# Service difficulty reports: N362NW

A list on [N362NW](https://openairdocs.org/aircraft/N362NW.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 · 202 reports

- [SDR DALA2026102305835](https://openairdocs.org/sdr/DALA2026102305835.md): Shear Tie · corroded · Oct 21, 2026 · N362NW · Airbus A320212 · Fuselage Internal Mounting Structure
  > LEVEL 2 CORROSION, LOWER FWD FUSELAGE, FWD CARGO COMPARTMENT AT FR33 BETWEEN STGR 40L AND STGR 41L, FRAME CLIP WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 100-251. REPLACED SHEAR TIE AT FWD CARGO COMPARMENT AT FR 33 BETWEEN STGR 40L AND STGR 40L AND S
- [SDR DALA2026102105778](https://openairdocs.org/sdr/DALA2026102105778.md): Anchor Fitting · corroded · Oct 20, 2026 · N362NW · Airbus A320212 · Fuselage, Landing Gear Attach Fittings
  > LOWER FUSELAGE, LT MLG ANCHORAGE FITTING WITH CORROSION. REPAIRED LT MLG ANCHORAGE FITTING UPPER AND LOWER BEARING FACES, LUG BORE AND EDGE CHAMFERS I.A.W. SRM 57-26-13-300-008 REV.159 DATED 15 SEP, 26. THIS IS A REPAIR CATEGORY C. REPAIR LIFE LIMIT AT 48000
- [SDR DALA2026102105777](https://openairdocs.org/sdr/DALA2026102105777.md): Coupling · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN AT Y-1292 BETWEEN FR67 AND FR68 FLOOR SUPPORT, COUPLING AREA, AT INBD UPPER SECTION COUPLING ANGLE WITH CORROSION. FOUND DURING PROCESS OF ORNRC 200-327. REPLACED COUPLING P/N: D5347210220000 LOC BTW FR67 AND FR68 Y- 1292 LONGITUDINAL FLO
- [SDR DALA2026102105776](https://openairdocs.org/sdr/DALA2026102105776.md): Floor Support · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN BTWN FR 67 - 68, -Y 765, FLOOR SUPPORT CORRODED. REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, REV 159, DWG D53474250, SHEET 9, ISSUE Q, DWG D38370319, SHEET 3, ISSUE C, DWG D53472800, SHEET 10, ISSUE A, & DWG 53472816, SHEET 2, ISS
- [SDR DALA2026102105775](https://openairdocs.org/sdr/DALA2026102105775.md): Floor Support · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN BTWN FRS 66 - 69, -Y 1292, FLOOR SUPPORTS CORRODED. REPLACED THE FLOOR SUPPORTS IAW SRM 51-72-11-911-001, PARA 2.A(1), REV 159, DWG 10N01036, SHEET 4, REV B, DWG D53472816, SHEETS 1 & 2, REV A, DWG D53472800, SHEET 9, REV A, DWG D5347418
- [SDR DALA2026102105774](https://openairdocs.org/sdr/DALA2026102105774.md): Shear Plate · corroded · Oct 19, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AFT PASSENGER CABIN, BTWN FRS 69-70, RT FLOOR SHEAR PLATE CORRODED. REPLACED THE SHEAR PLATE IAW SRM 51-72-11-911-001, REV 159 AND DWG D534 74180, SHEET 6, ISSUE U. (LP: 1874370, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026101005579](https://openairdocs.org/sdr/DALA2026101005579.md): Floor Support · corroded · Oct 9, 2026 · N362NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 68, -Y 464.8, LONGITUDINAL FLOOR SUPPORT WITH CORROSION. REPLACED FLOOR SUPPORT AT AFT PASSENGER FLOOR SUPPORT AT AFT PASSENGER CABIN BTW FR 68 & FR 70, -Y464.8 IAW SRM 51-72-11-911-001, PARAG 2.A (1), SRM 51-42-
- [SDR DALA2026081404665](https://openairdocs.org/sdr/DALA2026081404665.md): Frame · cracked · Aug 12, 2026 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > FOUND CRACK IN FR16 LT, OUTBBOARD FLANGE, UPPER AREA ABOVE DOOR STOP 7, AT HOLE NR 6, COMPLIED WITH ER/A 567055-14. (1753281) (AIRCRAFT GROUNDED).
- [SDR DALA2026060803417](https://openairdocs.org/sdr/DALA2026060803417.md): Blade · bird ingestion · Jun 8, 2026 · N362NW · Airbus A320212 · Turbine Engine Compressor Section
  > ON DEPT OUT OF HOU, BIRDSTRIKE ON RT ENG, HIGH VIB INDICATION ON ECAM MAX 8.8 N1, ENG CONT TO RUN WITH THRUST PULLED BACK. C/W BIRDSTRIKE INSP IAW 72-00. FOUND MULTIPLE BLADES DAMAGED BEYOND REPAIR, ACOUSTIC PANES DAMAGE & RUB STRIP OUT OF LIMITS PER 72-21. R
- [SDR DALA2026052803241](https://openairdocs.org/sdr/DALA2026052803241.md): Union · leaking · May 27, 2026 · N362NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3262 - MISC - DECLARED EMERGENCY DUE TO PARTIAL LOSS OF THE GREEN SYSTEM HYDRAULIC FLUID. AIRCRAFT TAXIED TO THE GATE UNDER ITS OWN POWER. CORRECTIVE ACTION: FOUND LEAK AT GREEN SYSTEM HP MANIFOLD UNION. REMOVED PRESSURE SWITCH AND REPLACED O'RING AND RE-
- [SDR DALA2026021901182](https://openairdocs.org/sdr/DALA2026021901182.md): Power Supply · no test · Feb 19, 2026 · N362NW · Airbus A320212 · Emergency Lighting
  > EMERGENCY LIGHTS EPSU AFT GALLEY AREA DID NOT TEST (REFER TO AMDS CARD 5210-7089-RF, LF, LA, RA (RII)). REPLACED BATTERY OF THE EPSU 13WL AS PER A320 FAM AMM33-51-38-000-002-A, AS PER A320 FAM AMM 33-51-38-400-002-A. REPLACED WIRING 3351-5078 ON AFT DOOR LH
- [SDR DALA2026021901219](https://openairdocs.org/sdr/DALA2026021901219.md): Structure · damaged · Feb 16, 2026 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > UNREPAIRED EXISTING HOLES DIAMETER EQUAL TO OR GREATER THAN MINIMUM STARTING HOLE DIAMETER WAS FOUND. ON HOLES H1: 0.2634 IN, H2: 0.3321IN, H7: 0.2017 IN, H8: 0.2920 IN, HA:0.2027 IN, HB: 0.2620 IN, HC: 0.2030 IN, HD: 0.2631 IN, H9: 0.2032 IN, H10: 0.2631 IN
- [SDR DALA2026021901223](https://openairdocs.org/sdr/DALA2026021901223.md): Door Frame · damaged · Feb 15, 2026 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > DURING C-CHK AND WHILE INSPECTING PER EM 5311-01246-01A AT FR16 LHS DOUBLE JOGGLE AREA EXISTING REPAIRSFOUND AT HOLES NR 3, 4, 5, & 6. ELONGATED HOLE NR 5 IN UCD LAYER. PER SECTION DTE OF 567055-14 REV F, THE REPAIR OF SECTION X IS LIMITED TO 6 MONTHS SERVICE
- [SDR DALA2025111108224](https://openairdocs.org/sdr/DALA2025111108224.md): Oxygen Mask · unwanted deploy · Nov 10, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > OXYGEN MASKS AT 14DEF DEPLOYED, ONE MASK. LANYARD WAS PULLED AND OXYGEN WAS FLOWING. OXYGEN GEN DID NOT ACTIVATE, VERIFIED BY TEMP & ARMING PIN STILL INSTALLED. RESTOWED MASKS AT 14DEF IAW AMM 35-21. OK FOR SVC. (LP: 7997714)
- [SDR DALA2025102907908](https://openairdocs.org/sdr/DALA2025102907908.md): None · none · Oct 28, 2025 · N362NW · Airbus A320212 · Standard Practices/Structures
  > ER/A 567055-14 REV E ISSUED TO ACCOMPLISH REPEAT INSPECTIONS AT HOLES #3-#6 ON FR16 LHS DOUBLE JOGGLE AREA. FOLLOW ON INSPECTIONS ARE REQUIRED. ACCOMPLISH ER/A 567055-14 REV E SECTION IX REPEAT INSPECTIONS AT HOLES #3-#6 ON FR16 LHS EVERY 6,800FC FOLLOWING THE
- [SDR DALA2025072305522](https://openairdocs.org/sdr/DALA2025072305522.md): Module · faulted · Jul 21, 2025 · N362NW · Airbus A320212 · Emergency Lighting
  > SHIP 3262, ROW 1 AFT AISLE EMERGENCY LIGHT INOP. T/S PER A320 AWM 33-51-06. SWAPPED ROW 1 FWD AND AFT LED MODULES AND VERIFIED FAULT IS IN AFT LED MODULE, WILL REQUIRE NEW AFT LED, FWD TO MEL 33-50-03A, MEL/PLAC INSTALLED, NO (M) PROC, MCC NOTIFIED. FWD AND
- [SDR DALA2025072305523](https://openairdocs.org/sdr/DALA2025072305523.md): Wire · broken · Jul 17, 2025 · N362NW · Airbus A320212 · Light System Wiring
  > SHIP 3262, BROKEN EXPOSED WIRING AT ROW 24 DEF. REPAIRED EMERGENCY PATH LIGHTING WIRING AT ROW 24DEF IAW A320 AMM 20-90. (LP: 7455352)
- [SDR DALA2025071005207](https://openairdocs.org/sdr/DALA2025071005207.md): Oxygen Bottle · inoperative · Jul 6, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 DISC: AFT RT LAV OXY INOP (LATCH). C/A: R/R EMERGENCY O2 CONTAINER AT RT AFT LAV PER A320 AMM 35-21-41. OPS NML. PLAC RMVD. M PROC RVSD. (LP: 7455313)
- [SDR DALA2025071005190](https://openairdocs.org/sdr/DALA2025071005190.md): Latch · damaged · Jul 6, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 DISC: MID, AFT GALLEY OXY PSU LATCH DAMAGED. C/A: SECURED & REPACKED O2 MASKS @ AFT GALLEY MIDDLE O2 PSU PANEL. MEL AND PLACARD REMOVED. M PROC REVERSED. OK FOR SERVICE. IN REF TO A320 AMM 35-20. (LP: 7455314)
- [SDR DALA2025051603791](https://openairdocs.org/sdr/DALA2025051603791.md): Unknown · odor · May 14, 2025 · N362NW · Airbus A320212 · Air Distribution System
  > SHIP 3262 - MISC/DE - DUE TO FUMES IN AFT GALLEY AREA. CORRECTIVE ACTION: SUSPECTED TYPE 9 (ELECTRICAL) SMELL. NO TROUBLE FOUND. OK FOR SERVICE. (LP: 6973965)
- [SDR DALA2025050903590](https://openairdocs.org/sdr/DALA2025050903590.md): Oxygen Mask · faulted · May 6, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 DISC: ROW 27 DEF O2 MASK WILL NOT STOW. C/A: STOWED PER 320 AMM 35-21. OPS GOOD. (LP: 6973931)
- [SDR DALA2025050903589](https://openairdocs.org/sdr/DALA2025050903589.md): Oxygen Mask · faulted · May 6, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 DISC: ROW 26 DEF O2 MASKS WILL NOT STOW. C/A: STOWED PER 320 AMM 35-21. OPS GOOD. (LP: 6973930)
- [SDR DALA2025050703520](https://openairdocs.org/sdr/DALA2025050703520.md): Oxygen Mask · unwanted deploy · May 4, 2025 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 OXYGEN MASK DEPLOYED IN AFT LAV RIGHT. RESTOWED AS PER A320 AMM 5-21, OK FOR SVC. (LP: 0948853)
- [SDR DALA2025050703519](https://openairdocs.org/sdr/DALA2025050703519.md): Frame · damaged · May 4, 2025 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 ERA 568055 REV D SECTION VIII ISSUED FOR FRAME 16 LHS BUSHING REPAIR. FOLLOW ON ACTION REQUIRED. REPAIR IS LIMITED TO 6 MONTHS FROM SECTION VIII ACCOMPLISHMENT. ADDIONAL ENG APPROVAL REQUIRED FOR SERVICE BEYOND THIS LIMITED ERA REVISION REQUIRED AS
- [SDR DALA2025050703518](https://openairdocs.org/sdr/DALA2025050703518.md): Frame · damaged · May 4, 2025 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 DAMAGE TOLERANCE EVALUATION (DTE) ERA 567055-14AD REV D SECTION VIII ISSUED FOR LHS FR 16 HOLES 5 AND 6 BUSHING REPAIR. FOLLOW ON ACTION REQUIRED. ASSOCIATED ER/A CHANGED FROM 00-567055 TO 14-567055 FOR AC 3262. (LP: 0948415)
- [SDR DALA2025011000204](https://openairdocs.org/sdr/DALA2025011000204.md): Wire · damaged · Jan 7, 2025 · N362NW · Airbus A320212 · Light System Wiring
  > SHIP 3262 DISC: FOUND EMERGENCY SEAT LIGHTS AT 22D AND 23D OUT. C/A: FOUND DAMAGED WIREING, FIXED DAMAGED WIRING REF A320 AMM CHAPTER 20. OPS CK GOOD. AC OK FOR SVC. (LP: 6574737)
- [SDR DALA2024100109588](https://openairdocs.org/sdr/DALA2024100109588.md): Light · inoperative · Sep 30, 2024 · N362NW · Airbus A320212 · Emergency Lighting
  > SHIP 3262 DISC: SEAT 29 EEPMS INOP/MISSING. R & R SEAT 29 EMERGENCY ESCAPE LIGHT ASSY PER A320 AMM 33-51. OPS CHECK GOOD. NO (M) PROCEDURES. PLACARD REMOVED, OK TO CLOSE. * SEAT 29 EEPMS INOP/MISSING. C/A: FWD TO MEL 33-50-03A. NO M PROCEDURES. PLACARD INSTAL
- [SDR DALA2024083008572](https://openairdocs.org/sdr/DALA2024083008572.md): Life Raft · inoperative · Aug 25, 2024 · N362NW · Airbus A320212 · Life Raft
  > SHIP 3262 DISC: 32ABC LIFE RAFT INOP REF LOG 0519894
- [SDR DALA2024081107986](https://openairdocs.org/sdr/DALA2024081107986.md): Oxygen Mask · unwanted deploy · Aug 7, 2024 · N362NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3262 DISC: OXYGEN MASKS FELL OUT DURING TAKEOFF. PIN WAS NOT PULLED OUT, ABLE TO TEMPROARILY STOW MASKS AND TAPE DOOR SEMI SHUT. C/A: SECURED 19ABC CEILING PANEL PER A320 AMM 25-23. OPS CHECK NORMAL. OK FOR SVC AT 19ABC O2 MASK PANEL. (LP: 0489421)
- [SDR DALA2024050905052](https://openairdocs.org/sdr/DALA2024050905052.md): Pitot Tube · fod · May 8, 2024 · N362NW · Airbus A320212 · Pitot/Static System
  > SHIP 3262 - ATO - AT 120 KNOTS DUE TO LOSS OF CAPTAIN'S AIRSPEED TAPE. CORRECTIVE ACTION: FOUND PITOT PROBE #1 (9DA1) BLOCKED WITH FOREIGN DEBRIS. CLEARED BLOCKAGE AND CLEANED PITOT PROBE #1 (9DA1) AND R/R ADM 1 (19FP1). OPS CHECK GOOD. (LP: 5615908)
- [SDR DALA2024032603760](https://openairdocs.org/sdr/DALA2024032603760.md): Door Frame · cracked · Mar 22, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > AD RELATED: AA 5311-01216, LH FRAME 68 DOORSTOP FITTING #1, HOLE #1 HAS CRACK INDICATION. HOLE DIAMETER.260. ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: ACCOMPLISHED ER/A 616511-14 AD PRI REV O USING A320 SRM 53-41-12 - AS BASE REPAIR JOB COMPLETE. (LP: 02
- [SDR DALA2024032503713](https://openairdocs.org/sdr/DALA2024032503713.md): Door Frame · cracked · Mar 22, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: AD RELATED: L/H FR.68, STGR. 22, FRAME WEB HORIZONTAL FLANGE LOWER SURFACE RADIUS CRACKED APROX" 1 INCH IN LENTHG.REQUESTING REPAIR DISPOSITION.ADITIONAL ENGENIRING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACOMPLISHED PRIOR TO FURTHER FLIG
- [SDR DALA2024032503712](https://openairdocs.org/sdr/DALA2024032503712.md): None · none · Mar 22, 2024 · N362NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3262 DISC: COMPLY WITH ER/A 567055-14 REV C PRI REF BY AIRBORNE/PEMCO NR.15033.0227. C/A: RECEIVED FINAL & ACCOMPLISHED ERA 567055- 14AD REC C JOB COMPLETED. (LP: 0257137)
- [SDR DALA2024032503711](https://openairdocs.org/sdr/DALA2024032503711.md): Door Frame · cracked · Mar 22, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: AD RELATED: R/H FR.68, STGR. 22, FRAME WEB HORIZONTAL FLANGE LOWER SURFACE RADIUS CRACKED APROX" 1.5 INCH IN LENTHG.REQUESTING REPAIR DISPOSITION.ADITIONAL ENGENIRING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACOMPLISHED PRIOR TO FURTHER FL
- [SDR DALA2024032503710](https://openairdocs.org/sdr/DALA2024032503710.md): Door Frame · cracked · Mar 22, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: AD RELATED: AA 5311-01216, RH FRAME 68 DOORSTOP FITTING #1, HOLE #1 HAS CRACK INDICATION. HOLE DIAMETER.260. ACTIONS REQUIRED PRIOR TO FURTHER FLIGHT. C/A: ACCOMPLISHED ER/A 616531-14AD REV 0 PRI USING A320 SRM 53-41-12 AS BASE REPAIR JOB ACCO
- [SDR DALA2024032503709](https://openairdocs.org/sdr/DALA2024032503709.md): None · none · Mar 21, 2024 · N362NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3262 DISC: ER/A 567055-14AD HAS BEEN REVISED TO 'C'. FOLLOW ON ACTION IS RE QUIRED. C/A: PERFORM SECTION VII EVERY 2000FC AFTER 20MAR2024. ASSOCIATED ER/A 14-567055 ADDED FOR AC 3262. (LP: 0255465)
- [SDR DALA2024032303697](https://openairdocs.org/sdr/DALA2024032303697.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: FUSELAGE/LH FR68 AT STGR22L/ RADIAL FLANGE FILLET LOWER RADIUS - CRACKD I. FOLLOW ON ACTION IS REQUIRED. C/A: C/W ER/A 616511-14 (LP: 0256063)
- [SDR DALA2024032303696](https://openairdocs.org/sdr/DALA2024032303696.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: DAMAGE TOLERANCE EVALUATION ( DTE) FUSELAGE/LH FR68 AT STGR22L/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: C/W ER/A 14-616511. (KP: 0256059)
- [SDR DALA2024032303695](https://openairdocs.org/sdr/DALA2024032303695.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: DAMAGE TOLERANCE EVALUATION ( DTE) FUSELAGE/LH FR68 AT STGR22L/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF ER/A 616511-14AD.
- [SDR DALA2024032303694](https://openairdocs.org/sdr/DALA2024032303694.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: DAMAGE TOLERANCE EVALUATION ( DTE) FUSELAGE/LH FR68 AT STGR22L/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF ER/A 616511-14AD. (LP: 0256047)
- [SDR DALA2024032303693](https://openairdocs.org/sdr/DALA2024032303693.md): Stop Fitting · unknown · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: ER/A 616531-14AD ISSUED FOR REPAIR INSTALLED AT FR68 RH AND DOOR STOP 1. FOLLOW ON ACTION IS REQUIRED. C/A: REF ER/A 616531-14 AD.
- [SDR DALA2024032303692](https://openairdocs.org/sdr/DALA2024032303692.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: DAMAGE TOLERANCE EVALUATION (DTE) FUSELAGE/RH FR68 AT STGR22R/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: ER/A 616531-14. (LP: 0256032)
- [SDR DALA2024032303691](https://openairdocs.org/sdr/DALA2024032303691.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: DAMAGE TOLERANCE EVALUATION (DTE) FUSELAGE/RH FR68 AT STGR22R/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: REF ER/A 616531-14 AD. (LP: 0256024)
- [SDR DALA2024032303690](https://openairdocs.org/sdr/DALA2024032303690.md): Fillet · cracked · Mar 21, 2024 · N362NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3262 DISC: ER/A 616531-14AD ISSUED FOR REPAIR FUSELAGE/RH FR68 AT STGR22R/ RADIAL FLANGE FILLET LOWER RADIUS - CRACK. C/A: PERFORM SECTION II WITHIN 37900FC AFTER SECTION I. ER/A TO BE RE VISED PRIOR TO THIS TIME TO PROVIDE METHOD. ASSOCIATED AA 5311-012
- [SDR DALA2023082106768](https://openairdocs.org/sdr/DALA2023082106768.md): Unknown · unknown · Aug 20, 2023 · N362NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3262 - MISC/DE - DUE TO HYD Y RSVR LO LVL ECAM MESSAGE. CORRECTIVE ACTION: FOUND A CUT O-RING IN THE YELLOW SYSTEM MAIN HP MANIFOLD (3011GM) CHECK VALVE (3059GM). REPLACED O-RING. LEAK CHECKED GOOD. (2928013)
- [SDR DALA2023072505989](https://openairdocs.org/sdr/DALA2023072505989.md): Unknown · unknown · Jul 24, 2023 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 HOLE #6 AT DOOR FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882936)
- [SDR DALA2023072505988](https://openairdocs.org/sdr/DALA2023072505988.md): Unknown · unknown · Jul 24, 2023 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 HOLE #5 CRACKED ON FRAME. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV. A. (2882931)
- [SDR DALA2023072505987](https://openairdocs.org/sdr/DALA2023072505987.md): Unknown · unknown · Jul 24, 2023 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 HOLE #4 AT FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882930)
- [SDR DALA2023072505986](https://openairdocs.org/sdr/DALA2023072505986.md): Unknown · unknown · Jul 24, 2023 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 HOLE #3 ON FRAME CRACKED. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD REV A. (2882928)
- [SDR DALA2023072505990](https://openairdocs.org/sdr/DALA2023072505990.md): Unknown · unknown · Jul 23, 2023 · N362NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3262 FR 16LH HOLES #5 AND #6 DISCREPANCIES FOUND. CORRECTIVE ACTION: REPAIRED PER ERA 567055-14AD. (2881575)

Next page: https://openairdocs.org/aircraft/N362NW/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 = 'N362NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N362NW/reports

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