# Service difficulty reports: N801UA

A list on [N801UA](https://openairdocs.org/aircraft/N801UA.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 · 104 reports

- [SDR CALA2026082118776](https://openairdocs.org/sdr/CALA2026082118776.md): Battery · faulted · Aug 20, 2026 · N801UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY SYSTEM TEST FAULT, EPSU BATTERY EMER RT, RE-TESTED EMERGENCY LIGHTING SYSTEM ON THE PTP PANEL, TEST OK IAW AMM 33-51-00-710-001-A.
- [SDR CALA2026041015252](https://openairdocs.org/sdr/CALA2026041015252.md): Fuel Cap · missing · Apr 9, 2026 · N801UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING PLACED ON CDL DDP C/W. INSTALLED NEW FUEL CAP REF AMM 28-25-41.
- [SDR CALA2025111611226](https://openairdocs.org/sdr/CALA2025111611226.md): Valve · leaking · Nov 13, 2025 · N801UA · Airbus A319131 · Hydraulic System, Main
  > DIRTY SOCK/OIL ODOR IN FLT DECK AFTER GEARDOWN ON FINAL APPROACH. PERFORM AMM 05-50-00-810-831-A IDENTIFICATION OF THE CAUSE FOR CABIN ODOR, SMOKE OR FUME, AND TSM TASK 71-00-00-810-801-A SMOKE AND/OR OIL SMELL IN THE CABIN DUE TO AN ENGINE LEAKAGE. ACCOMPLI
- [SDR CALA2025102810634](https://openairdocs.org/sdr/CALA2025102810634.md): Filter · odor · Oct 26, 2025 · N801UA · Airbus A319131 · Air Distribution System
  > FUEL SMELL STILL DETECTABLE IN THE CABIN. REMOVED AND REPLACED BOTH RECIRCULATION FILTER CARTRIDGE PER AMM 21-21-41-400-001-A OPS TEST NORMAL, NO FUEL SMELL A THIS TIME, OK FOR SERVICE.PARTS USED: 31-2121-3-0008, QTY:1 ADD EMP: U114389
- [SDR CALA2025102010316](https://openairdocs.org/sdr/CALA2025102010316.md): Holder · torn · Oct 20, 2025 · N801UA · Airbus A319131 · Passenger Compartment Equipment
  > FWD CABIN CURTAIN HOLDBACK DEVICE TORN. REMOVED AND REPLACED FWD CURTAIN TIE BACK. OPS CK NORMAL.
- [SDR CALA2025093009432](https://openairdocs.org/sdr/CALA2025093009432.md): Door · inoperative · Sep 29, 2025 · N801UA · Airbus A319131 · Passenger Compartment Equipment
  > OVRHD BIN 1F INOP OVERHEAD BIN 1 EF WONT LATCH CLOSED MEL 2528AF REJECTED 2528AF IS FOR THE OVERHEAD BIN STORAGE BOX LOCK, NOT THE OVERHEAD BIN DOOR ITSELF..MEL 2528AL IS FOR THE OVERHEAD STOWAGE BIN DOOR SECURED CLOSED. COVER PLATE/RETAINER BROKEN ALLOWING AC
- [SDR CALA2025071006421](https://openairdocs.org/sdr/CALA2025071006421.md): Bottle · no discrepancy · Jul 7, 2025 · N801UA · Airbus A319131 · Emergency Equipment
  > SLIDE PRESSURE DOOR 1R BORDERLINE. NEEDS SERVICING SOON. CHECKED DOOR 1RT RESERVOIR PRESSURE AND FOUND IN THE GREEN BAND PER GAGE MODEL "A". PER AMM TASK 25-62-00-210-001-A. NO OTHER DEFECTS NOTED. VERDEJO, ISSAC (V950090) CHECKED DOOR 1RT RESERVOIR PRESSURE
- [SDR CALA2025070706270](https://openairdocs.org/sdr/CALA2025070706270.md): Battery · failed · Jul 5, 2025 · N801UA · Airbus A319131 · Emergency Lighting
  > RH EPSU BATTERY FAULT REPLACED RH OVERWING EPSU IAW AMM 33-51-38, OPS CHECK GOOD.
- [SDR CALA2025052905087](https://openairdocs.org/sdr/CALA2025052905087.md): Packing · damaged · May 26, 2025 · N801UA · Airbus A319131 · Main Landing Gear
  > HYD Y RSVR LO LVL FOUND FWD UNION ON FIN 2577GM(DUAL DIST BRAKE VLV) LEAKING. REPLACED DAMAGED PACKING ON 2577GM REF MM 32-43-14, SERVICED YELLOW SYS BACK TO NORMAL, CHECKED ENG 2 HYD PUMP CASE DRAIN DPI AS PRECAUTIONARY AND IT IS NOT POPPED OUT. DRY MOTORD EN
- [SDR CALA2025031902960](https://openairdocs.org/sdr/CALA2025031902960.md): Cover · loose · Mar 17, 2025 · N801UA · Airbus A319131 · Escape Slide
  > DOOR 2R LIFE RAFT PANCOVER LOCKING LATCHLOOSE ATTEMPTED TO FIT MULTIPLE DIFFERENT SLIDE COVERS ON DOOR 2R, NO FIX. LATCHES DO NOT LINE UP PROPERLY. WORK DONE IN REF WITH AMM 25-62-44. SUSPECT FRAME OF SLIDE WARPED/BENT, SEE ATTAHCED PICTURES FOR CLARIFICATION.
- [SDR CALA2024122701671](https://openairdocs.org/sdr/CALA2024122701671.md): Warning Message · illuminated · Dec 25, 2024 · N801UA · Airbus A319131 · Landing Gear Brake System
  > RIGHT BRAKE PRESSURE INDICATES 3000 PSI CONTINUOUSLY VERIFIED NO BSCU FAULTS AND APPLIED INOP STICKER ADJACENT TO TRIPLE VERIFIED NO BSCU FAULTS AND APPLIED INOP STICKER ADJACENT TO TRIPLE INDICATOR. DEFERRED DIRECTLY BY TOMC COULD NOT REPLACE INDICATOR DUE
- [SDR CALA2024121901576](https://openairdocs.org/sdr/CALA2024121901576.md): Light · malfunctioned · Dec 18, 2024 · N801UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ILLUMINATED W/SWITCHIN ARM CYCLED NO SMOKING SIGN SWITCH AND ALL LIGHTS OPS CK GOOD.
- [SDR CALA2024052801597](https://openairdocs.org/sdr/CALA2024052801597.md): Outflow Valve · faulty · May 21, 2024 · N801UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > CABIN LOST PRESSURIZATION AT FL240 LOCKED FOR SIGNOFF ITEM UNLOCKED BY TOMC. POST FLIGHT REPORT AND ECS REPORT 19 ATTACHED. PFR AND ECS REPORT 19 ROTABLE PARTS ADDED ROTABLE PARTS CHANGE WAS INDICATED - TT # 1681100 SN OFF 2338 ROTABLE PARTS ADDED ROTABLE PART
- [SDR CALA2024022200506](https://openairdocs.org/sdr/CALA2024022200506.md): O-Ring · damaged · Feb 21, 2024 · N801UA · Airbus A319131 · Hydraulic System, Main
  > YELLOW SYSTEM HYD QTY DEPLETED. LOW PRESS LIGHT ILLUMINATED. PER PILOTS. REF 7141314 AIR RETURNED PER FLT CREW HYD PUMP WAS TURNED OFF WITHIN 1 MIN OF LOW PRESS FOUND YELLOW SYSTEM PTU MANIFOLD LEAKING FROM PLUG ON THE BOTTOM FOUND CHECK VALVE ON BOTTOM OF MAN
- [SDR CALA2023121303637](https://openairdocs.org/sdr/CALA2023121303637.md): Clamp · damaged · Dec 6, 2023 · N801UA · Airbus A319131 · Waste Disposal System
  > WASTE TANK LINE FWD OF THE WASTE TANK, SEPARATED DUE TO FAILED CLAMP. LOCKED FOR MAINTENANCE FERRY TO ORD. POSITIONED THE WASTE LINE CLAMP SLEEVE BETWEEN THE SEPARATED WASTE LINES AND SECURED WITH SPEED TAPE FOR THE MAINTENANCE FERRY. ORD MX REPLACED CLAMP.
- [SDR CALA2023100602973](https://openairdocs.org/sdr/CALA2023100602973.md): Fuel Cap · missing · Oct 2, 2023 · N801UA · Airbus A319131 · Fuel Storage
  > FUELER REPORTS MISSING WING FUEL CAP. REQ CDL. CAP MISSING PLACED ON CDL DDP C/W
- [SDR CALA2023052601662](https://openairdocs.org/sdr/CALA2023052601662.md): Seal · vibration · May 24, 2023 · N801UA · Airbus A319131 · Aerodynamic Fairings
  > ABNORMAL AIRFRAME VIBRATION FLAPS 1 IN CLMB FLAPS 2 3 4 IN DESEN T REPAIR REF SRM 53-45-00-005. DAILY REINSPECT OF TAPE REQ. SEAL FLT HOURS. TO BE REPLACED AT EARLIEST OPPORTUNITY BUT NOT LATER THAN 600 FOUND AFT RIGHT EDGE SEAL LOOSE ON BELLY FAIRING PANEL 1
- [SDR CALA2023042601248](https://openairdocs.org/sdr/CALA2023042601248.md): Battery · inoperative · Apr 24, 2023 · N801UA · Airbus A319131 · Emergency Lighting
  > OPS CHECK FAILED FOR EMERGENCY LIGHTS, N0.2 SERVICE CHECK STEP 1 4 PER STS NR0040 REMOVED AND REPLACED 12 WL AND 11 WL BATTERY OF THE ESPU IAW AMM REMOVED AND REPLACED 12 WL AND 11 WL BATTERY OF THE EPSU IAW AMM 33-51-38. PERFORMED OPERATIONAL CHECK EPSU IAW A
- [SDR CALA2022101402819](https://openairdocs.org/sdr/CALA2022101402819.md): Fuel Cap · missing · Oct 14, 2022 · N801UA · Airbus A319131 · Fuel Storage
  > FUEL CAP MISSING REPORTED BY RAMP ACP MEL REQUIREMENTS. INSTALLED SERVICABLE FUEL CAP AND LANYARD.
- [SDR CALA2022072001813](https://openairdocs.org/sdr/CALA2022072001813.md): None · cracked · Jul 19, 2022 · N801UA · Airbus A300* · Nacelle/Pylon Structure
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 7/20/22. PDA 2 #1 ENG OUTBD T-R TO PYLON FLEX SEAL - AFT MOST LOCATION - CRACKED AND MISSING PIECE AT FWD CORNER. REPLACED #1 ENG OUTBD T-R TO PYLON FLEX SEAL, ALL OK.
- [SDR CALA2022072001826](https://openairdocs.org/sdr/CALA2022072001826.md): Seal · cracked · Jul 19, 2022 · N801UA · Airbus A319131 · Nacelle/Pylon, Frame/Spar/Rib
  > PDA 2 #1 ENG INBD T-R TO PYLON FLEX SEAL - SECOND FROM AFT - CRACKED AND MISSING PIECES..SEE PHOTO INSPECT TAPE EACH FLIGHT PER PART 2A AND PERMANENT REPAIR WITHIN 50 FLIGHT HOURS. REF ECRA 5450-02357 REV-B FIG 3 ITEM 110 AFT EDGE CRACKED AND MISSING SEGMENT..
- [SDR CALA2022040800933](https://openairdocs.org/sdr/CALA2022040800933.md): Frame · corroded · Apr 7, 2022 · N801UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010. CORROSION ON DR SILL BEAM FR66-FR68 STGR 23RH. PERFORMED REWORK REPLACEMENT OF RH DOOR SILL BEAM IS REQUIRED, PERFORMED ON DOOR SILL BEAM, THE REWORK ON
- [SDR CALA2022040600893](https://openairdocs.org/sdr/CALA2022040600893.md): Floor Support · corroded · Apr 5, 2022 · N801UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON AFT CABIN DR SILL BEAM AT FR.68 RH (A3NB-53-3-6187 ZONE 200 SEQ.618. LHT NR #5001115178-0010.
- [SDR CALA2022040600886](https://openairdocs.org/sdr/CALA2022040600886.md): Frame · cracked · Apr 5, 2022 · N801UA · Airbus A319131 · Fuselage Main, Frame
  > CRACK FOUND ON FUSELAGE AT FR35 LH STRG 30L HOLE#2. DAMAGED REPAIRED IAW ECRA 5331-02884, WORK ACCOMPLISHED BY 5H0356 & INSPECTED BY 5H0619.
- [SDR CALA2022040600885](https://openairdocs.org/sdr/CALA2022040600885.md): Frame · cracked · Apr 5, 2022 · N801UA · Airbus A319131 · Fuselage Main, Frame
  > CRACK FOUND ON FUSELAGE AT FR35RH STRG 30R HOLE#2. DAMAGED REPAIRED IAW ECRA 5331-02884, WORK ACCOMPLISHED BY 5H0356 & INSPECTED BY 5H0619.
- [SDR CALA2022033100814](https://openairdocs.org/sdr/CALA2022033100814.md): Bracket · corroded · Mar 28, 2022 · N801UA · Airbus A319131 · Fuselage Structure (General)
  > DURING INSPECTION OF THE BULK CARGO COMPARTMENT FOUND CORROSION IN FRAME 64 TO FRAME 65 STR 33 TO 25 REQ. EVALUATION AS NOTED ON LTPR NR# 5001118110-0020. INSPECTION PERFORMED ON AFT CRG COMPARTMENT, FOUND CORROSION ON CONSIDERED MAJOR AND PERMANENT CATEGORY A
- [SDR CALA2022032100722](https://openairdocs.org/sdr/CALA2022032100722.md): Flap Track · damaged · Mar 20, 2022 · N801UA · Airbus A319131 · Wing, Fuselage Attach Fittings
  > LH FLAP TRACK 2 AFT ATTACH BOLT 9 REQ EVA (A3NB-57-3-6286, SEQ# 1501).DURING INSTALLATION OF LH FLAP TRACK NO.2 BEAM, WE NOTICED A DAMAGE IN THE UPPER SURFACE. FURTHER EVALUATION IS REQUIRED AS NOTED ON LTPR NR# 5001117024-0110. DURING INSTALLATION OF FLP TRK#
- [SDR CALA2022030700582](https://openairdocs.org/sdr/CALA2022030700582.md): None · corroded · Mar 5, 2022 · N801UA · Airbus A319131 · Fuselage Structure (General)
  > DURING INSPECTION OF THE BULK CARGO COMPARTMENT FOUND CORROSION IN FRAME 64 TO FRAME 65 STR 33 TO 25 REQ. EVALUATION, AS NOTED ON LTPR NR# 5001118110-0040.
- [SDR CALA2022020100288](https://openairdocs.org/sdr/CALA2022020100288.md): Door Sill · corroded · Feb 1, 2022 · N801UA · Airbus A319131 · Fuselage, Wing Attach Fittings
  > CORROSION ON AFT CABIN FLR DR SILL BEAM FR.68 LH (A3NB-53-3-6187 ZONE:200 SEQ#618) AS NOTED ON LTPR NR# 5001115247-0010. CORROSION FOUND AT L2 DOOR SILL BEAM ADJACENT TO FR 68. REWORKED NO FURTHER ACTIONS REQUIRED. PERFORMED IAW SRM 51-74-00. AFTER REWORK WAS
- [SDR CALA2021031000278](https://openairdocs.org/sdr/CALA2021031000278.md): Seal · missing · Mar 7, 2021 · N801UA · Airbus A319131 · Engine Thrust Reverser
  > PDA 2 #1 ENG OUTBD SIDE T-R TO PYLON AFT MOST FLEXSEAL SEGMENT MISSING AT FWD END -- SEE PHOTO PHOTO ADDED REF ECRA 5450-02357 REV-B FIG 3 ITEM 120. THE AFT EGDE OF FLEXSEAL ITEM 120 IS INTACT AND NOT DAMAGED. PERFORMED INTERIM REPAIR PER PART 1D OF ECRA 5450-
- [SDR CALA2020010600089](https://openairdocs.org/sdr/CALA2020010600089.md): Hinge Fitting · broken · Jan 3, 2020 · N801UA · Airbus A319131 · Landing Gear Doors
  > RT MLG FWD DOOR HINGE FITTING 2 BROKEN HI-LOCKS MOST OBD SUP TAS K PER HGR NR9290353 GEN AT HAECO LCQ. UPDATING THE ATA CHAPTER TO 5300 ACCOMPLISH INTERIM REPAIR PER EC/RA 5311-02357 ACCOMPLISH PERMANENT REPAIR PER PART 3 OF EC/RA 5311-02357 ON OR BEFORE 03 JU
- [SDR CALA2020010600074](https://openairdocs.org/sdr/CALA2020010600074.md): Pressure Panel · cracked · Jan 2, 2020 · N801UA · Airbus A319131 · Fuselage Main, Structure
  > LH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLE 2,3,4,14,15,16, 17,19,20,22,23,24,25,26,27 AND 28 ARE CRACKED TO THE PRESSURE PA NEL. HOLE 28 IS ALSO CRACKED IN THE TITANIUM ANGLE SUPPORT TASK AD 2018-06-04 PER HAECO LCQ NR 9290281 GENERATED ACCOMPLISHED INTE
- [SDR CALA2020010600073](https://openairdocs.org/sdr/CALA2020010600073.md): Pressure Panel · cracked · Jan 2, 2020 · N801UA · Airbus A319131 · Fuselage Main, Structure
  > RH SIDE PRESSURE PANEL BETWEEN FRAME 35-36. HOLES 2,3,4,14,16,18,19,20,21,22,24,25,26,27,28 ARE CRACKED IN THE PRESSURE PANEL. H OLE 2 IS ALSO CRACKED IN THE CORNER FITTING SUPPORT TASK AD 2018 -06-04 PER HAECO LCQ NR 9290282 GENERATED ACCOMPLISHED INTERIM RE
- [SDR CALA2019051700778](https://openairdocs.org/sdr/CALA2019051700778.md): Spring · defective · May 16, 2019 · N801UA · Airbus A319131 · Cargo/Baggage Doors
  > AT 3500FT MSL, CARGO DOOR OPEN ECAM, AFT CARGO DOOR INDICATED OPEN. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN. CHECK AFT CARGO DOOR MEL 5270D. MAC METER INITIATED FOR WITH VENDOR, MAC RELATED WORK ORDER 000000001914103 AND PRTR, REPLACED HANDLE FLAP MECHANI
- [SDR CALA2019012500147](https://openairdocs.org/sdr/CALA2019012500147.md): Warning System · false activation · Jan 23, 2019 · N801UA · Airbus A319131 · Door Warning System
  > AFT CARGO DOOR ECAM. OPERATED AFT CARGO DOOR SEVERAL TIMES PER AMM52-32-00-710--001-A. OPERATIONAL CK GOOD.
- [SDR CALA2018011200170](https://openairdocs.org/sdr/CALA2018011200170.md): Cids · malfunctioned · Jan 12, 2018 · N801UA · Airbus A319131 · Emergency Lighting
  > IN FLT, THE CABIN LIGHTS FLICKERING ALONG WITH THE EMERGENCY LIGHTS. SEAT BELT CHIME DING INTERMITTANT. PERFORMED HIT CIDS2 DATA INTM FAIL AT FLT PH 06. RESET CIDS DIR2 AT CFDS. ALL CIDS LIGHT COTROL. FUNCTIONS NORMAL IAW AMM23-73-00.
- [SDR CALA2017112204190](https://openairdocs.org/sdr/CALA2017112204190.md): Sign · missing · Nov 22, 2017 · N801UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT SIGN MISSING. REPLACED THE SIGN ASSY. OPS CHECKED GOOD IAW AMM 33-00-00.
- [SDR CALA2017111804141](https://openairdocs.org/sdr/CALA2017111804141.md): Cable · broken · Nov 18, 2017 · N801UA · Airbus A319131 · Escape Slide
  > R2 DOOR SLIDE SOFT COVER RELEASE CABLE SAFETY BROKEN. INSTALLED A SLIDE.
- [SDR CALA2017092403317](https://openairdocs.org/sdr/CALA2017092403317.md): Cids · intermittent · Sep 24, 2017 · N801UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS ILLUMINATE WITH THE SWITCH ARMED. EMERGENCY LIGHTS GO OUT AFTER RECYCLING TO OFF THEN ARMED. RESET CID SYS, ALL LIGHTS CHECKED NORMAL IAW 33-23-00
- [SDR CALA2017063002057](https://openairdocs.org/sdr/CALA2017063002057.md): Light · faulty · Jun 30, 2017 · N801UA · Airbus A319131 · Emergency Equipment
  > L2 DOOR SLIDE ARM LIGHT ON ECAM PAGE ILLUMINATED AFTER DOOR CLOSED. REMOVED AND REPLACED THE SLIDE ARMED LIGHT IAW AMM 52-73-21-400-002-A AND TSM 52-13-00-810-803-A.
- [SDR CALA2016123001198](https://openairdocs.org/sdr/CALA2016123001198.md): Power Supply · inoperative · Dec 30, 2016 · N801UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS TEST FAILED AT PTP PANEL CABIN EMERGENCY POWER SUPPLY AND BATTERY POS 13WL WERE REPLACED IAW AMM 33-51-38 PG BLOCK 401 OP TEST IAW 33-51-38-740-050
- [SDR CALA2016092795778](https://openairdocs.org/sdr/CALA2016092795778.md): Skin · dented · Sep 26, 2016 · N801UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > SMALL DENT FOUND ON RT FUSELAGE, ONE FOOT ABOVE UPPER WINDOW LINE & 7 WINDOWS AFT OF OVERWING EXIT. DENT WAS OUT OF LIMITS IAW SRM 53-41- 11 FIG.101. FABRICATED & INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG 231, PG 503-504.
- [SDR CALA2016092795777](https://openairdocs.org/sdr/CALA2016092795777.md): Skin · dented · Sep 26, 2016 · N801UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN DENTED AT THREE PLACES BETWEEN FRAMES 23 & 24 AND STRINGERS 23 & 24L. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-11 FIG.115. FABRICATED AND INSTALLED A REPAIR DOUBLER IAW SRM 53-00-11 FIG.232 PG. 505-506.
- [SDR CALA2014081391970](https://openairdocs.org/sdr/CALA2014081391970.md): Skin · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.
- [SDR CALA2014081391969](https://openairdocs.org/sdr/CALA2014081391969.md): Skin · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.7.
- [SDR CALA2014081391968](https://openairdocs.org/sdr/CALA2014081391968.md): Skin · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT WING LOWER FUEL TANK LANDING 540HB HOLE AE & 540KB HOLE H WERE FOUND CORRODED. HOLES WERE REAMED TO 0.391 & 0.406 & REPAIRED IAW ECRA 5721-01374.
- [SDR CALA2014081391967](https://openairdocs.org/sdr/CALA2014081391967.md): Skin · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Wing, Plate/Skin
  > LEFT WING LOWER FUEL TANK LANDING 540HB HOLE B & 540KB HOLE D WERE FOUND CORRODED. HOLES WERE REAMED TO 0.363 & REPAIRED IAW SRM 57-21-11 PARA 5 B FIG 202.
- [SDR CALA2014081391964](https://openairdocs.org/sdr/CALA2014081391964.md): Fitting · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Main Landing Gear
  > LEFT MLG UPPER SIDE STAY BUSHING SHOWS EVIDENCE OF ROTATION. SEALANT IS SPLIT. CORROSION FOUND. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCH & FIP IAW 5
- [SDR CALA2014081391963](https://openairdocs.org/sdr/CALA2014081391963.md): Fitting · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Main Landing Gear
  > RIGHT MLG UPPER SIDE STAY BUSHING HAS EVIDENCE OF ROTATION. SEALANT FOUND SPLIT. REMOVED CORROSION BY OVER SIZING SIDE STAY FITTING LUG & INSTALLING HIGH INTERFERENCE FIT BUSHINGS IAW SRM 57-26-13 PARAGRAPH 5 E FIG 206. ACID ETCHED & FPI IAW 57-00-0PR8 & NT
- [SDR CALA2014081191928](https://openairdocs.org/sdr/CALA2014081191928.md): Door Sill · corroded · Aug 8, 2014 · N801UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R2 DOOR SILL FRAME 66 - 68 CORROSION FOUND OUT OF LIMITS. REPAIRED IAW SRM53-41-14 PARA 5A FIG 201.

Next page: https://openairdocs.org/aircraft/N801UA/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 = 'N801UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N801UA/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.