# Service difficulty reports: N368NW

A list on [N368NW](https://openairdocs.org/aircraft/N368NW.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 · 197 reports

- [SDR DALA2026081104624](https://openairdocs.org/sdr/DALA2026081104624.md): Brake · binding · Aug 8, 2026 · N368NW · Airbus A320212 · Landing Gear Brake System
  > UPON LDG IN ATL AUTOBRAKES SELECTED LOW. AC TOUCHDOWN AT 2000 APPROACHING 2ND HIGH SPEED TURN OFF AC WAS DOING 100 KTS. MANUAL BRAKES APPLIED TO FURTHER DECEL. UPON MANUAL BRAKING AC VEERED HARD LEFT. FULL RUDDER DEFLECTION WAS INSUFFICIENT. TILLER USED TO MAI
- [SDR DALA2026030801600](https://openairdocs.org/sdr/DALA2026030801600.md): Hose · contaminated · Mar 5, 2026 · N368NW · Airbus A320212 · Air Distribution System
  > STRONG FUMES IN COCKPIT & CABIN AFTER SHUTDOWN AND PARKED AT THE GATE APU OFF AND STILL STRONG SMELL, SUSPECT JETWAY AIR IS BAD. FOUND GROUND AIR HOUSE IS CONTAMINATED AND SENDING BAD AIR TO A/ C. DISCONNECTED GROUND AIR & RUN APU AND PACKS NO MORE STRONG ODE
- [SDR DALA2026020700891](https://openairdocs.org/sdr/DALA2026020700891.md): Oxygen Mask · unwanted deploy · Feb 4, 2026 · N368NW · Airbus A320212 · Passenger Oxygen System
  > OXYGEN MASKS DROPPED AT SEAT 17DEF. RESTOWED THE O2 MASKS AT ROW 17DEF IAW AMM 35-21. ACFT OK FOR SERVICE. (LP: 7700414)
- [SDR DALA2026020600852](https://openairdocs.org/sdr/DALA2026020600852.md): Window Frame · cracked · Feb 1, 2026 · N368NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE RH SIDE POCKET INTERNAL AREA, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 10 O CLOCK, CRACK LENGTH IS 0.115 INCH, AD 2020-17- 03 / WORKCARD 5311-01226 -01. REQUESTING REPAIR DISPOSITION. REPAIR MUST
- [SDR DALA2026020600851](https://openairdocs.org/sdr/DALA2026020600851.md): Window Frame · cracked · Feb 1, 2026 · N368NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE LH SIDE POCKET INTERNAL AREA, FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 O CLOCK, CRACK LENGTH IS 0.095 INCH, AD 2020-17- 03 / WORKCARD 5311-01226 -01. REQUESTING REPAIR DISPOSITION. REPAIR MUST
- [SDR DALA2026020200746](https://openairdocs.org/sdr/DALA2026020200746.md): Window Frame · cracked · Feb 1, 2026 · N368NW · Airbus A320212 · Fuselage Main, Structure
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE RH SIDE POCKET INTERNAL AREA, AT LOWER INBOARD RADIUS, CRACK DIRECTION IS HORIZONTAL, CRACK LENGTH IS 0.375 INCH, AD 2020- 17-03 / WORKCARD 5311-0122 6-01. COMPLIED WITH ER/A 631326-14AD REV. ORIGI
- [SDR DALA2026020200745](https://openairdocs.org/sdr/DALA2026020200745.md): Fitting · not reported · Feb 1, 2026 · N368NW · Airbus A320212 · Fuselage Main, Structure
  > PERFORM ER/A 596680-14AD CONTINUITY FITTINGS LT & RT SIDE REPLACEMENT. COMPLIED WITH ER/A 596680-14AD REV A. MATCHES WITH ALL STEPS ON PRI 596680-14AD REV 0, PRI 596680-14AD REV 1, PRI 596680-14AD REV2 AND PRI 596680-14AD REV 3. STEPS RELATED TO ITEMS OF ER/A
- [SDR DALA2026020600850](https://openairdocs.org/sdr/DALA2026020600850.md): Repair · not entered · Jan 30, 2026 · N368NW · Airbus A320212 · Standard Practices/Structures
  > TIME LIMITED REPAIR ERA 631329-14AD REV ORIGINAL. WINDSHIELD FRAMING CENTER POST MIRROR FITTING REPAIR IS LIMITED TO 53,909 TFC. ACCOMPLISH ERA 631326-14AD SECTION II PRIOR TO 53,909 TFC. CONTACT LIAISON ENGINEERING FOR FURTHER INSTRUCTIONS. ASSOCIATED AA 531
- [SDR DALA2026013000728](https://openairdocs.org/sdr/DALA2026013000728.md): Fitting · out of limits · Jan 26, 2026 · N368NW · Airbus A320212 · Fuselage Main, Structure
  > TIME LIMITED REPAIR ERA 596680-14AD REV A. CONTINUITY FITTING REPLACEMENT IS LIMITED TO 53,909 TFC. ACCOMPLISH ERA 596680-14AD SECTION III PRIOR TO 53,909 TFC. CONTACT LIAISON ENGINEERING FOR THE PERMANENT REPAIR. ASSOCIATED AA 5311-01226 ADDED FOR AC 3268 AS
- [SDR DALA2026012200491](https://openairdocs.org/sdr/DALA2026012200491.md): Dampener · failed · Jan 16, 2026 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > TEST OR PASSENGER DOOR DAMPENER CYLINDER 831 DID NOT PASS. REMOVED DOOR DAMPENER IN UNSERVICEABLE CONDITION ON PASSENGER DOOR 831 IAW AMM 52-11- 14-000-001-B, STEP 3.B, D & STEP 4. (LP: 1405368)
- [SDR DALA2026010500050](https://openairdocs.org/sdr/DALA2026010500050.md): Oxygen Bottle · expired · Jan 4, 2026 · N368NW · Airbus A320212 · Portable Oxygen System
  > EXPIRED DUE DATE HYDROSTATIC TEST OXYGEN BOTTLE IN FWD CLOSET RH AT PASSENGER CABIN. REPLACED OXYGEN BOTTLE IN FWD CLOSET RH AT PASSENGER CABIN AS PER DWG DELTA AIR LINES 25-5429 REV: E ISSUE DATE: 21-JAN-15 SHEET 9 OF 24 ITEM 31 JOB COMPLETE. (LP: 1385818)
- [SDR DALA2026010500049](https://openairdocs.org/sdr/DALA2026010500049.md): Reservoir · out of adjust · Dec 31, 2025 · N368NW · Airbus A320212 · Escape Slide
  > SAFETY HOLE NOT ALIGNED ON RESERVOIR LT SIDE. PERFORMED ADJUSTMENT PROCEDURE TO INSTALL THE LOCK PIN ON THE RESERVOIR LT SIDE IAW AMM 25 -62-00-820-001-A. (LP: 1379088)
- [SDR DALA2025112008496](https://openairdocs.org/sdr/DALA2025112008496.md): Anchor · damaged · Nov 18, 2025 · N368NW · Airbus A320212 · Wing, Landing Gear Attach Fittings
  > REMOVED 3 NUTS FROM LT MLG RETRACT ACTUATOR MOUNT REMOVED 2 REMAINDER NUTS FROM RETRACT ACTUATOR MOUNT PLATE. REMOVED AND REPLACED LT MLG JACK ANCHORAGE ASSY PER ER/A 630497- 14, REV ORIG PER SECTION I PERMANENT REPAIR INSTRUCTIONS; REFER TO L.P 1309462. (LP:
- [SDR DALA2025112008495](https://openairdocs.org/sdr/DALA2025112008495.md): Not Reported · damaged · Nov 18, 2025 · N368NW · Airbus A320212 · Wing Main, Frame Structure
  > WORKING PRI ER/A 630497 REV "O". ACCOMPLISHED ALL REPAIR INSTRUCTIONS PRE PRI ER/A 630497 REV "O" PRI REVISIONS 1-4. FINAL ER/A 630497 REV. ORIGINAL SECTION I: PERMANENT REPAIR INSTRUCTIONS MATCH. (LP: 1309501)
- [SDR DALA2025112008492](https://openairdocs.org/sdr/DALA2025112008492.md): Threshold · none · Nov 18, 2025 · N368NW · Airbus A320212 · Standard Practices/Structures
  > NEW INSPECTION THRESHOLD REQUIRED PER ER/A 563946-14 REV B. THIS LOG PAGE SUPERSEDES LOG PAGE 0565626 PER ER/A 563946-14 REV B. DTE STAGE 2 AND 3 REQUIRED. ACCOMPLISH INSPECTION PER ER/A 563946-14 REV B PRIOR TO SIXTY-FOUR THOUSAND TWO HUNDRED (64,200) TOTAL
- [SDR DALA2025111808414](https://openairdocs.org/sdr/DALA2025111808414.md): Hinge · corroded · Nov 18, 2025 · N368NW · Airbus A320212 · Landing Gear Doors
  > FOUND CORROSION ON LT MLG ACTUATING CYLINDER INBOARD HINGE. COMPLIED WITH ER/A 630497- 14. (1309462).
- [SDR DALA2025092206898](https://openairdocs.org/sdr/DALA2025092206898.md): Bottle · low pressure · Sep 20, 2025 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > L2 DOOR EMERGENCY OPERATING CYLINDER/ACCUMULATOR PRESSURE LOW. SERVICED L2 DOOR EMERGENCY CYLINDER/ACCUMULATOR PRESSURE PER A320 AMM TASK 52-10-00-610-881C1. LEAK CHECK GOOD. A/C OK FOR SVC. (LP: 7342882)
- [SDR DALA2025071705369](https://openairdocs.org/sdr/DALA2025071705369.md): Bottle · low pressure · Jul 15, 2025 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3268 DISC: L2 DOOR OPEN ASSIST BOTTLE PRESSURE LOW. C/A: SERVICED L2 DOOR OPEN ASSIST BOTTLE PER A320 AMM 52-10-00-610- 801C1. FOUND FILLING VALVE LEAKING. R/R FILLING VALVE SEAL PER A320 CMM 5-11-05. SERVICED DOOR OPEN ASSIST BOTTLE. NO LEAKS NOTED. OK F
- [SDR DALA2025070104937](https://openairdocs.org/sdr/DALA2025070104937.md): Wire · pulled · Jun 30, 2025 · N368NW · Airbus A320212 · Light System Wiring
  > SHIP 3268 DISC: EMERGENCY CLEAR PATHWAY LIGHT AT ROW 32DEF INOP. C/A: FOUND WIRES FOR ROW 32DEF ESCAPE PATHWAY LIGHTING PULLED FROM ITS SPLICE UNDER THE SEAT TRACK COVERS BEHIND ROW 33DEF. REPLACED SPLICE AND CRIMPED NEW CONTACTS REF. A320 ESPM 20-43-13. OPS
- [SDR DALA2025042403199](https://openairdocs.org/sdr/DALA2025042403199.md): Linkage · lack of lube · Apr 20, 2025 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3268 L1 MAIN CABIN WAS DIFFICULT TO OPEN GATE AGENT LATCHED AND UNLATCHED SEVERAL TIMES BEFORE IT OPENED. CCYCLED L-1 DOOR FOUND TO OPEN NORMAL FROM INSIDE AND STIFF FROM OUTSIDE CLEANED AND LUBED OUTSIDE LINKAGE DOOR OPS NORMAL PER A-320 AMM 52-11 A/C OK
- [SDR DALA2025042103043](https://openairdocs.org/sdr/DALA2025042103043.md): Oxygen Mask · unwanted deploy · Apr 18, 2025 · N368NW · Airbus A320212 · Passenger Oxygen System
  > AFTER LANDING FA REPORTS CREW O2 MASK DEPLOYED IN AFT GALLEY. STOWED O2 MASK IN AFT GALLEY IAW A320 AMM 35-21. SECURITY CHECK GOOD. (LP: 7245446)
- [SDR DALA2024101710172](https://openairdocs.org/sdr/DALA2024101710172.md): Idg · faulty · Oct 15, 2024 · N368NW · Airbus A320212 · AC Generator-Alternator
  > SHIP 3268 - ATO - AT 60 KNOTS DUE TO ELEC IDG 2 OIL LO PR ECAM MESSAGE. CORRECTIVE ACTION: MAINTENANCE STILL IN PROGRESS. (LP: 6639004)
- [SDR DALA2024090808792](https://openairdocs.org/sdr/DALA2024090808792.md): Flange · cracked · Sep 3, 2024 · N368NW · Airbus A320212 · Fuselage Main, Attach Fittings
  > SHIP 3268 DISC: SB 53-1491 - S18 REAR FUSELAGE, FR68RH HORIZONTAL FLANGE FILLET RADIUS AT STR22RH - CRACK. ER/A 616556-14AD REV A REQUIRES SECTION II FOLLOW-ON INSPECTIONS FOR CONTINUED AIRCRAFT AIRWORTHINESS. C/A: ER/A 616556-14AD REV A SECTION II FOLLOW-ON I
- [SDR DALA2024070406747](https://openairdocs.org/sdr/DALA2024070406747.md): Indication Sys · faulted · Jun 29, 2024 · N368NW · Airbus A320212 · Fuel Indicating System
  > ATB - DUE TO FUEL QUANTITY INDICATION DISCREPANCIES. R/R FQIC. OPS CHECK GOOD.
- [SDR DALA2024060205724](https://openairdocs.org/sdr/DALA2024060205724.md): Unknown · odor · May 30, 2024 · N368NW · Airbus A320212 · Air Distribution System
  > SHIP 3268 DISC: DIRTY SOCK SMELL WITH PACKS ON AND APU BLEED ON. SMELL GOT BETTER WITH PACKS TURNED OFF. C/A: C/W WORKCARD 0550-2002 STEPS 1-4 TMOYER 977572 REMOVED AND REPLACED BOTH RECIRC FILTERS PER A320 AMM 21-21 TMOYER 977572. C /W W/C 2100-2005 STEPS 1-6
- [SDR DALA2024040203983](https://openairdocs.org/sdr/DALA2024040203983.md): Oxygen Mask · unwanted deploy · Mar 27, 2024 · N368NW · Airbus A320212 · Passenger Oxygen System
  > SHIP 3268 DISC: OXYGEN PANEL MASK DEPLOYED / LOCATIONS:101. C/A: RE PACKED R1 DOOR OXYGEN PANEL PER A320 AMM 35-21. A/C OK FOR SVC. (LP: 0265252)
- [SDR DALA2024090808793](https://openairdocs.org/sdr/DALA2024090808793.md): Unknown · unknown · Mar 19, 2024 · N368NW · Airbus A320212 · Fuselage Structure (General)
  > SHIP 3268 DISC: DTE ERA 616556-14. REPAIR PER ERA 616556-14AD REQUIRES DTE. C/A: PER ER/A 616556-14AD REV A, DTE STAGE 2 ACCOMPLISHED. DTE STAGE 3 IS TRACKED ON NEW LOG PAGES 0537276, 0537285, AND 0537291. PLEASE CLOSE THIS LOG PAGE, 0252606. (LP: 0252606)
- [SDR DALA2024032103595](https://openairdocs.org/sdr/DALA2024032103595.md): Frame · cracked · Mar 19, 2024 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > R/H FR.68 STGR.22, FRAME WEB HORIZONTAL FLANGE LOWER SURFACE RADIUS CRACKED APROX' 1.5 INCH IN LENTHG AT I/B SIDE REQUESTING REPAIR DISPOSITION ADITIONAL ENGENIRING DOCUMENTATION IS REQUIRED. C/A: C/W ALLSTEPS OF PRI 616556-14AD REVD AWAITING ENGINEERING C/W A
- [SDR DALA2023120710043](https://openairdocs.org/sdr/DALA2023120710043.md): Unknown · unknown · Dec 5, 2023 · N368NW · Airbus A320212 · Life Raft
  > SHIP 3268 DISC: LIFE RAFT IN OVERHEAD BIN AT ROW 32 HAS A LOOSE CORD. C/A: SECURED CORD RAFT OK FOR SERVICE. (LP 5019872)
- [SDR DALA2023101108335](https://openairdocs.org/sdr/DALA2023101108335.md): Unknown · unknown · Oct 6, 2023 · N368NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > SHIP 3268 - SMKE - DUE TO STRONG SMELL IN THE CABIN AND COCKPIT, AND BLACK SMOKE COMING FROM ENGINE #1. CORRECTIVE ACTION: FOUND EVIDENCE OF BIRD STRIKE ON ENGINE #1. REPLACED # 1 ENGINE PER AMDS WORK CARD 2100-2004. OK FOR SERVICE. (4383582)
- [SDR DALA2023072105891](https://openairdocs.org/sdr/DALA2023072105891.md): Unknown · unknown · Jul 21, 2023 · N368NW · Airbus A320212 · Emergency Lighting
  > SHIP 3268 EMERGENCY LIGHTS AT SEATS 1&2 DC INOP. CORRECTIVE ACTION: FOUND BROKEN WIRE AT CONNECTOR 9150VC. RETERMINATED WIRE PER A320 ESPM 20-44-12; A320 AWM 33-51-06. OPS CHK GOOD. (9651398)
- [SDR DALA2023051003671](https://openairdocs.org/sdr/DALA2023051003671.md): Unknown · unknown · May 9, 2023 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3268 L1 DOOR DIFFICULT TO CLOSE. CORRECTIVE ACTION: REPLACED UPPER HINGE AND BEARING ASSY PER A320 SRM 51-71-11. RIG AND OPS CHECK GOOD. (9956992)
- [SDR DALA2023021501198](https://openairdocs.org/sdr/DALA2023021501198.md): None · none · Feb 15, 2023 · N368NW · Airbus A320212 · Door Warning System
  > SHIP 3268 L1 DOOR LIGHT SHOWS DOOR IS OPEN WHEN IT IS CLOSED. CORRECTIVE ACTION: READJUSTED AND CYCLED DOOR. OPS CHECK GOOD. (9499404)
- [SDR DALA2022093006406](https://openairdocs.org/sdr/DALA2022093006406.md): None · none · Sep 21, 2022 · N368NW · Airbus A320212 · Flight Compartment Windows
  > SHIP 3268 - ATO - DUE TO BIRD STRIKE AND CRACKED F/O WINDSHIELD. CORRECTIVE ACTION: REPLACED F/O FIXED WINDSHIELD PER A320 AMM 56-11. OK FOR SERVICE. (8954583)
- [SDR DALA2022030701466](https://openairdocs.org/sdr/DALA2022030701466.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Rudder Control System
  > SHIP 3268 CHAFING MECHANICAL CONTROL CABLE LEFT OF RUDDER AT FR 70 LEVEL OF STR 23 AND Y512 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED RUDDER CONTROL CABLE A320 FAM AMM 27-21-61. (2144134)
- [SDR DALA2022030701462](https://openairdocs.org/sdr/DALA2022030701462.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 CRACK INDICATION ON FRAME 20 LH SIDE CROSSBEAM SPLICING AREA AT OPEN FASTENER HOLE H26. CORRECTIVE ACTION: COMPLIED WITH 596951-14AD REV 1. (2144126)
- [SDR DALA2022030701461](https://openairdocs.org/sdr/DALA2022030701461.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 CRACK INDICATION ON FRAME 16 RH SIDE CROSSBEAM SPLICING AREA AT OPEN FASTENER HOLE H8. CORRECTIVE ACTION: COMPLETED WITH ERA 596939-14AD REV.ORIGINAL. (2143742)
- [SDR DALA2022030701460](https://openairdocs.org/sdr/DALA2022030701460.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 CRACK INDICATION FOUND IN HOLE C LOCATED AT FR 16 RH SIDE AT LEVEL OF DOOR STOP 7. CORRECTIVE ACTION: COMPLIED WITH ER/A 588153-14AD REV A. (2143398)
- [SDR DALA2022030701453](https://openairdocs.org/sdr/DALA2022030701453.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Wing, Center Box
  > SHIP 3268 CORROSION MLG BAY ON MID BEAM LOWER SURFACE ZONE 671 ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 597464-14 REV.ORIGINAL. (2144133)
- [SDR DALA2022030701452](https://openairdocs.org/sdr/DALA2022030701452.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 CRACK INDICATION WAS FOUND IN CONTINUITY FITTING RH SIDE LOCATED ON FRAME 2 IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 596680-14AD REV ORIGINAL. (2144129)
- [SDR DALA2022030701451](https://openairdocs.org/sdr/DALA2022030701451.md): None · none · Mar 4, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 CRACK INDICATION WAS FOUND IN CONTINUITY FITTING LH SIDE LOCATED ON FRAME 2 IN COCKPIT. CORRECTIVE ACTION: COMPLIED WITH ER/A 596680-14 REV ORIGINAL. (2144118)
- [SDR DALA2023010500072](https://openairdocs.org/sdr/DALA2023010500072.md): Skin · damaged · Mar 3, 2022 · N368NW · Airbus A320212 · Wing, Plate/Skin
  > ELONGATED HOLE CUT-OUT STRUCTURE BWT RIB 14 AND RIB 15 FUEL TANK ON LH WING. CORRECTIVE ACTION: REPAIRED PER A320 SRM 57-21-11-300-002. (2142880)
- [SDR DALA2022030401380](https://openairdocs.org/sdr/DALA2022030401380.md): None · none · Mar 3, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 DURING M2 AT SAL AND WHILE MODIFYING PER EM 5311-01221-04, A CRACK WAS FOUND IN HOLE H8 OF CROSSBEAM SPLICE JUNCTION AT FR16 RHS. CORRECTIVE ACTION: COMPLIED WITH ERA 596939-14AD. (2142906)
- [SDR DALA2022030401379](https://openairdocs.org/sdr/DALA2022030401379.md): None · none · Mar 3, 2022 · N368NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3268 CORROSION FLOOR BEAM -Y1292 LOCATED BTW FR 64 TO FR 66 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11 AND 51-72-11. (2142917)
- [SDR DALA2022030401377](https://openairdocs.org/sdr/DALA2022030401377.md): None · none · Mar 3, 2022 · N368NW · Airbus A320212 · Service Doors
  > SHIP 3268 DENT ACCESS DOOR 314AR EDGE DURING LOWERING AIRCRAFT PROCEDURES IN THS COMPARTMENT. CORRECTIVE ACTION: REPLACED OB SKIN ON ACCESS DOOR 314AR PER A320 SRM 51-72-11. (2142804)
- [SDR DALA2022030301347](https://openairdocs.org/sdr/DALA2022030301347.md): None · none · Mar 2, 2022 · N368NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3268 CORROSION STRINGER 41R LOCATED BTW FR30 TO FR34 IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER PER A320 SRM 51-72-11. (2141497)
- [SDR DALA2022030301346](https://openairdocs.org/sdr/DALA2022030301346.md): None · none · Mar 2, 2022 · N368NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3268 BENT FLOOR STRUCTURE CROSS BEAM LOCATED FR33 BTW STR 38L TO STR 38R IN FWD CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED CROSSBEAM PER SRM A320 51-42-11 AND 51-72-11. (2141496)
- [SDR DALA2022030201335](https://openairdocs.org/sdr/DALA2022030201335.md): None · none · Mar 1, 2022 · N368NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3268 IMPROPERLY INSTALLED PASSENGER CREW DOOR 831 TELESCOPIC ROD ON DOOR FITTING. CORRECTIVE ACTION: R/R AND RIG TELESCOPIC ROD PER A320 AMM 52-11-14. OK FOR SERVICE. (2140123)
- [SDR DALA2022030101279](https://openairdocs.org/sdr/DALA2022030101279.md): None · none · Feb 28, 2022 · N368NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3268 DURING ACCOMPLISHMENT OF 5311-01221 (SB A320-53-1295) A CRACK WAS FOUND IN HOLE 26 AT CROSSBEAM SPLICING FR20 LHS. CORRECTIVE ACTION: COMPLIED WITH ERA 32-596951. (2138882)
- [SDR DALA2022030101277](https://openairdocs.org/sdr/DALA2022030101277.md): None · none · Feb 28, 2022 · N368NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3268 FABRICATE FLOOR BEAM -Y1292 LOC. BTW FR64 TO FR66 (1E/A). AT AFT GALLEY AREA DUE TO CORROSION. CORRECTIVE ACTION: FABRICATED AND INSTALLED FLOOR BEAM PER ERA 597140-14 REV ORIGINAL. OK FOR SERVICE. (2138937)

Next page: https://openairdocs.org/aircraft/N368NW/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 = 'N368NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N368NW/reports

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