# Service difficulty reports: N477UA

A list on [N477UA](https://openairdocs.org/aircraft/N477UA.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 · 108 reports

- [SDR CALA2026061917198](https://openairdocs.org/sdr/CALA2026061917198.md): Power Supply · faulted · Jun 18, 2026 · N477UA · Airbus A320232 · Emergency Lighting
  > FOUND L EPSU MESSAGE WHILE PERFORMING EMERGENCY LIGHTING TEST. R & R LC EPSU BOX PER AMM33-51-38, OPS CHECKED GOOD.
- [SDR CALA2026041615409](https://openairdocs.org/sdr/CALA2026041615409.md): Filter · odor · Apr 15, 2026 · N477UA · Airbus A320232 · Air Distribution System
  > TAXI OUT-FUMES IN COCKPIT / CABIN. INSPECTED APU COMPARTMENT FOR LEAKS AND ANY SIGNS OF ABNORMAL CONDITIONS REF. 05-50-00-810-831-A. NO OIL RESIDUE OR LEAKS OBSERVED. APU OIL LEVEL IS AT FULL MARK. RAN BOTH PACK OFF APU, RAN FOR 30 MINS, RAN IN NORMAL & H
- [SDR CALA2026030214143](https://openairdocs.org/sdr/CALA2026030214143.md): Power Supply · faulted · Feb 28, 2026 · N477UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT CHECK GIVES FAULT: EPSU UNIT EMER L. REMOVED AND REPLACED LC OVERWING EXIT EPSU IAW AMM 33-51-38-000-001-A/400-001-A OPS CHECK NORMAL TEST PASSED, GOOD TO CONTINUE
- [SDR CALA2025121212066](https://openairdocs.org/sdr/CALA2025121212066.md): Power Supply · inoperative · Dec 11, 2025 · N477UA · Airbus A320232 · Emergency Lighting
  > AFTER EPSU BATTERY REPLACEMENT, EPSU UNIT FAULT AT LEFT OVERWING EXIT REMOVED EPSU WITH UNIT FAULT, AT LEFT OVERWING EXIT, AND REPLACED WITH NEW. AMM 33-51-38. (FIN: 11WL) OPS CHECK OK, OK FOR SERVICE.
- [SDR CALA2025121212050](https://openairdocs.org/sdr/CALA2025121212050.md): Power Supply · inoperative · Dec 11, 2025 · N477UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY ROW LIGHTING AT SEAT ROWS 26-28 INOP REPLACEMENT OF LEFT OVERWING EPSU UNIT (11WL) (REF LOG PAGE 7240234) FIXED LIGHING ISSUE ON SEATROWS 26-28. AMM REF 33-51-38. OPS CHECK OK, OK FOR SERVICE.
- [SDR CALA2025090408457](https://openairdocs.org/sdr/CALA2025090408457.md): Target · loose · Sep 2, 2025 · N477UA · Airbus A320232 · Door Warning System
  > DOOR R AFT EMER EXIT INDICATION ECAM WARNING ON CLIMB. REMOVED EMERGENCY EXIT HATCH AT ROW 21DEF FOR INSPECTION AND CLEANING REF: AMM 52-21-11-000-001-A. DURING INSPECTION AND CLEANING OF THE AFT RIGHT EMERGENCY HATCH FOUND THE TARGET BRACKET ON THE COVER FLA
- [SDR CALA2025082508094](https://openairdocs.org/sdr/CALA2025082508094.md): Frame · cracked · Aug 21, 2025 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > RH FRAME 16 DOUBLE JOGGLE FASTENER HOLE #6 HAS A CRACK INDICATION IN THE FRAME LAYER, AT 1 OCLOCK (VIEWED FROM THE OUTSIDE) 60% S.H. ACCOMPLISHED INTERIM REPAIR AT RH FR 16 DBL JOGGLE HOLE # 6 IAW ECRA 5311-03392 PART 1.1. ACCOMPLISH INITIAL INSP OF RH FR16 D
- [SDR CALA2024111201108](https://openairdocs.org/sdr/CALA2024111201108.md): Fuel Cap · missing · Nov 10, 2024 · N477UA · Airbus A320232 · Fuel Storage
  > PDA 2 REF LP 9830015 - FUEL CAP REPORT MISSING IN BUR THE FUEL CAP IS NOT RII SEE GMM 09-25-05. FUEL CAP MISSING. UPDATED MAA CODE FIX USING VENDOR MAA SCREEN VERIFY NO FUEL LEAKS AND CONTACT TOMC TO APPLY CDL 28A MAC METER INITIATED. MAC RELATED WORK ORDER 00
- [SDR CALA2023082102603](https://openairdocs.org/sdr/CALA2023082102603.md): Fuel Cap · missing · Aug 18, 2023 · N477UA · Airbus A320232 · Aircraft Fuel System
  > PDA 2 FUEL CAP MISSING ON ARRIVAL. FUEL CAP M&E # IS 31-2825-9-0001 REQUEST TO PLACE ON MELC COMPLIED WITH MEL DISPATCH DESK: 24 NAME: CP DATE: 18-AUG-23- NOC DESK: 24 NAME: CP DATE: 18-AUG-23- OK TO DEFER PER CDL 28A CAP, COUPLING R OFF 31-2825-9-0001 2320 ON
- [SDR CALA2023073102390](https://openairdocs.org/sdr/CALA2023073102390.md): Accumulator · leaking · Jul 28, 2023 · N477UA · Airbus A320232 · Hydraulic Power System
  > ECAM CAUTION MESSAGE - Y RSVR LO LVL MESSAGE INOP - HYD YELLOW SYS ACCUM LEAK. R&R YELLOW HYD ACC REF MM 29-13-42. OPS CK LK CK GOOD. PARTS USED: 31-2911-3-0032,QTY:1 40-0595-3-1976,QTY:1 31-2912-9-9001,QTY:1 40-0595-3-1983,QTY:1 1842157,QTY:1 ROTABLE
- [SDR CALA2023051201469](https://openairdocs.org/sdr/CALA2023051201469.md): Cap · missing · May 11, 2023 · N477UA · Airbus A320232 · Fuel Storage
  > REFUEL-DEFUEL COUPLING CAP REPORTED MISSING WITH NO FUEL LEAK NO TED. CREW CHECKED AREA NO DAMAGE OR LEAKS COMPLIED WITH MEL STICKER APPLIED DISPATCH DEFERRED DIRECTLY BY TOMC REPLACED REFUEL COUPLING CAP IAW AMM 28-25-41-400-005-A. ROTABLE PARTS CHANGE WAS IN
- [SDR CALA2023041001087](https://openairdocs.org/sdr/CALA2023041001087.md): Windshield · failed · Apr 10, 2023 · N477UA · Airbus A320232 · Flight Compartment Windows
  > FO WINDSHIELD SHATTERED.LOOKS LIKE OUTER PANE. REMOVED AND REPLACED WHC 2 (2DG2). OPS TEST GOOD. NO / FAULTS NOTED AT THIS TIME. REMOVED AND REPLACED R1 WINDOW OPS CHECK GOOD.
- [SDR CALA2023020600347](https://openairdocs.org/sdr/CALA2023020600347.md): Battery Pack · not reported · Feb 6, 2023 · N477UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTING BATTERY CAPACITY OPERATIONAL CHECK {A3NB-33-3-6013} - FWD LEFT EMERGENCY LIGHTS BATTERY FAILED THE CAPACITY TEST. REMOVED AND REPLACED THE LEFT EMERGENCY LIGHTS BATTERY PER AMM 33-51-38. OPS CHECK GOOD.
- [SDR CALA2022101002744](https://openairdocs.org/sdr/CALA2022101002744.md): Frame · cracked · Oct 7, 2022 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > LEFT FR 35 STR 30 HOLE 1,2,3, HAS A OUT OF ROUND INDICATION IN THE FR LAYER INTERIOR FACE AT 3-7 O''CLOCK AND AFT SKIN LAYER FWD SKIN LAYER AS VIEWED FROM EXTERIOR ADDITIONALY HOLE FOUND AT L/H FR35 STR28 FOUND CRACKED PER HAECO LCQ N/R 9290148/30148/9290149
- [SDR CALA2022100702736](https://openairdocs.org/sdr/CALA2022100702736.md): Fitting · cracked · Oct 6, 2022 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > RIGHT FR35, STGR 30, HOLE #2 HAS A CRACK INDICATIONS IN THE FRAM E LAYER 7 O''CLOCK POSITION, AFT SKIN LAYER 6 O''CLOCK POSITION, A ND FWD SKIN LAYER O''CLOCK POSITION, AS VIEWED FROM EXTERIOR GENE RATED BY V061671 AT HAECO LCQ PER NR 9290145 (30145) O''CLOCK
- [SDR CALA2022100702734](https://openairdocs.org/sdr/CALA2022100702734.md): Frame · corroded · Oct 6, 2022 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > AFT CARGO RH SIDE AT FR57 STGR37 HAS CORROSION PER HAECO LCQ N/R 9290712/30712 GEN BY V935513 REMOVED AND REPLACED STRINGER 37 RT FRAME 57 IAW A320 SRM 51-72- 11 AND EC/RA 5341-01340 NO REINSPECT REQUIRED BY MECH V052030 IN SP BY V935513
- [SDR CALA2022100302587](https://openairdocs.org/sdr/CALA2022100302587.md): Door · corroded · Oct 1, 2022 · N477UA · Airbus A320232 · Fuselage Structure (General)
  > R2 DOOR AND FR68 FWR FACE LOWER AREA HAVE CORROSION PER HAECO LC Q N/R 9290381/30381 GEN BY V061682 SEE LP''S 9647687 AND 9647706 FOR DIPS AND REPETITVE INSP REQUIREMENT FOR THE REPAIR OF THE R2 DOOR AND FR68 FWR FACE LOWER AREA HAVE CORROSION PER ECRA 5341-01
- [SDR CALA2022100302586](https://openairdocs.org/sdr/CALA2022100302586.md): Flange · cracked · Oct 1, 2022 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > RH FR68 AT STR22 WEB FLANGE HAS CRACK INICATION IN FLANGE RADIUS ADJACENT TO LOWER IB DOOR STOP PER HAECO LCQ N/R 9290234/30234 G EN BY V892444 THE RH FR68 STR 22 EXTERNAL SURFACES OF THE FRAME AND REPAIR ON OR BEFORE 54,067 TOTAL AIRCRAFT FC''S. ACCOMPLISH RE
- [SDR CALA2022092802541](https://openairdocs.org/sdr/CALA2022092802541.md): None · none · Sep 27, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > FABRICATE CLEAT FOR FWD CARGO PIT FR30 PER HAECO LCQ N/R 9290783 /30783 GEN BY V052030 REMOVED AND REPLACED CLEAT AT FRAME 30 BETWEEN STRINGERS 42R-43R IN THE FORWARD CARGO BAY IAW A320 SRM 51-72-11 BY MECH V052030 I NSP BY V061647
- [SDR CALA2022092802531](https://openairdocs.org/sdr/CALA2022092802531.md): None · none · Sep 26, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT R/H FR28 BETWEEN STRINGERS 42R-43R CLEAT HAS CORRO SION (A3NB-05-3-6013). GENERATED BY V919150 AT HAECO LCQ PER NR 9290367 (30367). REMOVED AND REPLACED CLEAT AT FR28, STR 42R-43RT IAW A320 SRM 51 -72-11-911-001. PERFORMED BY V052030
- [SDR CALA2022092802532](https://openairdocs.org/sdr/CALA2022092802532.md): None · none · Sep 26, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > WINDSHIELD LOWER CENTER POST LEFT CONTINUITY FITTING HAS CRACK I NDICATION ON UPPER LEG APPROX.600 OB OF CTR POST PER HAECO LCQ N/R 9290692/30692 GEN BY V892444 REMOVED AND REPLACED WINDSHIELD LOWER CENTER POST L/H AND R/H CO NTINUITY FITTINGS IAW A320 EC/RA
- [SDR CALA2022092602500](https://openairdocs.org/sdr/CALA2022092602500.md): None · corroded · Sep 24, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT RH FR27 BETWEEN STRINGERS 43R-44 CLEAT HAS CORROSION. GENERATED BY V919150 AT HAECO LCQ PER NR 9290370 (30370) {A3NB-05-3-6013} REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FRAME 27 RT IAW A320 SRM 51-72-11. ACP BY V052030 INSP BY V061771.
- [SDR CALA2022092602499](https://openairdocs.org/sdr/CALA2022092602499.md): None · corroded · Sep 24, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT RH FR28 BETWEEN STRINGER 41R-42R CLEAT HAS CORROSION. GENERATED AT HAECO LCQ PER NR 9290368 (30368) BY V919150. {A 3NB-05-3-6013} REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FR28
- [SDR CALA2022092602497](https://openairdocs.org/sdr/CALA2022092602497.md): None · corroded · Sep 24, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT RH FR28 BETWEEN STRINGERS 43R-44 CLEAT HAS CORROSION AROUND FASTENERS. REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FR28 RT.
- [SDR CALA2022092602496](https://openairdocs.org/sdr/CALA2022092602496.md): None · corroded · Sep 24, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT R/H FR27 BETWEEN STRINGERS 42R-43R CLEAT HAS CORROSION. GENERATED AT HAECO LCQ BY V919150 PER NR 92 90366 (30366) REMOVED AND REPLACED CLEAT IN FWD CARGO PIT FR27 RT IAW A320 SRM 51-22-11 ACM BY V052030 INSP BY V061771
- [SDR CALA2022092302467](https://openairdocs.org/sdr/CALA2022092302467.md): None · corroded · Sep 22, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO PIT R/H BETWEEN FR24-31 STRINGER 42R HAS CORROSION SPO TS PER HAECO LCQ N/R 9290358/30358 GEN BY V919150 REMOVED AND REPLACED STRINGER 42 RT FR 24-31 IAW A320 SRM 51-72- 11-911-001 BY MECH V052030 INSP BY V061771
- [SDR CALA2022092302466](https://openairdocs.org/sdr/CALA2022092302466.md): None · corroded · Sep 22, 2022 · N477UA · Airbus A300* · Fuselage, Wing Attach Fittings
  > FWD CARGO PIT R/H BETWEEN FR 24-29 STRINGER 43R HAS CORROSION AR OUND FASTENERS PER HAECO LCQ N/R 9290359/30359 GEN BY V919150 REMOVED AND REPLACED STRINGER 43 R/H FR 24-29 IAW A320 SRM 51-72 -11-911-001 BY MECH V052030 INSP BY V061771
- [SDR CALA2022092102436](https://openairdocs.org/sdr/CALA2022092102436.md): Fitting · cracked · Sep 20, 2022 · N477UA · Airbus A300* · Fuselage Main, Frame
  > L/H FR 68 DOOR STOP #1 HOLE#3 HAS A CRACK IN FRAME AT 5 O''CLOCK PER HAECO LCQ N/R 9290274/30274 GEN BY V061632
- [SDR CALA2022091902406](https://openairdocs.org/sdr/CALA2022091902406.md): Door Sill · corroded · Sep 16, 2022 · N477UA · Airbus A300* · Fuselage Structure (General)
  > R2 DOOR SILL AFT CORNER HAVE CORROSION AROUND GIRD BAR PLATE PER HAECO LCQ NR 9290380/30380 GENERATED BY V061682 (SUPPORT TASK) REMOVED & REPLACED R2 DOOR SILL IAW A320 SRM 51-72-11. PERFORMED BY V052030 INSP BY V061771.
- [SDR CALA2022091902404](https://openairdocs.org/sdr/CALA2022091902404.md): Fitting · corroded · Sep 16, 2022 · N477UA · Airbus A300* · Fuselage Structure (General)
  > R2 DOOR AND FR68 AFT LWR CORNER FITTING HAS CORROSION. GENERATED BY V061682 ON HAECO LCQ NR 9290382/30382 REMOVED AND REPLACED R2 DOOR AFT CORNER FITTING AT FR 68 IAW A32 0 SRM 51-42-11-001. ACMP BY MECH V052030 INSP BY V061771
- [SDR CALA2022091902403](https://openairdocs.org/sdr/CALA2022091902403.md): None · corroded · Sep 16, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > AFT CARGO FR 63-64 STR 41L HAS CORROSION PER HAECO LCQ NR 929068 2/30682 GENERATED BY N078570 (SUPPORT TASK) REMOVED AND REPLACED STRINGER 41L FR 63-64 IAW A320 SRM 51-72-11 -911-001. PERFORMED BY V052030 INSP BY V061771
- [SDR CALA2022091902402](https://openairdocs.org/sdr/CALA2022091902402.md): Frame · corroded · Sep 16, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > AFT CARGO DOOR BOTTOM FRAME HAS CORROSION ON TORSION BOX UPPER S URFACE PER HAECO LCQ NR 9290433/30433 GENERATED BY V919150 (A3NB -05-3-6023) REMOVED & REPLACED AFT PIT TORSION BOX COVER SHEET IAW A320 SRM 51-42-11-001. PERFORMED BY V052030 INSP BY V061771.
- [SDR CALA2022091902401](https://openairdocs.org/sdr/CALA2022091902401.md): None · corroded · Sep 16, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > AFT CARGO FR 63-64 STR 42L HAS CORROSION PER HAECO LCQ NR 929068 4/30684 GENERATED BY N078570 (SUPPORT TASK) REMOVED & REPLACED AFT CARGO STRINGER 42L IAW A320 SRM 51-72-11- 911-002. PERFORMED BY V052030 INSP BY V061771
- [SDR CALA2022091602380](https://openairdocs.org/sdr/CALA2022091602380.md): None · corroded · Sep 15, 2022 · N477UA · Airbus A300* · Fuselage, Seat/Cargo Attach Fittings
  > FWD CARGO DOOR BOTTOM FRAME TORSION BOX HAS CORROSION SPOTS ON UPPER SURFACE PER HAECO LCQ NR 9290355/30355 GENERATED BY V919150 (A3NB-05-3-6013) REMOVED & REPLACED COVER SHEET TORSION BOX IAW A320 SRM 51-42-11 -001. PERFORMED BY V052030 INSP BY V061771.
- [SDR CALA2022091402361](https://openairdocs.org/sdr/CALA2022091402361.md): Rib · corroded · Sep 12, 2022 · N477UA · Airbus A300* · Empennage Structure
  > RH ELEVATOR TIP HAS CORROSION (SUPPORT TASK). GENERATED BY V0616 82 AT HAECO LCQ, PER NR 9290678 (30678). CORROSION FOUND TO BE ON R/H ELEVATOR TIP CAP MOUNTING RIB AND T O BE OUT OF LIMITS IAW SRM A320 55-21-12-04-A. REMOVED AND REPLA CED WITH NEW RIB IAW A32
- [SDR CALA2022091402356](https://openairdocs.org/sdr/CALA2022091402356.md): None · corroded · Sep 12, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > AFT CARGO FR 63-64 STR 42R HAS CORROSION. GENERATED BY N078570 A T HAECO LCQ PER NR. 9290683 (30683).(SUPPORT TASK) REMOVED AND REPLACED STR 42R AT FR 60-FR64 AFT CARGO IAW;A320 S RM 51-72-11-911-002. INSTALLED 2EA CLENTS AT FR 60 IAW A320 SRM 51-22-11-911-00
- [SDR CALA2022090702301](https://openairdocs.org/sdr/CALA2022090702301.md): Intercostal · cracked · Sep 5, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > AD RELATED (AD 2022-02-11) LH FR16 DOOR STOP #7 HOLE #1 IN FRAME @ 7 OCLOCK AND HOLE #3 IN INTERCOSTAL AT 9 OCLOCK PER HAECO LCQ NR 30232/9290232 SUPPORT TASK GENERATED BY V061632 REMOVED & REPLACED INTERCOSTAL IAW A320 SRM 51-42-11/001 PAR 6 E,F ON LH FR16 D
- [SDR CALA2022090702299](https://openairdocs.org/sdr/CALA2022090702299.md): Intercostal · cracked · Sep 5, 2022 · N477UA · Airbus A300* · Fuselage Main, Frame
  > AD RELATED (AD 2022-02-11) RH FR20 #7 DOOR STOP HOLE #1 CRACK IN FRAME @ 9 OCLOCK PER HAECO LCQ NR 9290236/30236 GENERATED BY V0 61632 SUPPORT TASK REMOVED AND REPLACED INTERCOSTAL IAW A320 SRM 51-42-11/001 PAR 6 E,F ON RH FR20 #7 DOOR STOP HOLE #1. PERFORMED
- [SDR CALA2022090202247](https://openairdocs.org/sdr/CALA2022090202247.md): Intercostal · none · Aug 31, 2022 · N477UA · Airbus A320232 · Fuselage Main, Frame
  > R/H FR 16 #7 DOOR STOP HOLE #1 CRACK IN INTERCOSTAL AT 10 O''CLOC K AND HOLE #3 INTERCOSTAL AT 1 O''CLOCK (AD 2022-02-11) PER HAECO LCQ N/R 9290235/30235 GEN BY V061632 RMVD AND RPLD INTERCOSTAL AT R/H FR 16 #7 IAW A320 SRM 51-42-11/ 001 AND APPLIED PROTECTIVE
- [SDR CALA2022082902193](https://openairdocs.org/sdr/CALA2022082902193.md): Gusset · cracked · Aug 26, 2022 · N477UA · Airbus A300* · Fuselage Main, Structure
  > FRAME 68 GUSSET AT STR 14 LEFT BOTTOM HOLE HAS CRACK INDICATION PER HAECO LCQ N/R 9290376/30376 GEN BY V892444 FABRICATED NEW GUSSET FITTING AT L/H STR14 PER A320 SRM 51-72-11 -911-001 AND INSTALLED PER A320 SRM 51-72-11-911-001 BY MECH V92 9027 INSP BY NO7857
- [SDR CALA2019101101732](https://openairdocs.org/sdr/CALA2019101101732.md): Apu · odor · Oct 9, 2019 · N477UA · Airbus A320232 · Airborne Auxiliary Power Unit (APU) System
  > CREW REPORTS OZONE BURNING SMELL THROUGHOUT AIRCRAFT WITH BLEEDS ON. CREW SHUTDOWN ENG 1 BLEED AND SMELL DISSIPATED. SMELL RETURNED WITH APU BLEED ON. ACCOMPLISHED HIGH POWER RUN ON #1 ENGINE WITH ENGINE BLEEDS ON, NO DETECTION OF SMOKE ODOR OR FUMES IN THE CA
- [SDR CALA2019072401229](https://openairdocs.org/sdr/CALA2019072401229.md): Fuel Cap · missing · Jul 22, 2019 · N477UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP REPORTED MISSING ON LP 3820243 OFF FLIGHT 2316 EWR-AUS. FUEL CAP PLACED ON CDL 28A. REF L/P 3820243 FOR ITEM FUEL CAP ON CDL.
- [SDR CALA2018110502302](https://openairdocs.org/sdr/CALA2018110502302.md): Engine · making metal · Nov 5, 2018 · N477UA · Airbus A320232 · Engine Oil System (Airframe Furnished)
  > #2 ENG MAIN MCD FOUND 1 ROUND METALIC MAGNETIC JAGGED BALL APROX DIA.045". INSPECTED MASTER MCD PER AMM 79-00-00-200-011-A. UPLOAD DEBRIS P ICTURES TO RVI SITE. CONTACTED TOMC ENGINE DESK: BRIAN. DEBRIS/ CHIP SAMBLE TAKEN AND TO BE SENT TO SFO LAB FOR ANALYSI
- [SDR CALA2017122804639](https://openairdocs.org/sdr/CALA2017122804639.md): Cids · malfunctioned · Dec 28, 2017 · N477UA · Airbus A320232 · Emergency Lighting
  > CABIN EMERGENCY LIGHTS ON REGARDLESS OF SWITCH POSITION. ACCOMPLISHED A CIDS RESET, OPS CHECKED OK.
- [SDR CALA2017111704126](https://openairdocs.org/sdr/CALA2017111704126.md): Lens · missing · Nov 17, 2017 · N477UA · Airbus A320232 · Emergency Lighting
  > MISSING EMERGENCY EXIT LIGHT LENS UNDER SEAT 32A. INSTALLED THE LENS.
- [SDR CALA2017090103018](https://openairdocs.org/sdr/CALA2017090103018.md): Circuit Breaker · malfunctioned · Sep 1, 2017 · N477UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS WILL NOT SHUT OFF. CYCLED CIDS CIRCUIT BREAKER. CHECKED OK
- [SDR CALA2017062602003](https://openairdocs.org/sdr/CALA2017062602003.md): Cids · malfunctioned · Jun 26, 2017 · N477UA · Airbus A320232 · Audio/Video Monitoring
  > NR 2 SVC, CABIN EMERGENCY LIGHT TEST SHOW "EPSU BATTERY AFT L" MSG DISPLAYED ON PTP. ROW 38L SEAT EEL LIGHT INOP. RESET CIDS SYSTEMS AND PERFORMED CABIN EMERGENCY LIGHT TEST. PASSED REF AMM 33-51-00-0501.
- [SDR CALA2017061201819](https://openairdocs.org/sdr/CALA2017061201819.md): Hinge Bracket · cracked · Jun 12, 2017 · N477UA · Airbus A320232 · Escape Slide
  > FWD LEFT ENTRY DOOR, FWD HINGE BRACKET ON SLIDE IS CRACKED. REPLACED THE NR 1 LT FWD SLIDE.
- [SDR CALA2016041895274](https://openairdocs.org/sdr/CALA2016041895274.md): Skin · gouged · Apr 12, 2016 · N477UA · Airbus A320232 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR EXTERIOR SKIN, UPPER AFT SKIN GOUGED. REPAIRED IAW SRM 52-31-00-201 FIG 209.
- [SDR CALA2016041195266](https://openairdocs.org/sdr/CALA2016041195266.md): Skin · gouged · Apr 8, 2016 · N477UA · Airbus A320232 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR HAS A SKIN GOUGE AT THE UPPER AFT AREA. INSTALLED DOUBLER REPAIR IAW SRM 52-31-00-201 FIG 209

Next page: https://openairdocs.org/aircraft/N477UA/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 = 'N477UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N477UA/reports

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