# Service difficulty reports: N439UA

A list on [N439UA](https://openairdocs.org/aircraft/N439UA.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 · 157 reports

- [SDR CALA2026062217269](https://openairdocs.org/sdr/CALA2026062217269.md): Fuel Cap · missing · Jun 22, 2026 · N439UA · Airbus A320232 · Fuel Storage
  > FUEL CAP FOUND MISSING ON ARRIVAL REPLACED MISSINF FUEL CAP.
- [SDR CALA2026042715734](https://openairdocs.org/sdr/CALA2026042715734.md): Hydraulic Line · leaking · Apr 22, 2026 · N439UA · Airbus A320232 · Hydraulic System, Main
  > *EMERGENCY* GRN HYD. SYS QTY. READING 0. FOUND NUM 1 ENG. PYLON DRAINING HYD FLUID CONSTANTLY. INFO UPDATE. LEAK FOUND AT THIS GROMMET(DESCRIPTION) FOCUSED ON SMALLER OF THE TWO LARGE LINES. INFO UPDATE. LEAK FOUND AT THIS GROMMET(DESCRIPTION) FOCUSED ON S
- [SDR CALA2025081507819](https://openairdocs.org/sdr/CALA2025081507819.md): Door · lack of lube · Aug 15, 2025 · N439UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR 2L SLIDE WILL NOT DISARM. CREW VERIFIED FAS ABLE TO DISARM SLIDE. CHECKED GIRT FITTINGS AND LUBED ARM. NO DEFECTS NOTED IAW AMM 52-10-00. OK FOR SERVICE.
- [SDR CALA2025072506906](https://openairdocs.org/sdr/CALA2025072506906.md): Power Supply · inoperative · Jul 24, 2025 · N439UA · Airbus A320232 · Emergency Lighting
  > EPSU UNIT EMER L FAULT UPDATDED LOG WITH SDR REPORTING DUE TO BEING EMERGENCY LIGHTS SYSTEM REF GMM 04-20-16. REMOVED AND REPLACED EMERGENCY POWER SUPPLY UNIT AND BATTERY IAW AMM 33-51-38. OPS CHECK GOOD NO DEFECTS NOTED. NO FAULTS.
- [SDR CALA2025072506922](https://openairdocs.org/sdr/CALA2025072506922.md): Computer · faulted · Jul 22, 2025 · N439UA · Airbus A320232 · Pitot/Static Anti-Ice System
  > ALL CAPTS AIR DATA AND ANTI ICE PROBES FAILED ON DEPARTURE PILOTS REP MULTI ANTI-ICE CAPT PROBE MSGS ON ECAM. SW'ED AIR DATA SW TO POS 3. MSGS STOPPED. FOUND "NO PHC 1 DATA" FAIL MSG ON PFR. SEE PHOTO. R&R PHC 1. INSTALL TEST GOOD. REF AMM 30-31-34-400-002-A &
- [SDR CALA2025042904309](https://openairdocs.org/sdr/CALA2025042904309.md): Fuel Cap · missing · Apr 28, 2025 · N439UA · Airbus A320232 · Fuel Storage
  > FUEL CAP MISSING. REPLACED FUEL CAP COUPLING, REF AMM 28-25-00. AC GLEW INTO DSM MISSING FUEL CAP. FOUND FUEL CAP MISSING DURING RON CHECK.
- [SDR CALA2025022502469](https://openairdocs.org/sdr/CALA2025022502469.md): Control Servo · faulted · Feb 22, 2025 · N439UA · Airbus A320232 · Landing Gear Steering System
  > N/W STRG FAULT IN FLIGHT ACPD BSCU1 BITE REF MM 32-46-00-740-001-A, FOUND FAULT "STEERING ELECTRO-HYD MODULE (6GC)". REMOVED NWS SERVO 6GC REF MM 32-51-51-000-001-A. PART ON ORDER REPLACED NLG STEERING CONTROL MODULE (6GC) REF MM 32-51-51-400-001-A STEP 4A-C,
- [SDR CALA2025021102287](https://openairdocs.org/sdr/CALA2025021102287.md): Fitting · fod · Feb 8, 2025 · N439UA · Airbus A320232 · Passenger/Crew Doors
  > FA REPORTS DOOR 2L STIFF TO DISARM FOUND DEBRIS ON FLOOR FITTING. CLEANED AS REQURIED AND DOOR 2L ARMS AND DISARMS NORMALLY.
- [SDR CALA2025012802095](https://openairdocs.org/sdr/CALA2025012802095.md): Controller · faulted · Jan 28, 2025 · N439UA · Airbus A320232 · Landing Gear Steering System
  > WHEEL N/W STEERING ECAM AFTER GEAR RETRACTION. DEBRIEFED CREW CAPT STATED ONCE LANDING GEAR CAME UP N/W STEERING MESSAGE APPEARED ON ECAM. UPON APPROACH WHEN LANDING WAS EXTENDED MESSAGE CLEARED. AIRCRAFT TAXI ON ITS OWN POWER TO GATE. CURRENTLY NO MESSAGE PRE
- [SDR CALA2024042601248](https://openairdocs.org/sdr/CALA2024042601248.md): Spoiler · vibration · Apr 23, 2024 · N439UA · Airbus A320232 · Spoilers
  > AIRFRAME VIBRATION NOTICED AT SPEEDS GREATER THAN 290 KIAS. NUMBER 5 SPOILER VIBRATING.
- [SDR CALA2024032200847](https://openairdocs.org/sdr/CALA2024032200847.md): Limiter · tripped · Mar 19, 2024 · N439UA · Airbus A320232 · Trailing Edge Flaps
  > FLIGHT CREW REPORTS FLAPS OVERSPEED DUE TO GO AROUND FLAPS 3, HEARD AUDIBLE CHIME 3 TIMES, CREW STATED THEY DID NOT OBSERVE THE DURATION OR HOW MUCH OF AN OVERSPEED THE AIRCRAFT REACHED. VARGAS TOMC REQUIRES TASK 05-51-13-200-001 INSPECTION AFTER FLAP/SLAT EX
- [SDR CALA2023071002208](https://openairdocs.org/sdr/CALA2023071002208.md): Brake · unknown · Jul 8, 2023 · N439UA · Airbus A320232 · Standard Practices/Structures
  > HIGH SPEED REJECT AT 120KTS RH OUTBOARD BRAKE 675C NOSE STAYED ON GND PERFORMED EMERGENCY BRAKE APPLICATION / HOT BRAKE INSPECTION REF AMM 05-51-16-200-001-A. ALL CHECKS NORMAL UNDER OVERHEAT THRESHOLD. NORMAL BRAKE AND ALTERNATE BRAKE NORMAL
- [SDR CALA2023040601058](https://openairdocs.org/sdr/CALA2023040601058.md): Check Valve · low · Apr 6, 2023 · N439UA · Airbus A320232 · Hydraulic Power System
  > CREW REPORT: GREEN HYD LOW RES IN FLT FOUND GREEN SYS RESERVOIR EMPTY WITH EVIDENCE OF LEAKING IN LH WHEEL WELL FOUND LEAK AT HP MANIFOLD CHECK VALVE 1059GM O-RINGS ON ORDER. REMOVED AND REPLACED HP MANIFOLD CHECK VALVE 1059GM OPERATION CHECK GOOD NO LEAKS FOU
- [SDR CALA2023022700559](https://openairdocs.org/sdr/CALA2023022700559.md): Accumulator · broken · Feb 27, 2023 · N439UA · Airbus A320232 · Hydraulic Power System
  > ECAM CAUTION MESSAGE - B RSVR LO LVL MESSAGE INOP - HYD CLIMBING THROUGH 10000AIR RETURN EVIDENCE FOR BLUE POWER ACCUMULATOR WITH DIAPHRAGM BROKEN, NIS ADDED MATERIAL REQUIRED.. ISOLATED BLUE POWER ACCUMULATOR FOR THE SYSTEM FOR CHECK FOR MEX, M&E 31-2912-9-9
- [SDR CALA2022093002565](https://openairdocs.org/sdr/CALA2022093002565.md): None · cracked · Sep 28, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 WEB HORIZONTAL FLANGE AT STGR22 LEVEL LH SIDE, CRACK LENGHT IS 1.218 INCH APPROX, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308627 NITIAL INSPECTIONS OF R
- [SDR CALA2022093002564](https://openairdocs.org/sdr/CALA2022093002564.md): Skin · none · Sep 28, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > DURING PERFORMED AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR DOUBLER LOCATED LOWER FUSELAGE SKING AT FR31 TO FR32 BTW 38L TO STRG 39L. SEE AEROMAN NON ROUTINE 2022-308900 01-E FIGURE 005 VIEW B (SHEET 02) DOUBLER REPAIR MATERIAL: DAMAGE IAW NTM 51-90-00, T
- [SDR CALA2022093002562](https://openairdocs.org/sdr/CALA2022093002562.md): None · corroded · Sep 28, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-308753 MEASURES AFTER REWORK WAS L:2.388 INCH W:1.169 INCH, ELECTRONIC CRACK AND CORROSION INDICATION NOT FOUND, IAW SRM A320 53-41-14-283-002 FIGURE 002 SHEET 01, THIS IS CALIP
- [SDR CALA2022092802528](https://openairdocs.org/sdr/CALA2022092802528.md): Doubler · none · Sep 28, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > DURING PERFORMED AGING AIRCRAFT INSPECTION FOUND EXISTING REPAIR DOUBLER LOCATED LOWER FUSELAGE SKING AT FR31 TO FR32 BTW 38L TO STRG 39L. SEE AEROMAN NON ROUTINE 2022-308900 01-E FIGURE 005 VIEW B (SHEET 02) DOUBLER REPAIR MATERIAL: DAMAGE IAW NTM 51-90-00, T
- [SDR CALA2022092802539](https://openairdocs.org/sdr/CALA2022092802539.md): Floor Support · none · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 AND STR 23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-308750 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.66 AND STR. AREA IS: 0.091", NOMINAL THICKNESS ON AREA IS: 0.150" PERFORMED IAW NTM NTM 51-10-02 AND NTM 51
- [SDR CALA2022092802544](https://openairdocs.org/sdr/CALA2022092802544.md): None · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER OUTBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-308621 NITIAL INSPECTIONS OF REPAIRED FIT
- [SDR CALA2022092802543](https://openairdocs.org/sdr/CALA2022092802543.md): None · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA SEE AEROMAN NON ROUTINE 2022-308624 NITIAL INSPECTIONS OF REPAIRED FITTIN
- [SDR CALA2022092802542](https://openairdocs.org/sdr/CALA2022092802542.md): None · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 9 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308622 NITIAL INSPECTIONS OF REPAIRED FITTI
- [SDR CALA2022092802540](https://openairdocs.org/sdr/CALA2022092802540.md): None · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER OUTBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308623 NITIAL INSPECTIONS OF REPAIRED FITT
- [SDR CALA2022092802537](https://openairdocs.org/sdr/CALA2022092802537.md): Skin · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > NO RECORD PROVIDED FOR AGING AIRCRAFT INSPECTION AND RECORD REVIEW TO ACCOUNT FOR INSTALLATION AND RE-INSPECTION STATUS OF EXISTING DOUBLER ON EXTERIOR FUSELAGE FRAME 32, STRINGER 38-39L, SEE AEROMAN NON ROUTINE 2022-308927. WITH INSPECTION THRESHOLD 65,000FC
- [SDR CALA2022092802536](https://openairdocs.org/sdr/CALA2022092802536.md): None · cracked · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION ARE 1 AND 5 OCLOCK REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (2 EA). 2022-308620 ITIAL INSPECTIONS OF REPAIRED FITTING INSTALLED ON FR
- [SDR CALA2022092802538](https://openairdocs.org/sdr/CALA2022092802538.md): None · none · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL FR67 TO FR68 AND STR23L IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-308752 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.67 TO FR.68 W:1.971IN NOMINAL THICKNESS ON AREA IS 0.315 IN IAW SRM A320 THIS REPAIR CATEGORY A, PERFORMED D
- [SDR CALA2022092802535](https://openairdocs.org/sdr/CALA2022092802535.md): Skin · none · Sep 27, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > NO RECORD PROVIDED FOR AGING AIRCRAFT INSPECTION AND RECORD REVIEW TO ACCOUNT FOR INSTALLATION AND RE-INSPECTION STATUS OF EXISTING DOUBLER ON EXTERIOR FUSELAGE FRAME 69-70 STRINGER 29-30R. SEE AEROMAN NON ROUTINE 2022-308928 LAGE SKIN AT FR69/FR70 BETWEEN 5-3
- [SDR CALA2022092602520](https://openairdocs.org/sdr/CALA2022092602520.md): None · damaged · Sep 26, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > PERMANENT REPAIR "PE REPAIR AREA AND NOT FOUND CRACK INDICATION. GENER RFORMED DVI ON INTERNAL AND EXTERNAL REPAIR AREA AND STRUCTURE PERFORMED HFEC INSPECTION ON INTERNAL AND EXTERNAL SKIN AT ATE A 2ND DIP THAT REFERENCE THE LOG PAGE NUMBER OF DTA DIP FOR AND
- [SDR CALA2022092602494](https://openairdocs.org/sdr/CALA2022092602494.md): Skin · corroded · Sep 24, 2022 · N439UA · Airbus A300* · Fuselage Structure (General)
  > CORROSION SKIN BTW FR 69 TO FR 70 AND BTW STR 1L TO STR 2L ON UP PER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-308664. AIRED AREA OF FUSELAGE SKIN AT FR69/70 BETWEEN S-2 LH AND S-2RH ABOVE FOR PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION CTION DONE ON CUT O
- [SDR CALA2022092302461](https://openairdocs.org/sdr/CALA2022092302461.md): None · cracked · Sep 22, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 WEB HORIZONTAL FLANGE AT STGR22 LEV EL RH SIDE, CRACK LENGHT IS 0.768 INCH APPROX, CONTACT ENGINEERI NG FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-308629. NITIAL INSPECTIONS O
- [SDR CALA2022091902416](https://openairdocs.org/sdr/CALA2022091902416.md): Skin · corroded · Sep 19, 2022 · N439UA · Airbus A300* · Nacelle/Pylon Structure
  > CORROSION EXTERNAL SKIN LOC FR 69 AND 19 INCH BTW STR 1R TO STR 2R ON UPPER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-308667. AIRED AREA AS PER PART 2 OF LATEST REVISION OF EC5331-02959 ON ACHES 100000 FC BUT BEFORE REACHES 101000 FC, FM NOT RELEVANT. D HFEC AND
- [SDR CALA2022091902415](https://openairdocs.org/sdr/CALA2022091902415.md): Skin · corroded · Sep 19, 2022 · N439UA · Airbus A300* · Nacelle/Pylon Structure
  > CORROSION SKIN BTW FR 69 TO FR 70 AND BTW STR 1L TO STR 2L ON UPPER FUSELAGE. SEE AEROMAN NON ROUTINE 2022-308664. AIRED AREA OF FUSELAGE SKIN AT FR69/70 BETWEEN S-2 LH AND S-2RH ABOVE FOR PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION CTION DONE ON CUT OU
- [SDR CALA2022090502280](https://openairdocs.org/sdr/CALA2022090502280.md): None · corroded · Sep 5, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 AND STR 23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-308750 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.66 AND STR. AREA IS: 0.091", NOMINAL THICKNESS ON AREA IS: 0.150" PERFORMED IAW NTM NTM 51-10-02 AND NTM 51
- [SDR CALA2022090502279](https://openairdocs.org/sdr/CALA2022090502279.md): None · corroded · Sep 5, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL FR67 TO FR68 AND STR23L IN PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.67 TO FR.68 W:1.971IN NOMINAL THICKNESS ON AREA IS 0.315 IN IAW SRM A320 THIS REPAIR CATEGORY A, PERFORMED DETAIL VISUAL INSPECTION ON AND STR.
- [SDR CALA2022083102226](https://openairdocs.org/sdr/CALA2022083102226.md): None · none · Aug 31, 2022 · N439UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > CORROSION LOWER SILL LOCATED FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-308753 MEASURES AFTER REWORK WAS L:2.388 INCH W:1.169 INCH, ELECTRONIC CRACK AND CORROSION INDICATION NOT FOUND, IAW SRM A320 53-41-14-283-002 FIGURE 002 SHEET 01, THIS IS CALIP
- [SDR CALA2022082902221](https://openairdocs.org/sdr/CALA2022082902221.md): Doubler · cracked · Aug 29, 2022 · N439UA · Airbus A300* · Fuselage Miscellaneous Structure
  > NO RECORD PROVIDED FOR AGING AIRCRAFT INSPECTION AND RECORD REVIEW TO ACCOUNT FOR INSTALLATION AND RE-INSPECTION STATUS OF EXISTING DOUBLER ON EXTERIOR FUSELAGE FRAME 32, STRINGER 38-39L, WITH INSPECTION THRESHOLD 65,000FC (FLIGHT HOURS NOT RELEVANT) INTERVALS
- [SDR CALA2022081602093](https://openairdocs.org/sdr/CALA2022081602093.md): Floorbeam · corroded · Aug 13, 2022 · N439UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM +Y765 LOCATED FR68 TO FR70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM Y765 AND FASTENERS LOC FR66 TO F P/N: 20915A22 S/N: 003591 DUE DATE 30-MAY-2023 R70 AT AFT GALLEY AREA IAW SRM A320 51-42-11, DWG D53472000, DWG 53472092 AND DWG
- [SDR CALA2022072501868](https://openairdocs.org/sdr/CALA2022072501868.md): Angle · cracked · Jul 24, 2022 · N439UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK FRAME 66 ANS STR23L ANGLE IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-308749 REMOVED AND REPLACED FRAME 66 AND STR. 23L ANGLE IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DRAWING D53474250, PERFORMED DETAIL VISUAL INSPECTION AFFECTED AREA AND NOT FO
- [SDR CALA2022072501867](https://openairdocs.org/sdr/CALA2022072501867.md): Angle · cracked · Jul 24, 2022 · N439UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK FRAME 68 AND STR23L ANGLE IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-308751 REMOVED AND REPLACED FRAME 68 AND STR 23L ANGLE IN PASSENGER CABIN IAW SRM A320 51-72-11 AND DWG D53474250, PERFORMED DETAIL VISUAL INSPECTION ON AFFECTED AREA AND NOT FOUN
- [SDR CALA2022072001842](https://openairdocs.org/sdr/CALA2022072001842.md): None · missing · Jul 20, 2022 · N439UA · Airbus A300* · Fuselage Floor Panel
  > MISSED DRILL FLOOR BEAM -Y765 LOCATED FR65 TO FR66 AT AFT GALLE Y AREA REMOVED AND REPLACE FLOOR BEAM -Y765 LOCATED FR64 TO FR66 AT AFT GALLEY AREA IAW A320 SRM 51-72-911-001 AND DWG D53472200 AND D4949524 ADD EMP:V939311
- [SDR CALA2022072001829](https://openairdocs.org/sdr/CALA2022072001829.md): Beam · corroded · Jul 19, 2022 · N439UA · Airbus A320232 · Fuselage Main, Frame
  > CORROSION FLOOR STRUCTURE LOCATED FR 16 AND Y503.2 IN PASSENGER CABIN REMOVED AND REPLACED FLOOR BEAM Y503.2 LOCATED BTW FR12 TO FR16 DUE DATE: OCT 09 2022; DEPTH GAGES PN:20915A22 SN: IN PASSENGER CABIN IAW A320 SRM 51-72-11-911-001, A320 SRM 003591, DUE DAT
- [SDR CALA2022072001817](https://openairdocs.org/sdr/CALA2022072001817.md): Beam · corroded · Jul 18, 2022 · N439UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION SEAT TRACK Y-765 LOCATED FR21 IN PASSENGER CABIN (1EA) REMOVED AND REPLACED SEAT TRACK Y-765 LOCATED ON FWD GALLED AREA BTW FR12 TO FR24 IN PASSENGER CABIN IAW A320 SRM 51- 72-11 AND DWG D53110984000, D53112812001 ENTRY MADE TO REMOVE IP RESTRICTION.
- [SDR CALA2022072001816](https://openairdocs.org/sdr/CALA2022072001816.md): Beam · corroded · Jul 18, 2022 · N439UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR STRUCTURE LOCATED FR16 AND Y765 IN PASSENGER CAB IN REMOVED AND REPLACED SEAT TRACK Y765 AND FASTENER LOC. BTW FR12,DEPTH GAGES P/N: 20915A22,S/N:003591 DUE DATE: MAY 30 2023 TO FR24 IN PASSENGER CABIN IAW A320 SRM 51-42-11 AND DWG D531128
- [SDR CALA2022072001815](https://openairdocs.org/sdr/CALA2022072001815.md): Seat Track · corroded · Jul 18, 2022 · N439UA · Airbus A320232 · Fuselage Main, Structure
  > CORROSION FLOOR STRUCTURE LOCATED FR16 AND Y 1292 IN PASSENGER CABIN REMOVED AND REPLACED SEAT TRACK Y 1292 LOCATED BTW FR 12 TO FR USED: ELECTRONIC CALIPER P/N: 500-196-30,S/N:A21033544,DUE 24 IN PASSENGER CABIN IAW A320 SRM 51-72-11-911-001, DATE: OCT 09
- [SDR CALA2022072001812](https://openairdocs.org/sdr/CALA2022072001812.md): Floorbeam · misinstalled · Jul 18, 2022 · N439UA · Airbus A320232 · Fuselage Floor Panel
  > MISSED DRILL FLOORBEAM -Y1292 LOCATED FR65 TO FR66 AT AFT GALLE Y AREA REMOVED AND REPLACED FLOORBEAM -Y1292 AND FASTENERS LOC FR64 TO FR66 AT AFT GALLEY AREA IAW SRM A320 51-42-11 AND DWG D5347220 ADD EMP:V939315
- [SDR CALA2022071801807](https://openairdocs.org/sdr/CALA2022071801807.md): None · corroded · Jul 18, 2022 · N439UA · Airbus A300* · Cabin Equipment/Furnishings
  > CORROSION FLOOR BEAM +Y765 LOCATED FR68 TO FR70 AT AFT GALLEY AREA REMOVED AND REPLACED FLOOR BEAM Y765 AND FASTENERS LOC FR68 TO FR70.
- [SDR CALA2022071801806](https://openairdocs.org/sdr/CALA2022071801806.md): None · none · Jul 18, 2022 · N439UA · Airbus A320232 · Fuselage Floor Panel
  > MISSED DRILL FLOOR BEAM -Y1292 LOCATED FR65 TO FR66 AT AFT GALLEY AREA. REMOVED AND REPLACED FLOOR BEAM -Y1292 AND FASTENERS LOC FR64 TO FR66 AT AFT GALLEY AREA.
- [SDR CALA2022071801800](https://openairdocs.org/sdr/CALA2022071801800.md): Seat Track · corroded · Jul 17, 2022 · N439UA · Airbus A320232 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK LOCATED FR21 Y-1292 IN PASSENGER CABIN REMOVED AND REPLACED SEAT TRACK Y-1292 AND FASTENER LOC. BTW 500-196-30, S/N: A21033544, DUE DATE; OCT 09 2022,DEPTH FR12 TO FR24 IN PASSENGER CABIN AND SPLICE (1EA) LOC. GAGES P/N; 20915A22, S/N 003
- [SDR CALA2022071501774](https://openairdocs.org/sdr/CALA2022071501774.md): Seat Track · corroded · Jul 15, 2022 · N439UA · Airbus A320232 · Passenger/Crew Doors
  > CORROSION FLOOR STRUCTURE LOCATED FR16 AND Y 1292 IN PASSENGER CABIN REMOVED AND REPLACED SEAT TRACK Y 1292 LOCATED BTW FR 12 TO FR USED: ELECTRONIC CALIPER P/N: 500-196-30,S/N:A21033544,DUE 24 IN PASSENGER CABIN IAW A320 SRM 51-72-11-911-001, DATE: OCT 09
- [SDR CALA2022071501773](https://openairdocs.org/sdr/CALA2022071501773.md): Seat Track · corroded · Jul 15, 2022 · N439UA · Airbus A320232 · Passenger/Crew Doors
  > CORROSION SEAT TRACK Y-765 LOCATED FR21 IN PASSENGER CABIN (1EA) REMOVED AND REPLACED SEAT TRACK Y-765 LOCATED ON FWD GALLED AREA BTW FR12 TO FR24 IN PASSENGER CABIN IAW A320 SRM 51- 72-11 AND DWG D53110984000, D53112812001

Next page: https://openairdocs.org/aircraft/N439UA/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 = 'N439UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N439UA/reports

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