N193DN

Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 116,980 hrs · 17,720 cycles

EMERGENCY LIGHTS AT ROWS 44AB TO 54AB INOPERATIVE. R & R POWER SUPPLY M9010 IAW AMM 33-51 (8054751)

Part: COAMING — CRACKED (ZONE 400) · airframe 116,511 hrs · 17,631 cycles

NUMBER 1 PYLON CRACK ON INBOARD SIDE OF PYLON COMING FROM AFT UPPER CORNER OF PYLON ACCESS PANEL 416BR. CORRECTIVE ACTION: REPAIRED PER ER/A 628915-14. (1279528)

Part: SKIN — DAMAGED (ZONE 300 ELEV) · airframe 116,511 hrs · 17,631 cycles

LEFT HORIZONTAL STAB LOWER SKIN DAMAGED. REPAIRED LOWER SKIN OF LEFT ELEVATOR OF HORIZONTAL STAB PER B767-300 SRM 55-20-01 REPAIR 1 (1274500)

Part: SKIN — CRACKED (ZONE 400) · airframe 116,504 hrs · 17,629 cycles

SHIP 193 NBR 1 PYLON-CRACK ON INBOARD SIDE OF PYLON COMING FROM AFT UPPER CORNER OF PYLON ACCESS PANEL 416BR. CORRECTIVE ACTION: C/W TIME LIMITED REPAIR INSTRUCTIONS REF ERA 628915-14 (1271020)

Part: ENGINE — MAKING METAL (LEFT) · airframe 116,504 hrs · 17,629 cycles

DIV/IFSD- DIVERTED TO KEF DUE TO LEFT ENGINE FAILURE. MAINTENANCE FOUND METAL IN TAIL PIPE. REPLACED LEFT ENGINE. (7922122) ENGINE: PWA, PW4060.

Part: ENGINE — FAILED (LEFT) · airframe 116,497 hrs · 17,628 cycles

DIVERTED TO KEF DUE TO LEFT ENGINE FAILURE. MAINTENANCE FOUND METAL IN TAIL PIPE. LEFT ENGINE REPLACEMENT IN WORK.(A010420)

Part: WARNING MESSAGE — FALSE ACTIVATION · airframe 115,657 hrs · 17,507 cycles

FCTL MISSED APPROACH WITH GO AROUND INTO HND DUE TO LE DISAGREE EICAS MESSAGE. CREW C/W QRH AND LANDED WITHOUT INCIDENT. TS PER FIM. NO FSEU FAULTS. OPS CK SYS. A/C RTS. (7348477)

Part: BATTERY PACK — NO TEST (ZONE 800) · airframe 115,171 hrs · 17,432 cycles

SHIP 193 LT O/W SLIDE SQUIB LIGHT NOT ILLUMINATED DURING SQUIB TEST 1. CORRECTIVE ACTION: T/S PER B767 FIM 25-65-00. FOUND BAD LT O/W SLIDE BATTERY. R/R LT O/W SLIDE BATTERY PER B767-300 AMM 25-65-17. LT O/W SLIDE SQUIB TEST CKS GOOD. P/N ON AD2013-1A. (7317455)

Part: CIRCUIT BREAKER — FAULTED (ZONE 200) · airframe 115,128 hrs · 17,425 cycles

SHIP 0193 DURING SQUIP TEST ON P61 L/H EMERGENCY EXIT LIGHT NOT ILLUMINATED. CORRECTIVE ACTION: C/B RESET P11 PANEL P35/P36 IAW B767-300 AMM 25-65. (7317444).

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 114,918 hrs · 17,394 cycles

SHIP 0193 EMER LIGHTS FROM SEAT 45AB TO 54AB ON LEFT SIDE INOP. CORRECTIVE ACTION: FOUND BAD FUSE ON POWER SUPPLY M9010. REPLACED FUSE OPS NML PER B767 AMM 33-51 OKAY FOR SVC. (7479515)

Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 114,853 hrs · 17,383 cycles

SHIP 193 ON SVC CHK FOUND EEPL'S OUT ROW 44A-55A. CONNECTIVE ACTION: R&R BATTERY PACK ASSY M9010 REF B767-300 AMM 33-51-07. OPS CHK NML. (7554285)

Part: FUSE — INOPERATIVE (ZONE 200) · airframe 114,793 hrs · 17,373 cycles

SHIP 193 ON SVC CHK FOUND EMERGENCY PATH LIGHTS FROM ROWS 44 TO 54 LEFT SIDE INOP. REPLACED FUSE 1-4 ON BATTER POWER SUPPLY (M9010). OPS CHK NML REF CMM 25-65-02 & B767 WDM 33-51-31. A/C OK FOR SVC (7554281)

Part: WIRE — PULLED (ZONE 200) · airframe 114,145 hrs · 17,273 cycles

ROW 47FG EMERGENCY ESCAPE PATH LIGHTING IS INOPERATIVE. MAINTENANCE FOUND A WIRE PULLED FROM THE CONTOR. THE WIRE WAS RECRIMPED PER SWPM 20-64 AND EEPL OPERATIONAL CHECK WAS GOOD. AIRCRAFT IS OK FOR SERVICE. (LP #6439121)

Part: HEATER — INOPERATIVE (PITOT TUBE) · airframe 113,259 hrs · 17,071 cycles

SHIP 0193 -DIV- TO SLC DUE TO CAPT PITOT HEAT INOP. CORRECTIVE ACTION: R/R CAPT PITOT PROBE.(6715556)

Part: BATTERY — NO TEST (L1 DOOR SLIDE) · airframe 112,924 hrs · 17,012 cycles

SHIP 193 ON WAKE UP, TEST 1 LT ESCAPE SLIDE WILL NOT TEST. CORRECTIVE ACTION: R & R L SLIDE BATTERY AND CHARGER IAW B767 IPC 25-65 AND AMM 25-65. OPS CHECK GOOD. (9739074)

Part: BRAKE — FIRE (NR 1) · airframe 112,708 hrs · 16,976 cycles

SHIP 0193 -FIRE- NUMBER 1 BRAKE FIRE ON TAXI IN. CORRECTIVE ACTION: C/W INSPECTIONS PER AMM. REPLACED NUMBER 1 BRAKE AND WHEEL ASSY. REPLACED NUMBER 2, 5, AND 6 BRAKE ASSY DUE TO EXTINGUISHING AGENT USED. (6628592)

Part: FILTER — ODOR (CABIN) · airframe 112,122 hrs · 16,896 cycles

SHIP 193 DIRTY SOCK SMELL ON TAXI IN WITH JUST THE RIGHT ENGINE RUNNING. CORRECTIVE ACTION: REMOVED AND REPLACED BOTH RECIRC FAN FILTERS AS PRECAUTION AS PER B767-300ER AMM 21-25. NO FURTHER DEFECTS NOTED. (5131862)

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 111,603 hrs · 16,821 cycles

SHIP 193 EMERGENCY EXIT LIGHTS AT DOORS 2L AND 2R ARE FLICKERING NONSTOP. CORRECTIVE ACTION: TS PER B767-300 WDM 33-51-11. FOUND HIGH RESISTANCE ON PIN 1 OF CONECTOR D95363P. FOUND TERMINAL LOOSE ON GD9761-DC. RESERCURED LOOSE TERMINAL. HIGH RESISTANCE NO LONGER PRESENT. EXIT LIGHTS OPS CHL NML (6181952)

Part: BATTERY — INOPERATIVE (ZONE 200) · airframe 111,533 hrs · 16,808 cycles

SHIP 193 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:607. CORRECTIVE ACTION: POWER SUPPLY & BATTERY R&R (0461752)

Part: POWER SUPPLY — FAULTED (EMERGENCY LIGHTS) · airframe 111,371 hrs · 16,785 cycles

AIRCRAFT 0193, AFTER PUSHBACK & ENG START, F/A ADVISED THAT 2L DOOR EMERY LIGHTS ARE ON AND BLINKING. RESETTING THE EMERY LIGHTS DID NOT HELP. CORRECTIVE ACTION: REMOVED AND REPLACED POWER SUPPLY M1210 PER B767 AMM 33-51 TEST GOOD. (LP 6039750)

Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 111,317 hrs · 16,777 cycles

PRIOR TO PUSH BACK EMERGENCY LIGHTS START TO FLICKER IN 4L/4R. RE-SEATED CONNECTOR D95363 PER WDM 33-51-11. ALL EMERGENCY LIGHTS OPS.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 111,317 hrs · 16,777 cycles

DURING SVC CHECK FOUND EXIT LIGHT AT 2R DOOR AND EXIT LIGHT AT 2R FA SEAT INOP. AS WELL AS 2L DOOR EXIT LIGHT AND 2L FA SEAT INOP. REPLACED BATTERY CHARGER AND BATTERY (M1210). REPINNED CONNECTOR PLUG D95363P IAW B767 SWPM CH 20. FOUND PIN 5 OF D95363P IN INCORRECT POSITION, RE-POSITIONED PIN 5 REF B767-300 WDM 33-51-11 & BSWPM CH.20.

Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 111,272 hrs · 16,769 cycles

SHIP 193 CABIN DOORS 2L AND 2R EXIT SIGNS FLASH INTERMITTANTLY. CORRECTIVE ACTION: CARRIED OUT EMERGENCY LTS FUNCTIONAL TESTS WITH NO FAULTS. (6041298)

Part: LIGHT — NO TEST (CABIN) · airframe 111,126 hrs · 16,749 cycles

AIRCRAFT 0193, DURING SERVICE CHECK THE LEFT EMERGENCY LIGHT DID NOT TEST WHEN TEST 1 SELECTED. CORRECTIVE ACTION: RELOCATE A/C OFF GATE. POWERED A/C DOWN COMPLETELY AFTER MOVE. POWERED A/C BACK UP AND SQUIB TEST NOW OPS CHECKS GOOD. (LP 6041240).

Part: SQUIB — NO TEST (DOOR SLIDE) · airframe 110,243 hrs · 16,620 cycles

LEFT EMER ESCAPE SLIDE LIGHT SQUIB WOULD NOT TEST DURING PDC. CORRECTIVE ACTION: REPLACED OVERWING ESCAPE SLIDE PSU IAW B767 AMM 33-51 SQUIB LIGHTS TESTNORMAL

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,963 hrs · 16,403 cycles

SHIP 193 CEILING EMERGENCY LIGHTFLICKERING RT SIDE OF CABIN / INTERIOR. CORRECTIVE ACTION: RESET UTILITY BUSES. OPS CHK NML REF B767 AMM 33-21. (0081087)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,327 hrs · 16,303 cycles

SHIP 193 ON ARRIVAL FA'S STATE 2R DOOR WILL NOT DISARM. CORRECTIVE ACTION: C/W REP CHK OF THE 2R DOOR SLIDE ARMING INDICATORS. OK TO CONT ON B767-300 MEL 52-11-01. (4560897)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,286 hrs · 16,291 cycles

SHIP 193 GOT FWD ACCESS DOOR ON EICAS DURING DESCENT @ 15000 FT 270KT. CORRECTIVE ACTION: ADJUSTED FWD ACCESS DOOR SENSOR AND TARGET IAW B767 AMM 52-71-00 . MEL CLEARED PLACARD REMOVED. (4560869)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 FOUND LH WING LOWER SKIN NOT FLASH AT RIB 31. CORRECTIVE ACTION: REPAIRED THE DAMAGED LOWER SKIN AT LH WING STR L-6.5 BETWEEN WSTA 990.2 AND WSTA 1018.2 AS PER PRI 611798-14 (2975132)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 HFEC FOUND 01 EA CRACK AT BS 1809.5 BULKHEAD FORWARD OUTER CHORD RH SIDE AND SECTION 08 (RH) MUST BE ACCOMPLISHINGED PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR BULKHEAD FORWARD OUTER CHORD AT BS 1809.5 RH SIDE REF TO JOB CARD NO:5310-01376-0805 (2973407)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 EO TASK-HFEC FOUND 01 EA CRACK AT BS 1809.5 BULKHEAD FORWARD OUTER CHORD REFER TO W/C 5310-01376-1703 STEP 2 CIRCLE NOTE 3, AND NOTE THAT SECTION 08(RH)MUST BE ACCOMPLISH PRIOR TO FURTHER FLIGHT. CORRECTIVE ACTION: ACCOMPLISHED THE REPAIR FOR BULKHEAD FORWARD OUTER CHORD AT BS 1809.5 RH SIDE REF TO JOB CARD NO:5310-01376-0805 REV. JUN 07.2019. (2973403)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 OPEN HOLE HFEC INSPECTION FOUND 01 EA CRACK AT THE LOWER ROW FORWORD ON ONE FASTENER HOLE. CORRECTIVE ACTION: BS 1809.5 BULKHEAD RH OUTER CHORD PERMANENT REPAIRED REF TO W/C 5310-01376-0805. (2972511)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 OPEN HOLE HFEC INSPECTION FOUND 02 EA CRACKS AT TWO FASTENER HOLES, ONE IS THE FIFTH COUNT FROM BOTTOM OF THE ELEVEN FASTENER HOLE, THE OTHER ONE IS SEVENTH. CORRECTIVE ACTION: BS 1809.5 BULKHEAD RH OUTER CHORD PERMANENT REPAIRED REF TO W/C 5310-01376-0805. (2972507)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 DURING CCK AT STAG, A DENT WAS NOTED ON THE LH LOWER WING SKIN, STR L-6.5, WSTA 1005. REPAIR WAS ACCOMPLISHED PER ER/A 611798-14AD SECTION I. FOLLOW ON INSPECTIONS ARE REQUIRED PER SECTION II. CORRECTIVE ACTION: ACCOMPLISH ER/A 611798-14AD SECTION II INSPECTIONS BEFORE 12,000 FLIGHT CYCLES OR 32,000 FLIGHT HOURS (2971218)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 CABIN CANTED PRESSURE DECK UPPER SURFACE FOUND CORROSION AT STA955, RBL62. CORRECTIVE ACTION: CORR BY NING 00997886 CAN 13SEP23 ATA 5716 RII: N ENTR 00172993 W REPAIRED THE CORROSION CENTER WING UPPER SKIN AT STA 955, RBL62 AS PER PRI 534311-14 REV 0. (2967009)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 FOUND LH WING NO.2 SLAT TRAILING EDGE INNER SURFACE WORN AT WS 900 AREA. CORRECTIVE ACTION: LH WING NO.2 SLAT TRAILING EDGE INNER SURFACE REPAIRED AT WS 900 AREA AS PER B767-300 SRM 57-43-02-2R-1&SRM 51-70-10-2R-4 (2967251)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 MTC TASK-CABIN CANTED PRESSURE DECK UPPER SURFACE FOUND CORROSION AT STA 955, RBL69. CORRECTIVE ACTION: REPAIRED THE CORROSION CENTER WING UPPER SKIN AT STA 955, RBL69 AS PER PRI534311-14 REV 0. (2967001)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,270 hrs · 16,288 cycles

SHIP 193 R/H WING I/B FLAP AFT FLAP UPPER SURFACE FOUND ONE DENT FAR AWAY FROM T/E 2.5 INCH AND I/B EDGE 18 INCH. CORRECTIVE ACTION: R/H WING I/B FLAP AFT FLAP UPPER SURFACE REPAIRED AS PER B767- 300 SRM 57-53-01-2R-1&SRM51-70-10-2R-2 (2967392)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 108,270 hrs · 16,288 cycles

SHIP 193 SEAT TRACK - CABIN SEAT TRACK FOUND CORROSION AT STA1351 TO STA1373. CORRECTIVE ACTION: REPAIRED THE DAMAGED SEAT TRACK AS PER B767-300 SRM 53-00 (2963846)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 108,067 hrs · 16,249 cycles

SHIP 193 L FWD DOOR INTERMITTENT IND OPEN WITH DOOR CLOSED AND ARMED. CORRECTIVE ACTION: DEFER TO MEL/PLAC IAW B767 MEL 52-71-01 M PROC C/W (4423508)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 107,413 hrs · 16,133 cycles

SHIP 0193 -DIV- TO DUB DUE TO LAVATORIES INOP. CORRECTIVE ACTION: UPON ARRIVAL THE LAV TANKS WERE FOUND TO BE FULL. SERVICED AND OPS CHECKS NORMAL.(4795574)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 106,870 hrs · 16,048 cycles

SHIP 193 FOUND 18GH SEAT EMERGENCY LIGHT (WHITE) INOP. CORRECTIVE ACTION: FOUND WIRE BROKEN AT COMMON FAULT AREA ON SEAT FRAME. RE-PINNED MATE-N-LOK CONNECTOR PER SWPM 20-42-01. SEAT 18GH EMER LTS OPERATING NORMAL. MEL AND PLACARD REMOVED. (4734814)

Part: FSEU — FAULTED (FLAP / SLAT SYS) · airframe 105,823 hrs · 15,829 cycles

DECLARED EMERGENCY INTO ATL DUE TO PILOT REPORT OF TE FLAP AND LE SLAT DISAGREE. CORRECTIVE ACTION: PERFORMED FSEU BITE CHECK. FOUND FAULT CODE 27-51333 MULTIPLE LEGS. REPLACED FSEU OPS CHECKS GOOD. (9881802)

Part: NONE — NONE (SLIDE LIGHT) · airframe 105,696 hrs · 15,809 cycles

SLIDE INDICATOR LIGHT INOPERATIVE OR DAMAGED. CYCLED SWITCH. NO TROUBLE FOUND.

Part: WARNING MESSAGE — FALSE ACTIVATION (L2 DOOR) · airframe 105,573 hrs · 15,783 cycles

SHIP 193 AFTER PUSHBACK L FWD DOOR ECIAS MSG AND ASSOC SLIDE ARMED LIGHT FLASHING PROBLEM RESOLVED IT SELF OK TO CONT IN SERVICE. CORRECTIVE ACTION: LIGHT FUNCTION NML ASWELL AS DOOR OK TO CON IN SVC (9457296)

Part: LOCK — FAULTED (PAX DOOR) · airframe 105,348 hrs · 15,731 cycles

SHIP 193 L FWD ENT DOOR M/C APPEARED ON PUSHBACK AFTER R ENG START REACHED IDLE SPEED. CORRECTIVE ACTION: FOUND DEBRIS IN L FWD DOOR LOCKING MECHANISM. REMOVED DEBRIS CYCLED DOOR AND ARMING LEVER. ALL INDICATIONS NML PER B767-300 AMM 52-71 AND 52-73. NO 30 DAY HISTORY. (9436454)

Part: ALTIMETER — MALFUNCTIONED (FIRST OFFICER'S) · airframe 105,328 hrs · 15,727 cycles

ALTIMETER DISAGREE EICAS MESSAGE. FO ALTIMETER BOUNCING BETWEEN 200 AND 300 FT LOWER THAN CAPTAIN`S. RAN QEH AND USED ALTIMETER DATA ALTERNATE. RESET RT ALTIMETER C/B. COMPLIED WITH RT ADC BITE. NO FURTHER ISSUES NOTED. C/W IAW AMM 34-13-01. SYSTEM OK FOR SERVICE.

Part: NONE — NONE · airframe 104,880 hrs · 15,644 cycles

SHIP 193 E-PATH LIGHTS INOP @ 31AB TO 41AB. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY IAW B767 AMM 33-51. (9118484)

Part: NONE — NONE · airframe 104,812 hrs · 15,633 cycles

SHIP 0193 -ATO- DUE TO RIGHT PACK OFF MESSAGE. CORRECTIVE ACTION: PERFORMED BITE CHECK OF PACK CONTROLLER. NO FAULTS FOUND. RE-RACKED FLOW CONTROL CARD. RT PACK FLOW CONTROL CARD AND FLOW CONTROL VALVE REPLACED ON FOLLOW UP LOG. (9118448)

Part: NONE — NONE · airframe 104,664 hrs · 15,607 cycles

SHIP 193 EMER LIGHTS LOCATED ON AFT SIDE OF AFT GALLEY CENTER AND RT WHITE LITES INOP, CORRECTIVE ACTION: REPLACED AND RETESTED CNTR AND RT EMER LIGHTS (9087298)

Part: NONE — NONE · airframe 104,370 hrs · 15,564 cycles

AIRCRAFT 193, SEAT 1BC EMERGENCY ESCAPE PATH LIGHT INOP. CORRECTIVE ACTION: REPLACED CHARGER. LP 9025158

Part: NONE — NONE · airframe 103,981 hrs · 15,499 cycles

SHIP 0193 -DIV- TO SNN DUE TO LOSS OF CTR SYS HYD QTY AND PRESSURE AFTER EDI DEPARTURE. CORRECTIVE ACTION: LEAK IDENTIFIED AT A RT WING INBOARD SPOILER ACTUATOR. REPLACED #8 SPOILER PCA PER B767 AMM 27-61-02 OPS CHK GOOD. (8966558)

Part: NONE — NONE · airframe 102,586 hrs · 15,242 cycles

SHIP 0193 -ATO- AT 110 KNOTS DUE TO BIRD STRIKE TO LEFT ENGINE. CORRECTIVE ACTION: C/W BIRD STRIKE INSPECTION PER B767 AMM. FOUND 2 LEFT ENGINE EXIT GUIDE VANE BASES DAMAGED. REPAIRED DAMAGE PER ERA 597642-14. NO EVIDENCE OF CORE INGESTION OR OTHER DAMAGE NOTED. C/W HIGH ENERGY STOP INSPECTION PER B767 AMM-NTF. (8207880)

Part: NONE — NONE · airframe 102,195 hrs · 15,160 cycles

SHIP 193 LLCR-2- EMERGENCY EXIT SIGNS DIM. CORRECTIVE ACTION: OPS CHECK NORMAL. O.K FOR SERVICE (8208608)

Part: CONTROLLER — FAULTED (CABIN PRESSURE) · airframe 101,929 hrs · 15,095 cycles

SHIP 0193 -MISC- EICAS MESSAGE CABIN AUTO INOP AFTER PUSHBACK. C/W QRH (SELECTED MANUAL CABIN PRESSURE CONTROL). WHILE RETURNING TO BLOCKS, CABIN PRESSURE INCREASED DURING THROTTLE ADVANCEMENT. CREW OPENED OUTFLOW VALVE MANUALLY CAUSING RAPID PRESSURE DECREASE IN CABIN. CORRECTIVE ACTION: REPLACED BOTH CABIN PRESSURE CONTROLLERS.

Part: NONE — NONE · airframe 101,344 hrs · 14,968 cycles

SHIP 193 DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY ESCAPE PATH LIGHTS (WHITE) INOPERATIVE AT SEATS 13B, 32B AND 35F. CORRECTIVE ACTION: CHECK VOLTAGE NO VOLTAGE AT 3 LOCATIONS. REINSTALLED CONNECTORS AT 13B AND 35F. CHECKS GOOD. REPLACED FUSE IN BATTERY PACK. SYSTEM OPERATIONS IS NORMAL. MCO/PLACARD IS REMOVED. (LP 8037461)

Part: NONE — NONE · airframe 101,378 hrs · 14,974 cycles

SHIP 193 DURING SERVICE CHECK FOUND CEILING MAIN AISLE EMERGENCY ABEAM L4 LAV INOPERATIVE. CORRECTIVE ACTION: REPLACED CEILING LIGHT ASSEMBLY. SYSTEM OPERATION IS NORMAL. MCO/PLACARD REMOVED. (LP 8037460)

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 100,975 hrs · 14,899 cycles

SHIP 193 EXTERIOR EMERGENCY LIGHTING SYSTEM IS INOPERATIVE. CORRECTIVE ACTION: REPLACED POWER SUPPLY AND BATTERY PACK. SYSTEM OPERATION IS NORMAL. (LP 6383207)

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 2 EA DENTS ON UPPER SURFACE OF R/H HORIZONTAL STA. 25" AFT OF FRONT SPAR, 4" I/B OF RIB STA 157.27 AND 31" AFT OF FRONT SPAR, 2" I/B OF RIB STA 157.27. C/W ERA 592734-14. (LP 1904406)

Part: SKIN — NOT REPORTED (BS 952 RBL86-89) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 DURING H CHECK MAINTENANCE FOUND UPPER SURFACE OF RT WING CTR SECTION STA 952 RBL 86-89. REPAIRED PER ERA 592436-14. (LP 7030796)

Part: COUNTERBALANCE — FAILED (PAX DOOR) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 FORWARD L/H DOOR IS TOO HEAVY TO OPEN IN MANUAL MODE. CORRECTIVE ACTION: REPLACED COUNTERBALANCE ASSEMBLY PRIOR TO FURTHER FLIGHT.

Part: SKIN — CRACKED (RT WING) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND 1 EA FASTENER CRACKED ON RT LOWER SKIN STRINGER L-6.5. C/W ERA 592453-14AD. (LP 1900572)

Part: COUNTERBALANCE — FAILED (LT DOOR) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 AFT L/H DOOR. DOOR TO HEAVY TO OPEN IN MANUAL MODE. CORRECTIVE ACTION: REPLACED COUNTER BALANCE. (LP 1900796)

Part: STRINGER — DAMAGED (WING) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND LOWER WING SKIN STRINGER L6.5 MOD, FOUND HOLE #2 STEP 10.D HOLE SIZE GREATER THAN 0.3185. HOLE DIAMETER IS 0.375. C/W ERA 592453-14AD. (LP 1900580)

Part: SEAT TRACK — CORRODED (BS 1075 LBL 11) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON PAX CABIN SEAT TRACK AT STA 1075 LBL 11. REPLACED SEAT TRACK. (LP 1900511)

Part: COUNTERBALANCE — FAILED (RT DOOR) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 R/H DOOR. DOOR TO HEAVY TO OPEN IN MANUAL MODE. CORRECTIVE ACTION: REPLACED COUNTERBALANCE. (LP 1900764)

Part: BOTTLE — NOT REPORTED (OVERWING SLIDE) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 OFFWING SLIDE BOTTLES NEED REPLACED. CORRECTIVE ACTION: REPLACED SLIDE.

Part: COUNTERBALANCE — FAILED (RT DOOR) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 FORWARD RT DOOR IS TOO HEAVY TO OPEN IN MANUAL MODE. CORRECTIVE ACTION: REPLACED COUNTER BALANCE. SYSTEM OPERATION IS NORMAL. (LP 1900745)

Part: SKIN — DAMAGED (RT WING) · airframe 105,823 hrs · 15,829 cycles

SHIP 193 DURING HCK AT ATS-MCI, AN OVERSIZED HOLE/FREEZE PLUG WAS FOUND INSTALLED ON RH LOWER WING SKIN DURING EM5724-01010-40B. ER/A 592453-14AD. CORRECTIVE ACTION: ER/A 592453-14AD REVISED TO REV. A. ACCOMPLISH ER/A 592453-14AD REV A SECTION II INSPECTIONS. (1899766)

Part: STIFFENER — DAMAGED (BS 1153) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND AFT CARGO BAY STA 1153 FWD FACE WEB STIFFENER AT RBL 8 HAS DAMAGE IN RADIUS. C/W 592815-14. (LP 1899368)

Part: FLOORBEAM — CORRODED (BS 888 LBL 9) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 FORWARD MID LAV FLOOR BEAM UPPER SURFACE CORRODED STATION 888 LBL 9. REPRIED PER SRM 53-00-51. (LP1892290)

Part: STRUCTURE — CORRODED (BS 955 LBL 67-73) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON UPPER SURFACE OF LEFT WING CENTER SECTION STA 955 LBL 67-73. REPAIRED PER ERA 592546-14. (LP 1891208)

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION: HORIZONTAL STAB. CENTER SECTION UPPER SKIN UPPER SURFACE RIGHT SIDE 30" FROM CENTER 12" AFT OF FWD EDGE. REPAIRED PER ERA 592478-14 REF LP 1889089. (LP 1890093)

Part: COUNTERBALANCE — DAMAGED (SERVICE DOOR) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 FWD RT SERVICE DOOR IS TOO HEAVY TO OPEN IN MANUAL MODE. CORRECTIVE ACTION: REPLACED COUNTERBALANCE ASSEMBLY. SYSTEM OPERATION IS NORMAL. (LP 1883303)

Part: SKIN — CORRODED (HORIZONTAL STAB) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 DURING INSPECTION MAINTENANCE FOUND CORROSION HORIZONTAL STAB. CENTER SECTION UPPER SKIN UPPER SURFACE RIGHT SIDE 30" FROM CENTER 25" FWD FROM AFT EDGE. C/W ERA 592369-14. (LP 1881824)

Part: RIVET — LOOSE (BS 1733) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND LOOSE RIVET ON RIGHT HAND FUSELAGE STATION 1733, 15" BELOW HORIZONTAL STABILIZER FABRICATED AND INSTALLED NEW SKIN PANEL PER SRM 53-80-01. (LP 1875038)

Part: SHEAR TIE — CORRODED (BS 1219 S36-37L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1219 STR 36-37L. SHEAR TIE REPLACED. (LP 1874067)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE STA 1197+132 BETWEEN STRS 37L AND 38L FOUND TO BE OUT OF LIMITS DUE TO DAMAGE BEING WITHIN 20X OF A FASTENER HOLE. SHEAR TIE REPLACED. (LP 1874054)

Part: SHEAR TIE — CORRODED (BS 1219 S38-39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1219 STR 38-39R. SHEAR TIE REPLACED. (LP 1874062)

Part: SHEAR TIE — CORRODED (BS 1219 S38-39L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1219 STR 38-39L. SHEAR TIE REPLACED PER SRM 53-00-07. (LP 1874063)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+66 STR 38- 39L. SHEAR TIE REPLACED. (LP 1874039)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+66 STR 39R- 38R. REMOVED AND REPLACED SHEAR TIE PER SRM. (LP 1873969)

Part: SHEAR TIE — CORRODED (BS 1197 S35-36L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+66 STR 35- 36L. SHEAR TIE REPLACED. (LP 1874046)

Part: GUSSET — CORRODED (BS 1154 RBL21) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON GUSSET ATTACHED TO WEB STA 1154 RBL 21.5. REPLACED GUSSET PER SRM. (LP 1874256)

Part: SHEAR TIE — CORRODED (BS 1197-S35-36) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS1197 STR 35 -36. REPLACED SHEAR TIE. (LP 1874015)

Part: SHEAR TIE — CORRODED (BS 1197 S27-38R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+66 STR 37- 38R. THE OUT OF LIMITS DUE TO DAMAGE BEING WITHIN 20X OF A FASTENER HOLE PER 53-00-07. SHEAR TIE REPLACED. (LP 1873958)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+66 STR 36- 37R. SHEAR TIE REPLACED. (LP 1874029)

Part: SHEAR TIE — CORRODED (BS 1219 S38R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SEAR TIE CLIP STA 1219, STR 38R. SHEAR TIE REPAIRED PER SRM 53-00-07. (LP 1874004)

Part: SHEAR TIE — CORRODED (BS 1219 S37-38L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY SHEER TIE/CLIP BS 1219 STR 37-38L. SHEAR TIE REPLACED PER SRM. (LP 1874065)

Part: SHEAR TIE — CORRODED (BS 1197-S37-38R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS1197 STR 37 -38R. SHEAR TIE REPLACED PER SRM. (LP 1874244)

Part: RIVET — LOOSE (BS 1733) · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND LOOSE RIVET ON FUSELAGE OUTER SKIN STA 1733 15" BELOW HORIZONTAL STABILIZER LOWER SKIN REMOVED DAMAGED SKIN PANEL FROM R/H HORIZONTAL STABILIZER LOWER AREA DUE TO SEVERE GOUGE. EVALUATED FOUND OUT OF LIMITS. INSTALLED NEW PANEL. (LP 1874073)

Part: FLOORBEAM — CORRODED (BS 1197 RBL 42) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON NUT PLATE ATTACHED TO CARGO FLOOR BEAM FLANGE STA 1197+4 RBL 42. REPLACED FLOOR BEAM. (LP 1874402)

Part: SHEAR TIE — CORRODED (BS 1197 S38-39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECITON MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO BAY FRAME SHEER TIE/CLIP BS 1197+88 STR 38- 39R. REPLACED SHEAR TIE PER SRM. (LP 1874048)

Part: LANYARD — FRAYED (OVERWING EXIT) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 DUAL OVER WING EMERGENCY EXITS DOOR 844 RIGHT SIDE EXTERNAL FLAP DOOR FLAP FORWARD LANYARD IS FRAYED. CORRECTIVE ACTION: REPLACED LANYARD. SYSTEM OPERATION IS NORMAL. (LP 1871933)

Part: SHEAR TIE — CORRODED (BS 1197 S38R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT STA 1197+132, STR 38R. REPLACED SHEAR TIE PER SRM. (LP 1869497)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUN CORROSION LEVEL 2 ON SHEAR TIE STA 1197+22 BETWEEN S37R AND S38R. REPLACED SHEAR TIE PER SRM. (LP 1869490)

Part: SHEAR TIE — CORRODED · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON SHEAR AND REPLACED. (LP 1868516)

Part: SHEAR TIE — CORRODED (BS 1197 S39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE STA 1197+132, STR 39R, SHEAR TIE REPLACED. (LP 1868497)

Part: SHEAR TIE — CORRODED (BS 1197 S36R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1197+44,STR 36R. SHEAR TIE REPLACED PER SRM. (LP 1868495)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSEPCTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE 1197+22 BETWEEN S36R AND S37R. SHEAR TIE REPLACED PER SRM. (LP 1868507)

Part: SHEAR TIE — CORRODED (BS 1175 S39L-R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAITNENANCE FOUND CORROSION LEVEL 2 ON SHEAT TIE 1175 BETWEEN S39R AND S39L. SHEAR TIE REPLACED PER SRM. (LP 1868498)

Part: SHEAR TIE — CORRODED (BS 1219 S33R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVE 2 ON SHEAR CLIP STA 1219, STR 33R . REPLACED SHEAR TIE. (LP 1868521)

Part: SHEAR TIE — CORRODED (BS 1197 S37-38L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE STA 1197 BETWEEN S37L AND S38L. SHEAR TIE REPLACED PER SRM. (LP 1868490)

Part: FLOORBEAM — CORRODED (BS 1153 RBL 23) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON LOWER SURFACE OF FLOOR BEAM TOP FLANGE STA 1153 RBL 23.5. REPLACED CHORD PER SRM. (LP 1868419)

Part: SHEAR TIE — CORRODED (BS 1197 S37R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1197+132, STR 37R. SHEAR TIE REPLACED PER SRM. (LP 1868511)

Part: SHEAR TIE — CORRODED (BS 1263 S36R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1263+19, STR 36R. REPLACED SHEAR TIE. (LP 1868403)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT 1197 BETWEEN S37L AND 36L. SHEAR TIE REPLACED PER SRM. (LP 1868519)

Part: SHEAR TIE — CORRODED (BS 1197 S39L-R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE SAT 1197 BETWEEN S39L AND S39R AND REPLACED SHEAR TIE. (LP 1867280)

Part: SHEAR TIE — CORRODED (BS 1197 S36-37L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE AT STA 1197+132 BETWEEN STRS 36L AND 37L. REPLACED SHEAR TIE. (LP 1867271)

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON NUT PLATE STA 1197+132 BL 13L AFT CARGO FLOOR BEAM. REPLACED INNER CHORD "TEE CAP" AT STA 1197+132 AFT CARGO FLOOR BEAM. (LP 1865936)

Part: SHEAR TIE — CORRODED (BS 1197 S35-36R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE IN AFT CARGO AT STA 1197+66, STR 36R AND STR 35R, FOUND OUT OF LIMITS. SHEAR TIE REPLACED. (LP 1865411)

Part: SHEAR TIE — CORRODED (BS 1153 S38-39L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAITNENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE STA 1153 BETWEEN S38L AND S39L. SHEAR TIE REPLACED. (LP 1865453)

Part: SHEAR TIE — CORRODED (BS 1219 S35R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INPSECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1219, STR 35R EVALUATED CORROSION ON SHEAR TIE IN AFT CARGO AT STA 1219, STR 35R AND STR 34R, FOUND OUT OF LIMITS. SHEAR TIE REPLACED PER SRM. (LP 1865585)

Part: SHEAR TIE — CORRODED (BS 1175 S38-39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INPSECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE 1175 BETWEEN S39R AND 38R. REPLACED SHEAR TIE. (LP 1865532)

Part: SHEAR TIE — CORRODED (BS 1219 S39L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1219, STR 39L EVALUATED CORROSION ON SHEAR TIE IN AFT CARGO AT STA 1219, STR 39L AND STR 39R, FOUND OUT OF LIMITS. SHEAR TIE REPLACED PER SRM. (LP 1865563)

Part: SHEAR TIE — CORRODED (BS 1219 S34R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1219, STR 34R AND REPLACED SHEAR TIE. (LP 1865650)

Part: SHEAR TIE — CORRODED (BS 1241 S39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1241, STR 39R AND REPLACED SHEAR CLIP. (LP 1865660)

Part: SHEAR TIE — CORRODED (BS 1351 S39L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA. 1351, STR 39L. SHEAR TIE REPLACED PER SRM. (LP 1865420)

Part: SHEAR TIE — CORRODED (BS 1241 S36R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1241, STR 36R. SHEAR CLIP REPLACED. (LP 1865667)

Part: SHEAR TIE — CORRODED (BS 1153 S36L-R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE 1153 BETWEEN S39L AND S39R. SHEAR TIE REPLACED. (LP 1865427)

Part: SHEAR TIE — CORRODED (BS 1153 S38-39R) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR TIE STA 1153 BETWEEN S38R AND 39R. SHEAR TIE REPLACED. (LP 1865468)

Part: SHEAR TIE — CORRODED (BS 1175-37-38L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 SHEAR TIE STA 1175 BETWEEN S37L AND S38L. REPLACED SHEAR TIE. (LP 1865486)

Part: SHEAR TIE — CORRODED (BS 1351 S38L) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON SHEAR CLIP STA 1351, STR 38L. SHEAR TIE REPLACED. (LP 1865674)

Part: NUT PLATE — CORRODED (BS 1197) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON NUTPLATE ATTACHED TO CARGO FLOOR BEAM UPPER FLANGE STA 1197+4 RBL 42. REPLACED FLOOR BEAM PER SRM. (LP 1633315)

Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 100,956 hrs · 14,893 cycles

DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 AFT CARGO FLOOR BEAM ON NUT PLATE STA. 1197+66 BL 8L. REPLACED INNER CHORD UPPER FLANGE. (LP 1860067)

Part: LATCH — NO TEST (LT OVRWG SLIDE) · airframe 100,956 hrs · 14,893 cycles

SHIP 193 L/H OVER-WING EMERGENCY SLIDE #3 LATCH FAILED PULL TEST. CORRECTIVE ACTION: CORRECTED L/H #3 SLIDE LATCH. SYSTEM OPERATION IS NORMAL. (LP 1856561)

Part: SOCKET — DEFECTIVE (EMERGENCY LIGHT) · airframe 100,905 hrs · 14,885 cycles

EMERGENCY LIGHTS AT SEAT 19FG ARE INOPERATIVE. MAINTENANCE REPLACED SOCKETS AND CONNECTORS. SYSTEM OPERATION IS NORMAL.

Part: PITOT LINE — DISCONNECTED (LEFT) · airframe 100,063 hrs · 14,764 cycles

AIR TURNBACK DUE TO THE CAPTAIN'S AIRSPEED INDICATION AT ZERO ON TAKE OFF, ALONG WITH RUDDER RATIO, AILERON LOCKOUT, IAS DISAGREE FAULTS. FOUND PITOT LINE TO LEFT ADC NOT CONNECTED. CONNECTED PITOT LINE AND PERFORMED A LEAK CHECK OF SYSTEM. ALL CHECKED NORMAL.

Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 99,773 hrs · 14,715 cycles

EMERGENCY LIGHTS INOPERATIVE SEAT GROUP 33 34 AB AND 19 GF ALL THREE SEATS FOUND WIRES BROKEN AT SIDEWALL. REPLACED TERMINALS AT SEATS 33 AB 34 AB AND 19 GF

Part: CONNECTOR — EXPOSED (EMERGENCY LIGHT) · airframe 99,520 hrs · 14,684 cycles

EMERGENCY PATH LIGHT WIRING HARNESS QUICK DISCONNECT PLUG EXPOSED AT SEAT 26G BY SIDEWALL LWR RT. RE-SECURED WIRING AT SEAT 26G, O.K. FOR SERVICE. (LP6560246)

Part: LIGHT — INOPERATIVE (CREW REST) · airframe 96,574 hrs · 14,304 cycles

DURING SERVICE CHECK, FOUND ALL EMERGENCY LIGHTS INOP IN LOWER CREW REST. REPLACED ALL BULBS. SYSTEM OPERATION IS NORMAL.

Part: BUMPER — DAMAGED (CABIN) · airframe 95,045 hrs · 14,095 cycles

FOUND EMERGENCY FLOOR LIGHTING SEAT AISLE BUMPER DAMAGED AT 28B. REPLACED BUMPER. SYSTEM OPERATION IS NORMAL.

Part: SWITCH — DEFECTIVE (EMERGENCY LIGHTS) · airframe 92,743 hrs · 13,773 cycles

FOUND ALL EMERGENCY LIGHTS UNABLE TURN OFF WHEN M43 EMERGENCY LIGHTS CONTROL PANEL IS IN THE OFF POSITION. FOUND THE FWD ATTENDANT PANEL S1 SWITCH DEFECTIVE AND REPLACED. SYSTEM OPS NORMAL.

Part: WIRE — DETACHED (EMERGENCY LIGHT) · airframe 92,629 hrs · 13,754 cycles

EMERGENCY LIGHTS AT SEAT 19G ARE INOPERATIVE. MAINTENANCE TERMINATED THE CONNECTIONS. SYSTEM OPERATION IS NORMAL.

Part: CONNECTOR — DAMAGED (FIRE LOOP) · airframe 89,224 hrs · 13,233 cycles

LEFT ENGINE FIRE LOOP 2 STATUS MESSAGE DURING FLIGHT. REPAIRED THE CONNECTORS AT BOTTOM 6 O`CLOCK POSITION. SYSTEM OPERATION IS NORMAL

Part: RELAY — FAILED (SPEED BRAKE) · airframe 87,734 hrs · 12,992 cycles

ON LANDING WITH SPEED BRAKES LEVER ARMED THE SPEED BRAKES DID NOT AUTOMATICALLY EXTEND. AUTO BRAKE SYSTEM INOPERATIVE. REPLACED AUTO SPEED BRAKE EXTENSION RELAY. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 86,577 hrs · 12,816 cycles

LADDER EXIT SIGN INOPERATIVE. RELAMPED SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 86,577 hrs · 12,816 cycles

FORWARD EXIT SIGN IS INOPERATIVE AND REPLAMPED. SYSTEM OPERATION IS NORMAL.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

CABIN FRAME AT BS 1307, S13R FOUND WITH CORROSION, R & R.

Part: TRUSS — CORRODED (BS 1197) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

RT CABIN OTBD TRUSS AT S20R BS 1197+66- BS 1197+88. FOUND WITH CORROSION, R & R.

Part: TRUSS — CORRODED (BS 1175-1197) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

CABIN TWO OTBD TRUSS AT S20R BS 1175-1197+22. FOUND WITH CORROSION, R & R.

Part: TRUSS — CORRODED (BS 1197) · airframe 83,569 hrs · 12,360 cycles

RIGHT CABIN O/B TRUSS AT BS 1197+44 -1197+66 S20R FOUND WITH CORROSION, R & R.

Part: TRUSS — CORRODED (BS 1153-1175) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

CABIN LT TRUSS AT BS 1153-1175, FOUND WITH CORROSION, R & R.

Part: FLOORBEAM — CORRODED (BS 1480) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

LT CABIN AFT FLOORBEAM AT BS 1480 FOUND WITH CORROSION AND REPAIRED.

Part: STRINGER — CORRODED (BS 1197) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

STRINGER 20R BS 1197+88 FOUND CORRODED. STRINGER REPLACED.

Part: FRAME — CORRODED (BS 1307) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

CABIN FRAME AT BS 1307, S19-20R CORRODED. FOUND WITHOUT OF LIMIT AND REPLACED.

Part: FRAME — CORRODED (BS 1285) · corrosion level 2 · airframe 83,569 hrs · 12,360 cycles

CABIN FRAME AT BS 1285, S17R FOUND CORRODED AND FOUND OUT OF LIMITS AND REPLACED.

Part: FLOORBEAM — CORRODED (BS 287) · airframe 83,569 hrs · 12,360 cycles

CABIN FWD GALLEY FLOORBEAM AT BS 287, RBL 63 UPPER CHORD CORRODED. R & R IAW ERA 534314-14.

Part: FRAME — CRACKED (BS 883) · airframe 83,569 hrs · 12,360 cycles

FOUND ONE CRACK ON THE LT BS 883.5 FRAME INNER CHORD SURFACE AND TRANSITION RADIUS. REPAIRED.

Part: STRINGER — CRACKED (LT WING) · airframe 79,945 hrs · 11,838 cycles

LT WING STRINGER 6.5 HAS CRACKED HOLE NR 1. REPAIRED IAW ERA 533647-14AD. LP 1892101.

Part: CHARGER — INOPERATIVE · airframe 79,399 hrs · 11,750 cycles

WHILE PERFORMING OPS CHECK OF EMERGENCY LIGHTS FOUND BATTERY CHARGER M9009 INOPERATIVE. REPLACED BATTERY CHARGER. SYSTEM OPERATION IS NORMAL.

Part: TERMINAL — LOOSE (EMERGENCY LIGHT) · airframe 73,547 hrs · 10,874 cycles

EMERGENCY EXTERIOR LIGHT INOPERATIVE AT L1 DOOR. MAINTENANCE FOUND GROUND WIRE RING TERMINAL GD4734-DC LOOSE, SECURED TERMINAL SYS OPS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 73,044 hrs · 10,793 cycles

EMERGENCY LIGHT INOPERATIVE AT 32AB-42AB. MX REPLACED POWER SUPPLY & REPLACED CONNECTOR. SYS OPS IS NORMAL.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,453 hrs · 10,700 cycles

FOUND SEAT EMERGENCY LIGHTS 31A-41A INOPERATIVE. THE BATTERY CHARGER AT M9010 WAS REPLACED. SYS OPS IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,453 hrs · 10,553 cycles

EMERGENCY SEAT MOUNTED LIGHTING INOPERATIVE AT 41C. MX SECURED. SYS OPS NORMAL.

Part: SKIN — DAMAGED (BS 287-654) · airframe 71,595 hrs · 10,571 cycles

FOUND TWENTY LIGHTNING STRIKE DAMAGE POINTS BETWEEN BS 287 AND 654+110, S34-36L. REMOVED DAMAGE IAW SRM 53-00-01, REPAIR B SECTION C/W BHEC INSPECTION OF HOLES IAW SRM 53-00-01, FIG 201, NO CRACKS FOUND.

Part: FLOORBEAM — MISREPAIRED (BS 654) · airframe 70,875 hrs · 10,467 cycles

FLOORBEAM MISREPAIRED IAW SRM AT BS 654+121 RBL 54.75. REPAIRED IAW SRM 53-00-51, REPAIR 1, FIG 201.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,910 hrs · 10,193 cycles

RIGHT SIDE ROW 1-GH-5GF EMERGENCY LIGHTS ARE INOPERATIVE. FUSES IN THE CHARGER ASSEMBLY WERE REPLACED. SYSTEM OPERATION IS GOOD.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 68,910 hrs · 10,193 cycles

EMERGENCY LIGHTS ROWS 1AB - 6AB ARE INOPERATIVE. MAINTENANCE REPLACED THE FUSE IN THE CHARGER ASSY SYSTEM CHECKS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,356 hrs · 9,864 cycles

EMERGENCY LIGHTS AT 27AB ARE INOPERATIVE. TWO LIGHTS WERE REPLACED AT 27B. SYSTEM OPERATION IS NORMAL.

Part: SOCKET — DEFECTIVE (CABIN) · airframe 64,742 hrs · 9,654 cycles

MAINTENANCE FOUND FORWARD CABIN EMERGENCY ESCAPE PATH LIGHTS INOPERATIVE, ROW 6AB AFT NEEDS NEW SOCKET. MAINTENANCE REPLACED THE SOCKET AT SEAT 6AB. SYSTEM OPERATION IS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,611 hrs · 9,381 cycles

WHITE EMERGENCY LIGHT AT 25FG IS INOPERATIVE. MX REPLACED THE BULBS AND SOCKET ASSY BUT NO HELP. FWD IAW MEL 33-51-03A.

Part: SKIN — CORRODED (BS 955) · corrosion level 2 · airframe 59,899 hrs · 9,027 cycles

BS 955 LT SKIN INNER FACE FOUND CORROSION AFT FAIL-SAFE STRAP TRIMMED OFF AND SKIN REPAIRED IAW ER/A 482274-14AD.

Part: SPAR — DELAMINATED (RUDDER) · airframe 59,899 hrs · 9,027 cycles

RUDDER FRONT SPAR EXTERNAL SURFACE AT RUDDER STA 144, RT L/E FLANGE FOUND DELAMINATED. REPAIR WITH RESIN CARRIED OUT AT DELAMINATED AREA IAW ER/A 482281-14.

Part: FRAME — CRACKED (BS 903 S20-21R) · airframe 59,899 hrs · 9,027 cycles

CABIN RT BS 903 BTWN S20R-21R. FRAME INNER CHORD FOUND CRACKED. REPAIRED IAW ER/A 482276-14AD.

Part: FRAME — CRACKED (BS 903 S20-21L) · airframe 59,899 hrs · 9,027 cycles

CABIN LT BS 903 BTWN S20L-21L. FRAME INNER CHORD FOUND CRACKED AND REPAIRED IAW ER/A 482276-14AD.

Part: FITTING — CRACKED (BS 955 BULKHEAD) · airframe 59,899 hrs · 9,027 cycles

FUSELAGE LT BS 955 REAR SPAR BULKHEAD FITTING AREA FOUND 2 CRACKS APPROX .1875" LONG AND STRAP REPAIRED IAW ER/A 482274-14AD.

Part: APU — FAILED · airframe 59,442 hrs · 8,631 cycles

APU DOOR STATUS MESSAGE DISPLAYED AFTER APU SHUTDOWN ON GROUND. FWD TO MCO AND PLACARD IAW MEL M49-11-01B. APU AIR INTAKE DOOR CLOSED MANUALLY. APU RENDERED INOP T/S IAW FIM 49-11-00-10 FIG 104 - APU OP NORMAL- MCO/PLACARD REMOVED. ETOPS CATEGORY 'E': PROBLEMS WITH SYS CRITICAL TO ETOPS

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 59,319 hrs · 8,617 cycles

32G EMERGENCY EXIT LIGHT INOP. R & R SEAT HARNESS.

Part: IDG — FAILED (NR 1 ENGINE) · airframe 58,157 hrs · 8,457 cycles

LEFT IDG FAILED - APU INITIALLY STARTED THEN AUTO SHUT DOWN WITH OIL QTY MSG. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: OVEN — SPARKS (AFT GALLEY) · airframe 57,253 hrs · 8,346 cycles

NR 6 OVEN IN AFT GALLEY SPARKED AND HAD BURNING ODOR C/B PULLED ISOLATED/C REPLACED NBVR 6 OVEN CKS GD. ETOPS CATEGORY 'F': ANY OTHER EVENT DETRIMENTAL TO ETOPS

Part: FLOORBEAM — CORRODED (BS 720) · airframe 51,895 hrs · 7,692 cycles

DURING B ZONE MOD, FOUND CORROSION ON FLOORBEAM AT BS 720 LBL 26 UPPER CHORD REMOVED CORROSION ON FLOORBEAM, FOUND TO BE OUT OF LIMITS. REPAIRED IAW SRM 53-00-51 FIG 201 DWG NR 06T083N032 DDN NR 55. INSTALLED IAW SRM 53-00-21, 51-40-02 DWG NR 06T083N032 DDN NR 35.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 51,895 hrs · 7,692 cycles

CORROSION ON FLOORBEAM BS 720 RBL 26 UPPER CHORD. REPAIRED FLOORBEAM PER SRM 53-00-01 FIG 201.

Part: CONNECTOR — LOOSE (IDG) · airframe 50,153 hrs · 7,480 cycles

RIGHT GEN DRIVE LIGHT ILLUMINATED SHORTLY AFTER T/O. RETURNING TO JFK FOR REPAIRS. FOUND CONNECTOR LOOSE ON IDG, TIGHTEN SAME. RECONNECTED IDG. RAN R ENGINE AND LOADED RT IDG. OPS NORMAL.

Part: ENGINE — MALFUNCTIONED (APU) · airframe 48,146 hrs · 7,242 cycles

APU AIR LOW DUCT PRESSURE--13 PSI. REMOVED AND REPLACED APU PER MM. RETURNED APU BLEED VALVE TO NORMAL.

Part: TRANSMITTER — INTERMITTENT (HYD SYSTEM) · airframe 47,596 hrs · 7,177 cycles

CENTER HYD QTY DROPPED TO ZERO 3X ON TAXI OUT. RESERVOIR LIGHT CAME ON OVERHEAD ALSO. FWD TO MCO AND PLACARD PER MEL 29-33-02. CTR HYD QTY INDICATION INOP. PERFORM REP CK. REPLACED CENTER RESERVOIR QTY TRANSMITTER PER M/M REMOVED MCO A PLAC LEAK CHECK OK.

Part: CONTROL MODULE — MALFUNCTIONED (STABILIZER TRIM) · airframe 46,233 hrs · 7,012 cycles

DISCONTINUED TAKEOFF AT 65-70 KIAS FOR AN UNSCHEDULED TRIM LIGHT STAB TRIM/AILERON LOCK-OUT MODULE SAM M524 W/ FAULT BALL STCM. FAULT BALL RESET. PRIMARY AND ALTERNATE STAB TRIM OPERATED FULLY NORMAL WITH NO FURTHER EICAS MSGS. FIM PROC 27-09-00 FIG 106A CARRIED OUT SATIS. ADC TEST L AND R CARRIED OUT SATIS IAW MM. REMOVED AND REPLACED LEFT STAB TRIM CONTROL MODULE AS PER AMM. LEAK CHK GOOD. PERFORMED REQUIRED RII INSP PER TOPP 40-30-05 ITEM 6 AND TOPP 40-10-20 PG 3/B ITEM 2 NOTE BOX.

Part: BYPASS VALVE — LEAKING (NLG STEERING) · airframe 45,640 hrs · 6,942 cycles

AT PUSH BACK, STEERING BYPASS VALVE NOTICED LEAKING. FOUND UNION TUBE ON BYPASS VALVE LOOSE. TIGHTENED UNION TUBE TUBE, OPS CHECK GOOD.

Part: MODULE — UNKNOWN (P-50 PANEL) · airframe 45,591 hrs · 6,937 cycles

ON T/O UNSCHED STAB TRIM LIGHT ILLUMINATED RETURNED TO GATE. LEFT SAM FAULT STCM REPLACED FSPM CARD M838 LEFT SIDE RAN TEST PER AMM TEST GOOD.

Part: MOUNT — CRACKED (NR 1 ENGINE) · airframe 44,261 hrs · 6,778 cycles

DURING ENG EXT HARDWARE INSP, FOUND AFT MOUNT RAILS CRACKED. REPLACED NR 1 ENG.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 42,204 hrs · 6,527 cycles

EMERGENCY LIGHT SEAT 25A INOP ON LIGHTS TEST. REPLACED LIGHT ASSY. OPS CK NORMAL.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 42,176 hrs · 6,523 cycles

MAIN BATTERY CHARGER STATUS MSG. SWAPPED MAIN BATTERY AND CHARGER WITH APU BATT AND CHARGER.

Part: STARTER — SEIZED (NR 1 ENGINE) · airframe 42,099 hrs · 6,513 cycles

LEFT ENGINE START VLV WILL NOT ENGAGE, NO ROTATION. FOUND NR 1 ENG STARTER SEIZED. REPLACED NR 1 ENG STARTER AND SERVICED PER AMM. LEAK CHECK OK. STARTED ENG AT GATE, IND AND OPN CHECKS NORMAL.

Part: SMOKE — DETECTED (COCKPIT) · airframe 41,051 hrs · 6,381 cycles

SMOKE IN FWD HALF OF CABIN AND SMOKE IN COCKPIT. PERFORMED ENGINE RUN AND DUCT BURN OUT PER AMM. NO TROUBLE FOUND AND INSPECTED E/E, NO TROUBLE FOUND.

Part: ENGINE — SMOKE (NR 2) · airframe 41,051 hrs · 6,381 cycles

SMOKE IN FWD HALF OF CABIN AND SOME IN COCKPIT. PERFORMED ENGINE RUN/ DUCT BURNOUT PER MM, NO TROUBLE FOUND. INSPECTED E/E, NO TROUBLE FOUND.

Part: ODOR — DETECTED (CABIN) · airframe 40,669 hrs · 6,334 cycles

ON APPROACH F/A`S REPORTED HOT RUBBER SMELL IN CABIN DOOR 2L. CHECKED WITH ALL GALLEY EQUIPMENTS ON AND APU AND PACKS RUNNING. NO ODORS SUSPECT FOUND.

Part: SENSOR — FAILED (NR 1 ENGINE) · airframe 40,219 hrs · 6,276 cycles

LT REVERSER UNLOCKED LIGHT ILLUMINATED DURING TAKEOFF ROLL. EXTINGUISHED AFTER ABORT. REPLACED RT THRUST REVERSER ACTUATOR PROX SENSOR S-1608.

Part: ACTUATOR — MALFUNCTIONED (LT A/C PACK) · airframe 39,958 hrs · 6,241 cycles

LT PACK TEMP LIGHT ILLUMINATED AT FL280. PACK THEN TRIPPED AND WOULD NOT RESET. T/S PER FIM FOUND LT PACK EXH ACT INOP. REPLACED ACTUATOR, OPS CHECKS NORMAL PER AMM.

Part: SEAL — DAMAGED (COCKPIT WINDOW) · airframe 38,364 hrs · 6,025 cycles

EXTREMELY LOAD EAR PIERICING SQUEAL AT 8.0 PSID COMING FROM L2 WINDOW. REPLACED L2 WINDOW SEAL PER AMM. PRESSURIZED TO 8.0 PSID. NO SQUEAL NOTED.

Part: ODOR — DETECTED (MID GALLEY) · airframe 33,653 hrs · 5,392 cycles

MID GALLEY FREEZER GAVE OFF AN ELECTRICAL SMELL. DEACTIVATE FREEZER AND FWD TO MCO. C/B PULLED AND COLLARED.

Part: ACTUATOR — MALFUNCTIONED (LT O/B AILERON) · airframe 33,627 hrs · 5,388 cycles

AILERON LOCKOUT IN FLIGHT AND C/B POPPED. A/C DIVERTED DUE TO WEATHER AND LT O/B AILERON LOCKED OUT. CLEANED LT O/B AILERON LOCKOUT ACT CONNECTOR AND SWAPPED LEFT AND RIGHT SAMS. ALL AILERONS OPERATIONAL. AS PRECAUTION PUT THE AILERON LOCKOUT SYS TO MCO 27-11-02A.

Part: PSEU — FAILED (E/E BAY) · airframe 22,196 hrs · 3,558 cycles

CONFIG LIGHT AND WARNING HORN WOULD NOT SILENCE. DIVERTED TO LGW. PSEU FAILED. REPLACED AND CHECKS GOOD.

Part: POWER SUPPLY — INOPERATIVE (EXIT SIGN) · airframe 21,323 hrs · 3,385 cycles

ON L/O CHECK FOUND AISLE EXIT SIGN AT RIGHT OVERWING EXIT HATCHES INOPERATIVE. RESEAT CONNECTOR ON POWER SUPPLY MODULE M732 CHECKS OK.

Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 20,107 hrs · 3,184 cycles

NR 2 ENGINE HAD COMPRESSOR STALL AT ROTATION OF 170 KTS. ENGINE TEMP WENT TO 673. ENGINE EXPERIENCED MULTIPLE STALLS. REPLACED NR 2 ENGINE.

Part: IDG — FAILED (LT ENGINE) · airframe 18,939 hrs · 3,004 cycles

DIVERTED TO JFK DUE TO LT IDG FAILED AND GEN BREAKER TRIPPED. REPLACED LT IDG.

Part: MODULE — FAILED (AFT LAV TANK) · airframe 16,792 hrs · 2,651 cycles

AFTER T/O FIRST CLASS AND RT AFT LAV INOP. AFT WASTE SHUT DOWN. REPLACED AFT WASTE TANK LOGIC CTL MODULE, OPS NORMAL. ALSO FOUND AFT RT-R2- LAV VLV STUCK OPEN. ABLE TO CLOSE SAME MANUALLY, CONNECTED FLUSH SWITCH AND INOPED LAV. NEEDS NEW TOILET. FWD MCO AND PLACARD PER MEL 25-20-01.

Part: WIRE — BROKEN (SKEW SWITCH) · airframe 15,465 hrs · 2,430 cycles

L/E SLAT ASYMMETRY EICAS INDICATION AND CAUTION LIGHTS CAME ON. FOUND BROKEN WIRE TO LEFT SKEW SWITCH CAUSED BY DAMAGED HARNESS CONDUIT. REPAIRED WIRE.

Part: COMPUTER — FAILED (E/E BAY)

NO AIRSPEED INDICATION CAPTS SIDE ON T/O ROLL. REPLACED CADC. OPS CHECK NORMAL.

Part: BULB — BROKEN (CABIN)

EMERGENCY LIGHTS AT 1D AND 2B INOP. REBULBED.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

F/C AND B/C SEAT MOUNTED EMERGENCY LIGHTS ALL INOP. REPLACED POWER SUPPLY.