N336NW
Service difficulty reports · 236
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
Query with SQL
duckdb -csv -c "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 = 'N336NW' AND registry_match = 'registration' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
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 = 'N336NW' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2026072804385Oxygen Mask · unwanted deployFWD LAV O2 MASK DEPLOYED IN FLIGHT. REPACKED OXYGEN MASK ASSY IAW AMM 35-21 PROCEDURES. OK FOR SVC. (LP: 9583816, AIRCRAFT WAS GROUNDED)SDR DALA2026053103285Window Frame · crackedCRACK INDICATION FOUND IN OPEN FASTENER HOLE LOCATED ON FRAME 4 LATERA L WINDOW UPPER JUNCTION RT SIDE. CRACK DEPTH: 0.078 INCH, CRACK DIRECTION: 3 O`CLOCK VIEW LOOKING FWD. REPAIR MUST BE ACCOMPLISHED PRIOR TO FURTHER FLIGHT. A.A 5311 -01236-02. COMPLIED WISDR DALA2026052803240Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND (1 EA) ON RH CONTINUITY FITTING OF THE WINDSHIE LD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 5311-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RSDR DALA2026052803239Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L=0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONT SDR DALA2026052803238Window Frame · crackedAIRCRAFT 3236, CRACK INDICATION FOUND ON LH CONTINUITY FITTING OF THE WINDSHIELD LOWE R ATTACHMENT AREA, L= 0.118 INCH APPROX. (AD 2020-17-03 WORK CARD 53 11-01226-01.) CORRECTIVE ACTION: PERFORMED REPAIR INSTRUCTIONS ON WINDSHIELD CENTER POST; LH AND RH FRONTSDR DALA2026052803230Window Frame · crackedAIRCRAFT 3236, DURING M2 CHECK AT AEM (SAL), WHILE EXECUTION OF HFEC INSPECTION OF THE WINDSHIELD CENTRAL NODE CONTINUITY FITTINGS AND WINDSHIELD FRAMES ON LH AND RH SIDES AS PER JOB CARD 5311-01226-01 (IN ORDER TO COMPLY WITH FAA AD 2020-17-03 AND SB A320-53-SDR DALA2026060103310Skin · damagedDURING CURRENT HEAVY CHECK PERFORMED ON AEM SAL, AN EXISTING REPAIR WAS FOUND ON THE BUTT JOINT LOCATED AT FR24 BETWEEN STGR23LH AND STGR24LH ON THE SKINS PN D53112242202 AND PN D53231369200. THE REPAIR WAS EVALUATED AGAINST THE SRM 53-00-11 TABLE 203. SRM 53-SDR DALA2026052803236Skin · damagedAIRCRAFT 3236, DURING CURRENT HEAVY CHECK PERFORMED AT AEM (SAL), AN EXISTING REPAIR WAS FOUND ON THE EXTERNAL SKIN AT LEVEL OF FR29 AND STGR4L. THE REPAIR WAS EVALUATED AGAINST THE SRM 53-00-11 FIGURE 204 AND THE PITCHES THAT FIGURE 1 SHOWS WERE FOUND OUT OF SDR DALA2026053103291Skin · damagedDURING M2 AND WHILE PERFORMING AAI INSPECTIONS EXISTING REPAIR, INSTALLED PER 547923-14 REV B WAS FOUND INSTALLED ON EXTERNAL FUSELAGE SKIN AT FR24 BETWEEN STGR20LH AND STGR23LH WITH FASTENERS INSTALLED INCORRECTLY ON CHEM-MILLED POCKET. *DTE* PER SECTION DTESDR DALA2026052703205Repair · misinstalledAAI FINDING-DURING INSPECTION OF AMDS 5310-4051 FOUND PREVIOUS ACCOMPL ISHED SRM REPAIR INSTALLED AT FR23 BETWEEN STRINGERS 23L AND 24L.DURING INSPECTION OF INTERIOR OF FUSELAGE FOUND REPAIR FASTENERS IMPROPERLY INSTALLED.REPAIR ASSOCIATED WITH LOG PAGE 296344SDR DALA2026052703204Fitting · damagedBURRED MATERIAL (OVALIZATION) ON LOWER LATERAL FITTING LT SIDE RACK 80VU ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURTHER FLIGHT REFER TO AA CARD 2515-01014-02A AD RELEATED. COMPLIED WITH ER/A 633192-14AD REV. ORIGINAL APPROVED DATE 23- MAY-2SDR DALA2026052703213Window Frame · damagedDURING M2 AND WHILE INSPECTION PER EM 5311-01236-02, CRACK FOUND IN THE UPPER JUNCTION FASTENER HOLE OF FR4 LATERAL WINDOW FRAME, RHS, AT THE INTERFACE WITH RHS FRONT WINDSHIELD FRAME. PER SECTION DTE OF 633157-14AD THE REPAIR OF SECTION I IS LIMITED TO 26,60SDR DALA2026052703203Fitting · cracked*DTE* DURING M2 AND WHILE ACCOMPLISHING EM 5311-01246-01, BOTH LH/RH CONTINUITY FTGS FOUND CRACKED AND ALSO FRONT WINDSHIELD FRAME HOLE D1 CRACKED. C/A: *DTE* PER SECTION DTE OF 633213-14AD, THE REPAIR OF SECTION I IS LIMITED TO 60,000 TOTAL FC (FROM A/C FIRSTSDR DALA2026052703211Fitting · damagedDURING M2 AND WHILE ACCOMPLISHING EM 2515-01014-02A, MATERIAL BURR WAS FOUND IN THE LT LWR LATERAL FITTING OF RACK FIN 80VU. PER SECTION II OF ER/A 633192-14AD ACCOMPLISH SECTION II INITIAL INSEPCTION WITHIN 19,500 FC FROM SECTION I (22MAY26). REPEAT SECTION SDR DALA2026051603022Floor Support · crackedCRACK (2 E/A) LOCATED ON FLOOR SUPPORT Y254 BTW FR49 TO FR51 IN PASSENGER CABIN. PERFORMED REPAIR INSTRUCTIONS ON FLOOR SUPPORT Y254 BTW FR49 TO FR51 IN PASSENGER CABIN AS PER A320 SRM 53-00-14-300-005 MEASURES OF CRACKS (2 EA) WERE: P1 L= 3.376 IN P2 L= 2.59SDR DALA2026052403140Aoa · damagedLIGHTENING STRIKE ON ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE. REPLACED ANGLE OF ATTACK (3FP3) BTW FR23 TO FR24 AT STR26L FWD FUSELAGE AS PER A320 FAM AMM 34-11-19-000-001-A AND AS PER A320FAM AMM 34-11-19-400-001-A. TEST ARE GOOD. (LP: SDR DALA2026050502833Web · crackedCRACKED WEB -Y765 LOCATED BTW FR 8 TO FR 11 IN COCKPIT. REPLACED WEB -Y765 LOCATED BTW FR 8 TO FR 11 IN COCKPIT AS PER A320 SRM 51-42-11,SRM 51-72-11 ,DWG D53113219 RELEASE ISSUE: BOO DWG D53110285 ISSUE: H00 AND DWG D53113378 ISSUE: B00 MEASURE OF CRACK IS:SDR DALA2026050102778Receptacle · corrodedCORROSION ON ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RH WING (REFER TO RII AMDS CARD 2751-9202). REPLACED ELECTRICAL RECEPTACLES (7540 VC) (7542 VC) ON RT WING IAW AIRBUS ESPM 20-56-42 PAGEBLOCK 0301 CONFIG 01, AIRBUS ESPM 20-44-11 PAGEBLOCK 0101 CONFIGSDR DALA2026042902709Web · corrodedLEVEL 2 CORROSION WEB FRAME 20 RH SIDE AT -Y1732 AT FWD GALLEY AREA. RELEASE DATE: 01/FEB/19 AND DWG: D53111226 ISSUE: B00 RELEASE DATE: 05/JUN/12. MEASURES ARE: L= 5.516 INCHES, W= 1.613 INCHES, SEE INDIVIDUAL SIGN OFF ON ORNRC 66/220 RII INSPECTION COMPLETESDR DALA2026042502627Floor Support · brokenBROKEN FLOOR SUPPORT +Y254 FR 33 TO FR 34 IN PASSENGER CABIN. REPLACED FLOOR SUPPORT Y254, LOC. BTW FR24 TO FR35 IN PAX CABIN IAW SRM 51-42-11, SRM 51-72 -11, & DWG: D53231346, ISSUE: D00, RELEASE DATE: 06/AUG/92. DWG: D52110920, ISSUE: E00, RELEASE DATE: 28SDR DALA2026042502624Floor Support · corrodedCORROSION FLOOR SUPPORT -Y254 LOCATED BTW FR 16 TO FR 20 AT FWD GALLEY A REA (SSI 531189). REPLACED FLOOR SUPPORT -Y254 LOCATED BTW FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG: D53112819 ISSUE: FOO RELEASE DATE 22-NOVSDR DALA2026042502623Floor Support · corrodedCORROSION FLOOR SUPPORT +Y254 LOCATED BTW FR 16 TO FR 21 AT FWD GALLEY AREA (SSI 531189). REPLACED FLOOR SUPPORT Y254 LOCATED BTW FR 16 TO FR 24 AT FWD GALLEY AREA AS PER A320 SRM 51-42-11,A320 SRM 51-72-11 AND DWG D53112816 ISSUE: GOO RELEASE DATE:08/JAN/97 SDR DALA2026042002473Floor Support · corrodedCORROSION FLOOR SUPPORT -Y765 LOCATED BTW FR 67 TO FR 69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-72-11, AND DRAWING D53472093 (LP: 1552628). AIRCRAFT WAS GROUNDED.SDR DALA2026042002470Web · corrodedCORROSION WEB FRAME 16 RH SIDE AT FWD GALLEY AREA. REPLACED WEB, LOC. BTW FR12 TO 16 RH SIDE AT FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112780, & DWG D53918884. TOOK MEASURES OF CORROSION ON WEB ARE: L= 3.832IN W=1.570 IN. (LP: 1551636). ASDR DALA2026042002469Seat Track · crackedCORRODED SEAT TRACK -Y1292 LOCATED AT FR 66 AT AFT GALLEY AREA. REPLACED SEAT TRACK -Y1292 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11, AND DWG 10N01036. TOOK MEASURE CORROSION WERE: L: 0.620 INCH, W: 0.450 INCH, D: 0.035 INCH, (LSDR DALA2026042002468Fitting · crackedCRACKED FITTING. LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT. REPLACED FITTING (1 EA) LOCATED BTW FR 11 TO FR 12 AND -Y 765 IN COCKPIT TOOK MEASURES OF CRACK L:0.468 INCH IAW SRM 51- 42-11, SRM 51-72-11, AND DWG D53110097. (LP: 1551630). AIRCRAFT WAS SDR DALA2026041702445Floor Support · corrodedCORROSION FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOOR BEAM -Y1162.5 LOCATED BTW FR 68 TO FR 69 AT AFT GALLEY AREA AS PER A320 SRM 51-42-11 , A320 SRM 51-72-11 AND DWG D53472780; RELEASE DATE: 26-APR-18; ISSUESDR DALA2026041702444Seat Track · corrodedCORROSION SEAT TRACK +Y765 LOCATED AT FR 66 AT AFT GALLEY AREA ( SSI 534147). REPLACED SEAT TRACK Y765 LOC. BTW FR64 TO FR66, AT AFT GALLEY AREA AS PER A320 SRM 51-42-11, A320 SRM 51-72-11 AND DWG 10N01036 RELEASE DATE 15-JUL-15 ISSUE C. TOOK MEASURE OF CORROSDR DALA2026041702441Floor Support · corrodedCORROSION FLOOR SUPPORT +Y1162.5 LOCATED BTW FR 68 TO FR 69 AFT GALLEY AREA (SSI 534147). REPLACED FLOOR SUPPORT LOC Y1162.5 BETWEEN FR68 TO FR69 FLOOR STRUCTURE AFT GALLEY AREA AS PER A320 SRM 51-42-11, SRM 51- 72-11 AND DWG D53472000 RELEASE DATE 06-JAN-03SDR DALA2026041702439Floorbeam · corrodedCORROSION FLOORBEAM BTW Y1292 TO Y 1162.5 AND FR 66 TO FR 68 AT AFT GALLEY AREA (SSI 534147). REPLACED FLOORBEAM AND FASTENERS LOC Y1292 TO Y1162.5 BETWEEN FR66 TO FR68 FLOOR STRUCTURE AFT GALLEY AREA AS PER A320 SRM 51- 42-11, A320 SRM 51-72-11 AND DWG D5347SDR DALA2026041702438Seat Track · corrodedCORROSION SEAT TRACK -Y765 LOCATED AT FR 66 AT AFT GALLEY AREA ( SSI 53 4147). C/A: REPLACED SEAT TRACK -Y765 LOCATED AT FR 64 TO FR 66 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11 AND DWG 10N01036 REV. C RELEASE DATE 05/JUN/14 MEASURE ARE L:SDR DALA2026041702437Seat Track · corrodedCORROSION SEAT TRACK +Y765 LOCATED BTW FR 16 AND FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y765 LOC. BTW FR12 TO FR24 AT FWD GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM51-42-11 AND DWG D53112812; RELEASE DATE: 08-JAN-97; ISSUE: E00; D53110SDR DALA2026042002466Dampener · failedSHIP 3236 DISC: DONT WORK CORRECTLY PASSENGER CREW DOOR 831 DAMPER (REFERENCE RII AMDS CARD 5210-7089-LF). C/A: REMOVED DOOR DAMPER FROM PASSENGER CREW DOOR 831 PN FE174-004 SN 786 ON UNSERVICEABLE CONDITION AS PER A320 FAM AMM 52-11-14-000 -001-A. EXCEPT STEPSDR DALA2026041502380Dampener · failedPASSENGER CREW DOOR 842 DAMPER DOESN`T WORK CORRECTLY. REMOVED DOOR DAMPER PASSENGER CREW DOOR 842 ON UNSERVICEABLE CONDITION PN FE174-004 SN 604. IAW AMM 52-13-14-000- 001-A EXCEPT STEP 3A. ITEM (4) AND 3D. REPLACED DOOR DAMPER IAW AMM52-13-14-000-001-A ANSDR DALA2026041302315Seat Track · corrodedCORROSION SEAT TRACK +Y1292 AT FR 16 HARD POINT AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y1292 LOCATED BETWEEN FR12 TO FR24 IN FORWARD GALLEY AREA AS PER A320 SRM 51-72-11, A320 SRM 51-42-11, DWG D53112812 RELEASE DATE 08-JAN-97 ISSUE E00, DWG D53SDR DALA2026041202305Floor Support · corrodedCORROSION FLOORBEAM +Y765 LOCATED BTW FR 67 TO FR 68 AT AFT GALLEY A REA (SSI 534147). REPLACED FLOOR BEAM Y765 LOCATED BTW FR 66 TO FR 70 AT AFT GALLEY AREA AS PER A320 SRM 51-72-11; A320 SRM 51-42-11 AND DWG D53472815 RELEASE DATE 18-DEC-06. ISSUE G. MEASURSDR DALA2026041302314Hinge Pin · corrodedCORROSION PINS HINGE AILERON ON LH AND RH WING (6E/A). OBTAINED PINS HINGE AILERON ON LH AND RH WING (6E/A) AS PER AIPC 27-14-05-31A AND AIPC 27-14-05-32. THE INSTALLATION IS TO BE ACCOMPLISHED ON AMDS CARD 5760-1010S-LT AND AMDS CARD 5760- 1010S-RT. RII INSPSDR DALA2026040802230Shear Plate · corrodedCORRODED SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23R AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23R AT AFT GALLEY AREA IAW SRM 51-72-11, SRM 51-42-11 AND DRAWING D53474180 ISSUE AA, DWG-D92490174 ISSUE AD. MEASURESDR DALA2026040802229Shear Plate · corrodedCORRODED SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23L AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOCATED BTW FR 69 TO FR 70 LEVEL STR 23L AT AFT GALLEY AREA AS IAW SRM 51-72-11, SRM 51-42-11 AND DRAWING D53474180, ISSUE AA, AND DRAWING D92490174, MEASSDR DALA2026040402159Seat Track · corrodedCORRODED SEAT TRACK -Y765, FR 20 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK BTWN FR 12 TO FR 24 IAW SRM 51-72-11, SRM 51-42- 11, DWG D53110984, ISSUE C00 & DWG D53112812, ISSUE E00. (LP: 1525075) AIRCRAFT WAS GROUNDED.SDR DALA2026040402158Dampener · malfunctionedDOES`NT WORK CORRECTLY, PASSENGER CREW DOOR 832 DAMPER. REMOVED AND REPLACED DOOR DAMPER FROM PASSENGER CREW DOOR 832 ON UNSERVICEABLE CONDITION FOR NEW DOOR DAMPER IAW AMM 52-13-14-000-001-A. AND AMM 52-13-14-400-001-A. (LP: 1520281) AIRCRAFT WAS GROUNDEDSDR DALA2026033002095Support · corrodedCORROSION LOWER SILL LOCATED AT FR 68 LT SIDE AT AFT GALLEY AREA. PERFORMED PERMANENT REPAIR ON LOWER SILL A320 SRM 53-41-14-300-001, MEASUREMENT OF CORROSION: L= 1.536 INCH W= 0.894 INCH D= 0.041 INCH. (LP: 1519027)SDR DALA2026040402157Dampener · malfunctionedDOESN`T WORK CORRECTLY, PASSENGER CREW DOOR 841 DAMPER. REMOVED AND REPLACED OLD DOOR DAMPER FOR NEW DOOR DAMPER ON PASSENGER CREW DOOR 841 IAW AMM 52-11-14-000-001-A AND AMM 52-11-14-400- 001-A. (LP: 1517067) AIRCRAFT WAS GROUNDEDSDR DALA2026033002094Seat Track · corrodedCORRODED SEAT TRACK, -Y1292 BTW FR 16 TO FR 20, FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-72-11, SRM 51-42-11, & DWG D53112812, ISSUE E00, DWG D53110984, ISSUE C00, & DWG D53110920, ISSUE E00. MEASUREMENT OF CORROSION: L: 1.340 INCH, W: 0.890 ISDR DALA2026033002093Dummy Rail · corrodedCORRODED DUMMY RAIL Y503.2 LOCATED BTW FR 12 TO FR 16 FWD GALLEY AREA. REPLACED THE DUMMY RAIL IAW SRM 51-42-11, SRM 51-72-11, DWG D53112825, ISSUE E00. DWG D53112758, ISSUE F00, & DWG D53110984, ISSUE C00. TOOK MEASUREMENT OF CORROSION: L: 0.543 INCH, WSDR DALA2025110608078Probe · faultedATO - AT APPROXIMATELY 20 KTS DUE TO FUEL L OUTER TK LO TEMP ECAM WARNING. FLIGHT CREW MEL PLACARDED AND CONTINUED. T/S PER TSM A319 28-42-00-810-816-A. PERFORMED POWER ON BITE EQIS. TESTS PASSED. NO FAULTS ON PFR & LAST LEG. PREVIOUS LEG REPORT ON CH 1 AND SDR DALA2025101607562Oil System · low pressureRETURNED TO SLC DUE TO LEFT ENGINE LOW OIL PRESSURE AND ENGINE WAS SHUT DOWN. ENGINE CHANGE REQUIRED DUE TO ENGINE OPERATED BELOW AMM OIL PRESSURE LIMITS. (LP: 7404148)SDR DALA2025101307453Inlet · contaminatedON THE GOURND, AFTER 5 MIN OF APU RUNNING, DIRTY SOCK ODOR/SMELL PRESENT AFTER SELECTING APU BLEED ON. SMELL SEEMS TO DISSAPATE AFTER SELECTING BLEED OFF. PERFORMED SMOKE AND FUME T/S IAW A320 AMDS WORKCARD # 0550-2002. FOUND SOURCE TO BE APU INLET DUCT CONTASDR DALA2025101007391Unknown · odorDIRTY SOCK SMELL ON APPLICATION OF APU BLEED A GATE. REF LOG # 1241745 FOR CORRECTIVE ACTIONS. (LP: 7404134)SDR DALA2025100607234Hydraulic System · leakingHYD LEAK IN MAIN WHEEL WELL, LEFT SIDE, IN OVERHEAD TRAY. LEAK CAUSING APU SMOKE + FUMES. LEAK RATE WITHIN AMM LIMITS PER A320 AMM 29-00-00 PLACING ON MON. REF L/P 1233149
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