# Service difficulty reports: N836UA

A list on [N836UA](https://openairdocs.org/aircraft/N836UA.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 · 119 reports

- [SDR CALA2026102220526](https://openairdocs.org/sdr/CALA2026102220526.md): Floor Support · cracked · Oct 20, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO, FRMS 28 - 34, STR 35R. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11/001 2E, SRM 51-44-11/001, SRM 51-46-11/00 1, & SRM 51-75-12-911-002.
- [SDR CALA2026101320315](https://openairdocs.org/sdr/CALA2026101320315.md): Floor Support · corroded · Oct 10, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOORBOARD PROFILE AT FR 58-59 STR 38L, FLOORBOARD RISER/RAMP CORRODED. REMOVED AND REPLACED AFT CARGO FLOORBOARD RISER AT FR 58-59 STR 38L IAW SRM 51-42-11 AND SRM 51-72-11-911-001.
- [SDR CALA2026100720181](https://openairdocs.org/sdr/CALA2026100720181.md): Seat Track · corroded · Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK Y-765 AND FRAME 20 2 AEREAS. REMOVED AND REPLACED SEAT TRACK 765 IAW A319 SRM 51-42-11 FROM F R12-FR24.
- [SDR CALA2026100720173](https://openairdocs.org/sdr/CALA2026100720173.md): Seat Track · corroded · Oct 5, 2026 · N836UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION LOCATED AT SEAT TRACK Y-1292 AND FRAME 20. REMOVED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 RE V 159 PAR 2.F, REPLACED SEAT TRACK Y-1292 FR12-FR24 IAW A319 SRM 51-42-11/001 REV.159 PAR. 2.F.
- [SDR CALA2026100620132](https://openairdocs.org/sdr/CALA2026100620132.md): Window Frame · cracked · Oct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT WINDSHIELD FRAME CONTINUITY FITTING AREA ROTO TEST INSPECTIO N FOUND CRACK INDICATION IN MOST I/B HOLE GEN BY V929087 ON AAR LCQ NR 9298821/26821 UP DATED EFSR REPAIRED R/H WINDSHIELD FRAME MOSL I/B FASTENER HOLE IAW A319 EC RA NO.5311-03421 OVERSIZE AND
- [SDR CALA2026100620130](https://openairdocs.org/sdr/CALA2026100620130.md): Floorbeam · corroded · Oct 3, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor Beam
  > AFT WET AREA, LT FLOOR BEAM Y160.5, BARREL NUT CORRODED IN LAV MOUNT FITTING, JUST AFT OF FR 68. REMOVED AND REPLACED L/H FLOOR BEAM Y160.5 FR68-70 IAW A319 SRM 51-72-11-911-001
- [SDR CALA2026092920004](https://openairdocs.org/sdr/CALA2026092920004.md): Floor Support · corroded · Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT FLOOR BOARD PROFILE AT FR 56-58 STR38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR BOARD PROFILE A T FR56-58 STR 38L IAW A319 SRM 51-44-11.
- [SDR CALA2026092920000](https://openairdocs.org/sdr/CALA2026092920000.md): Floor Support · corroded · Sep 29, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT, FR 52-56, STR38L HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO COMPARTMENT FLOOR SUPPORT IAW SRM 51-41-4.
- [SDR CALA2026092819921](https://openairdocs.org/sdr/CALA2026092819921.md): Skin · damaged · Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT TOP SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 146 INCHES FROM INBD EDGE AND 12 1/2 INCHES FROM T/E. DEFECT IS 1 3/4 INCH IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN IAW SRM 55-21-11-300-005. CATEGORY A REPAIR.
- [SDR CALA2026092819919](https://openairdocs.org/sdr/CALA2026092819919.md): Skin · damaged · Sep 25, 2026 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LEFT TOP & BOTTOM SKIN PANEL FOUND LIQUID ENGRESS INDICATION AT 160" FROM INBD EDGE, AND 9 1/2" FROM T/E. DEFECT IS 2 INCHES IN SIZE. REPAIRED THE LT ELEVATOR TOP SKIN 160IN FROM INBD EDGE 9.5IN FROM T/E 2 INCHES IN DIA IAW SRM 55-21-11-300-005.
- [SDR CALA2026092519838](https://openairdocs.org/sdr/CALA2026092519838.md): Floorbeam · damaged · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Main, Floor Beam
  > FWD CARGO FLOORBEAM, FR28, STR 38R-38L HAD MULTIPLE ELONGATED HOLES. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-42-11-001A,
- [SDR CALA2026092519836](https://openairdocs.org/sdr/CALA2026092519836.md): Floor Support · corroded · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY FLOOR SUPPORT AT FR 59-63, STR 38L HAS MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE AFT CARGO PROFILE PANEL IAW SRM 51-42-11.
- [SDR CALA2026092519834](https://openairdocs.org/sdr/CALA2026092519834.md): Panel · corroded · Sep 24, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT SLOPING PANEL PROFILE AT FR 54-56, STR 35R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO SLOPING PANEL PROFILE IAW SRM 51-42-11.
- [SDR CALA2026092819868](https://openairdocs.org/sdr/CALA2026092819868.md): Profile · corroded · Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD PIT PROFILE AT FR 27, S38L WAS CORRODED. REMOVED AND REPLACED FWD PIT PROFILE IAW SRM 5 1-42-11.
- [SDR CALA2026092519805](https://openairdocs.org/sdr/CALA2026092519805.md): Fitting · corroded · Sep 23, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > L2 DOOR CUTOUT, AFT CORNER FITTING CORRODED. REMOVED AFT CORNER ON L2 DOOR IAW SRM 51-42-11/001, REV 159, PAR 2.G, 2.F. REPLACED THE AFT CORNER ON L2 DOOR IAW SRM 51-42-1 1/001, REV 159. PARA 2.E,2.F.
- [SDR CALA2026092419768](https://openairdocs.org/sdr/CALA2026092419768.md): Fitting · corroded · Sep 21, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FRAME 68 HAS A DRILLED OUT FASTENER WITH CORROSION AROUND IT AFT CABIN. REMOVED AND REPLACED FITTING AT AFT CABIN FLOOR IAW SRM 51-42-11.
- [SDR CALA2026092219672](https://openairdocs.org/sdr/CALA2026092219672.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY FLOORBOARD AT FR 52-56, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219670](https://openairdocs.org/sdr/CALA2026092219670.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY, FLOORBOARD AT FR 51-52, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED THE FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219668](https://openairdocs.org/sdr/CALA2026092219668.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO COMPARTMENT FLOORBOARD AT FR 59 - 63, STR 38R HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO FLOORBOARD IAW SRM 51-42-11.
- [SDR CALA2026092219666](https://openairdocs.org/sdr/CALA2026092219666.md): Floorboard · corroded · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Floor Panel
  > AFT CARGO BAY CENTER FLOORBOARD AT FR 51 HAD MULTIPLE SPOTS OF CORROSION. REMOVED AND REPLACED AFT CARGO PROFILE PANEL AT FR57 IAW SRM 51-42-11.
- [SDR CALA2026092219664](https://openairdocs.org/sdr/CALA2026092219664.md): Panel · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO RT BOTTOM SLANT TO FLOOR PROFILE STR 38 HAD A CRACK AT FR 28 +1. REMOVED AND REPLACED PROFILE PANEL ON FWD CARGO BAY IAW SRM 51-42-11-001.
- [SDR CALA2026092219662](https://openairdocs.org/sdr/CALA2026092219662.md): Seal · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Nacelle/Pylon, Main Frame
  > RIGHT PYLON FWD INBD BLADE SEAL CRACKED. REMOVED AND REPLACED BLADE SEAL AT RT PYLON FWD INBD IAW SRM 51-42-11.
- [SDR CALA2026092219660](https://openairdocs.org/sdr/CALA2026092219660.md): Panel · cracked · Sep 19, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO LT BOTTOM SLANT FLOOR PROFILE HAD MULTIPLE CRACKS AROUND FASTENER HOLES AT FR 28 +10 IAW AAR LCQ N/R 9298507/26507. REMOVED AND REPLACED FWD CARGO PROFILE PANEL IAW SRM 51-42- 11.
- [SDR CALA2026101220280](https://openairdocs.org/sdr/CALA2026101220280.md): Gusset · cracked · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 66, STRINGER 14R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026092119617](https://openairdocs.org/sdr/CALA2026092119617.md): Support · corroded · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA, LT FR 69 - 70, SHEAR PLATE SUPPORT CORRODED. REMOVED AND REPLACED SHEAR PLATE SUPPORT ON AFT WET AREA BTW FR 70 -FR 69 LT STR 23 IAW SRM 51-42-11.
- [SDR CALA2026092119615](https://openairdocs.org/sdr/CALA2026092119615.md): Panel · corroded · Sep 18, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FWD CARGO SLOPING PANEL VERTICAL PROFILE 10" FWD OF FR30, STR 38R CORRODED. REMOVED AND REPLACED FWD CARGO PROFILE PANEL AT FR 30, STR 38R IAW SRM 51-42-11.
- [SDR CALA2026101220277](https://openairdocs.org/sdr/CALA2026101220277.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68, STRINGER 14L GUSSET PLATE 2ND HOLE FROM BOTTOM IS VISIBLY OUT OF ROUND. THE GUSSET PLATE WAS R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026101220275](https://openairdocs.org/sdr/CALA2026101220275.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > FRAME 68, STRINGER 12R, GUSSET PLATE MIDDLE HOLE IS VISIBLY ELONGATED IN GUSSET PLATE LAYER. GUSSET PLATE R & R IAW SRM 53-41-12-300-018, FIGURE 1.
- [SDR CALA2026101220271](https://openairdocs.org/sdr/CALA2026101220271.md): Gusset · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FR 66, STR 16L GUSSET PLATE TOP HOLE HA S A REJECTABLE INDICATION. GUSSET PLATE REMOVED AND REPLACED IAW SRM 53-41-12-300-018, FIGURE 1. FLOWCHART SOLUTION 1. GVI & HFEC INSPECTION COMPLETED PER NTMS 51-90-00, 5110-08 AND 51-10-01. NO DAMAGE FOUND ON FRAME I
- [SDR CALA2026092219644](https://openairdocs.org/sdr/CALA2026092219644.md): Door Sill · corroded · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > L2 DOOR SILL HAS CORROSION JUST INBD OF AFT GIRT BAR FITTING. EVALUATED & REPAIRED L-2 DOORSILL JUST INBD OF AFT GIRT BAR FITTING, REPAIR/EVAL FOUND TO BE CATEGORY A NO FURTHER ACTION REQUIRED IAW SRM 53-41-14-300-001, & 53-41-14-283-002.
- [SDR CALA2026092219642](https://openairdocs.org/sdr/CALA2026092219642.md): Shear Plate · corroded · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT WET AREA, RT FR 69 - 70,SHEAR PLATE CORRODED. REMOVED AND REPLACED SHEAR PLATE IAW SRM 51-42-11/001 AND 5 1-72-11-911-002.
- [SDR CALA2026091819548](https://openairdocs.org/sdr/CALA2026091819548.md): Door Frame · cracked · Sep 17, 2026 · N836UA · Airbus A319131 · Fuselage Main, Structure
  > RIGHT EMERGENCY EXIT, FWD LOAD TRANSMITTING PROFILE SHOWS SIGNS OF CRACKING. REMOVED & REPLACED THE FRAME SEGMENT IAW SRM 51-72-11-911-001, & SRM 51-42-11-001.
- [SDR CALA2026080618338](https://openairdocs.org/sdr/CALA2026080618338.md): None · no discrepancy · Aug 4, 2026 · N836UA · Airbus A319131 · Standard Practices/Structures
  > AFTER LANDING..STRONG ELECTRICAL BURNING ODOR. NO SMOKE APPARENT. INSPECTED FWD GALLEY AREA, FLIGHT COMPARTMENT FOR REPORTED ODOR/SMELL DID NOT FIND ANY SOURCE FROM ACFT. DID FIND HEAVY ODOR FROM ROOF TAR VEHICLE PARKED AT GATE AREA EMMITTING HEAVY PUNGENT
- [SDR CALA2026030214153](https://openairdocs.org/sdr/CALA2026030214153.md): Acm · faulted · Feb 26, 2026 · N836UA · Airbus A319131 · Cabin Cooling System
  > A/C PACK NR 1 OVHT. PACK OUTLET TEMP GOT AS HIGH AS 136 DEGREES. WITH THE PACK SELECTED ON & THE FCV SHOWING OPEN, THE ACM DOES NOT APPEAR TO BE RUNNING. SUSPECT THE ACM FAILED. PACK 1 SWITCH SELECTED OFF, VERIFIED THE FCV IS CLOSED ON THE BLEED PAGE, AND
- [SDR CALA2026022714116](https://openairdocs.org/sdr/CALA2026022714116.md): A/C Pack · odor · Feb 26, 2026 · N836UA · Airbus A319131 · Cabin Cooling System
  > THE CABIN CREW REPORTED SMELLING AN ACRID ODOR ON ARRIVAL. SUSPECT RELATED TO THE PACK 1 OVERHEAT. THE ODOR WAS ABLE TO BE DUPLICATED ONLY WHEN RUNNING PACK 1 OFF THE APU. ACCOMPLISHED CONDITIONAL INSPECTION IAW AMM 05-51-10-200-801-C1, PARA 1, ODOR WAS ISOLA
- [SDR CALA2025101610189](https://openairdocs.org/sdr/CALA2025101610189.md): Actuator · faulted · Oct 14, 2025 · N836UA · Airbus A319131 · Compressor Bleed Control
  > ENGINE 1 COMPRESSOR VANE ECAM REJECTED T.O. LESS THAN 50KTS ADDED. R & R NUMBER 1 ENG VSV ACTUATOR PER 75-32-41-400-010-010-A AFTER INSTALLATION PERFORMED LEAK CHECK AND POWER ASSURANCE RUN NO LEAKS AND NO ECAM MESSAGE NOTED.
- [SDR CALA2025030302548](https://openairdocs.org/sdr/CALA2025030302548.md): Packing · damaged · Feb 28, 2025 · N836UA · Airbus A319131 · Hydraulic System, Main
  > HYD Y RSVR LO LVL ECAM AT FL370 FOUND YELLOW SYSTEM QUANTITY ABOVE AMBER BOX. SERVICED QUANTITY INTO SERVICEABLE BAND AND RAN HYDRAULICS. FOUND LEAK AT PTU 3039 GM CONNECTION. REF AMM 12-12-29, AMM 29-00-99. REMOVED CHECK VALVE 3039GM, REPLACED FAILED PACKING
- [SDR CALA2024021900459](https://openairdocs.org/sdr/CALA2024021900459.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 33 INCHES FROM I/B EDGE, 20 1/ 2 INCHES FROM TRAILING EDGE AND 2 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 33IN FROM I/B 20.5IN FROM T/E 2I N DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024021900458](https://openairdocs.org/sdr/CALA2024021900458.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 20 INCHES FROM I/B EDGE, 19 IN CHES FROM TRAILING EDGE AND 2 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 20IN FROM I/B 19IN FROM T/E ZONE 1 2IN DIA IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024021900457](https://openairdocs.org/sdr/CALA2024021900457.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 26 INCHES FROM I/B EDGE, 11 1/ 2 INCHES FROM TRAILING EDGE AND 1 3/4 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 26IN FROM I/B 11.5 IN FROM T/E 1.75 IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAI R.
- [SDR CALA2024021900456](https://openairdocs.org/sdr/CALA2024021900456.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 22 INCHES FROM I/B EDGE, 7 1/2 INCHES FROM TRAILING EDGE AND 2 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 22IN FROM I/B 7.5IN FROM T/E ZON E 1 AND 3. 2IN DIA IAW A319 SRM 55-21-11-300-005 CATEGORY A REPA IR.
- [SDR CALA2024021900455](https://openairdocs.org/sdr/CALA2024021900455.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 83 INCHES FROM I/B EDGE, 22 INCHES FROM TRAILING EDGE, 2 1/2 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 83IN FROM I/B 22IN FROM T/E 2.5I N DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024021900454](https://openairdocs.org/sdr/CALA2024021900454.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > LH ELEVATOR HAS LIQUID INGRESS AT 96 1/2 INCHES FROM I/B EDGE, 1 0 INCHES FROM TRAILING EDGE, 4 INCHES IN DIAMETER. REPAIRED LH ELEVATOR UPPER SKIN 96.5 INCHES FROM T/E 4IN DIA ZON E 1 IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024021900453](https://openairdocs.org/sdr/CALA2024021900453.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS LIQUID INGRESS AT 21 INCHES FROM I/B EDGE, 24 IN CHES FROM TRAILING EDGE AND 1 INCH IN DIAMETER. REPAIRED RH ELEVATOR UPPER SKIN 21IN FROM I/B 24IN FROM T/E 1.5I N DIA ZONE 1 IAW A319 SRM 55-21-11-300-005 CATEGORY A REPAIR.
- [SDR CALA2024021900452](https://openairdocs.org/sdr/CALA2024021900452.md): Skin · contaminated · Feb 16, 2024 · N836UA · Airbus A319131 · Elevator, Plate/Skin
  > RH ELEVATOR HAS LIQUID INGRESS AT 39.5 INCHES FROM I/B EDGE, 11 INCHES FROM TRAILING EDGE AND 1.5 INCHES IN DIAMETER. REPAIRED RH ELEVATOR UPPER SKIN 39.5IN FROM I/B 11IN FROM T/E 1. 5IN IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-005
- [SDR CALA2023101803107](https://openairdocs.org/sdr/CALA2023101803107.md): Connector · loose · Oct 16, 2023 · N836UA · Airbus A319131 · Engine Fuel System Wiring
  > EPR MODE FAULT - ENG 1. REFER TO TSM CHAPTER 77 ECAM AND UAL A32 0 MEL CARD 73 120. P2 T2 SENSOR FAULT ON POST FLIGHT REPORT INSPECTED AND FOUND CONNECTOR "B" LOOSE ON ENGINE 1 P2/T2 SENSOR. RESECURED AND NO FAULT MSG ACTIVE AT THIS TIME. REQUIRES OPS CHECK. A
- [SDR CALA2023072802363](https://openairdocs.org/sdr/CALA2023072802363.md): Fuel Cap · missing · Jul 26, 2023 · N836UA · Airbus A319131 · Fuel Storage
  > PILOTS REPORT MISSING FUEL CAP ON LOG PAGE 5272816 SDR UPDATED. PDA DOCUMENTED PER GMM 02-30-95 TOMC NOTIFIED. ACCORDING TO SCEPTRE OFF SERIAL # WAS 7032. MISSING REFUEL CAP, PLACING ON CDL 28A MISSING FUEL CAP PLACED ON CDL 28A. DISPATCH DESK: 13 NAME: AP DAT
- [SDR CALA2022090502277](https://openairdocs.org/sdr/CALA2022090502277.md): Fuel Cap · missing · Sep 2, 2022 · N836UA · Airbus A300* · Aircraft Fuel System
  > *THIS IS A SUPPLEMENTAL REPORT TO THE ORIGINAL REPORT, WITH THE SAME CONTROL NUMBER, CIRCULATED ON 09/05/2022* FUELER FOUND FUEL CAP MISSING. INSTALLED NEW FUEL CAP. OPS GOOD.
- [SDR CALA2022082402146](https://openairdocs.org/sdr/CALA2022082402146.md): Door · leaking · Aug 24, 2022 · N836UA · Airbus A319131 · Passenger/Crew Doors
  > DOOR 2L LEAKOUTSIDE VISIBLE AFT LOWER CORNER UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE FIX USING VENDOR MAA SCREEN UPDATED MAA CODE EFS USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK DOOR 2L PLEASE CONTACT TO
- [SDR CALA2021090301503](https://openairdocs.org/sdr/CALA2021090301503.md): Eec · failed · Sep 3, 2021 · N836UA · Airbus A319131 · Fuel Controlling System
  > ONE TLA FAULT DISPLAYED ON UPPER ECAM SCREEN. - ENG 2 INTERMITTENT IN FLIGHT7 OR 8 TIMES USE TSM 76-00-00-810-802-B TO TROUBLESHOOT THE WIRING. PFR ATTACHED. CHECK CFDS ENG 2 FADEC A&B FOR FAULT CODE "TRAL" AND CHECK WIRING PER ABOVE FIM. CODE TRAL PER FIM TAS

Next page: https://openairdocs.org/aircraft/N836UA/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 = 'N836UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N836UA/reports

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