# Service difficulty reports: N827UA

A list on [N827UA](https://openairdocs.org/aircraft/N827UA.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 CALA2026101320340](https://openairdocs.org/sdr/CALA2026101320340.md): Feeder Cable · damaged · Sep 27, 2026 · N827UA · Airbus A319131 · Electrical Power System Wiring
  > DURING ALI VISIT, FOUND RT PYLON IDG FEEDER CABLE WIRE 2422-4519 INSULATION DAMAGED UNDER PANEL 521BT BETWEEN RIB 5A & PS 6480/RIB09 STA MLB. PERFORMED DAMAGE ASSESSMENT OF RT PYLON WIRE 2422-4519 IAW ESPM 20-53-21-02. REPAIRED WIRE WITH A GRADE 3 TEMP REPAIR
- [SDR CALA2026010912821](https://openairdocs.org/sdr/CALA2026010912821.md): Cover · unsecure · Jan 8, 2026 · N827UA · Airbus A319131 · Flight Compartment Equipment
  > FIRST OFFICER CHAIR WIRES HANGING OUT.WON`T MECHANICALLY OPERATE. CAN'T SLIDE IT MANUALLY. SECURED LOOSE SEAT PLASTIC COVER FOR SEAT ELEC SWITCH ON FO'S SEAT.
- [SDR CALA2025120411762](https://openairdocs.org/sdr/CALA2025120411762.md): Battery Pack · inoperative · Dec 3, 2025 · N827UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY. REMOVED AND REPLACED THE RT EPSU BATTERY PACK IAW AMM 33-51-38/401, OPS TESTED GOOD.
- [SDR CALA2025120211668](https://openairdocs.org/sdr/CALA2025120211668.md): Power Supply · no test · Nov 29, 2025 · N827UA · Airbus A319131 · Emergency Lighting
  > REMOVED EPSU (11WL) BATTERY, FOR USE ON A/C 4040, AND LOWER SIDEWALL PANEL AT LT WING EMERGENCY EXIT. REF 33-51-38-000-002-A. INSALLED NEW EPSU (11WL) AT LT WING EMERGENCY EXIT IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2025090508533](https://openairdocs.org/sdr/CALA2025090508533.md): Relay · faulted · Sep 3, 2025 · N827UA · Airbus A319131 · Engine Indicating System
  > AFTER T/O RECEIVED ENG 2 EGT OVER LIMIT EGT WAS AROUND 650 FLASH ING RED FOUND SEVERAL EGT THERMOCOUPLE CONNECTIONS LOOSE. REPLACED ALL 4 THERMOCOUPLES IAW AMM 77-21-15. PERFORMED BOROSCOPE INSPECTION OF COMBUSTION CHAMBER, HPT 1, 2, VANES AND BLADES. FOUND TH
- [SDR CALA2025081807859](https://openairdocs.org/sdr/CALA2025081807859.md): Strut · leaking · Aug 14, 2025 · N827UA · Airbus A319131 · Nose/Tail Landing Gear
  > FOUND LEAK FROM BACK SIDE OF STRUT HOUSING. A CONSTANT STREAM APPEARS TO BE COMING FROM BETWEEN BARREL & SWIVEL TUBE. NGL HAS HISTORY OF FLUID & NITROGEN SERVICE. ACCOMPLISHED CHECK OF NLG STEERING, HYD SYS HAS AN INTERNAL LEAK.. LEAKING FLUID SMELLS LIKE HY
- [SDR CALA2025060605340](https://openairdocs.org/sdr/CALA2025060605340.md): Unknown · vibration · May 31, 2025 · N827UA · Airbus A319131 · Standard Practices/Structures
  > MULTIPLE THUMPS/VIBRATIONS DURING CLIMB BTWN 7K-15K ALT AT 250-2 80 KTS. LOCKED FOR FERRY T/S IN PROGRESS.
- [SDR CALA2025031302790](https://openairdocs.org/sdr/CALA2025031302790.md): Battery · faulted · Mar 12, 2025 · N827UA · Airbus A319131 · Emergency Lighting
  > OPERATIONAL CHECK OF CABIN EMERGENCY LIGHTS {A3NB-33-3-6012} - BATTERY TEST SHOWING FAULT EPSU BATTERY EMERGENCY FWD LEFT. REMOVED AND REPLACED FWD LEFT EMERGENCY BATTERY PER AMM 33-51-38-000-002-A. OPS CHECK GOOD.
- [SDR CALA2025030302540](https://openairdocs.org/sdr/CALA2025030302540.md): Power Supply · no test · Mar 1, 2025 · N827UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - EPSU FWD LH MESSAGE FAILURE DISPLAYED ON TEST. REMOVED AND REPLACED FWD EMERGENCY POWER SUPPLY UNIT AS PER AMM 33-51-38/401. OPERATIONAL TEST GOOD.PARTS USED: 31-3350-9-9001, QTY:1
- [SDR CALA2024102300897](https://openairdocs.org/sdr/CALA2024102300897.md): Unknown · odor · Oct 19, 2024 · N827UA · Airbus A319131 · Air Distribution System
  > PREVIOUS FLIGHT CREW REPORTED ELECTRICAL ACRID SMELL IN FLIGHT DECK ONLY. NEED TO PERFORM AMM 05-51-10-200-801-C1 ATTACHED SMOKE FORM LABOR HOURS UPDATED. PERFORMED TASK 05-51-10-200-801-C1 ALONG WITH ECRA 0500-01058 FOUND NO EVIDANCE OF AN ODOR IN THE FLIGHTD
- [SDR CALA2024101400831](https://openairdocs.org/sdr/CALA2024101400831.md): Outflow Valve · faulted · Oct 11, 2024 · N827UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > ON CLMB THROUGH 7000 HAD 4 LOUD THUMPS FOLLOWED BY A DECREASG SH UDDER CREW REPORTED A THUMP WITH A SHUDDER. NOT FELT IN BACK ONLY FELT BY FWD FLT ATT AND FLT CREW. NO PASSENGERS COMMENTED ON NOISE. HAPPENED 4 TIMES 1 TO 2 MINTUES APART ON CLIMB NEVER HAPPENED
- [SDR CALA2024031900780](https://openairdocs.org/sdr/CALA2024031900780.md): Pressure Blkhd · cracked · Mar 17, 2024 · N827UA · Airbus A319131 · Fuselage Main, Bulkhead
  > DURING INSPECTION OF THE LH FUSELAGE PRESSURE BULKHEAD AT FR35 STR30LH HOLES PER EA 5310-07772 (SB A320-53-1393 R00), CRACK INDICATIONS WERE NOTED IN HOLE #2 (PREVIOUSLY REPAIRED PER ECRA 5310-07330A LOG PAGE 5963767). UPON FURTHER INSPECTIONS THE CRACK INDICA
- [SDR CALA2024041101029](https://openairdocs.org/sdr/CALA2024041101029.md): Frame · cracked · Mar 13, 2024 · N827UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 20 UPPER DOUBLE JOGGLE AREA HOLE C & 6 HAS CRACK INDIC ATIONS IN FRAME LAYER 12 OCLOCK 100% S.H AND 3 & 9 OCLOCK, 40% S. H. #C AND #D PER PART 2 OF LATEST REVISION OF EC/RA 5311-03164 ON CYCLES. REPEAT INSPECTIONS INTERVALS NOT TO EXCEED 7,300 OR BEFORE
- [SDR CALA2024040200923](https://openairdocs.org/sdr/CALA2024040200923.md): Frame · cracked · Mar 13, 2024 · N827UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 20 UPPER DOUBLE JOGGLE AREA HOLE C & 6 HAS CRACK INDIC ATIONS IN FRAME LAYER 12 OCLOCK 100% S.H AND 3 & 9 OCLOCK, 40% S. H. REPEAT INSPECTIONS INTERVALS NOT TO EXCEED 7,300 OR BEFORE THE AIRCRAFT REACHES 41,855 TOTAL ACFT FLT CYCLES, PERFORMED INTERIM
- [SDR CALA2024031400723](https://openairdocs.org/sdr/CALA2024031400723.md): Bottle · no test · Mar 13, 2024 · N827UA · Airbus A319131 · Emergency Equipment
  > L1 DOOR DAMPER DID NOT OPERATE DURING SLIDE DEPLOY OPS CHK. GENE RATED BY ON HAECO LCQ NR 9296917/32917 REMOVED AND REPLACED L-1 DOOR DAMPER CYLINDER IAW A319 AMM 52-11 -14-400-001-B/000-001-B. ACMP BY INSP BY ROTABLE PARTS CHANGE WAS INDICATED - TT # 1715249
- [SDR CALA2024031200692](https://openairdocs.org/sdr/CALA2024031200692.md): Frame · corroded · Mar 10, 2024 · N827UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR 16 UPPER DOUBLE JOGGLE AREA HOLE ''A'' HAS CRACK INDICATION IN FRAME LAYER, 5 OCLOCK, 100% S.H GENERATED BY V892444 ON HAECO LCQ NR 9296308/32308
- [SDR CALA2024022900603](https://openairdocs.org/sdr/CALA2024022900603.md): Profile · corroded · Feb 27, 2024 · N827UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO RH FR28 SPANWISE PROFILE PANEL HAS PULLED FASTENERS AT NUTPLATE. REMOVED AND REPLACED FWD CARGO RH FR 28 SPAN WISE PROFILE PANEL IAW A319 SRM 51-72-11-911-002 AND SRM 51-42-11-001.
- [SDR CALA2024022800591](https://openairdocs.org/sdr/CALA2024022800591.md): Floor Support · cracked · Feb 27, 2024 · N827UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FLT DECK FLOOR SUPPORT WEB @ RH FRAME 9-10 IS CRACKED.
- [SDR CALA2024030400632](https://openairdocs.org/sdr/CALA2024030400632.md): Fitting · cracked · Feb 16, 2024 · N827UA · Airbus A319131 · Fuselage Main, Structure
  > FLIGHT DECK WINDSHIELD CENTER POST LOWER NODE LEFT AND RIGHT CONTINUITY FITTINGS CRACKED ON HORIZONTAL FLANGE AFT FACE PER HAECO LCQ N/R 9296331/32331 GEN BY V061671 REPAIR PER HAECO REO-L24846 REV IR WITH NO DEVIATIONS. INCLUDED A T WINDSHIELD HOLE, ACCOMPLIS
- [SDR CALA2024021200376](https://openairdocs.org/sdr/CALA2024021200376.md): Floorbeam · cracked · Feb 8, 2024 · N827UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT PIT LT SIDE FR58 UPPER CENTER BETWEEN STRG 38L AND 38R PROFILE CRACKED. REMOVED AND REPLACED PROFILE PANEL AT AFT CARGO COMPARTMENT FR 5 8 CENTER UPPER BETWEEN STRG. 38L TO 38R IAW A319 SRM 51-72-11-91 1-001/002.
- [SDR CALA2024020500324](https://openairdocs.org/sdr/CALA2024020500324.md): Torque Box · corroded · Feb 4, 2024 · N827UA · Airbus A319131 · Fuselage Main, Structure
  > AFT PIT TORSION BOX COVERSHEET CORRODED. REMOVED AND REPLACED AFT CARGO TORSION BOX COVER SHEET AND THRES HOLD SHEET IAW A319 SRM 51-72-11-911-001 AND SRM 51-72-11-911-00 2.
- [SDR CALA2024020500325](https://openairdocs.org/sdr/CALA2024020500325.md): Panel · corroded · Feb 3, 2024 · N827UA · Airbus A319131 · Emergency Equipment
  > R-2 DOOR GIRT BAR MATING PLATE HAS MULTIPLE AREAS OF CORROSION ON SURFACE PER HAECO LCQ N/R 9296387/32387. REMOVED AND REPLACED DISCREPAMT R2 DOOR SILL IAW A319 SRM 51-42- 11-001- AND 51-72-11-001
- [SDR CALA2024012900245](https://openairdocs.org/sdr/CALA2024012900245.md): Floor Support · corroded · Jan 28, 2024 · N827UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT RT SIDE FR55 PROFILE CORRODED. REMOVED AND REPLACED PROFILE PANEL AT AFT CARGO FR55 R/H IAW A31 9 SRM 51-72-11-911-001 SRM 51-42-11-001 AND SRM 51-72-11-911-002.
- [SDR CALA2024012900244](https://openairdocs.org/sdr/CALA2024012900244.md): Floor Support · cracked · Jan 28, 2024 · N827UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT LT SIDE FR58 LOWER PROFILE CRACKED. REMOVED AND REPLACED PROFILE PANEL PLATE AT AFT PIT FR58 LOWER I AW A319 SEM 51-72-11-911-001 AND 51-42-11-001.
- [SDR CALA2024012900243](https://openairdocs.org/sdr/CALA2024012900243.md): Floor Support · corroded · Jan 28, 2024 · N827UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT PIT FR58 CTR PROFILE CORRODED. REMOVED AND REPLACED PROFILE PANEL SECTION AT AFT PIT FR58 IAW A 319 SRM 51-72-11-911-001 AND SRM 51-42-11-001
- [SDR CALA2024012200170](https://openairdocs.org/sdr/CALA2024012200170.md): Door Frame · cracked · Jan 19, 2024 · N827UA · Airbus A319131 · Fuselage Main, Structure
  > L/H O/W EMERGENCY HATCH CRACK B/W RIVETS ON HAECO LCQ NR 9296337/32337 REMOVED AND REPLACED FRAME SEGMENT ON LH O/W EMERGENCY HATCH IAW A319 SRM 51-72-11-911-001 7 SRM 51-42-11/001
- [SDR CALA2024012200171](https://openairdocs.org/sdr/CALA2024012200171.md): Door Frame · cracked · Jan 18, 2024 · N827UA · Airbus A319131 · Fuselage Main, Structure
  > R/H O/W EMERGENCY HATCH CRACK B/W RIVETS ON HAECO LCQ NR 9296336(32336) REMOVED AND REPLACED FRAME SEGMENT ON RH O/W EMERGENCY HATCH IAW A319 SRM 51-72-911-001 AND SRM 51-42-11/001
- [SDR CALA2023121503651](https://openairdocs.org/sdr/CALA2023121503651.md): Fitting · damaged · Dec 15, 2023 · N827UA · Airbus A319131 · Landing Gear Doors
  > GENERATE RFTS FOR DIRECTION ON THE MAIN LANDING GEAR DOOR FITTIN G SHEARED FASTENER FOUND AT HOLE L3 AS REFERENCED BY ECRA 5330-0 7177 (LH).
- [SDR CALA2023121503650](https://openairdocs.org/sdr/CALA2023121503650.md): Fitting · sheared · Nov 28, 2023 · N827UA · Airbus A319131 · Landing Gear Doors
  > DISCOVERED TWO SHEARED HIGH LOCKS, ONE ON EACH SIDE ( FWD AND AFT) OF THE HING AND ACTUATOR FITTING FOR THE R/H MLG DOOR AT KEELBEAM. FASTENERS HAVE BEEN REMOVED AND FASTENER LOCATION IS R3 AND R9. OLD FASTENERS MEASURE.0265 REPLACED R3 & R9 FASTENERS PER EC
- [SDR CALA2023102003133](https://openairdocs.org/sdr/CALA2023102003133.md): Fuel Cap · missing · Oct 19, 2023 · N827UA · Airbus A319131 · Fuel Storage
  > REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NO TED. REQUEST CDL 28A FOR MISSING FUEL CAP, NO LEAKS NOTED. NEW REFUEL/DEFUEL COUPLING CAP IAW AMM 28-25-41.
- [SDR CALA2023061201829](https://openairdocs.org/sdr/CALA2023061201829.md): Fuel Cap · missing · Jun 8, 2023 · N827UA · Airbus A319131 · Fuel Storage
  > PDA 2 FUEL FOUND MISSING ON ARRIVAL TO JAX. INSTALLED NEW FUEL CAP.
- [SDR CALA2023032000810](https://openairdocs.org/sdr/CALA2023032000810.md): Sensor · unknown · Mar 20, 2023 · N827UA · Airbus A319131 · Engine Indicating System
  > EPR MODE FAULT - ENG 2. REFER TO A320 TSM 77-ECAM AND UA A320 ME L CARD 73 120. R/R P2/T2 SENSOR REF AMM 73-22-11. PERFORMED OPERATIONAL CHECK FOR P2/T2 SENSOR. OPERATIONAL CHECK. PASSED FOR BOTH 2A AND 2B CHANNEL
- [SDR CALA2023032000817](https://openairdocs.org/sdr/CALA2023032000817.md): Sensor · unknown · Mar 20, 2023 · N827UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > ENG2 EPR MODE FAULT ECAM MSG ON TAKEOFF ROLL. REJECTED T/O. PILOT REPORTED THE RTO WAS A LOW ENERGY STOP, LESS THAN 60 FOUND CONNECTOR BACKSHELL CROSS THREADED. PLUG LOCATED ON P2T2 REMOVED BACKSHELL FOUND BROKEN WIRE. KNOTS. PILOT STATED THE AUTO BRAKES DID
- [SDR CALA2021091501579](https://openairdocs.org/sdr/CALA2021091501579.md): Cap · broken · Sep 15, 2021 · N827UA · Airbus A319131 · Emergency Lighting
  > EPL ON END CAP AILSE SIDEOF PAX SEAT 8C IS BROKEN. REPLACED SEAT MOUNTED EPL IAW AMM 31-51-11-400-002-A OPS. CHK''S. GOOD IAW AMM 33-51-00-501. ACP''D IDT INSP OF EPL AT SEAT 8C, OPS CHECK GOOD REF AMM 33-51-00-501.
- [SDR CALA2021080601277](https://openairdocs.org/sdr/CALA2021080601277.md): Seal · missing · Aug 6, 2021 · N827UA · Airbus A319131 · Landing Gear Doors
  > PDA 3 L-SHAPE RUBBER SEAL MISSING FROM AFT SIDE OF NOSE GEAR DOORS.RIG HTSIDE REF L-P 6799242. SEE L-P 6763146.
- [SDR CALA2021041400464](https://openairdocs.org/sdr/CALA2021041400464.md): Battery · failed · Apr 13, 2021 · N827UA · Airbus A319131 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS OPERATIONAL CHECK: - EEL TEST FAILS EPSU UNIT FWD L. REPLACED EEL POWER SUPPLY UNIT FWD LEFT 10WL IAW AMM 33-51-38-400-001-AO, ALSO REPLACED BATTERY PACK FWD LEFT IAW AMM 33-51-38-400-002-AO. RETESTED OPS. TEST GOOD. ROTABLE PARTS CHANG
- [SDR CALA2020030600572](https://openairdocs.org/sdr/CALA2020030600572.md): Oxygen Box · faulty · Mar 2, 2020 · N827UA · Airbus A319131 · Crew Oxygen System
  > F/O O2 MASK WILL NOT TEST REMOVED AND REPLACED OXYGEN BOX REF AMM 35-21-41. OPS CKS AND LEAK CKD GOOD. AMM FOLLOWED IS 35-11-41.
- [SDR CALA2020030600570](https://openairdocs.org/sdr/CALA2020030600570.md): Valve · inoperative · Mar 2, 2020 · N827UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > SKIN VALVE FAULT DISPLAYED ON UPPER ECAM SCREEN. - V ENT CT VALVE NOT CLOSING WITH SKIN.. FAULT 22HQ REPLACED ON LOG PAGE 4615093.
- [SDR CALA2020022900555](https://openairdocs.org/sdr/CALA2020022900555.md): Outflow Valve · malfunctioned · Feb 28, 2020 · N827UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > VENT AVNCS SYS FAULT UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CREW PERFORMED AEVC TEST FAULTING 22HQ. APPLY MEL 2126C MAC RELATED WORK ORDER 000000002377099 AND PRTR OK TO USE MEL 2126C FOR SKIN AIR OUTLET VALVE 22HQ INOP. VALVE D EACTIVATED REF AMM 21-26-
- [SDR CALA2020011900192](https://openairdocs.org/sdr/CALA2020011900192.md): Skin · not reported · Jan 17, 2020 · N827UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > REQUIRE DIP OF SMALL CUTOUT EXTERNAL TEMPORARY DOUBLER REPAIR IAW SRM 53-00-11-300-011 ACCOMPLISHED ON LOG PAGE #3415550 FOR A LIFE LIMITED TIME. ACCOMPLISHED TEMPORARY REPAIR OF LOGPAGE 3415550 FOR A SMALL CUTOUT DOUBLER REPAIR ON THE LH FUSELAGE BODY FAIRING
- [SDR CALA2019060700909](https://openairdocs.org/sdr/CALA2019060700909.md): Skin · punctured · Jun 7, 2019 · N827UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > PUNCTURE IN SKIN IN LINE WITH AFT EDGE OF PANEL 197GB ON GOLD ST RIPE, APPROX 4" X 3". THIS IS LEFT SIDE OF FUSELAGE APPROX STA 2 2428/FR56 AT FLOOR LINE. REPAIR ACCOMPLISHED ON LOG PAGE 3415550
- [SDR CALA2019050300689](https://openairdocs.org/sdr/CALA2019050300689.md): Battery · discharged · May 2, 2019 · N827UA · Airbus A319131 · Emergency Lighting
  > (SUPPORT TASK) THE EMERGENCY LIGHT TEST AT THE PTP FAILS WITH TH E MESSAGE ''EPSU BATTERY AFT L?. REFER TO N/R: 9303386. REMOVED AND REPLACED BATTERY & EPSU 13WL AFL LECT. IAW AMM 33-51-38-000-002-A AND 33-51-38-400-002-A. OPERATIONAL TEST GOOD IAW AMM SUBTASK
- [SDR CALA2018122902680](https://openairdocs.org/sdr/CALA2018122902680.md): Indicator · false indication · Dec 29, 2018 · N827UA · Airbus A319131 · Hydraulic Handpump, Main
  > GREEN HYD RESERVIOR DROPPED TO HALF AFTER GEAR RETRACTION. UPON GEAR EXTENSION HYDRAULIC QTY WENT BACK TO NORMAL. REPORTED BY CREW TOMC SMITH UPDATED MAA CODE FIX USING VENDOR MAA SCREEN CONTACT TOMC 847-700-9980 MAC RELATED WORK ORDER 000000001703210 AND PRT
- [SDR CALA2018122872663](https://openairdocs.org/sdr/CALA2018122872663.md): Line · leaking · Dec 27, 2018 · N827UA · Airbus A319131 · Hydraulic System, Main
  > HYDRAULIC LEAK ONRIGHT MAIN LANDINGGEAR INVESTIGATE AND CONTACT TOMC. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V913928 MAC RELATED WORK ORDER 000000001703129 AND PRTR CLEANED AREA AND FOUND THE RH MLG STAY LOCK AC
- [SDR CALA2017122304573](https://openairdocs.org/sdr/CALA2017122304573.md): Skin · cracked · Dec 22, 2017 · N827UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN AT FRAME 35, STRINGER 30L, AFT LOWER FASTENER HOLE HAS A CRACK INDICATION. ACCOMPLISHED ALL STEPS OF ECRA 5310-07330.
- [SDR CALA2017120104244](https://openairdocs.org/sdr/CALA2017120104244.md): Skin · dented · Nov 29, 2017 · N827UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > DENT ON EXTERIOR FUSELAGE SKIN LH SIDE AT FRAME 11 JUST ABOVE STRINGER R23. REPAIRED DENT ON EXTERIOR FUSELAGE SKIN LH SIDE AFT OF FRAME 11 ABOVE STGR 23 REF SRM 53-00-11-300-029. INSPECTION THRESHOLD FRO M TIME OF REPAIR EMBODIMENT IS 60,000 FLT CYCLES OR 12
- [SDR CALA2017120104239](https://openairdocs.org/sdr/CALA2017120104239.md): Skin · none · Nov 28, 2017 · N827UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > REF EA 2300-01842 OP-0 ACCOMPLISH DOUBLER REPAIR AT ANTENNA FR 63-64 STR 41L-STR 42L. ACCOMPLISHED REPAIR DOUBLER AT AIRPHONE ANTENNA FR 63-64 STR 41L -STR 42L REFERENCE SRM 53-00-11-300-029. FUTURE INSPECTION THRES HOLD FROM TIME OF REPAIR EMBODIMENT IS 56,50
- [SDR CALA2017112704232](https://openairdocs.org/sdr/CALA2017112704232.md): Structure · corroded · Nov 27, 2017 · N827UA · Airbus A319131 · Fuselage Main, Structure
  > R2 FWD INBD DOOR SILL GIRT BAR ATTACHMENT AREA FOUND TO BE CORRODED. BLENDED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-41-14-283-002. PERFORMED A REPAIR, PRINCIPLES 1 AND 9 IAW SRM 53-41-14 -300-001, SHEETS 2, AND 5.
- [SDR CALA2017111704125](https://openairdocs.org/sdr/CALA2017111704125.md): Slide · contaminated · Nov 17, 2017 · N827UA · Airbus A319131 · Escape Slide
  > LEFT OVERWING SLIDE HAD EXCESSIVE MOISTURE INGRESS. REMOVED AND INSTALLED THE SLIDE.
- [SDR CALA2017060501726](https://openairdocs.org/sdr/CALA2017060501726.md): Power Supply · no test · Jun 5, 2017 · N827UA · Airbus A319131 · Emergency Lighting
  > DURING 2 SVC, CABIN EMERGENCY LIGHTS TEST FAILED ON CIDS BY DISPLAYING EPSU BATTERY LT, AND EPSU COMM FWD. LT. REPLACED AFT CABIN EMERGENCY POWER SUPPLY AND BATTERY IAW AMM 33-51-38, TEST NOW PASSES.

Next page: https://openairdocs.org/aircraft/N827UA/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 = 'N827UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N827UA/reports

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