# Service difficulty reports: N371NW

A list on [N371NW](https://openairdocs.org/aircraft/N371NW.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 · 185 reports

- [SDR DALA2026070603919](https://openairdocs.org/sdr/DALA2026070603919.md): Light · broken · Jun 30, 2026 · N371NW · Airbus A320212 · Emergency Lighting
  > ROW 15DEF EPL HOUSING BROKEN. R & R 15DEF EPL HOUSING REF AMM 33-51. (LP: 8879288, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026052703212](https://openairdocs.org/sdr/DALA2026052703212.md): Percussion Mech · faulted · May 22, 2026 · N371NW · Airbus A320212 · Escape Slide
  > L1 DOOR SLIDE DEPLOYED (PARTIAL DEPLOYMENT). R & R L1 DOOR SLIDE ASSY IAW AMM 52-11. R & R DIAPHRAGM IN PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER OF THE PASSENGER/CREW DOOR IAW AMM 52-10. ALL RII STEPS ACCOMPLSIHED. (LP: 8881442
- [SDR DALA2026020200750](https://openairdocs.org/sdr/DALA2026020200750.md): Oxygen Mask · unwanted deploy · Jan 31, 2026 · N371NW · Airbus A320212 · Passenger Oxygen System
  > OXYGEN PANEL, MASK DEPLOYED DURING TAKEOFF, AT SEAT 23ABC. TRIED OUR BEST TO STOW THEM, BUT THEY WILL NEED TO BE PUT BACK TOGETHER CORRECTLY. STOWED PSU PANEL AT ROW 23 ABC REF AMM 35-21. (LP: 1429256)
- [SDR DALA2026013000732](https://openairdocs.org/sdr/DALA2026013000732.md): Battery Pack · inoperative · Jan 26, 2026 · N371NW · Airbus A320212 · Emergency Lighting
  > FOUR WALL MOUNTED EMERGENCY LIGHTS INOPERATIVE AT EXIT DOORS. R & R BOTH EPSU BATTERIES IAW AMM 33-51. NO HELP. R & R EPSU AT 12WL NO HELP ALL 4 LIGHT ASSY'S INOP. R & R AT 16 FED OPS CHECK GOOD IAW AMM 3351. R&R LIGHTS AT 16A, 15A & 15F. LIGHTS OPS CHECKED
- [SDR DALA2026012800697](https://openairdocs.org/sdr/DALA2026012800697.md): Panel · open · Jan 23, 2026 · N371NW · Airbus A320212 · Passenger Oxygen System
  > OXYGEN PANEL OPENED IN FLIGHT. DEFER OXYGEN MODULE AT SEAT 12ABC TO MEL AND PLACARD IAW MEL 35-21-01A. M PROCEDURE C/W. FOUND OXYGEN PANEL LATCH NOT ENGAGED. CLOSED & LATCH 12A OXYGEN PANEL PROPERLY. OK FOR SVC. IAW AMM 35-21. M PROC REV. MEL PLAC REM. (LP: 8
- [SDR DALA2026012300520](https://openairdocs.org/sdr/DALA2026012300520.md): Power Supply · faulted · Jan 19, 2026 · N371NW · Airbus A320212 · Emergency Lighting
  > DURING OPS TEST OF THE EMERGENCY LIGHTS FAULT EPSU UNIT 11WL (REFER TO AMDS CARD 5210-7089-LF (RII)). REMOVED EMERGENCY POWER SUPPLY UNIT EPSU (11WL) UNSERVICEABLE CONDITION IAW AMM 33-51-38-000-001-A AND AS PER A320 FAM AMM33-51-38-400-001- A. TESTED GOOD.
- [SDR DALA2025120408848](https://openairdocs.org/sdr/DALA2025120408848.md): Light · detached · Dec 3, 2025 · N371NW · Airbus A320212 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED AND INOPERATIVE. HANGING DOWN, WIRE STILL ATTACHED. RESECURED EMERGENCY SEAT MOUNTED LIGHT AS REQUIRED. OK FOR SVC SEAT ROW 30D. (LP: 1333983)
- [SDR DALA2025112008497](https://openairdocs.org/sdr/DALA2025112008497.md): Light · damaged · Nov 19, 2025 · N371NW · Airbus A320212 · Emergency Lighting
  > EMERGENCY SEAT MOUNTED LIGHTING DAMAGED / INOP. ATTACHED WOTH 2-SIDED TAPE AND NO LONGER MOUNTED TO SEAT. NEEDS TO BE REMOUNTED. SECURED AS REQUIRED. (LP: 1311690)
- [SDR DALA2025042403200](https://openairdocs.org/sdr/DALA2025042403200.md): Lever · inoperative · Apr 19, 2025 · N371NW · Airbus A320212 · Emergency Equipment
  > SHIP 3271 WHILE PERFORMING 2A AIRFRAME CHECK. PERFORMED OPERATIONAL CHECK OF ALL CREW/PASSENGER DOOR GIRT BAR FITTING STOP LEVERS. FOUND R1 FWD GIRT BAR FITTING STOP LEVER NON OPERATIONAL/ FAILS TO RETURN TO REGULAR POSITION. R/R R1 DOOR FWD GIRT BAR FITTING S
- [SDR DALA2025020100766](https://openairdocs.org/sdr/DALA2025020100766.md): Duct · contaminated · Jan 29, 2025 · N371NW · Airbus A320212 · Engine Bleed Air System
  > SHIP 3271 DISC: FLIGHT ATTS AND OFF DUTY PILOT DETECTED AN ELECTRICAL ODOR IN THE REAR OF THE A/C ON TO OUT OF ATL. THE ODOR QUICKLY DISSIPATED. C/A: T/S PER WC 0550-2002 AND 0550-2003. DECISION TABLE LEADS TO NO.2 ENG AS POSSIBLE SOURCE. INSPECTED NO.2 SPINNE
- [SDR DALA2024081107979](https://openairdocs.org/sdr/DALA2024081107979.md): Unknown · unknown · Aug 6, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS. ER/A 615255-14AD REV A REQUIRES STAGE 3 DTE. C/A: PER ER/A 615255-14AD REV A, STAGE 3 DTE IS REQUIRED ON OR BEFORE 48,500 FC FROM SECTION I REPAIR EMBODIMENT OR 97,000 FH FROM SEC TION I REPAIR
- [SDR DALA2024081107978](https://openairdocs.org/sdr/DALA2024081107978.md): Unknown · unknown · Aug 6, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS. ER/A 615255-14AD REV A REQUIRES STAGE 3 DTE. C/A: PER ER/A 615255-14AD REV A, STAGE 3 DTE IS REQUIRED ON OR BEFORE 29,700 FC FROM SECTION I REPAIR EMBODIMENT OR 59,400 FH FROM SEC TION I REPAIR
- [SDR DALA2024081107977](https://openairdocs.org/sdr/DALA2024081107977.md): Unknown · unknown · Aug 6, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS. ER/A 615255-14AD REV A REQUIRES STAGE 3 DTE. C/A: PER ER/A 615255-14AD REV A, STAGE 3 DTE IS REQUIRED ON OR BEOFRE 67,700 FC FROM SECTION I REPAIR EMBODIMENT OR 135,400 FH FROM SE CTION I REPAIR
- [SDR DALA2024081107976](https://openairdocs.org/sdr/DALA2024081107976.md): Unknown · unknown · Aug 6, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: FUSELAGE / BULKHEADS / FR35 AT STGR30LH / CRACKS. ER/A 615255-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRWORTHINESS. C/A: ER ER/A 615255-14AD REV A, SECTION II FOLLOW-ON INSPECTIONS ARE REQUIRED ON OR BEFORE 12,100 FC
- [SDR DALA2024071207056](https://openairdocs.org/sdr/DALA2024071207056.md): Oxygen Panel · loose · Jul 7, 2024 · N371NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3271 DISC: OXYGEN PANEL LOOSE / LOCATIONS:33D. C/A: RESECURED OXYGEN PANEL AT 33D PER A320 AMM 35-21. OPS CHECK GOOD. OK FOR SERVICE. (LP: 0432959)
- [SDR DALA2024032703837](https://openairdocs.org/sdr/DALA2024032703837.md): Oxygen Mask · unwanted deploy · Mar 24, 2024 · N371NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3271 DISC: WHILE CLOSING OVERHEAD BINS OXYGEN MASKS DEPLOYED OVER 12ABC. RE-SECURED MASK PER A320 AMM 35-21. OP CHECK GOOD. MEL & PLACARD. REMOVED. M PROCEDURES REVERSED. OK FOR SVC.
- [SDR DALA2024032003528](https://openairdocs.org/sdr/DALA2024032003528.md): Seal · leaking · Mar 15, 2024 · N371NW · Airbus A320212 · Emergency Exits
  > SHIP 3271 DISC: LT FWD EMERGENCY EXIT HATCH HAS PRESSURIZATION LEAK DURING FCF. C/A: REMOVED EMERGENCY DOOR HATCH LT FWD RE-ACCOMODATED PRESSURIZATION SEAL AND RE INSTALLED EMERGENCY DOOR HATCH ASPER AMM 52-21-11-400-001-A (RESERVOIR LOOKPIN REMOVED) THEN PERF
- [SDR DALA2024031403320](https://openairdocs.org/sdr/DALA2024031403320.md): Bulkhead · damaged · Mar 7, 2024 · N371NW · Airbus A320212 · Fuselage Main, Bulkhead
  > SHIP 3271 DISC: DTE ERA 615255-14AD, REPAIR PER ERA 615255-14AD REQUIRES DTE FOLLOW UP PRIOR TO 08-22-2024. PERFORMED REPAIR ON BULKHEADS FR 35 AT STRG 30 LH FUSELAGE AS PER ER/A 615255-14AD REV. ORIGINAL AND PRI 615255-14AD REV 0, PRI615255-14AD REV 1, PRI 6
- [SDR DALA2024031403319](https://openairdocs.org/sdr/DALA2024031403319.md): Window Post · damaged · Mar 7, 2024 · N371NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3271 DISC: DTE ERA 615061-14AD. REPAIR PER ERA 615061-14AD AT AREA #1 ( CONTINUITY FITTINGS & MIRROR FITTING) REQUIRES DTE FOLLOW UP PRIOR TO 60,126 TOTAL FLIGHT CYCLES. PERFORMED REPAIR ON WINDSHIELD FRAMING CENTER POST AND CONTINUITY FITTING LH/RH IN
- [SDR DALA2024030402916](https://openairdocs.org/sdr/DALA2024030402916.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR48 TO FR5 0 BTW STR2L TO STR5L ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERAT
- [SDR DALA2024030102884](https://openairdocs.org/sdr/DALA2024030102884.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 72 AT STR 26 R AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INSTAL
- [SDR DALA2024030102883](https://openairdocs.org/sdr/DALA2024030102883.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC FR34 T O FR35 BTW STR33L TO STR34L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING
- [SDR DALA2024030102882](https://openairdocs.org/sdr/DALA2024030102882.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR LOWER SILL LOCATED FR68 AND STR23R AT AFT GALLEY AREA. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INSTALLED
- [SDR DALA2024030102881](https://openairdocs.org/sdr/DALA2024030102881.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR25 TO FR26 BTW STR42R TO STR43L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING
- [SDR DALA2024030102880](https://openairdocs.org/sdr/DALA2024030102880.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR52 TO FR5 3 BTW STR1 L TO STR1R ON UPPER FUSELAGE. C/A: COMPLIED WITH PRI 575822-14 REV 0, VALIDATED ER/A 575822-14 REV ORIGINAL MATCHES PRI 575822-14 REV 0. EXISTING ALTERATION INSTA
- [SDR DALA2024030102879](https://openairdocs.org/sdr/DALA2024030102879.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR35 TO FR3 6 BTW STR2L TO STR2R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERAT
- [SDR DALA2024030102878](https://openairdocs.org/sdr/DALA2024030102878.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOC. FR56 TO FR57 BTW STR40L TO STR44L AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING
- [SDR DALA2024030102877](https://openairdocs.org/sdr/DALA2024030102877.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR58 TO FR5 9 BTW STR18L TO STR21L ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTER
- [SDR DALA2024030102876](https://openairdocs.org/sdr/DALA2024030102876.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR48 TO FR5 0 BTW STR2R TO STR5R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERAT
- [SDR DALA2024030102875](https://openairdocs.org/sdr/DALA2024030102875.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR58 TO FR5 9 BTW STR18R TO STR21R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTER
- [SDR DALA2024030102874](https://openairdocs.org/sdr/DALA2024030102874.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR SKIN LOCATED FR29 TO FR3 0 BTW STR1L TO STR1R ON UPPER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING ALTERAT
- [SDR DALA2024030102873](https://openairdocs.org/sdr/DALA2024030102873.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: 1 CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 69 TO FR70 BTW STR31R TO STR32R AT LOWER FUSELAGE. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EX
- [SDR DALA2024030102872](https://openairdocs.org/sdr/DALA2024030102872.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR EXTERNAL SKIN LOCATED FR 36 TO FR37 BTW STIFFENER1 TO STIFFENER 2 IN CENTER FUEL TANK. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORI
- [SDR DALA2024030102871](https://openairdocs.org/sdr/DALA2024030102871.md): None · none · Feb 29, 2024 · N371NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3271 DISC: CONFIRM DT EVALUATION FOR POSSIBLE FCS REPAIR LOWER SILL LOCATED AT LE VEL STR23R FR66 AT AFT GALLEY AREA. C/A: COMPLIED WITH ERA 575822-14 REV ORIGINAL, VALIDATED ER/A 575822-14 REV A AND MATCHES ERA 575822-14 REV ORIGINAL EXISTING REPAIR INST
- [SDR DALA2024022102451](https://openairdocs.org/sdr/DALA2024022102451.md): Receptacle · corroded · Feb 18, 2024 · N371NW · Airbus A320212 · Nacelle/Pylon, Main Frame
  > SHIP 3271 DISC: PITTING CORROSION TRACES ON SPIGOT RECEPTACLE INNER BORE AT LH PYLON. C/A: REMOVED AND REPLACED LOWER SPIGOT FITTING ON PYLON LH AS PER A320 SRM 51-42-11-801, SRM 54-51-12-300-001, SRM 54-51-44-11 AND AMM54-41- 400-001-A. INSTALL SPIGOT BALL JO
- [SDR DALA2024021602273](https://openairdocs.org/sdr/DALA2024021602273.md): Door · bent · Feb 16, 2024 · N371NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3271 DISC: AAI FINDING: DURING INSPECTION OF EXTERNAL FUSELAGE. AFT LOWER CORNER OF L1 DOOR IS DENTED/BENT INWARD. C/A: PERFORMED PERMANENT REPAIR LOC. EXTERNAL FUSELAGE. AFT LOWER CORNER OF L1 DOOR AS PER A320 SRM 52-10-00-300-003 PARAGRAPH 2.FIGURE 001
- [SDR DALA2024021502250](https://openairdocs.org/sdr/DALA2024021502250.md): Doubler · misinstalled · Feb 14, 2024 · N371NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LEFTHAND SIDE FR23L AT STR22L TWO (2) FASTENERS ARE LOCATED IN THE RADIUS OF THE CHEM-MIL AREA. THE REPAIR DOUBLER WAS INSTALLED AS PER ER/A 560683-14 REV B ON 27 JUL 201. C/A: PER
- [SDR DALA2024021502249](https://openairdocs.org/sdr/DALA2024021502249.md): Doubler · misinstalled · Feb 14, 2024 · N371NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON THE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69 - FR70 BETWEEN STR 31R AND STR 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD. REV A: T WO (2) FASTENERS ARE LOCATED IN THE REPAIR DOUBLER ARE IMPROP
- [SDR DALA2024020201490](https://openairdocs.org/sdr/DALA2024020201490.md): Trunnion · out of limits · Feb 2, 2024 · N371NW · Airbus A320212 · Trailing Edge Flaps
  > SHIP 3271 DISC: REWORK WAS FOUND OUT OF LIMITS ON UPPER STRUCTURE FLAP TRUNNION INBOARD FLAP ON LH WING MEASURE OF MAXIMUN DEPTH 0.298IN AND TRUNNION SHAFT DIAMETER 3.086IN CONTAC LIAISON ENGINEERING. ADDITIONAL ENGINEERING D OCUMENTATION IS REQUIRED PRIOR TO
- [SDR DALA2024020201489](https://openairdocs.org/sdr/DALA2024020201489.md): Paint · missing · Feb 1, 2024 · N371NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3271 DISC: AAI FINDING: DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69-FR 70 BETWEEN STR 31R AND STR 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD REV A: NU MEROUS FASTERS THROUGHOUT THE RE
- [SDR DALA2024020201488](https://openairdocs.org/sdr/DALA2024020201488.md): Sealant · missing · Feb 1, 2024 · N371NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3271 DISC: AI FINDING: DURING INSPECTION OF EXISTING REPAIR DOUBLER LOCATED ON T HE FUSELAGE EXTERIOR, LOCATED ON THE RIGHTHAND SIDE FR69- FR70 BETWEEN STR 31R AND 32R (LAV VENT EXHAUST) REF ER/A 589202-14AD REV A: ARE A BOVE STR 31R IS MISSING FAYING SEA
- [SDR DALA2024020201487](https://openairdocs.org/sdr/DALA2024020201487.md): Connector · cracked · Feb 1, 2024 · N371NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > SHIP 3271 DISC: CRACK INTERNAL STRUCTURE SECTION CONNECTION LOCATED FR66 AT LEVEL STR INGER 23L AT AFT GALLEY AREA A. C/A: REPLACED INTERNAL STRUCTURE SECTION CONNECTION AND FASTENERS LOCATED FR66 AT LEVEL STRINGER 23L AT AFT GALLEY AREA AS PER A320SRM 51-42-1
- [SDR DALA2024012901210](https://openairdocs.org/sdr/DALA2024012901210.md): Frame · cracked · Jan 27, 2024 · N371NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3271 DISC: CRACK INDICATION ON FRAME 16 LH SIDE ON INTERCOSTAL FITTING OPEN FASTENER HOLE 1 AT DOOR STOP FITTING 7 POSITION, CRACK DIRECTION IS 6 OCLOCK, CRACK DEPTH IS 0.085 INCH, AT FWD GALLEY AREA (1 EA) C/A: REPLACED INTERCOSTAL FITTING AND FASTENERS
- [SDR DALA2024011800746](https://openairdocs.org/sdr/DALA2024011800746.md): Fastener · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 1666434 PERM REPAIR C/W ON FASTENER AT FR 61 - 2.5 INCHES ABOVE STR 38 R PER A320 SRM 53-41-11. REF LOG # 0646895. C/A: PER SRI 53-41-11 PAGE 233 REQUIRES REINSPECTION AT 60000 FC / 120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-
- [SDR DALA2024011800745](https://openairdocs.org/sdr/DALA2024011800745.md): Fastener · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage, Wing Attach Fittings
  > SHIP 3271 DISC: REF LOG PAGE 1666423 PERM REPAIR C/W ON FASTENER ONE INCH FWD OF FR59 ON STR 38 PER A320 SRM 53-41-11 REF LOG #0646904. C/A: ER SRI 53-41-11 PAGE 233 REQUIRES REINSPECT AT 60000 FC /120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-005 LOG-PAGE
- [SDR DALA2024011800744](https://openairdocs.org/sdr/DALA2024011800744.md): Fastener · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 166422 PERM REPAIR C/W ON FASTENER AT 8.5 INCHES FWD OF FR 63 ON STR 39 PER A320 SRM 53-41-11 REF LOG # 0646910. C/A: PER SRI 53-41-11 PAGE 233 REQUIRES REINSPECTION AT 60000 FC / 120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-00
- [SDR DALA2024011800743](https://openairdocs.org/sdr/DALA2024011800743.md): Fastener · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 1666256 PERM REPAIR C/W ON FASTENER AT 8.5 INCHES FWD OF FR 63 ON STR 39 PER A320 SRM 53-41-11 REF LOG # 0646884. C/A: PER SRI 53-41-11 PAGE 233 REQUIRES REINSPECTION AT 60000 FC / 120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-0
- [SDR DALA2024011800742](https://openairdocs.org/sdr/DALA2024011800742.md): Fastener · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 1666435 TERM IN ERROR. PERM REPAIR C/W ON FASTENER 6.5 INCHES FWD OF FR 62 ON STR 39R PER A320 SRM 53-41-11 REF LOG #0646889. C/A: ER SRI 53-41-11 PAGE 233 REQUUIRES REINSPECTION AT 60000FC / 120000FH FROM FIRST FLIGHT PER SRI 53-4
- [SDR DALA2024011800741](https://openairdocs.org/sdr/DALA2024011800741.md): Unknown · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 1666114 TERM IN ERROR PERM. REPAIR C/W ON FASTENER AT FR 60 STR 38R PER A320 SRM 53-41 -11. REF LOG # 0646901. C/A: PER SRI 53-41-11 PAGE 233 REQUIRES REINSPECT AT 60000 FC / 120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-005. (L
- [SDR DALA2024011600660](https://openairdocs.org/sdr/DALA2024011600660.md): Unknown · unknown · Jan 15, 2024 · N371NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3271 DISC: REF LOG PAGE 1666261 PERM REPAIR C/W ON FASTENER ONE INCH FWD OF FR59 ON STR 38 PER A320 SRM 53-41-11 REF LOG #0646904. C/A: PER SRI 53-41-11 PAGE 233 REQUIRES REINSPECT AT 60000 FC /120000 FH FROM FIRST FLIGHT PER SRI 53-41-11-205-005. (LP: 01

Next page: https://openairdocs.org/aircraft/N371NW/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 = 'N371NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N371NW/reports

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