N191DN

Part: LENS — DAMAGED (ZONE 200) · airframe 122,851 hrs · 18,324 cycles

EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING LOCATIONS:605. READJUSTED EMERGENCY HANDLE COVER CLAMP AS NECESSARY. OK FOR SVC. (1296424)

Part: TARGET — OUT OF RANGE (ZONE 800) · airframe 121,934 hrs · 18,170 cycles

DURING ENGINE START THE L FWD ENTRY DOOR EICAS AND OVERHEAD LIGHT ILLUMINATED. FA SAID SLIDE LIGHT WAS FLASHING ON DOOR. FOUND DOOR CLOSED SENSOR S194 TARGET OUT OF RANGE. ADJUSTED S194 . NO ADJUSTMENT REQUIRED FOR S195. REFERENCE AMM TASK 52-71-00 (7075034)

Part: FLAP SYSTEM — FAULTED · airframe 120,190 hrs · 17,896 cycles

SHIP 0191 -FCNT/DE- WHILE IN CRUISE AND THEN ON APPROACH WHEN SELECTING 15* OF FLAPS, THE FLIGHT CREW NOTED A "T/E FLAP SHUTDOWN" MESSAGE WHICH WAS ACCOMPANIED WITH A "T/E FLAP DISAGREE" EICAS MESSAGE. A GO-AROUND WAS PERFORMED AND THE QRH WAS COMPLIED WITH. ALT FLAPS 20* WAS SELECTED FOR LANDING AND ATC DECLARED AN EMERGENCY FOR THE CREW. THE LANDING WAS UNEVENTFUL. CORRECTIVE ACTION: MAINTENANCE WAS NOT ABLE TO IDENTIFY ANY SPECIFIC FAULT. THEY CHECKED FLAP POSITION SENSOR VALUES AND REPLACED THE CENTER FLAP/STAB POSITION MODULE (FSPM) AND FLAP/SLAT SHUTOFF VALVE. (LP #5783903)

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 119,416 hrs · 17,739 cycles

SHIP 191 L/H WING NO.3 SLAT EXTERNAL SKIN FWD EDGE FASTENER HOLE FOUND CRACK 41.5" TO O/B EDGE. CORRECTIVE ACTION: L/H WING NO.3 SLAT EXTERNAL SKIN AND RIB AT OSS792 WAS FOUND CRACK. TRIMMED OUT THE DAMAGE SKIN AND THE CRACK AREA ON THE RIB . PERFORMED REPAIR AS PER PRI:623244-14 REV.0. COMPARED AND COMPLIED WITH ER/A: 623244-14 REV.ORIGINAL NO DEVIATION. (0732508)

Part: SKIN — CRACKED (ZONE 500 SLAT) · airframe 119,416 hrs · 17,739 cycles

SHIP 191 L/H WING NO.3 SLAT EXTERNAL SKIN FWD EDGE FASTENER HOLE FOUND CRACK 41.5" TO I/B EDGE. CORRECTIVE ACTION: L/H WING NO.3 SLAT EXTERNAL SKIN AND RIB AT OSS723 WAS FOUND CRACK. TRIMMED OUT THE DAMAGE SKIN AND THE CRACK AREA ON THE RIB . PERFORMED REPAIR AS PER PRI:623243-14 REV.0. COMPARED AND COMPLIED WITH ER/A: 623243-14 REV.ORIGINAL NO DEVIATION. (0732500)

Part: WINDOW — TWISTED (ZONE 800) · airframe 119,336 hrs · 17,727 cycles

SHIP 191 EMERGENCY EXIT WINDOW ON RT SIDE HANDLE TWISTED. CORRECTIVE ACTION: AFT RH OVERWING EXIT DOOR INTERIOR GRAB HANDLE RE-ALIGNED OK. NO FURTHER DEFECTS NOTED. (6689702)

Part: LIGHT — INOPERATIVE (2R DOOR) · airframe 119,312 hrs · 17,723 cycles

SHIP 191 2R DOOR SLIDE ARMED INDICATING LIGHT INOP/STAYS ON. CORRECTIVE ACTION: FCP VERIFIED BY MTC. COULD NOT DUPLICATE FAULT. OPS TEST GOOD REF B767-300 AMM 52-73 (0690908)

Part: SEAL — LEAKING (HYD SYSTEM) · airframe 117,524 hrs · 17,443 cycles

MISC/DE- CREW ELECTED DE DUE TO LT HYD QTY INDICATION DECREASE DURING FLIGHT. C/W QRH AND LANDED AND TAXIED IN NORMALLY. REPLACED PLATE AND SEALS BETWEEN EHSV AND NUMBER 12 SPOILER ACTUATOR. SERVICED HYD AND LEAK CHECKED. RTS. (LP 6080089)

Part: DISPLAY — FAILED (ADI) · airframe 117,334 hrs · 17,419 cycles

SHIP 0191 -DIV- TO CDG DUE TO CAPT ADI DISPLAY FAILED. QRH C/W AND ALT SYMBOL GENERATOR SELECTION NO HELP. CORRECTIVE ACTION: REPLACED CAPT ADI DISPLAY. (6080022)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 115,160 hrs · 17,091 cycles

SHIP 191 SEAT 41F SEAT MOUNTED EMERGENCY ESCAPE PATH LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED SEAT ESCAPE PATH LIGHT ASSY PER B767 AMM 33 -51. OPS NORMAL. (5550172)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 115,160 hrs · 17,091 cycles

SHIP 191 SEAT 4D, 5D, &6D SEAT MOUNTED ESCAPE PATH LIGHTS INOP. CORRECTIVE ACTION: SECURED CONNECTOR, EMERGENCY ESCAPE PATH LIGHTS WORKING NORMAL. (5550173)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 115,117 hrs · 17,083 cycles

SHIP 191 EXIT SIGN OVERHEAD ROW 20 RIGHT AISLE INBOARD SCREW AND NUT LOOSE. CORRECTIVE ACTION: EXIT SIGN ON ROW 20 RH ATTACHED IN CORRECT POSITION IAW B767- 300AMM 33-50 FOUND SATIS (5550150)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,853 hrs · 17,035 cycles

SHIP 191 2R DOOR ARMING FLAG INOP. R/R SLIDE ARMED INDICATOR PER B767 AMM 52-11 OPS CK GOOD MEL/ PLAC RMVD (0097535)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,459 hrs · 16,964 cycles

SHIP 191 1L DOOR ARMED LIGHT ON DOOR INOP. CORRECTIVE ACTION: OPS CK 1L DOOR CLOSE AND ARM GOOD NO DEFECTS (4428140)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,108 hrs · 16,908 cycles

SHIP 191 ALT FL 360 INTERMITTENT ALT DISAGREE HORN AND WARNING, R AP ENGAGED . L ALT AROUND 36220 FT , RT ALT 36000 FT. AFTER DESCENT TO FL 330 L ALT CREEPING UP TO 33300 FT WITH RT ALT LEVEL AT 33000 AND STANBY ALT AT 33650 FT . L ALT RESETTLED AT 33200 . CONTINOUS ALT DISAGREE. CORRECTIVE ACCTION: REPLACED LT ADC PER AMM 34-12. (4613175)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 114,026 hrs · 16,897 cycles

SHIP 191 R1 DOOR ARMING FLAG IN INOP. CORRECTIVE ACTION: FOUND LOOSE SCREW ON TERMINAL. SECURED LOOSE HARDWARE OK FOR SERVICE. MEL/PLAC REMOVED M PROC REVERSED. (4613124)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,862 hrs · 16,874 cycles

SHIP 191 ATTENDANT PANEL SWITCH LIGHT INOP - SWITCH STILL OPERATES / LOCATIONS:DOOR. CORRECTIVE ACTION: OPS CHECK OF 2L DOOR WARNING LIGHT PER B767 AMM 52-71. ALL CHECKS NML (2969668)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,816 hrs · 16,868 cycles

SHIP 0191 -DIV- TO TER DUE TO CREW O2 PRESSURE ZERO PRIOR TO ENTERING ATLANTIC TRACK. CORRECTIVE ACTION: FOUND SECOND OBSERVER OXYGEN MASK BOX SUPPLY HOSE RUPTURED. REPLACED HOSE AND CREW O2 BOTTLE. (4569744)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,565 hrs · 16,831 cycles

SHIP 0191 -MISC/DE- CREW ELECTED DE DUE TO NLG DOWN INDICATION INOPERATIVE. LANDED WITHOUT ISSUE. CORRECTIVE ACTION: JFK MTC C/W ERA FOR INSTALLATION OF ALTERNATE PART INDICATOR. 10-DAY MONITOR RAISED FOR PERMANENT REPAIR. (4918540)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,348 hrs · 16,804 cycles

SHIP 191 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:1-1. CORRECTIVE ACTION: SLIDE INDICATOR LIGHT CHECKED SATIS (2900339)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 113,293 hrs · 16,797 cycles

SHIP 191 2 LEFT ARMING LIGHT ON 1L PANEL INOP. CORRECTIVE ACTION: R AND R 2L DOOR ARMED LIGHT PER B767-300 AMM 33-22. OPS CHK GOOD . MEL AND PLACARD REMOVED. OK FOR SVC (4924316)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,623 hrs · 16,698 cycles

SHIP 191 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:20B. CORRECTIVE ACTION: REINSTALLED EMERGENCY LIGHT ASSY AT 20B AISLE. OPS CHK GOOD PER B767-300 AMM 33-51. (2817090)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,401 hrs · 16,666 cycles

SHIP 0191 -ATB- BIRD STRIKE OCCURRED SHORTLY AFTER LIFTOFF. F/O INSTRUMENTS AFFECTED UNABLE TO CONTINUE RVSM. CORRECTIVE ACTION: PERFORMED OVERWEIGHT LANDING INSPECTION. R/R F/O PITOT PROBE.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,333 hrs · 16,651 cycles

SHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN AFT AREA AT LH SIDE ABOUT FSS 245. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 245 AS PER B767-300 SRM55-30-01-2R-1&SRM51- 70-10-2R-4 (2767859)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,333 hrs · 16,651 cycles

SHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN AFT AREA AT LH SIDE ABOUT FSS 170. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 170 AS PER B767-300 SRM 55-30-01-2R-1& SRM 51-70-10-2R-4 (2767866)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 112,333 hrs · 16,651 cycles

SHIP 191 FOUND DELAMINATION ON VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN MID AREA AT LH SIDE ABOUT FSS 65. CORRECTIVE ACTION: VERTICAL STABILIZER AUXILIARY SPAR TO FRONT SPAR SKIN REPAIRED AT LH SIDE ABOUT FSS 65 AS PER B767-300 SRM 55-30-01-2R-1 & SRM 51-70-10-2R-4 (2767844)

Part: NONE — NONE · airframe 111,655 hrs · 16,509 cycles

SHIP 191 #1 ENG PYLON IS CRACKED ON INBD SIDE AT FWD ACCESS HOLE. CRACK IS APPROX 1.75 INCHES- MARKED. CORRECTIVE ACTION: DAMAGE AREA REPAIRED PER B767 SRM 54-53-01. (2634216)

Part: NONE — NONE · airframe 111,599 hrs · 16,498 cycles

SHIP 191 RED EMERGENCY LT AT 1R DOOR. CORRECTIVE ACTION: INSTALLED RED EMERGENCY WALL-MOUNTED PROXIMITY LIGHT LENS AT 1R DOOR PER B767 AMM 33-51 (9477653)

Part: NONE — NONE · airframe 111,594 hrs · 16,495 cycles

SHIP 191 SEAT MOUNTED ESCAPE PATH LIGHTS INOP AT SEAT 22F & 39F. CORRECTIVE ACTION: SEAT 22F MATE-N-LOK CONNECTOR BROKEN, REPLACED MALE CONNECTOR PER SWPM 20-42. SEAT 39F CONNECTOR PINS WORN. RE-PINNED CONNECTOR & WIRES AT 39F PER SWPM 20-42. SEATS 22F & 39F NOW OPERATING NORMAL. OK FOR SERVICE. (9477627)

Part: WARNING LIGHT — UNKNOWN (L2 DOOR SLIDE) · airframe 111,239 hrs · 16,425 cycles

L2 DOOR SLIDE LIGHT BLINKS WHEN DISARMED. T/S PER WDM 52-71-11 AND 767 MM 52-71-01-964-211 STEPG FOUND DOOR GIRT BAR SENSOR S212 CORRECTLY ADJUSTED. PERFORMED OPS CK OF L2 DOOR ARM MULTIPLE TIMES WITH GALLEY LIGHTS IN VARIOUS CONDITIONS AND CONFIGURATIONS OPS NORMAL.

Part: SLIDE — NONE (L2 DOOR) · airframe 111,239 hrs · 16,425 cycles

L2 DOOR SLIDE BLINKS WHEN DISARMED. CONFIRMED SLIDE OPERATES NORMAL AND ITS ERRONEOUS INDICATION. M ACTIONS C/W. PLACARD INSTALLED. AIRCRAFT OK FOR SERVICE.

Part: NONE — NONE (SLIDE INDICATOR) · airframe 110,854 hrs · 16,347 cycles

SHIP 191 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:607. CORRECTIVE ACTION: OPERATED DOOR ARM/DISARM 2L SIX TIMES. OPS NML, OK FOR SVC (2522670)

Part: WIRE — FAULTED (SENSOR) · airframe 110,593 hrs · 16,285 cycles

SHIP 191 -ATB- DUE TO LE ASSYM INDICATION AFTER TAKEOFF. MTC C/W OVERWEIGHT LANDING INSPECTION. PSEU FAULT S276. CONFIRMED WIRING FAULT NEAR SENSOR. R/R SENSOR. A/C RTS. (9821244)

Part: NONE — NONE · airframe 110,365 hrs · 16,235 cycles

SHIP 191 ELECTRICAL SMELL ON FIRST OFFICER SIDE OF COCKPIT CONCENTRATED SEAT PAN LEVEL. CORRECTIVE ACTION: ACCOMPLISHED GVI INSPECTION/ SMELL BEHIND PANELS P61 AND ACCESS P-6 NO EVIDENCE OF ELECTRICAL SMELL, ALSO INSPECTED E/E AND FWD ACCESSORY NO SIGNS OF ANY SMELL. CHECKED115 VAC ON RT EFB OUTLET , OPEN ACCESS PANEL REMOVED NO EVIDENCE FROM ARCING , BURNS , AND WIRING INSULATION IAW AMM 20-60 NO DAMAGE FOUND. IT WAS DRAINED 1 USQ OIL FROM EACH ENGINE REMAINED WITH 23 QTS OIL INDICATION, ALSO CHECKED IDG OIL LEVEL OK IAW B767-300 AMM 12-13. RAN BOTH ENGINES TWICE FOR A PERIOD MORE THAN 15 MIN, AND CYCLED ENGINE BLEEDS AND RECIRCULATION FANS DESCRIBED ON AMM21- 00-21 , TESTED WINDOWS/PITOTS/FOOT HEATERS DURING ALL RAN TIME, NO SOURCE FROM ELECTRICAL SMELL . ALSO LET ALL GALLEYS FWD/AFT OVENS AND CHILLERS ON , NO EVIDENCE FROM SMOKE / FUMES OR ELECTRICAL SMELL. MCC AWARE FROM ALL THESE STEPS. (9551470)

Part: NONE — NONE · airframe 110,289 hrs · 16,223 cycles

SHIP 191 DOOR 1L SLIDE INDICATOR LIGHT NOT WORKING. CORRECTIVE ACTION: NO TROUBLE FOUND OPS NML. (8989395)

Part: LIGHT — MISINSTALLED · airframe 108,968 hrs · 16,006 cycles

SHIP 191 DURING INSPECTION OF EMERGENCY LIGHTS DURING SVC FOUND EMERGENCY LIGHTS NOT INSTALLED PROPERLY AT SEATS 27F, 28F, AND 35F. CORRECTIVE ACTION: RE-SECURED PATH LIGHTING AS REQUIRED PER B767 AMM 33-51. OK FOR SVC. (8504235)

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 108,327 hrs · 15,888 cycles

SHIP 191 OVHD EMERGENCY LIGHTS UNARMED ANNUNCIATOR LES MISSING. CORRECTIVE ACTION: INSTALLED REPLACEMENT LENS ASSY. EMER LIGHTS UNARMED ANNUCIATOR OPS NML PER B767-300 AMM 33-51. (8849038)

Part: NONE — NONE · airframe 108,101 hrs · 15,831 cycles

SHIP 191 ESCAPE PATH LT 25 A-B DAMAGED. CORRECTIVE ACTION: REMOVED AND REPLACED ESCAPE PATH LIGHTING AT SEAT 25A-B PER CMM 25-28-89. (8152210)

Part: NONE — NONE · airframe 107,966 hrs · 15,788 cycles

SHIP 191 SEATS 25AB + 27GF EEPLS ITS ASSEMBLY LOOSE. CORRECTIVE ACTION: RESECURED LOOSE EMERGENCY LIGHT SHROUDS PER B767 AMM 25-25. (8365221)

Part: NONE — NONE · airframe 107,725 hrs · 15,737 cycles

SHIP 191 AFT LEFT DOOR ARM INDICATION INOP, CORRECTIVE ACTION: REMOVED AND REPLACED 2L ENTRY DOOR CLOSED SENSOR. ARM LIGHT CHECKED GOOD PER B767 AMM 52-73 (8278926)

Part: SENSOR — OUT OF LIMITS (SLAT SYSTEM) · airframe 107,725 hrs · 15,737 cycles

SHIP 0191 -MISC/DE- EICAS MESSAGE (LE SLAT ASYM) DISPLAYED WITH ASSOCIATED LIGHT WHEN FLAPS 25 SELECTED DURING APPROACH. CREW DECLARED EMERGENCY, C/W QRH AND LANDED. REPLACED H7 OUTBOARD UP SLAT SENSOR S305. (8278924)

Part: NONE — NONE · airframe 107,640 hrs · 15,716 cycles

SHIP 191 2L "SLIDE" ARM LIGHT INOP, CORRECITIVE ACTION: REMOVED AND REPLACED DOOR 2L SLIDE ARMED LIGHT REF. B767 WDM 52- 71-11.OPS NORMAL. (8204766)

Part: NONE — NONE · airframe 107,117 hrs · 15,599 cycles

SHIP 191 EMERGENCY LIGHT RT SIDE AFT OF WING INOP. CORRECTIVE ACTION: REMOVED BULB CLEANED CONTACT OPS CHECKS GOOD (7939381)

Part: HOUSING — BROKEN (CABIN) · airframe 106,763 hrs · 15,528 cycles

SHIP 191 EMERGENCY PATH LIGHTING HOUSING BROKEN NOT ATTACHED AT SEAT 19A, 28F, 38F. CORRECTIVE ACTION: REPLACED TRIM/HOUSING AT SEATS 19A, 28F AND 38F AND SECURED HOUSING. SYSTEM OPERATION IS NORMAL. (LP 8025335)

Part: LIGHT — MISSING (CABIN) · airframe 106,818 hrs · 15,539 cycles

SHIP 191 EMERGENCY ESCAPE PATH LIGHTS FOUND MISSING AT 40F. CORRECTIVE ACTION: REPLACED LIGHT ASSEMBLY. MCO/PLACARD REMOVED. SYSTEM OPERATION IS NORMAL. (LP 8025336)

Part: SHROUD — DAMAGED (EMERGENCY LIGHT) · airframe 106,581 hrs · 15,494 cycles

SHIP 191 EMERGENCY PATH LIGHTS DAMAGED AT 14 A/B AND 22 A/B. CORRECTIVE ACTION: REPLACED EMERGENCY PATH LIGHT SHROUDS. SYSTEM OPERATION IS NORMAL. (LP 79017424)

Part: SKIN — DENTED (BS 654 S4-5L) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 LEFT UPPER EXTERNAL FUSELAGE STA654+110 TO STA654+121 S4L TO S5L FOUND DENT. REPAIRED PER SRM 53-00-01. (LP 1870137)

Part: SPAR — DELAMINATED (VERTICAL STAB) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND LEFT INTERNAL VERT STAB FROM FSS92.25 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865361)

Part: SPAR — DELAMINATED (VERTICAL STAB) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND RIGHT INTERNAL VERT STAB FROM FSS92.25 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865357)

Part: SKIN — DELAMINATED (NR 5 SLAT) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND DELAMINATION SIGN FROM I/B EDGE 63INCH #5 SLAT UPPER SURFACE PREVIOUS REPAIR AND REPAIRED PER SRM. (LP 1865371)

Part: SPAR — DELAMINATED (VERTICAL STAB) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND LEFT VERT STAB FROM FSS95 TO FSS145 FROM FRONT SPAR TO AUX SPAR FOUND DELAMINATION. AREA REPAIRED PER SRM 55-30-01 AND 51-70-10. (LP 1865369)

Part: SKIN — WORN (NR 5 SLAT) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND #5 SLAT LOWER SURFACE T/E AREA WORN FROM I/B EDGE 40". AREA REPAIRED PER SRM. (LP 1865372)

Part: FITTING — CRACKED · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND 1EA CRACK ON RH LOWER UNDER -WING LONGERON FITTING. LONGERON FITTING REPLACED. (LP 1864036)

Part: FRAME — CRACKED (BS 883) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECITON FOUND 01EA CRACK APPROX 0.200 INCH IN LENGTH ON RH BS883.5 FRAME INNER CHORD TRANSITION RADIUS. CRACKED REPAIRED. (LP 1861056)

Part: STRINGER — DENTED (BS 434-456 S31L) · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND FWD CARGO COMPARTMENT FOUND 01EA STRINGER UPPER SURFACE DENT AT S-31L BETWEEN STA434 TO STA 456. REPAIRED PER SRM. (LP 1861086)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

SHIP 191 DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPATMENT FOUND SHEAR TIE CORROSION AT STA1197+22 BETWEEN STR38R AND STR37R. SHEAR TIE REPLACEDL. (LP 1859614)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197 BETWEEN S-38R TO S-37R. REPLACED SHEAR TIE. (LP 1859603)

Part: SHEAR TIE — CORRODED (BS 742 S35-36R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA742 FOUND SHEAR TIE CORROSION BETWEEN STR 35R AND STR36R. REPLACED SHEAR TIE. (LP 1859617)

Part: SHEAR TIE — CORRODED (BS 1219 S36-37R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FOUND 1EA SHEAR TIE CORROSION AT STA1219 BETWEEN S-37R TO S-36R. SHEAR TIE REPLACED. (LP 1859597)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

WHILE IN CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+110 BETWEEN S-39L TO S-39R. SHEAR TIE REPLACED. (LP 1858789)

Part: SHEAR TIE — CORRODED (BS 676 S36-27L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA676 FOUND SHEAR TIE CORROSION BETWEEN STR36L AND STR37L. SHEAR TIE REPLACED. (LP 1858559)

Part: SHEAR TIE — CORRODED (BS 654 S37-38L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA654+44 FOUND SHEAR TIE CORROSION BETWEEN STR37L AND STR38L. REPLACED SHEAR TIE. (LP 1858527)

Part: SHEAR TIE — CORRODED (BS 654 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA654+22 FOUND SHEAR TIE CORROSION BETWEEN STR39L AND STR39R. SHEAR TIE REPLACED. (LP 1858546)

Part: SHEAR TIE — CORRODED (BS 654 S37-38L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

WHILE IN CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AT FWD CARGO COMPARTMENT STA654 FOUND SHEAR TIE CORROSION BETWEEN STR37L AND 38L. SHEAR TIE REPLACED. (LP 1858533)

Part: SHEAR TIE — CORRODED (BS 654 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENACE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA654+44 FOUND SHEAR TIE CORROSION BETWEEN STR39L AND STR39R. REPLACED SHEAR TIE. (LP 1858655)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+110 BETWEEN S-39R TO S-38R. SHEAR TIE REPLACED. (LP 1858543)

Part: SHEAR TIE — CORRODED (BS 632 S36-37L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA632 FOUND SHEAR TIE CORROSION BETWEEN STR36L AND STR37L. REPLACED SHEAR TIE. (LP 1858548)

Part: SHEAR TIE — CORRODED (BS 654 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 FWD CARGO COMPARTMENT STA654+121 FOUND SHEAR TIE CORROSION BETWEEN STR39L AND STR39R AND REPLACED. (LP 1858570)

Part: SHEAR TIE — CORRODED (BS 742 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND FWD CARGO COMPARTMENT STA742 FOUND SHEAR TIE CORROSION BETWEEN STR38R AND STR39R.REPLACED SHEAR TIE. (LP 1858523)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197 BETWEEN S-39R TO S-38R. REPLACED SHEAR TIE. (LP 1858530)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197 BETWEEN S-37R TO S-36R. REPLACED SHEAR TIE. (LP 1859615)

Part: SHEAR TIE — CORRODED (BS 1219 S37-38R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1219 BETWEEN S-38R TO S-37R. REPLACED SHEAR TIE. (LP 1859618)

Part: SHEAR TIE — CORRODED (BS 1175 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT STA1175 BETWEEN S-39R TO S-39L AFT CARGO COMPARTMENT AND REPLACED. (LP 1857377)

Part: SHEAR TIE — CORRODED (BS 1219 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1219 BETWEEN S-39R TO S-39L. SHEAR TIE REPLACED. (LP 1859620)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197 BETWEEN S-39L TO S-38. SHEAR TIE REPLACED. (LP 18587458)

Part: SHEAR TIE — CORRODED (BS 1395 S37-38R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1395 BETWEEN S-37R TO S-38R. REPLACED SHEAR TIE. (LP 1857461)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197+110 BETWEEN S-38R TO S-37R. REPLACED SHEAR TIE. (LP 1857440)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND ON SHEAR TIE CORROSION AT STA1197+44 BETWEEN S-39R TO S-39L. REPLACED SHEAR TIE. (LP 1857436)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01EA SHEAR TIE CORROSION AT STA1197+110 BETWEEN S-37L TO S-38L. REPLACED SHEAR TIE. (LP 1857518)

Part: SHEAR TIE — CORRODED (BS 1241 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT ON SHEAR TIE CORROSION AT STA1241 BETWEEN S-39L TO S-38L. REPLACED SHEAR TIE. (LP 1857422)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT STA1197+22 BETWEEN S-39R TO S-38R. REPLACED SHEAR TIE. (LP 1857381)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND ON SHEAR TIE CORROSION AT STA1197+132 BETWEEN S-39R TO S-38R. REPLACED SHEAR TIE. (LP 1857439)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE CORROSION AT STA1197+132 BETWEENS-36L TO S-37L. REPLACED SHEAR TIE. (LP 1857398)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND SHEAR TIE AT STA1197+44 BETWEEN S-39R TO S-38R WITH CORROSION LEVEL 2 . SHEAR TIE REPLACED. (LP 1857385)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND ON SHEAR TIE CORROSION AT STA1197+132 BETWEEN S-39L TO S-39R. REPLACED SHEAR TIE. (LP 1857437)

Part: SHEAR TIE — CORRODED (BS 1562 S39L/R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND 1 EACH SHEAR TIE CORROSION AT STA 1562 BETWEEN S-39L AND S-39R. REPLACED SHEAR TIE. (LP 1858409)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND SHEAR TIE WITH CORROSION LEVEL 2 AT AT STA1197 +22 BETWEEN S-38L TO S-39L. SHEAR TIE REPLACED. (LP 1857369)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197+1 32 BETWEEN S-38L TO S-39L.REPLACED SHEAR TIE. (LP 1857515)

Part: SHEAR TIE — CORRODED (BS 1175 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1175 BETWEEN S-39L TO S-38L. REPLACED SHEAR TIE. (LP 1859610)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND ON SHEAR TIE CORROSION AT STA1197+66 BETWEEN S-39R TO S-38R. REPLACED SHEAR TIE. (LP 1857426)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1197 BETWEEN S-39R TO S-39L. REPLACED SHEAR TIE. (LP 1857451)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT SHEAR TIE WITH CORROSION AT STA1197+88 BETWEEN S38L TO S39L. REPLACED SHEAR TIE. (LP 1857372)

Part: SHEAR TIE — CORRODED (BS 1219 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING CHECK MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND 01 EA SHEAR TIE CORROSION AT STA1219 BETWEEN S-39R TO S-38R. REPLACED SHEAR TIE. (LP 1859622)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA1197+66 BETWEEN S-39R TO S-39L. REPLACED SHEAR TIE. (LP 1857419)

Part: SHEAR TIE — CORRODED (BS 1241 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA1241 BETWEEN S-39R TO S-39L. REPLACED SHEAR TIE. (LP 1857405)

Part: SHEAR WEB — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT FOUND ON SHEAR TIE CORROSION AT STA1197+88 BETWEEN S-38R TO S-39R. REPLACED SHEAR TIE. (LP 1857434)

Part: SHEAR TIE — CORRODED (BS 1285 S39L-R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT SHEAR TIE CORROSION AT STA1285 BETWEEN S-39R TO S-39L. SHEAR TIE REPLACED. (LP 1857402)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO COMPARTMENT ON SHEAR TIE CORROSION AT STA1197+66 BETWEEN S-38L TO S-37L. SHEAR TIE REPLACED. (LP 1857430)

Part: SHEAR TIE — CORRODED (BS 566) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FORWARD CARGO COMPARTMENT. STA566 SHEAR TIE BETWEEN STR AND STR 39R . REPLACED SHEAR TIE. (LP 1857312)

Part: SKIN — CRACKED (BS1629-1654) · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION OF THE EXTERNAL SURFACE OF THE FUSELAGE SKIN MAINTENANCE FOUND CRACKS ON S-14AR BETWEEN FRAMES 1629 -1654 AND S-13AR BETWEEN FRAMES 1654-1678. REPAIRED PER SRM 53-80-01. (LP 1857296)

Part: SHEAR TIE — CORRODED (BS 654) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

SHIP 191 DURIING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT FORWARD CARGO COMPARTMENT. STA 654 AND REPLACED. (LP 1856328)

Part: SEAT TRACK — CORRODED (BS 1270-1285) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAITNENANCE FOUND CORROSION LEVEL 2 ON CABIN SEAT TRACK AT BS 1270 TO BS 1285 RBL 88.5 AREA . REPLACED SEAT TRACK. (LP 1856319)

Part: SHEAR TIE — CORRODED (BS 1219 S35-36R) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

SHIP 191 DURING INPSECTION MAINTENNACE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT STA1219 BETWEEN S-36R TO S-35R. SHEAR TIE REPLACED. (LP 1856332)

Part: SEAT TRACK — CORRODED (BS 1125-1131) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON CABIN SEAT TRACK AT BS 1125 TO BS 1131 RBL 88.5 AREA. SEAT TRACK REPAIRED PER SRM. (LP 1853553)

Part: SEAT TRACK — CORRODED (BS 1197 RBL 88) · corrosion level 2 · airframe 106,338 hrs · 15,448 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON CABIN SEAT TRACK AT BS 1197+55 RBL 88.5. SEAT TRACK REPAIRED PER SRM. (LP 1853562)

Part: INDICATOR — MALFUNCTIONED (SLIDE ARMING) · airframe 105,384 hrs · 15,226 cycles

AFT LEFT DOOR SLIDE LIGHT FLASHES ONCE EVERY 20 TO 40 SECS. CORRECTIVE ACTION: REPLACED LEFT AFT DOOR SLIDE ARMED LIGHT ASSEMBLY. MCO/PLAC REMOVED. SYSTEM OPERATION IS NORMAL.

Part: POWER SUPPLY — MALFUNCTIONED (EMERGENCY LIGHTS) · airframe 104,323 hrs · 15,017 cycles

FOUND RT MID CABIN EMERGENCY LGTS ALL DIM.REPLACED POWER SUPPLY BETWEEN SEATS 21FG AND 22FG. SYSTEM OPERATION IS NORMAL.

Part: ACTUATOR — FAILED (MLG) · airframe 103,985 hrs · 14,967 cycles

PERFORMED AN AIR TURN BACK DUE TO CREW REPORTING UNABLE TO RETRACT LEFT MAIN LANDING GEAR WITH ASSOCIATED GEAR DOOR AND GEAR DISAGREE INDICATIONS. MAINTENANCE FOUND A FAILED LEFT MAIN LANDING GEAR SIDE BRACE ACTUATOR. REPLACED THE ACTUATOR AND OPS CHECKED THE LANDING GEAR, FOUND NORMAL.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 103,985 hrs · 14,967 cycles

CREW REST EXIT SIGN AT LADDER AND COMMON AREA INOPERATIVE. FOUND ALL 24 BULBS BURNTOUT RELAMPED SAME

Part: LIGHT — DETACHED (CABIN) · airframe 102,082 hrs · 14,683 cycles

EMERGENCY SEAT MOUNTED LIGHTING AT 27F ARE INOPERATIVE. REATTACHED SEAT EMERGENCY PATH LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,558 hrs · 14,491 cycles

OVER WING EGRESS LIGHTS ARE INOPERATIVE. REPLACED M731 BATTERY PACK. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DIRTY (TE FLAP) · airframe 100,541 hrs · 14,488 cycles

TE FLAP ASYMMETRY WITHOUT TE FLAP ASYMMETRY LIGHT. DEFINITE LEFT ROLLING MOMENT WITH AUTOPILOT OFF. LANDED WITH LEFT FLAP BETWEEN ONE AND FIVE AND RIGHT FLAP AT FIVE. FLAPS CAME UP NORMALLY AFTER LANDING. REMOVED CONNECTOR FROM OUTBD LT FLAP TRANSMITTER POS 1. RAN FLAPS BACK UP ELECTRICALLY. THEN LOWERED FLAPS BACK DOWN HYDRAULICALLY. WAS ABLE TO DUPLICATED THE FLAP POSITION INDICATION ASYMMETRY THE PILOT SAW. NO FAULT LIGHTS. CLEANED AND RESECURED CONNECTOR. OPS CHKS GOOD

Part: DOOR — MISSING (LT TORQUE TUBE) · airframe 102,570 hrs · 14,752 cycles

LEFT INBD TORQUE TUBE SLOT DOOR MISSING ON ARRIVAL. FWD TO CDL 27-51-02. PANEL REPLACED.

Part: ACCESS DOOR — MISSING (NR 1 NACELLE) · airframe 99,962 hrs · 14,407 cycles

FOUND ON WALK AROUND- CIRCLE NACELLE STRUT ACCESS DOOR MISSING. NR 1 ENGINE I/B SIDE. REPLACED CIRCLE NACELLE STRUT ACCESS DOOR.

Part: SKIN — DAMAGED (LT WING) · airframe 99,930 hrs · 14,403 cycles

LEFT WING LOWER SKIN STR L-9.5 WSTA 879.2 - 990.2 HOLE DISCREPANCIES. REPAIRED PER ERA 574700-00.

Part: SKIN — DAMAGED (LT WING) · airframe 99,930 hrs · 14,403 cycles

LEFT WING LOWER SKIN STR L-9.5 WSTA 879.2 - 990.2 HOLE DISCREPANCIES REPAIRED PER ERA 574700-14AD.

Part: SKIN — CRACKED (PYLON) · airframe 99,888 hrs · 14,396 cycles

THE PYLON SKIN IS CRACKED AND BROKEN AT THE OPENING OF THE I/B ACCESS PANEL 436BR. REPAIRED PER SRM 54-53-01.

Part: NOT REPORTED — DEFECTIVE (WING) · airframe 99,888 hrs · 14,396 cycles

OPEN HOLE SCAN REVEALED DEFECTS IN THE 3RD HOLE FROM THE O/B END. C/W ERA 574676-14.

Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 99,953 hrs · 14,406 cycles

CORROSION LEVEL: 2 RIGHT FWD UPPER SKIN CORR ON HORIZ STAB BOX AT L/E. REPAIRED PER ERA 574592-14.

Part: SKIN — DAMAGED (RT WING) · airframe 99,888 hrs · 14,396 cycles

RIGHT WING LOWER SKIN STR 6.5 HAS HOLE. C/W ERA 574676-14.

Part: NONE — NONE (NONE) · airframe 111,378 hrs · 16,454 cycles

SHIP 191 AD 2018-11-14 AMOC APPROVAL REQUIRES REPETITIVE INSPECTIONS EVERY 12000 CYCLES OR 32000 HOURS (WHICHEVER OCCURS FIRST) PER ERA 574676-14AD. CORRECTIVE ACTION: ER/A 574676-14AD REVISED TO REV. A. ACCOMPLISH ER/A 574676-14AD REV A SECTION II INSPECTIONS. (0917214)

Part: SKIN — DAMAGED (RT WING) · airframe 99,888 hrs · 14,396 cycles

RIGHT WING LOWER SKIN STR L-9.5 WSTA 879.2 - 990.2 HAS HOLE. C/W ERA 574699-14.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 96,612 hrs · 13,950 cycles

CREW REPORTED THAT ON GEAR RETRACTION, THE RIGHT MAIN STAYED DOWN (GREEN) EICAS, DISCRETE MESSAGES, GEAR DISAGREE AND GEAR DOORS DISPLAYED QRH PROCEDURES COMPLETED. ALTERNATE GEAR EXTENSION USED. FOUND THE RIGHT MLG FLEXIBLE HYDRAULIC LINE THAT SUPPLIES THE TILT ACTUATOR, SIDE BRACE AND DRAG BRACE ACTUATORS WITH A HOLE. THE LINE WAS REPLACED.

Part: LIGHT — UNSECURE (SEATS) · airframe 96,284 hrs · 13,900 cycles

EMERGENCY SEAT MOUNTED EMERGENCY LIGHTS AT 41B AND 34F ARE INOPERATIVE. SECURED THE LIGHTS AT SHROUD. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 94,249 hrs · 13,592 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE. FOUND LIGHT ASSEMBLY LOOSEN AND SECURED.

Part: LIGHT — LOOSE (CABIN) · airframe 94,249 hrs · 13,592 cycles

EMERGENCY FLOOR LIGHTING INOPERATIVE AT 41B. FOUND LIGHT ASSEMBLY LOOSEN SECURED LIGHT ASSEMBLY. SYSTEM OPERATION NORMAL.

Part: SPEED BRAKE — MALFUNCTIONED · airframe 93,861 hrs · 13,528 cycles

SPEED BRAKE DIDN'T DEPLOY DURING LANDING FROM ARMED POSITION. PERFORMED AUTO SPEED BRAKE OPERATION TEST. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — LOOSE (CABIN) · airframe 93,675 hrs · 13,503 cycles

EMERGENCY SEAT MOUNTED LIGHTING ARE INOPERATIVE AT 40F. SECURED LIGHT MODULE. SYSTEM OPERATION IS NORMAL.

Part: FIRE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 93,585 hrs · 13,489 cycles

WHEN EXTENDING LANDING GEAR ON FINAL, RED WHEEL WELL FIRE ANNUNCIATOR ILLUMINATED AND THEN CLEARED AFTER 5 SECONDS LANDED NORMALLY. PERFORMED VISUAL INSPECTION ON WHEEL WELL AREA NO TROUBLE FOUND.

Part: BULKHEAD WEB — CORRODED (BS 955) · corrosion level 2 · airframe 82,704 hrs · 11,849 cycles

BS 955 LT REAR SPAR BULKHEAD WEB FOUND CORRODED. REPAIRED IAW ERA 530670-14.

Part: SKIN — CRACKED (RT WING) · airframe 82,704 hrs · 11,849 cycles

FOUND RT WING SKIN CRACKED, AT WS 996, S9.5R. REPAIRED IAW ERA 530669-14.

Part: BULKHEAD — CORRODED (BS 955) · corrosion level 2 · airframe 82,704 hrs · 11,849 cycles

BS 955 LT REAR SPAR BULKHEAD FOUND WITH CORRODED. REPAIRED IAW ERA 530670-14.

Part: PRESSURE DECK — CRACKED (BS 955) · corrosion level 2 · airframe 82,704 hrs · 11,849 cycles

CABIN OVERWING CANTED PRESSURE DECK INTERNAL CROSS DRAIN PATH FOUND CORRODED AT BS 955 BETWEEN LBL 2 - 10. REPAIRED.

Part: SKIN — CRACKED (LT WING) · airframe 82,704 hrs · 11,849 cycles

FOUND LT WING CRACKED WING STATION 966, S9.5L. REPAIRED IAW ERA 530688-14.

Part: TEE FITTING — CORRODED (BS 955) · airframe 82,704 hrs · 11,849 cycles

TEE FITTING FOUND CORRODED RT SIDE BS 955. TEE FITTING REPLACED.

Part: FRAME — CRACKED (BS 903.5) · airframe 82,704 hrs · 11,849 cycles

FRAME INNER CHORD TRANSITION RADIUS CRACKED. CRACK LENGTH APPROXIMATELY 0.32" ON RT SIDE BS 903.5. L89R BELOW WL 200, REPAIRED.

Part: FRAME — CORRODED (BS 1285) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

FRAME ANGLE FOUND CORRODED AT BS 1285 BETWEEN S19 - 20R. REPLACED.

Part: SEAT TRACK — CORRODED (BS 935) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 935 AND LBL 88.5. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1046) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 1046 AND RBL 88.5, FOUND CORRODED. REPAIRED.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

CENTER WING UPPER SKIN UPPER SURFACE AT REAR SPAR BS 955 AND LBL 86 AREA FOUND CORRODED. REPAIRED.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · airframe 82,702 hrs · 11,848 cycles

OVERWING ESCAPE EXIT RT AFT DOOR LOWER AFT DOOR FRAME FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: DOOR FRAME — CORRODED (EMERGENCY EXIT) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

OVERWING ESCAPE EXIT RT FWD DOOR LOWER FWD DOOR FRAME FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1064) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1064 AND RBL 88.5, REPAIRED.

Part: SEAT TRACK — CORRODED (BS 833) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 833 AND LBL 88.5 FOUND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (BS 965) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 965 AND LBL 88.5 FOUND CORRODED, REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1077) · airframe 82,702 hrs · 11,848 cycles

CORROSION FOUND ON SEAT TRACK BS 1077 AND RBL 88.5. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 999) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 999 AND RBL 88.5. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1095) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1095 AND RBL 88.5 FOUND CORROSION. REPAIRED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 953) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 953 AND RBL 88.5 FOUND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (BS 870) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 870 AND RBL 88.5 FOUND CORRODED. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 967) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 967 AND RBL 88.5, FOUND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (BS 850) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 850 AND RBL 88.5, FOUND CORRODED. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1015) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 1015 AND RBL 88.5 FOUND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (BS 892) · airframe 82,702 hrs · 11,848 cycles

CORROSION FOUND ON SEAT TRACK BS 892 AND RBL 88.5 FOUND CORROSION. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 816) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORROSION AT BS 816 AND RBL 88.5. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 1030) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 1030 AND RBL 88.5 FOUND CORRODED. REPAIRED.

Part: SEAT TRACK — CORRODED (BS 900) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 900 AND LBL 88.5 FOUND CORRODED. REPLACED.

Part: SEAT TRACK — CORRODED (BS 784) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 784 AND LBL 88.5 FOUND CORRODED. REPAIRED.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

FLOORBEAM UPPER TEE FOUND CORRODED AT BS 1480 AND RBL 50. REPLACED 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1201) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK CORRODED BS 1201 AND LBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1197+23 AND RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1197+38 RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK CORRODED BS 1197+11, LBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1400) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK CORRODED AT CABIN BS 1400 AND RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1102) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1102 AND RBL 88.5 FOUND CORRODED. REPLACED THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1128) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1128 AND LBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1112) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1112 AND RBL 88.5 FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1197+40 AND LBL 88.5 FOUND CORRODED. REPLACED IAW SRM 51-41-02.

Part: SEAT TRACK — CORRODED (BS 1158) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1158 AND LBL 88.5 FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1197+86 RBL 88.5. R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1197+102 LBL 88.5 FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1415) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK, AT BS 1415 AND LBL 88.5 FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1173) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1173 AND RBL 88.5, R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1400) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1400 AND LBL 88.5, FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1128) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1128 RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: STRINGER — CORRODED (BS 1054) · airframe 82,702 hrs · 11,848 cycles

STRINGER 18L, BS 1054 FOUND CORRODED. FOUND OUT OF LIMIT IAW SRM 53-00-01. R & R IAW SRM 51-40-02.

Part: SEAT TRACK — DAMAGED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 1197+115 RBL 88.5 DAMAGED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1142) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1142 AND LBL 88.5, FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 82,702 hrs · 11,848 cycles

NR 2 PYLON AFT LOWER STRUT ACCESS DOOR 446BL CUTOUT AREA FOUND CRACKED. REMOVED AND INSTALLED FILLER IAW SRM 54-53-01.

Part: SEAT TRACK — CORRODED (BS 1192) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1192 AND LBL 88.5, FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1384) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK AT BS 1384, LBL 88.5 FOUND CORRODED. REPLACED THE SEAT TRACK IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1175) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK BS 1175 AND LBL 88.5, FOUND CORRODED. REPLACED IAW SRM 51-40-02.

Part: SPAR — CRACKED (NR 2 NACELLE) · airframe 82,702 hrs · 11,848 cycles

NR 2 NACELLE STRUT FWD UPPER SPAR WEB AROUND THE OTBD DRAIN HOLE FOUND CRACK. REPAIRED IAW ERA 14-530674.

Part: SEAT TRACK — CORRODED (BS 1197) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK CORRODED BS 1197+88 AND LBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1153) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1153 AND RBL 88.5. R & R IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1197) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK CORRODED BS 1197+132 AND LBL88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1226) · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1226 AND RBL 88.5, R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1351) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1351 AND RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

FLOORBEAM UPPER TEE FOUND CORRODED AT BS 1480 AND RBL 82. REPLACED IAW SRM 51-40-02.

Part: FLOORBEAM — NICKED (BS 842) · airframe 82,702 hrs · 11,848 cycles

CABIN FLOORBEAM UPPER TEE FOUND NICKED AT BS 842 AND RBL 33. FLOORBEAM REPLACED IAW SRM 53-00-51.

Part: SEAT TRACK — CORRODED (BS 1370) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1370 AND LBL 88.5. REPLACED IAW SRM 53-00-52.

Part: SEAT TRACK — CORRODED (BS 1269-1285) · airframe 82,813 hrs · 11,864 cycles

SEAT TRACK FOUND CORRODED AT RBL 88.5 BETWEEN BS 1269 AND 1285.

Part: SEAT TRACK — CORRODED (BS 1241-1260) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT RBL 88.5 BETWEEN BS 1241 & 1260. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 332) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORROCDC BS 332 AND RBL 88.5. REPLACED IAW SRM 51-40-02.

Part: SEAT TRACK — CORRODED (BS 1377) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED BS 1377 AND RBL 88.5, R & R THE SEAT TRACK.

Part: SEAT TRACK — CORRODED (BS 1322) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

SEAT TRACK FOUND CORRODED AT BS 1322 AND RBL88.5, R & R THE SEAT TRACK.

Part: STRINGER — CORRODED (BS 960) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

CABIN STRINGER 19R END FITTING FOUND CORROSION AT BS 960. FOUND OUT OF LIMIT IAW SRM 53-00-03, FIG 101. T R & R IAW SRM 51-40-02.

Part: SHEAR TIE — CORRODED (BS 1197) · corrosion level 2 · airframe 82,702 hrs · 11,848 cycles

AFT CARGO AT BS 1197+44 BETWEEN STRINGER S38-39L SHEAR TIE CORRODED. CORROSION REMOVED AND FOUND OUT OF LIMITS. SHEAR TIE R & R IAW SRM 51-40-02.

Part: SKIN — DAMAGED (NR 9 SLAT) · airframe 78,653 hrs · 11,288 cycles

NR 9 INBD END OF SLAT HAS DAMAGE TO END POTTING END SKIN. R & R DAMAGED SKIN AND DOUBLERS IAW SRM 57-43-02.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 82,511 hrs · 11,820 cycles

8 X 12 INCH DELAMINATION ON RT SIDE OF VERTICAL STAB. REPAIRED IAW SRM 55-30-01.

Part: ROLLER TRAY — DAMAGED (AFT CARGO) · airframe 82,511 hrs · 11,820 cycles

AFT CARGO ROLLER TRAY DAMAGED. PERFORMED PERMANENT REPAIR ON AFT CARGO ROLLER TRAY IAW ERA 516401-14, REV ORIG AND SRM 53-00-53.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 91,666 hrs · 13,205 cycles

MAIN DECK/CORROSION FOUND ON FLOOR STRUCTURE EXCEED LIMIT/STA 287, RBL 20.

Part: FLOORBEAM — CORRODED (BS 287 RBL 20) · airframe 73,847 hrs · 10,558 cycles

DURING FLATBED MODIFICATION FOUND UPPER FLANGE OF FLOORBEAM AT BS 287, RBL 20 CORRODED. FOUND CORROSION EXCEEDING SRM LIMITS. REPAIR CARRIED OUT ON FLOOR BEAM IAW SRM 53-00-51.

Part: TRACK — DAMAGED (LE SLATS) · airframe 73,847 hrs · 10,558 cycles

L/E SLATS DOWN STOP/TRACK REPAIRED IAW AA 5750-01178.

Part: FITTING — DAMAGED (WING) · airframe 73,847 hrs · 10,558 cycles

UPPER WING SKIN PANEL LOAD FITTING DAMAGED. REPAIRED IAW AA 5724-01005.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 82,511 hrs · 11,820 cycles

AFT CARGO FLOOR PANEL BS 1350 MOST RT OTBD HAS 4 INCH CRACK AND 1 X 3 INCH PUNCTURE. REPAIR ACCOMPLISHED IAW SRM 53-00-50, PAR 4C.

Part: NOSE COWL — DENTED (NR 1 ENGINE) · airframe 82,511 hrs · 11,820 cycles

BIRDSTRIKE, NR 1 ENGINE NOSE COWL DENT AT 3 O`CLOCK POSITION. INSPECTED IAW SRM 54-13-01, PG 104. TIME LIMITED REPAIR IAW PS 900-5-1, NR 04.

Part: STRUCTURE — DAMAGED (TE FLAP) · airframe 70,226 hrs · 10,088 cycles

INBD MAIN FLAP DAMAGED. REPAIRED IAW AA 5750-01165.

Part: PIN — BACKED OUT (CABIN) · airframe 70,093 hrs · 10,072 cycles

EMERGENCY PATH LIGHTS AT 5G ARE INOPERATIVE. MAINTENANCE FOUND A PIN PUSHED BACK ON POWER SUPPLY WIRE AND RESECURED. SYSTEM OPERATION IS NORMAL.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 69,826 hrs · 10,039 cycles

EMERGENCY PATH LIGHTS AT SEAT 38B ARE INOPERATIVE. MTC REPLACED THE HARNESS. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DENTED (TE FLAP) · airframe 69,569 hrs · 10,001 cycles

RIGHT WING I/B AFT FLAP LWR SURFACE FOUND DENT MARK. METAL HOT BOND REPAIR PERFORMED AS PER B767-300 SRM 57-53-01. REPAIR 1 FIG 201 AND SRM 51-70-10 REPAIR 4 FIG 201 AND 202.

Part: FLOOR PANEL — CRACKED (AFT CARGO) · airframe 82,511 hrs · 11,820 cycles

AFT CARGO FLOOR PANEL, BS 1350 MOST RT OTBD HAS 4 IN CRACK AND 1" X 3" PUNCTURE. FOLLOWED SRM 53-60-53, P101 C. PERFORMED TIME LIMITED REPAIR BY SRM B767 53-60-53, P101C.

Part: STRUCTURE — DAMAGED (WING) · airframe 67,039 hrs · 9,664 cycles

LOWER WING SKIN TENSION BOLT HOLE. REPAIRED IAW AA 5700-01029.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,085 hrs · 9,535 cycles

EMERGENCY LIGHTS AT FROM ROWS 21AB THROUGH 31AB ARE INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN BATTERY PER AMM. SYSTEM OPERATION IS NORMAL.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 66,062 hrs · 9,532 cycles

EMERGENCY LIGHTS AT SEATS 21-33AB ARE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK CHARGER M9009. SYSTEM OPERATION IS NORMAL.

Part: SKIN — DENTED (FUSELAGE) · airframe 82,511 hrs · 11,820 cycles

SMALL DENT AFT OF CENTER CARGO DOOR. REPAIRED IAW SRM 53-00-01, REPAIR 8, STEP 4.

Part: SKIN — DENTED (FUSELAGE) · airframe 82,511 hrs · 11,820 cycles

SMALL DENT AFT OF CENTER CARGO DOOR. REPAIRED IAW SRM 53-00-01, REPAIR 8, STEP 4.

Part: WIRE HARNESS — DETACHED (EMERGENCY LIGHTS) · airframe 62,729 hrs · 9,120 cycles

EMERGENCY ESCAPE PATH LIGHT HARNESS AT 39B IS NOT ATTACHED. MX RE-ATTACHED THE PATH LIGHT HARNESS AT 39B. SYS OPS ARE NORMAL. (DL76L101503)

Part: FMC — MALFUNCTIONED (LEFT) · airframe 60,992 hrs · 8,841 cycles

RTB DUE TO FMC ANUNCIATOR LIGT ILLUM ON LT ENG STARTUP. REPLACED FMC IAW AMM CROSS LOADED FMS SOFTWARE IAW AMM. ALL CHECKS GOOD. R & R L FMC IAW THE MM. CROSS LOADED FMS SOFTWARE IAW THE MM CHECKS OK. MCO AND PLAC REMOVED ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,941 hrs · 8,833 cycles

DURING OP 7802 FND 2 EA AFT LT WING EMERGENCY LIGHTS INOP. ALSO 2 EA RT WING EXT EMERGENCY LIGHTS INOP AND DOOR 2R. RELAMPED 2 EA AFT LT WING EMERGENCY LIGHTS AND R & R EMERGENCY BATT CHARGER ASSY M733, OPS OK.

Part: DISPLAY — FAILED (COCKPIT) · airframe 60,839 hrs · 8,821 cycles

CAPT-S FMS CDU DISPLAY FAILED ON TAXI OUT. REMOVED AND REPLACED LT MCDU IAW AMM. ALL CHECKS NORMAL. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS.

Part: OVERHEAT SENSOR — DEFECTIVE (LT PACK) · airframe 59,683 hrs · 8,661 cycles

L PACK OFF L PACK TEMP LIGHTS ILLUM W/ INOP AND PACK OFF LIGHTS ON TAXI OUT. REPLACED ACM INLET SENSOR, NO HELP WILL NOT RESET. REPLACED COMP OUTLET OVERHEAT SENSOR M555 L PACK CHECKS GOOD MFR 641137-1. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: FAN — OVERHEATED (E&E BAY) · airframe 59,573 hrs · 8,648 cycles

ON TAXI OUT BURNING ELECTRICAL SMELL DETECTED BY SEVERAL FLIGHT ATTENDANTS IN AFT GALLEY. DESCRIBED AS INTERMITTENTLY WAFFING AROUND GALLEY. COUNTER LIGHTS TURNED OFF AND BREAKER PULLED. FOUND AFT EQ EXH FAN 1 MOTOR OVERHEATED AND GENERATED THE BURNING SMELL. PULLED C/B AND DISCONNECTED CONNECTOR OFF THE MOTOR. A/C OK FOR SERVICE. ITEM ALREADY ON MCO. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: UNKNOWN — ODOR (CABIN) · airframe 58,749 hrs · 8,546 cycles

BY 2R JUMPSEAT BURNING SMELL FOR 20 SECS THEN DISSIPATED AND DID NOT RETURN. AFTER CPT CONVERSATION CHECKED ALL AFT GALLEY COMPARTMENT AN ACCESSORIES IN PARTICULAR COFFEEMAKERS, OVENS, GALLEY LIGHTS BALLAST IN THE GALLEY LIGHTS BALLAST IN THE GALLEY CEILING. ALSO CARGO BULK COMPARTMENT FOR SMELL COMING FROM VENTILATE AND WATER COMPRESSOR, NIL FOUND A/C OK FOR SERVICE.

Part: CHILLER — ODOR (AFT GALLEY) · airframe 58,707 hrs · 8,541 cycles

AFTER CRUISE ALTITUDE DETECTED NON-ELECTRICAL SMOKE ODOR FROM AFT GALLEY FLOOR VENT CO-PILOT SIDE. CHECKED AFT GALLEY EQPMNT NO TROUBLE FOUND. DEACTIVATED AFT GALLEY CHILLERS DUE TO ODOR DISSIPATED AFTER CREW PULLED CIRCUIT BREAKERS. FWD TO NEF CODE 253.07. ETOPS CATEGORY 'B': DIVERSION OR TURNBACK.

Part: FRAME — CRACKED (FS 903.5 WL 190) · airframe 56,800 hrs · 8,315 cycles

DURING HMV AT HAECO IN HKG MAINTENANCE, FOUND A .25 INCH CRACK ON THE LT FS 903.5 FRAME AT WL 190. A REPAIR WAS INSTALLED PER ERA 471737-14AD.

Part: STARTER — FAILED (LEFT) · airframe 56,458 hrs · 8,271 cycles

AFTER PUSH NR N2 RISE ON ENGINE START. REPLACED NR 1 ENG STARTER PER AMM 80-11-01. SERVICED OIL. CRANKED ENG AND LEAK CHECK PERFORMED OPS CK NORMAL. STARTER MFG 774860A4 S/N 960225.

Part: WARNING LIGHT — FALSE ACTIVATION (NR 1 ENG) · airframe 56,209 hrs · 8,240 cycles

AFTER LT ENG START AND APU SHUTDOWN LEFT GEN OFF LIGHT WITH LT ISOLATION BUSS TIE LIGHT. RAN ENG CYCLED POWER FOR LT ENG AND APU SEVERAL TIMES WITH LOAD ON GENERATORS. PERFORMED BITE AND BPCU HAD PILOT DUPLICATE POWER TRANSFER. WHEN PROBLEM OCCURRED NO FAULTS NOTED. LT GEN AND APU AND A/C POWER OPS CHEC K NORMAL AS PER AMM.

Part: STARTER — UNKNOWN (NR 1 ENGINE) · airframe 56,108 hrs · 8,228 cycles

THE LEFT ENG WENT TO 14 PERCENT N2 ON START AND THEN BEGAN TO DECREASE RPM. ALL OTHER INDICATIONS NORM. REMOVED AND REPLACED LT ENG STARTER PER M/M. PERFORMED OPS CHK OF STARTER OK FOR SERVICE.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 55,972 hrs · 8,212 cycles

SEAT 28FG EMERGENCY LIGHT ASSY INOP. REPLACED SEAT HARNESS AT SEAT 28FG, CHECKS GOOD PER AMM.

Part: DISPLAY — FAILED (COCKPIT) · airframe 55,939 hrs · 8,208 cycles

RT FMC CDU FAILED ON TAXI. REPLACED F/OS CDU PER MM. OPS NORMAL. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: ENGINE — OIL CONSUMPTION (NR 1) · airframe 53,117 hrs · 7,861 cycles

DUE TO CONTINUED INCREASE IN OIL USAGE, REPLACE ENG. REPLACED ENGINE.

Part: ANGLE — CRACKED (NR 2 PYLON) · airframe 52,651 hrs · 7,798 cycles

NR 2 PYLON MIDSPAR CLOSEOUT ANGLES WER CRACKED AT THE MIDSPAR FITTINGS. THE ANGLE WAS REPLACED.

Part: BRAKE — OVERHEATED (NR 5) · airframe 51,490 hrs · 7,661 cycles

EXCESSIVELY HOT BRAKES FOLLOWING LANDING. LEFT AFT MAIN OUTBOARD WAS 9 DURING TAXI NR 5, NUMBER FWD OF IT HEATING AS RESULT 6 BRAKE TEMP SUSPECT POSSIBLE DRAGGING BRAKE. NO OTHER INDICATIONS. REPLACED NR 5 MAIN BRAKE PER M/M. PERFORMED CONDITIONAL INSPECTION OF BRAKES AND TIRES ON LT LANDING GEAR PER M/M 05-51-14-212-094 DUE TO HIGH TEMP AND NR 5 MAIN TIRE FUSE PLUG MELTING. NO DAMAGE NOTED ON REMAING TIRES AND BRAKES. NO DAMAGE NOTED ON NR 5 BRAKE AXLE. OPERATED BRAKES CKS GOOD.

Part: STARTER — FAILED (NR 2 ENGINE) · airframe 51,433 hrs · 7,652 cycles

RIGHT ENGINE STARTER MOTOR FAILED DURING START CYCLE. STARTER MOTOR REPLACED. OIL SERVICE ACTIONED. DRY CYCLE OK. CHECK START ACTIONED ON PUSHBACK. MF PART NR 774860A4.

Part: ALTIMETER — FAILED (COCKPIT) · airframe 49,758 hrs · 7,444 cycles

CAPT ALT INOP FAILED AT 13,000'. REMOVED AND REPLACED CAPT'S ALT INDICATOR PER MM 34-13-01-004-001. TEST OK PER MM. TEST ON ADC 1 AND 2 ALSO OK.

Part: FITTING — DAMAGED (NR 1 NACELLE) · airframe 48,770 hrs · 7,320 cycles

THE NR 1 PYLON MID SPAR ATTACH FITTING WAS DAMAGED BY AND ELECTRICAL SHORT. THE DAMAGED AREA OF THE FITTING WAS BLENDED AWAY, NO REINFORCEMENT NECESSARY.

Part: FITTING — ARCED (LT PYLON) · airframe 48,770 hrs · 7,320 cycles

FOUND ARCING TO LT PYLON MID STRUT FITTING OUTBOARD SIDE. REMOVED LT OTBD PYLON PANELS 437 ELX 437 AL. ALSO, REMOVED TOP WING TO PY ACCESS PANEL. REPAIRED WIRE W/SPLICE PER SWPM. PUMP OPS CKS NML. NEEDS CLAMP/PNLS REINSTALLED. INSTALLED CLAMPS AND CLOSED PANELS.

Part: ENGINE — MAKING METAL (NR 2) · airframe 48,389 hrs · 7,275 cycles

FOUND METAL IN GEARBOX IN NR 2 ENGINE. REPLACING NR 2 ENGINE. T/S PER FIM FOUND PMA BAD ON FURTHER INVESTIGATION FOUND BEARING FAILED REMOVED PM9 DRIVE HOUSING FOUND METAL PARTIC FALLING FROM CASE INTO GEAR BOX ENG SHOP CALLED OUT TO REVI PROBLEM. INSPECTED METAL AND ENG, CHG WILL BE REQUIRED DUE T METAL IN GEARBOX. REMOVED AND REPLACED NR 2 ENG ON R/C 1-3 1T149.

Part: CIRCUIT CARD — MALFUNCTIONED (T/O CONFIG) · airframe 44,364 hrs · 6,790 cycles

ON START OF TAKEOFF ROLL A/S LESS THAN 60KTS TAKEOFF CONFIG WARNING LIGHT EICAS FLAP CONFIG. FLAP INDICATION 15 FLAP HANDLE 15 IN DETENT. RAN TAKEOFF CONFIG TEST. FAILED FLAP PORTION. REPLACED CARD M620. RAN ANOTHER TAKEOFF WARNING TEST. ALL TESTS NORMAL.

Part: MODULE — INOPERATIVE (SPOILERS) · airframe 44,346 hrs · 6,787 cycles

ON TAKEOFF ROLL GOT SPOILER AND T/O CONFIG MSG. MTC IN PROGRESS. REPLACED TO CONFIGURATION WARNING MODULE AS PER AMM 31-51-04. NO FAULTS.

Part: SWITCH — FOULED (SPOILERS) · airframe 43,903 hrs · 6,736 cycles

RTO AT 80 KTS DUE TO SPOILER WARN AND CONFIG MSG. FOUND S493 SPOILER HANDLE POSITION SWITCH CONTACTS FOULED. CLEANED ROLLERS AND CONTACTS. RAN SPOILER INTERFACE TEST PER MM CHECKS OK.

Part: ODOR — DETECTED (CABIN) · airframe 37,073 hrs · 5,816 cycles

ON TAKEOFF NOTICED AN ELECTRICAL ODOR INSIDE THE CABIN AROUND THE WING AREA. SHORTLY AFTER THE ODOR DISSIPATED AND WAS FINE THE REST OF THE FLIGHT. INSPECTED AIRCRAFT AND SYSTEMS. UNABLE TO DUPLICATE.

Part: MONITOR — OVERHEATED (CABIN) · airframe 31,975 hrs · 5,060 cycles

IFE SYS CONTROL PNL AREA AND OVERHEAD BINS AT ROW ONE EXHIBITED A BURNING ODOR DURING MID CLIMBOUT. ODOR DISSIPATED WITHIN A FEW MINUTES BUT F/A COULD NOT TURN SYS OFF. FOUND WALL MOUNTED VIDEO MONITOR AT SEATS 1A AND 1B AT FAULT MONITOR NIIS JFK. FWD TO MCO AND PLAC PER MEL 25-20-01J. DISCONNECTED AND STOWED CONNECTORS. SYSTEM SHUT DOWN WITH TIME LIMIT, NEEDS DPN 251711825. REPLACED WALL MOUNTED VIDEO MONITOR. OPS CHECK NORMAL. NO ODOR NOTED. REMOVED MCO AND PLACARD.

Part: FILTER — DIRTY (CABIN) · airframe 31,599 hrs · 5,006 cycles

APPROX 2 1/5 HRS IN FLIGHT PAX AROUND 33FG REPORTED ODOR WHICH DISSIPATED THIS RE-OCCURRED TWICE MORE WITHIN 15-20 MINUTES TURNED OFF UTIL BUS PLUS RECIRC FANS AND PROCEEDED TO CDG/C BITE CHECK ON TEMP CONTROLLERS PACK CONTROLLERS AND BLEED AIR SUPPLY UNITS NO FAULTS VERIFY PACK COMPARTMENTS ALL NORMAL RAN BOTH ENGINES ALL NORMAL INSPECTED CABIN AREA OVERHEAD BINS AND UNITS UNDER SEATS ALL NORMAL. ALL FLUIDS QTY NORMAL. FOUND ZONE SENSORS FILTERS IN AFT CABIN VERY DIRTY. CLEANED SAME.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 30,856 hrs · 4,899 cycles

1L DOOR EMERGENCY LIGHT INOPERATIVE. RELAMPED. OPS CHECK GOOD.

Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHT) · airframe 30,856 hrs · 4,899 cycles

SEAT 24A/B EMERGENCY LIGHT INOPERATIVE. REPLACED SEAT HARNESS. OPS CHECK GOOD.

Part: PANEL — CRACKED (LT WING) · airframe 24,036 hrs · 3,758 cycles

LEFT WING LOWER CLOSURE PANEL TRAILING EDGE CHANNEL AND FWD EDGE WIGGLE PLATES CRACKED AND DAMAGED. REPLACED PANELS.

Part: SHUTOFF VALVE — FAILED (NR 2 ENGINE) · airframe 21,341 hrs · 3,339 cycles

ON TAKEOFF DUCT PRESS FLUCTUATED PLUS MINUS 15 PSI. REPLACED PRSOV PER MM. CKS OK.

Part: CONTROL PANEL — SMOKE (ENTERTAINMENT) · airframe 17,964 hrs · 2,802 cycles

MAIN IN FLIGHT ENTERTAINMENT CONTROL CENTER STARTED. SMOKING AFTER PUSHBACK. CMD SWITCHES OFF AND SMOKE STOPPED. FOUND PESC-V UNIT AT FAULT. REPLACED PESC-V.

Part: FUSE — FAILED (CABIN) · airframe 15,420 hrs · 2,386 cycles

FOUND EMERGENCY LIGHTS ROW 39 AB - 31 AB INOP. BROKEN WIRE AT 39 AB. REPAIRED WIRE AT 39 AB, NO HELP. REPLACED FUSE AT POWER SUPPLY M9010, CKS OK.

Part: OVEN — DIRTY (GALLEY)

FLIGHT ATTENDANTS REPORTED SMOKE SMELL IN MID GALLEY AFTER ARRIVAL AT GATE. EXAMINED THE OVENS IN MID GALLEY AND CLEANED ACCORDINGLY. ALSO, CHECKED CEILING PANELS AROUND GALLEY, NO EVIDENCE OF BURNING OR SMOKE SMELL OBSERVED.

Part: LINE — FAILED (NR 2 ENGINE)

RT HYD QTY ZERO EICAS MSG RT HYD DISPLAYED. SYS PRESS LIGHT ILLUM, RESVR QTY LIGHT ILLUM, EICAS MSG RT SYS PRESS DISPLAYED INFO PRIOR TO FLUID LOSS NOTED RT HYD SYS PRESSURE FLUCTUATIONS BETWWEN 1800 AND 3000 PSI. FOUND HYDRAULIC LINE ON FILTER BLOCK RIGHT ENGINE CRACKED. MADE TEMP. REPAIR. FLUSHED SYSTEM, REPLACED ENGINE PUMP AND FILTERS. LEAK CHECK AND OPERATIONAL CHECK NORMAL.

Part: ENGINE — FAILED (NR 2)

BIRD STRIKE ON TAKEOFF JFK, APPEARED TO BE RIGHT ENGINE. RETURNED TO JFK. SHUT DOWN ENGINE AFTER LANDING. RT EEC INOP WITH EICAS MSG. BOTH ENGS OPERATED WITHIN NORMAL LIMITS. RADOME AND RT OUTBD FLAP ALSO DAMAGED. ENGINE AND RADOME CHANGED. A/C TO BE FERRIED TO ATL FOR FLAP REPLACEMENT.

Part: WIRE — BROKEN (CABIN)

ON LAYOVER CHECK, FOUND EMERGENCY LIGHT INOP AT 22B. FOUND BROKEN WIRE AT PLUG NEAR SIDEWALL. REPAIRED BROKEN WIRE. EMERGENCY LIGHT CK OK.

Part: ACTUATOR — FAILED (RT TE FLAP)

T/E FLAP DISAGREE WHEN GOING FROM 20 DEG TO 25 DEG POSITION. FOUND LOAD RELIEF ACTUATOR STUCK IN EXTENDED POSITION. REPLACED ACTUATOR AND OPS OK.