N538US

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,087 hrs · 28,606 cycles

SHIP 5638 -MISC/DE- DUE TO SEVERAL LEFT AIR DATA SYSTEM RELATED FAULTS. CORRECTIVE ACTION: REPLACED LEFT AIR DATA COMPUTER.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 87,027 hrs · 28,585 cycles

SHIP 5638 L2 DOOR SLIDE LANYARD LOOSE. CORRECTIVE ACTION: SECURED LANYARD - ALL CHECKS OK. (5086592)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,978 hrs · 28,553 cycles

SHIP 5638 A BLOCK OUT GATE AGENT WAS CLOSING AND REPORTED 2L SLIDE ROPE HANGING DOWN. CORRECTIVE ACTION: STOWED MOORING LINE. (5086558)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,683 hrs · 28,402 cycles

SHIP 5638 LANYARD AT DOOR 2 HANGING OUT. CORRECTIVE ACTION: RESECURED LANYARD AT DOOR 2 AS REQUIRED. A/C OK FOR SERVICE. (4863421)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,590 hrs · 28,343 cycles

SHIP 5638 LANYARD LOOSE UNDER 2L DOOR. CORRECTIVE ACTION: RESECURED LANYARD AS REQUIRED PER B757 AMM 52-11. DOOR OPS NORMAL. (4316572)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,534 hrs · 28,322 cycles

SHIP 5638 SLIDE PACK LANYARD 2L DOOR CAME LOOSE. CORRECTIVE ACTION: RESECURED DOOR 2L SLIDE PACK LANYARD. CONFIRMED SECURE. (4316538)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,527 hrs · 28,316 cycles

SHIP 5638 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:603. CORRECTIVE ACTION: SLIDE INDICATOR LIGHT IS INSTALLED CORRECTLY. (0014661)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,501 hrs · 28,300 cycles

SHIP 5638 SLIDE ATTACHMENT LANYARD LOOSE. CORRECTIVE ACTION: SECURED SLIDE ATTACHMENT LANYARD REF B757 AMM 25-60. (4316510)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 86,496 hrs · 28,296 cycles

SHIP 5638 LANYARD ON L2 DOOR GIRT BAR MECHANISM LOOSE. CORRECTIVE ACTION: RESECURED DOOR L2 LANYARD FOR GIRT BAR ATTACHMENT REF B757 AMM 25-60 (4316500)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,994 hrs · 28,020 cycles

SHIP 5638 2L EMERGENCY SLIDE STRIP HANGING OFF OF DOOR FRAME. CORRECTIVE ACTION: REINSTALLED DOOR 2 L SLIDE PER W/C 2566-9001-2L NRO 630578. VERIFIED INSTALLATION OF SLIDE PER WC 2566- 9001-2L. (4956732)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,384 hrs · 27,680 cycles

SHIP 5638 L2 DOOR EXTERIOR BUTTERFLY HANDLE NOT OPENING PROPERLY. CORRECTIVE ACTION: REMOVED AND REPLACED OUTER HANDLE CENTER BEARING REF B757 AMM 52 -11. (4776816)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,247 hrs · 27,609 cycles

SHIP 5638 EXIT SIGN AFT OF DOOR 2L NEEDS REINSTALLED PARTS IN COCKPIT. CORRECTIVE ACTION: SECURED EXIT SIGN. OK FOR. SERVICE. (4704246)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,239 hrs · 27,605 cycles

SHIP 5638 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS. 2L SLIDE BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: T/S PER FIM 25-66-815-802. CHECKED AND CLEAN GRIT BAR AND SENSOR. OPS CHECKED DOOR WITH LIGHT OPERATIONAL. OPS CHECK GOOD PER B757 AMM 25-66 FCP REMOVED. (2737418)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,181 hrs · 27,573 cycles

SHIP 5638 FOUND 1R ASSIT BOTTLE BELOW LIMITS. CORRECTIVE ACTION: R/R 1R EMERGENCY POWER RESERVOIR IAW B757 AMM 52-11. (4704214)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 85,013 hrs · 27,480 cycles

SHIP 5638 2L DOOR EXIT SIGN COVER BROKEN. CORRECTIVE ACTION: R/R EXIT LIGHT LENS COVER IAW B757 AIPC 33-51-01-34. (9886284)

Part: UNKNOWN — UNKNOWN · airframe 84,923 hrs · 27,437 cycles

SHIP 5638 3R DOOR DOES NOT DISARM PROPERLY (SLIDE LITE OUT) KNUCKLE KNOCKER NOT RETRACTED. CORRECTIVE ACTION: FOUND FROZEN AFTER LANDING. WAITED FOR DOOR TO THAW. OPS NORMAL. (9886206)

Part: NONE — NONE · airframe 84,800 hrs · 27,372 cycles

SHIP 5638 2L EXIT SIGN LENS COVER MISSING. CORRECTIVE ACTION: R/R 2L EXIT SIGN LENS COVER REF B757 CMM 33-51-31. (2642324)

Part: LENS — UNSECURE (EMERGENCY LIGHT) · airframe 84,346 hrs · 27,138 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. LOCATIONS: 2R. SECURED PLASTIC LENS-OPS NORMAL.

Part: NONE — NONE (NONE) · airframe 84,336 hrs · 27,134 cycles

COMPLY WITH ERA 604746-14AD REV. ORIGINAL. COMPLIED WITH ERA 604746-14AD REV. ORIGINAL,

Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 84,336 hrs · 27,134 cycles

AMOC NEEDED PRIOR TO 50,000 FC TOTAL SECTION I REPAIR SSI 53-60-24 ER/A 604746-14.

Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 84,279 hrs · 27,111 cycles

SHIP 5638 CORROSION ON UPPER SKIN BTW STA WBL 80 TO WBL 132 AT AND STRINGER U-13 TO U-14 FRONT SPAR RH WING (RH-AD). CORRECTIVE ACTION: SUMMARY OF NRC00190: UPPER SKIN BTW STA BBL 70.5 TO WSTA 220, REAR SPAR TO S-14 RH WING (RH-AD) WAS REPAIRED PERMANENTLY PER ER/A 603439-14 REV. ORIGINAL SECTION I. (2531684)

Part: SKIN — DAMAGED (RT WING) · airframe 84,288 hrs · 27,113 cycles

ER/A 603439-14, RIGHT WING UPPER SURFACE SKIN BBL 70.5 TO WSTA 220, REAR SPAR TO S14 CORRODED. REPAIRED IAW REF ERA 603439-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 84,288 hrs · 27,113 cycles

CENTER WING BOX UPPER SKIN PANEL U- 10, RBL 52.00 TO RBL 70.50 CORRODED. REPAIRED IAW ERA 603536-14.

Part: FUEL TANK — CORRODED (BS 984) · corrosion level 2 · airframe 84,288 hrs · 27,113 cycles

CORROSION ON UPPER SKIN ON CENTER TANK STA 984 WING BOX RH SIDE AT PASSENGER CABIN. CORRECTIVE ACTION: SUMMARY OF NRC00175: UPPER SKIN ON CENTER TANK STA 984 WING BOX RH SIDE AT PASSENGER CABIN WAS REPAIRED PER ER/A 603536-14 REV: ORIGINAL, SECTION I: PERMANENT REPAIR. (2531488)

Part: SNUBBER — OUT OF LIMITS (R4 DOOR) · airframe 84,266 hrs · 27,105 cycles

OUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT R4 DOOR. R4 DOOR SNUBBER WAS REPLACED WITH A SERVICEABLE ONE PER B757-200 AMM 52-11-10.

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 OUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT L4 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00202. L4 DOOR ROTARY SNUBBER WAS REPLACED WITH A SERVICEABLE ONE PER B757-200 AMM 52-11. (2486865)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 OUT OF LIMITS COMPENSATOR INDICATOR ON SNUBBER AT L2 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00200. L2 DOOR ROTARY SNUBBER WAS REPLACED WITH A SERVICEABLE ONE PER B757-200 AMM 52-11. (2486832)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 AA.AD. AWR: DURING CKECK MEASURE ON GIRT BAR TO VERIFY A MINIMUM ENGAGEMENT THE MEASURE IS OUT OF LIMIT AT 2L DOOR. IN REF STEP 12 CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00255. L2 DOOR GIRT BAR WAS REPLACED FOR A SERVICEABLE ONE PER AMDS. (2485255)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 AA. AD. AWR: MTC REQUEST: DURING CKECK MEASURE ON GIRT BAR TO VERIFY A MINIMUM ENGAGEMENT THE MEASURE IS OUT OF LIMIT AT 4R DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00254. R4 DOOR GIRT BAR WAS REPLACED FOR A SERVICEABLE ONE PER AMDS. (2485257)

Part: SKIN — CORRODED · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 A.A. -AD CORROSION ON HOLES: HOLE #2 ON SKIN/FITTING AT 12 HRS, HOLE #4 ON FITTING AT 1 HRS POS, HOLE #7 ON FITTING AT12 HRS POS, HOLE #9 ON SKIN AT 10 HRS, HOLE #10 ON FITTING AT 10 HRS POS AND SCRATCH ON HOLE #3 SKIN/FITTING AT 2 HRS, (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00180: HOLES #2, #3, #4, #7, #9 & #10 WERE REPAIRED PER PRI 603236-14 REV. 1 AND ER/A 603236-14AD REV. ORIG SECTION I: PERMANENT REPAIR IN REFERENCE TO LOG PAGE 2482521, NRC 00182. (2483716)

Part: SKIN — SCRATCHED · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 A.A - AD. HOLE #1 SCRATCH ON SKIN BTW 6 AND 7 O CLOCK POSITION, HOLE #2 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE, HOLE #3 CORROSION BTW 8 AND 10 O CLOCK POSITION, HOLE #4 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE, HOLE #7 SCRATCHES ON FITTING BTW 11 AND 1 O CLOCK POSITION, HOLE #9 SCRATCHES ON SKIN ALL AROUND HOLE. (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00210: HOLES #1, #2, #3, #4, #7 & #9 WERE REPAIRED PER ERA 603248-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 603248-14 REV. 1 IN REFERENCE TO LOG PAGE 2482471 , NRC 00211. (2483733)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 A.A. -AD CORROSION ON HOLES: HOLE#12 ON FITTING AT 11 HRS POS, HOLE #14 ON SKIN AT 2 HRS, HOLE #17 ON FITTING AT 11 HRS, HOLE #18 ON FITTING 11 HRS POS AND SCRATCH ON HOLE #13 SKIN AND FITTING AT 11 HRS POS,(REF. CARD) CORRECTIVE ACTION: SUMMARY OF NRC 00182: HOLES #12, #14, #17, #18 AND #13 WERE REPAIRED PER PRI 603236-14 REV. 1 AND ER/A 603236-14AD REV. ORIG SECTION I: PERMANENT REPAIR. (2482521)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 A. A. - AD. RH ENG DRAG FTG CLAMP-UP HOLES #11, #12, #13, #14, #15 AND #16, DAMAGES ARE FOUND AS FOLLOW: HOLE #11 SCRATCHES ON SKIN ALL AROUND HOLE, HOLE #12 GOUGE ON FITTING BTW 6 AND 7 O CLOCK POSITION, HOLE #13 SCRATCHES ON FITTING BTW 10 AND 12 O CLOCK POSITION, HOLE #14 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE, HOLE #15 CORROSION ON FITTING BTW 9 AND 11 O CLOCK POSITION, HOLE #16 CORROSION ON FITTING BTW 9 AND 11 O CLOCK POSITION. (REF. CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00211: HOLE #11, HOLE #12, HOLE #13, HOLE #14, HOLE #15 AND HOLE #16 WERE REPAIRED PER ERA 603248-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 603248-14 REV. 1. (2482471)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 603236-14AD. CORRECTIVE ACTION: REF ERA 603236-14AD.

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 603248-14AD. CORRECTIVE ACTION: REF ERA 603248-14AD.

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 DISBONDED AREA OF 9.25IN LENGTH AND 2.0IN WIDTH WAS FOUND ON LOWER SKIN OF SLAT #2 AT OSS 580 APPROX. CORRECTIVE ACTION: SUMMARY OF NRC 00013; DISBONDED AREA AT OSS 580 APPROX OF SLAT #2 WAS REPAIRED PER B757-200 S.R.M. (2479555)

Part: NONE — NONE · airframe 84,266 hrs · 27,105 cycles

SHIP 5638 AFTER REMOVAL WASTE DRAIN VALVE ( AFT VALVE ) CORROSION WAS FOUND ON CUTOUT INTERNAL DOUBLER AT AFT WASTE PAN . IN REF. NRC 00238. CORRECTIVE ACTION: SUMMARY OF NRC 00257, DOUBLER AT AFT WASTE PAN WAS REPLACED PER DWG 146N3650 REV. AH AND B757-200 SRM. (2478209)

Part: NONE — NONE · airframe 83,941 hrs · 27,024 cycles

SHIP 5638 - ATB - DUE TO THE LOSS OF THE LNAV AND VNAV. CORRECTIVE ACTION: PERFORMED AN MCDP FAULT REVIEW WITH ASSOCIATED FAULTS. REPLACED THE RIGHT FMC COMPUTER.

Part: NONE — NONE · airframe 83,850 hrs · 27,003 cycles

SHIP 5638 EMERGENCY LT OVER SEAT 3C MISSING LENS. CORRECTIVE ACTION: REPLACED MISSING COVER 03C PER CMM 33-21-46 OK FOR SERVICE MEL + PLACARD REMOVED. (9204456)

Part: NONE — NONE · airframe 83,859 hrs · 27,006 cycles

SHIP 5638 LOCATIONS:401 AFT ATTENDANT CALL LTS INOP, PAX CALL, LAV CALL, FA CALL ALL INOP. CORRECTIVE ACTION: R/R AFT EMERGENCY EXIT SIGN IAW B757 AMM 33-51 OPS CHK GOOD. (2386695)

Part: TRIM SWITCH — INTERMITTENT · airframe 83,663 hrs · 26,950 cycles

SHIP 5638 -ATB- DUE TO LOSS OF RUDDER TRIM CAPABILITIES. CORRECTIVE ACTION: MTC FOUND TRIM SWITCH INTERMITTING. REPLACED RUDDER AND AILERON CONTROL PANEL. REPLACED THE RUDDER TRIM INDICATOR. ACCOMPLISHED ALL REQUIRED MCDP TESTS.

Part: LENS — MISSING · airframe 83,165 hrs · 26,806 cycles

SHIP 5638 EMERG. LIGHT LENS MISSING IN CENTER AISLE ABOVE SEAT 25C. CORRECTIVE ACTION:INSTALLED LENS COVER ABOVE 25C CHKS GOOD. (8438313)

Part: NONE — NONE · airframe 82,587 hrs · 26,639 cycles

SHIP 5638 ULTRASONIC INSPECTION SHOWS DISBOND BETWEEN BEAR STRAP AND SKIN AROUND CUTOUT IN BEAR STRAP. CORRECTIVE ACTION: COMPLETED ALL STEPS PER PRI 598685-14 REV 0 AND REV 1 & INSURED ALL STEPS MATCH WITH FINALE ERA 598685-14 REV. ORIG. (2193823)

Part: NONE — NONE · airframe 82,587 hrs · 26,639 cycles

SHIP 5638 ER/A 598685-14AD REV ORIG WRITTEN TO DOCUMENT DEVIATIONS TO WC 5331-01232-02G REPAIR TO SATISFY AD 2012-25-11. STAGE II DTE APPROVAL RECEIVED FROM BAC. CORRECTIVE ACTION: REF ERA 598685-14AD REV ORIG. (2193735)

Part: NONE — NONE · airframe 82,057 hrs · 26,493 cycles

SHIP 5638 DURING SVC, FOUND R1 DOOR HANDLE COVER PLATE MISSING. CORRECTIVE ACTION: INSTALLED HANDLE LINING INSERT AT DOOR 1R. (8573942)

Part: NONE — NONE · airframe 81,788 hrs · 26,408 cycles

SHIP 5638 - ATO - AS POWER WAS ADVANCED FOR TAKEOFF THE DOOR 2R DOOR INDICATION ILLUMINATED. CORRECTIVE ACTION: GATE RETURN AND APPLIED MEL. (1/18 LAX) DOOR INDICATION SYSTEM SUBSEQUENTLY CHECKED FOR PROPER ADJUSTMENT AND RETURNED TO SERVICE.

Part: NONE — NONE · airframe 81,788 hrs · 26,408 cycles

SHIP 5638 CABIN EMER LIGHTS INOP AT 4A, 5D, 16A, 40A. CORRECTIVE ACTION: RELAMPED CEILING EMER LIGHT AT ROW 40A - OPS CK GOOD. LIGHTS AT 4A & 16A GO TO M731 BATTERY PACK FUSE 4. REMOVED & REPLACED M731 FUSES. 4A & 16A CEILING LIGHTS OPS CK GOOD. RELAMPED LIGHT BULB FOR OVER HEAD EMERGENCY LIGHT LOCATED ABOVE 5D PER B757 AMM 33-51. OPS CL GOOD. (8479609)

Part: FLAP SYSTEM — OVERSPEED · airframe 81,788 hrs · 26,408 cycles

SHIP 5638 - MISC/DE - OVER TRAVEL SELECTION OF FLAPS WITH FLAP OVERSPEED DURING APPROACH INTO TPA. EICAS MESSAGE TE FLAP DISAGREE DISPLAYED WITH ASSOCIATED LIGHT. C/W QRH AND COMPLETED APPROACH. CORRECTIVE ACTION: C/W FLAP OVERSPEED INSPECTION AND NO-GO ODI PROCEDURES. NO TROUBLE FOUND.

Part: NONE — NONE · airframe 81,456 hrs · 26,261 cycles

SHIP 5638 AFT LEFT DOOR (CAPT SIDE REAR) LOOSE LANYARD ON BOTTOM. CORRECTIVE ACTION: SECURED LANYARD. (8109773)

Part: NONE — NONE · airframe 81,374 hrs · 26,228 cycles

SHIP 5638 DOOR OR GIRT BAR PROXIMITY SENSOR COVER DAMAGE/MISSING / LOCATIONS:610. CORRECTIVE ACTION: REATTACHED GUARD COVER AND INSTALLED CORD. (2016535)

Part: NONE — NONE · airframe 81,046 hrs · 26,129 cycles

SHIP 5638 WHILE PERFORMING AMDS CARD 0591-0201 FOUND L4 DOOR AFT DOOR STOP BEARING PLATES MISSING. CORRECTIVE ACTION: ATTACHED MISSING BEARING PLATES PER B757 AMM 52-11. (5363653)

Part: DOOR — OUT OF ADJUST (MAIN) · airframe 80,849 hrs · 26,065 cycles

SHIP 5638 ENTRY DOOR HARD TO OPEN OR CLOSE / LOCATIONS: 3L. CORRECTIVE ACTION: ADJUSTED TRIM. OPS CHECK NORMAL. (1930372)

Part: HANDLE — UNSECURE (L3 DOOR) · airframe 80,655 hrs · 26,010 cycles

SHIP 5638 DOOR 3L DOOR HANDLE POPPED UP ON TAKEOFF. NO INDICATIONS ON FLIGHT DECK PRESSURIZATION NORMAL. CORRECTIVE ACTION: CHECKED DOOR OPERATION PER B757 AMM 52-11-00. NO FAULTS NOTED. (7329490)

Part: SIGN — BROKEN (CABIN) · airframe 80,548 hrs · 25,981 cycles

SHIP 5638 CUSTOMER BROKE EXIT SIGN ON OVERHEAD AT MID-CABIN. CORRECTIVE ACTION: SECURED SIGN. OPS NML. (7329449)

Part: LANYARD — OUT OF POSITION (L3 DOOR SLIDE) · airframe 80,429 hrs · 25,949 cycles

SHIP 5838 3L DOOR WILL NOT ARM. CORRECTIVE ACTION: VERIFIED LANYARD GETTING PINNED AT THE BAR ARMING ASSY. REPOSITION LANYARD TO TIDY. CHECKED NORMAL SAME. (7850486)

Part: LIGHT — INOPERATIVE (SEAT ROW 15) · airframe 80,024 hrs · 25,841 cycles

SHIP 5638 ROW 15 SEAT AISLE AFT LIGHT INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY W/ SAME OPS GOOD. (7368904)

Part: LIGHT — INOPERATIVE (SEAT ROW 42) · airframe 80,024 hrs · 25,841 cycles

SHIP 5638 ROW 42 SEAT AISLE LIGHT INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY W/ SAME OPS GOOD. (7368905)

Part: COVER — DETACHED (EMERGENCY LIGHT) · airframe 79,389 hrs · 25,643 cycles

SHIP 5638 THE COVER OVER THE 2L EMERGENCY EXIT LIGHTS FELL DOWN. CORRECTIVE ACTION: RE-ATTACHED OVERHEAD LIGHT SIGN COVER. VERIFIED SECURED. (7394267)

Part: BUSHING — CORRODED (NR 1 NACELLE) · corrosion level 2 · airframe 77,968 hrs · 25,270 cycles

DURING L CHECK MAINTENANCE FOUND LEVEL 2 CORROSION ON NR 1 PYLON FORWARD UPPER SPAR FITTING LUG BUSHING. REPAIRED PER ERA 588240-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,968 hrs · 25,270 cycles

EMERGENCY EXIT LIGHTS AT L4 DOOR UPPER EXIT SIGN, R4 LOWER DOOR EXIT SIGN, LAV EMERGENCY PATH LIGHT AND L4 EXTERIOR EXIT LIGHT. CORRECTIVE ACTION: REPLACED BATTERY PACK M737. SYSTEM OPERATION IS NORMAL.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,968 hrs · 25,270 cycles

DURING INSPECTION FOUND EMERGENCY AISLE LIGHTS AT ROW 19, 21 AND 23 AND RIGHT AFT OVER-WING AFT DOOR HANDLE LIGHT INOPERATIVE. CORRECTIVE ACTION REPLACED BATTERY AT RIGHT ROW 21 AND RE-LAMPED LIGHTS AT ROW 19 AND RIGHT AFT OVER-WING DOOR HANDLE. SYSTEM OPERATION IS NORMAL.

Part: WATER HEATER — SHORTED (LAVATORY) · airframe 77,709 hrs · 25,191 cycles

SHIP 5638 FA IN AFT GALLEY REPORTED THAT IN THE AFT LEFT LAV (CAPTAINS SIDE ) WHEN USING THE FAUCET AND TOUCHING THE METAL ON THE DOOR HE GOT AN ELECTRICAL SHOCK. HE SAID IT OCCURED 2-3 TIMES. CORRECTIVE ACTION: REMOVED & REPLACED LOC 203 LAV WATER HEATER PER B757 AMM 38-13-51. OPS CHK NML. (6381251)

Part: GIRT BAR — OBSTRUCTED (DOOR SLIDE) · airframe 77,625 hrs · 25,171 cycles

(AIRCRAFT 5638, L/P 6381240) AIR GRILL FOUND UNDER GIRT BAR. AFT LT DOOR WON'T ARM. CORRECTIVE ACTION: REMOVED AIR GRILL, DOOR ARM DISARM OPS GOOD CHKD OK PRE B757 AMM 52-11.

Part: ENGINE — MAKING METAL (NR 2) · airframe 77,463 hrs · 25,127 cycles

SHIP 5638 - ATB - ON CLIMB, FLT CREW EXPERIENCED RIGHT ENGINE VIBRATIONS, DECISION MADE TO RETURN TO SEA. MTC FOUND METAL IN THE TAILPIPE. CORRECTIVE ACTION: R/R #2 ENGINE PER AMDS WORK CARDS. OPS AND LEAK CHECK OKAY.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,456 hrs · 25,125 cycles

EMERGENCY EXIT SIGNS INOPERATIVE. INSTALLED IN CORRECT POSITION IAW AMM 33-51.

Part: BEARING — WORN (R1 DOOR) · airframe 77,110 hrs · 25,034 cycles

(AIRCRAFT 5638, L/P 6375784) UNABLE TO OPEN R1 DOOR FROM OUTSIDE. CORRECTIVE ACTION: REPLACED WORN BASKET AND OUTER BUTTERFLY BEARING PER B757 AMM 52-11-13.

Part: FAN — FAILED (LT RECIRCULATION) · airframe 76,951 hrs · 24,989 cycles

SHIP 5638 -DIV- TO NAS DUE TO THE CREW REPORTED ELECTRICAL SMELL FROM FORWARD CABIN AREA. SHUT OFF GALLEY POWER BUT SMELL RETURNED 30 MINUTES LATER. CORRECTIVE ACTION: INSPECTED E/E, AFT CARGO AREA NTF. REPLACED LT RECIRC FAN AND FILTER PER AMM OP CKS GOOD.

Part: DOOR — OUT OF RIG (R1) · airframe 76,571 hrs · 24,873 cycles

SHIP 5638 UNABLE TO CLOSE 1 R SERVICE DOOR. STUCK AT MID TRAVEL. CORRECTIVE ACTION: REMOVED EXTERIOR HANDLE AND RIGGED DOOR. FOUND LOWER GUIDE ARM WORN, REPLACED GUIDE ARM AND BUSHINGS. REASSEMBLED AND RII C/W. (6643776)

Part: HANDLE — OUT OF SEQUENCE (R1 DOOR) · airframe 75,983 hrs · 24,694 cycles

(AIRCRAFT 5638, L/P 5920778) #1 RT DOOR WILL NOT CLOSE. HANDLES LOCKED UP OUT OF SECQUENCE WORKED AT GETTING HANDLES BACK IN SECQUENCE. OPEN AND CLOSED FROM INSIDE AND OUTSIDE OF DOOR OPS CK GOOD AMM 52-30.

Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 75,493 hrs · 24,558 cycles

(AIRCRAFT 5638, L/P 1185560) 2L ESCAPE SLIDE ARMED COND IND DOES NOT COME OUT WHEN DOOR ARMED. ADJUSTED KNUCKLE KNOCKER WORKS NML.

Part: INDICATOR — MALFUNCTIONED (DOOR SLIDE) · airframe 74,193 hrs · 24,237 cycles

(AIRCRAFT 5638, L/P 1026257) SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CHECKED SLIDE LIGHT AT LOC 601.CKS GOOD.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 74,134 hrs · 24,222 cycles

EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS: 26. CORRECTIVE ACTION: FOUND SIGN INSTALLED UPSIDE DOWN. INSTALLED SIGN CORRECTLY. (1015135)

Part: INDICATOR — OUT OF ADJUST (L2 DOOR) · airframe 73,222 hrs · 24,000 cycles

SHIP 5638 2L DOOR KNUCKLE WILL NOT POP OUT. CORRECTIVE ACTION: ADJUSTED 2L DOOR KNUCKLE BUSTER PER AMM 52-11. OPS CHECK GOOD. (5612630)

Part: HOUSING — UNKNOWN (EMERGENCY LIGHT) · airframe 72,447 hrs · 23,809 cycles

(AIRCRAFT 5638, L/P 5061527) OVERHEAD EMERGENCY LIGHT AT ROW 3 INOP. REPLACED EMERGENCY LIGHT HOUSING AT ROW 3 OVERHEAD REF B757 AMM 33-50.

Part: RESERVOIR — DEFECTIVE (R1 DOOR) · airframe 72,342 hrs · 23,774 cycles

1R DOOR EMERGENCY POWER RESERVOIR NOT PRESSURIZED. REMOVED 1R DOOR EMERGENCY POWER RESERVOIR PER AMM 52-11. REPLACE DOOR EMERGENCY PWR RESERVOIR PER AMM 52-11. REMOVED PINS. A/C OK FOR SVC.

Part: SENSOR — MALFUNCTIONED (L3 DOOR) · airframe 72,335 hrs · 23,770 cycles

3 LEFT DOOR SLIDE LIGHT ON WHILE DOOR IS DISARMED (ICE). REMOVED AND INSTALLED GIRT BAR PROXIMITY SENSOR (AFT) PER AMM 25-66.

Part: SKIN — WORN (LT WING) · airframe 72,266 hrs · 23,747 cycles

(AIRCRAFT 5638, L/P 0782703) INITIAL INSPECTION. WORN WING LWR SKIN FWD AREA STA BBL 70 AT LT WING(AI). SUMMARY OF NRC 00150. WORN WING LWR SKIN FWD AREA BBL 70 AT LT WING WAS REPAIRED PER ETI-57-18-022 REV.2 AND ER/A 572213-14 REV. ORG. REPAIR APPROVAL IS LIMITED TO 31,700 TOTAL CYCLES ONLY. ADDITIONAL ENGINEERING AUTHORIZATION (ER/A REVISION) IS REQUIRED FOR CONTINUED SERVICE BEYOND THIS LIMIT. PER ER/A 572213-14 REV. ORIGINAL SEC. DTE CREATE UNDER LOG PAGE 0779912 IN REFERENCE PER ER/A 572213-14 REV. ORIGINAL SEC. DTE

Part: DOUBLER — CORRODED (FUSELAGE) · airframe 72,266 hrs · 23,747 cycles

INITIAL INSPECTION, CORROSION ON PREVIOUS REPAIR DOUBLER OF FLOORBEAM AT STA 365 BTW STA RBL 2.0 TO RBL 24. REPAIR DOUBLER WAS REPLACED PER SRM 53-00-51 FIGURE 201 TABLE 1 REPAIR 5 AND 51-40-02 PAR 7.

Part: FLOOR PANEL — BROKEN (CABIN) · airframe 72,266 hrs · 23,747 cycles

BROKEN FLOOR PANELS 230-72 AND 230-66 AT PAX CABIN. FLOOR PANELS 230-72 AND 230-66 WERE MANUFACTURING, REPLACED AND IDENTIFIED PER AMM 51-01-01-201.

Part: FLOOR PANEL — DELAMINATED · airframe 72,266 hrs · 23,747 cycles

DURING REMOVAL FERRULES WERE FOUND DELAMINATED THE FLOOR PANELS 250-26, 250-28 AND 250-29. FLOOR PANEL 250-26, 250-28 AND 250-29 WERE MANUFACTURING, REPLACED AND IDENTIFIED PER AMM 53-01-01-201.

Part: PANEL — DAMAGED (CARGO BAY) · airframe 72,266 hrs · 23,747 cycles

PERFORM PERMANENT REPAIR ON AFT CARGO COMPARTMENT LEFT HAND SIDE PANEL. SIDE PANEL WAS REPAIRED PER SRM 53-00-53 REPAIR 3 FIG 201.

Part: FLOOR PANEL — DELAMINATED · airframe 72,266 hrs · 23,747 cycles

DURING REPLACE OF FERRULES WAS FOUND DELAMINATED FLOOR PANEL 220-2. FLOOR PANEL 220-2 WAS MANUFACTURING, REPLACED AND IDENTIFIED PER AMM 53-01-01-201.

Part: FLAP SYSTEM — MALFUNCTIONED (TE FLAPS) · airframe 71,242 hrs · 23,477 cycles

DURING APPROACH, WHEN THE FLAPS WERE SELECTED TO 30, REMAINED STUCK AT BETWEEN 20 & 25 DEGREES WITH A TRAILING EDGE FLAP DISAGREE LIGHT ILLUMINATED. A GO AROUND WAS ACCOMPLISHED AND QRH ACCOMPLISHED AND A EMERGENCY DECLARED. A NORMAL LANDING ACCOMPLISHED, ON ENGINE SHUTDOWN FLAP LEVER REMAIN IN 30 DEGREES AND FLAPS EXTENDED TO 30 AFTER ENGINE STOPPED. THE T/E FLAP DISAGREE LIGHT WAS NO LONGER ILLUMINATED. COMPLIED WITH NO GO ODI PREVENTION PRIOR TO FLIGHT T/S. ACCOMPLISHED BIT ON FSEU 1, 2, AND 3. INTERMITTENT MESSAGE 305, FLAP DISAGREE . CLEARED AND RESET. RAN FLAPS L/E & T/E FOR 5 CYCLES, NO FAULTS NOTED, NO MESSAGE ON FSEU AFTER FLAP TEST.

Part: PROCESSOR — FAILED (FUEL QTY) · airframe 69,587 hrs · 23,058 cycles

AIR TURN BACK DUE TO A LOSS OF LEFT WING FUEL TANK QUANTITY AND ASSOCIATED LOSS OF FUEL TOTALIZER. TROUBLESHOT IAW FIM 28-41, FAULT CODE LM IFQC CIRCUIT BOARD FAILED. R & R FUEL QUANTITY PROCESSER IAW AMM 28-41. CHECKED GOOD.

Part: LANYARD — LOOSE (R1 DOOR) · airframe 69,255 hrs · 22,973 cycles

ENTRY DOOR SEAL NOISY, LOCATIONS 602. CHECK R1 DOOR SEAL AND FRAME FOR SECURITY AND CONDITION. FOUND OUT DOOR SLIDE LANYARD LOOSE. RE-SECURED LANYARD. PRESSURIZATION AIRCRAFT PER AMM 21-31. NO LOUD NOISE NOTICED INSIDE.

Part: HOUSING — CRACKED (R3 DOOR SLIDE) · airframe 67,757 hrs · 22,565 cycles

R3 DOOR SLIDE HOUSING IS CRACKED. REPAIRED THE SLIDE HOUSING

Part: LANYARD — UNSECURE (R3 DOOR) · airframe 66,945 hrs · 22,350 cycles

R3 DOOR WOULD NOT ARM. SECURED THE SLIDE LANYARD.

Part: SLIDE — DAMAGED · airframe 66,686 hrs · 22,267 cycles

SLIDE O-RING IS HANGING OUT. REPOSITION SLIDE CORD TO ORIGINAL POSITION OP CHECK GOOD OK FOR SVC.

Part: LEVER — DIRTY (ARMING) · airframe 66,335 hrs · 22,171 cycles

ON ARRIVAL, L2 DOOR SLIDE ARMING LEVER WILL NOT DISENGAGE. OPS CHECK IAW AMM 52-11. REMOVED DEBRIES. OK FOR SERVICE.

Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 67,600 hrs · 22,521 cycles

DURING WALK AROUND FOUND DENT ON LEFT LE HORIZONTAL STAB APPROX. 6.7 INCH LONG X 4 INCH'S HIGH X .35 INCH'S DEEP. PERFORMED TIME LIMITED REPAIR PER ERA 554526-14 REV ORIG.

Part: PLATE — CORRODED (L4 DOOR) · corrosion level 2 · airframe 72,266 hrs · 23,747 cycles

(AIRCRAFT 5638, L/P 2815744) LOWER HINGE CAM PLATES RUSTED FOR L-4 DOOR. (REF; NR 40). PERMANENT REPAIR WAS PERFORMED PER ER/A 476391-14MA REV B SECTION 111.

Part: COVER — OUT OF ADJUST (LT OVERWING) · airframe 64,689 hrs · 21,760 cycles

LEFT OVERWING ARM / DISARM COVER DOOR LATCHES INOPERTIVE. ADJUSTED THE LT OVERWING DOOR ARM / DISARM COVER. DOOR IS IN SECURED POSITION.

Part: PANEL — CORRODED · airframe 62,599 hrs · 21,160 cycles

RT SIDE PANEL AT E7 RACK INSTALLATION HAS EXFOLIATING CORROSION. CORROSION BEYOND ALLOWABLE LIMITS OF SRM 53-00-53, MATERIAL LOSS 80 PERCENT. REPLACED SIDE PANEL 146N15391U10 IAW ER/A 373211-14MA AND DWG 146N5413, SHT 1 AND DWG 146N5390.

Part: STRINGER — DAMAGED (BS 1240-1260) · airframe 62,595 hrs · 21,158 cycles

STRINGER 16 RT, BS 1240-1260 DAMAGED BEYOND LIMITS. REPAIRED STR 16 RT AT BS 1240-1260 IAW SRM 53-00-03, REPAIR 1. CATEGORY A REPAIR REF SRM 53-00-03, REPAIR 1, PAGE 202, NOTE K.

Part: WEB — CORRODED (BS 1440-1460) · airframe 62,595 hrs · 21,158 cycles

AFT CARGO BAY BS 1440-1460, RBL 23, OTBD SIDE CORNER CORRODED ON WEB. FOUND WEB AT BS 1440 TO 1460, RBL 23 IN AFT PIT TO BE CORRODED 80 PERCENT THRU MATERIAL, THIS IS OUT OF LIMITS IAW SRM 53-60-15, PAGE 107. R & R WEB IAW DWG 146N8522, REV E. SRM 51-40-02, PAGE 1-7, SRM 51-40-05, PAGE 2 AND SRM 51-20-01, PAGE 11 & 12.

Part: LUG — DAMAGED (NR 2 PYLON) · airframe 59,125 hrs · 20,121 cycles

DURING INSPECTION AFTER BUSHING REMOVAL ON NR 2 PYLON UPPER SPAR FITTING LUG BORES, MECHANICAL DAMAGE WAS FOUND INSIDE THE OTBD LUG. REPAIRED IAW ER/A 529473-14, PRI REV 0, ER/A 529473-14, PRI REV 1.

Part: FITTING — DAMAGED (NR 1 NACELLE) · airframe 59,125 hrs · 20,121 cycles

DAMAGE FOUND INSIDE THE OTBD LUG ON NR 1 PYLON UPPER SPAR FITTING LUG BORES. REPAIRED CARRIED OUT IAW SRM.

Part: LUG — DAMAGED (NR 2 PYLON) · airframe 59,125 hrs · 20,121 cycles

AFTER BUSHING REMOVAL ON NR 2 PYLON UPPER SPAR FITTING LUG BORES, MECHANICAL DAMAGE WAS FOUND INSIDE THE INBD LUG. FITTING LUG BORES REPAIRED IAW PRI 529473-14 AD, REV 0.

Part: WEB — CHAFED (LT WING) · airframe 59,125 hrs · 20,121 cycles

LT WING L/E BULLNOSE LOWER WEB FOUND CHAFING. FABRICATED IAW DWG 114N1806, REV B. DAMAGED WEB REMOVED AND NEW WEB INSTALLED IAW SRM.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 55,775 hrs · 19,098 cycles

EMERGENCY EXIT SIGN AT SEAT 21ABC AND SEAT 22DEF INOPERATIVE. FOUND FUSE OPEN OF POWER SUPPLY "M10567". REPLACED FUSE AND OPS CHECKED OK IAW AMM 33-51. ACFT OK FOR SVC.

Part: SHEAR WEB — CORRODED (BS 1180) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN, BS 1180, LT MOST OTBD FLOOR TO CREASE BEAM SHEAR WEB FOUND CORROSION IAW CORROSION TASK NR CP53-241-01I LT. SUMMARY:CORROSION AT CABIN BS1180 LT MOST OTBD FLOOR TO CREASE BEAM SHEAR WEB REMOVED IAW SRM 51-10-01. ORIGINAL THK=0.050", MATERIAL REMOVED=0.020", MATERIAL REMAINING=0.030" FOUND OUT OF LIMIT IAW SRM 53-60-13, FIG 101. REPAIR CARRIED OUT IAW PRI ER/A510828-14 REV 0 DATED 24 JAN 13 08:59 AWAITING FINAL ER/A. PRI ER/A REV0 FOUND IAW FINAL ER/A 510828-14, REV.

Part: INTERCOSTAL — CRACKED (BS 1420-1440) · airframe 54,087 hrs · 18,569 cycles

AFT CARGO BAY AT BS 1420-1440 BL0 FLOOR SUPPORT UPPER INTERCOSTAL AT AFT SIDE FOUND CRACKED APPROX 1" AS MARKED. CRACKED UPPER INTERCOSTAL AT STA 1420-1440, BL0. REMOVED AND NEW FABRICATED UPPER INTERCOSTAL INSTALLED IAW SRM 51-40-02. NEW UPPER INTERCOSTAL FABRICATED IAW PRI ER/A 510832 REV 0, DATED 25 JAN 13 AWAITING FINAL ER/A. PRI ER/A 510832-14, PRI ER/A 510832-14, REV 0 FOUND IAW FINAL ER/A510832-14.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

BS 345, RBL 40 FLOORBEAM UPPER TEE FOUND CORROSION IAW CORROSION TASK NR CP53-222-01I RT. CORROSION REMOVED IAW SRM 51-10-01. ORIGINAL THK=0.125", MATERIAL REMOVED=0.035", MATERIAL REMAINING=0.090" FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101. REPAIR CARRIED OUT IAW PRI ER/A 510638-14.

Part: STRAP — BROKEN (BS 365-377) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

BS 365-377, LBL 24, FLOOR SUPPORT LOWER ANGLE ATTACHED STRAP FOUND BROKEN. BROKEN ATTACHED STRAP REPAIRED IAW PRI ER/A 510635-14.

Part: FLOORBEAM — CORRODED (BS 345-365) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN BS 345-365, RBL 63 FLOORBEAM FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-01. ORIGINAL THK=0.050", MATERIAL REMOVED=0.020", MATERIAL REMAIN=0.030" FOUND OUT OF LIMIT IAW SRM 53-00-51, FIG 101. DAMAGE FLOORBEAM R & R IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 405) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

BS 405, RBL 24-45 FLOORBEAM FOUND CORRODED. FLOORBEAM R & R AS IAW SRM 51-40-2.

Part: SEAT TRACK — CORRODED (BS 405) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN BS 405, RBL 24, SEAT TRACK CORRODED. DAMAGE CABIN SEAT TRACK R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 700-720) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

BS 700-720, FLOOR SUPPORT CORRODED. DAMAGE FLOOR SUPPORT R & R IAW SRM 51-40-20.

Part: FLOORBEAM — CORRODED (BS 405) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN BS 405, RBL 53-63 FLOORBEAM FOUND CORROSION IAW CORROSION TASK NR CP53-222-01I RT. DAMAGE FLOORBEAM REMOVED IAW SRM 51-40-02. NEW FLOORBEAM FABRICATED IAW DWG 141N5188, REV AA AND INSTALLED IAW SRM 51-40-02.

Part: FLOORBEAM — CORRODED (BS 405) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN BS 405, RBL 13-24 FLOORBEAM FOUND CORROSION IAW CORROSION TASK NR CP53-222-01I RT. CABIN BS405 RBL13-24 FLOOR BOX BEAM R & R IAW SRM 51-40-02.

Part: FLOOR SUPPORT — CORRODED (BS 760-780) · corrosion level 2 · airframe 54,087 hrs · 18,569 cycles

CABIN BS 760-780 LT MOST OTBD FLOOR SUPPORT CORROSION. DAMAGE FLOOR SUPPORT LT MOST OTBD R & R IAW SRM 51-40-02.

Part: SKIN — DENTED (BS 1540) · airframe 54,087 hrs · 18,569 cycles

DENT FOUND LOWER FUSELAGE BS 1540 ABOVE STRINGER S25R AREA. REPAIRED IAW SRM 53-00-01, REPAIR 2, FIG 201.

Part: SOCKET — DIRTY (EMERGENCY LIGHT) · airframe 53,837 hrs · 18,491 cycles

L4 DOOR EXTERIOR EMERGENCY LIGHT WON'T ILLUMINATE. CHECKED CONDITION OF SOCKET AND WIRE, FOUND NORMAL. CLEANED BULB SOCKET CONTACT POINT, OPS CHECKED OK.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 53,700 hrs · 18,447 cycles

EMERGENCY LIGHTS AT SEAT 17ABC AND 18DEF AND EXIT SIGN ABOVE SEAT 17ABC INOPERATIVE. REPLACED BATTERIES FOR POWER SUPPLY AND CHECKED OK IAW AMM 33-51.

Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 53,551 hrs · 18,399 cycles

SEAT 17AB OTBD EMERGENCY LIGHT INOPERATIVE. LAMPED, NO HELP. REPAIR LIGHT SOCKET ON 17AB EMERGENCY LIGHTS CHECKED OK IAW AMM 33-51.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 53,061 hrs · 18,246 cycles

DURING LINE CHECK MAINTENANCE, FOUND EMERGENCY LIGHTS FROM 27-31 INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK PER AMM 33-50. OPERATION OF LIGHTS NOW CHECK GOOD.

Part: LIGHT — MISSING (SEAT 1 AB) · airframe 52,443 hrs · 18,044 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHT AT SEAT 1 AB MISSING. MAINTENANCE INSTALLED LIGHT AT SEAT 1 AB. OPERATION OF SEAT LIGHT NOW CHECKED GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,717 hrs · 16,702 cycles

DURING A LINE CHECK, MAINTENANCE FOUND THE SEAT 1B (AFT) EMERGENCY PATH LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD. (2010-00843)

Part: GATE — CORRODED (R2 DOOR) · corrosion level 2 · airframe 47,323 hrs · 16,631 cycles

DURING L-CHECK FOUND CORROSION ON DOOR R2 LOWER GATE EDGE AND SEAL RETAINER EDGE. REPAIRED PER SRM 51-10-02, MM 52-09-01-401-926A-A.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 45,856 hrs · 16,389 cycles

BUSINESS CLASS EMERGENCY LIGHT AT LEFT OVERHEAD BIN AREA INOPERATIVE. REPLACED POWER SUPPLY ASSEMBLY.

Part: BATTERY — DISCHARGED (CABIN) · airframe 44,853 hrs · 16,019 cycles

DOOR 1R EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY. LIGHT CHECKED OK.

Part: BRAKE — MALFUNCTIONED (RT MLG) · airframe 41,668 hrs · 15,145 cycles

AFTER LANDING AND TRANSFER TO NORMAL BRAKES, THE FLIGHT CREW REPORTED THAT THE RT BRAKE PEDAL WENT ALL OF THE WAY TO THE FLOOR WITH NO BRAKING ACTION ON THE RT MAIN LANDING GEAR BRAKES. LT MAIN LANDING GEAR BRAKES OPERATED NORMALLY. ONCE IN THE GATE, MAINTENANCE FOUND THE BRAKES ON THE RT MAIN LANDING GEAR TO OPERATE NORMALLY. (S)

Part: WARNING LIGHT — FALSE ACTIVATION (LT ENG BLEED) · airframe 38,816 hrs · 14,734 cycles

REJECTED TAKEOFF AT DUS LESS THAN 120 KNOTS FOR FAULTY LEFT ENGINE BLEED AIR LIGHT. A/C EXITED RUNWAY, RECYCLED SWITCH AND REMOVED ITS LIGHT, TAXIED BACK FOR TAKEOFF. TAKEOFF WAS NORMAL, NO FURTHER INCIDENTS. CLIMB-OUT WAS NORMAL. MAINTENANCE DID A COMPLETE PNEUMATIC OPS CHECK ON BOTH ENGINES. ALL CHECKS GOOD AT THIS TIME, OPERATIONAL CHECKED GOOD, AND AIRCRAFT WAS RETURNED TO SERVICE.

Part: INVERTER — BURNED (STANDBY) · airframe 36,743 hrs · 14,432 cycles

EICAS STATUS MESSAGE -STBY INVERTER-, ALONG WITH SLIGHT SMELL OF BURNING ELECTRICS THRU OUT CABIN AND COCKPIT. MAINTENANCE: PERFORMED TSM PROCEDURE 24-37-00, FOUND OLD STANDBY INVERTER BURNT; REPLACED STATIC (STANDBY) INVERTER. AIRCRAFT OK FOR SERVICES.

Part: WIRE — BROKEN (EMERGENCY EXIT) · airframe 35,885 hrs · 14,103 cycles

EXIT INDICATOR EMERGENCY LIGHT INOPERATIVE. TROUBLE SHOT PER WDM 33-51-21. REPAIRED BROKEN WIRES AND REPLACED POWER UNIT M732. OPS CHECKS GOOD. OK FOR SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 33,505 hrs · 13,184 cycles

DURING LINE CHECK, FOUND POWER SUPPLY AT STA 1240 RT INOP. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE.

Part: SMOKE — DETECTED (LT MLG WW) · airframe 17,882 hrs · 7,224 cycles

AFTER LANDING, THE TOWER REPORTED A TYPE OF SMOKE COMING FROM THE LEFT MAIN GEAR AREA. ROLLED EMERGENCY EQUIPMENT WITH NO ABNORMALITIES NOTED. FLIGHT ATTENDANT REPORTED ACRID SMELL IN CABIN UPON TAXI IN. MAINTENANCE INSPECTED BRAKES. NO TROUBLE FOUND.

Part: OIL FILTER — CONTAMINATED (NR 2 ENGINE)

AFTER PUSHBACK, NR 2 ENGINE OIL FILTER MESSAGE DISPLAYED AFTER ENGINE START. AIRCRAFT RETURNED TO GATE. GROUND MAINTENANCE INSPECTED AND REPLACED THE OIL FILTER AND HOUSING. NO CONTAMINATES WERE FOUND. ENGINE RUN AND LEAK CHECK OK. AIRCRAFT RETURNED TO SERVICE.