# Service difficulty reports: N854UA

A list on [N854UA](https://openairdocs.org/aircraft/N854UA.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 2 · 96 reports

- [SDR CALA2026052016423](https://openairdocs.org/sdr/CALA2026052016423.md): Controller · faulted · May 18, 2026 · N854UA · Airbus A319131 · Cabin Temperature Control System
  > COND ZONE REGUL FAULT EC AM ON CLB. TEMP CLBED AN D MAINTANED AB OVE 90F UNTIL DESCENT T/S PER TSM TASK 21-63-00-810-827-A & R/R ZONE TEMP CNTRL. PER AMM 21-83-34-400-001-A. OPS CHECK PASS OPS CHK TEMP CONTROL SYS PER AMM 21-63-00-710-004-A. NO FAULTS FOUN
- [SDR CALA2026050115916](https://openairdocs.org/sdr/CALA2026050115916.md): Frame · mechanic error · Apr 29, 2026 · N854UA · Airbus A319131 · Fuselage Main, Frame
  > AFT CARGO BAY FR. 60 LT FASTENER HOLE STRINGER 37 VERTICAL FLANGE HOLE MISDRILLED. FASTENER HOLE AT FRAME 60, STRINGER 37 LEFT, VERTICAL FLANGE REPAIRED PER EC/RA 5341-01568 AND REQUIRES REPETITIVE INSPECTIONS.
- [SDR CALA2026042915829](https://openairdocs.org/sdr/CALA2026042915829.md): Fitting · cracked · Apr 19, 2026 · N854UA · Airbus A319131 · Fuselage Main, Structure
  > FLIGHT DECK, WINDSHEILD CONTINUITY FITTING LT AND RT HAS CRACK I NDICATION APROX..40 INCH FROM CENTER POST. PERFORMED INTERIM REPAIR IAW ECRA 5311-03450 AND REO-L25896 REV IR WITH NO DEVIATIONS. PAR T 2: ACCOMPLISH INITIAL INSPECTIONS AT FRONT WINDSHIELD F
- [SDR CALA2026042215594](https://openairdocs.org/sdr/CALA2026042215594.md): Bracket · damaged · Apr 19, 2026 · N854UA · Airbus A319131 · Fuselage Main, Attach Fittings
  > AFT CARGO PIT FRM 60 L/H STRGR 37 REQUIRES FABRICATION OF SUPPOE RT (D5347032201200). GENERATED BY V945000 ON AAR LCQ NR 9298495 / 30495 UPDATED EFSR FABRICATED NEW SUPPORT FOR AFT CARGO PIT FR 60 L/H STRGR 37 IAW A319 SRM 51-26-11-911-001-A AND 51-27-11-911-0
- [SDR CALA2026041415365](https://openairdocs.org/sdr/CALA2026041415365.md): Frame Angle · cracked · Apr 11, 2026 · N854UA · Airbus A319131 · Fuselage Main, Structure
  > R/H EMERGENCY EXIT HATCH AFT VERTICAL FRAME HAS A CRACK AT FASTENER. R & R VERTICAL FR ON R/H EMERGENCY EXIT HATCH IAW SRM 51-42-11
- [SDR CALA2026020213515](https://openairdocs.org/sdr/CALA2026020213515.md): Battery · no test · Feb 2, 2026 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY AFT LEFT, MESSAGE AFTER EMERGENCY LIGHTS TEST. REMOVED AND REPLACED EPSU BATTERY IAW AMM 33-51-38. TESTED OK.
- [SDR CALA2025102710578](https://openairdocs.org/sdr/CALA2025102710578.md): Power Supply · faulty · Oct 25, 2025 · N854UA · Airbus A319131 · Emergency Lighting
  > FWD LEFT EMERGENCY POWER SUPPLY UNIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT PSEU PER AMM 33-51-38. OPS CHECK GOOD. TEST OK.
- [SDR CALA2025102010291](https://openairdocs.org/sdr/CALA2025102010291.md): Light · no test · Oct 20, 2025 · N854UA · Airbus A319131 · Emergency Lighting
  > REQUIRES TO PERFORM CABIN EMERGENCY LIGHT CHECK PER TASK CARD 18-3351-1-0003 ON SC. PERFORMED CABIN EMERGENCY LIGHT CHECK PER TASK CARD 18-3351-1-0003 ON SC.
- [SDR CALA2025072106757](https://openairdocs.org/sdr/CALA2025072106757.md): Battery Pack · no test · Jul 19, 2025 · N854UA · Airbus A319131 · Emergency Lighting
  > DURING EMERG LIGHT CHECK FOUND FAULT EPSU UNIT FWD L REF AMM 33-51-38 REPLACED EPSU BATTERY. OPS TEST GOOD AT THIS TIME. UPDATING SDR
- [SDR CALA2024071102002](https://openairdocs.org/sdr/CALA2024071102002.md): Control Valve · inoperative · Jul 3, 2024 · N854UA · Airbus A319131 · Cabin Cooling System
  > ON CLIMB OUT-COCKPIT HADALMOST NO AIRFLOW-RESULT OVERHEATED. RETURNED TO DEP AIRPORT. REMOVED AND REPLACED #1 PACK FLOW CONTROL VALVE REF AMM 21-51-51/401. OPS CHECK AND LEAK CHECK GOOD.
- [SDR CALA2024070500146](https://openairdocs.org/sdr/CALA2024070500146.md): Control Valve · faulty · Jul 3, 2024 · N854UA · Airbus A319131 · Cabin Cooling System
  > ON CLIMB OUT-COCKPIT HADALMOST NO AIRFLOW-RESULT OVERHEATED-RETU RNED TODEP AIRPORT. VALVE, FLOW CON OFF 31-2161-9-0002 2267 ON 31-2161-9-0002 1734 VALVE, FLOW CON OFF 31-2161-9-0002 2267 ON 0000 REMOVED AND REPLACED #1 PACK FLOW CONTROL VALVE REF AMM 21-51-51
- [SDR CALA2024042601245](https://openairdocs.org/sdr/CALA2024042601245.md): Fuel Cap · missing · Apr 24, 2024 · N854UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTED FUEL CAP MISSING CDL REQUESTED VERIFIED NO LEAKS CDL 28A REJECTING FOR SIGN OFF INSTALLED REFUEL/DEFUEL COUPLING/CAP IN REF AMM 28-25-41. NO PARTS TAG PIC ADDED REQUIRES A PDA REPORT DUE TO PART MISSING DEFECT NOTED. PDA REPORT COMPLETED REF LO
- [SDR CALA2024042401212](https://openairdocs.org/sdr/CALA2024042401212.md): Fuel Cap · missing · Apr 24, 2024 · N854UA · Airbus A319131 · Fuel Storage
  > PDA 2 PDA REPORTED DUE TO FUEL CAP MISSING. FUEL CAP INSTALLED SEE REF LOG 7752261. TOMC ADVISED. MISSIBG FUEL CAP HAS BEEN INSTALLED UNDER LP 7752261. NO FUTHER ACTION REQUIRED. SAME LP MARKED AS SDR.
- [SDR CALA2023072102295](https://openairdocs.org/sdr/CALA2023072102295.md): Battery · inoperative · Jul 20, 2023 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (13WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. REPLACEMENT PERFORMED IAW AMM:33-51-38-000-002/33-51-38-400-002 REV 120. P/N OFF:AD3214-31 S/N OFF:287690, P/N ON:AD3214-31, S/N ON:291649. EPSU BATTERY (13WL) FAI
- [SDR CALA2023072102294](https://openairdocs.org/sdr/CALA2023072102294.md): Battery · inoperative · Jul 20, 2023 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (12WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. REPLACEMENT PERFORMED IAW AMM:33-51-38-000-002/33-51-38-400-002 REV 120. P/N OFF:AD3214-31 S/N OFF:287725, P/N ON:AD3214-31, S/N ON:295191. EPSU BATTERY (12WL) FAI
- [SDR CALA2023072102293](https://openairdocs.org/sdr/CALA2023072102293.md): Battery · inoperative · Jul 20, 2023 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (11WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. REPLACEMENT PERFORMED IAW AMM:33-51-38-000-002/33-51-38-400-002 REV 120. P/N OFF:AD3214-31 S/N OFF:291022, P/N ON:AD3214-31, S/N ON:292643. EPSU BATTERY (11WL) FAI
- [SDR CALA2023072102292](https://openairdocs.org/sdr/CALA2023072102292.md): Battery · inoperative · Jul 20, 2023 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY (10WL) FAILED ON EMERGENCY LIGHTNING BATTERY CAPACITY TEST AND REQUIRE REPLACEMENT. REPLACEMENT PERFORMED IAW AMM:33-51-38-00-002/33-51-38-400-002 REV 120. P/N OFF:AD3214-31, S/N OFF:287685, P/N ON:AD3214-31, S/N ON:315313. EPSU BATTERY (10WL) FAI
- [SDR CALA2023052201594](https://openairdocs.org/sdr/CALA2023052201594.md): Fuel Cap · missing · May 20, 2023 · N854UA · Airbus A319131 · Fuel Storage
  > FUEL CAP WAS REPORTED MISSING DURING PILOT WALKAROUND. FOUND FUEL CAP INSTALLED BUT FUEL LANYARD BROKEN. REMOVED AND REPLACED FUEL CAP LANYARD WITH A NEW UNIT. OPS GOOD.
- [SDR CALA2022060601430](https://openairdocs.org/sdr/CALA2022060601430.md): Uplock · out of adjust · Jun 4, 2022 · N854UA · Airbus A319131 · Landing Gear System
  > NOSE GEAR WOULD NOT RETRACT ON CLIMB OUT REMOVED AND REPLACED NLG UPLOCK ASSY IAW AMM 32-31-21-000-001-A. EMP: V9934084 WC: 28978 STA: ST ENG BFM ROTABLE PARTS CHANGE WAS INDICATED - TT # 1898198 SN OFF 3292 IPC REFERENCE # UPLOCK, ASSY, N OFF 18-3231-9-9004
- [SDR CALA2022031000632](https://openairdocs.org/sdr/CALA2022031000632.md): Idg · failed · Mar 10, 2022 · N854UA · Airbus A319131 · AC Generator-Alternator
  > ENGINE 2 GENERATOR FAILED WITH ECAM MESSAGE: ELEC GEN 2 FAULT, CREW RESET GENERATOR AND CAME BACK ONLINE BRIEFLY THEN FAULTED AGAIN. C/W # 2 ENG EEC IDT REQUIREMENTS. VERIFIED PART NUMBER EFFECTIVITY AND SECURITY OF INSTALLATION TROUBLESHOT MAINTENANCE ISSUES
- [SDR CALA2021072101144](https://openairdocs.org/sdr/CALA2021072101144.md): Floor Panel · gouged · Jul 20, 2021 · N854UA · Airbus A319131 · Fuselage Floor Panel
  > A3NB-05-3-6022 AFT CARGO FLOOR STRUCTURE I/B FROM DOOR CUTOUT BE TWEEN C58-59 HAS GOUGE. DOT 102-94() REMOVED AND REPLACED SHEET COVER ASSY P/N 5347715400400, BATCH 0 003816227 IAW A319 SRM 51-42-11. RESORED FINISHED PROTECTION IAW A319 SRM 51-75-12. ACCOMPLIS
- [SDR CALA2021072101142](https://openairdocs.org/sdr/CALA2021072101142.md): Rib · damaged · Jul 19, 2021 · N854UA · Airbus A319131 · Leading Edge Devices
  > (A3NB 17-5700-1-2915) UPON REMOVAL OF LH #4 SLAT, FOUND DAMAGED RIB AT #9 TRACK I/B SIDE () REMOVED AND REPLACED LH #4 SLAT RIB FITTING AT #9 TRACK IAW SRM 51-42-11 AND SRM 51-49-00. WORK ACCOMPLISHED BY EMP# V934627 AR VT AEROSPACE MOBILE BFM.
- [SDR CALA2021063000994](https://openairdocs.org/sdr/CALA2021063000994.md): Support Angle · corroded · Jun 29, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) MAIN CABIN, AFT CABIN FR 68 JUST OUTBOARD OF FLOOR BEAM AT Y1292, FLOOR STRUCTURE HAS CORROSION ON EDGE. DOT 10 2-130() CUT-OUT DAMAGED AREA OF FLOOR BEAM/ DOORSLIDE AT FR68 Y1292. INS TALLED REPAIR PARTS 2EA. FILLER AND 1EA. REPAIR ANGLE IAW
- [SDR CALA2021063000992](https://openairdocs.org/sdr/CALA2021063000992.md): Floorbeam · corroded · Jun 28, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > (A3NB-53-3-6185) MAIN CABIN, AFT CABIN FR 66 BEAM BETWEEN Y254 & Y254 HAS CORROSION. DOT 102-133. FLOOR BEAM WAS ELEVATED AND FOUND OUT OF ALLOWABLE DAMAGE IAW A3 19 SRM 53-00-14-283, NEW FLOOR BEAM WAS FABRICATED TO MAT. P/NDA N338C06 BATCH#1837634 IAW SRM51-
- [SDR CALA2021062800980](https://openairdocs.org/sdr/CALA2021062800980.md): Seat Track · corroded · Jun 27, 2021 · N854UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > (A3NB-53-3-6320) MAIN CABIN SEAT TRACK R/H I/B Y765 C20-24 HAS C ORROSION ON CROWN. DOT 102-125() REMOVED AND REPLACED FLOOR BEAM P/N: D53112813000251 BATCH: 0003 786788 IAW A319 SRM 51-45-11. WORK ACCOMPLISHED BY EMP# V934700 AT BFM VT AEROSPACE MOBILE.
- [SDR CALA2021062800976](https://openairdocs.org/sdr/CALA2021062800976.md): Floorbeam · corroded · Jun 25, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > (A3NB-53-3-6038) MAIN CABIN FLOOR STRUCTURE AT Y254 HAS CORROSIO N AT CC16 P/N P/N D53112817004. DOT 102-120 () FLOOR BEAM FOUND OUT OF ALLOWABLE DAMAGE LIMITS IAW A319 SRM 53- 11-14-283-005 AND REPLACED IAW SRM 51-72-11-911.
- [SDR CALA2021062800975](https://openairdocs.org/sdr/CALA2021062800975.md): Floorbeam · corroded · Jun 25, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-25-3-6221 DOT 42-025 AFT CABIN FLOOR SUPPORT BEAM CORRODED FR66 Y765 LAV MOUNT AREA () REMOVED AND REPLACED FOR A NEW FLOORBEAM P/N D5347204000200 IAW A319 SRM 51-42-11.
- [SDR CALA2021062500960](https://openairdocs.org/sdr/CALA2021062500960.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > A3NB-25-3-6221 DOT 42-026 AFT CABIN FLOOR SUPPORT BEAM CORREDED FR66 Y1292 LAV MOUNT AREA (). REPLACED AFT CABIN FLOOR SUPPORT BEAM FR66 Y1292 IAW SRM 51-42-1 1.
- [SDR CALA2021062500959](https://openairdocs.org/sdr/CALA2021062500959.md): Floorbeam · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > (A3NB-53-3-6038) MAIN CABIN FLOOR STRUCTURE Y1292 HAS CORROSION AND SCRATCHES AROUND FASTGENER HOLES C-12-16 P/N D5311281520201. DOT 102-116 () REMOVED AND REPLACED WITH NEW FLOOR BEAM P/N=D5311281300251 BATC H:0003786788 IAW A319 SRM 51-42-11.
- [SDR CALA2021062500956](https://openairdocs.org/sdr/CALA2021062500956.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185O) MAIN CABIN, AFT CABIN FR66-67 Y254-765 FLOOR B EAM 24IN. FROM CENTERLINE HAS CORROSION ON UPPER SURFACE. REMOVED AND REPLACED FLOOR BEAM P/N D5347209400800, BATCH:000271 6526 IAW A319 SRM 51-42-11.
- [SDR CALA2021062500953](https://openairdocs.org/sdr/CALA2021062500953.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6185) MAIN CABIN, AFT CABIN FR68-67 Y765 FLOOR BEAM H AS CORROSION ON TOP SURFACE. DOT 102-131 (). REPLACED FLOOR BEAM WITH NEW FLOOR BEAM PN#D5347219220000 IAW A3 19 SRM 51-42-11. FR 67-68 Y765.
- [SDR CALA2021062500952](https://openairdocs.org/sdr/CALA2021062500952.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6040) DOT 42-032 FWD CABIN FLOOR SUPPORT BEAM HAVE CO RROSION FR20 TO FR 21 -Y765() REMOVED OLD AND INSTALLED NEW FLOOR BEAM P/N D5311281400200 BATC H 003786788, IAW A319, SRM 51-42-11 ATTACHED FORM 44-0008.
- [SDR CALA2021062500951](https://openairdocs.org/sdr/CALA2021062500951.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6038) MAIN CABIN FLOOR STRUCTURE Y503 HAS CORROSION A ND SCRATCHES AROUND FASTENER HOLES C-15-16 P/N. REPLACED FLOOR BEAM P/N:D5311282600200 BATCH:0003804422 IAW A319 SRM 51-72-11-911-001. ATTACHED FORM 44-0008.
- [SDR CALA2021062500950](https://openairdocs.org/sdr/CALA2021062500950.md): Floor Support · corroded · Jun 24, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > (A3NB-53-3-6038) MAIN CABIN FLOOR STRUCTURE Y765 HAS CORROSION A ND SCRATCHES AROUND FASTENER HOLES C-12-16 P/N D5311281300251. D OT 102-118 (). REMOVED AND REPLACED FLOOR BEAM WITH NEW FLOOR BEAM P/N D5311281 400200, BATCH 003786788. IAW A319 SRM 51-42-11, FR
- [SDR CALA2021062500949](https://openairdocs.org/sdr/CALA2021062500949.md): Floorbeam · corroded · Jun 23, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-25-3-6221 DOT 42-027 AFT CABIN FLOOR SUPPORT BEAM CORRODED FR66 Y254 AREA () REMOVED OLD FLOOR BEAM (SUPPORT) AND REPLACED WITH NEW FLOOR BEA M P/N:D534728802000 BTCH:0001820499 IAW A319 SRM 51-42-11. ATTAC CHED FORM: 44-0008. ACCOMPLISHED BY V934700 AT B
- [SDR CALA2021062500948](https://openairdocs.org/sdr/CALA2021062500948.md): Floorbeam · corroded · Jun 23, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-53-3-6222 AFT MAIN CABIN FLOOR SUPPORT Y254 HAS CORROSION A T FR68. (DOT 38-46) () BEAM WAS FOUND OUT OF ALLOWABLE DAMAGE IAW 53-00-14-283 L=3.0 W= 3.0" D=0.070" (EXCLUDED AREA) AND FLOOR BEAM WAS REPLACED IAW SR M 51-72-11-911. PN=D534721962000 BATCH=000
- [SDR CALA2021061800886](https://openairdocs.org/sdr/CALA2021061800886.md): Shear Panel · corroded · Jun 16, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6222 MAIN CABIN FLOOR LH SHEAR PLATE AT FR69-70 CORROD ED.(DOT 38-44)() REMOVED AND REPLACED SHEAR PLATGE P/N #D5347112420000 BATCH#0003 640061 MAIN CABIN FR.69 TO FR70 L/H IAW SRM 51-42-11. SFR 102568 4.
- [SDR CALA2021061400866](https://openairdocs.org/sdr/CALA2021061400866.md): Floor Support · corroded · Jun 14, 2021 · N854UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > A3NB-53-3-6222 MAIN CABIN FLOOR RH SHEAR PLATE AT FRFR69-70 CORR ODED. (DOT 38-43)
- [SDR CALA2021061400863](https://openairdocs.org/sdr/CALA2021061400863.md): Beam · corroded · Jun 13, 2021 · N854UA · Airbus A319131 · Fuselage Structure (General)
  > A3NB-53-3-6185 MAIN CABIN FLOOR SUPPORT -Y1732 HAS CORROSION AT FR68. (DOT 38-42) ()
- [SDR CALA2021061400861](https://openairdocs.org/sdr/CALA2021061400861.md): Beam · corroded · Jun 13, 2021 · N854UA · Airbus A319131 · Fuselage Main, Structure
  > (A3NB-53-3-6185) MAIN CABIN, AFT CABIN FR68 Y1292 FLOOR BEAM HAS CORROSION AROUND FASTENER HOLES.DOT 102-129(). FURTHER DETAILS AWAITED
- [SDR CALA2021061400854](https://openairdocs.org/sdr/CALA2021061400854.md): Floorbeam · corroded · Jun 11, 2021 · N854UA · Airbus A319131 · Fuselage Main, Floor Beam
  > A3NB-53-3-6040 DOT 42-029 FWD CABIN FLOOR SUPPORT BEAM CORRODED FR20 -Y189. EMP# V954339 SUPPORT FLOOR BEAM WAS MEASURED IAW SRM 53-11-14-283-002 AND FOU ND OUT OF LIMITS AND FLOOR BEAM WAS REPLACED IAW SRM 51-72-11-91 1-007. SFR#1025651 WORK ACCOMPLISHED BY E
- [SDR CALA2020080901085](https://openairdocs.org/sdr/CALA2020080901085.md): Connector · unsecure · Aug 3, 2020 · N854UA · Airbus A319131 · Door System Wiring
  > AFT CARGO DISPLAYED ON UPPER ECAM SCREEN. - DOOR VERIFIED DOOR CLOESD AND PLACARDED. PERFORMED TSM 52-32-00-810-801-A. FOUND A CONNECTOR AT 7537VP LOOSE. SECURED THE CONNECTOR AND PERFORMED OPERATIONAL TEST OF DOOR AND VERIFIED USING PARAMETER CALLUP MENU.
- [SDR CALA2019042900674](https://openairdocs.org/sdr/CALA2019042900674.md): Radio · failed · Apr 29, 2019 · N854UA · Airbus A319131 · Communications System
  > SMELL OF AVIONICS SMOKE IN FLIGHT DECK NO ECAM CHECKED AREA REMOVED RH AND LH MCDU. SUSPECTED SMELL IS COMING FROM CENTER CONSOLE AND BECOMES STRONGER AROUND THROTTLE CONTROL ASSY. FLIGHT CREW CLAIMED THEY SAW SMOKE REFLECTED BY THE SUN AT EYE LEVEL NEAR CENTE
- [SDR CALA2017121104389](https://openairdocs.org/sdr/CALA2017121104389.md): Fan · odor · Dec 11, 2017 · N854UA · Airbus A319131 · Air Distribution Fan
  > FAINT ODOR IN COCKPIT DURING CLIMB OUT. REMOVED AND REPLACED FAN BLOWER IAW AMM 21-26-51. OPS CHECK OK.NO LEAKS NOTED
- [SDR CALA2017112604218](https://openairdocs.org/sdr/CALA2017112604218.md): Altimeter · faulty · Nov 26, 2017 · N854UA · Airbus A319131 · Altimeter, Barometric/Encoder
  > STANDBY ALTIMETER INDICATION ERRONEOUS. REMOVED AND REPLACED STANDBY ALTIMETER PER AMM 34-21-22. OPS CHECK GOOD.
- [SDR CALA2017111704096](https://openairdocs.org/sdr/CALA2017111704096.md): Skin · gouged · Nov 17, 2017 · N854UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SKIN FRAMES 13 - 14, STRINGERS 22 - 23L GOUGED OUT OF LIMITS, FABRICATED AND INSTALLED A DOUBLER IAW SRM 53-00-11-300-042, FIG 20148.
- [SDR CALA2017011600125](https://openairdocs.org/sdr/CALA2017011600125.md): Battery · discharged · Jan 16, 2017 · N854UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED FOR EPSU BATTERY AFT L. REPLACED BATTERY FOR AFT L. OPS CK GOOD. REF AMM 33-51-38/401
- [SDR CALA2016072995599](https://openairdocs.org/sdr/CALA2016072995599.md): Power Supply · warning light · Jul 26, 2016 · N854UA · Airbus A319131 · Emergency Lighting
  > EPSU L FAULT. REPLACED 11WL POWER SUPPLY ON ACCOUNT OF SHORT IN SLIDE CA USED UNIT FAILURE, IAW MM 33-51-38. RECONNECTED ALL UNDERSEAT LIGHT CONNECTIONS, REPLACED BULBS AND REPLACED LIGHT COVERS ON LEFT WING ROOT.
- [SDR CALA2016072895592](https://openairdocs.org/sdr/CALA2016072895592.md): Power Supply · shorted · Jul 25, 2016 · N854UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY CABIN LIGHT TEST FAILED. R & R THE POWER SUPPLY. R & R THE SLIDE ASSEMBLY, TESTED GOOD
- [SDR CALA2016070895516](https://openairdocs.org/sdr/CALA2016070895516.md): Power Supply · malfunctioned · Jul 3, 2016 · N854UA · Airbus A319131 · Emergency Lighting
  > "EPSU UNIT EMER L." FOUND BOTH INTERNAL AND EXTERNAL LOAD LIGHTS FLASHING ON 11WL. REPLACED POWER SUPPLY AND BATTERY PACK IAW AMM 33-51-38-400-001-A

Next page: https://openairdocs.org/aircraft/N854UA/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 = 'N854UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N854UA/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.