# Service difficulty reports: N335NB

A list on [N335NB](https://openairdocs.org/aircraft/N335NB.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 · 198 reports

- [SDR DALA2026090805017](https://openairdocs.org/sdr/DALA2026090805017.md): Piston · intermittent · Sep 5, 2026 · N335NB · Airbus A319114 · Landing Gear Brake System
  > ON TAXI OUT CA RIGHT BRAKE PEDAL CHATTERED AND THEN WENT TO THE FLOOR. AFTER RETURNING TO GATE NOISE FROM PREVIOUS FLIGHT RETURNED. C/A: T/S IAW A319 TSM 32-42-00-810-841-A & TSM 32-42-00-810-912-A. FOUND #4 BRAKE PISTON AT 1 O'CLOCK POSITION INTERMITTENTLY GR
- [SDR DALA2026070803983](https://openairdocs.org/sdr/DALA2026070803983.md): Latch · missing · Jun 30, 2026 · N335NB · Airbus A319114 · Passenger Oxygen System
  > 11DEF PASSENGER OXYGEN STORAGE, FOUND FWD LATCH FOR O2 GENERATOR PANEL MISSING. FWD TO MEL 35-21 -01A. -M- PROCEDURES C/W. WILL NEED LATCH. REPLACED PASSENGER SERVICE UNIT AT ROW 11DEF IAW AMM 25-25. OPS CHKD GOOD. M PROCEDURE REVERSED. MEL AND PLACARD REMO
- [SDR DALA2026051903076](https://openairdocs.org/sdr/DALA2026051903076.md): Light · failed · May 17, 2026 · N335NB · Airbus A319114 · Passenger Compartment Lighting
  > WE HAD A LOT OF WATER COME OUT OF GASPERS AT 16DF. PAX REPORTED SPARK FROM OVERHEAD LIGHT. NOW THAT LIGHT IS OUT. INSPECTED THE OVERHEAD PANEL AT 16DEF NOT FAULTS DETECTED PER AMM 33-20, ACFT OK FOR SERVICE. (LP: 8880930). AIRCRAFT WAS GROUNDED
- [SDR DALA2026040802235](https://openairdocs.org/sdr/DALA2026040802235.md): Plenum · contaminated · Apr 6, 2026 · N335NB · Airbus A319114 · APU Oil System
  > OIL ODOR THROUGHOUT CABIN & COCKPIT ON ACFT ENTRY. APU LEAK CHK & INSP FOR CONTAMINATION C/W ON LOG 8044937, COMPLETES SMOKE AND FUMES WORKCARD 0550-2002 AND 0550- 2001 AND DUE TO PREVIOUS HIS ON NR 2 ENG. COMPLETED ENG 1 & 2 BOROSCOPE WORKCARD 7900-2001. REI
- [SDR DALA2026040302147](https://openairdocs.org/sdr/DALA2026040302147.md): Ecs · contaminated · Mar 31, 2026 · N335NB · Airbus A319114 · Cabin Cooling System
  > STRONG DIRTY SOCK ODOR COMING FROM FLIGHT DECK. NOTICED THE ODOR IMMEDIATELY UPON BOARDING. APU & PACKS ON FOR MEL. SUSPECT POSSIBLE APU BLEED CONTAMINATION. PERFORMED LEVEL A DECONTAMINATION OF ECS PER WORKCARD 2100-2007. REF MD LOG 1521040 FOR COMPLETION OF
- [SDR DALA2026011500365](https://openairdocs.org/sdr/DALA2026011500365.md): Stop Fitting · damaged · Jan 14, 2026 · N335NB · Airbus A319114 · Passenger/Crew Doors
  > REPAIR PERFORMED ON FR 68 LT AT DOOR STOP FITTING NR 1 IAW ERA 631655-14, AND SRM 53-41-12-300-011. IAW SRM 53-41-12-205-010, REPEAT INSPECTIONS ARE REQUIRED. ACCOMPLISH ER/A 631655-14 SECTION II WITHIN 19,700FC FROM 21JUN25 (30,878FC). ASSOCIATED ER/A 00-6316
- [SDR DALA2025091906891](https://openairdocs.org/sdr/DALA2025091906891.md): Ecs · odor · Sep 19, 2025 · N335NB · Airbus A319114 · Air Distribution System
  > DURING DESCENT BELOW 10,000' AIRCRAFT HAD VERY STRONG DIRTY SOCKS SMELL. AFTER LANDING DURING TAXI IN WAS MILDER. ECS DECONTAMINATION REVERSE DUCT BURN PROCEDURE ACCOMPLISHED FOR LEVEL B CONTAMINATION REF AMDS WORKCARD 2100-2005. (7643012).
- [SDR DALA2025080505866](https://openairdocs.org/sdr/DALA2025080505866.md): Unknown · odor · Aug 1, 2025 · N335NB · Airbus A319114 · Air Distribution System
  > PILOTS FA'S & PAX MENTIONED DIRTY SOCK SMELL. PERFORMED PACK BURNOUT REF A319 AMM 21-00-00-615-803-A.
- [SDR DALA2025063004867](https://openairdocs.org/sdr/DALA2025063004867.md): Door Frame · cracked · Jun 27, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 CRACK INDICATION ON FR 20 AT FWD GALLEY AREA, DOUBLE JOGGLE AREA, HOLE 6, RH SIDE, CRACK POSITION AT 10 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 626357-14AD. (1049480).
- [SDR DALA2025062704817](https://openairdocs.org/sdr/DALA2025062704817.md): Frame · cracked · Jun 26, 2025 · N335NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3135 CRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H16 IN CROSSBEAM SPLICING AREA. CRACK DIRECTION 12 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 626548-14AD. (1047744).
- [SDR DALA2025062704816](https://openairdocs.org/sdr/DALA2025062704816.md): Frame · cracked · Jun 26, 2025 · N335NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3135 CRACK INDICATION ON FRAME 16 RH SIDE OPEN FASTENER HOLE H2 IN CROSSBEAM SPLICING AREA. CRACK DIRECTION 4 OCLOCK. CORRECTIVE ACTION: COMPLIED WITH ER/A 626548-14AD. (1047686).
- [SDR DALA2025062704815](https://openairdocs.org/sdr/DALA2025062704815.md): Skin · dented · Jun 26, 2025 · N335NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3135 FOUND 2 DENTS LOCATED BELOW F/O SLIDING WINDOW- DENT ARE CREASED AGAINST THE INTERIOR FRAME STRUCTURE. CORRECTIVE ACTION: COMPLIED WITH ER/A 626900-14. (1048079).
- [SDR DALA2025062704814](https://openairdocs.org/sdr/DALA2025062704814.md): Floor Support · corroded · Jun 26, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 CORROSION FLOOR STRUCTURE UPPER SURFACE OF THE UPPER SKIN OF THE CENTER WING BOX FROM FR41 TO FR42 BETWEEN Y1292 AND Y1732 IN PASSENGER CABIN. CORRECTIVE ACTION: COMPLIED WHIT ER/A 626649-14. (1048074).
- [SDR DALA2025062604804](https://openairdocs.org/sdr/DALA2025062604804.md): Rib · gouged · Jun 25, 2025 · N335NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3135 GOUGE OB FLAP ON INBOARD RIB LOWER AREA AT INTERCONNECTING STRUT ARE ON RH WING. CORRECTIVE ACTION: COMPLIED WITH ER/A 626573-14. (1045570).
- [SDR DALA2025062604803](https://openairdocs.org/sdr/DALA2025062604803.md): Crossbeam · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 CRACK INDICATION WAS FOUND AT HOLE #2 AND #16 OF CROSSBEAM JUNCTION AREA OF FR16RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 626548-14AD. (1045556).
- [SDR DALA2025062604802](https://openairdocs.org/sdr/DALA2025062604802.md): Bulkhead · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Bulkhead
  > SHIP 3135 CRACK WAS FOUND AROUND A FASTENER HOLE COMMON TO THE BULKHEAD AT FR35 AND STGR 30 LH LEVEL. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1042906).
- [SDR DALA2025062604801](https://openairdocs.org/sdr/DALA2025062604801.md): Bulkhead · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Bulkhead
  > SHIP 3135 FOUND CRACK AT HOLE #1, #3 AND #8 COMMON TO THE BULKHEAD AT FR35 AAND STGR 30 LH LEVEL. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1045874).
- [SDR DALA2025062604800](https://openairdocs.org/sdr/DALA2025062604800.md): Structure · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 CRACK WAS FOUND AROUND A FASTENER HOLE COMMON TO THE BULKHEAD AT FR35 AND STGR 30 LH LEVEL. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1045830).
- [SDR DALA2025062604799](https://openairdocs.org/sdr/DALA2025062604799.md): Frame · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 FOUND CRACK AT HOLE W1, W3 IN FRAME35 WEB & HOLE #2 IN FRAME FLANGE. CORRECTIVE ACTION: COMPLIED WITH ER/A 575262-14AD. (1045802).
- [SDR DALA2025062604798](https://openairdocs.org/sdr/DALA2025062604798.md): Stiffener · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 CRACK INDICATION ON HORIZONTAL UPPER STIFFENER OF LATERAL WINDOW FRAME 4 LH SIDE. CORRECTIVE ACTION: COMPLIED WITH ER/A 575007-14AD. (1045582).
- [SDR DALA2025062604797](https://openairdocs.org/sdr/DALA2025062604797.md): Skin · chafed · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Plate/Skin
  > SHIP 3135 CHAFING MARK ON EXTERNAL FUSELAGE SKIN AT FRAME 34 BETWEEN STRINGER 43 LH AND RH. CORRECTIVE ACTION: COMPLIED WITH ER/A 575113-14AD. (1045547).
- [SDR DALA2025062504770](https://openairdocs.org/sdr/DALA2025062504770.md): Door Frame · cracked · Jun 25, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135, FOUND CRACK AT HOLE ON FASTENER HOLE #6 AT THE DOUBLE JOGGLE AREA OF THE RH FRAME 20 AROUND PASSENGER SERVICE DOOR. COMPLIED WITH ER/A 626357-14AD.
- [SDR DALA2025062504771](https://openairdocs.org/sdr/DALA2025062504771.md): Web · damaged · Jun 24, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135, MISDRILL ON VERTICAL WEB BTW FR57 TO FR58 AT LEVEL OF STR 41R AFT. REPLACED VERTICAL WEB AND FASTENERS LOC BTW FR 57 TO FR58 AT LEVEL OF STR 41R AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1043544)
- [SDR DALA2025062304693](https://openairdocs.org/sdr/DALA2025062304693.md): Stringer · corroded · Jun 22, 2025 · N335NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3135 CORROSION STRINGER 43L BTW FR64 TOFR65 IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON STRINGER STR43L BTW FR64 TO FR66 AS PER A319 SRM 53-41-13-300-004. (1039732).
- [SDR DALA2025062304692](https://openairdocs.org/sdr/DALA2025062304692.md): Stringer · corroded · Jun 22, 2025 · N335NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3135 CORROSION STRINGER 41R BTW FR61 AND FR62 IN AFT CARGO. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON STRINGER 41R BTW FR61 TO FR63 AS PER A319 SRM 53-00-13-300-001. (1039725).
- [SDR DALA2025062304685](https://openairdocs.org/sdr/DALA2025062304685.md): Door Frame · cracked · Jun 21, 2025 · N335NB · Airbus A319114 · Fuselage Main, Structure
  > SHIP 3135 CRACK INDICATIONS ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE 4 AT DOOR STOP FITTING 1 POSITION. CORRECTIVE ACTION: PERFORMED PERMANENT REPAIR ON FR68 LH AT LEVEL DOOR STOP FITTING #1 AS PER A319 SRM 53-41-12-300-011. (1038266).
- [SDR DALA2025062004653](https://openairdocs.org/sdr/DALA2025062004653.md): Rib · gouged · Jun 19, 2025 · N335NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3135 GOUGE OB FLAP ON INBOARD RIB LOWER AREA AT INTERCONNECTING. CORRECTIVE ACTION: COMPLIED WITH ER/A 626603-14. (1033780).
- [SDR DALA2025062004651](https://openairdocs.org/sdr/DALA2025062004651.md): Stringer · corroded · Jun 19, 2025 · N335NB · Airbus A319114 · Fuselage Main, Longeron/Stringer
  > SHIP 3135 CORROSION STRINGER 41L LOCATED BTW FR 64 TO FR 65 AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED STRINGER 41L LOCATED BTW FR 64 TO FR 65 AND FASTENERS IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (1033763).
- [SDR DALA2025061804590](https://openairdocs.org/sdr/DALA2025061804590.md): Shear Tie · corroded · Jun 17, 2025 · N335NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > SHIP 3135 CORROSION SHEAR TIE LOCATED FR 60 BTW STR 42L TO STR 43L IN AFT CARGO COMPARTMENT. CORRECTIVE ACTION: REPLACED SHEAR TIE AND FASTENERS LOCATED FR60 BTW STR 42L TO STR 43L IN AFT CARGO COMPARTMENT AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (1030238)
- [SDR DALA2025061704579](https://openairdocs.org/sdr/DALA2025061704579.md): Bonding Plate · broken · Jun 16, 2025 · N335NB · Airbus A319114 · Leading Edge Devices
  > SHIP 3135 BROKEN BONDING PLATE FLAP TRACK FAIRING 2 (531CB) ON LH WING. CORRECTIVE ACTION: REPLACED BONDING PLATE FLAP TRACK FAIRING #2 (531CB) ON LH WING IAW ER/A 622998-14TR. (1028240).
- [SDR DALA2025061604541](https://openairdocs.org/sdr/DALA2025061604541.md): Access Panel · cracked · Jun 14, 2025 · N335NB · Airbus A319114 · Vertical Stabilizer, Plate/Skin
  > CRACKED ACCESS PANEL 322AL LEADING EDGE VERTICAL STABILIZER. COMPLIED WITH ER/A 626387-14. (1023933).
- [SDR DALA2025061604538](https://openairdocs.org/sdr/DALA2025061604538.md): Shear Tie · gouged · Jun 13, 2025 · N335NB · Airbus A319114 · Fuselage Internal Mounting Structure
  > GOUGE SHEAR TIE LOCATED FR29 AND BTW STR43R TO STR42R IN FWD CARGO COMPARTMENT. REPLACED SHEAR TIE AND FASTENERS LOCATED FR29 AND BTW STR43R TO STR42R IN FWD CARGO COMPARTMENT AS PER A319 SRM 51-72-11.
- [SDR DALA2025061004423](https://openairdocs.org/sdr/DALA2025061004423.md): Support Angle · cracked · Jun 9, 2025 · N335NB · Airbus A319114 · Elevator Structure
  > SHIP 3135 CRACK SUPPORT ANGLE ELEVATOR HINGE ARM 1 LOC. LOWER POSITION ON LH HORIZONTAL STABILIZER. CORRECTIVE ACTION: REPLACED SUPPORT ANGLE ELEVATOR HINGE ARM 1 AND FASTENERS LOC. LOWER POSITION ON LH HORIZONTAL STABILIZER AS PER A319 SRM 51-42 -11 AND A319
- [SDR DALA2025060904395](https://openairdocs.org/sdr/DALA2025060904395.md): Skin · dented · Jun 7, 2025 · N335NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3135 FOUND DENTS ON UPPER AND LOWER SURFACE IB FLAP ON RH WING. CORRECTIVE ACTION: REPAIRED UPPER AND LOWER SURFACE IB FLAP ON RH WING AS PER A319 SRM 57-52-00-300-091. (1011630).
- [SDR DALA2025061104452](https://openairdocs.org/sdr/DALA2025061104452.md): Strut · corroded · Jun 4, 2025 · N335NB · Airbus A319114 · Wing Main, Frame Structure
  > SHIP 3135 CORROSION INTERNAL AND EXTERNAL BARREL ON INTERCONNECTING STRUT LH WIN G. CORRECTIVE ACTION: REPLACED INTERCONNECTING STRUT LH WING AS PER A320 FAM AMM 27-51 -44-000-001-A, AS PER A320 FAM AMM 27-51-44-400-001-A. (1004355)
- [SDR DALA2025053004145](https://openairdocs.org/sdr/DALA2025053004145.md): Web · corroded · May 29, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 CORROSION WEB LOCATED BETWEEN FR16 AND STR23R FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED WEB AND FASTENERS LOC. BTW FR12 TO FR16 AND STR23R FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0994737).
- [SDR DALA2025052904139](https://openairdocs.org/sdr/DALA2025052904139.md): Skin · corroded · May 28, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 SWOLLEN SKIN AND CORROSION WAS FOUND ON THE FOUR TROLLEY RETAINER BLOCKS COMPARTMENT (109 TO 112) LOWER SKIN AT G1 GALLEY. CORRECTIVE ACTION: COMPLIED WITH ER/A 626528-14. (0991778)
- [SDR DALA2025052904138](https://openairdocs.org/sdr/DALA2025052904138.md): Fitting · corroded · May 28, 2025 · N335NB · Airbus A319114 · Nacelle/Pylon, Main Frame
  > SHIP 3135 CORROSION SPIGOT FITTING RECEPTACLE BORE ON LH PYLON. CORRECTIVE ACTION: REPLACED SPIGOT FITTING RECEPTACLE LH PYLON AS PER A319 SRM 54- 51-12-300-001. (0991894)
- [SDR DALA2025052904137](https://openairdocs.org/sdr/DALA2025052904137.md): Support Fitting · loose · May 28, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 LOOSE FRAME 12 SUPPORT STRUCTURE BOLT FITTING BELOW BATTERY IN LATERA L AVIONIC COMP RH. CORRECTIVE ACTION: REPLACED SUPPORT FITTING STRUCTURE FRAME 12 BELOW BATTERY IN LATERAL AVIONIC COMP RH. AS PER A319 SRM 51-42-11 AND A319 SRM 51-72-11. (0991794
- [SDR DALA2025052904136](https://openairdocs.org/sdr/DALA2025052904136.md): Floor Support · corroded · May 28, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 CORROSION FLOOR BEAM -Y765 AT FR68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 LOC FR66 TO FR70 AFT GALLEY AREA AS PER A319 SRM 51-72-11 AND A319 SRM 51-42-11. (0991733)
- [SDR DALA2025052804116](https://openairdocs.org/sdr/DALA2025052804116.md): Shear Plate · corroded · May 27, 2025 · N335NB · Airbus A319114 · Fuselage Miscellaneous Structure
  > SHIP 3135 CORROSION SHEAR PLATE STR 23 R LOCATED BETWEEN FR69 TO FR70 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED SHEAR PLATE AND FASTENERS LOCATED BETWEEN FR69 TO FR70 AT LEVEL STR 23R AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0989504)
- [SDR DALA2025052804115](https://openairdocs.org/sdr/DALA2025052804115.md): Bracket · cracked · May 27, 2025 · N335NB · Airbus A319114 · Fuselage Main, Attach Fittings
  > SHIP 3135 CRACK BRACKET LOCATED AT FR 68 BTW STR 4R TO STR 5R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED BRACKET LOCATED AT FR 68 BTW STR 4R TO STR 5R AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0989499).
- [SDR DALA2025052704065](https://openairdocs.org/sdr/DALA2025052704065.md): Seat Track · corroded · May 26, 2025 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3135 CORROSION SEAT TRACK -Y1292 AT LEVEL FR20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 AND FASTENERS LOCATED ON FR12 TO FR24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0987856).
- [SDR DALA2025052704064](https://openairdocs.org/sdr/DALA2025052704064.md): Frame · corroded · May 26, 2025 · N335NB · Airbus A319114 · Fuselage Main, Frame
  > SHIP 3135 CORROSION FRAME WEB LOCATED BETWEEN FR69 TO FR70 AND STR23R AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FRAME WEB AND FASTENERS LOC. BTW FR 69 TO FR 70 AT LEVEL STR 23R AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0987835).
- [SDR DALA2025052604009](https://openairdocs.org/sdr/DALA2025052604009.md): Flap Track · corroded · May 25, 2025 · N335NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3135 CORROSION ON BEARING TRACK 4 O/B FLAP LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK 4 O/B FLAP LH WING AS PER A320 FAM AMM 57 -53-21-000-001-A AND AMM 57-53-21-400-001-A. (0986303).
- [SDR DALA2025052604008](https://openairdocs.org/sdr/DALA2025052604008.md): Flap Track · corroded · May 25, 2025 · N335NB · Airbus A319114 · Trailing Edge Flaps
  > SHIP 3135 CORROSION BEARING TRACK 3 O/B FLAP LH WING. CORRECTIVE ACTION: REPLACED BEARING TRACK 3 O/B FLAP LH WING AS PER A320 FAM AMM 57 -53-21-400-001-A AND AMM 57-53-21-000-001. (0986297).
- [SDR DALA2025052604007](https://openairdocs.org/sdr/DALA2025052604007.md): Seat Track · corroded · May 25, 2025 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3135 SEAT TRACK -Y1292 OUT OF LIMITS AS PER JOB CARD 2500-2031. CORRECTIVE ACTION: REPLACED SEAT TRACK -Y1292 LOCATED BTW FR36 TO FR41 AS PER A319 SRM 51-72-11, A319 SRM 51-42-11. (0986336).
- [SDR DALA2025052604006](https://openairdocs.org/sdr/DALA2025052604006.md): Seat Track · corroded · May 25, 2025 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3135 CORROSION SEAT TRACK -Y765 AT LEVEL FR20 FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y765 AND FASTENERS LOC. AT FR12 TO FR24 FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0986324).
- [SDR DALA2025052604003](https://openairdocs.org/sdr/DALA2025052604003.md): Seat Track · corroded · May 24, 2025 · N335NB · Airbus A319114 · Fuselage, Seat/Cargo Attach Fittings
  > SHIP 3135 CORROSION SEAT TRACK +Y765 AT FR16 AT FWD GALLEY AREA. CORRECTIVE ACTION: REPLACED SEAT TRACK Y765 AND FASTENERS LOCATED ON FR 12 TO FR 24 AT FWD GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11.
- [SDR DALA2025052603997](https://openairdocs.org/sdr/DALA2025052603997.md): Floorbeam · corroded · May 23, 2025 · N335NB · Airbus A319114 · Fuselage Main, Floor Beam
  > SHIP 3135 CORROSION FLOOR BEAM -Y1292-1162 AT FRAME 68 AT AFT GALLEY AREA. CORRECTIVE ACTION: REPLACED FLOOR BEAM -Y1292-1162 AND FASTENERS LOCATED ON FRAME 66 TO 68 AT AFT GALLEY AREA AS PER A319 SRM 51-42-11, A319 SRM 51-72-11. (0982805).

Next page: https://openairdocs.org/aircraft/N335NB/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 = 'N335NB' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N335NB/reports

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