# Service difficulty reports: N804UA

A list on [N804UA](https://openairdocs.org/aircraft/N804UA.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 · 111 reports

- [SDR CALA2026102220518](https://openairdocs.org/sdr/CALA2026102220518.md): Elec Connector · fod · Oct 22, 2026 · N804UA · Airbus A319131 · Landing Gear System Wiring
  > BRAKES AUTO BRK FAULT ECAM ON FINAL APPROACH, DID CHECKLIST, CYCLED LANDING GEAR, NORMAL LANDING AND BRAKES POST FLT FAULTING BRK SELECTOR VALVE (23GG) ON BSCU 2. RAN NORMAL BRAKING AND LRU WIRING AND BSCU TEST BOTH FAULTING BRK SELECTOR VALVE (23GG). NO FAULT
- [SDR CALA2026072017895](https://openairdocs.org/sdr/CALA2026072017895.md): Lgciu · faulted · Jul 17, 2026 · N804UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > AFTER T/O UNABLE TO RET GEAR AS HAND WAS LOCKED IN DWN POS. FOLLOWED FIM TASK 32-31-00-810-885-A UP TO AND INCLUDING STEP 4.B. FOUND LT MLG SHOCK UNDERSERVICED, SERVICED LT MLG STRUT IAW AMM 12-12-32-610-001-C1. WHILE ACCOMPLISHING AMM 32-31-00-710-002-A. F
- [SDR CALA2026042715738](https://openairdocs.org/sdr/CALA2026042715738.md): Spinner · leaking · Apr 15, 2026 · N804UA · Airbus A319131 · Engine (Turbine/Turboprop)
  > ENG1 SOURCE OF FUMESDURING T/O AND CLIMBINTERRIGATED E1 UPON ARRIVAL AT GATE, FOUND STRONG FUEL SMELL IN E1 IN COMPARISON TO E2. RAN BOTH PACKS APROX 5 MIN. NO OIL SMELLS NOR SMOKE IN CABIN NOR NEAR E1 AT THIS TIME. REQ FURTHER TROUBLESHOOTING REF. AMM 71-00-0
- [SDR CALA2026012013094](https://openairdocs.org/sdr/CALA2026012013094.md): Fuel Cap · missing · Jan 17, 2026 · N804UA · Airbus A319131 · Fuel Storage
  > REFUELING CAP MISSING ON ARRIVAL
- [SDR CALA2025122912494](https://openairdocs.org/sdr/CALA2025122912494.md): Control Lever · faulted · Dec 27, 2025 · N804UA · Airbus A319131 · Landing Gear Selector
  > AFTER LIFTOFF, MLG LEVER DOWNLOCK DOES NOT RELEASE FOR A FEW SECONDS.RELEASE ON 2ND/3RD. PERFORMED LGCIU BITE TEST IAW AMM 31-32-00. BITE TESTED GOOD. NO FAULT. NO HISTORY. PER TSM 32-31-00-810-885-A, PERFORMED FUNCTIONAL TEST OF NORMAL RETRACTION & EXTENSI
- [SDR CALA2025060505288](https://openairdocs.org/sdr/CALA2025060505288.md): Bottle · no discrepancy · Jun 2, 2025 · N804UA · Airbus A319131 · Standard Practices/Structures
  > DUE TO SLIDE DEPLOYMENT, REPLACEMENT OF THE DIAPHRAGM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRED R&R DOOR R2 DIAPHRAGM IN THE PERCUSSION MECHANISM OF THE DOOR DAMPER AND EMERGENCY OPERATION CYLINDER PER AMM 52-10-00-610-001-A. CHARGED THE DOO
- [SDR CALA2025060505285](https://openairdocs.org/sdr/CALA2025060505285.md): Slide · unwanted deploy · Jun 2, 2025 · N804UA · Airbus A319131 · Escape Slide
  > R2 EMERGENCY ESCAPE SLIDE DEPLOYED DURING MAINTENANCE REPLACED R2 EMERGENCY ESCAPE SLIDE PER AMM 25-62-44-400-802A. OPS CHECK GOOD.PARTS USED: 31-2561-9-0015, QTY:1 ROTABLE PARTS CHG:TT # 1482000 SN OFF 6666 PN OFF 31-2561-9-0015.SLIDE, ASSY, EV OFF 31-256
- [SDR CALA2025031002668](https://openairdocs.org/sdr/CALA2025031002668.md): Battery · faulted · Mar 9, 2025 · N804UA · Airbus A319131 · Emergency Lighting
  > FORWARD DOOR ESCAPE SLIDE PACK ASSEMBLY INSTALL {A3NB-25-3-0020} - EMERGENCY SYSTEM LIGHTS BITE CHECK FAILS (NO SYS OK LIGHT) WITH STATUS MESSAGE (EPSU INT LOAD FWD L) REMOVED AND REPLACED BATTERY OF EPSU IAW AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2025012902106](https://openairdocs.org/sdr/CALA2025012902106.md): Door · out of adjust · Jan 29, 2025 · N804UA · Airbus A319131 · Passenger/Crew Doors
  > CATERING REPORT DOOR 2L NOT FULLY OPENING LUBRICATED DOOR DAMPER CYLINDER JOINTS AND PERFORMED DAMPER CYLINDER REF AMM 52-10-00-710-001-A. DOOR OPENS AND LOCKS, BUT REQUIRES SIGNIFICANT FORCE TO GET INTO THE OPEN AND LOCKED PISTION. DOOR OPERATES SMOOTHLY AF
- [SDR CALA2025012902105](https://openairdocs.org/sdr/CALA2025012902105.md): Bottle · out of rig · Jan 29, 2025 · N804UA · Airbus A319131 · Passenger/Crew Doors
  > R2 DOOR WILL NOT FULLY OPEN LUBRICATED DOOR DAMPER CYLINDER JOINTS AND PERFORMED DAMPER CYLINDER REF AMM 52-10-00-710-001-A. DOOR OPENS AND LOCKS, BUT REQUIRES SIGNIFICANT FORCE TO GET INTO THE OPEN AND LOCKED PISTION. DOOR OPERATES SMOOTHLY AFTER INTIAL OPE
- [SDR CALA2025011300078](https://openairdocs.org/sdr/CALA2025011300078.md): Frame · damaged · Jan 10, 2025 · N804UA · Airbus A319131 · Fuselage Main, Frame
  > REMOVED AND RE-INSTALL APPLICABLE COMPONENTS COMMON TO FRAME 55A TO ACCOMPLISH PARTIAL FRAME REPLACEMENT. ACCOMPLISHED REPAIR OF FR55A IAW UAL ECRA 5341-01470 THIS REPAIR HAS BEEN APPROVED AS A CAT A REPAIR WITH NO ADDITIONAL INSPECTI ON REQUIRMENTS. IT IS A
- [SDR CALA2025010900072](https://openairdocs.org/sdr/CALA2025010900072.md): Shear Tie · corroded · Dec 19, 2024 · N804UA · Airbus A319131 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT FR55A WITH CORROSION BETWEEN STGR39R AND S TGR38R TOP SURFACE () OF EC/RA 5341-01470 ON OR BEFORE THE 19TH APRIL 2025. T RH FRAME 55A UPPER CAP AT STRINGER 38R-39R WAS REPAIRED AT BFM. ACCOMPLISH A PERMANENT REPAIR PER PART 3 OF THE LATES
- [SDR CALA2024121903120](https://openairdocs.org/sdr/CALA2024121903120.md): Channel · damaged · Dec 18, 2024 · N804UA · Airbus A319131 · Passenger/Crew Doors
  > L2 DOOR BOTTOM CORNER WAS DAMAGE. DOT 210-05 ()
- [SDR CALA2022110203019](https://openairdocs.org/sdr/CALA2022110203019.md): Warning Message · false activation · Nov 2, 2022 · N804UA · Airbus A319131 · Flight Control System
  > *EMERGENCY DECLARED* F/CTL FLAPS LOCKED ECAM MESSAGE. CORELATED FAULT MESSAGES: FLP 2 CHK RH MECH DRIVE AND FLP 1 CHK RH MECH DRIVE CREW REPORTED TE FLAPS LOCKED WHEN FLAPS LEVER WAS MOVED FROM 1 TO 2 THEN BACK TO 1 BEFORE FLAPS FULLY REACHING 2. TSM 27-51-00
- [SDR CALA2022071301730](https://openairdocs.org/sdr/CALA2022071301730.md): None · inoperative · Jul 13, 2022 · N804UA · Airbus A319131 · Trailing Edge Flap Control System
  > FLAPS LOCKED - ALIGNMENT FAULT DISPLAYED ON UPPER EC AM SCREEN. - F-CTL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V939358 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. PERFORM WTB MAC RELATED WORK ORDER 000000003
- [SDR CALA2022053001382](https://openairdocs.org/sdr/CALA2022053001382.md): Angle · cracked · May 28, 2022 · N804UA · Airbus A319131 · Emergency Exits
  > LH SIDE EMERGENCY EXIT DOOR FORWARD SUPPORT ANGLE HAS CRACK. GEN ERATED BY V061771 PER HAECO LCQ NR 9292847/44847 REMOVED AND REPLACED DISCREPANT LH DUCT EMERGENCY EXIT FORWARD S UPPORT ANGLE IAW A319 SRM 51-42-11-001. PERFORMED BY V061616 INS P BY N078570
- [SDR CALA2022053001381](https://openairdocs.org/sdr/CALA2022053001381.md): Angle · cracked · May 28, 2022 · N804UA · Airbus A319131 · Emergency Exits
  > LH SIDE EMERGENCY EXIT DOOR AFT SUPPORT ANGLE HAS CRACK. GENERAT ED BY V061771 PER HAECO LCQ NR 9292848/44848 REMOVED AND REPLACED DISCREPANT LH NICKS EMERGENCY EXIT AFT SUPP ORT ANGLE IAW A319 SRM 51-42-11-001. PEROFRMED BY V061616 INSP B Y N078570
- [SDR CALA2022053001380](https://openairdocs.org/sdr/CALA2022053001380.md): Angle · cracked · May 28, 2022 · N804UA · Airbus A319131 · Emergency Exits
  > RH SIDE EMERG EXIT DOOR FORWARD SUPPORT ANGLE HAS A CRACK. GENER ATED BY V061632 PER HAECO LCQ NR 9292858/44858 REMOVED AND REPLACED DISCREPANT RH SIDE EMERGENCY EXIT FORWARD S UPPORT ANGLE IAW A319 SRM 51-42-71-001. PERFOREMD BY V061616 INS P BY N078570.
- [SDR CALA2022052701362](https://openairdocs.org/sdr/CALA2022052701362.md): Angle · cracked · May 26, 2022 · N804UA · Airbus A319131 · Emergency Exits
  > R/H SIDE EMERGENCY EXIT DOOR AFT SUPORT ANGLE HAS CRACK: SUPPORT TASK GENERATED BY V061771 AT HAECO LCQ PER NR 9292849 (44849) REMOVED AND REPLACED DISCUPART R/H SIDE EMERGENCY EXIT AFT SUPPO RT ANGLE IAW A319 SRM 57-42-11-001 PERFORMED BY V061616 INSP BY V917
- [SDR CALA2022052701360](https://openairdocs.org/sdr/CALA2022052701360.md): Fitting · damaged · May 25, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > UPON REMOVAL LH FWD KEEL BEAM REINFORCEMENT ANGLE FOUND TO HAVE DAMAGED HOLES AND LH AFT KEEL BEAM REINFORCEMENT ANGLE FOUND TO HAVE DAMAGED HOLES. AT LH KEEL BEAM AFT INTERNAL WEB HOLES L21,L 81,L82,L83,L84,L85 SHOW ELONGATION ON W10 RIB. HOLES L72,L73,L75,L
- [SDR CALA2022051801271](https://openairdocs.org/sdr/CALA2022051801271.md): None · corroded · May 16, 2022 · N804UA · Airbus A300* · Fuselage Main, Frame
  > GUSSET CONNECTING STR26 WITH FRAME 66 HAS CORROSION A3NB-53-3-63 27 PER HAECO LCQ N/R 9292749/44749 GEN BY V061334 RMVD AND RPLD GUSET AT STR26 FR66 R/H SIDE IAW A319 SRM 51-42-11 /001 NO SIR RE-INSP NOTED BY MECH V061630 INSP BY N078570
- [SDR CALA2022051601242](https://openairdocs.org/sdr/CALA2022051601242.md): None · cracked · May 14, 2022 · N804UA · Airbus A319131 · Fuselage Main, Frame
  > LH FR68 AFT FACE AT STR22 FLANGE HAS CRACK INDICATION. NNER & HORIZONTAL FLANGES FILET RADII PER PART 2, ITEM 1 OF LATE FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION AT INTERVALS NOT TO INSP: LC25. PTC:30657 ST REVISION OF ECRA 5341-01309 ON OR BEFORE 50355 TOTA
- [SDR CALA2022050901185](https://openairdocs.org/sdr/CALA2022050901185.md): None · corroded · May 8, 2022 · N804UA · Airbus A319131 · Fuselage Main, Structure
  > AFT CARGO TORSION BOX COVER SHEET HAS CORROSION. GENERATED BY V0 52030 ON HAECO LCQ NR 9292430/44430 REMOVED AND REPLACED AFT CARGO COVER SHEET IAW A319 SRM 51-72-11 ACMP BY MECH V052030 INSP BY V061334
- [SDR CALA2022050901180](https://openairdocs.org/sdr/CALA2022050901180.md): None · corroded · May 8, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > MAIN CABIN BETWEEN FR69-70 STRINGER 23L SHEAR PLATE HAS SPOTS OF CORROSION ON UPPER SURFACE. GENERATED BY V919150 PER HAECO LCQ NR 9292781/44781. REMOVED AND REPLACED SHEAR PLATE AT FR69-70 STR. 23L IAW A319 SR M 51-72-11, SRM 51-11-12 AND SRM 51-42-11. MECH V
- [SDR CALA2022050901168](https://openairdocs.org/sdr/CALA2022050901168.md): None · corroded · May 6, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/Skin
  > MAIN CABIN BETWEEN FR69-70 STRINGER 23R SHEAR PLATE HAS SPOTS OF CORROSION ON UPPER SURFACE. GENERATED BY V919150 PER HAECO LCQ NR 9292782/44782 REMOVED AND REPLACED SHEAR PLATE ON STRINGER 23R AT FR69-70 IAW UAL A319 SRM 51-42-11-001-A. ACMP BY MECH V061616 I
- [SDR CALA2022050201116](https://openairdocs.org/sdr/CALA2022050201116.md): Fitting · corroded · May 1, 2022 · N804UA · Airbus A300* · Fuselage Main, Structure
  > AFT WET AREA R2 DOOR SILL HAS CORROSION AT FRAME 65. GENERATED B Y V052030 PER HAECO LCQ NR 9292440/44440 REMOVED AND REPLACED DISCREPANT R2 DOOR SILL IAW A319 SRM 51-72- 11-911-002 SRM 51-42-11 PER MECH V061616 MECH V937663
- [SDR CALA2022042701077](https://openairdocs.org/sdr/CALA2022042701077.md): Skin · punctured · Apr 21, 2022 · N804UA · Airbus A319131 · Empennage Structure
  > LEFT ELEVATOR HAS 10 PUNCTURES DUE TO HAIL. 1) 97 INCHES FROM INBOARD, 15 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 9) 102 INCHES FROM INBOARD, 11.5 INCHES FROM TRAILING EDGE,.5 INCHES DIAMETER. 2) 104 INCHES FROM INBOARD, 11 INCHES FROM TRAILING E
- [SDR CALA2022042701076](https://openairdocs.org/sdr/CALA2022042701076.md): Skin · punctured · Apr 21, 2022 · N804UA · Airbus A319131 · Empennage Structure
  > RIGHT ELEVATOR HAS SEVEN PUNCTURES DUE TO HAIL. 1) 21 INCHES FROM INBOARD, 23 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 2) 85 INCHES FROM INBOARD, 16 INCHES FROM TRAILING EDGE, 1 INCH DIAMETER. 3) 100 INCHES FROM OUTBOARD EDGE, 12 1/2 INCHES FROM TRAILI
- [SDR CALA2022042501053](https://openairdocs.org/sdr/CALA2022042501053.md): Skin · none · Apr 21, 2022 · N804UA · Airbus A319131 · Elevator, Plate/Skin
  > PER NR 9292544/44544 "HAIL DAMAGE" LH ELEVATOR UPPER SURFACE HAS (8EA) SPOTS OF DISBAND. GENERATED BY N078570. REPAIRED LH CLEAVER PN D5528000301200 SN CG1854 UPPER SKIN 9EA A REAS 1IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-004 CAT A REPAIR. MECH V061767 INSP BY
- [SDR CALA2022042501052](https://openairdocs.org/sdr/CALA2022042501052.md): Skin · damaged · Apr 21, 2022 · N804UA · Airbus A319131 · Elevator, Plate/Skin
  > PER NR 9292547/44547 "HAIL DAMAGE" RH ELEVATOR UPPER SURFACE HAS (6EA) SPOTS OF DISBAND. GENERATED BY N078570. REPAIRED RH ELEVATOR PN D5528000301300 SN CG1854 UPPER SKIN 6EA AREAS 1IN DIA ZONE 1 IAW A319 SRM 55-21-11-300-004 CAT A REPAIR REMOVED DOT 76. MECH
- [SDR CALA2022032300760](https://openairdocs.org/sdr/CALA2022032300760.md): Pump · leaking · Mar 23, 2022 · N804UA · Airbus A319131 · Engine Oil Quantity
  > ENGINE 2 OIL QUANTITY FLASHES GREEN - ENG 2 RIGHT ENG OIL QTY WENTTO 0.0 IN FLIGHTOIL PRESSURE WAS OK ENG-2. CREW VEBAL; DURING EVENT MAINTAINED OIL PRESS AT ALL TIMES, OIL TEMPERTURE REMAINED NORMAL AND ENG WAS NOT SHUT DOWN IN FLIGHT. ENG WAS SHUT DOWN AFTE
- [SDR CALA2020072701072](https://openairdocs.org/sdr/CALA2020072701072.md): Safety Valve · malfunctioned · Jul 21, 2020 · N804UA · Airbus A319131 · Landing Gear Retraction/Extension System
  > SYS DISAGREE DISPLAYED ON UPPER ECAM SCREEN - L-G LANDING GEAR REQUIREDMANUAL EXTENSIONNORMAL LANDING LOCKING PLEASE ACCOMPLISH TSM 32-31-00-810-842A DURING INSPECTION OF BOTH MAIN LANDING GEARS, NOTICED LEFT MAIN LANDING DOOR UPLOCK IS OUT OF SEQUENCE. PARTS
- [SDR CALA2018112102408](https://openairdocs.org/sdr/CALA2018112102408.md): Window Frame · cracked · Nov 20, 2018 · N804UA · Airbus A319131 · Fuselage Main, Structure
  > REF TO AAR NON ROUTINE 9611821 (ESR #8) R/H WINDSHIELD FR 4 SIDE POST AFT LOWER WEB HAS A CRACK INDICATION. ECRA AND DIP DEFERRAL ARE TO CLOSE EXISTING C-CHECK PACKAGE AND RE-OPEN AS STAND ALONE EVENT, NO FLIGHT ALLOWED RE-POSITION A/C FOR A STAND ALONE CHECK
- [SDR CALA2018110972319](https://openairdocs.org/sdr/CALA2018110972319.md): Web · cracked · Nov 6, 2018 · N804UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > REF TO AAR NON ROUTINE-9611820 (ESR 7) L/H WINDSHIELD FR 4 SIDE POST AFT LOWER WEB CRACK INDICATION, INTRIM REPAIR ACCOMPLISHED PER PART 1 OF ECRA 5311-02039. INTRIM REPAIR ACCOMPLISHED PER PART 1 OF ECRA 5311-02039, DTA DIP REQUESTED, TO ACCOMPLISH INITIAL IN
- [SDR CALA2018110502311](https://openairdocs.org/sdr/CALA2018110502311.md): Actuator · no test · Nov 5, 2018 · N804UA · Airbus A319131 · Flight Control System
  > (A3NB-27-4-6031) REMOVE AND REPLACE THE THSA. REFER TO AAR N/R: 9611965. CHANGED DUE TO A FAILED JAMMING TEST AND A LEAK. REMOVED & REPLACED THSA IAW A319 AMM 27-44-51-000-001 & AMM 27-4 4-51-400-001. PERFORMED THSA ELECTRICAL CONTROL OPS TEST IAW A31 9 AMM 27
- [SDR CALA2018110502292](https://openairdocs.org/sdr/CALA2018110502292.md): Battery · unknown · Nov 3, 2018 · N804UA · Airbus A319131 · Emergency Lighting
  > (A3NB-33-3-6013) REPLACE ALL EPSU BATTERIES AS AN ALTERNATIVE PR OCEDURE TO COMPLY WITH BATTERY CAPACITY CHECK. REFER TO AAR N/R: 9612056. REMOVED AND REPLACED ALL EPSU BATTERIES AS AN ALTERNATIVE PROCED URE TO COMPLY WITH BATTERY CAPACITY CHECK. SPEC NO. A3NB
- [SDR CALA2018110502291](https://openairdocs.org/sdr/CALA2018110502291.md): Pressure Panel · cracked · Nov 3, 2018 · N804UA · Airbus A319131 · Fuselage Main, Structure
  > R/H PRESSURE PLATE AT FR 43 FOUND TO BE CRACKED. REPLACE PLATE P ER OP 007 OF AD. AAR N/R 9611972 REPAIRED R/H PRESSURE PLATE AT FR 43 IAW ECRA 5331-02282. REPAIR IS APPROVED AS PERMANENT WITH NO REINSPECTION REQUIRED.PRESSURE PLATE REPLACED ON CUSTOMER CARD E
- [SDR CALA2018110502286](https://openairdocs.org/sdr/CALA2018110502286.md): Door Frame · cracked · Nov 3, 2018 · N804UA · Airbus A319131 · Fuselage Main, Structure
  > REF TO AAR NR-9611849- L-1 PAX DOOR CUTOUT AT FR 20. CRACK INDI CATION AT DOOR STOP FITTING #7 I/B UPPER HOLE. REF TO ECRA 5311-02037 PART 1 INTERIM REPAIR-COMPLETED AND DIP CREATED TO ACCOMPLISH THE INITIAL INSPECTION REQUIRMENTS AS PER PART 2 OF ECRA 5311-0
- [SDR CALA2018110502272](https://openairdocs.org/sdr/CALA2018110502272.md): Wire · worn · Nov 2, 2018 · N804UA · Airbus A319131 · Light System Wiring
  > CEILING PANEL MOUNTED EMERGENCY LIGHT WIRING AT R/H FR 58 STR 10 HAS MISSING SHIELDING. FIN 205WL-WIRE NO. 3351-1284 AAR N/R 961 1976. REPAIRED WIRE 3351-1284 AT FR58 STR 10R IAW A319 ESPM 20-53-21, PERMENANT REPAIR 1-E PERFORMED OP CHECK IAW A319 AMM 33-51-00
- [SDR CALA2018102702201](https://openairdocs.org/sdr/CALA2018102702201.md): Container · broken · Oct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen System
  > PASSENGER OXYGEN CONTAINER AT SEAT 31DEF FAILED TO OPEN DURING MANUAL DROP TEST. REMOVED AND INSTALLED NEW O2 CONTAINER AT SEAT 31DEF PER AM M 35-21-41-000-001-A AND 35-21-41-400-001-A. REMOVED SAFETY RING PER AMM 35-21-41-400-001-A. OPERATIONAL TEST DONE ON T
- [SDR CALA2018102702203](https://openairdocs.org/sdr/CALA2018102702203.md): Container · broken · Oct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen System
  > PASSENGER OXYGEN CONTAINER AT SEAT 29DEF FAILED TO OPEN DURING MANUAL DROP TEST. REMOVED AND INSTALLED NEW OXYGEN CONTAINER AT SEAT ROW 29DEF PER AMM 35-21-41-000-001-A AND 35-21-41-400-001-A. REMOVED SAFETY RING PER AMM 35-21-41-400-001-A. OPERATIONAL TEST OF
- [SDR CALA2018102702202](https://openairdocs.org/sdr/CALA2018102702202.md): Container · broken · Oct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen System
  > PASSENGER OXYGEN CONTAINER AT SEAT 12DEF FAILED TO OPEN DURING MANUAL DROP TEST. REMOVED PASSENGER OXYGEN CONTAINER AT SEAT 12DEF PER AMM 35 -21-41-000-001-A. REPLACED PASSENGER OXYGEN CONTAINER AT SEAT 12D EF PER AMM 35-21-41-400-001-A. OPS CHECK PERFORMED ON
- [SDR CALA2018011500208](https://openairdocs.org/sdr/CALA2018011500208.md): Power Supply · faulty · Jan 15, 2018 · N804UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY LIGHT TEST FAILS TEST WITH FAULT ESPU "L" REPLACED EPSU AND BATTERY AT 21L. REF TSM TASK 33-51-00-810-801 AND AMM33-51-00-710-001. CKS OK, NO FAULTS PRESENT.
- [SDR CALA2017020300257](https://openairdocs.org/sdr/CALA2017020300257.md): Light · malfunctioned · Feb 3, 2017 · N804UA · Airbus A319131 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FOR LEFT OVERWING EXIT IS ON IN FLIGHT RESET SYSTEM, OPS CHECKED NORMAL
- [SDR CALA2017012900191](https://openairdocs.org/sdr/CALA2017012900191.md): Angle · corroded · Jan 29, 2017 · N804UA · Airbus A319131 · Fuselage Miscellaneous Structure
  > CORROSION ON L2 DOOR SILL ON EXISTING REPAIR AT FR68. REMOVED AND REPLACED REPAIR ANGLE IAW SRM 53-41-14 FIG 201 AND SRM 51-72-11.
- [SDR CALA2017012900190](https://openairdocs.org/sdr/CALA2017012900190.md): Stringer · corroded · Jan 29, 2017 · N804UA · Airbus A319131 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT STRINGER 39R H AS CORROSION AT FRAME 61 REMOVED AND REPLACED STRINGER 39R IN AFT CARGO COMPARTMENT BETWEEN FRAME 61 TO FRAME 64 IAW SRM 51-42-11 PARAGRAPHS 5,6, AND 7.
- [SDR CALA2016101795808](https://openairdocs.org/sdr/CALA2016101795808.md): Skin · damaged · Oct 14, 2016 · N804UA · Airbus A319131 · Wing, Plate/Skin
  > RT WING 640 RB FUEL ACCESS LANDING AFT FLANGE THIRD HOLE INBD FROM CENTER LINE HAS A ELONGATED HOLE. REAMED HOLE AND FABRICATED REPAIR BUSHING AND INSTALLED IAW SRM 57-21-11 FIG 203 SRI57-21-11-2-003-00 TABLE 204
- [SDR CALA2015111794822](https://openairdocs.org/sdr/CALA2015111794822.md): Frame · cracked · Nov 10, 2015 · N804UA · Airbus A319131 · Fuselage Main, Frame
  > LEFT FRAME 35 CRACKED AT 5:00 POSITION AT HOLE 2. CARRIED OVER FROM 5 14 2015. REAMED LT FRAME 35, NR 2 HOLE. INSTALLED FREEZE PLUGS & INSTALLED FASTENERS IN HOLES 1 - 4 IAW ECRA 5330-05205.
- [SDR CALA2015072294152](https://openairdocs.org/sdr/CALA2015072294152.md): Line · loose · Jul 21, 2015 · N804UA · Airbus A319131 · Engine Oil Distribution (Airframe Furnished)
  > ENG 2 SN V11091, DURING CRZ OIL QTY INDICATION FLASHING & DOWN TO 4 QTS, OIL TEMP & PRESS SHOWS NORMAL. ENG 2 WAS REPLACED PRIOR TO THIS FLIGHT. FLIGHT 276-20 NOW DIVERTING. FOUND OIL LINE LEAKING. TORQUED, ACCOMPLISHED HIGH POWER RUN TO LEAK CHECK, NO LEA
- [SDR CALA2015050693664](https://openairdocs.org/sdr/CALA2015050693664.md): Door Frame · corroded · May 5, 2015 · N804UA · Airbus A319131 · Fuselage Main, Structure
  > R1 DOOR CUT OUT AFT LOWER CORNER CORRODED FRAME 20R. ORGINAL MATERIAL THICKNESS IN THIS AREA IS.120 TO.160. REMOVED CORROSION.023 TO.031 IN AREAS & FOUND TO BE IN LIMITS IAW SRM 53-11-12 PARA 4A TABLE 1. NDT INSPECTED AREA IAW NTM 51-10-04PB4 TO VERIFY

Next page: https://openairdocs.org/aircraft/N804UA/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 = 'N804UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N804UA/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.