N181DN

Part: WIRE HARNESS — FAULTED (FUEL SYSTEM) · airframe 132,808 hrs · 19,846 cycles

ATB, LT FUEL QTY INOP APPROX. ONE HOUR AFTER DEPARTURE. UNABLE TO CONTINUE ETOPS. FQIS BITE FAULTS LEG 0 LMTU CONTAMINATED, 601. R/ R LM TANK WIRE HARNESS AND TANK UNITS 1,3,5,6 IAW FIM 28-41 -815-847-004 AND AMM 28-41. RE-INSTALLED LT MAIN TANK ACCESS PANELS IAW AMM 28-11, NO LEAKS NOTED, ALL INDICATIONS NORMAL. C/W SFAR 88 AND ALL CDCCL'S FQPU OPS CK AND FQIS DENSITOMETER OPS TEST OK.

Part: PAWL — DAMAGED (ARMING LEVER) · airframe 132,689 hrs · 19,819 cycles

SHIP 181 R1 DOOR WOULD NOT ARM. R/R R1 DOOR ARMING LEVER PAWL IAW B767-300 AMM 52-11. (9164472)

Part: ACCESS DOOR — MISSING (RT NACELLE) · airframe 132,689 hrs · 19,819 cycles

SHIP 181 RT PYLON INBOARD SIDE NACELLE STRUT ACCESS DOOR MISSING. CORRECTIVE ACTION: REPLACED ACCESS DOOR ASSY REF B767-300 IPC 54-53-01-01 (9164456)

Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 132,655 hrs · 19,809 cycles

RETURNED TO ATL DUE TO RIGHT ENGINE COMPRESSOR STALL DURING CLIMB. T/S RIGHT ENGINE STALL IAW FIM, FAILED VSV SYNCHRONIZING RING INSPECTION. REPLACED NR 2 ENGINE.

Part: NONE — NONE · airframe 132,292 hrs · 19,728 cycles

SHIP 181 R1 DOOR HARD TO ARM, CORRECTIVE ACTION: RESET HANDLE ON R1 DOOR OPS OK PER B767-300 CH 52-11. (9096354)

Part: NONE — NONE · airframe 132,108 hrs · 19,700 cycles

SHIP 181 1R DOOR EXTREMELY HARD TO CLOSE. TOOK A PILOT AND FLIGHT ATTENDANT TO CLOSE AND ARM IN HNL. REPEAT WRITE UP. CORRECTIVE ACTION: OPS CHECKED 1R DOOR AND SLIDE ARMING. CHECKED COUNTERBALANCE AND CRUSH CARTRIDGE. ALL GOOD PER B767 AMM 52-11-00. DOOR OPERATED WITH NORMAL RESISTANCE. (9096535)

Part: NONE — NONE · airframe 132,096 hrs · 19,698 cycles

SHIP 181 2L DOOR WILL NOT ARM, CORRECTIVE ACTION: CLEARED DEBRIS OK FOR SVC (9096530)

Part: NONE — NONE · airframe 131,938 hrs · 19,672 cycles

SHIP 181 -ATB/IFSD- LEFT ENGINE SHUTDOWN DUE TO OIL LOSS, ABNORMAL OIL TEMPERATURE, LOW OIL PRESSURE AND VIBRATION. CORRECTIVE ACTION: C/W ENGINE VISUAL INSPECTION, FOUND #3 SCAVENGE OIL LINE RUPTURED. METAL WAS ALSO FOUND ON MASTER MCD, #3 MCD, #4 MCD, AND OIL FILTER. METAL PARTICLES IN TAIL PIPE, ENGINE CHANGE REQUIRED. MAINTENANCE IN PROGRESS. (9087334)

Part: NONE — NONE · airframe 131,926 hrs · 19,670 cycles

SHIP 181 -ATB/IFSD- LEFT ENGINE SHUTDOWN DUE TO OIL LOSS, ABNORMAL OIL TEMPERATURE, LOW OIL PRESSURE AND VIBRATION. CORRECTIVE ACTION: C/W ENGINE VISUAL INSPECTION, FOUND #3 SCAVENGE OIL LINE RUPTURED. METAL WAS ALSO FOUND ON MASTER MCD, #3 MCD, #4 MCD, AND OIL FILTER. METAL PARTICLES IN TAIL PIPE, ENGINE CHANGE REQUIRED. MAINTENANCE IN PROGRESS. (A007693)

Part: SQUIB — FAILED INSP · airframe 131,431 hrs · 19,591 cycles

AIRCRAFT 0181, DURING SVC CHECK, TEST 2 SPOILER SQUIB WILL NOT TEST. CORRECTIVE ACTION: REPLACED OVERWING ESCAPE SYSTEM K4 RELAY SPOILER SQUIB. (9305431)

Part: NONE — NONE · airframe 131,427 hrs · 19,590 cycles

AIRCRAFT 181, RT OFF WING ESCAPE SLIDE INFALTION CYLINDER DAMAGED. CORRECTIVE ACTION: REPLACED RIGHT OFF WING SIDE CYLINDER. (9305411, 2336458)

Part: NONE — NONE · airframe 131,427 hrs · 19,590 cycles

AIRCRAFT 0181, SUPPLEMENTAL INFORMATION. R1 DOOR SHOWING OPEN ON EICAS AFTER BEING CLOSED. CORRECTIVE ACTION: DEFERRED PER MEL 52-71-01-REPLACED PSEU. (2324298)

Part: NONE — NONE · airframe 131,361 hrs · 19,573 cycles

SHIP 181 DURING SVCCK EMER ESCAPE L SYS 2 SQUIB TEST INOP. LAMP CHECKS GOOD, CORRECTIVE ACTION: SQUIB TEST PANEL OPS NML PER B767 AMM 26-21. (8907343)

Part: NONE — NONE · airframe 131,346 hrs · 19,571 cycles

SHIP 0181 -FCNT- DURING CRUISE MULTIPLE POTABLE WATER DRAINS FLOODED. THE AUTOPILOT DISCONNECTED AND WOULD NOT RE-ENGAGE WITH FRICTION IN LATERAL CONTROL. A/C DESCENDED, LATERAL CONTROL RETURNED TO NORMAL. A/C CONTINUED AT LOWER ALTITUDE. CORRECTIVE ACTION: DRAIN MAST HEATER CIRCUIT BREAKERS FOUND OPEN. FOUND AIR LEAK AT WHEELWELL FWD BULKHEAD AREA. REPAIR LEAK PER B767 AMM 05-51-24. LEAK CHECK GOOD. (8907312)

Part: NONE — NONE · airframe 131,351 hrs · 19,572 cycles

SHIP 181 1R DOOR WILL NOT ARM, CORRECTIVE ACTION: CYCLED DOOR- 1R DOOR ARMS NML. (8907340)

Part: COVER — DAMAGED · airframe 131,196 hrs · 19,545 cycles

SHIP 181 L2 DOOR SLIDE LIGHT COVER/ASSEMBLY HAS COME OFF/DAMAGED. CORRECTIVE ACTION: RESECURED L2 DOOR SLIDE LIGHT ASSY AS NECESSARY. OK FOR SVC. (8502394)

Part: DOOR — DIRTY · airframe 131,146 hrs · 19,535 cycles

SHIP 181 R1 DOOR WOULD NOT SHOW CLOSED AND WOULD NOT ARM, CORRECTIVE ACTION: REMOVED DEBRIS FROM 1R DOOR PER B767-300 AMM 52-12 OPS CHECK GOOD. (8502346)

Part: INDICATOR — INOPERATIVE · airframe 130,899 hrs · 19,498 cycles

SHIP 181 2L DOOR WILL NOT ARM, CORRECTIVE ACTION: DOOR CAN BE MECHANICALLY ARMED. SLIDE ARMED LIGHT & NUCKER BUSTER INOP. FWD TO MEL 52-11-01 (8666858) SUPPLEMENTAL INFOMATION' SHIP 181 2L DOOR WILL NOT ARM, CORRECTIVE ACTION: R/R DOOR 2L SLIDE ARM IND LIGHT AS PER B767 AMM 52-73. A/C OK FOR SVC (8666858)

Part: INDICATOR — INOPERATIVE · airframe 130,806 hrs · 19,483 cycles

SHIP 181 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:607, CORRECTIVE ACTION: R/R DOOR ARMED FLAG AT LOC 607 PER B767-300 AMM 52-11. ALL OPS CK NML. (2225885)

Part: NONE — NONE · airframe 130,230 hrs · 19,335 cycles

SHIP 181 DTE ER/A 590247-14 REPAIR APPROVAL LIMITED TO 37,500 FLIGHT CYCLES ONLY. CORRECTIVE ACTION: ADDITIONAL ENGINEERING AUTHORIZATION IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. (2117937)

Part: NONE — NONE · airframe 130,025 hrs · 19,275 cycles

SHIP 181 01EA DENT FOUND ON THE LH H/STAB LOWER SURFACE FROM H/ STAB MOVEABLE SEAL DOOR 2" , FROM AUX SPAR 42". CORRECTIVE ACTION: PUNCTURE REPAIRED ON THE LH H/STAB LOWER SURFACE AS PER B767-300 PRI 596384. (2075647)

Part: NONE — NONE · airframe 130,025 hrs · 19,275 cycles

SHIP 181 FOUND LHW OB SLAT NO.2 UPR SUFACE BULGE FORM OB EDGE 10 INCHES. CORRECTIVE ACTION: LHW OB SLAT NO.2 UPR SUFACE FORM OB EDGE 10 INCHES REPAIRED: AS PER B767-300 SRM 51-70. (2067730)

Part: NONE — NONE · airframe 130,025 hrs · 19,275 cycles

SHIP 181 RHW NO.7 SLAT LEADING EDGE 01 EA DENT FORM I/B EDGE 88 INCH. CORRECTIVE ACTION: DENT AREA REPAIRED AND REPAIR PARTS MADE FORM ALCLAD SHT 7075T6- 0.063" AND ALCLAD SHT 7075T6-0.071" AS PER B767-300 SRM 57-43 (2066762)

Part: NONE — NONE · airframe 129,919 hrs · 19,239 cycles

SHIP 181 COCKPIT EMERGENCY LIGHT COVER AND BASE CAME OFF ON TAKEOFF. CORRECTIVE ACTION: REPLACED COCKPIT EMERGENCY ASSY IN REF TO 767 AMM 33-51 OPS CHECK NORMAL. (8154910)

Part: NONE — NONE · airframe 129,431 hrs · 19,127 cycles

SHIP 181 DOOR 2 RIGHT EXIT COVER DIFFUSER LENS IS MISSING. CORRECTIVE ACTION: EXIT COVER IS STILL ATTACHED. NO TROUBLE FOUND. (8070320)

Part: SENSOR — OUT OF ADJUST (THRUST REVERSER) · airframe 128,485 hrs · 18,923 cycles

SHIP 181 -ATO LT AMBER THRUST REVERSER INDICATION DISPLAYED DURING TAKEOFF ROLL. CORRECTIVE ACTION: ADJUSTED OUTBOARD TR HALF AUTO STOW SENSOR, REPLACED OUTBOARD ACTUATOR FOUND WIRE 206R-18 FROM D4192J PIN 12 TO D4214P PIN 26 SHORTED TO GROUND AND REPAIRED WIRE. A/C IS RTS

Part: PROXIMITY SWITCH — FAILED (PAX DOOR) · airframe 128,065 hrs · 18,826 cycles

SHIP 181 ENTRY DOOR LIGHT ON. CORRECTIVE ACTION REPLACED S195 L FWD ENTRY DOOR LOCK PROX SWITCH. (LP 7283418)

Part: FRAME — DAMAGED (BS 390 S24-25L) · airframe 127,792 hrs · 18,759 cycles

SHIP 181 - DURING INSPECTION MAINTENANCE FOUND FRAME 390 DAMAGED BETWEEN SR 24L AND 25L. REPAIRED PER SRM 53-00-07. (LP 1765156)

Part: EEC — FAULTED (LT ENGINE) · airframe 127,523 hrs · 18,711 cycles

DUE TO AUTO-THROTTLE INOPERATIVE ALONG WITH VNAV DATA ISSUES AND SPEED RESTRICTED. CORRECTIVE ACTION: FOUND LEFT ENGINE EEC FAULT, REPLACED LEFT ENGINE EEC AND FMC PER B767AMM. DURING OPERATIONAL CHECK, FOUND LEFT ENGINE CHANNEL A BLANK. PIMU FAULTS CHANNEL A DATA BUS INOPERATIVE. RESEATED ALL LEFT ENGINE FIREWALL AND EEC CANNON PLUGS, OPERATIONAL CHECKS COMPLIED WITH NO FAULTS NOTED. TAT PROBE WAS REPLACED AS PRECAUTION. SYSTEM OPERATION IS NORMAL.

Part: IDG — FAILED (NR 2) · airframe 125,915 hrs · 18,306 cycles

SHIP 181 - ATO - AT 15KTS DUE TO #2 ENGINE DID NOT ACCELERATE ABOVE IDLE WHEN THROTTLES ADVANCED. CORRECTIVE ACTION: MAINTENANCE REPORTED NO ENGINE RELATED FAULTS ON EICAS, EEC, PIMU AND WHEN #2 IDG DISCONNECTED ENGINE IMMEDIATELY SPOOLED UP TO NORMAL IDLE SPEED AND NORMAL OPERATION THEREAFTER. A/C DISPATCHED WITH IDG INOPERATIVE PER MEL 24-00-01. #2 IDG REPLACED. SYSTEM OPERATION IS NORMAL.

Part: MODULE — MISWIRED (EMERGENCY LIGHTS) · airframe 125,692 hrs · 18,264 cycles

DURING SERVICE CHECK, FOUND LLCC MODULE EMERGENCY LIGHTS ARE INOPERATIVE. FOUND R2-7007 MISWIRED, REWIRED AND THE SYSTEM OPS GOOD.

Part: WIRE — BROKEN (CREW REST) · airframe 125,654 hrs · 18,250 cycles

AFT CREW REST LADDER EXIT LIGHT INOPERATIVE. FOUND R2-7007 MISWIRED AND REWIRED, FOUND BROKEN WIRE AT R003 AND RETERMINATED. SYSTEM OPERATION IS GOOD.

Part: SKIN — CRACKED (LT WING) · airframe 125,615 hrs · 18,245 cycles

DURING HFEC ON LHW LWR WING SKIN AT RIB 30 WSTA 962.2 STR L-9.5 FOUND #66 FASTENER HOLE WITH 02 CRACK INDICATION AT 12 O'CLOCK & 6 O'CLOCK POSITION LOOKING UP VIEW FWD WITH APPROX LENGTH 0.65" AND 0.6" RESPECTIVELY AS MARKED. C/W ERA 584147-14. (LP 1431686)

Part: SKIN — CRACKED (LT WING) · airframe 125,592 hrs · 18,240 cycles

CRACK INDICATION FOUND OPEN HOLE INSPECTION AT LHW LOWER WING SKIN AT STR-9.5 HOLE NO 64. C/W ERA 584147-14 (LP 1431678)

Part: BATTERY PACK — NOT REPORTED (EMERGENCY LIGHTS) · airframe 125,389 hrs · 18,213 cycles

AIRCRAFT DUE EMERGENCY LIGHTS POWER SUPPLY BATTERY REPLACEMENT. REPLACED 18 EMERGENCY LIGHTS POWER SUPPLY BATTERIES. SYSTEM OPERATION IS NORMAL.

Part: SHROUD — DAMAGED (CABIN) · airframe 124,627 hrs · 18,102 cycles

DURING CRV, EMERGENCY LIGHT SHROUD DAMAGED AT SEAT 25B AND 26B. REPLACED SEAT MOUNTED EMERGENCY LIGHT SHROUD. SYSTEM OPERATION IS NORMAL. (LP 1278637)

Part: CONTROL MODULE — MALFUNCTIONED (LAVATORY) · airframe 122,885 hrs · 17,874 cycles

SHIP 0181 - DIV - TO DTW DUE TO MULTIPLE LAVS INOP. CORRECTIVE ACTION: MTC REPLACED THE LOGIC CONTROL MODULE (LCM), POINT LEVEL SENSORS (2 EACH) AND WIRING HARNESS ROBBED FROM A SPARE WASTE TANK ASSEMBLY. VACUUM WASTE SYSTEM DUCTING AND CONNECTIONS INSPECTED. SYSTEM OPS VERIFIED IN GROUND AND PRESSURIZED MODES. AIRCRAFT IS RTS.

Part: ACCESS PANEL — MISSING (LT PYLON) · airframe 121,906 hrs · 17,734 cycles

LEFT ENGINE OUTBOARD PYLON STRUT ACCESS PANEL MISSING. INSTALLED NEW PANEL.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 121,205 hrs · 17,631 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHTS INOPERATIVE. FOUND M738 POWER SUPPLY BAD. REPLACED BATTERY PACK AND POWER SUPPLY. SYSTEM OPERATION IS GOOD.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 118,767 hrs · 17,300 cycles

EMERGENCY LIGHTS AT ROW 19 AB ARE INOPERATIVE. MAINTENANCE FOUND A TERMINAL CONNECTOR LOOSE AND SECURED.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 118,750 hrs · 17,298 cycles

FOUND THREE OUTSIDE EMERGENCY LIGHTS INOPERATIVE AT THE AFT LEFT FUSELAGE AND AFT LEFT ENTRY DOOR LOCATIONS. REPLACED M739 EMERGENCY LIGHT CHARGER AND BATTERY PACK ASSEMBLE. SYSTEM OPS NORMAL.

Part: SERVO — LEAKING (YAW DAMPNER) · airframe 117,266 hrs · 17,085 cycles

DIVERTED DUE TO THE LT HYD SYSTEM QUANTITY DECREASING. REPLACED RT YAW DAMP SERVO AND SERVICED THE LT HYD SYSTEM. ACFT RETURNED TO SERVICE.

Part: SKIN — CORRODED (BS 1582) · airframe 117,559 hrs · 17,123 cycles

FUSELAGE SKIN, BS 1582, STRINGER 25L CORRODED. C/W ERA 555656-14.

Part: SKIN — CORRODED (ACCESS DOOR) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 EMP CONTROL BAY ACCESS DOOR INNER SKIN FOUND CORROSION AND REPLACED PER SRM 51-40-02.

Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,185 hrs · 17,073 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON CANTED DESK ON STA 955. LBL15. C/W ERA 563602-14AD.

Part: SPAR WEB — CORRODED (WING) · airframe 117,185 hrs · 17,073 cycles

CORROSION LEVEL: 2 CORROSION WAS FOUND ON THE WING CTR SECTION REAR SPAR WEB UNDER THE RT SIDE FRAME FITTING ON THE FS 955 BULKHEAD. C/W ERA 563342-14.

Part: FRAME — CORRODED (BS 1809) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 INTERIOR STRUCTURE AFT CHORD FOUND CORROSION AT STA 1809 BETWEEN S-39L AND S-39R OUT OF LIMITS AND REPLACED CHORD.

Part: SHEAR TIE — CORRODED (BS 1502) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1502 , BETWEEN S-39L AND S-38L REPLACED PER 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1197+110 , BETWEEN S-39L AND S-39R. REPLACED PER SRM 51-40-02. (LP 0336671)

Part: SKIN — DELAMINATED (SLAT) · airframe 117,020 hrs · 17,043 cycles

#10 SLAT UPPER SURFACE AT I/B AFT CORNER FOUND DELAMINATION AND REPAIRED PER SRM 51-70-10

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 COOROSION FOUND ON SHEAR TIE ,STA1197+110,S-13R-S-14R. REPLACED PER SRM 51-40-02

Part: SHEAR TIE — CORRODED (BS 742) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 742 BETWEEN S-37R AND S-36R AND REPLACED PER SRM 51-40-02. (LP 0336717)

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA 1197+22, BETWEEN S-39L AND S-38R. REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA 1197+44 , BETWEEN S-39L AND S-38R AND REPLACED PER SRM 51-40-02. (LP 0336676)

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1197+110 , BETWEEN S-38R AND S-37R AND REPLACED PER SRM 51-40-02. / (LP 0336593)

Part: FAIRING — COKED (NR 1 NACELLE) · airframe 117,020 hrs · 17,043 cycles

#1 NACELLE AFT FAIRING I/B EXTERIOR SURFACE FOUND COKING. EVALUATED AND REPAIRED #1 NACELLE AFT FAIRING I/B EXTERIOR SURFACE COKING PER SRM 51-70-10

Part: PANEL — DETACHED (FAIRING) · airframe 117,020 hrs · 17,043 cycles

L/N NACLLE STRUT FAIRING I/B UPPER PANEL FOUND DISENGAGE. REPAIRED PER SRM 51-70-10.

Part: SHEAR TIE — CORRODED (BS 1087) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 COOROSION FOUND ON SHEAR TIE ,STA1087 S-16R-S-17R. REPLACED PER SRM 51-40-02. (LP 0336831)

Part: SHEAR TIE — CORRODED (1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 02EA SHEAR TIE CORROSION AT STA 1197 , BETWEEN S-39L AND S-38R. REPLACED PER SRM 51-40-02.

Part: FAIRING — COKED (NR 2 NACELLE) · airframe 117,020 hrs · 17,043 cycles

#2 NACELLE AFT FAIRING I/B EXTERIOR SURFACE FOUND COKING. EVALUATED AND REPAIRED #2 NACELLE AFT FAIRING I/B EXTERIOR SURFACE COKING.

Part: SHEAR TIE — CORRODED (BS 1285) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA 1285 , BETWEEN S-38L AND S-38R REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA 1197+88, BETWEEN S-39L AND S-37R. REPLACED SRM 51-40-02. (LP 0336616)

Part: SHEAR TIE — CORRODED (BS 1439) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1439 , BETWEEN S-39R AND S-39. REPLACED PER SRM 51-40-02. (LP 0336667)

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+88 , BETWEEN S-38L AND S-37L REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1351) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 COOROSION FOUND ON SHEAR TIE ,S-16L-S-17L,STA1351 AND REPLACED PER SRM 51-40-02. LP 0336820)

Part: SHEAR TIE — CORRODED (BS 1241) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 08EA SHEAR TIE CORROSION AT STA 1241 , BETWEEN S-33L AND S-38R AND REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1329) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 05EA SHEAR TIE CORROSION AT STA 1329 , BETWEEN S-39R AND S-35L REPLACED PER SRM 51-40-02.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 117,185 hrs · 17,073 cycles

DURING H CK AT STAG, CORROSION WAS NOTED ON THE CENTER WING TANK REAR SPAR UPPER CHORD AND PRESSURE DECK ANGLE, STA 955, LBL 15. C/W ERA 563602-14.

Part: SHEAR TIE — CORRODED (BS 1219) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 10 EA SHEAR TIE CORROSION AT STA 1219. BETWEEN S-36L AND S-34R. REPLACED PER SRM 51-40-02. (LP0335289)

Part: FUEL TANK — CORRODED (CENTER) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 CENTER TANK UPPER SKIN FOUND CORROSION AT STA 955 RBL 80 TO RBL 82 C/W ERA 563598-14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

HFEC INSPECTION FOUND 01EA CRACK ON RT 859.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AND REPAIRED.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, CORROSION FOUND ON FRAME OUTER FLANGE, STA1241, S-16L C/W ERA 563638-14.

Part: FRAME — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

HFEC INSPECTION FOUND 01EA CRACK ON RT 903.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS AND REPAIRED.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 742 BETWEEN S-38R AND S-37R. REPLACED PER SRM 51-40-02.

Part: SKIN — CORRODED (BS 1087-1109) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND SKIN CORROSION BETWEEN STA 1087 AND STA 1109. UNDER STRINGER. C/W ERA 563670-14. (LP 0330277)

Part: SHEAR TIE — CORRODED (BS 1351) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA1351. BETWEEN S-39L AND S-36L AND REPLACED. (LP 0335146)

Part: FITTING — CRACKED (RT WING) · airframe 117,020 hrs · 17,043 cycles

INSPECTION FOUND 01EA CRACK ON RH WING LOWER UNDERWING LONGERON FITTING. REPLACED UNDERWIND LONGERON FILLTING

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, SEAT TRACK -CORROSION FOUND ON SEAT TRACK RBL 88.5 AROUND STA1428 AND STA1443 FOUND OUT OF LIMITS. C/W ERA 563530-14.

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

THE HOLE ON FLOORBEAM ELONGATED AT STA 1324 RBL 88.5. THE ELONGATED HOLE ON FLOORBEAM AT STA 1324 RBL88.5 REPAIRED PER ERA 563564-14.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, CORROSION FOUND ON SEAT TRACK RBL88.5 AROUND STA 753 AND STA 1098. REPAIRED PER SRM 53-00-52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, SEAT TRACK CORROSION FOUND ON SEAT TRACK LBL 88.5 AROUND STA1362 AND STA 1444. REPLACED PER SRM 51-40-02 AND ERA 563530-14.

Part: SHEAR TIE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, AFT CARGO COMPARTMENT FOUND 07 EA SHEAR TIE CORROSION AT STA 1307. BETWEEN S-39R AND S-33L AND REPLACED.

Part: BRACKET — BROKEN (EVAC SLIDE) · airframe 117,020 hrs · 17,043 cycles

ALL ATTACHED BRACKETS FOR LOWER HOLDING STICK OF LT OFF WING EVACUATION SLIDE FOUND BROKEN. LEFT OFF WING EVACUATION SILDE PACK REPLACED. SYSTEM OPERATION IS NORMAL.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON FRAME OUTER CHORD STA1307 S-20R TO S-19R. FOUND OUT OF LIMITS AND REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, AFT CARGO COMPARTMENT FOUND 07 EA SHEAR TIE CORROSION AT STA 1197+66 BETWEEN S-37L AND S-35R. REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, FWD CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 764 BETWEEN S-37R AND S-36R REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+66. BETWEEN S-36L AND S-35L. REPLACED PER SRM 51-40-02. (LP0335169)

Part: SHEAR TIE — CORRODED (BS 742) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 FWD CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA 742 BETWEEN S-36R AND S-35R AND REPLACED PER SRM 51-40-02. (LP 0335402)

Part: FRAME SPLICE — CORRODED (BS 1502) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA FRAME SPLICE SURFACE CORROSION AT STA 1502. BETWEEN S-25R AND S-26R. REPLACED PER SRM 51-40-02. (LP 0330165)

Part: SKIN — CRACKED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

INSPECTION FOUND 04EA CRACKS ON THE FUSELAGE SKIN AT FS 1197+99 VHF ANTENNA MOUNTING. CRACKED SKIN REPAIRED PER SRM 53-00-01.

Part: SHEAR TIE — CORRODED (BS 1518) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1518. BETWEEN S-39L AND S-39R. CORRODED SHEAR TIE REPLACED PER SRM 51-40-02. (LP 0335198)

Part: SHEAR TIE — CORRODED (BS 1241) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 03 EA SHEAR TIE CORROSION AT STA 1241. BETWEEN S-37R AND S-34R AND REPLACED PER SRM 51-40-02

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2AFT CARGO COMPARTMENT FOUND 02 EA SHEAR TIE CORROSION AT STA 1197+132. BETWEEN S-37L AND S-35L AND OUT OF LIMITS. REPLACED PER SRM 51-40-02. (LP 0330149)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, AFT CARGO COMPARTMENT FOUND 02 EA SHEAR TIE CORROSION AT STA 1263 BETWEEN S-39L AND S-37. REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 04EA SHEAR TIE CORROSION AT STA 1197+132. BETWEEN S-38L AND S-37R ANDREPLACED PER SRM 51-40-02. (LP 0336813)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, BULK CARGO COMPARTMENT FOUND 03EA SHEAR TIE CORROSION AT STA1540 BETWEEN S-38L AND S-38R. REPLACED PER SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1417) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 BULK CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA 1417. BETWEEN S-39R AND S-39L AND REPLACED PER SRM 51-40-02. (0335141)

Part: SHEAR TIE — CORRODED (BS 1285) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1285. BETWEEN S-37L AND S-36L AND REPLACED. (LP 0335149)

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2, BULK CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA 1562 BETWEEN S-38L AN D S-38R. REPLACED PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 SEAT TRACK - CORROSION FOUND ON SEAT TRACK RBL 88.5 AROUND STA 1098 AND STA 1208 AND OUT OF LIMITS. REPAIRED PER SRM 53-00-52.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2, CORROSION FOUND ON FRAME WEB, AROUND STA 1329 S-17R OUT OF LIMITS REPAIRED PER SRM 53-00-07 AND 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 CORROSION FOUND ON SEAT TRACK LBL88.5, AROUND STA1230 AND STA1362 FOUND OUT OF LIMITS AND REPLACED.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 SEAT TRACK - CORROSION FOUND ON SEAT TRACK RBL88.5 AROUND STA1208 AND STA1428 OUT OF LIMITS. REPLACED PER SRM 51-40-02.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

EXTRA FASTENER HOLE FOUND ON SEAT TRACK LBL 11, STA1480 FOUND CORRODED AND REPAIRED PER SRM 53-00-52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL: 2 SEAT TRACK-CORROSION FOUND ON SEAT TRACK LBL88.5 AROUND STA 1098 AND STA 1230 FOUND OUT OF LIMITS AND REPAIRED PER SRM 53-00-52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2 CORROSION FOUND ON SEAT TRACK RBL11 AROUND STA1362 AND STA1517 OUT OF LIMITS. REPAIRED PER SRM 53-00-52.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 117,020 hrs · 17,043 cycles

CORROSION LEVEL 2 SEAT TRACK. CORROSION FOUND ON SEAT TRACK RBL11 AROUND STA654+44 AND STA782 OUT OF LIMITS REPAIRED PER SRM 53-00-52.

Part: OUTLET — DEFECTIVE (CABIN) · airframe 116,271 hrs · 16,923 cycles

FLIGHT ATTENDANT REPORTED BURNING RUBBER SMELL BY ROWS 17 AND 18 BOTH LEFT AND RIGHT SIDE OF AIRCRAFT. SMELL DISSIPATED IN APPROXIMATELY 15 MINUTES. CHECK ROWS 15-19 FOUND BAD OUTLET POWER AND OUTLET REPLACED. SYSTEM OPERATION IS NORMAL

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 116,091 hrs · 16,895 cycles

DURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT SEATS 38 GF, 40A, AND 41A INOPERATIVE. REPAIRED THE SEAT CONNECTOR AT 38EF. SYSTEM OPERATION IS NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 114,408 hrs · 16,635 cycles

EMERGENCY LIGHTS AT SEAT 1A, 2A, AND 3A ARE INOPERATIVE. MAINTENANCE FOUND M9008 F1 FUSE INOPERATIVE. REPLACED THE POWER PACK. SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 114,332 hrs · 16,621 cycles

EXTERIOR EMERGENCY LIGHTS RIGHT SIDE OVERWING OUT. REPLACED THE LAMP AND CHECKED OK.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 114,340 hrs · 16,623 cycles

SEAT 21 THRU 31 EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED BATTERY CHARGER AND BATTERY AT STA 1400.

Part: SKIN — CRACKED (BS 1582) · airframe 113,948 hrs · 16,560 cycles

FOUND A SKIN CRACKED DUE TO CORROSION AT BS 1582 & STRINGER 25L. CUT THE CORROSION FROM FUSELAGE SKIN LAYER. PERFORMED DVI INTERNAL, COMPLIED WITH ERA 555656-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 112,344 hrs · 16,308 cycles

ON PDC, FOUND L EMERGENCY ESCAPE LEFT ON TEST 1 INTERMITTENT. REPLACED BATTERY POWER SUPPLY M961. SYSTEM OPERATION IS NORMAL.

Part: SKIN — CRACKED (NACELLE) · airframe 108,766 hrs · 15,785 cycles

PYLON SIDE SKIN CRACKED AT ACCESS PANEL 436BL CUTOUT. REPAIRED IAW SRM 54-53-01, REPAIR 7.

Part: FRAME — CRACKED (BS 883) · airframe 108,991 hrs · 15,816 cycles

FRAME INNER CHORD IS CRACKED IN TRANSITION RADIUS FS 883.5, RBL 89 BELOW WL 200, MKD. C/W REPAIR.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 107,916 hrs · 15,662 cycles

EMERGENCY LIGHTS AT SEAT 36F ARE INOPERATIVE. MAINTENANCE CONNECTED THE CONNECTOR. SYSTEM OPS NORMAL.

Part: SKIN — DAMAGED (BS 730) · airframe 104,203 hrs · 15,147 cycles

LIGHTNING STRIKE, BS 730 STRINGER 5L. DRILLED OUT DAMAGE IAW SRM 53-00-01. REPAIR 8.

Part: SKIN — DAMAGED (BS 654) · airframe 104,203 hrs · 15,147 cycles

LIGHTNING STRIKE, BS 654+121 STRINGER 6L. DRILLED OUT DAMAGE IAW SRM 53-00-01.

Part: SKIN — DAMAGED (BS 818) · airframe 104,203 hrs · 15,147 cycles

LIGHTNING STRIKE BS 818 STRINGER 5L. DRILLED OUT DAMAGE IAW SRM 53-00-01 REPAIR 8.

Part: SKIN — DAMAGED (BS 830) · airframe 104,203 hrs · 15,147 cycles

LIGHTNING STRIKE BS 830 AT STRINGER 5L. DRILLED OUT DAMAGE IAW SRM 53-00-01, REPAIR 8.

Part: SKIN — DAMAGED (BS 654) · airframe 99,687 hrs · 14,502 cycles

FUSELAGE SKIN BS 654+88 TO 654+110, S-39R, FWD ATG 4 ANTENNA DAMAGED. COMPLIED WITH ERA 521275-14.

Part: SKIN — DAMAGED (BS 654) · airframe 99,687 hrs · 14,502 cycles

FUSELAGE SKIN BS 654+88 TO 654+110, S39R, FWD ATG 4 ANTENNA DAMAGED. COMPLIED WITH ERA 521275-14.

Part: SKIN — NICKED (BS 1197) · airframe 99,687 hrs · 14,502 cycles

SMALL NICK IN FUSELAGE SKIN AT BS 1197, STRINGER 39R. BLENDED NICK AND RESTORED FINISH, OK FOR SERVICE IAW SRM 53-00-01.

Part: FITTING — MISINSTALLED (LT WING) · airframe 99,656 hrs · 14,492 cycles

LEFT WING, UNDERWING LONGERON FITTING HOLES SHORT EDGE MARGIN. REPAIRED IAW ERA 520536-14AD.

Part: FLOORBEAM — CRACKED (BS 1502) · airframe 99,656 hrs · 14,492 cycles

BS 1502 LBL 28 FLOORBEAM WEB FOUND CRACKED. REPAIRED IAW ERA 520028-14.

Part: FLOORBEAM — CRACKED (BS 1502) · airframe 99,656 hrs · 14,492 cycles

BS 1502, LBL 28.85, FLOORBEAM WEB CRACKED. REPAIRED IAW ERA520028-14.

Part: SKIN — PUNCTURED (RT WING TE FLAP) · airframe 99,656 hrs · 14,492 cycles

RT WING I/B AFT FLAP LOWER SURFACE FOUND PUNCTURED. METAL HOT BOND REPAIR CARRIED OUT IAW SRM 57-53-01.

Part: SKIN — DENTED (BS 698) · airframe 99,656 hrs · 14,492 cycles

BS 698 S39L TWO DENTS IN SKIN. REPAIRED IAW ERA 520024-14.

Part: SEAT TRACK — CORRODED (BS 733-1098) · corrosion level 2 · airframe 99,656 hrs · 14,492 cycles

MAIN DECK BS 733 TO 1098 SEAT TRACK CROWN & LIP CORRODED. REPAIRED PER SRM 53-00-52.

Part: FLOORBEAM — CORRODED (BS 325) · airframe 99,656 hrs · 14,492 cycles

BS 325 RBL 20-55 FLOORBEAM UPPER SURFACE CORRODED. REPAIRED PER SRM 53-00-51. (LP 1186655)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 99,455 hrs · 14,464 cycles

EMERGENCY LIGHTS FROM ROW 32 AND AFT BOTH SIDES ARE INOPERATIVE. MX REPLACED THE BATTERY PACK. SYSTEM OPS NORMAL.

Part: SKIN — DAMAGED · airframe 117,020 hrs · 17,043 cycles

LIGHTNING STRIKE DAMAGE ON LEFT FUSELAGE SKIN RIVET HEADS AT STA 144.5/S-24, STA 168.5/S-25 STA 203.5/S-27.5, AND STA 228/S-23 REMOVED FASTENERS. C/W TEMP REPAIR PER B767-300 SRM 53-00-01 REPAIR 8 SECTION II STEP 4. REQUIRES CAT C REPAIR INSP PER TABLE II. DVI EVERY 1500 CYCLES AND PERM REPAIR BY 6000 CYCLES PERMANENT REPAIR FINISHED AS PER B767-300 SRM 53-00-01 REPAIR 8 .CLOSED LOG AND REMOVED MONITOR INSP

Part: CONTROL PANEL — INTERMITTENT (ESCAPE SLIDE) · airframe 96,794 hrs · 14,126 cycles

DURING PDC FOUND LT EMERGENCY ESCAPE SQUIB LIGHT INTERMITENT IN TEST 1. REPLACED SQUIB TEST PANEL.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 96,336 hrs · 14,066 cycles

NR 2 PYLON MID SPAR WEB CRACKED.

Part: VALVE — INOPERATIVE (FWD CARGO HEAT) · airframe 95,371 hrs · 13,921 cycles

RETURNED TO DEPARTURE DUE TO FWD CARGO OVERHEAT MESSAGE. REPLACED FWD CARGO HEAT VALVE IAW AMM LEAK CHECKED GOOD.

Part: SKIN — CRACKED (RT WING) · airframe 93,119 hrs · 13,643 cycles

RT AFT PITCH LOAD FITTING, INBD FORWARD HOLE FOUND CRACKED AT WING SKIN. REPAIRED AS PER ERA 501560-14AD REV ORG.

Part: FRAME — CRACKED (FS 1809 S5R) · airframe 93,119 hrs · 13,643 cycles

FS 1809.5 STR 5R FWD OUTER CHORD CRACKED APROX 7/8 INCH LENGTH. CUTOUT THE CRACK AREA AND REPAIRED AS PER B767-300 SRM 53-80-08 REPAIR 9, FIGURE 201, CAT B REPAIR.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON FWD UPPER SPAR WEB BOTH DRAIN HOLE AND EXISTING SLOT HOLE FOUND CRACKED. REPAIRED PER ERA 502700-14AD REV 1.

Part: BOLT — MISINSTALLED (NR 12 SLAT) · airframe 93,119 hrs · 13,643 cycles

RIGHT WING NR 12 SLAT INBOARD MAIN TRACK DOWNSTOP ASSY AFT BOLT FOUND NOT PROTRUDING. NR 11 SLAT OTBD MAIN TRACK DOWNSTOP ATT BOLT FOUND NOT PROTRUDING, AND NR 10 SLAT OTBD MAIN TRACK ATT BOLT FOUND NOT PROTRUDING. DOWNSTOP ASSY ATT BOLT AND NUT REPLACED AS PER EA-01-469704AD ME22 OPN 2201 CARDS E1760, E1763, AND E1766.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON FWD UPPER SPAR WEB ARAE ONE FASTENER HOLE CRACKED AT WEB ON RT SIDE JUST FWD OF PREVIOUS REPAIR SLOT AREA AND REPAIRED PER ERA 502700-14AD REV 1.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON FWD UPPER SPAR WEB BOTH DRAIN HOLE AND EXISTING SLOT HOLE AREA FOUND CRACKED AND REPAIRED PER ERA 502700-14AD REV 1.

Part: SPAR — CRACKED (NR 1 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 1 PYLON FWD UPPER SPAR WEB LT DRAIN HOLE EXISTING SLOT HOLE AREA FOUND CRACKED AND ACCOMPLISHED ERA 502699-14AD.

Part: SKIN — CRACKED (RT WING) · airframe 93,119 hrs · 13,643 cycles

RT WING AFT PITCH LOAD FITTING I/B FWD HOLE IS CRACKED AT THE WING SKIN. WORKING FROM A PRI.

Part: FITTING — DAMAGED (LT PYLON) · airframe 93,119 hrs · 13,643 cycles

LEFT WING PYLON AFT PITCH LOAD BACKUP FITTING O/B BOLT HOLE HAS SHORT EDGE MARGIN. WORKING FROM PRI.

Part: HINGE FITTING — CRACKED (TE FLAP) · airframe 93,119 hrs · 13,643 cycles

RT WING I/B AFT FLAP FWD HINGE ARM IS CRACKED AND REPAIRED PER B767-300 SRM 57-53-02 FIG 201 REPAIR 1.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON STRUT MID SPAR WEB LT AFT CUTOUT IS CRACKED. WORKING FROM PRI.

Part: SKIN — CORRODED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FUSELAGE SKIN AT FS 1197 - 1197+44 AT STR 36L IS CORRODED AND REPAIRED PER B767-300 SRM 53-00-01 REPAIR 12 FIG 201.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 93,119 hrs · 13,643 cycles

LT WING I/B MAIN FLAP O/B L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-05 PAR 5A(1) FIG 5.

Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

CABIN FLOORBEAM AT FS 1518 LBL 26 - LBL 40 UPPER FLANGE IS CRACKED AND REPAIRED PER B767-300 SRM 53-00-01 REPAIR 1 FIG 201.

Part: FAIRING — DAMAGED (LT HORIZ STAB) · airframe 93,119 hrs · 13,643 cycles

LT HORIZONTAL STAB L/E FAIRING 332CL HAS CORE DAMAGE AND IS REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 3.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FUSELAGE SKIN AT FS 1543 BL 0 HAS A LIGHTNING STRIKE. WORKING FROM PRI.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 93,119 hrs · 13,643 cycles

LT WING I/B AFT FLAP LWR SURFACE IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 201 SHT 1.

Part: WEDGE — DEFORMED (LE SLAT) · airframe 93,119 hrs · 13,643 cycles

NR 5 SLAT T/E WEDGE I/B EDGE IS DEFORMED AND REPAIRED PER B767-300 SRM 57-43-02 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 3.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 93,119 hrs · 13,643 cycles

LT WING O/B FLAP MID L/E FAIRING IS DELAMINATED AND REPAIRED PER B767-300 SRM 57-53-01 REPAIR 1 TABLE 1 AND 51-70-03 PAR 5A(1) FIG 5.

Part: FAIRING — DAMAGED (LT HORIZ STAB) · airframe 93,119 hrs · 13,643 cycles

LT HORIZONTAL STAB L/E FAIRING 332DL HAS CORE DAMAGE AND IS REPAIRED PER B767-300 SRM 55-10-01 REPAIR 1 FIG 201 AND 51-70-10 REPAIR 4 FIG 202 SHT 3.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON STRUT FWD UPPER SPAR FITTING AFT BUSHING IS MIGRATED AND REPLACED PER B767-300 SRM 54-53-90 FIG 201 REPAIR 2.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 2 PYLON STRUT LWR SPAR FITTING ATTACH BUSHING IS MIGRATED AND REPLACED PER B767-300 SRM 54-53-90 FIG 201 REPAIR 4.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 93,119 hrs · 13,643 cycles

NR 1 PYLON STRUT FWD UPPER SPAR FITTING AFT BUSHING IS MIGRATED AND REPLACED PER B767-300 SRM 54-53-90 FIG 201 REPAIR 2.

Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FS 1809.5 FWD UPPER CHORD AT STR 5R IS CRACKED AND BEING REPAIRED PER B767-300 SRM 53-80-08 REPAIR 9 FIG 201.

Part: STRAP — CRACKED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FS 955 RT REAR SPAR BULKHEAD HAS A FASTENER HOLE CRACKED AT THE FAILSAFE STRAP, WORKING FROM PRI.

Part: FITTING — CRACKED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FS 955 RT REAR SPAR BLKHD HAS A FASTENER HOLE CRACKED IN THE "T" FITTING AT THE FAILSAFE STRAP, WORKING FROM PRI.

Part: STRAP — CRACKED (FUSELAGE) · airframe 93,119 hrs · 13,643 cycles

FS 955 LT REAR SPAR BLKHD HAS A FASTENER HOLE CRACKED AT THE FAILSAFE STRAP, WORKING FROM A PRI.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 91,396 hrs · 13,389 cycles

LIGHTNING STRIKE AT STA 1543 BL 0. REPAIRED PER ERA 497575-14. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,376 hrs · 13,246 cycles

EMERGENCY PATH LIGHTS AT ROWS 6FG - 20FG ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND POWER SUPPLY M9011AND WIRE HARNESS AT SEAT 19FG. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,532 hrs · 12,879 cycles

EMERGENCY EXIT LIGHT OVERHEAD OF COCKPIT DOOR IS INOPERATIVE. MX REPLACED THE LIGHT ASSY. SYS OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,741 hrs · 12,769 cycles

EMERGENCY LIGHTS SEAT 31AB AND 31FG ARE INOPERATIVE. MX REPLACED THE BATTERY PACK. SYS OPERATION IS NORMAL.

Part: LIGHT — ODOR (READING) · airframe 86,292 hrs · 12,714 cycles

IN FLIGHT, THE READING LIGHTS IN COACH CABIN AB STARTED FLICKERING AND A BURNING ODOR FOLLOWED. THE ROTARY SWITCH ON F/A PANEL DID NOT KILL THE POWER. MX UNLATCHED PASS SERVE POWER SWITCH ON THE L1 DOOR OF THE F/A PANEL WHICH KILLED THE POWER TO THE AFFECTED LIGHT AND THE ODOR DISSIPATED. MX THEN RAN CABIN LIGHTS FOR 2 HOURS AFTER RESETTING THE CIRCUIT BREAKER. SYS OPS IS NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 85,930 hrs · 12,666 cycles

EMERGENCY LIGHTS AT 25GF ARE INOPERATIVE. MX FOUND A CONNECTOR BROKEN AND REPLACED THE CONNECTOR AND FUSE AT THE BATTERY PACK. SYS OPS ARE NORMAL.

Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 85,930 hrs · 12,666 cycles

EMERGENCY LIGHTS AT 25GF ARE INOPERATIVE. MX FOUND A CONNECTOR BROKEN AND REPLACED THE CONNECTOR AND FUSE AT THE BATTERY PACK. SYS OPS ARE NORMAL.

Part: GENERATOR — MALFUNCTIONED (LEFT) · airframe 82,999 hrs · 12,220 cycles

LEFT GENERATOR FELL OFF LINE - RTB MX IN PROGRESS. BITE CHECKED BPCU/ FAULT LT GEN. GCU CODE 54 AP-720614. INSPECTED WIRE AST P37 PNL AND IDG. RT & LT GCU BPCU IAW AMM. RAN ENG PLACED LOAD ON GEN OPS CHK NORMAL. VOLTS FREQS OK. ACFT OK FOR SERVICE. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: OXYGEN BOTTLE — LOW PRESSURE (CREW O2) · airframe 81,512 hrs · 12,020 cycles

CREW O2 NEEDS SERVICING. REMOVED AND REPLACED CREW O2 BOTTLE IAW AMM 12-15-08, LEAK CHECK GOOD. CHECKED ALL MASKS, CHECK GOOD.

Part: PITOT HEAD — WARNING LIGHT (LEFT) · airframe 78,293 hrs · 11,616 cycles

CAPTS PITOT HEAT LIGHT ILLUMINATED AFTER PUSHBACK. REMOVED AND REPLACED CAPTS PITOT PROBE.

Part: SHUTOFF VALVE — FAULTED (NR 1 ENGINE) · airframe 78,158 hrs · 11,599 cycles

LEFT ENG ANTI-ICE AFTER TAXI. FOUND HPSOV AT FAULT. FWD TO MEL.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 78,143 hrs · 11,597 cycles

AFTER LEVEL OFF AT FL 364 THE LEFT ENGINE SPOOLED BACK ON ITS OWN FOLLOWED BY NUMEROUS EEC AND ENGINE OUT MESSAGES. T/S PER FIM INSPECTION FUEL SAMPLES PLUS NR 1 ENG FUEL FILTER FOR CONTAMINATION. FILTER PLUS FUEL SAMPLE FOUND CLEAN C/W ENG FU SUCTION FEED OPS TEST PER M/M. NR 1 ENG OPS NORMAL. REMOVED PLUS INSPECTION L FWD PLUS AFT BOOST PUMPS. CHKS NORMAL. INST BOOST PUMPS PER M/M. REPLACED N1 ENG FUEL PUMP PLUS FMU PER M/M.

Part: NOZZLE — FAILED (GEARBOX) · airframe 78,098 hrs · 11,592 cycles

NR 1 ENG FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12. C/W EA 51-470869-12 FOUND CONTAMINATES IN BOTH NOZZLES. REQUIRES ENG CHG. REPLACED NR 1 ENG PER R/C TRANSMITTAL 23-.

Part: NOZZLE — FAILED (NR 1 ENGINE) · airframe 78,098 hrs · 11,592 cycles

FAILED INSPECTION OF MAIN GEARBOX OIL NOZZLES PER EA-51470869-12 ON NR 1 ENGINE.

Part: SWITCH — FAILED (EMERGENCY LIGHTS) · airframe 77,514 hrs · 11,526 cycles

EMERGENCY LIGHTS WILL NOT TURN OFF. REPLACED EMERGENCY LIGHT PANEL DAL P/N 331702405.

Part: CHARGER — CORRODED (EMERGENCY LIGHTS) · airframe 69,688 hrs · 10,569 cycles

ALL 4 OVERWING EMERGENCY EXIT SIGNS WOULD ONLY ILLUMINATE FOR 15-30 SECONDS BEFORE TURNING OFF WHEN THE COCKPIT EMERGENCY LIGHT SWITCH WAS PLACED TO ON. REPLACED THE BATTERY PACK, NO HELP. REPLACED THE POWER SUPPLY/CHARGER AND THE SYSTEM OPERATED NORMAL, MFG P/N OF CHARGER WAS 2012-1, DPN 333780101, S/N OFF28335.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 69,587 hrs · 10,557 cycles

CAPT ALTIMETER FAILED AT 35780 FT. REMOVED AND REPLACED CAPT ALTIMETER PER AMM. TESTS OK. NO FLAGS.

Part: PUMP — UNSERVICEABLE (FUEL SYSTEM) · airframe 67,315 hrs · 10,286 cycles

DURING TAXI OUT CREW REPORTED CENTER FUEL READING 2200 LBS LOW AND RT MAIN APPROX 1900 LBS HIGH. ITEM HAS 1 PREV WRITE UP RETURNING TO GATE FOR MTC INSP. REF ITEM 7 THIS LOG REPLACED BOTH RT MAIN TANK BOOST PUMPS MOTIVE CHECK VALVE AND DISCHARGE CHECK VALVE. REMOVED AND REPLACED BOTH RT TANK BOOST PUMPS AS WELL AS MOT CHECK VALVE AND DISCHARGE CHECK VALVE. VERIFIED CONTINUOUS PUMP OPERATION AND NO FURTHER FUEL MIGRATION OR TRANSFER.

Part: CIRCUIT BREAKER — TRIPPED (BOOST PUMP) · airframe 66,291 hrs · 10,161 cycles

LEFT FWD FUEL PRESS LIGHT ILLUMINATED AFTER START OF RT ENG. FOUND BOOST PUMP C/B POPPED LWR P6. RETURNED TO GATE. RESET C/B. OPERATED PUMP FOR ABOUT 1/2HR. SYSTEM OPS NORMAL. NO MSG/NO LIGHT.

Part: ENGINE — CRACKED (NR 1 ENG) · airframe 66,057 hrs · 10,131 cycles

FAILED BORO_TFR CRACKS NR 1 ENG REPLACED IAW 1T148, ETOPS CATEGORY (F): ANY OTHER EVENT DETRIMENTAL TO ETOPS.

Part: FRAME — CRACKED (BS 903) · airframe 66,051 hrs · 10,128 cycles

THE LT FRAME IS CRACKED AT BS 903.5. A REPAIR ANGLE WAS INSTALLED.

Part: ODOR — DETECTED (CABIN) · airframe 66,013 hrs · 10,120 cycles

RETURNED TO CDG DUE TO F/A'S REPORTING STRONG BURNING ODOR OBSERVED THROUGHOUT ACFT BUT WAS STRONGEST IN MID CABIN. MADE OVERWEIGHT LANDING 370K POUNDS. TOUCHDOWN AT LESS THAN 100 FPM DESCENT RATE. SMOOTH LANDING. INSPECTED CABIN, AIR SYSTEM, ENGINES, NO TROUBLE NOTED. PERFORMED IDLE AND HIGH POWER RUNS, COULD NOT DUPLICATE. DUE TO TEMP CONTROL VALVE MCO, BORROWING TEMP VALVE AND CONTROLLER. REPLACED SAME.

Part: VALVE — FAILED (NR 2 ENGINE) · airframe 65,863 hrs · 10,102 cycles

TAKEOFF ABORTED AT 80 KNOTS DUE TO RT ENG PRV CAUTION WITH A RIGHT ENG BLEED LIGHT. BRAKE TEMPS RANGE FROM A 3 TO A 7 ON RIGHT REAR BRAKE ASSY. FWD TO MCO AND PLACARD PER MEL M36-11-02. PERFORMED BITE CHECK OF BLEED AIR MODULE. NO FAULTS. LOCKED OUT RT ENG HPSOV PER MEL 36-11-02. PERFORMED INSPECTION OF WHEELS AND BRAKES NO PROBLEMS FOUND. REPLACED HPSOV

Part: CONTROLLER — FAILED (LT ENGINE) · airframe 64,743 hrs · 9,958 cycles

LEFT ENGINE PNEUMATIC SUPPLY PULSES TO 0 PSI ON THROTTLE RETARD THEN CATCHES UP. PRESSURIZATION OK BUT PULSES ALSO. REPLACED LT ENG HP S/O VLV PER MM. REPLACED HP CONTROLLER. NDS CK OUT. NO HELP. REPLACED LT ENG BLEED AIR CARD AND PRV CONTROLLER PER MM. CKS NORMAL. REMOVED MCO/PLAC.

Part: CHARGER — UNKNOWN (CABIN) · airframe 64,242 hrs · 9,886 cycles

MID CABIN SEAT EMERGENCY LIGHTS FROM SEAT ROW 6-20 FG. REPLACED POWER SUPPLY.

Part: COFFEEMAKER — BURNED (AFT GALLEY) · airframe 62,726 hrs · 9,686 cycles

ELECTRICAL ODOR WAS DETECTED INFLIGHT AROUND THE AFT GALLEY AREA ON THE COPILOTS SIDE OF THE AIRCRAFT. F/A'S PULLED CB'S FOR THE 2 COFFEEMAKERS ON THAT SIDE AND ODOR WENT AWAY CB'S LEFT OUT FOR REMAINDER OF THE FLIGHT. UPON ARRIVAL FOUND ALL CB'S IN/RESET. FOUND NO WATER AT BOTH COFFEEMAKERS ON RT SIDE AFT GALLEY, BLED AIR FROM LINES, BREWED SEVERAL POTS AND ALL CKS GOOD. INSPECTED COMPTS, CHILLER AND OVENS.

Part: SLIDE — UNSERVICEABLE (R1 DOOR) · airframe 61,574 hrs · 9,532 cycles

INADVERTENT SLIDE DEPLOYMENT AT R1 DOOR BY MTC PERSONNEL. DEPLOYMENT SUCCESSFUL.

Part: COMBUST CHAMBER — CRACKED (NR 2 ENGINE) · airframe 58,231 hrs · 9,033 cycles

ENGINE FAILED BORO OP 5067 COMBUSTION CHAMBER LINER CRACKED. REPLACED ENGINE.

Part: ENGINE — STALLED (NR 2) · airframe 55,469 hrs · 8,628 cycles

NR 2 ENG STALLED ON TAKEOFF ROLL 110 KNOTS, RT ENG SURGE DET ON EICAS ENG EXCT RECORD 660 FOR 12 SEC. REPLACED NR 2 ENG S/N 723843 PER TRANS 1T149.

Part: POWER SUPPLY — INOPERATIVE (ROWS 1-6) · airframe 53,722 hrs · 8,358 cycles

ON LAYOVER FOUND EMERGENCY TRACK LIGHTING INOP ON SEATS 1-6. REPLACED LIGHT POWER SUPPLY.

Part: CDU — INOPERATIVE (COCKPIT) · airframe 51,570 hrs · 8,019 cycles

LEFT FMC CDU DISPLAY INOP. REPLACED CAPT. CDU. CONFIRMED BLOWER OK. 10 MINS AFTER REPLACEMENT CAPT CDU BLANKED OUT. INSTALLED ORIGINAL CDU. CYCLED C.B. E8 SEVERAL TIMES CDU RECOVERED AND REMAINED ACTIVE. FWD TO MCO/PLAC PRECAUTIONARY. 2.5 AMP C.B. LISTED IF REQUIRED.

Part: COOLER — DEFECTIVE (NR 1 ENGINE) · airframe 46,782 hrs · 7,173 cycles

ON CLIMB REPORTED ENG OIL TEMP HIGH. CONFIRMED NOT A INDICATION PROBLEM. MTC IN WORK. OIL FILTER/CHIP DETECTOR CLEAN. NO EEC FAULTS. T/S PER FIM NO FAULTS. REPLACED AIR/OIL COOLER AND VALVE. ALSO REPLACED FUEL/OIL COOLER BY PASS VALVE.

Part: SMOKE DETECTOR — INOPERATIVE (CARGO BAY) · airframe 46,034 hrs · 7,028 cycles

FWD CARGO DET 2 STATUS MSG RELAMP, NO HELP. REPLACED DETECTOR OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 44,479 hrs · 6,769 cycles

EMERGENCY LIGHT ESCAPE PATH INOP AT SEAT 22F AND 32B. TROUBLE SHOT SYSTEM FOUND BOTH ROWS FROM 30 AFT INOP. ISOLATED MALFUNCTION TO SEAT 32B. SEAT 22F WAS RELAMPED, NO HELP SO SEAT 32B AND 22F WERE TRANSFERRED TO MCO. PER MEL 33- 51-03D.

Part: CIRCUIT BOARD — FAULTY (E/E BAY) · airframe 43,104 hrs · 6,561 cycles

REJECTED T/O DUE TO AUDIBLE WARNING WITH NO OTHER INDICATION. GW 361.3, NO TR''S USED, USED RTO AUTO BRAKES, WIND 350/14KTS. GND SPEED 110KTS. DUE TO HISTORY OF AURAL WARNINGS GOING OFF W/ NO OTHER INDICATIONS CHANGED THE M1000 CARD FOR AURAL WARNING AND CHIME. ALSO CHANGED THE WARNING ELEC POWER SUPPLY M621 MODULE B AND AS A PRECAUTION CHANGED DUCT LEAK AND WHEEL WELL FIRE CONT M691. OPS CHECK NORMAL PER MM.

Part: ENGINE — FAILED (NR 2) · airframe 42,704 hrs · 6,499 cycles

COMPRESSOR STALL ON RIGHT ENGINE AT 31000FT. STALL WAS FELT BY FLIGHT CREW. CONTINUED TO ATL FOR RIGHT ENGINE CHANGE. SMALL AMOUNTS OF METAL FOUND IN TAILPIPE.

Part: UNKNOWN — ODOR (GALLEY) · airframe 40,257 hrs · 6,106 cycles

ACFT RTB WITH BURNING ELECTRICAL INSULATION SMELL. MTC FOUND ODOR EMANATING FROM MID AUX GALLEY. PULLED ALL CB FOR GALLEY. FWD TO MCO.

Part: WIRE — CHAFED (NR 1 ENGINE)

PER MSU - RECORD WIRE REPAIRED ON INSPECTION OF LT ENG EEC CONTROL WIRES. FOUND 3 WIRES WITH CHAFE ON INSULATION. NO LEGIBLE WIRE NR FOUND. REPAIRED WIRES PER CHAP 20 OF BOEING WIRING MANUAL FWD TO MCO. NO WIRES DAMAGED ONLY INSULATION.

Part: VALVE — LEAKING (BRAKE SYSTEM)

ACFT RETURNED TO BLOCKS, RT HYD SYS FAILURE. MTC FOUND RT BRAKE METERING VALVE LEAKING. REPLACED METERING VALVE, OPS CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERGENCY LIGHT AT CROSSOVER AISLE L1 L2 DOORS INOP. REPLACED BATTERY PACK.

Part: SPAR WEB — CRACKED (NR 1 PYLON)

PYLON NR 1 ENGINE NACELLE STRUT, AFT UPPER SPAR WEB FS 222, LBL4, CRACK REPAIR. A .75 INCH LONG CRACK WAS FOUND EMANATING FROM THE AFT, OUTBD CORNER OF A CUTOUT IN THE AFT UPPER SPAR WEB OF THE NR 1 ENGINE NACELLE STRUT AT FS 222, LBL4. THE CRACK WAS ROUTED OUT AND A STEEL DOUBLER REPAIR WAS INSTALLED AROUND THE CORNER OF THE CUTOUT PER ER/A 365126-14, REV B.

Part: BRAKE — BURNED (NR 4)

A/C ARRIVED GATE WITH NR 4 BRAKE ON FIRE. EXTINGUISHED FIRE COOLED BRAKE AND REPLACED BRAKE AND WHEEL ASSY PER M/M. REPLACED WHEEL AND BRAKE, SYSTEM NORMAL.

Part: EGT INDICATION — HIGH (NR 1 ENGINE)

LT ENGINE EGT EXCEEDED MAX CONTINOUS EGT IN CLIMB. EGT REACHED 626 DEG, THRUST LEVER WAS PULLED BACK MANUALLY TO PREVENT EGT GOING HIGHER. EGT WAS 60 TO 80 DEG HIGHER THAN RT ENG FOR SAME EPR SETTING. NO SURGE OR STALL INDICATED ON ENGINE EXCEEDANCE PAGE. NO PIMU BITE FAULTS. ENGINE OK FOR SERVICE PER FIM 71-05-00, FIG 108.

Part: COFFEEMAKER — FAILED (AFT GALLEY)

AFT GALLEY ELECTRICAL SMELL REPORTED BY FLIGHT ATTENDANT. REPLACED COFFEEMAKER.

Part: WINDOW — AIR LEAK (LT COCKPIT)

VERY LOUD SQUEAL WHEN CLIMBING THRU FL320, COULD NOT STOP. STOPPED ON IT'S OWN DESCENDING THRU 14,000 WITH CABIN AT SEA LEVEL AND DIFF = 6.0. RETURNED TO JFK. REPLACED L2 WINDOW, PRESSURE AND LEAK CHECKED GOOD.

Part: FAN — FAILED (FWD CARGO COMPT)

AFTER TAKEOFF 1.5 HOURS INTO FLIGHT, SMELLED ELECTRICAL FUMES IN COCKPIT ACCOMPANIED BY FWD EQUIPMENT EXHAUST FAN STATUS MESSAGE ON EICAS. CALLED FLIGHT CONTROL AND MTC COORDINATOR TO DISCUSS SITUATION AND DECIDED TO PULL P-22 CB. FUMES DISSIPATED AND FLIGHT WAS CONTINUED. UPON FURTHER INVESTIGATION FOUND THE FWD EXH EQUIP COOL FAN C/B ON P-6 PANEL POPPED. REPLACED FWD EQUIPMENT EXHAUST FAN, SYSTEM CHECKS NORMAL.

Part: PANE — CRACKED (CABIN)

DURING INSPECTION, FOUND CABIN WINDOW OUTER PANE CRACKED, AT SEAT ROW LOCTION LEFT SIDE 27A. REPLACED WINDOW PER MM.

Part: ENGINE — FAILED (NR 1)

FOUND METAL ON CHIP DETECTORS AND OIL SCREEN. REPLACED ENGINE, ROUTED TO SHOP.

Part: EEL ASSY — LOOSE (CABIN)

EMERGENCY TRACK LIGHT LOOSE RT SIDE, RT AFT LAV. REPLACED TRACK LIGHT ASSY, OPS CKS OK.

Part: CONTROL PANEL — FAILED (INSTR PNL LIGHTS)

ON DESCENT HAD A STRONG SMOKE ODOR IN FWD CABIN AND FLT DECK. UTILITY BUSES OFF. SMOKE ODOR DIMINISHED QUICKLY. FOUND SMOKE ODOR COMING FROM FLIGHT DECK INSTRUMENT LIGHT CONTROL PANEL. REPLACED PANEL OPERATION NORMAL.

Part: SKIN — DAMAGED (RT TE FLAP)

DURING LETTER CHECK INSP. FOUND AREA OF DAMAGE ON LOWER SURFACE OF T/E FORE FLAP MARKED IN LINE WITH NR 8 TIRE, RT WING. INSTALLED PERMANENT REPAIR PER SRM 57-53-01 FIG 201.