# Service difficulty reports: N436UA

A list on [N436UA](https://openairdocs.org/aircraft/N436UA.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 · 121 reports

- [SDR CALA2026101220263](https://openairdocs.org/sdr/CALA2026101220263.md): None · no discrepancy · Oct 10, 2026 · N436UA · Airbus A320232 · Standard Practices/Structures
  > BIRD STRIKE DURING TAKEOFF ROLL APPROX 145 KTS. SEEMED ISOLATED TO FRONT LEFT NOSE/FUSELAGE. DEBRIEFED CREW. ACFT WAS IN TAKE-OFF CONFIGURATION DURING TAKE-OFF ROLL. NO ABNORMAL ENGINE INDICATIONS. NO ODOR IN THE AIR CONDITIONING. RADIOS AND NAVIGATION OPERA
- [SDR CALA2026012613310](https://openairdocs.org/sdr/CALA2026012613310.md): None · none · Jan 26, 2026 · N436UA · Airbus A320232 · Standard Practices/Structures
  > WATCH DOOR SLIDE SAFETY VIDEO R1 COMPLIED WITH WATCHING AIRBUS DOOR VIDEO
- [SDR CALA2026012613291](https://openairdocs.org/sdr/CALA2026012613291.md): Control Cable · abnormal · Jan 26, 2026 · N436UA · Airbus A320232 · Service Doors
  > R1 DOOR ARM DOES NOT FULLY RECESS TO ARM POSITION INITIATED R1 DOOR ESCAPE SLIDE REMOVAL UP TO STEP 4. B(3)(F) IAW AMM 25-62-44-000-802-A, & AMM 52-10-00-860-001-A SPECIAL PRECAUTIONS BEFORE WORKING ON DOOR. CLEANED ENDS OF GIRT BAR, STILL WORKS CORRECTLY W
- [SDR CALA2025122312373](https://openairdocs.org/sdr/CALA2025122312373.md): Smoke Detector · false activation · Dec 20, 2025 · N436UA · Airbus A320232 · Smoke Detection
  > PILOTS REPORT AFT CARGO SMOKE INDICATION ON ECAM WITH ANNUNCIATOR 5-8 MINS FROM LANDING. NO VISABLE SMOKE IN CABIN & NO ODOR DETECTED. FIRE DEPARTMENT DID NOT PICK UP ANYTHING ON INFRARED SCANNERS AFTER LANDING. UPON OPENING AFT CARGO DOOR, NO UNUSUAL CONDIT
- [SDR CALA2025080807516](https://openairdocs.org/sdr/CALA2025080807516.md): Fuel Cap · missing · Aug 5, 2025 · N436UA · Airbus A320232 · Fuel Storage
  > DURING WALK AROUMD NOTICE CAP,COUPLING REFUELING UNDERWING MISSING.
- [SDR CALA2025080607376](https://openairdocs.org/sdr/CALA2025080607376.md): Indicator · detached · Aug 3, 2025 · N436UA · Airbus A320232 · Escape Slide
  > PIECE OF METAL DETACHED FROM DOOR 2L ESCAPE SLIDE BUSTLE COVER. REINSTALLED ARMING INDICATOR ON DOOR 2L. OP CHECK GOOD.
- [SDR CALA2025070106112](https://openairdocs.org/sdr/CALA2025070106112.md): Slide · faulted · Jun 28, 2025 · N436UA · Airbus A320232 · Escape Slide
  > EMERGENCY SLIDE DOOR 2R BAD FROM STOCK. REMOVED DOOR 2R SLIDE REF AMM 25-62-44-000-802-A UP TO AND INCLUDING STEP A 4,G. COMPLETED REMOVAL OF SLIDE PER AMM 25-62-44-000-802-A. SN A6692. REQUESTING INSPECTION VERIFICATION FOR ELECTRICAL WIRING ROUTING AND GIRT
- [SDR CALA2024102300904](https://openairdocs.org/sdr/CALA2024102300904.md): Slide · out of alignment · Oct 21, 2024 · N436UA · Airbus A320232 · Escape Slide
  > 2L DOOR SLIDE ALIGNMENTNOT ALIGNING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. CHECK 2L DOOR AREA FOR DEBRIS MAC METER INITIATED FOR.WITH VENDOR ID V081328 MAC RELATED WORK ORDER 00000000312059 - REMOVED DEBR
- [SDR CALA2024070501963](https://openairdocs.org/sdr/CALA2024070501963.md): Fitting · cracked · Jul 2, 2024 · N436UA · Airbus A320232 · Landing Gear Doors
  > RH MLG DOOR ACTUATOR FWD FITTING HORIZONTAL FLANGE HAS GOUGE ADJACENT TO OB FASTENER. REMOVED AND REPLACED RH MLG DOOR ACTUATOR FWD FITTING HINGE FITT ING AND CONNECTING PLATE IAW AIRBUS REPAIR DWG R533-70501 ISSUE F AND R533-70500 ISSUE F, AS DIRECTED BY EC
- [SDR CALA2023072402318](https://openairdocs.org/sdr/CALA2023072402318.md): Fuel Cap · missing · Jul 20, 2023 · N436UA · Airbus A320232 · Fuel Storage
  > PDA 2 FOR FUEL CAP MISSING ON ARRIVAL CONTACTED TOMC REGARDING PDA REF GMM 02-30-95. REQUEST CDL 28A DUE TO PARTS NIS IN DENVER. PLACARD INSTALLED DEFERRED PER CDL 28A. PLACARD INSTALLED. VERIFIED NO LEAKS DISPATCH DESK: 04 NAME: RP DATE: 19-JUL-23- APPROVED
- [SDR CALA2023061401849](https://openairdocs.org/sdr/CALA2023061401849.md): Door · missing · Jun 12, 2023 · N436UA · Airbus A320232 · Doors
  > LAV SERVICE DOOR MISSING. REQUEST CDL FOR MISSING LAV SERVICE DOOR. REMOVED ALL RELATED TOMC APPROVED CDL 52A. HARDWARE AND COMPLIED WITH MAINTEANCE TASKS. DISPATCH DESK: S30 NAME: C.E DATE: 11-JUN-23- NOC DESK: A320 NAME: J.R DATE: 11-JUN-23- OKAY TO CD
- [SDR CALA2022090502282](https://openairdocs.org/sdr/CALA2022090502282.md): Fuel Cap · missing · Sep 5, 2022 · N436UA · Airbus A300* · Aircraft Fuel System
  > PDA 3. FUEL CAP MISSING ON ARRIVAL. REPLACED FUEL CAP
- [SDR CALA2022081902120](https://openairdocs.org/sdr/CALA2022081902120.md): Bottle · none · Aug 19, 2022 · N436UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR EMERGENCY ASSIST BOTTLE AT 2 L & 1R NEED SERVICING. SERVICED DOOR BOTTLES PER AMM 52-10-00-614-001-A.
- [SDR CALA2021111802132](https://openairdocs.org/sdr/CALA2021111802132.md): None · faulty · Nov 18, 2021 · N436UA · Airbus A320232 · Compressor Bleed Governor
  > ENG 2 COMPRESSOR VANEECAM AT APPROX 90KTSON TAKEOFF REQUSTED VSV ACTUATOR. NONE IN STOCK ORD. REF LOG PG 7432865 FOR ALL REPAIRS ADD EMP:U116632. PER LP 7432865, REPLACED #2 ENG VSV ACTUATOR, NO LEAKS FOUND ON IDLE AND OPS CHECKS NORMAL ON POWER RUN REF AMM 75
- [SDR CALA2021102501958](https://openairdocs.org/sdr/CALA2021102501958.md): Bulkhead · none · Oct 22, 2021 · N436UA · Airbus A320232 · Fuselage Main, Frame
  > LH FR 68 #1L X4 DOOR STOP FITTING MOUNT HOLES IN FRAME HAVE AN OUT OF ROUND INDICATION, AS PER NTM 51-10-01-250-801-A-01, SUBTAS K 51-10-1-253-001-A, ITEM C. (7)(C) TABLE 5. DOT #11-07 - EA 534 0-01724 002 - NR 9294294 (28294) GENERATED BY V062335 AT HAECO L C
- [SDR CALA2021102201947](https://openairdocs.org/sdr/CALA2021102201947.md): Beam · cracked · Oct 21, 2021 · N436UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > LH FRAME 43 FOOT AFT INBOARD ATTACHMENT HOLE IS CRACKED IN THE C ENTER WING BOX UPPER MOST LAYER AT 2:00 - SUPPORT TASK AD 2020-1 8-06 - NR 9294751 (28751) GENERATED BY V061633 AT HAECO LCQ. REPLACED FRAME AND REAMED HOLE TO.4060 TO REMOVE INDICATION IAW EC/R
- [SDR CALA2021102201946](https://openairdocs.org/sdr/CALA2021102201946.md): None · none · Oct 20, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO FR50 STRGT41RT STRINGER CORRODED. GENERATED BY N078592 ON HAECO LCQ NR 9294560/28560 0-13-205-002 TABLE 5 INSPECTION THRESHOLD FROM TIME OF EMBODIMEN T FC 60,000 OR FH 120,000 WHICHEVER VALUE IS ACHIEVED FIRST. SUB SEQUENT INSPECTIONS TBD. INSPECTION
- [SDR CALA2021102201945](https://openairdocs.org/sdr/CALA2021102201945.md): None · weak · Oct 20, 2021 · N436UA · Airbus A320232 · Lighting System
  > FORWARD EMERGENCY LIGHTS BATTERY PACK 10WL FAILS TO ILLUMINATE W ITH THE CONTROL SWITCH IN ARM AND C/B''S PULLED - SUPPORT TASK - NR 9294241 (28241) GENERATED BY V061627 AT HAECO LCQ. REMOVED AND REPLACED 10WL EPSU BATTERY AND OP CHECKS GOOD IAW A3 20 AMM 33-5
- [SDR CALA2021102201942](https://openairdocs.org/sdr/CALA2021102201942.md): None · weak · Oct 20, 2021 · N436UA · Airbus A320232 · Lighting System
  > EMERGENCY LIGHTS FAIL TO ILLUMINATE FOR THE BATTERY PACKS AT THE BATTERY PACKS AT THE L/H AND R/H OVERWING (11WL & 12WL) WITH THE CONTROL SWITCH IN ARMED AND THE C/B''S PULLED - SUPPORT TASK - N R 9294239 (28239) GENERATED BY V061627 AT HAECO LCQ. REMOVED AND
- [SDR CALA2021102201941](https://openairdocs.org/sdr/CALA2021102201941.md): Fitting · corroded · Oct 20, 2021 · N436UA · Airbus A320232 · Passenger/Crew Doors
  > L2 DOOR LOWER AFT CORNER FITTING HAS CORR. PER HAECO LCQ NR 9294 490/28490. GENERATED BY V061334 REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNER FITTING A320 UAL SRM 51-42-11-001. PER MECH V061737. REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNE
- [SDR CALA2021102201940](https://openairdocs.org/sdr/CALA2021102201940.md): Fitting · corroded · Oct 20, 2021 · N436UA · Airbus A320232 · Passenger/Crew Doors
  > L2 DOOR LOWER AFT CORNER FITTING HAS CORR. PER HAECO LCQ NR 9294 490/28490. GENERATED BY V061334 REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNER FITTING A320 UAL SRM 51-42-11-001. PER MECH V061737. REMOVED AND REPLACED WITH NEW L-2 DOOR LOWER AFT CORNE
- [SDR CALA2021100601797](https://openairdocs.org/sdr/CALA2021100601797.md): None · none · Oct 6, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > ON HAECO LCQ REF NR 9294610 JUST FWD OF FR64 @ STRINGER 41R- STR INGER IS CORRODED GENERATED BY V899260 REMOVED AND REPLACED STRINGER 41R IN AFT CARGO IAW A320 SRM 51-7 2-11-911-001 WORK ACCOMPLISHED BY MECH V052030 AND INSP BY V0613 34
- [SDR CALA2021100601794](https://openairdocs.org/sdr/CALA2021100601794.md): Fitting · none · Oct 5, 2021 · N436UA · Airbus A320232 · Fuselage Main, Frame
  > R2 DOOR LOWER SILL FWD CORNER FITTING HAS CORR - A3NB-53-3-6033 - NR 9294554 (28554) GENERATED BY V061334 AT HAECO LCQ. REMOVED & REPLACED WITH NEW R-2 DOOR LOWER SILL FWD CORNER FITTI N PER A320 UAL SRM 51-42-11/001. DOT REMOVED. ACCOMPLISHED BY V0 61737, INS
- [SDR CALA2021100601779](https://openairdocs.org/sdr/CALA2021100601779.md): Fitting · corroded · Oct 4, 2021 · N436UA · Airbus A320232 · Fuselage Main, Frame
  > R2 DOOR LOWER SILL AFT CORNER FITTING HAS CORR - A3NB-53-3-6033 - NR 9294552 (28552) GENERATED BY V061334 AT HAECO LCQ. REMOVED AND REPLACED R2 DOOR LOWER AFT CORNER FITTING IAW A320 S RM 51-72-11-911-001 PAR. 2D REMOVED DOT. ACCOMPLISHED BY V074845, INSP BY
- [SDR CALA2021100101758](https://openairdocs.org/sdr/CALA2021100101758.md): None · corroded · Oct 1, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO FR 61 ART STR 40 STRINGER CORRODED. (A3NB-53-4-6199). GENERATED BY N078592 AT HAECO LCQ PER NR 9294540 (28540). OCCURS FIRST. SUBSEQUENT INSPECTION INTERVALS AND INSPECTION MET HOD TBD. CURRENT PTT:77217 PTC:30071. MECH:V063868 INSP:LC119 REPAIRED ST
- [SDR CALA2021100101733](https://openairdocs.org/sdr/CALA2021100101733.md): Plate · none · Sep 29, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO AT LWR DOOR OPENING SILL WEB AT FWD CORNER HAS 3 EA GO UGES.(A3NB-53-4-6179). GENERATED BY N078592 AT HAECO LCQ PER NR. 9294563 (28563) REMOVED AND REPLACED AFT CARGO LWR DOOR SILL WEB IAW A320 SRM 51 -42-11. PERFORMED BY V052030 AND INSP BY V061334.
- [SDR CALA2021100101732](https://openairdocs.org/sdr/CALA2021100101732.md): None · abnormal · Sep 29, 2021 · N436UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CABIN BELOW R2 DOOR SILL AFT OF FRAME 66 STRINGER HAS EXFOLI ATION CORROSION (A3NB-53-3-6033) GENERATED BY V052030 AT HAECO LCQ PER NR 9294659 (28659). REMOVED AND REPLACED STRINGER 25RT AFT OF FR 66RT IAW A320 SRM 5 1-42-11. PERFORMED BY V913406 AND INSP
- [SDR CALA2021100101728](https://openairdocs.org/sdr/CALA2021100101728.md): Stringer · corroded · Sep 29, 2021 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > AFT CARGO FR59 STRGR43LT STRINGER CORRODED. (A3NB-53-4-6199). GE NERATED BY N078592 AT HEACO LCQ PER NON-ROUTINE 9294543. (28453) INSPECTED BY V061334. REMOVED AND REPLACED STRINGER AT FR.59 STRGR 43L. IAW A320 SRM 5 1-72-11-911-001. PERFORMED BY V052030 INSP
- [SDR CALA2021090301493](https://openairdocs.org/sdr/CALA2021090301493.md): Gusset · damaged · Sep 2, 2021 · N436UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RIGHT INNER CAP JOINT-GUESSET PLATES AT FR 66 AND 68. ALL FASTEN ER HOLES HAVE AN OUT OF ROUND INDICATION, AS PER A319/A320 NTM 5 1-10-01-250-801-A-01, SUBTASK 51-10-01-253-001-A ITEM C.(7) (C) TABLE 5. DOT 11-04 - A3NB-53-4-0033 - NR 9294296. FABRICATED & IN
- [SDR CALA2021090301487](https://openairdocs.org/sdr/CALA2021090301487.md): Gusset · damaged · Sep 1, 2021 · N436UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > LEFT INNER CAP JOINT-GUSSET PLATES AT FR 66 AND 68. ALL FASTENER HOLES HAVE AN OUT OF ROUND AS PER A319/A320 NTM 51-10-01-250-80 1-A-01, SUBTASK 51-10-01-253-001-A ITEM C. (7)(C) TABLE 5. DOT 1 1-02 - A3NB-53-4-0032 - NR 9294297 (28297) GENERATED BY V062335 AT
- [SDR CALA2019112542046](https://openairdocs.org/sdr/CALA2019112542046.md): Frame · damaged · Nov 20, 2019 · N436UA · Airbus A320232 · Fuselage Main, Frame
  > DURING L/H FR35 INSPECTION PER EA 5330-05216 FOUND NUMEROUS HOLES HAD DEFECTS REPAIRED IN ACCORDANCE WITH ECRA 5331-02514 PLACED ON DIP TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF ECRA 5331-02514 ON OR BEFORE 18 MAY 2020. PLANNING TO CONTACT ENGINEERING AFT
- [SDR CALA2019112532037](https://openairdocs.org/sdr/CALA2019112532037.md): Structure · defective · Nov 19, 2019 · N436UA · Airbus A320232 · Fuselage Structure (General)
  > DURING R/H FR35 INSPECTION PER EA 5330-05216 FOUND NUMEROUS HOLES HAD DEFECTS REPAIRED IN ACCORDANCE WITH ECRA 5331-02515 PLACED ON DIP TO ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF 3 OF ECRA 5331-02515 ON OR BEFORE 18 MAY 2020. PLANNING TO CONTACT ENGINEERIN
- [SDR CALA2017120804333](https://openairdocs.org/sdr/CALA2017120804333.md): Warning Light · false activation · Dec 8, 2017 · N436UA · Airbus A320232 · Escape Slide
  > DOOR 1L SLIDE LGHT ILLUMINATED WITH DOOR CLOSED AND SLIDE ARMED. PERFORMED AN OPERATIONAL TEST OF DR 1L IAW AMM 53-73-00 AND LITE OPERATED AS IT SHOULD.
- [SDR CALA2017050101229](https://openairdocs.org/sdr/CALA2017050101229.md): Battery Pack · no test · May 1, 2017 · N436UA · Airbus A320232 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, BATTERY AFT LEFT DISPLAYED. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-51-38. OPS CHECKED GOOD.
- [SDR CALA2017040700906](https://openairdocs.org/sdr/CALA2017040700906.md): Connector · unsecure · Apr 7, 2017 · N436UA · Airbus A320232 · Equipment/Furnishings Wiring
  > DURING THE PAX DOOR ESCAPE RELEASE OPS CHECK, FOUND THE L2 DOOR SLIDE ARM LIGHT ON WHILE HANDLE IN UNARMED. DISCOVERED A CONNECTOR IMPROPERLY CONNECTED. CONNECTED THE CONNECTOR PROPERLY IAW AMM 52-13-00-710-001.
- [SDR CALA2017040700885](https://openairdocs.org/sdr/CALA2017040700885.md): Stringer · corroded · Apr 4, 2017 · N436UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > STRINGER 31R, 6 INCHES FORWARD OF FRAME 66, BELOW THE OUTFLOW VALVE, FOUND CORRODED. REMOVED AND REPLACED THE STRINGER IAW SRM 51- 44-11, TABLES 3 AND 5, 51-42-11 PARA 6 AND 7.
- [SDR CALA2016101795814](https://openairdocs.org/sdr/CALA2016101795814.md): Power Supply · inoperative · Oct 15, 2016 · N436UA · Airbus A320232 · Emergency Lighting
  > MID L EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY AND BATTERY, OPS CHECK NORMAL.
- [SDR CALA2016061395442](https://openairdocs.org/sdr/CALA2016061395442.md): Warning Message · false activation · Jun 10, 2016 · N436UA · Airbus A320232 · Emergency Lighting
  > BATTERY EMERGENCY LT MSG DURING EMEGENCY LIGHT TEST IAW NR 2 SERVICE CHECK. POWER UP ACFT AND ACP TASK 33-51-00-710-007-B. OPS TEST OF EMERGENCY LIGHTING BY LIGHT EMEGENCY RG PUSHBUTTON SWITCH. TEST OK.
- [SDR CALA2016012595022](https://openairdocs.org/sdr/CALA2016012595022.md): Light · malfunctioned · Jan 21, 2016 · N436UA · Airbus A320232 · Emergency Lighting
  > REF 2 SVC, EMER LIGHTS FAILED TEST. RESET CIDS PANEL. EMER LIGHT TEST PASSED.
- [SDR CALA2015072494158](https://openairdocs.org/sdr/CALA2015072494158.md): Connector · loose · Jul 23, 2015 · N436UA · Airbus A320232 · Landing Gear System Wiring
  > MAIN LANDING GEAR FAULT, LGCIU 1 UNLOCK INDICATION. MISSED APPROACH, FOUND ELEC CONNECTOR LOOSE AT 96A. PERFORMED LGCIU 1 & 2 TEST THROUGH MCDU, ALL PASSED WITH NO MSG DISPLAYED.
- [SDR CALA2015030993399](https://openairdocs.org/sdr/CALA2015030993399.md): Power Supply · inoperative · Feb 27, 2015 · N436UA · Airbus A320232 · Emergency Lighting
  > BATTERY EMER RT MSG DISPLAYED AFTER EMER LIGHTS OPERATIONAL TEST. POWER SUPPLY WILL NOT TEST. REPLACED POWER SUPPLY & BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.
- [SDR CALA2015030493210](https://openairdocs.org/sdr/CALA2015030493210.md): Power Supply · inoperative · Feb 27, 2015 · N436UA · Airbus A320232 · Emergency Lighting
  > BATTERY EMER RT MSG DISPLAYED AFTER EMER LIGHTS OPERATIONAL TEST. FAILS BATTERY RT POWER SUPPLY, WILL NOT TEST. REPLACED POWER SUPPLY & BATTERY IAW AMM 33-51-38. OPERATIONS CHECKED GOOD.
- [SDR CALA2013123094046](https://openairdocs.org/sdr/CALA2013123094046.md): Windshield Wiper · out of adjust · Dec 29, 2013 · N436UA · Airbus A320232 · Windshield/Door Rain/Ice Removal
  > CAPTAIN`S WIPER BLADE HAS POOR CONTACT WITH WINDSCREEN. ADJUSTED CAPTAIN`S WIPER ARM IAW AMM.
- [SDR CALA2013120693513](https://openairdocs.org/sdr/CALA2013120693513.md): Cable · out of adjust · Dec 4, 2013 · N436UA · Airbus A320232 · Passenger/Crew Doors
  > R2 PASSENGER DOOR ARMING HANDLE IS CREEPING OPEN IN FLIGHT APPROXIMATELY.50 INCH WHEN CABIN DIFFERENTIAL PRESS IS ABOVE 3.0 PSI. DURING DESCENT BELOW 5000 FT HANDLE RETURN TO NORMAL. SECURED & ADJUSTED DOOR 2R ARMING HANDLE CABLE.
- [SDR CALA2013121993812](https://openairdocs.org/sdr/CALA2013121993812.md): Unknown · malfunctioned · Dec 3, 2013 · N436UA · Airbus A320232 · Door Warning System
  > DOOR 2R STILL IS SHOWING UNARMED. WERE AT 19,000FT & DOOR 2L IS ARMED. ACCOMPLISHED OPERATIONS CHECKED IAW AMM 52-73-00-710-001A. ECAM INDICATIONS CHECKED GOOD WITH DOOR ARMED & DISARMED ON GRD AIRCRAFT PRESSURIZED.
- [SDR CALA2013120393420](https://openairdocs.org/sdr/CALA2013120393420.md): Handle · out of rig · Dec 2, 2013 · N436UA · Airbus A320232 · Passenger/Crew Doors
  > AFTER TAKEOFF DOOR 2L & 2R SHOW DISARMED ON EWD & BLINK RED AT DOORS INTERMITTENTLY. ACCOMPLISHED PRESSURIZATION IAW THE JRH & AMM TO 0.9 DIFF FOUND DOORS NOT BLINKING. IF THE ARM HANDLE IS SLIGHTLY TAPED THE DOOR PRESSURIZED INDICATORS START BLINKING. FOUN
- [SDR CALA2013120293345](https://openairdocs.org/sdr/CALA2013120293345.md): Frame · cracked · Nov 28, 2013 · N436UA · Airbus A320232 · Fuselage Main, Structure
  > FRAME 68 CRACKED AT LOWER INBD HOLE AT L2 DOOR NR 1 STOP. AREA REPAIRED IAW REO-L014 20 & ECRA 5340-01569.
- [SDR CALA2013120293379](https://openairdocs.org/sdr/CALA2013120293379.md): Wire Harness · faulty · Nov 27, 2013 · N436UA · Airbus A320232 · Landing Gear System Wiring
  > LG LGCIU 1 FAULT.
- [SDR CALA2013111892985](https://openairdocs.org/sdr/CALA2013111892985.md): Sill · corroded · Nov 17, 2013 · N436UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > L2 DOOR SILL IS CORRODED FRAME 66, INBD GIRT BAR ATTACHMENT HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. INSTALLED SILL IAW SRM 51-42-11, PAGE 25.
- [SDR CALA2013111492917](https://openairdocs.org/sdr/CALA2013111492917.md): Stringer · corroded · Nov 13, 2013 · N436UA · Airbus A320232 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT FRAME 56-57, STRINGER42L HAS SURFACE CORROSION. STRINGER 42L FRAME 56-57 CORROSION IS OUT OF LIMITS. R & R STRINGER 42L & SIX EACH SHEAR TIES FRAME 53-60 IAW SRM 51-42-11. WORKED ON TIMCO NR 23259.

Next page: https://openairdocs.org/aircraft/N436UA/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 = 'N436UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N436UA/reports

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