# Service difficulty reports: N802UA

A list on [N802UA](https://openairdocs.org/aircraft/N802UA.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 · 124 reports

- [SDR CALA2026101920451](https://openairdocs.org/sdr/CALA2026101920451.md): Hydraulic Line · leaking · Oct 15, 2026 · N802UA · Airbus A319131 · Hydraulic System, Main
  > GREEN HYD SYS LOW PRESSURE. ECAM RUN MANUAL GEAR EXTENSION. FOUND HYD LINE LEAKING IN LEFT WING BETWEEN RIB 1 AND RIB 2. REMOVED LINE #30 REF IPC 29-11-05-02. REPLACED LEAKING LINE WITH SERVICABLE ONE REF LINE #30 REF IPC 29-11-05-02. LEAK CHECKS GOOD, RESET
- [SDR CALA2026052216453](https://openairdocs.org/sdr/CALA2026052216453.md): Fitting · cracked · May 17, 2026 · N802UA · Airbus A319131 · Landing Gear Doors
  > RIGHT MLG DOOR FWD HINGE FITTING FWD OTBD FASTENER HEAD SHEARED. UPON FURTHER EVALUATION FOUND A CRACK THAT WAS OUT OF LIMITS ON BOTH UPPER AND LOWER RT MLG FITTINGS. REMOVED AND REPLACED FITTINGS IAW SRM 51-72-11/R533 70500, REV F AND R533 70501, REV G.
- [SDR CALA2026033114959](https://openairdocs.org/sdr/CALA2026033114959.md): Battery · no test · Mar 30, 2026 · N802UA · Airbus A319131 · Emergency Lighting
  > RIGHT EMERGENCY EPSU BATTERY FAILED. REMOVED AND REPLACED RT EMERGENCY EPSU BATTERY IAW AMM 33-51-38-000/400-002-A, OKAY FOR SERVICE.
- [SDR CALA2026020413585](https://openairdocs.org/sdr/CALA2026020413585.md): Wire · chafed · Feb 2, 2026 · N802UA · Airbus A319131 · Fuel System Wiring
  > FOUND CHAFING DAMAGE TO CONDUIT & CORRESPONDING DAMAGE TO WIRES 4513-QG16 (R,Y,B) APPROX 5 FT FROM CONNECTOR 22QA-A, JUST FWD OF RT LANDING LIGHT. DAMAGE FOUND USING TDR/FILTERED PROBE. IAW AWM 28-21-02. PRIOR TO FINDING DAMAGE, FOUND NO CONTINUITY FROM 22QA
- [SDR CALA2025112411410](https://openairdocs.org/sdr/CALA2025112411410.md): Light · no discrepancy · Nov 21, 2025 · N802UA · Airbus A319131 · Emergency Lighting
  > WHILE ACCOMPLOSHING EMERGENCY LIGHTS SYSTEM TEST I GOT A MX MESSAGE. EPSU INT LOAD FWD LT FURTHER TROUBLESHOOTING REQUIRED. REF AMM 33-51-00-710-001-A ACCOMPLISHED BITE OF EMERGENCY LIGHT EPSU'S REF AMM 33-51-00-710-001-A, OP CK OK, COULD NOT DUPLICATE FAULT
- [SDR CALA2025111611225](https://openairdocs.org/sdr/CALA2025111611225.md): Filter · contaminated · Nov 13, 2025 · N802UA · Airbus A319131 · Air Distribution System
  > CREW REPORTED AFTER YELLOW SYSTEM OVERHEAT ECAM MESSAGE, STRONG ODOR OBSERVED IN FLIGHT DECK AND CABIN. R & R BOTH RECIRC FILTER CARTRIDGES IAW AMM 21-21-41-000-001-A AND 21-21-41-400-001-A. PERFORMED OPS CHECK OF YELLOW HYD SYS IAW AMM 29-13-00, OPS CHECKED
- [SDR CALA2025090908634](https://openairdocs.org/sdr/CALA2025090908634.md): Hydraulic Line · leaking · Sep 6, 2025 · N802UA · Airbus A319131 · Hydraulic System, Main
  > EMERGENCY DECLARED INTO DEN. CREW STATES AT 30K FT, GOT ECAM Y SYS LO, & THEN SAW ENG PUMP NO PRESSURE & Y SYS NO QTY. SHUTDOWN PUMP. ENG 2 PYLON DRAIN LEAKING HYD FLUID. LEAK LOCATION. ON ARRIVAL FLUID WAS STILL IN YELLOW SYSTEM & VERIFIED NO PUMPS WERE RAN D
- [SDR CALA2025081507812](https://openairdocs.org/sdr/CALA2025081507812.md): Battery · no test · Aug 15, 2025 · N802UA · Airbus A319131 · Emergency Lighting
  > COMPLIED WITH CABIN EMERGENCY LIGHT TEST, AFTER TEST WAS PERFORMED FAULT EPSU BATTERY EMER L WAS SHOWN ON CIDS PANEL. TESTED SYSTEM TWICE, FAULT SHOWED BOTH TIMES. REMOVED AND CLEANED FWD LEFT BATTERY CONTACTS AND REINSTALLED BATTERY IAW MM 33-51-38. OPS CHEC
- [SDR CALA2025072506901](https://openairdocs.org/sdr/CALA2025072506901.md): Shaft · broken · Jul 24, 2025 · N802UA · Airbus A319131 · Passenger Compartment Equipment
  > AFT JUMP SEAT BROKEN BLOCKING EXIT ITEM FLAGGED FOR SDR REPORTING REINSTALLED, JUMP SEAT, INBOARD SEAT PIVOT HINGE PIN.REFERENCE IFM 25-11-48. OPERATIONALLY CHECKS GOOD.
- [SDR CALA2025061105466](https://openairdocs.org/sdr/CALA2025061105466.md): Outflow Valve · faulted · Jun 8, 2025 · N802UA · Airbus A319131 · Pressure Regulator/Outflow Valve
  > VENT BLOWER FAULT AND EXTRACT FAULT MESSAGESIN INITIAL CLIMB.TER RAIN AND WX DISPLAYS LOST. INSTALLED SKIN AIR OULET VALVE IAW WITH AMM 21-26-400-001-A-01 SEALANT AND TAPE WILL NEED TO BE CHECKED AFTER EVERY FLIGHT STEP (17) BEFORE REPLACING SKIN AIR OUTLET
- [SDR CALA2025042104061](https://openairdocs.org/sdr/CALA2025042104061.md): Battery Pack · no test · Apr 19, 2025 · N802UA · Airbus A319131 · Emergency Lighting
  > EPSU BATTERY L AND EPSU BATTERY AFT L APPEARING ON FAP AFTER EMERGENCY LIGHT TEST REMOVED AND REPLACED ESPU BATTERY L AND AFT L. PEFORMED OPS CHECK, OPS CHECK GOOD. REF AMM 33-51-38.
- [SDR CALA2025030402567](https://openairdocs.org/sdr/CALA2025030402567.md): Lgciu · faulted · Feb 25, 2025 · N802UA · Airbus A319131 · Cargo/Baggage Doors
  > DURING DECENT AT ABOUTFL210 GOT DOOR AFTCARGO ECAM WITHNORMAL PR ESSURIZATION UPDATED MAA CODE FIX USING VENDOR MAA SCREEN DEFER REF MEL 5270CD. CONFIRMED AFT CARGO DOOR CLOSED AND LATCHED-MEL 5270CD APPLIED FOR DOOR INDIC INOP. CONFIRMED AFT CARGO DOOR CLO
- [SDR CALA2025012702050](https://openairdocs.org/sdr/CALA2025012702050.md): Packing · leaking · Jan 23, 2025 · N802UA · Airbus A319131 · Hydraulic System, Main
  > FOUND YELLOW SYSTEM MANIFOLD CHECK VALVE ORING LEAKING. REMOVED AND REPLACED ORING FOR PTU, YELLOW SYSTEM MANIFOLD CHECK VALVE. LEAK CHECKS GOOD. REF AMM 29-13-15-400-001-A.
- [SDR CALA2024112901360](https://openairdocs.org/sdr/CALA2024112901360.md): Latch · unsecure · Nov 27, 2024 · N802UA · Airbus A319131 · Cargo/Baggage Doors
  > DOOR AFT CARGO DOOR ECAM DURING TAKEOFF. REJECTED TAKEOFF. FOUND AFT CARGO DOOR LATCH NOT FULLY STOWED RECURED AND VERIFIED DOOR IS CLOSED A/C OK FOR SERVICE
- [SDR CALA2024112101222](https://openairdocs.org/sdr/CALA2024112101222.md): Switch · out of adjust · Nov 18, 2024 · N802UA · Airbus A319131 · Door Warning System
  > [LEVEL 0 CHRONIC]-AFT CARGO DOOR IND-DUE TO HISTORY, PLS CHK THE ADJUSTMENT OF THE 34WV PROX SWITCH AND DOOR LATCHING MECHANISM PER AMM 52-32-00-720-001-A.THE PROX SWITCH INDUCTANCE CAN ALSO BE VERIFIED PER AMM 32-31-73-820-008-A TO CHECK CORRECT NEAR AND FAR
- [SDR CALA2024061701833](https://openairdocs.org/sdr/CALA2024061701833.md): Skin · dented · Jun 16, 2024 · N802UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > LOWER AFT FUSELAGE APPROX FR71-72 AROUND SAFETY STAY AREA HAS MU LTIPLE DENTS AND CREASES (4EA). REPAIRED FUSELAGE SKIN LOWER PANEL IAW A319 SRM 53-51-29-300-002.
- [SDR CALA2024061801851](https://openairdocs.org/sdr/CALA2024061801851.md): Skin · damaged · Jun 15, 2024 · N802UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > ECRA 5331-03043 REV A PART 3 STEP 1 INSTRUCTS TO CONTACT ENGINEE RING BEFORE A/C REACHES 36,859 TFC FOR PERMANENT REPAIR INSTRUCT IONS. CURRENT CYCLES 35441. REQUIRES RFTS.
- [SDR CALA2023120503543](https://openairdocs.org/sdr/CALA2023120503543.md): Anti-Ice Valve · faulty · Dec 2, 2023 · N802UA · Airbus A319131 · Airfoil Anti/De-ice System
  > CREW REPORTED WING ANTI ICE FAULT ON CLIMB OUT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN LH WING ANTI -ICE VALVE FAULT. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V919182 LH WING ANTI -ICE VALVE FAULT. MAC RELAT
- [SDR CALA2023101603069](https://openairdocs.org/sdr/CALA2023101603069.md): Line · leaking · Oct 13, 2023 · N802UA · Airbus A319131 · Hydraulic System, Main
  > HYD G RSVR LO LVL ON TAXI OUT. WE ARE DISABLED WEST RAMP 3W FOUND LEAK ON THE GREEN PRESSURE LINE REPLACED HYD LINE TO LEFT MAIN LANDING GEAR BRAKE ABOVE THE GEAR RETRACT ACTUATOR, REF GPM 01-13-1-0-13 AND 01-13-020. NO LEAKES NOTED AFTER GREEN SYSTEM PRESSUR
- [SDR CALA2023083002671](https://openairdocs.org/sdr/CALA2023083002671.md): Skin · damaged · Aug 28, 2023 · N802UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN FR73-FR74, STRINGER 31L TO 31R CREASED - INTERIM REPAIR ACCOMPLISHED REF EC/RA 5351-01212. OR BEFORE A/C REACHES 35,932 TOTAL FLIGHT CYCLES, 82,693 TOTAL INSP NOT TO EXCEED INTERVALS OF 120 FLIGHT CYCLES THEREAFTER. FLIGHT HRS OR 21-SEP-24 WHICHE
- [SDR CALA2023021300428](https://openairdocs.org/sdr/CALA2023021300428.md): Unknown · none · Feb 13, 2023 · N802UA · Airbus A319131 · Air Conditioning System
  > PACK 1 AND 2 FAULT DISPLAYED ON UPPER ECAM SCREEN. - AIR PACK ONE INDICATEDOVERHEAT WITHOUT ANOVERHEAT MESSAGE LOCKED DOOR OPEN PER AMM 21-61-00 IN COMPLIANCE WITH MEL COMPLIED WITH MEL APPROVED FOR MEL 2152N REMOVED AND REPLACED PACK 1 AIR OUTLET ACTUATOR OPS
- [SDR CALA2021100401774](https://openairdocs.org/sdr/CALA2021100401774.md): Fuel Cap · missing · Oct 3, 2021 · N802UA · Airbus A319131 · Aircraft Fuel System
  > PDA 2 RE LP 7156148, FUEL CAP REPORTED MISSING ON ARRIVAL ORD OFF FLIGHT 289-30. CAP PLACED ON CDL 28A. PDA ENTERED INTO HISTORY.
- [SDR CALA2021092201644](https://openairdocs.org/sdr/CALA2021092201644.md): Frame · corroded · Sep 21, 2021 · N802UA · Airbus A319131 · Fuselage Structure (General)
  > AFT CARGO FR67 AFT SIDE BETWEEN STR 41R-42L HAS CORROSION ON OUT ER FLANGE PER NR 9296815 / 20815 GEN BY N078570. REMOVED CORROSION FROM FR67 AFT SIDE BETWEEN STR 41R-42L AND REP AIRED FRAME IAW SRM 53-41-12-300-014. INSTALLED ALTERNATIVE FAST ENERS IAW SRM 51
- [SDR CALA2021092201642](https://openairdocs.org/sdr/CALA2021092201642.md): Fitting · none · Sep 21, 2021 · N802UA · Airbus A319131 · Fuselage, Landing Gear Attach Fittings
  > KEEL BEAM LH MLG ELONGATED HOLES REFERENCE NON ROUTINES 9296412 HOLE L2, 9296420 HOLE L74, 9296656 HOLE L10, 9296419 HOLE L81, 9 296414 HOLE L20, 9296415 HOLE L15, 9296657 HOLE L11, 9296416 HOL E L17, 9296413 HOLE L18, 9296417 HOLE L16, 9296418 HOLE L78. GEN E
- [SDR CALA2021092201638](https://openairdocs.org/sdr/CALA2021092201638.md): Keelbeam · none · Sep 21, 2021 · N802UA · Airbus A319131 · Fuselage, Landing Gear Attach Fittings
  > KEEL BEAM RH MLG ELONGATED HOLES REPAIRS REFERENCE NON ROUTINES 9296421 HOLE R1, 9296422 HOLE R9, 9296423 HOLE R81. GENERATED BY V061630 ON HAECO LCQ NR 9296826/20826 HAECO TECHNICIAN V061630 & QC LC-66 ACCOMPLISHED REPAIRS ON RH K EEL BEAM AND MLG DOOR FITTIN
- [SDR CALA2021092201629](https://openairdocs.org/sdr/CALA2021092201629.md): Fitting · corroded · Sep 20, 2021 · N802UA · Airbus A319131 · Fuselage Structure (General)
  > CORROSION UNDER NUTPLATE LOCATED AT FWD CARGO DOOR THRESHOLD (AF T END) FR 28, STR 39R (A3NB-05-3-6016). GENERATED BY V925611, AT HAECO LCQ PER NR 9296486 (20486). REMOVED AND REPLACED 1EA CORNER SUPPORT FITTING PART NO. D532313 3520000, PO NO. 1100049.1 IAW A
- [SDR CALA2021092201627](https://openairdocs.org/sdr/CALA2021092201627.md): Fitting · corroded · Sep 20, 2021 · N802UA · Airbus A319131 · Fuselage, Seat/Cargo Attach Fittings
  > FORWARD CARGO COMPARTMENT DOOR TORSION BOX BETWEEN FR24-28 HAS C ORROSION SPOTS ON UPPER SURFACE AROUND 4EA NET TIE DOWN FITTING (A3NB-53-3-6105). GENERATE BY V919150 AT HAECO LCQ PER NR 929656 9 (20569) REMOVED AND REPLACED TORSION BOX AT FWD CARGO COMPARTMEN
- [SDR CALA2021092001611](https://openairdocs.org/sdr/CALA2021092001611.md): Frame · cracked · Sep 19, 2021 · N802UA · Airbus A319131 · Fuselage Main, Frame
  > RH FR 4 UPPER FITTING HAS CRACK INDICATION IN HOLE IN VERTICAL F RAME - AD RELATED SUPPORT TASK - NR 9296424 (20424) GENERATED BY V892444 AT HAECO LCQ. HAECO TECHNICIAN V061630 & QC LC-66 REPAIRED RH FR4 UPPER FITTIN G CRACK INDICATION HOLE IAW EC/RA 5311-0264
- [SDR CALA2021092001609](https://openairdocs.org/sdr/CALA2021092001609.md): Threshold · corroded · Sep 19, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT DOOR THRESHOLD BETWEEN FR24-28 HAS COR ROSION SPOTS ON UPPER SURFACE DOT M054 A3NB-53-3-6105 PER HAECO LCQ NR 9296567/20567 GENERATED BY V919150. REMOVED AND REPLACED FWD CARGOSILL PLATE IAW A319 SRM 51-42-11 A ND 51-72-11 MECH BY V91
- [SDR CALA2021092001605](https://openairdocs.org/sdr/CALA2021092001605.md): Battery · discharged · Sep 18, 2021 · N802UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHTS OP''S TEST FROM THE PTP FAILS FOR THE EPSU AFT L - A3NB-33-3-0004 - NR 9296002 (20002) GENERATED BY V061627 AT H AECO LCQ. REMOVED AND REPLACED 13WL (AFT L) EPSU BATTERY IAW A319/320 AMM 33-51-38, SYSTEM OPERATION CHECKS GOOD IAW A319/A320 AMM
- [SDR CALA2021091701589](https://openairdocs.org/sdr/CALA2021091701589.md): Door Sill · corroded · Sep 15, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > AFT CARGO DOOR SILL TOP SURFACE HAS CORROSION IN MULTIPLE AREAS FROM FR 56-59 (A3NB-53-4-6179). GENERATED BY V077960 AT HAECO LC Q PER NR 9296531 (20531). REMOVED AND REPLACED AFT CARGO DOOR SILL IAW A319 SRM 51-42-11 PERFORMED BY V913406 AND INSP BY V925611.
- [SDR CALA2021091701588](https://openairdocs.org/sdr/CALA2021091701588.md): Torque Box · corroded · Sep 15, 2021 · N802UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO DOOR TORSION BOX TOP SURFACE HAS CORROSION IN MULTIPLE AREAS FROM FR 56-59 (ANB3-53-4-6179). GENERATED BY V077960 AT H AECO LCQ PER NR 9296532 (20532). REMOVED AND REPLACED AFT CARGO DOOR TORSION BOX TOP IAW A319 SRM 51-72-11 AND 53-41-49-283-004. AP
- [SDR CALA2021091001542](https://openairdocs.org/sdr/CALA2021091001542.md): Fitting · corroded · Sep 8, 2021 · N802UA · Airbus A319131 · Passenger/Crew Doors
  > L-1 DOOR SILL AFT CORNER FITTING INNER SURFACE HAS CORROSION. DO T: A16 - A3NB-53-3-6038 - NR 9296469 (20469) REMOVED AND REPLACED L-1 DOOR SILL AFT CORNER FITTING IAW A319 S RM 51-72-11.
- [SDR CALA2021091001540](https://openairdocs.org/sdr/CALA2021091001540.md): Fitting · corroded · Sep 8, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > L-1 DOOR SILL FWD CORNER FITTING INNER SURFACE HAS CORROSION.DOT:A13 - A3NB-53-3-6038 - NR 9296464 (20464) GENERATED BY N078570 AT HAECO LCQ. REMOVED AND REPLACED L-1 DOOR SILL FWD CORNER FITTING IAW A319 S RM 51-42-11. ACCOMPLISHED BY V052030, INSP BY V06133
- [SDR CALA2021090601506](https://openairdocs.org/sdr/CALA2021090601506.md): Fitting · corroded · Sep 3, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R-1 DOOR SILL AFT CORNER FITTING INNER SURFACE HAS CORROSION (A3 NB-53-3-6038). REMOVED AND REPLACED R1 DOOR SILL AFT CORNER FITTING IAW A319 SR M 51-42-11.
- [SDR CALA2021090301494](https://openairdocs.org/sdr/CALA2021090301494.md): Fitting · corroded · Sep 2, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > R-1 DOOR SILL FWD CORNER FITTING INNER SURFACE HAS CORROSION. (A 3NB-53-3-6038). GENERATED BY N078570, AT HAECO LCQ PER NR 929646 2(20462). REMOVED AND REPLACED R1 DOOR SILL FWD CORNER FITTING IAW A319 SR M 51-42-11. PERFORMED BY V052030 AND INSP BY V061334.
- [SDR CALA2021081601339](https://openairdocs.org/sdr/CALA2021081601339.md): Skin · punctured · Aug 15, 2021 · N802UA · Airbus A319131 · Rudder, Plate/Skin
  > R/H SIDE OF RUDDER HAS THREE EACH PUNCTURES AT APPROXIMATELY SIX TRAILING EDGE SCREWS UP AND FORWARD AS MARKED A3NB-55-3-6024 PE R HAECO LCQ NR 9296161/20161. REPAIRED RH SIDE OF RUDDER 3 EA AREAS AT SIX T/E SCREWS UP AND FWD IAW UAL ECRA 5541-01052 AND REO-L
- [SDR CALA2021081601335](https://openairdocs.org/sdr/CALA2021081601335.md): Intercostal · cracked · Aug 13, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > RT O/WING ESCAPE HATCH L/H LOAD TRASMITTING PROFILE HAS CRACK PR ESENT ACROSS 2 RIVETS (AD RELATED) A3NB-52-4-6032. PER HAECO LCQ N/R 9296350/20350. REMOVED AND REPLACED 1EA LOAD TRASMITTING PROFILE/SEGMENT FWD ON R/H OVERWING ESCAPE HATCH IAW A319 SRM 51-42-1
- [SDR CALA2021081601334](https://openairdocs.org/sdr/CALA2021081601334.md): Intercostal · cracked · Aug 13, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LT O/WING ESCAPE HATCH R/H LOAD TRANSMITTING PROFILE HAS CRACK P RESENT ACROSS 3 RIVETS (AD RELATED) A3NB-52-4-6032. PER HAECO LC Q N/R 9296348/20348. REMOVED AND REPLACED 1EA LOAD TRANSMITTING PROFILE/SEGMENT FWD O N R/H OVERWING ESCAPE HATCH IAW A319 SRM 5
- [SDR CALA2021080601267](https://openairdocs.org/sdr/CALA2021080601267.md): Shear Plate · corroded · Aug 4, 2021 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > LT LATERAL SHEER PLATE FR69 TO FR 70 HAS CORROSION AT FASTNER HO LES AND BARE METAL AT SPOTS. (A3NB-53-3-6222). GENERATED BY N078 592 ATH HAECO LCQ PER NR 9296442 (20442). BLEND CORROSION LH SHEER PLATE FOUND TO BE BEYOND ALLOWABLE LIMI TS. REMOVED AND REPLACE
- [SDR CALA2021061100845](https://openairdocs.org/sdr/CALA2021061100845.md): Warning Message · false activation · Jun 11, 2021 · N802UA · Airbus A319131 · Central Warning
  > DOOR AFT CARGO MSGIN FLIGHT INSPECTED THE AFT CARGO DOOR LATCH, LOCKING MECHANISMS, AND PROXIMITY SWITCHES REF AIRBUS A319 AMM 52-32-00. THE AFT CARGO DOOR LATCH, LOCKING MECHANISMS, AND PROXIMITY SWITCHES ARE GOOD. WITH THE AFT CARGO DOOR CLOSED ALL OF THE LO
- [SDR CALA2020030700590](https://openairdocs.org/sdr/CALA2020030700590.md): Pressure Panel · cracked · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Main, Bulkhead
  > SUPPORT TASK AD2018-06-04 RH FRAME 36 PRESSURE PNL FASTENER HOLE S 1,2,4,13,14,15,17,19,20,21,22,23,24,25,26,27 & 28 ARE CRACKED CONTACT ENG. FOR REPAIR INST. & REPAIR BEFORE NEXT FLIGHT PER NR 9290353 GEN AT HAECO LCQ. INTERIM REPAIR C/W REF. EC/RA 5331-02628
- [SDR CALA2020030700589](https://openairdocs.org/sdr/CALA2020030700589.md): Angle · damaged · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > EA RELATED TASK EA 5330-05216 RMV AND RPLC TITANMUM ANGLE AT FR 36 COMMON TO THE PRESSURE PANEL HAS REQUESTED BY AIRBUS TD 80748 969 006 2020 NO.A GEN PER NR9290446 AT HAECO LCQ. INTERIM REPAIR ACCOMPLISHED PER PART 1 OF ECRA 5331-02630 AT HAE CO - LCQ DURING
- [SDR CALA2020030700588](https://openairdocs.org/sdr/CALA2020030700588.md): Fitting · damaged · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > EA RELATED TASK EA5330-05216 003, RMV AND RPLC RH CORNER FITTING FR36 COMMON TO PRESSURE PANEL DUE TO OVERSIZED HOLE NO.4 GEN. B Y V061609 PER NR 9290433 AT HAECO LCQ. ACCOMPLISH AN INITIAL INSPECTION AT RH FR35-36 PRESSURE PANEL HOLES #A1, #A2, #A4, #A8, #A10
- [SDR CALA2020030700587](https://openairdocs.org/sdr/CALA2020030700587.md): Fitting · not reported · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > EA RELATED TASK EA 5330-05216 002 RMV AND RPL CORNER FITTING AT LH FR36 COMMON TO THE PRESSURE PANEL AS REQUESTED BY AIRBUS TD 8 0748969 006 2020 NO.A PER NR 9290447 GEN BY V061609 AT HAECO LCQ C/W INTERIM REPAIR PER EC/RA 5331-02630. ACCOMPLISH PERMANENT REPA
- [SDR CALA2020030700586](https://openairdocs.org/sdr/CALA2020030700586.md): Pressure Panel · cracked · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Main, Bulkhead
  > SUPPORT TASK AD2018-06-04 LH FR 36 PRESSURE PNL FASTENER HOLES 2,4,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27 & 28 ARE CRACKED. CONTACT ENG. FOR REPAIR INSTRUCTIONS & BEFORE NEXT FLIGHT PER NR 9290352 GEN BY V061633 AT HAECO LCQ. INTERIM REPAIR ACCOMPLISHE
- [SDR CALA2020030700585](https://openairdocs.org/sdr/CALA2020030700585.md): Pressure Panel · cracked · Mar 5, 2020 · N802UA · Airbus A319131 · Fuselage Main, Bulkhead
  > SUPPORT TASK AD2018-06-04 LH FR 36 PRESSURE PNL FASTENER HOLES 2,4,13,14,15,16,17,18,19,20,21,22,23,24,25,26,27 & 28 ARE CRACKED. CONTACT ENG. FOR REPAIR INSTRUCTIONS & BEFORE NEXT FLIGHT PER NR 9290352 GEN AT HAECO LCQ. INTERIM REPAIR ACCOMPLISHED PER PART
- [SDR CALA2020010600080](https://openairdocs.org/sdr/CALA2020010600080.md): Oxygen Mask · leaking · Jan 3, 2020 · N802UA · Airbus A319131 · Crew Oxygen System
  > CAPT O2 MASK HAS LEAK AND WILL NOT EXPAND TOPUT ON SWAPPPED 2ND OBSERVER SEAT O2 MACK OVER TO THE CAPT O2 MASK LOCATION. OPS AND LEAK CHECK GOOD REF. A319 AMM35-12-41.
- [SDR CALA2019052400829](https://openairdocs.org/sdr/CALA2019052400829.md): Handle · unsecure · May 23, 2019 · N802UA · Airbus A319131 · Cargo/Baggage Doors
  > AFT CARGO DOOR INDICATE OPEN AIRBORNE. FOUND DOOR HANDLE NOT COMPLETELY FLUSH, SECURED HANDLE IN FULLY CLOSED POSITION. GREEN MARKS WERE DISPLAYED LOCKED IN SIGHT WINDOWS UPON ARRIVAL. REF AMM 52-70-00-040-001-A. NO DEFECTS, NOTED.
- [SDR CALA2017121404455](https://openairdocs.org/sdr/CALA2017121404455.md): Power Supply · inoperative · Dec 14, 2017 · N802UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILED EPSU BATTERY EMER R ON PTP. REPLACED EPSU 12WL BATTERY AS PER AMM 33-51-38 PB401. NOW OP TEST OK FOR SERVICE.

Next page: https://openairdocs.org/aircraft/N802UA/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 = 'N802UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N802UA/reports

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