# Service difficulty reports: N351NW

A list on [N351NW](https://openairdocs.org/aircraft/N351NW.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 6 · 257 reports

- [SDR DALA2026101305621](https://openairdocs.org/sdr/DALA2026101305621.md): Thrust Reverser · faulted · Oct 11, 2026 · N351NW · Airbus A320212 · Engine Thrust Reverser
  > ATB - DUE TO ENG 2 REVERSE UNLOCKED ECAM WARNING AFTER TAKEOFF. NR 2 T/R PLACED ON MEL. RE-ACTIVATED NBR 2 ENGINE THRUST REVERSER, FAILED INBOARD TR LOWER LATCH SWITCH, REPLACED NBR 2 ENGINE INBOARD THRUST REVERSER UPPER DOOR LATCH. (LP 9485726 - AIRCRAFT WA
- [SDR DALA2026091305113](https://openairdocs.org/sdr/DALA2026091305113.md): Microphone · inoperative · Sep 12, 2026 · N351NW · Airbus A320212 · Crew Oxygen System
  > F/O OS MASK MICROPHONE NOT WORKING. C/A: SWAPPED THIRD OBSERVER SEAT OT MASK WITH F/O AND FWD THIRD OBSERVER SAET TO MEL 25-11-07. R/R THIRD OBESERVER O2 MASK PER A320 AMM 35-12. LEAK AND OPS TESTS OK. RFID INDUCTION C/W. F/O MASK RFID REPLACEMENT C/W TO REFLE
- [SDR DALA2026091405115](https://openairdocs.org/sdr/DALA2026091405115.md): Microphone · inoperative · Sep 11, 2026 · N351NW · Airbus A320212 · Crew Oxygen System
  > F/O OXYGEN MASK MICROPHONE DOESN'T WORK. RESEATED MIC CONNECTOR. CHK NORMAL. IAW AMM 35-13. (LP: 9494820, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026091305109](https://openairdocs.org/sdr/DALA2026091305109.md): Warning Message · illuminated · Sep 10, 2026 · N351NW · Airbus A320212 · Fuel Indicating System
  > CAUTION ON ECAM - TK LO TEMP LEFT OUTTER LO TEMP. FLIGHT CREW PLACARD VALIDATION IS ACCOMPLISHED REJECTED TAKEOFF DUE TO FUEL L OUTER TK LO TEMP INDICATION. LEFT OUTER TANK INDICATED -51C. AFTER CLEARING RUNWAY, FUEL TEMP INDICATED~ +42C. FLIGHT CREW PLACARD
- [SDR DALA2026091405114](https://openairdocs.org/sdr/DALA2026091405114.md): Oxygen Mask · inoperative · Sep 8, 2026 · N351NW · Airbus A320212 · Crew Oxygen System
  > F/O 02 MASK MIC INOP. R & R F/O 02 MASK IAW AMM 35-12 OPS NORMAL. (LP: 9494800, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026060203348](https://openairdocs.org/sdr/DALA2026060203348.md): Fitting · damaged · Jun 1, 2026 · N351NW · Airbus A320212 · Fuselage Main, Structure
  > AVIONICS COMPARTMENT RACK 80VU, LH AND RH LATERAL PYRAMIDS FITTINGS WITH ELONGATED HOLES.AIRBUS MUST BE CONTACTED BEFORE FURTHER FLIGHT, REPAIRED FWD FUSELAGE EQUIPMENT / RACK 80VU LH AND RH LOWER LATERAL SUPPORT FOR MATERIAL BURRED (OVALIZATION) IAW ER/A 634
- [SDR DALA2026060103311](https://openairdocs.org/sdr/DALA2026060103311.md): Door Sill · corroded · May 29, 2026 · N351NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, AFT PASSENGER CABIN, LH DOOR LOWER CUT OUT SILL BEAM AREA CENTER ANGLE WITH CORROSION. REPLACED (SHAPE) CENTER ANGLE P/N: D5348004820203 AT AFT PASSENGER CABIN L/H DOOR LOWER CUT OUT SILL BEAM IAW A320 SRM 51 -72-11-911-001 REV 157.00 DATED
- [SDR DALA2026053103300](https://openairdocs.org/sdr/DALA2026053103300.md): Hinge Arm · corroded · May 29, 2026 · N351NW · Airbus A320212 · Vertical Stabilizer
  > LEVEL 2 CORROSION, CORROSION SSI:553006 RUDDER HINGE ARM NR 7 STUD HOLES L/R SIDES WITH CORROSION. REPAIRED VERTICAL STABILIZER RUDDER HINGE ARM BR1 OVERSIZED HOLE AND HINGE BR7 REPLACEMENT IAW DELTA ER/A 634168-14 REVISION ORIGINAL DATED 27-MAY-26. NOTE: FOR
- [SDR DALA2026053103290](https://openairdocs.org/sdr/DALA2026053103290.md): Door Sill · corroded · May 29, 2026 · N351NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, AFT PASSENGER CABIN, AFT R/H DOOR CUTOUT AT Y-1235MM FR68 SILL BEAM WITH CORROSION. FOUND DURING PROCESS WITH ORNRC 200- 278. PERFORMED REPAIR AFT PASSENGER CABIN AFT RH DOOR CUT OUT SILL BEAM BETWEEN FR 67 +335MM AND FR 68 +35MM I/A/W A32
- [SDR DALA2026053103296](https://openairdocs.org/sdr/DALA2026053103296.md): Support Fitting · not reported · May 28, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > ER/A 634037-14AD ISSUED FOR REPAIR TO LT & RT LOWER LATERAL SUPPORT FITTINGS OF THE 80VU RACK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500FC OF SECTION I AND EVERY 1000FC THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3251 ASSOCIATED ER/A
- [SDR DALA2026052803235](https://openairdocs.org/sdr/DALA2026052803235.md): Stop Fitting · scratched · May 27, 2026 · N351NW · Airbus A320212 · Fuselage Main, Structure
  > AIRCRAFT 3251, UPPER FUSELAGE PAX CABIN BETWEEN FR15 AND FR16 R/H SIDE AT STOP FITTING #1, INTERCOSTAL WITH SCRATCHES AND TOOL MARK. CORRECTIVE ACTION: ACCOMPLISHED INTERCOSTAL REPLACEMENT AT FR16 RH DOOR STOP #1 IAW ER/A #589110-14AD REV A. (LP 1615986 - AIRC
- [SDR DALA2026052803234](https://openairdocs.org/sdr/DALA2026052803234.md): Seat Track · corroded · May 27, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > AIRCRAFT 3251, UPPER FUSELAGE, FWD ENTRY AREA SEAT TRACK BETWEEN FR 20 AND FR 21 Y-1292 WITH CORROSION LEVEL 2. CORRECTIVE ACTION: REPLACED SEAT TRACK P/N: D5311281400200 AT Y-1292 BTWN FR12 AND FR24 IAW A320 SRM 51-72-11-911-001 PARG 2 REV 157.00 DATED 15/APR
- [SDR DALA2026052803233](https://openairdocs.org/sdr/DALA2026052803233.md): Floor Support · corroded · May 27, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AIRCRAFT 3251, AFT PASSENGER CABIN BETWEEN FR 66-68, -Y 765 FLOOR BEAM WITH LEVEL 2 CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM P/N: 5347219320000 AT Y-765 BTW FR66 TO FR70 IAW A320 SRM TASK 51-72-11-911-001 PARAG 1A (1) REV 157.00 DATED 15/APR/26 AND AI
- [SDR DALA2026052803232](https://openairdocs.org/sdr/DALA2026052803232.md): Floor Support · corroded · May 27, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > AIRCRAFT 3251, AFT PASSENGER CABIN BETWEEN FR 66-68, -Y 1292, FLOOR BEAM WITH LEVEL 2 CORROSION. REPLACED FLOOR BEAM P/N: D5347217220390, P/N: D5347218920200, COUPLING P/N: D5347210220600, D5347210220400, D5347210220200, BTW FR66 TO FR69 AT -Y1292 IAW A320 S
- [SDR DALA2026052703210](https://openairdocs.org/sdr/DALA2026052703210.md): Web · damaged · May 26, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > A.A. WORK CARD 5311-01244-02B, REQUESTING REPAIR DISPOSITION. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED, AND REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. REFER TO EM 5311- 01244 AND SB A320-53-1491. INSTRUCTIONS TO LIASON IN EARTH FOLDER "DELTA
- [SDR DALA2026052703209](https://openairdocs.org/sdr/DALA2026052703209.md): Seat Track · corroded · May 26, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, A1R116 2-79 (200-336). AFT PASSENGER CABIN AT FR66 Y-765, SEAT TRACK WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 200- 277. C/A: REPLACED SEAT TRACK P/N: 14N00031-103 FROM FR64 TO FR66 -Y 765 WET AREA, DUE TO CORRODED OUT-LIMITS I/A/W
- [SDR DALA2026052703208](https://openairdocs.org/sdr/DALA2026052703208.md): Seat Track · corroded · May 26, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, AFT PASENGER CABIN AT FR66 Y-1292, SEAT TRACK WITH CORROSION. NOTE: FOUND DURING PROCESS OF ORNRC 200-278. C/A: REPLACED SEAT TRACK P/N: 14N00031-101, COUPLING P/N: D5347210420200, D5347210220200, D5347210220400 AND D5347210220600 FROM FR 64
- [SDR DALA2026052703207](https://openairdocs.org/sdr/DALA2026052703207.md): Seat Track · corroded · May 26, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3251 DISC: LEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 65, Y 1292, SEAT TRACK BEAM WITH CORROSION. C/A: REPLACED SEAT TRACK P/N = 14N00031-115, COUPLING P/N: D5347210420400, D5347210420200, FROM FR64 TO FR66 Y 1292 WET AREA DUE TO CORRODED OUT-LIMITS IAW
- [SDR DALA2026052703206](https://openairdocs.org/sdr/DALA2026052703206.md): Seat Track · corroded · May 26, 2026 · N351NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, AFT PASSENGER CABIN AT FR 65, Y 765, SEAT TRACK BEAM WITH CORROSION. REPLACED SEAT TRACK P/N= 14N00031-117 FROM FR 64 TO FR 66 Y 765 WET AREA DUE TO CORRODED OUT LIMITS I/A/W A320 SRM 51-72-11-911- 001 REV= 157.00 DATED 15-APR-26 REF: NAT D
- [SDR DALA2026052703215](https://openairdocs.org/sdr/DALA2026052703215.md): None · none · May 23, 2026 · N351NW · Airbus A320212 · Standard Practices/Structures
  > ER/A 589110-14AD REV 'A' ISSUED FOR REPAIR AT FR16RH & DOOR STOP 1. FOLLOW ON ACTION REQUIRED. PERFORM SECTION IV EVERY 11500FC AFTER SECTION III. THIS SUPERSE DES LOG 1704322. ASSOCIATED ER/A 14-589110 ADDED FOR AC 3251. (LP: 1608765) AIRCRAFT WAS GROUNDED
- [SDR DALA2026052403141](https://openairdocs.org/sdr/DALA2026052403141.md): Stringer · corroded · May 23, 2026 · N351NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION, LOWER FUSELAGE, FWD CARGO COMPARTMENT, AT FR.32+75MM, STR.40LH WITH CORROSION. REPAIRED STRINGER 40L, SECTION BETWEEN FR 31 +215MM AND FR 32 + 305MM IAW SRM 53-21-13-300-018, PARAG 1, PARAG 2A, FIGURE 001. THIS TASK IS CATEGORY B REPAIR AND
- [SDR DALA2026053103289](https://openairdocs.org/sdr/DALA2026053103289.md): None · none · May 21, 2026 · N351NW · Airbus A320212 · Standard Practices/Structures
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 102900FC FROM SECTION I. ER/A TO BE REVI SED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 AD
- [SDR DALA2026053103288](https://openairdocs.org/sdr/DALA2026053103288.md): None · none · May 21, 2026 · N351NW · Airbus A320212 · Standard Practices/Structures
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR INSTALLE D AT FR68RH AND S-22 PER ER/A 634286-14AD. C/A: SECTION I IS LIMITED TO 71500FC FROM SECTION I. ER/A TO BE REVIS ED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASSOCIATED ER/A 14-634286 ADDE
- [SDR DALA2026053103287](https://openairdocs.org/sdr/DALA2026053103287.md): None · none · May 21, 2026 · N351NW · Airbus A320212 · Standard Practices/Structures
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPAIR AT FR68R H & S-22 PER ER/A 634286-14AD. ER/A TO BE REVISED PRIOR 32328FC FROM SECTION I (40K FC FROM SB 53-1290 EMBODIMENT) ELSE REMOVE A/C FROM SERVICE. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP:
- [SDR DALA2026053103286](https://openairdocs.org/sdr/DALA2026053103286.md): None · none · May 21, 2026 · N351NW · Airbus A320212 · Standard Practices/Structures
  > ER/A 634286-14AD ISSUED FOR REPAIR AT FR68RH AT S-22. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II EVERY 16200FC AFTER SECTION I. ASSOCIATED ER/A 14-634286 ADDED FOR AC 3251. (LP: 1605169, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026051603024](https://openairdocs.org/sdr/DALA2026051603024.md): Attach Bracket · corroded · May 14, 2026 · N351NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, LOWER FUSELAGE TOILET SERVICE PANEL SUPPORT ATTACH BRACKETS AND RIVETS CORRODED. REPLACED SUPPORTS P/N: 5348220020000, D5348007321500, D5348027421600, SHIMS (2EA) D5348007320800 AND SPRING (2EA) P/N: D5348007421401 IAW A320 SRM 51-72-11-911
- [SDR DALA2025080405801](https://openairdocs.org/sdr/DALA2025080405801.md): Light · broken · Aug 1, 2025 · N351NW · Airbus A320212 · Emergency Lighting
  > FOUND EMERGENCY LIGHT HOUSING BROKEN OF SEAT 24DEF. R & R SEAT 24FED EMERGENCY LIGHT HOUSING IN REF TO A320 CMM 25-23- 51. OPS CHECK NML. OK FOR SVC.
- [SDR DALA2025062504773](https://openairdocs.org/sdr/DALA2025062504773.md): Cooling Fan · contaminated · Jun 24, 2025 · N351NW · Airbus A320212 · Airborne Auxiliary Power Unit (APU) System
  > SHIP 3251, DIRTY SOCK ODOR IN FLIGHT DECK. FOUND APU COOLING FAN WET WITH OIL. T/S PER A320 TSM 49 -00. NO EXTERNAL LEAKS. VERIFIED APU COOLING FAN NOT LEAKING. APU INTAKE PLENUM DIRTY, SUSPECT INTERNAL LEAK. C/W AMDS W/C 4916-2001 AND R/REINSTALL APU ACCESS
- [SDR DALA2025051203647](https://openairdocs.org/sdr/DALA2025051203647.md): Slip Joint · leaking · May 10, 2025 · N351NW · Airbus A320212 · Fuel Storage
  > SHIP 3251 DISC: TAXING OUT AT SLC -AIR LWING LEAK- COMPLIED WITH ECAM AND RESET ENG 1 BLEED MESSAGE CLEARED, DISCONTINUED. C/A: PERFORMED T/S IAW A320 TSM 36-22-00-810-801-A. FOUND PYLON PNEUMATIC SLIP JOINT LEAKING DIRECTLY ONTO PYLON BLEED LOOP. REMOVED AND
- [SDR DALA2025012700639](https://openairdocs.org/sdr/DALA2025012700639.md): Sense Line · loose · Jan 25, 2025 · N351NW · Airbus A320212 · Pneumatic Indicating System
  > SHIP 3251 DISC: REJECTED TAKEOFF (THRUST ADVANCED, 0 KTS). DURING ICE CLEARING PROCEDURE (70% N1) AIR ENG 2 BLEED ABNORM PR, ABOVE 50% N1, ENG BLEED DROPS TO 0 PSI. C/A: POST FLT REPORT,PRESS REG-V 4001HA2 OR, SOL 10HA2 OR SENSE LINE 36-11-00. INSPECTED SENSE
- [SDR DALA2025011900435](https://openairdocs.org/sdr/DALA2025011900435.md): None · none · Jan 8, 2025 · N351NW · Airbus A320212 · Standard Practices/Structures
  > SHIP3251 DISC: ER/A 604897-14 / SECTION III INSPECTIONS. C/A: ER/A 604897-14, REV C / AT, OR PRIOR TO 8,000 FLIGHT CYCLES FROM SECTION II REPAIR (43,171 TOTAL FLIGHT CYCLES), AND REPETITIVELY EVERY 1,500 FLIGHT CYCLES THEREAFTER, ACCOMPLISH SECTION II INSPECTI
- [SDR DALA2024100709726](https://openairdocs.org/sdr/DALA2024100709726.md): Unknown · odor · Oct 3, 2024 · N351NW · Airbus A320212 · Air Distribution System
  > .SHIP 3251 DISC: POSSIBLE DIRTY SOCK ODOR DETECTED BY FA & GATE AGENT GETTING ON AIRCRAFT IN CHS - ALSO "SWEET" CRAYON SMELL NOTED. C/A: FOUND OIL AT APU PLENUM/ SEAL. REF LOG 0590544 FOR FURTHER CORRECTIVE ACTION. FWD APU TO MEL 49-10-01A. NO "M" PROCEDURES.
- [SDR DALA2024092809494](https://openairdocs.org/sdr/DALA2024092809494.md): Cooling Fan · leaking · Sep 27, 2024 · N351NW · Airbus A320212 · Airborne Auxiliary Power Unit (APU) System
  > SHIP 3251 DSIC: ON DESCENT INTO SLC AROUND 11000' MSL GOT THE DIRTY SOCK SMELL FROM THE A/C SYSTEM. AFTER ENGINES WERE SHUT DOWN AT GATE THE SMELL WENT AWAY. C/A: PERFORMED CAUSE TABLE. FOUND APU TO BE AT FAULT. (595143). INSPECTED APU FOUND OIL IN INLET. REMO
- [SDR DALA2024090408709](https://openairdocs.org/sdr/DALA2024090408709.md): Inlet · contaminated · Sep 1, 2024 · N351NW · Airbus A320212 · APU Core Engine
  > SHIP 3251 DISC: AT APPROX 2000 FT ON FINAL APPROACH FA ALERTED PILOTS OF DIRTY SOCK SMELL IN COMFORT + AREA. SMOKE AND FUME QRH RUN ON GROUND. FUMES DISAPATED WITH #2 PACK OFF. C/A: WORKED TASK CARD #2100-2005 TO STEP 6. WORKED TASK CARD #0550- 2002 UP TO STEP
- [SDR DALA2024083008570](https://openairdocs.org/sdr/DALA2024083008570.md): Bottle · low pressure · Aug 25, 2024 · N351NW · Airbus A320212 · Emergency Equipment
  > SHIP 3251 DISC: L2 DOOR ASSIST BOTTLE LOW. C/A: CHANGED L2 DOOR EMERG OPERATION CYLINDER PER A320 AMM 52-10. RII STEPS COMPLETED. (LP: 5092141)
- [SDR DALA2024082708466](https://openairdocs.org/sdr/DALA2024082708466.md): Apu · leaking · Aug 22, 2024 · N351NW · Airbus A320212 · APU Oil System
  > AT 6000' ON DECENT INTO (ENGINES IDLE) DTW (PACKS ON) ODOR ( ACRID) RETURNED TO FLIGHT DECK ONLY. C/A: PERFORMED JOB CARD 0550-2002, CORDINATED WITH MCC TO DO DECONTAMINATION AND INSPECTION OF ENGINES. PERFORMED BLACK LGHT CHECK OF #1 ENG BLEED SYSTEM. NO SIGN
- [SDR DALA2024082308388](https://openairdocs.org/sdr/DALA2024082308388.md): Inlet · contaminated · Aug 21, 2024 · N351NW · Airbus A320212 · APU Core Engine
  > SHIP 3251 DISC: AT GATE (BNA) APU BLEED ON STRONG ACRID (SMELL IN FLIGHT DECK ONLY) APU BLEED OFF SMELL IS NO LONGER PRESENT. ENG NOT RUNNING. C/A: DURING INSPECTION OF APU ODOR IAW A320 AMM 49-00 FOUND APU INLET SHROUD COVERED W/ OIL. C/W W/C 2100-2005. NO IS
- [SDR DALA2024082208334](https://openairdocs.org/sdr/DALA2024082208334.md): Module · odor · Aug 19, 2024 · N351NW · Airbus A320212 · Equipment/Furnishings Wiring
  > SHIP 3251 DISC: FLIGHT CREW REPORTS ELECTRICAL SMOKE SMELL IN FIRST CLASS CABIN. OUTLET 2C,2D WENT OUT. SMELL PRESENT FOR FIRST 15 MINS IN FLIGHT. REST OF FLIGHT OK. C/A: C/W NO GO ODI PREVENTION PROGRAMA320 ATA 2172. FOUND ELECTRICAL ODOR FROM SEAT POWER MODU
- [SDR DALA2024072407434](https://openairdocs.org/sdr/DALA2024072407434.md): Inlet · dirty · Jul 22, 2024 · N351NW · Airbus A320212 · APU Core Engine
  > UPON ACTIVATION OF APU BLEED CABIN FILLED WITH FUMES STRONGEST AT AFT ROWS. DISAPATED WITH BLEED SHUTOFF. C/A: ACFT WAS NO FLT. NO OIL/HYD USAGE. NO EVIDENCE OF OIL IN APU COMPARTMENT.. APU INLET FOUND VERY DIRTY. REF LOG 6137579 FOR APU MEL. R/R BOTH RECIRC F
- [SDR DALA2024062706536](https://openairdocs.org/sdr/DALA2024062706536.md): Computer · faulty · Jun 26, 2024 · N351NW · Airbus A320212 · Stabilizer Control System
  > SHIP 3251 DISC: DURING CLIMB WITH A/P OFF FWD STICK REQUIRED TO MAINTAIN PITCH. WITH NEUTRAL STICK, A/C PITCH INCREASES APPROX 1/2O PER SEC. HAPPENS DURING LAND TOO. C/A: EFCS GROUND SCAN FAULT "ELAC2-COM OR WIRING FROM ACCLRM3". GAINED ACCESS TO ACCLRM 3 AND
- [SDR DALA2024062706535](https://openairdocs.org/sdr/DALA2024062706535.md): Computer · faulty · Jun 26, 2024 · N351NW · Airbus A320212 · Stabilizer Control System
  > SHIP 3251 DISC: DURING CLIMB WITH A/P OFF FWD STICK REQUIRED TO MAINTAIN PITCH. WITH NEUTRAL STICK, A/C PITCH INCREASES APPROX 1/2O PER SEC. HAPPENS DURING LAND TOO. C/A: EFCS GROUND SCAN FAULT "ELAC2-COM OR WIRING FROM ACCLRM3". GAINED ACCESS TO ACCLRM 3 AND
- [SDR DALA2024062106278](https://openairdocs.org/sdr/DALA2024062106278.md): Unknown · odor · Jun 20, 2024 · N351NW · Airbus A320212 · Air Distribution System
  > SHIP 3251 DISC: ON TAXI OUT STRONG DIRTY SOCK ODOR FOLLOWED BY BURRING RUBBER SMELL FOLLOWED BY STRONG FUEL ORDER. DONNED O2 MASK. GATE RETURN SMELL WAS AFTER APU SHUTDOWN. C/A: C/W NO GO ODI AMDS WORK CARD 0550-2002. DECISION TREE LEADS TO APU. FOUND APU GENE
- [SDR DALA2024053005671](https://openairdocs.org/sdr/DALA2024053005671.md): Fcu · faulted · May 29, 2024 · N351NW · Airbus A320212 · Autopilot System
  > SHIP 3251 - DIV - TO ATL DUE TO FCU 1+2 FAULT. CORRECTIVE ACTION: REPLACED FLIGHT CONTROL UNIT.
- [SDR DALA2024020501519](https://openairdocs.org/sdr/DALA2024020501519.md): Spoiler Sys · faulted · Feb 5, 2024 · N351NW · Airbus A320212 · Drag Control System
  > SHIP 3251 DISC: FCNT - UNCOMMADED ROLL ON SPOILER DEPLOYMENT. UPON DEPLOYMENT OF SPEED BRAKES, AICRAFT ABRUPTLY PULLED RIGHT. WHEN SPEED BRAKES RETRACT, AIRCRAFT PULLS LEFT BUT LESS ABRUPTLY. F/CTL PAGE SHOWN NO DISCPREPENCIES OR ABNORMAL DEPLOY/STOY RATES. C
- [SDR DALA2024011400565](https://openairdocs.org/sdr/DALA2024011400565.md): Unknown · unknown · Jan 13, 2024 · N351NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3251 DISC: PERFORM PERMANENT REPAIR ON FR29 TO FR 30 AT LEVEL STRG 1L TO STRG 1R / TIMING ANTENNA COVER PLATE. C/A: COMPLIED WITH ER/A 604897-14 REV. B MATCHES WITH ALL STEPS ON PRI 604897-14 REV.B PRI REV.0, PRI 604897-14 REV.B PRI REV.1, PRI604897-14 RE
- [SDR DALA2024011600659](https://openairdocs.org/sdr/DALA2024011600659.md): Damper · no test · Jan 12, 2024 · N351NW · Airbus A320212 · Passenger/Crew Doors
  > DON'T PASS TEST PASSENGER CREW DOOR 841 DOOR DAMPER AT FWD. C/A: FWD TO MEL 52-10-04. T/S REF. A320 TSM 52-11-00-810-823-A. NO TROUBLE FOUND AT R1 DOOR DAMPER AND PRESSURE IS GOOD. MEL AND PLACARDS REMOVED. NO " M" PROCEDURES. OK FOR SERVICE.
- [SDR DALA2024011400562](https://openairdocs.org/sdr/DALA2024011400562.md): Unknown · unknown · Jan 10, 2024 · N351NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3251, INSPECTIONS HAVE BEEN ADDED VIA SEPARATE LOG PAGE 0751012. CLOSED LOG AND REMOVED MONITOR INSP.) DTE DURING ACCOMPLISHMENT OF AA 2330-01179-02H, FUSELAGE SKIN WAS GOUGED DURING REMOVAL OF PCS TIMING ANTENNA COVER PLATE (PN 21299). DURING CURRENT CH
- [SDR DALA2024010200006](https://openairdocs.org/sdr/DALA2024010200006.md): Slide · deformed · Dec 31, 2023 · N351NW · Airbus A320212 · Escape Slide
  > DEFORMATION OF ESCAPE SLIDE RAFT ON PASSENGER CREW DOOR 842. REPLACED ESCAPE SLIDE RAFT ON PASSENGER CREW DOOR 842 THIS INSTALLATION TO BE DOCUMENTED WITH AMDS CARD 5210-7089-RA-DE RII INSPECTION COMPLETE. REMOVED UNSERVICEABLE ESCAPE SLIDE RAFT ON PASSENGER
- [SDR DALA2024010210744](https://openairdocs.org/sdr/DALA2024010210744.md): Unknown · unknown · Dec 28, 2023 · N351NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3251 DISC: DENT EXTERNAL SKIN LOCATED BTW FR 29 TO FR 30 AND STR 36R TO STR 37R A T LOWER FUSELAGE. C/A: EVALUATED DENT LOCATED ON EXTERNAL SKIN BTW FR 29 TO FR 30 AND STRG 36R TO STRG 37R LOWER FUSELAGE AND FOUND WITHIN LIMITS AS PERA320 SRM 53-00-11-283
- [SDR DALA2023121810320](https://openairdocs.org/sdr/DALA2023121810320.md): Unknown · unknown · Dec 14, 2023 · N351NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3251 DISC: ER/A 604897-14 REV A / SECTION II PERMANENT REPAIR. C/A: 604897-14, REV A / THIS LP IS UPDATED TO CORRECT "E" MONITOR TO INSPECTION "N" / THIS LP DOES REQUIRE MAINTENANCE ACTION IS NOT AN ENGINEERING FUNCTION-RELATED RESTRICTION. (LP: 0110023)

Next page: https://openairdocs.org/aircraft/N351NW/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 = 'N351NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N351NW/reports

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