N804UA

Service difficulty reports · 111

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR CALA2026102220518Elec Connector · fodBRAKES 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 FAULTOct 22, 2026 · N804UA · Airbus A319131 · Landing Gear System WiringSDR CALA2026072017895Lgciu · faultedAFTER 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. FJul 17, 2026 · N804UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR CALA2026042715738Spinner · leakingENG1 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 71-00-0Apr 15, 2026 · N804UA · Airbus A319131 · Engine (Turbine/Turboprop)SDR CALA2026012013094Fuel Cap · missingREFUELING CAP MISSING ON ARRIVALJan 17, 2026 · N804UA · Airbus A319131 · Fuel StorageSDR CALA2025122912494Control Lever · faultedAFTER 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 & EXTENSIDec 27, 2025 · N804UA · Airbus A319131 · Landing Gear SelectorSDR CALA2025060505288Bottle · no discrepancyDUE 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 DOOJun 2, 2025 · N804UA · Airbus A319131 · Standard Practices/StructuresSDR CALA2025060505285Slide · unwanted deployR2 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 31-256Jun 2, 2025 · N804UA · Airbus A319131 · Escape SlideSDR CALA2025031002668Battery · faultedFORWARD 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.Mar 9, 2025 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2025012902106Door · out of adjustCATERING 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 AFJan 29, 2025 · N804UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2025012902105Bottle · out of rigR2 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 OPEJan 29, 2025 · N804UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2025011300078Frame · damagedREMOVED 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 AJan 10, 2025 · N804UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2025010900072Shear Tie · corrodedAFT 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 LATESDec 19, 2024 · N804UA · Airbus A319131 · Fuselage Internal Mounting StructureSDR CALA2024121903120Channel · damagedL2 DOOR BOTTOM CORNER WAS DAMAGE. DOT 210-05 ()Dec 18, 2024 · N804UA · Airbus A319131 · Passenger/Crew DoorsSDR CALA2022110203019Warning Message · false activation*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 27-51-00Nov 2, 2022 · N804UA · Airbus A319131 · Flight Control SystemSDR CALA2022071301730None · inoperativeFLAPS 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 000000003Jul 13, 2022 · N804UA · Airbus A319131 · Trailing Edge Flap Control SystemSDR CALA2022053001382Angle · crackedLH 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 N078570May 28, 2022 · N804UA · Airbus A319131 · Emergency ExitsSDR CALA2022053001381Angle · crackedLH 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 N078570May 28, 2022 · N804UA · Airbus A319131 · Emergency ExitsSDR CALA2022053001380Angle · crackedRH 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.May 28, 2022 · N804UA · Airbus A319131 · Emergency ExitsSDR CALA2022052701362Angle · crackedR/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 V917May 26, 2022 · N804UA · Airbus A319131 · Emergency ExitsSDR CALA2022052701360Fitting · damagedUPON 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 ,LMay 25, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022051801271None · corrodedGUSSET 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 N078570May 16, 2022 · N804UA · Airbus A300* · Fuselage Main, FrameSDR CALA2022051601242None · crackedLH 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 TOTAMay 14, 2022 · N804UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2022050901185None · corrodedAFT 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 V061334May 8, 2022 · N804UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2022050901180None · corrodedMAIN 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 VMay 8, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022050901168None · corrodedMAIN 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 IMay 6, 2022 · N804UA · Airbus A319131 · Fuselage Main, Plate/SkinSDR CALA2022050201116Fitting · corrodedAFT 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 V937663May 1, 2022 · N804UA · Airbus A300* · Fuselage Main, StructureSDR CALA2022042701077Skin · puncturedLEFT 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 EApr 21, 2022 · N804UA · Airbus A319131 · Empennage StructureSDR CALA2022042701076Skin · puncturedRIGHT 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 TRAILIApr 21, 2022 · N804UA · Airbus A319131 · Empennage StructureSDR CALA2022042501053Skin · nonePER 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 BYApr 21, 2022 · N804UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2022042501052Skin · damagedPER 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 Apr 21, 2022 · N804UA · Airbus A319131 · Elevator, Plate/SkinSDR CALA2022032300760Pump · leakingENGINE 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 AFTEMar 23, 2022 · N804UA · Airbus A319131 · Engine Oil QuantitySDR CALA2020072701072Safety Valve · malfunctionedSYS 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 Jul 21, 2020 · N804UA · Airbus A319131 · Landing Gear Retraction/Extension SystemSDR CALA2018112102408Window Frame · crackedREF 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 Nov 20, 2018 · N804UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2018110972319Web · crackedREF 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 INNov 6, 2018 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2018110502311Actuator · no test(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 27Nov 5, 2018 · N804UA · Airbus A319131 · Flight Control SystemSDR CALA2018110502292Battery · unknown(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. A3NBNov 3, 2018 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2018110502291Pressure Panel · crackedR/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 ENov 3, 2018 · N804UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2018110502286Door Frame · crackedREF 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 5311-0Nov 3, 2018 · N804UA · Airbus A319131 · Fuselage Main, StructureSDR CALA2018110502272Wire · wornCEILING 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 33-51-00Nov 2, 2018 · N804UA · Airbus A319131 · Light System WiringSDR CALA2018102702201Container · brokenPASSENGER 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 TOct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2018102702203Container · brokenPASSENGER 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 OFOct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2018102702202Container · brokenPASSENGER 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 ONOct 26, 2018 · N804UA · Airbus A319131 · Passenger Oxygen SystemSDR CALA2018011500208Power Supply · faultyEMERGENCY 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.Jan 15, 2018 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2017020300257Light · malfunctionedEMERGENCY EXIT LIGHT FOR LEFT OVERWING EXIT IS ON IN FLIGHT RESET SYSTEM, OPS CHECKED NORMALFeb 3, 2017 · N804UA · Airbus A319131 · Emergency LightingSDR CALA2017012900191Angle · corrodedCORROSION 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.Jan 29, 2017 · N804UA · Airbus A319131 · Fuselage Miscellaneous StructureSDR CALA2017012900190Stringer · corrodedAFT 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.Jan 29, 2017 · N804UA · Airbus A319131 · Fuselage Main, Longeron/StringerSDR CALA2016101795808Skin · damagedRT 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 204Oct 14, 2016 · N804UA · Airbus A319131 · Wing, Plate/SkinSDR CALA2015111794822Frame · crackedLEFT 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.Nov 10, 2015 · N804UA · Airbus A319131 · Fuselage Main, FrameSDR CALA2015072294152Line · looseENG 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 LEAJul 21, 2015 · N804UA · Airbus A319131 · Engine Oil Distribution (Airframe Furnished)SDR CALA2015050693664Door Frame · corrodedR1 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 May 5, 2015 · N804UA · Airbus A319131 · Fuselage Main, Structure
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