# Service difficulty reports: N369NB

A list on [N369NB](https://openairdocs.org/aircraft/N369NB.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 · 147 reports

- [SDR DALA2026102205809](https://openairdocs.org/sdr/DALA2026102205809.md): Unknown · odor · Oct 21, 2026 · N369NB · Airbus A319114 · Air Distribution System
  > DECLARED AN EMERGENCY DUE TO DIRTY SOCK ODOR IN FWD CABIN. NO TROUBLE FOUND. LEVEL B DECONTAMINATION BEING PERFORMED. MAINTENANCE STILL IN PROGRESS. (LP: 9203806, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026102005761](https://openairdocs.org/sdr/DALA2026102005761.md): Unknown · odor · Oct 20, 2026 · N369NB · Airbus A319114 · Air Distribution System
  > FUME EVENT AT 23,000 FT DESCENDING- DIRTY SOCK ODOR IN COCKPIT. CALLED CABIN, FA SAID NO SMELL. FA'S CALLED AT 14,000FT AND CONFIRMED DIRTY SOCK. RAN EQRH FUMES, FUMES DISSIPATED AT 10,000 W/ VENTILATION OVRD. C/A: PERFORMED WALKAROUND OF A/C, FOUND NO EVIDENC
- [SDR DALA2026081004596](https://openairdocs.org/sdr/DALA2026081004596.md): Oxygen Box · unwanted deploy · Aug 5, 2026 · N369NB · Airbus A319114 · Passenger Oxygen System
  > PASSENGER OXYGEN STORAGE, PASSENGER OXYGEN MODULES, ROW 12 ABC O2 MASKS DROPPED AT PUSH BACK. REPACKED O2 MASKS AT PSU SEAT 12ABC & RESET DOOR PER AMM35- 21. (LP: 2822134, AIRCRAFT WAS GROUNDED)
- [SDR DALA2026062703819](https://openairdocs.org/sdr/DALA2026062703819.md): Oxygen Mask · damaged · Jun 24, 2026 · N369NB · Airbus A319114 · Crew Oxygen System
  > SCRATCHED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT. REMOVED CREW OXYGEN MASK POSITION 3RD OCCUPANT ON COCKPIT ON UNSERVICEABLE CONDITION IAW AMM 35-12-41-000-002A STEP 4.. REPLACED CREW OXYGEN MASK OBSERVER POSITION ON COCKPIT IAW FAM AMM 35-12-41-000
- [SDR DALA2026062103687](https://openairdocs.org/sdr/DALA2026062103687.md): Stiffener · unsecure · Jun 17, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > DURING M2 AND WHILE INSPECTING PER 5316-01052-05B THE HORIZONTAL STIFFENER OF LATERAL WINDOW FR4 RHS WAS FOUND COMPLETELY REMOVED DUE TO PREVIOUS REWORK PER THIS ER/A ORIGINAL REVISION. PER SECTION IV OF 573692-14 REV B, ACCOMPLISH SECTION IV REPETITIVE INSPE
- [SDR DALA2026060903444](https://openairdocs.org/sdr/DALA2026060903444.md): Stringer · corroded · Jun 6, 2026 · N369NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 38RH FROM FR59 TO FR60 IN AFT CARGO COMPARTMENT (SS I: 534150). REPLACED STRINGER SECTION 38RH BTW FR 59 TO FR 63 IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM 51-72-11 AND DRAWING E53476330 ISSUE AD, RELEASE DATE 11/JUL/18, M
- [SDR DALA2026053103284](https://openairdocs.org/sdr/DALA2026053103284.md): Fitting · corroded · May 30, 2026 · N369NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON RH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON RH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL CORROSION SPIGOT FITTINGWAS: P1: L:2.418 INCH, P2: L: 2.872 INCH, SEE INDIVIDUAL SIGN OFF
- [SDR DALA2026053103283](https://openairdocs.org/sdr/DALA2026053103283.md): Fitting · corroded · May 30, 2026 · N369NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > LEVEL 2 CORROSION, CORROSION SPIGOT FITTING RECEPTACLE ON LH PYLON. REPLACED SPIGOT FITTING RECEPTACLE ON LH PYLON AS PER A319 SRM 54-51-12-300-001. TOOK MEASURE INITIAL ON CORROSION SPIGOT FITTING RECEPTACLE WAS: P1: L:3.058 INCH, P2: L: 1.602 INCH. SEE INDI
- [SDR DALA2026052703189](https://openairdocs.org/sdr/DALA2026052703189.md): Seat Track · corroded · May 27, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y1292 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA (SSI:534147). REPLACED SEAT TRACK -Y1292 AND FASTENERS LOC. BETWEEN FR64 TO FR66 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11 AS PER A319 SRM51-72-11 AND DWG 10N01048 ISSUE:A
- [SDR DALA2026052703183](https://openairdocs.org/sdr/DALA2026052703183.md): Shear Plate · corroded · May 25, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, SHEAR PLATE STR 23 R LOC. FR 69 TO FR 70 AT AFT GALLEY AREA. APPLIED PROTECTIVE TREATMENT IN NEW HOLES ON SHEAR PLATE IAW SRM 51-21-11,.AND REPLACED SHEAR PLATE LOCATED BTW FR69 TO FR70 AT LEVEL STR23R AT AFT GALLEY AREA IAW SRM 51-42 -11,
- [SDR DALA2026052703182](https://openairdocs.org/sdr/DALA2026052703182.md): Fitting · corroded · May 24, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, CORROSION CENTER FITTING FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA ( SSI:534147). REPLACED CENTER FITTING LOCATED FR 66 TO FR 68 RH SIDE AT AFT GALLEY AREA. INITIAL MEASURE OF CORROSION WAS: L:0.4930 IN W: 0.2075 IN D:0.040 IN AS PER A319 S
- [SDR DALA2026052703181](https://openairdocs.org/sdr/DALA2026052703181.md): Seat Track · corroded · May 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION, CORROSION SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA (SSI: 531189). REPLACED SEAT TRACK -Y765 LOC. FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-72-11 A319 SRM 51-42-11 DWG D53112812 ISSUE: E00 RELEASE DATE: 22-MAR-06 D
- [SDR DALA2026052403139](https://openairdocs.org/sdr/DALA2026052403139.md): Seat Track · corroded · May 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORRIOSION SEAT TRACK -Y765 LOC. FR 64 TO FR 66 AT AFT GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, AND DWG NAT10N01048 ISSUE E. MEASURE OF THE CORROSION ARE L: 0.923 IN W: 0.354 IN. (LP: 1609533) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026052403138](https://openairdocs.org/sdr/DALA2026052403138.md): Floor Support · corroded · May 24, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION FR 68 FLOOR SUPPORT -Y765 AT AFT GALLEY AREA. REPLACED THE FLOOR SUPPORT -Y765 LOC. FR 66 TO FR 70 IAW SRM 51-42-11, SRM 51-72-11, DWG D53472780 ISSUE: K AND DWG D53478309 ISSUE E. MEASURE OF THE CORROSION ARE L: 1.298 IN W:1.061 IN D: 0.040
- [SDR DALA2026052403137](https://openairdocs.org/sdr/DALA2026052403137.md): Seat Track · corroded · May 24, 2026 · N369NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > LEVEL 2 CORROSION ON SEAT TRACK -Y1292 LOC BTW FR 12 TO FR 24 AT FWD GALLEY AREA. REPLACED THE SEAT TRACK IAW SRM 51-42-11, SRM 51-72-11, DWG D531128126 ISSUE E00 AND DWG D53110920 ISSUE E00, MEASURES OF THE CORROSION ARE: L= 0.901INCH, W= 0.385 INCH, D= 0.0
- [SDR DALA2026052403136](https://openairdocs.org/sdr/DALA2026052403136.md): Web · corroded · May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. REPLACED WEB AND FASTENERS LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA IAW SRM 51-42-11, DWG D53474180, ISSUE: E. (LP: 1609209) AIRCRAFT WAS GROUNDED.
- [SDR DALA2026052403135](https://openairdocs.org/sdr/DALA2026052403135.md): Web · corroded · May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, ON WEB LOCATED AT LEVEL S23R BTW FR 69 TO FR 70 AFT GALLEY AREA. INSTALLED WEB, BRACKET (1 EA) AND FASTENERS LOCATED AT LEVEL STR23RH BTW FR69 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-42- 11,DWG: D53474180 ISSUE: E. (LP: 1609200) AIRCRAF
- [SDR DALA2026052403134](https://openairdocs.org/sdr/DALA2026052403134.md): Floor Support · corroded · May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 3 CORROSION, EVIDENCE OF REWORK FLOOR SUPPORT +Y254 LOC. FR 16 TO FR 20 AT FWD GALLEY AREA. REPLACED THE FLOOR SUPPORT Y254 AND FASTENERS LOCATED BTW FR12 TO FR24 AT FWD GALLEY AREA IAW SRM 51-42-11 AND DWG D53112816, ISSUE: G00, DWG D53110984 ISSUE: C
- [SDR DALA2026052403133](https://openairdocs.org/sdr/DALA2026052403133.md): Cover Plate · damaged · May 23, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT. REPLACED COVER SHEET LOCATED FROM FR55A TO FR59 IN AFT CARGO COMPARTMENT IAW SRM 51-42-11, SRM 51-72-11 AND DWG E53476320, ISSUE: BD. MEASURE OF ELONGATED HOLE IS: D = 0.300
- [SDR DALA2026052403132](https://openairdocs.org/sdr/DALA2026052403132.md): Floor Support · corroded · May 21, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION FLOOR SUPPORT -Y1292-1162.5 LOC. FR 66 TO FR 68 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1292, -Y1162.5 AND LOCATED BETWEEN FR66 TO FR68 AT AFT GALLEY AREA IAW SRM 51-42-11 AND SRM 51-72-11 AND DWG D53472816, ISSUE F, AND DWG D53472780 I
- [SDR DALA2026052403127](https://openairdocs.org/sdr/DALA2026052403127.md): Floor Support · corroded · May 21, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > LEVEL 2 CORROSION, FLOOR SUPPORT -Y1162.5 FROM FR68 TO FR69 AT AFT GALLEY AREA. REPLACED FLOOR SUPPORT -Y1162.5 LOCATED BETWEEN FR68 TO FR69 AT AFT GALLEY AREA IAW SRM 51-42-11 AND A319 SRM 51-72-11 AND DWG D53472780.
- [SDR DALA2026052403129](https://openairdocs.org/sdr/DALA2026052403129.md): Dampener · failed · May 20, 2026 · N369NB · Airbus A319114 · Passenger/Crew Doors
  > DONT PASS OPERATIONAL TEST DAMPER PASSENGER CREW DOOR 832 AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 832 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-13-14-000 -001-B EXCEPT STEP 3A ITEM (4) AND 3E. JOB IN PROGRESS. (LP: 1604234) AIRCRAFT WAS
- [SDR DALA2026052403128](https://openairdocs.org/sdr/DALA2026052403128.md): Dampener · failed · May 19, 2026 · N369NB · Airbus A319114 · Passenger/Crew Doors
  > DONT PASS OPERATIONAL TEST DOOR DAMPER ON PASSENGER DOOR 841 AT FWD GA LLEY AREA AT AFT GALLEY AREA. REMOVED DOOR DAMPER OF PASSENGER CREW DOOR 841 ON UNSERVICEABLE CONDITION IAW FAM AMM 52-11-14- 000-001-B. EXCEPT 3.A.(4) AND 3.E. AIRCRAFT WAS GROUNDED
- [SDR DALA2026051903072](https://openairdocs.org/sdr/DALA2026051903072.md): Floor Support · corroded · May 18, 2026 · N369NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > CORROSION FLOOR SUPPORT +Y1162.5 LOC. FR 68 TO FR 69 AT AFT GALLEY AREA (SSI:534147). REPLACED FLOOR SUPPORT Y1162.5 LOC.FR68 TO FR69 AT AFT GALLEY AREA AS PER SRM 51-72-11, A319 SRM 51-42-11 AND DWG D53472780ISSUE: K RELEASE DATE:26-APR-18, DWG: D53474180 IS
- [SDR DALA2026030401477](https://openairdocs.org/sdr/DALA2026030401477.md): Door · malfunctioned · Feb 27, 2026 · N369NB · Airbus A319114 · Landing Gear Door Retract Section
  > LANDING GEAR DOORS NOT CLOSED, RT DOOR CLOSED, PROXIMITY SENSOR (26GA)TGT POS, LGCIU 1, RT DOOR CLOSED, PROXIMITY SENSOR (28GA) TGT POS, LGCIU 2. FOLLOW TSM TASK 32-31-00-810-861-A. (LP: 1470853)
- [SDR DALA2026011700392](https://openairdocs.org/sdr/DALA2026011700392.md): Light · damaged · Jan 13, 2026 · N369NB · Airbus A319114 · Emergency Lighting
  > EMERGENCY FLOOR LIGHTING DAMAGED OR INOPERATIVE / LOCATIONS:28D. SEAT BUSSEL THAT HOLDS LIGHT NEEDS TO BE REPAIRED & REPLACED. FWD (28D) EMERGENCY FLR LIGHT TO MEL 33-50-03A. MCC CONTACTED. CREW PLACARD INSTALLED. R & R DAMAGED HOUSING REF A319 AMM 25-21 OK F
- [SDR DALA2025111008214](https://openairdocs.org/sdr/DALA2025111008214.md): Microphone · stuck · Nov 9, 2025 · N369NB · Airbus A319114 · Communications System
  > CA 02 MASK MIC IS STUCK ON. RESET UNSUCCESSFUL. COULD NOT DUPLICATE FAULT ON GROUND. CA 02 MASK OPS NML. REF A319 AMM 35-12. (7727314).
- [SDR DALA2025110608084](https://openairdocs.org/sdr/DALA2025110608084.md): Oxygen Mask · leaking · Nov 4, 2025 · N369NB · Airbus A319114 · Crew Oxygen System
  > OBSERVER'S FIXED SEAT OXYGEN BOX AND MASK LEAKING. R & R OBSERVER STOWAGE BOX AND OXYGEN MASK IAW AMM 35-12. (8223896).
- [SDR DALA2025110608082](https://openairdocs.org/sdr/DALA2025110608082.md): Oxygen Mask · leaking · Nov 3, 2025 · N369NB · Airbus A319114 · Crew Oxygen System
  > CREW OXYGEN LEAKING AT A RATE OF 41 PSI SINCE LAST SERVICE. R & R THE OBSERVER STOWAGE BOX AND OXYGEN MASK IAW AMM 35-12. (1286068).
- [SDR DALA2025091906890](https://openairdocs.org/sdr/DALA2025091906890.md): Skin · dented · Sep 19, 2025 · N369NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > FOUND DENT BETWEEN FR10 AND FR11, AND APPR. 12" BELOW STR23 ON THE LEFT. CONFIRMED SURFACE PROTECTION ACCEPTABLE. EVALUATED PER A319 SRM 53-11-11-283-012. (7191121).
- [SDR DALA2025082706352](https://openairdocs.org/sdr/DALA2025082706352.md): Skin · damaged · Aug 26, 2025 · N369NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3169 CATTERING HAD GALLEY CART ROLL INTO SIDE OF LH AFT FUSELAGE BEHIND 2L DOOR. CORRECTIVE ACTION: COMPLIED WITH ER/A 628804-14. (7223438).
- [SDR DALA2025082606341](https://openairdocs.org/sdr/DALA2025082606341.md): Skin · dented · Aug 26, 2025 · N369NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > DENT AT THE LT FUSELAGE SKIN PANEL AFT OF FR70 AND BETWEEN STGR 16LH AND 17LH. COMPLIED WITH ER/A 628804-14. (1164780).
- [SDR DALA2025070905184](https://openairdocs.org/sdr/DALA2025070905184.md): Pressure Switch · leaking · Jul 7, 2025 · N369NB · Airbus A319114 · Hydraulic System, Main
  > SHIP 3169 - MISC - DECLARED EMERGENCY DUE TO LOSS OF YELLOW HYDRAULIC SYSTEM FLUID. CORRECTIVE ACTION: REPLACED LEAKING YELLOW HP MANIFOLD PRESSURE SWITCH AND ASSOCIATED SYSTEM FILTERS. (LP 7764502)
- [SDR DALA2025070104932](https://openairdocs.org/sdr/DALA2025070104932.md): Access Panel · cracked · Jun 30, 2025 · N369NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > SHIP 3169 CRACK ACCESS PANEL 322AL LEADING EDGE ON VERTICAL STABILIZER. CORRECTIVE ACTION: COMPLIED WITH ER/A 627102-14. (1055140).
- [SDR DALA2025070104931](https://openairdocs.org/sdr/DALA2025070104931.md): Access Panel · cracked · Jun 30, 2025 · N369NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > SHIP 3169 CRACK ACCESS PANEL 322BL LEADING EDGE ON VERTICAL STABILIZER. CORERCTIVE ACTION: COMPLIED WITH ER/A 627100-14. (1055104).
- [SDR DALA2025063004871](https://openairdocs.org/sdr/DALA2025063004871.md): Frame · cracked · Jun 29, 2025 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H3, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052345).
- [SDR DALA2025063004866](https://openairdocs.org/sdr/DALA2025063004866.md): Frame · cracked · Jun 29, 2025 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H4, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052350).
- [SDR DALA2025063004865](https://openairdocs.org/sdr/DALA2025063004865.md): Frame · cracked · Jun 29, 2025 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 CRACK INDICATION ON FRAME 16 LH SIDE IN OPEN FASTENER HOLE H2, AT CROSS BEAM SPLICING AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1052337).
- [SDR DALA2025063004870](https://openairdocs.org/sdr/DALA2025063004870.md): Crossbeam · cracked · Jun 28, 2025 · N369NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3169 FOUND CRACKS AT HOLES #2 #3 AND #4 OF CROSS BEAM JUNCTION AREA, FR16LH. CORRECTIVE ACTION: COMPLIED WITH ER/A 627149-14AD. (1051478).
- [SDR DALA2025062504769](https://openairdocs.org/sdr/DALA2025062504769.md): Bushing · worn · Jun 24, 2025 · N369NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3169, WEAR BONDED BUSHINGS ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 831. REPLACED BUSHES ON UPPER AND LOWER CONNECTION LINK AND SUPPORT ARM OF PASSENGER CREW DOOR 831 AS PER A320 FAM AMM 52-11-21-400- 001-A AS PER A320
- [SDR DALA2025062404733](https://openairdocs.org/sdr/DALA2025062404733.md): Bottle · no test · Jun 23, 2025 · N369NB · Airbus A319114 · Emergency Exits
  > SHIP 3169 DONT PASS OPERATIONAL TEST EMERGENCY DOOR DAMPER ON PASSENGER CREW DOO R 841. CORRECTIVE ACTION: REPLACED EMERGENCY DOOR DAMPER ON PASSENGER CREW DOOR 841 AS PER A320 FAM AMM-52-11-14-000-001-B AND AS PER A320 FAM AMMAMM-52- 11-14-400-001-B. (1041999
- [SDR DALA2025062304695](https://openairdocs.org/sdr/DALA2025062304695.md): Bushing · corroded · Jun 20, 2025 · N369NB · Airbus A319114 · Rudder Structure
  > SHIP 3169 CORROSION ON PLAIN BUSHINGS ON RUDDER HINGE BRACKET SIDE BR7. CORRECTIVE ACTION: REPLACED BUSHINGS OF HINGE #7 ON RUDDER AS PER A319 SRM 51-72-12- 911-002. (1036402).
- [SDR DALA2024112511195](https://openairdocs.org/sdr/DALA2024112511195.md): None · no discrepancy · Nov 22, 2024 · N369NB · Airbus A319114 · Standard Practices/Structures
  > SHIP 3169 NEED TO COMPLY WITH ERA 622523-14. CORRECTIVE ACTION: COMPLIED WITH ERA 622523-14. (0672127)
- [SDR DALA2024083008586](https://openairdocs.org/sdr/DALA2024083008586.md): Sliding Window · delaminated · Aug 27, 2024 · N369NB · Airbus A319114 · Flight Compartment Windows
  > SHIP 3169 CAPT SLIDING WINDOW DELAMINATING. CORRECTIVE ACTION: REPLACED PER A319 AMM 56-12. (0523700)
- [SDR DALA2024021902314](https://openairdocs.org/sdr/DALA2024021902314.md): Skin · dented · Feb 16, 2024 · N369NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3169 DENT ON RT WING INBOARD FLAP. CORRECTIVE ACTION: REPAIRED PER ER/A 615948-14. (5040095)
- [SDR DALA2023072606091](https://openairdocs.org/sdr/DALA2023072606091.md): Unknown · unknown · Jul 21, 2023 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 EXISTING REPAIR ON FASTENERS, HOLES NO. C, NO. D LOC. ON FRAME 16 LH SIDE JOG GLE AREA. CORRECTIVE ACTION: COMPLIED WITH ER/A 588166-14 AD REV.A (2877647)
- [SDR DALA2023072606090](https://openairdocs.org/sdr/DALA2023072606090.md): Unknown · unknown · Jul 21, 2023 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 EXISTING REPAIR ON FASTENERS HOLES 7, 8, A AND B LOC. ON FRAME 16 RH SIDE JOGGLE AREA. DOCUMENTED ON ER/A 588168-14 AD REV. CORRECTIVE ACTION: COMPLIED WITH ER/A 588168-14 AD REV.A. (2877585)
- [SDR DALA2023072105915](https://openairdocs.org/sdr/DALA2023072105915.md): Unknown · unknown · Jul 21, 2023 · N369NB · Airbus A319114 · Passenger/Crew Doors
  > SHIP 3169 OUT OF ADJUSTMENT PASSENGER CREW DOOR 842 POINT H ON UP AND DOWN POSI TION. CORRECTIVE ACTION: PERFORMED ADJUSTMENT ON POINT H IN UP AND DOWN POSITION AS PER A320 FAM AMM 52-13-21-400-001-A. (2876645)
- [SDR DALA2023072105911](https://openairdocs.org/sdr/DALA2023072105911.md): Unknown · unknown · Jul 20, 2023 · N369NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3169 FUSELAGE / FRAME/FORMERS / FR16RH AT DOOR STOP NO 7 LEVEL DOUBLE JOGGLE / HOLES 7 & B / CRACKS. CORRECTIVE ACTION: INSPECTION PER ER/A 588168-14. (2875666)
- [SDR DALA2023072005884](https://openairdocs.org/sdr/DALA2023072005884.md): Unknown · unknown · Jul 19, 2023 · N369NB · Airbus A319114 · Fuselage Main, Floor Beam
  > SHIP 3169 BROKEN FLOOR BEAM -Y1292 BOLT (1 EA) LOC. FR46 IN PASSENGER CABIN. CORRECTIVE ACTION: REPLACED BOLT LOC. ON FLOOR BEAM -Y1292 FR46 IN PASSENGER CABIN AS PER A319 SRM 51-42-11. (2874554)

Next page: https://openairdocs.org/aircraft/N369NB/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 = 'N369NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N369NB/reports

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