# Service difficulty reports: N432UA

A list on [N432UA](https://openairdocs.org/aircraft/N432UA.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 4 · 176 reports

- [SDR CALA2026102120485](https://openairdocs.org/sdr/CALA2026102120485.md): Fuel Cap · missing · Oct 19, 2026 · N432UA · Airbus A320232 · Fuel Storage
  > CA REPORTED FUEL CAP MISSING. OK TO APPLY CDL 28A. CREW INSTALLED PLACARD. REPLACED THE FUEL CAP IAW AMM 28-25-41.
- [SDR CALA2026092919980](https://openairdocs.org/sdr/CALA2026092919980.md): Wire · damaged · Sep 27, 2026 · N432UA · Airbus A320232 · Light System Wiring
  > EMERGENCY LIGHT SEAT AT 34C INOPERATIVE. RESTORED WIRING TO ORIGINAL CONDITION IAW AMM 33-51-00- 2-C. EMERGENCY ESCAPE PATH LIGHT WORKS AT SEAT ROW 34 C. NO DEFECTS NOTED, ALL EMERGENCY LIGHTS OPE CHECKED GOOD.
- [SDR CALA2026070917625](https://openairdocs.org/sdr/CALA2026070917625.md): Unknown · odor · Jul 6, 2026 · N432UA · Airbus A320232 · Air Distribution System
  > FA SMELLED BURNED TOAST ODOR IN AFT GALLEY. INSPECTED AFT GALLEY AND CABIN FOR FUMES AND SIGNS OF SMOKE IAW AMM 05-51-10. NO SIGNS OF ODOR. RAN THE APU AND PACKS AND COULD NOT REPLICATE ODOR. INSPECTED THE 2001VU PANEL REF AMM 24-92-00. NO DAMAGE OR ODOR FOU
- [SDR CALA2026052016418](https://openairdocs.org/sdr/CALA2026052016418.md): Uplock · faulted · May 15, 2026 · N432UA · Airbus A320232 · Landing Gear Retraction/Extension System
  > MLG NOT UPLOCKED AFTER TAKEOFF, ECAM NO HELP PERFORMED BITE TEST OF LGCIU 1 AND 2. LGCIU 1 REPORTED FAULT "N LG UPLOCK (2530GM)/(2527GM)". PILOTS REPORTED CYCLING GEAR IN FLIGHT, NO HELP. FOUND BACKSHELL ON CONNECTOR IAW AMM 32-31-21/401 CONFIG 00 SHEET 2.
- [SDR CALA2025110610935](https://openairdocs.org/sdr/CALA2025110610935.md): Liner · unsecure · Nov 4, 2025 · N432UA · Airbus A320232 · Escape Slide
  > L1 DOOR ESCAPE SLIDE LOOSE LINING WAS CAUGHT BETWEEN DOOR. SECURED ESCAPE SLIDE LINING AT THE L1 DOOR IAW AMM 25-62-44.
- [SDR CALA2025070806318](https://openairdocs.org/sdr/CALA2025070806318.md): Battery · faulted · Jul 7, 2025 · N432UA · Airbus A320232 · Emergency Lighting
  > EMER LIGHT TEST FAILED. ESPU BATTERY EMER L AND EPSU BATTERY AFT L MESSAGES DISPLAYED. REPLACED EPSU BATTERIES AT 11WL AND 13WL. EMERGENCY LIGHTS OPS CHECK GOOD, NO FAULTS ON CIDS.
- [SDR CALA2025062705985](https://openairdocs.org/sdr/CALA2025062705985.md): Cids · faulted · Jun 24, 2025 · N432UA · Airbus A320232 · Communications System
  > ALL INTERCOM FUNCTIONS INOP INCLUDING EMERGENCY. REPLACED DEU B 300RH05. SYS CHECKS NORMAL REF AMM 23-73-47PARTS USED: 31-2300-9-0005, QTY:1 ROTABLE PARTS CHG:TT # 1761896 SN OFF 9762 PN OFF 31-2300-9-0005. UNIT, CIDS DECO OFF 31-2300-9-0005 9762 ON 31-2300-
- [SDR CALA2024101700852](https://openairdocs.org/sdr/CALA2024101700852.md): Computer · faulted · Oct 15, 2024 · N432UA · Airbus A320232 · Central Display
  > IN FLIGHT LOST MOSTNAV AND ATTITUDE INFOON CA PFD AND ND ANDENG 1 EPR/EGT/N1/N2/FF TECH SUPPORT UPDATE: DMC 1 FAULTS NOTED IN AVIATAR, ADDING DMC-1 (1WT1) TO PARTS FOR REPLACEMENT REF AMM. 31-63-34. REF 31-63-81-810-867-A REMOVED AND REPLACED #1 DMC 1WT1 REF M
- [SDR CALA2024053001639](https://openairdocs.org/sdr/CALA2024053001639.md): Compressor · stalled · May 27, 2024 · N432UA · Airbus A320232 · Turbine Engine Compressor Section
  > ESDR EVENTNO 1 COMP STALL ON FLXABORT AT 20KTSNO FIRE ALARM OBSERVERED METAL SHAVINGS IN THE TAIL PIPE. ESDR EVENTNO 1 COMP STALL ON FLXABORT AT 20KTSNO FIRE ALARM OBSERVERED METAL SHAVINGS IN THE TAIL PIPE.SDR# 1036353 GENERATED AND ENGINE CHANGE RECORDED ON
- [SDR CALA2024031500744](https://openairdocs.org/sdr/CALA2024031500744.md): Oven · odor · Mar 14, 2024 · N432UA · Airbus A320232 · Buffet/Galleys
  > CREW REPORTS DURING CLIMBOUT THE AFT GALLEY HAD A ELECTRICAL ODOR NOTICED BY THE FLT ATTENDANTS. LASTED A SHORT TIME AND DISIPATED. NO EQUIPMENT WAS NOTICED TO BE INOPERATIVE AND PASSENGERS DID NOT NOTICE DURING THIS INCIDENT, COMPLIED WITH TASK 05-51-10-200-8
- [SDR CALA2023120103516](https://openairdocs.org/sdr/CALA2023120103516.md): Fuel Cap · missing · Nov 27, 2023 · N432UA · Airbus A320232 · Fuel Storage
  > PDA 2 FUEL CAP FOUND MISSING UPON ARRIVAL TO ORD. COMPLIED W CDL REQUIREMENTS. NO DAMAGE TO COUPLER, STICKER APPLIED. CDL 28A COMPLIED WITH. OK TO APPLY CDL 28A.TOMC SMITH FUEL CAP NIS DEN CAP, COUPLING R OFF 0000 ON 31-2825-9-0001 7103 INSTALLED MISSING FUEL
- [SDR CALA2023010600034](https://openairdocs.org/sdr/CALA2023010600034.md): Door Latch · mislocated · Jan 6, 2023 · N432UA · Airbus A320232 · Cargo/Baggage Doors
  > FORWARD CARGO DOOR INDICATED OPEN ON TAKEOFF ROLL UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V903723 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003064678 AND PRTR OWENS, KEVIN (V903
- [SDR CALA2022102702957](https://openairdocs.org/sdr/CALA2022102702957.md): Window Frame · cracked · Oct 25, 2022 · N432UA · Airbus A320232 · Flight Compartment Windows
  > CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER NODE LH SIDE INTERNAL AREA INBOARD VERTICAL FLANGE FROM UPPER TENSION BOLT, CRACK DIRECTION IS 2 OCLOCK, CRACK LENGHT IS 0.140 INCH APPROX., CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT
- [SDR CALA2022102702947](https://openairdocs.org/sdr/CALA2022102702947.md): Pressure Blkhd · cracked · Oct 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Plate/Skin
  > CRACK INDICATION ON FR36LH PRESSURE PANEL IN OPEN FASTENER HOLES A AND B COMMON TO LONGITUDINAL BEAM Y1292, CONTACT PLANNING TO ASSIGN AND ACCOMPLISH EA 5330-05216 OP2 BEFORE NEXT FLIGHT IN FWD CARGO COMPARTMENT (2 EA). ED PART 1 INTERIM REPAIR ON AEROMAN NR#2
- [SDR CALA2022102702946](https://openairdocs.org/sdr/CALA2022102702946.md): Skin · cracked · Oct 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION ON FRAME 35 LOWER AND MOST AFT OPEN FASTENER HOLE AT ELEVEN OF STGR30LH, CRACK DIRECTIONS ARE 7 AND 11 OCLOCK IN FWD CARGO COMPARTMENT (1 EA). SEE AEROMAN NO ROUTINE 2022-393517. 4.750MM, HOLE DIAMETER WITH CRACK REMOVED 9.042MM AND FINAL FWD
- [SDR CALA2022102702940](https://openairdocs.org/sdr/CALA2022102702940.md): Fitting · elongated · Oct 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > ELONGATED HOLES R2, R3, R7, R8, R10, R12, R13, R14, R15, R16, R17, R19,R21, R74, R76, R78, R81, R83 AND R85 LOCATED KEEL BEAM AREA AT FR42 RH SIDE, ENGINEERING MUST BE CONTACTED. SEE AEROMAN NON ROUTINE 2022-394203 ACCOMPLISHED REPAIR INSTRUCTION FOR HOLES R2,
- [SDR CALA2022102402917](https://openairdocs.org/sdr/CALA2022102402917.md): None · cracked · Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Structure (General)
  > CRACK INDICATION FOUND AT FASTENER HOLE LOCATED AT FRAME 35 AND STR 30 RH SIDE AT FWD CARGO COMPARTMENT. CRACK DIRECTION IS 3 AND 9 OCLOCK APROX LOOKING AFT. CRACK DEPTH IS 0.055 INCHES APROX. REPAIR BEFORE FURTHER FLIGHT. SEE AEROMAN NON ROUTINE 2022-394074 B
- [SDR CALA2022102402920](https://openairdocs.org/sdr/CALA2022102402920.md): None · cracked · Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30
- [SDR CALA2022102402919](https://openairdocs.org/sdr/CALA2022102402919.md): None · none · Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > ELONGATED HOLES L1, L2, L3, L10, L12, L13, L14, L15, L18, L20, L75, L76,L77, L78, L82, L83, L84 AND L85 LOCATED ON KEEL BEAM AREA AT FR42 LH SIDE. ENGINEERING MUST BE CONTACTED. SEE AEROMAN NON ROUTINE 2022-394202 CATEGORY B. AND MUST BE ACCOMPLISH INSPECTION
- [SDR CALA2022102402922](https://openairdocs.org/sdr/CALA2022102402922.md): None · cracked · Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION ON FRAME 35 LOWER AND MOST AFT OPEN FASTENER HOLE AT LEVEN OF STGR30RH, CRACK DIRECTIONS ARE 6 AND 12 OCLOCK IN FWD CARGO COMPARTMENT (4 EA) SEE AEROMAN NON ROUTINE 2022-393519 ACCOMPLISHED INTERIM REPAIR PART 1 PER ECRA 5331-02971 ON HOLE #
- [SDR CALA2022102402921](https://openairdocs.org/sdr/CALA2022102402921.md): None · cracked · Oct 22, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > REPAIR FOR CRACK INDICATION FR36LH PRESSURE PANEL TOMC-APPROVAL FROM SC1ELBYC COMMENT FASTENER HOLES (#2-4, 8, 9, 13-17, 19-23, 26 AND 27), REF ECRA 5311-02905 PLANNING TO CONTACT ENGINEERING AFTER FEBRUARY 10,2023 BUT BEFORE MARCH 10, 2023 FOR THE PERMANENT O
- [SDR CALA2022100602702](https://openairdocs.org/sdr/CALA2022100602702.md): Frame · cracked · Oct 4, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPP
- [SDR CALA2022100602693](https://openairdocs.org/sdr/CALA2022100602693.md): Frame · cracked · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 43 FOOT COUPLING LH SIDE IN OPEN FASTE NER HOLE BTW STGR21 AND STGR22, CRACK DIRECTIONS ARE 3 AND 9 OCL OCK IN PASSENGER CABIN (1 EA). SEE AEROMAN NON-ROUTINE 2022-393 695. REPLACED FRAME FOOT COUPLING LOCATED ON FR43 LH SIDE IAW EA
- [SDR CALA2022100602691](https://openairdocs.org/sdr/CALA2022100602691.md): Frame · cracked · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4
- [SDR CALA2022100602692](https://openairdocs.org/sdr/CALA2022100602692.md): Stiffener · cracked · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON VERTICAL STIFFENER OF THE LATERAL WINDOW FRAME 4 RIGHT SIDE LENGTH APPROXIMATELY =0.278 INCHES SEE AEROMAN NON ROUTINE 2022-393434. INDICATION NOT FOUND IAW NTM 51-10-08. THIS REPAIR IS CATEGORY A AND RE-INSPECTION ARE NOT REQUIRED PE
- [SDR CALA2022100602690](https://openairdocs.org/sdr/CALA2022100602690.md): Floor Panel · corroded · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOOR BEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-00
- [SDR CALA2022100602689](https://openairdocs.org/sdr/CALA2022100602689.md): Floorbeam · corroded · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor Beam
  > CORROSION FLOOR BEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001
- [SDR CALA2022100602688](https://openairdocs.org/sdr/CALA2022100602688.md): Floorbeam · elongated · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor Beam
  > ELONGATED HOLE FLOOR BEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-393859 REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA PERFORMED SCEPTRE ENTRY ON LOG PAGE NUMBER IS:9289332 MEASURE OF IAW SRM A320 51-72-11-911
- [SDR CALA2022100602687](https://openairdocs.org/sdr/CALA2022100602687.md): Crossbeam · cracked · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV A
- [SDR CALA2022100302650](https://openairdocs.org/sdr/CALA2022100302650.md): Flange · cracked · Oct 3, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION ON FRAME 4 SIDE POST UPPER ATTACHMENT LH SIDE IN OPEN FASTENER HOLE IN VERTICAL FLANGE, CRACK DIRECTION IS 9 OCLOCK IN COCKPIT (1 EA) SEE AEROMAN NON ROUTINE 2022-393470 REWORKED AREA PER PART 2 OF THE LATEST REVISION OF EC/RA 5311- FRAME UPP
- [SDR CALA2022100302617](https://openairdocs.org/sdr/CALA2022100302617.md): Crossbeam · cracked · Oct 2, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H3 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393809 PERFORMED SCEPTRE ENTRY LOG PAGE NUMBER 9334409. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H3 FWD GALLEY AREA I.A.W. EA 531
- [SDR CALA2022100302616](https://openairdocs.org/sdr/CALA2022100302616.md): Crossbeam · cracked · Oct 2, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION FOUND ON CROSSBEAM AREA, FR16 RH SIDE; HOLE H4 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393810 TRE ENTRY LOG PAGE NUMBER 9334428. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H4 FWD GALLEY AREA I.A.W. EA 5310-06784 REV
- [SDR CALA2022100302615](https://openairdocs.org/sdr/CALA2022100302615.md): Floorbeam · elongated · Oct 2, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor Beam
  > ELONGATED HOLE FLOORBEAM -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA.SEE AEROMAN NON ROUTINE 2022-393856. INSTALLED NEW FLOOR BEAM Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, DWG #D53472201 AND DWG #D534722 00. PERFOMED SCPETRE ENTRY L
- [SDR CALA2022090902315](https://openairdocs.org/sdr/CALA2022090902315.md): None · none · Sep 9, 2022 · N432UA · Airbus A320232 · Aircraft Fuel Filter/Strainer
  > REMOVE AND REPLACE AIR RELEASE VALVE FLOAT RH WING (FIN 87QM) THIS NR FOR TRACKING PURPOSE ONLY. SEE AEROMAN NON ROUTINE 2022- 394222. REMOVED AIR RELEASE VALVE FLOAT RH WING (FIN 87QM) P/N: FRH2800 SEQ# 438. THIS NR FOR TRACKING PURPOSE ONLY 02 S/N:FRTR0421AM
- [SDR CALA2022082602178](https://openairdocs.org/sdr/CALA2022082602178.md): None · none · Aug 26, 2022 · N432UA · Airbus A300* · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON VERTICAL STIFFENER OF THE LATERAL WINDOW FRAME 4 RIGHT SIDE LENGTH APPROXIMATELY =0.278 INCHES SEE AEROMAN NON ROUTINE 2022-393434. INDICATION NOT FOUND IAW NTM 51-10-08. THIS REPAIR IS CATEGORY A AND RE-INSPECTION ARE NOT REQUIRED PE
- [SDR CALA2022082402160](https://openairdocs.org/sdr/CALA2022082402160.md): Crossbeam · cracked · Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Frame
  > CRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H2 FWD GALL EY AREA. SEE AEROMAN NON ROUTINE 2022-393808 TRE ENTRY LOG PAGE NUMBER 9334419. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H2 FWD GALLEY AREA I.A.W. EA 5310-06784 REV A
- [SDR CALA2022082402159](https://openairdocs.org/sdr/CALA2022082402159.md): Crossbeam · cracked · Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION FOUND ON CROSSBEAM AREA, FR16 RH SIDE; HOLE H4 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393810 TRE ENTRY LOG PAGE NUMBER 9334428. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H4 FWD GALLEY AREA I.A.W. EA 5310-06784 REV
- [SDR CALA2022082402158](https://openairdocs.org/sdr/CALA2022082402158.md): Crossbeam · cracked · Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CRACK INDICATION FOUND ON CROSSBEAM AREA FR16 RH SIDE HOLE H3 FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393809 PERFORMED SCEPTRE ENTRY LOG PAGE NUMBER 9334409. PERFOMED PERMANENT REPAIR ON CROSS BEAM AREA FR 16 RH SIDE HOLE H3 FWD GALLEY AREA I.A.W. EA 531
- [SDR CALA2022082402157](https://openairdocs.org/sdr/CALA2022082402157.md): Floorbeam · elongated · Aug 24, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor Beam
  > ELONGATED HOLE FLOOR BEAM -Y1292 LOC. FR64 TO FR66 AT AFT GALLEY AREA.SEE AEROMAN NON ROUTINE 2022-393856. INSTALLED NEW FLOOR BEAM Y1292 LOC FR64 TO FR 66 AT AFT GALLEY AREA I.A.W. A320 SRM 51-42-11, DWG #D53472201 AND DWG #D534722 00. PERFOMED SCPETRE ENTRY
- [SDR CALA2022081902119](https://openairdocs.org/sdr/CALA2022081902119.md): Frame · cracked · Aug 19, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30
- [SDR CALA2022081902118](https://openairdocs.org/sdr/CALA2022081902118.md): Frame · cracked · Aug 19, 2022 · N432UA · Airbus A320232 · Fuselage, Wing Attach Fittings
  > CRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4
- [SDR CALA2022081602073](https://openairdocs.org/sdr/CALA2022081602073.md): Floorbeam · elongated · Aug 16, 2022 · N432UA · Airbus A320232 · Fuselage Main, Floor Beam
  > ELONGATED HOLE FLOORBEAM -Y765 BTW FR64 TO FR66 AT AFT GALLEY AREA. REPLACED FLOOR BEAM-Y765 LOC BTW FR64 TO FR66 AT AFT GALLEY AREA.
- [SDR CALA2022081002032](https://openairdocs.org/sdr/CALA2022081002032.md): Dummy Rail · corroded · Aug 9, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA
- [SDR CALA2022080501974](https://openairdocs.org/sdr/CALA2022080501974.md): Floorbeam · corroded · Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM -Y1292 LOC. BTW 12 TO FR24 IN PASSENGER CAB IN. SEE AEROMAN NON ROUTINE 2022-393811 REPLACED FLOOR BEAM -Y1292 LOC. BTW FR.12 FR.24 IN PASS CABIN OF CORROSION ARE: L=3.615 IN, W=1.212 IN, D=0.086 IN, TOOL USED IAW A320 SRM 51-72-11-911-001
- [SDR CALA2022080501973](https://openairdocs.org/sdr/CALA2022080501973.md): Dummy Rail · corroded · Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION RAIL DUMMY -Y81 AT FWD GALLEY AREA. SEE AEROMAN NON ROUTINE 2022-393815 REPLACED RAIL DUMMY -Y81 AT FWD GALLEY AREA IAW A320 SRM L=2.820 IN, W=2.017IN, D=0.116 IN, TOOL USED: CALIPER P/N: 51-72-11-911-001 AND DRAWING D53110984, PERFORMED DVI ON AREA
- [SDR CALA2022080501972](https://openairdocs.org/sdr/CALA2022080501972.md): Floorbeam · corroded · Aug 5, 2022 · N432UA · Airbus A320232 · Fuselage Floor Panel
  > CORROSION FLOORBEAM -Y765 LOC. BTW FR12 TO FR24 IN PASSENGER CABIN. SEE AEROMAN NON ROUTINE 2022-393813 REPLACED FLOORBEAM -Y765 LOC BTW FR.12 TO FR.14 IN PASSENGER MEASURE OF CORROSION ARE L=4.125 IN, W=1.217 IN, D=0.083IN, CABIN IAW A320 SRM 51-72-11-911-001
- [SDR CALA2019112542058](https://openairdocs.org/sdr/CALA2019112542058.md): Power Supply · failed · Nov 23, 2019 · N432UA · Airbus A320232 · Emergency Lighting
  > CIDS TEST FAILED. MSGS "EPSU EXT LOAD FWD L" REPLACED EPSU P/N 3214-54-10 AND EPSU BATTERY P/N AD3214-31. ORIGINAL MESSAGE GONE. NEW MESSAGE EPSU EXT LOAD FWD L PRESENT. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1104555 SN OFF 8398 POWER SUPPLY, C OFF 31-335
- [SDR CALA2018070301554](https://openairdocs.org/sdr/CALA2018070301554.md): Wire Harness · damaged · Jun 30, 2018 · N432UA · Airbus A320232 · Light System Wiring
  > EEPL HARNESS ROWS 29-31 DAMAGED. REMOVED AND REPLACED EEPL CABLE AT SEAT ROW 29-31 IAW AMM 33-51-22-400-802C1.
- [SDR CALA2018071001580](https://openairdocs.org/sdr/CALA2018071001580.md): Intercostal · cracked · Jun 25, 2018 · N432UA · Airbus A320232 · Fuselage Miscellaneous Structure
  > RT FWD PAX DOOR NR 1 DOOR STOP FITTING LOWER I/B FASTENER HOLE HAS CRACK INDICATION. REMOVED NR 1 DOOR STOP FITTING, REMOVED AND REPLACED DAMAGED INTERCOSTAL AT RT FWD PAX DOOR FR16 IAW ECRA 5311-01961, INSTALLED NR 1 DOOR STOP FITTING IAW AMM 52-11-31-000-002
- [SDR CALA2018070301558](https://openairdocs.org/sdr/CALA2018070301558.md): Beam · corroded · Jun 22, 2018 · N432UA · Airbus A320232 · Fuselage Main, Structure
  > LT AFT EMERGENCY EXIT DOOR CUTOUT. LOWER SURFACE BETWEEN THE LATCHES FOUND CORRODED AFTER CHECKING MATING SURFACE OF CORRODED HATCH. REMOVED CORRODED BEAM AT LT AFT EMERGENCY EXIT DOOR LOWER BEAM. MATCH DRILLED NEW BEAM AND INSTALLED NEW BEAM RESTORED SURFACE

Next page: https://openairdocs.org/aircraft/N432UA/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 = 'N432UA' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N432UA/reports

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