N325NB
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 2002-04-15 | 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.
135 reports on file, 2002-11-15 – 2026-08-08.
Part: LIGHT SYS — FAULTED (ZONE 200) · airframe 60,337 hrs · 31,272 cycles
AFTER ROTATING FA REPORTS CABIN EMERGENCY LIGHTS CAME ON MOMENTARY, THEN TURNED OFF. PERFORMED CIDS TEST IAW AMM 23-73. TEST OK. VERIFIED EMERGENCY EXIT LIGHTS OPS NORMAL IAW AMM 33-50. (LP: 9587650, AIRCRAFT WAS GROUNDED)
Part: SEAL — FAULTED (COCKPIT) · airframe 60,291 hrs · 31,250 cycles
AT CRUISE, ODORS & ELECTRIC ACRID ODORS. TURNED CABIN FANS OFF AS WE HEARD A HIGH WHINE SOUND. LASTED 3-5 MINS THEN DISSIPATED. . DISCOVERED CAPTAINS ELECTRIC MOTOR TO CHAIR WASN'T WORKING. INSPECTED FLT DECK & FWD AVIONICS BAY, FOUND C/B FOR CAPT CHAIR POPPED, NO ODOR PRESENT. DEFER CAPT ELECTRIC ADJUSTMENT, M PROCEDURE C/W, INSTALLED PLACARD. ACFT OK TO CONTINUE ON MEL. REF AMM 05 -51. (LP: 9587640, AIRCRAFT WAS GROUNDED)
Part: POWER SUPPLY — FAULTED (ZONE 200) · airframe 59,800 hrs · 30,992 cycles
EMERGENCY EXIT SIGNS INOPERATIVE. THE EXIT SIGNS ABOVE DOORS 2L AND 2R DO NOT ILLUMINATE WHEN THE GEAR IS DOWN, INSTEAD THE SMALL EMERGENCY LIGHTS BETWEEN THE EXIT SIGN AND DOOR COME ON. R & R EPSU AND EPSU POWER SUPPLY REF A319/320 AMM 33-51. FAULT STILL PRESENT. R BLAKE 727332. TRIED MULTIPLE OTHER EPSU POWER SUPPLIES NO HELP. REINSTALLED ORG REF A319 AMM 33-51. PER A319 AWM 33-51-03 R/R DEU B 3 20RH5 REF A319 AMM 23-73. NO HELP.RE INST ORG. R/R SWITCH 190RH REF A319 AWM 23-73-08 AND A319 ESPM 20-48-25. NO HELP. NEEDS FURTHER T/S. 936244. FOUND TERMINALS AT 45WL AND 33WL SWAPPED. ALSO FOUND TERNINALS AT 44WL AND 32WL SWAPPED. CORRECTED WIRING/ TERMINALS PER A320 AWM 33-51-03. ALL EXIT LIGHTS NOW OPERATE NML. (LP: 1616237, AIRCRAFT WAS GROUNDED)
Part: OXYGEN BOX — OPEN (ZONE 200) · airframe 59,641 hrs · 30,906 cycles
CREW REPORTS O2 MASK DOOR OPENED ON LANDING SEAT 12DEF. PACKED AND SECURED O2 MASK DOOR AT SEAT 12 DEF IAW AMM 35- 21. (LP: 8885420). AIRCRAFT WAS GROUNDED
Part: REPAIR — NOT REPORTED (ZONE 100) · airframe 59,520 hrs · 30,835 cycles
REMOVE EXISTING EXTERNAL REPAIR LOCATED BTWN FR1 AND FR3 STRG 34R AND RT LOWER STRG AND PERFORM VISUAL INSPECTION OF THE UNDERLYING STRUCTURE. REPAIRED R/H NOSE FWD FUSELAGE SKIN BETWEEN FRI-FR3 BETWEEN STRG -34R-36R I/A/W DELTA ER/A 633282-14AD REV: ORIGINAL DATED: 18/ APR/26. NOTE: THIS IS CLASSIFIED AS MAJOR REAPIR. (LP: 1551255). AIRCRAFT WAS GROUNDED
Part: SKIN — CRACKED (ZONE 100) · corrosion level 2 · airframe 59,520 hrs · 30,835 cycles
LOWER FUSELAGE AT FR65+220MM BETWEEN STRG 31R-32R SKIN PANEL CORRODED AND CRACKED. REPAIRED UPPER REAR FUSELAGE SKIN PANEL BETWEEN FR65-FR66 AND STRG 31RH-32RH I/A/W DELTA ER/A 632717-14 REV. ORIGINAL DATED 17 -APR-26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIR. ASSOCIATED ER/A 14-632717 ADDED FOR AC 3125. (1549551). AIRCRAFT WAS GROUNDED
Part: SKIN — DENTED (ZONE 200) · airframe 59,520 hrs · 30,835 cycles
UPPER FUSELAGE FR55+470MM BETWEEN STR 6L-7L SKIN PANEL WITH DENT. REPAIRED UPPER REAR FUSELAGE SKIN PANEL WITH DENT FR55+470MM BETWEEN STRG 6LH - 7LH IAW DELTA ER/A 633023-14 REV ORIGINAL DATED 15/APR/26. NOTE: THIS IS CLASSIFIED AS MAJOR REPAIR. ASSOCIATED ER/A 14-633023 ADDED FOR AC 3125. (LP: 1549686). AIRCRAFT WAS GROUNDED
Part: SKIN — NOT REPORTED (ZONE 200) · airframe 59,527 hrs · 30,838 cycles
DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR SKIN REPAIR INSTALLED AT FR 65 - 66 S31 - 32R IAW ER/A 632717-14. C/A: SECTION I IS LIMITED TO 6MO ( 182 DAYS ) FROM 15APR26. ER/A TO B E REVISED PRIOR TO THIS LIMIT ELSE REMOVED A/C FROM SERVICE. ASSOCIATED ER/A 14-632717 ADDED FOR AC 3125. (LP: 1549373). AIRCRAFT WAS GROUNDED
Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 59,519 hrs · 30,834 cycles
FR68 DOOR FRAME R/H, DOOR STOP FITTINGS 1,2,3,4,5,6 AND 7 LOCATIONS WERE FOUND THE HOLES (4 HOLES IN EACH FITTING) COMMON TO THE FRAME WEB GREATER THAN THE MAXIMUM STARTING HOLE DIAMETER (6.38MM/0.251") "ACTION REQUIRED PRIOR TO FURTHER FLIGHT, ENGINEERING EVALUATION REQUIRED, CONTACT LIAISON ENGINEERING FOR FURTHER DIRECTION". C/A: REPAIRED FUSELAGE FRAME FR68 RH DOOR STOP FITTINGS AREAS 1 THROUGH 7 HOLES OVERSIZED IAW DELTA ER/A 633159-14AD REV. ORIGINAL DATED 15-APR-26. NOTE: THE REPAIR IS CLASSIFIED AS MAJOR REPAIR. ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1547657) AIRCAFT WAS GROUNDED
Part: DOOR FRAME — NOT REPORTED · airframe 59,527 hrs · 30,838 cycles
DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLE D ON FRAME WEB FR68RH AT DOOR STOPS PER ER/A 633159-14AD. SECTION I IS LIMITED TO 37900FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1545998). AIRCRAFT WAS GROUNDED
Part: DOOR FRAME — DAMAGED (ZONE 200) · airframe 59,527 hrs · 30,838 cycles
ER/A 633159-14AD ISSUED FOR REPAIR TO FR68 RT FRAME WEB AT DOOR STOPS. FOLLOW ON ACTION REQUIRED. PERFORM SECTION II EVERY 19700FC AFTER SECTION I. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1545988). AIRCRAFT WAS GROUNDED
Part: DOOR FRAME — NOT REPORTED · airframe 59,527 hrs · 30,838 cycles
DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR INSTALLED AT FR68RH DOOR STOP AREA OF FRAME WEB PER ER/A 633159-14AD. C/A: SECTION I IS LIMITED TO 60000FC FROM 08APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED AA 5311-01216 ADDED FOR AC 3125 ASSOCIATED ER/A 14-633159 ADDED FOR AC 3125. (LP: 1546004). AIRCRAFT WAS GROUNDED
Part: SKIN — NOT REPORTED (ZONE 200) · airframe 59,520 hrs · 30,835 cycles
DAMAGE TOLERANCE EVALUATION (DTE) REQUIRED FOR FUSELAGE SKIN R EPAIR INSSTALLED AT FR56 AND S-6/7LH PER ER/A 633023-14. SECTION I IS LIMITED TO 6MO (182) DAYS FROM 10APR26. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-633023 ADDED FOR AC 3125. (LP: 1546857). AIRCRAFT WAS GROUNDED
Part: STRINGER — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
AFT CARGO BAY, BETWEEN FR 59 & FR 60, STR 43L, STRINGER EXISTING COUPLING REPAIR CORRODED. REPAIRED FUSELAGE S43L BTWN FR 58 - 61. IAW ER/A 633052-14, REV. ORIGINAL. MAJOR REPAIR.
Part: LUG — DAMAGED (ZONE 600 FLAP) · corrosion level 2 · airframe 59,520 hrs · 30,835 cycles
DAMAGE TOLERANCE EVALUATION ( DTE ) REQUIRED FOR REPAIR OF LUG B ORE AT RH WING OUTBOARD FLAP PER ER/A 633290-14. SECTION I LIMITED TO 6 MONTHS FROM 09APR26 ON FTN 1X6843. ER/A T O BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE COMPONENT FROM SERV ICE. ASSOCIATED ER/A 14-633290 ADDED FOR AC 3125. (LP: 1537909). AIRCRAFT WAS GROUNDED
Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 59,519 hrs · 30,834 cycles
REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT . FLIGHT DECK, WINDSHIELD FRAMING, LH/RH CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. REPLACED CONTINUITY FITTINGS (LH P/N D5311107720200) (RH P/N D5311107720300) I/A/W DELTA ER/A 632983-14AD. REV. ORIGINAL DATED 09- APR-26 AND REPAIR DWG R531-12919 ISSUE LAND R531-13426 ISSUE H. DOCUMENTED ON COOPESA PRI EO NO. 632983-14 DATED 06- MAR-26 PEGE 1 OF 9. NOTE: THIS REPLACEMENTS ARE CLASSIFIED AS MAJOR REPAIR AND CONTINUITY FITTINGS ARE SUBJET TO MANDATORY AT 8.800/FC REPETITIVE ISPECTION REQUIRED BY REF: S/B A320-53-1331 R01 AND S/B A320-53-1331 R03. ASSOCIATED ER/A 14-632983 ADDED FOR AC 3125. (LP: 1536474) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER AFT CABIN AT FR66, Y=765 SEAT TRACK WITH CORROSION. C/A: REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 Y=765 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION IAW DELTA ER/A 633001 -14 REV: ORIG DATED 07-APR-26 AND REF. DWG 14N00031 DOCUMENTED ON COOP PRI EO NUMBER 633001-14 REV : 00 DATED: 09-MAR-26. NOTE: FOR ORIGINAL TECHNICAL DOCUMENTS OF COOP. PRI (EO) ENGINEERING ORDER AND DELTA ER/A 633001-14 SEE DELTA WC 200-36 ASSOCIATED ER/A 14-633001 ADDED FOR AC 3125 9. (LP: 1534947) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER AFT CABIN AT FR 65, -Y=765 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-103 AT FR 64 TO FR 66 -Y=765 WET -AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11- 911- 001 REV: 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION IAW DELTA ER/A 633001-14 REV: ORIG DATED 07-APR-26 AND REF. DWG 14N00031 DOCUMENTED ON COOP PRI EO NUMBER 633001-14 REV : 00 DATED: 09-MAR-26. ASSOCIATED ER/A 14-633001 ADDED FOR AC 3125. (LP: 1534931) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER AFT CABIN AT FR 65, -Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 -Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION IAW DELTA ER/A 633001-14 REV. ORIGINAL DATED 07-APR-26 AND REF. DWG 14N00031 DOCUMENTED ON COOP PRI EO NUMBER 633001-14 REV. 00 DATED 09-MAR-26. NOTE: FOR ORIGINAL TECHNICAL DOCUMENTS OF COOP. PRI (EO) ENGINEERING ORDER AND DELTA ER/A 633001-14 SEE DELTA WC 200-369. ASSOCIATED ER/A 14-633001 ADDED FOR AC 3125. (LP: 1534957) AIRCRAFT WAS GROUNDED
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER CABIN AFT SECTION AT FR65, Y=1292 SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK P/N 14N00031-101 AT FR 64 TO FR 66 Y=1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW A319 SRM 51-72-11-911- 001 REV, 155.00 DATED 17-NOV- 25 AND FABRICATED SEAT TRACK SECTION IAW DELTA ER/A 633001-14 REV. ORIGINAL DATED 07-APR-26 AND REF. DWG 14N00031 DOCUMENTED ON COOP PRI EO NUMBER 633001-14 REV. 00 DATED 09-MAR-26. NOTE: FOR ORIGINAL TECHNICAL DOCUMENTS OF COOP. PRI (EO) ENGINEERING ORDER AND DELTA ER/A 633001-14 SEE DELTA WC 200-369. ASSOCIATED ER/A 14-633001 ADDED FOR AC 3125. (LP: 1534972) AIRCRAFT WAS GROUNDED
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER CABIN FLOOR SUPPORT AT Y-1720MM BETWEEN FR 20 & FR 21, WEB AND SUPPORT ANGLES (2EA) WITH CORROSION. REPLACED WEB P/N 5311278520300 AND SUPPORT ANGLE P/N D5311278620101 IAW A319 SRM 53-11-14-07B FIG 007 ITEMS 186A AND 190 AND A319 SRM 51-72-911-001 PARG 2 REV 155.00 DATED 17/NOV/26 ALSO REPLACED ANGLE ASSY PN D5361019900100 IAW A319 AIPL 53-12- 01-265 SHEET 1 ITEM 110 REV 134.01 DATED 12/FEB/26 AND INSTALLED IAW AIRBUS DGW'S D53112545 ISSUE D, D53112784 ISSUE E ITEM 1 AND D53112783 ISSUE E. (LP: 1531196) AIRCRAFT WAS GROUNDED. LEVEL 2 CORROSION.
Part: SUPPORT ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
LOWER FUSELAGE LT AVIONICS BAY, FR 13 BTWN STRINGERS 31L & 34L, VENTILATION DUCTS SUPPORT STRUCTURE INNER ANGLE WITH CORROSION. REPLACED ANGLE AT L/H AVIONICS COMPARTMENT FR 13 BETWEEN STGR 31L AND STGR 34L I.A.W A319 SRM 51-72-11-911- 001 REV. 155.00 DATED 17-NOV-25 AND REF. DWG# D53118086 REV. ( ISSUE A.00) DATED 09-JUL-99. CHARGED PROTECTIVE MATERIAL IN ITEM 7-432 DELTA W/C= 5175-2423. (LP: 1530067) AIRCRAFT WAS GROUNDED
Part: SKIN — DAMAGED (ZONE 100) · airframe 59,519 hrs · 30,834 cycles
LOWER EXTERNAL FUSELAGE AT FR 25+160MM, STGR 40L SKIN WITH TOOL MARKS. FOUND DURING PROCESS WITH ORNRC 100-269. REPAIRED LOWER FUSELAGE SKIN PANEL FROM FR25 +66.5MM TO FR25 + 296.6MM BETWEEN STRG 39LH-41LH DUE TO TOOL MARK OUT LIMITS I/A/W A319 SRM 53-21-11-300-090 FIGURE 001. REV.155.00 DATED 17-NOV- 26. NOTE: THIS IS CATEGORY B REPAIR WITH NSPECTION THRESHOLD FROM TIME OF ADL/REPAIR EMBODIMENT FC 60 000 / FH 120 000 SUBSEQUENT INSPECTION UNTIL 60 000 FC / 120 000 FH AT INTERVALS OF FC TBD/FH TBD INSPECTION METHOD TBD IN CASE OF AIRCRAFT LIFE EXTENSION MORE THAN 60 000 FC / 120 000 FH IAW SRM 53-21- 11-205-071 PARG 2.A TABLE 002 ZONE A FIG. 001. REV 155.00 DATED 17-NOV-26. (LP: 1520616) AIRCRAFT WAS GROUNDED.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER CABIN AT Y-1292, BETWEEN FR20 AND FR21 , SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK AT Y -1292, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWG D53112812, D53112813, D53110920, & D53112639. (LP: 1518547)
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
PASSENGER CABIN AT Y-765, BETWEEN FR20 AND FR21, SEAT TRACK CORRODED. REPLACED THE SEAT TRACK Y -765, BTW FR 12 TO FR 24 IAW SRM 51-72-11-911-001, PARAG 2.B, REV 155.00, DWGS D53112812, D53112813, D53112639, & D53110920. (LP: 1518556)
Part: POWER SUPPLY — INOPERATIVE (ZONE 200) · airframe 59,519 hrs · 30,834 cycles
PAX CABIN EMERGENCY POWER SUPPLY UNIT INOP. REPLACED EMERGENCY POWER SUPPLY UNIT IAW A319 AMM TASK 33-51-38- 000-001-A AND AMM TASK 33-51-38-400-001-A. (LP: 1510385)
Part: SUPPORT ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 59,519 hrs · 30,834 cycles
FORWARD PASSENGER DOOR (LT) CUTOUT SILL AREA BETWEEN FR16 AND FR20, SCUFF PLATE SUPPORT ANGLE WITH CORROSION. REPLACED SUPPORT ANGLE (FITTING) P/N: D5311219820006 IAW A319 SRM TASK 51-72-11-911-001 REV 155.00 DATED 17/NOV/25 AND DRAWING REF D531 12109 ISSUE C AND D531 12198 ISSUE J. (LP: 1510455)
Part: SLIDE — LOW PRESSURE (ZONE 800) · airframe 59,514 hrs · 30,833 cycles
RIGHT FWD DERVICE DOOR SLIDE HAS LOW PRESSURE. REMOVED AND REPLACED RIGHT FORWARD DOOR SLIDE IAW AMDS TC 2561-4004-RF. (LP: 9141074)
Earlier reports · 2002–2024 · 107 reports
2024
Part: SKIN — DENTED (FUSELAGE) · airframe 59,372 hrs · 30,757 cycles
SHIP 3125 THREE DENTS IN FUSELAGE UNDER FWD CARGO DOOR. CORRECTIVE ACTION: REPAIRED PER ER/A 501814-14. (0194327)
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 59,155 hrs · 30,659 cycles
SHIP 3125 DENT FWD OF L2 DOOR. CORRECTIVE ACTION: REPAIRED PER A319 SRM 53-41-11-283-059. (5381348)
2023
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,940 hrs · 30,534 cycles
SHIP 3125 EXIT LIGHT BURNED OUT AT POSITION 2L. CORRECTIVE ACTION: EXAMINED WIRING PER A319 ASM 33-51-02, FOUND 33WL 1 AND 3 ON 45WL 1 AND 3. PLACED WIRES ON PROPER SIGNS AND ALL LIGHTS OPS CHECK OK. REF A319 TSM 33-51-00-810- 807-A. (9938556)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 58,660 hrs · 30,379 cycles
SHIP 3125 INTERCOSTAL WEB AND SUPPORT CORRODED 4" FWD OF FR70 STR 23R. CORRECTIVE ACTION: REPLACED INTERCOSTAL WEB AND SUPPORT PER A319 SRM 51-42-11. (0038519)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,646 hrs · 30,370 cycles
SHIP 3125 FLOOR BEAM CORRODED 10" I/B OF R2 AFT GIRT BAR FITTING. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A319 SRM 51-42-11. (0026267)
Part: FLOORBEAM — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,646 hrs · 30,370 cycles
SHIP 3125 FLOOR BEAM CORRODED -Y765 FR 68. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 PER A319 SRM 51-42-11. (0026255).
Part: UNKNOWN — UNKNOWN (UNKNOWN) · corrosion level 2 · airframe 58,646 hrs · 30,370 cycles
SHIP 3125 SUPPORT STRAP AT FR 70 STR 24R CORRODED. CORRECTIVE ACTION: REPLACED STRAP AT FR 70 STR 24R PER A319 SRM 51-42-11. (0026259)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,298 hrs · 29,606 cycles
AIRCRAFT 3125, THE AIR QUALITY OFF THE PACKS WAS SUBSTANDARD, MUSTY SMELL. IN ADDITION, THE FLIGHT ATTENDANTS REPORTED THAT THE CABIN WAS HOT ALTHOUGH INDICATED TEMP WAS 68F. QRH 2.47 DIRECTED HOT AIR SWITCH OFF. THIS HELPED CABIN TEMP AND ALSO, WE COULD NO LONGER SMELL MUSTY ODOR. AFTER HOT AIR SWITCH OFF, LEFT PACK OUTLET + 35C, AND RIGHT PACK OUTLET TEMP -10. CORRECTIVE ACTION: REPLACED APU LUBE MODULE. (LP 9696766, 9696771)
Part: UNKNOWN — UNKNOWN · airframe 57,057 hrs · 29,467 cycles
AIRCRAFT 3125, SMOKE FUMES IN CABIN OF A/C WITH ONLY APU RUNNING. CORRECTIVE ACTION: PERFORMED DECONTAMINATE THE ECS WHEN THE APU IS INOP REVERSE FLOW. (LP 9895734)
Part: NOT REPORTED — NOT REPORTED (NOT REPORTED) · airframe 56,819 hrs · 29,316 cycles
SHIP 3125 -ATB- RETURNED TO TPA DUE TO #1 ENGINE STALL AND EGT RISE. THROTTLE PULLED BACK AND ATTEMPTED TO PUSH THROTTLE UP, EGT FOLLOWS. REPORTS OF AN AUDIBLE BANG. FOUND EXTENSIVE DAMAGE TO 4TH STAGE LPT BLADES. CORRECTIVE ACTION: C/W #1 ENGINE CHANGE REF AMDS CARD 7100-9901LT. LP 9560264
2022
Part: NONE — NONE · airframe 56,187 hrs · 28,967 cycles
SHIP 3125 - UPON INTITAL DESCENT INTO LGA CAPT + FO NOTICED THE "DIRTY SOCK" SMELL/ODOR. CORRECTIVE ACTION: C/W NO-GO-ODI PREVENTION 21-72. REPLACED BOTH REC AIR CABIN FILTERS PER A319 AMM 21 -21. (8943336)
Part: MASK — DEPLOYED · airframe 54,883 hrs · 28,300 cycles
SHIP 3125 - OXYGEN MASKS DROPPED DURING FLIGHT SEATS 16 DEF. CORRECTIVE ACTION: REPACKED OXYGEN MASKS AT SEAT ROW 16DEF. VERIFIED OXYGEN GENERATOR DID NOT ACTIVATE. REF A320 FAM AMM 35-21-43.(8931018)
Part: UNKNOWN — UNKNOWN (UNKNOWN) · airframe 57,859 hrs · 29,912 cycles
SHIP 3125 DISCREPANCIES FOUND IN DIAMETER AT HOLES #3,#4,#5 IN FR16 RHS DOORSTOP #7 DBL JOGGLE LEVEL. CORRECTIVE ACTION: INSPECTED HOLES PER STEP 6 SECTION 4 OF ER/A 569171-14AD REV C. (2229119)
2021
Part: FAN — NOISY (RECIRCULATION) · airframe 52,632 hrs · 27,071 cycles
SHIP 3125 - DIV - TO JAX DUE TO A METALLIC SMELL OF UNKNOWN SOURCE THROUGHOUT THE CABIN. CREW DONNED OXYGEN MASKS AND DECLARED AN EMERGENCY INTO JAX. AIRCRAFT WAS OPERATING ON A SINGLE PACK MEL. CORRECTIVE ACTION: COMPLIED WITH NO GO ODI. REMOVED AND REPLACED RIGHT CABIN RECIRCULATION FAN PER A319 AMM 21-21. (7351088)
Part: ACOUSTIC LINER — CORRODED (NR 2 INTAKE) · airframe 52,384 hrs · 26,963 cycles
SHIP 3125 - CORROSION ON ACOUSTIC INNER BARREL AIR INTAKE COWL LOWER AREA ENGINE 2. CORRECTIVE ACTION: REMOVED AIR INTAKE COWL. INSTALLED AIR INTAKE COWL AS PER A320 FAM, AMM 71-11. (1790418)
2020
Part: WARNING LIGHT — FALSE ACTIVATION (COCKPIT) · airframe 52,255 hrs · 26,908 cycles
SHIP 3125 - DIV - TO PIT DUE TO APU FIRE BOTTLE DISCHARGE LIGHT ILLUMINATED IN CRUISE. CORRECTIVE ACTION - FLIGHT CREW APPLIED MEL PLACARD AND FLIGHT CONTINUED.
2019
Part: PANEL — TORN (FUSELAGE) · airframe 51,108 hrs · 26,364 cycles
ON WALK AROUND TORN ON BODY PANEL 148DB. PER A319 SRM 53-35-11-300-09 DEFERRED SEAL TO MOM WITH DAILY INSPECTION OF SPEED TAPE REQUIRED WITH REPAIRS IN 600 HOURS. LOG PAGE STILL OPEN....
Part: FIRE WARNING — FALSE ACTIVATION (APU BAY) · airframe 50,600 hrs · 26,117 cycles
IN FLIGHT FL370 APU DISCH FIRE LIGHT CAME ON. WENT OUT AT 8800 MSL CABIN ALT 1100. INSPECTED BLOW OUT DISC ON FUSELAGE - NOT BLOWN. PERFORMED TSM TASK 26-22-00-810-806-A APU EXT LOOP OPERATES NORMALLY.
Part: COVER — MISSING (LT MLG) · airframe 49,305 hrs · 25,462 cycles
PDA PART DEPARTING AIRCRAFT. LOG PAGE 5290092 CLOSED. A/C 3125 FLT/CHK 0842 PILOT REPORT SDR: N POSITION: LT TASK HRS: 000009.2 TASK ELAPSE TIME HRS: 000009.2 01 18MAR19 W LEFT LANDING GEAR STRUT DUST COVER MISSING LOG-PAGE UPDATED @ 18MAR19 1846 UTC 02 18MAR19 W -PERFORMED VISUAL INSULA INSPECTION. NOTHING DAMAGED. APPLIED 2 LAYERS OF SPEED TAPE PER SECTION 1 OF REPAIR INSTRUCTION ERA 576567-14. REV ORIGINAL. REP INSP EACH FLIGHT. TERMINATE IN 10 CYCLES LOG-PAGE UPDATED @ 18MAR19 1846 UTC 03 18MAR19 RII: W *** CONTRACT MAINTENANCE EVENT - OCM: 211145 *** C/W TAPE INSP IAW ERA 576567-14 LOG-PAGE UPDATED @ 18MAR19 1952 UTC 04 18MAR19 S LOG WAS REDEFERRED TO UPDATE PARTS REQUIREMENT LOG-PAGE UPDATED @ 18MAR19 2151 UTC 05 DTW 18MAR19 RII: W VERIFIED SPEED TAPE SECURE ON LEFT MLG A/C OK FOR SVC. REF ERA 576567-14 ORIG LOG-PAGE UPDATED @ 18MAR19 2151 UTC 06 18MAR19 RII: W VERIFIED SPEED TAPE SECURE ON LFT MLG MISSING DUST COVER PER ERA 576567-14. A/C OK FOR SERVICE. LOG-PAGE UPDATED @ 18MAR19 2342 UTC 07 DFRD BY DOKEY 00381098 DTW 19MAR19 RII: N C/W REP CHECK SPEED TAPE IN GOOD. CONDITION OK FOR SVC PER ERA 576567-14. OK TO CONTINUE ON MON. LOG-PAGE UPDATED @ 19MAR19 0139 UTC 08 19MAR19 RII: CONTRACT MAIN.
2018
Part: FRAME — CRACKED (FUSELAGE) · airframe 47,307 hrs · 24,547 cycles
CRACK INDICATION ON FRAME 20 IN HOLE 5 & HOLE 6 RT SIDE UPPER CORNER OF DOOR FRAME IN PASSENGER CABIN. REPLACED FRAME 20 RT SIDE AND FASTENERS AS PER SRM 51-72-11 AND ERA 569173-14 REV ORIGINAL.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION ON FLOORBEAM - Y1162 BETWEEN FR68 TO FR69, AFT GALLEY AREA. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-72-11 AND DWG D53472780.
Part: FRAME SPLICE — CRACKED (FUSELAGE) · airframe 47,296 hrs · 24,540 cycles
CRACK SPLICE CONNECTION ON FR68 BTW STR 23L TO STR 24L AT AFT GALLEY AREA, REPLACED SPLICE CONNECTION ON FR68 BTW STR 23L TO STR 24L AT AFT GALLEY AREA AS PER SRM 51-42-11 AND DRAWING D5347108720300.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y464 LOC BTW FR 64 TO FR67 AT AFT GALLEY AREA. REPLACED FLOORBEAM -Y465 LOC BTW FR64 TO FR67 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DWG D53472816.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM Y503.2 LOC BTW FR 12 TO FR 16 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y503.2 LOC BTW FR12 TO FR16 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112826.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y765 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED FLOORBEAM +Y765 LOC BTW FR12 TO FR 24 AT GALLEY AREA FLOOR STRUCTURE AS PER SRM 51-72-11 AND DWG 53112812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA. REPLACED FLOORBEAM +Y1292 LOC FR64 TO FR66 AT AFT GALLEY AREA AS PER SRM 51-72-11.
Part: SKIN — DENTED (FUSELAGE) · airframe 47,296 hrs · 24,540 cycles
DENT EXTERNAL SKIN LOC BTW FR 12 TO FR 13 AND 10" ABOVE UPPER SIDE STR RT ON LOWER FUSELAGE. PERFORMED PERMANENT REPAIR EXTERNAL SKIN LOC BTW FR 12 TO FR 13 AND 10" ABOVE UPPER SIDE STR RT ON LOWER FUSELAGE AS PER SRM 53-00-11-300-029.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM AT LEVEL +Y1130 BTW FR 66+6INCH TO FR68 AT AFT GALLEY AREA. REPLACED FLOORBEAM AT LEVEL +Y1130 BTW FR 66+6" TO FR 68 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND DRAWING D53472172-20400.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y1162 BTW FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOORBEAM +Y1162 BTW FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-72-11 AND DWG D53472780.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y1379.5 LOC BTW FR12 TO FR16 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y1379.5 LOC BTW FR12 TO FR16 AT FWD GALLEY AREA ASPER SRM 51-72-11 AND DRAWING D53110984.
Part: FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION CENTER FITTING LOC BTW FR16 TO FR 20 LEVEL STR 23R AT FWD GALLEY AREA. REPLACED CENTER FITTING LOC BTW FR 16 TO FR20 AT LEVEL STR 23R AT FWD GALLEY AREA.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y81 LOC BTW FR12 TO FR16 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y81 LOC BTW FR12 TO FR16 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112828.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION LOWER SILL FR66 TO FR68 ST LEVEL STR 23L AT AFT GALLEY AREA, REPLACED LOWER SILL LOC AT LEVEL STR 23L BTW FR66 TO FR68 AFT GALLEY AREA FLOOR STRUCTURE ASPER SRM 51-72-11, SRM 51-42-11, DRW D53480505.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y1292 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53112812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA. REPLACED FLOORBEAM +Y1292 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y765 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y765 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11, AND DWG D53112812.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM -Y254 LEVEL FR16 AT FWD GALLEY AREA. REPLACED FLOORBEAM -Y254 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DRAWING D53110920.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA. REPLACED FLOORBEAM +Y765 BTW FR66 TO FR70 AT AFT GALLEY AREA SRM 51-72-11 AND DRAWING D53112826.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FLOORBEAM +Y254 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED FLOORBEAM +Y254 LOC BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER SRM 51-72-11 AND DWG D53112816.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-70) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION FOUND ON THE FLOOR SUPPORT, -Y765 BETWEEN FRAMES 66 TO 70. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND DWG D53472780.
Part: WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 47,296 hrs · 24,540 cycles
CORROSION WEB AT LEVEL STRINGER 23L AT AFT GALLEY AREA BETWEEN FRAME 69 TO FRAME 70, REPLACED WEB AND FASTENER AT LEVEL OF STRINGER 23L AT AFT GALLEY AREA BETWEEN FRAME 69 TO FRAME 70 ASPER SRM 51-42-11, 51-72-11 AND DRAWING NR D53474180.
2017
Part: STRINGER — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 46,788 hrs · 24,291 cycles
CORROSION FOUND AFT ATG 4 ANTENNA ON AN EXISTING STRINGER REPAIR, REPAIRED THE STRINGER IAW SRM 53-00-13-300-002, FIG 20102.
2016
Part: WIRE — OUT OF POSITION (CABIN) · airframe 42,460 hrs · 22,356 cycles
R1 EMERGENCY EXIT LIGHT REMAINS ON WHEN EMERGENCY EXIT LIGHT SWITCH IS IN THE ARMED POSITION. FOUND WIRE 1741 AT TERMINAL BLOCK 2749VT INSTALLED IN WRONG LOCATION, BLOCK 29, POSITION G. MOVED TO CORRECT LOCATION BLOCK 30, POSITION H.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,424 hrs · 22,340 cycles
CRACK INDICATION AT AFT FASTENER HOLE SIDE BOX BEAM AT FRAME 43 RT, PERMANENT REPAIR PER ERA 549739-14.
Part: BOX BEAM — CRACKED (FRAME 43) · airframe 42,424 hrs · 22,340 cycles
CRACK INDICATION AT AFT FASTENER HOLE SIDE BOX BEAM AT FRAME 43, REPAIRED IAW ERA 549762-14.
Part: BOX BEAM — CRACKED (FRAMES 43) · airframe 42,302 hrs · 22,276 cycles
CENTER FUSELAGE LT SIDE BOX BEAM AT FRAMES 43, Y1650, CRACK INDICATION, IAW ER/A 549762-14.
Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 40,870 hrs · 21,487 cycles
ROW 13, EMERGENCY EXIT LIGHT INOPERATIVE, REPAIRED WIRING.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS) · airframe 40,870 hrs · 21,487 cycles
ROW 11, EMERGENCY EXIT LIGHT INOPERATIVE, INSTALLED NEW CONNECTOR FOR EMERGENCY EXIT ROW LIGHT 11.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 40,741 hrs · 21,421 cycles
EPSU BATTERY FWD LT MESSAGE, REPLACED BATTERY PACK ON PSU 10WL.
2014
Part: STRINGER — CORRODED (FRAMES 59-60) · airframe 42,923 hrs · 22,575 cycles
CORROSION FOUND ON STRINGER 42L BETWEEN FRAMES 59 AND 60. REMOVED CORROSION, TREATED, PRIMED. A REPAIR WAS FABRICATED, AND INSTALLED IAW SRM.
Part: STRINGER — CORRODED (FRAMES 59-60) · airframe 42,923 hrs · 22,575 cycles
CORROSION FOUND ON STRINGER 43L BETWEEN FRAMES 59 AND 60. REMOVED CORROSION, TREATED AND PRIMED. A REPAIR WAS FABRICATED, AND INSTALLED IAW SRM.
2013
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 34,561 hrs · 17,936 cycles
CABIN EMERGENCY LIGHTS, AND TWO AFT EXIT SIGNS. THREE CEILING EMERGENCY LIGHTS NEAR ASSOCIATED INOPERATIVE EVACUATION LIGHTS INOPERATIVE ON EMERGENCY POWER. LIGHTS FLASH FOR A SECOND WHEN ON BATTERY POWER. ALL LIGHTS WORK NORMAL WHEN ACFT ON NORMAL POWER. R & R EMERGENCY POWER SUPPLY UNIT AND BATTERY PACK IAW MM 33-51-38-400 001-A. PERFORMED OPS TEST OF THE EMERGENCY LIGHTS IAW MM 33-51-00-710-001-A TEST OK. ACFT OK FOR SERVICE.
Part: EPSU — FAULTED (EMERGENCY LIGHTS) · airframe 32,671 hrs · 16,834 cycles
LT EPSU BATTERY FAULT R & R LT EPSU BATTERY IAW AMM 33-51-38 PB 401. OPS CHECKED GOOD.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 32,601 hrs · 16,792 cycles
EMERGENCY LIGHTS AT DOOR 2R INOPERATIVE. FOUND WIRES DISCONNECTED. RECONNECTED AND OPS CHECKED OK.
Part: BATTERY PACK — FAILED (EMERGENCY LIGHT) · airframe 32,601 hrs · 16,792 cycles
EMERGENCY LIGHT BATTERY PACK AT DOOR 1L FAILS TEST. R & R BATTERY PACK IAW AMM 33-51-38. OPS CHECKED OK.
2012
Part: WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 32,374 hrs · 16,625 cycles
SEAT 4 EMERGENCY LIGHT INOPERATIVE. FOUND BROKEN WIRE AND REPAIRED. OPS CHECK NORMAL.
Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 32,162 hrs · 16,494 cycles
EMERGENCY EXIT PATHWAY LIGHT INOPERATIVE AT SEAT 12 ABC. FOUND WIRE BROKEN AT WHITE CONNECTOR UNDER AFT SEAT SUPPORT BAR. CONNECTED CONNECTOR. OPS CHECKED GOOD.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 31,675 hrs · 16,242 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT LOCATION 06C. SECURED WIRING. CHECKED NORMAL. OK FOR SERVICE.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 31,675 hrs · 16,242 cycles
EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT LOCATION 06C. SECURED WIRING. CHECKED NORMAL. OK FOR SERVICE.
Part: PANEL — DAMAGED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 151HE DAMAGED 1 INCHES BY 1 INCH. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — PUNCTURED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FORWARD CARGO FLOOR PANEL 131AF MULTIPLE PUNCTURES. FLOOR PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: PANEL — DAMAGED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 151GE DAMAGED 1.5 INCHES BY 1 INCH. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: PANEL — GOUGED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FWD CARGO SLOPE PANEL 131CF SKIN GOUGES 2 BY 2 INCHES. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: PANEL — PUNCTURED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FORWARD CARGO SLOPE PANEL 132DG SKIN PUNCTURES 3 X 3 INCHES. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: PANEL — DAMAGED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FORWARD CARGO SLOPE PANEL 132EG IS DAMAGED. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: PANEL — DAMAGED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FORWARD CARGO SLOPE PANEL 131DG IS DAMAGED. SLOPE PANEL FABRICATED NEW IAW SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 161NF MULTIPLE PUNCTURES 2.0 INCHES BY 2.5 INCHES. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.
Part: PANEL — DELAMINATED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 151DE DELAMINATED 2 FT BY 2 INCHES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.
Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 152WG MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.
Part: PANEL — DELAMINATED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 162BF DELAMINATED 2 INCH BY 2 INCH. SLOPE PANEL FABRICATED PER DWG NR 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.
Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 152UG MULTIPLE PUNCTURES. FABRICATED NEW PANEL PER DWG 3D25-40532 AS PER SRM 53-02-00 FIG 209.
Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 152TG MULTIPLE PUNCTURES. FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 209 DWG NR 3D25-40532.
Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 151UG HAS EDGE DAMAGE 6 INCHES BY 1 INCH. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00 FIG 209 DWG 3D25-40532.
Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 152XG MULTIPLE PUNCTURES. FABRICATED SLOPE PANEL PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.
Part: PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO SLOPE PANEL 151BE MULTIPLE PUNCTURES. SLOPE PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — PUNCTURED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 161PF PUNCTURED 1.0 INCH BY 1.0 INCH. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW A319 SRM 53-02-00 FIG 209.
Part: PANEL — DELAMINATED (FWD CARGO) · airframe 31,595 hrs · 16,194 cycles
FORWARD CARGO SLOPE WALL PANEL 131BF PUNCTURED AND DELAMINATED. FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 209 DWG 3D25-40532.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 151CE DELAMINATED 3 INCH BY 3 INCHES. FABRICATED NEW FLOOR PANEL PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — DELAMINATED (AFT CARGO) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 151ZG DELAMINATED 4 INCHES BY 4 INCHES. FLOOR PANEL FABRICATED PER DWG 3D25-40532 IAW SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY FLOOR PANEL 261PF DAMAGED 4" BY 4". FABRICATED NEW FLOOR PANEL 261PF AT AFT UTILITY AREA IAW A319 SRM 53-02-00 FIG 209.
Part: FLOOR PANEL — DELAMINATED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FWD UTILITY FLOOR PANEL 231CF DELAMINATED. FABRICATED NEW FLOOR PANEL 231CF AT FWD UTILITY AREA IAW A319 SRM 53-02-00 FIG 209. DAMAGE DIM L=1.0" W=1.5".
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY FLOOR PANEL 232FF HAS CORROSION. FABRICATED NEW FLOOR PANEL 232FF AT FORWARD UTILITY AREA IAW A319 SRM 53-02-00 FIG 209. DAMAGE DIM L=1.5" W=1.5".
Part: SILL — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
RIGHT PASSENGER DOOR WAY AT FR16 INSIDE GIRT BAR FITTING DOOR SILL HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00, L=.180" W=.180" D=.016. NO ESTABLISHED LIMITS AVAILABLE IAW A319 SRM 51-11-14. REMOVED DOOR SILL FR16 TO FR20 IAW A319 SRM 51-42-11. RECEIVED NEW DOOR SILL. INSTALLED NEW DOOR SILL FR16 TO FR20 IAW A319 SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT CABIN UTILITY AREA FLOOR SUPPORT WEB UPPER SURFACE AREA COVERED BY SHEAR PLATE HAS CORROSION, LOC FR69-FR70, STR 23R. REMOVED CORROSION IAW A319 SRM 51-74-00 L=2.5 W=1.5 D=.054 ORIG. .063 NO ESTABLISHED LIMITS PER A319 SRM 53-41-14. REMOVED AND INSTALLED NEW FLOOR SUPPORT WEB FR69-FR70 STR 23R IAW A319 SRM 51-42-11.
Part: SKIN — DENTED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT FUSELAGE LOWER EXTERNAL SKIN (BELOW L2 DOOR 3 INCH FWD OF FR 68 BTW STR 28L - 29L) DENTED (PREVIOUSLY IDENTIFIED ON LP 3335721). HFEC IAW NTM 51-10-08 PT 6 INTERNAL AND EXTERNAL. NO DEFECTS. DIMENSION OF DENTED AREA L=2.7 W=1.5 D=0.053 A=1.85 B=0.58 ORIGINAL THICKNESS .063. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-11. CUTOUT DAMAGED SKIN IAW A319 SRM 53-41-11 FIG 213. L=1.160 W=1.150. PERFORMED HFEC INSPECTION OF CUTOUT IAW NTM 51-10-08 PT 6 WITH NO CRACK INDICATIONS NOTED. FABRICATED DOUBLER IAW A319 SRM 53-41-11 FIG 213. INSTALLED FILLER WASHER IAW A319 SRM 51-71-15. TOTAL WEIGHT OF REPAIR PARTS 0.181LB. INSTALLED DOUBLER IAW A319 SRM 51-42-11 AND 53-41-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY AREA FLOORBEAM BTW FR14 TO FR16 Y765 UPPER FLANGE HOLES HAS CORROSION. BLENDED CORRODED AREA IAW A319 SRM 51-74-00 DIM L=1.400 INCH W=1.200 INCH D=.065 INCH. FOUND OUT OF LIMITS IAW A319 SRM 53-11-14 FIG 102. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR64 TO FR66 Y-765 HARD POINT HOLES UPPER FLANGE SURFACE CORRODED. BLENDED AREA IAW A319 SRM 51-74-00. ORIGINAL THICKNESS .087" D+.060" L=1.5" W=1". REMAINING THICKNESS .027 FOUND OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED FLOORBEAM BETWEEN FRAME 64 AND 66 Y-765 IAW A319 SRM 51-42-11. LOCATED AND DRILLED NEW FLOORBEAM FASTENER HOLES IAW A319 SRM 51-44-11. INSTALLED NEW FLOORBEAM IAW A319 SRM 53-21-01 AND A319 SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR64 TO FR66 Y1292 HARD POINT HOLES AND UPPER FLANGES HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11 ORIG MAT. .087 INCH. DAMAGE DIM L=2.10" W=1.30" D=.027".
Part: FLOOR PANEL — CORRODED (CABIN) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY FLOOR PANEL 222FF HAS CORROSION. RECEIVED NEW FLOOR PANEL INSTALLED ON JOB CARD 2500-6601.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR68 TO FR69 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11. ORIG MAT. .157". DAMAGE DIM L=2.0" W=1.10" D=.037".
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR66 TO FR68 Y1292 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW A319 SRM 51-42-11. ORIG MAT. .087". DAMAGE DIM L=2.0" W=1.66" D=.032".
Part: FLOOR SUPPORT — CORRODED (CARGO BAY) · airframe 31,595 hrs · 16,194 cycles
AFT CARGO FLOOR PANEL 152BE CORRODED AROUND FASTENER HOLE .200 INCH BY .150 INCH. AFT CARGO FLOOR PANEL REPLACED IAW A319 SRM 51-72-00. INSTALLED ON W/C 2500-5919 PANEL 152BE. NO LIMITS AVAILABLE.
Part: SHEAR PLATE — CRACKED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA RT SIDE BTW FR 68 TO FR 69 STRINGER 23R SHEAR PLATE CRACKED. REMOVED SHEAR PLATE AND SUPPORT IAW SRM 51-42-11. LOCATED AND DRILLED NEW SHEAR PLATE IAW SRM 51-44-11. INSTALLED NEW SHEAR PLATE IAW SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY AREA FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND OUT OF LIMITS IAW SRM 53-11-14 FIG 107. REMOVED AND REPLACED IAW SRM 51-42-11.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY FLOOR PANEL 261FF CORRODED 5 INCHES BY 4 INCHES. FLOOR PANEL INSTALLED ON W/C 5310-6017.
Part: FLOOR PANEL — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY FLOOR PANEL 262FF CORRODED 3 INCH BY 5 INCH. FLOOR PANEL INSTALLED ON W/C 5310-6017.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-15. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY AREA FLOOR SUPPORT CORRODED. BLENDED AREA IAW SRM 51-74-00. REMOVED AND REPLACED FLOOR SUPPORT IAW SRM 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY AREA FLOOR SUPPORT CORRODED. BLENDED AREA IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14 FIG 106. REMOVED FLOOR SUPPORT IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT IAW SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
FORWARD UTILITY AREA FLOORBEAM AT FR 14 Y-81 UNDERNEATH OF RAIL HAS CORROSION. REMOVED AND REPLACED FR 14 BEAM Y-81 IAW SRM 51-42-11.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR 68 TO 69 Y-1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.
Part: FLOORBEAM — CORRODED (CABIN) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR 66 TO FR 68 Y-765 UPPER FLANGE HAS CORROSION. BLENDED AREA IAW SRM 51-74-00 ORIGINAL THICKNESS .157 INCH D=0.040 INCH DIA 3.5 INCH, FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REMOVED BEAM BETWEEN FRAME 66 AND 68 Y-765 IAW SRM 51-42-11. LOCATED AND DRILLED NEW FLOORBEAM IAW SRM 51-44-11. INSTALLED NEW FLOORBEAM IAW TRM 53-21-01 AND SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM AT FR68 Y-465 UPPER FLANGE HAS CORROSION. REMOVED AND REPLACED FLOORBEAM AT FR 68 Y-465 IAW SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR 66 TO FR 68 Y-1292 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 SRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 31,595 hrs · 16,194 cycles
AFT UTILITY AREA FLOORBEAM BTW FR 64 TO 66 Y-1292 HARD POINT UPPER FLANGE HOLES CORRODED. REMOVED CORROSION IAW A319 SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW A319 TRM 53-41-15. REMOVED AND REPLACED BEAM IAW A319 SRM 51-42-11.
2008
Part: PUMP — LEAKING (HYD SYSTEM) · airframe 19,289 hrs · 9,605 cycles
EN ROUTE GREEN SYS HYD QUANTITY DECREASING, GOT GREEN HYD LOW PRESS ON ECAM. WENT THROUGH ECAM COM, SHUT-DOWN GREEN HYD SYSTEM PER COM. QUANTITY AMOUNT GRADUALLY DECREASED BELOW AMBER BOX WHEN GOT THE ECAM MESSAGE GREEN LOW PRESS. PER COM LANDING GEAR ALTERNATE EXTENDED (VERIFIED ON AMMRS) WITH UNEVENTFUL LANDING AND TOWED TO GATE.
2002
airframe 4,853 hrs · 2,198 cycles
Received VENT EXTRACT FAULT shortly after takeoff. Crew experienced grinding noise, mild vibration and strong smoke smell. Returned to IAH and landed uneventfully. Found avionics cooling extract fan 18Q failed. Applied MEL 21-26-02 provisions and returned A/C to service.