# Service difficulty reports: N807UA

A list on [N807UA](https://openairdocs.org/aircraft/N807UA.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 · 95 reports

- [SDR CALA2026092119613](https://openairdocs.org/sdr/CALA2026092119613.md): Wire Harness · faulted · Sep 18, 2026 · N807UA · Airbus A319131 · Engine Fuel System Wiring
  > NORMAL START ON NUMBER 1 ENGINE. REJECTED TAKEOFF APPROX 60 KNOTS DUE TO NR 1 EGT READING 162 DEGREES. OTHERWISE NORMAL ENGINE INSTRUMENTS AND ACCELERATION NO SWERVING. ADDED FADEC 1B TEST RESUT PICTURE REF TSM 77-20-00-810-801-B, PERFORMED ENG 1 ECTRICAL CA
- [SDR CALA2026061917186](https://openairdocs.org/sdr/CALA2026061917186.md): Battery · discharged · Jun 18, 2026 · N807UA · Airbus A319131 · Emergency Equipment
  > FLASHLIGHT 1LNEEDS TO BE CHECKED REPLACED FLASHLIGHT BATTERY AT 1L REF AMM 25-65-98, AND REPLACED SEAL.
- [SDR CALA2026021013686](https://openairdocs.org/sdr/CALA2026021013686.md): Power Supply · no test · Feb 9, 2026 · N807UA · Airbus A319131 · Emergency Lighting
  > PROCEDURE - EPSU UNIT EMER L FAULT ON CIDS EMERGENCY LIGHT TEST R/R L EPSU BATTERY REF. AMM 33-51-38/401. OPS CHECK GOOD
- [SDR CALA2026011913053](https://openairdocs.org/sdr/CALA2026011913053.md): Power Supply · no test · Jan 18, 2026 · N807UA · Airbus A319131 · Emergency Lighting
  > FOUND EPSU UNIT AFT LIGHT FAULT DURING OPS CHECK OF THE EMERGENCY POWER SUPPLY. R & R AFT EPSU AND BATTERY IAW AMM 33-51-38-400-001-A. OPS CHECKED GOOD.
- [SDR CALA2025122312375](https://openairdocs.org/sdr/CALA2025122312375.md): Battery · no test · Dec 21, 2025 · N807UA · Airbus A319131 · Emergency Lighting
  > DURING CABIN EMERGENCY LIGHTING OPS TEST, FOUND RT EPSU BATTERY FAULTED. REMOVED & REPLACED RT EPSU IAW AMM 31-51-38. OPS TESTED GOOD.
- [SDR CALA2025101309930](https://openairdocs.org/sdr/CALA2025101309930.md): Sign · unsecure · Oct 10, 2025 · N807UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT SIGN NEXT TO DOOR 1L NOT SECURED. EMERGENCY EXIT SIGN NEXT TO DOOR 1L IS SECURED. SECURED PANEL ADJACENT TO DOOR 1L EMERGENCY EXIT SIGN WITH TAPE. OK TO APPLY NEF 2522CL FOR LOSE PANEL. EMERGENCY EXIT SIGN NEXT TO DOOR 1L IS SECURED. SECURED PA
- [SDR CALA2025041803983](https://openairdocs.org/sdr/CALA2025041803983.md): Unknown · vibration · Apr 18, 2025 · N807UA · Airbus A319131 · Fuselage Structure (General)
  > AIRFRAME VIBRATION ABOVE COST INDEX ZERO. HIGHER THE INDEX GREATER THE VIBRATION. FLIGHT ATT
- [SDR CALA2025032800497](https://openairdocs.org/sdr/CALA2025032800497.md): Transducer · faulted · Mar 24, 2025 · N807UA · Airbus A319131 · Drag Control System
  > SPEED BRAKE 3 4 FAULT REMOVED AND REPLACED SPEEDBRAKE CONTROL TRANSDUCER IN REF AMM CHECK GOOD. OK TO CONTINUE. PERFORMED OPERATIONAL TEST OF THE SEC1, SEC:1 2 AND SEC 3 SYSTEMS REF. TASK 27-94-00-710-001-A.
- [SDR CALA2025032003018](https://openairdocs.org/sdr/CALA2025032003018.md): Slide · not reported · Mar 17, 2025 · N807UA · Airbus A319131 · Standard Practices/Structures
  > FORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - RETURN DOOR 1R TO NORMAL AFTER SLIDE REPLACEMENT REF AMM 52-10-00-860-002-A. REACTIVATEDD DOOR 1R. REF AMM 52-10-00-860-002-A. DOOR R 1 ACTIVATED FOR ABOVE AMM, REF GMM 09-25-05.
- [SDR CALA2025031902963](https://openairdocs.org/sdr/CALA2025031902963.md): Proximity Switch · malfunctioned · Mar 16, 2025 · N807UA · Airbus A319131 · Door Warning System
  > GATE RETURNFWD CARGO DOOR FWD CAGO DOOR CONFIRM LOCKED AND CLOSE REF MEL5270 CE 5270CE APPROVED DDP ACOMPLIS DOOR CLOSED AND LOCK *DM* AVIATAR SHOWS "DOOR FWD CARGO" HITTING CONSISTANTLY EACH FLIGHT. REF TSM 52-31-00-810-801-A. ADDING PROX SWITCHES 28WV AND 30
- [SDR CALA2024123003187](https://openairdocs.org/sdr/CALA2024123003187.md): Frame · cracked · Dec 28, 2024 · N807UA · Airbus A319131 · Fuselage Main, Frame
  > AD RELATED TASK (AD 2022-08-08). TWO CRACK INDICATIONS HOLE #A A T 9 AND 3 HRS O''CLOCK POSITION IN FRAME LAYER WITH 100% FSH (BOT H) AT RH FRAME 16 UPPER DOUBLE JOGGLE AREA "REPAIR BEFORE NEXT F LIGHT". TO ACCOMPLISH INITIAL INSP OF RH FR16 UPPER DOUBLE JOGG
- [SDR CALA2024123003183](https://openairdocs.org/sdr/CALA2024123003183.md): Window Frame · cracked · Dec 23, 2024 · N807UA · Airbus A319131 · Fuselage Main, Structure
  > WINDSHIELD LOWER NODE, LH AND RH CONTINUITY FITTINGS HAVE CRACK INDICATIONS IN HORIZONTAL FLANGE AFT FACE, THROUGH THICKNESS OF FITTINGS. CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEX T FLIGHT. WINDSHIELD LOWER NODE L/H & R/H CONTINUITY FITTINGS REMO
- [SDR CALA2024123003177](https://openairdocs.org/sdr/CALA2024123003177.md): Frame · cracked · Dec 21, 2024 · N807UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR16 UPPER DOUBLE JOGGLE HOLE #6 HAS CRACK INDICATION IN FRAM E LAYER..328 AND INSTALLED 1ST OVERSIZED FASTENER IAW SRM FROM RPR EMBODIMENT WITH SUBSEQUANT INSP AT 6,800 FC IAW SRI 53-11-12-300-12. THIS IS A CAT B RPR REQUIRES INSP AT 6,800 FC 53-11-12-205
- [SDR CALA2024123003186](https://openairdocs.org/sdr/CALA2024123003186.md): Frame · cracked · Dec 17, 2024 · N807UA · Airbus A319131 · Fuselage Main, Frame
  > CRACK INDICATION HOLE #4 AT 12 HRS O''CLOCK POSITION IN FRAME LAY ER WITH 90.5% FSH AT RH FRAME 16 UPPER DOUBLE JOGGLE AREA. REPAIRED DISCREPANT HOLE #4 AND ASSOCIATED HOLE #3 AS DIRECTED B ADL REPAIR EMBODIMENT 6800 FC. FH NOT RELEVANT EA 5311-02442 002 AND
- [SDR CALA2024112502942](https://openairdocs.org/sdr/CALA2024112502942.md): Fuel Cap · missing · Nov 23, 2024 · N807UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL CAP MISSING, NO CAP OR LANYARD PRESENT OK TO DEFER. APPLIED CDL. DEFERRED DIRECTLY BY TOMC THIS IS NOT AN INSPECTION ITEM REF GMM 09-10-05 AND 09-25-05. MISSING CAP WAS INITIALLY REPORTED. NO CAP OR LANYARD PRESENT OK TO DEFER. INSTALLED NEW FUE
- [SDR CALA2023072802359](https://openairdocs.org/sdr/CALA2023072802359.md): Stringer · cracked · Jul 27, 2023 · N807UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > BAG CART HIT THE AFTFUSELAGE DURING STORM EXTENDS ABOUT 20" AFT OF PUNCTURED AREA AND IS ABOUT 4" TALL. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN AREA BETWEEN FRAMES 57-59 AND APPROXIMATELY AT STRINGERS 36-38LH P
- [SDR CALA2023061201828](https://openairdocs.org/sdr/CALA2023061201828.md): Door · open · Jun 9, 2023 · N807UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO DOOR OPEN ONDEPT. PILOT STATED DOOR INDICATION CAME ON AFTER TAKEOFF AND WENT OUT LOCKED UPON GATE RETURN. OPS CHECK DOOR OPS CHECK NORMAL. COMPLIED WITH MEL 5270CE AFTER LANDING. VERIFIED ALL DOOR LATCH INDICATIONS SHOWED PLACING INDICATION ON PLACA
- [SDR CALA2022080801995](https://openairdocs.org/sdr/CALA2022080801995.md): None · missing · Aug 8, 2022 · N807UA · Airbus A300* · Fuel Storage
  > PDA 2 FUEL CAP AND LANYARD FOUND MISSING ON ARRIVAL. CONTACTED SFO HMC THEY ARE CHECKED WITH FUELERS NO INFORMATION TO CONFIRM FUEL CAP WAS LEFT OFF. CONTACTED ESC TO INFORM THEM OF CAP MISSING ON ARRIVAL. PDA INFORMATION SENT TO ENGINEERING.
- [SDR CALA2022041801009](https://openairdocs.org/sdr/CALA2022041801009.md): Splice · corroded · Apr 17, 2022 · N807UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > CORROSION FOUND ON EXISTING REPAIR ON STR 42L BETWEEN FR59-FR60 ON HAECO LCQ REF 9296918/28918 SUPPORT TASK. NR GENERATED BY V07 9881 REMOVED & REPLACED STRINGER REPAIR IAW A319 SRM 53-41-13-300-010 AT HAECO LCQ ON HANGAR NR 9296918/28918 PERFORMED BY MECH V03
- [SDR CALA2022041100953](https://openairdocs.org/sdr/CALA2022041100953.md): Fitting · loose · Apr 10, 2022 · N807UA · Airbus A319131 · Elevator Structure
  > RIGHT ELEVATOR OUTBD SERVO ATTACHMENT FITTING OUTBD SIDE BUSHING LOOSE IN FITTING ON HAECO LCQ REF 9296494/28494 SPEC A3NB-55-3- 0001. NR GENERATED BY V061070 REMOVED RIGHT ELEVATOR O/B SERVO ATTACHMENT FITTING O/B SIDE BUS BY MECH V917417 RII INSP PERFORMED B
- [SDR CALA2022041100947](https://openairdocs.org/sdr/CALA2022041100947.md): Skin · cracked · Apr 9, 2022 · N807UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FRAM 35 STR 30 LH HOLE #2 HAS CRACK INDICATION IN AFT SKIN LAYER AT 11 AND 5 O''CLOCK DIRECTIONS ON HAECO LCQ REF 9296337/28337 S UPPORT TASK. TO ACCMP INITIAL INSPECTIONS OF THE FR35 STR30LH HOLE#2 IN AFT S BEFORE THE ACFT REACHES 41,126 TOTAL ACFT FC/93,240
- [SDR CALA2022040600892](https://openairdocs.org/sdr/CALA2022040600892.md): Beam · corroded · Apr 5, 2022 · N807UA · Airbus A319131 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR STRUCTURE RH DOOR SILL BEAM AT FR68 PER HAECO LCQ N/R 9296748/28748 GENERATED BY V061619. REPAIRED R2 DOOR SILL BEAM IAW A319 SRM 53-41-14-300-001. MECH B Y V061619 INSP BY V901665
- [SDR CALA2022040600891](https://openairdocs.org/sdr/CALA2022040600891.md): Beam · corroded · Apr 5, 2022 · N807UA · Airbus A319131 · Fuselage Main, Structure
  > CORROSION ON CABIN FLOOR STRUCTURE LH DOOR SILL AT FR 68 A3NB-53 -3-6187.PER HAECO LCQ N/R 9296661/ 28661 GENERATED BY V892443. REPAIRED L2 DOOR SILL BEAM IAW SRM53-41-14-300-001.) MECH BY V06 1619 INSP BY V901665.
- [SDR CALA2022040600879](https://openairdocs.org/sdr/CALA2022040600879.md): None · corroded · Apr 4, 2022 · N807UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO DOOR TORQUE BOX HAS MULTIPLE AREAS OF CORROSION ON UPP ER SURFACE ON HAECO LCQ REF 9296693/28693 SPEC A3NB-53-3-6217. N R GENERATED BY V079881 BLEND CORROSION, BEYOND ALLOWABLE LIMITS. REMOVED & REPLACED TOR QUE BOX COVER PLATE IAW A319 SRM 51-72-11-
- [SDR CALA2022031700684](https://openairdocs.org/sdr/CALA2022031700684.md): None · cracked · Mar 16, 2022 · N807UA · Airbus A319131 · Fuselage Structure (General)
  > 27JUL SFO CF -9:EXTERNAL FUSELAGE SKIN HAS DOUBLER INSTALLED FRAME 26 A T STR 41 LT.:REINSPECT DOUBLER PER PER SRI-53-00-11-2-003-00 USING AIRBUS NTM 51-10-16 (EDDY CURRENT) B EFORE 48000 FC. OK TO CF PER SRI 53-00-11-2-003-00 AND SFOIQ WAL SH. 13OCT OPB I
- [SDR CALA201906301080](https://openairdocs.org/sdr/CALA201906301080.md): Accumulator · damaged · Jun 26, 2019 · N807UA · Airbus A319131 · Hydraulic System, Main
  > BLUE HYD SYS RES LO LVL ECAM. FOUND BLUE SYSTEM ACCUMULATOR, GAS CHARGING VALVE ORING BLOWN OUT. REPLACED PER 29-12-22. LEAK FIXED, BUT ACCUMULATOR WILL NOT HOLD A PRECHARGE. CREW REPORTED THEY TURNED OFF THE BLUE PUMP SWITCH WHEN THEY GOT THE LOW LEVEL ECAM M
- [SDR CALA2017102303766](https://openairdocs.org/sdr/CALA2017102303766.md): Power Supply · faulty · Oct 23, 2017 · N807UA · Airbus A319131 · Emergency Lighting
  > SOME EMERGENCY LIGHTS STAY ON IN REAR OF CABIN. REMOVED AND REPLACED POWER SUPPLY AND BATTERY AT 11WL IAW AMM 33-51-15.
- [SDR CALA2017101303613](https://openairdocs.org/sdr/CALA2017101303613.md): Cover · missing · Oct 13, 2017 · N807UA · Airbus A319131 · Emergency Lighting
  > ROW 20ABC MISSING COVER FOR EMERGENCY LIGHT. REPLACED EMERGENCY LIGHT PROTECTIVE COVER.
- [SDR CALA2017051201373](https://openairdocs.org/sdr/CALA2017051201373.md): Panel · cracked · May 12, 2017 · N807UA · Airbus A319131 · Emergency Equipment
  > RT OVERWING EVACUATION SLIDE OUTER SURROUND PANEL HAS SEVERAL CRACKS AT LOWER AFT CORNER AREA. REMOVED AND REPLACED RT OVERWING SLIDE REF AMM 25-62-42-400-001A.
- [SDR CALA2015101294581](https://openairdocs.org/sdr/CALA2015101294581.md): Power Supply · inoperative · Oct 10, 2015 · N807UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT SIGNS MID & AFT CABIN NOT LIT WHEN EMER LIGHT IS ON. REPLACED ESPU'S 11WL & 13WL IAW MM 33-51-58-401. OPERATIONS CHECKED OK.
- [SDR CALA2015101294580](https://openairdocs.org/sdr/CALA2015101294580.md): Light · inoperative · Oct 10, 2015 · N807UA · Airbus A319131 · Emergency Lighting
  > AFT OVERHEAD EMER LIGHT BY LAVATORIES INOPERATIVE. REPLACED LIGHT ASSEMBLY ON THE AFT OVERHEAD EXIT SIGN 18-3351-3-0004.
- [SDR CALA2013120993555](https://openairdocs.org/sdr/CALA2013120993555.md): Seal · unsecure · Dec 7, 2013 · N807UA · Airbus A319131 · Engine Thrust Reverser
  > RUBBER SEAL HANGING FROM NR 1 ENG REVERSER. CNA OUTER SEAL OUT OF RETAINER APPROXIMATELY 3.5 FT 9 O’CLOCK POSITION. SECURED SEAL & APPLIED RTV 732.
- [SDR CALA2013101892181](https://openairdocs.org/sdr/CALA2013101892181.md): Uplock Sensor · faulted · Oct 18, 2013 · N807UA · Airbus A319131 · Landing Gear Position and Warning
  > CREW REPORTED LGCIU 1 FAULT. FOUND NLG DOWN LOCK SENSOR 18GA AT FAULT. R & R SENSOR 18GA & LGCIU 1 IAW AMM 32-31-73,32-31-71. ALSO FOUND INTERMITTENT SHORT A ON 1300VC & B ON SENSOR. REMOVED 1300VC & CLEANED OUT CONNECTOR, NO SHORT. WIRES CHECKED GOOD FRO
- [SDR CALA2013102192203](https://openairdocs.org/sdr/CALA2013102192203.md): Interface Unit · malfunctioned · Oct 17, 2013 · N807UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > REF LOG 1 FOR THE CLUNKING NOISE & VIBRATION, CREW REPORTS AT THAT TIME BRIEFLY HAD A UNUSUAL ODOR IN THE FLT DECK & ALSO REPORTED SMELLING IN THE CABIN. THE ODOR DISSIPATED QUICKLY. BOTH LGCIUS WERE REPLACED, NO OTHER ACTION NECESSARY IAW MM 05-51-10.
- [SDR CALA2013082090595](https://openairdocs.org/sdr/CALA2013082090595.md): Battery · inoperative · Aug 19, 2013 · N807UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY R MESSAGE. REPLACED BATTERY IAW AMM.
- [SDR CALA2013082090594](https://openairdocs.org/sdr/CALA2013082090594.md): Battery · inoperative · Aug 19, 2013 · N807UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY L FWD MESSAGE. REPLACED BATTERY IAW AMM.
- [SDR UALA2013062604470](https://openairdocs.org/sdr/UALA2013062604470.md): Hook And Loop · loose · Jun 23, 2013 · N807UA · Airbus A319131 · Life Jacket
  > HOOK AND LOOP ON LIFE VEST DOOR UNDER RIGHT OBSERVER SEAT COMING OFF. DOOR WILL NOT STAY IN PLACE. SECURED HOOK AND LOOP FOR RT OBSERVER IN FD. OK TO CONTINUE.
- [SDR UALA2013061204012](https://openairdocs.org/sdr/UALA2013061204012.md): Unknown · unknown · Jun 8, 2013 · N807UA · Airbus A319131 · Electrical Power System
  > EMERGENCY GENERATION SYS OPS TEST FAILS STEP 4A.1 THE GREEN LINES BETWEEN EMERGENCY GENERATOR & AC ESS BUSS BAR, THE EMERGENCY GENERATOR & ESS TR AND THE ESS TR & DC ESS BUSS BAR NEVER COME INTO VIEW. REPLACED CSM IAW MM, OPS CHECKED NORMAL.
- [SDR UALA2013051303308](https://openairdocs.org/sdr/UALA2013051303308.md): Cylinder · leaking · May 10, 2013 · N807UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > LEFT MAIN GEAR UNLOCK ACTUATOR IS LEAKING. REPLACED LEFT MLG LOCK STAY ACTUATOR CYLINDER IAW AMM, CHECKED OK.
- [SDR UALA2013050703203](https://openairdocs.org/sdr/UALA2013050703203.md): Floor Panel · delaminated · May 5, 2013 · N807UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY FLOOR PANEL 151VG DELAMINATED 34 INCHES X 17 INCHES. REPLACED AFT FLOOR PANEL IAW AMM 53-42-16 & 53-42-14.
- [SDR UALA2013042902962](https://openairdocs.org/sdr/UALA2013042902962.md): Screw · backed out · Apr 26, 2013 · N807UA · Airbus A319131 · Fixed Inner Doors
  > COCKPIT DOOR STUCK CLOSED. WILL NOT OPEN MANUALLY OR ELECTRICALLY. SECURED SCREW THAT HAD BACKED OUT. DOOR OPS CHECKED NORMAL.
- [SDR UALA2013041502584](https://openairdocs.org/sdr/UALA2013041502584.md): Latch · loose · Apr 15, 2013 · N807UA · Airbus A319131 · Fixed Inner Doors
  > UNABLE TO OPEN COCKPIT DOOR IN DESCENT USING D-RING. USED UNLOCK SWITCH TO OPEN DOOR. FOUND UPPER DOOR LATCH LOOSE AT TENON. SUSPECT INTERNAL MECHANISM SPRING BROKEN. REMOVED AND REPLACED UPPER LATCH DOOR MECHANISM, ADJUSTED THE ROD FOR THE LATCH IAW AMM,
- [SDR UALA2013030801399](https://openairdocs.org/sdr/UALA2013030801399.md): Strap · stuck · Mar 7, 2013 · N807UA · Airbus A319131 · Flight Compartment Equipment
  > THE 1L INBOARD JUMPSEAT STRAP IS STUCK. FOUND SEAT BELT STUCK IN TRACK. REMOVED, OPS CHECKED GOOD.
- [SDR UALA2013013000567](https://openairdocs.org/sdr/UALA2013013000567.md): Structure · damaged · Jan 30, 2013 · N807UA · Airbus A319131 · Engine Air Intake System
  > LOOKING INTO INLET OF NR 1 ENG, 2 O`CLOCK POS. PREVIOUS REPAIR COMING LOOSE AND HAS APPROX A ONE HALF INCH HOLE IN PATCH. FOUND DAMAGE AT PREVIOUS REPAIR LOCATED AT 11 O`CLOCK POSITION. ACCOMPLISHED REPAIR REF AMM MT 71-006. PERMANENT REPAIR TO BE ACCOMPL
- [SDR UALA2012100805668](https://openairdocs.org/sdr/UALA2012100805668.md): Power Supply · failed · Oct 5, 2012 · N807UA · Airbus A319131 · Emergency Lighting
  > DURING EEL TEST FAILING WITH MSG. EPSU FWD L BATTERY. REPLACED POWER SUPPLY PER AMM, RETESTED GOOD. P/N AD-3214-30.
- [SDR UALA2012042002382](https://openairdocs.org/sdr/UALA2012042002382.md): Solenoid · failed · Apr 20, 2012 · N807UA · Airbus A319131 · Passenger Oxygen System
  > DURING OPS TEST OF O2 MASKS AT 1AB & LAST ROWS. SEATS FAILED TO DROP AT 7ABC, 10ABC, 21ABC, 23ABC, 8DEF, 25DEF & 26DEF. REPLACED SOLENOIDS IAW AMM35-21-41. REPOSITIONED OXYGEN MASKS AT REMAINER OF SEATS. DROP TESTED NORMAL IAW AMM 35-23-00.
- [SDR UALA2012042002372](https://openairdocs.org/sdr/UALA2012042002372.md): Girt Bar · out of adjust · Apr 19, 2012 · N807UA · Airbus A319131 · Emergency Equipment
  > DOOR 2R SHOWS SLIDE NOT ARMED. F/A NOTICED ARMING HANDLE NOT FULL DOWN. SHOWED ARM B4. ACCOMPLISHED INSPECTION OF DOOR ADJUSTMENT PER MM. ADJUSTED ESCAPE SLIDE GIRT BAR TRAVEL PER MM. OPERATED DOOR SLIDE SEVERAL TIMES AND FOUND OPERATION NORMAL WITH COCK
- [SDR UALA2012040902175](https://openairdocs.org/sdr/UALA2012040902175.md): Panel · failed · Apr 7, 2012 · N807UA · Airbus A319131 · Escape Slide
  > RIGHT AFT SLIDE INDICATION INOPERATIVE ON DOOR OXYGEN SYSTEM ECAM PAGE - DOOR OXYGEN. SLIDE INDICATION WAS GOOD BEFORE DEPARTURE BUT INOPERATIVE SOMETIME DURING CLIMBOUT. REPLACED SLIDE ARMED IND LIGHT PANEL ASSY PER AMM. ECAM AND DOOR ASSY OP CHECKED NORMA
- [SDR UALA2012021600953](https://openairdocs.org/sdr/UALA2012021600953.md): Skin · leaking · Feb 15, 2012 · N807UA · Airbus A319131 · Wing, Plate/Skin
  > FOUND A FUEL LEAK ON THE LT WING ROOT. TANK ENTRY CREW FOUND LEAK, WILL ACP TANK ENTRY AFTER ON COMPLETION OF ACFT 2885 TANK REPAIRS. FUEL LEAKING FROM LT WING ROOT AT 45 DROPS PER MINUTE. ACCOMPLISHED TROUBLESHOOTING FUEL LEAKS USING BLOW BACK METHOD. LEA
- [SDR UALA2011101905660](https://openairdocs.org/sdr/UALA2011101905660.md): Slide · unwanted deploy · Oct 19, 2011 · N807UA · Airbus A319131 · Escape Slide
  > L2 DOOR SLIDE DEPLOYED. SLIDE REMOVED FROM AIRCRAFT. REPLACED L2 DOOR SLIDE/RAFT IAW AMM.

Next page: https://openairdocs.org/aircraft/N807UA/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 = 'N807UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N807UA/reports

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