N178DN

Part: PUMP — FAULTED (FUEL SYS) · airframe 144,177 hrs · 21,179 cycles

DIVERTED TO SLC DUE TO LEFT ENGINE NOT RESPONDING TO THROTTLE COMMANDS. REPLACED LEFT FUEL PUMP, FUEL METERING UNIT, EEC AND FLOW CONTROL VALVE. OPS CHECK NORMAL.(7622729)

Part: IRU — FAULTED (ZONE 200) · airframe 143,664 hrs · 21,089 cycles

DIVERSION TO MSP DUE TO F/O ADI DISPLAY ISSUES. R & R IRU. OPS NORMAL.

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 141,339 hrs · 20,625 cycles

SHIP 178 UPPER L4 DOOR EMERGENCY EXIT SIGN DOES NOT ILLUMINATE. CORRECTIVE ACTION: REPLACED M1210 EMEY LTS POWER SUPPLY PER B767 AMM 33-51 ALL CKS GOOD (6931787)

Part: HEATER — ODOR (AFT DOOR) · airframe 140,771 hrs · 20,515 cycles

SHIP 178 FUME EVENT AT 37000 FT DURING CRUISE. AFT GALLEY BURNING RUBBER SMELL. CORRECTIVE ACTION: T/S PER SSM 21-45-05. R/R B470 RT AFT DOOR AREA HEATER PER B767- 300 AMM 21-23. OK FOR SVC. (6393838)

Part: WARNING MESSAGE — ILLUMINATED (STAB TRIM) · airframe 140,012 hrs · 20,372 cycles

SHIP 0178 -ATO- IN KEF @ APPROX. 65 KNOTS DUE TO UNSCHLD STAB TRIM MESSAGE. CORRECTIVE ACTION: CONTRACT MTC C/W FIM TASKS. C/W HIGH ENERGY STOP INSPECTION. A/C RTS (5706690)

Part: FRAME — CRACKED (NOT REPORTED) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 UPPER AFT FASTENER HOLE FOUND CRACK, CORRECTIVE ACTION: REPAIRED PER PRI 617880-14AD (0343375)

Part: UNKNOWN — CRACKED (BS 1810 S12AR) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 ER/A 617880-14AD ISSUED FOR CRACKS ON THE OUTER CHORD AT STA 1809.5 AND S-12A RH. CORRECTIVE ACTION: ACCOMPLISH ER/A 617880-14AD SECTION II WITHIN 36 MONTHS OR 6,000FC WHICHEVER OCCURS FIRST FOLLOWING THE ACCOMPLISHMENT OF SECTION I AND EVERY 36 MONTHS OR 6,000FC WHICHEVER OCCURS FIRST THEREAFTER. (0342924)

Part: SPRING — INOPERATIVE (L1 GAS SPRING) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 FWD LEFT ENTRY DOOR, INTERIOR SIDE GREEN BAR ASSEMBLY-GAS STRUT DOESN'T HOLD BAR UP. REMOVED AND REPLACED GAS SPRING REF B767 AMM 25-66-03 (0335131)

Part: SKIN — DENTED (BS 1582 S20L) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 LT SIDE OF FUSELAGE- SKIN IS DENTED OUTWARD AND A FASTENER IS PULLED THRU THE SKIN AT APPROX STA 1582 STR 20L. ACCOMPLISHED REPAIR PER PRI 617777-14 REV 0, PRI 617777-14 REV 1 AND ERA 617777-14 REV A.

Part: FAIRING — CRACKED (NR 2 NACELLE) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 #2 PYLON LWR AFT FAIRING HAS VERTICAL CRACK ON I/B SIDE FWD OF T /E REMOVABLE PANEL. CORRECTIVE ACTION: REPAIRED REF B767 SRM 54-53-01-2R-7 (0334681)

Part: SKIN — DAMAGED (BS 592 S6L) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 LIGHTENING STRIKE AT FASTENER ST 592 ABOVE STRINGER 6L. CORRECTIVE ACTION: REPAIRED REF B767-300 SRM 53-00-01 REPAIR 14. (0325067)

Part: SKIN — DAMAGED (BS 654 S7L) · airframe 138,941 hrs · 20,180 cycles

SHIP 178 LIGHTENING STRIKE STA 654 + 16 AT FASTENER ON STRINGER 7L. CORRECTIVE ACTION: EVALUATE AND REPAIR AS REQUIRED PER B767-300 SRM 53-00-01. INSTALLED REPAIR DECAL PER PS 900-5-1 NO. 4 (0325202)

Part: CONNECTOR — LOOSE (EMERGENCY LIGHTS) · airframe 138,261 hrs · 20,048 cycles

SHIP 178 PAX SEAT 1A - 5A EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: T/S REF B767 WDM 33-51-13. FOUND LOOSE CONNECTOR IN SIDEWALL. RE-SECURED CONNECTOR. CKS OK. ALL EMERGENCY LIGHTS CKS OK AT PRESENT TIME. (5729169)

Part: DOOR — UNKNOWN (L2) · airframe 138,218 hrs · 20,039 cycles

SHIP 178 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR HANDLE & OPS CHK NML. DOOR ARMED OK. REF B767 AMM 42 -73 (5729150)

Part: INDICATOR — MALFUNCTIONED (L1 DOOR) · airframe 138,161 hrs · 20,028 cycles

SHIP 178 GATE AGENT REPORTS L1 DOOR EXTERIOR ARMING INDICATION DOES NOT RETRACT WHEN DOOR IS DISARMED. CORRECTIVE ACTION: L1 DOOR ARMING MECHANISM OPS NML PER B767 AMM 52-11. (5729106)

Part: SHEAR TIE — DAMAGED (BS 1540 S38-39R) · corrosion level 2 · airframe 138,027 hrs · 20,000 cycles

SHIP 178 SHEAR TIE DAMAGED - STA. 1540 BETWEEN STR. 39R AND STR. 38R. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 000-0001:5300-0780/063 00063 REMOVED AND REPLACED SHEAR TIE REF: BACDWG 146T1222 (0164315)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 137,419 hrs · 19,874 cycles

SHIP 178 2L DOOR WILL NOT ARM WHEN DOOR WAS CLOSED. CORRECTIVE ACTION: REMOVED DOOR DEBRIS. OPS CHECK HANDLE. OPS CHECKS GOOD PER B767 AMM 52-11. (5025860)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 136,353 hrs · 19,690 cycles

SHIP 178 FA HAD TROUBLE ARMING 1L DOOR. CORRECTIVE ACTION: CLEANED DEBRIS, CYCLED ARMING MECHANISM NUMEROUS TIMES. OPS NORMAL IAW B767 AMM 25-66. (4490340)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 136,206 hrs · 19,667 cycles

SHIP 178 SHORT PERIOD OF FUMES IN COCKPIT ON DECENT NOT ABLE TO ISOLATE LOCATION OR CAUSE BEFORE IT DISSIPATED. CORRECTIVE ACTION: T/S FOUND UPPER EICAS DISPLAY INOP AND SOURCE. OF SMELL R/R UPPER EICAS DISPLAY PER AMM 31-41 IPS NRML C/W NO GO ODI PROCEDURES AND ODI CAPTURE INSPECTED OVENS AND E/E COMPARTMENT NO OTHER DEFECTS NOTED (4977084)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 136,042 hrs · 19,642 cycles

SHIP 178 2L DOOR CANNOT BE ARMED. CORRECTIVE ACTION: REMOVED FOD FROM DOOR HANDLE. CHECKS GOOD. (4977002)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,476 hrs · 19,551 cycles

SHIP 178 2R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND EXTERIOR HANDLE NOT COMPLETELY CLOSED, CLOSED HANDLE. DOOR OPERATES & ARM DISARM NORMAL. OK FOR SVC. (4646058)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,058 hrs · 19,476 cycles

SHIP 178 FOUND R1 DOOR EXTERIOR DOOR HANDLE PAWL DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED R1 DOOR EXTERIOR/ DOOR INTERLOCK PAWL IAW B767-300 52-11. OPS CHK NML THIS COMPLIES WITH SECTION II PERMANENT REPAIR OF ER/A 608654-14 (4785262)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 135,002 hrs · 19,467 cycles

SHIP 178 ENTRY DOOR ARMING LEVER HARD TO OPERATE / LOCATIONS: 2L. CORRECTIVE ACTION: CLEANED FOD FROM GIRT BAR. 2L DOOR NOW ARMS/DISARMS OK AT LGW. A /C OK FOR SVR. (2747727)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,802 hrs · 19,433 cycles

SHIP 178 1L DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: FLIGHT CREW PLACARD INSTALLED AT JFK PER MEL 52-11-01. (2722593)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,755 hrs · 19,425 cycles

SHIP 0178 -DIV- TO LAX DUE TO 3 LAVATORIES INOPERATIVE WITH TANK INOP LIGHT ILLUMINATED. SECOND TANK IND HALF FULL. CORRECTIVE ACTION: VERIFIED ONE TANK FULL AND SECOND TANK HALF FULL. SYSTEM SERVICED AND OPS NML. (4779011)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,667 hrs · 19,408 cycles

SHIP 0178 -FCNT/DE- CREW ELECTED DE DUE TO TE FLAP DISAGREE INDICATION DURING APPROACH. CREW PERFORMED A GO AROUND C/W QRH AND LANDED WITHOUT INCIDENT. CORRECTIVE ACTION: T/S PER FIM. PSEU FAULTED S287. R/R S287. PERFORMED FLAP LUBRICATION AND CYCLED FLAPS 5 TIMES WITH NO FAULTS.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,636 hrs · 19,401 cycles

SHIP 178 2L DOOR DIFFICULT TO ARM, CORRECTIVE ACTION: CLEARED DEBRIS FROM 2L DOOR AREA. CYCLED DOOR OPEN/CLOSE ARMS OK REF B767 AMM 52-73. OK FOR SVC (9448132)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,552 hrs · 19,386 cycles

SHIP 178 1L DOOR SLIDE LIGHT WILL NOT ILLUMINATE. CORRECTIVE ACTION: PERFORMED OPS TEST ON 1L DOOR OPS C/K NML NO FAULTS NOTED. (4774898)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 134,459 hrs · 19,371 cycles

SHIP 178 2R DOOR EXIT SIGN LENS IS MISSING.CORRECTIVE ACTION: REPLACED MISSING EXIT SIGN LENS IAW B767 AMM 33-51. (4774856)

Part: NONE — NONE · airframe 134,377 hrs · 19,360 cycles

SHIP 178 SEAT 17A EMERGENCY PATH LIGHT INOP. R/R EMERGENCY LIGHT ASSY AT SEAT 17A PER B767 AMM 33-51. OPS CK GOOD.

Part: NONE — NONE · airframe 134,367 hrs · 19,359 cycles

SHIP 178 DOOR 2L SLIDE LIGHT INOP. CORRECTIVE ACTION: R/R SLIDE RAFT ARM LIGHT ASSY PER B767-300 AMM 52-73. OPS CHK NML. MEL & PLAC RMVD. NO M PROCEDURES. (2652413)

Part: NONE — NONE · airframe 134,306 hrs · 19,349 cycles

SHIP 0178 -DIV- DIVERTED TO PHX DUE TO LEFT WING ANTI-ICE LIGHT ILLUMINATED. CORRECTIVE ACTION: REPLACED LEFT WING ANTI-ICE VALVE. OPS CHECKS GOOD. (4188280)

Part: NONE — NONE · airframe 134,238 hrs · 19,335 cycles

SHIP 178 1R DOOR NOT ABLE TO ARM. CORRECTIVE ACTION: CYCLE DOOR OPS CHK GOOD PER B767 AMM 52-11. (4188232)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 134,070 hrs · 19,303 cycles

SHIP 178 ARM LIGHT DIDN'T LIGHT UP. CORRECTIVE ACTION: CYCLE BRAKER ALL LIGHT CAME BACK ON. RESET PER B767 AMM 52-73 (9974080)

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 134,070 hrs · 19,303 cycles

SHIP 178 REAR EMERGENCY EXIT SIGN AT OVERHEAD 16 EDC MISSING. CORRECTIVE ACTION: REPLACED EMERGENCY EXIT SIGN COVER AT OVERHEAD AISLE 16 EDC. (9974076)

Part: NONE — NONE · airframe 134,160 hrs · 19,320 cycles

'SUPPLEMENTAL INFOMATION' SHIP 178 1L DOOR ARMING FLAG MISSING. CORRECTIVE ACTION: REMOVED AND REPLACED THE #1 MAIN ENTRY DOOR ARE FLAG PLACARD, REF B767-300 AMM 52-70-00. FLAG OPS CHECKS OK. MEL CLEARED PLACARD REMOVED. (9974068)

Part: INDICATION SYS — FALSE INDICATION (TE FLAPS) · airframe 133,637 hrs · 19,224 cycles

DUE TO TE DISAGREE INDICATION DURING DESCENT. CREW DECLARED EMERGENCY. C/W QRH AND LANDED UNEVENTFULLY. T/S PER FIM. OPS NML. OK TO RTS PER MCC. (9926573)

Part: DOOR — FOD (L2) · airframe 133,575 hrs · 19,212 cycles

L2 DOOR WILL NOT ARM. REMOVED DEBRIS, L2 DOOR NOW OPS CHECKS NORMAL. ARMS NORMALLY. OK FOR SERVICE.

Part: GIRT BAR — DIRTY · airframe 133,555 hrs · 19,208 cycles

SHIP 178 L AFT ENTRY DOOR UNABLE TO ARM. CORRECTIVE ACTION: FOUND AND REMOVED DEBRIS FROM GRIT BAR HOUSING. CYCLED SEVERAL TIMES. PER B767 M/M 52-12. OK FOR SVC (9926546)

Part: BUSHING — GROOVED · airframe 133,248 hrs · 19,145 cycles

SHIP 178 AFT TRUNNION BUSHING HAS GROOVES WORN INTO FWD UPPER SURFACE. CORRECTIVE ACTION: SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION (2498458)

Part: GIRT BAR — FOD · airframe 133,200 hrs · 19,135 cycles

SHIP 178 AT DEP. 2L DOOR WOULD NOT ARM. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR. 02L DOOR OPS NML PER B767-300 AMM 52-11. (9481116)

Part: NONE — NONE · airframe 133,248 hrs · 19,145 cycles

'SUPPLEMENT INFOMATION' SHIP 178 RH OUTBOARD TE FLAP DMG DENT. DENT MEASURES ROUGHLY 4X6.5". DMG LOCATED 11.5" FROM T/E OF FLAP AND 16" FROM FLAP TRACK FAIRING. CORRECTIVE ACTION: INSALLE PERM REPAIR PER ERA603346-14 REV 0 SECT III OK TO CLOSE MON (9380177)

Part: NONE — NONE · airframe 132,865 hrs · 19,069 cycles

SHIP 178 2L DOOR WILL NOT ARM, CORRECTIVE ACTION: FOUND FOD STUCK 2L DOOR GIRT BAR. REMOVE FOD. OPS CHECK NORMAL PER B767 AMM 25-66 (8582640)

Part: NONE — NONE · airframe 132,617 hrs · 19,021 cycles

'SUPPLEMENTAL INFOMATION' SHIP 178 EMERGENCY LIGHT IN CEILING ABOVE G22 INOP. CORRECTIVE ACTION: R/R BATT AND BATT CHARGER PER B767 AMM 33-51 (9292705)

Part: NONE — NONE · airframe 131,926 hrs · 18,883 cycles

SHIP 178 LH FWD ENTRY DOOR MOUNTED SLIDE RAFT FOUND PACK BALL LOOSE, CORRECTIVE ACTION: REMOCED AND REPLACED L1 FWD ENTRY DOOR SLIDE PACK REFER TO AMDS W/C 5200-4473 (2300346)

Part: NONE — NONE · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 RH MLG W/W STA 955 FOUND CORROSION AT IB GAP BETWEEN REAR SPAR BULKHEAD AND SIDE FRAME FITTING. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 599695-14 (2298247)

Part: NONE — NONE · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 CABIN SEAT TRACK ON FLOOR PANEL MATING SURFACE FOUND CORROSION AT LBL 11 STA 1230-1361, CORRECTIVE ACTION: THE NEW SEAT TRACK INSTALLED AS PER B767 -300 SRM 51-40. (2298245)

Part: LONGERON — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT LONGERON CHORD CORROSION AT STA 1097 AND S-23L LOWER. CORRECTIVE ACTION: LONGERON CORROSION REMOVED AND ACCOMPLISHED AS PER PRI599869-14. (2294455)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 FWD GALLEY FLOORBEAM AT STA 287 RBL 59 FOUND WITH CORROSION. CORRECTIVE ACTION: THE CORRODED UPPER CHORD REPLACED & AT STA 287 RBL 71.62 ONE ENLARGED HOLE OF U CHANNEL REPAIRED AND ACCOMPLISHED AS PER PRI 600081-14. (2294451)

Part: STRUCTURE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 BULK CARGO COMPARTMENT T CHORD CORROSION AT STA 1562 AND S-39L TO S-39R. CORRECTIVE ACTION: CORRODED LOWER CHORD REPAIRED AND ACCOMPLISHED AS PER PRI599984-14. (2294459)

Part: SKIN — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SKIN CORROSION AT STA1197+10 AND S-36R. CORRECTIVE ACTION: CORROSION REMOVED AND ACCOMPLISHED AS PER PRI 599942-14. (2294464)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 LH CABIN SEAT TRACK AT LBL 11 STA 1439-1480 FOUND WITH CORROSION ON FLOOR PANEL MATING SURFACE, CORRECTIVE ACTION: THE CORRODED SEAT TRACK REPLACED AS PER B767-300 SRM 51-40-02. (2290205)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 BULK CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1518 AND S-38R TO S-39R, CORRECTIVE ACTION: BULK CARGO FRAME AT STA 1518 BETWEEN S-38R AND S-39R. THE CORRODED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40-02. (2288453)

Part: FRAME — CORRODED · airframe 131,926 hrs · 18,883 cycles

SHIP 178 EO TASK HFEC INSPECTION FOUND 01 EA CRACK AT LH-BS859.5 FRAME INNER CHORD TRANSITION RADIUS, CORRECTIVE ACTION: LH CABIN AT STA 859.5 FRAME. 01 EA CRACKED INNER CHORD TRANSITION RADIUS REPAIRED AND ACCOMPLISHED AS PER W/C:5311- 01195-09A. (2286961)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 FWD GALLEY FLOORBEAM AT STA 347 RBL 35-48 FOUND WITH CORROSION. CORRECTIVE ACTION: THE CORRODED REPAIR STRAP REPLACED AND FABRICATED AS PER ER/A 519773-14.REV A. (2285743)

Part: FLOORBEAM — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 LH CABIN FLOORBEAM AT STA 1480 LBL 50 FOUND WITH CORROSION, CORRECTIVE ACTION: CORRDED FLOOR BEAM UPPER CHORD REPAIRED BY THE SPLICE LINE AT STA1480 LBL19 AS PER B767-300 SRM 53-00. (2285417)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 CABIN SEAT TRACK ON FLOOR PANEL MATING SURFACE FOUND CORROSION AT LBL 54.75 STA 1197- 1197+132, CORRECTIVE ACTION: SEAT TRACK REPAIRED BY THE SPLICE AT STA 1197+99 & STA 1197+11. LBL54.75 AS PER B767-300 SRM 53-00. (2284209)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 CABIN SEAT TRACK ON FLOOR PANEL MATING SURFACE FOUND CORROSION AT LBL 11 STA 1197- 1197+132, CORRECTIVE ACTION: THE CORRODED SEAT TRACK BETWEEN STA 1197+99 AND STA 1230 LBL 11 REPAIRED BY SPLICE AT STA 1197+99 LBL 11 AS PER B767-300 SRM 53- 00-52 (2284188)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 RH CABIN SEAT TRACK AT RBL 88 UNDER RH FWD LAV FOUND CORROSION. CORRECTIVE ACTION: THE CORROED SEAT TRACK REMOVED AND REPLACED AS PER B767-300 SRM 51-40 (2281613)

Part: PICKLE FORK — CORRODED · airframe 131,926 hrs · 18,883 cycles

SHIP 178 DURING HCK AT STAG, CORROSION WAS NOTED ON THE RH PICKLE FORK (SIDE FRAME FITTING), STA 955. ER/A 599695-14 SECTION I WAS ACCOMPLISHED, FOLLOW ON ACTION IS REQUIRED FOR SECTION II, CORRECTIVE ACTION: ACCOMPLISH ER/A 599695-14 SECTION II INSPECTION BEFORE 21,726 TOTAL FLIGHT CYCLES, THEN AT 2844 FLIGHT CYCLE INTERVALS THEREAFTER. (2279497)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1263 AND S-39L TO S-39R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277519)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1175 AND S-37L TO S-38L, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277511)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1197 +88 AND S-37L TO S-38L. CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277523)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 BULK CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1439 AND S-39L TO S-39R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277532)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1197 +66 AND S-36L TO S-37L, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277551)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 BULK CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1502 AND S-38L TO S-39L, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277548)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1219 AND S-35R TO S-36R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277554)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 BULK CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1417 AND S-39L TO S-39R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277536)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1307 AND S-39L TO S-39R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277498)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1280 AND S-35R TO S-36R, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277504)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1219 AND S-37L TO S-38L, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277543)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 131,926 hrs · 18,883 cycles

SHIP 178 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA 1197 AND S-37L TO S-38L, CORRECTIVE ACTION: THE CORROED SHEAR TIE REPLACED AS PER B767-300 SRM 51-40 (2277557)

Part: NONE — NONE · airframe 131,926 hrs · 18,883 cycles

SHIP 178 ER/A 574133-14AD SECT I REPAIR WAS ACCOMPLISHED ON A/C 178 , CORRECTIVE ACTION: ACCOMPLISH ER/A 574133-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR. (2260159)

Part: NONE — NONE · airframe 131,926 hrs · 18,883 cycles

'SUPPLEMENTAL INFOMATION' SHIP 178 R/H ENG L/H NACELLE STRUT ACCESS DOOR (446AL) MISSING DURING WAC FOUND, CORRECTIVE ACTION: INSTALLED RH ENG L/H NACELLE STRUT ACCESS DOOR 446AL AS PER B767 -300 AMM 54-53-01 (7338908)

Part: NONE — NONE · airframe 131,908 hrs · 18,880 cycles

SHIP 178 ER/A 574132-14AD TEMP REPAIR WAS ACCOMPLISHED ON A/C 178 IN THE LH WING SKIN AT STR L-6.5 BETWEEN WSTA 990 AND 1018. CORRECTIVE ACTION: ACCOMPLISH ER/A 574132-14AD REV. A SECTION III PRIOR TO 6,000 CYCLES OR 18,000 FLIGHT HOURS AFTER SECTION I REPAIR (2202463)

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 131,903 hrs · 18,879 cycles

SHIP 178 PER CUSTOMER REQUEST ROBBED EMERGENCY LIGHT BATTERIES (QTY 10) FOR AC 1708. MAINTENANCE INSTALLED SERVICEABLE EMERGENCY LIGHT BATTERIES AND REPLACED MISSING CHARGER. SYSTEM OPERATION IS NORMAL. (LP 1781685)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 131,421 hrs · 18,782 cycles

FOUND LEFT AFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE, SEATS 34AB, 37AB, 40AB AND EXIT SIGN. REPLACED BATTERY PACK M739 AND CHARGER. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 131,119 hrs · 18,726 cycles

L4 AND LT EXTERIOR OFF WING SLIDE FLOOD LIGHTS INOPERATIVE. REPLACED CHARGER AND BATTERY (M738). SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 131,035 hrs · 18,714 cycles

FOUND OVERHEAD EMERGENCY LIGHTS AT SEATS 39 LEFT INOPERATIVE. REPLACED BATTERY PACK AT M739. SYSTEM OPS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 130,978 hrs · 18,703 cycles

ON SERVICE CHECK FOUND LEFT AFT OVERHEAD EMERGENCY EXIT LIGHTS SIGNS INOPERATIVE. REPLACED BATTERY PACK M739. SYSTEM OPERATION IS NORMAL.

Part: BULB — BURNED OUT (EMERGENCY LIGHTS) · airframe 130,579 hrs · 18,628 cycles

CREW REST LADDER AND COMMCON AREA EMERGENCY EXIT SIGNS ARE INOPERATIVE. FOUND ALL 24 BULBS BURNT OUT AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: SPHERICAL BEARIN — ROTATED (RT MLG) · airframe 127,703 hrs · 18,262 cycles

DUE TO ROTATION, REPLACE R/H MLG SPHERICAL BEARING. C/W SRM 53-50-90. (LP 0957696)

Part: SHROUD — DEFECTIVE (EMERGENCY LIGHT) · airframe 127,703 hrs · 18,262 cycles

EMERGENCY ESCAPE PATH LIGHTS AT SEAT 33B ARE INOPERATIVE. REPLACED EMERGENCY LIGHT SHROUD ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: ACCESS DOOR — MISSING (NR 1 NACELLE) · airframe 127,703 hrs · 18,262 cycles

ON WALK AROUND FOUND ON NR 1 ENGINE INBOARD PYLON NACELLE STRUT ACCESS DOOR MISSING. REPLACED ACCESS DOOR.

Part: SKIN — DAMAGED (WING) · airframe 127,112 hrs · 18,185 cycles

AD/EM-EO TASK-WHEN PERFORMING W/C# 5724-01010-41A,THE FASTENER CODE A,HOLE NO.1 DIAMETER MEASURED IS 0.5442?,FANSTENER CODE B, HOLE NO.2 DIAMETER IS 0.3585?THE FASTENER CODE A,HOLE NO.1 AND FASTENER CODE B,HOLE NO.2 REPAIRED PER ER/A 574132-14. (LP 0880758)

Part: SKIN — CRACKED (RT WING) · airframe 127,112 hrs · 18,185 cycles

HFEC INSPECTION FOUND 01EA CRACK APPROX 0.110 IN LENGTH AT THE FWD DIRECTION AND 01EA CRACK APPROX.0.100 LENGTH AT THE AFT DIRECTION OF THE MOST O/B HOLE AT RH WING LOWER SKIN AND REPAIRED. (LP 0880785)

Part: SKIN — DAMAGED (WING) · airframe 127,112 hrs · 18,185 cycles

FOUND THE FASTENER CODE B,NO.66 HOLE MEASURED DIAMETER IS 0.6772? BEFORE 1/16 OVERSIZE REPAIRED PER ERA 574133-14. (LP 0880769)

Part: SKIN — DAMAGED (LT WING) · airframe 133,900 hrs · 19,271 cycles

DURING CCK AT STAG AND DURING ACCOMPLISHMENT OF EM 5724-01010-41A, DISCREPANCYS WERE NOTED IN THE LH WING SKIN. ER/A 574132-14AD. ER/A 574132-14AD REVISED TO REV. B. ACCOMPLISH ER/A 574132-14AD REV B SECTION II INSPECTIONS. STATE INSPECTION RESULTS ON THIS LOGPAGE.

Part: LIGHT — LOOSE (SEAT 26B) · airframe 124,857 hrs · 17,891 cycles

EMERGENCY SEAT MOUNTED LIGHTING AT 26B IS INOPERATIVE. FOUND HARDWARE MISSING AND REPLACED. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHTS) · airframe 123,054 hrs · 17,653 cycles

EMERGENCY LIGHTS AT 31A ARE INOPERATIVE. RECONNECTED THE WIRE HARNESS, SYSTEM OPERATION IS NORMAL.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 121,520 hrs · 17,445 cycles

EMERGENCY LIGHTS INOPERATIVE AFT OF RIGHT WING X2. REPLACED THE LAMPS, OK.

Part: SKIN — LOOSE (LT WING) · airframe 121,473 hrs · 17,439 cycles

PASSENGER NOTED ON AREA AROUND THE LEFT OUTBOARD SPOILER THAT APPEAR TO HAVE EITHER A TEAR OR STRIP OF METAL FOUND THREE LOCK FASTENERS ALONG THE FWD EDGE AND TWO BLIND RIVETS ALONG THE INB EDGE OF THE LT WING FIXED TE PANEL FWD INBD CORNER FAILED. ACCOMPLISHED TIME LIMITED REPAIR IAW ER/A 561663-14.

Part: SMOKE DETECTOR — MALFUNCTIONED (FWD CARGO BAY) · airframe 121,129 hrs · 17,394 cycles

AFTER BLOCK IN, FORWARD CARGO DETECTOR 2 STATUS MESSAGE. REPLACED CARGO SMOKE DETECTOR.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 120,447 hrs · 17,310 cycles

EMERGENCY LIGHTS AT SEAT 24FG AND 37FG ARE INOPERATIVE. CONNECTOR AT 37FG IS PUSHED OUT SECURED PIN AND RECONNECTED. SYSTEM OPERATION IS NORMAL

Part: SPHERICAL BEARIN — DAMAGED (RT MLG) · airframe 127,703 hrs · 18,262 cycles

RH MLG SPHERICAL BEARING FOUND SIGNS OF ROTATION, REPLACED BEARING C/W ERA 567722-14 (LP 2907406)

Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 119,291 hrs · 17,164 cycles

CORROSION LEVEL: 2, BULK CARGO AT STA 1562, BETWEEN STR 38L-38R FOUND WEB CORRODED AND REPLACED PER ERA 551308-14.

Part: RIB — CRACKED (LT WING SLAT) · airframe 119,089 hrs · 17,137 cycles

LEFT WING NR 1 SLAT INBD RIB FOUND CRACKED. REPLACED THE RIB IAW SRM 51-40-02.

Part: SKIN — DELAMINATED (RT WING SLAT) · airframe 119,089 hrs · 17,137 cycles

RIGHT WING NR 10 SLAT TRAINING EDGE WEDGE FOUND DELAMINATED. REPAIRED THE SLAT IAW SRM 57-43-02.

Part: FITTING — CRACKED (LONGERON) · airframe 119,089 hrs · 17,137 cycles

HFEC INSPECTION FOUND ONE CRACK ON THE LT LOWER UNDERWING LONGERON FITTING. THE LONGERON FITTING WAS REPLACED.

Part: SKIN — DELAMINATED (LT WING SLAT) · airframe 119,089 hrs · 17,137 cycles

LEFT WING, NR 2 SLAT EXTERNAL SURFACE DELAMINATED. REPAIRED THE SLAT IAW SRM 57-43-02 AND 51-70-10.

Part: STRINGER SPLICE — CORRODED (BS 1582) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

BULK CARGO AT BS 1582, STRINGER SPLICE 39R FOUND CORRODED. REPLACED THE STRINGER SPLICE.

Part: SHEAR TIE — CORRODED (BS 1219) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

AFT CARGO AT BS 1219. BETWEEN STRINGERS 35-36L SHEAR TIE DOUND CORRODED. REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1219) · airframe 119,089 hrs · 17,137 cycles

AFT CARGO AT BS 1219. BETWEEN STRINGERS 37L - 38L SHEAR TIE CORRODED. REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1562) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

BULK CARGO AT BS 1562. BETWEEN STRINGERS 38L - 38R. SHEAR TIE CORRODED. REPLACED THE SHEAR TIE.

Part: STRAP — CORRODED (BS 1562-1582) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

BULK CARGO BETWEEN BS 1562 - 1582, STRINGER 38L - 38R FWD OF WASTE TANK DRAIN PORT SURROUNDING LOWER PLATE FOUND CORRODED. THE STRAP WAS REPLACED.

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

FORWARD CARGO AT BS 654, BETWEEN STRINGERS 34-35R, SHEAR TIE FOUND CORRODED. REPLACED THE SHEAR TIE.

Part: SHEAR TIE — CORRODED (BS 1395) · corrosion level 2 · airframe 119,089 hrs · 17,137 cycles

AFT CARGO AT BS 1395, STRINGERS 39L-39R SHEAR TIE CORRODED. REPLACED THE SHEAR TIE.

Part: BULKHEAD — CRACKED (BS 1809) · airframe 119,089 hrs · 17,137 cycles

DURING HFEC INSPECTION, A CRACK INDICATION WAS FOUND ON THE BS 1809 BULKHEAD, STRINGER 7R. REPAIRED IAW SRM 53-80-08.

Part: BULKHEAD — CRACKED (NLG WW) · airframe 119,089 hrs · 17,137 cycles

INSPECTION FOUND ONE CRACK ON RT NOSE WHEEL WELL BULKHEAD BS 287. REPAIRED IAW SRM 51-70-12.

Part: SKIN — DAMAGED (BS 654) · airframe 119,089 hrs · 17,137 cycles

FUSELAGE EXTERIOR SURFACE FROM BS 654+88 TO 654+ 110, STRINGER 30 - 31L FOUND DENTED AND CRACKED. REPAIRED IAW SRM 53-00-01.

Part: STRINGER — CRACKED (BS 1654) · airframe 119,089 hrs · 17,137 cycles

BS 1654.5, STRINGER 3R FOUND CRACKED. REPLACED THE STRINGER IAW SRM 51-40-02.

Part: FAILSAFE — CRACKED (BS 955) · airframe 119,089 hrs · 17,137 cycles

DURING HFEC INSPECTION OF THE BS 955 FAILSAFE STRAP. A CRACK INDICATION WAS FOUND. APPROX 3/4" IN LENGTH. REPAIRED.

Part: FAILSAFE — CRACKED (BS 955) · airframe 119,089 hrs · 17,137 cycles

DURING ET/UT INSPECTION OF BS 955 FAILSAFE STRAP CRACKED. REPAIRED.

Part: SPAR — CRACKED (NR 2 PYLON) · airframe 127,372 hrs · 18,220 cycles

NR 2 PYLON FWD UPPER SPAR WEB CRACKS AT FUEL LINE AND DRAIN LINE CUTOUTS. C/W ERA 384281-14. (LP 2729051)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 115,432 hrs · 16,668 cycles

EMERGENCY LIGHT AT 39F ARE INOPERATIVE. MAINTENANCE REPINNED AT SEAT DISCONNECT.

Part: SKIN — CORRODED (FUSELAGE) · airframe 119,619 hrs · 17,203 cycles

FUSELAGE SKIN BULGED CORRODED AND CRACKED AT FS 1582 STRINGER 25L TO 26L. REMOVED DAMAGE AND SUBMITTED RESULTS TO ENGINEERING. C/W ERA541005-14.

Part: SKIN — CORRODED (BS 1582) · airframe 113,341 hrs · 16,407 cycles

CORROSION WAS FOUND ON THE FWD SKIN PANEL AT THE BS 1582 BUTT SPLICE. CLEAN UP CORROSION AND INSTALL A REPAIR DOUBLER IAW ERA.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 113,197 hrs · 16,388 cycles

DURING SERVICE CHECK FOUND LT SIDE OF OVERHEAD EMERGENCY LIGHTS FROM ROW 17-31 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK. SYSTEM OPS IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 111,487 hrs · 16,179 cycles

EMERGENCY LIGHTS IN ROW 31FG-41FG ARE INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK CHARGER ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: SKIN — GOUGED (FUSELAGE) · airframe 108,284 hrs · 15,796 cycles

FOUND A GOUGE TO FUSELAGE SKIN 28 INCHES AFT OF CARGO DOOR CUTOUT LOWER AFT CORNER. BURNISHED DAMAGE IAW SRM 53-00-01.

Part: OVEN — SMOKE (GALLEY) · airframe 107,858 hrs · 15,739 cycles

PERFORMED AN AIR TURN BACK DUE TO SMOKE COMING FROM THE FORWARD GALLEY OVENS. CREW FOLLOWED THE QRH AND PULLED CIRCUIT BREAKERS. SMOKE DISSIPATED BUT EXCESSIVE HEAT REMAINED IN THE AREA. MAINTENANCE FOUND THAT ALL THREE FORWARD GALLEY OVENS HAD EVIDENCE OF SMOKE. REPLACED THE OVENS.

Part: STRINGER — CRACKED (LT WING) · airframe 104,491 hrs · 15,303 cycles

LT WING INBOARD DRY BAY INTERIOR WS 344.3 STRINGER 27L FOUND CRACKED APPROX 1.5 INCHES LONG. CRACKED STRINGER REPAIRED IAW ERA 518785-14.

Part: SEAT TRACK — CORRODED (BS 347) · corrosion level 2 · airframe 104,491 hrs · 15,303 cycles

SEAT TRACK FOUND CORRODED AT BS 347, RBL 54.75. REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — NOT REPORTED (FUSELAGE) · airframe 104,452 hrs · 15,297 cycles

MAIN DECK FLOOR BEAM UPER CHORD.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 102,340 hrs · 15,015 cycles

DURING DRC FOUND EMERGENCY LIGHTS ROW AB 14-20 AND OVERWING EXIT SIGNS INOPERATIVE. MX REPLACED THE BATTERY CHARGER M9011 IAW AMM 33-51. SYS OPS IS NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 100,380 hrs · 14,739 cycles

EMEREGENCY LIGHTS AT MID RT LAVATORY ARE INOPERATIVE. MX REPAIRED BROKEN WIRES. SYSTEM OPS ARE NORMAL.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 99,635 hrs · 14,638 cycles

EMERGENCY PATH LIGHTS FROM 14-20AB ARE INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLY AND FUSE IN THE POWER SUPPLY. SYS OPERATION IS NORMAL.

Part: SUPPORT — CORRODED (TE FLAP) · airframe 98,738 hrs · 14,519 cycles

LT & RT INBOARD FLAP. INBOARD AND OUTBOARD SUPPORT CORROSION OR TOOLING DAMAGE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,100 hrs · 13,800 cycles

EMERGENCY PATH MARKER LIGHTS AT SEAT 34F ARE INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (COCKPIT) · airframe 92,985 hrs · 13,786 cycles

EMERGENCY EXIT LIGHT IN COCKPIT DOORWAY DOES NOT ILLUMINATE WHEN SELECTED ON. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND BATTERY. SYSTEM OPERATION IS NORMAL.

Part: BEARING — MIGRATED (RT MLG SUPPORT) · airframe 92,473 hrs · 13,713 cycles

RT MLG SUPPORT ATTACH BEARING AT FS 1043 MIGRATED AND REPAIRED IAW SRM 53-50-90, REPAIR 3.

Part: FITTING — DAMAGED (NR 2 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 2 PYLON AFT STRUT FITTING FASTENER HOLE FOUND OVERSIZE AND REPAIRED IAW ERA 487050-14.

Part: FRAME — CRACKED (BS 1809) · airframe 92,473 hrs · 13,713 cycles

LEFT FS 1809 OUTER CHORD INNER FLANGE CRACKED AT 1 EA FASTENER HOLE AND REPAIRED IAW EA 01-074914-12, ME 07, REV S.

Part: SKIN — DELAMINATED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

NR 5 SLAT UPPER SURFACE INBD EDGE DELAMINATED AND REPAIRED IAW SRM 57-43-02. REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

NR 6 SLAT WEDGE UPPER SURFACE OTBD EDGE DELAMINATED AND REPAIRED IAW SRM 57-43-02, REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.

Part: WEDGE — DAMAGED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

NR 8 SLAT WEDGE UPPER SURFACE INBD EDGE FOUND DEFORMED AND REPAIRED IAW SRM 57-43-02. REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIG 202.

Part: FLAP — DELAMINATED (RT WING) · airframe 92,473 hrs · 13,713 cycles

RT WING INBD MAIN FLAP L/E OTBD END DELAMINATED AND REPAIRED IAW SRM 57-53-01. REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

NR 11 SLAT WEDGE UPPER SURFACE OTBD EDGE DELAMINATED AND REPAIRED IAW SRM 57-43-02, REPAIR 1, FIG 201 AND SRM 51-70-10, REPAIR 4, FIG 202.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 1 PYLON STRUT LWR SPAR FITTING ATT BUSHING REPLACED IAW SRM 54-53-90, FIG 201 REPAIR 4.

Part: SKIN — CRACKED (NR 2 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 2 PYLON TORQUE BOX PANEL NR 442BL CUTOUT SKIN CRACK. REPAIR ACCOMPLISHED IAW ER/A 487058-14, REV O.

Part: FITTING — CRACKED (RT WING) · airframe 92,473 hrs · 13,713 cycles

RT WING FRONT SPAR UPPER LINK PITCH LOAD FITTING FASTENER HOLE CRACK. REPAIR ACCOMPLISHED IAW ER/A 487054-14AD.

Part: SKATE ANGLE — CHAFED (LT WING) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD SKATE ANGLE INTERIOR CHAFED AREA REPAIRED IAW ER/A 487057-14.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 2 PYLON STRUT FWD UPPER SPAR FITTING ATT BUSHING REPLACED IAW SRM 54-53-90, REPAIR 2.

Part: BUSHING — MIGRATED (NR 1 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 1 PYLON STRUT FWD UPPER SPAR FITTING ATTACH BUSHING REPLACED IAW SRM 54-53-90, FIG 201, REPAIR 2.

Part: PANEL — CRACKED (NR 2 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 2 PYLON TORQUE BOX PANEL 446BR CUTOUT CRACK REPAIR ACCOMPLISHED IAW SRM 54-53-01, REPAIR 7, FIG 201.

Part: BUSHING — MIGRATED (NR 2 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 2 PYLON STRUT LWR SPAR FITTING ATT BUSHING REPLACED IAW SRM 54-53-90, FIG 201, REPAIR 4.

Part: SKIN — CRACKED (NR 1 PYLON) · airframe 92,473 hrs · 13,713 cycles

NR 1 PYLON TORQUE BOX PANEL NR 436BR CUTOUT SKIN CRACK. REPAIR ACCOMPLISHED IAW SRM 54-53-01, FIG 201, REPAIR 7.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP WEDGE AREA LWR SURFACE FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATE AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP WEDGE AREA LWR SURFACE FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 ABD SRM 51-70-06 FIG 9.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATED AREA. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 6.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATE. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATE AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING O/B FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATE. COMPOSITE WET LAYUP REPAIR CARRIED OUT AT DELAMINATE AREA AS PER SRM 57-53-01 REPAIR 1 AND SRM 51-70-06 FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP WEDGE LWR SURFACE FOUND DELAMINATED. COMPOSITE WET LAYUP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP WEDGE AREA LWR SURFACE FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP WEDGE UPPER SURFACE FOUND DELAMINATED. COMPOSITE WET LAYUP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: SKIN — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP WEDGE AREA UPPER SURFACE FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: FLAP — DELAMINATED (RT WING) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP L/E INBD END FOUND DELAMINATE. COMPOSITE PREPREGHOT BOND CARRIED OUT AT DELAMINATE AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP L/E FAIRING FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING OTBD FLAP LWR SURFACE WEDGE AREA FOUND DELAMINATED. COMPOSITE WET LAY UP REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-06, FIG 9.

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,473 hrs · 13,713 cycles

CABIN STA 903 BETWEEN STR 20R AND 21R FRAME INNER CHORD CRACK. REPAIR ACCOMPLISHED IAW ER/A 487038-14AD.

Part: WEDGE — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

RT WING OTBD FLAP AFT WEDGE FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01, REPAIR 1 AND SRM 51-70-07, FIG 11.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

LT WING NR 1 SLAT WEDGE AREA UPPER SURFACE (1 IN FROM OTBD EDGE) FOUND DELAMINATED METAL. HOT BOND REPAIR PERFORMED IAW SRM 57-43-02, REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIG 201.

Part: WEDGE — DELAMINATED (LE SLAT) · airframe 92,473 hrs · 13,713 cycles

LT WING NR 2 SLAT WEDGE AREA UPR SURFACE (30IN FROM OTBD EDGE) FOUND DELAMINATION. METAL HOT BOND REPAIR PERFORMED AT DELAMINATION AREA IAW SRM 57-43-02, REPAIR 1 AND SRM 51-70-10, REPAIR 4, FIG 201.

Part: FAIRING — DELAMINATED (TE FLAP) · airframe 92,473 hrs · 13,713 cycles

LT WING INBD MAIN FLAP L/E OTBD END FAIRING FOUND DELAMINATED. COMPOSITE PREPREG HOT BOND REPAIR CARRIED OUT AT DELAMINATED AREA IAW SRM 57-53-01. REPAIR 1 AND SRM 51-70-05, FIG 5.

Part: FRAME — CRACKED (FUSELAGE) · airframe 92,473 hrs · 13,713 cycles

CABIN STA 903 BEWTEEN STR 20L AND 21L FRAME INNER CHORD CRACKED. REPAIR ACCOMPLISHED IAW ER/A 487037-14AD.

Part: WIRE — CUT (EMERGENCY LIGHT) · airframe 90,548 hrs · 13,472 cycles

RED WALL MOUND EMERGENCY LIGHT AT AFT RT LAV INOP FOUND WIRE CUT. REPAIRED IAW MM CH 20. LIGHTS CK OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 90,163 hrs · 13,419 cycles

EMERGENCY PATH LIGHTS AT SEAT 37F AND 38F ARE INOPERATIVE. MAINTENANCE REPAIRED DAMAGED CONNECTOR AT OUTBOUND END OF SEAT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: TURBINE BLADES — DAMAGED (NR 1 ENGINE) · airframe 88,152 hrs · 13,150 cycles

DURING ROUTINE BORO OPERATION 5067, FOUND 2ND STG TURBINE BLADE DAMAGED BEYOND LIMITS. OP 5067 NR 1 ENG.

Part: SKIN — PUNCTURED (FUSELAGE) · airframe 87,713 hrs · 13,091 cycles

GROUND DAMAGED OF THE LT LWR SKIN STA 1712. 34R-36R AMT DROPPED AN OBJECT PUNCTURING THE SKIN. AT STA 1712 BETWEEN 32R AND34R REPAIR IAW THE ERA 478509-14.

Part: PUMP — FAILED (FUEL SYSTEM) · airframe 87,004 hrs · 12,993 cycles

RTB-RT CENTER FUEL PUMP LOW PRESSURE LIGHT ILLUMINATED. INSP WIRING PER FIM 930900. REMOVED AND REPLACED RT CTR FUEL PUMP P/N 281002120. OP CHECKS GOOD AND LEAK CHECKS GOOD. REMOVED MCO/PLAC.

Part: VSI — INOPERATIVE (RIGHT) · airframe 86,262 hrs · 12,899 cycles

F/O VSI INDICATOR INOPERATIVE. R & R F/O VSI INDICATOR PER M/M CHECKS OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: PROBE — INOPERATIVE (TAT) · airframe 80,966 hrs · 12,251 cycles

TAT LIGHT AFTER TAKEOFF. REPAIRS IN PROGRESS. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 80,387 hrs · 12,174 cycles

REPLACED NR 1 ENGINE DUE TO HIGH EGT INSTALLED 727650.

Part: CONTROLLER — MALFUNCTIONED (CABIN TEMP) · airframe 76,866 hrs · 11,731 cycles

AFT CABIN TEMP CONTROLLER INOP AFT CABIN TEMP VARIED WIDELY. UNABLE TO CONTROL IN ANY MODE. ZONE TEMP CONTROLLER FAULTS AFT CABIN TRIM VALVE. REPLACED AFT CABIN TRIM VALVE PER AMM. CHKS OK.

Part: FITTING — CRACKED (BS 1809 S12R) · airframe 76,593 hrs · 11,698 cycles

FATIGUE CRACK IN TENSION FITTING COMMON TO 1809.5 CHORD REPLACEMENT. OVERSIZED HOLE, COLD WORKED, INSTALLED OVERSIZED FASTENER.

Part: FRAME — UNKNOWN (BS 1809) · airframe 76,593 hrs · 11,698 cycles

FUSELAGE BS 1809.5 BULKHEAD OUTER CHORD REPAIR IAW EO 01-074914-12 ME08 RT C/W 01-074914-12 ME08 RT.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,532 hrs · 11,690 cycles

EMERGENCY LIGHTS FIRST CLASS INOP. REPLACED FUSES AND CHARGER 9008. OPS CK GOOD.

Part: TRANSMITTER — UNKNOWN (HYD QTY) · airframe 76,311 hrs · 11,663 cycles

RTB - ON TAXI LEFT HYD QTY WENT TO 0 THEN, LATER RETURNED TO .84. REPLACED LEFT HYD QTY TRANSMITTER PER M/M 29 WTY CKS NML. LEAK OP CKS GOOD REMOVED MCO AND PLACARD.

Part: COMPRESSOR — BURNED (WATER SYSTEM) · airframe 76,214 hrs · 11,650 cycles

A/C 178 ON FLT 154/25 OUT OF JFK RETURNED TO THE GATE WITH STRONG BURNING RUBBER SMELL AROUND AFT GALLEY. JFK MTC FOUND WATER COMPRESSOR BURNED UP. REPLACED WATER COMPRESSOR OPS CK GOOD REMOVED MCO/PLAC.

Part: TURBINE — UNKNOWN (APU) · airframe 75,045 hrs · 11,509 cycles

APU AUTO SHUT DOWN. REPLACED APU.

Part: ENGINE — FAILED (APU) · airframe 74,325 hrs · 11,418 cycles

APU WEAK ON START. ONLY PROVIDED 22 PERCENT MAX MOTOR AFTER 50 SECONDS. REPLACED APU PER M/M. OPS CKS AND LEAK CHECK GOOD. MCO/PLAC REMOVED.

Part: ENGINE — WEAK (APU) · airframe 74,315 hrs · 11,417 cycles

APU WEAK ON ENG START. ONLY PROVIDED 22 PERCENT MAX MOTORING AFTER 50 SECONDS. TRIED SURGE CONTROL VALVE NO HELP. REPLACED APU.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 73,363 hrs · 11,299 cycles

BATTERY PACK FOR EMERGENCY LIGHTS FAIL DURING TEST. REPLACED BATTERY PACK AND PWR SUPPLY ASSY, EMERGENCY LIGHTS GOOD.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHT) · airframe 70,585 hrs · 10,966 cycles

EMERGENCY EXIT LIGHTS AT SEAT 20 A/B INOP. REPAIRED HARNESS.

Part: SWITCH — FAULTY (SLATS) · airframe 70,232 hrs · 10,922 cycles

L/E SLAT ASYMMETRY LIGHT ILLUMINATED AFTER T/O, LIGHT ILLUMINATED AFTER FLAP INDICATED UP. CLEANED ICE FORMATION ON FLAP/SLAT STUCTURE. PERFORMED PSEU BIT, SHOWED SWITCH S295 TARGET FAULT. CHECKED SWITCH AND TARGET, ALL SECURED. CYCLED FLAP/SLAT SEVERAL TIMES WITHOUT FAULTS.

Part: TEE FITTING — CRACKED (NR 1 PYLON) · airframe 69,957 hrs · 10,885 cycles

THE NR 1 ENGINE PYLON MID SPAR FITTING CLOSEOUT TEE WAS FOUND CRACKED. REPLACED THE CRACKED CLOSEOUT TEE. REF AD 2005-19-23.

Part: ATTACH FITTING — DAMAGED (PYLON) · airframe 69,957 hrs · 10,885 cycles

NACELLES/PYLONS ATTACH FITTING - MID SPAR FITTING REPAIR IAW EO 01-074944-12 ME03 POSITION 1 C/W 01-074944-12 ME03 POSITION 1.

Part: WIRE — SHORTED (1R DOOR) · airframe 69,677 hrs · 10,850 cycles

1L FLT ATT PANEL SLIDE LIGHT INOP. FWD TO MCO AND PLACARD PER MEL 52-11-01. FOUND CB FOR THE DOORS ARMED POPPED. POSITION T35. RESET DOOR 1R ARMED AND CB POPPED AGAIN. OBSERVED SPARKS AROUND DOOR 1R ARMED LIGHT. CB COLLARED OUT. REPAIRED SHORT.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENGINE) · airframe 69,234 hrs · 10,795 cycles

LEFT ENGINE REVERSER LIGHT CAME ON MOMENTARILY. TROUBLESHOT PER FIM, UNABLE TO DUPLICATE.

Part: BRAKE ASSY — LEAKING (MLG) · airframe 69,037 hrs · 10,762 cycles

DURING LANDING ROLLOUT TOWER ALERTED CREW OF SMOKE/VAPOR IN WHEEL WELL AREA. BAA REQUESTED MTC CHECK PRIOR TO TOW ONTO STAND. AFTER INSPECTION, FOUND NR 4 BRAKE UNIT LEAKING AT BRAKE CYLINDER. ISOLATED SYSTEM AND TOWED ONTO STAND. BRAKE REPLACED PER MM AND ALL CHECKS OK.

Part: GIRT BAR — STICKING (R1 DOOR) · airframe 68,607 hrs · 10,701 cycles

1R ENTRY DOOR SLIDE WILL NOT ARM. LUBRICATED GIRT BAR ARM HANDLE.

Part: ENGINE — ODOR (NR 2) · airframe 67,225 hrs · 10,504 cycles

ON CLIMBOUT CABIN CREW REPORTED SMOKE DETECTORS SOUNDING. PERFORMED TASK 21-00-21-102-030 NOTHING ABNORMAL FOUND. INSPECT APU BLEED VALVE APU BLEED DUCT RT LT FLOW CONTROL VALVES INSPECTED CABIN INTERIOR NO ODOR. RAN BOTH ENGINES AT HIGH POWER SETTING 1.3 EPR DURING AN HOUR WITH BLEED ON OR OFF AND CABIN SELECTOR FROM COLD TO WARM UNABLE TO DUPLICATE ANYTHING ABNORMAL. MTC FERRY TO ATL.

Part: ACTUATOR — INOPERATIVE (MLG) · airframe 63,024 hrs · 9,904 cycles

AIR/GND DISAGREE STATUS MSG AND ICE DETECTOR FAULT ILLUM ON LIFT OFF. REPLACED RT TRUCK TILT ACTUATOR.

Part: LAMP — INOPERATIVE (EMERGENCY SLIDE) · airframe 62,795 hrs · 9,872 cycles

OVERWING EMERGENCY SLIDE LIGHT ON AFT RT SIDE INOPERATIVE RELAMPED LIGHT.

Part: FLANGE — CRACKED (NR 1 ENGINE) · airframe 62,069 hrs · 9,773 cycles

NR 1 ENGINE FLANGE CRACK FOUND DURING ROUTINE BORESCOPE. REPLACING ENGINE.

Part: FLAP — DEBONDED (LT WING) · airframe 58,619 hrs · 9,236 cycles

LEFT WING INBOARD AFT FLAP DISBONDED. REPAIRED PER ER/A 423421-14.

Part: WEDGE — DEBONDED (LT WING TE FLAP) · airframe 58,227 hrs · 9,173 cycles

LT WING INBOARD AFT FLAP TE WEDGE DISBONDED. REPAIRED PER ER/A 423265-14

Part: SKIN — DELAMINATED (T/E FLAP) · airframe 57,989 hrs · 9,131 cycles

LT WING INBOARD AFT FLAP WAS FOUND WITH NUMEROUS DISBONDS. RESKINNED IAW ER/A 423259-14. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: RIB — DAMAGED (LT WING TE FLAP) · airframe 57,431 hrs · 9,032 cycles

LT INBOARD AFT FLAP TRAILING EDGE WEDGE LEADING EDGE RIBS WERE FOUND WITH OVERSIZED HOLES. HOLES REPAIRED PER ER/A 423104-14 (NORDAM EWO'S E0043938 AND E0043943).

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 55,765 hrs · 8,727 cycles

RIGHT WING NR 8 SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418117-14.

Part: WEDGE — DEBONDED (L/E SLAT) · airframe 55,765 hrs · 8,727 cycles

LEFT WING NR 5 SLAT T/E WEDGE DISBONDED. REPAIRED PER ER/A 418116-14.

Part: CHILLER — MALFUNCTIONED (AFT GALLEY) · airframe 55,310 hrs · 8,623 cycles

AT CRUISE THERE WAS AN ELECTRICAL SMELL IN THE AFT GALLEY AND A HEAVY VIBRATION IN THE FLOOR AREA. WHEN THE CB FOR THE CHILLER THAT COOLS THE FOOD CARTS WAS PULLED THE VIBRATION STOPPED AND THE ELECTRICAL SMELL ABATED. AS PRECAUTIONARY ACTION DEACTIVATED BOTH CHILLERS AT AFT GALLEY. PULLED CB/S AND COLLARED. FWD TO MCO PER MEL 25-20-01C.

Part: STRUCTURE — VIBRATION (FUSELAGE) · airframe 55,001 hrs · 8,562 cycles

FLIGHT ATTENDANTS NOTICED VIBRATIONS IN THE AREA OF THE MID GALLEY WITH MORE NOTICED ON THE RIGHT SIDE. CONFIRMED BY THE RELIEF PILOT AND NOTICED THAT VIBS DECREASED WITH ACFT SLOWING DOWN BELOW 300 KTS. ON APPROACH THE VIBRATIONS INCREASED AND THEN WENT AWAY DURING LANDING ROLL OUT. THOROUGHLY INSPECTED AIRCRAFT WITH NO DEFECTS NOTED.

Part: COWLING — DAMAGED (NR 1 ENGINE) · airframe 54,678 hrs · 8,511 cycles

DURING CLIMB HAD L/E FLAP ASYMMETRY MSG WHEN FLAP SELECTED TO 1 UNIT POS. AT FL 5K ELECTED TO RETURN TO LAX. ON ARRIVAL FOUND THAT THE NR 1 ENG CORE COWLS HAD OPENED AND PEALED BACK. ALSO FOUND DAMAGE TO THE NR 5 SLAT. ADDITIONAL INFORMATION LATER WHEN MORE IS AVAILABLE. REPLACED LT ENG EXHAUST NOZZLE, CORE COWL, BURNISHED LOWER WING SURFACE INBOARD NR 1 PYLON, REPAIRED WING CLOSURE PANEL.

Part: CONNECTOR — NOT SEATED (CABIN) · airframe 51,999 hrs · 8,010 cycles

E-PATH LIGHTS INOP AT 22F, 27B, 30B, 34B AND 36B. RESEATED CONNECTORS, OPS OK. FOUND DURING LAYOVER CHECK.

Part: HEAT EXCHANGER — CRACKED (A/C BAY) · airframe 51,991 hrs · 8,009 cycles

RTB..ON TAXI RT PACK INOP. RT DUCT LEAK EICAS MSG. FOUND RT HEAT EXCHANGER CRACKED LEAKING HOT AIR AND PRIMARY ALSO DAMAGED. DUE CREW DUTY TIME FLT CXLD. REPLACED RT HEAT EXCHANGER ASSY WITH PART SHIPPED FROM ATL. LEAK AND OPS CK OK. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 50,706 hrs · 7,782 cycles

EMERGENCY PATH LIGHTS INOP FROM ROWS 6A/B TO 20A/B. REPLACED BATTERY POWER SUPPLY UNIT.

Part: PUMP — LEAKING (HYDRAULIC SYS) · airframe 49,988 hrs · 7,673 cycles

4 HOURS INTO FLIGHT, CTR HYD "RSVR" LIGHT AND "CTR HYD QTY" EICAS MESSAGE CAME ON. CTR HYD QUANTITY INDICATED 0.47RF. SWITCHED OFF ELEC PUMPS AND QTY CONTINUED TO DECREASE. SWITCHED ELEC PUMPS BACK ON AND ADP OFF AND QUANTITY CONTINUED TO DECREASE. SWITCHED ALL PUMPS OFF AND QTY LOSS STOPPED. CA FOUND LEAK ON ADP PRESSURE & CASE DRAIN FILTER MODULE. REPLACED PACKINGS AND LEAK CHECK THEN OK.

Part: OXYGEN SYSTEM — MISSING (CABIN) · airframe 49,371 hrs · 7,581 cycles

DURING INSPECTION OF OXYGEN MASK EO PER AD FOUND NO OXYGEN EQUIPMENT IN PSU ABOVE SEATS 20 A AND B. NO OXYGEN GENERATOR OR MASKS OR ANYTHING. EO 1-85011-12AD REPLACED PSU AND OXYGEN GEN. ON, OFF A 351001259, B 353201010.

Part: SMOKE — DETECTED (FWD GALLEY) · airframe 48,634 hrs · 7,466 cycles

ODOR OF BURNING PLASTIC/ELEC. SMOKE SEEMED TO COME FROM FWD GALLEY CEILING. PULL ALL FWD GALLEY C/B. ODOR DISAPPEARED IN ABOUT TEN MINUTES. PUSH C/B BACK IN. NO SMELL NOTED. A/C OK FOR SVC.

Part: WIRE — BROKEN (NR 2 ENGINE) · airframe 48,353 hrs · 7,429 cycles

RIGHT ENGINE HPSOV ON TAKEOFF ROLL, RETURN TO CVG. . REPAIRED BROKEN WIRE ON D4208P RAN ENGINE LEAK AND OPS CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 48,353 hrs · 7,429 cycles

ON T/O GOT RT HP BLEED AND FOLLOWED POM. RETURNED TO CVG. REPLACED NBR 2 ENG HPSO VALVE PER MM 36-11-07-4-03 NO FURTHER FAULTS.

Part: LINE — SEVERED (HYD SYSTEM) · airframe 48,155 hrs · 7,393 cycles

AFTER LANDING GOT ANTI-SKID EICAS FOLLOWED SHORTLY BY RT HYD QTY EICAS. FOUND LT GEAR STRUT DOOR DAMAGED AND ONE HYD LINE SEVERED. REPLACED LINE.

Part: COMPUTER — MALFUNCTIONED (E/E BAY) · airframe 48,109 hrs · 7,384 cycles

A 1200 LB FUEL IMBALANCE RT SIDE LOW WHILE BURNING OUT OF CTR TANK. CORRECTED, 10 MIN LATER SAME IMBALANCE. FMC INITIALLY 1000 MORE THAN TOTALIZER. TOTALIZER INDICATED 700 LBS OVERBURN FROM FLT PLAN, BY 35 MIN LATER TOTAL WAS 4000 LB LESS THAN FMC. FUEL NOW 2500 LB OVERBURN FROM FLT PLAN. REBAL FUEL 600 LB SPLIT TILL LANDING. THEN 2000 LB SPLIT AT GATE. COCKPIT NOW READS 3500 LB HIGHER ON RT SIDE. REPLACED FQIS COMP AND COCKPIT IND SUMPED ALL TANKS. ALL OPS CHECK NORMAL.

Part: BATTERY — INOPERATIVE (ROWS 1 - 5) · airframe 45,867 hrs · 6,997 cycles

EMERGENCY TRACK LIGHTING IN B/C ROWS 1 THRU 5 LT AND RT SIDE INOP. REPLACED BATTERY PWR SUPPLY AND BATTERY, LIGHTS CKS NORMAL. ETOPS CATEGORY ''F'': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: COUPLING — BROKEN (RT WING) · airframe 43,814 hrs · 6,627 cycles

FUEL LEAK, PUSHED WITH 137,000 FUEL. ON TAXI OUT, GROUND CONTROL REPORTED WHITE SMOKE FROM RIGHT ENGINE. FUEL DROPPEDTO 127000. FUEL USED STILL SHOWED .3 LEFT AND RIGHT. FUEL LOAD AT SHUTDOWN: L/40.8 C/50.7 R/36.2 TOTAL/127.7. INITALL LOAD: L/40.8 C/55.8 R/40.9 TOTAL/137.5. FOUND FUEL LEAKING OUT OF PANEL TO DRY BAY AREA I/B OF RT ENG PYLON. REMOVED PANEL AND FOUND FUEL FEED LINE COUPLING NUT BROKEN. REPLACED FUEL FEED LINE PER MM AND REPLACED ALL O-RINGS. SECURED COUPLINGS, ENG DRY MOTORED. PERFORMED LEAK CHECK, NO LEAKS. CLOSED ACCESS PANEL.

Part: COUPLING — FAILED (RT WING) · airframe 43,814 hrs · 6,627 cycles

ON TAXI REPORTED MASSIVE FUEL LEAK RT WING. MTC TRACED LEAK TO BROKEN COUPLING IPC REF 28-22-07-07 SHEET 2 ITEM 345 (P/N 343T0010-44). REPLACED FUEL FEED LINE AND ASSOCIATED COUPLING AND O-RINGS. LEAK CHECKED FUEL LINES, NO LEAK DETECTED. ETOPS CATEGORY ''F'': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: HARNESS — BROKEN (ROW 22FG)

SEAT MOUNTED PROX LIGHTING SYSTEM INOP AT 22FG. FOUND BROKEN WIRE AT SEAT HARNESS TO SIDEWALL CONECTOR. FWD TO MCO AND PLACARD PER MEL 33-51-03B.

Part: LENS — MISSING (ROW 6AB)

SEAT MOUNTED PROXIMITY LIGHTING AT 6AB MISSING 1 LENS (WHITE) AND BOTH BULBS. RELAMPED LIGHT AND REPLACED MISSING BULBS, OPERATIONAL CHECK GOOD.

Part: WIRE — CHAFED (PYLON)

MSU TO CHECK FOR DAMAGED/CHAFFING WIRING FOR LT/RT ENG EEC CONTROL WIRES. C/W PYLON WIRE INSPECTION OF CHAFFED WIRES, FOUND DAMAGE TO OUTER INSULATION REPAIRED CHAFFED INSULATION BOTH ENGS PER BOEING STD PRACTICE 20-10-13.

Part: POWER SUPPLY — INOP (ROW 4B)

LT SIDE BUSINESS CLASS EMERGENCY LIGHTS INOP. REPLACED CHARGER, OPS OK. FOUND SEAT 4AB LIGHTS INOP. REPAIRED WIRING HARNESS OPS OK.

Part: LIGHT — INOPERATIVE (ROW 3-10)

SEAT MOUNTED PROXIMITY LIGHTING INOP AT SEATS 3AB AND 10AB. ALSO, LIGHT LENS COVERS MISSING. RELAMPED PROXIMITY LIGHTING AT SEAT ROWS 3AB AND 10AB. REPLACED MISSING LENS COVERS, LIGHTING OPS CKS OK.

Part: LIGHT — INOPERATIVE (ROW 30 FG)

SEAT MOUNTED PROXIMITY LIGHTING INOP AT SEAT ROW 30FG. FWD TO MCO AND PLACARD PER MEL 33-51-03B. RELAMPED SAME, NO HELP.

Part: LIGHT — INOPERATIVE (ROW 35 AB)

SEAT MOUNTED PROXIMITY LIGHT INOP (1 WHITE) AT SEAT ROW 35AB FWD TO MCO AND PLACARD PER MEL 33-51-03B. RELAMPED SAME, NO HELP.

Part: ENGINE — FAILED (NR 1)

FOUND METAL ON NR 3 BEARING CHIP DETECTOR. REPLACED ENGINE.

Part: ACTUATOR — LEAKING (RUDDER)

A/C 178 ATB FOR PARTIAL LOSS OF LEFT SYS HYDRAULIC FLUID, REPORTED IN FLT. FOUND RUDDER RATIO ACT EHV LEAKING. REPLACED SAME, OPS CHECK.

Part: CONTROL MODULE — LEAKING (RT HORIZ STAB)

C HYDRAULIC SYSTEM LEAKING IN CRUISE. QTY DROPPED TO 0.32. DURING GEAR/FLAP EXTENSION QTY DROPPED TO 0.08. CREW DECLARED EMERGENCY. MX FOUND RT STAB TRIM CONTROL MODULE LEAKING. REPLACED RIGHT STAB TRIM CONTROL MODULE. OPS CHECK GOOD.

Part: FUSE — BLOWN (CABIN)

EMERGENCY TRACK LIGHTING IN FIRST CLASS OUT. REPLACED FUSES, OPS CHECK OK.

Part: CONTROLLER — FAILED (COCKPIT)

AT 29,000 FT HEARD LOUD SQUEAL IN COCKPIT, ALSO CABIN DIFFERENTAL GAUGE CLOSE TO RED BAND. FLIGHT ATTENDANTS REPORTED LOUD HISS FROM 12AB AREA. NOISE QUIT WHILE DESCENDING THROUGH 18,000. SYSTEM INOP IN AUTO 2, MANUAL CONTROL WAS OK. RETURNED TO JFK. REPLACED CONTROLLER AND SELECT PANEL, SYSTEM CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EMERGENCY ESCAPE SLIDE NO TEST SYSTEM ONE. REPLACED LEFT ESCAPE SLIDE BATTERY PACK AND CHARGER. OPERATION CHECKS GOOD. NO HISTORY. REPLACED BATTERY PACK, CHARGER, AND K838. OPS CHECK OK.

Part: ENGINE — MALFUNCTIONED (NR 2)

OIL QTY DROPPED TO 5 QTS ON RT ENG FOR MOST OF FLT. ON DESCENT INTO ATL, DROPPED TO 2 QTS AND RETURNED TO 5 AFTER LEVEL OFF. DUE TO HISTORY, ENGINE WAS REPLACED AND ROUTED TO SHOP.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

NR 2 ENGINE COMPRESSOR STALLED ON T/O. THROTTLED BACK, ENGINE OPERATED NORMAL AT LOW POWER SETTINGS. ENGINE WAS NOT SHUTDOWN, OVERTEMP 684 DEGREES. REPLACED NR 2 ENGINE AND ROUTED TO SHOP.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

AT APPROX 1,000 FEET AFTER TAKEOFF IN FRA, THE LT ENGINE HAD A SERIES OF COMPRESSOR STALLS, OVERTEMP WARNING CAME ON, TEMP WENT TO 737 DEGREES, POWER DROPPED BACK TO NEAR IDLE. WITNESSES REPORTED FLAMES FROM LEFT ENGINE AND BAD VIBRATIONS. THE ENGINE WAS SHUT-DOWN AND A/C RETURNED TO FRA. FUEL DUMP WAS USED. REPLACED NR 1 ENGINE PER CARD DECK 1T148. PRE-FLIGHT CHECK AND OVERWEIGHT LANDING INSPECTION PERFORMED.

Part: COMPRESSOR — STALLED (NR 1 ENGINE)

AT 1,100 FT AFTER T/O, THE LT ENG COMP STALLED AND EGT WENT TO 652 DEGREES. PWR WAS REDUCED TO IDLE AND ENG OPS NOR TO LANDING. REVERSERS NOT USED, OVERWT LANDING ACCOMP VSI 300 FPM SPEED AT 170, LANDING SMOOTH. EVIDENCE OF BIRD STRIKE ON NOSE COWL, PERFORMED BORE OF ENG, FOUND OK, PERFORMED HIGH POWER RUNUP AND ALL OK.

Part: QTY TRANSMITTER — MALFUNCTIONED (CENTER HYD RES)

DURING CRUISE FL 290, CENTER HYDRAULIC QUANTITY LIGHT CAME ON WITH DROP IN BRAKE PRESSURE. ALSO, HAD RESERVE BRAKES AND STEERING LIGHT COME ON AND OFF. THEN QTY INDICATION FLUCTUATIONS. DIVERTED JFK, LANDED WITHOUT INCIDENT. VERIFIED HYDRAULIC QTY FULL, REPLACED CENTER SYSTEM QTY TRANSMITTER. OPERATION NORMAL. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK

Part: SENSOR — FAILED (LT LE SLAT)

DURING CLIMB-OUT, HAD SLAT ASSYMETRY LIGHT VISUAL CHECK OK SLATS APPEARED UP. ACCOMPLISHED ABNORMAL PROCEDURES, RETURNED JFK. THE SLAT LIGHT CAME ON AT FLAPS 1 DEGREE TO FULL UP. INTERROGATED PSEU, HAD FAULT CODE 280, LEFT OUTER SLAT NR 5 SENSOR. REPLACED SENSOR OPERATION NORMAL.

Part: COMPRESSOR — STALLED (NR 2 ENGINE)

DURING TEST FLIGHT FOR ETOPS ENGINE CHANGE ACCEPTANCE, NR 2 ENGINE HAD COMPRESSOR STALLS ON TAKEOFF. RETURNED CPH. ENGINE WAS REMOVED AND ROUTED TO SHOP.

Part: ENGINE — FAILED (NR 2)

ON PUSHBACK, DURING ENGINE START DID NOT HAVE N2 ROTATION. RETURNED TO BLOCK. STARTER AND TRANSMISSION TOWER SHAFT WAS REMOVED DURING TROUBLESHOOTING. DETERMINATION WAS MADE TO REPLACE ENGINE FOR RETURN TO SERVICE AND CONTINUE TROUBLESHOOTING STARTER AND TRANSMISSION PROBLEMS ON GROUND.