# Service difficulty reports: N486UA

A list on [N486UA](https://openairdocs.org/aircraft/N486UA.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 · 108 reports

- [SDR CALA2025052204901](https://openairdocs.org/sdr/CALA2025052204901.md): Battery · discharged · May 21, 2025 · N486UA · Airbus A320232 · Emergency Lighting
  > INT LOADS EMERGENCY L FAULT REMOVAL AND REPLACED EMERGENCY EXIT LH BATTERY OF THE EMERGENCY POWER SUPPLY UNIT (EPSU) IAW AMM TASK 33-51-38-400-002-A, OK TO SERVICE.
- [SDR CALA2024051301457](https://openairdocs.org/sdr/CALA2024051301457.md): Frame · cracked · May 9, 2024 · N486UA · Airbus A320232 · Fuselage Main, Frame
  > LH FR 16 UPPER DOUBLE JOGGLE AREA, HOLE 6 HAS CRACK INDICATION I N FRAME LAYER 705 SCREEN HEIGHT @ 2 OCLOCK DIRECTION. REPAIRED LH FR16 DOUBLE JOGGLE AREA HOLE# 6 PER ECRA 5311-03211 ALLOWING DEVIATION TO EA 5311-0442 OPS 001, REFERANCE SRM OK TO CARRY PER S
- [SDR CALA2023122003689](https://openairdocs.org/sdr/CALA2023122003689.md): Skin · corroded · Dec 19, 2023 · N486UA · Airbus A320232 · Passenger/Crew Doors
  > CORROSION AROUND LAV VACUUM EXHAUST PORT. LOCATED AFT AND BELOW R2 CABIN DOOR. COMPLIED WITH FINAL VTMAE EA320-5341-13-A3456 REV A AND UAL EC/R A 5341-01423 REV A.
- [SDR CALA2023122003681](https://openairdocs.org/sdr/CALA2023122003681.md): Skin · corroded · Dec 19, 2023 · N486UA · Airbus A320232 · Wing, Plate/Skin
  > DURING OK TO CLOSE INSPECTION PANEL 621BT, ON RH WING TOP SKIN PANEL APPROX RIB 10 AND STRINGER 11, A CORROSION SPOT WAS FOUND. IDT, COMPLIED WITH FINAL VTMAE EA 320-5720-13-A3467 REV- AND UAL EC/RA #5721-01484,IDT.
- [SDR CALA2023102703207](https://openairdocs.org/sdr/CALA2023102703207.md): Thrust Reverser · warning message · Oct 24, 2023 · N486UA · Airbus A320232 · Engine Thrust Reverser
  > REVERSER FAULT DISPLAYED ON UPPER ECAM SCREEN. ENG 1 FADEC CLASS 2 UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V082625 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. LOCAL FBO TO MAC RELATED WORK ORDER 0000000030888
- [SDR CALA2023041001084](https://openairdocs.org/sdr/CALA2023041001084.md): Flap System · faulty · Apr 9, 2023 · N486UA · Airbus A320232 · Trailing Edge Flap Control System
  > FLAPS FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL ECAM FOLLOWED TRAILINGEDGE FLAPS RAMAINED UPLEADING EDGE DEVICES DEPLOYED LOCKED BY TOMC PER TOMC SR MGR CFDS HITS THE FLAP MECH DRIVE UNIT. WHEN DEPLOYING THE FLAP HANDLE THE TORQUE TUBES SPIN A FEW ROTATION
- [SDR CALA2023031700779](https://openairdocs.org/sdr/CALA2023031700779.md): Motor · defective · Mar 16, 2023 · N486UA · Airbus A320232 · Hydraulic Filter, Main
  > FLIGHT CREW REPORTS TO TOMC HYD B ELEC PUMP OVHT, HYD B SYS LO PR, C/W QRH ELEC PUMP OFF, OVHT MSG WENT OUT. VARGAS TOMC LOCKED BY TOMC UNLOCKED FOR CLEARING ACTION AT STATION R&R BLUE HYD ELEC PUMP IAW AMM 29-12-51 OPS CHECK GOOD NO LEAK NOTED AT THIS TIME OK
- [SDR CALA2022022400496](https://openairdocs.org/sdr/CALA2022022400496.md): Battery Pack · failed · Feb 24, 2022 · N486UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: {A3NB-33-3-6012} - EPSU TEST FAULTS EPSU BATTERY EMER R. 33-51-38. REPLACED BATTERY PACK, IAW AMM 33-51-38-400-002-AO, RETESTED GOOD.
- [SDR CALA2022010300018](https://openairdocs.org/sdr/CALA2022010300018.md): Brake Sys · warning message · Jan 3, 2022 · N486UA · Airbus A300* · Brake
  > *EMERGENCY DECLARED* AUTO BRAKES FAULT ON APPROACH. PFR SHOWS FAULTING 16GG SERVO. PERFORMED BSCU CHANNEL 1 AND 2 AUTOBRAKE AND NORMAL BRAKE BITE 32-42-00 AND 32-46-00. TEST, BRK NORM SERVO VALVE 3 (16GG) ON BSCU 2 CONNECTOR FAULTED. FOUND MOISTURE BUILD UP ON
- [SDR CALA2021120802300](https://openairdocs.org/sdr/CALA2021120802300.md): None · failed · Dec 7, 2021 · N486UA · Airbus A320232 · Hydraulic Power Accumulator, Main
  > HYD G ENG 1 PUMP LO PR ON ECAM TS FOUND NUMBER ONE ENGINE HYD PUMP SHAFT BROKEN. INSPECTED CASE WORKS NORMALY. CYCLED HYD AUCTORS. CK OK. CLOSED ENGINE COWLING DRAIN FOUND FILTER CLEAN. REINSTALLED PER AMM 29-11-43 NO ROTABLE PARTS CHANGE WAS INDICATED - TT #
- [SDR CALA2021120102218](https://openairdocs.org/sdr/CALA2021120102218.md): Structure · corroded · Dec 1, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6299) AFT RH FR68 AT STRG23 HAS CORROSION. DOT 52-46 () WORK PER FINAL EA 320-5341-13-A2716 REV - AND UAL ECRA 5341-0128 6 ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPACE MOBILE. NR#001 5810.
- [SDR CALA2021120102206](https://openairdocs.org/sdr/CALA2021120102206.md): Hinge Arm · delaminated · Nov 30, 2021 · N486UA · Airbus A320232 · Flight Control System
  > (A3NB-55-3-6005) LH ELEVATOR #4 HINGE ARM IS DELAM. (REMOVE AND REPLACE DELAM LH #4 ELEVATOR HINGE ARM) REMOVED AND REPLACED LH #4 ELEVATOR HINGE ARM PN#D5598152200200 BFM ST AEROSPACE MOBILE. NR#0016181 IAW SRM 51-42-21 & SRM 51-72-11-911-001. REMOVED AND REI
- [SDR CALA2021120102205](https://openairdocs.org/sdr/CALA2021120102205.md): Lever · chipped · Nov 30, 2021 · N486UA · Airbus A320232 · Empennage Structure
  > A3NB-55-3-6005 RH ELEVATOR HINGE ARM LWR EDGE I/B SIDE CHIPPED D OT 42-070 () REMOVED LINES HYD ACCESS IAW AMM 27-34-51-000-001-A. RECEIVED NE W PART P/N D55981442003002 B/N 0003855407 LOCATED AND DRILLED IA W SRM 51-44-21 INSTALED NEW PART IAW SRM 51-42-21/00
- [SDR CALA2021112902183](https://openairdocs.org/sdr/CALA2021112902183.md): Stringer · corroded · Nov 28, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > AFT CRG COMPT: FLOOR BILDGE STR38 RH BETWEEN FR58 AND FR59 HAS C ORROSION EVIDENCE. DOT 61-047 (A3NB-53-4-6179) () REPAIR @ STR 38 R/H FR C58-C59 ACCOMPLISHED ON FINAL EA 320-5341 -13-A2728 AND UAL EC/RA 5341-01285. REPAIR CATEGORY A. ACCOMPLIS HED BY EMP#V934
- [SDR CALA2021112902181](https://openairdocs.org/sdr/CALA2021112902181.md): Stringer · corroded · Nov 28, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > AFTG CRG COMPT: FLOOR BILDGE STR37 RH BETWEEN FR59 AND FR60 HAS CORROSION EVIDENCE. DOT 61-48 (A3NB-53-4-6179) () REPAIR @ STR 37 R/H FR C59-C60, ACCOMPLISHED ON FINAL EA 320-534 1-13-A2728 AND UAL EC/RA 53-41-01285 REPAIR CATEGORY A. ACCOMPLI SHED BY EMP#V934
- [SDR CALA2021112902185](https://openairdocs.org/sdr/CALA2021112902185.md): Frame · corroded · Nov 28, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6299) AFT RH FR68 AT STRG23 HAS CORROSION. DOT 52-46 ()
- [SDR CALA2021112302163](https://openairdocs.org/sdr/CALA2021112302163.md): Beam · corroded · Nov 22, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > A3NB-53-3-6038 CABIN FLOOR STRUCTURE SUPPORT BEAM HAVE CORROSION FR 16 Y518 DOT 42-052 () REMOVED AND REPLACED CABIN SUPPORT BEAM AT FR12-24 Y518 IAW SRM RUDDER IAW AMM 27-24-00-710-001-A CHECK GOOD ACCOMPLISHED BY EMP 51-42-11 & SRM 51-21-14. INSTALLED CABLE
- [SDR CALA2021112202152](https://openairdocs.org/sdr/CALA2021112202152.md): Stringer · corroded · Nov 21, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6299) R/H FR66-68 STR24R HAS CORROSION (REMOVE AND RE PLACE STRINGER OR REPAIR) REMOVED DAMAGED STRINGER SECTION 24R FR 64-67, INSTALLED NEW STR INGER SECTION 24R FR 64-67 P/N D5348004720801 AND AFT STR TIES A ND SHEAR TIES REMOVED TO FOM IAW SRM 51
- [SDR CALA2021112202142](https://openairdocs.org/sdr/CALA2021112202142.md): Beam · corroded · Nov 19, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6222) FLOOR BEAM Y1162.5 BETWEEN FR 68/69 HAS CORROSI ON. 52-42 () FLOOR BEAM Y1162.5 BETWEEN FR68-FR69 REMOVED AND REPLACED IAW SR M 51-72-11. ACCOMPLISHED BY EMP#V933868 AT BFM ST AEROSPACE MOBI LE. NR#0015806
- [SDR CALA2021112202141](https://openairdocs.org/sdr/CALA2021112202141.md): Door Sill · corroded · Nov 19, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6299) AFT RH DOOR SILL HAS CORROSION IN SEVERAL LOCAT IONS. DOT 52-45. REMOVED AND REPLACED AFT R2 DOOR SILL IAW SRM 51-42-11, DWG D534 80595. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. N R#0015809
- [SDR CALA2021111502102](https://openairdocs.org/sdr/CALA2021111502102.md): Seat Track · damaged · Nov 14, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-05-3-6018) O/B R/H SEAT TRACK HAS CROWN DAMAGE AT F/R 44. DOT 09/09 () O/B RH SEAT TRACK AT FR44 REPLACED IAW SRM 51-72-11-911-002. P/N D537111320300 B/N:0003856506. ACCOMPLISHED BY EMP#V933868 AT ST AEROSPACE MOBILE. NR#0015757
- [SDR CALA2021111502101](https://openairdocs.org/sdr/CALA2021111502101.md): Beam · corroded · Nov 14, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6186) SEAT TRACK OVER FLOOR BEAM Y1292 FR57 TO FR64 H AS SEVERAL SPOTS WITH CORROSION. DOT 52-51.() REMOVED DAMAGED FLOOR SEAT TRACK FR47-64 IAW SRM 51-42-11. INSTA LLED NEW FLOOR SEAT TRACK P/N# D5397217620400 BATCH# 0003863708 IAW SRM 51-42-11. EM
- [SDR CALA2021111502108](https://openairdocs.org/sdr/CALA2021111502108.md): Beam · corroded · Nov 14, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM Y512.5 BEYWEEN FR 69/70 HAS CORROSIO N. DOT 52-35()
- [SDR CALA2021110302023](https://openairdocs.org/sdr/CALA2021110302023.md): Stringer · corroded · Nov 2, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (A3NB-53-4-6179) AFT CRG COMPT: STR41 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE DOT 61-056. IAW SRM 51-42-11/001 AND NDT''D CUT OUT IAW NTM 51-10-08 PART 6. SRM 53-00-13-300-001 FIG 001 SHEET 5 INSTALLED STRINGER REPAIR INSPECTION THRESHOLD FROM TIME OF
- [SDR CALA2021110302026](https://openairdocs.org/sdr/CALA2021110302026.md): Seat Track · damaged · Nov 2, 2021 · N486UA · Airbus A320232 · Standard Practices/Structures
  > (A3NB-05-3-6018) RH O/B SEAT TRACK BETWEEN F/R 38-39 HAS DAMAGE ON CROW AREA. DOT 09/06 () R/H O/B SEAT TRACK BETWEEN FR38-FR39 REPLACED IAW SRM 51-72-11-9 11-002 P/N D5713014720302 B/N:0003857847 ACCOMPLISHED BY EMP#V93 3868 AT BFM ST AEROSPACE MOBILE. NR#001
- [SDR CALA2021110302025](https://openairdocs.org/sdr/CALA2021110302025.md): Stringer · corroded · Nov 2, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (A3NB-53-4-6179) AFT CRG COMPT: STR42 LH BETWEEN FR63 AND FR64 H AS CORROSION EVIDENCE. DOT 61-055 IAW SRM 51-42-11/001 AND NDT''D CUT OUT IAW NTM 51-10-08 PART 6. SRM 53-00-13-300-001 FIG 001 SHEET 5. INSTALLED STRINGER REPAIR INSPECTION THRESHOLD FROM TIME O
- [SDR CALA2021110302022](https://openairdocs.org/sdr/CALA2021110302022.md): Stringer · corroded · Nov 2, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO COMPT FLOOR BILDGE STR39 RH FR61 HAS CORROSION EVIDENCE. DOT 61-052 0003827275 AND COUPLING A53986217 BATCH 0003853799 IAW SRM SHEETS 02 AND 05. WORK ACCOMPLISHED ON VT MAE N/R 0015734 BY OF ADL/REPAIR EMBODIMENT FC 60000 / FH 120000 WHICHEVER ACHIEV
- [SDR CALA2021110302024](https://openairdocs.org/sdr/CALA2021110302024.md): Stringer · corroded · Nov 2, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO COMP: FLOOR BILDGE STR42 LH FR55 HAS CORROSION EVIDENCE. DOT 61-046 BATCH 000382727 AND COUPLING A53986217 BATCH 0003853799 IAW SRM 04, 05 & 06. WORK ACCOMPLISHED ON VT MAE N/R 0015728 BY VT MAE /REPAIR EMBODIMENT FC 60000 / FH 120000 WHICHEVER ACHIE
- [SDR CALA2021102902002](https://openairdocs.org/sdr/CALA2021102902002.md): None · corroded · Oct 28, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (A3NB-53-4-6179) AFT CRG COMPT: FLOOR BILDGE STR41 LH BETWEEN FR 53 AND FR54 HAS CORROSION EVIDENCE. DOT 61-45 FOUND STR41L FR53-54 OUT OF LIMITS IAW SRM 53-41-13-283-002 FIG 003. REMOVED AND INSTALLED NEW STRINGER IAW SRM 51-42-11. P/N D5 347042020800 BATCH 0
- [SDR CALA2021102601979](https://openairdocs.org/sdr/CALA2021102601979.md): None · none · Oct 26, 2021 · N486UA · Airbus A320232 · Fuselage Main, Attach Fittings
  > (A3NB-53-4-6179) AFT CRG COMPT: FLOOR BILDGE STR41 LH BETWEEN FR 53 AND FR54 HAS CORROSION EVIDENCE. DOT 61-45
- [SDR CALA2021102201956](https://openairdocs.org/sdr/CALA2021102201956.md): None · none · Oct 22, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803
- [SDR CALA2021102201951](https://openairdocs.org/sdr/CALA2021102201951.md): Beam · none · Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > A3NB-53-3-6038 CABIN FWD FLOOR STRUCTURE SUPPORT BAM HAVE CORROS ION FR20 Y254 DOT 42-047 () REPLACED SUPPORT BAM P/N D5311146100200 BATCH:0003854609 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001. Y254 BETWEEN FR 12 TO F R 24. ACCOMPLISHED BY EMP#V935834 AT
- [SDR CALA2021102201950](https://openairdocs.org/sdr/CALA2021102201950.md): Beam · none · Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802
- [SDR CALA2021102201949](https://openairdocs.org/sdr/CALA2021102201949.md): Seat Track · none · Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > A3NB-53-3-6038 CABIN FLOOR SEAT TRACK Y-1292 FR20 HAVE WEAR MARK S AND GOUGES. DOT 42-053 EVALUATED FLOOR BEAM IAW SRM A320 53-00-15-283-002 FOUND OUT OF LIMITS, REPLACED BY NEW FLOOR BEAM PN:D5311278220201 BATCH:00038 6549, REPLACED IAW A320 SRM 51-42-11-001.
- [SDR CALA2021102201948](https://openairdocs.org/sdr/CALA2021102201948.md): Beam · none · Oct 21, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6222) FLOOR BEAM -Y765 BETWEEN FR 66/70 HAS CORROSIO N. DOT 52-40 () REMOVED AND REPLACED FLOOR BEAM BETWEEN FR66 TO 70 AT -Y765 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT BFM ST AEROSPA CE MOBILE. NR 0015803
- [SDR CALA2021102001936](https://openairdocs.org/sdr/CALA2021102001936.md): Floorbeam · corroded · Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > A3NB-53-3-6038 CABIN FWD FLOOR STRUCTURE SUPPORT BAM HAVE CORROS ION FR20 Y254 DOT 42-047 () REPLACED SUPPORT BAM P/N D5311146100200 BATCH:0003854609 IAW A32 0 SRM 51-42-11 AND SRM 51-72-11-911-001. Y254 BETWEEN FR 12 TO F R 24. ACCOMPLISHED BY EMP#V935834 AT
- [SDR CALA2021102001935](https://openairdocs.org/sdr/CALA2021102001935.md): None · none · Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLT) ROTO PROBE OF LH FR16 #7 DOOR STOP FITT ING HOLES FOUND CRACKS AT THE I/B UPPER AND I/B LOWER HOLES. CRA CKS ARE IN THE INTERCOSTAL ONLY. () REPAIRED L/H FR16 #7 DOOR STOP FITTING HOLES BY REPLACING INTERC OSTAL FITTING ON EC/RA 5311-0
- [SDR CALA2021102001934](https://openairdocs.org/sdr/CALA2021102001934.md): Floorbeam · corroded · Oct 20, 2021 · N486UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > (A3NB-53-3-6222) FLOOR BEAM Y254 BETWEEN FR 66/68 HAS CORROSION DOT 52-39 REMOVED AND REPLACED FLOOR BEAM Y254 BETWEEN FR 66/68 P/N D53472 17320100 IAW A320 SRM 51-42-11. ACCOMPLISHED BY EMP#V935833 AT S T AREORSPACE MOBILE. NR#0015802
- [SDR CALA2021101801917](https://openairdocs.org/sdr/CALA2021101801917.md): Intercostal · cracked · Oct 17, 2021 · N486UA · Airbus A320232 · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLT) ROTO PROBE OF LH FR16 #7 DOOR STOP FITT ING HOLES FOUND CRACKS AT THE I/B UPPER AND I/B LOWER HOLES. CRA CKS ARE IN THE INTERCOSTAL ONLY. ()
- [SDR CALA2021101801915](https://openairdocs.org/sdr/CALA2021101801915.md): Intercostal · cracked · Oct 17, 2021 · N486UA · Airbus A320232 · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLT) ROTO PROBE OF RH FR16 #7 DOOR STGOP FIT TIING HOLE FOUND CRACKS AT THE I/B TOP AND I/B BOTTOME HOLES. CR ACKS ARE IN THE INTERCOSTAL ONLY. ()
- [SDR CALA2021101801914](https://openairdocs.org/sdr/CALA2021101801914.md): Beam · corroded · Oct 17, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM Y1162.5 BETWEEN FR 68/69 HAS CORROSI ON. DOT 52-32 () REMOVED AND REPLACE FLOOR BEAM Y1162.5 FR 68-69 AND HARD POINT I AW SRM 51-42-11. ACCOMPLISHED BY EMP#V933438 AT ST AEROSPACE MOB ILE. NR#0015797
- [SDR CALA2021101801913](https://openairdocs.org/sdr/CALA2021101801913.md): Beam · corroded · Oct 17, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM Y1292 BETWEEN FR 68/70 HAS CORROSION DOT 52-32. () REMOVED AND REPLACED FLOOR BEAM Y1292 FR 68-70 AND HARD POINTS O N W/C 15797. ACCOMPLISHED BY EMP#V933438 AT ST AEROSPACE MOBILE. NR#0015795
- [SDR CALA2021101801912](https://openairdocs.org/sdr/CALA2021101801912.md): Beam · corroded · Oct 17, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM Y1292 BETWEEN FR 64/66 HAS CORROSION. DOT 52-31 () REMOVED AND REPLACE FLOOR BEAN Y1292 FR 64-66 AND 5 EA BRACKET A SSY IAW SRM 51-42-11. ACCOMPLISHED BY EMP#V923438 AT ST AEROSPAC E MOBILE. NR#0015794
- [SDR CALA2021101801911](https://openairdocs.org/sdr/CALA2021101801911.md): Beam · corroded · Oct 17, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM Y765 BETWEEN FR 64/66 HAS CORROSION DOT 52-30. () REPLACED FLOOR BEAM Y765 BETWEEN FR66 AND FR69. P/N D53472090002 000 BATCH:0003830224 IAW A320 SRM 51-42-11 AND SRM 51-72-11-911- 001. ACCOMPLISHED BY EMP#V934700 AT ST AEROSPACE MOB
- [SDR CALA2021101401878](https://openairdocs.org/sdr/CALA2021101401878.md): None · none · Oct 14, 2021 · N486UA · Airbus A320232 · Cabin Equipment/Furnishings
  > (A3NB-25-3-6221) FLOOR BEAM -Y765 BETWEEN FR 68/70 HAS CORROSION DOT 52-33 () REMOVED AND REPLACED FLOOR BEAM P/N D5347209200000 BETWEEN FR 68 /70 IAW SRM 51-42-11.
- [SDR CALA2021101101847](https://openairdocs.org/sdr/CALA2021101101847.md): Beam · corroded · Oct 10, 2021 · N486UA · Airbus A320232 · Fuselage Structure (General)
  > (A3NB-25-3-6221) FLOOR BEAM -Y765 BETWEEN FR 68/70 HAS CORROSION DOT 52-33 () REMOVED AND REPLACED FLOOR BEAM P/N D5347209200000 BETWEEN FR 68 /70 IAW SRM 51-42-11.
- [SDR CALA2018091901952](https://openairdocs.org/sdr/CALA2018091901952.md): Engine · failed · Sep 16, 2018 · N486UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > ENG 1 FAIL IN FLIGHT ON CLIMBOUT. UNABLE TO RELIGHT. DEBRIEFED CREW. ON CLIMBOUT PASSING THRU 12K THE LT ENGINE VERY LOUD BANG AND IMMEDIATE SHUT DOWN. NO FIRE INDICATION BUT CREW BLEW BOTTLE AS PRECAUTION. PASSENGERS SAID NO FLAME VISIBLE. NO INDICATION OF BI
- [SDR CALA2017091103155](https://openairdocs.org/sdr/CALA2017091103155.md): Power Supply · failed · Sep 11, 2017 · N486UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT POWER SUPPLY UNIT FAILED AT THE L1 DOOR. REPLACED THE EPSU IAW AMM 33-51-38-00-0-001.
- [SDR CALA2017091103154](https://openairdocs.org/sdr/CALA2017091103154.md): Safety Wire · broken · Sep 11, 2017 · N486UA · Airbus A320232 · Escape Slide
  > LEFT AFT PAX DOOR EVACUATION SLIDE RELEASE BAR MECHANISM SAFETY WIRE BROKEN. REPLACED LH AFT SLIDE ASSY PER AMM 25-62-44/401
- [SDR CALA2017041000943](https://openairdocs.org/sdr/CALA2017041000943.md): Skin · dented · Apr 10, 2017 · N486UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > DENT NOTED ON LOWER FUSELAGE 2" AFT OF FR24 BETWEEN STR 41L AND STR 42L. DENT MEASURES 7.5"L X 4.5"W X 0.425"D. FABRICATED REPAIR DOUBLER/FILLER, ALODINED AND PRIMED. INSTALLED REPAIR IAW 5854 REV B STEP 9. REPAIR WAS ACCOMPLISHER PER ECRA 5321-01943.

Next page: https://openairdocs.org/aircraft/N486UA/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 = 'N486UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N486UA/reports

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