# Service difficulty reports: N363NW

A list on [N363NW](https://openairdocs.org/aircraft/N363NW.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 5 · 222 reports

- [SDR DALA2026090104921](https://openairdocs.org/sdr/DALA2026090104921.md): Light · inoperative · Aug 26, 2026 · N363NW · Airbus A320212 · Emergency Lighting
  > SEAT 10D EMERGENCY LIGHT INOP. R & R 10D EMER ESCAPE PATH LIGHT IAW AMM 33-51-19. LIGHT OPERATES NORMALLY, OKAY FOR SERVICE. (LP: 8828773, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026082404778](https://openairdocs.org/sdr/DALA2026082404778.md): Indication Sys · inoperative · Aug 23, 2026 · N363NW · Airbus A320212 · Fuel Indicating System
  > ATB - DUE TO FUEL QTY IMBALANCE, RIGHT INBOARD TANK READ 1,200 LBS HIGHER THAN LEFT INBOARD TANK. REPLACED FQIC. (LP: 8828758, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060203357](https://openairdocs.org/sdr/DALA2026060203357.md): Oxygen Mask · unwanted deploy · May 26, 2026 · N363NW · Airbus A320212 · Passenger Oxygen System
  > AFT RIGHT LAV O2 MASK DEPLOYED AT CRUISE PAX IN LAVATORY. FWD TO MCO AND PLACARD PER MEL 35-21-02 AFT RIGHT LAVATORY OXY INOP, (M) PROCEDURES C/W. MCO AND PLACARD INSTALLED. R/R AFT RIGHT LAV EMERGENCY OXY CONTAINER PER AMM 35-21. OPTS CHECK GOOD. OK FOR SERV
- [SDR DALA2025032302157](https://openairdocs.org/sdr/DALA2025032302157.md): Battery Pack · no test · Mar 22, 2025 · N363NW · Airbus A320212 · Emergency Lighting
  > SHIP 3263 DISC: DURING SVC FOUND CABIN EMERGENGY LIGHTS AT ROWS 24-25, 28-29 AND 30. INOP. C/A: PER A320 AMM 33-51. R/R POWER UNIT BATTERY PACK AT 11WL. OPS CHECK GOOD. OK FOR SVC. (LP: 7215020)
- [SDR DALA2025021601168](https://openairdocs.org/sdr/DALA2025021601168.md): Outlet · smoke · Feb 16, 2025 · N363NW · Airbus A320212 · AC Power Distribution System
  > SHIP 3263 DISC: DURING BOARDING, SEAT 3A +3B ELECTRICAL OUTLET SMOKING/ ONCE POWERED DOWN SMOKE STOPPED. C/A: R/R SPM P/N RD-FA3622-01 S/N OFF/ON 333933/427987, R/R DC-SEB, R/R PED OUTLET AT SEAT 3AB REF PAC A320 AIPC (SPM) 23-81-08, (DC-SEB) 23-32-07, (PED O
- [SDR DALA2024100109585](https://openairdocs.org/sdr/DALA2024100109585.md): Filter · odor · Sep 30, 2024 · N363NW · Airbus A320212 · Air Distribution System
  > SHIP 3263 DISC: BOARDING ONTO THE AIRCRAFT THE CREW SMELLED DIRTY SOCK SMELL. C/A: PERFORMED WORK CARD 2100-2005. ALL OPS TESTS GOOD. AS PRECAUTION R+R RECIRCULATION FILTERS PER A320 AMM 21-21. ODI STEPS C/W REF LOG 0583248. (LP: 6653438)
- [SDR DALA2024052105382](https://openairdocs.org/sdr/DALA2024052105382.md): Proximity Sensor · faulted · May 20, 2024 · N363NW · Airbus A320212 · Landing Gear Position and Warning
  > SHIP 3263 - DIV - TO BWI DUE TO LANDING GEAR FAILING TO RETRACT. SYSTEM FAULTING NLG EXTEND PROX SENSORS. CORRECTIVE ACTION: MAINTENANCE IN PROGRESS.
- [SDR DALA2024031403322](https://openairdocs.org/sdr/DALA2024031403322.md): Light · detached · Mar 8, 2024 · N363NW · Airbus A320212 · Emergency Lighting
  > SHIP 3263 DISC: EMERGENCY PATH LIGHT AT SEAT 27F IS DETACHED FROM THE SEAT. C/A: RESECURED SAME. OK FOR SERVICE. (LP: 5273818)
- [SDR DALA2024022102450](https://openairdocs.org/sdr/DALA2024022102450.md): Module · failed · Feb 18, 2024 · N363NW · Airbus A320212 · Emergency Lighting
  > SHIP 3263 DISC: ROW 15 AISLE SEAT FWD EMERGENCY LIGHT INOP. C/A: REMOVED FWD LIGHT MODEUL PER A320 MM 33-51 412796. INST LITE MODULE CKS OK PER A320MM 33-51. (LP: 4897943)
- [SDR DALA2024021502253](https://openairdocs.org/sdr/DALA2024021502253.md): Anti-Ice Valve · faulted · Feb 13, 2024 · N363NW · Airbus A320212 · Engine Anti-Icing System
  > SHIP 3263 - ATB - DUE TO ANTI ICE ENG2 VALVE CLSD ECAM MESSAGE. CANNOT CONTINUE INTO ICING CONDITIONS. CORRECTIVE ACTION: R/R #2 ENGINE ANTI-ICE VALVE. NO HELP. ITEM PLACED ON MEL PROCEDURES C/W (LOCKED VALVE IN OPEN POSITION). (LP: 4897922)
- [SDR DALA2024020901762](https://openairdocs.org/sdr/DALA2024020901762.md): Extinguisher · discharged · Feb 7, 2024 · N363NW · Airbus A320212 · Extinguishing System
  > SHIP 3263 DISC: FWD CARGO FIRE EXTINGUISHER DISCHARGED. C/A: BEGAN RESTORATION OF FES SYS PER A320 AMM 26-23 (889397) REMOVED AND REPLACED FWD CARGO FIRE BOTTLE PER A319-320 AMM 26-16. RFID PENDING (221599) RFID TAGE INSTALLED. MEL/PLAC RMVD. OK FOR SERVICE. (
- [SDR DALA2024012200909](https://openairdocs.org/sdr/DALA2024012200909.md): Oxygen Mask · unwanted deploy · Jan 20, 2024 · N363NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3263 DISC: O2 MASKS CAME DOWN AT 13DFE UPON LANDING. C/A: REPACK O2 MASKS AT 13DEF PER A 320 AMM 35-21. (LP: 8914028)
- [SDR DALA2024011400564](https://openairdocs.org/sdr/DALA2024011400564.md): Unknown · unknown · Jan 11, 2024 · N363NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3263 DISC: AD RELATED:(5311-01244-01A) PREVIOUS REPAIR PART INSTALL AT L/H FR. 68, STGR 22LH, REQUESTING DELTA LIASON ENGINEERING TO DETERMINE IF SRM 53-41-12-300-011- STOP FTG HOLES OF LH AFT DOOR - REPAIR PART INSTALLATION WAS ACOMPLISHED WITH OR WITHOU
- [SDR DALA2024011400563](https://openairdocs.org/sdr/DALA2024011400563.md): Unknown · unknown · Jan 11, 2024 · N363NW · Airbus A320212 · Fuselage Main, Attach Fittings
  > SHIP 3263 DISC: BATHTUB FITTING ON FR.68 LOWER L/H SIDE, FOUND GOUGED DURRING INSPECTION. REF BY AIRBORNE/PEMCO NR.14821.0068. C/A: REMOVED AND REPLACED BATHTUB FITTING ON FR 68 LOWER L/H SIDE (#1 DOOR STOP AREA) AIW A320 SRM 53-41-12-300-011. SEALANT P/N PS87
- [SDR DALA2024011400566](https://openairdocs.org/sdr/DALA2024011400566.md): Unknown · unknown · Jan 10, 2024 · N363NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3263 DISC: AD RELATED:(5311-01244-01B) PREVIOUS REPAIR PART INSTALL AT R/H FR. 68, STGR 22RH, REQUESTING DELTA LIASON ENGINEERING TO DETERMINE IF SRM 53-41-12-300-011- STOP FTG HOLES OF RH AFT DOOR - REPAIR PART INSTALLATION WAS ACOMPLISHED WITH OR WITHOU
- [SDR DALA2023051003669](https://openairdocs.org/sdr/DALA2023051003669.md): Unknown · unknown · Nov 12, 2022 · N363NW · Airbus A320212 · Nacelle/Pylon, Attach Fittings
  > SHIP 3263 #2 ENGINE PYLON AFT MOUNT INBD SIDE DAMAGED. CORRECTIVE ACTION: COMPLIED WITH ERA 603758-14. (2492432)
- [SDR DALA2022082205659](https://openairdocs.org/sdr/DALA2022082205659.md): None · none · Aug 19, 2022 · N363NW · Airbus A320212 · Emergency Lighting
  > SHIP 3263 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:32D. CORRECTIVE ACTION: SECURED 32D EMERG LIGHT IN PLACE. OK FOR SERVICE. (2372165)
- [SDR DALA2021123008174](https://openairdocs.org/sdr/DALA2021123008174.md): None · none · Dec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK FOUND ON WINDSHIELD FRAME RH SIDE, CRACK LENGTH: 0.200 INCH, CRA CK AT 11 O CLOCK. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING R EPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. SIDE AS PER ER/A 595453-14AD REV. ORIGINAL AND
- [SDR DALA2021122908147](https://openairdocs.org/sdr/DALA2021122908147.md): None · none · Dec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK FOUND ON CONTINUITY FITTING LH SIDE, CRACK LENGTH: 0.190 INCH APPROX, VERTICAL DIRECTION. AD 2020-17-03/ WORKCARD 5311-01226- 01 REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTION ON CONTINUI
- [SDR DALA2021122908146](https://openairdocs.org/sdr/DALA2021122908146.md): None · none · Dec 29, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK FOUND ON CONTINUITY FITTING RH SIDE, CRACK LENGTH: 0.190 INCH, V ERTICAL CRACK. AD 2020-17-03/ WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. PERFORMED REPAIR INSTRUCTIONS FOR CONTINUITY FITTIN
- [SDR DALA2021122908139](https://openairdocs.org/sdr/DALA2021122908139.md): None · none · Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA RH SIDE, CRACK DIRECTION: 07 O CLOCK ( D1-D2=0.075 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA RH SIDE AS PER ER/A 543313-14
- [SDR DALA2021122908138](https://openairdocs.org/sdr/DALA2021122908138.md): None · none · Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > CRACK INDICATION FOUND IN OPEN FASTENER HOLE (1EA) LOCATED AT UPPER AT TACHMENT FRAME 4 SIDE POST AREA LH SIDE, CRACK DIRECTION: 01 O CLOCK APPROX (D1-D2=0.0665 INCH). PERFORMED PERMANENT REPAIR ON UPPER ATTACHMENT FRAME 4 SIDE POST AREA LH SIDE AS PER ER/A 54
- [SDR DALA2021122908133](https://openairdocs.org/sdr/DALA2021122908133.md): None · none · Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > OUT LIMIT FRAME 68 DOOR STOP FITTING 1L DIAMETER HOLE ?1= 0.252INCH,?2= 0.254INCH,?3=0.251INCH,?4=0.258INCH AA 5311 -01216 AD RELATED ACTIONS R EQUIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). PERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1L
- [SDR DALA2021122908132](https://openairdocs.org/sdr/DALA2021122908132.md): None · none · Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > OUT LIMIT FRAME 68 DOOR STOP FITTING 1 RH HOLE DIAMETER ?1= 0.257IN, ?2 =0.258IN, ?3=0.256IN, ?4=0.256IN AA 5311-01216 AD RELATED. ACTIONS REQ UIRED PRIOR TO FURTHER FLIGHT AT AFT GALLEY AREA (4 EA). ERFORMED PERMANENT REPAIR FRAME 68 DOOR STOP FITTING 1 RH AT
- [SDR DALA2021122908131](https://openairdocs.org/sdr/DALA2021122908131.md): None · none · Dec 28, 2021 · N363NW · Airbus A320212 · Fuselage Main, Keel
  > WEAR ON FITTING KEEL BEAM FWD, FWD LUG,FWD FACE RH SIDE IN MAIN WHEE L WELL (1 EA). PERFORMED REPAIR LOC. ON FITTING KEEL BEAM FWD, FWD LUG,FWD FACE RH SIDE IN MAIN WHEEL WELL (1 EA). AS PER PRI 595936-14AD, REV. 0. AND ER/A 595936-14AD, REV. ORIGINAL. APP
- [SDR DALA2021122808096](https://openairdocs.org/sdr/DALA2021122808096.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR THE LH FRAME 68 INSPECTING FOR CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066495)
- [SDR DALA2021122808095](https://openairdocs.org/sdr/DALA2021122808095.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR LH & RH FRAME 68. CORRECTIVE ACTION: COMPLIED WITH ERA. (2066491)
- [SDR DALA2021122808094](https://openairdocs.org/sdr/DALA2021122808094.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR RH FRAME 68 INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066486)
- [SDR DALA2021122808093](https://openairdocs.org/sdr/DALA2021122808093.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD DTA REQUIRED FOR THE FRAME 68 LH & RH INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. (2066483)
- [SDR DALA2021122808092](https://openairdocs.org/sdr/DALA2021122808092.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD SEC III REQUIRED FOR THE RH FRAME 68. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUE ON MON. (2066476)
- [SDR DALA2021122808091](https://openairdocs.org/sdr/DALA2021122808091.md): None · none · Dec 27, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 ER/A 595940-14AD SEC II REQUIRED FOR LH AND RH FRAME 68 INSPECTING FOR CRACKS. CORRECTIVE ACTION: COMPLIED WITH ERA. CONTINUED ON MON. (2066465)
- [SDR DALA2021122708048](https://openairdocs.org/sdr/DALA2021122708048.md): None · none · Dec 24, 2021 · N363NW · Airbus A320212 · Trailing Edge Flaps
  > SHIP 3263 CORROSION INTERCONNECTING STRUT OB FLAP ON CONNECTOR LH WING. CORRECTIVE ACTION: REMOVED AND REPLACED CONNECTOR ON INTERCONNECTING STRUT LH WING AS PER A320 AWM 27-51-12. (2063606)
- [SDR DALA2021122708043](https://openairdocs.org/sdr/DALA2021122708043.md): None · none · Dec 24, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 GOUGE SHEAR TIE LOCATED FR32 BTW STR 43L TO STR 44 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER 51-42-11 AND 51-72-11. (2063686)
- [SDR DALA2021122708047](https://openairdocs.org/sdr/DALA2021122708047.md): None · none · Dec 23, 2021 · N363NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3263 SEAT TRACK Y1292 AT LEVEL FR64 TO FR66 AT AFT GALLEY AREA OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND REPLACED SEAT TRACK PER ER/A 595627-14 REV. ORIGINAL. (2062573)
- [SDR DALA2021122708046](https://openairdocs.org/sdr/DALA2021122708046.md): None · none · Dec 23, 2021 · N363NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3263 SEAT TRACK -Y1292 AT LEVEL FR 64 TO FR66 AT AFT GALLEY AREA OUT OF LIMITS. CORRECTIVE ACTION: FABRICATED AND REPLACED SEAT TRACK PER ER/A 595630-14 REV. ORIGINAL. (2062571)
- [SDR DALA2021122908155](https://openairdocs.org/sdr/DALA2021122908155.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > DTA MONITOR INSPECTION LOG REFERENCE ER/A 595412-14 SECTION II REQUIRES DTA APPROVAL WITHIN 30600 CYCLES. ASSOCIATED ER/A 00-595412 ADDED FOR AC 3263. (LP# 2067204)
- [SDR DALA2021122908154](https://openairdocs.org/sdr/DALA2021122908154.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > DTA MONITOR INSPECTION LOG REFERENCE ER/A 595453-14 SECTION II REQUIRES DTA APPROVAL WITHIN 30600 CYCLES. DISCONTINUE REVENUE SERVICE WITHIN 30600 CYCLES AFTER SECT I PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-595453 ADDED FOR AC 3263. (
- [SDR DALA2021122908153](https://openairdocs.org/sdr/DALA2021122908153.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > DTA MONITOR INSPECTION LOG REFERENCE ER/A 543312-14 REV A SECTION VI REQUIRES DTA APPROVAL WITHIN 48000 CYCLES AFTER SECT III. DISCONTINUE REVENUE SERVICE WITHIN 48000 CYCLES AFTER SECT III PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-5433
- [SDR DALA2021122908152](https://openairdocs.org/sdr/DALA2021122908152.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > FUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT, SECTION V. ACCOMPLISH ER/A 543312-14 REV A SECTION V INSPECTION WITHIN 3,299 CYCLES AFTER SECTION III REPAIR, AND THEREAFTER WITHIN EVERY 11,000 CYCLES. (LP# 2067128)
- [SDR DALA2021122908151](https://openairdocs.org/sdr/DALA2021122908151.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > FUSELAGE / FRAMES / LHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT. ACCOMPLISH ER/A 543312-14 REV A SECTION IV INSPECTIONS WITHIN 21,100 CYCLES AFTER SECTION III AND THEREAFTER WITHIN EVERY 5,200 CYCLES. ASSOCIATED ER/A 00-543312 ADDED FOR AC 3263. (LPL# 2067
- [SDR DALA2021122908150](https://openairdocs.org/sdr/DALA2021122908150.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > DTA MONITOR INSPECTION LOG REFERENCE ER/A 543313-14 REV A SECTION VI REQUIRES DTA APPROVAL WITHIN 48000 CYCLESAFTER SECT III. DISCONTINUE REVENUE SERVICE WITHIN 48000 CYCLES AFTER SECT III PENDING A DAMAGE TOLERANCE AND FATIGUE REVIEW. ASSOCIATED ER/A 00-54331
- [SDR DALA2021122908149](https://openairdocs.org/sdr/DALA2021122908149.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > FUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT WITH DEVIATIONSFOR SECTION V. ACCOMPLISH ER/A 543313-14 REV A SECTION V INSPECTION WITHIN 3,299 CYCLES AFTER SECTION III REPAIR, AND THEREAFTER WITHIN EVERY 11,000 CYCLES. ASSOCIATED ER/A 00-5
- [SDR DALA2021122908148](https://openairdocs.org/sdr/DALA2021122908148.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > FUSELAGE / FRAMES / RHS LATERAL WINDOW FRAME & GUSSET / REPLACEMENT WITH DEVIATIONS. ACCOMPLISH ER/A 543313-14 REV A SECTION IV INSPECTIONS WITHIN 21,100 CYCLES AFTER SECTION III AND THEREAFTER WITHIN EVERY 5,200 CYCLES. ASSOCIATED ER/A 00-543313 ADDED FOR AC
- [SDR DALA2021122308007](https://openairdocs.org/sdr/DALA2021122308007.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 CORROSION INTERNAL STRUCTURE SKIN LAP JOINT AREA BTW STR 40/42 R AND BTW FR 33/34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: COMPLIED WITH PRI 595841-14 REV. 0. AND ER/A 595841-14AD REV. ORIGINAL. (2061442)
- [SDR DALA2021122308006](https://openairdocs.org/sdr/DALA2021122308006.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 CORROSION SHEAR TIE LOCATED FR29 BTW STR44 TO STR43L IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-42-11 AND 51-72-11. (2061439)
- [SDR DALA2021122308005](https://openairdocs.org/sdr/DALA2021122308005.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 CORROSION STRINGER 42R LOCATED BTW FR30 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-42-11 AND 51-72-11. (2061434)
- [SDR DALA2021122308004](https://openairdocs.org/sdr/DALA2021122308004.md): None · none · Dec 22, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 CORROSION SHEAR TIE LOCATED FR33 BTW STR42R TO STR43R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE PER A320 SRM 51-72-11 AND 51-42-11. (2061424)
- [SDR DALA2021122207983](https://openairdocs.org/sdr/DALA2021122207983.md): None · none · Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 CRACK INDICATION FOUND IN OPEN HOLE 07 LOCATED AT FRAME 16 LH SIDE. CORRECTIVE ACTION: REPAIRED PER PRI #595385-14AD REV.0, REV.1 AND ER/A #595385-14AD REV.ORIGINAL. (2060316)
- [SDR DALA2021122207982](https://openairdocs.org/sdr/DALA2021122207982.md): None · none · Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3263 CRACK INDICATION FOUND IN OPEN HOLE 06 LOCATED AT FRAME 16 LH SIDE. CORRECTIVE ACTION: COMPLIED WITH PRI #595385-14AD REV.0, REV.1 AND ER/A #595385-14AD REV.ORIGINAL. (2060311)
- [SDR DALA2021122207968](https://openairdocs.org/sdr/DALA2021122207968.md): None · none · Dec 21, 2021 · N363NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3263 CORROSION STRINGER 44 LOCATED BTW FR31 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED REPAIR ON STRINGER PER A320 SRM 53-00-13. (2060446)

Next page: https://openairdocs.org/aircraft/N363NW/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 = 'N363NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N363NW/reports

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