# Service difficulty reports: N332NW, cancelled Mar 15, 2025

A list on [N332NW, cancelled Mar 15, 2025](https://openairdocs.org/deregistered/N332NW-2025-03-15.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 4 · 188 reports

- [SDR DALA2023070705491](https://openairdocs.org/sdr/DALA2023070705491.md): Unknown · unknown · Jul 5, 2023 · N332NW · Airbus A320211 · Life Raft
  > SHIP 3232 32ABC LIFE RAFT INOP. CORRECTIVE ACTION: REPLACED RAFT PER A320 AMM 25-61. (9669959)
- [SDR DALA2023070305336](https://openairdocs.org/sdr/DALA2023070305336.md): Unknown · unknown · Jun 30, 2023 · N332NW · Airbus A320211 · Trailing Edge Flaps
  > SHIP 3232 LH OUTBOARD FLAP RIB 1 REPAIR. CORRECTIVE ACTION: COMPLIED WITH ERA 610112-14. (2842864)
- [SDR DALA2023042003117](https://openairdocs.org/sdr/DALA2023042003117.md): Unknown · unknown · Apr 19, 2023 · N332NW · Airbus A320211 · Emergency Lighting
  > SHIP 3232 20E SEAT HAS EXPOSED WIRE FOR ESCAPE LIGHTING. DAMAGED CAUSED BY PASSENGER. CORRECTIVE ACTION: SPLICED WIRE AT 20E PER A320 ESPM CHP 20. REF A320 WDM 33-51-07. OPS CHECK GOOD. (4752580)
- [SDR DALA2023032202156](https://openairdocs.org/sdr/DALA2023032202156.md): Unknown · unknown · Mar 22, 2023 · N332NW · Airbus A320211 · Air Conditioning System
  > SHIP 3232 CREW REPORTS: SMOKE/FUMES ON LANDING. BEGAN AT FWD GALLEY, WITH SMELL OF FUEL & AND WISPY LIGHT GRAY SMOKE APPEARED. SMOKE QUICKELY DISIPATED ROUGHLY 2 MINUTES AFTER ORIGINAL SMOKE/FUMES APPEARED. CORRECTIVE ACTION: INSPECTED FOR OIL LEAKS AND ENGINE
- [SDR DALA2022111807432](https://openairdocs.org/sdr/DALA2022111807432.md): Unknown · none · Nov 17, 2022 · N332NW · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3232 NEED TO COMPLY WITH INSPECTION AREA FOR WC 5311-01244-01A, SB A320-53-1491 R0, EASA PAD 21-090 (LH SIDE). CORRECTIVE ACTION: COMPLIED WITH. (2500127)
- [SDR DALA2022111707406](https://openairdocs.org/sdr/DALA2022111707406.md): Repair · none · Nov 17, 2022 · N332NW · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3232 PREVIOUS REPAIR LOCATED IN INSPECTION AREA FOR WC 5311-01244-01B, SB A320-53-1491 R0, EASA PAD 21-090 (RH SIDE). CORRECTIVE ACTION: COMPLIED WITH ERA 603790-14AD. (2499626)
- [SDR DALA2022111707404](https://openairdocs.org/sdr/DALA2022111707404.md): Frame · none · Nov 16, 2022 · N332NW · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3232 AD 2022-15-05, ER/A 603790-14AD SECTION II AND SECTION IV ISSUED FOR LH FR68 WEB AT DOOR- STOP FITTING 1. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH ER/A 603790-14AD SECTION II. (2499236)
- [SDR DALA2022111707403](https://openairdocs.org/sdr/DALA2022111707403.md): Frame · none · Nov 16, 2022 · N332NW · Airbus A320211 · Fuselage Main, Frame
  > SHIP 3232 AD 2022-15-05, ER/A 603790-14AD SECTION I AND SECTION III ISSUED FOR LH FR68 WEB AT DOOR- STOP FITTING 1. FOLLOW ON ACTION IS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH ER/A 603790-14AD SECTION I. (2499230)
- [SDR DALA2022111507361](https://openairdocs.org/sdr/DALA2022111507361.md): Door Frame · damaged · Nov 14, 2022 · N332NW · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3232 FITTING REPAIR INSTALLED ON R2 DOOR SURROUND AFT FRAME FR68, LH AT STGR-22 AND DOOR STOP 1 PER ERA 587207-14AD REV A. FOLLOW-ON INSPECTIONS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. (2495951)
- [SDR DALA2022111507360](https://openairdocs.org/sdr/DALA2022111507360.md): Door Frame · damaged · Nov 14, 2022 · N332NW · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3232 FITTING REPAIR INSTALLED ON R2 DOOR SURROUND AFT FRAME FR68, LH AT STGR-22 AND DOOR STOP 1 PER ERA 587207-14AD REV A. FOLLOW-ON INSPECTIONS REQUIRED. CORRECTIVE ACTION: COMPLIED WITH INSPECTION. (2495945)
- [SDR DALA2022100706507](https://openairdocs.org/sdr/DALA2022100706507.md): None · none · Oct 7, 2022 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 2DC PSU O2 PANEL WOULD NOT DROP. CORRECTIVE ACTION: R/R PSU WIRE HARNESS PER DELTA W/C 2527-01041-02. OPS CHK GOOD. (9395863)
- [SDR DALA2022081605538](https://openairdocs.org/sdr/DALA2022081605538.md): None · none · Aug 13, 2022 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 AFT LT LAV O2 PANEL DID NOT DROP DURING TEST. CORRECTIVE ACTION: REPACKED MASKS AND REPLACED STOW SWITCH. OPS CHECK GOOD. (9066639)
- [SDR DALA2022071904975](https://openairdocs.org/sdr/DALA2022071904975.md): Housing · broken · Jul 19, 2022 · N332NW · Airbus A320211 · Emergency Lighting
  > SHIP 3232 SEAT MOUNTED EMERG LIGHT HOUSING AT ROW 27 DEF BROKEN. CORRECTIVE ACTION: HOUSING TO BE REPLACED PER A320 AMM 33-51. (9189024)
- [SDR DALA2022042502881](https://openairdocs.org/sdr/DALA2022042502881.md): None · none · Apr 23, 2022 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 DURING TEST SEAT 17 DEF PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (8755887)
- [SDR DALA2022042502880](https://openairdocs.org/sdr/DALA2022042502880.md): None · none · Apr 23, 2022 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 DURING TEST SEAT 23 ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OPS TEST GOOD. (8755886)
- [SDR DALA2021110806843](https://openairdocs.org/sdr/DALA2021110806843.md): Light · inoperative · Nov 5, 2021 · N332NW · Airbus A320211 · Emergency Lighting
  > SHIP 3232 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE AT SEAT 19D. CORRECTIVE ACTION: RESUCURED LIGHT ASSY AS SEAT 19D. OK FOR SERVICE. (2008041)
- [SDR DALA2021081904817](https://openairdocs.org/sdr/DALA2021081904817.md): Latch · lack of lube · Aug 18, 2021 · N332NW · Airbus A320211 · Emergency Equipment
  > SHIP 3232 ENTRY DOOR ARMING LEVER HARD TO OPERATE. LOCATION: R1. CORRECTIVE ACTION: CLEANED AND LUBRICATED R1 DOOR GIRT BAR LATCHES. LUBED DOOR ARMING LEVER. R1 DOOR ARMS WITH NORMAL EFFORT AND CONSISTENT INDICATION OF ECAM. OK FOR SERVICE.
- [SDR DALA2021071303941](https://openairdocs.org/sdr/DALA2021071303941.md): Skin · corroded · Jul 12, 2021 · N332NW · Airbus A320211 · Wing, Plate/Skin
  > SHIP 3232 CORROSION UPPER SURFACE UPPER SKIN LOCATED BTW RIB19 TO RIB20 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR PER PRI ER/A #592618-14 REV. O AND ER/A 592618-14 REV. ORIGINAL. (1873200)
- [SDR DALA2021071203894](https://openairdocs.org/sdr/DALA2021071203894.md): Panel · cracked · Jul 9, 2021 · N332NW · Airbus A320* · Vertical Stabilizer, Plate/Skin
  > SHIP 3232 CRACK LEADING EDGE ACCESS PANEL 322AL ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED ACCESS PANEL 322AL AS PER ER/A 592557-14 REVISION ORIGINAL 07-JUL-21 AND ERA 592257-14 PRI REV.0 AND A320 SRM TASK 55-32-11. (1869484)
- [SDR DALA2021070703764](https://openairdocs.org/sdr/DALA2021070703764.md): Web · corroded · Jul 6, 2021 · N332NW · Airbus A320211 · Nacelle/Pylon Miscellaneous Structure
  > SHIP 3232 CORROSION HORIZONTAL WEB AFT MOVABLE FAIRING ON RH PYLON. CORRECTIVE ACTION: REPLACED HORIZONTAL WEB AFT MOVABLE FAIRING ON RH PYLON AS PER SRM A320 51-72-11. JOB COMPLETE. (1865794)
- [SDR DALA2021070203658](https://openairdocs.org/sdr/DALA2021070203658.md): Skin · corroded · Jul 2, 2021 · N332NW · Airbus A320* · Wing, Plate/Skin
  > SHIP 3232 CORROSION UPPER SURFACE UPPER SKIN LOCATED BTW RIB24 TO RIB25 TRAILING EDGE AREA ON RH WING. CORRECTIVE ACTION: EVALUATED REWORKED AREA ON UPPER SURFACE UPPER SKIN LOCATED BTW RIB24 TO RIB25 TRAILING EDGE AREA ON RH WING AND FOUND WITHIN LIMITS AS PE
- [SDR DALA2021051702723](https://openairdocs.org/sdr/DALA2021051702723.md): Panel · no test · May 16, 2021 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 DURING TEST SEAT 22ABC PSU OXY PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7283069)
- [SDR DALA2021051702722](https://openairdocs.org/sdr/DALA2021051702722.md): Panel · no test · May 16, 2021 · N332NW · Airbus A320211 · Passenger Oxygen System
  > SHIP 3232 DURING TEST SEAT 14ABC PSU OXYGEN PANEL DID NOT OPEN. CORRECTIVE ACTION: REPACKED MASKS. OK FOR SERVICE. (7283068)
- [SDR DALA2021022301059](https://openairdocs.org/sdr/DALA2021022301059.md): Light · detached · Feb 22, 2021 · N332NW · Airbus A320211 · Emergency Lighting
  > SHIP 3232 SEATS 31D 17D 15D EMERGENCY SEAT MOUNTED LIGHTING DAMAGED. CORRECTIVE ACTION: RESECURED LIGHTING. OK FOR SERVICE. (1737306)
- [SDR DALA2021070703765](https://openairdocs.org/sdr/DALA2021070703765.md): Fitting · cracked · Dec 18, 2020 · N332NW · Airbus A320211 · Wing Main, Frame Structure
  > SHIP 3232 ER/A 588785-14AD IS GENERATED FOR THE RH AFT SPAR TO PINTLE FITTING JOINT AT HOLE 16R. (CRACK): CORRECTIVE ACTION: PER ER/A #588785-14AD REV.ORIGINAL. OK TO CONTINUE ON MONITOR. REPETITIVE INSPECTION IS REQUIRED 25,200 FLIGHT CYCLES OR 41,400 FLIGHT
- [SDR DALA2020120803997](https://openairdocs.org/sdr/DALA2020120803997.md): Housing · damaged · Dec 7, 2020 · N332NW · Airbus A320211 · Emergency Lighting
  > EMERGENCY ESCAPE PATH LIGHT AT SEAT 19DEF DAMAGED. CORRECTIVE ACTION: R & R EMERGENCY LIGHT HOUSING AND TESTED LIGHTING SYSTEM. OK FOR SERVICE.
- [SDR DALA2022111507362](https://openairdocs.org/sdr/DALA2022111507362.md): Door Frame · damaged · Jul 31, 2020 · N332NW · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT DOOR STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD. (1587429)
- [SDR DALA2022111507359](https://openairdocs.org/sdr/DALA2022111507359.md): Web · cracked · Jul 31, 2020 · N332NW · Airbus A320211 · Fuselage Main, Structure
  > SHIP 3232 ER/A 587207-14AD ISSUED FOR LH FR68 WEB AT STOP 1 CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 587207-14AD REV A. (1587431)
- [SDR DALA202001220500](https://openairdocs.org/sdr/DALA202001220500.md): Battery Pack · no test · Jan 20, 2020 · N332NW · Airbus A320211 · Emergency Lighting
  > EMERGENCY TEST FAILS LT BATTERY, REPLACED LT BATTERY FOR EPSU
- [SDR DALA2019092205475](https://openairdocs.org/sdr/DALA2019092205475.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE AT FRAME 36 AND Y1292 + 5 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 7 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC. AT F
- [SDR DALA2019092205474](https://openairdocs.org/sdr/DALA2019092205474.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292+5 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LO
- [SDR DALA2019092205473](https://openairdocs.org/sdr/DALA2019092205473.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 +3 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF PRESSURE DECK MEMBRANE LOC AT FR36
- [SDR DALA2019092205472](https://openairdocs.org/sdr/DALA2019092205472.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND Y1292 + 2 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 AND 6 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FSTENER HOLE OF THE PRESSURE DECK MEMBRANE LO
- [SDR DALA2019092205471](https://openairdocs.org/sdr/DALA2019092205471.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED
- [SDR DALA2019092205470](https://openairdocs.org/sdr/DALA2019092205470.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +7 INCH OF THE RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 1 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED
- [SDR DALA2019092205469](https://openairdocs.org/sdr/DALA2019092205469.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+3 INCH ON RT SIDE (CRACK INDICATION IS 11 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR
- [SDR DALA2019092205468](https://openairdocs.org/sdr/DALA2019092205468.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC AT FR36 AND -Y1292+2INCH RT SIDE (CRACK DIRECTION IS 10 O'CLOCK) IN FWD CARGO COMPARTMENT, PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DUCT MEMBRANE LOC AT FR 36 A
- [SDR DALA2019092205467](https://openairdocs.org/sdr/DALA2019092205467.md): Angle · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CRACK INDICATION ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED AT FRAME 36 AND Y1292+ 1 INCH OF LT SIDE IN FWD CARGO COMPARTMENT (2 EA) (CRACK LENGTH 0.923 AND 0.498 INCH APPROX), PERFORMED REPAIR INSTRUCTIONS ON INTERNAL STRUCTURE ON TITANIUM ANGLE LOCATED
- [SDR DALA2019092205466](https://openairdocs.org/sdr/DALA2019092205466.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +6 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION ARE 6 AND 12 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOC
- [SDR DALA2019092205465](https://openairdocs.org/sdr/DALA2019092205465.md): Pressure Deck · cracked · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Bulkhead
  > CRACK INDICATION ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE LOCATED AT FRAME 36 AND -Y1292 +4 INCH OF RT SIDE IN FWD CARGO COMPARTMENT (CRACK DIRECTION IS 11 O'CLOCK), PERFORMED REPAIR INSTRUCTIONS ON OPEN FASTENER HOLE OF THE PRESSURE DECK MEMBRANE L
- [SDR DALA2019092205464](https://openairdocs.org/sdr/DALA2019092205464.md): Spar · corroded · Sep 22, 2019 · N332NW · Airbus A320211 · Wing, Rib/Bulkhead
  > CORROSION FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING, PERFORMED REPAIR INSTRUCTIONS ON FALSE SPAR BOX LOCATED ON FITTING AT RIB 5 INTERNAL AREA ON LT WING AS PER PRI 581186-14 REV 0 AND REV 1 AND ER/A 581186-14 REV ORIGINAL.
- [SDR DALA2019092205463](https://openairdocs.org/sdr/DALA2019092205463.md): Stringer · corroded · Sep 22, 2019 · N332NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 41R LOWER FLANGE, BTW FRAME 25 AND FRAME 28 IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRG 41R LOC BTW FR 24 TO FR 30 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND DRAWING #D53231586.
- [SDR DALA2019092205462](https://openairdocs.org/sdr/DALA2019092205462.md): Spar · corroded · Sep 21, 2019 · N332NW · Airbus A320211 · Wing, Rib/Bulkhead
  > CORROSION FALSE SPAR BOX SKIN LOCATED RIB5 BOTTOM SURFACE ON RT WING, PERFORMED TIME-LIMITED REPAIR FALSE SPAR BOX SKIN LOCATED RIB 5 BOTTOM SURFACE ON RT WING AS PER PRI 581187-14 REV 0 AND ER/A 581187-14 REV ORIGINAL.
- [SDR DALA2019091505409](https://openairdocs.org/sdr/DALA2019091505409.md): Cleat · corroded · Sep 14, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION CLEAT BTW STR 43L TO 42L AT LEVEL OF FR33 IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT BTW STR 43L TO STR 42L LEVEL FR33 FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D5323039820001.
- [SDR DALA2019091505408](https://openairdocs.org/sdr/DALA2019091505408.md): Cleat · corroded · Sep 14, 2019 · N332NW · Airbus A320211 · Fuselage Miscellaneous Structure
  > CORROSION CLEAT AT LEVEL OF FR31 AND BTW STRG 41R AND STRG 42R IN FWD CARGO COMPARTMENT (1 EA), REPLACED CLEAT AT LEVEL OF FR31 AND BTW STR 41R AND STR 42R IN FWD CARGO COMPARTMENT (1E/A) AS PER SRM 51-42-00, 51-72-11 AND DRAWING D53230514
- [SDR DALA2019091105299](https://openairdocs.org/sdr/DALA2019091105299.md): Stringer · corroded · Sep 10, 2019 · N332NW · Airbus A320211 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT, REPLACED STRINGER LOC. STRINGER 42L BTW FR27 TO FR31 IN FWD CARGO COMPARTMENT AS PER SRM 51-72-11 AND 51-42-11. DRAWING D53231626.
- [SDR DALA2019090705246](https://openairdocs.org/sdr/DALA2019090705246.md): Strap · corroded · Sep 7, 2019 · N332NW · Airbus A320211 · Fuselage Main, Plate/Skin
  > CORROSION INTERNAL STRUCTURE (SKIN AREA), LOC FRAME 26+3INCH, STRINGER 40R, IN FWD CARGO COMPARTMENT (1 EA), REPLACED STRAP FITTING ON INTERNAL STRUCTURE FR 26 BTW 40R TO STR 41R AS PER SRM 51-72-11 AND SRM 51-42-11 AND DWG #D53231380.
- [SDR DALA2019090405189](https://openairdocs.org/sdr/DALA2019090405189.md): Frame · cracked · Sep 4, 2019 · N332NW · Airbus A320211 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 16 LT IN LOWER INBOARD HOLE OF DOOR STOP FITTING 7 CRACK POSITION 3 O'CLOCK AT FWD GALLEY AREA, REPLACED FITTING LOCATED ON FR 16 ON DOOR STOP FITTING #7 LT SIDE ASPER SRM 51-72-11 AND DWG D53112300.
- [SDR DALA2019083005188](https://openairdocs.org/sdr/DALA2019083005188.md): Seat Track · corroded · Aug 29, 2019 · N332NW · Airbus A320211 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y765 PREVIOUSLY REWORKED AND EVALUATED WITH CARD 2500-2031-DE WAS FOUND OUT LIMITS, REPLACED SEAT TRACK -Y765 BTW FR 41 TO FR 47 IN PASSENGER CABIN ASPER SRM 53-31-15-02A AND 51-72-11 AND DWG #D53472554.
- [SDR DALA2019082905185](https://openairdocs.org/sdr/DALA2019082905185.md): Floorbeam · corroded · Aug 28, 2019 · N332NW · Airbus A320211 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM -Y1292 AT LEVEL OF FR 68 AT AFT GALLEY AREA, REPLACED FLOORBEAM -Y1292 LOC. FR68 AT AFT GALLEY AREA ASPER SRM 51-72-11 AND 51-42-11, DWG # D53472000.

Next page: https://openairdocs.org/deregistered/N332NW-2025-03-15/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE n_number = 'N332NW' AND deregistration_id = 'N332NW-2025-03-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N332NW-2025-03-15/reports

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