# Service difficulty reports: N366NB

A list on [N366NB](https://openairdocs.org/aircraft/N366NB.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 · 155 reports

- [SDR DALA2026092405334](https://openairdocs.org/sdr/DALA2026092405334.md): Unknown · unknown · Sep 22, 2026 · N366NB · Airbus A319114 · Landing Gear System
  > STOPPED ON TAXIWAY AND AIRCRAFT WOULDN'T MOVE UNDER OWN POWER WITH BOTH ENGINES RUNNING. NEEDED A TOW BACK INTO GATE. ACFT STOPPED ON UNEVEN TAXIWAY SURFACE. TOWED TO GATE AND PERFORMED GVI OF NLG AND MLG IAW AMM 32-11 AND AMM 32-21. NO DEFECT NOTED. A/C OK F
- [SDR DALA2026061103519](https://openairdocs.org/sdr/DALA2026061103519.md): Fitting · not reported · Jun 9, 2026 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > PERFORM ER/A 633646-14AD FOR REPLACEMENT OF CONTINUITY FITTINGS LH AND RH. COMPLIED WITH ER/A 633646-14AD REV ORIGINAL MATCHES WITH ALL STEPS OF ER/A 633646-14AD PRI REV 0 AND PRI REV 1 IT IS BEENVALIDATED. PERFORMED REPAIR INSTRUCTIONS ON CONTINUITY FITTINGS
- [SDR DALA2026060903445](https://openairdocs.org/sdr/DALA2026060903445.md): Window Frame · cracked · Jun 6, 2026 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON CENTER POST UPPER TENSION BOLT LH AREA AT 1 OCLOCK, CRACK LENGTH 0.125 IN APPROX AND RH AREA AT 11 OCLOCK, CRACK L ENGTH 0.187 IN APPROX LOOKING INBOARD.MORE OVER CRACK INDICATION FOUN D ON CENTER POST LOWER CORNER LH. CRACK LENGT 0.3
- [SDR DALA2026060503395](https://openairdocs.org/sdr/DALA2026060503395.md): Fitting · not reported · Jun 1, 2026 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > ER/A 633553-14AD HAS BEEN ISSUED FOR WINDSHIELD CENTER POST MIRR OR FITTING REPAIR. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 17700FC FROM SECTION I WHICH IS APPROVED AS CATEGORY 'C'. SECTION II IS TBD AT THIS TIME NEEDING ADDITI ONAL EVALUATION FO
- [SDR DALA2026060503394](https://openairdocs.org/sdr/DALA2026060503394.md): Fitting · not reported · Jun 1, 2026 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > ER/A 633646-14AD ISSUE FOR WINDSHIELD CENTER POST CONTINUITY FIT TING REPLACEMENT. FOLLOW ON ACTION IS REQUIRED. SECTION I IS LIMITED TO 17700FC FROM SECTION I. SECTION II IS TB D AT THIS TIME AS ORIGINAL APPROVAL IS CATEGORY 'C'. ASSOCIATED ER/A 14-633646 AD
- [SDR DALA2026052403130](https://openairdocs.org/sdr/DALA2026052403130.md): Seat Track · corroded · May 21, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION SEAT TRACK -Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA.: REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BTW FR12 TO FR24 FWD GALLEY AREA IAW SRM 51-42-11, SRM 51-72-11 AND DWG D53112812 ISSUE E00. DWG D53110920 ISSUE E00.RELEASE, DWG D53110
- [SDR DALA2026051903073](https://openairdocs.org/sdr/DALA2026051903073.md): Seat Track · corroded · May 18, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK -Y765 LOCATED AT FR 20 FWD GALLEY AREA (SSI 5311 89). REPLACED SEAT TRACK -Y765 AND FASTENERS LOC. BTW FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 ANDDWG D53112812 ISSUE E00. RELEASE DATE 08-JAN-97, DWG D53110
- [SDR DALA2026051102935](https://openairdocs.org/sdr/DALA2026051102935.md): Receptacle · corroded · May 10, 2026 · N366NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORRSION, CORROSION SPIGOT RECEPTACLE FITTING ON RH PYLON. REPLACED SPIGOT RECEPTACLE FITTING ON RH PYLON AS PER A319 SRM 54-51-41-000-001- A, A319 SRM 54-51-41-400-001-A AND A319 SRM54- 51-12-300-001 MEASURED OF CORROSION AREA: D:0.0041 INCH AND OF D
- [SDR DALA2026051102934](https://openairdocs.org/sdr/DALA2026051102934.md): Shear Tie · corroded · May 9, 2026 · N366NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > LEVEL 2 CORROSION, CORROSION SHEAR TIE FR 28 AND BTW STR 41R TO STR 42R IN FWD CARGO CO MPARTMENT (SSI 532180). REPLACED SHEAR TIE AND FASTENERS LOC. FR28 BTW STR 41R TO STR 42R IN FWD CARGO AS PER A319 SRM 51-42-11 AND DWG D53233523, ISSUE D00, RELEASE DATE
- [SDR DALA2026051102933](https://openairdocs.org/sdr/DALA2026051102933.md): Hinge Fitting · worn · May 9, 2026 · N366NB · Airbus A319114 · Elevator Structure
  > WEAR ON HINGE FITTING 1, 2, 3, 4, 5 AND 6 ON RH ELEVATOR. REPLACED HINGE FITTING #1, #2, #3, #4, #5 AND #6 ON RH ELEVATOR AS PER A320 FAM AMM 55-16-42-000-001-A AND AS PER A320 FAM AMM 55-16-42-400-001-A SEE INDIVIDUAL SIGN OFF ON ORNRC 40/300 RII INSPECTION
- [SDR DALA2026051102932](https://openairdocs.org/sdr/DALA2026051102932.md): Receptacle · corroded · May 9, 2026 · N366NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORRSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER AS PER A319 SRM 54-51-12 AND AS PER A319 SRM 51-74-00 AND SRM 51-44-11 AND AS PER A320 FAM AMM 54-51-41-000-001-A AND AMM 54-51-41-400 -00
- [SDR DALA2026050102765](https://openairdocs.org/sdr/DALA2026050102765.md): Shear Plate · corroded · Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 SHEAR PLATE STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE AND FASTENERS LOC. STR 23R BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1571111- AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102764](https://openairdocs.org/sdr/DALA2026050102764.md): Web · corroded · Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 WEB BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA (SSI 534 147). REPLACED WEB, AND FASTENERS BTW FR69 TO FR70 AND STR23R AT AFT GALLEY AREA AS PER A319 SRM 51-72-11, A319 SRM 51-42-11. (LP 1571108 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102763](https://openairdocs.org/sdr/DALA2026050102763.md): Web · corroded · Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION LEVEL 2 WEB FRAME 20 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOC ON FR20 TO FR24 RH SIDE AT LEVEL STR 23 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 AND SRM 51-42-11. (LP 1570957 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102762](https://openairdocs.org/sdr/DALA2026050102762.md): Seat Track · corroded · Apr 30, 2026 · N366NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LEVEL 2 SEAT TRACK +Y1292 LOCATED AT FR 20 AT FWD GALLEY AREA (SSI 531189). REPLACED SEAT TRACK Y1292 AND FASTENERS LOC.BTW FR 12 TO FR 24 FWD GALLEY AREA AS PER A319 SRM 51-42-11 A319 SRM 51-72-11. (LP 1570948 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026050102761](https://openairdocs.org/sdr/DALA2026050102761.md): Frame · corroded · Apr 29, 2026 · N366NB · Airbus A319114 · Fuselage Main, Frame
  > CORROSION LEVEL 2 WEB FRAME 16 AT LEVEL STR 23L AT FWD GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED BTW FR12 TO FR16 AT LEVEL STR23L AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (LP 1569531 - AIRCRAFT WAS GROUNDED)
- [SDR DALA2026042902697](https://openairdocs.org/sdr/DALA2026042902697.md): Web · corroded · Apr 26, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION WEB BTW FR 69 TO FR 70, STR 23L REPLACED THE WEB IAW SRM 51-42-11, SRM 51-72-11, AND DWG D53474180, ISSUE: AA. MEASUREMENT OF CORROSION: L= 0.7260 INCH, W=0.4440 INCH. AIRCRAFT WAS GROUNDED
- [SDR DALA2026042902696](https://openairdocs.org/sdr/DALA2026042902696.md): Web · corroded · Apr 26, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION ON WEB FRAME 16, STR 23R. REPLACED THE WEB IAW SRM 51-42-11, SRM 51-72-11, DWG D53918884 & DWG D53114392. CORROSION: L= 0.833INCH W=0.520 INCH. ACFT WAS GROUNDED.
- [SDR DALA2026042502620](https://openairdocs.org/sdr/DALA2026042502620.md): Shear Plate · cracked · Apr 23, 2026 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CRACK SHEAR PLATE STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA. REPLACED SHEAR PLATE LOC. STR 23L BTW FR69 AND FR70 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DWGD53474180 ISSUE: AA RELEASE DATE: 09-SEP-24. TOOK MEASURE OF CRACK ON SHE
- [SDR DALA2026010900209](https://openairdocs.org/sdr/DALA2026010900209.md): Selector Valve · faulted · Jan 9, 2026 · N366NB · Airbus A319114 · Landing Gear Brake System
  > DIVERTED TO MIA DUE TO AN AUTO BRAKE FAULT. DIVERTED FOR A LONGER RUNWAY. SYSTEM FAULTED THE NORMAL BRAKES SELECTOR VALVE 23GG. REPLACED THE SELECTOR VALVE 23GG AND BSCU. (LP: 8056258)
- [SDR DALA2025080705918](https://openairdocs.org/sdr/DALA2025080705918.md): Oxygen Mask · inoperative · Aug 6, 2025 · N366NB · Airbus A319114 · Crew Oxygen System
  > PRIMARY OBSERVERS SLIDING SEAT - SEAT UNUSABLE O2 MASK INOPERATIVE. REMOVED AND REPLACED RT OBSERVER'S O2 MASK STOWAGE BOX IAW A319 AMM 35-12.
- [SDR DALA2025072505600](https://openairdocs.org/sdr/DALA2025072505600.md): Sidewall Panel · delaminated · Jul 24, 2025 · N366NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3166 FOUND LAMINATE DAMAGED IN FWD GALLEY. CORRECTIVE ACTION: REPLACED LAMINATE ON GALLEY WALL PER PER P.S. 900-9-1-11. (1102988).
- [SDR DALA2025071505313](https://openairdocs.org/sdr/DALA2025071505313.md): Light · unsecure · Jul 15, 2025 · N366NB · Airbus A319114 · Emergency Lighting
  > SHIP 3166 EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE. CORRECTIVE ACTION: RESECURED EMERGENCY FLOOR LIGHTING IN REF TO A319 AMM 33-50. (1082829).
- [SDR DALA2025052303990](https://openairdocs.org/sdr/DALA2025052303990.md): Compressor · damaged · May 23, 2025 · N366NB · Airbus A319114 · Turbine Engine Compressor Section
  > SHIP 3166 - ATB- DECLARED AN EMERGENCY AND RETURNED TO IAH DUE TO RIGHT ENGINE COMPRESSOR STALL. CORRECTIVE ACTION: MULTIPLE HPC BLADES FOUND DAMAGED ON BORESCOPE INSPECTION. REPLACED NBR 2 ENGINE. (LP 7251270)
- [SDR DALA2025050303399](https://openairdocs.org/sdr/DALA2025050303399.md): Bottle · low pressure · Apr 30, 2025 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 R1 DOOR DAMPER CHARGE OUT OF LIMITS. NEED SERVICE. SERVICED R1 DOOR DAMPER AND EMERG OPERATION CYLINDER USING ALTERNATE PROCEDURE IAW A319 AMM 52-10-00-610-801. LEAK CHKS GOOD. OK FOR SERVICE. (LP: 7193198)
- [SDR DALA2025032202146](https://openairdocs.org/sdr/DALA2025032202146.md): Bottle · low pressure · Mar 17, 2025 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 DISC: RT FWD DOOR EOAM LOW PRESSURE. C/A: RE-CHARGE RT FWD DOOR EOAM PER A319 AMM 52-10 ALTERNATE PROCEDURE.OK FOR SVC. (LP: 6826127)
- [SDR DALA2025031501993](https://openairdocs.org/sdr/DALA2025031501993.md): Skin · corroded · Mar 13, 2025 · N366NB · Airbus A319114 · Wing, Plate/Skin
  > SHIP 3166, CORROSION FOUND DURING INSPECTION OF RH WING AFT LOWER SKIN. CONTACT LIAISON ENGINEERING FOR REPAIR PROCEDURES PRIOR TO FURTHER FLIGHT. PER INSPECTION FC5720-01103. C/A: COMPLIED WITH PRI 624952-14 REVISION 0,1,2,3 AND E/RA 624952-14 REVISION ORIGI
- [SDR DALA2025031602003](https://openairdocs.org/sdr/DALA2025031602003.md): Skin · corroded · Mar 12, 2025 · N366NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3166 REPORTED CORROSION AROUND THE LAV OUTLET VENT, AT APPROXIMATELY 7.6 INCH AFT OF FR 69. CORRECTIVE ACTION: COMPLIED WITH ER/A 624952-14. (0854158)
- [SDR DALA2025020700963](https://openairdocs.org/sdr/DALA2025020700963.md): Bottle · low pressure · Feb 7, 2025 · N366NB · Airbus A319114 · Service Doors
  > SHIP 3166 R1 DOOR EMERGENCY OPERATING CYLINDER/ACCUMULATOR PRESSURE LOW. CORRECTIVE ACTION: SERVICED R1 DOOR EMERGENCY OPERATING CYLINDER/ACCUMULATOR PRESSURE PER A319 AMM TASK 52-10-00-610-801C1. (6823390)
- [SDR DALA2024112111124](https://openairdocs.org/sdr/DALA2024112111124.md): Junction Box · cracked · Nov 21, 2024 · N366NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3166 FWD OTBRD CORNER OF #2 PYLON ELECTRICAL JUNCTION BOX CRACKED. CORRECTIVE ACTION: REPAIRED PER A319 SRM 54-50-00. (0670518)
- [SDR DALA2024060505800](https://openairdocs.org/sdr/DALA2024060505800.md): Radome · damaged · Jun 2, 2024 · N366NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3166 DAMAGE ON NOSE RADOME CENTER. CORRECTIVE ACTION: APPLIED EROSION PROTECTION TAPE PER A319 AMM 53-15-11-300-001-A. (4896208)
- [SDR DALA2024032803910](https://openairdocs.org/sdr/DALA2024032803910.md): Anti-Ice Valve · faulted · Mar 26, 2024 · N366NB · Airbus A319114 · Airfoil Anti/De-ice System
  > SHIP 3166 - ATB - DUE TO LEFT WING ANTI-ICE VALVE FAULT WITH BLEED PRESSURE ABNORMAL MESSAGE. COULD NOT CONTINUE DUE TO WEATHER CONDITIONS. CORRECTIVE ACTION: REPLACED LT ENGINE PRV, OVERPRESSURE VALVE, AND LT WING ANTI-ICE VALVE. (LP 5414078)
- [SDR DALA2024032803909](https://openairdocs.org/sdr/DALA2024032803909.md): Anti-Ice Valve · unknown · Mar 26, 2024 · N366NB · Airbus A319114 · Airfoil Anti/De-ice System
  > SHIP 3166 - ATB - DUE TO LEFT WING ANTI-ICE VALVE NOT SHOWING OPEN WITH BLEED PRESSURE ABNORMAL MESSAGE. COULD NOT CONTINUE DUE TO WEATHER CONDITIONS. CORRECTIVE ACTION: REPLACED LT WING ANTI-ICE VALVE. (LP 5414076)
- [SDR DALA2023122010423](https://openairdocs.org/sdr/DALA2023122010423.md): Unknown · unknown · Dec 19, 2023 · N366NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3166 DENT ON LEFT HAND SIDE OF APU INLET RIGHT IN FRONT OF APU ACCESS DOOR. CORRECTIVE ACTION: REPAIRED PER ERA 614446-14. (4863946)
- [SDR DALA2023121910374](https://openairdocs.org/sdr/DALA2023121910374.md): Unknown · unknown · Dec 19, 2023 · N366NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3166 DENT ON SKIN FWD OF FR80 LWR SKIN. CORRECTIVE ACTION: LOCATED FASTENER HOLES AND FABRICATED -1 DOUBLER & -2 FILLER IAW SRM 53-51-11-300-010, INSTALLED -1 & -2 REPAIR PARTS IAW SRM 53-51-11-300-010. (4863949)
- [SDR DALA2023103008926](https://openairdocs.org/sdr/DALA2023103008926.md): Unknown · unknown · Oct 28, 2023 · N366NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3166 CRACK INDICATION ON FRAME 16 RH SIDE UPPER DOUBLE JOGGLE AREA AT OPEN FASTENER HOLE C. CORRECTIVE ACTION: REPAIRED PER ER/A 612815-14AD. (0038107)
- [SDR DALA2023103008924](https://openairdocs.org/sdr/DALA2023103008924.md): Unknown · unknown · Oct 28, 2023 · N366NB · Airbus A319114 · Aerodynamic Fairings
  > SHIP 3166 DAMAGE TO 191BB PANEL LEADING EDGE. CORRECTIVE ACTION: REPAIRED PER ER/A 542077-14TR. (0039475)
- [SDR DALA2023103008921](https://openairdocs.org/sdr/DALA2023103008921.md): Unknown · unknown · Oct 28, 2023 · N366NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > SHIP 3166 CRACK LEADING EDGE ACCESS PANEL 322CL EXTERNAL SKIN ON VERTICAL STABILIZER. CORRECTIVE ACTION: REPAIRED PER ER/A 613081-14. (0039388)
- [SDR DALA2023103008928](https://openairdocs.org/sdr/DALA2023103008928.md): Unknown · unknown · Oct 28, 2023 · N366NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3166 CORROSION ON I/B INTERCONNECTING STRUT SENSOR CONNECTOR ON RH WING. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT SENSOR CONNECTOR ON RH WING AS PER A320 FAM AMM 27-51-44-400-002-A AND AMM 27-51-44-000-002-A. (0038147)
- [SDR DALA2023102708842](https://openairdocs.org/sdr/DALA2023102708842.md): Unknown · unknown · Oct 27, 2023 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3166 OVERSIZED HOLE NO.1 AND HOLE NO.3 LOC. ON DOOR STOP FITTING 7 FR.66 RH. CORRECTIVE ACTION: REPAIRED PER ER/A 612926-14AD. (0036509)
- [SDR DALA2023102708846](https://openairdocs.org/sdr/DALA2023102708846.md): Unknown · unknown · Oct 26, 2023 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3166 CRACK WAS FOUND IN FR16 RHS AT FASTENER HOLE #C, NEAR DORR STOP #7. CORRECTIVE ACTION: REPAIRED PER ER/A 612815-14AD. (0036457)
- [SDR DALA2023102708845](https://openairdocs.org/sdr/DALA2023102708845.md): Unknown · unknown · Oct 26, 2023 · N366NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3166 ELONGATED HOLES FOUND IN FR 66 RHS AT ATTACHMENT OF DOOR STOP #7 AT THE UPPER OUTB'D AND LOWER OUTB'D HOLE POSITIONS. CORRECTIVE ACTION: REPAIRED PER ER/A 612926-14AD. (0035646)
- [SDR DALA2023102508766](https://openairdocs.org/sdr/DALA2023102508766.md): Unknown · unknown · Oct 24, 2023 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 EXCESSIVE PLAY PASSENGER CREW DOOR 842 UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM. CORRECTIVE ACTION: REPLACED BUSHES ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 842 AS PER A320 FAM AMM52-13-21-000-001-A, A320 FAM A
- [SDR DALA2023102608801](https://openairdocs.org/sdr/DALA2023102608801.md): Unknown · unknown · Oct 23, 2023 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 832 EMERGENCY DOOR DAMPER AT AFT GALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED EMERGENCY DOOR DAMPER AS PER A30 FAM AMM 52-13-14-000-001-B AND AS PERA320 FAM AMM 52-13-14-400-001-B. (0030992)
- [SDR DALA2023102308673](https://openairdocs.org/sdr/DALA2023102308673.md): Unknown · unknown · Oct 21, 2023 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 EXCESSIVE PLAY PASSENGER CREW DOOR 832 ON UPPER AND LOWER CONNECTION L INK AND SUPPORT ARM. CORRECTIVE ACTION: REPLACED BUSHES ON UPPER AND LOWER CONNECT UP ION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 832 AS PER A320 FAM AMM 52-13- 21-000-001-A,
- [SDR DALA2023102308672](https://openairdocs.org/sdr/DALA2023102308672.md): Unknown · unknown · Oct 21, 2023 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 831 EMERGENCY DOOR DAMPER AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-14-000-001-B AND AMM 52-11-14-400-001-B. (0028105)
- [SDR DALA2023102008649](https://openairdocs.org/sdr/DALA2023102008649.md): Unknown · unknown · Oct 19, 2023 · N366NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3166 DONT PASS OPERATIONAL TEST PASSENGER CREW DOOR 841 EMERGENCY DOOR DAMPER AT FWD GALLEY AREA (1 EA). CORRECTIVE ACTION: REPLACED DOOR DAMPER ON PASSENGER CREW DOOR 841 AS PER A320 FAM AMM 52-11-14-000-001-B AND AMM 52-11-14-400-001-B. (0024998)
- [SDR DALA2023100308107](https://openairdocs.org/sdr/DALA2023100308107.md): Unknown · unknown · Sep 30, 2023 · N366NB · Airbus A319114 · Nacelle/Pylon, Plate/Skin
  > SHIP 3166 FOUND NBR 1 ENGINE PYLON PANEL HAS EROSION & SMALL HOLE. # 414FR. CORRECTIVE ACTION: REPAIRED PER ERA 612551-14. (4575918)
- [SDR DALA2023082506925](https://openairdocs.org/sdr/DALA2023082506925.md): Unknown · unknown · Aug 25, 2023 · N366NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3166 DAMAGE TO 191BB PANEL LEADING EDGE. CORRECTIVE ACTION: REPAIRED PER. A319 SRM 53-35-11-300-036. (4928074)
- [SDR DALA2023072005883](https://openairdocs.org/sdr/DALA2023072005883.md): Unknown · unknown · Jul 14, 2023 · N366NB · Airbus A319114 · Nacelle/Pylon Structure
  > SHIP 3166 DAMAGE TO WING TO BODY FAIRING RT. SIDE PANEL 192EB. AT BOTTOM OF FASTENER EDGE. CORRECTIVE ACTION: PERFORMED REPETITIVE INSPECTION OF SPEED TAPE PER SRM 51-77-12-911-001. (8675608)

Next page: https://openairdocs.org/aircraft/N366NB/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 = 'N366NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N366NB/reports

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