# Service difficulty reports: N352NW

A list on [N352NW](https://openairdocs.org/aircraft/N352NW.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 · 179 reports

- [SDR DALA2026092805368](https://openairdocs.org/sdr/DALA2026092805368.md): Computer · faulty · Sep 25, 2026 · N352NW · Airbus A320212 · Flight Control System
  > ON THE ARRIVAL TO DTW, THE ACFT HAD A NOSE DOWN PITCH. THE ECAM FOR FLT CONTROL ELAC 2 PITCH FAULT COMPLIED WITH ECAM & QRH. IAW AMM 27 93 34, TSM 27-93-00 810 867 710-001, REPLACED ELAC 2. OPS TESTED GOOD. PERFORMED EFCS AND SIDESTICK TESTING, NO FAULTS. A
- [SDR DALA2026080704568](https://openairdocs.org/sdr/DALA2026080704568.md): Window Frame · cracked · Aug 6, 2026 · N352NW · Airbus A320212 · Fuselage Main, Structure
  > AD 2020-17-03 / A.A WORKCARD 5311-01226-01. REQUESTING REPAIR DISPOSITION. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. FLIGHT DECK, WINDSHIELD FRAMING, L/H R/H CONTINUITY FITTING CRACKED. CONTACT LIAISON ENGINEERING FOR FURTHER DISPOSITION. PERFORME
- [SDR DALA2026080204455](https://openairdocs.org/sdr/DALA2026080204455.md): Shear Plate · corroded · Jul 30, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, SHEAR PLATE CORRODED AT -Y1150 BETWEEN FR 69 TO FR 70. REPLACED SHEAR PLATE AT PAX CABIN -Y1150 BETWEEN FR 69 TO FR 70 IAW SRM 51-72-11-977-001, PARA 2, SRM REV 158.00, & AIRBUS REF DWG D53474180. (LP: 172925
- [SDR DALA2026072804384](https://openairdocs.org/sdr/DALA2026072804384.md): Fitting · damaged · Jul 24, 2026 · N352NW · Airbus A320212 · Fuselage Main, Structure
  > DAMAGE TOLERANCE EVALUATION ( DTE) REQUIRED FOR REPLACEMENT CENTER WINDOW FRAMES AND CONTINUITY FITTINGS PER ER/A 635072-14AD. SECTION I IS LIMITED TO 60000 TOTAL AIRCRAFT FLIGHT CYCLES. ER/A TO BE REVISED PRIOR TO THIS LIMIT ELSE REMOVE A/C FROM SERVICE ASS
- [SDR DALA2026072004241](https://openairdocs.org/sdr/DALA2026072004241.md): Frame · damaged · Jul 16, 2026 · N352NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3252 DISC: NIV STEPS 6 AND 16 IF DAMAGE FOUND CONTACT ENGINEERING UPPER FUSELAGE PAX CABIN AT FR 20 RH DOUBLE JOGGLE AREA AT HOLES NR 5 AND 6 FOUND WITH BURR DAMAGE INDICATION AT FRAME LAYER. NOTE: PER MONITOR LOG PAGE 0252469 RELATED TO ER/A #550431-14AD
- [SDR DALA2026071504153](https://openairdocs.org/sdr/DALA2026071504153.md): Fitting · corroded · Jul 14, 2026 · N352NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, FWD CARGO BAY, DOOR CUTOUT AT FR 24A & 25MM, DOOR SILL CORRODED. REPLACED CORNER FITTING AT FWD CARGO BAY DOOR CUT OUT FR 24A LOWER SILL AREA IAW SRM 51-72-11-911-001, REV 158.00 AND DRAWING D53231725. (LP: 1699971, AIRCRAFT WAS GROUNDED).
- [SDR DALA2026071504150](https://openairdocs.org/sdr/DALA2026071504150.md): Door Sill · corroded · Jul 13, 2026 · N352NW · Airbus A320212 · Fuselage Main, Structure
  > LEVEL 2 CORROSION, FWD CARGO COMPARTMENT DOOR CUTOUT AT FR 28 - 25MM, DOOR SILL WITH CORROSION. REPLACED CORNER FITTING AT FWD CARGO COMPARTMENT DOOR CUTOUT FR28 LOWER SILL AREA IAW SRM 51-72- 11-911-001 REV 158.00 AND REFERENCE DRAWING 532 31725. (LP: 169793
- [SDR DALA2026071304084](https://openairdocs.org/sdr/DALA2026071304084.md): Skin · scratched · Jul 9, 2026 · N352NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > FWD UPPER FUSELAGE AROUND PCS/TIMING ANTENNA CUTOUT AT FR29+ 195MM AND BETWEEN STRINGER 1L-1R SKIN PANEL WITH SCRATCH. C/A: PERFORMED FUSELAGE SKIN REPAIR BETWEEN FR 29 AND FR 30 AT STGR 1R IAW DELTA ER/A # 635410-14 REV: ORIGINAL DATED 03-JUL-26. NOTE: PERFOR
- [SDR DALA2026071304083](https://openairdocs.org/sdr/DALA2026071304083.md): Skin · nicked · Jul 9, 2026 · N352NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > FWD FUSELAGE FR13+65MM AND 400MM ABOVE OF LEFT SIDE STRG SKIN PANEL WITH NICK. PERFORMED PERMANENT FUSELAGE SKIN REPAIR AT FWD FUSELAGE FROM FR 12 +238MM TO FR 13 +155MM, BETWEEN Z-520 AND Z-742 L/H SIDE I.A.W A320 SRM 53-11-11-300-041 PARAG 1 AND PARAG 2A FI
- [SDR DALA2026070603921](https://openairdocs.org/sdr/DALA2026070603921.md): Repair · not reported · Jul 3, 2026 · N352NW · Airbus A320212 · Fuselage Structure (General)
  > ER/A 635410-14 PERFORMS A REPAIR AT FR29 & S-1 LH & RH PER SRM T ASK 53-21-11-300-087. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN THE SOONER OF 40000FC OR 80000FH FROM SECTION I AND EVERY SOONER OF 2900FC OR 5800FH THEREAFTER. ASSOCIATED ER/A 14-
- [SDR DALA2026070603920](https://openairdocs.org/sdr/DALA2026070603920.md): Support Fitting · damaged · Jul 3, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > ER/A 635102-14AD ISSUED FOR REPAIR TO LH & RH LOWER LATERAL SUPPORT FITTINGS OF THE 80VU RACK. FOLLOW ON ACTION IS REQUIRED. PERFORM SECTION II WITHIN 19500FC FROM SECTION I AND EVERY 1000F C THEREAFTER. ASSOCIATED AA 2515-01014 ADDED FOR AC 3252 ASSOCIATED E
- [SDR DALA2026070904011](https://openairdocs.org/sdr/DALA2026070904011.md): Seat Track · corroded · Jul 2, 2026 · N352NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL SEAT TRACK CORRODED AT Y1292, FR 66. REPLACED LONGITUDINAL FLOOR SEAT TRACK (ORIGINAL P/N: 14N00031- 101) AT Y1292 FROM FR64 TO FR 66 IAW A320 SRM TASK 51-72-11-911- 001 PARAG 2C AND INSTALLED IAW
- [SDR DALA2026070503909](https://openairdocs.org/sdr/DALA2026070503909.md): Seat Track · corroded · Jul 2, 2026 · N352NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR SEAT TRACK CORRODED AT Y765, FR65. REPLACED LONGITUDINAL FLOOR SEAT TRACK (ORIGINAL P/N 14N00031- 1003) AT Y 765 FROM FR 64 TO FR 68 IAW A320 SRM TASK 51-72-11- 911-001 PARAG 2C, AND INSTALL
- [SDR DALA2026070503908](https://openairdocs.org/sdr/DALA2026070503908.md): Intercostal · corroded · Jul 2, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, LOWER FUSELAGE, FWD CARGO COMPARTMENT, FROM FR 27 & 28, ON STR 38 LH, INTERCOSTAL LOWER SECTION WITH CORROSION. REPLACED INTERCOSTAL AT FWD CARGO COMPARMENT FROM FR27 AND FR28, AT STR 38 LT IAW A320 SRM 51-72-11-911-001 REV 158.00 DATED 01
- [SDR DALA2026070203879](https://openairdocs.org/sdr/DALA2026070203879.md): Stringer · corroded · Jul 1, 2026 · N352NW · Airbus A320212 · Fuselage Main, Longeron/Stringer
  > LEVEL 2 CORROSION, LOWER FUSELAGE,FWD CARGO COMPARTMENT,FROM FR 33 & 34,ON STR 38 RH,INTERCOSTALLOWER SECTION WITH CORROSION. REPLACED INTERCOSTAL AT FWD CARGO COMPARMENT, FROM FR33 AND FR34, AT STR 38RH IAW SRM 51-72-11-911-001, REV 158.00 DATED 01 /JUN/26
- [SDR DALA2026070103872](https://openairdocs.org/sdr/DALA2026070103872.md): Floor Support · corroded · Jun 29, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, UPPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR BEAM CORRODED AT -Y254 BETWEEN FR68 TO FR69. REPLACED LONGITUDINAL FLOOR BEAM AT -Y254 BTWN FR68 TO FR70 IAW A320 SRM TASK 51-72-11-911-001 PARAG C (1), SRM 53-41-14-01A, FIG 301, ITEM 225.
- [SDR DALA2026062503773](https://openairdocs.org/sdr/DALA2026062503773.md): Support · corroded · Jun 24, 2026 · N352NW · Airbus A320212 · Trailing Edge Flaps
  > LH WING, OTBD FLAP, SUPPORT AT TRACK 3, RIB 5 AND TRACK 4, BETWEEN INNER RIB 14 AND OUTER RIB 14, WITH CORROSION INTERNAL STRUCTURE. FOR REMOVAL OF THE LH WING OUTBOARD FLAP S/N: D01703, SEE DELTA WORK CARD 2750-6020-LT. (LP: 1664687, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062403745](https://openairdocs.org/sdr/DALA2026062403745.md): Floor Support · corroded · Jun 23, 2026 · N352NW · Airbus A320212 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, PPER FUSELAGE, AFT PAX CABIN, LONGITUDINAL FLOOR SUPPORT CORRODED AT Y1292, BETWEEN FR67 AND FR68. REPLACED LONGITUDINAL FLOOR SUPPORT AT UPPER FUSELAGE AFT PAX CABIN BETWEEN FR66 AND FR68 Y1292 IAW SRM 51-72-11-911-001 REV 158 AND DWG D53
- [SDR DALA2025112508586](https://openairdocs.org/sdr/DALA2025112508586.md): Fitting · damaged · Nov 22, 2025 · N352NW · Airbus A320212 · Fuselage Main, Attach Fittings
  > LH UPPER ACTUATOR FITTING HAS TWO FASTENERS PULLED THROUGH FITTING. REPAIRED PER PRI 604353-14AD REV. 0, 1, 2, 3, 4, 5 AND 6 AND COMPLIED WITH ER/A 604353-14AD REV. B SECTION III. (LP: 1316696)
- [SDR DALA2025102907909](https://openairdocs.org/sdr/DALA2025102907909.md): Engine · bird ingestion · Oct 29, 2025 · N352NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > BIRD STRIKE IN #2 ENGINE ON FINAL APPROACH. NO ABNORMAL ENGINE INDICATIONS. ENGINE WAS AT LOW POWER. SMELLED LIKE FOOD COOKING IN OVEN ACCORDING TO FAS. LATER LATER SMELLED LIKE FRIED CHICKEN. PERFORMED AMM 05-51-14. CLEARED ENGINE OF DEBRIS REF A320 AMM 72-00
- [SDR DALA2025101007392](https://openairdocs.org/sdr/DALA2025101007392.md): Control Unit · faulted · Oct 9, 2025 · N352NW · Airbus A320212 · Power Lever
  > DIV - DIVERTED TO RDU DUE TO AN ENG 2 THROTTLE LEVER DISAGREE MESSAGE. REPLACED THROTTLE CONTROL UNIT PER A320AMM 76-11. OPERATIONAL CHECK GOOD, NO FAULTS.(LP: 7403542)
- [SDR DALA2025100607231](https://openairdocs.org/sdr/DALA2025100607231.md): Oil System · leaking · Oct 1, 2025 · N352NW · Airbus A320212 · APU Oil System
  > AFTER APU START UP AND WARM UP AT THE GATE WHEN THE APU BLEED SELECTED ON THE DIRTY SOCK SMELL FILLED THE COCKPIT AND ENTIRE CABIN. SMELL WAS VERY STRONG. PERFORMED GVI OF APU COMPARTMENT. FOUND EVIDENCE OF AN OIL LEAK ON PLENUM. OK FOR SVC. (LP: 7403510)
- [SDR DALA2025091106704](https://openairdocs.org/sdr/DALA2025091106704.md): Light · detached · Sep 9, 2025 · N352NW · Airbus A320212 · Emergency Lighting
  > EMERGENCY EXIT LIGHTING UNIT UNDER SEAT 28D LOOSE/HANGING DOWN. FOUND 28D SEAT EMER LIGHT BOX BROKEN, REPLACED BOX, OP CHECKS GOOD, OK FOR SERVICE. (LP: 7848226)
- [SDR DALA2025090406538](https://openairdocs.org/sdr/DALA2025090406538.md): Filter · odor · Sep 4, 2025 · N352NW · Airbus A320212 · Air Distribution System
  > SHIP 3252 DISC: WITH APU BLEED "ON" DIRTY SOCK ODOR STRONGER IN FLIGHT DECK AFT F/A ALSO COMPLAINED ABOUT ODOR IN AFT CABIN, APU BLEED WAS TURNED OFF SMELL DISSIPATED. C/A: AFTER COMPARTMENT WASH, RAN APU FOR 30+ MINUTES-NO LEAKS FOUND. C/W AMDS WORK CARD 491
- [SDR DALA2025090106462](https://openairdocs.org/sdr/DALA2025090106462.md): Bracket · excess play · Aug 27, 2025 · N352NW · Airbus A320212 · Landing Gear Position and Warning
  > ATB DUE TO L/G DOORS NOT CLOSED, L/G GEAR NOT UPLOCKED, AND L/G SHOCK ABSORBER FAULT ECAM WARNINGS. FOUND EXCESSIVE PLAY OF FLIGHT/GROUND SENSING MECHANISM BRACKET DUE TO LOOSE BOLT AND WORN-OUT BUSHINGS. REPLACED FLIGHT/GROUND SENSING MECHANISM BUSHED LEVER,
- [SDR DALA2025071505318](https://openairdocs.org/sdr/DALA2025071505318.md): Computer · faulted · Jul 12, 2025 · N352NW · Airbus A320212 · Fuel Quantity Indicator
  > SHIP 3252 - MISC - DECLARED EMERGENCY FOR SUSPECTED FUEL LEAK. CENTER TANK QUANTITY FLUCTUATING. MEL ALREADY APPLIED FOR CENTER TANK AUTO FEED SYSTEM. CORRECTIVE ACTION: REPLACED FQIC. (LP: 7745944)
- [SDR DALA2025051203645](https://openairdocs.org/sdr/DALA2025051203645.md): Buss · abnormal · May 11, 2025 · N352NW · Airbus A320212 · AC Power Distribution System
  > SHIP 3252 DISC: WHILE CLOSING CIRCUIT BREAKERS FOR BREAK SELECTOR VALVE REPLACEMENT, AC 2 BUS DROPPED OFF-LINE. ATTEMPTED RESETS, NO HELP. UPON INITIATING BPCU BITE THROUGH CFDS, THE 123VU PANEL SPARKED. C/A: REF HANGAR VISIT P334905220250503 NR 32 FOR CORRECT
- [SDR DALA2025050103356](https://openairdocs.org/sdr/DALA2025050103356.md): Hydraulic Line · leaking · Apr 30, 2025 · N352NW · Airbus A320212 · Hydraulic System, Main
  > SHIP 3252 DISC: PASSING N8000' ON DESCENT, GOT A DIRTY SOCK SMELL. SMELL SEEMED TO GO AWAY AFTER ABOUT 1 MINUTE. C/A: PERFORMED OPS TEST OF LT + RT PACK PER A320 AMM 21-00. COULD NOT DUPLICATE. FOUND HYD FLUID THROUGHOUT A/C BELLY ORIGINATING FROM FWD CARGO BE
- [SDR DALA2025041502958](https://openairdocs.org/sdr/DALA2025041502958.md): Fairing · damaged · Apr 12, 2025 · N352NW · Airbus A320212 · Aerodynamic Fairings
  > SHIP 3252 DISC: PANEL 197GB WING TO BODY FAIRING HAS SEVERAL FASTENER HOLES DAMAGED. SCEPTRE LOG PAGE ENTERED FOR SDR REPORTING. SUMMARY SEE NR FOR ADDITIONAL INFORMATION 016-0001:10-0553-8-6853/001 00007 ACCOMPLISHED HOLE REPAIR PER A320 SRM 51-77-12. (LP: 0
- [SDR DALA2025032002103](https://openairdocs.org/sdr/DALA2025032002103.md): Light · inoperative · Mar 15, 2025 · N352NW · Airbus A320212 · Emergency Lighting
  > SHIP 3252 DISC: FLOOR PROXIMITY EMERGENCY LIGHT AT ROW 29D INOP. C/A: WRONG LIGHT SENT. RECIEVED RED LIGHT. NEEDS WHITE LIGHT FIXTURE MPN# BR9471-4FS STK# 31-2500-3-2311 IAW REF AIPC FIG. 33 -51-09-80 ITEM 010A. NASI LGA. INSTALLED NEW LIGHT HOUSING AS PER A32
- [SDR DALA2024100709725](https://openairdocs.org/sdr/DALA2024100709725.md): Unknown · odor · Oct 4, 2024 · N352NW · Airbus A320212 · Air Distribution System
  > WORKING ACARS DUE TO F/A REPORT OF BURNING RUBBER ODOR IN THE AFT GALLEY AND AFT CABIN. C/A: C/W WC 0550-2003 VERIFICATION CHECK FOR RESIDUAL ODOR. NO ODOR PRESENT AT THIS TIME.
- [SDR DALA2024051405169](https://openairdocs.org/sdr/DALA2024051405169.md): None · none · May 9, 2024 · N352NW · Airbus A320212 · Standard Practices/Structures
  > SHIP 3252 DISC: ON APPROACH WITH/ STORMS IN WAY DISCONTINUED APPROACH HAD A 10KT GAIN THAT CAUSED APPROX. 2 KT OVERSPEED WITH FLAPS TRANSITIONING FROM 1 TO 0. PERFORMED FLAP OVERSPEED INSPECTION IAW A320 AMM 05-51-13. NO DEFECTS NOTED. OK FOR SERVICE. (LP: 5
- [SDR DALA2024050905049](https://openairdocs.org/sdr/DALA2024050905049.md): Filter · damaged · May 7, 2024 · N352NW · Airbus A320212 · Air Conditioning System
  > SHIP 3252 DISC: ON TAXI IN, BOTH PILOTS SMELLED A FAINT PLASTIC BURNING SMELL IN COCKPIT. 5 MIN LATER ECAM SMOKE LAV DET FAULT (1626, AUS). C/A: C/W W/C 0550-2002, UPON INSP FOUND DEMISTER FILTER IN BAD CONDITION W/PLASTIC SMELL. R&R AS PER A320 AMM 21-26. PER
- [SDR DALA2024032303701](https://openairdocs.org/sdr/DALA2024032303701.md): Slide Raft · no test · Mar 19, 2024 · N352NW · Airbus A320212 · Escape Slide
  > SHIP 3252 DISC: DONT PASS OPERATIONAL TEST SLIDE RAFT PASSENGER CREW DOOR 832 AT AFT G ALLEY AREA. C/A: REPLACED SLIDE RAFT 832 PN D30665-705, SN A5584RP ON UNSERVICEABLE CONDITION BY SLIDE RAFT PN D30665-705, SN A5562RP ON SERVICEABLE CONDITION AS PER AMDS CA
- [SDR DALA2024032303688](https://openairdocs.org/sdr/DALA2024032303688.md): Slide Raft · no test · Mar 19, 2024 · N352NW · Airbus A320212 · Escape Slide
  > SHIP 3252 DISC: DO NOT PASS TEST SLIDE RAFT 831 AT FWD GALLEY AREA. C/A: REPLACED SLIDE RAFT ON UNSERVICEABLE CONDITION P/N: D30664-709, S/N:M20728, FTN: 5G6221, FOR NEW SLIDE RAFT ON SERVICEABLECONDITION P/N: D30664-705, S/N: A5089RP, FTN: 1F6597 ON PASSENGER
- [SDR DALA2024032303687](https://openairdocs.org/sdr/DALA2024032303687.md): Rib · corroded · Mar 19, 2024 · N352NW · Airbus A320212 · Nacelle/Pylon, Frame/Spar/Rib
  > SHIP 3252 DISC: CORROSION RIB 8 ON REFORCING PLATE ON LH PYLON. C/A: COMPLIED WITH ER/A 616310-14AD REV.ORIGINAL. JOB COMPLETE. ASSOCIATED ER/A 00-616310 ADDED FOR AC 3252. (LP: 0251584)
- [SDR DALA2024031903447](https://openairdocs.org/sdr/DALA2024031903447.md): Power Supply · inoperative · Mar 17, 2024 · N352NW · Airbus A320212 · Emergency Lighting
  > SHIP 3252 DISC: INOP EPSU 10WL AT FWD GALLEY AREA. C/A: REMOVED EMERGENCY POWER SUPPLY UNIT 10WL IN UNSERVICEABLE CONDITION P/N: 3214-54-10 S/N: 1395 ON FWD GALLEY AREA AS PER A 320 FAM AMM 33-51-38-000-001-A STEP 3.C AND 4.A (1) THRU 4.A. (4) JOB IN PROGRESS
- [SDR DALA2024032003529](https://openairdocs.org/sdr/DALA2024032003529.md): Plate · corroded · Mar 16, 2024 · N352NW · Airbus A320212 · Nacelle/Pylon, Plate/Skin
  > SHIP 3252 DISC: CORROSION RIB 8 REFORCIN PLATE ON RH PYLON. C/A: OMPLIED WITH ER/A 616311-14AD REV. ORIGINAL MATCHES WITH ALL STEPS ON PRI 616311-14AD REV.0 AND PRI 616311-14AD REV.1 IT HASBEEN VALIDATED. PERFORMED REPAIR INSTRUCTIONS ON RH WING RIB 8 AND STRI
- [SDR DALA2024031903445](https://openairdocs.org/sdr/DALA2024031903445.md): Bearing · migrated · Mar 13, 2024 · N352NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3252 DISC: MIGRATED BEARING ON LOWER CONNECTION NEXT TO DOOR STRUCTURE REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA. C/A: 3 CORR BY NOYOLA 00943462 SAL 13MAR24 ATA 5214 RII: Y ENTR 02156330 W REPLACED BEARING ON LOWER CONNECTION NEXT TO DOOR STR
- [SDR DALA2024031903443](https://openairdocs.org/sdr/DALA2024031903443.md): Bearing · migrated · Mar 13, 2024 · N352NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3252 DISC: MIGRATED BEARING ON UPPER AND LOWER CONNECTION LINK FROM SUPPORT ARM OF PASSENGER CREW DOOR 832 REFER TO AMDS CARD 5210-7089-LA RII AT AFT GALLEY AREA. C/A: REPLACED BEARING ON UPPER AND LOWER CONNECTION LINK FROM SUPPORT ARM OF PASSENGER CREW
- [SDR DALA2024031903442](https://openairdocs.org/sdr/DALA2024031903442.md): Shear Tie · not reported · Mar 13, 2024 · N352NW · Airbus A320212 · Fuselage Internal Mounting Structure
  > SHIP 3252 DISC: REPLACE FR43 LH, FRAME FOOT COUPLING BTW STRINGER 18L TO STRINGER 24L IN PASSENGER CABIN (ONLY FOR PORPOSES SDR REPORTABLE CHECK BOX). C/A: REPLACED FR43 LH, FRAME FOOT COUPLING BTW STRINGER 18L TO STRINGER 24L IN PASSENGER CABIN (ONLY FOR PORP
- [SDR DALA2023100208047](https://openairdocs.org/sdr/DALA2023100208047.md): Unknown · unknown · Oct 2, 2023 · N352NW · Airbus A320212 · Landing Gear Position and Warning
  > SHIP 3252 - ATB - DUE TO NOSE GEAR FAILING TO RETRACT. FOUND 24 AND 25GA PROXIMITY SENSOR TARGET MOUNTS LOOSE. CORRECTIVE ACTION: REPLACED NLG STRUT EXTEND PROXIMITY SENSOR TARGET HARDWARE. OPS CHECK GOOD. (4860148)
- [SDR DALA2023092507836](https://openairdocs.org/sdr/DALA2023092507836.md): Unknown · unknown · Sep 24, 2023 · N352NW · Airbus A320212 · Fuel Quantity Indicator
  > SHIP - 3252 - DIV TO SLC DUE TO INTERMITTENT LOSS OF RT FUEL QTY INDICATION AND FUEL QTY DEGRADED ECAM MESSAGE. CORRECTIVE ACTION: DEFERRED RT FUEL QTY INDICATION SYSTEM PER MEL AND CONTINUED. R/R FUEL QTY INDICATING COMPUTER PER AMM 28-42. (4385084)
- [SDR DALA2023083007063](https://openairdocs.org/sdr/DALA2023083007063.md): Unknown · unknown · Aug 29, 2023 · N352NW · Airbus A320212 · Emergency Lighting
  > SHIP 3252 SEAT 29D EXIT PATH LIGHTING BROKEN HANGING. CORRECTIVE ACTION: SECURED LIGHTING ASSY. OK FOR SERVICE. (4516540)
- [SDR DALA2023081606681](https://openairdocs.org/sdr/DALA2023081606681.md): Unknown · unknown · Aug 15, 2023 · N352NW · Airbus A320212 · Leading Edge Slat Control System
  > SHIP 3252 - DIV - TO RIC DUE TO F/CTL SLATS LOCKED ECAM MESSAGE AND WEATHER IN RDU. CORRECTIVE ACTION: PERFORMED SLATS AND FLAPS OPERATIONAL TEST. OPS CHECK GOOD. CONTINUED IN SERVICE. (4398562)
- [SDR DALA2023061204786](https://openairdocs.org/sdr/DALA2023061204786.md): Unknown · unknown · Jun 11, 2023 · N352NW · Airbus A320212 · Landing Gear Brake System
  > SHIP 3252 - ATO - DISCONTINUED TAKE OFF IN MSP AT APPROXIMATELY 10-15KTS DUE TO BRAKES SYS 1 FAULT. CORRECTIVE ACTION: REPLACED BSCU. OPS CHECK GOOD. (LP 9485062)
- [SDR DALA2023052404130](https://openairdocs.org/sdr/DALA2023052404130.md): Unknown · unknown · May 23, 2023 · N352NW · Airbus A320212 · Door Warning System
  > SHIP 3252 ON DECENT, R FWD CABIN DOOR MESSAGE. CORRECTIVE ACTION: FOUND OBSTRUCTION ON R FWD/PAX CREW DOOR HOOK PROX. SW. AND DOOR FRAME. REINSTALLED TRIM AROUND DOOR AS REQUIRED. PERFORMED OPERATIONAL TEST OF THE DOOR WARNING SYSTEM OF R FWD PAX/CREW DOOR PER
- [SDR DALA2023042403167](https://openairdocs.org/sdr/DALA2023042403167.md): Unknown · unknown · Apr 23, 2023 · N352NW · Airbus A320212 · Door Warning System
  > SHIP 3252 AT 3000FT AGL MASTER CAUTION L FWD CABIN DOOR. WENT OUT AFTER 3 SECONDS. OCCURRED AGAIN ON FINAL APPROACH. CORRECTIVE ACTION: CLEANED L1 DOOR SILL AREA. L1 DOOR GND OPS CKD NML. ALL INDICATIONS NML. NO 90 DAYS HISTORY. A/C OK FOR SVC. (4706132)
- [SDR DALA2023032402285](https://openairdocs.org/sdr/DALA2023032402285.md): Unknown · unknown · Mar 23, 2023 · N352NW · Airbus A320212 · Emergency Lighting
  > SHIP 3252 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:21D. CORRECTIVE ACTION: RECONNECTED ELECTRICAL CONNECTOR. OK FOR SERVICE. (2684412)
- [SDR DALA2023012000451](https://openairdocs.org/sdr/DALA2023012000451.md): Light · unsecure · Jan 19, 2023 · N352NW · Airbus A320212 · Emergency Lighting
  > EMERGENCY EXIT PATH LIGHT AT SEAT 24D WAS DAMAGED. SECURED EMERGENCY EXIT PATH LIGHT IAW AMM 33-50.

Next page: https://openairdocs.org/aircraft/N352NW/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 = 'N352NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N352NW/reports

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