# Service difficulty reports: N877UA

A list on [N877UA](https://openairdocs.org/aircraft/N877UA.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR CALA2025112411419](https://openairdocs.org/sdr/CALA2025112411419.md): Stringer · corroded · Nov 15, 2025 · N877UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > AFT CABIN BELOW FLOORBOARDS CORRODED STRINGER 31R AT FR 65 FWD L OWER CORNER OF OUT FLOW CUT-OUT. REMOVED AND REPLACED DISCREPANT FR64-67 STR 31R STRINGER AND PER FORMED OVER SIZING REPAIR AS DIRECTED BY ECRA 5341-01535 CAR A R EPAIR. NO FURTHER ACTION REQUIR
- [SDR CALA2025111411210](https://openairdocs.org/sdr/CALA2025111411210.md): Fitting · cracked · Nov 10, 2025 · N877UA · Airbus A319132 · Elevator Structure
  > UPON REMOVAL FOUND SECONDARY FINDING NR 2 HINGE ARM LOWER SANDWHICH FITTING CRACKED. REMOVED AND REPLACED NR 2 HINGE ARM FITTING IAW SRM 55-36-42-300-003 NO FURTHER ACTION REQUIRED.
- [SDR CALA2025111211163](https://openairdocs.org/sdr/CALA2025111211163.md): Structure · corroded · Nov 8, 2025 · N877UA · Airbus A319132 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON SPIGOT BEARING INNER BORE HAS PITTING CORROSION. R & R NR 2 PYLON SPIGOT BEARING IAW AMM 54-51-41-000- 001-A, AND 54-51-41-400-001-A.
- [SDR CALA2025111211147](https://openairdocs.org/sdr/CALA2025111211147.md): Fitting · corroded · Nov 7, 2025 · N877UA · Airbus A319132 · Nacelle/Pylon, Main Frame
  > NUMBER 2 PYLON SPIGOT BEARING LOWER FITTING HAS PITTING CORROSION. REMOVED AND REPLACED THE NR 2 PYLON SPIGOT BEARING LOWER FITTING IAW SRM 54-51-12-300-002.
- [SDR CALA2025111211145](https://openairdocs.org/sdr/CALA2025111211145.md): Sleeve · corroded · Nov 7, 2025 · N877UA · Airbus A319132 · Nacelle/Pylon, Main Frame
  > NUMBER 2 ENGINE SPIGOT SLEEVE AND ATTACHING NUT HAVE PITTING CORROSION. RECEIVED AND REPLACED ENGINE 2 PYLON SPIGOT SLEEVE AND NUT IAW AMM 57-26-12-400-002-A.
- [SDR CALA2025111011034](https://openairdocs.org/sdr/CALA2025111011034.md): Stringer · corroded · Nov 4, 2025 · N877UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CORROSION AT FR61 STR 40R AFT PIT. REMOVED & REPLACED STRINGER 40R FROM FR61-FR64 IN AFT CARGO IAW A319 SRM 51-42-11/001.
- [SDR CALA2025111011032](https://openairdocs.org/sdr/CALA2025111011032.md): Stringer · corroded · Nov 4, 2025 · N877UA · Airbus A319132 · Fuselage Main, Longeron/Stringer
  > CORROSION AT FR61 STR41R AFT PIT. REMOVED & REPLACED STRINGER 41R FROM FR61-FR64 IN AFT CARGO IAW SRM 51-42-11/001.
- [SDR CALA2025110210791](https://openairdocs.org/sdr/CALA2025110210791.md): Skin · cracked · Oct 27, 2025 · N877UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > CRACK INDICATION AT HOLE NR 3 STR 30LT AT APROX BTW 1 & 2 O'CLOCK POSITION (INTERNAL VIEW) WITH 76% FSH IN THE FWD SKIN LAYER. PERFORMED OVERSIZING REPAIR AT LT AND RT FR35 SIDESHELL IAW EC/RA 5330-07616.
- [SDR CALA2025111011073](https://openairdocs.org/sdr/CALA2025111011073.md): Threshold · corroded · Oct 23, 2025 · N877UA · Airbus A319132 · Fuselage Main, Structure
  > AFT CARGO DOOR SILL PLATE HAS CORRODED NUTPLATES AND STRUCTURE O N UNDERSIDE 5 PLACES. REMOVED AND REPLACED DISCREPENT AFT CARGO THRESHOLD SILL PLATE I AW A319 SRM 51-42-11/001.
- [SDR CALA2025102710579](https://openairdocs.org/sdr/CALA2025102710579.md): Floor Support · cracked · Oct 23, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR PROFILE PANEL SUPPORT HOLE ELONGATED AT FR 63 STRINGER 35. REMOVED AND REPLACED PROFILE PANEL ON AFT CARGO BAY FLOOR,FR63/S TR35. IAW SRM 51-72-11-911-001.
- [SDR CALA2025102310436](https://openairdocs.org/sdr/CALA2025102310436.md): Fitting · corroded · Oct 21, 2025 · N877UA · Airbus A319132 · Emergency Equipment
  > FR 66R STR 23R FWD OF GIRT BAR FITTING HAS CORROSION. REPAIRED RT DOOR SILL FR 66 STR 23R FWD OF GIRT BAR FITTING IAW SRM 53-41-14-283-002.
- [SDR CALA2025102310435](https://openairdocs.org/sdr/CALA2025102310435.md): Seat Track · corroded · Oct 21, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE RT OTBD SEAT TRACK Y-1292 CORRODED AT FR 66. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-42-11/001.
- [SDR CALA2025102110348](https://openairdocs.org/sdr/CALA2025102110348.md): Floor Support · corroded · Oct 20, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT Y-1732 CORRODED FR 66 FWD LOWER CORNER R-2 DOOR. REMOVED AND REPLACED FLOOR SUPPORT Y-1732 R/H FR66 IAW SRM 51-42-11/001.
- [SDR CALA2025102110347](https://openairdocs.org/sdr/CALA2025102110347.md): Floor Support · corroded · Oct 20, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT Y-765 FR 64-70 HAS 2EA OUT OF LIMITS CORROSION SPOTS AT FR 66 AND 67. REMOVED AND REPLACED DISCREPANT Y-765 FR64-70 FLOOR SUPPORTIAW SRM 51-42-11-001.
- [SDR CALA2025101410058](https://openairdocs.org/sdr/CALA2025101410058.md): Seat Track · corroded · Oct 10, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT Y1292 SEAT TRACK FR 41-47 REQUIRES REPLACEMENT. REMOVED LT Y1292 SEAT TRACK FR 41-47 IAW SRM 51-42-11/001 R EV.154, REPLACED LH Y1292 SEAT TRACK FR 41-47 IAW SRM 51-42 -11/001 REV 154.
- [SDR CALA2025101410057](https://openairdocs.org/sdr/CALA2025101410057.md): Seat Track · corroded · Oct 10, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE SEAT TRACK Y512 CORRODED APROX 6 INCHES AF T OF FR 66. REMOVED AND REPLACED Y512 SEAT TRACK FR64-70 IAW SRM 51-42-11-001.
- [SDR CALA2025101510119](https://openairdocs.org/sdr/CALA2025101510119.md): Door Sill · corroded · Oct 9, 2025 · N877UA · Airbus A319132 · Fuselage Main, Structure
  > FRAME 68, STRINGER 23 ON DOOR SILL AFT INBD FLANGE HAS AREA OF CORROSION. REPAIRED RT DOOR SILL R2 AT FRAME 68 IAW A319 SRM 53-41-14-300 -001.
- [SDR CALA2025101309951](https://openairdocs.org/sdr/CALA2025101309951.md): Seat Track · corroded · Oct 9, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT Y-1292 SEAT TRACK FR 4147 REQUIRES REPLACEMENT. REMOVED AND REPLACED SEAT TRACK -Y1292 AT FR 41-47 IAW SRM 51-72-11-911-002 AND 51-42-11/001.
- [SDR CALA2025101309950](https://openairdocs.org/sdr/CALA2025101309950.md): Seat Track · corroded · Oct 9, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE LT OTBD SEAT TRACK Y 1292 CORRODED AT FR 65. REMOVED AND REPLACED THE SEAT TRACK BETWEEN FR 64-70 Y1292 IAW SRM 51-42-11-001.
- [SDR CALA2025102110323](https://openairdocs.org/sdr/CALA2025102110323.md): Seat Track · corroded · Oct 8, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > FWD WET AREA Y765 SEAT TRACK AT FR 16 HAS AREA OF CORROSION. R & R FR 12-24 Y765 SEAT TRACK IAW SRM 57-42-21-001.
- [SDR CALA2025101009902](https://openairdocs.org/sdr/CALA2025101009902.md): Attach Angle · cracked · Oct 8, 2025 · N877UA · Airbus A319132 · Wing Miscellaneous Structure
  > RIGHT WING FIXED L/E RIB 15 HAS CRACKED SMALL ANGLE AT INNER BOT TOM CORNER. REMOVED AND REPLACED RH WING FIXED L/E RIB 15 ATTACHED ANGLE IAW A319 SRM 51-42-11-001.
- [SDR CALA2025100809801](https://openairdocs.org/sdr/CALA2025100809801.md): Door Frame · corroded · Oct 7, 2025 · N877UA · Airbus A319132 · Fuselage Main, Structure
  > R2 LOWER DOOR FRAME UNDERNEATH THE SCUFF ON SHAPE SEAL HAS EXFOL IATIONS. REMOVED AND REPLACED DISCREPANT R2 LOWER SHAPE SILL IAW A319 SRM 57-42-11-002.
- [SDR CALA2025100809800](https://openairdocs.org/sdr/CALA2025100809800.md): Plate · worn · Oct 7, 2025 · N877UA · Airbus A319132 · Nacelle/Pylon, Main Frame
  > LEFT WING PYLON HYDRAULIC BULKHEAD FITTING PLATE IS WORN. REMOVED AND REPLACED LH WING HYDRAULIC BULKHEAD MOUNTING PLATE I AW A319 SRM 57-21-11-300-005.
- [SDR CALA2025100809798](https://openairdocs.org/sdr/CALA2025100809798.md): Seat Track · corroded · Oct 7, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > LEFT Y1292 SEAT TRACK FR 47-64 REQUIRES REPLACEMENT. REMOVED THE SEAT TRACK LH IAW SRM 51-42-11/001. REPLACED SEAT TRACK IAW A319 SRM 51- 42-11/001 REC. 154.
- [SDR CALA2025100709736](https://openairdocs.org/sdr/CALA2025100709736.md): Seat Track · corroded · Oct 4, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN RT FR20 SEAT TRACK Y-765 RT HAS CORROSION SPOT ON UPPER SURFACE. MAIN CABIN RH FR12 THRU FR24 SEAT TRACK Y-765 REMOVED AND REPLACED IAW SRM 51-42-11/001 AND 51-72-11-911-002.
- [SDR CALA2025100609645](https://openairdocs.org/sdr/CALA2025100609645.md): Fitting · corroded · Oct 3, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > TORSION-BOX COVER SHEET AT FR58 AFT COVER SHEET SUPPORT FITTING HAS CORROSION ON LOWER SURFACE. REMOVED AND REPLACED SUPPORT FITTING AT AFT CARGO DOOR TOSION BO X COVER SHEET FR 58 IAW A319 SRM 51-42-11-001.
- [SDR CALA2026090119127](https://openairdocs.org/sdr/CALA2026090119127.md): Frame · cracked · Sep 30, 2025 · N877UA · Airbus A319132 · Fuselage Main, Frame
  > RIGHT FR 16 DOUBLE JOGGLE HOLE NR 7 CRACKED AT 9 O' CLOCK IN FRAME LAYER. ACCOMPLISHED OVERSIZING REPAIR ON THE RT FR 16 DOUBLE JOGGLE IAW SRM 53-11-12-300-012. REAMED HOLE TO.2170" (SECOND OVERSIZE) PERFORMED ROTO SCAN WITH NO DEFECTS NOTED. T
- [SDR CALA2025100109512](https://openairdocs.org/sdr/CALA2025100109512.md): Floor Support · corroded · Sep 30, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE FLOOR SUPPORT Y 765 CORRODED AT FR 66. REMOVED FLOOR SUPPORT Y765 FR66 - 70 IAW SRM 51-72-11-911-001 REV.154, REPLACED FLOOR SUPPORT IAW SRM 51-72-1 1-911-001 REV 154.
- [SDR CALA2025100109490](https://openairdocs.org/sdr/CALA2025100109490.md): Seat Track · corroded · Sep 27, 2025 · N877UA · Airbus A319132 · Fuselage, Seat/Cargo Attach Fittings
  > MAIN CABIN RT, BETWEEN FRS 20-21, SEAT TRACK Y-1292 WAS CORRODED. SEAT TRACK REMOVED & REPLACED IAW SRM 51-42-11/001 & 51-72-11-911-002.
- [SDR CALA2025100109488](https://openairdocs.org/sdr/CALA2025100109488.md): Floor Support · corroded · Sep 27, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > CABIN FLOOR SUPPORT -Y765 CORRODED AT FR 67. REMOVED THE FLOOR SUPPORT, -Y765 FR67-70 IAW SRM 51-42-11/001, REV 154, REPLACED THE FLOOR SUPPORT, -Y765, FR67-70 IAW SRM 51-72-11/0 01, REV 154.
- [SDR CALA2025100109486](https://openairdocs.org/sdr/CALA2025100109486.md): Tee Angle · cracked · Sep 27, 2025 · N877UA · Airbus A319132 · Fuselage Miscellaneous Structure
  > RIGHT AFT ANGLE CRACKED. REMOVED TEE ANGLE ON FR41-42 KEEL BEAM IAW SRM 51-42-11/001 REV.154 AND EA 5331-01718 REV.D
- [SDR CALA2025042104052](https://openairdocs.org/sdr/CALA2025042104052.md): Hinge Fitting · worn · Apr 19, 2025 · N877UA · Airbus A319132 · Fuselage, Door Hinge
  > LH MLG DOOR FWD HINGE FTG FWD LUG FWD FACE HAS WEAR UNDER BOLT HEAD PER HAECO LCQ N/R 9294196/40196 GEN BY V892444 ENTERED ESFR REMOVED AND REPLACED LMLG DOOR FWR HINGE FITTING IAW A319 SRM 51 -72-11.
- [SDR CALA2025032403101](https://openairdocs.org/sdr/CALA2025032403101.md): Unknown · odor · Mar 22, 2025 · N877UA · Airbus A319132 · Air Distribution System
  > BURNING RUBBER SMELL BACK OF AIRCRAFT PER FA FA REPORTED SHORT PEROID OF BURNUNG SMELL AT AFT LAV AREA WHEN A/C APPOCHED TO THE GATE, PILOT REPORTS SMOOTH LANDING NO HARD BRAKING. NO SIGN OF SMOKE OR FIRE DURING EXTERIOR, CARGO AND INTERIOR GVI. CARGO AND LAV
- [SDR CALA2024122601665](https://openairdocs.org/sdr/CALA2024122601665.md): Fuel Cap · missing · Dec 22, 2024 · N877UA · Airbus A319132 · Fuel Storage
  > PDA 2 FUEL CAP MISSING FROM ACFT UPON ARRIVAL AT DFW REQUEST TO PLACE REFUEL CAP ON CDL 28A. ESFR ACCOMPLISHED. DISPATCH DESK: 11 NAME: NM DATE: 22-DEC-24-APPROVED CDL 28A FOR MISSING FUEL CAP PLACED REFUEL CAP ON CDL 28A.
- [SDR CALA2024122301619](https://openairdocs.org/sdr/CALA2024122301619.md): Battery Pack · no test · Dec 21, 2024 · N877UA · Airbus A319132 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - AFT LEFT ELPS BATTERY FAILED CAPACITY TEST. REPLACED ELPS BATTERY PER AIRBUS AMM 33-51-38. PARTS USED: 18-3351-3-0001,QTY:1
- [SDR CALA2024011200091](https://openairdocs.org/sdr/CALA2024011200091.md): Hose · leaking · Jan 10, 2024 · N877UA · Airbus A319132 · Hydraulic System, Main
  > GREEN HYD LEAK FOR CORRELATED CORRECTIVE SIGN OFF REFER TO LOG PAGE # 6778660. AFTER LANDING FOUND LEFT MLG DOOR ACTUATOR AFT LINE WITH HOLE LEAKING ON KEEL BEAM CONNECTION. LINE N.I.S. AT IAH. REMOVED AND REPLACED LEFT MLG DOOR ACTUATOR AFT LINE IN REF WITH A
- [SDR CALA2023092002833](https://openairdocs.org/sdr/CALA2023092002833.md): Fuel Cap · missing · Sep 18, 2023 · N877UA · Airbus A319132 · Fuel Storage
  > PDA 2 FOUND FUEL CAP MISSING ON ARRIVAL COMPLIED WITH CDL,NO LEAKSN UPDATED WITH PIC AND PLACED ON MEL DISPATCH DESK: 33 NAME: BDS DATE: 17-SEP-23- OK TO APPLY CDL....TOMC SMITH REPLACED FUEL CAP PARTS USED: 1859148,QTY:1 ROTABLE PARTS CHANGE WAS INDICATED
- [SDR CALA2023072102309](https://openairdocs.org/sdr/CALA2023072102309.md): Antenna · missing · Jul 19, 2023 · N877UA · Airbus A319132 · VHF Communications System
  > PDA 1 PDA FOUND #2 VHF LOWER ANTENNA MISSING INTO DEN. #2 VHF ANTENNA REPLACED PER AMM 23-12-11-400-001-A AND ACCOMPLISHED OPERATIONAL TEST PER AMM 23-12-00-710-001-A,OPS CHECKS GOOD SEALANT WILL BE INSTALLED ON LOG # 5210428. PARTS USED: 18-2312-3-0004,QTY
- [SDR CALA2023072102306](https://openairdocs.org/sdr/CALA2023072102306.md): Connector · cracked · Jul 19, 2023 · N877UA · Airbus A319132 · Door System Wiring
  > ECAM AFT CARGO DOOR REJECTED TO. FOUND CANNON PLUG BACKSHELL CRACKED/BROKEN ON AFT CARGO DOOR SILL INTERMITTENT INDICATION OF DOOR NOT LOCKED.VERIFIED AFT CARGO DOOR CLOSED AND LOCKED REQUEST MEL.VERIFIED AFT CARGO DOOR CLOSED AND ALL MANUAL LOCK INDICATORS AR
- [SDR CALA2023063002088](https://openairdocs.org/sdr/CALA2023063002088.md): Battery · inoperative · Jun 28, 2023 · N877UA · Airbus A319132 · Emergency Lighting
  > EPSU BATTERY 12WL TEST UNSATISFACTORY, EPSU BATTERY 12WL NEED TO BE REPLACED AS PER AMM 33-51-38/401 REV.120, RECORDED ON LTPR NR 5001242562-0010. EPSU BATTERY 12WL WAS REPLACED AS PER AMM 33-51-38/401 REV.120 P/N OFF: AD3214-31, S/N OFF: 274272, P/N ON: AD321
- [SDR CALA2023063002087](https://openairdocs.org/sdr/CALA2023063002087.md): Battery · inoperative · Jun 28, 2023 · N877UA · Airbus A319132 · Emergency Lighting
  > EPSU BATTERY 11WL TEST UNSATISFACTORY, EPSU BATTERY 11WL NEED TO BE REPLACED AS PER AMM 33-51-38/401 REV.120, RECORDED ON LTPR NR 5001242560-0010. EPSU BATTERY 11WL WAS REPLACED AS PER AMM 33-51-38/401 REV.120 P/N OFF: AD3214-31, S/N OFF: 291526, P/N ON: AD321
- [SDR CALA2023063002086](https://openairdocs.org/sdr/CALA2023063002086.md): Battery · inoperative · Jun 28, 2023 · N877UA · Airbus A319132 · Emergency Lighting
  > EPSU BATTERY 10WL TEST UNSATISFACTORY, EPSU BATTERY 10WL NEED TO BE REPLACED AS PER AMM 33-51-38/401 REV.120, RECORDED ON LTPR NR 5001242475-0010. EPSU BATTERY 10WL WAS REPLACED AS PER AMM 33-51-38/401 REV.120 P/N OFF: AD3214-31, S/N OFF: 250834, P/N ON: AD321
- [SDR CALA2023063002085](https://openairdocs.org/sdr/CALA2023063002085.md): Battery · inoperative · Jun 28, 2023 · N877UA · Airbus A319132 · Emergency Lighting
  > EPSU BATTERY 13WL TEST UNSATISFACTORY, EPSU BATTERY 13WL NEED TO BE REPLACED AS PER AMM 33-51-38/401 REV.120, RECORDED ON LTPR NR 5001242566-0010. EPSU BATTERY 13WL WAS REPLACED AS PER AMM 33-51-38/401 REV.120 P/N OFF: AD3214-31, S/N OFF: 231496, P/N ON: AD321
- [SDR CALA2023030300606](https://openairdocs.org/sdr/CALA2023030300606.md): Fastener · missing · Mar 3, 2023 · N877UA · Airbus A319132 · Nacelle/Pylon Structure
  > PDA 3 REF L-P3899302 FASTENER MISSING ENG2 PYLON OUTER PANEL 482AR. REPLACED FASTENER REF IPC 54-53-11-01A, TOMC ANDERSON NOTIFIED.
- [SDR CALA2022100602725](https://openairdocs.org/sdr/CALA2022100602725.md): Spring Assy · missing · Oct 6, 2022 · N877UA · Airbus A319132 · Steering Unit
  > PDA 3 NLG TOWING BOX BYPASS LEVER ONE SPRING CLIP MISSING (OUT OF TWO) -- SEE PHOTO PHOTO ADDED INSTALLED NEW SPRING CLIP AT NLG ELECT TOWING BOX -- REF IPC 32-51-12-01E
- [SDR CALA2022100302653](https://openairdocs.org/sdr/CALA2022100302653.md): Valve · faulty · Oct 3, 2022 · N877UA · Airbus A319132 · Air Distribution System
  > VENT SKIN VALVE FAULT. RESET SKIN AIR OUTLET AND AVIONICS VENT SYSTEM. SYSTEM OPS CHECK NORMAL REF AMM 21-26-00-710-001-A.
- [SDR CALA2021102902003](https://openairdocs.org/sdr/CALA2021102902003.md): None · none · Oct 28, 2021 · N877UA · Airbus A319132 · Lighting System
  > PDA 2 RH RETRACTABLE LANDING LIGHT MISSING REFERENCE LP 7322952. FLT 2069. MISSING PARTS IPC 33-42-11-01A ITEMS 10/20/30/40. ITEM PLACED ON CDL. REPLACED MISSING TERMINALS AND TAPED. COMPLIED WITH CDL 33G. ENTERED INTO HISTORY
- [SDR CALA2021072601178](https://openairdocs.org/sdr/CALA2021072601178.md): Skin · buckled · Jul 24, 2021 · N877UA · Airbus A319132 · Fuselage Main, Plate/Skin
  > AFT LOWER FUSELAGE SKIN BUCKLED AT FR73 AND FR 74 AT ALL 4 CORNE RS OF AFT JACK POINT STRUCTURE. REF TO AIRBORNE/PEMCO NR 11080.0025 REMOVED DAMAGED SKIN AND SUPPORTING SHEAR TIES AT FR 73-74, STR. 31L-31R IAW A319- SRM 53-51-29. FABRICATED NEW REPAIR DOUBLER
- [SDR CALA2021012000057](https://openairdocs.org/sdr/CALA2021012000057.md): Switch · failed · Jan 18, 2021 · N877UA · Airbus A319132 · Hydraulic System, Main
  > HYD G ENGINE 1 PUMP LO PR TOMC KROWN CHECKED GREEN HYD MODULE AND CASE DRAIN DPI, NOT POPPED. CHECKED SECURITY OF FIREWALL DISCONNECTS, TIGHT. RAN ENGINE AND GOOD PRESSURE, CYCLED GREEN PUMP AND OPERATED NORMAL. CONTINUE TO T-S 71-51-02 SHEET 1, WIRES GOOD.

## 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 = 'N877UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N877UA/reports

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