# Service difficulty reports: N361NW

A list on [N361NW](https://openairdocs.org/aircraft/N361NW.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 3 · 126 reports

- [SDR DALA2026100705553](https://openairdocs.org/sdr/DALA2026100705553.md): Light · detached · Oct 5, 2026 · N361NW · Airbus A320212 · Emergency Lighting
  > FLOOR PROXIMITY EMERGENCY LIGHT ATTACHED TO SEAT 30D WAS DETACHED FROM UNDER THE SEAT. SECURED THE EMERGENCY LIGHTING. CHKD GOOD. IAW AMM 33-52. (LP: 8963817, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026072304302](https://openairdocs.org/sdr/DALA2026072304302.md): Alternator · detached · Jul 21, 2026 · N361NW · Airbus A320212 · Accessory Gearboxes
  > RETURNED TO DTW DUE TO LOSS OF NBR 2 ENGINE OIL QUANTITY AND PRESSURE. CREW SHUT ENGINE DOWN WHEN QUANTITY AND PRESSURE WENT TO ZERO. MTC FOUND ENGINE CONTROL ALTERNATOR DETACHED FROM AGB MOUNTING PAD. MAINTENANCE IN PROGRESS. (LP: 8844868. AIRCRAFT WAS GROU
- [SDR DALA2026060703412](https://openairdocs.org/sdr/DALA2026060703412.md): Engine · making metal · Jun 5, 2026 · N361NW · Airbus A320212 · Engine (Turbine/Turboprop)
  > RETURNED TO MSP DUE TO REPORT OF #2 ENGINE EGT OVERLIMIT. METAL FOUND IN TAILPIPE, ENGINE CHANGE REQUIRED. (LP: 8940774, AIRCRAFT WAS GROUNDED.)
- [SDR DALA2026011700398](https://openairdocs.org/sdr/DALA2026011700398.md): Unknown · smoke · Jan 16, 2026 · N361NW · Airbus A320212 · Air Distribution System
  > CREW REPORTED SMOKE AND FUMES IN THE AFT CABIN DURING LANDING ROLL OUT. SMOKE DISSIPATED QUICKLY. NO TROUBLE FOUND. PERFORMED NO-GO ECS DECONTAMINATION. EVENT WAS POSSIBLY CAUSED BY RUNWAY TREATMENT CONTAMINATION. (LP: 7729026)
- [SDR DALA2026011700399](https://openairdocs.org/sdr/DALA2026011700399.md): Door · open · Jan 12, 2026 · N361NW · Airbus A320212 · Passenger Oxygen System
  > DURING BOARDING, OVERHEAD PANEL IN ROW 23ABC WHICH SERCURES PAX O2 MASK FELL DOWN. DEFERRED SEAT ROW 23ABC O2 MASK PER A320 MEL 35-21-01B. M PROCEDURES C/W PLACARD INSTALLED. R & R OVERHEAD O2 PANEL PER CMM 25-28-02. DOOR STAYS CLOSED. PERFORMED OPS CHECK PER
- [SDR DALA2025112008494](https://openairdocs.org/sdr/DALA2025112008494.md): None · none · Nov 18, 2025 · N361NW · Airbus A320212 · Standard Practices/Structures
  > ER/A 543344-14 REV A REQUIRES NEW INSPECTIONS. LOGPAGE 2378650 WILL BE CLOSED AND NO LONGER WILL TRACK THE REPAIR PER ER/A 543344-14 REV ORIGINAL. THIS LOG WILL TRACK THE REQUIREMENTS PER ER/A 543344-14 REV A. NEW INSPECTIONS REQUIRED PER ERA 543344-14 REV A
- [SDR DALA2025112008493](https://openairdocs.org/sdr/DALA2025112008493.md): Not Reported · none · Nov 18, 2025 · N361NW · Airbus A320212 · Standard Practices/Structures
  > ER/A 543343-14 REV A REQUIRES NEW INSPECTIONS. NEW INSPECTIONS REQUIRED PER ERA 543343-14 REV A STARTING AT 39,000 TFC AND EVERY 1,600 FC THEREAFTER. LOGPAGE 2378641 WILL BE CLOSED AND NO LONGER WILL TRACK THE REPAIR PER ER/A 543343-14 REV ORIGINAL. THIS LOG
- [SDR DALA2025120308812](https://openairdocs.org/sdr/DALA2025120308812.md): Retainer · corroded · Nov 12, 2025 · N361NW · Airbus A320212 · Buffet/Galleys
  > CORROSION ON LOWER TROLLEY RETAINER BLOCKS ON GALLEY G1 AT FWD GALLEY AREA. COMPLIED WITH ERA 630077-14 REV. ORIGINAL APPROVED DATE: 07-NOV- 25 MATCHES WITH ALL STEPS ON ERA 630077-14 REV. ORIGINAL, PRI REV0 AND PRI REV.1, IT HAS BEEN VALIDATED, PERFORMED REP
- [SDR DALA2025111308312](https://openairdocs.org/sdr/DALA2025111308312.md): Elec Connector · corroded · Nov 9, 2025 · N361NW · Airbus A320212 · Communications System Wiring
  > CORROSION ON ELECTRICAL CONECTOR W311 OF VIASAT ANTENNA LOC ON UPPER FUSELAGE. REMOVED VIASAT ANTENNA GM40 P/N: 1196634-004 S/N: 50204- GM4042641 ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 44-31- 02-000-801C2 STEP 2.C(1)AND STEP 3.A(4)(6)(8) DUE TO CORROS
- [SDR DALA2025111108221](https://openairdocs.org/sdr/DALA2025111108221.md): Skin · corroded · Nov 9, 2025 · N361NW · Airbus A320212 · Wing, Plate/Skin
  > CORROSION BOTTON SKIN LOWER SURFACE ON PYLON REINFORCING PLATE BTW RIB 7 AND RIB 8 AT STR 6, LT WING. COMPLIED WITH ER/A 630034-14AD REV.ORIGINAL MATCHES WITH ALL STEPS ON ER/A 630034-14AD PRI REV.0 AND ER/A 630034-14AD PRI REV.1IT HAS BEEN VALIDATED. PERFO
- [SDR DALA2025110908150](https://openairdocs.org/sdr/DALA2025110908150.md): None · none · Nov 8, 2025 · N361NW · Airbus A320212 · Standard Practices/Structures
  > DTE ERA 630034-14AD REVISION ORIGINAL. REPAIR PER ERA 630034- 14AD SECTION I IS TIME LIMITED REQUIRING DTE FOLLOW UP PRIOR TO 97,447 TFC OR 198,940 TFH, WHICHEVER COMES FIRST. REVISE AND UPDATE ERA 630034-14AD WITH DTE RESULTS PRIOR TO 97,447 TFC OR 198,940 T
- [SDR DALA2025110408058](https://openairdocs.org/sdr/DALA2025110408058.md): Strut · corroded · Nov 2, 2025 · N361NW · Airbus A320212 · Trailing Edge Flaps
  > CORROSION ON INTERCONNECTING STRUT OB FLAP ON RH WING. REMOVED INTERCONNECTING STRUT RH WING UNSERVICEABLE CONDITION P/ N D5757032201100 S/N 02507 AS PER A320 FAM AMM 27-51-44-000-001- A STEP 1 THRU 4.A EXCEPT STEP 3.D(2). JOB IN PROGRESS. REPLACED INTERCONNE
- [SDR DALA2025110408057](https://openairdocs.org/sdr/DALA2025110408057.md): Strut · corroded · Nov 2, 2025 · N361NW · Airbus A320212 · Trailing Edge Flaps
  > SHIP 3261 DISC: CORROSION INTERCONNECTING STRUT OB FLAP ON LH WING. C/A: REMOVED INTERCONNECTING STRUT LH WING UNSERVICEABLE CONDITION P/ N D5757032201100 S/N 2285 AS PER A320 FAM AMM 27-51-44-000-001-A STEP 1 THRU 4.A EXCEPT STEP 3.D(2). JOB IN PROGRESS. REPL
- [SDR DALA2025080105791](https://openairdocs.org/sdr/DALA2025080105791.md): Unknown · odor · Jul 29, 2025 · N361NW · Airbus A320212 · Air Distribution System
  > FLIGHT ATTENDANT REPORTED POSSIBLE DIRTY SOCK SMELL AT MID CABIN DURING DESCENT. THEN REPORTED IT WAS GONE, BUT CAME BACK DURING LANDING. NO SMELL OR ODOR IN FLIGHT DECK. REF LOG PAGE 1112138 FOR CORRECTIVE ACTION.
- [SDR DALA2025072905704](https://openairdocs.org/sdr/DALA2025072905704.md): Oil System · leaking · Jul 28, 2025 · N361NW · Airbus A320212 · APU Oil System
  > SHIP 3261 DIRTY SOCK ODOR DETECTED WHEN CATERING AIRCRAFT. BEGAN INSPECTION PER TASK CARD 4900-2001, STEPS 1 & 2 COMPLETED. COMPLIED WITH STEP A, DEBRIEF FLIGHT CREW & ENSURE THE LOD PAGE IN ACCURATE. COMPLIED STEP B. COMPLIED WITH STEP C; ENSURE THE ELEC S
- [SDR DALA2025032302159](https://openairdocs.org/sdr/DALA2025032302159.md): Unknown · odor · Mar 23, 2025 · N361NW · Airbus A320212 · Air Distribution System
  > SHIP 3261 DISC: F/A REPORTED ACETONE SMELL COMING FROM ROW 17-18 COULD NOT ISOLATE SMELL WAS GETTING WORSE DIVERTED TO RAP. C/A: TROUBLESHOT PER A320 TSM 05-50-00-810-831-A. DETERMINED ODOR TO BE A TYPE 10 PER THE TSM. ODOR CLEARED AFTER PASSENGER BAGS WERE RE
- [SDR DALA2024081308061](https://openairdocs.org/sdr/DALA2024081308061.md): Rib · damaged · Aug 9, 2024 · N361NW · Airbus A320212 · Horizontal Stabilizer, Spar/Rib
  > SHIP 3261 DISC: RH HORIZONTAL DAMAGED ON RIB 14 WEB AND END BRACKET. C/A: REMOVED DAMAGED WEB AND END BRACKET PER A320SRM 51-42-21 (925483) C/W PRI 619934-14 REV 0 (925483)(QC4080) C/W PRI 619934-14 REV 1(984172) (QC 1440) C/WSTEPS 1-6 OF ERA 619934-14 REV OR
- [SDR DALA2024081308060](https://openairdocs.org/sdr/DALA2024081308060.md): Skin · damaged · Aug 9, 2024 · N361NW · Airbus A320212 · Horizontal Stabilizer, Plate/Skin
  > SHIP 3261 DISC: RH HORIZONTAL DAMAGED ON TRAILING OB EDGE UPPER AND LOWER SKIN CORNERS. C/W PRI 619808-14 REV 0 C/W PRI 619808-14 REV 1 C/W PRI 619808-14 REV 2 AND 3 C/W PRI 619808-14 REV 4 C/W PRI 619808- 14 REV 5 C/W PRI 619808-14 REV 6 C/W ERA 6
- [SDR DALA2024081308059](https://openairdocs.org/sdr/DALA2024081308059.md): Unknown · unknown · Aug 8, 2024 · N361NW · Airbus A320212 · Horizontal Stabilizer Structure
  > SHIP 3261 DISC: C/W ERA 619847-14 REV ORIGINAL RH STABILIZER AND SURROUNDING AREA INSPECTIONS. C/A: C/W PRI 619847-14 REV 0. (890669) VERIFIED ALL RII STEPS OF PRI 629847-14 REV 0. C/W PRI 619847-14 REV 1 VERIFIED ALL RII STEPS OF PRI 619847-14 REV 1 COMPLETED
- [SDR DALA2024081308058](https://openairdocs.org/sdr/DALA2024081308058.md): Support · damaged · Aug 8, 2024 · N361NW · Airbus A320212 · Horizontal Stabilizer Miscellaneous Structure
  > SHIP 3261 DISC: THE TOP SUPPORT WEBS OF THE LT AND RT LOWER THS ACTUATOR MOUNTING ARMS ARE DAMAGED AT THE I/B, UPPER EDGES, FWD OF THE H. STAB SPLICE PLATE. C/A: C/W PRI 619935-14 REV 0 (417296) (QC5352)(484068) C/W ERA 619935 -14 REV ORIG. CONFIRMED ALL PRI R
- [SDR DALA2024081107984](https://openairdocs.org/sdr/DALA2024081107984.md): Stabilizer · ground damage · Aug 7, 2024 · N361NW · Airbus A320212 · Horizontal Stabilizer Structure
  > SHIP 3261 DISC: AC WING HIT OUR HORIZONTAL STABILIZER. C/A: WORKING W/C 2734-4001-RT COMPLIED WITH STEP 1 BULLET POINT K3 WILL REQ CONTINUING K4 AND REST (341468) CONTINUED WITH ELEVATOR REMOVAL PER A320 WORKCARD 2734-4001-RT THRU STEP 5.(859799) RT ELEV REMOV
- [SDR DALA2024072907532](https://openairdocs.org/sdr/DALA2024072907532.md): Flap System · malfunctioned · Jul 25, 2024 · N361NW · Airbus A320212 · Trailing Edge Flap Control System
  > SHIP 3261 ON ARRIVAL, SLOWING FROM 210 KTS TO 180KTS, FLAPS WERE SELECTED FROM POSITION 1 TO 2 AND THE AIRCRAFT BEGAN TO IMMEDIATELY ROLL TO THE RIGHT. AUTOPILOT WAS ENGAGED AND COULD NOT CORRECT COURSE FOR ABOUT 10-15 SECONDS, AND 20-30 SECONDS BEFORE AIRCRAF
- [SDR DALA2024062706534](https://openairdocs.org/sdr/DALA2024062706534.md): Unknown · odor · Jun 26, 2024 · N361NW · Airbus A320212 · Air Distribution System
  > SHIP 3261 DISC: DIRTY SOCK SMELL IN COCKPIT- DONNED O2- RETURNED TO GATE. C/A: INSPECTED APU COMPARTMENT IAW WC# 0550-2002. NO DEFECTS OR CONTAMINATION FOUND. C/W WORKCARD# 7900-2001. ENGINE OIL FUMES ODOR FOR #1 ENG. AND WORKCARD# 2100-2007. ALL CHECKED GOOD
- [SDR DALA2024051505247](https://openairdocs.org/sdr/DALA2024051505247.md): Ground Wire · loose · May 12, 2024 · N361NW · Airbus A320212 · Light System Wiring
  > 11D EMERGENCY LIGHTS NOT WORKING. OK TO DEFER THE EMERGENCY LIGHT ON THE SEAT TRIM OF LLD TO A320 MEL 33-50-03A, MEL AND PLACARD INSTALLED. NO "M" PROCEDURES TO C /W. MCC NOTIFIED. FOUND POWER & GROUND WIRES GOING INTO LIGHT DISCONNECTED & LOOSE. RESECURED P
- [SDR DALA2024020901759](https://openairdocs.org/sdr/DALA2024020901759.md): Vertical Beam · cracked · Feb 7, 2024 · N361NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3261 DISC: FWD AVIONICS BAY, AT FR-1, TOP OF VERTICLE POST AT R/H Y-330 HAS 1.5 IN CRACK. SEEN ON O/B SIDE. REF BY AIRBORNE/PEMCO NR.15017.111. C/A: C/W STEPS 1-3 OF PRI615368-14 REV 0 EA HOLE CRACKED AWATING ENGINEERING P108 1604328 Q951 516209 C/W ALL
- [SDR DALA2024020801681](https://openairdocs.org/sdr/DALA2024020801681.md): Vertical Beam · damaged · Feb 6, 2024 · N361NW · Airbus A320212 · Fuselage Main, Bulkhead
  > SHIP 3261 DISC: STAGE II/III DAMAGE TOLERANCE EVALUATION REQUIRED FOR REPAIR INS TALLED AT FR1 BULKHEAD VERTICAL POST. FOLLOW ON ACTION IS REQUIR ED AS PER ER/A 615368-14. C/A: ER/A 615368-14 TO BE REVISED WITH UP-ISSUE STAGE II/III APPROVAL PRIOR TO 6 MONTH (
- [SDR DALA2024010800210](https://openairdocs.org/sdr/DALA2024010800210.md): Anti-Ice System · failed · Jan 6, 2024 · N361NW · Airbus A320212 · Airfoil Anti/De-ice System
  > DIVERTED TO CVG DUE TO FAILURE OF RT WING ANTI-ICE. CORRECTIVE ACTION: DEFERRED WING ANTI-ICE PER MEL. LATER REPLACED THE RT WING ANTI-ICE CONTROL RELAY 5DL.
- [SDR DALA2023122410553](https://openairdocs.org/sdr/DALA2023122410553.md): Unknown · unknown · Dec 23, 2023 · N361NW · Airbus A320212 · Aerodynamic Fairings
  > SHIP 3261 DISC: CREW REPORTS WTB FAIRING 191DT MISSING ON WALKAROUND. C/A: REMOVED PANEL 191DT PER A320 AMM 53-35-11(840719) UPON INSPECTION FOUND WINDOW BETWEEN FR 44L AND FR43L GOUGED. REMOVED WINDOW PER A320 AMM 56-21-13(845719). REPLACED WINDOW PER A320 AM
- [SDR DALA2023122410552](https://openairdocs.org/sdr/DALA2023122410552.md): Unknown · unknown · Dec 22, 2023 · N361NW · Airbus A320212 · Light System Wiring
  > SHIP 3261 DISC: LT OVERWING EMERGENCY LIGHTS FOR ESCAPE SLIDE INOP. C/A: INSTALLED LT FWD SLIDE ESCAPE LIGHT CANNON PLUG CONNECTOR PER A320 AWM 33-51-04 AND A320 ESPM 20-48-21. (LP: 5089161)
- [SDR DALA2022030301363](https://openairdocs.org/sdr/DALA2022030301363.md): None · none · Mar 2, 2022 · N361NW · Airbus A320212 · Extinguishing System
  > SHIP 3261 DURING FIRE TEST FOR NBR 1 ENGINE AGENT 1 SQUIB WILL NOT TEST. CORRECTIVE ACTION: RESEATED CANNON PLUG ON NBR 1 ENG NBR 1 FIRE BOTTLE SQUIB PER A320 AMM 26-21. TESTS OK. (8236148)
- [SDR DALA2022021601015](https://openairdocs.org/sdr/DALA2022021601015.md): None · none · Feb 15, 2022 · N361NW · Airbus A320212 · Passenger/Crew Doors
  > SHIP 3261 LH AFT PASSENGER/CREW DOOR HAS DAMAGE TO LOWER DOOR SKIN. CORRECTIVE ACTION: REMOVED DAMAGE ON LH AFT PASSENGER/CREW DOOR AT LOWER SKIN EDGE. OK FOR SERVICE. CONTINUE ON MON. (2122757)
- [SDR DALA2022020800829](https://openairdocs.org/sdr/DALA2022020800829.md): None · none · Feb 7, 2022 · N361NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3261 MAIN CABIN FR70 STR23 SEALING ANGLE ASSY IS CORRODED. CORRECTIVE ACTION: REPAIRED PER ER/A 597015-14 REV ORGINAL. (2113713)
- [SDR DALA2022020800819](https://openairdocs.org/sdr/DALA2022020800819.md): None · none · Feb 7, 2022 · N361NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3261 CRACK IN NEED OF REPAIR PER AMDS 5311-01239-01B WORKCARD. CORRECTIVE ACTION: REPAIRED PER DELTA WORK CARD. OK FOR SERVICE. (2113647)
- [SDR DALA2022020400715](https://openairdocs.org/sdr/DALA2022020400715.md): None · none · Feb 3, 2022 · N361NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3261 AFT MAIN CABIN FLOORBEAM Y765 FRAME 68 STR23LH HAS CORROSION. CORRECTIVE ACTION: COMPLIED WITH ERA 596592-14 REV O. (2109232)
- [SDR DALA2022020400714](https://openairdocs.org/sdr/DALA2022020400714.md): None · none · Feb 3, 2022 · N361NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3261 CROWN OF FUSELAGE BETWEEN FR 44-45 AND BETWEEN STRINGER 1L & R EXTERNAL SURFACE REQUIRES CLEANING AND NDT CHECK FOR POSSIBLE CORROSION OF SCREW HOLES FOR ADF-1 ANTENNA MOUNT. CORRECTIVE ACTION: CLEANED CORROSION PER ERA. OK FOR SERVICE. (2109227)
- [SDR DALA2022012000397](https://openairdocs.org/sdr/DALA2022012000397.md): None · none · Jan 19, 2022 · N361NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3261 AFT MAIN CABIN FLOORBEAM Y1292 FRAME 68-69 STR 23LH HAS CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2091714)
- [SDR DALA2022012000396](https://openairdocs.org/sdr/DALA2022012000396.md): None · none · Jan 19, 2022 · N361NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3261 MAIN CABIN FR68 - FR69 Y-1292 FLOOR BEAM IS CORRODED. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2091504)
- [SDR DALA2022012000395](https://openairdocs.org/sdr/DALA2022012000395.md): None · none · Jan 19, 2022 · N361NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3261 MAIN CABIN FR66 - FR68 Y-1292 FLOOR BEAM IS CORRODED. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. (2091500)
- [SDR DALA2022012000394](https://openairdocs.org/sdr/DALA2022012000394.md): None · none · Jan 19, 2022 · N361NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3261 MAIN CABIN AT FR66 Y-1292 SEAT TRACK IS CORRODED. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11. (2091491)
- [SDR DALA2022011900378](https://openairdocs.org/sdr/DALA2022011900378.md): None · none · Jan 18, 2022 · N361NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3261 SEAT TRACK AT FR20 TO FR21 -Y765 IN MAIN CABIN IS CORRODED OUT OF LIMITS. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11. (2090344)
- [SDR DALA2022011900377](https://openairdocs.org/sdr/DALA2022011900377.md): None · none · Jan 18, 2022 · N361NW · Airbus A320212 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3261 SEAT TRACK AT FR20 T0 FR21 IN MAIN CABINS CORRODED BEYOND ALLOWABLE DAMAGE. CORRECTIVE ACTION: REPLACED SEAT TRACK PER A320 SRM 51-72-11. (2090341)
- [SDR DALA2022011800326](https://openairdocs.org/sdr/DALA2022011800326.md): Floorbeam · corroded · Jan 17, 2022 · N361NW · Airbus A320212 · Fuselage Main, Floor Beam
  > SHIP 3261 AFT MAIN CABIN FLOORBEAM -Y254 FRAME 68 STR 23RH HAS CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-72-11. OK FOR SERVICE. (2089552)
- [SDR DALA2022011700307](https://openairdocs.org/sdr/DALA2022011700307.md): None · none · Jan 16, 2022 · N361NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3261 FWD L-1 DOOR, FWD UPPER CORNER DOOR CUTOUT (DOOR STOP 7), FR16 AT DOUBLE JOGGLE AREA IN OUTER FLANGE OF FRAME, FWD FASTENER ROW 3RD FASTENER HOLE FROM TOP (HOLE#5) HAS CRACK INDICATION APPROXIMATELY 7 OCLOCK POSITION AS VIEWED FROM INSIDE THE AIRCRAF
- [SDR DALA2022011700306](https://openairdocs.org/sdr/DALA2022011700306.md): None · none · Jan 16, 2022 · N361NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3261 CRACK INDICATION NOTED ON LH FR 20 DOOR STOP #7 AREA AT HOLE #8. CORRECTIVE ACTION: COMPLIED WITH ER/A 595833-14AD REV ORIGINAL. (2088331)
- [SDR DALA2022011700304](https://openairdocs.org/sdr/DALA2022011700304.md): None · none · Jan 16, 2022 · N361NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3261 FWD MAIN CABIN FLOORBEAM Y 503.2 FRAME 16 STR 23LH HAS CORROSION. CORRECTIVE ACTION: REPLACED FLOORBEAM PER A320 SRM 53-11-14 AND 51-72-11. (2088508)
- [SDR DALA2022011700309](https://openairdocs.org/sdr/DALA2022011700309.md): None · none · Jan 14, 2022 · N361NW · Airbus A320212 · Fuselage Main, Plate/Skin
  > SHIP 3261 FUSELAGE / SKIN / FRAME 20 LH AT DOOR STOPS NUMBER 7/ DOUBLE JOGGLE / HOLE 8 SKIN / CRACK. CORRECTIVE ACTION: COMPLIED WITH ERA 595833-14 SECTION II INSPECTION. OK FOR CONTINUED SERVICE. (2086503)
- [SDR DALA2022010600103](https://openairdocs.org/sdr/DALA2022010600103.md): None · none · Jan 6, 2022 · N361NW · Airbus A320212 · Fuselage Main, Frame
  > SHIP 3261 AFT MAIN CABIN PAX DOOR SILL SHAPE SILL FRAME 66-68 STR 23LH HAS CORROSION. CORRECTIVE ACTION: R/R PER A320 SRM 51-42-11. (2076797)
- [SDR DALA2022010300028](https://openairdocs.org/sdr/DALA2022010300028.md): None · none · Jan 2, 2022 · N361NW · Airbus A320212 · Fuselage Floor Panel
  > SHIP 3261 AFT MAIN CABIN FLOORBEAM -Y765 FRAME 66-68 STR 23RH HAS CORROSION. CORRECTIVE ACTION: REPLACED FLOOR BEAM PER A320 SRM 51-42-11. (2073193)
- [SDR DALA2024012401065](https://openairdocs.org/sdr/DALA2024012401065.md): Track · gouged · Dec 28, 2021 · N361NW · Airbus A320212 · Fuselage Main, Structure
  > SHIP 3261 DISC: COCKPIT R/H SIDE SLIDING WINDOW BOTTOM TRACK GOUGED AT FWD 2ND FASTENER. C/A: BLENDED DAMAGED AREA ON COCKPIT R/H SIDE SLIDING WINDOW BOTTOM TRACK IAW A320 SRM 53-11-12, EVALUATED AREA ORIGINAL MATERIAL THICKNESS 0.125" REMAINING MATERIAL 0.116
- [SDR DALA2021122908145](https://openairdocs.org/sdr/DALA2021122908145.md): None · none · Dec 28, 2021 · N361NW · Airbus A320212 · Fuselage Floor Panel
  > FWD MAIN CABIN FLOORBEAM -Y1732 FRAME 20 STR 23RH HAS CORROSION JF040. REMOVED CORROSION ON FWD MAIN CABIN FLOORBEAM WEB AT -Y1732 FRAME 20 STR 23 IAW A320 SRM 51-74-00, EVALUATED AREA ORGINAL THICKNESS 0.063" REMAINING THICKNESS 0.020" 2.0" X 1.5" AREA, FOUND

Next page: https://openairdocs.org/aircraft/N361NW/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 = 'N361NW' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N361NW/reports

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