N585NW
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 |
|---|---|---|---|
| NORTHWEST AIRLINES INC | Operator | on 2008-12-28 | Operator named in NTSB report |
Accident & incident history
Operated by NORTHWEST AIRLINES INC (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.
206 reports on file, 2004-09-22 – 2026-05-09.
Part: FRAME — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,887 hrs · 26,160 cycles
CORROSION ON FRAME STA 1460 BTW STGR 28L TO 28R BILGE AREA AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. FRAME STA 1460 BTW STGR 28L TO 28R BILGE AREA AT AFT CARGO COMPARTMENT WAS REPAIRED PER ERA 634167-14 REV ORIGINAL SECTION I: REPAIR INSTRUCTIONS AND PRI 634167-14 REV 0 TO REV 5. (1585439) AIRCRAFT WAS GROUNDED
Part: TRIGGER — CRACKED (ZONE 800 SLIDE) · airframe 78,886 hrs · 26,159 cycles
CRACK ON RELEASE TRIGGER OF RT OVER WING SLIDE AT FUSELAGE. RELEASE TRIGGER ON RH OVER WING SLIDE WAS REPLACED PER CMM 25-65-19. (1582619) AIRCRAFT WAS GROUNDED
Part: INTERCOSTAL — OUT OF LIMITS (ZONE 100) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
IN REFERENCE NRC 00185: CORROSION OUT OF LIMITS, THICKNESS MEASURE WAS ACOMPLISHED ON INTERCOSTALS BTW STA 1500 TO STA 1521 AND S30-S29L PER B757-300 SRM 53-00-04-1A PROCEDURE 1, NOTE F, DETAIL II. COROSION LEVEL 2. INTERCOSTALS BTW STA 1500 TO STA 1521 AND S30-S29L WAS REPLACED PER B757-300 SRM 51- 40-02-0G PAR 7, D.(1580815) AIRCRAFT WAS GROUNDED
Part: FLOOR SUPPORT — OUT OF LIMITS (ZONE 200) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
CORROSION OUT OF LIMITS, THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FLOOR STRINGERS UPPER/LWR (ATTACH POINTS) 2.9, 7.55 & 10.45 LBL/RBL AND BTW BS 1508 TO BS 1511 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT PER SRM 53-00 -53-1A PROCEDURE 1, ALLOWABLE DAMAGE 1 FIGURE 101, DETAIL IX. AND B757 NDT MANUAL PART 51-00-10 PAR. 4. A. CORROSION LEVEL 2. FLOOR STRINGERS UPPER/ LWR (ATTACH POINTS) 2.9, 7.55 & 10.45 LBL/RBL AND BTW BS 1508 TO BS 1511 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT WERE REPAIRED PER B757-300 SRM 53-00-53-2R PROCEDURE 1 REPAIR 1 (1580827) AIRCRAFT WAS GROUNDED
Part: INTERCOSTAL — OUT OF LIMITS (ZONE 100) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
AFTER CORROSION REMOVAL, MEASUREMENT THICKNESS WAS ACOMPLISHED ON INTERCOSTAL BTW STA 1400 TO 1420 AND STGR 29R BILGE AREA AFT CARGO COMPARTEMENT, THEREFORE IT IS OUT OF LIMITS PER B757-300 SRM 53-00-04-1A PROCEDURE 1, NOTE F, DETAIL II. CORROSION LEVEL 2. INTERCOSTAL BTW STA 1400 TO 1420 AND STGR 29R BILGE AREA AFT CARGO COMPARTEMENT WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR 7. (1580326) AIRCRAFT WAS GROUNDED
Part: RESERVOIR — MISINSTALLED (ZONE 800) · airframe 78,886 hrs · 26,159 cycles
IN REF TO: AMDS 5211-3001-1R. EMERGENCY POWER RESERVOIR DISCONECT (WRONG INSTALLED). EMERGENCY POWER RESERVOIR WAS VERIFIED AND INSTALLED CORRECTLY PER. B757-300 AMM 52-11-30-404-013. (1580438) AIRCRAFT WAS GROUNDED
Part: FRAME — OUT OF LIMITS (ZONE 100) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
AFTER CORROSION REMOVAL (UT) MEASUREMENT THICKNESS WAS ACOMPLISHED ON FRAME CLIP ON BS 1500 BTW S-27R AND S-26R AFT CARGO COMPARTMENT, IS OUT OF LIMITS PER B757-300 SRM 53-00-53-1A PROCEDERE 1. CORRECTIVE ACTION: SUMMARY OF NRC 00559. FRAME CLIP ON BS 1500 BTW S-27R AND S-26R AFT CARGO COMPARTMENT WAS REPLACED PER B757-300 SRM 51-40-02-0G PAR 4. (1579000) AIRCRAFT WAS GROUNDED
Part: FRAME — NOT REPORTED (ZONE 100) · airframe 78,886 hrs · 26,159 cycles
DTE, ERA 633921-14, MONITOR INSPECTION LOG REPAIR TO FUSELAGE FRAME STATION 540 BETWEEN STRINGERS 22L-26L. REF ERA 633921-14. (1579287) AIRCRAFT WAS GROUNDED
Part: HINGE ARM — WORN (ZONE 800) · airframe 78,886 hrs · 26,159 cycles
IN REFRRENCE AMDS 5211-6001-4R: AFTER REMOVAL LOWER HINGE ARM, WEAR WAS FOUND ON GUIDE PIN OF R4 DOOR. 4R DOOR LOWER HINGE ARM WAS REPAIRED PER ER/A 634114-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR AND PER PRI 634114-14 REV. 2. (1577149) AIRCRAFT WAS GROUNDED
Part: FRAME — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
IN REFRRENCE AMDS 5211-6001-4R: AFTER REMOVAL OF SLIDE INDICATOR POSITION, CORROSION WAS FOUND ON FRAME WEB, R4 DOOR. CORROSION LEVEL 2. FRAME WEB, R4 DOOR WAS REPLACED IAW SRM 51-40-02-0G PAR. 4.B, PAR. 5.B, PAR. 6 .B AND PAR. 7.D. (1574721) AIRCRAFT WAS GROUNDED
Part: PIN — WORN (ZONE 800 HINGE) · airframe 78,886 hrs · 26,159 cycles
AFTER REMOVAL LOWER HINGE ARM, WEAR WAS FOUND ON GUIDE PIN OF 2R DOOR. 2R DOOR LOWER HINGE ARM WAS REPAIRED PER ER/A 634074-14 REV. ORIGINAL SECTION I: PERMANENT REPAIR, PRI 634074-14 REV. 1. (1573261) AIRCRAFT WAS GROUNDED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
CORROSION ON INTERCOSTAL BTW BS 1580 TO 1600, S29R OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2. INTERCOSTAL BTW BS 1580 - 1600, S29R OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-40-02-0G PAR 7.D. (1572695) AIRCRAFT WAS GROUNDED.
Part: RESERVOIR — LOW PRESSURE (ZONE 800) · airframe 78,886 hrs · 26,159 cycles
SHIP 5805 IN REFERENCE TO AMDS 5211-2001: LOW PRESSURE ON R1 DOOR EMERGENCY POWER RESERVOIRS. CORRECTIVE ACTION: SUMMARY OF NRC 00512: 1R DOOR RESERVOIR WAS REPLACED PER B757-300 AMM 52-11-30. (1565961) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,886 hrs · 26,159 cycles
CORROSION ON RH OUTBD/INBD PASSENGER SEAT TRACK BTW STA =365 TO STA= 380. CORROSION LEVEL 2. RH OUTBD/INBD PASSENGER SEAT TRACK BTW STA =365 TO STA= 380 WERE REPLACED PER B757-300 SRM 51-40-02-0G PAR 7. (1557725) AIRCRAFT IS GROUNDED
Part: LEVER — STUCK (ZONE 800) · airframe 78,752 hrs · 26,110 cycles
SHIP 5805 4R DOOR ARM LEVER STUCK. COULD NOT BE ARMED. CORRECTIVE ACTION: FOUND BEARING ON HORIZONTAL SHAFT STIFF. R/R AFT TORQUE TUBE BEARING PER B757 CMM 52-11. INSTALLED ESCAPE SLIDE PER AMM 25-66. C/W RII. PERFORMED GIRT BAR CLEAN/LUBE PER W/C 2566-2001-06. RR DOOR ARMS AS REQUIRED PER AMM 52-11. (8334188)
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 78,752 hrs · 26,110 cycles
SHIP 5805 R2 DOOR EMERGENCY EXIT LIGHT OVERDOOR INOP. CORRECTIVE ACTION: R & R BATTERY AT M11612 AS PER B757 AMM 33-51. OPS CHECK GOOD. (8334181)
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 78,752 hrs · 26,110 cycles
SHIP 5805 EMER LIGHTS ABOVE AISLE IN FIRST CLASS AT 2L DOOR REMAIN IN ARMED POSITION. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY LIGHTS NOW GND CK OK PER B757 AMM 33-51.(8334184)
Earlier reports · 2004–2025 · 189 reports
2025
Part: OIL SYSTEM — LOW PRESSURE (RT ENGINE) · airframe 78,126 hrs · 25,868 cycles
ATB/IFSD/DE - AIRCRAFT RETURNED TO DTW DUE TO RIGHT ENGINE IFSD DUE TO ZERO OIL PRESSURE AND OIL QUANTITY. RIGHT ENGINE OPERATED ABOVE IDLE POWER WITH ZERO OIL PRESSURE AND OIL QUANTITY, REMOVED AND REPLACED ENGINE.
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 77,924 hrs · 25,791 cycles
L1 DOOR OUTSIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED M730 POWER SUPPLY PER B757 AMM 33-51. OPS NORMAL. SEE LOG PAGE 7646084. (7646086)
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 77,924 hrs · 25,791 cycles
L2 DOOR OUTSIDE EMERGENCY LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED M730 POWER SUPPLY PER B757 AMM 33-51 OPS NORMAL. SEE LOG PAGE 7646084. (7646087)
Part: WIRE — DAMAGED (ZONE 200) · airframe 77,924 hrs · 25,791 cycles
FLOOR PROXIMITY LIGHTS ARE INOP SEAT ROWA 4,5 AND MID GALLEY 2(2 WHITE) AND LAV "V" RED. INSPECTED MOLEX CONNECTOR ON SEAT 4. 5 AND 6- ALL ARE SECURE. INSPECTED SEAT TO SEAT WIRING AND FOUND ONE RED WIRE IN FRONT OF SEAT 5CD DAMAGED. REFERENCE B757 WD 33- 51-21. PAGE 3 SHOT 2 FOR WIRE RUN. REPAIRED DAMAGED WIRE SEAT 5CD PER B757 SWPM 20-10-14. REMOVED AND REPLACED POWER SUPPLY M730 IAW B757 AMM 33-51. ALL LIGHTS FUNCTION AS NORMAL. (7646084)
Part: LIGHT — DAMAGED (ZONE 200) · airframe 77,621 hrs · 25,693 cycles
SHIP 5805 EMERGENCY SEAT MOUNTED LIGHTING DAMAGED, INOP, LOCATIONS:2C. SECURED SEAT 2C PATH LIGHT OPS OK. (1251697)
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 77,037 hrs · 25,522 cycles
DURING SVC CHECK FOUND RH AFT EMERGENCY DOOR EXIT SIGN AND AISLE LIGHTS FOR ROWS 39 + 40 DEF OUT. R/R BATTERY PACK M11082 PER B757 AMM 33-51. OPS CHECK GOOD. (7321335)
Part: PUSHROD — OUT OF ADJUST (GIRT BAR) · airframe 77,000 hrs · 25,511 cycles
SLIDE INDICATOR LIGHT INOP OR DAMAGED. FOUND GIRT NOT ENGAGED WITH SLIDE ARMED. FOUND FWD GIRT BAR PUSH ROD OUT OF ADJUSTMENT. ADJUSTTED L4 DOOR FWD GIRT BAR PUSH ROD IAW B757 AMM 52-11. RII CW. (1143301)
Part: GIRT BAR — DIRTY (ZONE 800) · airframe 76,987 hrs · 25,508 cycles
ON TAKEOFF ROLL ABOVE DOOR 4L ( CAPTAINS SIDE). ALL OTHER FOOR ARMED INDICATORS FUNCTIONAL. LIFTING RUBBER SEAL CONFIRMED GIRT BAR ENGAGED. SLUDE WARNING LIGHT ILLUMINATED WHEN DOOR WAS ARMED FIR DEPARTURE. / INTERIOR. CLEANED AROUND GIRT BAR AREA, SECURED STRAP FOR BUSTLE OPS CHKD DOOR ARMING LEVER SEVERAL TIMES LEVER MOVES NML ALL ARMED INDICATIONS GOOD, SLIDE WARNING LT NML, REF B757 AMM 52-11.
Part: CAP — INOPERATIVE (ZONE 200) · airframe 76,932 hrs · 25,493 cycles
4L SLIDE LIGHT INOP. FOUND FAULTY CAP. REMOVED AND REPLACED CAP PER AMM 33-51. OPS CHK OK.
Part: GIRT BAR — OUT OF ADJUST (ZONE 800) · airframe 76,880 hrs · 25,475 cycles
L4 GIRT BAR DOES NOT ENGAGE DURING VISUAL CHECK. ADJUSTED GIRT BAR FEET IAW AMM 25-66.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 76,904 hrs · 25,485 cycles
SHIP 5805 4L DOOR SLIDE LIGHT WENT OUT IN AIR. CORRECTIVE ACTION: RELAMPED, REMOVED EXCESSIVE DEBRIS FROM GIRT BAR AREA OF DOOR. OPS NOW OK. REF B757-300 AMM 25-66. (7296864)
Part: CHARGER — INOPERATIVE (ZONE 200) · airframe 76,756 hrs · 25,437 cycles
SHIP 5805 EMX LIGHTS OUT SEAT 456. CORRECTIVE ACTION: REMOVED AND REPLACED CHARGER PER 757 MM 33-51 OPS CK GOOD. (7296807)
Part: GIRT BAR — DISENGAGED (ZONE 800) · airframe 76,596 hrs · 25,389 cycles
SHIP 5805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:611. CORRECTIVE ACTION: FOUND DOOR 4 LEFT GIRT BAR SLIDER NOT ENGAGING FLOOR FITTING. ADJUSTED GIRT BAR SLIDER PER B757 AMM 25-66. OPS CHK NML. (1041841)
Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 76,462 hrs · 25,341 cycles
SHIP 5805 LT AFT DOOR SLIDE ARM LIGHT INOP. CORRECTIVE ACTION: FOUND GIRT BAR END BAR NOT SECURED IN CAM. SECURED END OPS CKS GOOD. (7251896)
Part: SWITCH — INOPERATIVE (ZONE 800 SLIDE) · airframe 76,452 hrs · 25,338 cycles
SHIP 5805 DOOR 4R SLIDE ARMED LIGHT NOT ON WITH DOOR ARMED LEVER IN ARMED POSITION. CORRECTIVE ACTION: FOUND 4R SLIDE LIGHT SWITCH INOP. R&R SWITCH AS PER B757 WDM 25- 66-11. OPS CHK OK. (7251886)
Part: GIRT BAR — FOD (ZONE 800) · airframe 76,323 hrs · 25,290 cycles
SHIP 5805 AT DEPARTURE DOOR 4L SLIDE LIGHT WOULDN'T NOT ARM AND FA REPORTED THE DOOR FELT STRANGE. CORRECTIVE ACTION: FOUND DEBRIS BLOCKING GIRT BAR. CLEARED DEBRIS. DOOR ARM/DISARM AND LIGHT OPS NML. (7251820)
Part: SLIDER — FAULTED (ZONE 800) · airframe 76,190 hrs · 25,233 cycles
SHIP 5805 4L GIRT BAR DISLODGED DURING CATERING. CORRECTIVE ACTION: INSTALLED GIRT BAR FWD SLIDER FLOOR FITTING PER B757 AMM 25-66. GIRT BAR ENGAGES & DISENGAGES PER B757 AMM 52-11. (6544040)
Part: SLIDER — FAULTED (ZONE 800) · airframe 76,190 hrs · 25,233 cycles
SHIP 5805 DOOR 4L ARM LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: AFTER REINSTALLING FWD GIRT BAR SLIDER. ESCAPE SLIDE ARM LIGHT OP'S NORMAL REF: B757 AMM 25-66 & 52-11. OK FOR SVC. PLACARD REMOVED. (6544036)
Part: GIRT BAR — NOT SEATED (ZONE 800) · airframe 76,063 hrs · 25,181 cycles
SHIP 5805 DOOR 4L ARMED LIGHT INOP. CORRECTIVE ACTION: DURING GVI OF L4 SLIDE AND DOOR OPERATION, FOUND GIRT BAR FITTING NOT FULLY SEATED. RE-SEATED FITTING AND SLIDE LIGHT NOW TURNS ON. (7180161)
Part: BATTERY — NO TEST (ZONE 200) · airframe 76,063 hrs · 25,181 cycles
SHIP 5805 DURING SERVICE CK FOUND EMG LIGHTS ROW 4, 5, 6 AND GALLEY LIGHTS INOP. CORRECTIVE ACTION: R/R EMG LIGHTS BATTERY PER B757 AMM 33-51. (7180162)
Part: FAN — ODOR (ZONE 100) · airframe 75,980 hrs · 25,149 cycles
SHIP 5805 FAINT BURNING SMELL EQPT OVHT EICAS MESSAGE AND LEFT RECIRC FAN EICAS MESSAGE ASSOCIATED WITH INOP LIGHT ON SWITCH AFTER LANDING DURING TAXI IN. CORRECTIVE ACTION: R/R LT RECIRC FAN IAW B757 AMM 21-25. OPS TEST GOOD. (7180118)
Part: LIGHT — DAMAGED (ZONE 200) · airframe 75,632 hrs · 25,009 cycles
SHIP 5805 EMERGENCY FLOOR LIGHTING ON SEAT 14E DAMAGED. CORRECTIVE ACTION: NSTALLED LIGHT, CKS OK. (0828370)
Part: LENS — MISSING (ZONE 200) · airframe 75,581 hrs · 24,989 cycles
SHIP 5805 LT OVER WING EXIT LENS COVER MISSING. CORRECTIVE ACTION: INSTALLED 'EXIT' SIGN LENS AT SEAT ROW 27ABC. REF B757 AMM 33-51. (6842320)
Part: GIRT BAR — FOD (ZONE 800) · airframe 75,417 hrs · 24,919 cycles
SHIP 5805 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ 1R AND 4L INOP. FOUND GIRT BAR DEBRIS BLOCKING ENGAGEMENT. REMOVED DEBRIS. OK FOR SVC. ARMED & DISARMED DOOR LIKE NORMAL. WORK REF B757 AMM 25 -66. LIGHT OPERATES OK. MEL REMOVED. (0781531)
Part: COVER — DETACHED (ZONE 200) · airframe 75,198 hrs · 24,822 cycles
SHIP 5805 AFT LAV EMERGENCY LIGHT SIGN COVER HAS FALLEN OFF AND NEEDS TO BE RECONNECTED. CORRECTIVE ACTION: INSTALLED EMERGENCY LIGHT COVER. OK FOR SVC. (6843422)
2024
Part: GIRT BAR — UNSECURE (ZONE 800) · airframe 75,159 hrs · 24,806 cycles
SHIP 5805 CATERING REPORTS L4 DOOR GIRT BAR HANGING. CORRECTIVE ACTION: DOOR SLIDE & ASSIST BOTTLES PINED. RE ATTATCHED GIRT BAR TO ARMING PAW. DOOR ARMING OPERATES NORMALLY. DOOR SLIDE & ASSIST BOTTLE PINS REMOVED. PER B757 AMM 25-66. (6553478)
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 74,981 hrs · 24,735 cycles
SHIP 5805 ROW 14 SEAT EMER LIGHT WHITE INOP. CORRECTIVE ACTION: R/R EMERGENCY PATH LIGHT AT ROW 14 REF B757 AMM 33-51. OPS CHECK NORMAL. OK FOR SERVICE. PLACARD REMOVED. (4000968)
Part: GIRT BAR — DETACHED (ZONE 800) · airframe 74,970 hrs · 24,731 cycles
SHIP 5805 4L DOOR ARMED LIGHT NOT COMING ON WHEN DOOR IS ARMED. CORRECTIVE ACTION: FOUND GIRT BAR DETACHED FROM FWD END OF SLIDE AND CATCHIN ON DOOR RAME. PINED SLIDE. REATTACHED GIRT BAR TO SLIDE REF 757 AMM 25-66. REMOVED SLIDE DEACTIVATION PIN AND STOWED. BUSTLE REINSTALLED. ALL RII C/W.
Part: SLIDER — ABNORMAL (4L DOOR/GIRT BAR) · airframe 74,904 hrs · 24,707 cycles
SHIP 5805 FLIGHT ATTENDANT SUSPECTS DAMAGE TO 4L DOOR/GIRT BAR. CORRECTIVE ACTION: FOUND FWD GIRT BAR LIDDER OUT OF POSITION. REPOSITIONED FWD SLIDER REF B757 AMM 25-66. 4L GIRT BAR AND SLIDE INDICATION OPS CKS GOOD. (4000927)
Part: LIGHT — INOPERATIVE (4L) · airframe 74,912 hrs · 24,711 cycles
SHIP 5805 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S 4L INOP. CORRECTIVE ACTION: PERFORMED GIRT BAR PROX SENSOR ADJUSTMENT PER B757 AMM 25-66-11. OPS CHECKS GOOD. (0682085)
Part: GIRT BAR — DISENGAGED (ZONE 800) · airframe 74,797 hrs · 24,665 cycles
SHIP 5805 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT AT 4L INOP. CORRECTIVE ACTION: FOUND FWD GIRT BAR FITTING NOT ENGAGED INTO BAR. REINSTALLED GIRT BAR FITTING IN GIRT BAR MECH. PER B575 AMM 25-66. CKS GOOD.(0664416)
Part: SLIDER — OUT OF POSITION (GIRT BAR) · airframe 74,752 hrs · 24,648 cycles
SHIP 5805 4L DOOR SLIDE WILL NOT ARM. CORRECTIVE ACTION: FWD SLIDER OUT OF PLACE ON GIRT BAR. REPOSITION SLIDER. REF B757 AMM 52-11. OPS CKS GOOD. (6627074)
Part: GIRT BAR — FOD (ZONE 200) · airframe 74,722 hrs · 24,636 cycles
SHIP 5805 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT/S/ 4L INOP. CORRECTIVE ACTION: REMOVED DEBRIS AND BOTTLE CAP AT DOOR 4L FWD PROX SENSOR AREA. ARMED AND DISARMED DOOR SEVERAL TIMES, GIRT BAR ENGAGES NORMALLY DOOR 4L SLIDE LIGHT OPS CKS NORMAL PER B757 AMM 25-66. (0650820)
Part: INDICATOR — INOPERATIVE (ZONE 800) · airframe 74,618 hrs · 24,593 cycles
SHIP 5805 4L DOOR LIGHT UNABLE TO INDICATE IF DOOR IS ARMED. CORRECTIVE ACTION: REMOVED DEBRIS FROM GIRT BAR FWD PROX SWITCH AREA REF B757 AMM 25-66 , CKS GOOD. (6686278)
Part: METERING VALVE — FIRE (ZONE 700) · airframe 74,497 hrs · 24,552 cycles
SHIP 5805 AFTER RETURN TO GATE FROM MAINT TAXIS HIGH POWER RUN NOTICED LT MLG #2 BRAKE FIRE. CORRECTIVE ACTION: R/R BRAKE METERING VALVE PER B757 AMM 32-41.NO LEAKS NOTED. HEAT DAMAGE INSP. ACCOMPLISHED ON LOG #S 6686228, 6686232, 6686234,6686236. (6686226)
Part: INDICATOR — FOD (ZONE 800) · airframe 74,459 hrs · 24,542 cycles
SHIP 5805 L-4 DOOR ARMED LT INOP. CORRECTIVE ACTION: REMOVED DEBRIES FROM LOT, OPS CHECK NORMAL, DOOR ARM/ DISARM NORMAL. (6686216)
Part: LAMP — INOPERATIVE (INDICATOR LIGHT) · airframe 73,597 hrs · 24,263 cycles
4L SLIDE LIGHT INOP. RELAMPED, FOUND FWD MOUNT OF GIRT BAR AT 4L MISALIGNED. REINSTALLED GIRT BAR PER B757 AMM 25-66. OPS CK GOOD. LIGHT OPERATES NORMALLY. (5895922)
Part: GUIDE ARM — OUT OF ADJUST (RT AFT DOOR) · airframe 73,477 hrs · 24,227 cycles
SHIP 5805 RT AFT ENT DOOR HANDLE POPPED OUT OF POSITION 3 TIMES CAUSING THE RT AFT ENTRY DOOR EICAS MESSAGE TO ILLUMINATE. AS RESR AND THE MESSAGE WENT AWAY. CORRECTIVE ACTION: INSP.RT ASFT ENTRY DOOR AND FOUND OUT OF LIMITS REF.B757 AMM 52- 16 ADJUSTED GUIDE ARM, LATCH CAMS, AND DOOR STOP PINS TO BRING R4 DOOR WITHIN LIMITS REF. B757 AMM 52-11. PRESSURIZED OK FOR SVC PER B757 AMM 52-11-00. (5925284)
Part: HANDLE — OUT OF POSITION (RT AFT DOOR) · airframe 73,477 hrs · 24,227 cycles
SHIP 5805 "R AFT ENT DOOR" EICAS MESSAGE DISPLAYED ON EICAS SCREEN DURING CLIMBOUT FROM SEA CONTINUED OPS PER QRH 1.9 PRESSURIZATION NORMAL. DOOR LEVER HAD MOVED UP ON TAKEOFF. DOOR HANDLE WAS ON TOP OF KNUCKLE KNOCKER. CORRECTIVE ACTION: NSP RIGHT AFT ENTRY DOOR AS PER B757 AMM 52-11. FAST TEST ALL TEST WITHIN LIMITS AS PER B757 AMM 52-11. RT AFT DOOR INDICATION TEST GOOD AS PER B757 AMM 52-71. PRESSURISED A/C. ALL TEST GOOD
Part: SENSOR — DIRTY (SLIDE INDICATOR) · airframe 73,452 hrs · 24,221 cycles
SHIP 5805 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:611. CORRECTIVE ACTION: FOUND SENSOR AREA DIRTY. CLEANED AS REQ. REF B757 AMM 52-71. ARMED LIGHTS NOW ILLUMINATE WHEN ARMED. (0397077)
Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 73,104 hrs · 24,100 cycles
SHIP 5805 ON SVC, SEAT EMER AISLE WAY LIGHTS ROWS 14-20 INOP. CORRECTIVE ACTION: T/S REF B757 WDM 33-51-21 FOUND SHORT TO GND IN SEAT TRACK WIRING AND REPAIRED REF SWPM20 FURTHER FOUND EMER POWER SUPPLY M11612 FUSE FOR PIN 10 OPEN. R+R'D FUSE AND OPS CHECKED GOOD. (5298495)
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 73,097 hrs · 24,096 cycles
SHIP 5805 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:603. CORRECTIVE ACTION: RESECURED EMERGENCY EXIT SIGN LOCATION 603 PER B757 AMM 33-51. (0295494)
Part: COVER — LOOSE (EMERGENCY LIGHT) · airframe 72,914 hrs · 24,027 cycles
SHIP 5805 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:610. CORRECTIVE ACTION: RESECURED LENS COVER PREFORMED OPS CK AS PRECAUTION OPS GOOD. (0258611)
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,227 hrs · 23,765 cycles
SHIP 5805 -MISC/DE- DUE TO LEFT FLAP INDICATION LAGGING BEHIND RIGHT. R & R K10244 RELAY, R & R RT FLAP TRANSMITER, CKS GOOD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,111 hrs · 23,721 cycles
SHIP 5805 EXIT SIGN FELL OFF AT DOOR 3. CORRECTIVE ACTION: SECURED 3L & R DOOR EMER EXIT SIGN PER B757 AMM 33-51. (9938872)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 72,079 hrs · 23,707 cycles
14D EMERGENCY ESCAPE LIGHT INOPERATIVE. R/R EMERGENCY PATH LIGHT AT 14D PER B757 CMM 25-22-57. OPS CK GOOD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,875 hrs · 23,629 cycles
SHIP 5805 FOUND DOOR 2L MISSING STOP ON FWD SIDE (PLATE). CORRECTIVE ACTION: INSTALLED NEW PLATE ON FWD SIDE OF DOOR FRAME. PER B757 AMM 5211. (4585866)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,052 hrs · 23,368 cycles
SHIP 5805 DOOR 4R WOULD NOT ILLUMINATE SLIDE LIGHT. CORRECTIVE ACTION: REMOVED DEBRIS FROM DOOR CHANNEL OPS CKS GOOD IAW B757 AMM 52-11 OK FOR SVC. (4985626)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,993 hrs · 23,351 cycles
SHIP 5805 1R AND 4R DOORS WILL NOT ARM. CORRECTIVE ACTION: FOUND SAFETY LANYARD NOT STOWED CORRECTLY STOWED & ARMED DOORS NML. (4985606)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,000 hrs · 23,049 cycles
SHIP 5805 EMERGENCY LIGHTS AT SEAT ROWS 41 THRU 45 INOP. CORRECTIVE ACTION: /S REF B757 FIM 33-51. FOUND BLOWN FUSE IN POWER SUPPLY M736. REPLACED FUSE. CHECKED WIRING, CHECKS GOOD. FOUND LIGHT EMITTING DIODE AT SEAT 43 BAD. REPLACED FUSE AND LIGHT EMITTING DIODE AT SEAT ROW 43. CHECKS GOOD. (9958828)
Part: CONTROL MODULE — FAULTED (SPOILERS) · airframe 69,094 hrs · 22,681 cycles
SHIP 5805 - FCNT - DUE TO UN-COMMANDED ROLL AND SPOILER EICAS MSG ON DECENT. CORRECTIVE ACTION: FOUND FAULT ON SCM. REPLACED #12 SPOILER AND SCM. C/W ALL RII REQUIREMENTS.
2022
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,790 hrs · 22,561 cycles
ROW 36 SEAT EMERGENCY LIGHT WAS INOPERATIVE. FOUND A DAMAGED WIRE UNDER SEAT 36A. SPLICED THE WIRE IAW SWPM 20-30 . OPS CHECKED GOOD.
Part: DOUBLER — CORRODED (BS 1540-1560) · corrosion level 2 · airframe 68,474 hrs · 22,439 cycles
SHIP 5805 CORROSION ON EXTERNAL SKIN DOUBLERS BTW STA 1540-1560 BTW STRINGER 27RH-29RH IN REF NRC 00179. CORRECTIVE ACTION: SUMMARY OF NRC 00280: EXTERNAL SKIN DOUBLERS BTW STA 1540-1560 BTW STRINGER 27RH-29RH WAS REPLACED WERE REPLACED PER PRI 545850-14 REV. 0 AND ERA 545850-14 REV ORIGINAL. (2457558)
Part: STRINGER SPLICE — CORRODED (BS 1520-1560) · corrosion level 2 · airframe 68,474 hrs · 22,439 cycles
SHIP 5805 CORROSION ON PREVIOUS REPAIR SPLICE AND SRINGER SECTIONS FROM STA 1520 TO 1560 S-29RH AT UNDER WASTE SYSTEM ENCLOSURE . C2. CORRECTIVE ACTION: SUMMARY OF NRC 00179: PREVIOUS REPAIR SPLICE AND SRINGER SECTIONS FROM STA 1520 TO 1560 S-29RH WERE REPLACED PER ER/A 587847-14 REV. ORIGINAL SECTION I: PERMANENTE REPAIR. (2457919)
Part: ANGLE — CORRODED (BS 1546 S28R) · corrosion level 2 · airframe 68,474 hrs · 22,439 cycles
SHIP 5805 AWR HIDDEN DAMAGE IN REF NRC 00183: CORROSION ON ANGLE STA 1546 APPROX BTW S-28 RH & S-28RH OF AFT CARGO COMPARTMENT. CORRECTIVE ACTION: SUMMARY OF NRC 00276: ANGLE WAS FABRICATED PER DRAWING 146N3653 REV: AND REPLACED UNDER NRC. (2457708)
Part: DOUBLER — CORRODED (BS 1543 S28R) · airframe 68,474 hrs · 22,439 cycles
SHIP 5805 CORROSION ON INTERNAL PRODUCTION DOUBLER AT AFT LAVATORIES SERVICE PANEL STA 1546 APPROX BTW S-28 RH & S- 28RH, UNDER WASTE SYSTEM ENCLOSURE. C2. CORRECTIVE ACTION: SUMMARY OF NRC 00183: INTERNAL PRODUCTION DOUBLER WAS REPLACED PER PRI 602868-14 REV.0 AND ERA 602868-14 REV ORIGINAL. (2457871)
Part: FRAME — CRACKED (BS 1540 S28-29R) · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 DURING INSPECTION PER REMOVED PARTS: CRACK ON FRAME STA 1540 RBL 12 BTW S- 28R/29R AT AFT CARGO. IN REF NRC 179. C2. CORRECTIVE ACTION: SUMMARY OF NRC 00286: FRAME STA 1540 RBL 12 BTW S- 28R/29R WAS REPAIRED PER ER/A 602910-14 REV ORIGINAL SECTION I: PERMANENT REPAIR AND PRI 602910-14 REV. 0. (2455008)
Part: BRACKET — CORRODED (NLG) · corrosion level 2 · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 CORROSION ON BRACKET OF NLG UNSAFE LIGHT AT NOSE LANDING GEAR. CORRECTIVE ACTION: SUMMARY OF NRC 00140: BRACKET OF NLG UNSAFE LIGHT AT NOSE LANDING GEAR (3 EA S) WERE REPLACED PER DWG 284N1762 REV: A. (2453392)
Part: GIRT BAR — DAMAGED (R4 DOOR) · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 FWD LEAF SPRING DOES NOT RETAIN THE SLIDER ON GIRT BAR OF R4 DOOR SLIDE IN REF AMDS 2561-01257-01F STEP 11 NEED REPLACE THE GIRT BAR. CORRECTIVE ACTION: SUMMARY OF NRC 00129: GIRT BAR ON 4R DOOR WAS REPLACED AND PART NUMBER WAS VERIFIED PER B757-300 IPC 25-66-05 AND REPLACEMENT WAS ACCOMPLISHED UNDER CARD AMDS. (2452435)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 WEAR ON EXTERNAL FUSELAGE SKIN BTW STA 1180+ 100-1180+120 STRG-1 ( AFT SETTLEMENT AREA OF SATELLITE TV ANTENNA RADOME). CORRECTIVE ACTION: SUMMARY OF NRC 00193: WEARS ON EXTERNAL FUSELAGE SKIN BTW STA 1180+100-1180+120 STRG-1 WERE BLENDED OUT PER B757-300 SRM. THEREFORE WEAR 1 IS WITHIN LIMITS AND WEAR 2 IS OUT LIMITS PER B757-300 SRM, HFEC INSPECTION WAS ACCOMPLISHED ON EXTERNAL FUSELAGE SKIN BTW STA 1180+100-1180+120 STRG-1 ( AFT SETTLEMENT AREA OF SATELLITE TV ANTENNA RADOME). NO CRACKS WERE FOUND ON BLENDED AREA. PER B757-300 SRM. WEAR 2 ON STA 1180+104 WAS REPAIRED PER ERA 602903-14 REV. (2452077)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 DTE, 602910-14 FUSELAGE / MAIN FRAME / STA 1540 FRAME S-28R & S- 29R / CORROSION AND CRACK. CORRECTIVE ACTION: REF ERA 602910-14. (2451989)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 CORROSION ON L4 DOOR PNEUMATIC ACTUATOR AT PASSENGER COMPARTMENT. CORRECTIVE ACTION: SUMMARY: PNEUMATIC ACTUATOR AT L4 DOOR WAS REMOVED AND REPLEACED BY SERVICEABLE PNEUMATIC ACTUATOR PER B757-300 AMM 52-11-35. (2451046)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,610 hrs · 23,532 cycles
SHIP 5805 DTE - 602903-14 - ERA A WORN AREA WAS FOUND ON THE FUSELAGE SKIN AT STA 1180+104 AND S-1. CORRECTIVE ACTION: REF ERA 602903-14 REV A. (2450512)
Part: NONE — NONE · corrosion level 2 · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 CORROSION ON WEB OF LH WING FIXED LEADING EDGE PANEL ABOVE LH PYLON. CORRECTIVE ACTION: SUMMARY OF NRC 00247: WEB OF LH WING FIXED LEADING EDGE PANEL ABOVE LH PYLON WAS REPAIRED PER B757-300 SRM. (2448047)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 ERA 602868-14 ISSUED FOR INTERCOSTAL AT STATION 1540-1560, S-27R TO S-29R. CORRECTIVE ACTION: REF ERA 602868-14. (2446274)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 FWD AND AFT LEAF SPRINGS DOES NOT RETAIN THE SLIDER ON GIRT BAR OF L4 DOOR SLIDE IN REF AMDS. CORRECTIVE ACTION: SUMMARY OF NRC S/N:000130. GIRT BAR WAS VERIFIED AND REPLACED PER B757-300 IPC 25-66-05 AND INSTLLED UNDER W/C. (2446588)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
AIRCRAFT 5805, INITIAL INSPECTION: MISSING AFT GIRT BAR CRANK AND CAM ON LOWER GATE AREA ON R1 DOOR . CORRECTIVE ACTION: NEW CAM WAS INSTALLED AND ADJUSTED ON 1R DOOR PER B757-300 AMM 52-11-25-825-001. (LP 2439407)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 FRAYED ALSO BROKEN HARNESS, ON EMERGENCY SLIDERS L4, L1 AND R1. CORRECTIVE ACTION: SUMMARY OF NRC 00227:HARNESS OF 1L AND 1R DOOR SLIDES WERE REPLACED BY AMDS; 4L DOOR WAS ATTENDED UNDER NRC 00134 P/N WERE VERIFIED PER B757-300 IPC 25-66-01. (2437497)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 TORN HARNESS OF L2 AND L4 DOOR SLIDES. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00134: HARNESS OF L2 AND L4 DOOR SLIDES WERE REPLACED BY AMDS AND WERE VERIFIED PER B757-300 IPC 25-66-01. (2437368)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 DENT IN LWR FWD CARGO DOOR. CORRECTIVE ACTION: SUMMARY: DENT IN LWR FWD CARGO DOOR WAS REPAIRED PER B757-300 SRM 52-30-01-2R PROCEDURE 4. (2437326)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 IN REF. LP 8742426 DENT IN LWR FWD CARGO DOOR. CORRECTIVE ACTION: SUMMARY: DENT IN LWR FWD CARGO DOOR WAS REPAIRED PER B757-300 SRM 52-30-01-2R PROCEDURE 4. (2437180)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 [AD // AA] VISUAL INSPECTION WAS ACCOMPLISHED ON RH ENG DRAG FTG HOLES 11 TO 18 AND FOLLOWING DAMAGES WERE FOUND: HOLE #11, SCRATCHES ON FITTING ALL AROUND HOLE ; HOLE #13 SCRATCH ON FITTING BTW 10-11 CLOCK POS ; HOLE #18 CORROSION ON SKIN AND FITTING BTW 9-11 CLOCK POS. IN REF TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC 00142: [AD // AA] RH ENG DRAG FTG HOLES #11, #13 AND #18 WERE REPAIRED PER CARD. (2433146)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 CRACKED STABILIZER STRAP BTW STA 345 TO STA 365 AND BL0 AT ABOVE NLG W/W. CORRECTIVE ACTION: SUMMARY OF NRC 00139: STABILIZER STRAP BTW STA 345 TO STA 365 AND BL0 AT ABOVE NLG W/W (E&E) WAS REPAIRED PER B757-300 SRM. (2433741)
Part: CHARGER — INOPERATIVE · airframe 68,064 hrs · 22,307 cycles
SHIP 5805 DURING SVC CHK, FOUND BS1300 CEILING EMERGENCY EXIT SIGN LIGHT OUT. CORRECTIVE ACTION: RELAMPED, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY CHARGER M11081 PER B757 AMM 33-51, OPS CHECK GOOD. (9121246)
Part: ISOLATION VALVE — MISLOCATED · airframe 67,763 hrs · 22,211 cycles
SHIP 5805 - ATO - DUE TO LEFT BLEED OFF MESSAGE. CORRECTIVE ACTION: NO MAINTENANCE PERFORMED. ISOLATION VALVE SWITCH IN INCORRECT POSITION FOR TAKE-OFF. (8439194)
Part: NONE — NONE · airframe 66,727 hrs · 21,859 cycles
SHIP 5805 FOUND EMERGENCY AISLE LIGHT AT ROW 34 INOP. CORRECTIVE ACTION: RELAMPED, REMOVED AND REPLACED AISLE LIGHT ASSY PER B757 AMM 33-51. OPS CHECK NORMAL. (8742467)
Part: NONE — NONE · airframe 68,472 hrs · 22,438 cycles
SHIP 5805 DENT IN LWR FWD CARGO DOOR. CORRECTIVE ACTION: SUMMARY: DENT IN LWR FWD CARGO DOOR WAS REPAIRED PER B757-300 SRM 52-30-01-2R PROCEDURE 4. (8742426)
Part: FILTER — ODOR (RECIRC FAN) · airframe 66,268 hrs · 21,709 cycles
SHIP 5805 -SMKE- AFTER LANDING THE CREW REPORTED LIGHT SMOKE WITH ELECTRICAL SMELL. QUICKLY DISSIPATED AFTER C/W QRH. CORRECTIVE ACTION: T/S AND FOUND C/B J5 OUT ON P37 PANEL. REPLACED LT AND RT RECIRC FAN FILTERS PER B757 AMM 21-25. REPLACED RH RECIRCULATION FAN PER B757 AMM 21-25, OPS CK GOOD AND CLEARED EXISTING DEFERRAL.
Part: NONE — NONE · airframe 66,077 hrs · 21,632 cycles
SHIP 5805 EMERGENCY SIGN LENS CRACKED. CORRECTIVE ACTION: INSTALLED EMERGENCY SIGN REF B757 AMM 33-51. (2072678)
2021
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 64,891 hrs · 21,299 cycles
SHIP 5805 EMERG EXIT AFT LENS COVER MISSING BETWEEN ROWS 37ABC & 37DEF OVHD. CORRECTIVE ACTION: REPLACED LENS COVER AT 37CD. OK FOR SVC PER B757 MM 33-51. (8010675)
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 64,167 hrs · 21,103 cycles
SHIP 5805 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:603. CORRECTIVE ACTION: RE-SECURRED DOOR 2L EMERGENCY EXIT LIGHT DIFFUSER LENS. (1855949)
Part: PSEU — MALFUNCTIONED (DOOR WARNING SYS) · airframe 63,828 hrs · 20,990 cycles
SHIP 5805 ON INITIAL CLIMBOUT RECEIVED THE FOLLOWING EICAS MESSAGES: CARGO DOORS ACCESS DOORS EMER DOORS R ENTRY DOORS L ENTRY DOORS. CORRECTIVE ACTION: REPLACED PSEU PER B757 MM 32-09-04. OPS CK OK. (7475646)
Part: INDICATOR — MALFUNCTIONED (R4 DOOR) · airframe 63,575 hrs · 20,904 cycles
SHIP 5805 4R KNUCKLE KNOCKER STAYS FLUSH WITH DOOR WHEN IT IS ARMED. CORRECTIVE ACTION: GRIT BAR REMOVED DEBRIS AND OLD GREASE. APPLIED NEW GREASE TO GRIT BAR. DOOR ARMS DISARMS OPS CHECK GOOD. REF B757 AMM 12 21. (7630730)
2020
Part: SWITCH — INOPERATIVE (EMERGENCY TEST) · airframe 62,202 hrs · 20,276 cycles
THE AFT LIGHT EMERGENCY TEST SWITCH WAS DISCOVERED TO BE INOPERATIVE. THIS IS CONSIDERED TO BE A DEFECT IN THE EMERGENCY ESCAPE SYSTEM AND COULD HAVE AN ADVERSE EFFECT ON THE EVACUATION ROUTE. MAINTENANCE FOUND THE SWITCH CAUSING A FLICKERING OF THE LIGHTS AND APPLIED SECTION 1 OF ER/A 588159-14. IAW B757-300 WDM 33-51-11 THE AFT EMERGENCY LIGHT TEST SWITCH WAS REPLACED. OPERATIONAL CHECK WAS NORMAL. THE AIRCRAFT IS OK FOR SERVICE.
Part: SPRING — FAILED (GIRT BAR) · airframe 62,013 hrs · 20,224 cycles
DURING L2 SLIDE INSTALLATION, AFT/FWD GIRT BAR LEAF SPRINGS DOES NOT RETAIN. CORRECTIVE ACTION: GIRT BAR REPLACED.
Part: STRINGER — CORRODED (BS 1540-1560) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
CORROSION LEVEL 2: DURING INITIAL INSPECTION FOUND CORROSION ON STRINGER 29RH FROM STA 1540 TO 1560 AT AFT CARGO COMPARTMENT (C2). STRINGER REPAIRED, PER ERA 587847-14.
Part: HARNESS — TORN (ESCAPE SLIDE) · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND HARNESS ASSEMBLY ON L1 AND R2 EMERGENCY ESCAPE SLIDES WERE FOUND TORN. CORRECTION ACTION: REPLACED HARNESS ASSEMBLY.
Part: FRAME — CORRODED (BS 1560) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
CORROSION LEVEL 2: DURING INITIAL INSPECTION FOUND CORROSION ON FRAME STA Y=1560 BETWEEN 4 RBL AND 14 RBL AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED PER ERA 587835-14.
Part: WIRE HARNESS — DAMAGED (ESCAPE SLIDE) · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND TORN EMERGENCY SLIDE HARNESS ASSEMBLY ON PASSENGER R4 DOOR. CORRECTIVE ACTION: REPLACED EMERGENCY SLIDE HARNESS ASSEMBLY.
Part: SKIN — DENTED (BS 620) · airframe 62,013 hrs · 20,224 cycles
DURING INITIAL INSPECTION FOUND DENT AND PROTUBERANCE ON EXTERNAL FUSELAGE SKIN FS 620, S16L NEAR TO PREVIOUS REPAIR. EXTERNAL FUSELAGE SKIN FS 620 S16L WAS REPAIRED PER ER/A 587829-14.
Part: FLOOR SUPPORT — CORRODED (BS 1640-1660) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
DURING INITIAL INSPECTION FOUND LEVEL 2 CORROSION ON FLOOR SUPPORTS (2EA) STA 1640 TO 1660 AND 1660 TO 1681 RBL58 AT PAX CABIN FLOOR STRUCTURE. REPAIRED FLOOR SUPPORTS, PER ERA 587625-14.
Part: CREASE BEAM — CRACKED (BS 418) · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND CRACK ON CREASE BEAM TRUSS AT STA 418 AND 65 LBL PASSENGER CABIN. REPAIRED PER ERA 587698-14.
Part: FRAME — CORRODED (BS 1560) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
DURING INITIAL INSPECTION CORROSION LEVEL 2 FRAME CLIP STA 1560 BETWEEN STR 26-27 RT WAS REPLACED.
Part: FLOOR SUPPORT — CORRODED (BS 1520-1540) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION FOUND CORROSION LEVEL 2, INTERCOSTAL ON STA 1520 TO 1540 RBL 4 WAS REPAIRED (PERMANENT REPAIR ), PER ER/A 587708-14.
Part: SUPPORT — CORRODED (WASTE TANK) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND CORROSION LEVEL 2 ON SUPPORTS (2EA) OF WASTE TANK PANEL STA 1545 AND 1557 STR 29 RT AFT CARGO COMPARTMENT (C2) AND REPLACED PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1660-1681) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND LEVEL 2 CORROSION ON FLOOR SUPPORT AT STA 1660/1681, WAS REPAIRED ER/A 587628-4.
Part: SKIN — DAMAGED (BS 1340-1360) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
CORROSION LEVEL: 2 FOUND DURING INITIAL INSPECTIO ON INTERNAL FUSELAGE SKIN FROM FS 1340 TO 1360 BTW S-29L AND S-30 (AFT ATG ANTENNA)(SM). REPLACED FILLER(INTERNAL DOUBLER),EXTERNAL DOUBLER AND STIFFENER PER SRM.
Part: SKIN — DENTED (NR 3 SLAT WEDGE) · airframe 62,013 hrs · 20,224 cycles
DURING INSPECTION FOUND DENTS ON RIGHT WING SLAT 6 WEDGE #24, 37 AND 39 OUT OF LIMITS. DENTS REPAIRED PER SRM 51-70-10.
Part: SKIN — DENTED (NR 3 SLAT WEDGE) · airframe 62,013 hrs · 20,224 cycles
DURING INSEPCTION FOUND DENTS OUT OF LIMITS ON LH WING SLAT PANEL # 3, WEDGE AREA, ZONE 1 DENT #21, ZONE 2 DENT #49 AND 78, DENTS WERE REPAIRED PER SRM 51-70-10.
Part: SKIN — DEBONDED (NR 8 SLAT WEDGE) · airframe 62,013 hrs · 20,224 cycles
MAINTENANCE FOUND 3 DISBONDS ON T.E SLAT WEDGE 8 UPPER SURFACE AT OSS=452, OSS=453, OSS=560. DISBONDS REPAIRED PER RM 51-70-10. (LP 1603359)
Part: SEAT TRACK — CORRODED (BS 1620-1640) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
CORROSION LEVEL: 2 CORROSION ON SEAT TRACK FLANGE FROM STA 1620 TO 1640 RBL 25 AT PAX CABIN FLOOR STRUCTURE. REPLACED PER SRM 51-40-02
Part: WEDGE — DEBONDED (SLAT TE) · airframe 62,013 hrs · 20,224 cycles
DISBOND WAS FOUND ON SLAT T.E. WEDGE 2 AT OSS=580 REPAIRED PER SRM 57-43-02 AND 51-70-10
Part: FLOOR SUPPORT — CRACKED (BS 1320-1340) · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION : CRACKED INTERCOSTAL ANGLE BTW STA. Y=1320 AND Y=1340 BL=0 AT MAIN DECK FLOOR STRUCTURE AT AFT CARGO. REPAIRED PER SRM 53-00-51.0
Part: FLOOR SUPPORT — CRACKED (BS 1180) · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION : CRACKED INTERCOSTAL ANGLE BTW STA. Y=1180+ 80 AND Y=1180+100 BL=0 AT MAIN DECK FLOOR STRUCTURE AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-51.
Part: FLOOR SUPPORT — CRACKED (BS 1200-1220) · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION : CRACKED INTERCOSTAL ANGLE BTW STA. Y=1200 AND Y=1220 BL=0 AT MAIN DECK FLOOR STRUCTURE AT AFT CARGO. REPAIRED PER SRM 53-00-51.
Part: FLOOR SUPPORT — CRACKED (BS 1420-1440) · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION : CRACKED INTERCOSTAL ANGLE BTW STA. Y=1420 AND Y=1440 BL=0 AT MAIN DECK FLOOR STRUCTURE AT AFT CARGO COMPARTMENT. REPAIRED PER SRM 53-00-51.
Part: SUPPORT — CORRODED (BS 1460-1480) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
CORROSION ON ANCHOR FITTING SUPPORT Y=1460 AND Y=1480 5 RBL AT AFT CARGO COMPARTMENT. REPLACED SUPPORT.
Part: STRAP — CRACKED (BS 580) · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION: CRACK ON FLOOR BEAM STRAP AT FWD CARGO COMPARTMENT BTW STA 580 AND LBL 24.75. REPAIRED PER SRM 53-00-51. (LP 1594046)
Part: STRAP — CRACKED (BS 365-377) · airframe 62,013 hrs · 20,224 cycles
CRACK ON FLOOR BEAM STABILIZATION STRAP PREVIOUS REPAIR BTW STA 365/377 AND 47 LBL AT PASSENGER CABIN (CPAX). FLOOR BEAM STABILIZATION STRAP WAS REPAIRED PER ERA 384483-14. (LP 1593763)
Part: PAN — CORRODED (LAVATORY) · corrosion level 2 · airframe 62,013 hrs · 20,224 cycles
INITIAL INSPECTION: CORROSION ON LAVATORY DOUBLER PAN AT AFT CARGO COMPARTMENT. REPLACED DOUBLER PAN.
Part: FLOORBEAM — CRACKED (BS 780) · airframe 62,013 hrs · 20,224 cycles
CRACK ON FLOOR BEAM STRAP AT FWD CARGO COMPARTMENT (C-1) BTW STA 780+120 AND RBL 24.75. REPAIRED PER SRM 53-00-51.
Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 61,570 hrs · 20,087 cycles
(AIRCRAFT 5805, L/P 6495502) 2L DOOR SLIDE PACK HAS CORD SHOWING OUTSIDE OF CASE. CORRECTIVE ACTION: RESECURED MOORING LINE INTO POUCH IAW B757 AMM 25-66. NO FURTHER FAULTS NOTED.
Part: ESCAPE ROPE — UNSECURE (L2 DOOR) · airframe 61,495 hrs · 20,062 cycles
SHIP 5805 L-2 ESCAPE ROPE HANGING IN DOORWAY. CORRECTIVE ACTION: STOWED L2 DOOR SLIDE MOUNTING CORD INTO SLIDE PACK PER B757 AMM 25-66. (6377086)
Part: LANYARD — UNSECURE (L2 DOOR SLIDE) · airframe 61,488 hrs · 20,060 cycles
SHIP 5805 GREEN CORD HANGING FROM 2L DOOR SLIDE COMPARTMENT. CORRECTIVE ACTION: STOWED 2L DOOR SLIDE MOORING CORD INTO SLIDE PACK. (6377078)
2019
Part: LENS — MISINSTALLED (R2 DOOR SLIDE) · airframe 61,007 hrs · 19,912 cycles
(AIRCRAFT 5805, L/P 1405979) CREW REPORTED 2R "SLIDE" LIGHT LENS IS UPSIDE DOWN. CORRECTIVE ACTION: REORIENTED LIGHT LENS RIGHT SIDE UP AS REQUIRED.
Part: LENS — DAMAGED (EMERGENCY LIGHT) · airframe 60,982 hrs · 19,905 cycles
(AIRCRAFT 5805, L/P 1398465) EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING. CORRECTIVE ACTION: REPLACED L2 DOOR EXIT SIGN COVER REF. B757 AMM 33-51.
Part: LIGHT — INOPERATIVE (ROW 41) · airframe 60,924 hrs · 19,887 cycles
(AIRCRAFT 5805, L/P 6571768) ROW 41 SEAT MOUNTED EMER LIGHT INOP (WHITE). CORRECTIVE ACTION: REMOVED AND REPLACED LIGHT ASSY REF B757 WDM 33-51.
Part: SPRING — DAMAGED (EXTERIOR HANDLE) · airframe 60,528 hrs · 19,745 cycles
SHIP 5805 FOUND 2L DOOR OUTSIDE HANDLE RELEASE SPRING DAMAGED. CORRECTIVE ACTION: R/R DOOR HANDLE RELEASE SPRING PER B757 AMM 52-11. OPS CK GOOD. (6238492)
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 60,407 hrs · 19,706 cycles
EMERGENCY LIGHT AT ROW 5 SEAT INOPERATIVE. FOUND A BROCKEN SPLICE, REPAIRED IAW SWPM 20-30-12. OPS CHECKED GOOD.
Part: WIRE — BROKEN (CABIN) · airframe 60,106 hrs · 19,622 cycles
(AIRCRAFT 5805, L/P 6124516) EMG LIGHTS BETWEEN 33C THROUGH 38C INOP. FOUND BROKEN WIRE AT SEAT 38 DEF. REPAIRED WIRE REF WDM 33-51 AND SWPM CH 20.
Part: COLLAR — DAMAGED (L2 GUST LOCK) · airframe 59,991 hrs · 19,594 cycles
GUST LOCK RELEASE ON 2 L DOOR IS STUCK IN THE UP POSITION. R/R HOLD OPEN LOCK UPPER COLLAR IAW B757 52-11.
Part: COVER — MISSING (R1 DOOR HANDLE) · airframe 59,984 hrs · 19,592 cycles
R1 DOOR MISSING COVER PLATE BEHIND DOOR HANDLE. REPLACED MISSING DOOR HANDLE COVER. (5373734)
Part: HOUSING — CRACKED (EMERGENCY LIGHT) · airframe 59,371 hrs · 19,434 cycles
SHIP 5805 EMERGENCY LIGHT HOUSING BROKEN @ ROW 17DEF. CORRECTIVE ACTION: INSTALLED NEW HOUSING. CKS GOOD. (5513537)
Part: LIGHT — UNSECURE (CABIN) · airframe 58,884 hrs · 19,307 cycles
(AIRCRAFT 5805, L/P 1092689) EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. RESECURED LIGHT. OPS NML.
Part: SWITCH — DEFECTIVE (L4 DOOR) · airframe 58,609 hrs · 19,234 cycles
SHIP 5805 4L GIRT BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: R/R SLIDE LIGHT SWITCH PER AMM 33-51. ALL OPS NML. (5285338)
Part: LIGHT — UNSECURE (CABIN) · airframe 57,697 hrs · 18,956 cycles
UNDER SEAT EMERGENCY LIGHT HANGING BELOW SEAT AT 20R. INSTALLED NEW EMERGENCY LIGHT ASSY & OP CKS NORMAL IAW AMM 33-51.
Part: WIRE — BROKEN (CABIN) · airframe 57,668 hrs · 18,946 cycles
SHIP 5805 SEAT EMER LIGHT AT 5D INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE UNDERNEATH SEAT 5D. SPLICED WIRE REF SWPM 20-30. (3747450)
Part: WIRE SPLICE — DAMAGED (CABIN) · airframe 57,578 hrs · 18,917 cycles
(AIRCRAFT 5805, L/P 3747420) FLOOR MOUNTED EMER LIGHT AFT OF RT AFT LAV PARTITION INOP. FOUND DAMAGED WIRE UNDERNEATH SEAT 40DEF. REPAIRED 2 BAD SPLICES, OPS CHECK GOOD. REF: WDM 33-51-22. RESTORED ALL ACCESS.
2018
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 56,956 hrs · 18,746 cycles
(AIRCRAFT 5805, L/P 3303788) ON PREFLIGHT FOUND EXIT SIGN LENS MISSING AT ROW 37. REPLACED EXIT SIGN LENS. OPN GOOD. REF B757 AMM 33-24.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,676 hrs · 18,665 cycles
(AIRCRAFT 5805, L/P 4561178) SEVERAL EMER. EXIT LIGHTS INOP THROUGHOUT CABIN. REPLACED BATTERY PACKS AT POWER SUPPLY'S M11490 & M11486 PER AMM 33-51-07. ALL CK'S GOOD. OK FOR SVC.
Part: SKIN — DELAMINATED (TE FLAP) · airframe 56,547 hrs · 18,632 cycles
LT O/B AFT FLAP LOWER SURFACE HAS SMALL DENT WITH DELAMINATION 1 FOOT OUTB OF NR 2 CANOE. LT O/B AFT C/W PERMANENT REPAIR PER SRM 57-53-01 FIGURE 201.
Part: LIGHT — DETACHED (CABIN) · airframe 56,425 hrs · 18,599 cycles
EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP / LOCATIONS:15D. EMERGENCY PATH LIGHT DETACHED / INTERIOR. SECURED EMER PATH LIGHT AT 15D.
Part: CONNECTOR — NOT SEATED (EMERGENCY LIGHTS) · airframe 56,201 hrs · 18,542 cycles
L3 DOOR EMERGENCY EXIT SIGN AND THE OVERHEAD CENTER EXIT SIGN WERE INOPERATIVE. RESEATED THE CONNECTOR ON THE POWER SUPPLY, OPS OK IAW AMM 33-51-07.
Part: LIGHT — UNSECURE (CABIN) · airframe 55,762 hrs · 18,441 cycles
EMERGENCY SEAT MOUNTED LIGHTING DAMAGED/INOP LOCATIONS:15D. SECURED EMERGENCY LIGHT SEAT 15D OP CK NORMAL OK FOR SERVICE.
Part: LENS — MISSING (CABIN) · airframe 55,235 hrs · 18,316 cycles
LT FWD OVERWING EXIT EMER EXIT IDENTIFIER LENS MISSING. REMOVED & REPLACED EXIT IDENTIFIER ASSY OPS CHECK GOOD.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,705 hrs · 18,160 cycles
EMERGENCY EXIT LIGHTS ROWS 41 - 45 INOPERATIVE. R & R EMERGENCY LIGHT POWER PACK (M736) IAW AMM 33-51.
Part: SKIN — DENTED (BS 640-660) · airframe 61,383 hrs · 20,022 cycles
FUSELAGE SKIN DENTED BETWEEN BS 640 - 660, STRINGERS 17L & 18L. EVALUATED THE DENTS AND FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED IAW ER/A 556509-14.
2017
Part: COVER — BROKEN (GIRT BAR) · airframe 53,195 hrs · 17,684 cycles
L2 DOOR AFT GIRT CAR PROTECTIVE COVER BROKE OFF. REMOVED COVER IAW ERA 560980-14MA, REV ORIGINAL, OPTION 2. REPLACED GIRT BAR SWITCH COVER.
Part: BRACKET — LOOSE (L2 DOOR) · airframe 52,398 hrs · 17,453 cycles
L2 DOOR AFT SENSOR BRACKET CAME LOOSE, CANNOT ARM DOOR. REATTACHED THE SENSOR BRACKET. DOOR CLOSES, OPENS AND ARMS NORMAL.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 50,823 hrs · 16,975 cycles
EMERGENCY LIGHT AT SEAT ROW 32 INOPERATIVE. FOUND BROKEN WIRES UNDER THE SEAT. REPAIRED IAW SWPM20-35-12. OPS CHECKED GOOD. OK FOR SERVICE.
Part: DOOR — DAMAGED (L2) · airframe 50,493 hrs · 16,854 cycles
L2 DOOR WILL NOT CLOSE. REPAIRED IAW ERA 532494-14.
2016
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 50,086 hrs · 16,696 cycles
ON SVC FOUND EMER LIGHTS OUT AT LT AFT OVERWING AND TWO EMER LIGHTS ON BULL NOSE AFT OF EXIT DOOR. FOUND POWER SUPPLY / BATTERY M11383 INOP. INSTALLED NEW POWER SUPPLY AND TEMP INSTALLED A GOOD BATTERY LIGHTS CHECKED GOOD. REMOVED BATTERY AND REINSTALLED IN ORIGINAL LOCATION. B757-AMM 33-51-07. INSTALLED NEW BATTERY. OPS CHECKED GOOD.
Part: SKIN — CRACKED (FUSELAGE) · airframe 54,672 hrs · 18,149 cycles
SKIN PANEL 197LL HAD A CRACKED EDGE ADJACENT TO HYD ACCESS DOOR AFT HINGE. REPAIRED THE SKIN PANEL IAW SRM 51-70-17, AND 51-70-14.
Part: BLEED AIR SYS — FAILED · airframe 49,326 hrs · 16,429 cycles
ACFT DIVERTED DUE TO DUAL ENGINE BLEED FAILURE. DESCENDED TO 10,000 FEET AND APU WAS STARTED TO MAINTAIN CABIN PRESSURIZATION. EMERGENCY WAS DECLARED, PERFORMED RAPID DESCENT PER QRH TO 10,000, MASKS WERE DONNED IN FLIGHT DECK, NO MASKS DEPLOYED IN CABIN, CABIN REACH APPROXIMATELY 10,500 MSL. REPLACED LEFT ENGINE FAN AIR MODULATING VALVE, FAN AIR TEMP SENSOR, PRESSURE REGULATING SHUTOFF VALVE, REVERSE FLOW CONTROLLER, HIGH STAGE REGULATORS, AND REPLACED OVERHEAD PNEUMATIC CONTROL PANEL. BOTH ENGINE BLEEDS NOW CHECK NORMAL. ACFT RETURNED TO SERVICE.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 49,273 hrs · 16,412 cycles
EXIT SIGN MISSING BY DOOR 3. INSTALLED EXIT LENS COVER. OK FOR SERVICE.
Part: COVER — UNSECURE (EMERGENCY LIGHT) · airframe 48,341 hrs · 16,114 cycles
AN EMERGENCY EXIT LIGHT COVER FELL OFF. REINSTALLED SAME EXIT LIGHTED SIGN COVER AS REQUIRED BY SECURING WITH THE SET SCREW.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 48,185 hrs · 16,058 cycles
DURING SERVICE CHECK FOUND EMERGENCY LIGHTING FROM ROWS 33- 38 AND O/H BIN EMERGENCY LIGHTS AT ROW 31-40 DEF AND 38 ABC INOPERATIVE. R & R BATTERY PACK AND CHARGER M11081 IAW AMM 33-51. OPS CHECK NORMAL.
Part: SERVICE PANEL — CORRODED · corrosion level 2 · airframe 48,125 hrs · 16,037 cycles
SURFACE CORROSION AFT OF THE AFT LAVATORY SERVICE PANEL. C/W PRI 545850-14, REV 0 AND REV 1.
Part: SKIN — DELAMINATED (LEFT ELEVATOR) · airframe 48,090 hrs · 16,025 cycles
LH ELEVATOR UPPER SKIN TRAILING EDGE DELAMINATED REPAIR PER ER/A 545800-14 /
Part: LUG — CORRODED · airframe 48,091 hrs · 16,025 cycles
NR 5 BALLSCREW LUG CORRODED. REMOVED NR 5 BALLSCREW, REF AMM 27-51-11 NR 5 BALLSCREW REPLACED ON AMDS WC 2751-2542, JOB 042-0002.
2015
Part: SWITCH — INOPERATIVE (EMERGENCY LIGHTS) · airframe 46,429 hrs · 15,413 cycles
EMERGENCY LIGHT SWITCH GUARD INOPERATIVE. AUTO ARMING FEATURE NOT WORKING. R & R EMERGENCY SWITCH GUARD IAW AMM 33-51.
Part: WIRE — EXPOSED (EMERGENCY LIGHTS) · airframe 45,291 hrs · 15,037 cycles
EXPOSED RED WIRE ON FLOOR AT SEAT 5D. PLACED RED EMERGENCY ESCAPE PATH LIGHT WIRE BACK INTO FLOOR CONDUIT IAW 33-51-11. OK FOR SERVICE.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 44,897 hrs · 14,889 cycles
FOUND FOUR EMERGENCY LIGHT BATTERY PACKS FAILING TEST. R & R THE EMERGENCY BATTERY PACKS IAW MM 33-51-07. EMERGENCY LIGHT, OPS CHECKS PASSED. OK FOR SERVICE.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 44,093 hrs · 14,612 cycles
ROW 25 EMERGENCY LIGHT INOPERATIVE. SPLICED BROKEN WIRE IAW SWPM, CHAP 20. OK FOR SERVICE.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 44,017 hrs · 14,583 cycles
DURING SERVICE CHECK, FOUND SEAT MOUNTED EMERGENCY LIGHT AT 1CD INOPERATIVE. ATTACHED THE CONNECTOR. OPS CHECKED GOOD.
2014
Part: SKIN — DAMAGED (BS 760-781) · airframe 42,542 hrs · 14,120 cycles
DURING MAINTENANCE CHECK, FOUND DAMAGE ON FUSELAGE SKIN BETWEEN BS 760-781 S14-16L. REPAIRED IAW ERA 524450-14, REV A.
Part: UNKNOWN — UNKNOWN (EMERGENCY LIGHTS) · airframe 41,260 hrs · 13,747 cycles
PERIODIC BLINKING OF FLOOR AND OVER EXIT EMERGENCY SIGNS. TESTED OK .
Part: FLOORBEAM — CORRODED (BS 1640) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
CORROSION FOUND ON MAIN CABIN FLOORBEAM UPPER SURFACE ON PREVIOUS REPAIR SECTION AT BS 1640, RBL-35-60. COMPLIED WITH ERA 524451-14, REV ORIGINAL.
Part: FRAME — CHAFED (BS 1280) · airframe 41,104 hrs · 13,693 cycles
MAIN CABIN BS 1280, FRAME CHAFED S14R. COMPLIED WITH ERA 524452-14AD, REV ORIGINAL.
Part: SKIN — DENTED (BS 760-780) · airframe 41,104 hrs · 13,693 cycles
ON ARRIVAL, FOUND DENTS AND SCRATCHES APPROXIMATELY 4 FEET AFT OF L2 DOOR. COMPLIED WITH ER/A 524450-14, REV ORIGINAL.
Part: GATE — CORRODED (L2 DOOR) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
L2 PAX DOOR, LOWER GATE, EDGE AREA HAS CORROSION. R & R LOWER GATE IAW AMM 52-11 AND AMM 52-11.
Part: CREASE BEAM — CORRODED (BS 778) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
MAIN CABIN RT CREASE BEAM INBD ANGLE HAS CORROSION AT BS 778. COMPLIED WITH ER/A 524454-14, REV ORIGINAL.
Part: FRAME — CRACKED (BS 780) · airframe 41,104 hrs · 13,693 cycles
FRAME CRACKED BS 780 + 35, STRINGER 16L FROM EDGE TO FASTENER HOLE. COMPLIED WITH ERA 524445-14, REV ORIGINAL AT STA 780+35, STRINGER 16L.
Part: SKIN — DENTED (BS 1701-1720) · airframe 41,104 hrs · 13,693 cycles
EXTERIOR FUSELAGE SKIN HAS TWO DENTS BETWEEN BS 1701 AND 1720 S18-19L. COMPLIED WITH ER/A 524449-14.
Part: FLOOR SUPPORT — CORRODED (BS 377) · airframe 41,104 hrs · 13,693 cycles
CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE AT BS 377.7 BL-0. REMOVED CORROSION ON MAIN CABIN FLOOR SUPPORT UPPER SURFACE AT BS 377.7, BL-0 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51. R & R FLOOR SUPPORT, BL-0 BETWEEN STA 324 TO STA 418 IAW SRM.
Part: STRAP — BROKEN (BS 1640) · airframe 41,104 hrs · 13,693 cycles
AFT CARGO BAY BS 1640 LBL 25 FLOORBEAM STABILIZATION STRAP BROKEN. REPAIRED STRAP IAW ER/A 384483-14MA, REV D.
Part: FLOORBEAM — CORRODED (BS 365) · airframe 41,104 hrs · 13,693 cycles
CORROSION ON CABIN FLOORBEAM UPPER SURFACE BS 365, RBL-31. FOUND OUT OF LIMITS IAW SRM 53-00-51. TRIMMED FLOORBEAM UPPER TEE LBL 10 TO RBL 33.5 , INSTALLED & ACCOMPLISHED PERMANENT REPAIR CAT "A" IAW SRM.
Part: STRAP — CORRODED (BS 365-377) · airframe 41,104 hrs · 13,693 cycles
FOUR CRACKS ON FLOORBEAM STABILIZATION STRAP BETWEEN BS 365-377. REPAIRED FLOORBEAM STABILIZATION STRAP IAW ERA 384483.
Part: SEAT TRACK — CORRODED (BS 1635-1640) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
CORROSION ON MAIN CABIN SEAT TRACK BS 1635-1640, RBL-45. R & R SEAT TRACK.
Part: STRAP — BROKEN (BS 377) · airframe 41,104 hrs · 13,693 cycles
BROKEN FLOORBEAM STABILIZATION STRAP AT BS 377 LBL 45. REPAIRED STABILIZATION STRAP IAW ERA 384483-14MA REV D.
Part: STRINGER — CRACKED (BS 780) · airframe 41,104 hrs · 13,693 cycles
BS 780+24, STRINGER 16L CRACKED FROM EDGE TO FASTENER HOLE. REPLACED STRINGER SECTION IAW SRM.
Part: FLOOR SUPPORT — CORRODED (BS 418) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
CORROSION ON MAIN CABIN FLOOR SUPPORT AT BS 418, RBL 45. R & R FLOOR SUPPORT IAW -SRM FROM BS 365 - 418.
Part: SEAT TRACK — CORRODED (BS 720-740) · corrosion level 2 · airframe 41,104 hrs · 13,693 cycles
MAIN CABIN SEAT TRACK UPPER SURFACE HAS AREAS OF CORROSION AT RBL-24, BETWEEN BS 720 - 740. BLENDED AREAS, BOTH BLENDOUT AREAS FOUND TO BE OUT OF LIMITS IAW SRM. SEAT TRACK BS 640 - 780, REPLACED.
Part: SKIN — DENTED (BS 614) · airframe 41,104 hrs · 13,693 cycles
LEFT EXTERIOR FUSELAGE HAS A SHARP DENT AT BS 614 AND BETWEEN STRINGERS 16 - 17L. DENT TRIMMED OUT IAW SRM 53-00-01 FIG 201, REPAIR 3. REPAIRED IAW SRM 53-00-01.
Part: CREASE BEAM — CORRODED (BS 680-740) · airframe 41,104 hrs · 13,693 cycles
MAIN CABIN CREASE BEAM INBD ANGLE HAS AREAS OF CORROSION BETWEEN BS 680 - 740. REMOVED CORROSION FROM CREASE BEAM ANGLE IAW SRM 53-00-51. REMAINING MATERIAL THICKNESS AFTER CORROSION REMOVAL FOUND TO BE WITHIN LIMITS IAW SRM.
Part: SILL — CORRODED (BS 580) · airframe 41,104 hrs · 13,693 cycles
FWD CARGO DOOR SILL DENTED AT BS 580. REPAIR WELDED AND NO ADDITIONAL DAMAGE FOUND.
Part: SKIN — GOUGED (STAB) · airframe 40,769 hrs · 13,587 cycles
DURING LEAK CHECK-2, A GOUGE WAS FOUND IN THE L/E SKIN. GOUGE REMOVED BY DRILLING OUT. REMOVED L/E PANEL FOR REPAIR. REPAIRED L/E STAB IAW ER/A 500382-14, REV ORIGINAL AND SRM 51-70-10.
2013
Part: FAN — CONTAMINATED (GALLEY OVEN) · airframe 40,355 hrs · 13,412 cycles
FORWARD GALLEY OVENS SMOKE WHEN ON FOR COOKING. REMOVED TRAY ASSY. FOUND PLASTIC MELTED ON FAN GUARD, REMOVED AND CLEANED FAN GUARD, OK FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,026 hrs · 13,282 cycles
AISLE LIGHT AT SEAT 23 INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW WDM 33-51. OPS CHECKED GOOD.
Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,026 hrs · 13,282 cycles
DURING SERVICE CHECK, FOUND ROWS 21- 36 ABE SEAT EMERGENCY LIGHTS INOPERATIVE. FOUND FUSE OPEN IN BATTERY PACKS. REPLACED FUSES. CHECKED GOOD IAW WDM 33-51-21.
Part: BULB — INOPERATIVE · airframe 38,310 hrs · 12,702 cycles
EMERGENCY LIGHT EXIT SIGN BULBS AR INOPERATIVE ABOVE R2 DOOR. REPLACED BULBS. OPS NORMAL.
Part: CONNECTOR — SHORTED (EMERGENCY LIGHTS) · airframe 37,380 hrs · 12,384 cycles
ON A-CHECK, FOUND LT OVERWING AFT EXIT LIGHT INOPERATIVE. FOUND CONNECTORS SHORTED TOGETHER. RECONFIGURED CONNECTORS WDM 33-51-22 EMERGENCY LIGHTS TEST OK FOR SERVICE.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,892 hrs · 12,166 cycles
LT EXTERIOR OVERWING EMEGENCY LIGHTS INOPERATIVE. REPLACED LAMP, OPS CHECKED GOOD.
2012
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,816 hrs · 12,138 cycles
DURING S/C FOUND SEAT EMERGENCY LIGHTS INOPERATIVE FOR EMERGENCY BATTERY PACK, M11612 POWER SUPPLY. R & R POWER SUPPLY BATTERY PACK ASSY WITH SERVICABLE UNIT. OPS CHECKED GOOD IAW AMM 33-57.
Part: BULB — WRONG PART (EMERGENCY LIGHT) · airframe 36,622 hrs · 12,060 cycles
NUMEROUS BULLNOSE EMERGENCY LIGHTS DIM WHEN TESTING. INSPECTED AND FOUND INCORRECT LIGHT BULBS INSTALLED. R & R LIGHT BULBS. OPS NORMAL. OK FOR SERVICE.
2011
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 5,230 hrs · 1,770 cycles
DURING A NON-ROUTINE LINE MAINTENANCE INSPECTION, OVERHEAD EMERGENCY LIGHTS BETWEEN DOORS 2L AND 2R AND SEAT ROW 21 WHERE FOUND INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY AND BATTERY PER B757ER AMM 33-51. AFTER REPLACEMENT OF BATTERY AND POWER SUPPLY EMERGENCY LIGHTS OPERATION IS NORMAL.
2007
Part: POWER SUPPLY — UNSERVICEABLE (NR 1 ENGINE) · airframe 18,054 hrs · 5,877 cycles
DURING TAKEOFF ROLL, ENGINE NR 1 EPR "DROPPED OFF" AND L ENG PRIM CONT MSG ANNUNCIATED. TAKEOFF ABORTED AT 110 KNOTS. MAINTENANCE REPLACED THE PMA AND PERFORMED A HIGH ENERGY STOP INSPECTION.
2005
Part: ODOR — DETECTED (CABIN) · airframe 9,440 hrs · 3,170 cycles
DURING TAXI , PASSENGER AND CREW SMELLED ELECTRICAL ODOR NEAR ROW 6. AIRCRAFT RETURNED TO BLOCKS AND FLIGHT CHANGED TO A/C5643. CHECK SEAT BOXES IN 1ST CLASS AND NOTHING FOUND. RAN NR 1 ENGINE AND PACKS AND THERE WAS A STRONG OIL SMELL IN THE COCKPIT AND CABIN. REPLACED THE EQUIPMENT COOLING FILTER AND BURNED OFF OIL SMELL BY RUNNING BOTH ENGINES, PACKS AND APU.
2004
Part: LINE — CHAFED (RT WING) · airframe 6,053 hrs · 2,093 cycles
THE FUEL SUPPLY TUBE IN THE RIGHT PYLON WAS FOUND TO BE CHAFING AGAINST THE PYLON SUPPORT STRUCTURE (P/N 112N4115-6). THE DAMAGE TO THE FUEL TUBE EXCEEDED THE ALLOWABLE 0.004 INCH OF DAMAGE. REPLACED THE FUEL LINE. REPAIRED PER EO 2822-01068-01. OPERATIONAL CHECK GOOD.