-34-01. LEAK AND OPS CHECK OK.

Part: SENSOR — MALFUNCTIONED (ENGINE TEMP) · airframe 83,732 hrs · 21,815 cycles

LEFT ENGINE OIL TEMP FLUCTUATES IN FLIGHT, READ DOWN TO 32*C WHILE RT SIDE READS 80*C, THEN INDICATION WENT BLANK. T/S IAW FIM 79-34 FT 807. REMOVED AND REPLACED LEFT ENGINGE OIL TEMP SENSOR IAW AMM 79-34-01 OPS AND LEAK CK GOOD.

Part: VALVE — FAILED (LT ANTI ICE SYS) · airframe 83,699 hrs · 21,810 cycles

LEFT ENGINE ANTI-ICE VALVE IS EITHER FAILING OR STICKING . VALVE LIGHT STAYS ON UNTIL POWER IS PUSHED UP ON GROUND AND IN FLIGHT. THE LEFT ANTI-ICE VALVE WAS REPLACED IAW AMM 30-21-03. OPS & LEAK CHECKED OK.

Part: OIL SYSTEM — FALSE INDICATION (RT ENGINE) · airframe 83,446 hrs · 21,764 cycles

RIGHT ENGINE OIL FLUCTUATES BETWEEN 100-20 THEN BLANKED. REMOVED CLEANED AND INSPECTED RT ENG OIL TEMP SENSOR IAW AMM 79-34-01 OPS TEST NORMAL ON ENG RUN UP IAW AMM 71-00-00.

Part: WIRE — DAMAGED (ANTI ICE SYSTEM) · airframe 83,419 hrs · 21,760 cycles

RIGHT ENGINE ANTI-ICE EICAS MESSAGE. PERFORMED TROUBLESHOOTING IAW FIM 30-21 FT 806 , AND WDM 30-21-11-1. FOUND THREE BROKEN WIRES. PERFORMED REPAIR AND PINNING OF ALL THREE WIRES IAW SWPM 20-10-13. PERFORMED OPS CHECK OF ANTI-ICE AND RT THRUST REVERSER CHECKS GOOD IAW AMM 71-00-00 & 78-00-00.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 83,415 hrs · 21,758 cycles

NR 1 ENGINE LP COMPRESSOR BLADES LEADING EDGES HAVE NICKS. BLENDED THE COMPRESSOR BLADES IAW AMM 72-31-02-308-045-400, & 70-11-06-232-001-1400.

Part: BLADE — DAMAGED (NR 2 ENGINE) · airframe 83,415 hrs · 21,758 cycles

THE NR2 ENGINE HAS 14 FAN BLADES HAVE NICKS ON THE L/E OF BLADES . BLENDED THE FAN BLADES IAW AMM 72-31-02-308-045-H00.

Part: CIRCUIT CARD — MALFUNCTIONED (OVERHEAT LOOP) · airframe 83,415 hrs · 21,758 cycles

STATUS MESSAGE FOR RT ENG OVERHEAT LOOP 1. REMOVED AND REPLACED THE OVERHEAT DETECTOR IAW AMM 26-11-02-424-033, AND REMOVED AND REPLACED M689 FIRE DETECTOR CARD IAW AMM TASK 26-10-01-024-024. OPS CHECK GOOD.

Part: LAMP — UNSECURE (EMERGENCY LIGHTS) · airframe 83,415 hrs · 21,758 cycles

SEVERAL EXTERIOR EMERGENCY LIGHTS INOPERATIVE. CLEANED AND RESEATED THE LAMPS IAW AMM 33-51-00-715-200 & BSWPM 20-10-04. OPS CHECKED GOOD.

Part: OVERHEAT LOOP — FALSE INDICATION (RT NACELLE) · airframe 83,324 hrs · 21,738 cycles

STATUS MESSAGE RT ENGINE OVERHEAT LOOP 1. COMPLIED WITH FIRE DETECTION BITE PROCEDURE, FIM 26-11 FT 808, MESSAGE CLEARED, SYS OK.

Part: BULB — INOPERATIVE (OIL TEMP) · airframe 83,243 hrs · 21,720 cycles

NR 2 ENGINE OIL TEMPERATURE BLANKED OUT, AND FLUCTUATES INTERMITTENTLY. REMOVED AND REPLACED NR 2 ENGINE OIL TEMPERATURE BULB IAW AMM 79-34-01 NO LEAKS FOUND , OPS CHECKED NORMAL.

Part: VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 83,202 hrs · 21,712 cycles

LEFT A/C PACK NO PACK OFF LIGHT AND L PACK OFF EICAS MESSAGE. REMOVED AND REPLACED THE LEFT FLOW CONTROL AND SHUTOFF VALVE IAW AMM 21-51-01. OPS AND LEAK CHECKED NORMAL.

Part: WARNING MESSAGE — FALSE ACTIVATION (APU) · airframe 83,141 hrs · 21,697 cycles

APU FAULT EICAS MESSAGE DURING START, & AFTER LANDING. PERFORMED APU ECU BITE IAW FIM 49-11 FT 958 RESET ECU EICAS MESSAGE CLEARED APU START NORMAL.

Part: SENSOR — FAULTY (AC PACK) · airframe 83,017 hrs · 21,672 cycles

LEFT PACK TEMP EICAS. REMOVED AND REPLACED LEFT PACK OUTLET TEMP SENSOR. CLEARED MESSAGE, OPS CHECKS GOOD REF AMM 21-51-06.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,010 hrs · 21,671 cycles

LT PACK TEMP EICAS MSG. T/S IAW FIM 21-51 FT 803. NO FAULTS NOTED. OPS CK, OK FOR SVC.

Part: SHUTOFF VALVE — MALFUNCTIONED (AC BAY) · airframe 83,002 hrs · 21,669 cycles

LEFT PACK TEMP EICAS INFLIGHT(<P>PERFORMED PACK TEMP CONTROLLER BITE PROCEDURE IAW FIM 21-51 FT 803 NO FAULTS NOTED SYS OK.&NBSP;</P><P>PER FIM 21-61 FT 808 &NBSP;R&AMP;R TRIM AIR PRSOV IAW AMM &NBSP;21-61-06/401-404. SYS OPS TEST NORMAL. THIS CLEARS MDDR CONT # 70477. PLACARD REMOVED</P>)

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 83,026 hrs · 21,674 cycles

LEFT PACK TEMP EICAS INFLIGHT. PERFORMED PACK TEMP CONTROLLER BITE PROCEDURE IAW FIM 21-51- FT 803, NO FAULTS NOTED

Part: A/C PACK — FAULTY (AC BAY) · airframe 82,960 hrs · 21,661 cycles

ALL TEMP ZONES IN AUTOMATIC, WOULD NOT WARM IT'S ZONE PAST 21 DEGREES C. LT PACK INOPERATIVE IN AUTO. TRANSFERRED TO MEL 21-51-03-01, CAT C, MDDR 70477.

Part: WARNING LIGHT — FALSE ACTIVATION (LT A/C PACK) · airframe 82,942 hrs · 21,656 cycles

LEFT PACK OVERHEAT ILLUMINATED. QRH COMPLETED. LT PACK RUNS IN " N" POSITION. PERFORMED PACK TEMP CONTROLLER BITE PROCEDURE IAW FIM 21-51 FT803 NO FAULTS NOTED SYS OK.

Part: CONTROL VALVE — DEFECTIVE (AC BAY) · airframe 82,911 hrs · 21,650 cycles

OBSERVED LT PACK OVERHEAT EICAS QRH COMPLETE AND LT PACK RUN IN N-POSITION, LP 788170-3, TRANSFERRED TO MEL 21-51-03-01 CAT-C; LP 788180, M8. R & R TEMP CONTROL VALVE REF AMM 21-51-03. THIS CLEARS MDDR 70063. OPS CK OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 82,879 hrs · 21,645 cycles

LT PACK EICAS MSG TEMP. REPLACED LT PACK TEMP CONTROL VALVE IAW AMM 21-51-12, PRECAUTIONARY. PART BAD, REINSTALLED ORIGINAL PACK TEMP CONTROL VALVE , T/S IAW FIM 21-51, FAULT TREE 803, SYS CHECK OK.

Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 82,870 hrs · 21,641 cycles

LEFT PACK TEMP EICAS TS IAW FIM 21-51- FT 803 FOUND LT TEMP CONTROL VALVE FAULT. RESET SYS OPS CHECK GOOD.

Part: O-RING — LEAKING (APU) · airframe 82,782 hrs · 21,626 cycles

OIL COOLER BYPASS VALVE LEAKING, APU. REPLACED APU OIL COOLER BYPASS VALVE O-RINGS IAW AMM 49-27-10-404-006, STEP 1 A-F, ACCOMPLISHED LEAK CHECK IAW AMM 49-11-00-802-002.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 82,733 hrs · 21,615 cycles

RIGHT ENG PRV STATUS MESSAGE. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/104. NO FAULTS NOTED, EICAS MESSAGE CLEARED.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 82,733 hrs · 21,615 cycles

RIGHT ENGINE PRV STATUS MESSAGE. PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101 FIG 104. NO FAULTS NOTED, EICAS MESSAGE CLEARED.

Part: CONTROL VALVE — INOPERATIVE (AC PACK) · airframe 82,733 hrs · 21,615 cycles

RIGHT A/C PACK FLOW CONTROL VALVE INOPERATIVE. R & R RT FLOW CONTROL VALVE IAW AMM 21-51-01, OPS CK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (RT ENGINE) · airframe 54,288 hrs · 37,751 cycles

STATUS MESSAGE FOR RT ENGINE PRV. IAW FIM 36-10-FT 847 PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101 FIG 104. NO FAULTS NOTED. EICAS MSG CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,670 hrs · 21,602 cycles

RT ENGINE PRV EICAS ON CLIMBOUT IAW FIM 36-10, FT 847 PERFORMED AIR SUPPLY BITE PROCEDURE IAW FIM 36-20-00/101, FIG 104, NO FAULTS NOTED EICAS MSG CLEARED.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 82,658 hrs · 21,599 cycles

ZONE TEMP CONTROLLER UNABLE TO MAINTAIN TEMP FLIGHT CREW MODULATION TRIM AIR TO MAINTAIN TEMP. PERFORMED TASK 21-51-14-705-075, PACK TEMP CONTROLLER BITE FOUND LT TSMP COND VALVE FAULT, TESTED GOOD. BITE TEST ZONE TEMP CONTROLLER. AUX ZONE TEMP CONTROLLER TEST OK.

Part: COMPENSATOR — INOPERATIVE (FUEL SYSTEM) · airframe 82,643 hrs · 21,597 cycles

CENTER FUEL QTY INOPERATIVE. REPLACED COMPENSATOR ASSY FOR CENTER MAIN TANK IAW AMM 28-41-02-001-001.

Part: CONNECTOR — LOOSE (FIRE LOOP) · airframe 82,603 hrs · 21,591 cycles

FWD EICAS MESSAGE FOR RT ENGINE FIRE LOOP 1 AND 2. PERFORMED TROUBLESHOOTING IAW FIM 26-11 FT 804, FOUND HI & RES C PIN. FOUND 1 & 2 LOWER LOOP CONNECTOR LOOSE. SECURED IAW AMM 26-11-02 TEST GOOD & IAW AMM 26-11-00.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,547 hrs · 21,582 cycles

LT PACK TEMP CAUTION MESSAGE AND 451646 MT/S IAW AMM 21-51-00 RESET FAULT NO DEFECTS NOTED.

Part: CIRCUIT CARD — MALFUNCTIONED (NR 2 FIRE LOOP) · airframe 82,540 hrs · 21,581 cycles

EICAS STATUS MESSAGE FOR RT ENGINE FIRE LOOP NR 2. REPLACED NR 2 LOOP PRINTED CIRCUIT CARD FOR RT ENG IAW AMM 26-11-02.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 82,521 hrs · 21,578 cycles

FWD EQUIPMENT OVERHEAT EICAS MESSAGE RECEIVED DURING CLIMB. CHECKLIST PERFORMED, EICAS MESSAGE CLEARED IAW CHECKLIST T/S IAW FIM 21-58-F/T 912, NO DEFECTS NOTED.

Part: WARNING MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 82,512 hrs · 21,575 cycles

LT PACK TEMP EICAS MSG RECEIVED AT CRUISE. PERFORMED CHECKLIST, CLEARED EICAS MSG. PERFORMED BITE TEST IAW AMM 21-51-00-705, NO DEFECTS NOTED.

Part: UNKNOWN — MALFUNCTIONED (COCKPIT) · airframe 82,512 hrs · 21,575 cycles

EICAS LT PACK TEMP INTERMITTENT DURING CRUISE. T/S IAW FIM 21-51, FT 844 BITE PROCEDURES, SYS CHECK GOOD.

Part: FIRE DETECTOR — FAULTY (NR 2 ENGINE) · airframe 82,506 hrs · 21,574 cycles

RT ENGINE FIRE LOOP 2 EICAS MSG. TRANSFER TO MDDR 68667 IAW MEL 26-11-01-01, CAT C, DUE DATE 03-AUG 2016, PLACARD INSTALLED. REMOVED AND REPLACED NR 2 ENG UPPER AFT FIRE DETECTOR AS PER AMM 26-10-02 OPS CHECK NORMAL, MDDR CLEARED.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,471 hrs · 21,565 cycles

2 STARTS ON APU BOTH RESULTED IN APU FAULT, CLEARED, APU START NORMAL. PERFORMED APU BITE PROCEDURES IAW FIM 49-11, FT 958 FAULTS CLEARED. APU START NORMAL.

Part: COOLING FAN — FAILED (FWD EQUIPMENT) · airframe 82,450 hrs · 21,560 cycles

FWD EQUIPMENT SUPPLY FAN 1 EICAS MESSAGE. CIRCUIT BREAKER WILL NOT RESET. REMOVED AND REPLACED COOLING SUPPLY FAN IAW AMM 21-58-06. OPS CHECK GOOD.

Part: CONTROLLER — INOPERATIVE (CABIN TEMP) · airframe 82,463 hrs · 21,563 cycles

FWD AND AFT TEMP TEMP CONTROLLERS INOPERATIVE. PERFORMED ZONE TEMP CONTROLLER BITE IAW AMM 21-61, FAULT TREE 803, NO FAULTS NOTED. SYS CHECK OK.

Part: CONTROLLER — MALFUNCTIONED (LT A/C PACK) · airframe 82,464 hrs · 21,564 cycles

CREW REPORTED INTERMITTENT LT PACK TEMP EICAS MESSAGE. REMOVED AND REPLACED THE LT PACK TEMP CONTROLLER ASSY SYS BITE TEST OK IAW AMM 21-51-14/404.

Part: FIRE LOOP — FAULTY (RT ENGINE) · airframe 82,410 hrs · 21,553 cycles

RIGHT ENGINE FIRE LP 2 EICAS MESSAGE TRANSFERRED TO MDDR 68398 IAW 26-11-01-01, CAT C. REMOVED AND REPLACED UPPER AFT LOOP IAW AMM 26-11-02. OPS CK OK. MDDR 68398 CLEARED.

Part: DETECTOR — FAULTY (CARGO BAY) · airframe 82,395 hrs · 21,551 cycles

EICAS MSG FWD CARGO DET 1, TRANSFERRED TO MDDR 68348 IAW MEL 26-16-01-01-01, CAT C. REMOVED AND REPLACED FWD CARGO NR 1 DETECTOR IAW AMM 26-16-01. OPS CHECK OK.

Part: WARNING MESSAGE — FALSE ACTIVATION (LT A/C PACK) · airframe 82,395 hrs · 21,551 cycles

LEFT PACK TEMP EICAS MESSAGE. PERFORMED PACK TEMPERATURE CONTROLLER BITE TEST. BITE TESTED OK, NO MESSAGE FOUND IAW AMM 21-61-12-715.

Part: HOSE — LEAKING (PNEUMATIC SYS) · airframe 82,373 hrs · 21,548 cycles

LEAKING RUBBER HOSE IN LEFT PACK BAY DISCOVERED DURING WALKAROUND. SECURED THE LINE AND RECONNECTED IAW AMM 21-51-03, NO LEAKS NOTED.

Part: CIRCUIT CARD — FAILED (NR 2 FIRE LOOP) · airframe 82,350 hrs · 21,541 cycles

NR 2 ENGINE FIRE LOOP 2 MESSAGE EICAS. REPLACED NR 2 ENGINE LOOP 2 FIRE DETECTION PRINTED CIRCUIT CARD IAW AMM 26-10-01. CHECKED OK.

Part: CIRCUIT CARD — FAILED (LT A/C PACK) · airframe 82,350 hrs · 21,541 cycles

WHEN LEFT PACK TURNED OFF, NO PACK OFF LIGHT AND NO L PACK OFF EICAS MESSAGE. REPLACED LEFT PACK FLOW CONTROL PRINTED CIRCUIT CARD IAW AMM 21-51-09. OPS CHECKED GOOD.

Part: FLUID — LOW (RT IDG) · airframe 82,330 hrs · 21,537 cycles

RIGHT IDG VALVE STATUS TROUBLESHOOTING, FIM 24-20, FT 802. NO DEFECT NOTED ADDED ONE PINT, OIL TO IDG OK FOR SERVICES.

Part: SHUTOFF VALVE — MALFUNCTIONED (HEAT EXCHANGER) · airframe 82,350 hrs · 21,541 cycles

STATUS MESSAGE RT IDG VALVE. REPLACED IDG AIR OIL HEAT EXCHANGER AIR SHUTOFF VALVE IAW AMM 24 11-07 OPS AND LEAK CHECKED OK.

Part: CIRCUIT CARD — FAILED (LT ENGINE SPEED) · airframe 82,350 hrs · 21,541 cycles

LT ENGINE SPEED CARD EICAS MESSAGE DISPLAYED. REPLACED LT ENG N2 SPEED CARD IAW AMM 73-21-54. OPS CHECKED GOOD.

Part: SWITCH — DEFECTIVE (FUEL SYSTEM) · airframe 82,322 hrs · 21,535 cycles

DURING ENGINE START RT ENGINE VALVE LIGHT FAILED TO CYCLE LAMP TEST CONFIRMED THAT THE LIGHT WAS FUNCTIONING PROPERLY. PLACED ON DEFERRAL. REPLACED SW LIGHT IAW 33-13-00. OPS CK OK IAW 28-22-01. THIS CLEARS MEL.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 82,298 hrs · 21,531 cycles

STATUS MESSAGE, FORWARD CARGO DETECTOR 1 PERFORMED LOWER CARGO SMOKE DETECTION SYS BITE IAW FIM 26-16, FT 806. SYS CHECKS OK, EICAS MESSAGE CLEARED.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 82,298 hrs · 21,531 cycles

FLIGHT DECK TEMP EICAS, IN FLIGHT DECK TEMP, INOPERATIVE LIGHT ILLUMINATED MANUAL CONTROL, WORKS OK. PERFORMED ZONE TEMP CONTROL BITE PROCEDURE IAW FIM 21-61.

Part: STATUS MESSAGE — FALSE ACTIVATION (COCKPIT) · airframe 82,302 hrs · 21,532 cycles

FUEL QTY TOTALIZER INOPERATIVE STATUS MESSAGE. QTY BITE IAW FIM 28-41 F/T 852, NO FAULTS AT THIS TIME.

Part: CONTROL VALVE — FAULTY (ACM) · airframe 82,294 hrs · 21,531 cycles

INTERMITTENT LT PACK OFF, EICAS MESSAGE DURING DESCENT. TRANSFERRED TO MDDT 67731 IAW MEL 21-51-03-01, CAT C. REMOVED AND REPLACED LEFT ACM TEMP CONTROL VALVE AS PER AMM 21-51-12. OPS CHECK NORMAL.

Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 82,293 hrs · 21,528 cycles

LEFT PACK TEMP EICAS MSG IN CRUISE AT FL 360. PERFORMED PACK BITE CHECK IAW FIM 21-51, FT 803, NO FAULTS AT THIS TIME.

Part: SWITCH — FAULTY (AC BAY) · airframe 82,252 hrs · 2,152 cycles

LT PACK BITE MAINTENANCE MESSAGE. REPLACED ALTITUDE SWITCH IAW AMM 21-51-17, OPS CHECK NORMAL.

Part: WARNING LIGHT — ILLUMINATED (RT ENGINE) · airframe 82,220 hrs · 21,513 cycles

RIGHT ENGINE VALVE LIGHT DID NOT CYCLE DURING START.

Part: STRUCTURE — DAMAGED (NR 7 SLAT) · airframe 82,215 hrs · 21,511 cycles

NUMBER 7 LOWER INBD SLAT DAMAGED. TEMPORARY REPAIR ACCOMPLISHED IAW 767-3, SRM 57-43-01-1A-1. ALLOWABLE DAMAGE 1 NOTE P & DETAIL & PERMANENT REPAIR BEFORE 24 MONTHS OR AT THE NEXT STRUCTURES C CHECK.

Part: INDICATOR — INOPERATIVE (CABIN TEMP) · airframe 82,217 hrs · 2,151,221 cycles

FORWARD COMPARTMENT TEMP READOUT INOPERATIVE.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 82,211 hrs · 21,509 cycles

FOUR INTERNAL EMERGENCY LIGHTS NOT ILLUMINATING WHEN SYS TURNED ON. REMOVED EMERGENCY LIGHT POWER SUPPLY M739 IAW AMM 33-51-07-002-006. INSTALLED OVERHEAD EMERGECY LIGHT M739 IAW AMM 33-51-07-402-010.

Part: SKIN — CORRODED (RT WING) · airframe 82,211 hrs · 21,509 cycles

RIGHT WING, LOWER SKIN AT REAR SPAR, WBL 708 HAS EXFOLIATION. CORROSION WAS REMOVED BY BLENDING TO A 0.111 INCH MINIMUM THICKNESS FROM ORIGINAL THICKNESS OF 0.193 INCHES. REWORKED AREA WAS SHOT PENNED, ALODINED & PRIMED. STAGE 1 STATIC STRENGTH APPROVAL REQUIRED BY 25 MAR 2017.

Part: SENSOR — DELAMINATED (FUEL LEVEL) · airframe 82,211 hrs · 21,509 cycles

FUEL LEVEL SENSOR IS DELAMINATING IN RT WING SURGE TANK. R & R RT WING FUEL LEVEL SENSOR UNIT IAW MM 28-21-03-004-008 PGS 1 - 3 & MM 28-21-03-404-004 PGS 1 - 3.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,211 hrs · 21,509 cycles

LEFT OVERWING EXTERIOR EMERGENCY LIGHTS INOPERATIVE. R & R M736 BATTERY ASSEMBLY IAW AMM 33-51-07-422-012 STEPS 5A - 5D. ADJUSTED TARGET ON 5198 IAW 53-71.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,211 hrs · 21,509 cycles

PORTABLE EMERGENCY LIGHT IN FLIGHT DECK INOPERATIVE. R & R FLIGHT DECK PORTABLE EMERGENCY LIGHT IAW TASK 33-51-01-862-014.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 82,211 hrs · 21,509 cycles

LEFT A ZONE EMERGENCY LIGHTS INOPERATIVE FROM BULLNOSE AFT. R & R M735 BATTERY ASSEMBLY IAW AMM TASK 33-51-07-422-010 STEPS 5A TO 5D.

Part: SMOKE DETECTOR — NO TEST (CARGO BAY) · airframe 82,211 hrs · 21,509 cycles

AFT CARGO FIRE DETECTION FAIL TO GIVE WARNING DURING SMOKE TEST. CLEANED AFT CARGO FIRE DETECTOR TUBING IAW MM TASK 26-16-00-107-011, METHOD 1, STEP 3, F1-3F10.

Part: SKIN — DENTED (BS 535) · airframe 82,211 hrs · 21,509 cycles

FOUND DENT IN FUSELAGE AT 535 FWD OF BULK PIT DOOR. REPAIRED DENT ON FUSELAGE IAW SRM 53-00-01-2R-6 PAGES 2 - 4 FIG 201 SHEET 1 - 3.

Part: PRECOOLER — CRACKED (NR 2 ENGINE) · airframe 82,211 hrs · 21,509 cycles

NR 2 ENG PNEUMATIC AIR SUPPLY PRECOOLER CRACKED ON WELDS & LEAKS AT WELDS UNDER PRESS. R & R 2 ENG PRECOOLER IAW AMM 36-11-15-404-020-001. OPERATIONS & LEAK CHECKS GOOD.

Part: FRAME — CRACKED (BS 859) · airframe 82,211 hrs · 21,509 cycles

BS 859.5, RBL 87, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 PAGE 89-97 FIG 8 REV 2 ECRA N649GT-53-B767-002 REV.

Part: RELAY — MALFUNCTIONED (STNDY POWER) · airframe 82,211 hrs · 21,509 cycles

STANDBY POWER SYS CHECK FAILED IF EITHER TB14FC3 IS JUMPERED TO GROUND. STBY BUSS OFF LIGHT DOES NOT COME ON OR IF P6J17 CB IS RESET. R & R STBY POWER RELAY K105 IAW AMM TASK 24-33-01-004-004 PAR 2 & TASK 24-33-01-404-005 PAR 3.

Part: FRAME — CRACKED (BS 859) · airframe 82,211 hrs · 21,509 cycles

BS 859.5, LBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK IN RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 FIG 7 PAGES 80 - 88 REV 2 EO 5753A038.

Part: FRAME — CRACKED (BS 903) · airframe 82,211 hrs · 21,509 cycles

BS 903.5, RBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SB 767-53A0209 FIG 18 PAGE 181 - 189 REV 2 & ECRA N649GT-53-B767-002.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,211 hrs · 21,509 cycles

ALL EXTERIOR EMERGENCY SLIDE LIGHTS & RT OVERWING LIGHTS FAILED ENDURANCE TEST. R & R THE BATTERY ASSEMBLIES.

Part: FRAME — CRACKED (BS 903) · airframe 82,211 hrs · 21,509 cycles

BS 903.5, LBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SERVICE BULLETIN 767-53A0209 PGS 172 - 180 FIG17 REV.2.

Part: INLET — CORRODED (NR 2 ENGINE) · airframe 82,211 hrs · 21,509 cycles

NUMBER 2 ENG NOSE INLET COWLING, INTERIOR HAS A PATCH OF CORROSION INTERNALLY & INBD SIDE, ACOUSTIC PANEL, APPROX 8 O' CLOCK.. R & R NR 2 NOSE COWL IAW AMM 71-11-01-404-005-H00 REV118 22 APR 16.

Part: SKIN — DAMAGED (BS 1178-1197) · airframe 82,211 hrs · 21,509 cycles

BS 1197 + 78, BELOW STRINGER 18 HAS LIGHTNING STRIKE DAMAGE ON SKIN. REMOVED LIGHTNING STRIKE DAMAGE & INSTALLED A FLUSH SKIN REPAIR WITH INTERNAL DOUBLER IAW SRM 53-00-01-2R-6, ALODINE & PRIMED IAW SRM 51-10-2 PAGE 8.

Part: RADAR — MALFUNCTIONED (WX SYSTEM) · airframe 82,213 hrs · 21,510 cycles

WEATHER RADAR INOPERATIVE LT & RT POSITION. PERFORMED OPERATIONS TEST IAW AMM 34-43-00-715-001-001. SYS TESTS NORMAL ON MAS WO HM77-20004.

Part: FRAME — CRACKED (BS 886) · airframe 82,211 hrs · 21,509 cycles

BS 883.5, RBL 89, BELOW WL 200, INNER FRAME TRANSITION HAS CRACK AT RADIUS. ACCOMPLISHED SB 767-53A0209 PGS 108 - 117 FIG 10 REV 2. NO FURTHER ACTION REQUIRED.