N1361A

Piper PA-18 None injury — operator not yet resolved

ATA 2751

TRAILING EDGE FLAP DISAGREE DISPLAYED 5 TIMES DURING THE TAXI TO TAKEOFF AND THEN WENT AWAY. CREW ABORTED TAKEOFF (ATO) AND CONFERENCED WITH THE FOO AND MX. CAPTAIN OK TO CONTINUE FLIGHT SINCE MESSAGE WASN'T PRESENT BEFORE TAKING OFF. ACFT RETURNED TO SERVICE AND DEPARTED WITHOUT FURTHER INCIDENT.

ATA 2750

DURING TAXI OUT TO TAKE OFF T/E DISAGREE KEPT POPPING UP AND A/C RETURNED TO THE GATE AND MTX GROUNDED A/C . AFTER TROUBLR SHOOTING REMOVED AND REPLACED FSEU IAW AMM 27-51-01OPS CHECK GOOD NO FAULTS NOTED AT THIS TIME AND RETURNED A/C TO SERVICE.

ATA 2421

ON T/O, RT GEN OFF ON THRUST ADVANCE. CREW DEFERRED IAW 24-00-1-1 AND PERFORMED AN ABORTED TAKE OFF (ATO). MTC DEFERRED PER MEL 24-00-1-1 MX PROCEDURES C/W PLACARD INSTALLED. A/C DOWNGRADED TO ETOPS 120. ACFT RETURNED TO SERVICE.

ATA 2611

BATHROOM SMOKE DETECTOR WENT OFF TWICE IN FLIGHT NO EICAS OR OTHER INDICATION OF FIRE.AFTER LANDING DEFERRED LAVATORY SMOKE DETECTION SYSTEM IAW ABX MEL 26-26-3-2 MX ACTIONS C/W PLACARD INSTALLED MBCB 08-30-2026. AND RETURNED A/C TO SERVICE.

ATA 2612

MAIN CARGO FIRE MSG, MTX GROUNDED ACFT AND VERIFIED NO FIRE, PERFORMED OPS CHECK AND FOUND GOOD IAW AMM 26-14-00, ACFT REMAINS ETOPS 180. AND RETURNED ACFT TO SERVICE.

ATA 3416

ON APPROACH, GEAR NOT DOWN EICAS AND BELL AT 2500 FEET FOLLOWED BY LAND 2 NO LAND 3 ON ASA. ACCOMPLISHED LAST FLIGHT FAULTS ON MCDP AND RADIO ALTIMETER TESTS IAW B767 AMM 22-00-02 AND 34-33 FAULT TREE 810, NO DEFECTS NOTED AT THIS TIME, AC DOWNGRADED TO CATI PENDING TESTS 30/40. A/C REMAINS ETOPS 180. A/C RETURNED TO SERVICE.

ATA 3444

DURING DESCENT, GEAR NOT DOWN RED EICAS MESSAGE CAME ON AROUND 5000FT ON THE ARRIVAL WITH FLAPS SET AT 1 SEVERAL TIMES WITH THROTTLES AT IDLE. C/W 30/40 TEST NO FAULTS NOTED, MCDP FLIGHT REPORT FLAGGED L-RADIO ALTIMETER DEFERRED PER MEL 34-33-01-2A-1. MAINTENANCE PROCEDURES COMPLIED WITH PLACARD INSTALLED. MBCB 04-06-2026. DUE TO L RADIO ALT DI A/C DOWNGRADED TO CAT II, SEE ITEM 3 FOR RALM DOWNGRADE. REF LP 39420-17/2. AIRCRAFT RETURNED TO SERVICE.

ATA 8011

DURING ENGINE START, L ENG STARTER EICAS MESSAGE, UNABLE TO START NO. 1 ENGINE, NO N2. AIRCRAFT RETURNED TO BLOCKS (BTB). T/S #1 ENG STARTER IAW B767 FIM 80-11 FT 805. REMOVED AND REPLACED #1 ENG STARTER IAW B767 AMM 80-11-02. OPS CHECK #1 ENG IAW B767 AMM 71-00-00. OPS CHECK GOOD AT THIS TIME. A/C RELEASED ETOPS 180. A/C RETURNED TO SERVICE.

ATA 7510

DURING TAXI OUT, AFTER L ENG START EICAS MESSAGE L ENG ANTI-ICE VALVE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). REMOVED AND REPLACED L ENG TAI VALVE IAW AMM 30-21-03. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. A/C REMAINS ETOPS 180. AIRCRAFT RETURNED TO SERVICE.

ATA 2150

ON TAXI OUT, L PACK TEMP EICAS MESSAGE ILLUMINATED. AIRCRAFT RETURNED TO BLOCKS (BTB). MAINTENANCE DEFERRED L PACK PER MEL 21-51-1-1. MTX PROCEDURES CW. PLACARD INSTALLED. AC RELEASED NO ETOPS. A/C RETURNED TO SERVICE.

ATA 3030

DURING TAXI, F/O'S PITOT LIGHT PROBE NOT WORKING. AIRCRAFT RETURNED TO BLOCKS. (BTB). REMOVED AND REPLACED THE F/O'S PITOT PROBE IAW B767 AMM 54-11-01. OPS CHECK GOOD. PERFORMED LEAK CHECK OF SYS IAW B767 AMM 34-11-00. OPS AND LEAK CHECK GOOD. AIRCRAFT RETURNED TO SERVICE AND REMAINS NO ETOPS. A/C REMAINS RVSM COMPLIANT.

ATA 7700

ON TAKEOFF, RIGHT N1 DID NOT ADVANCE MORE THAN 60%. RH ENG NOT MAKING TAKEOFF PWR. ABORTED TAKEOFF, RETURNED TO BLOCKS (BTB). PERFORMED B767 FIM 71-01 FT 810 (R) PIMU BITE, PIMU FLAGGED EEC/PIMU MODE DISAGREE FAULT. PERFORMED CONTINUITY CHECK FROM EEC TO (R) PIMU D71990 (J6) PIN 22 TO D11788A PIN A10 AND D71986 (J4) PIN 6 TO D11788A PIN A11, CONTINUITY CHECK GOOD PER FIM DIRECTS YOU TO REPLACE (R) PIMU. SWAPPED (R) AND (L) PIMU'S IAW B767 AMM 77-35-02. FAULT FOLLOWED. VERIFIED (R) PIMU IS BAD. RELACED (R) PIMU UNIT WAS BAD FROM STOCK. RETURN A/C TO ORIGINAL CONFIG IAW B767 AMM 77-35-02. A/C REMAIN NO ETOPS. REF LP 39166-21/1 FOR (R) PIMU REPLACEMENT. REF LOG PAGE 39166-20/1. A/C RETURNED TO SERVICE.

ATA 2160

AFTER BLOCKOUT AND BOTH ENGINES RUNNING AFT CABIN TEMP FWD CABIN TEMP, FLT DECK TEMP EICAS MESSAGES DISPLAYED WITH DISCRETE LIGHTS ILLUMINATE.AC RETURNED TO GATE (BTB) AND MTX GROUNDED AC MTX EXECUTED BITE TEST OF ZONE TEMP CONTROLLER IAW FIM 21-61 FAULT TREE 803. BITE TEST PASSED INTERMITTENT FAULT. AND RETURNED AC TO SERVICE.

ATA 3420

AFTER PUSHBACK R IRS ALIGN EICAS AND DISCRETE LIGHT ILLUMINATED. PERFORMED QUICK ALIGN AND STATUS DID NOT CHANGE. AIIRCRAFT RETURNED TO GATE. MAINTENANCE GROUNDED AIRCRAFT. TRIED NEW CENTER IRU, NO HELP. WAPPED RIGHT & CENTER SYMBOL GENERATOR, NO HELP. ALL UNITS BACK TO ORIGINAL POSITIONS. REPLACED RIGHT IRS INST. SOURCE SELECT SWITCH, S12, PER B SWPM 20-84-15, REMOVED AND REPLACED RELAY K510 (ADIRU SELECT R) AND RELAY K137 ( IRS DC PWR DISCONNECT) NO FIX. REMOVED AND REPLACED IRMP IAW AMM 34-21-02 OPS CHECK GOOD. REMOVED AND REPLACED R IRU IAW B 767 AMM 34-21-01 OPS CHECK GOOD THIS CLEARED THE DI , PLACARDS REMOVED NO REACTIVATION PROCEDURES APPLY A/C DOWNGRADED CAT I. AIRCRAFT RETURNED TO SERVICE

ATA 3250

TUG DRIVER OVERTORQUED NOSE GEAR ON PUSH BACK AC RETURNED TO THE GATE AND MTX GROUNDED AC . MTX EXECUTED A PHASE 1 CONDITIONAL INSPECTION OF THE NLG STEERING SYSTEM IAW B767 AMM 05-51-29 NO DEFECTS NOTED @ THIS TIME. AND MTX RETURNED AC TO SERVICE.

ATA 5530

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN BETWEEN FSS 183.3 AND FSS 230.91.(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, PANEL SKIN BETWEEN FSS 183.3 AND AND FSS 230.91 WAS REPAIRED IAW TRE 6755078 REV 1 ISSUE DATE 18 JUL 2024, FAA FORM 8100-9 DATE 22 JUL 2024 &AMP; BAC MSG CMA TLS 24-0181. NO FURTHER DEFECTS NOTED</P>)

ATA 2841

LH WING, INNER ACCESS PANEL 521QB, RH FUEL QUANTITY INDICATION IN 888.8(<P>RH FUEL QUANTITY INDICATOR WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FUELING QUANTITY INDICATION WAS SATISFACTORY. GOOD FOR SERVICE.</P>)

ATA 2841

LH WING, INNER ACCESS PANEL 521QB, CENTER FUEL QUANTITY INDICATION, FLASHING INDICATION(<P>CENTER FUEL QUANTITY INDICATION WAS REPLACED IAW AMM 28-21-13-404-016 REV. 142 DATE 22 APR 24. OPERATIONAL TEST FOR PRESSURE FUELING SYSTEM QUANTITY INDICATION WAS SATISFACTORY. GOOD</P> / <P>FOR SERVICE.</P>)

ATA 2810

LH WING, INNER ACCESS PANEL 521QB, OUTBD REFUEL COUPLING, BEARING ROD ASSY WITH WORN(<P>LH WING INNER ACCESS PANEL 521QB OUTBD REFUEL COUPLING ROD WAS REPLACED IAW AMM 28-21-01-404-010 REV 142 22APR2024 TORQUE APPLIED 100LB-IN TORQUE N/S=0524121894EB-2025. NO FURTHER DEFECTS NOTED</P>)

ATA 5700

LH WING, INNER ACCESS PANEL 521QB, ON BOTH REFUEL COUPLINGS, CHAINS MISSING(<P>THE CAPS ASSY OF REFUEL COUPLINGS WERE REPLACED IAW AMM 28-21-01-404-010 REV:142 22/APR/2024. NO FURTHER DEFECTS NOTED</P>)

ATA 3240

NOSE LANDING GEAR WHEEL WELL, WEAR ON LEFT AND RIGHT SPIN BRAKES (PADS).(<P>NOSE LANDING GEAR WHEEL WELL, LEFT AND RIGHT SPIN BRAKES (PADS) WERE REPLACED IAW AMM 32-45-05-422-007 REV 142 DATE 22 APR 24. TORQUE APPLIED 35 LBIN S/N 0423902837 DATE 24 OCT 24. GOOD FOR SERVICE.</P>)

ATA 1100

LOWER FUSELAGE EXTERNAL SKIN, ILLEGIBLE LABELS ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2.(<P>LOWER FUSELAGE EXTERNAL SKIN, ON EMERGENCY ACCESS HANDLE OF RH COCKPIT WINDOW #2. LABELS WAS INSTALLED CORRECTLY IAW AMM 20-10-12-404-004 REV. 142 DATE 22 APR 24. NO FURTHER DEFECTS NOTED</P>)

ATA 5730

RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WITH LEAK(<P>RH WING, ACCESS PANEL 641BB, BASE OF FUEL STICK WAS REPLACED IAW AMM 28-44-01-404-033 REV 142 22-APR-24 ,</P> / <P>BONDING: 01 MILLIOHMS / SERIAL BONDING: 1534 / DATE EXP: 22-ENE-25, INSTALATION OF PANEL AND LEAK CHECK SEE TASK CARD CDCCL. NO FURTHER DEFECTS NOTED</P>)

ATA 5754

LH WING, SLAT #1, EXTERNAL SURFACE, MIDDLE SIDE WITH DELAMINATION(<P>LH WING, SLAT #1, EXTERNAL SURFACE WAS REPAIRED IAW SRM 57-43-02-2R-1 PAG 1-2 AND SRM 51-70-10-2R-4 FIG 201 SHEET PAG 8,16 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)

ATA 5530

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 185(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 185 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)

ATA 5530

VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, DELAMINATION ON PANEL SKIN AT FSS 169(<P>VERTICAL STABILIZER FWD TORQUE BOX RH SIDE, ON PANEL SKIN AT FSS 169 WAS REPAIRED IAW SRM 55-30-01-2R-1 FIG 201 SHEET 1 PAG 1-3 AND SRM 51-70-10-2R-4 FIG 201 SHEET 4 PAG 6-7 REV 49 APR 15/2024. NO FURTHER DEFECTS NOTED</P>)

ATA 5712

FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR.(<P>FUEL TANK LEFT WING, INTERNAL SURFACE, ON RIB 3 UPPER AND LOWER CHORDS WITH SEVERAL MIGRATED SHIMS FROM L6 TO FRONT SPAR. AREA ON LH WING RIB 3 AND L6 FRONT SPAR WAS CLEANED AND INSPECTED, SHIMS WERE FOUND NOT TO BE MIGRATED AND CORRECTLY INSTALLED IAW SRM 51-10-08-0G-0 PAR 4 REV 49 15APR24. ONLY REF DWG 112T5030 SH7-SH8. NO FURTHER DEFECTS NOTED</P>)

ATA 3200

WORN ON FITTING OF TRUCK POSITIONER, LEFT MAIN LANDING GEAR(<P>LH MLG SUPORT OF TRUCK POSITIONER WAS REPLACED IAW AMM 32-32-18-404-027 REV. 142 DATE 22 APR 24. TORQUE TO BOLTS WAS APPLIED 650 LB-IN AND 200 LB-IN WITH TOOL N/S 0823114442 DATE: 15-NOV-24. GOOD FOR SERVICE.</P>)

ATA 2810

RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK(<P>RH AUXILIARY CENTER TANK AT L-6 AND WBL 97 WITH FUEL LEAK. THE FUEL LEAK WAS EVALUATED, SEALANT REMOVED AND REPAIRED IAW AMM 28-11-00-308-013 REV 142 22APR24. THE TEST WAS SATISFACTORY.</P>)

ATA 2910

CHAFING IN HYDRAULICS LINES RH LANDING GEAR, IN THE MIDDLE OF THE BACK(<P>RH LANDING GEAR, IN THE MIDDLE OF THE BACK. HYDRAULICS LINES WAS REPLACED IAW AMM 20-11-00-910-801 REV. 142 DATE 22 APR 24 AND AMM 20-11-00-910-802 REV. 142 DATE 22 APR 24. TORQUE APPLIED 270 LB-IN 700 LB-IN S/N 0908000630 DATE 03 DEC 24. TORQUE APPLIED 35 LB-IN S/N 0823900285 DATE 15 NOV 24. NO LEAK FOUND.</P> / <P>GOOD FOR SERVICE.</P>)

ATA 5755

AUTO SPEEDBRAKE DEPLOY INOPERATIVE WHEN T/R PULLED(<P>SYSTEM AUTO SPEED BRAKE. ACTUATOR WAS REPLACED IAW AMM 27-62-04-422-023 REV- 142 DATE 22 APR 24. TORQUE APPLIED 80 LB-IN S/N 12995 DATE 11 JUN 25. GEAR TILT PRESSURE SWITCHES LH AND RH WERE REPLACED IAW AMM 27-62-10-024-002- REV. 142 DATE 22 APR 24. TORQUE APPLIED 270 LB-IN S/N 1218701402 DATE 11 JUN 25.-</P> / <P>NO LEAK FOUND. THE RELAY K518, ARMING SWITCH S371, RELAY K88 AND K87 WERE REPLACED IAW AMM 27-62-06-04-422-023. REV. 142 DATE 22 APR 24. OPERATIONAL TEST WAS SATISFACTORY. NO DISCREPANCY FOUND. GOOD FOR SERVICE.</P>)

ATA 2160

FWD TRIM VALVE FAIL.(<P>FWD TRIM VALVE WAS REPLACED IAW AMM 21-61-07-404-011-003 REV. 142 DATE 22 APR 24. TORQUE APPLIED 45 LB-IN S/N 0823900243 DATE 15 NOV 24. BONDING TEST WAS SATISFACTORY 2.2 MILLIOMHMS S/N DC- 005040 DATE 12 DEC 24. OPERATIONAL TEST WAS SATISFACTORY. GOOD FOR SERVICE.</P>)

ATA 2910

TORN HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR(<P>HYDRAULIC LINE TRUCK POSITIONER LEFT MAIN LANDING GEAR WAS REPLACED IAW AMM 32-32-18-404-024 REV 142 22-APR- -2024 TORQUE 170 LB IN S/N 224110689 DATE 02-FEB-2025. NO FURTHER DEFECTS NOTED</P>)

ATA 2560

EMERGENCY LIGHTS "UNARMED" LIGHT HALF BURNT OUT(<P>RELAMPED EMERGENCY LIGHTS "UNARMED" LIGHT IAW AMM 33-11-00. OPS CHECKS GOOD. NO FURTHER DEFECTS NOTED</P>)

ATA 2562

TAPE ON ELT BROKEN/TORN(<P>TRANSFERRED TO MDDR # 203295 PER MEL 25-63-10-01, CAT D.&NBSP; DUE DATE 19JUN24. PLACARDS INSTALLED.</P> / <P>PART ON HAND NOT CORRECT, TAPE REQUIRED PART OF ELT ASSY.&NBSP; MCC NOTIFIED. NEW ELT ON ORDER.&NBSP; DMI #203295 REMAINS OPEN.</P> / <P>REMOVED AND REPLACED LH ELT IAW AMM 25-63-03/401. NO DEFECTS REMAIN. THIS CLEARS MDDR 203295. PLACARDS REMOVED. MCC NOTIFIED.</P>)

ATA 3460

WHILE TAXIING ON GROUND IN MHT, A TURN SHOWED 26 KTS, WHICH I BELIEVE TO BE INCORRECT ON GROUND IN MHT. DURING CRUISE, ATC ADVISED WE WERE OFF COURSE AND LNAV SHOWED ON COURSE TO JWH, FIX WERE GIVEN A HEADING TO FLY. RECEIVED AN IRS NAV ONLY FLAG ON SCRATCH PAD ON FMC AFTER ATC ADVISED US OFF COURSE. WE WERE GIVEN A HEADING TO FSM, AND ADVISED ATC WE HAD NO NAV ABILITIES AFTER EVERYTHING DISAPPEARED WITH NO NAV INFO ON ND WITH NO FLIGHT DIRECTOR, NO AUTOPILOT, NO AUTOTHROTTLES, NO AUTOBRAKES & NO SPEEDBRAKES.(<P>R/R IFS MODE SELECTOR PANEL IAW AMM 34-21-02. OPS TEST GOOD. VERIFIED PART EFFECTIVE PER IPC 34-21-51-01. PERFORMED MCDP TEST 30 & 40, TEST 40 FAILED. TMC MULTIPLE FAULT IAW AMM 22-00-02. R/R TMC IAW AMM 22-31-01. OPS CHECK GOOD IAW AMM 22-00-02 (TEST 2). NO FAULT MSG. PER ENGINEERING REQUEST, R/R LH, CTR &AMP; RH IRU IAW AMM 34-21-01. PERFORMED 30 &AMP; 40 TEST IAW AMM 22-00-02. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. AIPC VERIFICATION 34-21-01-01. PER MMC, R/R CAPT & FO FMC IAW AMM 34-61-01. OPS CHECK GOOD. DATA CROSSLOAD SUCCESSFUL. AIPC VERIFICATION 34-61-01-03. NO FURTHER DEFECTS NOTED AT THIS TIME.

ATA 2740

UPON ROLL AT THRUST SET TO MASTER WARNING/CAUTION SIREN, EICAS MSG CONFIG / STABLIZER LOW SPEED REJECT(<P>T./S PER FIM TASK 31-51 FAULT TREE 807. R/R CONTORL "STAB TRIM POSITION SWITCH ASSY" IAW AMM 27-48-01.OPS CK GOOD NO MSG.&NBSP;</P>)

ATA 3416

CAPT ALTIMETER FAILED AND DISPLAYED OFF FLAG AT CRUISE. ACCOMPLISED QRH. NO CHANGE(<P>CAPTAIN ALTIMETER REMOVED AND REPLACED PER AMM 34-13-01/404. PERFOMRED OPS CHECK TO THE SYSTEM, ALL OPS CHECKED NORMAL. PITOT STATIC LEAK TEST PERFORMED, NO DEFECTS NOTED.</P>)

ATA 5400

#1 PYLON FAN COWL SUPPORT BEAM FITTING CRACKED.(<P>R/R #1 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO 4842022 AS PER B767 SRM 51-40-02 &AMP; DWG 311T2110. NO FURTHER DEFECTS NOTED.</P>)

ATA 5400

#2  PYLON FAN COWL SUPPORT FITTING CRACKED(<P>R/R #2 ENG PYLON FAN COWL SUPPORT STRUCTURE AFT FITTING P/N 311T2114-7 PO #4743771 AS PER BOEING DWG #311T2110 AND B767 SRM 51-40-02. NO FURTHER DEFECTS NOTED.</P>)

ATA 5400

#1 PYLON FAN COWL SUPPORT BEAM ANGLE P/N: 311U2510-113 IS CRACKED(<P>R/R CRACKED ANGLE R/N 311U2510-113. FABRICATED NEW ANGLE AND INSTALLED AS PER BOEING 767 SRM 51-40-02 AND DRAWING #311U2510 REV AL.</P>)

ATA 2560

FIRST AID KIT ON OVHD BIN HAS SAFETY SEAL BROKEN(<P>REMOVED AND REPLACED FIRST AID KIT IAW AMM 25-04-01. NO FURTHER DEFECTS NOTED.</P>)

ATA 5220

EMERGENCY EGRESS WINDOW CAPT SIDE WILL NOT OPEN. REMOVED CAPTS WINDOW EMERGENCY EGRESS PANEL AND REINSTALLED / ADJUSTED PANEL IAW B767 AMM 20-11-00. NO DEFECTS NOTED AT THIS TIME.</P>)

ATA 2200

CLIMBING THROUGH 10,000FT FLAPS UP & IN VNAV, NOTICED THE AIRPLANE SPEED BUG WAS AT 250KTS & THAT THE OVERSPEED TAPE WAS DOWN TO 250KTS. GIVEN A CLIMB TO FL230, BUT ELECTED TO STAY BELOW FL200 AND LEVELED OFF AT FL190 250KTS OF NOTE AT APPROX 14000FT, SLOWED TO 240 AND SELECTED FLAPS 1 AND THEN FLAPS UP AGAIN. OVERSPEED TAPE MOVED TO 260KTS BUT NO FURTHER. THERE IS NO QRH PROCEDURE AND NO EICAS OR STATUS MSG APPEARED. RETURNED TO AFW AT 250KTS AND LANDED WITHOUT FURTHER ISSUES. INSTALLED NEW FSEU & RH ADC. PERFORMED PITOT-STATIC SYSTEM TEST IAW AMM 34-11-00, OPERATED ATTITUDE TO 40,000FT AND AIRSPEED TO MACH 0.8. NO FAULTS OR ISSUES AT THIS TIME. PITOT-STATIC LEAKDOWN OK, PERFORMED AND WAS SUCCESSFUL.

ATA 3415

BARBER POLE WOULD NOT ADVANCE AFTER PASSING 10,000FT. INVESTIGATED AND FOUND VMO SWITCH TO BE IN THE ALT POSITION. SWITCHED VMO LIMITING SWITCH TO NORM POSITION IAW AMM 22-00-02</P>)

ATA 7200

ENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 11 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)

ATA 2810

CENTER WING, AUXILIARY FUEL TANK RBBL 97.95 AND STGR L-6 WITH FUEL LEAK(<P>FUEL LEAKS WERE REPAIRED</P>)

ATA 7200

ENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 2 HOURS(<P>MANIFOLD REPLACED</P>)

ATA 7200

ENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH WEAR AND LOOSE BETWEEN 11 HOURS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)

ATA 5312

FUSELAGE SECTION 45 STA 955 REAR SPAR BULKHEAD SIDE FITTINGS FAIL SAFE STRAP RH SIDE WITH CRACK INDICATION.(<P>FAIL SAFE STRAP WAS REPAIRED</P>)

ATA 5400

ENG #1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 9 HOURS(<P>THE CLAMP SUPPORT ROOD OF THE ACCESS 447BR PANEL WAS REPLACED</P>)

ATA 5400

RH. HYDRAULIC BAY, CLAMP TO STORE SUPPORT ROD OF THE ACCESS PANEL447BR IS BROKE.(<P>THE CLAMP OF THE SUPPORT OF ACCESS PANEL 447BR WAS REPLACED</P>)

ATA 5315

CABIN FLOOR STRUCTURE SEC 46 BETWEEN STA 1562 / 1582 - TWO LOCATIONS (LBL 88.5 AND RBL 88.5) UNION ANGLES WITH CRACK(<P>CABIN FLOOR STRUCTURE WAS REPLACED</P>)

ATA 7200

ENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 3 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)

ATA 7200

ENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 7.30 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)

ATA 2810

CENTER WING, AUXILIARY FUEL TANK, RBBL 97.95 AND STGR L-10 WITH FUEL LEAK(<P>FUEL LEAK WAS REPAIRED&NBSP;</P>)

ATA 7200

ENG#1 HPT ACTIVE CLEARANCE CONTROL MANIFOLD WITH BRACKET BROKEN BETWEEN 11 HRS(<P><SPAN>MANIFOLD REPLACED</SPAN></P>)

ATA 2150

STRONG "DIRTY SOCK" ODOR COMING FROM PACKS ON DESCENT BELOW 10,000 FT.(<P>UPON ARRIVAL AND DURING OPS OF PAX ON GROUND, DETECTED NO SMELL OR ODOR. GVI OF PAX PER AMM 21-23-00. FOUND NO DEFECTS AT THIS TIME. OK TO CONTINUE.</P>)

ATA 2560

FIXED ELT INOP(<P>TRANSFERRED TO MDDR 159654 UNDER MEL 25-63-10-02A CAT2 EXP 10 APR 22.</P> / <P>LOG PAGE 1377618: R/R FIXED ELT IAW AMM SUPPLEMENT DC 356-0220-00. OPS CHECK GOOD. NO DEFECTS NOTED. DMI NO. 159654 CLEARED.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)

ATA 3443

DURING CLIMB WXR FAIL ON EHSI. WEATHER RADAR INOP(<P><SPAN>PERFORMED FIM TASK 34-43 FAULT TREE 805. NO FAULTS FOUND.</SPAN></P>)

ATA 2421

APU GENERATOR INOP ( APU GENERATOR, EXCEPT ER OPERATIONS (NOTIFY DISPATCH) )(<P>TRANFER TO MDDR 156038 DDG 24-00-02A CAT C DUE DATE 11NOV21.DISP EH@1236.</P> / <P>03NOV21 - 1238759 - ITEM# 12&NBSP; - CVG - REMOVED AND REPLACE BPCU IAW AMM 21-41-03 AND RELAY K103 (S/N OFF CE60977 P/N - OFF- B-429-1) AND K114 (S/N OFF - CE60977 P/N OFF - B-429-1) IAW AMM 24-51-02 AND 24-41-01. APU OPS CKS GOOD. THIS CLEARS MDDR 156038.</P>)

ATA 2150

STRONG ODOR FROM BOTH PACKS, SIMILAR TO WET PAINT OR WET SOCKS. MOST NOTICEABLE WITH THRUST SETTING CHANGES.(<P>PERFORMED DVI OF PACKS FOR CONTAMINATION, NO CONTAMINANTS FOUND AT THIS TIME. PERFORMED OPERATIONAL CHECK OF PACK, COULD NOT DUPLICATE SMELL. REF AMM 21-00-00.</P>)

ATA 4900

APU INOP ( AUXILIARY POWER UNIT (APU), ER OPERATIONS NOT ALLOWED (NOTIFY DISPATCH) R60 )(<P>TRANSFERRED TO MDDR 155562 IAW MEL 49-11-01A, CAT C.</P> / <P>LP <SPAN>1429464 - </SPAN><SPAN>PERFORMED MCD TEST IAW 52-32-00 STEP 3H3, PERFORMED TEST ON APU AND GROUND POWER. TEST OK. NO FLICKERING LIGHTS. THIS REMOVES MDDR 155562.</SPAN></P>)

ATA 2100

RT PACK TEMP EICAS(<P>PLACED ON MEL 21-51-03&NBSP; MDDR 155001&NBSP; CAT - C&NBSP; &NBSP;DUE DATE&NBSP; 22 OCT 21&NBSP; MCC DW 0849Z.</P> / <P>12OCT-CVG MX: LP 1407496, ITEM M3: REMOVED AND REPLACED RH PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CK GOOD, MDDR 155001 CLEARED. MCC NOTIFIED. PLACARD REMOVED. LC @ 1417Z</P>)

ATA 3443

CAPT WX SELECT LIGHT INOP(<P>DEFERRED TO DMI # 154044, MEL 34-43-01-05, DUE 22 JAN 22, "CAT D" NO MX ACTION.</P> / <P>07OCT21 - 1361984 - ITEM# 4 - ONT - VERIFIED WXR PUSH BUTTON FUNCTIONS AS REQUIRED PER B767 AMM 34-43-00. LIGHTED "ON" PUSHBUTTON PN # 433-673-1006-6044 REQUIRED MXC NOTIFIED. MDDR# 154044 REMAINS OPEN.</P> / <P>09OCT21 - 1407478 - ITEM# 7 - CVG - REMOVED AND REPLACED CAPTAIN WX SELECT SWITCH ASSY IAW B767 SWPM 20-84-00. OPS CHECK GOOD IAW B767 AMM 34-43-00. THIS CLEARS DMI 154044. MCC NOTIFIED AND PLACARDS REMOVED.</P>)

ATA 2120

APU PNEUMATICS INOP, TRANSFER TO MDDR 153997 IAW MEL 49-11-01, CAT C. REF LOG 1361938 - ITEM 13 - 24 SEP 21 - DEACTIVATED APU BLEED SHUT OFF VALVE REF AMM 36-11-04. OPS CHK GOOD. AP 20708 C/W. RAN PACKS USING APU AIR- NO ODOR. RAN PACKS USING ENG BLEED AIR- NO ODOR. LOCKED APU BLEED SHUT OFF VALVE IN CLOSED POSITION. DMI CONTINUES. REF LOG 1361939 - ITEM; 16 - 24SEP21 - C/W AP-20708. REF LP 136198 ITEM 13 FOR OPS CHK. NO ODOR PRESENT AT THIS TIME IN FLT DECK. THIS CLEARS DMI MDDR 153997. APU PNUEMATICS REACTIVATED PER MEL 49-11-01-01. OPS CHK GOOD. MCC NOTIFIED PLACARDS REMOVED.

ATA 2120

NORMAL VERY MINOR OIL SMELL DURING DESCENT WITH APU OFF, SOURCE OF OIL SMELL IS NOT APU.(<P>CLEANED PNEUMATIC DUCTS IAW AMM 21-00-21-022-033 PER INSTRUCTION FROM MCC.</P>)

ATA 2150

AIR CONDITIONING SYSTEM STRONG SMELL OF OIL(<P>CONDUCTED CABIN CONDITIONAL INSPECTION IAW AMM 05-51-56-202-001. REDUCED OIL SMELL USING AMM 21-00-21-102-030. NO SMOKE OR ODOR DETECTED. OPS CHECK GOOD AT THIS TIME.</P>)

ATA 3443

WEATHER RADAR NOT PAINTING ECHO RETURNS.(<P>PERFORMED T/S PER B767 FIM 34-43 FAULT TREE 805 BLOCK 1-50. SYS OK. NO DEFECTS NOTED AT THIS TIME. NO FURTHER MX REQUIRED.</P>)

ATA 3160

BOTH PFD'S AND MFD'S, LOWER AND UPPER EICAS ALL BLANKED ON T/O ROLL ~ 70 KTS. REJECTED T/O(<P>TESTED SYMBOL GENERATORS. TEST PASSED. NO FAULTS NOTED IAW AMM 34-22-01-864-015. CONSULTED AMM 05-51-14. RTO INSPECTION. NO BRAKE MESSAGES. NO BRAKES ABOVE 4. NO MAINTENANCE ACTION REQUIRED REF BOEING AMM TASK 21-00-00-862</P>)

ATA 2150

LH PACK AUTO MODE INOP / ( PACK TEMPERATURE CONTROL SYSTEMS (-200/-300) , AUTO MODE )(<P>PERFORMED L PACK CONTROLLER BITE TEST NO FAULTS NOTED&NBSP; OPS CK GOOD IAW AMM 21-51-00.</P> / <P>&NBSP;</P> / <P>LH PACK AUTO MODE TRANSFERRED TO MDDR 152634 IAW DDG MEL&NBSP; 21-51-03-01.</P> / <P>&NBSP;</P> / <P>C/W AP 20590. REMOVED AND REPLACED LH PACK FLOW CONTROL SHUTOFF VALVE IAW AMM 21-51-01. OPS CHECKED GOOD. SEE LP 1391972 ITEM M6 FOR LH PACK OVER TEMP SWITCH REMOVAL AND INSTALL. THIS CLEARS MDDR 152634. MCC RON NOTIFIED. ALL PLACARDS REMOVED.</P> / <P>&NBSP;</P> / <P>&NBSP;</P>)

ATA 2150

L PACK OFF AND L PACK TEMP EICAS MSG. COMPLIED WITH QRH PROCEDURE. L PACK REMAINED IN STBY CONTROL SELECTOR(<P>PERTFORMED L PACK CONTROLLER BITE TEST. NO FAULTS NOTED OPS CHECK GOOD. REF 21-51-00</P>)

ATA 2150

L PACK OFF L PACK TEMP(<P><SPAN>R/R LH ACM TEMP CONTROLLED VALVE IAW AMM 21-51-12&NBSP;&NBSP;</SPAN></P> / <P><SPAN>REFERENCE LOGPAGE 1402271 ITEM 5 .. R/R PACK FLOW CONTROL CARD IAW AMM 21-51-09 OPS CHECK GOOD AT THIS TIME SEE LP 1402270 ITEM 2 .. S/N D00069...P/N 285T0093-11</SPAN></P>)

ATA 2150

RH PACK AUTO MODE INOP / ( PACK TEMPERATURE CONTROL SYSTEMS (-200/-300) , AUTO MODE )(<P>REFERENCE LOG 1402278 ITEM 5 ... PERFORM BIT RIGHT PACK CONTROLER FOUND RIGHT TEMP CONTROL VALVE LIGHT ILLUMINATED SUSPECT RIGHT TEMP VALVE&NBSP; FAULTY AND ALSO SUSPECT RIGHT PACK TEMP CONTROLLER FAULTY REMOVED AND INSTALLED ACM TEMP CONTROL VALVE. IAW AMM 21-51-12. OPS CHECK GOOD.&NBSP;</P>)

ATA 3697

EICAS MSG R ENG HPSOV COMPLIED WITH QRH PROCEDURE RT PACK REMAINED OFF FOR REMAINDER OF FLIGHT.(<P>PERFORMED BITE TEST. NOTED WIRE FAULT R ENG. HPSOV FOUND WIRE DISCONNECTED FROM R ENG. HPSOV. RESECURED WIRE OPS CHECKS GOOD NO FAULTS NOTED. REF AMM 36-11-00 AND WDM 20-10</P>)

ATA 2150

L PACK TEMP EICAS IN CRUISE COMPLIED WITH QRH AND OPERATED IN STBY-N MODE. TRANSFERRED TO DMI 152428 PER MEL 21-51-03-01 CAT C DUE DATE 03SEP21. PLACARDS INSTALLED. REMOVED AND REPLACED LT PACK TEMP RELAY K2021 IAW 21-51-00. OPN CK GOOD . ..REF LOGPAGE 1402269 PDX 27 AUG21,, R/R L PACK TEMP RELAY PER AMM 21-51-00 OPS CKS GOOD.

ATA 2150

INTERMITTANT R PACK TEMP SHORT FINAL(<P>REMOVED AND REPLACED R/H TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECK GOOD AND LEAK CHECK GOOD.</P>)

ATA 2150

"L PACK TEMP" EICAS MESSAGE IN CRUISE. COMPLIED WITH QRH AND USED STBY-N MODE(<P>TROUBLESHOT FIM 21-51 FT 844. OPS CHK GOOD AT THIS TIME.</P>)

ATA 3697

R ENGINE HPSOV EICAS MESSAGE AFTER TAKEOFF(<P>FOUND BROKEN TERMINAL OF R HPSOV. RETERMINATED. IAW SWPM 20-30-11. OPS CHECK OF HPSOV GOOD. IAW AMM 36-11-03. HIGH POWER RUNS ACCOMPLISHED. IAW AMM 71-00-00. NO DEFECTS NOTED.</P>)

ATA 2150

EICAS "L PACK OFF" AND "L PACK TEMP" DURING CLIMBOUT. FIRST PACK RESET PROBLEM REOCURRED. 2ND RESET NO RECCURRENCE.(<P>REMOVED AND REPLACED LH PACK TEMP SENSOR IAW AMM 21-51-08. OPS CHECK GOOD. NO FAULTS NOTED AT THIS TIME.</P>)

ATA 2150

ON FLIGHT DECK PREFLIGHT, EICAS MSG L PACK TEMP FOLLOWED BY L PACK OFF 2 MINS AFTER SELECTING LEFT PACK OFF(<P>TRANSFERRED TO MDDR 151815 PER DDG 21-51-03-01, CAT C. REACTIVATED LT PACK IAW AMM 21-00-00, REMOVED AND REPLACED LT PACK LOW LIMIT VALVE IAW AMM 21-51-11. OPS CHECKED GOOD, LEAK CHECKED GOOD. PERFORMED FIM 21-51-844, SYSTEM IS SATISFACTORY. OPS CHECKED PACK FOR 2 HOURS, NO DEFECTS NOTED.

ATA 3442

WX RADAR INTERMITTENT. TERRAIN FUNCTION OK.(<P>.WHILE PERFORMING WXR BITE PROCEDURE IAW FIM TASK 34-43 FAULT TREE 805 FOUND CB'S&NBSP; F2 WX RADAR AND F23 WX RADAR OUT. PUSH CB'S &AMP; BACK IN AND FINISHED PERFORMING WXR BITE PROCEDURE. WEATHER RADAR SYSTEM OPS CHECK GOOD IAW AMM 34-43-00 AND FIM 34-43</P>)

ATA 3442

WEATHER RADAR WILL NOT DISPLAY OR TEST ON FIRST OFFICER NAV DISPLAY(<P>PLACED ON MEL 34-43-01, CAT D, DUE ON 03 DEC 21, MDDR 151328</P> / <P>LP1370587 ITEM 4&NBSP; 05 AUG 21 TROUBLESHOT PER FIM 34-22 FT 808 - REMOVED AND REPLACED EFIS CONTROL PANEL IAW AMM 34-22-02 CHECKS GOOD NOTIFIED MCC - PLACARDS REMOVED. THIS CLEARS MDDR 151328.</P>)

ATA 2150

DURING FLT LT PACK OVERHEATED TWICE EICAS LEFT PACK OFF AND LEFT PACK TEMP RETURNED TO NORMAL TWICE FOR INFORMATION ONLY(<P>REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHK GOOD</P>)

ATA 2150

L PACK TEMP ON CLIMBOUT. L PACK OPERATES NORMALLY ON GROUND WITH APU AIR. ON ENGINES SURGING WAS NOTICED FOLLOWED BY EICAS MESSAGE. REPEAT WRITE-UP(<P>C/W WO# 84275 REV. D REMOVED AND REPLACED L/H FLOW CONTROL AND SHUT OFF VALVE IAW AMM 21-51-01. OPS CHECK GOOD.</P>)

ATA 2197

IN THE AIR BELOW 20,000 FEET AND ON THE GROUND, LEFT PACK SURGES,ACCOMPANIED BY MODERATE ODOR.(<P>TRANSFERRED TO MEL 21-51-01-01, MDDR 151157, CAT C. PERFORMED LEFT PACK TEMPERATURE CONTROLLER BITE TEST IAW AMM 21-51-14-705-035. NO FAULTS NOTED. PERFORMED VISUAL INSPECTION OF LEFT PACK BAY/COMPARTMENT AND FOUND MULTIPLE CONNECTORS LOOSE ON FLOW CONTROL/SHUTOFF VALVE,TEMPERATURE CONTROL VALVE AND LOW LIMIT VALVE. SECURED CONNECTORS AND PERFORMED AN OPS CHECK OF LT PACK IAW AMM 21-51-00. LEFT PACK OPERATED FOR OVER ONE HOUR AND NO DEFECTS WERE NOTED. ALL PARAMETERS NORMAL. MCC ADVISED,

ATA 7712

ON CLIMBOUT NAI ON, LEFT ENG N1 2% LOWER THAN R ENG. LEFT N1 SHOWED 103.1, R ENG SHOWED 105.5. AFTER NAI SWITCH OFF, BOTH ENG SHOWED SAME N1(<P>PERFORMED FIM TASK 77-12 FT 825, NO DISCREPANCIES FOUND. RUN ENGINES 1 AND 2 ABOVE IDLE AND NAI ON. IAW B767 AMM 77-00-00. UNABLE TO DUPLICATE DISCREPANCIES AT THIS TIME, OPS CHECK NORMAL, PARAMETERS WITHIN LIMITS.

ATA 3150

PACK TEMP EICAS ON (LEFT), TAXI-IN(<P>PERFORMED PACK TEMP CONTROLLER BITE TEST, TEST NORMAL IAW AMM 21-51-14</P>)

ATA 2150

FOUL SMELL LEFT PACK(<P>PERFORMED INSPECTION CHECK OF THE L/H COOLING PACK IAW AMM 21-51-00&NBSP; FOUND NO SOURCE OF FOD OR DEBRIS IN INLET OR IN PACK AREA. PERFORMED OPS CHECK OF L/H PACK IAW AMM 21-51-00.&NBSP; OPS CHECK GOOD.&NBSP; NO FOUL SMELL DETECTED.</P>)

ATA 3442

WEATHER RADAR IS NOT DEPICTING WEATHER ACCORDLY WITH EXTREME PRECIPITATION IN FRONT AND 4000' ABOVE AIRCRAFT WEATHER RADAR TILTED -3,-4,-5 DEG NOSE DOWN, IT ONLY SHOWED A DOT AND GREEN ONLY. ANY MORE DOWN WAS ALL GROUND CLUTTER AND NO WEATHER PRINTING, WEATHER VISUALLY OBSERBED.(<P>OPS TESTED BOTH L &AMP; R WEATHER RADAR SYSTEMS, MULTIPLE TIMES IAW AMM 34-43-00. OPS TEST GOOD, NO DEFECTS NOTED.</P>)

ATA 2822

"R FWD FUEL PUMP" ILLUMINATED IN FLIGHT.(<P>TRANSFERRED TO MDDR 150432 IAW DDG 28-22-01 CAT C, DUE 29JUL21. MX ACTION COMPLIED WITH. EH 1612Z</P> / <P>CVG - LOGPAGE 1470996 ITEM 5: REMOVED AND REPLACED RT FWD FUEL PUMP IAW AMM 28-22-03. OPS CK GOOD. LEAK CHECK GOOD. THIS CLEARS MDDR 150432, MCC NOTIFIED AND PLAC REMOVED.</P>)

ATA 2432

APU FAULT ON TAXI IN. APU RAN UP TO APPROXIMATLY 26%, THEN SPOOLED DOWN AGAIN.(<P>ITEM# 2 - AT APU START UP FOUND APU BATTERY VOLTAGE DROP BELOW 16V, AND AFTER APU&NBSP; @ 50% AMPERAGES WAS + 65 AMP. R&AMP;R APU BATTERY IAW AMM 24-31-04.</P> / <P>LOG # 1369479 - ITEM# 4 - R&AMP;R APU BATTERY CHARGER IAW AMM 24-31-05. OP'S CHECK GOOD. APU RUNS NORMAL AT THIS TIME.</P>)

ATA 4940

APU WOULD NOT START. APU FAULT EICAS MSG. THREE START ATTEMPTS(<P>C/W APU OPS CHECK IAW AMM 49-05-00. APU START SUCCESSFUL MULTIPLE TIMES. OPS CHECK GOOD AT THIS TIME. A\C OK FOR SERVICE.</P>)

ATA 7310

R ENG FUEL FILT STATUS MESSAGE(<P>REF DIM 73-11 FT 803 REMOVED FILTER FOUND NO CONTAMINATION REPLACED FUEL FILTER WITH NEW FILTER, PERFORMED ENG RUN REF AMM 71-00-00 NO&NBSP; MSG PRESSENT AT THIS TIME OPS CHECK GOOD&NBSP;</P>)

ATA 4900

APU FAULT. ALL 3 START ATTEMPTS. RPM NEVER EXCEEDED 32 RPM DURING START ATTEMPTS.(<P>PERFORMED APU BITE PROCEDURE PER FIM TASK 49-11 FT 987. "START ABORTED" FAULT, MSG CLEARED. PERFORMED OPS CHECK OF APU PER AMM 49-11-00. OPS GOOD.</P>)

ATA 3442

NO RADAR RETURN ON KNOWN THUNDERSTORMS UNLESS GAIN WAS SET ON MAX. EVEN THEN RADAR RETURNS WAS WEAK.(<P>PERFORMED WEATHER RADAR OPS TEST IAW AMM 34-43-00 AND FIM 34-43 FAULT TREE 805 FOR L/H AND R/H, OPS TEST IS GOOD AND NO FAULT FOUND.</P>)

ATA 4940

APU FAULT, APU WOULD NOT START, THREE ATTEMPTS MADE.(<P>FOUND APU OIL LEVEL LOW. SVCD APU IAW AMM 12-13-04. PERF FIM 49-11 FT 987. NO DEFECTS AT THIS TIME. PERF OPS IAW AMM 49-11-00. OPS CHECK GOOD. ECU BITE CHECK GOOD, NO ACTIVE FAULTS. LEAK CHECK GOOD.</P>)

ATA 3442

WX RADAR INTERMITTENT.(<P>PERFORMED WEATHER RADAR TEST IAW AMM 34-43-00 OPS TEST GOOD AT THIS TIME. CAN NOT DUPLICATE FAULT. OK FOR SERVICE.</P>)

ATA 2560

PER FCOM (LOPA) 2 EMERGENCY ESCAPE HARNESSES ARE MISSING ( FLIGHT CREW/SUPERNUMERARY ESCAPE DEVICES {ALL CARGO CONFIGURATION} ESCAPE HARNESS )(<P>TRANSFER TO MDDR 148096 PER MEL 25-61-01-02 CAT "C", DUE 16JUN21, PLACARD INSTALLED. DC 0529Z</P>)

ATA 4900

APU FAULT EICAS AFTER LANDING. ACCOMPLISHED QRH 2ND ATTEMPT SUCCESSFUL.(<P>C/W OPS CHECK OF APU IAW AMM 49-00-00. NO FAULTS AT THIS TIME. OPS CHECK GOOD.

ATA 7412

R ENG IGNITER 2 STATUS MESSAGE.(<P>REMOVED AND REPLACED LEFT AND RIGHT IGNITER ON ENGINE # 2 (P/N 10-630390-5) IAW B767 AMM 74-21-02. PROBLEM STILL EXISTS. TRANSFERRED TO DMI # 147418 IAW 74-00-01B, CAT C.</P><P>REMOVED AND REPLACED&NBSP;RH ENG #2 IGNITION LEAD(A2) IAW AMM 74-21-01 (P/N 10-631045-3A), ALSO REPLACED IGNITION EXCITER (#2) IAW AMM 74-11-01 PERFORMED ENG RUNS IAW AMM 71-00-00. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME. PLACARDS REMOVED, MCC NOTIFIED. THIS CLEARS DMI 147418.</P>)

ATA 7421

L ENG IGNITOR 2 STATUS MESSAGE AFTER START(<P>PERFORMED LEFT ENGINE IGNITION SYSTEM AUDIBLE TEST IAW AMM 74-00-00. OPS CHECK GOOD. NO DEFECTS NOTED. PERFORMED ENG RUN IAW AMM 71-00-00, ENGINE START SCCESSFUL. NO DEFECTS NOTED. NO STATUS MSG SHOWN<BR /></P>)

ATA 3040

DURING PRE-FLIGHT CHECKLIST FOUND RH FWD WINDOW HEAT KORRY SWITCH LIGHTS INOP. RELAMPED AND SWITCH WOULD NOT RETURN TO ORIGINAL CONFIQURATION(<P>REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL IAW AMM 30-41-02. OPS CHECK GOOD. NO DEFECTS NOTED.</P>)

ATA 2612

ON GROUND "MAIN CARGO FIRE" EICAS WARNING MESSAGE DISPLAYED DURING LOADING PROCESS(<P>SUPPLIED AIR TO BOTH PACKS, PERFORMED CARGO FIRE OPS TEST IAW AMM 26-11-00. OPS TEST GOOD AT THIS TIME. A/C OK FOR SERVICE<BR /></P>)

ATA 2121

AFT EQ EXH FAN 2 MSG(<P>RESET, OPS CHECKED GOOD IAW AMM 21-58-00.</P>)

ATA 2120

DIRTY SOCK/OIL SMELL UNDER APU PNEUMATICS. CUSTOMER REQUEST TO DEFER APU.(<P>TRANSFERRED TO MDDR # 145938 IAW MEL # 49-11-01-01, CAT C. DUE DATE 06MAR21. ALL PLACARDS INSTALLED. MX ACTION COMPLETED. JL 1600.&NBSP;APU PNEUMATIC DEFERRAL CLOSED + APU DEFERRAL OPEN REFERENCE DMI 145955.&NBSP;</P><P>AFW, 29APR, LP 1258628, ITEM M8: PERFORMED APU AIR SUPPLY SHUTOFF VALVE TEST &AMP; INSPECTON PER AMM SUBTASK 36-112-10-720-001, NO DEFECTS TO NOTE &AMP; REF W/O # 80304. THIS CLEARS MDDR # 145955. ACL 2232Z</P>)

ATA 2560

COCKPIT FLASH LIGHT BATTERIES DUE FOR&NBSP; SERVICE 2 EACH&NBSP; P/N P4-01-0021(<P>REMOVED AND REPLACED FLASH LIGHT BATTERIES AS NEEDED OPS CHK OK&NBSP; AS PER B767-300 AMM 25-60-00.</P>)

ATA 7830

# 1 ENG. OUTBD T/R ELECTRICAL MECHANICAL BRAKE DOES NOT STAY IN THE UNLOCK POSITION(<P>REMOVED AND REPLACED 3 1&NBSP; ENG. OUTBD THRUST REV ELECTRO MECHANICAL BRAKE IAW AMM 78-34-07.</P><P>PENDING OPS CHK . ACCOMPLISHED ELECTRO MECH. BRAKE CHECK PER MM 78-30-00-505-00</P>)

ATA 7200

ENG #2 (D) SUMP LINE HAS 1EA BROKEN CLAMP(<P>REMOVED AND REPLACED D SUMP BROKEN LINE CLAMP PER 79-21-09-400-501-H00</P>)

ATA 7200

ENG # 1 (D) SUMP LINE HAS BROKEN CLAMP .(<P>REMOVED AND REPLACED&NBSP; D SUMP BROKEN LINE CLAMP PER MM 79-21-09-400-801-H00.</P>)

ATA 3510

SERVICE CREW OXYGEN CYLINDERS TO FULL .(<P>REMOVED BOLT CREW O2 CYL. FOR SERVICING REF. MM 12-15-08</P><P>SERVICED BOLT CREW O2 BOTTLES PER&NBSP; AC 43.13-1B&NBSP; PAR 9-46-9-51</P><P>REINSTALLED CREW&NBSP; BOTTLE PER AMM 12-15-08.</P><P>NO LEAK NOTED .</P>)

ATA 2510

COCKPIT CAPTAIN SEAT R/H ARM REST LOOSE(<P>RESECURED LOOSE ARM REST BY COCKPIT CAPTAIN&NBSP; SEAT R/H SIDE PER&NBSP; B767- AMM 20-11-00-910-802</P>)

ATA 2520

COCKPIT F/O SEAT FWD AND AFT STOP OUT OF ADJUSTMENT(<P>REMOVED AND RE-INSTALLED COCKPIT F/O SEAT FOR RE ADJUSTING. OPS CHK GOOD AS PER 767 AMM 25-11-01.</P>)

ATA 2520

COCKPIT CAPTAIN SEAT FWD STOP OUT OF ADJUSTMENT(<P>REMOVED AND RE INSTALLED COCKPIT CAPTAIN SEAT AS PER 767&NBSP; AMM 25-11-01.</P><P>OPS CHK GOOD .</P>)

ATA 5414

# 1 ENG HAS WIRE BUNDLE CLAMP NOT SECURED (BOLT MISSING) @ 11 O' CLOCK POS. JUST FWD OF MAIN HYD. LINE .(<P>REMOVED AND REPLACED MISSING BOLT PER MM 20-11-00.</P>)

ATA 7200

# 1 ENG PDV ELECTRICAL CONNECTOR BACK SHELL LOOSE(<P>ASSEMBLED STRAIN RELIEF &AMP; BACKSHELL CONNECTOR # 1 ENG DPV P5 PER SWPM 20-60-09 REV 76 &AMP; W/D 78-34-11 REV 32.</P>)

ATA 7830

#1 ENG INBD T/R ELECTRICAL MECHANICAL BRAKE DOES NOT STAY IN THE UNLOCK ED POSITION. REMOVED &AMP; REPLACED #1 ENGINE INBD THRUST REV. ELECTRO MECHANICAL BRAKE IAW AMM 78-34-07.</P><P>PENDING OPS CHK . ACCOMPLISHED ELECTRO MECH BRAKE CHECK PER MM 78-30-00-705-001-H00</P>)

ATA 2560

COCKPIT CONTAINMENT BAG HAS BROKEN VACUUM SEAL P/N AS-002-1.(<P>REMOVED AND REPLACED AVSAX CONTAINMENT BAG AS PER B767-300 AMM 25-60-00</P>)

ATA 7830

#2 ENG INBD T/R PDU LOCK OUT IS MISSING HELICOIL.(<P>FOUND HELICOIL GOOD&NBSP; ATTACH BOLT IS DAMAGED ON THREAD REMOVED &AMP; REPLACED DAMAGED BOLT AT # 2 ENG. I/B&NBSP; T/R PDU LOCK OUT PER B767-300 AMM 20-11-00-910-802.</P>)

ATA 7500

"L BLD ISLN VAL" EICAS DURING PREFLIGHT.(<P>REMOVED AND REPLACED L ISO VALVE IAW AMM 36-11-04, OPS AND LEAK CHECKS GOOD AT THIS TIME.</P>)

ATA 7421

R ENGINE NO LIGHT OFF FIRST ATTEMPT WITH ENG START IN "SINGLE". SECOND START NORMAL WITH SWITCH IN "BOTH". DISCOVERED EICAS MESSAGE R ENG IGNITOR 2, CONFIRMED FAULT ON R PIMU. REMOVED R ENG NR 2 IGNITER AND INSTALLED NEW IGNITER IAW AMM 74-21-02. OPS CHECK GOOD.

ATA 7321

ITEM #1 INFO ONLY: R ENG NO LIGHT OFF FIRST ATTEMPT W/ENG START IN "SINGLE". SECOND ATTEMPT NORMAL START W/ SWITCH IN "BOTH".(<P>NOTED BY MX. PERFORMED IGNITION SYSTEM AUDIBLE TEST OF RH ENGINE IAW AMM 74-00-00. OPS CHECK GOOD AUDIBLE HEARD ON BOTH IGNITERS ON RH ENGINE.</P>)

ATA 7421

NO LIGHT OFF ON #2 ENGINE, PLACED ENGINE START SELECTOR TO BOTH. SUCCESSFUL START ON 2ND ATTEMPT.(<P>REMOVED AND REPLACED IGNITER RIGHT UPPER PLUG REF AMM 74-21-02-004-005-H00 AMM 74-21-02-404-006-H00. OPS CHECK GOOD.</P>)

ATA 8011

#1 ENG WOULD NOT START(<P>REMOVED AND REPLACED L/H ENG STARTER IAW AMM 80-11-01, OPS CHECK NORM @ THIS TIME.</P>)

ATA 3442

ON TAXI OUT BOTH WEATHER RADARS FAILED.(<P>INSTALLED DRIVE PEDESTAL UNIT PER AMM 34-43-05-024-001-002 AND 34-43-05-424-016-002 AND 34-43-05-024-007-002 AND 34-43-05-424-012-002. OPS CK OK PER 34-43-05-714-020-002.</P>)

ATA 3497

DURING INITIAL CLIMB RADAR ANT FAULT OCCURED APROX 30 MIN IN CRUISE. ANT FAULT WENT AWAY BOTH SYS L &AMP; R.(<P>PER FIM 34-43 F/T 805 NO FAULTS NOTED SYS OK. OPENED RADOME PER AMM 53-12-01 AND FOUND CONNECTOR D491 FLOODED WITH WATER. PER SWPM 20-63-00&NBSP;DISASSEMBLED CONNECTOR AND THOROUGHLY CLEAND AND DRIED. REASSEMBLED AND APPLIED F4 TAPE AS NECESSARY. PERF OPS TEST PER AMM 34-43-00 ALL OPS NORMAL AT THIS TIME.

ATA 3150

STATUS MESSAGE: CABIN ALT AUTO 1. PERFORMED FIM 21-31 F/T 809. NO DEFECTS NOTED AT THIS TIME. MSG CLEARED.

ATA 2562

FIXED ELT FAILED TEST. TRANSFER TO MDDR 142574, CAT D, EXPIRES 17JUN21 PER MEL 25-63-10-02C. PLACARDS INSTALLED.

ATA 3510

3EA SUPERNUMERARY OXYGEN MASKS INOP / ( CREW OXYGEN SYSTEM / SUPERNUMERARY OXYGEN MASKS / ASSOCIATED SEAT NOT OCCUPIED )(<P>PLACED ON MEL 141888 IAW MEL 35-11-02-03A, CAT C.</P><P>RIV MX, 06FEB. LP 1271467, ITEM M8: REMOVED AND REPLACED #1 SUPERNUMERARY SEAT O2 MASK PER AMM 35-11-51, OPS NORMAL. P/N OFF: MC10-08-114, S/N OFF: B119217. </P><P>LP 1271467, ITEM M9: REMOVED AND REPLACED #2 SUPERNUMERARY SEAT O2 MASK PER AMM 35-11-51 OPS NORMAL. P/N OFF: MC10-08-114, S/N OFF: B119215. </P><P>LP 1271468, ITEM M10: REMOVED AND REPLACED #3 SUPERNUMERARY O2 MASK PER AMM 35-11-51. OPS NORMAL.</P><P>ITEM M11: DUE TO REPLACEMENT OF ALL 3 SUPERNUMERARY O2 MASKS, THIS CLEARS DMI 141888. ALL PLACARDS REMOVED. SD 0140Z.</P>)

ATA 2150

RIGHT PACK TEMP EICAS INTERMITTENT FOR DURATION OF FLT. BITE RT PACK TEMP CONTROLLER IAW FIM 21-51 FT844, TEMP CONT VALVE V19 FAULTED. R & R TEMP CONTROL VALVE IAW 21-51-12. OPS CHECK NORMAL.

ATA 7421

RT ENGINE WOULD NOT LIGHT OFF ON SINGLE IGNITOR. NORMAL START WITH IGNITOR IN BOTH. STATUS MESSAGE R ENG IGNITOR 2. REMOVED AND REPLACED NR 2 ENGINE IGNITOR PLUG. OPERATIONS CHECK GOOD, IAW AMM 74-21-02 & 74-00-00.

ATA 3213

RIGHT MLG AFT DRAG BRACE ATTACH FITTING IS CHAFED. COMPLIED WITH BLENDING DENT/AREA, AS PER REPAIR PLAN MESSAGE NUMBER TLS-21-0055-06B(R1). REF NDT W/O TOL81602. NO DEFECTS NOTED. TREATED, PRIMED, AND PAINTED AREA, IAW B767 AMM 51-21-10-377-003. REPAIR COMPLIED WITH IAW EO 6757A219.

ATA 3422

EICAS MESSAGE "EICAS DISPLAY" AT FL370 CLIMBING TO FL390. CAPT EHSI & EADI, AS WELL AS LOWER EICAS WENT BLANK. CREW COMPLETED QRH. CALLED MCC AND RETURNED TO HNL. CONDITION REMAINED FOR REMAINDER OF FLIGHT. CIRCUIT BREAKERS ADI AND HSI POPPED. DISCOVERED BY MX POST FLIGHT. REMOVED AND REPLACED LOWER EICAS SCREEN. OPERATIONS NORMAL, PER AMM 31-41-01. P/N OFF-622-7999-003, S/N OFF-160VIY. REPLACED CAPT. EHSI INDICATOR, IAW AMM 34-22-04. P/N OFF-622-7999-003, S/N OFF-7566. REPLACED CAPT EADI, PER AMM 34-22-03. OPERATIONS CHECKS NORMAL. P/N OFF-622-7998-003, S/N OFF-1908. INSPECTED A/C PACK SYSTEM FOR ANY DISCREPANCIES-NONE FOUND. A/C REMAINS CATIII B STATUS. PER 21-51-00-216-001 INSPECTED ALL COOLING DUCT SCRFEENS. INSPECTED EHSI COOLING SCREEN, IAW AMM 34-22-00-006-028.

ATA 3422

INITIAL LEVEL OFF AT CRUISE FL410 UPPER EICAS DISPLAY INFORMATION BLURRED ALMOST UNREADABLE FOLLOWED BY SYMBOL GENERATOR FAILURE CA'S ADI. PRESSED EFI BUTTON TO ALT CORRECTING THE ADI DISPLAY INFORMATION SOON AFTER CA'S ADI FAILED IN EFI ALT MODE. DE-SELECTING ALT MODE DID NOT CORRECT THE PROBLEM. CA ADI CIRCUIT BREAKER POPPED FOLLOWED BY STRONG ODOR THAT LATER DISSIPATED DURING DECENT BACK TO HNL. NO EICAS MESSAGES WERE ASSOCIATED TO ADI OR EICAS. PERFORMED TROUBLESHOOTING OF CAPT ADI AND FOUND IT TO BE SHORTED. REMOVED AND REPLACED ADI, IAW AMM 34-22-03 AND AMM 34-22-00. OPERATIONS CHECKS GOOD AT THIS TIME. ALSO CHECKED COOLING OF ADI, IAW AMM 33-16-00 FOUND TO BE GOOD. INSTALLED LOWER EICAS DISPLAY, PER AMM 31-41-01, OPERATIONS NORMAL. P/N-OFF-622-7999-003, S/N-OFF-4689. ITEM 5: REMOVED AND REPLACED LEFT PACK TEMP CONTROLER, IAW AMM 21-51-19. OPERATIONS CHECKS ARE NORMAL. P/N-OFF-625946-9 S/N-OFF-0826-4184. ITEM 6: VALVE ASSEMBLY, IAW AMM 21-51-11. P/N-OFF-396496-1 S/N-OFF-392. REMOVED AND REPLACE LT PRIMARY HEAT EXCHANGER, PER AMM 21-51-02 P/N-OFF-194270-3 S/N-OFF-1. ITEM NR 8 REMOVED AND REPLACED LT SECONDARY HEAT EXCHANGER, IAW AMM21-51-02. P/N-OFF-194272-2 S/N-OFF-58-1184. ITEM NR 9 REMOVED AND REPLACED RT PRIMARY HEAT EXCHANGER, IAW AMM 21-51-02 P/N-OFF-194270-3 S/N-OFF-70-1729. ITEM NR 10 REMOVED AND REPLACED RT SECONDARY HEAT EXCHANGER, IAW AMM 21-15-02 P/N-OFF-194272-3 S/N-OFF-31-1966. ITEM NR 11 REMOVED AND REPLACED CAPT EADI, PER WO 6734A194 P/N-OFF-622-7998-003 S/N-OFF-7PWC. ITEM NR 12 REMOVED AND REPLACED TOP EICAS PER EO 6734A194. P/N-OFF-622-7999-003 S/N-OFF-5324. ITEM NR 13 REMOVED AND REPLACED CAPT EHSI, PER EO6734A194 P/N-OFF-622-7999-013 S/N-OFF-5398. ITEM NR 17 REMOVED AND REPLACED LOWER EICAS SCREEN, IAW EO6734A194 P/N-OFF-6227999-003 S/N-OFF-2050. ITEM NR 19 REMOVED AND REPLACED LT PACK LOW LIMIT VALVE IAW AMM21-51-11. P/N-OFF-3289696-1 S/N-OFF-2151.

ATA 2150

LEFT PACK OFF LIGHT INTERMITTENTLY ON WITH PACK OPERATING, PACK RESET SWITCHES, BOTH PACKS OPERATIVE. TRANSFERRED TO MDDR 139115, IAW MEL 21-52-01A, CAT C. REMOVED AND REPLACED FLOW CONTROL CARD ASSEMBLY, IAW AMM 21-51-09. PACK OFF LIGHT OPERATIONS CHECK GOOD. NO FURTHER DEFECTS NOTED. THIS CLEARS DMI 139115. T/S PER WDM 21-51-11.

ATA 2150

LEFT PACK INOPERABLE ITEM 2-TRANSFERRED TO MDDR NR 138933, IAW DDG 21-51-01-01, CAT C, DUE 14DEC20. COMPLIED WITH MX ACTIONS. 04DEC20 LOG 1235909 ITEM NR M3 IAH. REMOVED AND REPLACED O-RINGS TO AIR CYCLE MACHINE DUCTS, IAW AMM 21-51-03. OPERATIONS CHECK GOOD. NO FURTHER DEFECTS AT THIS TIME. THIS CLEARS MDDR NR 138933. NOTIFIED DISPATCH.

ATA 2150

LEFT PACK INOPERABLE EICAS MESSAGE. REPLACED FLEX DUCT RESTRAINT ON DUCT COUPLER, IAW AMM 21-51-00 AND 21-51-00-705. OPERATIONS CHECKS GOOD.

ATA 4950

APU PNEUMATIC FUNCTION INOPERABLE. ENTERED INTO DMI NR 138661, IAW MEL 49-11-01-01, CAT C. PERFORMED OPERATIONAL CHECK, NO FAULTS NOTED AT THIS TIME. THIS CLEARS DMI 138661.

ATA 7230

NR 2 RT ENGINE INLET GUIDE VANE AT 7 O'CLOCK BOBBLED ON LEADING EDGE. ENTERED INTO NON-MEL NR 138612.

ATA 7314

FOUND LT ENGINE FUEL PUMP SEIZED DURING BOROSCOPE. REMOVED AND REPLACED LT ENGINE FUEL PUMP, IAW AMM 73-11-01. PERFORMED ENGINE RUN, IAW 71-00-00. FOUND NO LEAKS, ENGINE PARAMETERS SATISFACTORY. NO FURTHER DEFECTS NOTED.

ATA 7314

ITEM M2-LT ENGINE HAS EVIDENCE OF BIRD STRIKE. NR 1 ENGINE ESN-702138 FOR BIRDSTRIKE, IAW B767 AMM 72-00-00-206-146. FOUND NO DAMAGE BY BIRDSTRIKE WITHIN THE LPC OR HPC. 18NOV20/1348170/ITEM M8/RIV-DURING BOROSCOPE OF NR 1 ENGINE HEARD GRATING NOISE WHILE TURNING ENGINE FROM CRANK PAD. FOUND FUEL PUMP SEIZED, IAW N2 CRANK PROCEDURE 72-00-00-982-007-H00 (GRATING HEARD), REF ITEM NR 11 LP 1348171 FOR FUEL PUMP. R & R AND PART INFO-SDR COMPLETED.

ATA 2697

LT ENGINE FIRE LOOP 1 STATUS MESSAGE. FOUND SHORT TO SHIELD ON WIRES W 5324-451R-16 AND W5324-452R-16. REPLACED WIRES W5324-451R-16, W5324-452-16, W5324-453R-16, W5324-454R-66, W5324-456R-16. OPERATIONS CHECK GOOD AT THIS TIME, IAW SWPM 20-10-13, SWPM 20-30-00 AND WDM 26-11-11.

ATA 2612

LT ENGINE FIRE LOOP STATUS MESSAGE. FOUND LT ENGINE FWD FIRE LOOP NOT IN ISOLATION. REPOSITIONED IN ISOLATION, VERIFIED CLEAR OF ALL MOUNTING BRACKETS. OPERATIONS CHECK GOOD, IAW AMM 26-11-00.

ATA 2612

LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. REPEAT WRITE UP. TRANSFER TO MDDR 136905. PLACED ON MEL 26-11-01, CAT "C". EXPIRED DATE 8 NOV 20. TJ 1102. WHILE RESEARCHING FAULT HISTORY FOUND M2026 WAS STATED AS CHANGED, BUT CONFIRMED M10224 WAS CHANGED BY MISTAKE WITH A BFS CARD. REMOVED AND REPLACED LEFT ENGINE AFOLTS CARD, IAW AMM 26-10-01. OPERATIONS CHECKS GOOD.

ATA 2612

STATUS MESSAGE LT ENGINE FIRE LOOP 1 INTERMITTENT, BUT REGULAR. TRANSFERRED TO MDDR 136787, IAW MEL 26-11-01-01 CAT C DUE 06NOV20. ETOPS 120 RESTRICTED. CVG C/W W/O 27520, IAW AP -17971, STEPS 1-3, ALL RESISTANCE VALUES ARE WITHIN LIMITS. REMOVED & REPLACED LOWER AFT FIRE LOOP ON NR 1 ENGINE, IAW AMM 26-11-02. OPERATIONS CHECK GOOD AT THIS TIME. THIS CLEARS DMI NR 136787. MCC NOTIFIED. PLACARDS REMOVED YK AT 1547.

ATA 7830

BTB DUE TO RT ENGINE WOULD NOT SPOOL PAST 60% N1 FOR TAKEOFF. REPLACED RT ENGINE RT T/R CDU FEED BACK ASSEMBLY, IAW AMM 78-31-21. RAN ENGINE TO VERIFY TAKE OFF THRUST ON L/P 1362873/1.

ATA 2612

STATUS MESSAGE: LT ENGINE FIRE LOOP 1. REMOVED AND REPLACED LT ENGINE FIRE LOOP 1 PRINTED CIRCUIT CARD WITH NEW. OPERATIONS CHECKS GOOD, REF B767 AMM 26-10-01-024-024 AND 26-10-01-424-025.

ATA 3350

BOTH EXTERIOR FUSELAGE LIGHTS FOR EMERGENCY LIGHTING NEAR FWD ENTRY DOOR ARE INOPERABLE. REMOVED AND REPLACED BOTTOM EXTERIOR EMERGENCY LIGHT, IAW B767 AMM 33-51-16. OPERATIONS CHECK GOOD. UPPER EXTERIOR EMERGENCY LIGHT FOUND TO BE NOT EFFECTIVE FOR THIS AIRCRAFT, IAW B767 SSM 33-51-01 POSITION L388.

ATA 2612

LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE INTERMITTENT IN FLIGHT. PERFORMED MEG CHECK BETWEEN PINS 18 AND 2 ON D2382 LOOP 1 AND PINS 18 AND 20 ON D2838 AT P54 PANEL BOTH WERE GOOD AT 110 MEG OHMS. REPLACED UPPER AFT ENGINE FIRE DETECTOR (T5681), IAW B767-300 AMM 26-11-02. OPERATIONS CHECK GOOD.

ATA 2150

PACK AMBIENT NOISE IN FLIGHT DECK EXCESSIVELY LOUD. DIFFICULT TO COMMUNICATE WITH OTHER CREW MEMBER. PERFORMED OPERATIONS CHECK FOR PACK SYSTEM. OPERATIONS CHECK GOOD. NO LOUD OR EXCESSIVE NOISE AT THIS TIME, NORMAL OPERATIONS, IAW B767AMM 21-51-00.

ATA 2612

STATUS MESSAGE: LT ENGINE FIRE LOOP 1. PERFORMED FIM 26-11 FT 804 AND FOUND NO FAULTS ON LT ENGINE FIRE LOOP 1. OPERATIONS TEST GOOD. MCC NOTIFIED.

ATA 2611

LT ENGINE FIRE LP 1 STATUS MESSAGE IN FLIGHT. TRANSFERRED TO MDDR NR 135887, IAW MEL 26-11-01-01, CAT C, DUE DATE 21OCT20. PLACARDS INSTALLED. C/W FIM TASK 26-11 FAULT TREE 805. SYSTEM TEST OKAY AT BLOCK 3. THIS CLEARS DMI 135887. PLACARDS REMOVED. DISPATCH NOTIFIED.

ATA 3610

FOUND LT ISOLATION VALVE EICAS MESSAGE DURING TRANSIT CHECK. REMOVED AND REPLACED LT ISOLATION VALVE, IAW AMM 36-11-04. LEAK CHECK AND OPERATIONS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

ATA 3610

DURING TRANSIT CHECK, FOUND 30 PSI INDICATION IN LT SYSTEM WITH BOTH ISOLATION VALVES IN THE CLOSED POSITION AND APU SHUTOFF VALVE IN THE OPEN POSITION. FOUND LT ISOLATION BYPASS CHECK VALVE SPRING BROKEN. REMOVED AND REPLACED BYPASS CHECK VALVE, IAW AMM 36-11-05. LEAK CHECK AND OPERATIONS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.

ATA 2611

STATUS MESSAGE LT ENG FIRE LOOP 1. PERFORMED TEST, IAW FIM 26-11-00-101. NO FAULTS NOTED AT THIS TIME.

ATA 3610

LT ENG BLEED OFF EICAS AND ASSOCIATED DISCREET LIGHT INTERMITTENT ON ARRIVAL. TRANSFERRED TO MDDR 135160, REF DDG 36-11-01-02A, DUE 08OCT20 RS-2238. PERFORMED OPERATIONS CHECK AND TEST OF AIR SUPPY DISTRIBUTION SYSTEM, PER AMM 36-11-00-715-149. VERIFIED SYSTEM IS OK. INSPECTION OF PRSOV AND FAMV AND SENSE LINES OK. ENG RUN, PER AMM 71-00-00, FOUND NO FAULTS. AIR SUPPLY BITE MODULE SHOWS, NO FAULTS. AIR SUPPY BITE MODULE SHOWS NO FAULTS AT THIS TIME. THIS CLEARS MDDR 135160.

ATA 3442

LEFT WX SYSTEM FAIL. MESSAGE ON EHSI INTERMITTENTLY, NOT PAINTING ANYTHING WHEN MESSAGE GOES AWAY. TRANSFERRED TO MDDR 134938, IAW MEL 34-43-01, CAT D DUE 22JAN21. PLACARD INSTALLED. LUC 2136Z.

ATA 3442

LEFT WX SYSTEM FAIL MESSAGE ON EHSI INTERMITTENTLY, NOT PAINTING ANYTHING WHEN MESSAGE GOES AWAY. TRANSFERRED TO MDDR 134938, IAW MEL 34-43-01, CAT D DUE 22JAN21. PLACARD INSTALLED. LUC 2136Z. 19OCT20, 1362863, ITEM 14, CVG. REMOVED AND REPLACED RADAR DRIVE ASSEMBLY, IAW B767 AMM 34-43-05-424-016. REMOVED AND REINSTALLED WXR ANTENNA PLANAR ARRAY, IAW B767 AMM 34-43-05-424-012. OPERATIONS CHECKS GOOD AT THIS TIME. THIS CLEARS MDDR 134938. MCC NOTIFIED. PLACARDS REMOVED TIME: 2248 INT:ID2248.

ATA 3442

WXR FAIL DURING CRUISE FLIGHT ON BOTH SIDES. REMOVED AND REPLACED DRIVE UNIT WEATHER RADAR, IAW AMM 34-43-05. OPS TEST OK.

ATA 2150

LEFT PACK INOP AIR CONDITIONING PACKS -200/300, NOTIFY DISPATCH, ER RESTRICTED R-60. TRANSFERRED TO MDDR 134625, IAW MEL 21-51-01-01 CAT C DUE DATE 28 SEP 20 DGG PROCEDURE C/W ACL 0716Z. PERFORMED VISUAL INSPECTION OF PACK BAY AREA, IAW FIM 21-00 TASK 802, FOUND FUEL LEAK ON LAP JOINT OF CENTER FUEL TANK OVER PLENUM (PACK1). THIS DMI REMAINS OPEN. REPAIRED FUEL FUEL LEAK, REPAIR OF CENTER FUEL TANK LEAKS ACCOMPLISHED BY SUNAERO UNDER REPAIR ORDER 29R84 AND PERFORMED PACK NR 1 ODOR BURNOUT PROCEDURE, IAW FIM TASK 21-00 TASK 802. NO ODOR PRESENT AFTER PROCEDURE AT THIS TIME. THIS CLEARS MDDR 134625.

ATA 3442

LT AND RT WXR FAIL DURING CRUISE FLIGHT, T/S PER FIM TASK 34-43 FAULT TREE 805. FOUND WXR FAIL ANT MESSAGE ON EHSI. REMOVED AND REPLACED WEATHER RADAR ANTENNA PLANES ARRAY, IAW B767 AMM 34-43-05. OPS CHECK GOOD, NO FAULTS AT THIS TIME.

ATA 3460

SWITCH TO/FROM EXT POWER CAUSING A DRASTIC POWER TRANSFER AND ERASED FMC FLIGHT PLAN, IAW FIM 24-20 F/T 801 NO FAULTS NOTED. CYCLED EXT POWER TO APU SEVERAL TIMES. NO MSG/FAULTS NOTED. OPS NORMAL AT THIS TIME.

ATA 2612

LT ENG FIRE LOOP INOP. TRANSFERRED TO MDDR 134503, IAW MEL 26-11-01-01, CAT C. CREW REPORTED NO FURTHER FIRE LOOP MSGS DURING FLIGHT. PERFORMED BITE OF FIRE LOOP SYSTEM, IAW 26-11-00. OPS CHECK GOOD. THIS CLEARS MDDR 134503. PLACARD REMOVED.

ATA 2611

LT ENG FIRE LP 1 STATUS MESSAGE. TRANSFERRED TO MDDR 134312, IAW MEL 26-11-01-01, CAT C. ACCOMPLISHED FIM 26-11 FT 804. ACCOMPLISHED LOOP RESISTANCE CHECK AND ISOLATION CHECK, ALL WITHIN LIMITS. ACCOMPLISHED VISUAL CHECK, FOUND LOOP GROUNDED TO FRAME, REPOSITION ACCOMPLISHED. OPS CHECK IAW AMM 26-11-00, OPS CHECK GOOD. THIS CLEARS MDDR 134312, PLACARD REMOVED.

ATA 2612

LEFT ENGINE FIRE LOOP 1 STATUS MESSAGE. PERFORMED OPERATIONAL TEST FOR LEFT ENGINE FIRE LOOP. OPS CHECK OK, IAW B767 AMM 26-11-215-075-003.

ATA 2611

LT ENG FIRE LP 1 STS MSG APPEARED IN FLT. TESTED LT ENG FIRE LP 1, IAW AMM 26-11-01, FAULT COULD NOT BE DUPLICATED.

ATA 3442

WX RADAR INOP(<P>PERFORMED&NBSP; OPS TEST IAW FIM 34-43 FAULT TREE 805. OPS CHECK GOOD. NO FAULT NOTED AT THIS TIME</P>)

ATA 2822

R CENTER FUEL PUMP. VERIFIED C1 PUMP OPERATING. PULLED AND COLLARD RT CENTER PUMP JT 2145Z. "1". OPS CHECKED RT CENTER FUEL PUMP IAW 28-22-00. NO FAULTS NOTED, BOOST PUMP OPS GOOD. REMOVED AND REPLACED FUEL PRESSURE SWITCH CENTER IAW 28-42-00. OPS CHECKED GOOD. R CENTER PUMP OPS CHECK GOOD IAW AMM 28-22-00.

ATA 4940

APU FAULT. APU WOULD NOT START. THREE ATTEMPTS MADE.(<P>PERFORM BITE AND SELF TEST OF ECU PER B767 AMM 49-61-05 START ABORT MESSAGE DISPLAYED. NO FAULTS NOTED AT THIS TIME. APU START BY MX SUCCESSFUL. OPS CHECK GOOD.<BR /></P>)

ATA 3610

RIGHT BLEED DUCT LEAK ILLUMINATED AT FL 410. PERFORMED INSPECTION. FOUND AIR SUPPLY DUCT CLAMP LOOSE. SECURED AND REINSTALLED PER AMM 21-51-23. OPS NORMAL. LEAK CHECKED NORMAL.

ATA 5730

CRACK INDICATION NOTED ON LH LOWER WING SKIN STA 990.2 STR L 9.5 HOLE 1 AT APPROX 12 O'CLOCK POSITION LOOKING AFTPERFORMED DOUBLER, TRIPLER, AND FILLER REPAIR ON LH LOWER WING SKIN STA 990.2 STR L 9.5 IAW EO 6757A088 AND SB AP767-57-010 R12

ATA 5730

CRACK INDICATION NOTED ON THE RT LOWER WING SKIN WS 990.2 STR 9.5, HOLE 1 AT APPROX 12 O'CLOCK POSITION LOOKING FWD. PERFORMED A DOUBLER, TRIPLER, AND FILLER REPAIR IAW EO 6757A088, AND SB AP767-57-010 R12.

ATA 2160

FLT DECK TEMP UNCONTROLLABLE FLT DECK TEMP (28-26)C. PERFORMED BITE CHECK ON ZONE TEMP CONTROLLER IAW AMM 21-61-03 FOUND NO FAULTS. MOVED TEMP CONTROLLER TO FULL C AND FULL W IAW AMM 21-51-00, PACK PROVIDED COLD AND HOT AIR OPS CHECK GOOD.

ATA 7310

EICAS MSG R ENG FUEL FILT (W/ ASSOCIATED STATUS MSG) AT HIGH THRUST CONDITIONS. MSG EXTINGUISHED AT CRUISE THRUST. FOLLOWED FIM 73-11 T/R 863, REMOVED AND REPLACED FUEL FILTER ELEMENT PER AMM 73-11-02. PERFORMED NR 2 ENGINE RUN PER AMM 71-00-00. OPS CHECK GOOD. NO MESSAGES DISPLAYED. NO LEAKS OBSERVED. AIRCRAFT OK FOR SERVICE. USED FILTER KIT 654T0035-21.

ATA 2562

ELT INOPERATIVE. REMOVED AND REPLACED THE ELT IAW EO SB034-0220-00, REV 3. OPS CHECKED NORMAL.

ATA 4940

APU FAULT ON GROUND, BITE CHECK OF THE APU ECU IAW AMM 49-61-05 AND SELF TEST. NO FAULT FOUND. OPS CHECKED GOOD IAW AMM 49-11-00.

ATA 2150

LEFT PACK TEMP ILLUMINATED IN FLIGHT, INOPERATIVE LIGHTS STAYS ILLUMINATED. PERFORMED RESET AND & TEST OF PACK TEMP CONTROLLER IAW AMM 21-51-00. NO FAULTS FOUND.

ATA 2150

ON GROUND AND CLIMB TO FL180 PACK OUTPUT NOISE LEVEL DETRIMENTAL TO COCKPIT COMMUNICATION. OPS CHECKED PACKS IAW AMM 21-51-00. NO DEFECTS NOTED. ALL OPS NORMAL.

ATA 3422

RT FLT DIRECTOR INOP ON CLIMB OUT(<P>REMOVED AND REPLACED RT SYMBOL GENERATOR PER B767 AMM 34-22-01. OPS CHECK GOOD.</P>)

ATA 2160

RIGHT PACK TEMP EICAS MESSAGE(<P>RESET R PACK CONTROLLER. RT PACK OPERATES NORMAL IN STANDBY MODE, REF AMM 21-61-00. TRANSFERRED TO MDDR 128437 PER DDG 21-51-03-01, CAT 'C', DUE 26MAY2020.</P><P>LP 1150826: REMOVED AND REPLACED PAX TEMP CONTROL VALVE IAW AMM 21-51-12. OPS CHECK GOOD. THIS CLEARS MDDR 128437. PLACARD REMOVED.<BR /></P>)

ATA 2150

RIGHT PACK AUTO FUNCTION INOP(<P>TRANSFER TO MDDR 128348 IAW DDG 21-51-03-01, CAT C, DUE DATE 24-MAY-20.</P><P>14MAY, ONT. LOG PAGE 1137900, ITEM M3: PERF BITE OF R/H TEMP CONTROLLER IAW FIM 21-51 F/T 844, NO FAULTS NOTED. OPERATED R/H PACK ON/OFF AND WITH BOTH PACK ON SEVERAL TIMES. NO FAULTS/MSGS NOTED. OPS CHECK NORMAL AT THIS TIME. THIS CLEARS MDDR 128348. PLACARDS REMOVED. DISP: YK @ 1232Z</P>)

ATA 2120

EQUIPMENT COOLING FILTER DIRTY.(<P>REMOVED AND REPLACED EQUIPMENT COOLING FILTER IAW AMM 21-58-30. NO ODOR IN FLT DECK NOTED. OPS CHECK NORMAL AT THIS TIME.<BR /></P>)

ATA 2120

ON APPROACH STRONG DIRTY PACK SMELL(<P>PERFORMED PACK SYSTEM TEST ON BOTH REF AMM 21-51-00/501. NO SMELLS ON GROUND AFTER RUNNING BOTH PACKS SEPARATELY. OK FOR RTS.</P>)

ATA 2121

NOTICEABLE ODOR CHEMICAL OR SMELLS LIKE WET PAINT WITH THRUST CHANGES ON CLIMB OUT AND DESCENT.(<P>INSPECTED FILTER IAW 21-58-30, FOUND FILTER DIRTY WITH BITS OF BROKEN PLASTIC, FOUND FWD SUPPLY FAN BLADES BROKEN. REMOVED AND REPLACED FWD SUPPLY FAN IAW AMM 21-58-06. OPS CHECKED GOOD, REF FIM TASK #8 FOR FILTER CHANGE.</P>)

ATA 3160

NOTE - ACFT ATB TO IAH DUE TO: CAPT ADI WENT BLANK DURING CLIMB FOLLOWED BY AN ELECTRICAL BURNING ODOR. CAPT ND WAS INTERMITTENT ON CLIMB ALSO.(<P>A) REMOVED AND REPLACED EADI (CAPT) IAW AMM 31-20-00 - OPS TEST OK.</P><P>B) PERFORMED OPS TEST ON CAPT EHSI IAW AMM 31-20-00. NO FAULTS FOUND.</P><P>C) PERFORMED EQUIPMENT COOLING SYSTEM INSP &AMP; CHECK IAW AMM 21-58-00-735-016-005. NO DEF NOTED.</P><P>E) ACCOMPLISHED SERVICE LETTER 767-21-054 AND 039 - PACK WATER EXTRACTOR LINE PLUGGED. FOUND ALL LINES FREE WITH NO BLOCKAGE OR DEBRIS.</P><P>F) REMOVED AND REPLACED LH AND RH PACK OUT TEMPERATURE SENSORS (REF FTD 21-09-003). BOTH PACKS CHECK OK&NBSP; (PACK BULBS PN MS28034-1, NSN)&NBSP;</P><P>G) PERFORMED&NBSP; PACK LOW LIMIT VALVE OPS TEST IAW AMM 21-51-00. OPS CHECK NML.</P><P>H) ACCOMPLISHED FUMES IN CABIN CONDITIONAL INSPECTION PER AMM TASK 05-51-56-202-001. NO ODOR OR DEFECTS NOTED.</P>)

ATA 3442

"WXR WEAK" MESSAGE ON MFD.(<P>PERFORMED FIM BITE PROCEDURE PER 34-43 FAULT TREE 805. TEST PASSED.</P>)

ATA 2150

RIGHT PACK TEMP CONTROL VALVE EICAS INDICATION INOPERATIVE. REMOVED AND REPLACED RT TEMP CNTL VALVE, OPS CHECK OK IAW&NBSP;AMM 21-51-04.

ATA 3610

L ENG BLEED VALVE CAUTION WHEN CHANGING THRUST. REMOVED & REPLACED THE LT HPSOV IAW AMM 36-11-07. OPS CHECKED GOOD IAW 36-11-07.

ATA 3442

WX AND TERR DO NOT DISPLAY ON F/O NAV DISPLAY(<P>PERFORMED OPS CHECK OF WEATHER RADAR SYSTEM ON FO SIDE IAW AMM 34-43-00. OPS CHECK GOOD. TEST OK.</P>)

ATA 2150

PACKS EXCESSIVELY LOUD DURING ALL PHASES OF FLIGHT. WORSE DURING THRUST CHANGES. OVER 80DB RECORDED IN CRUISE.(<P>PERFORMED OPS CHECK OF A/C PACKS IAW AMM 21-00-00. COULD NOT DUPLICATE DEFECT.&NBSP;</P><P>OSHA REQUIREMENTS ALLOW FOR 90 DB OF CONTINUOUS LOUDNESS FOR 08 HRS OF EXPOSURE.</P>)

ATA 2150

LEFT PACK INOP.(<P>TRANSFER TO MDDR 126021 IAW DDG 21-51-01-01, CAT C, DUE DATE 30-MAR-20. PLACARD INSTALLED.</P><P>LP 1071108: PERFORMED OPS CHECK OF LEFT PACK IAW B767 AMM 21-51-00. OPS CHECKS OK. NO FAULTS NOTED ON BITE CHECK/OPS CHECK. THIS CLEARS DMI 126021. PLACARDS REMOVED.<BR DATA-MCE-BOGUS="1" /></P>)

ATA 3442

WEATHER SYSTEM #1 DISPLAY WXR WEAK.(<P>PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM IAW B767 AMM 34-43-00. NO DEFECTS NOTED AT THIS TIME.</P>)

ATA 3440

WXR WEAK AMBER MESSAGE ON CAPT'S AND FO'S NAV DISPLAY ON LEFT RADAR SYSTEM.(<P>PERFORMED BITE TEST IAW FIM TASK 34-43 FAULT TREE 805. TEST OK.</P>)

ATA 2121

STATUS MSG: AFT EQ EXH FAN 2.(<P>T/S PER FIM 21-26, FAULT CLEARED. OPS CHECK GOOD. PER ATLAS MCC SWAP AFT EQ EXHAUST FANS 1 &AMP; 2. LP 1071043 - M4: PER MCC SWAPPED AFT EXH FANS 1 &AMP; 2 IAW AMM 21-58-41.</P><P>P/N OFF: 645890-1, S/N 1140; P/N ON: 645890-1, S/N 1142.</P>)

ATA 4920

APU INOP(<P>ATTEMPTED 3 STARTS. WILL NOT START. FOUND ECU FLAGS 34. THIS BECAME MDDR 124952 PER 49-11-01A CAT C, DUE 3MAR20. DISPATCH SP AT 08:45Z. MCC NOTIFIED. PLACARD INSTALLED.</P><P>LP 1071042, ITEM M3: REMOVED AND REPLACED APU BATTERY ASSY IAW AMM 24-31-04. OPS CHECK GOOD (P/N OFF: 4579/01855.000, S/N 032010).</P><P>LP 1071043, ITEM M5: REMOVED AND REPLACED APU BATTERY CHARGER PER AMM 24-31-05. OPS CHECK OK, BATTERY VOLTAGE AT 28V. THIS CLEARS MDDR 124952, PLACARD REMOVED. MCC ANASTASIO.</P>)

ATA 4940

APU FAILED TO START.(<P>FOUND APU BATTERY LOW VOLT AT START 9VDC. REMOVE AND REPLACE APU BATTERY IAW AMM 24-31-04. OPS CHECK NORMAL AT THIS TIME.</P>)

ATA 2150

EXCESSIVE AIRFLOW WITH BOTH PACKS OPERATING. BOTH LT AND RT PACKS OPERATION WAS CHECKED. OPS CHECKED NORMAL IAW TASK 21-51-00/501.

ATA 3442

ON CLIMBOUT IN VISIBLE PRECIPITATION, WXR FAIL MESSAGE DISPLAYED ON CAPT'S AND FO'S EHSI WITH LEFT RADAR SELECTED. SWITCHED TO RIGHT RADAR, NO FURTHER DEFECTS NOTED. PERFORMED TROUBLESHOOTING OF WXR LEFT AND RIGHT SYSTEMS. NO FAULTS NOTED AS PER FIM 34-43 FAULT TREE 803. OPS CHECKED NORMAL.

ATA 2121

AFT EQUIPMENT EXHAUST FAN 2 STATUS MESSAGE. TROUBLESHOT PER FIM 21-26 FT 806. MESSAGE ERASED. NO FURTHER FAULTS AT THIS TIME.

ATA 4920

DURING PRE-FLIGHT APU FAULT MESSAGE. APU AUTO SHUTDOWN. PERFORMED FIM 49-11 FT 995 LOW OIL PRESSURE ON BITE TEST, SUSPECTED BAD LOW PRESSURE SWITCH. REMOVED AND REPLACED SWITCH IAW AMM 49-94-02. OPERATIONAL TEST OK. PERFORMED FIM 49-11 FT 995, OIL WAS OVER SERVICED. REMOVED FILL CAP AND APPROX 3 QTS OF OIL DRAINED, NO EICAS MSG PRESENT. OPS CHK NORMAL. NO FUEL SENSE NOTED.

ATA 4940

APU FAILED ON GROUND TUG AND TAXI 3 TIMES IN 45 MINUTES. 3 STARTS SUCCESSFUL IN 1 HOUR. PERFORMED APU ECU BITE IAW FIM 49-11 FT 958. NO FAULTS NOTED. CLEARED MEMORY ON ECU. OPS CHECK NORMAL AT THIS TIME.

ATA 4990

APU FAILED TO START, LOW OIL. SERVICED APU TO LIMITS IAW 12-13-04. PERFORMED APU STARTUP, OPS CK GOOD.

ATA 3697

RIGHT ENGINE BLEED LIGHT ON DURING PRE-DEPARTURE CHECK. FOUND BROKEN WIRE AT TERMINAL 2. REPAIRED IAW SWPM 20-10-13. PERFORMED AIR SUPPLY BITE TEST IAW AMM 36-23-00. NO MESSAGES NOTED.

ATA 2150

PACKS ARE TOO LOUD AND MAKE COMMUNICATION TOO DIFFICULT.(<P>PERFORMED OPS TEST OF OF BOTH L/H AND R/H PACKS. OPS TEST GOOD IAW B 767 AMM 21-51-00. PERFORMED BIT TEST OF TEMP CONTROLLER IAW B767 AMM 21-51-14. NO DEFECTS NOTED.</P>)

ATA 3610

R ENG BLEED OFF EICAS, CYCLES ON AND OFF CONSTANTLY DURING FLIGHT WITH FLUCTUATING R BLEED DUCT PRESSURE.(<P>PERFORMED FIM 36-10 FT 838. NO DEFECTS NOTED WITH ENGINE RUN SYSTEM CHECKS OPS NORMAL, RH ENGINE.</P>)

ATA 2150

PACKS ARE EXTREMELY LOUD AND SURGE SIGNIFICANTLY. ACCOMPLISHED AN OPERATIONAL TEST ON BOTH PACKS WITH ENGINE BLEED AND ALSO APU BLEED IAW AMM 21-51-00. OBSERVED NO SURGE OR LOUD NOISE WHILE RUNNING WITH APU BLEED. WHEN RUNNING PACKS WITH ENGINE BLEED, OBSERVED NO SURGE BUT LITTLE LOUDER THAN NORMAL NOISE COMING FROM F/O WALL VENT. PERFORMED A BITE OF AIR SUPPLY BITE MODULE IAW FIM 36-20-00 WITH NO FAULTS NOTED AND BOTH PACK CONTROLLERS IAW AMM 21-51-00 WITH NO RESULTS. ALSO NOTICED NO FLUCTUATIONS IN DUCT PRESSURE OR ABNORMAL NOISE WITH PACKS RUNNING.

ATA 2150

IN FLIGHT WITH BOTH PACKS ON, THERE IS EXCESSIVE NOISE. WITH ONE PACK OFF, NOISE IS NORMAL. PERFORMED OPS TEST ON RT PACK WITH APU RUNNING IAW AMM 21-51-00.OPS CHECKED GOOD.

ATA 4940

APU INOP. REMOVED AND REPLACED EXCITER IGNITION IAW AMM 49-41-03. OPS CHECKED GOOD. REMOVED AND REPLACED THE IGNITION LEAD ON APU IAW AMM 49-41-04. OPS CHECKED GOOD.

ATA 2130

CABIN ALT AUTO 1 STATUS MESSAGE DISPLAYED.(<P>PERFORMED BITE TEST #1 CABIN PRESS CONTROL UNIT IAW FIM 21-31 FT 809, TEST OK.</P>)

ATA 7310

ITEM 1: EICAS MSG RH ENG FUEL FILTER CLIMBING THROUGH 10,000, N1 106.4. CLEARED WHEN THRUST REDUCED FOR CRUISE. NO ENGINE ABNORMALITIES NOTED.&NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; &NBSP; ITEM 2: STATUS MSG RH ENG FUEL FILTER ASSOCIATED WITH WRITE-UP.(<P>REMOVED AND REPLACED FUEL FILTER HOUSING ASSY IAW AMM 73-11-03, RAN ENGINE IAW AMM 72-00-00. LEAK CHECK GOOD.</P>)

ATA 3442

WEATHER RADAR WEAK MESSAGE FLASHING ON CAPTAIN'S LOWER DISPLAY DURING CLIMB OUT PERFORMED OPS TEST OF THE WEATHER RADAR SYSTEM, FOUND NO FAULTS AT THIS TIME. OPS CHECK GOOD IAW AMM 34-43-00

ATA 3510

CAPTAIN'S OXYGEN MASK DOES NOT STOP FLOW OF OXYGEN WHEN IN USE.(<P>SWAPPED LEFT SUPERNUMERARY SEAT MASK (OFF PART: P/N MC10-08-114, S/N B119143) WITH CAPTAIN MASK (OFF PART: P/N MC10-08-109, S/N SE63145) IAW B767 AMM 35-11-51. TRANSFERRED LEFT SUPERNUMERARY SEAT TO MDDR 120447 PER DDG 25-25-03, CAT 'D', DUE: 09-MAR-2020.</P><P>LP&NBSP;1229251 - M2: SUPERNUMERARY LEFT SEAT OXYGEN MASK HAS BEEN REMOVED AND REPLACED IAW B767 -300 AMM 35-11-51. OPS CHECK OK, NO DEFECTS FOUND AT THIS TIME. THIS CLEARS MDDR 120447. PLACARDS REMOVED AND MCC NOTIFIED.&NBSP;</P>)

ATA 3110

BOTH GEN DRIVE LIGHTS ILLUMINATED IN BRIGHT MODE.(<P>FOUND INCORRECT LIGHT BULBS IN BOTH GEN DRIVE DISC SWITCHES. RELAMPED BOTH SWITCHES IAW AMM 33-16-02. PERFORMED BITE TEST AND RESET TEST OF BPCU IAW AMM 24-11-00-745-001. NO FAULTS OR DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD&NBSP;</P>)

ATA 3442

WX RADAR DOES NOT PAINT VISIBLE BUILD UPS. DISPLAYS ONLY PAINTS SPLATTER PATTERN, FAILS TO ADVISE CREW OF PRECIPITATION.&NBSP;(<P>RERACKED LEFT R/T. PERFORMED OPERATIONAL TEST OF LEFT AND RIGHT WEATHER RADAR IAW AMM 34-43-00, SELF TEST AND OPS TEST GOOD.</P>)

ATA 2421

APU POWER DID NOT AUTO TRANSFER UPON ENGINE SHUTDOWN. APU POWER DID NOT TRANSFER FROM GPU TO APU. REMOVED AND REPLACED APU GENERATOR IAW AMM 24-21-01, AND TESTED IAW AMM 24-21-01/501. FOUND GOOD, OPS CHECK NORMAL.

ATA 2400

APU DID NOT AUTOMATICALLY SWITCH TO AIRCRAFT WHEN AIRCRAFT SHUTDOWN. FOUND BPCU FAULTING IAW FIM 24-20-00 FT 801. REMOVED AND REPLACED BPCU IAW 24-41-03, OPS CHECK GOOD.&NBSP;</P>)

ATA 2120

LEFT PACK INOP LIGHT DURING PRE-FLIGHT.&NBSP;(<P>TRANSFERRED TO MDDR 118637 PER MEL 21-51-01-01, CAT "C",&NBSP; DUE 14-OCT-19. C/W MX PROCEDURES.</P><P>LP 1223539 - M2:&NBSP;REMOVED AND REPLACED L/H DUCT AIR TEMP SENSOR IAW B767-300 AMM 21-61-02. OPS CHECK GOOD. THIS CLEARS MDDR #118637. PLACARDS REMOVED AND MCC NOTIFIED.&NBSP;<BR /></P>)

ATA 2150

RIGHT PACK TEMP EICAS MESSAGE ON APPROACH AND LANDING. REMOVED AND REPLACED RT PACK CONTROLLER IAW AMM 21-51-14/401. PERFORMED PACK CONTROLLER BITE TEST, NO FAULTS SHOWED REF 21-51-14/501. REMOVED AND REPLACED RT PACK TEMP CONTROL VALVE IAW 21-51-12. OPS CHECK AND LEAK CHECK GOOD.

ATA 2150

RT PACK TEMP EICAS MSG IN FLIGHT, IN AUTO MODE.(<P>PERFORMED BITE TEST ON RT PACK TEMP CONTROLLER, BITE PASS. OK FOR CONTINUED SERVICE AT THIS TIME IAW AMM 21-51-14.

ATA 2421

"R GEN OFF" EICAS IN FLIGHT AT FL 410. TROUBLESHOT RIGHT IDG IAW FIM 24-20 TASK 804, TABLE 102. "DP TRIP AND GEN/FDR" MESSAGE. C903 FOUND SHORTED BETWEEN L1 AND T1. REPLACED C903 IAW WDM 24-21-21. DID NOT FIX. SEE ITEM M4 ON LP 1100813 FOR CORRECTIVE ACTION. OFF PART (PN: B-430-1, SN: CL-45368) LP 1100813 - M4: TRANSFERRED TO MDDR #118049 IAW MEL 24-00-01-01, CAT B. LP 1100819 - M12: REMOVED AND REPLACED RT IDG IAW AMM 24-11-01. PERFORMED OPS TEST IAW AMM 24-11-00. OPS TEST AND DISCONNECT FUNCTION TEST GOOD AT THIS TIME. THIS CLEARS MDDR 118049, PLACARD REMOVED AND MCC NOTIFIED.

ATA 2150

RIGHT PACK HIGH TEMP EICAS MSG DURING TAXI INTO TPA. PERFORMED BITE TEST OF PACK TEMP CONTROLLER FLAGGED TEMP CONTROL VLV, CLEARED FAULT, RAN BITE SECOND TIME, NO FAULTS AT THIS TIME PER AMM 21-51-14-705.

ATA 4960

APU INOP. TRANSFERRED TO MDDR 117310 IAW MEL 49-11-01A, CAT "C", DUE 15SEP19. LP 1100647 - M4: REMOVED AND REPLACED APU CONTROL UNIT IAW AMM 49-61-05. OPS CHECK GOOD. THIS CLEARS DMI #117310. PLACARDS REMOVED.

ATA 2150

R PACK TEMP EICAS MSG FOR 20 SECONDS ON SHORT FINAL. PERFORMED BITE TEST ON RT PACK TEMP CONTROLLER AND SYSTEM TEST, NO CURRENT FAULTS NOTED IAW AMM 21-62-00. SYSTEM OK FOR CONTINUED SERVICE.

ATA 4940

APU FAULT MESSAGE AFTER LANDING. CAPTAIN REPORTED 2 ATTEMPTS. PERFORMED BITE CHECK OF ECU, NO FAULTS NOTED IAW AMM 49-61-05. APU STARTED ON 3RD ATTEMPT (1ST BY MX), OPS CHECK GOOD.

ATA 2150

"R PACK TEMP" EICAS DURING TAXI OUT. INOP LIGHT AND MESSAGE EXTINGUISHED AFTER STBY-N SELECTED.(<P>PERFORMED OPS CHECK ON R/H PACK IAW AMM 21-51-00. NO FAULTS NOTED, OPS NORMAL.</P>)

ATA 3422

ELECTRICAL FUMES DETECTED SHORTLY AFTER ADI FAILURE. AFTER REMOVING AND REPLACING THE CAPTAIN`S EADI, PERFORMED SMOKE OR FUMES IN CABIN INSPECTION. NO DEFECTS NOTED AT THIS TIME IAW AMM 05-51-56-202-001 REV. 128. CAPT EADI WAS SOURCE OF SMOKE. AFTER R & R CAPT EADI, NO SMOKE IAW AMM 34-22-03.

ATA 2563

DURING WORK CARD NUMBER A-23-999-01, ELT OPERATIONAL CHECK. ELT OPERATIONAL CHECK FAILED, DID NOT RECEIVED DISTRESS SIGNAL. COMPLIED WITH MAINTENANCE ACTION. PERFORMED FIM 23-24 FAULT TREE 803, BLOCKS 1-24. REACTIVATED ELT AND COMPLIED WITH EO 6723A093. OPS CHECKED GOOD,

ATA 3610

RIGHT ENGINE BLEED OFF LIGHT WITH RIGHT ENGINE BLEED EICAS AFTER BLOCK OUT. ACCOMPLISHED QRH PROCEDURES LIGHT REMAINED ON. INCREASED THRUST TO 77% N2 - NO CHANGE. REMOVED AND REPLACED #2 ENGINE PRV IAW 36-11-07. NO HELP. REMOVED AND REPLACED RIGHT ENGINE BLEED AIR CARD (M860). IAW AMM 36-11-03. OPS CHECK GOOD AT THIS TIME.

ATA 3610

FOUND LH ENGINE PRSOV GROUND SERVICE SWITCH INTERMITTENT.(<P>REMOVED AND REPLACED SWITCH ASSY IAW 767 SWPM 20-81-00. SWITCH OPS CK GOOD.<BR /></P>)

ATA 4940

APU FAILED TO START AFTER LANDING. PERFORMED BITE CHECK OF ECU ABOUT START MESSAGE IAW AMM 49-61-05, SYSTEM TEST OK. PERFORMED PHYSICAL OIL CHECK AND SERVICED APU OIL IAW AMM 12-13-04. APU STARTED NORMAL ON 2ND ATTEMPT. OPS CHECK GOOD.

ATA 3442

WEATHER RADAR DOES NOT PAINT CELLS INSIDE OF 40 NM REGARDLESS OF TILT, GAIN, OR (L) (R) SELECTION.(<P>PERFORMED WEATHER RADAR OPS CHECK ON BOTH LEFT AND RIGHT SYSTEMS. NO FAULTS FOUND. WEATHER RADAR OPERATES NORMALLY REF B767 AMM 34-43-00.</P>)

ATA 2150

L PACK TEMP EICAS AT CRUISE, COMPLIED WITH QRH. (<P>PERFORMED T/S PER FIM 21-51-FT 844, COULD NOT DUPLICATE ITEM. NO FAULTS AT THIS TIME, SYSTEM FUNCTIONS NORMALLY.</P>)

ATA 2425

HYD GEN VAL MESSAGE(<P>LP 1072969 - M12: RECONNECTED HYDRAULIC MOTOR GENERATOR SHUTOFF VLV CANNON PLUG, TEST TO BE PERFORMED ON LP 1072969 - ITEM M11 PER AMM 24-25-03.<BR DATA-MCE-BOGUS="1" /></P><P>LP 1072969 - M11: T/S 'HYD GEN VAL" MSG, FOUND RELAY K860 TO BE FAULTY. R/R RELAY IAW FIM 24-25 FAULT TREE 803. PERFORMED OP'S CHECK IAW AMM 24-25-00. OPS CHECK OK.<BR /></P><P><BR /></P>)

ATA 2150

EICAS "LEFT PACK OFF" AND "LEFT PACK TEMP" IN DESCENT. (<P>C/W OPS CHECK OF LEFT PACK SYSTEM IAW 21-51-00. OPS CHECK NORMAL, NO FAULTS NOTED.</P>)

ATA 2150

&NBSP;LEFT PACK TEMP / OFF EICAS&NBSP;(<P>&NBSP;NO MESSAGE UPON ARRIVAL PERFORMED LEFT PACK OPERATIONAL TEST AND PACK TEMP CONTROLLER BITE, NO DEFECTS NOTED PER AMM 21-51-14-705-035 AND 21-51-00-705-013-003</P>)

ATA 7320

LEFT ENGINE CONTROL EICAS MESSAGE AFTER START. PERFORMED BITE OF LH EEC WITH PIMU FAULTED CHAN A & B FOR LT EEC , REMOVED AND REPLACED THE LT EEC IAW AMM 73-21-15. OPS CHECKED GOOD.

ATA 7200

AFTER LEFT ENGINE START RECEIVER EICAS MESSAGE L ENG CONTROL STATUS MESSAGE L ENG CONTROL(<P>PERFORMED FIM 73-21 FT 894 NO DEFECTS NOTED PIMU BITE TEST SHOW NO FAULTS EICAS MSG L ENG CONTROL GOOD&NBSP;</P>)

ATA 2150

LEFT PACK TEMP LEFT PACK OFF PACK RESET PER QRH PACK INOP HEAT LIGHT REMAINED. PERFORMED PROCEDURES IAW FIM 21-51 FT 844 OPS CK GOOD AND RUN FOR 30 MINUTES ON GROUND NO FAULTS NOTED.</P>)

ATA 7200

AFTER LEFT ENGINE START, RECEIVED EICAS MESSAGE L ENG CONTROL STATUS MESSAGE L ENG CONTROL. PERFORMED FIM 73-21 FLT 894 - NO DEFECTS NOTED. PIMU BITE SHOWS NO FAULTS.</P>)

ATA 2150

DURING OPERATIONAL CHECK OF THE E/E COOLING LOW FLOW FAIL FLOWS BALLS OF EADI-L, VOR-L, AND FMCDU-L.(<P>ACCOMPLISHED OPERATIONAL TEST IAW AMM 21-58-00-705; SYSTEM CHECKS OK.

ATA 3040

CAPT SIDE WINDOW FOGGING INOP.(<P>PERFORMED SIDE WINDOW CAPT'S SIDE HEATER ELEMENT LOOP RESISTANCE PER AMM TASK 30-41-00-765-046; FOUND WITHIN LIMITS. PERFORMED FLIGHT COMPARTMENT WINDOW ANTI-ICING. OPS CHECK FOUND OK.

ATA 2121

FWD EQUIPMENT FAN STATUS MESSAGE.(<P>REMOVED AND REPLACED THE FWD RACK EXHAUST FAN B12 AS PER AMM 21-58-06/401. OPS AND LEAK CHECK GOOD.

ATA 3040

CAPT'S SIDE WINDOW FOGGING UP. PERFORMED CAPTAINS SIDE WINDOW HEATER ELEMENT LOOP RESISTANCE CHECK IAW B767 AMM TASK 30-41-00-765-046 AND FOUND WITHIN LIMITS. PERFORMED WINDOW ANTI-ICING TEST IAW TASK 30-41-00-715-001. OPS CK NORMAL.

ATA 2121

FWD EQUIPMENT EXH FAN STATUS MESSAGE. REMOVED AND REPLACED THE FORWARD RACK EXHAUST FAN (B12) AS PER B767 AMM 21-58-06/401. OPS CHECK NORMAL, NO LEAKS.

ATA 3040

RIGHT FWD WINDOW HEAT SWITCH BROKEN.(<P>REMOVED AND REPLACED WINDOW HEAT CONTROL PANEL ASSY IAW AMM 30-41-02. OPS CHECK GOOD. NO DEFECTS NOTED AT THIS TIME.</P>)

ATA 7411

RIGHT ENGINE IGNITER 1 &AMP; 2 STATUS MESSAGES ILLUMINATED.(<P>REMOVED AND REPLACED #2 IGNITION EXCITER BOX. INSTALLATION OPS CHECK GOOD PER AMM 74-11-01. OFF PART (P/N&NBSP;10-631045-2, S/N&NBSP;UNNEP031).</P><P>LP 1050597 - M4: REMOVED AND REPLACED RH ENG IGNITER PLUGS 1 AND 2. INSTALLATION OPS CHECKS GOOD IAW AMM 74-11-01. (P/N CH31772A, S/N NSN)</P><P>LP 1050597 - M5: PERFORMED RH ENG RUN PER B767 AMM 71-00-00. "RH ENG IGNITER 2" STS MSG UPON ENGINE SHUTDOWN. REF LP 1050596 - M3 FOR DEFERRAL.</P><P>LP 1050596 - M3: DEFECT TRANSFERRED TO DMI 112680 PER MEL 74-00-01<STRONG>Ï»¿</STRONG>Ï»¿B CAT 'C'. DUE 14 JUN 19.&NBSP;</P><P>15JUN19: LP 1065628, ITEM M17: REMOVED AND REPLACED K1230 RELAY, OPS CHECK OK. PER AMM 71-00&AMP; SWPM 20-81-22.</P>)

ATA 2150

LEFT PACK TEMP W/ASSOCIATED LEFT PACK OFF NEAR TOP OF CLIMB. OPERATED IN STANDBY FOR REST OF FLIGHT. PERFORMED OPS CHECK OF LEFT PACK IAW AMM 21-00-00. PERFORMED BIT TEST FOR LEFT PACK SYSTEM IAW 21-51-14. OPS CHECKED GOOD AND NO FAULTS NOTED. INSPECTED LEFT COOLING PACK SYSTEM IAW AMM 21-51-00. AIR LEAK CHECK GOOD AND FOUND NO DEFECTS.

ATA 2150

LEFT PACK EICAS MESSAGE AND LEFT INOP LIGHT.(<P>RESET PACK CONTROL SWITCH, NO HELP. TRANSFERRED TO MDDR&NBSP; #112365 IAW MEL 21-51-01-01.</P><P>LOG PAGE 1050571 - M3: FOLLOWED FIM 21-51 TASK 877. REACTIVATED LT PACK IAW AMM 21-00-00/901. PERFORMED BITE TEST IAW AMM 21-51-14, NO FAULTS NOTED. INSPECTED COOLING PACK SYS IAW AMM 21-51-00, FOUND DUCT CONNECTION FROM SECONDARY HEAT EXCHANGER LEAKING. TIGHTENED RESTRAIN CABLES. PERFORMED OPS CHECK AND OPS NORMAL. MDDR # 112365 CLOSED, PLACARD REMOVED AND MCC NOTIFIED.&NBSP;</P>)

ATA 3425

CAPTAIN'S HSI FAILED COMPLETELY ON SHORT FINAL ACCOMPANIED BY A BURNING SMELL. (<P>REMOVED AND REPLACED CAPTAINS EHSI IAW AMM 34-22-04. OPERATIONAL TEST GOOD. </P><P>LP 1064180 - M6:&NBSP;PERFORMED INSPECTION OF EQUIPMENT COOLING SYSTEM IAW AMM 21-58-00. NO DEBRIS OR EVIDENCE OF BURNING FOUND. WHEN REMOVING AND REPLACING HSI, FOUND SCREEN TO BE BURNT.&NBSP;</P>)

ATA 7421

R ENG IGNITER 2 STATUS MESSAGE(<P>R ENG IGNITION AUDIBLE TESTED PER AMM 74-00-00. BOTH IGNITERS OK. NO ACTIVE MSG.</P>)

ATA 7421

R ENG IGNITER 2 STATUS MSG.(<P>PERFORMED PIMU BITE TEST AND PERFORMED RT ENGINE IGNITION AUDIBLE TEST GOOD IAW AMM 74-002-00. NO DEFECT NOTED AT THIS TIME.</P>)

ATA 2130

AFTER LANDING "CABIN ALT. AUTO 1" STATUS MESSAGE - CLEARED ON ENGINE SHUTDOWN.&NBSP;(<P>PERFORMED BOTH LEFT AND RIGHT CABIN PRESSURE BITE PROCEDURES PER FIM 21-31-00/101. NO FAULTS FOUND DURING BITE TEST. OPS CHECK NORMAL.&NBSP;</P>)

ATA 7421

RIGHT ENGINE NR 2 IGNITER MESSAGE DISPLAYED. (<P>R&AMP;R RT ENGINE NR 2 IGNITER PLUG IAW AMM 74-21-02. MESSAGE CLEARED OPS CHECK GOOD.&NBSP;<BR DATA-MCE-BOGUS="1" /></P>)

ATA 3454

ON P61 PANEL E/E COOLING MONITOR GETS NO TEST INDICATION FOR VOR-L. VERIFIED PRESSURE COMING OUT OF SENSE LINE ON L VOR AT COOLING MONITOR PANEL, FOLLOWED FIM TASK 21-58- FT A00 TO SHEET 2 BLOCK 22. TO DETERMINE HOW MUCH PRESSURE IS COMING FROM SENSE LINE. PERFORMED FIM 21-58 FT ACO. REMOVED AND REPLACED E/E COOLING MONITOR PANEL IAW AMM 21-58-34. OPS CHECKED GOOD.

ATA 3442

INTERMITTENT WEATHER RADAR, WEAK MESSAGE ON HSI WHEN WEATHER SYSTEM #1 (LEFT) SELECTED.&NBSP;(<P>PERFORMED OPS TEST ON LEFT AND RIGHT WEATHER RADAR SYSTEMS IAW B767 AMM 34-43-00. SYSTEM OPERATE NORMAL. NO FAULTS FOUND AT THIS TIME.&NBSP;</P>)

ATA 2150

IN CRUISE AT FL 380 LOUD SURGING OF SINGLE AIR CONDITIONING PACK. LEFT DUCT PRESSURE OBSERVED SURGING REPEATEDLY FROM 25 PSI TO 41 PSI RT DUCT PRESSURE AT 24 PSI(<P>PERFORMED BITE 21-51 FT 803 FOUND LOW LIMIT VALVE HARD FAULT REMOVED AND REPLACED LOW LIMIT VALVE IAW AMM 21-51-11 OPS TEST GOOD LEAK CHECK GOOD&NBSP;</P>)

ATA 4950

DURING APU SURGE VALVE FILTER CHANGE FOUND HOLE IN DUCTING SURGE VALVE. (<P>APU DEFERRED PER MEL 49-11-00A, AS PER MDDR 108778</P><P>LP 1022498-M6: REMOVED AND REPLACED APU SURGE DUCT FWD FLEX CONNECTOR IAW AMM 49-53-01. NO FURTHER DEFECTS NOTED AT THIS TIME. DMI 108778 CLOSED.&NBSP;</P><P><BR /></P><P><BR /></P>)

ATA 3442

WX RDR NOT PAINTING SIGNIFICANT PRECIP AMOUNTS IN ANY MODE ON DSCNT BEGAN PAINTING SOME WX BCD 5000'(<P>PERFORMED OPERATIONAL CHECK OF RT &AMP; LT WX RADAR SYSTEM PER AMM 34-43-00, OPS CHECK NORMAL.</P>)

ATA 3610

ENG NR 2&NBSP; &NBSP;PRESSURE&NBSP; REGULATING VALVE&NBSP; HAS PNEUMATIC&NBSP; LEAK&NBSP; AT CHECK&NBSP; &NBSP;LOCATION&NBSP; " K " AS PER EO 1936A088.(<P>REMOVED AND REPLACED&NBSP; NR 2&NBSP; ENG . PRESS.&NBSP; REG. VALVE&NBSP; O RING&NBSP; AT "K"&NBSP; LOCATION&NBSP; LEAK&NBSP; &NBSP;CHECK NORMAL&NBSP; REF.&NBSP; AMM 36-1-18.</P>)

ATA 7220

ENG NR 1 SPINNER&NBSP; BLACK&NBSP; AND WHITE&NBSP; SWIRL PAINT DAMAGED .(<P>PREPARED, CLEANED MASKED, PRIMED&NBSP; AND PAINTED&NBSP; BLACK&NBSP; AND WHITE&NBSP; SWIRL ENG NR 1 SPINNER&NBSP; IAW CF&NBSP; SRM 51-21-01-0G-0.</P>)

ATA 2150

L PACK TEMP MESSAGE AFTER BLOCKED OUT. WOULD NOT CLEAR. RETURN TO BLOCKS.(<P>CLEARED L PACK CONTROLLER AND OPS CHECKED L PACK IAW AMM 21-00-00. NO FURTHER DEFECT NOTED.</P>)

ATA 7230

RIGHT ENGINE FAN VIBRATIONS HIT 4.5 IN CLIMB &AMP; MAINTAINED 4.5 LEVEL CRUISE FLIGHT(<P>PERFORMED FAN TRIM BALANCE ON RT ENG IAW AMM 72-31-00. FAN VIB CORRECTED TO 0.8. REF LOG PAGE 1026507-6: ECM C/W.&NBSP;&NBSP;</P>)

ATA 7932

RIGHT ENGINE OIL PRESSURE EICAS MESSAGE&NBSP;(<P>DUE TO ENGINE SHUT DOWN ANOMALY WITH RIGHT ENGINE SPAR VALVE LOCK TO THE OPEN POSITION EICAS MESSAGE PRODUCE SIMILAR FAULT PRESENT IAW 26-11-00 ALL FAULTS CLEARED REF LOG PAGE 1048084 ITEM 4 OPS CHECK NORMAL DURING ENGINE RUN IAW AMM 71-00-00&NBSP;&NBSP;</P>)

ATA 2897

RIGHT FUEL SPAR VALVE EICAS MESSAGE&NBSP;(<P>PERFORMED WDM T/S IAW 28-22-21. FOUND 5A PIN AT SWITH 538 REPLACE SWITCH NO HELP. RE INSTALLED ORIGINAL PART BACK FOUND BROKEN WIRE @ WIRE 3026-20 IN WHEEL WELL SEE ITEM M5 LOG PAGE 1048085 FOR WIRE REPAIREED.</P><P>REPAIRED WIRE 302B BETWEEN CONNECTOR D5520 AND D1572&NBSP; IAW SWPM CH 20-20-01</P><P>LOG PAGE 1048085 ITEM M6; PERFORMED OPERATIONAL CHECK ON RIGHT SPAR VALVE IAW AMM 28-22-11. OPS CHECK GOOD AT THIS TIME, PERFORMED ENGINE RUN FOR PROPER SHUT DOWN OF ENGINE OPS CHECK NORMAL AT THIS TIME IAW AMM 71-00-00</P>)

ATA 2421

RIGHT GENERATOR DRIVE EICAS MESSAGE.&NBSP;(<P>DUE TO ENGINE SHUTDOWN ANOMALY WITH RIGHT ENGINE SPAR VALVE STUCK IN THE OPEN POSITION EICAS MESSAGE PRODUCE IS SIMILAR TO FIRE T-HANDLE BEING PULLED PERFORMED FAIL P RESET IAW 26-11-00 MESSAGE CLEARED OPS CHECK NORMAL AFTER ENGINE RUN IAW AMM 71-00-00 REFERENCE ITEM M2.&NBSP;</P>)

ATA 2160

AFT CABIN TEMP EICAS MESSAGE AND AFT CABIN INOP LIGHT ILLUMINATED&NBSP;(<P>TRANSFERRED TO MDDR 107095 PER DDG 21-61-01-02 CAT "C"&NBSP;</P><P>LP 1034027-M2 REMOVED AND REPLACED&NBSP; TRIM AIR MODULATING VALVE IAW AMM 21-61-07 OPS CHECK OK. THIS CLEARS DMI # 107095, PLACARDS REMOVED AND MX ACTIONS C/W.

ATA 7830

R ENG VIBRATION MONITOR 4.8 ON TAKEOFF /CLIMB OUT&NBSP;(<P>FOUND UPPER LATCH ON R/H REVERSE OUT OF ADJUSTMENT, ADJUSTED LATCH IAW AMM 78-31-02 PERFORMED ENGINE RUN IAW AMM 71-00-00 OPS CHECK VIBRATION NORMAL</P>)

ATA 3610

RT ENG. PRSOV FAILED PNEUMATIC HEALTH CHECK, OPEN SIGNAL WAS DETECTED. (<P>REMOVED AND REPLACED NR 2 ENG. PRSOV IAW AMM 36-11-09.</P>)

ATA 3610

LT ENG. FAV FAILED PNEUMATIC HEALTH CHECK OPEN AND CLOSED SWITCHES DISAGREE. (<P>REMOVED AND REPLACED NR 1 ENGINE FAN AIR VALVE IAW AMM 36-11-16.</P>)

ATA 3610

RT HPSOV FAILS TO GO OPEN POSITION DURING ASM TEST. (<P>REMOVED AND REPLACED NR 2 ENGINE HPSOV IAW AMM 36-11-07.</P>)

ATA 4940

APU STARTER MOTOR BRUSHES ARE WORN STARTER NEEDS TO BE REPLACED (REF. W/C #A-49-062-01)(<P>REMOVED AND REPLACED APU STARTER IAW AMM 49-41-01. PERFORMED SATISFACTORY OP CHECK IAW AMM 49-41-01 (NO DEFECTS NOTED).</P>)

ATA 2822

LT AFT FUEL BOOST PUMP C/B IS POPPING OUT.(<P>REMOVED AND REPLACED AFT LT FUEL BOOST PUMP IAW AMM 28-22-03.</P>)

ATA 3610

LT ENG FAV FAILED PNEUMATIC HEALTH CHECK. OPEN AND CLOSE SWITCHES DISAGREE.(<P>R/R NR 1 ENG FAN AIR VALVE IAW AMM 36-11-16.</P>)

ATA 3610

RT HPSOV FAILS TO GO INTO THE OPEN POSITION DURING ASM TEST.&NBSP;(<P>R/R NR 2 ENG HPSOV IAW AMM 36-11-07</P>)

ATA 4940

APU STARTER MOTOR BRUSHES ARE WORN, STARTER NEEDS TO BE REPLACED (REF WORK CARD NUMBER A-49-062-01).(<P>R/R APU STARTER IAW AMM 49-41-01. PERFORMED SATISFACTORY OPS CHECK IAW AMM 49-41-01. NO DEFECTS NOTED.</P>)

ATA 2822

LEFT AFT FUEL BOOST PUMP C/B POPS OUT AFTER 20-30 SECONDS OF OPERATION.&NBSP;(<P>R/R LT AFT FUEL BOOST PUMP IAW AMM 28-22-03.</P>)

ATA 3610

RT ENG PRSOV FAILED PNEUMATIC HEALTH CHECK. OPEN SIGNAL WAS DETECTED.(<P>R/R NR 2 ENG PRSOV IAW AMM 36-11-09</P>)

ATA 3442

WXR WEATHER RADAR SWITCH PUSH BUTTON SWITCH ON DASH PANEL BELOW HSI ON LIGHT DOESNT STAY ILLUMINATED&NBSP;(<P>CLEANED&NBSP;CONTACTS AND PROBES BEHIND WEATHER RADAR PUSH BUTTON SWITCH IAW AMM 34-43-00 OPS CHECK GOOD AT THIS TIME&NBSP;</P>)

ATA 4920

APU AUTO SHUTDOWN(<P>PERFORMED APU ECU RESET IAW B767 AMM 49-11-00. OPS CHECKS GOOD.<BR /></P>)

ATA 2150

RT PACK OFF EICAS MESSAGE. PERFORMED ADJUSMENT / TEST OF THE RT COOLING PACK IAW AMM 21-51-00, NO MESSAGES NOTED ON BITE TEST. MESSAGE NORMAL WHEN PACK IS IN OFF POSITION OPS CHECK GOOD, A/C OK FOR SERVICE.

ATA 3443

UNABLE TO SELECT TERRAIN MODE(<P>COMPLIED WITH WEATHER RADAR OPS CHECK IAW AMM 34-43-00 OPS CHECK OK&NBSP;</P>)

ATA 4960

APU WOULD NOT START AFTER LANDING&NBSP;(<P>REMOVED AND REPLACED ECU IAW AMM 49-61-05. OPS CK NORMAL.</P>)

ATA 4990

APU FAILED TO START ON THE GROUND, THREE ATTEMPTS. SERVICED THE APU OIL SYSTEM IAW AMM 12-13-04 , OPS CHECKED NORMAL IAW AMM 49-11-00.

ATA 4950

NO DUCT PRESSURE WITH APU RUNNING. REPLACED THE APU BLEED VALVE IAW AMM 36-11-10. OPS CHECKED OK.

ATA 8010

NR 1 ENGINE START SWITCH TO GROUND STARTER VALVE LIGHT ILLUMINATED AND DUCT PRESSURE DROPPED, THEN RECOVERED. PERFORMED ENGINE RUN OF BOTH NR 1 AND NR 2 ENGINE IAW AMM 71-00-00. NO FAULTS AT THIS TIME.

ATA 7732

NR 2 ENGINE FAN VIBRATION 3.4 IN CLIMB. NO FAULTS NOTED IN REF FIM 77-31 FT 803 AND FT 808.

ATA 4960

APU RELIABILITY COLD SOAK FAILED AFTER 3 ATTEMPTS. PERFORMED BITE OF APU ECU IAW AMM 49-11-01, FOUND 2 MESSAGES ON PREVIOUS ATART ATTEMPTS, "START ABORTED TWICE". CLEARED APU ECU.

ATA 3442

RIGHT WEATHER RADAR SYSTEM FAILED. T/S SYS IAW FIM 34-43 F/T 805 (WXR BITE PROCEDURE) WXR TEST PASSED SYS IS IN SERVICEABLE CONDITION.

ATA 4900

UPON LANDING APU WOULD NOT START ATTEMPTED 2 TIMES APU FAULT. PERFORMED BITE TEST OF ECU NO FAULTS AT THIS TIME NO PROBLEM IAW AMM 49-11-00. OPS CHECK OK.

ATA 7310

ON CLIMB OUT STATUS MESSAGE RT ENGINE FUEL FILTER. PERFORMED FIM 73-11 FT 803, REMOVED AND REPLACED FUEL FILTER PER AMM 73-11-02. ENGINE IDLE RUN PERFORMED OPS CHECK AND LEAK CHECK OK.

ATA 2150

ON APPROACH RT PACK EICAS MESSAGE. PERFORMED RT PACK TEMP CONTROLLER BITE IAW AMM 21-51-00-705-035, COULD NOT DUPLICATE DISCREPANCY. OPS CHECK GOOD.

ATA 4970

APU FAULT EICAS MSG DISPLAYED WHEN ATTEMPTING APU START AFTER LANDING. PERFORMED QRH PROCEDURE, APU FAULT RE-ILLUMINATED. (APU WOULD NOT START). PERFORMED BITE TEST OF ECU BOX, FOUND NO FAULTS AT THIS TIME. PERFORMED (4) SUCCESSFUL APU STARTS WITH NO PROBLEMS IAW AMM 49-11-00, FAULT TREE 815. OPS CHECK GOOD.

ATA 4970

APU FAULT EICAS MSG DISPLAYED WHEN ATTEMPTING APU START AFTER LANDING. PERFORMED QRH PROCEDURE, APU FAULT REILLUMINATED APU WOULD NOT START. PERFORMED BITE TEST OF ECU BOX FOUND NO FAULTS AT THIS TIME. PERFORMED 4 SUCCESSFUL APU STARTS WITH NO PROBLEMS IAW AMM 49-11-00 FAULT TREE 815. OPS CHECK GOOD.

ATA 3610

APU NOT SUPPLYING DUCT PRESSURE. REMOVED AND REPLACED APU BLEED AIR VALVE IAW AMM 36-11-10. OPS CHECK GOOD.

ATA 4970

APU FAULT. APU OPS CHECK NORMAL ON 2ND ATTEMPT PER AMM 49-11-00, ACCOMPLISHED APU BITE PER FIM 49-11-00 NO FAULTS NOTED , APU FAULT AND AUTO EVENT ( EGT 727 RPM 29% OIL FULL ) CLEARED PER AMM 31-41-00. OPS CHECKED APU WITHOUT FAULTS PER AMM 49-11-00.

ATA 4920

APU WOULD NOT START AFTER 2 ATTEMPTS ON GROUND IN HNL. PERFORMED APU BITE CHECK IAW AMM 49-61-05 NO FAULTS FOUND, APU START SUCCESSFUL FIRST ATTEMPT. OPS CHECK GOOD.

ATA 7732

AFTER ENG START LPT INDICATION WENT TO 5.0 DURING TAKE OFF, CLIMB, CRUISE INDICATION NORMAL. PERFORMED IDLE ENGINE RUNS IAW AMM 71-00-00, VIB WAS WITHIN LIMITS AT THIS TIME. NO DEFECT NOTED AT THIS TIME.

ATA 3442

RADAR DOES NOT DISPLAY KNOWN PRECIP, AND GETTING EXCESSIVE SPIKING. PERFORMED OPERATIONAL TEST OF WEATHER RADAR IAW AMM 34-43-00. OPS NORMAL AT THIS TIME.

ATA 7732

AFTER ENG START LPT INDICATION WENT TO 5.0 DURING TAKE OFF. CLIMB, CRUSE; INDICATION NORMAL. PERFORMED IDLE ENGINE RUNS IAW AMM 71-00-00. VIB WAS WITHIN LIMITS AT THIS TIME. NO DEFECTS NOTED AT THIS TIME.

ATA 3442

WEATHER RADAR NOT SHOWING RETURNS ON STORMS. PERFORMED FIM TASK 34-43 FT 805 AND AMM 34-43-00 715. WXR OPERATES SATISFACTORY NO DEFECTS NOTED.

ATA 2150

RIGHT PACK TEMP INOP. PERFORMED FIM TASK 21-51 FT 844, COULD NOT DUPLICATE. OPS CHECK GOOD.

ATA 3442

WX RADAR APPEARS TO BE BIASED LOW TO THE RIGHT SIDE. PAINTS GROUND RETURNS ON RIGHT BUT NOT SIGNIFICANTLY(FL410) WITHIN 40 NM AND VISIBLE TO THE NAKED EYE. PERFORMED OPERATIONAL TEST OF WEATHER RADAR SYSTEM IAW AMM 34-43-00-715, FOUND NO DEFECT AT THIS TIME.

ATA 4940

APU FAULT LIGHT ILLUMINATED WHEN ATTEMPTING TO START AFTER LANDING. PERFORMED BITE CHECK AND RESET OF ECU PER FIM 49-11 FAULT TREE 959. OK FOR SERVICE.

ATA 2150

INTERMITTENT RT PACK TEMP EICAS MSG. EICAS MAINT MESSAGE "RT PACK BITE". PERFORMED RT PACK BITE, BITE MSG FOR RT PACK TEMP VALVE. RESET CONTROLLER, RAN PACK OPS CKS NORMAL AT THIS TIME IAW AMM 21-60 FAULT TREE 804.

ATA 4990

APU FAULT EICAS MESSAGE WHILE STARTING APU ON GROUND, SECOND START ATTEMPT ALSO UNSUCCESFUL. SERVICED APU OIL IAW AMM 12-13-04. FOLLOWED FIM 49-11 FAULT TREE 987/988 NO FAULTS NOTED APU STARTED FIRST ATTEMPT.

ATA 4900

APU FAULT EICAS MESSAGE ON TAXI IN, APU WOULD NOT START. PERFORMED FIM 49-11 FT 987, BITE TEST, NO FAULTS NOTED, PREVIOUS FAULT A/C START CIRCUIT, OPS CHECK IAW AMM 49-11-00. OPS CHECK NORMAL, NO FAULTS ON BITE.

ATA 4900

APU WONT START ON GROUND DID NOT TRY INFLIGHT. ACCOMPLISHED BITE OF APU AS PER FIM 49-11 FT 987, NO FAULTS FOUND. APU OPS CHECK GOOD PER AMM 49-11-00.

ATA 7321

INTERMITTENT LT ENG INDICATION N2. REMOVED AND REPLACED EEC LT ENG IAW AMM 73-21-15. OPS CHECK GOOD AT THIS TIME.

ATA 7600

STATUS & ADVISORY STATUS MESSAGES LT ENG CONTROL. PERFORMED BITE CHECK PIMU MSG ON NR 1 ENG. PERFORMED ENGINE RUN AND NO MSG OR FAULTS NOTED DURING RUN, NOT CURRENT FAULT AT THIS TIME AS PER AMM 71-00-00.

ATA 7700

LEFT ENGINE CONTROL EICAS MESSAGE. QRH PROCEDURE COMPLIED WITH (BECAME LEFT ENGINE CONTROL STATUS MESSAGE). PIMU BITE PROCEDURE PERFORMED IAW 71-01-00, MESSAGE CLEARED. RAN BOTH ENGINE TO PERFORM ASSURANCE RUN PER AMM 71-00-00, MESSAGE DID NOT DUPLICATE. PERFORMED BITE ON PIMU AFTER ENGINE RUN, NO FAULTS NOTED. VERIFIES NO HISTORY, AIRCRAFT OK FOR SERVICE.

ATA 4950

APU AIR SHUT OFF RUNNING ONE PACK. T/S ECU & BITE NO FAULTS NOTED. APU OPS OK IN REF TO AMM 49-50.

ATA 3610

LEFT ENG PRSOV INOP. REMOVED AND REPLACED LEFT ENGINE PRSOV IAW AMM 36-11-09. OPS CHECK GOOD.

ATA 4950

APU AIR SHUT OFF RUNNING ONE PACK. T/S ECU & BITE NO FAULTS NOTED, RESTART APU OPS CHECK IN REF AMM 49-52-00.

ATA 3610

SIGNIFICANT SPLIT BETWEEN LT AND RT DUCT PRESS AFTER T/O TILL APPROX 17000. (INFO: RT PSI 40//LT PSI 13). ALSO SURGED THROUGHOUT CLIMB. DEFERRED LT ENG PRSOV IAW MEL 36-11-01-02A. REMOVED AND REPLACED LT ENG PRSOV IAW AMM 36-11-09. OPS CHECK GOOD.

ATA 3497

SHORTLY AFTER TAKEOFF LEFT WEATHER RADAR FAILED. PERFORMED REPAIR OF WIRE W781-004-20 AND W781-005-20 IAW WDM 34-43-12 & SWPM 20-10-13. LEFT WEATHER RADAR OPS CHECK GOOD IAW AMM 34-43-00.

ATA 3610

PER INBOUND CREW LEFT ENGINE BLEED REQUIRED SEVERAL CYCLES OF THE SWITCH TO COME ONLINE. FOUND LT ENGINE PRV CONTROLLER FAILED, REPLACED PRV CONTROLLER AS PER AMM 36-11-19. OPS CHECK GOOD IAW AMM 36-11-18 & 36-11-00.

ATA 3610

PER MCC REQUEST CHANGE LEFT ENGINE BLEED AIR CARD & PRSOV. REMOVED AND REPLACED LEFT ENG BLEED CARD AS PER AMM 36-11-12 OPERATIONAL TEST GOOD P/N OFF 285T1115-15 S/N D01248. REMOVED AND REPLACED LT ENG PRSOV AS PER AMM 36-11-09 NO AIR LEAKS DETECTED, NO DEFECTS NOTED AT THIS TIME, OPS CHECK GOOD PER AMM 36-11-09.

ATA 3697

LT ENG BLEED OFF. REMOVED PANEL 431AL, INSPECTED, CLEANED CONNECTOR. MANUALLY OPENED/CLOSED PRSOV IAW AMM 36-11-00-501. ENGINE RUN PERFORMED BY AIR CREW. INSTALLED PNL 434AL, OPS NORMAL.

ATA 7321

STATUS MSG R ENG CONTROL ON EICAS MSG RT ENG CONTROL DURING LNDG. T/S IAW F/M 37-21 FAULT TREE 878. FOUND CODES ON PIMU: 354-20-B "EEC CUPU FALL". R&R RT EEC IAW AMM 73-21-15.

ATA 7321

STATUS MESSAGE R ENG EEC C1. PERFORMED OPS CHECK R ENGINE EEC IAW AMM 77-35-00. NO FAULTS FOUND AT THIS TIME.

ATA 4950

APU DUCT PRESSURE LOW ( 12 PSI ). PERFORMED OPS CHECK ON AIR SUPPLY DISTRIBUTION SYSTEM IAW AMM 49-11-00 OPS CHECK GOOD AT THIS TIME.

ATA 3442

SHORTLY AFTER TAKE OFF LEFT WEATHER RADAR FAILED. TRANSF'D TO MEL 34-43-01 MDDR 95064.

ATA 3442

"WX FAIL" DISPLAYED ON BOTH L&R RADAR. ACCOMPLISHED OPERATIONAL CHK OF LT WX RDR SYS, OPS CKD GOOD IAW 34-43-00. RT WX RADAR, REMOVED AND REPLACED WEATHER RADAR TRANSCEIVER.

ATA 3442

WX FAIL DISPLAYED FOR BOTH L&R SYSTEM. XFER TO MDDR 94829 IAW MEL 34-43-01-02 CAT C DUE 17 JUN-18. REMOVED AND REPLACED LT AND RT WX RADAR TRANSCEIVER IAW AMM 34-43-01. OPS CHECK NORMAL. P/N 2041217-0418 S/N 7476 LT, P/N 2041217-0418 S/N 4051 RT. ALSO REMOVED AND REPLACED WX RADAR CONTROL PANEL IAW AMM 34-43-02. OPS CHECK NORMAL.

ATA 7421

RIGHT ENGINE IGNITER NR 2 STATUS MESSAGE. REMOVED AND REPLACED THE NR 2 IGNITER IAW AMM 74-21-02. OPS CHECKED NORMAL.

ATA 7421

RIGHT ENGINE IGNITOR 2 STATUS MESSAGE. COMPLIED WITH TROUBLESHOOTING IAW FIM 71-01 TASK A33, NO DEFECTS NOTED. OK FOR SERVICE.

ATA 2150

ON EICAS/MSG PAGE MISSING TIME COMPR OUT INDICATION FOR RIGHT PACK. REMOVED AND REPLACED RIGHT PACK COMPRESSOR OUTLET TEMP BULB IAW AMM 21-52-01.

ATA 2150

ON LEFT PACK BAY PNEUMATIC LEAK FROM THE COMPRESSOR OUTLET DUCT CLAMP. REMOVED AND REPLACED COMPRESSOR OUTLET SEALS IAW AMM21-51-02. OPS CHECK NORMAL NO LEAKS.

ATA 3442

WEATHER RADAR FAIL ILLUMINATED LT & RT WEATHER RADAR INOPERATIVE. REMOVED AND REPLACED THE WEATHER RADAR DRIVE UNIT IAW AMM 34-43-07, AND 34-43-05. OPS CHECKED GOOD.

ATA 3442

WEATHER RADAR RIGHT SYSTEM PAINTS GROUND AT 80 MILES, +2 DEGREES TILT, PAINTS GROUND ON ROTATION AT +5 DEGREES AND 3 MILES. REMOVED AND REPLACED THE WEATHER RADAR DRIVE UNIT IAW AMM 34-45-05. OPS CHECKED GOOD,

ATA 4950

APU FWD AIR SURGE FLEX DUCT DAMAGED. REMOVED AND REPLACED APU SURGE DUCT IAW AMM 49-53-01 OPS AND LEAK CHECKED GOOD.

ATA 2421

APU GEN LIGHT ILLUMINATED. REMOVED AND REPLACED THE APU GENERATOR CONTROL UNIT IAW AMM 24-22-02, OPS CHECKED GOOD.

ATA 4920

APU RELIABILITY COLD START ACCOMPLISHED ON FLIGHT CVG - SCK SAT -55C FL340, START UNSUCCESSFUL. THREE ATTEMPTS, NO START NOTED BY MX, ECU BITE PERFORMED, NO FAULTS FOUND, APU RUNS ON GROUND. AIRCRAFT OK FOR SERVICE IAW AMM 49-11-00.

ATA 2150

LEFT PACK TEMP EICAS MESSAGE. REMOVED AND REPLACED LEFT PACK TEMP CONTROL VALVE IAW AMM 21-51-12. OPS AND LEAK CHECK GOOD.

ATA 2120

FWD EQUIP COOLING AUTO INOPERATIVE. REMOVED AND REPLACED THE MANIFOLD INTER CONNECTOR DUCT IAW AMM 21-58-13, OPS CHECKED GOOD

ATA 2150

EICAS FOR THE LT PACK TEMP. FOLLOWED QRH PROCEDURE IN FLT, PERFORMED A LT PACK TEMP CONTROLLER BITE TEST ON GROUND, NO FAULTS NOTED, OPS CHECKED NORMAL IAW FIM 21-51 FT 808, NO FAULTS, OPS CHECKED GOOD.

ATA 2150

LEFT A/C PACK MALFUNCTIONED. REMOVED AND REPLACED LEFT ACM TEMP CONTROL VALVE IAW AMM 21-51-12, OPS & LEAK CHECKED OK.

ATA 2150

WHEN LEFT PACK SELECTED OFF, LEFT PACK OFF LIGHT DOES NOT ILLUMINATE AND NO LEFT PACK OFF EICAS. ACCOMPLISHED FIM 21-51 F/T 844 AND BITE TEST. OPS CK NORMAL IAW AMM 21-51-00.

ATA 2150

LEFT PACK WHEN SELECTED OFF DOES NOT PRODUCE A PACK OFF LIGHT ON OVERHEAD PANEL OR LEFT PACK OFF EICAS MESSAGE FOR 3 MINUTES. PERFORM OPS CHECK OF LEFT PACK IAW AMM 21-51-00, SYSTEM OPERATES NORMALLY , CAN NOT DUPLICATE FAULT. OPS CHECKED GOOD.

ATA 2150

LEFT PACK WHEN SELECTED OFF DOES NOT PRODUCE A PACK OFF LIGHT ON OVER HEAD PANEL OR LT PACK EICAS MESSAGE. OPS CHECKED THE LT PACK IAW AMM 21-51-00, CANNOT REPRODUCE FAULT.

ATA 5310

DURING POST FLIGHT WALK AROUND INSPECTION, MX FOUND DAMAGE ON AFT FUSELAGE FWD OF APU AREA. REPAIRED IAW EO 6753A652, REVISION 1, PART 2.

ATA 2800

RT SPAR VALVE SWITCH ILLUMINATED. REMOVED AND REPLACED THE SWITCH, OPS CHECK GOOD IAW AMM 33-16-02. REPAIRED A BROKEN WIRE W456-0222-18 AT PIN 6 ON RIGHT SPAR VALVE IAW SWPM 20-10-15. OPS CHECKED GOOD IAW AMM 28-22-00.

ATA 5610

FLIGHT COMPARTMENT R3 WINDOW HAS SIGNS OF BUBBLES. REMOVED AND REPLACED R3 WINDOW IAW AMM 56-11-10.

ATA 2150

LEFT PACK WATER EXRTACTOR IS CLOGGED. REMOVED AND REPLACED THE WATER EXTRACTOR IAW AMM 21-51-04. OPS CHECKED NORMAL

ATA 2430

APU BATTERY CHARGER & BATTERY FAILED A VOLTAGE TEST. REMOVED AND REPLACED THE APU BATTERY CHARGER AND BATTERY IAW AMM 24-31-00, AND 24-31-04.

ATA 5610

FLIGHT COMPARTMENT WINDOW L3 HAS SIGNS OF BUBBLES. REMOVED AND REPLACED THE L3 WINDOW IAW AMM 56-11-10. OPS CHECKED HEAT CONTROL, TESTED NORMAL.

ATA 3610

NR 1 ENGINE FAN AIR VALVE FAILED TO TEST. REMOVED AND REPLACED THE FAN AIR VALVE IAW AMM 36-11-16. OPS CHECKED GOOD.

ATA 4900

APU FAULT WHILE STARTING ON TAXI IN . TWO ATTEMPTS, ON SECOND ATTEMPT NOTICED AN RPM OF 22.1 AND 770 EGT BEFORE SHUTDOWN BY FAULT. FOUND OIL QTY LOW. SERVICED IAW AMM 12-13-04, NO LEAKS NOTED. APU STARTED FIRST ATTEMPT. PERFORMED A BITE CHECK IAW FIM 49-11 F/T 987 NO FAULTS NOTED.

ATA 4900

APU FAULT DURING START. APU STARTED ON FIRST ATTEMPT, PERFORMED APU BITE IAW FIM 49-11-00, NO FAULTS NOTED , APU OPS CHECK GOOD I.A.W AMM 49-11-00.

ATA 2150

LEFT PACK NOT SHUTTING OFF WHEN SWITCH IN OFF POSITION. CYCLED THE RT AND LT PACKS, OPS CHECKED GOOD IAW AMM 21-33-00.

ATA 7320

L ENG EEC C1 STATUS MSG. REMOVED AND REPLACED LEFT ENGINE EEC IAW AMM 73-21-51, PERFORMED OPS CHECK IAW 71-00-00 OPS CHECK NORMAL AT THIS TIME. NO STATUS MESSAGE PRESENT. PERFORMED IDLE RUN IAW AMM 71-00-00. OPS CHECK NORMAL.

ATA 3620

LEFT BLD VALVE EICAS PRIOR TO ENGINE START. PERFORMED BITE PER FIM 36-10-827 NO FAULTS FOUND, EICAS MESSAGE CLEAR.

ATA 4940

APU AUTO SHUTDOWN. REMOVED AND REPLACED APU ECU AMM 49-61-05 PERFORMED APU BITE PROCEDURE IAW FIM 49-11 FT 987, PERFORMED ENGINE RUN ON APU POWER IAW AMM 71-00-00, NO FAULTS NOTED.

ATA 3610

NR 2 ENGINE PRV CONTROLLER, PNEUMATIC HEALTH CHECK FAILED. REMOVED AND REPLACED THE NR 2 ENGINE PRV CONTROLLER IAW AMM 36-11-19. OPS CHECKED NORMAL.

ATA 2120

UPON PUSHBACK & ENGINE START, HAD AN EICAS MESSAGE FOR THE FWD EQUIP VALVE. R & R THE RELAY K10718 IAW SWPM 20-81-22. EQUIPMENT COOLING OPS CHECKED NORMAL. NO MESSAGES.

ATA 4930

EVIDENCE OF OIL LEAK AT APU BY FUEL CONTROL UNIT ASSY COUPLING. REMOVED AND REPLACED THE PACKING AT THE APU FUEL CONTROL UNIT ASSY IAW AMM 49-31-01. LEAK CHECKED OK.

ATA 7510

RIGHT ENGINE ANTI-ICE LIGHT. REMOVED AND REPLACED THE RIGHT COWL ANTI -ICE VALVE IAW AMM 30-21-03. RAN THE NR 2 ENGINE ANTI-ICE VALVE, OPERATES GOOD.

ATA 3610

ON FINAL APPROACH AND TAXI IN AT IDLE RPM, LEFT ENGINE BLEED OFF MESSAGE. EXTINGUISHED AT HIGHER RPM. REMOVED AND REPLACED THE LT ENGINE HIGH PRESSURE CONTROLLER IAW IAW AMM 36-11-08. OPS CHECKED GOOD.

ATA 3110

RIGHT GENERATOR CONTROL OFF LIGHT INOPERATIVE. REMOVED AND REPLACED THE LAMP IAW AMM 33-13-00, OPS CHECKED GOOD.

ATA 7510

RT ENGINE ANTI ICE EICAS WITH SWITCH OFF AND VALVE LIGHT ON, SWITCH ON IN DESCENT, AFTER DESELECTING. OPS CHECKED IAW AMM 30-21-03-714-062, OPS CHECKED GOOD NO FURTHER DEFECTS NOTED.

ATA 3442

RADAR DOES NOT COME ON WITH INITIAL SELECTION OF SWITCHES, MUST BE CYCLED SEVERAL TIMES TO ENGAGE RADAR. CLEANED AND RE-SEATED THE WEATHER RADAR SWITCHES. RADAR OPS CHECKS OK IAW AMM 34-43-00.

ATA 4930

APU DUCT PRESSURE LOW. CYCLED NO HELP. REMOVED AND REPLACED THE APU FUEL CONTROL IAW 49-31-01 AND APU SURGE VALVE IAW 49-53-01.

ATA 4930

APU FUEL FILTER HAS BOLT MISSING AND LEAKING FUEL. REMOVED AND REPLACED APU SURGE VALVE AND FUEL CONTROL. OP CHECKED IAW 49-31-01.

ATA 3442

CAPTAINS EFIS PANEL WEATHER RADAR BUTTON IS JAMBED. REPAIRED THE BUTTON, OPS CHECKED NORMAL IAW AMM 34-43-00.

ATA 3442

CAPTAIN`S RADAR DOESN'T PAINT ANYTHING WHEN ON LT OR RT SYSTEM , FIRST OFFICER`S RADAR WORKS. PERFORMED AN OPERATIONAL CHECK IAW AMM 34-43-00, NO FAULTS NOTED AT THIS TIME.

ATA 4997

APU DIED WHILE RUNNING. FOUND PUSHED PIN ON CONNECTOR D492 FOR APU ALTN CTRL CB. REPAIRED AND OP GOOD IAW AMM 49-41-01 AND 49-31-04.

ATA 4920

APU FAULT, WOULD NOT START ON 2 ATTEMPTS. RPM WOULD NOT EXCEED 15 PERCENT.

ATA 2612

EICAS MESSAGE FOR FIRE OVERHEAT SYS JUST PRIOR TO LANDING. TROUBLESHOT IAW FIM 26-11 FT 804, NO DEFECTS NOTED.

ATA 2612

MN CARGO LOOP 1 STATUS MESSAGE.

ATA 2612

APU FIRE LOOP 1 STATUS MESSAGE. PERFORMED TROUBLESHOOTING OF THE APU FIRE LOOP 1 IAW FIM 26-15-803. INSULATION RESISTANCE TEST PASSED. RESET AFOLTS CARD M685 SYSTEM FUNCTIONED NORMAL. REMOVED AND REPLACED THE APU FIRE DETECTION CIRCUIT CARD IAW AMM 26-10-01, OPS CHECKED GOOD.

ATA 4920

UNABLE TO START APU. OPS CHECK APU IAW FIM 49-11-988, APU OPS CHECKED NORMAL. NO DEFECTS NOTED. START EGT MAX 778, STABLE AT 343 EGT. KVA MAX ELEC AIR LOAD, EGT STABILIZED AT 450 DEGREES.

ATA 7310

RIGHT ENGINE SPAR VALVE OPERATIONAL CHECK UNSUCCESSFUL. RT ENGINE SPAR VALVE INDICATION INOPERATIVE. PERFORMED CONFIRMATION OF OPERATION IAW DDG 28-40-02.

ATA 2611

STATUS MSG AFTER LANDING. MAIN CARGO LOOP 1. REMOVED SMOKE DETECTOR M12213 IAW AMM 26-14-01. OPS CHECK GOOD AND PLACARDS REMOVED.

ATA 4940

APU COLD SOAK START FAILED ON THREE ATTEMPTS. REMOVED AND REPLACED THE STARTER , GROUND TESTED OK IAW AMM 49-41-01.

ATA 4920

APU COLD SOAK START FAILED THREE ATTEMPTS AT FL 410 -49. CHECKED OIL QTY AND BITE CHECKED ECU AND OPS CHECKED ON GROUND IAW AMM 12-13-01, 49-01-05, AND 49-11-00.

ATA 5414

NR 1 ENGINE, LEFT CORE COWL FAIRING SKIN INTERIOR SURFACE FOUND WORN LOCATED AT UPPER AFT CUT-OUT SECTION. THE SKIN WAS REPAIRED IAW SRM 54-42-01-2R-5, REPAIR 5, FIG 202, DETAIL 3, REV 104.

ATA 5410

NR 1 ENGINE LEFT CORE COWL ATTACH STOP FOUND WORN. THE STOP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE LEFT CORE COWL INTERIOR SURFACE AFT UPPER SECTION RUB STRIP FOUND WORN. THE SECTION OF THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE RIGHT CORE COWL FAIRING FLIPPER DOOR SEAL FOUND DAMAGED. THE DOOR SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE RIGHT CORE COWL UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE LEFT CORE COWL FAIRING INTERIOR SURFACE MOST AFT ANGLE FOUND CRACKED. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE LEFT CORE COWL FAIRING AFT UPPER EDGE STRIP SEAL FOUND DAMAGED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE NOSE COWL AT THE 1 TO 3 O'CLOCK POSITIONS, FOUND THE RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE NOSE COWL AT THE 3 TO 5 O'CLOCK POSITIONS FOUND THE RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE NOSE COWL AT 6 O'CLOCK POSITION FOUND RUB STRIP WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE LT FAN COWL PRESSURE RELIEF DOOR ASSY FWD LANYARD SUPPORT BRACKET FOUND WORN. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5330

RIGHT AFT UPPER FUSELAGE APPROX BETWEEN BS 1197+22 TO 1197+44, APPROXIMATELY 3 INCHES ABOVE STRINGER 19R, FOUND A DENT. REPAIRED IAW SRM 53-00-01-2R-14, REPAIR 14, FIG 201, REV 104.

ATA 7110

NR 2 ENGINE LT CORE COWL ATTACH 5TH HAT FROM LOWER FOUND WORN. MOST AFT FRAME ATTACH WORN HAT (5TH FROM LOWER) REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.

ATA 7110

NR 1 ENGINE, LT CORE COWL EXTERIOR FWD SURFACE WEAR STRIP FOUND DAMAGED. WEAR STRIP REMOVED AND REPLACED AS PER SRM 51-40-02 REV 104.

ATA 5410

NR 2 ENGINE LEFT CORE COWL MOST AFT FRAME FOUND A CHAFED. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, RT CORE COWL INTERIOR AREA DATA SUPPORT PLATE ATACH RIVET FOUND SHEARED. THE RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5610

COCKPIT, CAPTAIN SIDE WINDSHIELD FOUND CRACKED. THE WINDSHIELD WAS REMOVED AND REPLACED IAW AMM 56-11-01, REV 121.

ATA 4900

FOUND APU CYCLE COUNTER INDICATOR LOOSE NEAR E6 IN THE AFT CARGO BAY. THE APU CYCLE COUNTER INDICATOR WAS REMOVED AND REPLACED IAW AMM 49-72 00, REV 121. CHECKED IAW AMM 49-72-00, REV 121.

ATA 2121

FWD CARGO BAY, AIR COOLING FAN AT BS 390, LT CLEVIS ATTACHMENT FOUND BROKEN. THE ATTACH BRACKET WAS REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.

ATA 2160

EICAS DISPLAY FOR LT PACK PRIMARY HX IN NO INDICATION. THE TEMP TRANSMITTER WAS REMOVED AND REPLACED IAW AMM 21-52-03, REV 121. OPS TESTED IAW AMM 21-52-03, REV 121.

ATA 3610

LEFT HPC BITE SWITCH FAULT DURING AIR SUPPLY MODULE BITE TEST. THE 1 ENGINE HPC WAS REMOVED AND REPLACED. AIR SUPPLY MODULE BITE TEST CARRIED OUT IAW AMM 36-11-08, REV 121. FOUND SATISFACTORY.

ATA 7700

NR 2 ENGINE PRSOV FOUND WITH BROKEN SENSE LINE. THESHUTOFF VALVE WAS REMOVED AND REPLACED IAW IAW AMM 36-11-09, REV 121.

ATA 2160

RIGHT PACK COMPRESSOR OUTLET TEMP 2 SENSOR (TS5135) FOUND CORRODED. THE TEMP SENSOR WAS REMOVED AND REPLACED IAW AMM 21-56-06, REV 121. OPS TESTED IAW AMM 21-56-06, REV 121.

ATA 2170

RIGHT AIR CON BAY WATER EXTRACTOR ASSY OTBD DUCT FOUND CRACKED. THE DUCT WAS REMOVED AND REPLACED IAW AMM 21-51-04, REV 121, AND INSTALLATION TEST AND LEAK CHECKED GOOD IAW AMM 21-51-04, REV 121.

ATA 2820

DC FUEL PUMP ON MESSAGE SHOWS ON EICAS DISPLAY. APU FUEL PRESSURE SWITCH REPLACED IAW AMM 28-25-03, REV 121, AND PRESSURE SWITCH OPERATION TESTED GOOD IAW AMM 28-25-03, REV 121.

ATA 5311

A CRACK WAS FOUND APPROX. 0.7 INCHES IN LENGTH, DURING HFEC INSPECTION AT BS 903.5 RBL 89, BELOW WL 200 FRAME. REPAIRED IAW EN1146-17 REV, SB767-53A0209, FIG 24, REV 02.AND EO 6753A038, REV 8.

ATA 2197

LEFT AIR CONDITIONER BAY HEAT EXCHANGER PRIMARY AND SECONDARY LOWER BRACKET BONDING JUMPERS FOUND FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.

ATA 2150

LEFT AIR CONDITIONER BAY AT ACM OUTLET DUCT SENSE LINE RUBBER SLEEVE FOUND LEAKING. REMOVED AND REPLACED THE SLEEVE IAW AMM 20-11-00, REV 121. LEAKED CHECKED IAW AMM 21-51-00 FOUND GOOD IAW REV 121.

ATA 2150

LEFT AIR CONDITIONER BAY FWD REHEATER SENSE LINE SUPPORT CLAMP RUBBER TORN. REMOVED AND REPLACED THE SUPPORT CLAMP IAW AMM 20-11-00, REV 121.

ATA 5297

LEFT AIR CONDITIONER BAY ACCESS DOOR 193NL FOUND THREE BONDING JUMPERS DAMAGED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-10-21, REV 121, AND RESISTANCE CHECK PERFORMED IAW SWPM 20-20-00, REV 64.

ATA 2150

RIGHT AIR CONDITIONER BAY FWD REHEATER SENSE LINE SUPPORT CLAMP FOUND RUBBER TORN. REMOVED AND REPLACED THE SENSE LINE SUPPORT CLAMP IAW AMM 20-11-00, REV 121.

ATA 2150

RIGHT AIR CONDITIONER BAY, AT ACM OUTLET DUCT SENSE LINE RUBBER SLEEVE FOUND LEAKING. REMOVED AND REPLACE SENSE LINE SLEEVE IAW AMM 20-11-00, REV 121. CARRIED OUT LEAK CHECK IAW AMM 21-51-00, FOUND GOOD IAW REV 121.

ATA 5297

RIGHT AIR CONDITIONING BAY ACCESS DOOR 194LR FOUND WITH TWO BONDING JUMPERS DAMAGED AND FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 20-10-21, REV 121, AND BONDING RESISTENCE CHECK PERFORMED IAW SWPM 20-20-00, REV 64.

ATA 3097

FOUND MAINTENANCE EICAS MESSAGES FOR THE NR 2 WINDOW HEAT. REPLACED THE NR 2 WINDOW HEAT WIRE CABLE IAW SWPM 20-10-11, REV 65, AND CARRIED OUT WINDOW OPERATIONAL TEST IAW AMM 56-11-02, REV 121.

ATA 2160

RIGHT PACK COMPRESSOR INLET TEMP BULB FOUND CORRODED. THE INLET TEMP BULB WAS REMOVED AND REPLACED IAW AMM.

ATA 2120

EICAS SHOWS A FWD EQUIPMENT COOL VALVE MESSAGE AND P5 EQUIPMENT COOLING PANEL SHOWS VALUE LIGHT WHEN AIRCRAFT IN AIR MODE. FOUND GROUND EQUIPMENT COOLING EXHAUST VALUE INTERNAL POSITION CIRCUIT NO GOOD. EQUIPMENT COOLING OVERBOARD EXHAUST VALUE REMOVED & REPLACED IAW AMM 21-58-05, REV 121 & TESTED IAW AMM 21-58-05, REV 121, FOUND SATISFACTORY.

ATA 2897

LEFT ENGINE SPAR VALVE BONDING JUMPER FRAYED. THE BONDING JUMPER WAS REMOVED AND REPLACED IAW AMM 20-11-00, REV 121.

ATA 2897

RIGHT WING REAR SPAR VALVE CONNECTOR (D1572) CRACKED. THE CONNECTOR WAS REMOVED AND REPLACED IAW SOPM 20-61-11, REV 64. OPS TEST PERFORMED IAW AMM 28-22-01, REV 121.

ATA 4997

TWO BONDING WIRES AT THE APU AIR INLET FLAP ACTUATOR FOUND WORN. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 49-15-06, REV 121.

ATA 4997

APU AIR INTAKE ACTUATOR FOUND WITH TWO BONDINGS FRAYED. THE BONDING JUMPERS WERE REMOVED AND REPLACED IAW AMM 49-15-06, REV 121.

ATA 5320

ROLLER TRAY SUPPORT AT BS 1197+44, RBL 8.5, FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-07, DETAIL VIII, FIG 101, ALLOWABLE DAMAGE 1, REV 104. THE SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, RT CORE COWL PRECOOLER DUCT LIP FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-06, REV 121. LATCH CHECK CARRIED OUT IAW AMM 71-11-07, REV 121. FOUND SATISFACTORY.

ATA 5310

ROLLER TRAY SUPPORT AT BS 1197, RBL 8.5 FOUND CORRODED. THE ROLLER TRAY SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, RT CORE COWL PRECOOLER DUCT LIP FOUND WORN. REMOVED AND REPLACED IAW AMM 71-11-06, REV 121. LATCH CHECK CARRIED OUT IAW AMM 71-11-07, REV 121, FOUND SATISFACTORY.

ATA 5230

BULK CARGO DOOR INTERNAL FRAME LOWER MID SECTION FOUND EDGE CHAFED. THE FRAME WAS REMOVED IAW SRM 51-40-02-0G-O, REV 104. FABRICATED A NEW FRAME IAW DWG 146T6322, REV A. THE NEW FRAME WAS INSTALLED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE NOSE COWL UPPER AREA FOUND WITH SEVERAL FASTENERS LOOSE. THE FASTENERS WERE TIGHTEN IAW AMM 20-11-00, REV 121.

ATA 5320

AFT CARGO BAY 5L PDU PAN FOUND CORRODED. THE CORROSION WAS REMOVED AND FOUND WITHIN LIMITS IAW SRM 53-00-07, DETAIL 2, FIG 101, ALLOWABLE DAMAGED 1, REV 104.

ATA 5420

NR 2 ENGINE, LT CORE COWL MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL ATTACH BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL FAIRING MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 1 ENGINE, RT CORE COWL EXTERIOR SURFACE FOUND WITH A SCRATCH. THE SCRATCH WAS SMOOTHENED AND FOUND WITHIN LIMIT AS IAW SRM 54-45-01-1A-1, FIG 101, DETAIL 2, REV 104.

ATA 5410

NR 1 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND WITH SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.

ATA 5420

NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD END SUPPORT BRACKET FOUND WORN. THE SUPPORT BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, LT CORE COWL EXTERIOR FWD SURFACE WEAR STRIP FOUND DAMAGED. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, LEFT CORE COWL FAIRING EXTERIOR SURFACE AFT SECTION FOUND RIVETS SHEARED. THE SHEARED RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, LT CORE COWL EXTERIOR SURFACE FOUND SCRATCHED. THE SCRATCH WAS SMOOTHED AND FOUND WITHIN LIMIT IAW SRM 54-42-01-1A-1, FIG 101, DETAIL 3, REV 104.

ATA 5410

NR 2 ENGINE, LEFT CORE COWL FLIPPER DOOR FOUND DAMAGED. THE DOOR WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 2 ENGINE, LEFT CORE COWL AFT UPPER EDGE STRIP SEAL FOUND WORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5413

NR 2 ENGINE, LT CORE COWL MOST AFT LONGERON FOUND CRACKED. THE LONGERON WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LEFT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACHING RIVET FOUND SHEARED. THE SHEARED RIVET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL MOST AFT HAT CHANNEL TWO EXISTING REPAIRS FOUND WORN. THE HAT CHANNEL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5410

NR 2 ENGINE, LT CORE COWL SECOND ZEE FRAME FROM FWD FOUND EXISTING REPAIR WORN. THE ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, RT CORE COWL FAIRING MOST FWD END BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.

ATA 5420

NR 1 ENGINE, RT CORE COWL FAIRING SKIN INTERIOR SURFACE FOUND WORN. ACCOMPLISHED A FAIRING SKIN REPAIR IAW SRM 54-45-01-2R-11, FIG 202, DETAIL 3, REV 104.

ATA 5420

NR 1 ENGINE, LT CORE COWL FAIRING INTERIOR SURFACE AFT UPPER SECTION OF RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 104.