N589NW
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 2025-01-10 | Operator named in NTSB report |
Accident & incident history
Operated by DELTA AIR LINES 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.
192 reports on file, 2004-09-22 – 2026-07-10.
Part: WIRE — MISWIRED (ZONE 200) · airframe 78,523 hrs · 25,921 cycles
DURING SERVICE CHECK FOUND FWD GALLEY OVERHEAD CENTER EMERGENCY LIGHT L26 AND FLOOD LIGHT M11430 INOP. FOUND FWD LT OVERHEAD LIGHT L891 P/N 0105938-001 WIRE TERMINAL ON INCORRECT SCREW TO LIGHT HOUSING, CAUSING POWER SUPPLY FUSE TO TRIP. RESECURED TERMINAL AND REPLACED FUSE REF B757 WDM 33-51-12. OPS TEST GOOD EMERGENCY LIGHTS NOW WORKING. INSTALLED NEW POWER SUPPLY. (LP 6787976 - AIRCRAFT WAS GROUNDED)
Part: LEAF SPRING — NO TEST (ZONE 800) · airframe 78,387 hrs · 25,878 cycles
IN REFERENCE TO AMDS 2561-01257-01A STEPS 11, 12, 13 AND 14: LEAF SPRING NOT RETAIN THE SLIDER AND GO-NO GO TEST FAIL ON FWD /AFT FLOOR FITTINGS AT L1 DOOR. GIRT BAR L1 DOOR WAS REPLACED IAW IPC 25-66-05-05 AND AMM 25-66-10 & ADJUSTED WAS VERIFIED PER AMM 52-11-25 AND TEST ON SERVICEABLE GIRT BAR LOCK SPRING WAS PERFORMED UNDER AMDS 2561-01257-01A.TEST OK AND SYSTEM TEST WAS PERFORMED PER AMM 52-11-25.TEST OK. (1662748) AIRCRAFT WAS GROUNDED
Part: FLOOR PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION OUT OF LIMITS, IN REF NRC 362: CORROSION ON RH SIDE PANEL UPPER/LOWER SURFACE FROM BS 1440 TO BS 1480, AT AFT CARGO COMPARTMENT IAW SRM 53-00-53-1A PROCEDURE 1 ALLOWABLE DAMAGE 1 FIG. 11 NOTE C, DETAIL IX AND B757 NDT-4-51-00-10 STEP 4. CORROSION LEVEL 2; RH SIDE PANEL FROM BS 1440 TO BS 1520, AT AFT CARGO COMPARTMENT WAS REPLACED PER SRM 51-40-02-0G PAR. 7. D. (1660278) AIRCRAFT WAS GROUNDED.
Part: SKIN — CORRODED (ZONE 100) · airframe 78,387 hrs · 25,878 cycles
CORROSION ON EXTERNAL FUSELAGE SKIN AROUND OF PAN AT AFT WASTE SERVICE PANEL. FUSELAGE SKIN, BS 1540 & BS 1560, STGR 27R & STGR 29R. AFT LAVATORY SERVICE CUTOUT WAS REPAIRED IAW PRI 634692-14, REV 1, AND ENGINEERING REPAIR/AUTHORIZATION 634692-14 REV ORIGINAL SECTION I. (1656306) AIRCRAFT WAS GROUNDED.
Part: PANEL — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION OUT OF LIMITS: (UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON LT SIDE PANEL SURFACE FROM BS 1380 TO BS 1410 AT AFT CARGO BAY IAW SRM 53-00-53-1A PROCEDURE 1, DETAIL III, NOTE C, DETAILS IX. CORROSION LEVEL 2, LT SIDE PANEL SURFACE FROM BS 1380 TO BS 1410 AT AFT CARGO BAY WAS REPAIRED IAW SRM 53-00-53-2R. (1657206) AIRCRAFT WAS GROUNDED.
Part: PANEL — CORRODED (ZONE 200) · airframe 78,387 hrs · 25,878 cycles
CORROSION OUT OF LIMITS, CORROSION ON LH SIDE PANEL UPPER/LOWER SURFACE FROM BS 1530 TO BS 1550 IAW SRM 53-00-53-1A PROCEDURE 1, ALLOWABLE DAMAGE 1; NOTE C . DETAIL IX. FIG. 101. CORROSION LEVEL 2, LT SIDE PANEL FROM BS 1530 TO BS 1550 WAS REPAIRED PER SRM 53-00-53-2R PROCEDURE 2 REPAIR 2 AND REPLACED IAW SRM 53-00-53-2R PAR. 4 L TO N. (1654490) AIRCRAFT WAS GROUNDED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION ON FLOOR STRINGER (ATTACH POINT) BELOW 2.9 RBL AND BS 1518 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2, FLOOR STRINGER RBL 2.9 BTWN BS 1500 TO BS 1520 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT WAS REPLACED IAW SRM 51-40-02-0G. (1650417) AIRCRAFT WAS GROUNDED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
(UT) THICKNESS MEASUREMENT WAS ACCOMPLISHED ON FLOOR STRINGERS (ATTACH POINTS) 2.9, 7.55,RBL AND BTW BS 1320 TO BS 1340 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT, AREA IT IS OUT LIMITS PER SRM 53-00-53-1A PROCEDURE 1, DETAIL III, NOTE C (DETAIL VII); AND B757 NDT-4-51-00-10 STEP 4. FLOOR STRINGERS (ATTACH POINTS) 2.9 AND 7.55 RBL BTW BS 1320 TO BS 1340 OF FLOOR STRUCTURE AT AFT CARGO COMPARTMENT WERE REPAIRED PER B757-300 SRM. 53-00-53-2R PROCEDURE 1 REPAIR 1. (1645420) AIRCRAFT WAS GROUNDED
Part: INTERCOSTAL — CORRODED (ZONE 100) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION ON INTERCOSTAL BTW BS 1520 TO BS 1540 AND STRINGERS 30/29RH AT AFT CARGO COMPARTMENT. CORROSION LEVEL 2, INTERCOSTAL BTW BS 1520 TO BS 1540 AND STRINGERS 30/29RH AT AFT CARGO COMPARTMENT WAS REPLACED PER B757-300 SRM 51-40-02-0G AND MANUFACTURE PER DWG: 146N8401 REV: -. UNDER NRC 00497. (1643883) AIRCRAFT WAS GROUNDED
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION ON SIDE ANGLE AT LBL 60 FROM BS 700 - 780, ALSO AT BS 622 AT PAX CABIN. SIDE ANGLE AT LBL 60 FROM BS 700-780, ALSO AT STA 622 AT PAX CABIN WAS REPLACED REPLACE IAW SRM 51-40-02-0G CORROSION LEVEL 2. (1638862) AIRCRAFT WAS GROUNDED
Part: SKIN — DAMAGED (ZONE 100) · airframe 78,387 hrs · 25,878 cycles
PERFORM PERMANENT REPAIR ON LOWER FUSELAGE EXTERNAL SKIN AT STA720.8 STR 28R. LOWER FUSELAGE EXTERNAL SKIN AT STA 720.8 STR 28R WAS REPAIRED PER B757-300 SRM 53-00-01-2R PROCEDURE 29 REPAIR 29. (1636473) AIRCRAFT WAS GROUNDED.
Part: SKIN — DAMAGED (ZONE 100) · airframe 78,387 hrs · 25,878 cycles
PERFORM PERMANENT REPAIR ON LOWER FUSELAGE EXTERNAL SKIN AT BS 720.8, STR 28R. LOWER FUSELAGE EXTERNAL SKIN AT STA 720.8 STR 28R WAS REPAIRED PER B757-300 SRM 53-00-01-2R PROCEDURE 29 REPAIR 29. (1636516) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION LEVEL 2 ON SEAT TRACK RT INBD BTW BS 1280-1289, BTW BS 1289-1320, BTW BS 1320-1360 AT PAX CABIN. SEAT TRACK RH (INBOARD 2 SECTIONS) BTW BS 1280-1320 AND BTW BS 1320-1370 AND ANGLES AT RH SEAT TRACK (INBOARD 2 EAS) BS 1280 TO 1300 AND 1340 TO 1370 AT PAX CABIN WERE REPLACED PER SRM 51-40-02-0G AND IAW SRM 53-60-52-0I PROCEDURE 1. (LP 1634749 - AIRCRAFT WAS GROUNDED)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 78,387 hrs · 25,878 cycles
CORROSION LEVEL 2 ON RH SEAT TRACKS OUT/INBD BTW BS 365 AND BS 377 AT PAX CABIN. REPLACED SEAT TRACKS IAW SRM 51-40-02-0G AND IAW SRM 53-00-52-1A PROCEDURE 1. (LP 1633316 - AIRCRAFT WAS GROUNDED).
Part: STRAP — CRACKED (ZOEN 100) · airframe 78,387 hrs · 25,878 cycles
CRACK ON STABILIZATION STRAPS (3 EAS), 1EA AT STA 345 RBL 44 AT RH TUNNEL, 1 EA BTW BS 365-377, LBL 24, 1 EA AT BS 377 LBL. STABILIZATION STRAPS (3 EAS), WERE REPAIRED PER B757-300 SRM 53-00-51-2R REPAIR 12. (LP 1631967 - AIRCRAFT WAS GROUNDED)
Part: SIGN — INOPERATIVE (ZONE 200) · airframe 78,297 hrs · 25,847 cycles
DURING SVC CHK FOUND AFT GALLEY OVERHEAD EXIT SIGN INOP. RESEATED CONNECTOR & RELAMPED R&R EMER LIGHT POWER SUPPLY AND BATTERY AT M736 IN AFT GALLEY O/H REF B757 AMM 33-51 O/H EXIT SIGN IN AFT GALLEY OPS CHECK OKAY. (8690214) AIRCRAFT WAS GROUNDED
Part: LAMP — INOPERATIVE (ZONE 200) · airframe 77,879 hrs · 25,683 cycles
EMERGENCY LIGHT ABOVE ROW 45ABC INOP. REPLACED BOTH EMERGENCY LIGHTS AT 4L DOOR AND FUSEF3 OF M737 POWER SUPPLY PER B757 AMM 33-51, OPS CHKS GOOD. (8280765)
Earlier reports · 2004–2025 · 175 reports
2025
Part: COVER — DETACHED (ZONE 200) · airframe 77,351 hrs · 25,480 cycles
EMERGENCY LIGHT DAMAGED @ 28E. R & R 28E LIGHT COVER REF B757 AMM 33-52. (8089808)
Part: DOOR FRAME — FOD (ZONE 100) · airframe 77,284 hrs · 25,454 cycles
R1 DOOR WILL NOT ARM. CLEARED DOOR JAMB OF DEBRIS AND RESTOWED LANYARD THAT WAS CAUSING JAM. OPS CHECK NORMAL. (7974692)
Part: PANEL — INOPERATIVE (ZONE 200) · airframe 76,857 hrs · 25,305 cycles
FLIGHT DECK KORRY SWITCH ENTRY DOOR HALF INOPERATIVE. R & R THE ANNUNCIATOR PANEL IAW AMM 31-12. ALL INDICATIONS OPS NML. (7942016)
Part: ARMING LEVER — BINDING (ZONE 800) · airframe 76,831 hrs · 25,297 cycles
R1 SLIDE ARM LEVER STICKY. DOOR WAS SHOWING DISARMED BUT INDICATED ARM DURING OPEN LEVER MOVEMENT. "FWD" LEFT GIRT BAR NOT ENGAGING ON 1R. CORRECTIVE ACTION: FOUND 1R GIRT BAR FWD SLIDER OUT OF POSITION. REPOSITIONED & IR DOOR NOW ARMS/DISARMS NORMALLY. REF. B757 AMM 52-11. (6683785)
Part: INDICATOR — FOD (ZONE 200) · airframe 76,841 hrs · 25,301 cycles
SHIP 5809 DOOR 1R ARMING DOOR SYSTEM IN A " NOT ARMED " POSITION, KNUCKLE KNOCKER WSA GOOD BUT ARMING LIGHT WAS NOT ILLUMINATED. CORRECTIVE ACTION: DEBRIS REMOVED FROM TRACKS OPS CHK A FEW TIMES OK, IAW B757 AMM 52-02. (6683770)
Part: ARMING LEVER — BINDING (ZONE 800) · airframe 76,770 hrs · 25,282 cycles
1R DOOR ARMING LEVER BINDING. REMOVED DEBRIS FROM GIRT LATCHES ON FLOOR OPS NML. (6683754)
Part: GIRT BAR — OVERSERVICED (ZONE 800) · airframe 76,645 hrs · 25,244 cycles
FA REPORTS L1 DOOR UNABLE TO ARM SLIDE. FOUND EXCESSIVE AMOUNT OF GREASE IN GIRT BAR FITTINGS, HENCE RETAINING DEBRIS. REMOVED DEBRIS & GREASE & OPS CHECK ARMING DOOR FUNCTION PER B757 AMM 51-11. (7860996)
Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 76,515 hrs · 25,205 cycles
R2 DOOR SLIDE BOTTLE PRESSURE OUT OF GREEN BAND LOW. REMOVED R2 DOOR ESCAPE SLIDE ASSY PER JIC 2566-9001-2R. INSTALLED DOOR 2R ESCAPE SLIDE AND RAFT ASSY IAW JIC 2566-9001-2R. DOOR 2R ARM/DISARM OK & OPEN/CLOSE NORMAL. DOOR INDICATION CKS OK. VERIFIED PROPER INSTALLED PER AMDS JIC 2566-9001-2R. REQUIRED INSPECTION ITEMS COMPLETED. (7860909)
Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 76,515 hrs · 25,205 cycles
SEATS 24,25,26 WHITE EISLE EMERGENCY LIGHTS OUT. FOUND SUPPLY M11487 TO BE FAULTING. REMOVED AND REPLACED SUPPLY AND BATTERY PER B757 AMM 33-51. OPS NORMAL. (7860910)
Part: SKIN — DAMAGED (ZONE 600) · airframe 76,304 hrs · 25,144 cycles
LIGHTNING STRIKE ON RH WINGLET TIP FAIRING 4.5" FROM LEADING EDGE SKIN PANEL, ON THE VERY TOP. REMOVED LIGHTNING STRIKE DAMAGE PER AVIATION PARTNERS BOEING SRM 57-31-01. (1186653)
Part: WEDGE — DAMAGED · airframe 76,304 hrs · 25,144 cycles
LIGHTNING STRIKE DAMAGE ON TRAILING EDGE WEDGE AT THE TIP. CLEANED OUT LIGHTNING STRIKE DAMAGE PER AVIATION PARTNERS BOEING SRM 57-31-01. (1186664)
Part: SKIN — DAMAGED (ZONE 600) · airframe 76,304 hrs · 25,144 cycles
LIGHTNING STRIKE ON RH WINGLET TIP 8.5" FROM LEAD EDGE SKIN PANEL, ON THE VERY TOP. REMOVED LIGHTNING STRIKE DAMAGE PER AVIATION PARTNERS BOEING SRM 57-31-01. (1186655)
Part: SKIN — DAMAGED (ZONE 600) · airframe 76,304 hrs · 25,144 cycles
LIGHTNING STRIKE ON RT WINGLET TIP FAIRING 17" FROM LEAD EDGE SKIN PANEL, 3" FROM THE TOP. REMOVED LIGHTNING STRIKE DAMAGE PER AVIATION PARTNERS BOEING SRM 57-31-01. (1186660)
Part: LENS — DETACHED (ZONE 200) · airframe 75,735 hrs · 24,942 cycles
SHIP 5809 EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:604. CORRECTIVE ACTION: RE-ATTACHED EMERGENCY LIGHT PANEL PER B757 AMM 33-51. OPS CHECK OF EMERGENCY LIGHT NORMAL. (1065346)
Part: SKIN — DAMAGED (ZONE 100) · airframe 75,399 hrs · 24,817 cycles
SHIP 5809 LIGHTNING STRIKE DAMAGE AT STA720.8 STR 28R TWO HOLES LOCATED SIDE BY SIDE. CORRECTIVE ACTION: REMOVED DAMAGE FROM A/C PER B757-300 SRM 53-00-01-2R-14. PERFORMED HFFC OF CUTOUT AREA PER B757-300 SRM 53-00-01-2R-14. FABRICATED & DRILLED REPAIR DOUBLER PER B757- 300 SRM 53-00-01-02R-14 TREATED AND PRIMED DOUBLER PER SOPM 20- 44-04. DOUBLER. RII, INSTALLED REPAIR DOUBLER PER B757-300 SRM 53-00-01-2R-14. (0992722)
Part: BATTERY PACK — INOPERATIVE (ZONE 200) · airframe 75,404 hrs · 24,820 cycles
SHIP 5809 DURRING 757 CT MOD FOUND SEAT ROWS EMERGENCY LIGHT INOP AT SEAT 33-37. CORRECTIVE ACTION: R/R BATTERY PAK PER B757 AMM 33-51 OPS CK NORMAL. (6752623)
Part: FUSE — INOPERATIVE (ZONE 200) · airframe 75,266 hrs · 24,760 cycles
SHIP 5809 EMERGENCY PATH LIGHTING INOP ROWS 18-23. CORRECTIVE ACTION: T/S PER B757 WDM 33-51-21. REPLACED FUSE F1 ON POWER SUPPLY M11612. LIGHT OPS CKS NML. (7173944)
Part: PROXIMITY SENSOR — FOD (ZONE 800) · airframe 75,266 hrs · 24,760 cycles
SHIP 5809 4R ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHT INOP. CORRECTIVE ACTION: REMOVED DEBRIS FROM AROUND PROX SENSOR. SLIDE LIGHT COMES ON WHEN DOOR IS ARMED. (0951727)
Part: COVER — MISSING (ZONE 200) · airframe 75,151 hrs · 24,715 cycles
SHIP 5809 EXIT SIGN ADJACENT TO DOOR 3 IS MISSING COVER. CORRECTIVE ACTION: RESECURED EXIT SIGN COVER
Part: TRACK — FOD (GIRT BAR) · airframe 74,386 hrs · 24,414 cycles
SHIP 5809 4L SLIDE LIGHT ILLUMINATING INTERMITTENT. CORRECTIVE ACTION: CLEANED DEBRIS FROM GIRT BAR LOCKING TRACK AREA. DOOR AND SLIDE LIGHT OPERATE AS REQUIRED PER B757 AMM 25-66. (6798120)
Part: LINER — DAMAGED (ZONE 800) · airframe 74,356 hrs · 24,402 cycles
SHIP 5809 OVER WING EMERGENCY HATCHES FALLING OFF OF ONE OF THE WINGS AND CONTACTING THE GROUND DURING THE EVACUATION. CORRECTIVE ACTION: FOUND LINING DAMAGED AND HATCH COVER DAMAGED ON THE LT FWD OVERWING DOOR REPAIR LINING REF B757 CMM 25-22 AND REPLACED HATCH COVER REF B757 AMM 25-22. PERFORMED A PRESSURE LEAK TEST PER B757 AMM 05-51-24-702- 001. LEAK CHECK GOOD. (0757306)
Part: ENGINE — FAILED (RIGHT) · airframe 74,386 hrs · 24,414 cycles
ATO- DISCONTINUED TAKEOFF AT 95 KNOTS DUE TO RIGHT ENGINE FAILURE. CORRECTIVE ACTION: REPLACED RIGHT ENGINE. C/W WORK PACKAGE AND NRS. OSD: 2/5/2025
Part: ELEC CONNECTOR — DAMAGED (ZONE 200) · airframe 74,347 hrs · 24,399 cycles
SHIP 5809 ROW 48 CEILING EMERGENCYLIGHT INOP. CORRECTIVE ACTION: INSPECTED CANNON PLUG D00078, PIN 14 MISSING. LOCATED WIRE W6456-0314-20 CAPPED AND STOWED, SECURED INTO POSITION 14 PER B757 WDM 33-51-15. AFT AISLE LIGHT LOWERED CEILING L1120 OPS CKS NORMAL PER B757 AMM 33-51. (5848986)
2024
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 74,099 hrs · 24,295 cycles
SHIP 5809 MULTIPLE EMER LIGHTS INOP IN F/C CABIN. CORRECTIVE ACTION: REMOVED & REPLACED M730 POWER SUPPLY & BATTERY IN FWD GALLEY CEILING. REF B757 AMM 33-51. OPS CK GOOD. (6475375)
Part: LIGHT — MALFUNCTIONED (ZONE 200) · airframe 74,110 hrs · 24,298 cycles
SHIP 5809 SEAT EMER LIGHT INOP AT ROW 14 & LAST ROW. CORRECTIVE ACTION: EMERGENCY LIGHT AT ROW 14 FOUND IN WORKING CONDITION. R/R LIGHT ASSY ON LAST ROW PER B757 AMM 33-51. OPS TEST GOOD. (6475377)
Part: WIRE — BROKEN (ZONE 200) · airframe 74,103 hrs · 24,296 cycles
SHIP 5809 AFT GALLEY PARTITION WALL RED EMER LIGHT INOP. CORRECTIVE ACTION: REPLACED LIGHT ASSY, FOUND BROKEN WIRE UNDER SEAT 45RT. REPAIRED SPLICE. OPS CK GOOD. REF B757 AMM 33-51. (6475376)
Part: SWITCH — OUT OF ADJUST (L1 SLIDE) · airframe 72,994 hrs · 23,909 cycles
SHIP 5809 L1 DOOR SLIDE INDICATION INOP. CORRECTIVE ACTION: FOUND FWD SWITCH S10214 OUT OF ADJUSTMENT, RE ADJUSTED PER B757 AMM 25-66. (5142608)
Part: INDICATOR — MALFUNCTIONED (ZONE 800) · airframe 72,976 hrs · 23,904 cycles
SHIP 5809 SLIDE LIGHT FOR 1L DOOR IS ON & OFF INTERMITTENTLY. CORRECTIVE ACTION: OPERATED SLIDE MULTIPLE TIMES , COULD NOT DUPLICATE FAULT. (5570098)
Part: SENSOR — DIRTY (L1 GIRT BAR) · airframe 72,976 hrs · 23,904 cycles
SHIP 5809 1L SLIDE INDICATOR LIGHT WENT OUT AFTER TAKEOFF. CORRECTIVE ACTION: CLEANED GIRT BAR SENSOR OF DEBRIS AND GREASE. INDICATOR ILLUMINATES NORMAL. (0466497)
Part: INDICATOR — UNKNOWN (SLIDE) · airframe 72,966 hrs · 23,901 cycles
SHIP 5809 SLIDE INDICATOR LIGHT INOP OR DAMAGED / LOCATIONS:601. CORRECTIVE ACTION: LOC 601 SLIDE INDICATOR LIGHT OPS NORMAL. (0464211)
Part: LIGHT — INTERMITTENT (L1 DOOR SLIDE) · airframe 72,811 hrs · 23,856 cycles
SHIP 5809 1L DOOR SLIDE LIGHT INTERMITTENT ENTIRE FLIGHT. CORRECTIVE ACTION: UNABLE TO DUPLICATE TESTED GOOD CLEANED AND LUBED GIRT BAR FITTINGS. 5570032)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,811 hrs · 23,856 cycles
SHIP 5809 EMERGENCY LIGHTS AT ROWS 18-23 INOP. CORRECTIVE ACTION: REMOVED AND REPLACED BATTERY PACK AT M11612 IAW B757 AMM 33-51- 07. LIGHTS CHECK NORMAL. (5570020)
Part: STRAP — CRACKED (BS 377 BL 0) · airframe 72,771 hrs · 23,846 cycles
CRACKED STABILIZER STRAP BS 377 BL0 IN E/E COMPARTMENT. STABILIZER STRAP WAS REPAIRED IAW SRM 53-00-51-2R PROCEDURE 12 REPAIR 12.
Part: INDICATOR — INOPERATIVE (R4 DOOR SLIDE) · airframe 72,389 hrs · 23,717 cycles
SHIP 5809 4R AFT DOOR SLIDE ARM LIGHT NOT ILLUMUNATING. CORRECTIVE ACTION: RESECURED 4R GIRT BAR SENSOR ATTACH. DOOR OPS NML. (5867704)
Part: O-RING — LEAKING (HYD LINE) · airframe 72,321 hrs · 23,690 cycles
SHIP 5809 -MISC/DE- DUE TO CENTER HYDRAULIC SYSTEM QUANTITY INDICATION LOW. CORRECTIVE ACTION: FOUND C2 HYD PUMP PRESSURE LINE O-RING DAMAGED AT CENTER PUMP FILTER MODULE. REPLACED SAME.
Part: GIRT BAR — FOD (L1 DOOR SLIDE) · airframe 71,515 hrs · 23,389 cycles
SHIP 5809 DOOR 1L SLIDE LIGHT INOP WHEN SLIDE ARMED. CORRECTIVE ACTION: CLEARED DEBRIS FROM THE FWD LEFT DOOR GIRT BAR SENSORS AND OPS CHECKED DOOR ARMING SYSTEM PER B757 AMM 25-63. OPS CHECK GOOD. (5149866)
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,223 hrs · 23,284 cycles
SHIP 5809 1L DOOR SLIDE LIGHT INDICATOR INOPERATIVE. CORRECTIVE ACTION: REMOVED AND REPLACED 1L ESCAPE SLIDE ARMED CONDITION INDICATOR LIGHT ASSY PER B757 IPC 33-51. (5088552)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 71,057 hrs · 23,222 cycles
SHIP 5809 1L ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS. CORRECTIVE ACTION: CLEANED DEBRIS FROM GIRT BAR AREA. LUBRICATED DOOR ARMING PIN AT UPPER HINGE. CHK'S GOOD. (0082562)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,723 hrs · 23,096 cycles
SHIP 5809 ROW 28-33 LT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY PACK AT POWER SUPPLY M11383. OPS CK GOOD. OK FOR SVC. REF B757 AMM 33-51. (4603892)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,723 hrs · 23,096 cycles
SHIP 5809 ROW 41-43 LEFT OVERHEAD EMERGENCY LIGHTS INOPERATIVE. CORRECTIVE ACTION: REPLACED EMERGENCY LIGHT POWER SUPPLY M11490 PER B757 AMM 33-51. OPS CK GOOD. OK FOR SVC. (4603891)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,664 hrs · 23,073 cycles
SHIP 5809 PORTION OF EMERGENCY LIGHTS NOT ILLUMINTATED WHEN WE LOST GROUND POWER. CORRECTIVE ACTION: T/S PER WDM B757 33-51. FOUND BATTERY PACK INOP. REMOVED AND REPLAVED BATTERY PACK PER B757 AMM 33-51. (4603868)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,598 hrs · 23,057 cycles
SHIP 5809 DURING SLIDE DEPLOYMENT SAMPLING EMERGENCY LIGHTS FAILED TO ILLUMINATE TILL SLIDE DEFLATED AND RELEASED FROM GIRT BAR. CORRECTIVE ACTION REMOVED AND REPLACED 3R DOOR ESCAPE SLIDE PER AMDS CARD 2566-9002-3R. (2989234)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,605 hrs · 23,059 cycles
SHIP 5809 -MISC/DE- INTO DTW DUE RIGHT HYD QTY LOSS. CORRECTIVE ACTION: SECURED LOOSE B NUT ON RIGHT T/R HYDRAULIC LINE, REPLACED RT HYD SYS ACMP CASE DRAIN FILTER. LEAK CHECK GOOD.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,299 hrs · 22,976 cycles
SHIP 5809 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS: G1A. CORRECTIVE ACTION: REMOVED AND REPLACED POWER SUPPLY PER B757 33-51 OPS CHK GOOD OK FOR SVC. (2921410)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,299 hrs · 22,976 cycles
SHIP 5809 EMERGENCY LIGHTS AND OVHD LTS AT DOORS 1L/R AND 2L/R AND IN BETWWEN FLICKERING ON AND OFF THROUGHOUT FLIGHT. CORRECTIVE ACTION: REMOVED AND REPLACED EMERGENCY BATTERY PACK M730. REF B757 AMM 33-51 LIGHTS CHECK GOOD. OK FOR SERVICE. (9966164)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,271 hrs · 22,969 cycles
SHIP 5809 SMOKE+FUMES IN CABIN REPORTED BY FA. PILOTS COMLIED IAW QRH 8.4 NOTE: SMOKE+FUMES OCCURRED SIMULTANEOUSLY W/ R PACK TEMP EICAS. CORRECTIVE ACTION: T/S RT PACK TEMP MSG OPENED RT PACK BAY FOUND RT ACM SIEZED. R/R RT PACK LOW LIMIT VLV PER B757 MM21-51. R/R RT REHEATER PER B757 MM 21-51. RPLD RT ACM REF B757 MM 21-51. OPS AND LK CK GOOD. NO SMOKE/SMELLS. (9966135)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 70,138 hrs · 22,935 cycles
SHIP 5809 1L ENTRY DOOR SLIDE LIGHT INOP. CORRECTIVE ACTION: CYCLED ARM /DISARM LEVER . OPS CK. GOOD. REF. B757 25-66. (4651354)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,768 hrs · 22,833 cycles
SHIP 5809 -DIV- TO MSP DUE TO LEFT AND RIGHT BLEED OFF INDICATION WITH ANTI-ICE SELECTED, RAN QRH. CORRECTIVE ACTION: T/S R/R RT ENGINE HPSOV AND REPLACED BOTH OVER TEMP SENSOR & FATS, LEAK CHECK GOOD. C/W NO GO ODI STEPS.
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,373 hrs · 22,724 cycles
SHIP 5809 R4 DOOR, CATERING LEFT HANDLE OUT JAMMING AGAINST FUSELAGE. CORRECTIVE ACTION: FREED OUTSIDE HANDLE. - CLOSED DOOR. NO DAMAGE TO SKIN. B757 AMM 52-11. (4706232)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 69,354 hrs · 22,717 cycles
SHIP 5809 DOOR ARMED KNUCKLE KNOCKER INOPERATIVE / LOCATIONS:612. CORRECTIVE ACTION: ADJUSTED DOOR 4R LOWER LINING IAW B757 AMM 52-11. NOW KNUCKLE KNOCKER OPS OK. (2753070)
Part: NONE — NONE · airframe 68,765 hrs · 22,506 cycles
SHIP 5809 RT EMERGENCY ESCAPE SQUIB TEST 2 (BTL PRESSURE) NOT TESTING. CORRECTIVE ACTION: /S PER B757 FIM 25-65 TASK 803. FOUND BTL PRESSURE GOOD. REF B757 WDM 25-65-21. RESEATED CONNECTOR D5542. OPS NOW NML. TEST GOOD. (9497269)
Part: NONE — NONE · airframe 68,750 hrs · 22,499 cycles
SHIP 5809 - MISC/DE - DUE TO TRAILING EDGE LOCK OUT WITH A TRAILING EDGE DISAGREE MSG ON APPROACH. CORRECTIVE ACTION: C/W NO-GO PROCEDURES. RETURNED FLAPS TO UP POSITION ELECTRICALLY. CYCLED FLAPS HYDRAULICALLY TWICE WITH NO ISSUES.
Part: NONE — NONE · airframe 68,509 hrs · 22,391 cycles
SHIP 5809 WHILE WORKING AMDS W/C 2566-9201-3R, R3 DOOR SLIDE FAILED TO DEPLOY. CORRECTIVE ACTION: REMOVED AND REPLACED R3 SLIDE PER AMDS W/C 2566-9201-3R. (2606631)
Part: DOOR — OUT OF SEQUENCE (MAIN PAX) · airframe 68,351 hrs · 22,325 cycles
SHIP 5809 R AFT PAX DOOR WILL NOT CLOSE-GUST LOCK STUCK. CORRECTIVE ACTION: DOOR OUT OF SEQUENCE BY CATERING-RESEQUENCED DOO-OPS NML PER B757AMM 52-11. (9730268)
2022
Part: LENS — DETACHED (EMERGENCY LIGHT) · airframe 68,245 hrs · 22,277 cycles
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED OR MISSING / LOCATIONS:2 L. CORRECTIVE ACTION: REATTACHED 2L EMERGENCY LIGHT COVER.
Part: UNKNOWN — ODOR (CABIN) · airframe 68,075 hrs · 22,200 cycles
SHIP 5809 SMELLED FUMES "DIRTY SOCK" SMELL ON SHORT FINAL 7000FT - PARKING , BOTH ON ENGINE BLEED AND APU. 1L FA ALSO SMELLED IT. MAINT. PERF PER NOGO ODI ATA 2172 + T/S PER B757 FIM 21-00-01. FOUND DE-ICE FLUID INSIDE APU COMP + APU INLET. REMOVED SOME. INSPECTED 2.5 BLEED BOTH ENGINE NO OIL NOTED. INSPECTED COMPRESSOR DISCHARGE DUCT NO OIL NOTED. PERFORMED OIL CONTAMINATION REMOVAL FROM AC + PNEU. SYS. PER B757 FIM 21-00-01 . R/R BOTH RECIRC FILTER REF B757 AMM 21-25. INSPECTED APU INLET PLENUM NO FLUID NOTED. C/W MCC REQUEST LOG 2524033 HIGH POWER RUN COMPLETE REF B757 AMM 71-00.
Part: SQUIB — NO TEST · airframe 68,031 hrs · 22,183 cycles
SHIP 5809 RT EMERGENCY ESCAPE SQUIB TEST 2 NOT ILLUMINATING. CORRECTIVE ACTION: T/S PER FIM 25-65 BOTH LEFT AND RIGHT EMERGENCY ESCAPE SQUIB TEST 1 AND 2 SEVERAL TIMES. COULD NOT DUPLICATE THE FAULT. (9006698)
Part: SQUIB — NO TEST · airframe 68,031 hrs · 22,183 cycles
SHIP 5809 DURING SVC CHK FOUND R EMER ESCAPE SQUIB TEST 2 ( BTL PRESS) NOT ILLUMINATING. CORRECTIVE ACTION: T/S PER FIM 25-65 TASK 803. BOTH LEFT AND RIGHT EMERGENCY ESCAPE SQUIB TEST 1 AND 2 TEST OK. COULD NOT DUPLICATE FAULT.
Part: PROXIMITY SENSOR — MALFUNCTIONED (GIRT BAR) · airframe 67,975 hrs · 22,162 cycles
SHIP 5809 2R DOOR IN DISARMED POSITION SHOWS SLIDE LIGHT ILLUMINATED. CORRECTIVE ACTION: REMOVED AND REPLACED DOOR 2R (AFT) GIRT BAR PROXIMITY SENSOR PER B757 AMM 25-66. OPS CHECK GOOD AT THIS TIME. (9006668)
Part: LIGHT — INOPERATIVE (SEAT 41D) · airframe 67,975 hrs · 22,162 cycles
SHIP 5809 PAX SEAT 41D SEAT MOUNTED EMER. LIGHT INOP. CORRECTIVE ACTION: REMOVED AND REPLACED PAX SEAT 41D SEAT MOUNTED EMERGENCY LIGHT PER B757 AMM 33-51. OPS CHKS GOOD. (9006664)
Part: COVER — MISSING (SLIDE LIGHT) · airframe 67,975 hrs · 22,162 cycles
SHIP 5809 R2 DOOR SLIDE LIGHT ARMED COVER MISSING AND LIGHT INOP. CORRECTIVE ACTION: REPLACED SLIDE LIGHT ASSY. OPS CK GOOD. (9006660)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,948 hrs · 22,153 cycles
DURNING SVC CHK, FOUND MULTIPLE AFT CABIN EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS M11489 & M11490 IAW AMM 33-51. OPS CHECKED GOOD.
Part: GIRT BAR — OUT OF ADJUST (DOORS) · airframe 67,928 hrs · 22,138 cycles
DURING INSPECT GIRT BAR MECHANISM ADJUSTMENT WERE FOUND OUT LIMITS ON DOORS R4, L1 AND R1. GIRT BAR MECHANISM ADJUSTMENT & TEST PERFORMED ON DOORS R4, L1 AND R1 PER AMM 52-11-25 AND TESTED OK.
Part: SNUBBER — OUT OF LIMITS (L2 DOOR) · airframe 67,925 hrs · 22,137 cycles
L2 DOOR LENGTH OF ROTARY SNUBBER PIN IS OUT LIMITS IN REFERENCE AMDS. SNUBBER AT L2 DOOR WAS REPLACED PER B757-300 AMM 52-11-10. (2487099)
Part: SNUBBER — OUT OF LIMITS (L1 DOOR) · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 L1 DOOR LENGHT OF ROTARY SNUBBER PIN IS OUT LIMITS IN REFERENCE TASK CARD. CORRECTIVE ACTION: SUMMARY OF NRC S/N 00187: ROTARY SNUBBER WAS REPLACED PER B757 -300 AMM 52-11-10. (2486981)
Part: NONE — NONE · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 FWD SPRING ON GIRT BAR DOESN'T RETAIN IN SLIDER AT 1R DOOR. PTAS. CORRECTIVE ACTION: SUMMARY OF NRC 00082: FWD RETAINER SPRING OF PASSENGER DOOR 1R GIRT BAR WAS REPLACED PER B757-300 SRM. GIRT BAR WAS MESURED AND FUNCIONAL CHECK WAS PERFORMED PER A.A. (2484415)
Part: SPRING — OUT OF LIMITS · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 FWD SPRING ON GIRT BAR DOESN T RETAIN IN SLIDER, ALSO AFT SPRING NO GO TEST OUT OF LIMIT AT 4R DOOR. PTAS . CORRECIVE ACTION: SUMMARY OF NRC 00081: BOTH RETAINERS SPRINGS AT PASSENGER DOOR 4R GIRT BAR WERE REPLACED PER B757-200 SRM. (2483748)
Part: NONE — NONE · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 AFT SPRING ON GIRT BAR DOESN'T RETAIN IN SLIDER AT 2L DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00083: AFT RETAINER SPRING AT PASSENGER DOOR 2L WAS REPLACED PER B757-200 SRM. GIRT BAR WAS MESURED AND FUNCIONAL CHECK WAS PERFORMED PER A.A. (2483750)
Part: NONE — NONE · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 CRACKED LH STABILIZER STRAP BTW STA 365 TO STA 395 ABOVE NLG W/W (E&E). CORRECTIVE ACTION: SUMMARY OF NRC 00251: LH STABILIZER STRAP BTW STA 365 TO STA 395 WAS REPAIRED PER. ER/A 384483-14MA REV D. (2482535)
Part: PLATE — CORRODED (GIRT BAR RETAINR) · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 CORROSION ON GIRT BAR RETAINER PLATE AT 2L DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00097: PLATE ON GIRT BAR AT 2L DOOR WAS REPLACED PER B757-300 SRM. (2472545)
Part: PLATE — CORRODED (GIRT BAR RETAINR) · airframe 67,925 hrs · 22,137 cycles
SHIP 5809 CORROSION ON GIRT BAR RETAINER PLATE AT RL DOOR. CORRECTIVE ACTION: SUMMARY OF NRC 00098: PLATE ON GIRT BAR AT 2L DOOR WAS REPLACED PER B757-300 SRM. (2472456)
Part: NONE — NONE · airframe 67,778 hrs · 22,088 cycles
SHIP 5809 - FCNT - DUE TO A FLAP DISAGREE MSG AND A LE DISAGREE MSG AFTER COMPLETING THE QRH FOR THE FLAPS. CORRECTIVE ACTION: PERFORMED BITE CHECK ON ALL FSEUS. NO FAULTS. CYCLED FLAPS MULTIPLE TIMES WITH NO FAULTS. C/W NO-GO PROCEDURES.
Part: NONE — NONE · airframe 67,682 hrs · 22,057 cycles
SHIP 5809 EMERGENCY EXIT SIGN COVER LOOSE / LOCATIONS:38C. CORRECTIVE ACTION: RESECURED EXIT SIGN--CKS OK. (2416146)
Part: NONE — NONE · airframe 66,968 hrs · 21,825 cycles
SHIP 5809 4R DOOR GRIT BAR WON'T ARM. CORRECTIVE ACTION: INSPECTED REF B757 AMM 25-66. REMOVED DEBRIS. OPS NML. (9233118)
Part: LIGHT — INOPERATIVE · airframe 66,864 hrs · 21,782 cycles
SHIP 5809 ROW 41 SEAT MOUNTED EMER LIGHT INOP. CORRECTIVE ACTION: REMOVED & REPLACED SEAT MOUNTED EMER ASSY REF B757 WDM 33-52. OPS CK GOOD. (8306951)
Part: COVER — DETACHED · airframe 66,864 hrs · 21,782 cycles
SHIP 5809 EXIT SIGN COVER DETACHED FROM ABOVE DOOR. CORRECTIVE ACTION: RE-SECURED AISLE EMER EXIT SIGN COVER AS NECESSARY. SECURITY CK'S GOOD. (8306948)
Part: GCU — FAULT MESSAGE · airframe 66,740 hrs · 21,740 cycles
SHIP 5809 (MISC/DE) A/T DISCONNECTED SERVAL TIMES ON FINAL APPROACH, VARIOUS EICAS MESSAGES ON, FINALLY LEFT GEN OFF. AFTER STARTING APU ONLY L GEN OFF EICAS REMAINED. CORRECTIVE ACTION: T/S REPLACED L GCU PER B757 AMM 24-22. OPS CK GOOD. C/W STEP 1-4 OF NO GO ODI PREVENTION REMOVED AND REPLACED LT ENG IDG PER B757 AMM 24-11. OPS AND LK CK GOOD. INSTALLED SERVICEABLE FEEDER HARNESS.
Part: NONE — NONE · airframe 66,191 hrs · 21,563 cycles
SHIP 5809 - PRES - EMERGENCY DESCENT DUE TO LOSS OF PRESSURIZATION. FLIGHT CONTINUED TO DESTINATION. CORRECTIVE ACTION: REPLACED RELAYS K21 AND K10646. MTC FOUND LT HIGH STAGE VALVE STICKING. REPLACED HIGH STAGE VALVE, FAN AIR TEMP SENSOR, AND REVERSE CONTROLLER. C/W NO-GO PROCEDURES.
2021
Part: NONE — NONE · airframe 65,362 hrs · 21,305 cycles
SHIP 5809 AFT OVERHEAD AISLE EMERGENCY EXIT SIGN INOP. CORRECTIVE ACTION: T/S PER B757 WDM 33-51 ON PLUG D4522 PWR SUPPLY (M736) PIN 8 GND GOOD, NO VOLTAGE PIN 7 FUSE BLOWN ON PWR SUPPLY. REPLACED FUSE CONTINUES TO BLOW. PWR SUPPLY PLUG D78 PINS 13 & 14 SHARE THE SAME FUSE. PIN 14 GOES TO AISLE LIGHT (L1120) WHEN CHECKED IT IS GROUNDED. PER AA 2500-01799 THIS LIGHT HAS BEEN REMOVED, WIRES CAPPED AND STOWED. REMOVED PIN 14 FROM PLUG D78, CAPPED & STOWED PER AA 2500-01799 R2 PWR SUPPLY SYS CK GOOD. PER B757 AMM 33-51. (8354474)
Part: UNKNOWN — UNKNOWN · airframe 64,697 hrs · 21,121 cycles
SHIP 5809 4R DOOR HARD TO ARM.KNUCKLE KNOCKER NOT POPPING INTO POSITION. CORRECTIVE ACTION: INSPECTED 4R DOOR GIRT BAR FITTINGS AND SURROUNDING AREAS. FOUND DEBRIS. REMOVED SAME. OPS CHK OF 4R DOOR SLIDE ARM & DISARM CHKS GOOD. (1987964)
Part: NONE — NONE · airframe 64,487 hrs · 21,066 cycles
SHIP 5809 2L SLIDE ARM LIGHT NOT ILLUMINATING. CORRECTIVE ACTION: RELAMPED, REMOVED AND REPLACED NO 2 PASS DR PROX SNSR-B S10219 PER B757 AMM 25-66 AND WDM 25-66-11. OPS CK GOOD. (8189602)
Part: OXYGEN BOX — OPEN (SEAT 25DEF) · airframe 64,349 hrs · 21,033 cycles
SHIP 5809 25DEF O2 DOOR POPPED OPEN UNABLE TO STOW MASKS + CLOSE. CORRECTIVE ACTION: STOWED MASKS AND LATCHED PANEL CLOSED. (8071648)
Part: GUST LOCK — DAMAGED (R4 DOOR) · airframe 64,166 hrs · 20,983 cycles
SHIP 5809 WHILE WORKING R4 SLIDE FOUND GUS LOCK BEARING DAMAGED. CORRECTIVE ACTION: INSTALLED A SERVICEABLE DOOR 4R GUST LOCK BEARING REF B757 AMM 52-11. DOOR GUST LOCK OP'S NORMAL. (7885574)
2020
Part: FLOOR SUPPORT — CORRODED (BS 653) · corrosion level 2 · airframe 61,746 hrs · 20,025 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGERS LBL 16.10, LBL 10.45, LBL 7.55 ALSO RBL 2.90, RBL 7.55, AND RBL 16.10, STA 653 AT FWD CARGO COMPARTMENT. STRINGER REPAIRED PER SRM.
Part: FLOOR SUPPORT — CORRODED (FWD CARGO BAY) · corrosion level 2 · airframe 61,746 hrs · 20,025 cycles
DURING INTIAL INSPECTION FOUND CORROSION LEVEL 2 ON FLOOR STRINGER SUPPORTS FROM STA 780+140/780+148 , 10.45 AND 16.10 LT AT FWD CARGO COMPARTMENT. FLOOR STRINGER SUPPORT REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 780) · corrosion level 2 · airframe 61,746 hrs · 20,025 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGERS RBL 2.90, RBL 7.55 AND RBL 10.45, BETWEEN STA 780 +140 AND 780 +148 AT FWD CARGO COMPARTMENT. STRINGER REPAIRED PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 780) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGERS RBL 10.45 AND RBL 16.10, BETWEEN STA 780 + 60 TO 780 + 70 AT FWD CARGO COMPARTMENT. STRINGERS WERE REPAIRED, PER SRM.
Part: FRAME — CRACKED (BS 1681) · airframe 61,745 hrs · 20,024 cycles
WHILE PERFORMING AN INSPECTION FOUND A CRACK ON INBOARD FASTERNER HOLE OF FRAME 1681 LOWER SECTION JUST BELOW WL 208, RIGHT SIDE. THE FRAME STA 1681 LOWER SECTION WAS REPAIRED, PER ER/A 588552-14AD.
Part: FLOOR SUPPORT — CORRODED (BS 1360-1380) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGERS 7.55 AND 16.10 RT FROM STA 1360/1380 AT AFT CARGO COMPARTMENT. FLOOR STRINGER REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1515) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND CORROSION LEVEL 2 ON FLOOR STRINGER RBL 7 STA 1515 AT AFT CARGO COMPARTMENT. FLOOR STRINGER REPLACED PER SRM.
Part: SPAR — DAMAGED (RT WING) · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND A TOOL MARK ON UPPER FILLET INTERIOR AREA STA WBL 740 FRONT SPAR RT WING. REPAIRED PER ERA 588364-14.
Part: FLOORBEAM — CORRODED (BS 749) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON STRINGERS FLOOR SUPPORT RBL AND LBL 2.90, 7.55, 10.45, 16.10, STA Y= 749. BELOW NUTS (C-1). FLOOR STRINGERS REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 660-680) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION MAINTENANCE FOUND LEVEL 2 CORROSION ON FLOOR STRINGER RBL 2.90 STA 660-680 AT FWD CARGO COMPARTMENT. FLOOR STRINGER REPLACED PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1510) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSEPCTION FOUND CORROSION LEVEL 2 ON FLOOR STRINGER LBL 2 STA.1510 AT AFT CARGO COMPARTMENT (CCT). STRINGER REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1470) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION FOUND CORROSION LEVEL 2 ON FLLOR STRINGER STA 1470 RBL 10 AT AFT CARGO COMPARTMENT (CCT). STRINGER REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1470) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION FOUND CORROSION LEVEL 2 ON FLOOR STRINGER LBL 7 STA 1470 AT AFT CARGO COMPARTMENT (CCT). STRINGER WAS REPAIRED, PER SRM.
Part: FRAME — DAMAGED (BS 1280) · airframe 61,745 hrs · 20,024 cycles
AFTER BLEND OUT AREA ON BEAM AT STA 1280 BETWEEN STR 9/10 RT THICKNESS ON FRAME STA 1280 BETWEEN S-9/10 RT WAS FOUND OUT OF LIMITS, NOM THICKNESS WAS 0.080" REMAINING THICKNESS IS 0.030. FRAME WAS REPAIRED, PER ERA 588417-14AD.
Part: FLOOR SUPPORT — CORRODED (BS 1510-1518) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION CORROSION LEVEL 2 FOUND ON FLOOR STRINGER RBL 2 FROM STA 1510 TO 1518 AT AFT CARGO COMPARTMENT (CCT). STRINGER REPAIRED, PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1510-1518) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INSPECTION FOUND CORROSION LEVEL 2 ON FLOOR STRINGER LBL 7 FROM STA .1510 TO 1518 AT AFT CARGO COMPARTMENT (CCT). STRINGER REPLACED, PER SRM.
Part: FLOORBEAM — CORRODED (BS 549) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION FOUND LEVEL 2 CORROSION ON FLOOR STRINGERS LBL 7.55 AND LBL 10.45, STA 549 AT FWD CARGO COMPARTMENT. STRINGERS REPLACED, PER SRM.
Part: INTERCOSTAL — CORRODED (BS 680-700) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
AFTER BLEND OUT AREA ON INTERCOSTAL STA Y=680 700 S28L THICKNESS WAS FOUND OUT OF LIMITS. CORROSION LEVEL 2, INTERCOSTAL WAS REPAIRED PER SRM.
Part: PANEL — CORRODED (CABIN) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION FOUND CORROSION LEVEL: 2 ON LT SIDEPLATE FROM STA 1410 TO 1530 AT AFT CARGO COMPARTMENT (CCT) SIDE PANEL REPLACED.
Part: SEAT TRACK — CORRODED (CABIN) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
CORROSION LEVEL 2, DURING INITIAL INSPECTION CORROSION ON SEAT TRACK FROM STA 1290/1365 AND 25 RBL AT PASSENGER CABIN (W3). REPAIRED PER SRM.
Part: FLOOR SUPPORT — CORRODED (BS 1661-1681) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
CORROSION LEVEL 2 DURING INITIAL INSPECTION. CORROSION FLOOR SUPPORT CHANNEL FROM STA 1661/1681 AND 0 BL AT PASSENGER CABIN W40. FLOOR SUPPORT REPLACED.
Part: STRAP — CRACKED (FUSELAGE) · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION:CRACK ON FLOOR BEAM STABILIZER STRAP AT STA 1651 AND RBL 25, W4. STRAP REPAIRED, PER SRM 53-00-51.
Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 61,745 hrs · 20,024 cycles
CORROSION LEVEL: 2 DURING INSPECTION FOUND CORROSION ON UPPER CHORD BEAM, STA 365.25 BETWEEN BL 0 TO RBL 2 AT FLOOR PASSENGER CABIN STRUCTURE. REPARIED PER ERA 588248-14.
Part: STRAP — CRACKED (BS 1640) · airframe 61,745 hrs · 20,024 cycles
DURING INITIAL INSPECTION FOUND CRACKED STABILIZATION STRAP STA 1640 LBL=28 AT AFT CARGO COMPARTMENT. STABLIZER STRAP WAS REPAIRED, PER SRM 53-00-51.
Part: STRAP — CRACKED (BS 700-720) · airframe 61,745 hrs · 20,024 cycles
DURING INSPECTION FOUND CRACK ON STABILIZATION STRAP BETWEEN STA 700 TO STA 720 RBL 45 AT PASSENGER CABIN FLOOR STRUCTURE. STRAP REPAIRED, PER SRM 53-00-51.
Part: SKIN — DENTED (BS 600-640) · airframe 61,745 hrs · 20,024 cycles
DURING INSPECTION FOUND A DENT ON FUSELAGE SKIN AND INCOMING REPAIR AT STA 600-640 BETWEEN S-15LAND S-18L. REPAIRED PER ERA 525966-14.
Part: FLOOR PANEL — DENTED · airframe 61,745 hrs · 20,024 cycles
DURING INSPECTION FOUND PUNCTURES AND DENTS ONFLOOR PANEL #220-2, 220-3, 220-7, 220-12 AT PAX CABIN. FLOOR PANELS 220-3, 220-7, 220-12 WERE REPAIRED PER SRM 53-00-50 AND FLOOR PANEL 220-2 WAS FABRICATED AND REPLACED.
Part: STRAP — CRACKED (BS 364-377) · airframe 61,745 hrs · 20,024 cycles
DURING INIITAL INSPECTION FOUND CRACK ON STABILIZER STRAP FROM STA 365/377 AND 45 LBL AT PASSENGER CABIN (W1). REPAIRED PER SRM.
Part: TARGET — OUT OF ADJUST (PAX DOOR) · airframe 61,301 hrs · 19,882 cycles
UPON LANDING IN ATLANTA "LEFT AFT ENTRY DOOR" CAUTION LITE ILLUMINATED. ADJ TARGET/ SENSOR GAP PER B757 AMM 52-71. PROX BOX SENSOR NOW READS "NEAR" WITH DOOR CLOSED.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,296 hrs · 19,880 cycles
SHIP 5809 EMERGENCY LIGHTS ROW 1-6, 18-23 AND 27-32 INOP. CORRECTIVE ACTION: R/R BATTERY PACKS M730, M731 AND M733 IAW B757 AMM 33-51, ROWS 1-6 AND 18-23 OPS CHECK NORMAL. R/R BATTERY PACK M735 IAW B757 AMM 33-51, ROWS 27-32 OPS CHECK NORMAL. (6963440)
2019
Part: NONE — NONE · airframe 65,659 hrs · 21,410 cycles
SHIP 5809 HIS ER/A 564381-14 INCORPORATES FAA FORM 8110-3. ACCOMPLISH SECTION II INSPECTION INSTRUCTIONS. THE SUBJECT ER/A IS NOW AT REV. C. CORRECTIVE ACTION: REF ERA 564381-14AD REV C. (1122743)
Part: LIGHT — MISSING (CABIN) · airframe 58,193 hrs · 18,984 cycles
(AIRCRAFT 5809, L/P 5917702) UNDER SEAT EMERGENCY LIGHT AT SEAT 30D MISSING. REPLACED EMEGENCY LIGHT AT 30D IAW AMM 33-51 OPS CKS GOOD.
Part: GIRT BAR — UNSECURE (L4 DOOR) · airframe 57,065 hrs · 18,655 cycles
4L DOOR SLIDE WOULD NOT ARM. SECURED GIRT BAR AND OPS CHK PER AMM 52-11.
Part: TERMINAL — MALFUNCTIONED (WINDOW) · airframe 56,941 hrs · 18,616 cycles
SHIP 5809 ON CLIMB OUT OF SEA NOTICED LEFT WINDOW (CAPT) ELECTRICALTERMINAL GLOWING RED WITH LIGHT ELECTRICAL SMELL. TURNED OFF LEFT FWD WINDOW HEAT AND SMELL AND GLOWING TERMINAL EXTINGUISHED. CORRECTIVE ACTION: REMOVED NR 1 LEFT WINDOW & REPLACED WIRE D3326 A-AC PER WDM 30-41-11. TERMINATED WIRE WDM 30-41-11. REPLACED NR 1 LEFT WINDOW REF AMM 56-11, ACCOMPLISHED ALL 3 TORQUES & APPLIED SEALANT. WIRE HOOK UPS & OPS CK GOOD. AMM 30-41. (4980996)
2018
Part: GROUND STUD — DAMAGED (EMERGENCY LIGHTS) · airframe 56,161 hrs · 18,398 cycles
(AIRCRAFT 5809, L/P 4704670) EMERGENCY EXIT LIGHTS STAY ON WITH FLIGHT DECK SWITCH IN OFF POSITION. SUSPECT FLIGHT DECK SWITCH. REPAIRED BAD GROUND AT F/A PANEL IAW SWPM CH. 20. E-LITES CK OK AT THIS TIME.
Part: CONNECTOR — ARCED (L1 WINDOW) · airframe 55,779 hrs · 18,288 cycles
SHIP 5809 -FIRE- PRIOR TO DEPARTURE MOMENTARY FLAME AND ARCING FROM L-1 WINDOW CONNECTOR. CORRECTIVE ACTION: REPLACED L1 WINDOW AND WINDOW HEAT CONTROLLER OP CKS NML (4562108)
Part: LIGHT — INOPERATIVE (L2 DOOR) · airframe 55,108 hrs · 18,123 cycles
2L DOOR "ARMED" LITE EXTINGUISHED INFLIGHT. REMOVED AND REPLACED 2L DOOR ARM LIGHT BULBS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 54,261 hrs · 17,892 cycles
EMERGENCY LIGHT AT 24D IS INOP. R&R SEAT MOUNTED EMERGENCY LIGHT FIXTURE PER AMM 33-51.
Part: ATTACH BOLT — LOOSE (L4 DOOR) · airframe 54,253 hrs · 17,889 cycles
AT DEPARTURE CABIN SERVICE COULD NOT CLOSE THE L4 DOOR. FOUND LOWER GUIDE ARM SERRATED PLATE ATTACHED BOLTS LOOSE. SECURE BOLTS CHCK NML PER AMM 52-11.
Part: BATTERY PACK — NOT REPORTED · airframe 54,162 hrs · 17,862 cycles
R3 DOOR, REMOVED THE BATTERY. INSTALLED A NEW EMERGENCY BATTERY PACK, OPS CHECKED GOOD IAW AMM 33-51-07.
Part: LENS — LOOSE (EMERGENCY LIGHT) · airframe 54,162 hrs · 17,862 cycles
OVERWING EXIT SIGN COVER FALLING OFF ON THE LEFT SIDE OF AIRCRAFT. SECURED THE OVERWING EXIT SIGN.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,140 hrs · 17,852 cycles
DURING SERVICE. FOUND THE R2 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK ON POWER SUPPLY M11612 IAW AMM 33-51.
2017
Part: SKIN — GOUGED (BS 600-620) · airframe 53,290 hrs · 17,578 cycles
THREE GOUGES FOUND IN THE SKIN THAT ARE OUT OF LIMITS AT BS 600 - 620, BETWEEN STRINGER 1 & 2R. APPROXIMATELY FOUR INCHES FROM THE NR 4 LUG DOUBLER. COMPLIED WITH ERA 564381-14, REV A.
Part: LIGHT — BROKEN (SEAT 22) · airframe 53,281 hrs · 17,574 cycles
(AIRCRAFT 5809, L/P 4134764) 22E EMERGENCY LIGHT ASILE ILLUMINATION SUPPORT BROKEN. REPLACED EMERGENCY LIGHT ASSY AT SEAT 22E PER B757 AMM 33-51.
Part: WIRE — MISINSTALLED (LIGHT SWITCH) · airframe 50,282 hrs · 16,658 cycles
EMERGENCY EXIT LIGHTS TURN ON WITH THE SWITCH IN OFF POSITION. FOUND A WIRE FROM D10968 PIN E16 TO S6 ON THE EMERGENCY LIGHT SWITCH ON WRONG TERMINALS. CORRECTED THE PROBLEM, OPS TEST OK IAW AMM 33-51-00. AND WDM 33-51-11, PG1, SH1.
Part: FITTING — CORRODED (PARTITIONS) · airframe 53,357 hrs · 17,602 cycles
AFT PARTITION AT THE R1 DOOR, CREW REPORTED THAT THE PARTITION LOWER FLOOR ATTACHMENT FITTINGS, ONE COVER MISSING AND THE OTHER COVER BENT. DUE TO CORROSION ON FLOOR MOUNTING PLATES. REPLACED 2 WINDSCREEN FITTING COVERS ON AFT SIDE OF FWD GALLEY RT SIDE WINDSCREEN PER B 757 AMM 25-24. (9112542)
2016
Part: CRANK ASSY — DEFECTIVE (L2 DOOR) · airframe 49,660 hrs · 16,458 cycles
DOOR 2L JAMMED UNABLE TO OPEN. PREFORMED RII FOR L2 DOOR GIRT BAR REPLACEMENT PER AMM 25-66. REPLACED AND ADJUSTED AFT GIRT BAR CRANK PER AMM 52-11. REMOVED AND STOWED SLIDE SAFETY PIN. INSPECTED L2 GIRT BAR CRANK INSTALLATION PER AMM 52-11. VERIFIED SAFETY PIN REMOVED. RII COMPLETE.
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 2 · airframe 49,162 hrs · 16,295 cycles
CORROSION ON AFT CARGO COMPARTMENT R/H SIDE FLOOR PANEL, STA 1400-STA 1420. CORRECTIVE ACTION: ACCOMPLISHED PERMANENT REPAIR ON AFT CARGO COMPARTMENT R/H SIDE FLOOR PANEL STA 1400-STA 1420 IAW ER/A 547306-14 REV ORIG. (2703165)
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 49,138 hrs · 16,288 cycles
R2 DOOR EXTERIOR EMERGENCY EXIT SLIDE LIGHT INOPERATIVE. REMOVED AND REPLACED THE BULB IAW AMM33-51-06-962-001-002. OPS CHECK GOOD.
Part: SEAL DEPRESSOR — GOUGED (L4 DOOR) · airframe 49,138 hrs · 16,288 cycles
L4 DOOR CUTOUT, INNER UPPER SURFACE HAS GOUGE DAMAGE. BLENDED GOUGED ON L4 DOOR INNER UPPER SURFACE IAW SRM 53-60-15 ALLOWABLE DAMAGE 1. FABRICATED SEAL DEPRESSOR AND INSTALLED IAW SRM 51-40 -02 PG 3-4.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 49,138 hrs · 16,288 cycles
EMERGENCY EXIT LIGHT INOPERATIVE ON SEAT 23 DEF. TROUBLESHOT EMERGENCY LIGHT AND FOUND ONE GROUND WIRE BROKEN. REPAIRED BROKEN WIRE IAW SWPM 20-10-3 PAGE 7 TO 9, AND WDM 33-51-21 PG 1 SH3. PERFORMED EMERGENCY LIGHTS OPS TEST, TESTED GOOD.
Part: LENS — WRONG PART (EMERGENCY LIGHT) · airframe 47,169 hrs · 15,625 cycles
L2 DOOR AFT EMERGENCY EXIT SIGN HAS THE WRONG LENS INSTALLED. INSTALLED NEW LENS AT DOOR 2L AFT EMERGENCY EXIT SIGN, OPS CKS NORMAL.
Part: STRINGER — DAMAGED (BS 720-760) · airframe 46,781 hrs · 15,477 cycles
TWO LIGHTNING STRIKES ON CROWN OF FUSELAGE BETWEEN BS 720 AND 760. DRILLED OUT DAMAGE IAW SRM 53-00-01. REPAIR 6, SECTION 1, PARA 3. PERFORMED BHEC INSPECTION IAW SRM 53-00-01 REPAIR 6. NO DEFECTS NOTED. INSTALLED RIVETS IAW SRM 53-00-01, REPAIR 6, SEC 1 PARA 3.
Part: SKIN — DAMAGED (BS 720-760) · airframe 46,781 hrs · 15,477 cycles
TWO LIGHTNING STRIKES ON CROWN OF FUSELAGE BETWEEN BS 720 AND 760. DRILLED OUT DAMAGE IAW SRM 53-00-01, REPAIR 6, SECTION 1. PARAGRAPH 3, PERFORMED BHEC INSPECTION IAW SRM 53-00-01, REPAIR 6. NO DEFECTS NOTED. INSTALLED BLIND RIVETS, 2 EA IAW SRM 53-00-01, REPAIR 6, SECTION 1, PARA 3.
2014
Part: COVER — WORN (R1 DOOR SLIDE) · airframe 42,134 hrs · 13,875 cycles
R1 DOOR SLIDE COVER WORN ON BACK SIDE OF ATTACHMENT POINT. INSTALLATION OF NEW ESCAPE SLIDE ACCOMPLISHED ON TASK CARD.
Part: STRINGER — CRACKED (BS 780) · airframe 42,134 hrs · 13,875 cycles
CRACK ON END OF STRINGER 16R BS 780 +38. REPAIRED IAW ERA 528655-14 REV ORIGINAL.
Part: STRINGER — CRACKED (BS 780) · airframe 42,134 hrs · 13,875 cycles
CRACK ON END OF STRINGER 16L BS 780 + 36. REPAIRED IAW ERA 525968-14 REV ORIGINAL.
Part: FLOORBEAM — CORRODED (BS 345) · corrosion level 2 · airframe 42,134 hrs · 13,875 cycles
CORROSION ON MAIN CABIN FLOORBEAM UPPER TEE BS 345, LBL 20. REPAIRED BETWEEN LBL 58 TO RBL 17.5. IAW SRM 53-00-51.
Part: FLOOR PANEL — DAMAGED (CARGO BAY) · airframe 42,134 hrs · 13,875 cycles
AFT CARGO FLOOR DAMAGED. INTERIM REPAIR WAS ACCOMPLISHED IAW NWA DWG 5153-37933. FABRICATED REPLACEMENT FLOOR PANEL 161AF IAW SRM.
Part: FLOOR PANEL — DAMAGED · airframe 42,134 hrs · 13,875 cycles
FLOOR PANEL AFT OF DOOR HAS A .2500" HOLE , 5.7500" FROM L/E, 15 INCHES FROM RT SIDE PANEL EDGE. REPAIRED IAW DWG 5A53-37933 AND SRM.
Part: FLOORBEAM — CORRODED (BS 365) · corrosion level 2 · airframe 42,134 hrs · 13,875 cycles
CORROSION ON MAIN CABIN FLOORBEAM BS 365, RBL 24.5 AND RBL 45.5. BLENDED OUT CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM. REMOVED, FABRICATED AND INSTALLED REPAIR IAW SRM.
Part: SKATE ANGLE — CORRODED (BS 720-740) · corrosion level 2 · airframe 42,134 hrs · 13,875 cycles
CORROSION ON MAIN CABIN FLOOR STRUCTURE SKATE ANGLE, BS 720 - 740, RBL 63. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS. R & R SKATE ANGLE, ZEE, ON MAIN CABIN AT STA 670 TO 760, RBL 63, REF SRM.
Part: STRINGER — CRACKED (BS 780) · airframe 42,134 hrs · 13,875 cycles
CRACK ON END OF STRINGER 16R AT BS 780+24. R & R STRINGER IAW SRM.
Part: STRINGER — CRACKED (BS 780) · airframe 42,134 hrs · 13,875 cycles
CRACK ON END OF STRINGER 16L BS 780+24. REMOVED, FABRICATED, AND INSTALLED NEW STRINGER BS 776 - 780+24 IAW SRM.
Part: STRAP — CRACKED (BS 780) · airframe 42,134 hrs · 13,875 cycles
FWD CARGO CEILING STABILIZER STRAP IS CRACKED AT STA 780+120, RBL 25. CUT OUT DAMAGE, INSPECTED AND FABRICATED REPAIR, REF ERA 384483-14, REV.
Part: STRAP — CRACKED (BS 377) · airframe 42,134 hrs · 13,875 cycles
MAIN CABIN FLOORBEAM STABILIZING STRAP IS CRACKED BS 377. REPAIRED STRAP IAW ER/A 384483-14MA, REV D.
Part: STRAP — CRACKED (BS 1380) · airframe 42,134 hrs · 13,875 cycles
CABIN FLOORBEAM STABILIZATION STRAP CRACKED AT BS 1380, RBL 45 IN AFT CARGO CEILING. REPAIRED STRAP IAW SRM.
Part: ACM — SEIZED (LEFT) · airframe 42,053 hrs · 13,852 cycles
DURING DESCENT SMELLED ELECTRICAL SMOKE, F/O SAW SMOKE BY RT SEAT SIDEWALL. REPORTED ELECTRICAL ODOR AND HAZE IN AFT CABIN. DECLARED AN EMERGENCY. MAINTENANCE FOUND LT ACM SEIZED, REPLACED RECIRCULATING FAN FILTER, ACM, REHEATER AND LOW LIMIT VALVE. RAN ENG PERFORMED SMOKE ODOR CK IAW FIM 21-00-01. OP CKS GOOD.
Part: FUSE — FAILED (EMERGENCY LIGHT) · airframe 41,002 hrs · 13,533 cycles
DURING SERVICE CHECK, FOUND EMERGENCY EXIT SIGNS INOPERATIVE. FOUND TWO BLOWN FUSES ON L2-R2 POWER SUPPLY. R & R FUSES IAW AMM 33-51-07-962-017-002, STEP C-3.
Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,465 hrs · 13,342 cycles
EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK FUSE IAW AMM 33-51-07. OPS CHECKED NORMAL.
Part: GROUND STUD — CORRODED (EMERGENCY LIGHTS) · airframe 40,108 hrs · 13,200 cycles
LT SIDE OVERWING EXIT EMERGENCY LIGHTS ARE INOPERATIVE. FOUND GROUND PIN "GD44007-DC" CORRODED. REPLACED GROUND PIN IN GROUNDING BLOCK. LIGHT CHECKED GOOD.
Part: GROUND STUD — CORRODED (EMERGENCY LIGHTS) · airframe 40,108 hrs · 13,200 cycles
OVERHEAD BIN EMERGENCY AISLE LIGHTS AT ROWS 27,29, 32 INOPERATIVE. FOUND DEFECTIVE GROUND GD41009-DC PIN IN GROUNDING BLOCK. REINSTALLED PIN IN FREE SPOT IAW MM SWPM 20-10-11. LIGHTS CHECKED GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,097 hrs · 13,194 cycles
EMERGENCY LIGHT AT AFT OVERWING DOOR INOPERATIVE. R & R EMERGENCY POWER SUPPLY AND BATTERY IAW AMM 33-51. OPS CHECKED NORMAL.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,027 hrs · 13,156 cycles
EMERGENCY LIGHT INOPERATIVE AT SEAT 25 ABC. REPLACED THE POWER SUPPLY FOR EFFECTED SEAT.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 40,027 hrs · 13,156 cycles
EMERGENCY LIGHT INOPERATIVE AT SEAT 24 ABC. REPLACED BATTERY PACK, IAW WDM 33-51-22. CHECKED OK.
Part: SIGN — MISSING (EMERGENCY LIGHTS) · airframe 39,859 hrs · 13,097 cycles
LAVATORY C, EMERGENCY EXIT OVERHEAD SIGN MISSING BETWEEN 3L AND 3R. REPLACED MISSING OVERHEAD EXIT SIGN, CHECKED GOOD.
2013
Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 36,878 hrs · 12,001 cycles
EMERGENCY LIGHT AT SEAT 20 INOPERATIVE. FOUND WIRES RIPPED OUT OF SOCKET AND PULLED OUT OF CONDUIT REPAIRED WIRING AND SECURED IN CONDUIT NOW OPS NORMAL REF SWPM 20.
Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,652 hrs · 11,933 cycles
ROW 27 DEF EMERGENCY EXIT SIGN INOP. RELAMPED NO HELP. REPLACED FUSE IN M11384 POWER SUPPLY IAW 33-51-07. OPS CHECK GOOD.
Part: SOCKET — INOPERATIVE (EMERGENCY LIGHT) · airframe 36,399 hrs · 11,829 cycles
EMERGENCY ESCAPE PATH LIGHT ROW 14 INOPERTAIVE. REPLACED LAMP HOLDER, CHECKED GOOD.
2012
Part: SKIN — GOUGED (L2 DOOR) · airframe 35,404 hrs · 11,458 cycles
MX FOUND DOOR 2L HAS 2 GOUGES IN SKIN PANEL FROM EXTERNAL HANDLE OPERATION. R & R L2 DOOR EXTERNAL HANDLE SRM 51-40-02 AND ER/A 506549-14 REV ORIG.
Part: SOCKET — DAMAGED (EMERGENCY LIGHTS) · airframe 35,404 hrs · 11,458 cycles
MX DISCOVERED L4 DOOR EXTERIOR EMERGENCY EXIT LIGHT IS INOPERATIVE. R & R LAMP HOLDER FOR L4 DOOR EXTERIOR EMERGENCY LIGHT IAW AMM 33-50. OPS CHECKED GOOD.
Part: CABLE — FAILED (PAX DOOR) · airframe 35,404 hrs · 11,458 cycles
MX DISCOVERED NR 4 RT PASSENGER DOOR EMERGENCY POWER ACTUATION CABLE CHECK FAILED. ADJUSTED THE R4 DOOR EMERGENCY POWER ACTUATION CABLE IAW AMM 52-11.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 35,404 hrs · 11,458 cycles
ROW 6 LT SEAT MOUNTED EMERGENCY LIGHT IS INOPERATIVE. AFTER FURTHER TROUBLESHOOTING FOUND BROKEN WIRE TO EMERGENCY LIGHT. REPAIRED IAW SWPM 20-30-12, STEP F. PERFORMED GOOD OPS CHECK IAW AMM B757-A-33-51-11-201-925A-A STEP 2.C.
2011
Part: SOCKET — DAMAGED (EXTERIOR) · airframe 5,408 hrs · 1,831 cycles
DURING A SERVICE CHECK, MAINTENANCE FOUND THE EXTERIOR EMERGENCY LIGHT AT DOOR 4R INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT SOCKET. OPERATIONAL CHECK WAS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 32,058 hrs · 10,192 cycles
DURING LAYOVER CHECK FOUND EMERGENCY DOME LIGHTS INOP AT DOORS R1, L2, R4 AND L4 AND AISLE DOME LIGHTS BETWEEN L2 AND R2 DOORS. RELAMPED EMERGENCY AND AISLE DOME LIGHTS PER B757 AMM 33-51-09.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 31,609 hrs · 10,038 cycles
DURING A SERVICE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHLIGHT AT ROW 26ABC INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.
2010
Part: ANGLE — CRACKED (BS 1147) · airframe 28,626 hrs · 8,996 cycles
DURING L-CHECK FOUND CRACK IN RT MLG WHEEL WELL ANGLE ON BEAM AT BS 1147 RBL 70. REPAIRED IAW ERA 485743-14.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,626 hrs · 8,996 cycles
DURING LCK AT ST-AEROSPACE SAN ANTONIO, A FUSELAGE SKIN DENT WAS FOUND AT STA 1391 BETWEEN S28R AND S29R. ER/A 485739-14 SECT I REPAIR WAS ACCOMPLISHED AT THAT TIME. FOLLOW ON ACTION IS REQUIRED FOR SECT II DTA ACCOMPLISHMENT.
Part: SKIN — DENTED (FUSELAGE) · airframe 28,626 hrs · 8,996 cycles
DURING LCK 4 DENTS WERE FOUND ON THE FUSELAGE SKIN BETWEEN STA 605 AND 628, S-15L THROUGH S-18L. ER/A 485745-14 SECT IWAS COMPL AT THAT TIME, FOLLOW ON ACTION IS REQ FOR DTA. ACCOMP SECT II OF ER/A 485745-14 BY 28SEP2011. FOLLOW ON IS REQ A TIME LIMITED REPAIR.
2008
Part: BATTERY PACK — FAILED (CABIN) · airframe 21,064 hrs · 6,704 cycles
DURING EMERGENCY LIGHT BATTERY PACK DEEP CYCLE CHECK, ALL 15 EMERGENCY LIGHT BATTERY PACKS FAILED THE TEST. MX REPLACED THE BATTERY PACKS AND ALL OPS WERE NORMAL AFTER REPLACEMENT.
2006
Part: SLIDE — INOPERATIVE (R3 DOOR) · airframe 12,781 hrs · 4,146 cycles
THE NUMBER 3, RIGHT HAND, EMERGENCY DOOR INADVERTENTLY OPENED AND THE ESCAPE SLIDE DID NOT INFLATE. REMOVED AND REPLACED THE EVACUATION SLIDE, TESTED AND RETURNED TO SERVICE.
2004
Part: LINE — CHAFED (RT WING) · airframe 5,223 hrs · 1,773 cycles
THE 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.