N693DL
Registered owner: DELTA AIR LINES INC, GA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | on 2011-03-11 | Operator named in NTSB report |
Accident & incident history
Operated by Delta Airlines (per NTSB report)
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
200 reports on file, 1998-11-06 – 2026-07-29.
Part: CONTROL SYSTEM — OUT OF ADJUST (ELEVATOR) · airframe 86,371 hrs · 34,552 cycles
ATB- DUE ELEVATOR FEEL ISSUE AFTER TAKEOFF. ADJUSTED ELEVATOR CONTROL SYSTEM. ADJUSTED ELEVATOR FEEL SENSOR. TEST PASSED.(8816120)(AIRCRAFT GROUNDED)
Part: FRAME — DAMAGED (ZONE 200) · airframe 86,196 hrs · 34,490 cycles
AIRCRAFT 0693, DURING NDT INSPECTION DISCREPANT AREAS WERE FOUND AS FOLLOW: ZONE TO BE INSPECTED BLOCKED BY INTERCOSTAL CLIPS ON FRAME BS 600 BTW LONGERONS 2-3L, ALSO PLUG WAS FOUND ON FRAME BS 620 BTW LONGERONS. 3-4L IAW TASK CARD 5330-2564 STEP: 1. FRAME BS 600 BTW L2-3L WAS INSPECTED IAW ERA ER/A 635388-14 REV. ORIGINAL AND FRAME BS 620 BTW L3-4L WAS REPAIRED IAW SRM SRM 53-00-07-2R, REP. 1. PERFORM A DETAILED VISUAL INSPECTION ON REPAIRED FRAME BS 620 BTW L3-4L EVERY 12,000 FLIGHT CYCLES PER B757-200 SRM 53-00-07-2R REP. 1 PARAGRAPH 5A TABLE 203 ZONE 3.
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 86,196 hrs · 34,490 cycles
AFTER REMOVAL WASTE PAN AT LOWER FUSELAGE WAS FOUND CORROSION ON EXTERNAL FUSELAGE SKIN. REPAIRED PER PRI 635303-14. (1682936) (AIRCRAFT GROUNDED)
Part: SKIN — DAMAGED (ZONE 100) · airframe 86,196 hrs · 34,490 cycles
TWO ELONGATED HOLES LOCATED AT LOWER AFT CORNER AND LOWER FORWARD CORNER OF NR 1 CARGO DOOR CUTOUT IN REF CARD 5331 -01293-02A-01 STEP 6 & 7. REPAIRED PER ERA 635128-14 REV. (1681745) (AIRCRAFT GROUNDED)
Part: WEDGE — DEBONDED (NR 6 SLAT) · airframe 86,194 hrs · 34,489 cycles
DISBOND OF 1.2IN X 1.2IN ON PREVIOUS REPAIR AT UPPER SURFACE ISS114 LE SLAT 6, TRAILING EDGE WEDGE. AREA ON UPPER SURFACE ISS114 LE SLAT 6, TRAILING EDGE WEDGE WAS REPAIRED IAW SRM 51-70-10-2R PROCEDURE REPAIR GENERAL IAW SRM 57-43-02- 2R PROCEDURE 1 REPAIR 1 FIG. 201 NOTE B. (1663119) AIRCRAFT WAS GROUNDED.
Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 86,194 hrs · 34,489 cycles
LOW PRESSURE ON EMERGENCY RESEVOIR AT DOORS 2R AND 4L. EMERGENCY POWER RESERVOIR AT DOORS 2R AND 4L WERE REMOVED PER AMM 52-11-30 AND SERVICEABLE EMERGENCY POWER RESERVOIR AT DOOR 2R WAS REPLACED AND VERIFIED PER AIPC: 52-11-40-01A ITEM 590. INSTALLED UNDER AMDS 2040-0191-2R AND SERVICEABLE EMERGENCY POWER RESERVOIR AT DOOR 4L WAS REPLACED AND VERIFIED PER AIPC: 52-11-30-02 ITEM 85. AND INSTALLED UNDER AMDS 2040-0191-4L STEP 19. (1660435) AIRCRAFT WAS GROUNDED
Part: DOUBLER — DEBONDED (NR 7 SLAT) · airframe 86,194 hrs · 34,489 cycles
DEBONDED ON PRODUCTION DOUBLER OF 2.5IN X 1.5IN AT LOWER SURFACE OSS305.5 LE SLAT 7 TRAILING EDGE WEDGE. LOWER SURFACE OSS305.5 LE SLAT 7 TRAILING EDGE WEDGE WAS REPAIRED IAW SRM-51-70-10-2R IAW SRM-57-43-02-2R-1. (1657512) AIRCRAFT WAS GROUNDED.
Part: SWITCH — SHORTED (ZONE 200) · airframe 86,172 hrs · 34,480 cycles
FO SIDE VOR/DME AUTO/MAN SWITCH SHORTED WHEN PRESSED. SMOKE CAME OUT MOMENTARILY DURING FLIGHT. REPLACED VOR/DME PANEL IAW AMM 34-51. OPS NORMAL. INSPECTED SURROUNDING AREA NTF. (LP 8359410 - AIRCRAFT WAS GROUNDED)
Part: CONTROLLER — ARCED (ZONE 200) · airframe 85,320 hrs · 34,157 cycles
SHIP 693 L FWD WINDOW ARCHING INFLIGHT, RAN QRH THEN MINUTES LATER L-OUTER PAIN WINDOW CRACKED. CORRECTIVE ACTION: REMOVED & REPLACED CAPT'S WINDSHIELD IAW B757 AMM 56-11-01. R/R LT SIDE WINDOW HEAT CONTROLLER REF 757 MM 30-41-10. OPS CK GOOD - ALSO LEAK CK WINDOW ALL CKS PASS OK FOR SERVICE.
Part: SWITCH — FAULTED (GIRT BAR) · airframe 85,266 hrs · 34,133 cycles
CABIN CREW REPORTED THAT THE R2 DOOR SLIDE ARMED LIGHT STAYED ILLUMINATED AFTER DOOR SLIDE DISARMED. R & R R2 DOOR FWD GIRT BAR SWITCH S10220 IAW AMM 25-66. CHECKED GOOD. (8187689)
Earlier reports · 1998–2025 · 190 reports
2025
Part: SLIDE — OUT OF LIMITS (ZONE 800) · airframe 84,812 hrs · 33,959 cycles
FOUND R2 DOOR SLIDE OUT OF LIMITS. R & R R2 DOOR SLIDE IAW AMDS W/C 2566-9001-2R. (7887676)
Part: DOOR FRAME — FOD (ZONE 800) · airframe 84,558 hrs · 33,829 cycles
L3 DOOR WILL NOT ARM. INSPECTED L3 DOOR AND JAM. CLEANED OUT DEBRIS ON JAMB FRAME. OPERATE L3 DOOR AND CLOSED AND ARMED DOOR. OPS CHK GOOD. (7161976)
Part: FUSE — INOPERATIVE (ZONE 200) · airframe 84,545 hrs · 33,817 cycles
ON S/C FOUND EMERGENCY LIGHTS AT 2R DOOR AND 2R LAV INOP. FOUND ONE FUSE ON POWER SUPPLY M732 OPEN. R/R DEFECTIVE FUSE - LIGHT NOW OPS GOOD. REF B757 WDM 33-51-21. (7161960)
Part: STRAP — UNSECURE (ZONE 800) · airframe 84,451 hrs · 33,765 cycles
R2 DOOR ARM LIGHT ANNUNCIATED DOOR DISARMED. UPON INSPECTION OF 2R DOOR GIRT ASSEMBLY FOUND STRAP GETTING IN THE WAY OF SENSOR. RESECURED STRAP. OPS CHK OF DOOR GOOD PER B757 AMM 25-66. (7161922)
Part: GIRT BAR — FAULTED (ZONE 800) · airframe 84,356 hrs · 33,731 cycles
AFTER MAIN CABIN DOOR CLOSE, GIRT BAR DOORS CIRCUIT BREAKER POPPED AGAIN AFTER MAINTENANCE PREVIOUSLY PUSHED BACK IN. OPENED P34 JUNCTION BOX AND REPLACED K256 AND K257 RELAYS. REPLACED S10225 SWICH, FOUND TERMINALS DAMAGED AND SHORTING ON L00404 R2 GIRT DOOR ARMED LIGHT. R&R R2 DOOR GIRT BAR ARMED LIGHT. C/B STAYS IN.
Part: PROXIMITY SWITCH — OUT OF ADJUST (GIRT BAR) · airframe 84,368 hrs · 33,735 cycles
SHIP 693 R2 DOOR SLIDE ARMED LIGHT REMAINS ILLUMINATED. CORRECTIVE ACTION: REF B757 AMM 25-66. PERFORMED GIRT BAR PROX SWITCH GAP ADJUSTMENT. OPS NOW NML. (7715288)
Part: INDICATOR — FAULTED (ZONE 800) · airframe 84,356 hrs · 33,731 cycles
SHIP 693 3R DOOR KNUCKLE KNOCKER DOES NOT RETRACT WHEN DOOR IS ARMED. CORRECTIVE ACTION: ADJUSTED KNUCKLE KNOCKER AS NEEDED. OPS NORMAL REF: B757 AMM 25- 66. (1269156)
Part: CIRCUIT BREAKER — TRIPPED (ZON E800) · airframe 84,356 hrs · 33,731 cycles
SHIP 693 SLIDE ARM LIGHT INOP ON ALL DOORS. CORRECTIVE ACTION: FOUND C/B POPPED FOR GIRT BAR IND PUSHED IN NO FAULTS FOUND. (7715284)
Part: DOWNLOCK — OUT OF POSITION (ZONE 700) · airframe 84,198 hrs · 33,640 cycles
SHIP 693 LANDING GEAR "DOORS" LIGHT REMAINED ILLUMINATED AFTER GEAR EXTENSION WITH AN EICAS "GEAR DOORS" MESSAGE. CORRECTIVE ACTION: INSPECTED A/C AND FOUND RIGHT MLG DOOR OPEN AND RED UNSAFE LIGHT ILLUMINATED. T/S R/R UPLOCK SEQUENCE VALVE, R/R BOTH HYDRAULIC FUSES INLINE TO UPLOCK SEQUENCE VALVE, R/R RT MLG DOOR OPERATED SEQUENCE VALVE, R/R RT GEAR DOOR RELEASE INTERLOCK ACT, R/R RT TRUCK TILT ACTUATOR, R/R RT MALG DOOR SAFETY VALVE, R/R RT DOOR ACT, R/R RT MLG DOWNLOCK ACT AND PERFORMED GEAR SWING PER B757 AMM 32-32, CKS GOOD. (7715208)
Part: BATTERY PACK — FAULTED (ZONE 200) · airframe 84,162 hrs · 33,626 cycles
WHILE PERFORMING MG, FOUND EMERGENCY LIGHTS 4DC 5DC 15/15DEF AND R2 ON WHEN A/C DOWN POWERED AND EMERGENCY LIGHT SW OFF. REPLACED POWER SUPPLY M730 IN FWD CEILING PANEL PER AMM 33-51. REPLACED BATTERY PACK M732 PER B757 AMM 33-51 CHECKS GOOD BATTERY CHARGING CHARGE WILL BE COMPLETE AT 1530 MST. R /R BATTERY CHARGER AND BATTERY PACK M732 PER B757 AMM 33-51 OPS CHECK GOOD. (7354393)
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 84,142 hrs · 33,614 cycles
EMERGENCY EXIT LIGHTS INOP ROW 4 TO R2 DOOR. R & R BATTERY PACK IAW AMM 33-51. OPS CHECK GOOD. (7354381)
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 84,129 hrs · 33,605 cycles
EMERGENCY EXIT LIGHTS INOP. FOUND EMERGENCY LIGHTS ON R2 DOOR AND AFT PORTION OF FIRST CLASS INOP. REPLACED BATTERY PACK PER B757 AMM 33-51 OPS GOOD. (7354372)
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 83,940 hrs · 33,512 cycles
SHIP 693 ON SVC CHK FOUND M732 BATTERY PACK EMERGENCY LIGHTS INOP. CORRECTIVE ACTION: R/R M732 BATTERY AND CHARGER IAW B757 AMM 33-51. OPS CHK GOOD. (7475970)
Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 83,901 hrs · 33,501 cycles
SHIP 693 1R ENTRY DOOR KNUCKLE KNOCKER PROTRUDES FURTHER OUT THAN NORMAL WITH DOOR IN ARMED POSITION. CORRECTIVE ACTION: REMOVED R1 ESCAPE SLIDE COVER TO FOM. R/R THE BOX ASSY FOR THE R1 KNUCKLE KNOCKER PER B757 AIPC 52-11. R1 DOOR OPS CHECK GOOD PER B757 AMM 52-11. REMOVED PIN FROM R1 DOOR SLIDE AND REINSTALLED COVER PER B757 AMM 52-11. SLIDE SAFETY PIN REMOVED AND STOWED. (7475918)
Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 82,508 hrs · 32,795 cycles
SHIP 693 DOOR 1R EMERGENCY ASSIST AIR BOTTLE LOW PRESSURE. CORRECTIVE ACTION:REPLACED 1R PASSENGER DOOR EMERGENCY POWER RESERVOIR PER B757 AMM 52-11. (5694841)
Part: BRACKET — MISSING (ZONE 800) · airframe 82,500 hrs · 32,792 cycles
SHIP 693 DOOR 604 OPS CHECKS GOOD, BUT FOUND DOOR 604 MECHANISM MISSING THE BRACKET ASSY. CORRECTIVE ACTION: REPLACED KNUCKLE KNOCKER BOX ASSY. PER B757 CMM 52-11-07. (0777937)
2024
Part: BUSHING — WORN (GIRT BAR) · airframe 81,856 hrs · 32,494 cycles
SHIP 693 1R DOOR NOT FULLY DISARMING. CORRECTIVE ACTION: T/S INSTALLED GIRT BAR AND ADJ, REPLACED GIRT BAR AFT BRACKET ASSY BUSHINGS, ADJ FORE AND AFT RADIUS RODS. RPLACD FWD AND AFT CAM BUSHING PER B757 AMM 52-11. OPS CK GOOD. ADJ, RIG AND SAFETY OF DOOR MECH GOOD.
Part: GIRT BAR — OUT OF POSITION (ZONE 800) · airframe 81,854 hrs · 32,493 cycles
SHIP 693 1R DOOR UNABLE TO OPEN BY CATERING. CORRECTIVE ACTION: FOUND GIRT BAR NOT RELEASED AT 1R DOOR - RELEASED AND OPERATED SEVERAL TIMES - OPS GOOD. (6693769)
Part: SIGN — DETACHED (ZONE 200) · airframe 81,688 hrs · 32,366 cycles
SHIP 693 EXIT SIGN FELL OFF AT 2R (604). CORRECTIVE ACTION: REINSTALLED 2R DOOR EXIT COVER REF B757 AMM 33-51. (5260176)
Part: TRIGGER — CRACKED (ZONE 800) · airframe 81,679 hrs · 32,361 cycles
SHIP 693 IN REFERENCE RC 2040-0191-4R: DURING ADJUST OF NO. 4 RIGHT DOOR TRIGGER MECHANISM IS CRACKED. CORRECTIVE ACTION: SUMMARY OF NRC 00293: TRIGGER FORK WAS REPLACED PER B757-200 AMM 52-11-32. (0592859)
Part: SKIN — DENTED (ZONE 200) · airframe 81,679 hrs · 32,361 cycles
SHIP 693 IN REFERENCE TO NRC 00036: DENT (1 EA) ON FUSELAGE SKIN BWT STA. 1941 TO 1963 AND BTW S-3L TO S-6L AT AFT FUSELAGE BODY SECTION 48 "DENT #4; A=850" Y=0.050" A/Y=17. AREA IS OUT OF LIMITS PER B757-200 SRM 53-80-01-1A AD. CORRECTIVE ACTION: SUMMARY OF NRC 00267: FUSELAGE SKIN BWT STA. 1941 TO 1963 AND BTW S-3L TO S-6L AT AFT FUSELAGE BODY SECTION 48 WAS REPAIRED PER PRI 621163-14 REV 1 AND ER/A 621163-14 REV ORIGINAL SECTION I: PERMANENT REPAIR. (0592670)
Part: WEDGE — DEBONDED (NR 2 SLAT) · airframe 81,679 hrs · 32,361 cycles
SHIP 693 AD - AA - 1 DISBONDED AREA WAS FOUND ON TRAILING EDGE WEDGE UPPER SURFACE ON METAL BOND REPAIR AT SLAT 2 OSS591.80 OF 1.250 IN X 1.250 IN IN REFERENCE TO WC 5740-01145-05B, STEP 4. CORRECTIVE ACTION: SUMMARY OF NRC SERIAL 00027: DUE TO UNABLE TO REPAIR SLAT #2 BY SRM 57-43-02; SLAT #2 REPLACEMENT AND LOG FUNCTIONS ARE ACCOMPLISHED UNDER AMDS WORKCARD 2781-4380-02. (0592081)
Part: SKIN — CORRODED (ZONE 100) · corrosion level 2 · airframe 81,679 hrs · 32,361 cycles
SHIP 693 CORROSION ON INNER SKIN ON FWD CARGO DOOR CONTROL PANEL AT FUSELAGE. CORRECTIVE ACTION: SUMMARY OF NRC 00051: CORROSION ON INNER SKIN BEAR STRAP ON FWD CARGO DOOR CONTROL PANEL AT FUSELAGE WAS REPAIRED PER ER/A 621144-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR. (0590534)
Part: FITTING — INOPERATIVE (GIRT BAR) · airframe 81,679 hrs · 32,361 cycles
SHIP 693 AA. AD. IN REFERENCE AMDS 2560-01492-0201 STEP 2: LEAF SPRINGS DO NOT HOLD FITTINGS ON L2 GIRT BAR. CORRECTIVE ACTION: SUMMARY OF NRC 00040: LEAF SPRINGS ON FITTINGS ON L2 GIRT BAR WERE REPLACED BY NEW PER B757 200 SRM 51-40-02-0G AND CMM 25-66- 14.ALSO INSPECTION AND TEST OF THE GIRT BAR L2 DOOR WAS PERFORMED ON REFERENCE 2560-01492-0201 AND TEST. (0582929)
Part: NUT — LOOSE (ZONE 800) · airframe 81,679 hrs · 32,361 cycles
SHIP 693 MISSING LOCKWIRE AND LOOSE NUT OF EMERGENGY POWER RESERVOIR AT R4 AND R2 PASSENGER DOORS. CORRECTIVE ACTION: SUMMARY OF NRC 00129: B-NUT OF EMERGENCY POWER RESERVOIR AT R4 AND R2 PASSENGER DOORS WAS TIGHTENED AND LOCKWIRE WAS INSTALLED PER B757-200 AMM 52-11-30. (0579486)
Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 81,501 hrs · 32,249 cycles
SHIP 693 DOOR 1L "DISARM" GREEN PLACARD DOES NOT AUTOMATICALLY EXTEND WHEN DOOR IS DISARMED. CORRECTIVE ACTION: OUND HINGE PIN SEIZED. LUBRICATED PIN. IL DISARM SIGN OPS NML. (5897660)
Part: STOP FITTING — MISSING (L4 DOOR) · airframe 80,827 hrs · 31,856 cycles
SHIP 693 DURING GIRT BAR LUBE AND INSPECTION FOUND PAX DOOR 4L AFT NBR 3 FROM THE TOP DOOR FITTING STOP MISSING. CORRECTIVE ACTION: REPLACED PAX DOOR 4L AFT 3RD DOWN DOOR STOP PER B757 AMM 52-11. (5937893)
Part: INDICATOR — INOPERATIVE (L1 DOOR) · airframe 80,674 hrs · 31,775 cycles
SHIP 693 L1 DOOR KNUCKLE KNOCKER WILL NOT OPEN. CORRECTIVE ACTION: CYCLED L1 DOOR ARM LEVER L1 KNOCKER ENGAGES NML REF B757 AMM 52- 11. (5437160)
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,726 hrs · 31,338 cycles
SHIP 0693 DOOR 1R FLOOR PROX SWITCH. CORRECTIVE ACTION: T/S PER FIM 25-66-00-815-802, REMOVED AND REPLACED 1R GIRT BAR PROX SWITCHES REF B757 AMM 25-66 CKS GOOD. (0066655)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,568 hrs · 31,244 cycles
SHIP 0693 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS / 1R SLIDE LIGHT STAYS ILLUMINATED. CORRECTIVE ACTION: OPS CHECKED 1R DOOR, DOOR ARMING MECHANISM OPS NML. (0026649)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,536 hrs · 31,222 cycles
SHIP 0693 MULTIPLE DEEP SCRATCHES AND DENTED SKIN AFT OF AND BELOW AFT LEFT CABIN DOOR FOUND DURING WALKAROUND. CORRECTIVE ACTION: REF ERA 612890-14. (4509838)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,536 hrs · 31,222 cycles
SHIP 0693 FUSELAGE SKIN / STA 1681 - STA 1701 / STR 18L - STR 19L / DENT. CORRECTIVE ACTION: REF ERA 612890-14. (0023352)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,532 hrs · 31,221 cycles
SHIP 0693 1R SLIDE LIGHT WILL NOT EXTINGUISH, DOOR IS DISARMED. CORRECTIVE ACTION: CYCLED DOOR NUMEROUS TIMES, FOUND OPERATING NORMAL IAW B757 AMM 25-66.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,230 hrs · 31,034 cycles
SHIP 0693 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ R1 REMAINS ILLUMINATED. CORRECTIVE ACTION: INSPECTED, CLEANED AND LUBED GRIT BAR SLIDERS AND FLOOR FITTINGS PER B757-AMM-12-21-18. SLIDE LIGHT OPS NML. (2942151)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,208 hrs · 31,022 cycles
SHIP 0693 3R NOT ARMING. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR AREA PER B757 AMM 52-21. (4527522)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,164 hrs · 31,005 cycles
PRES/DIV/DE- DIV TO MTY DUE TO CABIN ALTITUDE WARNING. PERFORMED EMERGENCY DESCENT. NO PASSENGER OXYGEN MASKS DEPLOYED. CORRECTIVE ACTION: FOUND A BUILDUP OF DIRT /GREASE ON L1, L2, AND L3 DOOR SEALS/MATING SURFACES AND CLEANED THE SAME. (8/20 MSP) R/R O/H PANEL. C/W NO GO ODI CK OUTS.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 79,151 hrs · 31,002 cycles
SHIP 0693 A SCRATCH/DENT WAS INDUCED AT FUSELAGE SKIN, BETWEEN STA 1459-1480 AND BETWEEN S 6L & S 7L. CORRECTIVE ACTION: REF ERA 601684-14AD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 78,857 hrs · 30,843 cycles
SHIP 693 -ATO- DISCONTINUED TAKEOFF LESS THAN 30 KNOTS DUE TO RIGHT ENGINE HAD NO THROTTLE RESPONSE. CORRECTIVE ACTION: #2 ENGINE WAS REPLACED.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 78,814 hrs · 30,820 cycles
SHIP 0693 R1 SLIDE LIGHT ILLUMINATED/INOP. CORRECTIVE ACTION: OPS CHECKED R-1 DOOR SLIDE LT AND FOUND NO FAULTS, CHECKED GIRT BAR FITTINGS FOR DEBRIS NONE FOUND.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 78,156 hrs · 30,486 cycles
SHIP 693 SMOKEY HAZE IN AFT CABIN WITH ELECTRICAL SMELL, CORRECTIVE ACTION: FOUND APU BATTERY TO BE SOURCE OF SMOKE AND SMELL. REPLACED APU BATTERY AND CHARGER PER B757 AMM 24-31. TESTS GOOD. C/W NO GO ODI PROCEDURES. OK FOR SERVICE. (8568626)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 78,069 hrs · 30,431 cycles
SHIP 693 ON SVC CK FOUND EMERGENCY LIGHTS INOP FROM SEATS 27-32 FED AND OVER WING EXITS. CORRECTIVE ACTION: FOUND LOOSE CONNECTIONS AT BATTERY PACK M10568 LOOSE. SECURED AND TIGHTENED CONNECTIONS PER B757 AMM 33-51. (9467984)
Part: UNKNOWN — UNKNOWN · airframe 77,745 hrs · 30,276 cycles
SHIP 693 2L DOOR HARD TO CLOSE. CORRECTIVE ACTION: SECURED ROD END SUPPORT BRACKET TO THE SERRATED PLATE REF B757 AMM 52-11-04 OPS CKS GOOD. (2621673)
Part: UNKNOWN — UNKNOWN · airframe 77,745 hrs · 30,276 cycles
SHIP 693 2L DOOR WILL NOT ARM. CORRECTIVE ACTION: CYCLED DOOR OPS CKS OK PER B757MM 52-11. (9886414)
Part: UNKNOWN — ODOR (CABIN) · airframe 77,535 hrs · 30,134 cycles
SHIP 0693 - MISC/DE - DUE TO ELECTRICAL SMELL FROM FIRST CLASS LAV. CORRECTIVE ACTION: MTC COMPLETED FULL INSPECTION OF LAV WITH NO TROUBLE FOUND. C/W NO-GO PROCEDURES.
2022
Part: COVER — UNSECURE (EXIT SIGN) · airframe 76,883 hrs · 29,821 cycles
SHIP 693 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 2R. CORRECTIVE ACTION: RESECURED SAME. (2454438)
Part: COVER — UNSECURE (EXIT SIGN) · airframe 76,883 hrs · 29,821 cycles
SHIP 693 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 1R. CORRECTIVE ACTION: PERFORMED SECTION 3 PERMANENT REPAIR REF. ER/A REVISION 2 603089 -14. (2454437)
Part: NONE — NONE · airframe 76,718 hrs · 29,756 cycles
SHIP 693 DURING CLIMBOUT AND FOR DURATION OF FLIGHT RECEIVED A LEFT FWD CABIN DOOR LIGHT AND ACCOMPANYING ENTRY DOOR LIGHT ANNUNCIATOR. CORRECTIVE ACTION: INTERIOR HANDLE OF ENTRY DOOR WAS INSTALLED AND ADJUSTED CORRECTLY PER B757-200 AMM 52-11-00, STOP PINS ON L1 ENTRY DOOR WERE ADJUSTED PER B757-200 AMM 52-11-00 AND CABIN PRESSURE CONTROL SYSTEM TEST WAS PERFORMED PER B757-200 AMM 21-31-00 AND LIGHT DOOR AT CABIN ANNUNCIATOR DOES NOT COME ON AND TEST OK. (8924812)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
AIRCRAFT 0693, DRAG FTG OPEN HOLES NBR 1 TO NBR 10 AND FOLLOWING DAMAGES WERE FOUND: HOLE #3, CORROSION ON SKIN AND FITTING BTW 10-12 CLOCK POS ; HOLE #7 CORROSION ON SKIN AND FITTING BTW 8-12 CLOCK POS ; HOLE #8, CORROSION ON SKIN BTW 11-1 CLOCK POS ALSO CORROSION ON FITTING BTW 6-8 CLOCK POS. CORRECTIVE ACTION: HOLES ON RH ENG DRAG FTG WAS REPAIRED PER PRI 574479-14 REV.4 AND ERA 574479-14 REV. C SECTION VI: PERMANENT REPAIR AND TASK CARD 5720-01100-04B (LP2414110)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
AIRCRAFT 0693, HOLES NBR 1,2,4,5,6,9,10,11,12,14,15,16,17 AND 18 PREVIOUSLY INSPECTED UNDER AMDS 5720-01100-04B STEP 14 AND 5720-01100-05B STEP 14 FOUNDED IN TOLERANCE STANDAR, WERE REAMED TO FIRST OVERSIZE AND HOLE 1 REAMED TO 0.5800 INCH. CORRECTIVE ACTION: HOLES # 2, 5, 6, 9, 10, 11, 12, 14, 15, 16, 17 & 18 WERE REPAIRED PER AMDS 5720-01100-04B AND AMDS 5720-01100-05B AND HOLES #1 AND #4 WERE REPAIRED PER PRI 574479-14 REV.4 AND ERA 574479-14 REV. C SECTION VI: PERMANENT REPAIR. (LP 2412602)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
AIRCRAFT 0693, VISUAL INSPECTION WAS ACCOMPLISHED ON RH ENG DRAG FTG OPEN HOLES NBR 11 TO NBR 18 AND FOLLOWING DAMAGES WERE FOUND: HOLE #13, SCRATCHES AND CORROSION ON SKIN AND FITTING BTW 10-1 CLOCK POS. CORRECTIVE ACTION: HOLE #13 ON RH ENG DRAG FTG WAS REPAIRED PER PRI 574479-14 REV.4 AND ERA 574479-14 REV. C SECTION VI: PERMANENT REPAIR. (LP 2412586)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 FWD LEAF SPRING WRONG INSTALLED ON GIRT BAR OF DOOR 4R AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 00071: SPRING WAS REPLACED PER B757-200 51-40-02- 0G PAR. 4 AND ADJUST GIRT BAR MECHANISM MUST BE PERFORMED UNDER JOB 001-0307 AMDS. (2407748)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
AIRCRAFT 0693, CORROSION ON LOWER SILL OF AFTER CARGO DOOR, BETWEEN BS 1380 AND BS 1440. CORRECTIVE ACTION: SIDE PANEL (LOWER SILL) WAS REPLACED PER B-757-200 SRM 51-40-02-0G (LP2408783)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON FRAME (FWD FACE) STA 1400 BTW STRG-28LH-28RH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00778: FRAME (FWD FACE) STA 1400 BTW STRG-28LH-28RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2406411)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON SIDE PLATE LH STA 1310 AND 1360 (C2) IN REFERENCE TO NRC 612. CORRECTIVE ACTION: SUMMARY OF NRC 00887: SIDE PLATE LH STA 1310 AND 1360 WAS REPAIRED PER B757-200 SRM. (2406375)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REF NRC 0798: CORROSION ON FLOOR SUPPORT STRINGER LBL 2 BTW STA 1460-1480, AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00906: FLOOR SUPPORT STRINGER LBL 2 BTW STA 1460-1480 WAS REPAIRED PER B757-200 SRM. (2406308)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REF NRC 0798: CORROSION ON PREVIOUS REPAIR DOUBLER ON FLOOR SUPPORT STRINGER LBL 7 BTW STA 1460-1480, AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION:SUMMARY OF NRC 00907: FLOOR SUPPORT STRINGER LBL 7 BTW STA 1460-1480, AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM. (2406372)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON INTERCOSTAL BTW STA 1400-1420 STRG-28LH AT AFT CARGO COMPARTMENT IN ORDER TO PERFORM NRC 775. CORRECTIVE ACTION: SUMMARY OF NRC 00901: INTERCOSTAL BTW STA 1400-1420 STRG-28LH AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-200 SRM 51-40-02-0G PAR 4 AND 7 AND DWG 146N5425 REV A. (2404944)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON INTERCOSTAL STA 1127 TO 1140 AT LH BODY FAIRING. FUS. CORRECTIVE ACTION: SUMMARY OF NRC 00264: INTERCOSTAL WAS REPLACED PER. B757-200 SRM. (2404882)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT ON LH FRAME STA 1440 S-25-26LH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00762: FRAME STA 1440 S-25-26LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2401247)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT ON LH FRAME STA 1440 S-25-26LH AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00762: FRAME STA 1440 S-25-26LH AT AFT CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2401234)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REF NRC 800: CORROSION ON ANGLE BELOW LH SIDEPLATE BTW STA 1480 TO 1500 AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00902: ANGLE WAS REPLACED PER DWG 146N5448 REV A. AND B757-200 SRM. (2398894)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REFERENCE AMDS 5211-3001-4L STEP 3 LENGTH OF COMPENSATOR INDICATOR EXTENSION AT SNUBBER L4 DOOR IS OUT OF LIMITS. CORRECTIVE ACTION: SUMMARY OF NRC 00810: ROTARY SNUBBER AT L4 DOOR WAS REPLACED PER B757-200 AMM 52-11-10. (2398591)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON INTERCOSTAL BTW STA 1400 AND STA1420 BTW S-30 AND S-29LH AT AFT CARGO COMPARTMENT. (IN REF NRC 00778 ). CORRECTIVE ACTION: SUMMARY OF NRC 00899: INTERCOSTAL BTW STA 1400 AND STA1420 BTW S-30 AND S-29LH AT AFT CARGO COMPARTMENT WAS REPLACED PER. B757-200 SRM. (2397627)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 TOOL MARKS ON ACCESS PANEL STABILIZER 332CL, 332BL, 332DL, 342DR, 342CR. CORRECTIVE ACTION: SUMMARY OF NRC 00558:TOOL MARKS ON ACCESS PANEL STABILIZER 332CL , 332BL, 332DL, 342DR, 342CR WERE BLEND OUT PER B757-200 SRM. HFEC INSPECTION WAS ACCOMPLISHED ON BLENDED AREAS AND NO CRACKS WERE FOUND PER B757-200 SRM AND B757 NDT MANUAL PART 6, 51-00-19. MEASUREMENT THICKNESS WAS ACCOMPLISHED ON REWORKED AREAS OF ACCESS PANEL STABILIZER 332CL, 332BL, 332DL, 342DR, 342CR WITHIN LIMITS BUT ON ACCESS PANEL 332CL WAS FOUND WITH MINIMUM REMAINING THICKNESS, THEREFORE IT S OUT OF LIMITS PER B757-200 SRM 55-10-01-1A. ACCESS PANEL 332CL WAS REPAIRED PER ERA 602083-14 REV.ORIGINAL. (2398702)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON INTERNAL DOUBLER IN WASTE TANK SERVICE PANEL FROM STA 1681 TO 1701 BTW S-29L AND S-29R AT AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00729: INTERNAL DOUBLERS IN WASTE TANK SERVICE PANEL FROM STA 1681 TO 1701 BTW S-29L AND S-29R AT AFT CARGO COMPARTMENT WERE REPLACED PER DWG. (2396721)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 TORN SLIDE ATTACH STRAP ALSO CONTAMINACI N ON SLIDE AT L1 DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00110 : SLIDE ATTACH STRAP AND SLIDE L1 DOOR WERE REPLACED PER B757-200 AMM. 25-66 AND PROCESS OF INSTALLATION IS PER AMDS. (2395932)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT ON FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT IN REFECENCE LOG 2393424, 2395388. CORRECTIVE ACTION: SUMMARY OF NRC 00244: FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2395392)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT ON FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT IN REFERENCE LOG 2393424. CORRECTIVE ACTION: SUMMARY OF NRC 00244: FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2395388)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION OUT OF LIMITS ON FLOOR SUPPORT STRINGER (UPPER/ LOWER SURFACES) LBL 2 (BTW STA 660-680), LBL 7 (STA 640-680), LBL 10 (BTW STA 640-680 AND 693) AND LBL 16 (640-680) AT FWD CARGO COMPARTMENT. IN IN REF NRC 00255. CORRECTIVE ACTION: SUMMARY NRC 00886: FLOOR SUPPORT STRINGER LBL 2 (BTW STA 635-705), LBL 7 (BTW STA 635-705), LBL 10 (BTW STA 635-705) AND LBL 16 (BTW STA 635-705) WERE REPLACED PER B757 -200 SRM. (2393504)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT ON FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00244: FRAME STA 580 S-24L AT FWD CARGO COMPARTMENT WAS REPAIRED PER B757-200 SRM. (2393424)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON SLANT SUPPORT, STA 1460 S- 26LH AT AFT CARGO COMPARTMENT. IN REF NRC 760. C2. CORRECTIVE ACTION: SUMMARY OF NRC 0089: SLANT SUPPORT STA 1460 S -26LH WAS REPLACED PER DWG 453N1801 REV A. AND B757-200 SRM. (2393452)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 RUST ON GIRT BAR OF DOOR 4L AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00073: GIRT BAR OF DOOR 4L WAS REPLACED PER B 757-200 AMM 25-66-10. (2393101)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON ANGLES BELOW OF STOP FITTINGS BTW STA 560-620 AT FWD CARGO COMPARTMENT CUT OUT LOWER SILL AREA. CORRECTIVE ACTION: SUMMARY OF NRC 00261: ANGLES WERE REPLACED PER DWG 143N8560 REV G AND B757-200 SRM. (2392729)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 SCRATCHES ON FLAME SPRAY PANEL TO ECCESS 532HZ, 532FZ.AD. CORRECTIVE ACTION: SUMMARY OF NRC 00629: FLAME SPRAY PANEL TO ECCESS 532HZ, 532FZ.AD WERE REPAIRED PER PRI: 601755-14 REV: 0, REV: 1 AND ERA 601755-14 REV ORIGINAL SECTION I. (2389941)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 SCRATCHES ON FLAME SPRAY TO ACCESS 632HZ AT RH WING. AD. CORRECTIVE ACTION: SUMMARY OF NRC 00625: FLAME SPRAY TO ACCESS 632HZ AT RH WING. AD . WAS REPAIRED PER PRI 601659-14 REV: 0, REV: 1 AND ERA 601659- 14 REV ORIGINAL SECTION I. (2389948)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 SECTION I REPAIR TO RH WING DRY BAY BARRIER AT WSTA 285.65-313.5 REQUIRES SECTION II REPAIR WITHIN 24 MONTHS PER ERA 601659-14. CORRECTIVE ACTION: REF ERA 601659-14. (2389310)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 SECTION I REPAIR TO LH WING DRY BAY BARRIERS AT WSTA 258.50- 285.65 AND WSTA 285.65-313.5 REQUIRES SECTION II REPAIR WITHIN 24 MONTHS PER ERA 601755-14. CORRECTIVE ACTION: REF ERA 601755-14. (2389306)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DENT AND SCRATCH ON EXTERNAL FUSELAGE SKIN BTW BODY STA 1460-1480 BTW S-6L TO S-7L. CORRECTIVE ACTION: SUMMARY OF NRC 00862: EXTERNAL FUSELAGE SKIN BTW BODY STA 1460- 1480 BTW S-6L TO S-7L WAS REPAIRED PER ERA 601684-14 REV. ORIGINAL. SECTION I: PERMANENT REPAIR. (2389418)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 DTE, 601684-14 FUSELAGE / SKIN / STA 1460-1480 & S-6L TO S-7L / DENT & SCRATCH. CORRECTIVE ACTION: REF ERA 601684-14. (2388810)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. 01 DISBOND ON OSS 442 UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00832:UPPER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER B757-200 SRM. (2385209)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. 02 DISBONDS ON LE SLAT 4 TRAILING EDGE WEDGE, LH WING. ON OSS 442 UPPER SURFACE AND OSS 305 UPPER AND LOWER SURFACE. CORRECTIVE ACTION: SUMMARY OF NRC 00068: LE SLAT 4 TRAILING EDGE WEDGE, LH WING. ON OSS 442 WAS REPAIRED PER B757-200 SRM. (2384924)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REF NRC 00257: CORROSION ON FLOOR SUPPORT STRINGER RBL 2 (BTW STA 640-680), RBL 7 (BTW STA 640-680) AND RBL 10 (BTW STA 640- 680) AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY NRC 00888: FLOOR SUPPORT STRINGER RBL 2 (BTW STA 640-680), RBL 7 (BTW STA 640-680) AND RBL 10 (BTW STA 640-680) AT FWD CARGO COMPARTMENT WERE REPLACED PER B757-200 SRM. (2383945)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 AD // A.A. DAMAGES ON OPEN HOLES AT LH ENG DRAG FTG CLAMP-UP AS FOLLOW: HOLE #1 CORROSION ON SKIN BTW 5 AND 6 O CLOCK POSITION, HOLE #3 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE, HOLE #5 CORROSION AND SCRATCHES ON SKIN AND FITTING BTW 4 AND 6 O CLOCK POSITION, HOLE #6 SCRATCHES ON SKIN AND FITTING BTW 4 AND 7 O CLOCK POSITION, HOLE #7 CORROSION ON SKIN BTW 7 AND 10 O CLOCK POSITION, HOLE #8 SCRATCHES ON SKIN AND FITTING ALL AROUND HOLE, HOLE #9 CORROSION ON SKIN AND FITTING BTW 2 AND 4 O CLOCK POSITION, HOLE #10 SCRATCHES ON SKIN AND FITTING BTW 4 AND 6 O CLOCK POSITION. CORRECTIVE ACTION: SUMMARY OF NRC 00200: [AD // A.A] LH ENG DRAG FTG CLAMP-UP HOLE #1,#3,#5,#6 ,#7,#8, #9 AND #10 WERE REPAIRED PER TASK CARD. (2382449)
Part: UNKNOWN — UNKNOWN · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. 01 DISBOND ON DOUBLER REPAIR AT LE SLAT 6 TRAILING EDGE WEDGE, RH WING. ON ISS 115.3 UPPER SURFACE. CORRECTIVE ACTION: SUMMARY ON REF NRC 00099 DOUBLER REPAIR AT LE SLAT 6 TRAILING EDGE WEDGE, RH WING. ON ISS 115.3 UPPER SURFACE WAS REPAIRED PER B757-200 S.R.M. (2380686)
Part: UNKNOWN — UNKNOWN · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. DISBOND ON PREVIOUS REPAIR ON ISS 142, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE , LH WING. CORRECTIVE ACTION: SUMMARY ON REF NRC 00069 PREVIOUS REPAIR ON ISS 142, UPPER SURFACE, LE SLAT 5 TRAILING EDGE WEDGE, LH WING WAS REPAIRED PER B757-200 S.R.M. (2380678)
Part: UNKNOWN — UNKNOWN · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CRACK ON STABILIZATION STRAP IN STA 580 AND 25LBL AT FWD CARGO COMPARTMENT. CORRECTIVE ACTION:SUMMARY OF NRC 00242:AREA WAS REPAIRED ON STABILIZATION STRAP IN STA 580 AND 25LBL AT FWD CARGO COMPARTMENT PER B757-200 SRM. (2380918)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. DISBOND ON OSS 591, UPPER SURFACE, LE SLAT 2 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00067: LE SLAT 2 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER B757-200 S.R.M. (2379360)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.D. 03 DISBONDS ON LE SLAT 10 TRAILING EDGE WEDGE, RH WING. ON OSS 740 UPPER SURFACE AND OSS 836 UPPER SURFACE. CORRECTIVE ACTION: SUMMARY ON REF NRC 00100 SLAT 10 TRAILING EDGE WEDGE, RH WING. ON OSS 740 UPPER SURFACE AND OSS 836 UPPER SURFACE WAS REPAIRED PER B757-200 S.R.M. (2379635)
Part: NONE — NONE · corrosion level 2 · airframe 76,715 hrs · 29,754 cycles
SHIP 693 IN REF TO NRC 00819 (VISUAL INSPECT BY ER/A). CORROSION ON FLOOR SUPPORT BTW STA 365.25-377.7 LBL 65 AT PAX CABIN. CORRECTIVE ACTION: SUMMARY OF NRC 838: FLOOR SUPPORT WAS REPLACED PER B757-200 SRM. (2379327)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CRACK ON STABILIZATION STRAP STA 1660 RBL 26 AT PAXCABIN FLOOR STRUCTURE. CORRECTIVE ACTION: SUMMARY OF NRC 00701: CRACK ON STABILIZATION STRAP STA 1660 RBL 26 AT PAXCABIN FLOOR STRUCTURE WAS REPAIRED PER B757-200 SRM. (2375472)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 A.A. - A.D. DISBOND ON OSS 591, UPPER SURFACE, LE SLAT 2 TRAILING EDGE WEDGE, LH WING. CORRECTIVE ACTION:SUMMARY OF NRC 00067: LE SLAT 2 TRAILING EDGE WEDGE, LH WING. WAS REPAIRED PER B757-200 S.R.M. (2370337)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON MID FITTING ON GIRT BAR OF DOOR R1 AT PAXCABIN. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00072: MID FITTING ON GIRT BAR OF DOOR R1 AT PAX CABIN WAS REPLACED PER B757-200 AMM 25-66-10. (2359122)
Part: NONE — NONE · airframe 76,715 hrs · 29,754 cycles
SHIP 693 CORROSION ON MID FITTING ON GIRT BAR OF DOOR 4R AT PAXCABIN. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00070: MID FITTING ON GIRT BAR OF DOOR R4 AT PAX CABIN WAS REPLACED PER B757-200 AMM 25-66-10. (2359115)
Part: NONE — NONE · airframe 75,485 hrs · 29,196 cycles
SHIP 693 L-2 DOOR SLIDE FOUND CRACKED ON BACK. CORRECTIVE ACTION: REMOVED AND REPLACED L-2 DOOR SLIDE PER AMDS CARD. (8590101)
Part: NONE — NONE · airframe 75,460 hrs · 29,181 cycles
SHIP 693 EXIT LENS MISSING @ RT FWD OVERWING EXIT. CORRECTIVE ACTION: INSTALLED LENS. (8236390)
Part: NONE — NONE · airframe 75,399 hrs · 29,146 cycles
SHIP 693 MAIN CABIN DOOR 2L IS STICKING AND WILL NOT OPEN ALL THE WAY. CORRECTIVE ACTION: PERF DOOR INSP & CHECK PER B757 AMM 52-11. FOUND PAX RAG IN LOWER HINGE ASSY. REMOVED & CYCLE DOOR OPEN/ CLOSE SEVERAL TIMES NO ISSUE. DOOR OPS NML. OK FOR SVC. DOOR DOES NOT REQUIRE RIGGING. PERF DOOR HINGE POINT LUBE IAW B757 AMM 12-21. DOOR OK. (8236354)
Part: NONE — NONE · airframe 75,249 hrs · 29,074 cycles
SHIP 693 2L DOOR DIFFICULT TO OPEN. CORRECTIVE ACTION: FOUND L-2 SNUBBER BAD. REMOVED DOOR FOR ACCESS PER B757 AMM 52-11. REPLACED L-2 SNUBBER PER B757 AMM 52-11-00, RE-INSTALLED L-2 DOOR REF B757 AMM 52-11. (7978283)
Part: NONE — NONE · airframe 75,183 hrs · 29,040 cycles
SHIP 693 DURING INSPECTION OF #2 LEFT PASSENGER DOOR EMERGENCY POWER ASSIST MECHANISM FOUND INNER CHORD AT UPPER HINGE CUTOUT CRACKED. CORRECTIVE ACTION: REPLACED L-2 DOOR ON AMDS 5211-9001-2L. RII TASK COMPLIED. (7978249)
Part: NONE — NONE · airframe 75,183 hrs · 29,040 cycles
SHIP 693 REF LOG 7978249 #2 LEFT DOOR UPPER AND LOWER DOOR HINGE BEARINGS WORN. CORRECTIVE ACTION: REPLACED UPPER AND LOWER HINGE BEARINGS REF B757 AMM 20-10-02. (7978251)
2021
Part: NONE — NONE · airframe 75,170 hrs · 29,035 cycles
SHIP 693 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS: 1C. CORRECTIVE ACTION: ADJUSTED AS REQUIRED. OK FOR SVC. (2070087)
Part: NONE — NONE · airframe 74,812 hrs · 28,877 cycles
SHIP 693 DURING S/C FOUND R4 DOOR SLIDE PRESSURE LOW. CORRECTIVE ACTION: REMOVED R4 DOOR SLIDE PER B757 AMDS 2566-9001-49. (7942532)
Part: UNKNOWN — UNKNOWN · airframe 74,675 hrs · 28,806 cycles
SHIP 693 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS: 02R. CORRECTIVE ACTION: SECURED EMERGENCY 2 R EXIT SIGN. (1984942)
Part: NONE — NONE · airframe 74,634 hrs · 28,787 cycles
SHIP 693 2R EMERGENCY EXIT SIGN COVER FALLING OFF. CORRECTIVE ACTION: SECURED EXIT SIGN LIGHT COVER. (7848074)
Part: NONE — NONE · airframe 74,608 hrs · 28,767 cycles
SHIP 693 EXIT SIGN OVER 2R DOOR IS LOOSE. CORRECTIVE ACTION: SECURED EXIT SIGN IN POSITION. (7848054)
Part: NONE — NONE · airframe 74,546 hrs · 28,746 cycles
SHIP 693 EMERGENCY EXIT SIGNS INOPERATIVE / LOCATIONS:604. CORRECTIVE ACTION: REATTATCHED EXIT SIGN COVER AT 2R DOOR. OPS CK NML. (1960935)
Part: SIGN — DETACHED (CABIN) · airframe 74,447 hrs · 28,701 cycles
SHIP 693 EMERG EXIT SIGN AT 2R DOOR FELL OFF. CORRECTIVE ACTION: INSTALLED EXIT SIGN LENS AT 2R DOOR. (7848000)
Part: CONNECTOR — UNSECURE (EMERGENCY LIGHT) · airframe 74,418 hrs · 28,684 cycles
SHIP 693 EMERGENCY EXIT AISLE LIGHT ON ROW 20D,E,F INOP. CORRECTIVE ACTION: RESECURED EMERGENCY EXIT AISLE LIGHT CONNECTOR AT 20DEF PER B757 AMM 33-51 OPS CHK GOOD. (7927283)
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 74,394 hrs · 28,674 cycles
SHIP 693 EMERGENCY EXIT SIGN COVER LOOSE. CORRECTIVE ACTION: SECURED LOOSE COVER. (1941439)
Part: DOOR — FOD (R1) · airframe 74,384 hrs · 28,671 cycles
SHIP 693 DOOR 1R DISARMED BUT SLIDE ARMED LIGHT STILL ILLUMINATED. CORRECTIVE ACTION: REMOVED FOD FROM DOOR AND 1R DOOR OPS CHK NML PER B757 AMM 52-11. (7927276)
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 74,367 hrs · 28,667 cycles
SHIP 693 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604. CORRECTIVE ACTION: REASSEMBLED LENS AND REINSTALLED LENS AT 2R DOOR. (1932634)
Part: SIGN — DETACHED (EMERGENCY LIGHT) · airframe 74,367 hrs · 28,667 cycles
SHIP 693 REPEAT DISCREPANCY 2R EMERGENCY EXIT SIGN FELL OFF EXIT FRAME ON LANDING ROLL-OUT AFTER A VERY SMOOTH LANDING. CORRECTIVE ACTION: ADJ. LATCHES. OPS NORMAL. (7927242)
2020
Part: LENS — MISSING (TEST BUTTON) · airframe 72,463 hrs · 27,940 cycles
ON SERVICED CHECK FOUND PUSH BUTTON LENS FOR EMERGENCY LIGHT TEST MISSING ABOVE L4 DOOR (BUTTON STILL FUNCTIONAL) FORWARD TO NEF 33-24-05. CORRECTIVE ACTION: REPLACED LENS COVER. SYSTEM OPERATION IS NORMAL.
Part: SUPPORT — CRACKED (NR 2 NACELLE) · airframe 72,277 hrs · 27,877 cycles
DURING CHECK A CRACK WAS FOUND ON ENGINE NR 2 PYLON FAN COWL SUPPORT STRUCTURE RIGHT SIDE. REPAIRED PER ERA.
Part: WEDGE — DEBONDED (NR 6 SLAT) · airframe 72,277 hrs · 27,877 cycles
DURING INSPECTION MAINTENANCE FOUND NR 6 SLAT TRAILING EDGE WEDGE UPPER SURFACE HAS AN INDICATION OF DISBOND. REPAIRED NR 6 SLAT TRAILING EDGE WEDGE UPPER SURFACE ON INBOARD SIDE OF SLATE, PER SRM 51-70-10.
Part: SKIN — DENTED (BS 640 S5-6L) · airframe 74,044 hrs · 28,552 cycles
SHIP 693 ERA 495296-14 REV B FUSELAGE/SKIN/FS 640 BTWN S-5L & S-6L/DENT. CORRECTIVE ACTION: REF ERA 495296-14 REV B AND REV C. (1650018)
Part: SKIN — CRACKED (WING) · airframe 72,277 hrs · 27,877 cycles
CRACK FOUND IN THE WING SKIN COMMON TO THE DRAG FITTING AT HOLES NR 1 AND NR 4. C/W ERA 574479-14.
Part: DIFFUSER — MISSING (EMERGENCY LIGHT) · airframe 72,220 hrs · 27,848 cycles
EMERGENCY EXIT SIGN AT R2 DOOR MISSING LIGHT DIFFUSER. CORRECTIVE ACTION: REPLACED EXIT SIGN LENS. SYSTEM OPERATION IS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 71,779 hrs · 27,653 cycles
DURING SERVICE CHECK FOUND EMERGENCY LIGHTS AT ROWS 1,2 AND 3 INOPERATIVE. REPLACED BATTERY PACK M730. SYSTEM OPERATION IS NORMAL.
Part: INDICATOR — MALFUNCTIONED (L1 DOOR SLIDE) · airframe 71,397 hrs · 27,508 cycles
SHIP 693 1L DOOR SLIDE ENGAGEMENT WARNING PLACARD DEPLOYS WITH A SIGNIFICANT DELAY AND THEN EXTENDS EXCESIVELY. CORRECTIVE ACTION: LUBED SLIDE ENGAGEMENT NWARNING INDICATOR OPS CK GOOD. (6708466)
Part: COVER — LOOSE (EXIT SIGN) · airframe 71,098 hrs · 27,423 cycles
EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:604 / INTERIOR. CORRECTIVE ACTION: RESECURED COVER.
2019
Part: LENS — MISSING (CABIN) · airframe 70,054 hrs · 27,018 cycles
(AIRCRAFT 693, L/P 6214074) L2 DOOR EMERGENCY EXIT LIGHT COVER DIFFUSER LENS MISSING. CORRECTIVE ACTION: R/R R2 DOOR EMERGENCY EXIT LIGHT COVER PER AMM 33-51.
Part: GIRT BAR — DETACHED (L4 DOOR SLIDE) · airframe 69,033 hrs · 26,625 cycles
L4 SLIDE GIRT BAR DETATCHED FROM DOOR. REMOVED AND REINSTALLED PER WC 2566-9001-4L.
Part: LENS — UNKNOWN (CABIN) · airframe 68,723 hrs · 26,490 cycles
SHIP 693 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: REPLACED 1 EACH 2R EMERGENCY LIGHT LENS ASSY REF MM 33-50 CKS OK. (1059338)
Part: ENGINE — ODOR (NR 2) · airframe 68,447 hrs · 26,352 cycles
MILD DIRTY/GYM SOCK SMELL DEVELOPED DURING CLIMB AND DESCENT. ODOR DISSIPATED. OBSERVED BY MULTIPLE CREW MEMBERS. SMELL WAS PRIMARILY MID-CABIN. ASSOCIATED ER/A 14-576898 NBR 2 ENG REPLACED PER W/C 7100-9902E-02. C/W RI 576898-14 REV ORIG SECT 2. PERMANENT REPAIR.
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 68,094 hrs · 26,210 cycles
SHIP 693 2R EXIT LIGHT LENS COVER FELL OFF. CORRECTIVE ACTION: RE-INSTALLED LIGHT LENS. (5134312)
Part: FITTING — CRACKED · airframe 67,851 hrs · 26,110 cycles
SHIP 693 HFEC (ROTO) INSPECTIONS FOUND CRACK INDICATIONS AT FASTENER 1. AT RT ENG DRAG FITTING CLAMP UP REF NR. CORRECTIVE ACTION: REMOVED AND REINSTALLED R/H ENG DRAG I/B FITTING FOR REPAIR AS PER AD 2018-16-05 AND B757-2 SRM. ACCOMPLISHED REPAIR AT RT ENG DRAG FITTING FASTENER 1 AS PR ERA NR 574479-14AD. (0916731)
2018
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 67,745 hrs · 26,059 cycles
(AIRCRAFT 693, L/P 0867087) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:605 / INTERIOR. RESECURED EMERGENCY EXIT COVER LENS. OPS NML PER B757 AMM 33-51.
Part: WIRE — CHAFED (EMERGENCY LIGHT) · airframe 66,815 hrs · 25,634 cycles
WHITE SEAT 18D MOUNTED EMERGENCY LIGHT HAD A CHAFED WIRE. REMOVED & REPLACED THE LIGHT ASSY. OPS CHECKED GOOD.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 66,686 hrs · 25,587 cycles
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. REATTACHED EMERGENCY EXIT COVER AT DOOR 1R AS REQUIRED.
Part: LIGHT — SPARKS (LAVATORY) · airframe 66,512 hrs · 25,514 cycles
COCKPIT F/C LAV OCCUPIED LIGHT SPARKED WHEN TOUCHED. R&R COCKPIT F/C LAV OCCUPIED LIGHT ASSY. CKS OK IAW AMM 33-10.
Part: SPRING — DAMAGED (L1 DOOR) · airframe 65,645 hrs · 25,194 cycles
L1 DOOR DISARM PLACARD STICKS WHEN DISARM HANDLE MOVED TO DISARM. REMOVED AND REPLACED THE SPRING, OPS NORMAL.
Part: INDICATOR — OUT OF ADJUST (DOOR) · airframe 65,351 hrs · 25,075 cycles
DOOR ARMED KNUCKLE KNOCKER INOPERATIVE. ADJUSTED THE KNUCKLE KNOCKER ON L1 DOOR.
2017
Part: NONE — NONE (NONE) · airframe 67,416 hrs · 25,908 cycles
(AIRCRAFT 693, L/P 0301852) WHILE IN ATL FOR THE 2KU WIFI MODIFICATION AND DURING THE RADOME INSTALLATION PER GOGO DRAWING D18470-22207 REV. C (REFERENCE WORKCARD 2330-01349-01D) AT FR600 TO FR620 AND STR2R, MTC FOUND AN EXISTING LIGHTNING STRIKE REPAIR WITHIN 3? OF THE #4 LUG DOUBLER (P/N P35142-001). THE SKIN IS MADE FROM 0.080 THICK 2024-T3 CLAD SHEET CHEM-MILLED TO 0.040?AT THIS LOCATION. THIS ER/A AUTHORIZES THAT THE LIGHTNING STRIKE REPAIR IS ACCEPTABLE TO BE WITHIN THE PROXIMITY REQUIREMENTS OF THE 2KU LUG DOUBLER. ER/A 563403-14 IS AT REV A. THIS REVISION INCORPORATES THE COMPLETE DTE RESULTS.
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 64,293 hrs · 24,637 cycles
INTO ATL DUE TO CABIN ALTITUDE WARNING. CREW DESCENDED TO 10K FOR REMAINDER OF FLT. MASKS DID NOT DROP. PRESSURIZATION EVENTUALLY REGAINED THROUGH ALTERNATE CONTROLLER; EMERG RESCINDED. REPLACED NR 1 PRESS CONTROLLER PER AMM 21-31-02, REPLACED OUTFLOW VLV PER AMM 21-31-03. COMPLIED WITH SINGLE PACK CONFIDENCE CK PER AMM 21-51-00 AND EXCESSIVE CABIN PRESSURE LEAK CHECK PER AMM 05-51-24. PER MCC REQUEST REPLACED ALT WARNING SWITCH. ALL ITEMS TESTED PER AMM AND ODI CHECK LIST.
Part: PLACARD — UNSECURE (R3 DOOR) · airframe 63,373 hrs · 24,304 cycles
DOOR ARMED HANDLE INOPERATIVE. FOUND THE R3 DOOR HANDLE PLACARD CATCHING WHEN DOOR IS ARMED. APPLIED ADHESIVE TO THE PLACARD AND DOOR OPERATES CORRECTLY IAW AMM 52-02. OK FOR SERVICE.
Part: HANDLE — OUT OF POSITION (ENTRY DOOR) · airframe 62,835 hrs · 24,124 cycles
ON CLIMB OUT DOOR R FWD ENTRY DOOR HANDLE POPPED UP. WE GOT AN UPPER EICAS R FWD ENTRY DOOR PRESSURIZED NORMALLY. PERF QRH PROCEDURES. INSPECTED DOOR AND OPERATED DOOR PER AMM 52-11. ALL CKS OK.
Part: SENSOR — MALFUNCTIONED (BLEED AIR) · airframe 62,794 hrs · 24,107 cycles
AFTER SELECTING ENGINE ANTI-ICE, LEFT ENGINE BLEED OFF EICAS MESSAGE. WITH OFF LIGHT, FOLLOWED QRH AND IT REOCCURRED WITH FUMES THROUGHOUT CABIN. TURNED ENGINE ANTI-ICE OFF AND RESET WORKED. R & R 450 DEG TEMP SENSOR, AND THE FAN AIR TEMP SENSOR, ALSO THE FAN AIR MODULATION VALVE. THE HP VALVE CONTROLLER AND THE HP VALVE ALL IAW AMM 36-11, RAN ENG WITH PACKS AND ANTI-ICE ON. NO BLEED TRIP OR ODOR, NO CURRENT FAULTS OR MESSAGES. OK FOR SERVICE.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 62,776 hrs · 24,098 cycles
RIGHT HORIZONTAL STAB HAS A DENT AT APPROXIMATELY HSS 160 L/E AUX SPAR. ACCOMPLISHED A PERMANENT REPAIR IAW SRM.
Part: PIN — WRONG PART (L4 DOOR SNUBBER) · airframe 62,776 hrs · 24,098 cycles
L4 DOOR SNUBBER PIN EXTENSION IS NOT CORRECT. REMOVED AND REPLACED THE SNUBBER IAW AMM 52-11-10.
Part: FLOOR SUPPORT — CORRODED (BS 1500-1640) · airframe 62,776 hrs · 24,098 cycles
AFT CARGO BAY CENTER FLOOR SUPPORT AT RBL 3 IS CORRODED AT MULTIPLE AREAS, BS 1500 - 1640. REMOVED CORROSION IAW SRM 51-10-02 AND FOUND OUT OF LIMITS IAW SRM 53-00-53. REPAIRED THE FLOOR SUPPORT IAW SRM 53-00-53, REP 1, AND DWG 146N5390, REV C.
Part: SIDEWALL SUPPORT — CORRODED (BS 1375) · airframe 62,776 hrs · 24,098 cycles
AFT CARGO BAY SIDEWALL SUPPORT IS CORRODED BELOW TRANSITION PANEL AT BS 1375, RBL 28. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53. REMOVED THE SIDEWALL SUPPORT, FABRICATED AND INSTALLED A REPLACEMENT SIDEWALL SUPPORT IAW DWG 146N5427, REV A AND B, 146N5412, REV G AND SRM 51-40-02.
Part: FLOOR SUPPORT — CORRODED (BS 1445-1500) · airframe 62,776 hrs · 24,098 cycles
AFT CARGO BAY CENTER FLOOR SUPPORT AT LBL 8 IS CORRODED AT MULTIPLE AREAS, BS 1445 - 1500. REMOVED CORROSION AND FOUND OUT LIMITS, REPAIRED THE FLOOR SUPPORT IAW SRM 51-10-02, 53-00-53, 51-20-01, AND 51-40-02.
Part: PIN — WRONG PART (R1 DOOR SNUBBER) · airframe 62,776 hrs · 24,098 cycles
R1 DOOR SNUBBER PIN EXTENSION IS NOT CORRECT. REMOVED AND REPLACED THE DOOR SNUBBER IAW AMM 52-11-00.
Part: SEAT TRACK — GOUGED (FUSELAGE) · airframe 62,776 hrs · 24,098 cycles
MAIN CABIN SEAT TRACK LT O/B FROM STA 1073 TO 1180 HAS DEEP GOUGE AND FOUND OUT OF LIMITS AS PER TASK CARD 2021-2076. REMOVED MAIN CABIN SEAT TRACK STA 1073 - 1180 LT O/B IAW SRM 51-40-02. FABRICATED NEW SECTION OF SEAT TRACK AND SPLICE IAW SRM 53-00-52, REPAIR 3. INSTALLED NEW SEAT TRACK SECTION AND SPLICE IAW SRM 51-40-02 AND 53-00-52 REPAIR 3 OPTION 2.
Part: SKATE ANGLE — CORRODED (BS 1020-1040) · airframe 62,776 hrs · 24,098 cycles
MAIN LT SKATE ANGLE CORRODED BETWEEN BS 1020 - 1040. REMOVED CORROSION AND FOUND THE AREA TO BE OUT OF LIMITS IAW SRM 53-40-13. REMOVED DAMAGE SECTION OF THE SKATE ANGLE, FABRICATED A REPAIR STRAP AND REPAIR CHANNEL, HEAT TREATED TO T6 IAW AMS 2770N AND INSTALLED IAW SRM 53-00-13, REP 2.
Part: SKATE ANGLE — CORRODED (BS 730) · airframe 62,776 hrs · 24,098 cycles
MAIN CABIN BS 730, LBL 64 SKATE ANGLE CORRODED. REMOVED THE ANGLE BS 660 - 740, LBL 64, FOUND OUT OF LIMITS IAW SRM 53-40-13. INSTALLED A NEW SKATE ANGLE IAW DWG 143N8328, REV H.
2016
Part: PLATE — CRACKED (AFT BULKHEAD) · airframe 60,338 hrs · 23,205 cycles
ACRID ODOR OF BURNING ELECTRICAL, FOLLOWED BY WEATHER RADAR FAIL ON ND. DURING INSPECTION, FOUND D477 WEATHER RADAR CONNECTOR DAMAGED AT PRESSURE BULKHEAD, DISCONNECTED BOTH SIDES TO INSPECT THE CONNECTOR SUPPORT PLATE. FOUND PLATE CRACKED. INSTALLED TIME LIMITED REPAIR IAW ERA 548806-14 REV ORIG.
2015
Part: TARGET — DIRTY (GIRT BAR) · airframe 56,388 hrs · 21,547 cycles
R2 DOOR WILL NOT DISARM, SLIDE LIGHT DOES NOT EXTINGUISH. CLEANED DEBRIS FROM GIRT BAR TARGET.
Part: OIL SYSTEM — LEAKING (NR 1 ENGINE) · airframe 55,815 hrs · 21,343 cycles
ABORTED TAKEOFF, THE CREW REPORTED THAT THE COCKPIT AND CABIN FILLED WITH SMOKE WHILE ADVANCING THE THROTTLES. MAINTENANCE FOUND OIL STAINING ON THE HPC STAGES 6 AND 14 ON THE NR 1 ENGINE. R & R NR 1 ENGINE.
2014
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 54,207 hrs · 20,769 cycles
DURING AN A CHECK, FOUND RT DOOR EMERGENCY LIGHT INOPERATIVE. REPLACE POWER SUPPLY IAW AMM 33-53.
Part: SKIN — DAMAGED (BS 540) · airframe 53,693 hrs · 20,595 cycles
LIGHTNING STRIKE ON FASTENER BETWEEN S14-15L AT BS 540. C/W AND ERA 526733-14 REV ORIG.
Part: SKIN — DAMAGED (BS 540) · airframe 53,664 hrs · 20,585 cycles
LIGHTNING STRIKE ON FASTENER BETWEEN S14-15L AT BS 540. REMOVED FASTENER AND CLEANED UP DAMAGE AREA. INSPECTED AND NO CRACKS. REPAIRED IAW ERA 526733-14, REV.
2013
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 48,827 hrs · 18,894 cycles
EMERGENCY LIGHTS ROW 40 THRU 45 INOPERATIVE. REPLACED BATTERY PACK AT M9102 AFT GALLEY CEILING, AMM 33-51-07 P 201. OPS CHECKED GOOD.
2012
Part: SLIDE — LOW PRESSURE (L4 DOOR) · airframe 46,718 hrs · 18,109 cycles
MAINTENANCE DISCOVERED 4L DOOR SLIDE BOTTLE PSI IN RED. REMOVED AND REPLACED DOOR SLIDE PER B757 25-66.
2011
Part: FAN — FAILED (CABIN) · airframe 45,156 hrs · 17,474 cycles
AIRCRAFT EXECUTED DIVERSION AFTER FLIGHT ATTENDANTS REPORTED ELECTRICAL OVERHEAT FUMES IN CABIN. EMERGENCY PROCEDURES RESULTED IN DISSIPATION OF FUMES FROM CABIN FOR THE DURATION OF FLIGHT. MAINTENANCE INSPECTION REVEALED DAMAGED RIGHT RECIRCULATION AS THE CAUSE OF THE FUMES. R & R RT RECIRCULATION FAN AND MONITOR PER AMM 21-25.
Part: JACK — SHORTED (CABIN) · airframe 44,808 hrs · 17,337 cycles
PASSENGER REPORTED THAT SPARKS AND ELECTRICAL SMELL FROM HEADSET JACK AT SEAT 42F. CREW TURNED IFE POWER OFF AND FORWARD SYSTEM TO NEF. ON 11-05-11 ATL MAINTENANCE REPLACED VSBB. ITEM REMOVED FROM NEF.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO STR 27R CORRODED STA 1595-1600. FABRICATED CHANNEL PER DRAWING 146N3110 REV B. INSTALLED FABRICATED STRINGER SECTION CHANNEL ON STA 1589-1620 S27R IAW B757 SRM 53-00-03 STEP 10 FIG 201 PG 201 REPAIR 1. AT SAA/SAT DURING HMV ON N/R 185543 W/O 88596590001.
Part: FUSE — BLOWN (CABIN) · airframe 44,404 hrs · 17,187 cycles
R1 DOOR EMERGENCY EXIT SIGN AND O/H BIN LIGHTS AT SEATS 3 AND 6 INOP. T/S AND FOUND 2 EA FUSES BAD, REPLACED SAME CHECKS GOOD IAW AMM 33-51-07-962-071.
Part: CONNECTOR — DIRTY (CABIN) · airframe 44,404 hrs · 17,187 cycles
EMERGENCY LIGHT AT SEAT 19 FED INOP. REMOVED AND CLEANED CONNECTOR CHECKS GOOD IAW AMM 33-51-04-201.
Part: SKIN — DENTED (CARGO DOOR) · airframe 44,404 hrs · 17,187 cycles
FWD CARGO DOOR SKIN DENTED 18" AFT OF FWD EDGE 3" UP FROM BOTTOM. FABRICATED DOUBLER AND FILLER IAW SRM 757-52-30-01 REPAIR 4 PG 201. INSTALLED DOUBLER AND FILLER REPAIR AT FWD CARGO DOOR IAW SRM 757-52-30-01 REPAIR 4 PG 201. AT SAA/SATDURING HMV ON N/R 187827 W/O 88598850001.
Part: LINE — CHAFED (EVAC SLIDE) · airframe 44,404 hrs · 17,187 cycles
RT OVERWING ESCAPE SLIDE PNEUMATIC LINE, ATTACHED TO CARRIER, CHAFED AT CLAMP AND WORN THROUGH OUTER COVERING. REMOVED AND REPLACED RT OVERWING ESCAPE SLIDE PNEUMATIC LINE ATTACHED TO CARRIER, IN REF 757 AMM 25-65-03-404-025 PARA E STEP 1 TO 4. AT SAA/SAT DURING HMV ON N/R 191071 W/O 88601460001.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
FABRICATED J SECTION ANGLE, TREATED AND PRIMED IAW B757 SRM 53-00-07 REPAIR 5 PAGE 201 FIG 201. INSTALLED J SECTION ANGLE ON AFT CARGO FRAME AT STA 1480 ABOVE STR S-26L IAW B757 SRM 53-00-07 REPAIR 5 PG 201 FIG 201. AT SAA/SAT DURING HMV ON N/R 185588 W/O 88597350001.
Part: PAN — CORRODED (L1 DOOR) · airframe 44,404 hrs · 17,187 cycles
L-1 DOOR HANDLE BOX INNER BORE HAS PITTING CORROSION. INSTALLED NEW BEARING AND TRANSFERRED LATCHING CRANK ASSY AND BELLCRANK ASSY TO NEW HANDLE BOX PER BOEING CMM 52-11-07 PAGE 718 PAR G(2) TO (4). AT SAA/SAT DURING HMV ON N/R 185252 W/O 88601210001.
Part: PUSHROD — CORRODED (R1 DOOR) · airframe 44,404 hrs · 17,187 cycles
R1 LOWER GATE AFT PUSHROD HAS SURFACE CORROSION. REMOVED AND REPLACED R1 LOWER GAGE AFT PUSHROD IAW CMM 52-11-05 OPS CHECK ACCOMPLISHED ON JIC 78009 STEP 4. AT SAA/SAT DURING HMV ON N/R 1663204 W/O 88598320001.
Part: CRANK ASSY — CORRODED (R2 DOOR) · airframe 44,404 hrs · 17,187 cycles
R2 DOOR FWD UPPER LATCH CRANK CORRODED AND PITTED. REMOVED AND REPLACED R2 DOOR FWD UPPER LATCH CRANK IAW B757 CMM 52-11-15. ADJUSTMENT ACCOMPLISHED ON OPN NR 78012 (88587140001. AT SAA/SAT DURING HMV ON (N/R 185262) W/O 8850134000.
Part: FRAME — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO FRAME DENTED STA 1420 ABOVE STR 26L 2 PLACES FABRICATED J SECTION REPAIR PER B757 SRM 53-00-07, REPAIR 5 PAGE 201-212 FIGURE 201 TABLE 1. INSTALLED J SECTION REPAIR AT AFT CARGO FRAME STA 1420 ABOVE STR 26L REF B757 SRM 53-00-07 PAGE 201 REPAIR 5.
Part: FRAME — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO FRAME DENTED STA 1520 ABOVE STR 26L FABRICATED J SECTION PER SRM 53-00-07 REPAIR 5 FIGURE 201 TABLE 1 PAGE 201-212. INSTALLED REPAIR J SECTION ON STA 1520 S26L IAW B 757-SRM 53-00-07 REPAIR 5 STEP 10 AND 11 FIG 201 PG 201. AT SAA/SAT DURING HMV ON (N/R 185608) W/O 88597260001.
Part: SUPPORT — CORRODED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
MAIN CABIN FLOOR BL 0 CHORD CORROSION STA 345 TO 365. LOCATED AND DRILLED HOLE ON REPLACEMENT CHORD (SUPPORT) P/N 141N5191-1 B/N 0002095260 PER REF B757SRM 51-40-05 PG 1-10. INSTALLED CHORD (SUPPORT) AT MAIN CABIN FLOOR BL 0 FROM 324 TO STA 440 PER REF B757 SRM 51-40-02 PG 7 PARA 7D AT SAA/SAT DURING HMV ON (N/R 187837) W/O 88599210001.
Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 44,404 hrs · 17,187 cycles
SLAT 2 COVE SKIN PANEL IS CRACKED INBOARD SIDE OF INBOARD MAIN TRACK. FABRICATED FILLER DOUBLER TO SKIN COVE IAW ER/A 366767-14 MA REV A STEP 4 AND 6. TREATED AND PRIMED IAW STEPS 8 AND 9 INSTALLED PER ER/A AT SAA/SAT DURING HMV ON (N/R 191024) W/O 88595420001.
Part: FRAME — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO FRAME DENTED STA 1400 ABOVE STR 26L. FABRICATED J SECTION REPAIR IAW B757 SRM 53-00-07 REPAIR 5 STEP 4 FIG 201 PG 201 DETAIL I. INSTALLED REPAIR J SECTION ON STA 1400 S 26L. AFT CARGO COMPT IAW B757 SRM 53-00-07 REPAIR 5 DETAIL I FIG 201 PG 201 STEP 10 & 11 AT SAA/SAT DURING HMV ON (N/R 185513) W/O 88597390001.
Part: STRUCTURE — DAMAGED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
DENT ON FUSELAGE WITH 3 GOUGES INSIDE STA 1703 ABOVE STR 18L. FABRICATED REPAIR DOUBLER REF 757 SRM 53-00-01 REPAIR 3 PAGE 201 FIG 201 STEP 6. INSTALLED REPAIR DOUBLER REF 757 SRM 53-00-01 REPAIR 3 PAGE 201 FIG 201. AT SAA/SAT DURING HMV ON (N/R 203367) W/O 88592960001.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
MAIN CABIN FLOORBEAM CORRODED STA 1640 RBL 15 TO LBL 10. INSTALLED FABBED REPLACED CHORD IAW B757 SRM 53-00-01 REP 3 STEP 9, 10 FIG 201 PG 201.
Part: STRINGER — CORRODED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO STR CORRODED STA 1430-1460 AT 29R. PROCURED REPL STRINGER INSTALLED IAW 51-40-05 FIG 3 PG 4.
Part: FRAME — GOUGED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
AFT CARGO FRAME GOUGED ON UPPER RADIUS STA 1520 ABOVE STR 23-26R / FORMED NEW REPAIR SECTION J PER SRM 53-00-07 REPAIR 5 PG 201-212. THIS IS A CATEGORY B WITH THRESHOLD REPETITIVE INSP TO START AT 5010.0 AIRFRAME FLIGHT CYCLES. METHOD HIGH FREQUENCY EDDY CURRENT INTERVAL EVERY 12000 FLT CYCLES NDT PART 6 51-00-01 AND DETAILED INSP EVERY 12000 FLT CYCLES AND PER SRM 53-00-07 FIG 201 TABLE 11 REPAIR 5 ZONE 1 PG 210. A/C HAS 17038.0 FLT CYCLES.
Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 44,404 hrs · 17,187 cycles
SLAT 1 COVE PANEL CRACK I/B SIDE OF I/B MAIN TRACK. INSTALLED REPAIR PER ERA 366767 - 14MA REV A.
Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 44,404 hrs · 17,187 cycles
THREE CRACKS ON NR 9 SLAT COVE PANEL AT I/B TRACK. REPAIRED PER ERA 366767-14MA REV A.
Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 44,404 hrs · 17,187 cycles
SLAT 2 COVE SKIN PANEL CRACKED O/B SIDE OF MAIN TRACK. INSTALLED REPAIR PER ERA 366767-14MA REV A.
Part: SKIN PANEL — CRACKED (LE SLAT) · airframe 44,404 hrs · 17,187 cycles
SLAT 2 COVE SKIN PANEL CRACKED O/B OF I/B MAIN TRACK. INSTALLED DOUBLER REPAIR PER ERA 366767-14MA REV A.
Part: SKIN — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
DENT ON FUSE WITH 3 GOUGES STA 1703 ABOVE S 18L. PERM CAT B REPAIR PER SRM 53-00-01 REPAIR 3 PG 201 FIG 201.
Part: STRUCTURE — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
FSTA 640 BETWEEN S-6L DENT ON FUSELAGE. COMPLIED WITH ERA 495296-14 REV ORIGINAL DURING HMV AT ST AEROSPACE SAN ANTONIO.
Part: SKIN — DENTED (FUSELAGE) · airframe 44,404 hrs · 17,187 cycles
FUSE SKIN HAS 6 EA DENTS STA 600-640 S 15-17L AND 4 EA GOUGES ON S 16L STA 625-628. INSTALLED PERM CAT B REPAIR PER SRM 53-00-01 REP 3 FIG 201 PG 201.
2008
Part: UNKNOWN — SMOKE (CABIN) · airframe 32,832 hrs · 13,272 cycles
AFTER STARTING RT ENGINE AND PUTTING ON PACKS, COCKPIT FILLED WITH SMOKE. RAN LT AND RT PACKS OFF APU AIR. NO SMOKE OR ODOR. STARTED ENG OFF APU AIR CROSSBLEED STARTED LT ENG. RAN PACKS FULL H TO FULL COLD 3 TIMES. NO SMOKE OR ODOR. RAN ENG TO TAKEOFF PWR FOR 3 MIN. NO SMOKE OR ODOR. OK FOR SVC.
Part: BOLT — LOOSE (APU DOOR) · airframe 32,210 hrs · 13,080 cycles
WHILE WORKING ELEVATOR ASSY MESSAGE, FOUND APU DOOR HINGE BOLT LAYING ON TOP OF HORIZONTAL STABILIZER. REINSTALLED BOLT IN DOOR HINGE.
2005
Part: STRINGER CLIP — CORRODED (BS 1620)
FOUND CORROSION ON CLIP AT STR-30 BL 0 BS 1620. REMOVED STRINGER CLIP. FABRICATED AND INSTALLED NEW REPAIR STRINGER CLIP 6" BY 1" FROM 7075-T6 .050 IAW B757 SRM 51-40-02, 51-70-11, 53-00-03, 51-20-02 AND 51-40-02.
Part: SKIN — DENTED (FUSELAGE)
FUSELAGE HAS 2 ADJACENT SHARP CREASED DENTS LOCATED AFT OF THE AFT CARGO DOOR CUT OUT AT OR BETWEEN BS 1480 TO 1500 AND BETWEEN S-23R AND S-24R. CUT OUT DENTS. FABRICATED AND INSTALLED REPAIRS 7-1/2" BY 7-1/2" AND 1-1/2" BY 2" FROM 2024-T3 .050 IAW B757 SRM 53-00-01, FIG 101 DETAIL III, 53-00-01 FIG 206 AND INSTALLED ID TAG PER DELTA B757 STANDARD 900-S-0 NR 04.
Part: CHILLER — FUMES (GALLEY) · airframe 22,562 hrs · 9,886 cycles
FUMES LIKE SULPHUR COMING FROM FWD GALLEY FOUND. F/C FREEZER AT FAULT REPLACED.
2003
Part: PLACARD — WORN (CABIN) · airframe 14,568 hrs · 6,812 cycles
THE 3 RT RAFT SURVIVAL KIT HAS DIRECTIONS PLACARDS THAT IS HARD TO READ. REMOVED AND REPLACED 3 RIGHT SURVIVAL KIT.
2001
Part: WIRE — BROKEN (CABIN) · airframe 10,305 hrs · 4,776 cycles
EMERGENCY LIGHT 2CD INOPERATIVE. REPAIRED BROKEN WIRE.
1999
Part: TRIM — MALFUNCTIONED (HORIZ STAB)
DISCONTINUED TAKEOFF AT 90K. RED STABILIZER WARNING MESSAGE APPEARED ON T/O. AT PWR APPLICATION TRIM WAS 4.1 AT 90K TRIM WAS DRIVING UNCOMMANDED THROUGH 6.5 NOSE UP TO A FINAL OF 8.0 UNITS. FOUND RT SAM MODULE FAULTED, REPLACED SAME.
1998
Part: OVEN — FUMES (GALLEY)
FWD CABIN ATTENDENTS REPORTED FUMES. REPLACED F/C OVEN.