# Service difficulty reports: Airbus A320-232

A list on [Airbus A320-232](https://openairdocs.org/model/airbus-a320-232.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 653 · 32,613 reports

- [SDR YENA2026102200991](https://openairdocs.org/sdr/YENA2026102200991.md): Unknown · odor · Oct 21, 2026 · N640JB · Airbus A320232 · Air Distribution System
  > FLT#1161, LGA-DJT. AFTER DESCENDING THROUGH 4,000 FEET, F3/F4 COMPLAINED OF AN ODOR EVENT INCLUDING BURNING EYES AND HEADACHE CONCENTRATED IN THE AFT CABIN.; COMPLIED WITH INFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 1. ACCOMPLISHED DE-CONTAMIN
- [SDR AALA202610231336](https://openairdocs.org/sdr/AALA202610231336.md): Bottle · low pressure · Oct 20, 2026 · N649AW · Airbus A320232 · Passenger/Crew Doors
  > AIRCRAFT WAS NOT GROUNDED: L1 PASSENGER DOOR ASSIST BOTTLE PRESSURE REQUIRES SERVICING. MAINTENANCE SERVICED LEFT ONE PASSENGER DOOR ASSIST BOTTLE. LEAK CHECK PERFORMED. NO DEFECT NOTED. REFERENCE AMM 52-10-00
- [SDR CALA2026102220530](https://openairdocs.org/sdr/CALA2026102220530.md): Plate · corroded · Oct 20, 2026 · N438UA · Airbus A320232 · Fuselage Main, Structure
  > AFT CARGO BAY, AFT LAV EXHAUST VENT BETWEEN FR 69 & FR 70, STR 30R - 33R HAD CORROSION ON LOWER, INBD SIDE AT CONTACT POINT OF VENT OUTLET & AIRFRAME. R & R THE PLATE, FR 69-70 S30-33R IAW SRM 53-41-00-210 -030-C1, SRM 53-41-11-283-065, & SRM 51-72-11-911-001
- [SDR CALA2026102220520](https://openairdocs.org/sdr/CALA2026102220520.md): Sign · missing · Oct 20, 2026 · N438UA · Airbus A320232 · Emergency Lighting
  > MAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCH (4EA, FWD AND AFT) ARE NOT INSTALLED. INSTALLED MAIN CABIN EMERGENCY EXIT IDENTIFIERS AT THE LT & RT OVERWING HATCHES FWD AND AFT IAW AMM 33-51-13-400-001-A OPS CHECK GOOD IAW AMM 33-51-13-4
- [SDR AALA202610230169](https://openairdocs.org/sdr/AALA202610230169.md): Release Pin · out of position · Oct 19, 2026 · N679AW · Airbus A320232 · Emergency Exits
  > AIRCRAFT IN BASE MAINTENANCE: RIGHT OVERWING EMERGENCY EXITS SPRING LOADED RELEASE PINS ARE BOUND IN ARMED POSITION. MAINTENANCE PERFORMED UNLOAD RELEASE PINS AT RIGHT OVERWING EMERGENCY EXIT DOORS THAT WERE BOUNDED IN ARMED POSITION PER AMM 52-21-11-000-001-A
- [SDR AALA202610238487](https://openairdocs.org/sdr/AALA202610238487.md): Light · no test · Oct 19, 2026 · N679AW · Airbus A320232 · Emergency Lighting
  > AIRCRAFT IN BASE MAINTENANCE: DURING EMPERGENCY POWER SUPPLY UNIT TEST PER AMM 33-51-00-710-001 FAULT ATA 33-51-38 EMPERGENCY POWER SUPPLY UNIT INT LOAD EMERGENCY RIGHT, EMER LEFT, AFT LEFT AND EMPERGENCY POWER SUPPLY UNIT INT LOAD FORWARD LEFT IS SHOWN. MAINT
- [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 YENA2026101900988](https://openairdocs.org/sdr/YENA2026101900988.md): Warning Message · illuminated · Oct 17, 2026 · N612JB · Airbus A320232 · Landing Gear Retraction/Extension System
  > FLT#773, BOS-AUA-RTF. ON GEAR RETRACTION WE GOT ECAM L/G DOORS NOT CLOSED. ECAM TOLD US TO CYCLE THE GEAR BELOW 220 KTS, WE STILL HAD 1 FLAP AND APP 190 KTS, CYCLED ONCE MSG STILL THERE. DROPPED THE GEAR TO MAKE SURE IT STILL CAME DOWN. LEFT IT DOWN AND RETURN
- [SDR CALA2026101920441](https://openairdocs.org/sdr/CALA2026101920441.md): Battery Pack · faulted · Oct 16, 2026 · N465UA · Airbus A320232 · Emergency Lighting
  > DURING EMERGENCY LIGHT TEST, RECIEVED FAULT EPSU BATTERY WARNING. VERIFIED BATTERY FAULT ON EPSU 12WL SELF TEST IAW AMM 33-51-38, R & R THE BATTERY PACK, OP CHKD GOOD IAW AMM 33-51-38.
- [SDR CALA2026101520399](https://openairdocs.org/sdr/CALA2026101520399.md): Cover · broken · Oct 14, 2026 · N431UA · Airbus A320232 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 20C BROKEN, IAW AMM 33-51-18 REPLACED THE COVER. LIGHT OPERATIONAL.
- [SDR YENA2026101600982](https://openairdocs.org/sdr/YENA2026101600982.md): Engine · shutdown · Oct 13, 2026 · N593JB · Airbus A320232 · Engine (Turbine/Turboprop)
  > FLT 600, MSY-BOS (ENGINE SHUTDOWN). ENG 1, AUTO SHUTDOWN ON DESCENT. R & R NR 1 ENG IAW TASK CARD A320-71-00-20-400-040, OPS & LEAK CHKD GOOD. INSTALLED CRANK PAD, COVER PAD & HPC BORO PORTS A THRU G IAW EMM 72-00-00. INSTALLED HPT BORO PLUG T1/2L & EMM 7
- [SDR CALA2026101320323](https://openairdocs.org/sdr/CALA2026101320323.md): Lavatory · odor · Oct 12, 2026 · N452UA · Airbus A320232 · Waste Disposal System
  > FORWARD LAV - TOXIC ODOR WITH A YELLOWISH FLUID LEAKING OVER THE FLOOR INSPECTED LAVATORY FOR ANY LEAKS. NO LEAKS FOUND IAW AMM 25-40-00. LIQUID ON FLOOR LOOKED TO BE SPILLED VINEGAR.
- [SDR YENA2026101500980](https://openairdocs.org/sdr/YENA2026101500980.md): Stiffener · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Miscellaneous Structure
  > DURING HEAVY MAINTENANCE, ACCOMPLISH THE PERMANENT REPAIR TO CRACK DAMAGES ON VERTICAL STIFFENERS Y254 (POSITIVE AND NEGATIVE), Y765 (POSITIVE AND NEGATIVE), Y1292 (POSITIVE & NEGATIVE) AT FRONT SPAR OF THE CENTER WING IAW AEROMAN EA 57-0080-26 (COVER AND PAR
- [SDR YENA2026101500979](https://openairdocs.org/sdr/YENA2026101500979.md): Frame · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450767. CRACK INDICATION FOUND ON FASTENER HOLE (AFT-LOWER POSITION) LOCATED AT FR35 AT LEVEL OF STR30 LH SIDE, LOWER FUSELAGE. CRACK DEPTH = 0.156 INCHES APPROX, CRACK POSITION: 6 AND 12 OCLOCK LO
- [SDR YENA2026101500978](https://openairdocs.org/sdr/YENA2026101500978.md): Pressure Blkhd · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450769. CRACK INDICATION FOUND ON FR35 LH SIDE FWD FACE TO PRESSURE BULKHEAD FASTENER HOLE LOCATED AT LEVEL OF 1.5 INCH BELOW OF STR 30LH. CRACK DEPTH: 0.167 INCHES APPROX. CRACK POSITION: 9 AND 3
- [SDR YENA2026101500977](https://openairdocs.org/sdr/YENA2026101500977.md): Frame · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450712. CRACK INDICATION ON FRAME 16 RH SIDE IN OPEN FASTENER HOLE 6, CRACK DIRECTION IS 10 O'CLOCK, CRACK DEPTH IS 0.110 INCH, AT FWD GALLEY AREA (1 EA); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-
- [SDR YENA2026101500976](https://openairdocs.org/sdr/YENA2026101500976.md): Pressure Deck · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450766. CRACK INDICATION FOUND ON FASTENER HOLE #4 OF FR 36 PRESSURE DECK MEMBRANE LOCATED AT Y1292. CRACK DIRECTION 10 O'CLOCK LOOKING AFT. CRACK D= 0.163 INCHES.; "(RESOLVED ON W/O: 1486589 TASKC
- [SDR YENA2026101500975](https://openairdocs.org/sdr/YENA2026101500975.md): Pressure Deck · cracked · Oct 11, 2026 · N558JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450764. CRACK INDICATION FOUND ON FASTENER HOLE #7 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT Y1292. CRACK DIRECTION 11 O'CLOCK LOOKING AFT. CRACK D= 0.140 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCA
- [SDR YENA2026101500974](https://openairdocs.org/sdr/YENA2026101500974.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450763. CRACK INDICATION FOUND ON FASTENER HOLE #5 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 12 O'CLOCK LOOKING AFT. CRACK D = 0.172 INCHES.; "(RESOLVED ON W/O: 1486589 TASK
- [SDR YENA2026101500973](https://openairdocs.org/sdr/YENA2026101500973.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450762. CRACK INDICATION FOUND ON FASTENER HOLE #6 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 1 O'CLOCK LOOKING AFT. CRACK D= 0.145 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCA
- [SDR YENA2026101500972](https://openairdocs.org/sdr/YENA2026101500972.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450761. CRACK INDICATION FOUND ON FASTENER HOLE #7 OF FR36 PRESSURE DECK MEMBRANE LOCATED AT -Y1292. CRACK DIRECTION 6 O'CLOCK LOOKING AFT. CRACK D= 0.141 INCHES;"(RESOLVED ON W/O: 1486589 TASKCARD
- [SDR YENA2026101500971](https://openairdocs.org/sdr/YENA2026101500971.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450562. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 7 ( CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00043) REF AEROMAN WO# 2026-228/1. NR# 2026-450562. ACCOMPLI
- [SDR YENA2026101500970](https://openairdocs.org/sdr/YENA2026101500970.md): Skin · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, WEIGHT VARIANT UPGRADE FOR A/C N558JB - SRM REPAIR SURVEY, DEFECT 4400 62-29919; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00047) REF AEROMAN WO 2026-228/1 NR # 2026-450636 COMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER
- [SDR YENA2026101500969](https://openairdocs.org/sdr/YENA2026101500969.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00049) REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SK
- [SDR YENA2026101500968](https://openairdocs.org/sdr/YENA2026101500968.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00050) REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWE
- [SDR YENA2026101500967](https://openairdocs.org/sdr/YENA2026101500967.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00051) REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH
- [SDR YENA2026101500966](https://openairdocs.org/sdr/YENA2026101500966.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450569. CORROSION ON RH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 13 PLUS 3 INCHES. (CPCP FINDING).; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00052) REF AEROMAN WO# 2026-228/1. NR# 2026-45
- [SDR YENA2026101500965](https://openairdocs.org/sdr/YENA2026101500965.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00053) REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKI
- [SDR YENA2026101500964](https://openairdocs.org/sdr/YENA2026101500964.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, REF AEROMAN WO# 2026-228/1. NR# 2026-450551. CORROSION ON LH WING TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 PLUS 16 INCHES.; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00054) REF AEROMAN WO# 2026-228/1. NR# 2026-450551. ACCOMPLISH
- [SDR YENA2026101500963](https://openairdocs.org/sdr/YENA2026101500963.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Leading Edge Devices
  > DURING HEAVY MAINTENANCE, CORROSION ON SLAT 1 UPPER SURFACE ON LH WING; "(RESOLVED ON W/O: 1486589 TASKCARD: NR-00055) REF AEROMAN WO 2026 228/1 NR 2026-450462. REPAIRED SLAT 1 UPPER SURFACE ON LH WING IAW EC NO. A26-840-01, EA # 57-0089-26 REV 0 AND # 57-008
- [SDR YENA2026101500962](https://openairdocs.org/sdr/YENA2026101500962.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 ON LH WING ( CPCP FINDING); "REF AEROMAN 2026 228/1 NR2026-450552 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROMAN E
- [SDR YENA2026101500961](https://openairdocs.org/sdr/YENA2026101500961.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 17 PLUS 16 INCH ES LH WING (CPCP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450566 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORD
- [SDR YENA2026101500960](https://openairdocs.org/sdr/YENA2026101500960.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 10 LH WING (CP CP FINDING); "REF AEROMAN WO # 2026-228/1 NR # 2026-450544 ACOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TEOH LOWER SURFACE RIB 9-18 IN ACCORDANCE WITH AEROM
- [SDR YENA2026101500959](https://openairdocs.org/sdr/YENA2026101500959.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, CORROSION TOP SKIN OVERHANG LOWER SURFACE AT LEVEL RIB 11 PLUS 17 INCH ES LH WING (CPCP FINDING; REF AEROMAN WO # 2026-228/1 NR # 2026-450553 ACCOMPLISHED REPAIR OF THE LH WING TOP SKIN PANEL 2 TE OH LOWER SURFACE RIB 9-18 IN ACCORDAN
- [SDR YENA2026101500958](https://openairdocs.org/sdr/YENA2026101500958.md): Skin · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, EA A26-876-01 WING / LH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 9-18 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500957](https://openairdocs.org/sdr/YENA2026101500957.md): Pressure Deck · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, EA A26-816-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 LHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500956](https://openairdocs.org/sdr/YENA2026101500956.md): Frame · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Frame
  > DURING HEAVY MAINTENANCE, EA A26-843-01 FUSELAGE / NOSE FWD FUSELAGE / FR16 RHS / DOUBLE JOGGLE AREA / HOLE #6 / CRACK DAMAGE – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500955](https://openairdocs.org/sdr/YENA2026101500955.md): Pressure Blkhd · damaged · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Bulkhead
  > DURING HEAVY MAINTENANCE, EA A26-842-01 FUSELAGE / CENTER FUSELAGE / FR35 FWD FACE TO PRESSURE BULKHEAD ATTACHMENT / @ LEVEL OF STGR 30LH / FASTENER HOLES W1 & H2 / CRACK DAMAGE – TIME LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500954](https://openairdocs.org/sdr/YENA2026101500954.md): Skin · corroded · Oct 11, 2026 · N588JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, EA 26-872-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 13 / CORROSION - PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500953](https://openairdocs.org/sdr/YENA2026101500953.md): Floorbeam · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Floor Beam
  > DURING HEAVY MAINTENANCE, EA 26-807-01 WINGS / CENTER WING / FRONT SPAR / VERTICAL STRINGERS & HORIZONTAL FLOOR BEAMS / Y±254, Y±765, AND Y±1292 / AT FR36 / CRACKS (SB 57-1178) – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500952](https://openairdocs.org/sdr/YENA2026101500952.md): Pressure Panel · cracked · Oct 11, 2026 · N588JB · Airbus A320232 · Fuselage Main, Structure
  > DURING HEAVY MAINTENANCE, EA 26-817-01 FUSELAGE / CENTER FUSELAGE / PRESSURE DECK PANEL / FR36 RHS / ATTACHMENT HOLES / CRACKS – PERMANENT REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101500951](https://openairdocs.org/sdr/YENA2026101500951.md): Skin · corroded · Oct 11, 2026 · N558JB · Airbus A320232 · Wing, Plate/Skin
  > DURING HEAVY MAINTENANCE, EA 26-873-01 WING / RH WING / TOP SKIN PANEL #2 / TEOH LWR SURFACE / RIB 7 AND 13 / CORROSION - TIME-LIMITED REPAIR (CONSIDERED A MAJOR REPAIR)
- [SDR YENA2026101200947](https://openairdocs.org/sdr/YENA2026101200947.md): A/C Pack · odor · Oct 11, 2026 · N794JB · Airbus A320232 · Cabin Cooling System
  > FLT#751, BOS-MCO. MAGIC MARKER SMELL IN DECENT ISOLATED TO PACK. PACK BURN, NO ODOR NOTED AT THIS TIME A/C OK FOR SVC.
- [SDR YENA2026101200945](https://openairdocs.org/sdr/YENA2026101200945.md): Switch · faulted · Oct 11, 2026 · N715JB · Airbus A320232 · Light System Wiring
  > FLT#2751, TPA-SJU. EMERGENCY LIGHT DOES NOT WORK IN NORMAL CONFIG; R/R NO SMOKE SIGN TOGGLESWITCH. AS PER ESPM 20-45-21. OPS CK OK AS PER AMM 33-51-00.
- [SDR YENA2026101200942](https://openairdocs.org/sdr/YENA2026101200942.md): Control Servo · malfunctioned · Oct 10, 2026 · N508JL · Airbus A320232 · Flight Control System
  > FLT#789, DTW-FLL. DURING CLIMB NOTICED A SMALL AMOUNT OF FWD STICK ABOUT 1/4" REQUIRED TO FOLLOW FLIGHT DIRECTORS(NOSE WANTED TO PITCH UP) CONTINUED FOR 30 MINS AFTER TOC & WENT AWAY UNTIL DESCENT, RETURNED & WAS PRESENT FOR DURATION OF FLT. ACFT COMPLETELY CO
- [SDR CALA2026101220279](https://openairdocs.org/sdr/CALA2026101220279.md): Display · faulted · Oct 10, 2026 · N430UA · Airbus A320232 · Central Display
  > CAPTAINS PFD FAILED AT ROTATION SCREEN CAME ALIVE UPONLANDING. REMOVED AND REPLACED CAPT PFD AND RELAY 20WT1. OPS CHECK NORMAL IAW AMM 31-63-22-400-001-A.
- [SDR CALA2026101220263](https://openairdocs.org/sdr/CALA2026101220263.md): None · no discrepancy · Oct 10, 2026 · N436UA · Airbus A320232 · Standard Practices/Structures
  > BIRD STRIKE DURING TAKEOFF ROLL APPROX 145 KTS. SEEMED ISOLATED TO FRONT LEFT NOSE/FUSELAGE. DEBRIEFED CREW. ACFT WAS IN TAKE-OFF CONFIGURATION DURING TAKE-OFF ROLL. NO ABNORMAL ENGINE INDICATIONS. NO ODOR IN THE AIR CONDITIONING. RADIOS AND NAVIGATION OPERA
- [SDR YENA2026100900935](https://openairdocs.org/sdr/YENA2026100900935.md): Unknown · odor · Oct 9, 2026 · N648JB · Airbus A320232 · Air Distribution System
  > FLT#2695, HPN-MCO. ONE INFLIGHT REPORTED STRONG DIRTY SOCKS SMELL IN AFT GALLEY THRU ROW 22. WHEN CABIN TEMP CONTROLLERS MOVED BACK TO MAX COLD AFTER 10 MINS, NO ODOR OBSERVED. AIRCRAFT IN CRUISE FLIGHT LEVEL 1 EVENT.
- [SDR CALA2026100920256](https://openairdocs.org/sdr/CALA2026100920256.md): Battery Pack · no test · Oct 7, 2026 · N480UA · Airbus A320232 · Emergency Lighting
  > RAN EMERGENCY LIGHT BATTERY TEST. EPSU LOCATED IN FWD LT. REPLACED EPSU BATTERY IAW AMM 33-51-38-400-002-A.
- [SDR AALA202610081173](https://openairdocs.org/sdr/AALA202610081173.md): Door · out of adjust · Oct 6, 2026 · N680AW · Airbus A320232 · Fixed Inner Doors
  > AIRCRAFT WAS NOT GROUNDED: FLIGHT DECK DOOR UNACCEPTABLY DIFFICULT TO OPEN AND CLOSE. DOOR CATCHES AND GETS STUCK ON STRIKE PLATE BEFORE ABLE TO CLOSE AND LATCH OR OPEN BACK UP. MAINTENANCE FOUND MEASUREMENT LEFT FOR COCKPIT DOOR OUT OF LIMIT, ADJUSTED FLIGHT

Next page: https://openairdocs.org/model/airbus-a320-232/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 aircraft_model_key = 'A320232'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/airbus-a320-232/reports

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