N686DA

Part: CHARGER — NO TEST (ZONE 200) · airframe 85,698 hrs · 37,286 cycles

SHIP 686 DURING SVC FOUND SEAT 38 THRUE 42 EMERGENCY LIGHT INOP. CORRECTIVE ACTION: R/R CHAGER AND BATTERY PER B757 AMM 33-51 OPS CHECK NML. (7055182)

Part: LANYARD — DETACHED (ZONE 800) · airframe 85,169 hrs · 37,001 cycles

SHIP 686 L2 DOOR STRAP HANGING DOWN. CORRECTIVE ACTION: RE-ATTACHED VELCRO LANYARD, OPS CK NMRL. NON RII LIST REF TOPP ( 40-30-05). (7134444)

Part: LANYARD — OUT OF POSITION (ZONE 800) · airframe 85,132 hrs · 36,975 cycles

SHIP 686 R1 DOOR WON'T ARM. CORRECTIVE ACTION: FOUND SLIDE LANYARD BLOCKING GIRT BAR. STOWED SAME REF B757 AMM 52-12. OK FOR SVC. OPS CK NML. (7134416)

Part: GIRT BAR — FOD (ZONE 800) · airframe 85,078 hrs · 36,943 cycles

SHIP 686 1R DOOR WILL NOT ARM. CORRECTIVE ACTION: FOUND DEBRIS UNDER THE GIRT BAR. REMOVED DEBRIS DOOR ARM OPS CHK GOOD. REF B757 AMM 25-66. (6827774)

Part: SWITCH — LOOSE (R2 DOOR) · airframe 84,877 hrs · 36,861 cycles

SHIP 686 ON TAXI INTO GATE, INTERMITTENT. R CTR ENT DOOR EICAS MESSAGE. CORRECTIVE ACTION: FOUND R2 DOOR UNLOCK DETECTOR SENSOR SWITCH LOOSE. TIGHTEN SWITCH PER B757 SSM 52-71-01. OPS NORMAL. (6595366)

Part: ACTUATOR — LEAKING (APU IGV) · airframe 84,765 hrs · 36,818 cycles

SHIP 686 DURING TAXI ON RAMP STRONG CHEMICAL ODOR IN COCKPIT + FWD GALLEY AFTER SWITCHING FRROM ENG BLEED TO APU BLEED. CORRECTIVE ACTION: FOUND APU IGV ACTUATOR LEAKING APU COMPARTMENT WAS SATURATED. R/ R APU IGV ACTUATOR PER B757 AMM 49-52. NO LEAKS NOTED. VERIFIED AND CLEANED APU COMPARTMENT AND APU BLEED DUCT PER B757 FIM 21-00-01/301. (6595320)

Part: INDICATOR — INOPERATIVE (DOOR SLIDE) · airframe 83,998 hrs · 36,367 cycles

SHIP 686 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:602. CORRECTIVE ACTION: CLEANED AND OP CKD DOOR ARMING SYSTEM IAW B757AMM 25-66. OP CKS GOOD. (0553331)

Part: CAP — FAILED (ZONE 200) · airframe 83,681 hrs · 36,214 cycles

SHIP 686 RED EMER LIGHT SEAT ENDCAP INOP. SEAT 26F TRIM END PIECE. CORRECTIVE ACTION: R/R EPL BUMPER & LIGHT AT 26F IN REF WITH B757 CMMM 25-22-57. OPS NORMAL. (5507930)

Part: TRANSDUCER — FAULTED (NR 5 WHEEL SPEED) · airframe 83,543 hrs · 36,144 cycles

SHIP 0686 -MISC/DE- DUE TO NORMAL AND ALTERNATE ANTISKID MESSAGES. CORRECTIVE ACTION: REPLACED NUMBER 5 WHEEL SPEED TRANSDUCER.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 83,453 hrs · 36,094 cycles

SHIP 686 EMERG LIGHTS OUT ON SEAT ROWS 23-26. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK AT M10567 CKS OK, REF B757 AMM 33-51. (6148400)

Part: PANEL — DAMAGED (LT WING) · airframe 83,023 hrs · 35,865 cycles

AIRCRAFT 0686, DURING THE ONGOING MAINTENANCE CHECK OF THE DATUM AIRCRAFT, LH WING, DRY BAY PANEL, P/N: 112N8003-1, WAS FOUND WITH A TOOL MARK AFFECTING FLAME SPRAY COATING AND 1 EA. PLY AROUND THE DRY BAY DOOR LOCATED BETWEEN WSTA 231.5  WSTA 258.5. CORRECTIVE ACTION: REMOVE ALL SEALER AROUND FASTENERS AND DRY BAY BARRIER PANEL IN THE AREA PREVIOUSLY REPAIRED PER B757-200 SRM 51-00-10. PERFORM REPAIR PER B757-200 SRM 57-20-09, REPAIR 3, STEPS 4A THROUGH F IN ITS ENTIRETY. (LP 0312816)

Part: SLIDE — DAMAGED (RT OVERWING) · airframe 83,023 hrs · 35,865 cycles

AIRCRAFT 0686, DURING DISARM OFF-WING ESCAPE SYSTEM COMPARMENT OF THE OVERWING SLIDE WAS FOUND DISBONDED AND FRAYED JUMPER ON RH OVERWING SLIDE IN REF AMDS 5200-8595 STEP 1. CORRECTIVE ACTION: REPLACED RIGHT OVERWIND SLIDE AND JUMPER. (LP 0305579)

Part: LEAF SPRING — FAILED (GIRT BAR) · airframe 83,023 hrs · 35,865 cycles

AIRCRAFT 0686, DOOR GIRT BAR LEAF SPRINGS (FWD) DO NOT GET THE MINIMUM ENGAGEMENT DIMENSION AT 2R DOOR. CORRECTIVE ACTION: SPRING (FWD) AT 2R DOOR. WAS REPLACED BY NEW PER B757-200 SRM 51-40-02-0G PAR. 4 AND GIRT BAR LEAF SPRING (FWD) ENGAGEMENT DIMENSION WAS MEASURED UNDER AMDS 2560-01492-0101 STEP 2. D. AND GET THE MINIMUM ENGAGEMENT DIMENSION. (LP0304092)

Part: SKIN — DEBONDED (NR 7 SLAT) · airframe 83,023 hrs · 35,865 cycles

SHIP 686 AD - 02 DISBONDED AREAS WERE FOUND ON UPPER SKIN AT TRAILING EDGE WEDGE OF LE SLAT 7: 1) 2.75IN LENGTH AND 0.90IN WIDTH AT OSS 306, 2) 1.50IN LENGTH AND 0.625IN WIDTH AT OSS 438 APPROX IN REFERENCE TO JOB 079-0001 CARD 5740-01145-07G. CORRCTIVE ACTION: SUMMARY OF NRC 00026: UPPER SKIN AT TRAILING EDGE WEDGE OF LE SLAT 7 AT OSS 306 AND OSS 438 APPROX WAS REPAIRED PER B757/200 S.R.M. 51-70-10-2R REPAIR GENERAL AND S.R.M. 57-43-02-2R PROCEDURE 1. (0300264)

Part: GIRT BAR — WRONG PART (R1 DOOR SLIDE) · airframe 83,023 hrs · 35,865 cycles

SHIP 686 WRONG INSTALLED BAR ON SLIDE ARMING MECHANISM AT SERVICE DOOR 1R. CORRECTIVE ACTION: SUMMARY: BAR ON SLIDE ARMING MECHANISM AT SERVICE DOOR 1R WAS INSTALLED CORRECTLY PER B757-200 AMM 52-11. (0299298)

Part: NONE — NONE (ALTERATION) · airframe 83,023 hrs · 35,865 cycles

AIRCRAFT 0686, THIS ALTERATION REMOVES THE LOWER FORWARD ATG4 ANTENNA. THIS ANTENNA IS NO LONGER USED AND HAS ICA INSPECTIONS THAT CANNOT BE COMPLETE. CORRECTIVE ACTION: REMOVE ANTENNA, BLANKING PLATE AND COMPLETED HFEC INSPCTIONS. FABRICATED AND INSTALLED SKIN CUTOUT FILLER AND DOUBLERS AND RESTORE EXTERNAL FINISHES PER ER/A 616681-14. (LP 0252311)

Part: TRANSCEIVER — INOPERATIVE (WX RADAR) · airframe 82,640 hrs · 35,652 cycles

SHIP 0686 -DIV- WEATHER RADAR INOP. CORRECTIVE ACTION: REPLACED WEATHER RADAR TRANSCEIVER. C/W NO GO ODI.

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 81,326 hrs · 34,932 cycles

SHIP 0686 OPENED DOOR AND FOUND DOOR GIRT BAR DIS-CONNECTED. REMOVED BUSTLE FOR INSP OF SLIDE. INSTALLED SLIDE PIN. CORRECTIVE ACTION: RE-ATTACHED GIRT BAR, REMOVED AND STOWED 1L DOOR SLIDE PIN AND RE-ARMED ASSIST BOTTLE REF B757 AMM 25-66. C/W RII OF REMOVING PIN + RE-ARMING ASSIST BOTTLE REF B757 AMM 25-66. (4712276)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,976 hrs · 34,746 cycles

SHIP 0686 PUNCTURE ON CAPTAIN SIDE OF RUDDER APPROXIMATELY 2 FEET FROM TRAILING EDGE AND 1 FOOT FROM BOTTOM OF RUDDER. CORRECTIVE ACTION: ASSOCIATED ER/A 14-609672 ADDED FOR AC 0686 COMPLIED WITH PRI 609672-14, REV.0, REV. 1, REV. 2, REV. 3, ALL STEPS. FINAL ER/A 609672-14, REV. ORIG. MATCHES WITH THE PRI 609672-14 REV, O,1,2,3. (4185747).

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,610 hrs · 34,554 cycles

SHIP 686 EXIT ROW LIGHT COVER DETACHED ROW 25. CORRECTIVE ACTION: REINSTALLED LIGHT COVER. (4818024)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,293 hrs · 34,391 cycles

SHIP 686 FOUND EMERGENCY PATH LIGHTING INOP @ 26D. CASE WAS BROKEN. CORRECTIVE ACTION: REMOVED AND REPLACED EPL CASE IN REF TO B757 AMM 33-51. OPS CHECK GOOD. (2684043)

Part: LIGHT — INOPERATIVE · airframe 78,609 hrs · 33,528 cycles

SHIP 686 EXTERIOR EMERGENCY LIGHTING SYSTEM /BATTERY POWERED/ . R2 EXTERIOR EMER LIGHT WILL NOT TURN OFF. CORRECTIVE ACTION: PERFORMED OPS CHK PER AMM 33-51. 2R EXT LIGHT OPS TEST NORMAL. (2353366)

Part: NONE — NONE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DURING INSPECTION R1 DOOR GIRT BART WAS FOUND OUT OF LIMITS IN REF. AMDS. CORRECTIVE ACTION: SUMMARY OF NRC 00041. R1 DOOR GIRT BART WAS REPLACED BY SERVICIABLE PER B757-200 AMM AMM 25-66-10 AND ADJUST GIRT BAR MECHANISM WAS PERFORMER UNDER AMDS. (2297325)

Part: NONE — NONE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 REMOVE AND APPLY THE SEALANT OF THE RIGHT WING NDT INSPECT LOWER STRINGERS S-6 AND S-8 AT WS 711/711.5. CORRECTIVE ACTION: SUMMARY OF NRC 00037 SEALANT OF THE RIGHT WING NDT INSPECT LOWER STRINGERS S-6 AND S-8 AT WS 711/711.5 WAS REMOVED AND APPLIED PER B757-200 AMM 51-31 AND SHIMS WERE REPLACED PER ER/A N 599861-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2294915)

Part: FRAME — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 AD, AA. IN REF AMDS 5311-01227-01A: EXISTING REPAIR WAS FOUND DENTED IN THE INSPECTION AREA STA 1460 S-26L. CORRECTIVE ACTION: SUMMARY OF NRC 00156: FRAME ON STA 1460 S-25L TO S-27L WAS REPAIRED PER. ER/A 599756-14AD REV. ORIGINAL SECTION I: PERMANENT REPAIR. (2292677)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON FLOOR STRINGERS RBL 10.45, RBL 7.55 , RBL 2.90 AND LBL 10.45, LBL 7.55, LBL 2.90 BTW STA 730 AND STA 770 AT FWD CARGO COMPARTMENT (IN REF NRC: 00281). CORRECTIVE ACTION: SUMMARY OF NRC 00679: FLOOR STRINGERS RBL 10.45, RBL 7.55 , RBL 2.90 AND LBL 10.45, LBL 7.55, LBL 2.90 BTW STA 730 AND STA 770 AT FWD CARGO COMPARTMENT WERE REPAIRED PER B757-200 SRM. (2293845)

Part: PLATE — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON LH SIDE PLATE BTW STA 1300-1310 AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 00693: LH SIDE PLATE BTW STA 1300-1310 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2292461)

Part: STRINGER — INTERFERENCE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 ER/A 599861-14AD; WING / OUTER, RH / LOWER STRINGERS S-6 & S-8 SPLICES, WS 699 - 711.5 / RADIUS BLOCK INTERFERENCE. CORRECTIVE ACTION: REF ERA 599861-14AD. (2292273)

Part: PANEL — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON RH SIDE PANEL BTW STA 1257-1310, AT AFT CARGO COMPARTMENT (CCT). CORRECTIVE ACTION: SUMMARY OF NRC 00696: RH SIDE PANEL BTW STA 1257-1310, AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2290586)

Part: FRAME — NONE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DTE, ERA 599756-14 REV -, MONITOR INSPECTION LOG REPAIR AT FRAME STA 1460 BETWEEN S-25L & S-27L REQUIRES ADDITIONAL ENGINEERING APPROVAL, AN EXISTING REPAIR WAS FOUND AFFECTING THE STA 1460 BOTTOM FRAME, BETWEEN S-25L & S-27L. REF ERA 599756-14 REV ORG. (2291258)

Part: PANEL — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION OUT OF LIMITS ON RH SIDE PANEL BTW BSTA 1440-1530 AND BSTA 1574-1640 AT AFT CARGO COMPARTMENT IN REF NRC 00176. CORRECTIVE ACTION: SUMMARY OF NRC 00687: SIDE PANEL BTW STA 1440-1530 WAS REPLACED AND BSTA 1574-1640 WAS REPAIRED PER. B757 -200 SRM. (2290389)

Part: PANEL — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON LH SIDE PANEL BTW STA 1570-1580 AT AFT CARGO COMPARTMENT. (IN REF NRC: 00174). CORRECTIVE ACTION: SUMMARY OF NRC 00669: LH SIDE PANEL BTW STA 1570-1580 AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2288401)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON ON FLOOR STG RBL 16.10 ,2.90 AND LBL 2.90, LBL 16.10 ,LBL 10.45, BTW STA 620 AND STA 680 AT FWD CARGO COMPARTMENT IN REF NRC 278 (C1). CORRECTIVE ACTION: SUMMARY OF NRC 00705: SECTION FLOOR STG RBL 16.10 ,2.90 AND LBL 2.90, LBL 16.10 ,LBL 10.45, BTW STA 620 AND STA 680 AT FWD CARGO COMPARTMENT WERE REPLACED PER B757-200 SRM. (2288449)

Part: STRINGER — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON SUPPORT STA 1380-1440 STRG 27R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00289: SUPPORT STA 1380-1440 STRG 27R AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200, SRM. (2287372)

Part: SKIN — CORRODED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 A.A. /AD CORROSION ON LH WING DRAG FITTING HOLES: #2 - 5 HRS, #3 - 5 HRS, #6 - 6 HRS AND #8 - 5 HRS BTW SKIN AND FITTING ( REFERENCE CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00317: LH WING DRAG FITTING HOLES: #2, #3, #6 AND #8 SKIN AND FITTING WERE REPAIRED PER PRI 588312-14 REV 1 AND ER/A 588312-14AD REV. C SECTION V. (2287895)

Part: SKIN — CORRODED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 A.A. /AD CORROSION ON LH WING DRAG FITTING HOLES: #12 - 5 & 6 HRS, #13 - 6 HRS, #14 - 4 HRS, #15 - 9 HRS AND #16 - 6 HRS BTW SKIN AND FITTING (REFERENCE CARD). CORRECTIVE ACTION: SUMMARY OF NRC 00318: LH WING DRAG FITTING HOLES: #12, #13, #14, #15 AND #16 SKIN AND FITTING WERE REPAIRED PER PRI 588312-14 REV 1 AND ER/A 588312-14AD REV. C SECTION V. (2287863)

Part: PLATE — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON SIDE PLATE RH BTW STA 645 TO 660 FWD CARGO COMPARTMENT(CCD) IN REF NRC S/N:00255. CORRECTIVE ACTION: SUMMARY OF NRC 00677: CORROSION ON SIDE PLATE RH BTW STA 645 TO 660 FWD CARGO COMPARTMENT(CCD) WAS REPAIRED PER B757-200 SRM. (2288096)

Part: INTERCOSTAL — CRACKED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 : CRACK ON INTERCOSTAL STA 1638 STRG 13LH AT PAXCABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00389: INTERCOSTAL STA 1638 STRG 13LH AT PAXCABIN WAS REPAIRED PER B757-200 SRM. (2285115)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON LH OUTBD SEAT TRACK BTW STA 1480 TO 1485 AT PASSENGER CABIN (IN REF NRC: 00140). CORRECTIVE ACTION: SUMMARY OF NRC 648: CORROSION ON LH OUTBD SEAT TRACK BTW STA 1480 TO 1485 AT PASSENGER CABIN WAS REPAIRED PER B757-200 SRM. (2283456)

Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 80,382 hrs · 34,431 cycles

SHIP 686 REPAIR TO LH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588312-14 REV C. CORRECTIVE ACTION: C/W GVI OF LH ENG DIAG BRACE AND BRACE FITTINGS PER ERA 588312-14 REV C AND W/C 5720-01100-03A NO FURTHER DAMAGE NOTED OK TO CONT ON MON. (2283590)

Part: FRAME — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DENT ON LH FRAME STA 1240 BTW STR-26L-27L ALSO ON FRAME STA 1340 STR-26L AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00177: FRAME 1240, S-26L & S-27L WAS REPAIRED PER ER/A 599975-14 REV:ORIGINAL; SECTION I:PERMANENT REPAIR AND FRAME 1340 S-26L WAS REPAIRED PER B757-200 SRM. (2282681)

Part: FRAME — NONE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DTE, ER/A599975-14, FUSELAGE / MAIN FRAME / FRAME / STA 1240, S- 26L & S-27L / DENT TIME LIMITED. CORRECTIVE ACTION: REF ERA 599975-14. (2281812)

Part: SEAT TRACK — NONE · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 SUMMARY OF NRC 00372 CORROSION SEAT TRACK LBL 24 BTW STA 377 TO STA 395 AT W1. CORRECTIVE ACTION: SUMMARY OF NRC 00372 SEAT TRACK LBL 24 BTW STA 377 TO STA 395 AT W1 WAS REPLACED PER B757-200 SRM. (2281302)

Part: FRAME — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DENT ON FRAME BTW STA 660 AND S-23L FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00263 FRAME STA 660 BTW S-23LH FWD CARGO COMPARTMENT WAS REPAIRED PER. B757-200 SRM. (2279834)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON SEAT TRACK RBL 24 BTW STA 375 TO 377 ALSO STA 435 AT W1. CORRECTIVE ACTION: SUMMARY OF NRC 00366: ON SEAT TRACK RBL 24 BTW STA 375 TO 377 ALSO STA 435 AT W1 WAS REPLACE PER B757-200 SRM. (2279808)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON SEAT TRACK RBL 45 BTW STA 375 TO 377 AT W1. CORRECTIVE ACTION: SUMMARY OF NRC 00365: CORRODED SEAT TRACK RBL 45 BTW STA 365.25 TO 440 (AT W1) WAS REPLACED PER B757-200 SRM. (2278462)

Part: FRAME — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DENT ON FRAME STA 640 BTW S-24R AND S-23R FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00258 FRAME STA 640 BTW S-24R AND S-23R FWD CARGO COMPARTMENT WAS REPAIRED PER. B757-200 SRM. (2279035)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON FLOOR SUPPORTS BTW STA 1640- 1680 LB 0 AT PAXCABIN FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00430: FLOOR SUPPORTS BTW STA 1640-1680 LB 0 AT PAXCABIN FLOOR STRUCTURE WERE REPLACED PER B757-200 SRM. (2278494)

Part: BARRIER — NOT REPORTED (ZONE 500) · airframe 87,992 hrs · 38,391 cycles

REFERENCE ER/A 546346-14 LT WING FUEL TANK DRY BAY BARRIER. REPAIR OF TIME LIMITED WAS RE-ACCOMPLISHMENT ON LT WING FUEL TANK DRY BAY BARRIER WS 231.5-258.5 PER ER/A NO. 546346-14 REV. E, SECTION VI. (2279135)

Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON LH OUTBD SEAT TRACK BTW STA 1190TO 1210 AT PASSENGER CABIN (IN REF NRC: 00137). CORRECTIVE ACTION: SUMMARY OF NRC 00650: LH OUTBD SEAT TRACK BTW STA 1190TO 1210 AT PASSENGER CABIN WAS REPAIRED PER B757-200 SRM. (2279489)

Part: SKIN — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 DENT ON EXTERIOR FUSELAGE SKIN STA 440 TO 460 AND BTW S28L AND S29L ( FUS ). CORRECTIVE ACTION:SUMMARY OF NRC 00044: DENT ON EXTERIOR FUSELAGE SKIN STA 440 TO 460 AND BTW S28L AND S27L WAS REPAIRED PER PRI 600093-14 REV. 0 AND ERA 600093-14 REV. ORIG SECTION I: PERMANENT REPAIR. (2276709)

Part: WEB — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON WEB STA 1180-1182, S-17 RH FLOOR STRUCTURE AREA, IN REF NRC 00387. CORRECTIVE ACTION: SUMMARY OF NRC 00673: WEB STA 1180-1182, S-17 RH FLOOR STRUCTURE AREA WAS REPAIRED PER B757-200 SRM. (2276453)

Part: WEB — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON WEB STA 1380-1385 IN REF NRC 00387. CORRECTIVE ACTION: SUMMARY OF NRC 00674 : CORROSION ON WEB STA 1380-1385 WAS REPAIRED PER B757-200 SRM. (2270011)

Part: SLAT — NONE · airframe 78,343 hrs · 33,388 cycles

SHIP 686 A.A. - A.D. DISBOND ON OSS 772, UPPER SURFACE, LE SLAT 1 TRAILING EDGE WEDGE, LH WING. SUMMARY OF NRC 00053 : UPPER SURFACE, LE SLAT 1 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER SRM 51-70-10-2R PROCEDURE REPAIR GENERAL AND B757-200 SRM 57-43-02-2R. (2268650)

Part: SKIN — DEBONDED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 A.A. - A.D. 02 DESBONDS ON OSS 488 UPPER SURFACE, LE SLAT 8 TRAILING EDGE WEDGE, RH WING. CORRECTIVE ACTION: SUMMARY OF NRC:00057 DESBONDS ON OSS 488 UPPER SURFACE, LE SLAT 8 TRAILING EDGE WEDGE, RH WING WERE REPAIRED PER B757-200 SRM 51 -70-10-2R AND B757-200 SRM 57-43-02-2R PROCEDURE 1 REPAIR 1 FIGURE 201 NOTE D. (2268313)

Part: WEDGE — DEBONDED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 A.A. - A.D. DEBOND (2.700IN LENGTH X 1.200IN WIDTH) ON OSS 305, LOWER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00055: AREA ON LOWER SURFACE (OSS 305) OF SLAT 4 TRAILING EDGE WEDGE WAS REPAIRED PER B757-200 SRM. (2265444)

Part: STRAP — CRACKED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CRACK ON STABILIZATION STRAP IN STA 1600 AND 24 LBL AT AFT CARGO. CORRECTIVE ACTION: SUMMARY OF NRC 209: REPAIR PARTS WERE INSTALLED PER B757-200 S.R.M. 53-00-51-2R PROCEDURE 13 REPAIR 13. (2263458)

Part: FLOOR SUPPORT — CORRODED · corrosion level 2 · airframe 78,343 hrs · 33,388 cycles

SHIP 686 CORROSION ON SUPPORTS (4E/A) STA 1639 LBL 45 AND RBL 23 AND RBL 45 ALSO STA 1605 LBL 23 AT PAXCABIN FLOOR SUPPORT. CORRECTIVE ACTION: SUMMARY: SUPPORTS (4E/A) STA 1639 LBL 45 AND RBL 23 AND RBL 45 ALSO STA 1605 LBL 23 AT PAX CABIN FLOOR SUPPORT WERE REPLACED PER B757-200 SRM. (2262004)

Part: SHUTOFF VALVE — INOPERATIVE · airframe 78,102 hrs · 33,253 cycles

SHIP 686 -PRES/DIV- TO DEN DUE TO LOSS OF LT PACK AND RT PACK, UNABLE TO MAINTAIN CABIN PRESSURE WITH REMAINING PNEUMATIC SYSTEM. APU INOP. OXY MASKS DEPLOYED. INCIDENT OCCURRED DURING ICING CONDITIONS WITH PNEUMATIC ISOLATION VALVE OPEN, LT/RT ENG ANTI ICE SELECTED ON AND RT PACK IN AUTO. CORRECTIVE ACTION: T/S PERFORMED HP PNEU HEALTH CHECK R/R #2 ENGINE HPSOV, FAN AIR VALVE TEMP SENSOR. FAN AIR VALVE. (LOG 8718552) R/R REVERSE FLOW CONTROLLER, 14TH STAGE PILOT REGULATOR. OPS AND LEAK CHECK GOOD.

Part: UNKNOWN — UNKNOWN · airframe 78,072 hrs · 33,234 cycles

SHIP 686 MID-CABIN CEILING EXIT SIGN IS UPSIDE DOWN. CORRECTIVE ACTION: REINSTALLED EXIT LIGHT COVER IN THE CORRECT UPRIGHT POSTION. (8718535)

Part: NONE — NONE · airframe 77,959 hrs · 33,178 cycles

'SUPPLEMENTAL INFORMATION' SHIP 686 DOOR HANDLE COVER PLATE AT 1L KEEPS FALLING OFF. CORRECTIVE ACTION: REMOVED AND REPLACED COVER AS NEEDED PER B757 AMM 25-00. (2141817)

Part: NONE — NONE · airframe 77,959 hrs · 33,178 cycles

SHIP 686 L3 DOOR EXTERIOR EMERGENCY LIGHT INOP. CORRECTIVE ACTION: R/R L3 EXTERIOR EMERGENCY LIGHT ASSY AS PER B757 AMM 33-51. EMERGENCY LIGHT TEST CHECKS NORMAL. (8538566)

Part: NONE — NONE · airframe 77,886 hrs · 33,141 cycles

SHIP 686 ON S/C, L4 DOOR HANDLE TRIM COVER PLATE MISSING. CORRECTIVE ACTION: LOCATED AND SECURED TRIM PLATE TO 4L DOOR. (8538528)

Part: NONE — NONE · airframe 77,757 hrs · 33,071 cycles

SHIP 686 L-1 DOOR UNLOCK INDICATION DURING TAXI. CORRECTIVE ACTION: T/S PER FIM 32-09. SW S10094 OUT OF PROX. ADJUSTED SW S10094 PER B-757 AMM 52-71-00-825-001. OPS NORMAL. (8396264)

Part: NONE — NONE · airframe 77,757 hrs · 33,071 cycles

SHIP 686 L FWD ENT DOOR ANNUNCIATOR ON TAXI OUT. CORRECTIVE ACTION: ADJUSTED SENSOR IAW B757 AMM 52-71 PERFORMED SYTRM TEST OF DOOR WARNING SYSTEM IAW B757 AMM 52-71 CHECKS GOOD. (8396270)

Part: NONE — NONE · airframe 77,750 hrs · 33,069 cycles

SHIP 686 LEFT FWD ENTRY DOOR LT WONT EXTINGUISH. CORRECTIVE ACTION: CLEANED DOOR SENSOR. CHECKS GOOD PER B757 AMM 52-71. (8396254)

Part: NONE — NONE · airframe 77,335 hrs · 32,885 cycles

'SUPPLEMENTAL INFORMATION' SHIP 686 3R DOOR SLIDE ARMED LIGHT INOP. CORRECTIVE ACTION: REPLACED MISSING DOOR PROXIMITY ACTUATOR SWITCH, R3 DOOR AFT SLIDE PER B757 AMM 25-66. OPS TEST NORMAL. (8198069)

Part: NONE — NONE · airframe 77,219 hrs · 32,827 cycles

SHIP 686 4L DOOR WOULD NOT ARM AT DEPARTURE NO SLIDE LIGHT ILLUMINATED. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR FITTING. OPS CKD OK PER B757 AMM 52-11. (8198036)

Part: NONE — NONE · airframe 77,107 hrs · 32,777 cycles

SHIP 686 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS: 3L SLIDE LIGHT NOT ILLUMINATING WHEN DOOR IS ARMED. CORRECTIVE ACTION: RELAMPED 3L DOOR SLIDE ARMED LIGHT. OPS TEST GOOD. (1999790)

Part: NONE — NONE · airframe 77,057 hrs · 32,755 cycles

SHIP 686 UNABLE TO SEAL/ARM 4L DOOR DUE TO CABLE BINDING AT BASE. CORRECTIVE ACTION: ARMED DOOR 4L SEVERAL TIMES OK FOR SERVICE PER B757 AMM 25-66. (8074666)

Part: NONE — NONE · airframe 76,895 hrs · 32,680 cycles

SHIP 686 E-PATH LIGHT ASSY DAMAGED AT SEAT 44D. CORRECTIVE ACTION: REPLACED LIGHT ASSY HOUSING AT SEAT 44D LIGHT OPS CHK GOOD. IAW B757 AMM 33-51. (7528793)

Part: STABILIZER — DENTED · airframe 78,343 hrs · 33,388 cycles

SHIP 686 ON WALKAROUND, FOUND DENT 5.25 FEET OUTBD OF FUSELAGE AND LOCATED ON RT HORIZONTAL STAB. CORRECTIVE ACTION: DENT WAS REPAIRED WITH NRC 00081 AND B757-200 SRM 51-70-10-2R PROCEDURE REPAIRS GENERAL AND B757 -200 SRM 55-10-01-1A. (7528756)

Part: NONE — NONE · airframe 76,790 hrs · 32,636 cycles

SHIP 686 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS: 44D. CORRECTIVE ACTION: SECURED EMER LIGHT ON SEAT 44D. (1950751)

Part: SIGN — DETACHED (SEAT 44D) · airframe 76,727 hrs · 32,604 cycles

SHIP 686 EXIT SIGN DETACHED SEAT 44D. CORRECTIVE ACTION: REATTACHED EXIT SIGN SEAT 44D PER B757 AMM 25-60. (7528728)

Part: SLIDE — OUT OF POSITION (L2 DOOR) · airframe 76,701 hrs · 32,590 cycles

SHIP 686 FOUND EVACUATION SLIDE AT DOOR 2- LEFT STARTING TO MIGRATE OUT THE LOWER LEFT OF THE PACK ASSY. CORRECTIVE ACTION: REMOVED EVAC SLIDE AT DR2-L PER WORKCARD 2L, INSTALLED PER AMDS 2566-9001-2L JOB COMPLETE. RII COMPLETED. (7528705)

Part: LIGHT — BROKEN (SEAT ROW 38) · airframe 75,692 hrs · 32,222 cycles

SHIP 686 EMER AILE LIGHT OF ROW 38 BROKEN OFF SEAT. CORRECTIVE ACTION: RESECURE EMER. LIGHT BRACKET AT SEAT ROW 38DEF. (7644066)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 75,692 hrs · 32,222 cycles

SHIP 686 EMER LIGHTS FROM ROW 27 TO 32 INOP. REMOVED AND REPLACED BATTERY PACK IN EMERGENCY LIGHT POWER SUPPLY M10568 AND TEST OK PER B757 AMM 33-51.

Part: NONE — NONE · airframe 77,560 hrs · 32,975 cycles

SHIP 686 REPAIR TO RH WING UPPER SKIN COMMON TO DRAG FITTING ATTACHMENT REQUIRES SUPPLEMENTAL INSPECTIONS PER ERA 588313-14 REV A. CORRECTIVE ACTION: REF 588313-14 REV A. (1764480)

Part: PLATE — CORRODED (AFT CARGO BAY) · corrosion level 2 · airframe 74,250 hrs · 31,702 cycles

CORROSION LEVEL: 2 DURING INSEPCTION FOUND CORROSION ON RT SIDE PLATE BETWEEN STA 1280 TO 1380 AT AFT CARGO COMPARTMENT. RIGHT SIDE PLATE BETWEEN STA 1280 TO 1380 AT CARGO COMPARTMENT WAS REPLACED.

Part: DRAG BRACE — LOOSE (RT ENGINE) · airframe 74,250 hrs · 31,702 cycles

DURING INSPECTION FOUND CORROSION LEVEL 1 AT RT ENGINE DRAG FITTING FASTENERS NR 3 & 4. REPAIRED PER ERA 588313-14.

Part: FRAME — CRACKED (FUSELAGE) · airframe 74,250 hrs · 31,702 cycles

WHILE ACCOMPLISHING WORK CARD 5311-01207-01A, MTC REPORTED A CRACK INDICATION ON THE FRAME AT STA 1681. THE CRACK INDICATION IS REPORTED TO BE AT THE INBOARD HOLE COMMON TO THE CLIP AT WL 208 (JUST BELOW THE FLOOR LINE). REPAIRED PER ERA 581126-14.

Part: SKIN — DAMAGED (LT WING) · corrosion level 2 · airframe 74,250 hrs · 31,702 cycles

WHILE PERFORMING INSPECTION CORROSION AND SCRATCHES WERE FOUND AFFECTING HOLES 1-18 COMMON TO THE LT WING UPPER SKIN AND FORWARD DRAG FITTINGS. REPAIRED PER ERA 588312-14AD.

Part: DRAG BRACE — LOOSE (LT ENGINE) · airframe 74,250 hrs · 31,702 cycles

WHILE PERFORMING INSPECTION FOUND LOOSE FASTENERS NR 1 & 3 OF LEFT ENGINE DRAG FITTING. REPAIRED PER ERA 588312-14AD.

Part: FITTING — CORRODED (RT ENGINE) · airframe 74,250 hrs · 31,702 cycles

DURING INSPECTION FOUND LEVEL 1 CORROSION ON HOLES 1, 2 & 5 TO 10. DAMAGED HOLES AT RIGHT ENGINE DRAG FITTING CLAMP-UP AND DIAGONAL BRACE WERE REPAIRED, PER ERA 58813-14.

Part: PLATE — CORRODED (BS 1530) · corrosion level 2 · airframe 74,250 hrs · 31,702 cycles

CORROSION LEVEL: 2 - DURING INSPECTION FOUND CORROSION ON LEFT SIDE PLATE (JOINT SPICE AREA) STA 1530 AT AFT CARGO COMPARTMENT AND REPLACED PER SRM.

Part: LIFE VEST — MISSING (CABIN) · airframe 74,250 hrs · 31,702 cycles

DURING INITIAL INSPECTION FOUND MISSING FLIGHT ATTENDANT LIFE VEST (3 EA). CORRECTIVE ACTION: INSTALLED LIFE VEST.

Part: NONE — NONE · airframe 77,929 hrs · 33,163 cycles

SHIP 686 DISBOND OF 6.900" X 0.650" ON OSS 327 ON REPAIR DOUBLER UPPER SURFACE TRAILING EDGE WEDGE SLAT # 7 RH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00133:UPPER SURFACE TRAILING EDGE WEDGE SLAT # 7 RH WING WAS REPAIRED PER B757-200 SRM 57-43-02-2R-1 REPAIR 1. (1628806)

Part: D-RING — OUT OF POSITION (R1 DOOR) · airframe 74,050 hrs · 31,620 cycles

(AIRCRAFT 686, L/P 6421868) LOUD SQUEAL 1R DOOR AT LEVEL OFF FL390. CORRECTIVE ACTION: FOUND SLIDE D RING HANGING SECURED BACK ON DOOR PRESSURIZED A/C PER B757 AMM 21-31 GND CKS OK.

Part: LIGHT — INOPERATIVE (L1 SLIDE) · airframe 73,173 hrs · 31,283 cycles

(AIRCRAFT 686, L/P 5702324) AFTER T/O 1L SLIDE LIGHT WENT OUT. CORRECTIVE ACTION: R/R'D L1 SLIDE LED LIGHT CAP ASSY PER B757AMM 33-51. OPS NORMAL.

Part: FRAME — CRACKED (FUSELAGE) · airframe 72,496 hrs · 31,013 cycles

(AIRCRAFT 686, L/P 1258891) BHEC INSP OF LT BS 1681 FRAME INBD HOLE BELOW FLOOR SHOWS INDICATION. COMPLIED WITH ERA 581126-14AD REV ORG SECTION 1. PERMANENT REPAIR MONITOR ON LOG 1258721.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,143 hrs · 30,854 cycles

(AIRCRAFT 686, L/P 6261562) ROW 43 SEAT MOUNTED EMER LIGHT INOP. REMOVED & REPLACED SEAT MOUNTED LIGHT ASSY. OPS CHECK GOOD.

Part: SHROUD — DAMAGED (CABIN) · airframe 71,937 hrs · 30,784 cycles

SHIP 686 AISLE SIDE SEAT SHROUD DAMAGED AT SEAT 18D. EEPL (WHITE) MISSING. CORRECTIVE ACTION: REPLACED 18D SHROUD BUMPER ASSY AND EEPL LIGHT ASSY PER CMM 25-21. (5444996)

Part: PROXIMITY SWITCH — DIRTY (L2 DOOR) · airframe 71,398 hrs · 30,541 cycles

SHIP 686 2L DOOR SLIDE LIGHT STILL ILLUMINATED WHEN DOOR IS DISARMED HAVE TO ARM AND RE-ARM DOOR FOR LIGHT TO EXTINGUISH. CORRECTIVE ACTION: CLEANED GIRT BAR & SLIDE PROX SWITCHES CYCLED DOOR & SLIDE ENGAGEMENT & DISENGAGEMENT NUMEROUS TIMES. ALL OP'S CK'S GOOD. REF AMM 52-71. SLIDE LIGHT RESECURED AT DOOR 2L. (5711072)

Part: HOUSING — DAMAGED (EMERGENCY LIGHT) · airframe 69,848 hrs · 29,892 cycles

(AIRCRAFT 686, L/P 5199018) SEAT ROW 45 EMERGENCY PATH LIGHT HOUSING ASSY DAMAGED/HANGING. REPLACED ROW 45 EMERGENCY LIGHT HOUSING ASSY.

Part: RELIEF VALVE — POPPED (CABIN PRESSURE) · airframe 69,294 hrs · 29,607 cycles

-ATB- RETURNED TO MSP DUE TO PRESSURIZATION ISSUES. CORRECTIVE ACTION: MTC FOUND LOWER OVER PRESSURE RELIEF VALVE POPPED WITH INSULATION STICKING OUT. RESET PRESSURE RELIEF VALVES AND REPOSITIONED / SECURED INSULATION BLANKET. PERFORMED BITE OF BOTH CABIN PRESSURE CONTROLLERS, NO FAULTS NOTED. REPLACED LOWER POSITIVE RELIEF VALVE. PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CHECK - PASSED. PERFORMED STEP 2 OF NEXT MAINTENANCE LAYOVER SINGLE PACK CONFIDENCE CHECK, CHECK PASSED. CABIN PRESSURE SELECTOR CHANGED ON LOG 3896248.

Part: SKIN — DENTED (LT HORIZ STAB) · airframe 68,311 hrs · 29,256 cycles

LT HORIZONTAL STAB LOWER SKIN HAS SEVERAL DENTS BET STA 104.248 AND STA 176.249. REPAIRED IAW DRAWING 185N4003 AND B757-200SRM 51-70-10 REPAIR 2 PG 201.

Part: SKIN — CHAFED (NR 8 SLAT) · airframe 68,311 hrs · 29,256 cycles

RIGHT WING NR 8 LE SLAT LOWER SURFACE ABOVE INBD MAIN TRACK CHAFED. REPAIRED IAW SRM 57-43-02, REPAIR 1, FIG 201, SHT 4, AND SRM 51-70-10.

Part: D-RING — OUT OF POSITION (L1 DOOR) · airframe 67,393 hrs · 28,920 cycles

PRIOR TO PUSHBACK DOOR 1L WOULD NOT ARM. REPOSITION "D" RING CKS NML PER AMM 25-61.

Part: LAMP — INOPERATIVE (FIRE LIGHT) · airframe 66,577 hrs · 28,633 cycles

RIGHT ENGINE FUEL CONTROL SWITCH, FIRE LIGHT CAME OFF. LIGHT NO LONGER ILLUMINATES DURING TEST. REPLACED THE LAMP & INSTALLED THE LENS. LAMP OPERATES NORMALLY DURING TEST.

Part: ENGINE — FIRE (LEFT) · airframe 66,308 hrs · 28,536 cycles

LEFT ENGINE FIRE AFTER TAKEOFF, RETURNED TO DEPARTURE. REPLACED THE LEFT ENGINE IAW AMDS 7100-9902E.

Part: D-RING — UNSECURE (DOOR SLIDE) · airframe 65,921 hrs · 28,423 cycles

AFT RIGHT DOOR D-RING HANGING OUT OF SLIDE PACK. SECURED THE D-RING. OK FOR SERVICE.

Part: LIGHT — MISSING (ROW 21D) · airframe 65,758 hrs · 28,373 cycles

DURING SERVICE CHECK, FOUND EMERGENCY LIGHT 21D MISSING, FOUND LIGHT IN OVERHEAD BIN. REPLACED EMERGENCY LIGHT FIXTURE AT ROW 21D IAW CMM 25-21-52. OPS CHECKED GOOD.

Part: VALVE — MALFUNCTIONED (LT A/C PACK) · airframe 62,995 hrs · 27,403 cycles

FLIGHT 696, WHILE DESCENDING THROUGH 330, DECLARED EMERGENCY AND DESCENDED TO FL 140 DUE TO LEFT PACK FAILURE AND RIGHT PACK BEING ON MEL. TROUBLESHOT IAW FIM 21-51, TASK 803. NO FAULTS. UPON FURTHER INVESTIGATION, FOUND LEFT PACK TEMP EICAS MESSAGE. AUTO EVENT SHOWED PACK TEMP OUT TEMP -48. INSPECTED LEFT PACK. FOUND NO HOT AIR COMING FROM LOW LIMIT VALVE. REMOVED AND REPLACED LOW LIMIT VALVE B757 AMM 21-51. CHECKED GOOD.

Part: FITTING — GOUGED (LT OVERWING) · airframe 61,729 hrs · 26,977 cycles

LT AFT OVERWING EMERGENCY AXIT DOOR, DOOR-MOUNTED LOWER AFT FITTING IS GOUGED. INSPECTION, MEASURED, REWORKED AND FOUND TO BE OUT OF LIMITS. REMOVED PIVOT FITTING AND INSTALLED NEW. TORQUED REF SRM. ADJUSTED, TEST C/W.

Part: SLIDE — DAMAGED (L1 DOOR) · airframe 61,729 hrs · 26,977 cycles

L1 DOOR SLIDE FWD AND PIN LACINGS BROKEN. R & R L-1 DOOR SLIDE FWD AND AFT PIN LACINGS IAW EVACUATION SYSTEMS CMM 25-61-26.

Part: GATE — DAMAGED (R4 DOOR) · airframe 61,722 hrs · 26,974 cycles

R4 DOOR LOWER GATE AFT ROD END DAMAGED. R & R AFT ROD END AT R-4 LOWER GATE IAW CMM 52-11 ADJUSTMENT, ACCOMPLISHED ON CARD.

Part: GATE — CORRODED (L2 DOOR) · airframe 61,722 hrs · 26,974 cycles

CORROSION L-2 DOOR LOWER GATE UPPER AND LOWER EDGES HAVE PITTING CORROSION MULTIPLE SPOTS, JC-27. REMOVED CORROSION AT L-2 DOOR LWR GATE UPPER AND LOWER EDGES IAW SRM 52-10-02, FI1, CHECKED ALLOWABLE DAMAGE FOUND TO BE OUT OF LIMITS. R & R L-2 DOOR LOWER GATE IAW AMM 52-11-38-004-001, 52-11-38-404-009, ADJUSTMENT, ACCOMPLISHED ON CARD NR 52-11-9001-2L.

Part: FLOORBEAM — GOUGED (BS 1500) · airframe 61,722 hrs · 26,974 cycles

WHILE WC 2337-01151-09 AT BS 1500, RBL 28 FOUND GOUGE ON LWR FLOORBEAM. ACCOMPLISHED PERMANENT REPAIR ON BS 1500, RBL 28 LWR FLOORBEAM REF ER/A 544741-14, REV ORIGINAL REF THIS LOGPAGE & NRC 100-264 FOR REPAIR ACCOMPLISHMENT REF LOGPAGE 249110 FOR DTE ACCOMPLISHMENT AND TRACKING OF REPAIR.

Part: STRIP — DAMAGED (NR 5 SLAT) · airframe 61,722 hrs · 26,974 cycles

NR 5 SLAT LOWER CENTER T/E STRIP, INBD IS CHIPPED, BROKEN. ACCOMPLISHED REPAIR ON NR 5 SLAT CENTER T/E STRIP INBD END IAW SRM AND ER/A 510361-14MA, REV ORIGINAL.

Part: STRAP — DENTED (BS 1460-1480) · airframe 61,722 hrs · 26,974 cycles

AFT CARGO BAY CEILING STABILIZER STRAP RT SIDE ABOVE AVIONICS RACK IS DENTED BETWEEN BS 1460 - 1480. REMOVED DAMAGE SECTION OF STRAP. FABRICATED A NEW SECTION AND REPAIR SPLICE DRILLED AND INSTALLED IAW ERA 384483-14MA.

Part: FITTING — GOUGED (EMERGENCY EXIT) · airframe 61,722 hrs · 26,974 cycles

RIGHT FWD EMERGENCY EXIT DOOR, DOOR -MOUNTED LOWER FORWARD FITTING IS GOUGED. FOUND UNSERVICEABLE, R & R PIVOT FITTING ON RT FWD EMERGENCY EXIT DOOR REF SRM, ADJ AND TEST ACCOMPLISHED ON JOB CARD.

Part: SKIN — DENTED (BS 640) · airframe 61,722 hrs · 26,974 cycles

DENT ON FUSELAGE SKIN FWD AND AFT SIDE OF FRAME AT BS 640, BELOW SKIN LAP STR 14L. FOUND DENT TO BE OUT OF LIMITS REF SRM. COMPLIED WITH ER/A 544731-14 REV ORIGINAL. REF NRC.

Part: SKIN — DAMAGED (BS 740-760) · airframe 61,722 hrs · 26,974 cycles

LOWER FUSELAGE SKIN BS 740-760, STR 18-20L DAMAGED. FOUND OUT OF LIMITS IAW SRM. TRIMMED OUT DAMAGE. REPAIRED IAW SRM.

Part: SKIN — DENTED (BS 600-640) · airframe 61,722 hrs · 26,974 cycles

FUSELAGE SKIN BS 600-640, STR 15-19L, DENTED AND SCRATCHED. REPAIRED THE SKIN IAW ER/A 544731-14, REV ORIGINAL.

Part: ANGLE — CORRODED (CARGO DOOR) · airframe 61,722 hrs · 26,974 cycles

AFT CARGO DOOR 4TH LOWER WEB ANGLE FROM FWD HAS CORROSION ON AFT LOWER SIDE AND UNDER LEVELING COMPOUND. UPON FURTHER EVALUATION FOUND 100 PERCENT MATERIAL LOSS ON THE AFT CARGO DOOR 4TH LOWER WEB ANGLE AND T-ANGLE IAW SRM 51-10-02. R & R WEB ANGLE, PN: 146N6603-183, BN: 0002962244 AND T-ANGLE, PN: 146N6603-182 IAW SRM 51-40-02, PAR 4B PG 2 AND PAR 7D, PG 6-7 AND DWG 146N6603, SHEET 7.

Part: ANGLE — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

AFT CARGO DOOR 3RD LOWER WEB ANGLE FROM FWD HAS CORROSION ON LOWER FWD & AFT SIDES AND UNDER LEVELING COMPOUND. FOUND TO BE 100 PERCENT EXFOLIATED. FABRICATED REPAIR AND INSTALLED IAW SRM.

Part: WEB — CORRODED (CARGO DOOR) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CARGO DOOR NR 3 LOWER POSTION, CORROSION WAS FOUND ON THE WEB. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM. R & R WEB IAW SRM.

Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN FLOORBEAM, BS 365, UPPER FLANGE HAS CORROSION AROUND CLIP NUT HOLES BETWEEN BL 0 AND RBL 63. TRIMMED OUT AND ACCOMPLISHED PERMANENT REPAIR IAW SRM.

Part: FLOORBEAM — CORRODED (BS 377) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE AT BS 377, BETWEEN LBL 56 AND 61. TRIMMED OUT DAMAGE AND ACCOMPLISHED PERMANENT CAT "A". REPAIR IAW SRM.

Part: SKIN — DAMAGED (BS 1450) · airframe 61,722 hrs · 26,974 cycles

LOWER FUSELAGE RT SIDE BS 1450, AFT CARGO DOOR CONTROL PANEL CUTOUT SKIN, FRAME, AND LATCH CONTACT PAD ARE GOUGED/BENT. CUT OUT SKIN AND BLENDED. ACCOMPLISHED PERMANENT REPAIR IAW SRM. BENT LATCH CONTACT PAD WAS REPLACED IAW SRM.

Part: DOOR SILL — CORRODED (BS 339-377) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN CREASE BEAM AT L1 DOOR SILL IS CORRODED AROUND NUT PLATES BETWEEN BS 339 AND 377.7. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED MAIN CABIN CREASE BEAM AT L1 DOOR SILL, CHANNEL REPLACEMENT IAW DWG & SRM'S.

Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN FLOORBEAM AT BS 345, RBL 23, UPPER TEE HAS CORROSION AROUND A CLIPNUT HOLE. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. ACCOMPLISHED PERMANENT REPAIR ON MAIN CABIN FLOORBEAM AT BS 345, RBL 23 IAW ER/A 481634-14MA REV A, SECTION 1.

Part: SKIN — CHAFED (NR 4 SLAT) · airframe 61,722 hrs · 26,974 cycles

NR 4 SLAT UPPER T/E WEDGE LOWER SKIN IS CHAFED SEVERAL AREAS. PROCURED NR4 SLAT, REMOVAL AND INSTALLATION AND OPS /ADJUSTMENT CHECK TO BE ACCOMPLISHED ON JOB CARD. REQUIRED REPLACEMENT DUE TO THE REPAIR AREAS EXEEDING THE VACUUM BAG LIMITS, 200 SQ INCHES IAW SRM.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, BS 1510, LBL 3. REMOVED DAMAGE AREA FAB, LOCATED AND INSTALLED REPAIR. NDT FOR CRACK, NO CRACK FOUND. TREATED PRIMED AND ALUMINIZED IAW ERA. 332525-14MA, REV D.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, STA 1510, RBL 7. REMOVED DAMAGE AREA, FABRICATED REPAIR, LOCATED AND INSTALLED. NDT CUTOUT FOR CRACKS. NO CRACK FOUND. TREATED, PRIMED AND ALUMINIZED IAW ERA 332525-14MA, REV D.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, BS 1510, RBL 12. REMOVED DAMAGE AREA FABRICATED, LOCATED AND INSTALLED REPAIR NDT FOR CRACK NO CRACK NOTED TREATED PRIMED AND ALUMINIZED IAW ERA 332525-14MA, REV D.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, BS 1510, LBL 7. REMOVED DAMAGE AREA FAB REPAIR LOCATED AND INSTALLED NDT CUTOUT FOR CRACK. NO CRACK FOUND. TREATED, PRIMED AND ALUMINIZED IAW ERA 332525-14MA, REV D.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, BS 1510, RBL3. REMOVED DAMAGE AREA FABRICATED. REPAIR LOCATED AND INSTALLED. NDT CUT-OUT FOR CRACKS, NO CRACK FOUND TREATED PRIMED AND ALUMINIZED IAW ERA 332525-14MA, REV D.

Part: FLOORBEAM — CORRODED (BS 1510) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOORBEAM, BS 1510, LBL 3. REMOVED DAMAGE AREA FABRICATED, LOCATED AND INSTALLED REPAIR NDT FOR CRACK. NO CRACK FOUND. TREATED, PRIMED AND ALUMINIZED IAW ERA 332525-14MA, REV D.

Part: FLOOR SUPPORT — CORRODED (BS 1500-1520) · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOOR SUPPORT RBL 3, BS 1500-1520. R & R THE FLOOR SUPPORT. FABBRICATED A NEW FLOOR SUPPORT IAW SRM 51-40-02, 53-60-04, 51-10-02.

Part: SKIN — CHAFED (LT WING TE FLAP) · airframe 61,722 hrs · 26,974 cycles

OTBD MAIN FLAP BETW 19" TO 59" FROM INBD END 12" FROM AFT END UPPER SKIN HAS CHAFING. ACCOMPLISHED PERMANENT REPAIR ON LT OTBD MAIN FLAP BETW 19" TO 59" FROM INBD END, 12" FROM AFT END UPPER SKIN IAW SRM.

Part: FLOOR SUPPORT — CORRODED (BS 1616) · airframe 61,722 hrs · 26,974 cycles

CORROSION, AFT CARGO COMPARTMENT, FLOOR SUPPORT BS 1616, LBL 3, BILGE AREA. R & R FLOOR SUPPORT, FABRICATED THE NEW FLOOR SUPPORT, TREATED, PRIMED AND TOP-COAT IAW SRM 51-40-02, 53-60-04, AND 51-10-02.

Part: CREASE BEAM — CORRODED (BS 690-740) · corrosion level 2 · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN L2 DOOR SILL CREASE BEAM HAS CORROSION AROUND NUT PLATES BETWEEN BS 690 AND 740. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. REPLACED MAIN CABIN L2 DOOR SILL CREASE BEAM FROM BS 665-740, LBL 65 IAW SRM.

Part: STRAP — CRACKED (BS 365) · airframe 61,722 hrs · 26,974 cycles

LEFT NOSE TUNNEL BS 365.25, LBL 24 MAIN FLOORBEAM LOWER SUPPORT STRAP IS CRACKED THRU PREVIOUS REPAIR FASTENERS. CUT OUT DAMAGE, FABRICATED AND INSTALLED REPAIR, REF ERA 384483-14MA, REV D.

Part: SNUBBER — DAMAGED (R1 DOOR) · airframe 61,722 hrs · 26,974 cycles

R1 DOOR BODY TORQUE TUBE SNUBBER HAS INDICATOR POPPED. SNUBBER INSTALLED ON CARD 5210-01271-08.

Part: FLOORBEAM — CORRODED (BS 720) · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN FLOORBEAM AT BS 720 HAS CORROSION AROUND CLIP NUTHOLE AT LBL 2.5. REMOVED CORROSION IAW SRM 53-00-07 AD 1. FOUND BLEND OUT OF LIMITS IAW 53-00-07 AD1. ACCOMPLISHED PERMANENT REPAIR IAW SRM 53-00-51, REPAIR II, FIG 201.

Part: SEAT TRACK — CORRODED (BS 790-880) · airframe 61,722 hrs · 26,974 cycles

MAIN CABIN AT BS 790-880 LBL-45 FOUND SEAT TRACK WITH CORROSION AND DEEP GOUGE ON LOWER LEG OF TRACK. REMOVED AND INSTALLED NEW SECTION OF SEAT TRACK AT BS 790-BS 880 LBL 45 IAW SRM.

Part: JACKSCREW — CORRODED (LT WING TE FLAP) · airframe 61,722 hrs · 26,974 cycles

LEFT WING NR 3 FLAP JACK SCREW BALL NUT IS CORRODED. 77-65. REMOVED LT WING NR 3 FLAP JACK SCREW BALL NUT IN REF 757, AMM 27-51-11-024-001. DURING OK TO INSTALL, FOUND INNER BORE OF BALLSCREW YOKE RUSTY. REMOVED LT WING NR 3 AFT UNIVERSAL JOINT FROM INBD T/E FLAP OTBD TRACK IN REF TO AMM 27-51-11-024-001. INSTALLED AFT UNIVERSAL JOINT AND BALLSCREW ASSY ON LT WING NR 3 T/E FLAP TRACK IN REF TO AMM 27-51-11-424-020 TORQUE ID 14-289, DUE DATE 16SEP16,VERIFIED AEROSHELL 33 USED. SAA 042. PERFORMED OPS CHECK ON LT WING, NR 3 FLAP JACK SCREW BALL NUT IN REF TO AMM 27-51-02-825-001. OPS CHECK GOOD JOB COMPLETE.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 59,827 hrs · 26,233 cycles

EMERGENCY LIGHT INOPERATIVE AT SEAT 43FED. REPAIRED WIRE AND OPS CHECKED GOOD REF SWPM 20-64-17.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 58,111 hrs · 25,537 cycles

SEAT 43 DEF SEAT MOUNTED EMERGENCY LIGHT IS INOPERATIVE. REPAIRED BROKEN WIRE IAW SWPM 20-64-17, CHECKED GOOD.

Part: FAN — FAILED (CABIN) · airframe 57,740 hrs · 25,394 cycles

F/A`S REPORTED DETECTED AN ACRID SMOKE ODOR NEAR SEAT 23 & 24. REPLACED THE RT RECIRCULATING FAN AND FILTER IAW AMM 21-25.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 57,157 hrs · 25,152 cycles

FOUND ON SERVICE CK EMERGENCY LIGHT, RED, LENS MISSING AT SEAT 27D. REPLACED BROKEN 27D EMERGENCY SEAT RED AISLE LIGHT, OPS NORMAL.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 57,063 hrs · 25,109 cycles

SEAT 20D SEAT MOUNTED EMERGENCY LIGHT INOPERATIVE. INSTALLED NEW CONNECTOR AT SEAT 20D.

Part: PLATE — CORRODED (DOOR CAM) · airframe 64,438 hrs · 27,913 cycles

R1 DOOR LOWER HINGE, UPPER CAM PLATE HAS CORROSION. REMOVED AND REPLACED THE UPPER CAM PLATE IAW AMM 52-11-09-404-017.

Part: SKIN — TORN (CARGO DOOR) · airframe 54,164 hrs · 23,903 cycles

TEAR IN THE LOWER AFT CORNER OF THE CARGO DOOR SKIN. REPAIRED IAW ERA 497860-14 REV C.

Part: PANEL — DAMAGED (RT WING) · airframe 52,334 hrs · 23,189 cycles

RT WING PANEL 611DB HAS DAMAGE AT APROX-CENTER OF PANEL. REPAIRED PANEL IAW SRM 51-70-17. INSTALLED PANEL.

Part: WIRE HARNESS — DISCONNECTED (EMERGENCY LIGHT) · airframe 51,757 hrs · 22,939 cycles

SEAT 20DEF EMERGENCY LIGHT INOPERATIVE. FOUND ROW 20 EMERGENCY LIGHT HARNESS DISCONNECTED.

Part: UNKNOWN — ODOR (CABIN) · airframe 49,848 hrs · 22,117 cycles

AFT FLIGHT ATTENDANT REPORTED ELECTRICAL SMOKE SMELL IN CABIN. RETURNED TO GATE. INSPECTED AFT GALLEY, LAV, AND CABIN AREA ALL COMPONENTS OP OK AND NO SMELL ON ARRIVAL. SUSPECT EXHAUST IN AC SYSTEM, AIRCRAFT WAS OK FOR SERVICE.

Part: BOTTLE — DISCHARGED (L4 DOOR ASSIST) · airframe 49,095 hrs · 21,814 cycles

4L ENTRY DOOR EMERGENCY DOOR ASSIST BOTTLE REPORTED DISCHARGED. INSPECTION PERFORMED AND 4L ENTRY DOOR EMERGENCY DOOR ASSIST BOTTLE REPLACED.

Part: COFFEEMAKER — CONTAMINATED (GALLEY) · airframe 47,924 hrs · 21,304 cycles

NOXIOUS FUMES FROM AFT GALLEY WHILE AT FL370. FUMES DISSIPATED AFTER THE QRH WAS ACCOMPLISHED. FLIGHT DIVERTED TO FSD AND LANDED WITHOUT INCIDENT. FOUND PLASTIC ON BOTTOM OF COFFEE POT AND WARMING PLATE. CLEANED POT AND HOTPLATE. RAN ENGINES THROUGH BLEED SHIFT. NO ODOR IN GALLEY.

Part: BOTTLE — DISCHARGED (L4 DOOR) · airframe 47,453 hrs · 21,122 cycles

DURING LINE CHECK FOUND L4 DOOR ASSIST BOTTLE READS EMPTY. REMOVED ASSIST BOTTLE PER B757 AMM 52-11. INSTALLED ASSIST BOTTLE PER B757 AMM 52-11. INSPECTED FINAL INSTALLATION AND SAFETY PER B757 AMM 52-11-30. A/C OK FOR SVC.

Part: UNKNOWN — ODOR (FWD CABIN/GALLEY) · airframe 46,331 hrs · 20,696 cycles

DURING CLIMB, CREW NOTICED A STRONG ELECTRICAL BURNING ODOR IN THE COCKPIT AND CABIN NEAR DOOR 2. GALLEY 2 CIRCUIT BREAKERS WERE PULLED. F/A INDICATED POSSIBLE COFFEE MAKER ODOR. MAINTENANCE CHECKED ALL RECIRCULATION AND COOLING FANS. RAN ENGINES, APU, AND PACKS WITH NO FINDINGS.

Part: TERMINAL — BROKEN (L2 DOOR) · airframe 45,182 hrs · 20,187 cycles

L2 DOOR SLIDE LIGHT WIRE TERMINAL BROKEN. REMOVED AND REPLACED L2 DOOR SLIDE LIGHT PER WDM-25-66-11. (DL757103092)

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,182 hrs · 20,187 cycles

MAIN CABIN INNER CUSP CHORD CORRODED STA 1180-1200R. CUT OUT DAMAGED AREA AND INSTALLED AND SPLICED NEW ANGLE. (DL757103096)

Part: LIFTER — WORN (R4 DOOR) · airframe 45,182 hrs · 20,187 cycles

R4 DOOR LOWER GATE HAVE FWD AND AFT GIRT BAR'S LIFTERS FITTING WORN ELONGATED. REMOVED AND REPLACED FWD AND AFT LIFTERS. (DL757103101)

Part: HINGE FITTING — DAMAGED (NR 2 PYLON) · airframe 45,182 hrs · 20,187 cycles

AFTER REMOVAL OF NR 2 PYLON RT SIDE AFT TR HINGE FTG P/N 311N3555-28 FOUND LWR FWD HOLE OVERSIZED AT STA 144 NOTE: HOLE IS THROUGH TR HINGE FTG AND BULKHEAD FTG P/N 311N3231-1. NEW SKIN SECTION NOT DRILLED. REPAIRED PER ERA 486191-14. (DL757103095)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,182 hrs · 20,187 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1600-1620 BETWEEN STR 29R& 30. REMOVED AND REPLACED INTERCOSTAL. (DL757103097)

Part: FITTING — CHAFED (NR 1 PYLON) · airframe 45,182 hrs · 20,187 cycles

NR 1 PYLON O/B BULKHEAD FITTING AT NAC 201 BOTTOM AREA HAS A DEEP CHAFE INDICATION. REMOVED AND REPLACED GUSSET REF ERA 48661888-14. (DL757103099)

Part: INTERCOSTAL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 45,182 hrs · 20,187 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1520-1540 BETWEEN STR 28 & 29 R. REMOVED AND REPLACED INTERCOSTAL. (DL757103098)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,182 hrs · 20,187 cycles

DENT AND GOUGE ON FUSELAGE SKIN AT STA 1699 AND .5 INCH BELOW S15L UP TO 3.5 IN ABOVE S-15L. REPAIR PER ERA 486832. (DL757103094)

Part: SKIN — DAMAGED (FUSELAGE) · airframe 45,182 hrs · 20,187 cycles

DENT AND GOUGE ON FUSELAGE SKIN AT STA 1699 AND 1 INCH ABOVE S-16L. BLENDED AND MEASURED OUT OF LIMITS AND INSTALLED REPAIR. (DL757103093)

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 35,117 hrs · 15,908 cycles

AT FLT LVL 360 LOUD BANG FROM LEFT ENGINE. ENGINE SHUT ITSELF DOWN. PASSENGERS ON LEFT SIDE OF A/C SAW FLAMES FROM TAILPIPE OF LEFT ENGINE. REPLACED ENGINE.

Part: COOLING FAN — ODOR (C-1 CARGO BAY) · airframe 33,370 hrs · 15,238 cycles

EQUIPMENT COOLING OVERHEAT WITH ODOR, NOT VISIBLE SMOKE. PLACED IN ALTN, ODOR DISSIPATED. REPLACED FWD EQUIPMENT COOLING FAN.

Part: CLIP — BROKEN (L-2 DOOR GIRTBAR) · airframe 30,961 hrs · 14,316 cycles

L-2 DOOR SLIDE DEPLOYED WHILE ARMED WHEN OPENED FROM THE OUTSIDE. FOUND GIRT BAR RETAINING CLIP BROKEN ON ONE END. SUSPECT INTERFERENCE WITH GIRT BAR END FITTING BEING DETACHED FROM FLOOR FITTING. REPLACED CLIP.

Part: SPRING — WORN (R4 DOOR GIRT BAR) · airframe 28,424 hrs · 13,334 cycles

ON ARRIVAL F/A REPORTED R4 DOOR SLIDE DIFFICULT TO DISARM. FOUND GIRT BAR RETAINING SPRINGS WORN. REPLACED GIRT BAR PER MM, RII COMPLIED WITH.

Part: BEAR STRAP — DENTED (FUSELAGE) · airframe 27,427 hrs · 12,963 cycles

THE SKIN AND UNDERLYING BEAR STRAP WERE DENTED BY GROUND EQUIPMENT AT THE LOWER EDGE OF THE C2 DOOR CUTOUT AT FS 1430 JUST ABOVE THE LOWER DOOR SILL AT STRINGER 27R. THE DENTED AREA OF SKIN AND BEAR STRAP WERE CUTOUT WITH A 7 X 1.5 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER PER ER/A 087312-14.

Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 26,853 hrs · 12,710 cycles

FUSELAGE SKIN FS 840 STRG 9L-10L, LIGHTNING STRIKE REPAIR, AN EXISTING TEMPORARY DOULBER FOR A LIGHTNING STRIKE DAMAGE WAS REMOVED FROM THE FUSELAGE SKIN AT FS 840 BETWEEN STRINGERS 9L & 10L. THE DAMAGE CUTOUT WAS INSPECTED AND OVERSIZED AND THE EXISTING REPAIR FASTENER HOLES INSPECTED AND OVERSIZED. THE AREA WAS REPAIRED WITH AND EXPANDED ALUMINUM REPAIR DOUBLER PER ER/A 385299-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 26,853 hrs · 12,710 cycles

FUSELAGE SKIN FS 1510 STR 28R-29R AND 28L-29L: AIRFONE ANTENNA CUTOUT CORROSION REPAIR. THE AIRFONE ANTENNA CUTOUTS AT FS 1510 BETWEEN STRINGERS 28R & 29R AND BETWEEN 28L & 29L WERE FOUND CORRODED. THE CUTOUTS WERE ENLARGED TO REMOVE THE CORROSION DAMAGE. THE CUTOUTS WERE THEN REPAIRED WITH EXTERNAL ALUMINUM REPAIR DOUBLERS PER ER/A 385303-14, REV A.

Part: COMPRESSOR — FAILED (NR 2 ENGINE) · airframe 20,491 hrs · 9,650 cycles

ON TAKEOFF AT 1500 FT ASPD 190 NR 2 ENG COMP STALL FOLLOWED BY EGT IN YELLOW. EPR DROPPED TO 1.0. REDUCED POWER TO IDLE AND STAYED THERE THE REMAINDER OF THE FLIGHT WITH EGT 475. ENGINE FAILED 2ND AND 3RD STAGE BOROSCOPE. REPLACED NR 2 ENGINE PER 6T103 RII COMPLETED ON 6T103.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 19,991 hrs · 9,417 cycles

ON TAKEOFF ROLL LEFT ENGINE DID NOT REACH TAKEOFF POWER LEFT ENGINE INDICATED 1.09 EPR RIGHT ENGINE 1.26 EPR TRIED TO RUN UP LEFT ENGINE FARTHER LEFT OIL PRESSURE RED WARNING INDICATED HIGH OIL PRESSURE STOPPED TAKEOFF ROLL AT VERY LOW SPEED LESS THAN 40 KNOTS. FOUND CUT O RING BETWEEN FUEL FLOW TRANSMITTER AND FUEL DISTRUBUSTION MANIFOLD LINE REPLACED O-RING RAN PER PFHB ALL IND NORMAL.

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 19,732 hrs · 9,305 cycles

NR 1 PYLON CRACKED AT FWD INBOARD TORQUE BOX CUTOUT 443AR AT UPPER FWD EXT CORNER. REPAIRED PER SRM 54-51-01.

Part: SKIN — CRACKED (LT WING PYLON) · airframe 19,732 hrs · 9,305 cycles

NR 1 PYLON CRACKED O/B FWD AT 433AL CUTOUT AFT UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2.

Part: SKIN — CRACKED (NR 2 NACELLE) · airframe 19,732 hrs · 9,305 cycles

PYLON SKIN CRACKED AT TORQUE BOX FWD I/B ACCESS CUTOUT FWD UPPER CORNER. REPAIRED PER SRM 54-51-01-2-2.

Part: ENGINE — MALFUNCTIONED (NR 1)

ON ENGINE RUN-UP PRIOR TO TAKEOFF, GOT A COMPRESSOR STALL AND SMOKE AND FLAMES OUT OF INLET AND EXHAUST. CREW PULLED OFF ACTIVE ON TO TAXIWAY SAW OIL PRESS AT ZERO AND THEN SHUT ENG DOWN. FIRE DEPT RESPONDED AND SHOT FIRE RETARDANT AND WATER INTO INTAKE AND EXHAUST. REPLACED ENGINE.

Part: WIRE — BROKEN (ROW 6C)

IR 6C EMER LIGHT INOP. REPLACED HARNESS.

Part: LIGHT — INOP (LT EMER EXIT)

IR LT AFT EMERGECEY LIGHT OVER WING LIGHT INOP, RELAMPED.

Part: TE WEDGE — DENTED (NR 8 LE SLAT)

WING RT, NR 8 SLAT, TRAILING EDGE WEDGE REPAIRED FOR DENT. THE TRAILING EDGE WEDGE ON THE RT WING NR 8 SLAT WAS FOUND WITH A 4 BY .875 BY .040 DEEP DENT. THE DAMAGED AREA WAS REPAIRED PER B757 SRM 57-43-02, FIG. 201. BECAUSE THE SLAT WEDGES ARE THE SUBJECT OF AD 91-22-51, ER/A 364600-14AD WAS ISSUED TO DOCUMENT THE REPAIR.

Part: ENGINE — TAILPIPE FIRE (NR 1)

LT ENG OVERTEMPED ON START/TAILPIPE FIRE. FOUND FCU C/P D05006 ON LT ENG DAMAGED. REPLACED C/P LT EEC AND LT FCU ENG RUN NORMAL. FIRE DAMAGE TO A/C CAUSING DELAMINATION OF LT WING T/E PNL AND LT INBD T/E FLAP O/B FLAP TRACK FAIRING. A/C FERRIED TO ATL.

Part: POWER SUPPLY — INOPERATIVE (L1 DOOR)

ON L/O, FOUND L1 DOOR EXTERIOR SLIDE LIGHT INOP. REPLACED BULB, NO HELP. REPLACED BATTERY POWER SUPPLY. OPS CK GOOD.

Part: SKIN — CRACKED (NR 9 LE SLAT)

THE TRAILING EDGE WEDGE ON THE NR 9 SLAT WAS FOUND WITH A .5 INCH CRACK ON THE UPPER SKIN APPROX 3 FROM THE TRAILING EDGE AND 46 FROM THE OUTBOARD EDGE. AS THE LEADING EDGE SLAT TRAILING EDGE WEDGES ARE THE SUBJECT OF AIRWORTHINESS DIRECTIVES, THIS ER/A WILL GIVE INSTRUCTIONS TO REPAIR THE DAMAGE.