# Service difficulty reports: N471UA

A list on [N471UA](https://openairdocs.org/aircraft/N471UA.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 2 · 98 reports

- [SDR CALA2025123012526](https://openairdocs.org/sdr/CALA2025123012526.md): Thermocouple · faulted · Dec 28, 2025 · N471UA · Airbus A320232 · Engine EGT/TIT Indicating System
  > ENROUTE AT FL300, NR 1 ENG EGT INDICATED TEMPS BETWEEN 027 & -046 DEGREES C. CREW REPORTS READINGS TO BE NORMAL AT START UP & ASCEND. DURING CRUISE NR 1 ENG EGT DECLINED FROM 300 TO -34 WITHIN 5 MINS, STAYED AROUND -34 DURING ENTIRE CRUISE (AROUND THE SAME T
- [SDR CALA2025120211628](https://openairdocs.org/sdr/CALA2025120211628.md): Power Supply · faulted · Dec 1, 2025 · N471UA · Airbus A320232 · Emergency Lighting
  > EPSU EXT LOAD EMER L FAULT FOUND ON EMERGENCY LIGHT BITE TEST. TESTED ALL EXTERNAL LIGHTS ON LH SIDE OF AIRPLANE. OVERWING EMERGENCY LIGHTS & LH OVERWING SLIDE (REF LP 7135969 FOR REMOVAL). ALL LIGHTS TESTED OK. REMOVED AND REPLACED EPSU POWER SUPPLY UNIT IAW
- [SDR CALA2025112411439](https://openairdocs.org/sdr/CALA2025112411439.md): Fuel Cap · missing · Nov 20, 2025 · N471UA · Airbus A320232 · Aircraft Fuel Distribution System
  > AIRCRAFT ARRIVED WITHOUT FUEL CAP, PLACED ON CDL. FUEL CAP PLACED ON CDL, REF L/P 7021387. REPLACED FUEL CAP, OPS CHECKED GOOD IAW AMM 28-00.
- [SDR CALA2025092509250](https://openairdocs.org/sdr/CALA2025092509250.md): Unknown · odor · Sep 24, 2025 · N471UA · Airbus A320232 · Air Distribution System
  > AFT FAS REPORTED SMELLING A HYDRAULIC FLUID ODOR AFTER LANDING. NO HYD LEAK OR LOSS NOTED, NO ODORS IN CABIN, OK FOR SVC.
- [SDR CALA2025081207632](https://openairdocs.org/sdr/CALA2025081207632.md): Battery · no test · Aug 10, 2025 · N471UA · Airbus A320232 · Emergency Lighting
  > LEFT AFT EPSU BATTERY FAILED TEST. REMOVED AND REPLACED AFT LEFT EPSU BATTERY, SYSTEM TEST OKAY.
- [SDR CALA2025043004344](https://openairdocs.org/sdr/CALA2025043004344.md): Fuel Cap · missing · Apr 25, 2025 · N471UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUELER REPORTED FUEL CAP IS MISSING. CHECK AREA FOR MISPLACED FUEL CAP. CHECKED WITH LOCAL FUELER. UNABLE TO LOCATE. NO LEAKS NOTED AT COUPLING. INOP STICKER APPLIED. PLACED ON CDL 28A.
- [SDR CALA2025031802908](https://openairdocs.org/sdr/CALA2025031802908.md): Slide · faulty · Mar 13, 2025 · N471UA · Airbus A320232 · Escape Slide
  > R1 DOOR SLIDE PN- D30664-705 S/N- A5823 AND GIRT BAR REMOVED PER WORKCARD. PLACED UNDER FWD GALLEY. SAFETY PIN IS INSTALLED. STARTED INSTALLING R1 DOOR SLIDE REF TASK CARD 31-25-62-1-3810 UP TO BLOCK 16 COMPLETED R1 DOOR SLIDE INSTALLATION PER WORK CARD 31-2
- [SDR CALA2024083000519](https://openairdocs.org/sdr/CALA2024083000519.md): Engine · unknown · Aug 28, 2024 · N471UA · Airbus A320232 · Engine (Turbine/Turboprop)
  > REJECTED TAKE OFF AT 60 KNOTS. ON T/O ENGINES DI D NOT COME UP T OGETHER A ND WERE SPLIT AT FLEX UPON ARRIVAL TO COCKPIT, NO STATUS MESSAGE WAS PRESENT. PRINTED A PFR. FOUND FAILURE "DMC2: NO ADF1 DATA" AND "DMC3: NO EEC2B DATA SOURCE EIS 3 AT 01:31 GMT ( SAME
- [SDR CALA2024031800776](https://openairdocs.org/sdr/CALA2024031800776.md): Thrust Reverser · damaged · Mar 10, 2024 · N471UA · Airbus A320232 · Engine Thrust Reverser
  > PDA 2 REF LP 7310261. DURING WALKAROUND FOUND E1 IB THRUST REVERSER HALF RIGHT WITH MISSING BLOCKER DOOR AND DAMAGE TO THE SLEEVE AND BYPASS. AIRPORT LOCAL AUTORITIES ACCOMPLISHED SEARCH OF REVERSER REMAINS U.NOT FIDING ANY REMAIN PDA CLOSED NO LOSSE HARDWARE
- [SDR CALA2023122003668](https://openairdocs.org/sdr/CALA2023122003668.md): Tee Angle · damaged · Dec 12, 2023 · N471UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF R/H AFT TI ANGLE REPLACEMENT HFEC ROTO INSP OF FASTENER HOLES #13 & #14 PRODUCED OUT OF ROUND INDICATION. PER HAECO LCQ NON ROUTINE 9294451/26451 REPAIRED AREA IAW HAECO REO-L24797 REV IR AND ECRA 5331-03072. REF LP 6553608 FOR DIP R
- [SDR CALA2023121403644](https://openairdocs.org/sdr/CALA2023121403644.md): Angle · cracked · Dec 12, 2023 · N471UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT AFT TI ANGLE CRACKED PER HAECO LCQ NON ROUTINE 9294188/26188 GENERATED BY V079881 025FH. THIS ECRA REPLACES THE RH AFT TI-ANGLE BETWEEN FAIRING AN ORIGINATING FROM PRIOR ACCOMPLISHMENT OF EA. D KEEL BEAM SIDE PANEL AT FR40-FR22 IAW AIRBUS SB A320-53-1259 R
- [SDR CALA2023120803599](https://openairdocs.org/sdr/CALA2023120803599.md): Frame · cracked · Dec 7, 2023 · N471UA · Airbus A320232 · Fuselage Main, Frame
  > LH FRAME 16 DOUBLE JOGGLE FASTENER HOLE "A" HAS A SMALL CRACK (4 5% FSH) INDICATION IN AT 9 O''CLOCK POSITION (FORWARD). UNABLE TO DETECT CRACK WITH SURFACE SCAN. AREA MARKED ON AIRCRAFT PER HAE CO LCQ NON ROUTINE 9294283/26283 REPAIRED DISCREPANT FASTENER HO
- [SDR CALA2023120503542](https://openairdocs.org/sdr/CALA2023120503542.md): Floor Support · corroded · Dec 1, 2023 · N471UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > AFT CABIN STRUCTURE, FR66-68 L/H Y765 TOP BEAM, MULTIPLE FASTENER HOLES HAVE CORROSION AROUND THEM. GEN BY V920443 ON HAECO LCQ NON ROUTINE 9294657/26357 FLOOR BEAM AT AFT CABIN FR66-68 LH Y=765 WAS REMOVED AND REPLACED IAW A320SRM 51-72-11-911-001 ACMP BY MEC
- [SDR CALA2023120503564](https://openairdocs.org/sdr/CALA2023120503564.md): Skin · contaminated · Nov 28, 2023 · N471UA · Airbus A320232 · Elevator, Plate/Skin
  > RH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 33 INC HES FROM IB EDGE AND 9 INCHES FROM AFT EDGE, 4.5 INCHES DIA. PER HAECO LCQ NON ROUTINE 9294369/26369 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 33 IN FROM I/B 9 IN FROM T/E 1.5 IN DIA 2EA AR
- [SDR CALA2023120503562](https://openairdocs.org/sdr/CALA2023120503562.md): Skin · contaminated · Nov 28, 2023 · N471UA · Airbus A320232 · Elevator Structure
  > RH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 70.25 INCHES FROM IB EDGE AND 10 INCHES FROM AFT EDGE, 1 INCH DIA. PER HAECO LCQ NON ROUTINE 9294370/26370 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 70.25 IN FROM VB 10 IN FROM T/E 1.5 IN DIA ZON
- [SDR CALA2023120503550](https://openairdocs.org/sdr/CALA2023120503550.md): Skin · contaminated · Nov 28, 2023 · N471UA · Airbus A320232 · Elevator, Plate/Skin
  > RH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 79.5 I NCHES FROM IB EDGE AND 9.5 INCHES FROM AFT EDGE, 1.5 INCH DIA. P ER HAECO LCQ NON ROUTINE 9294371/26371 REPAIRED RH ELEVATOR UPPER SKIN 79.5 IN FROM I/B 9.5 IN FROM T/E 1.5 IN DIA ZONE 1 IAW A32
- [SDR CALA2023120503560](https://openairdocs.org/sdr/CALA2023120503560.md): Skin · contaminated · Nov 28, 2023 · N471UA · Airbus A320232 · Elevator, Plate/Skin
  > RH ELEVATOR UPPER SURFACE HAS INDICATION OF WATER INGRESS 21.5 I NCHES FROM IB EDGE AND 11 INCHES FROM AFT EDGE, 2.5 INCHES DIA. PER HAECO LCQ NON ROUTINE 9294368/26368 GENERATED BY V892444 DRILLED WITNESS HOLES ON RH ELEVATOR UPPER SKIN 21.5 IN FROM I/B 11 IN
- [SDR CALA2023112703479](https://openairdocs.org/sdr/CALA2023112703479.md): Frame · cracked · Nov 24, 2023 · N471UA · Airbus A320232 · Fuselage Main, Frame
  > REPAIR BEFORE NEXT FLIGHT, R/H FR 43 FOOT, REMOVED FASTENER HOLE HAS A CRACK INDICATION AT THE 3:O''CLOCK POS IN THE FRAME LAYER GEN BY V062335 ON HAECO LCQ NR 9294098/26098 (AD RELATED TASK) REPAIRED DISCREPANCY HOLE FR43 RH RAW DRAWING 15R3370233B.
- [SDR CALA2023112703485](https://openairdocs.org/sdr/CALA2023112703485.md): Door Frame · cracked · Nov 22, 2023 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > LT AFT EMERGENCY EXIT HATCH CRACKED. REMOVED AND REPLACED FWD FRAME SEGMENT ON L/H AFT EMERGENCY HATC H IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2023112703483](https://openairdocs.org/sdr/CALA2023112703483.md): Frame · cracked · Nov 22, 2023 · N471UA · Airbus A320232 · Emergency Exits
  > RT AFT EMERGENCY EXIT HATCH CRACKED. REMOVED AND REPLACED AFT FRAME SEGMENT ON R/H AFT EMERGENCY HATC H IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2023112703481](https://openairdocs.org/sdr/CALA2023112703481.md): Frame · cracked · Nov 22, 2023 · N471UA · Airbus A320232 · Emergency Exits
  > RT FWD EMERGENCY EXIT HATCH CRACKED. REMOVED AND REPLACED FRAME SEGMENT & SEGMENT (FWD SIDE) ON R/H O /W EMERGENCY HATCH IAW A320 SRM 51-72-11-911-001.
- [SDR CALA2023071002206](https://openairdocs.org/sdr/CALA2023071002206.md): Door Latch · inoperative · Jul 6, 2023 · N471UA · Airbus A320232 · Oxygen System
  > FWD LAV O2 PANEL DOOR REPEATEDLY POPPED OPEN IN FLT. MASKS STAYE D STOWED. FWD LAV O2 BOX DOOR LATCH INOP COMPLIED MEL 3521B OK TO DEFER FWD LAV O2 MODULE INOP PARTS INFO UPDATE REPLACED LATCH MECAHNISM AND LATCH PIN WITHIN BOX PER CMM 75-3521-3-0025,QTY:1 3
- [SDR CALA2023030300599](https://openairdocs.org/sdr/CALA2023030300599.md): Sensor · faulted · Mar 3, 2023 · N471UA · Airbus A320232 · Fuel Controlling System
  > DURING FADEC FAULT CODES TASK CARD 18-73-22-1-7905 FADEC 1B SHOWED A FAULT. P2 T2 SENS/HC/EEC1. ON ENGINE 1. ACCOMPLISHED TSM 73-22-00-810-871-A, AND PERFORMED INSPECTION OF THE P2/T2 SENSOR IAW AMM 73-22-11-200-010, AND THE P2/T2 HAS BEEN TESTED IAW AMM 73-22
- [SDR CALA2022060801472](https://openairdocs.org/sdr/CALA2022060801472.md): Fuel Cap · missing · Jun 4, 2022 · N471UA · Airbus A300* · Aircraft Fuel System
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL REPORT SUBMITTED ON 6/04/22. PDA 3 FUEL CAP MISSING ON ARRIVAL PLACED ON CDL. INSTALLED NEW FUEL CAP AS REQUIRED.
- [SDR CALA2022011400147](https://openairdocs.org/sdr/CALA2022011400147.md): Stop Fitting · cracked · Jan 13, 2022 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLT) CRACK FOUND IN LH FR16 #1 DOOR STOP FIT TING HOLE #3 CRACK IS IN THE FRAME AND INTERCOSTAL. () REPIR L/H FILE #1 DOOR STOP FITTING HOLE #3 IAW EC/RA 5311-02702 ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. NR#00187 18.
- [SDR CALA2022011400145](https://openairdocs.org/sdr/CALA2022011400145.md): Fastener · cracked · Jan 13, 2022 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLIGHT) ROTO PROBE OF LH FR68 #1 DOOR STOP F ITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE.() REPAIRED LH FR68 #1 DOOR STOP FITTING IAW EC/RA 5341-01294. FORM 44-0008 ATTACHED EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERI NG AEROSPACE OF
- [SDR CALA2022011200120](https://openairdocs.org/sdr/CALA2022011200120.md): Fastener · cracked · Jan 12, 2022 · N471UA · Airbus A300* · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLIGHT) ROTO PROBE OF RH FR68 #1 DOOR STOP F ITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE.() REPAIRED RH FR68 #1 DOOR STOP FITTING IAW EC/RA 5341-01294. EMP# V934774 WORK ACCOMPLISHED AT ST ENGINEERING AREOSPACE OF MOBILE AT BFM ON NR# 00
- [SDR CALA2022011200119](https://openairdocs.org/sdr/CALA2022011200119.md): Fastener · out of round · Jan 12, 2022 · N471UA · Airbus A300* · Fuselage Main, Structure
  > (REPAIR BEFORE NEXT FLIGHT) VISUAL AND ROTO PROBE INSPECTION OF LH FR68 #7 DOOR STOP FITTING FASTENER HOLES FOUND #2 AND #4 HOLE S OUT OF ROUND.() REPAIRED LH FR68 #7 DOOR STOP IAW EC/RA 5341-01294 FORM 44-0008 ATTACHED. EMP# V935774 WORK ACCOMPLISHED AT ST EN
- [SDR CALA2022011200111](https://openairdocs.org/sdr/CALA2022011200111.md): None · cracked · Jan 10, 2022 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > ROTO PROBE OF LH FR68 #1 DOOR STOP FITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE SEE LP#7790391 FOR SCEPTER SIGNOFF. ACCOMPLISHED BY EMP#V935774 AT BFM ST AEROSPACE MOBILE. NR#0018923
- [SDR CALA2022011000096](https://openairdocs.org/sdr/CALA2022011000096.md): None · cracked · Jan 9, 2022 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > ROTO PROBE OF RH FR68 #1 DOOR STOP FITTING FASTENER HOLES FOUND A CRACK AT #3 HOLE
- [SDR CALA2022011000087](https://openairdocs.org/sdr/CALA2022011000087.md): None · out of round · Jan 9, 2022 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > VISUAL AND ROTO PROBE INSPECTIN OF LH FR68 #7 DOOR STOP FITTING FASTENER HOLES FOUND #2 AND #4 HOLES OUT OF ROUND
- [SDR CALA2022011000074](https://openairdocs.org/sdr/CALA2022011000074.md): None · none · Jan 7, 2022 · N471UA · Airbus A320232 · Standard Practices/Structures
  > (AD 2018-03-12) L/H FR66 DOOR STOP #6 TOP I/B HOLE HAS OVALITY.() REPAIRED LH FR66 DOOR STOP #6 IAW EC/RA 5341-01293 EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM O N NR#0018943
- [SDR CALA2022011000073](https://openairdocs.org/sdr/CALA2022011000073.md): None · none · Jan 7, 2022 · N471UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) L/H FR66 DOOR STOP #7 TOP AND BOTTOM O/B HOLES H AVE OVALITY. DOOR STOP #3 BOTTOM I/B HOLE HAS A REJECTABLE DAMAG E INDICATION. DOOR STOP #1 TOP O/B HOLE HAS A CRACK INDICATION,B OTTOM O/B HOLE HAS OVALITY REPAIRED L/H FR66 DOOR STOPS IAW EC/RA
- [SDR CALA2022011000068](https://openairdocs.org/sdr/CALA2022011000068.md): None · cracked · Jan 7, 2022 · N471UA · Airbus A320232 · Fuselage Structure (General)
  > (AD 2018-03-12) R/H SIDE FR66 DOOR STOP #7 TOP I/B HOLE HAS A CR ACK INDICATION. DOOR STOP #3 BOT I/B HOLE HAS REJECTABLE DAMAGE INDICATION.() REPAIRED R/H FR66 DOOR STOP #7 IAW EC/RA 5341-01293 EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB
- [SDR CALA2021121302352](https://openairdocs.org/sdr/CALA2021121302352.md): Intercostal · cracked · Dec 12, 2021 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > CRACKS FOUND IN THE RH FR16 #7 DOOR STOP FITTING FASTENER HOLES AT #1 AND #3 HOLES. CRACKS ARE IN THE INTERCOSTAL ONLY.
- [SDR CALA2021121202351](https://openairdocs.org/sdr/CALA2021121202351.md): Intercostal · cracked · Dec 12, 2021 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > CRACK FOUND IN THE RH FR20 #1 DOOR STOP FITTING FASTENER HOLE #3. CRACK IS IN THE INTERCOSTAL ONLY. REMOVED AND REPLACED R/H FR20 #1 DOOR STOP INTERCOASTAL IAW SRM 51-42-11. R5311 3118 FORM 44-0008 ATTACHED EMP# V935774 WORK AC COMPLISHED AT ST ENGINEERING A
- [SDR CALA2021120802303](https://openairdocs.org/sdr/CALA2021120802303.md): Stop Fitting · cracked · Dec 8, 2021 · N471UA · Airbus A320232 · Fuselage Main, Structure
  > CRACK FOUND IN THE RH FR20 #1 DOOR STOP FITTING FASTENER HOLE #3. CRACK IS IN THE INTERCOSTAL ONLY. REMOVED AND REPLACED R/H FR20 #1 DOOR STOP INTERCOASTAL IAW SRM 51-42-11. R5311 3118 FORM 44-0008 ATTACHED EMP# V935774 WORK AC COMPLISHED AT ST ENGINEERING A
- [SDR CALA2020011900164](https://openairdocs.org/sdr/CALA2020011900164.md): Skin · dented · Jan 15, 2020 · N471UA · Airbus A320232 · Leading Edge Devices
  > (SUPPORT TASK) L-23 NO DOT. LEFT WING NUMBER 2 SLAT HAS A DENT APPROX 8" O/B OF TRACK 5 AND 1" FWD OF STRINGER. NONROUTINE 9825786 ACCOMPLISHED REPAIR OF LEFT WING NUMBER 2 SLAT DENT APPROXIMATEL Y 8" O/B OF TRACK 5 AND 1" FWD OF STRINGER IAW SRM 57-40-00 -300
- [SDR CALA2020011300129](https://openairdocs.org/sdr/CALA2020011300129.md): Structure · corroded · Jan 10, 2020 · N471UA · Airbus A320232 · Emergency Exits
  > (A3NB-05-3-6164) LEFT AFT OVERWING HATCH HAS AREA OF CORROSION O N BOTTOM AFT LATCH FITTING ON INSIDE SURFACE. REMOVED AND REPLACED T-SECTION P/N D5227905420400 IAW A320 SRM 5 1-72-11-911-001, CMM 52-21-11-000-801-B01, ON LEFT AFT OVERWING HATCH AT BOTTOM AFT
- [SDR CALA2020011300128](https://openairdocs.org/sdr/CALA2020011300128.md): Rib · cracked · Jan 10, 2020 · N471UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK) AFT RIB CRACKED IN L/H AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED BEAM AND SEGMENT ON AFT END OF L/H AFT EMER GENCY EXIT HATCH IAW A320 SRM 51-72-11-911-001. DATA TRANSCRIBED FROM PAPER DOCUMENT AAR N/R: 9825233. WORK ACCOMPLISHED BNY MEC HA
- [SDR CALA2020011000112](https://openairdocs.org/sdr/CALA2020011000112.md): Gauge · stuck · Jan 7, 2020 · N471UA · Airbus A320232 · Passenger/Crew Doors
  > (SUPPORT TASK) REMOVE AND REPLACE THE AFT LEFT DOOR ASSIST BOTTL E ACTUATOR. REFER TO AAR N/R: 9825683. CHANGED DUE TO A STUCK GA UGE AFTER PRESSURE RELOADED. REMOVED AND REPLACED AFT LT DOOR ASSIST BOTTLE ACTUATOR IAW A320 AMM 52-13-14-000-001-B AND 52-13-14-
- [SDR CALA2020010600090](https://openairdocs.org/sdr/CALA2020010600090.md): Fitting · gouged · Jan 3, 2020 · N471UA · Airbus A320232 · Fuselage, Landing Gear Attach Fittings
  > AAR N/R S/N 9825822.(SUPPRT TASK) A44-030 LT MLG FWD ACTUATOR FI TTING STILL HAS GOUGE IN HOLE AFTER TAKING HOLE UP TO SECONDS OV ER NEEDS REPLACMENT REF EA 5330-04821 REV1 01 001. REMOVED AND REPLACED LH MLG FWD ACTUATOR FITTIN IAW A320 SRM 51- 72-11 AND AIRB
- [SDR CALA2020010600076](https://openairdocs.org/sdr/CALA2020010600076.md): Rib · cracked · Jan 2, 2020 · N471UA · Airbus A320232 · Emergency Exits
  > (SUPPORT TASK) A-30-007. FWD AND AFT RIBS CRACKED IN L/H FWD EME RGENCY EXIT HATCH. (MARKED) AAR NONROUTINE 9825235 REMOVED AND REPLACED FWD AND AFT RIBS AND SEGMENTS ON LH FWD EME RGENCY EXIT HATCH. IAW A320 SRM 51-72-11-911-001, RESTORED SURFA CE PROTECTION
- [SDR CALA2020010600007](https://openairdocs.org/sdr/CALA2020010600007.md): Rib · cracked · Dec 21, 2019 · N471UA · Airbus A320232 · Emergency Exits
  > AAR N/R S/N 9825234. SUPPORT TASK A-30-006, RIB CRACKED IN R/H F WD EMERGENCY EXIT HATCH.(MARKED) REMOVED AND REPLACED AFT BEAM AND SEGMENT ON R/H FWD EMERGENCY E XIT HATCH IAW A320 SRM 51-72-11-911-001
- [SDR CALA2019122102266](https://openairdocs.org/sdr/CALA2019122102266.md): Rib · dented · Dec 21, 2019 · N471UA · Airbus A320232 · Emergency Exits
  > RIGHT AFT OVERWING HATCH HAD DAMAGE ON THE RIB JUST BELOW PULL DOWN LEVER ON INSIDE OF HATCH. REMOVED AND REPLACED RIB IAW SRM 51-72-11.
- [SDR CALA2019122102265](https://openairdocs.org/sdr/CALA2019122102265.md): Rib · cracked · Dec 21, 2019 · N471UA · Airbus A320232 · Emergency Exits
  > FWD RIB CRACKED IN RT AFT EMERGENCY EXIT HATCH. REMOVED AND REPLACED FWD RIB ON THE RT AFT EMERGENCY EXIT HATCH IAW SRM 51-72-11.
- [SDR CALA2019032200453](https://openairdocs.org/sdr/CALA2019032200453.md): Landing Light · missing · Mar 21, 2019 · N471UA · Airbus A320232 · Exterior Lighting
  > PDA 2 LEFT LANDING LIGHT MISSING ON ARRIVAL PDA LOG CREATED BECAUSE OF LOGPAGE 9202691. CDL 33G DEFERAL NOT REQUIRED, ITEM CORRECTIVE ACTION DOCUMENTED REF LOG PAGE 9202718, 9202691. LOG TO DOCUMENT PDA ONLY. PDA REQUIREMENTS REFERENCED IN GMM 02-30-95 HAVE B
- [SDR CALA2017112104171](https://openairdocs.org/sdr/CALA2017112104171.md): Connector · damaged · Nov 21, 2017 · N471UA · Airbus A320232 · Light System Wiring
  > ROW 27ABC FLOOR EMERGENCY LIGHT INOPERATIVE. SECURED THE CONNECTOR PINS. ACCOMPLISHED AN OPERATIONAL CHECK IAW AMM 33 -51-00-710-009-A
- [SDR CALA2017042301123](https://openairdocs.org/sdr/CALA2017042301123.md): Strip · loose · Apr 23, 2017 · N471UA · Airbus A320232 · Passenger/Crew Doors
  > DOOR 1R WILL NOT ARM. FOUND RUBBER STRIP DISBONDED ON BOTTOM OF DOOR INTERFERING WITH GIRT BAR ACTION. RESECURED. OPS CHECKS NORMAL. VISUAL CHECK AND CONFIRMED SLIDE ARM AND DISARM NORMAL WITH REF TO AMM 25-62-44. SAFETY PIN REMOVED & STOWED. DOOR ASSIST REACT
- [SDR CALA2017013000218](https://openairdocs.org/sdr/CALA2017013000218.md): Battery · faulty · Jan 30, 2017 · N471UA · Airbus A320232 · Emergency Lighting
  > AFT LT EEL BATTERY FAILED CAPACITY TEST. REPLACED BATTERY REF AMM 33-51-38-000-002A AND 33-51-38-400-002A. OPS CHECKED OK

Next page: https://openairdocs.org/aircraft/N471UA/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 = 'N471UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N471UA/reports

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