Airbus A320-232

Service difficulty reports · 32,653

Newest first. General aviation reporting is voluntary.

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 aircraft_model_key = 'A320232'
  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 GTIA2024091338368Control Lever · malfunctionedAFTER TAKEOFF COULD NOT GET THE LANDING GEAR HANDLE TO RETRACT POSITION. LANDED UNDER MAX LDG WEIGHT.-AFTER TROUBLESHOOTING FOUND THE LANDING GEAR CONTROL LEVER NOT RELEASING TO THE UP POSITION. R&R L/G CONTROL LEVER IAW AMM 32-31-11. OPS CHECK GOOD.Sep 10, 2024 · N634NK · Airbus A320232 · Landing Gear SelectorSDR AALA202409120007Connector · disconnectedAIRCRAFT WAS GROUNDED: DURING PS CHECK FOUND WHITE SEAT-MOUNTED EMERGENCY AISEL LIGHT LH ROW 19 INOP. REPLACED SEAT EMERG LIGHT ASSY AND TERMINAL 3 CONNECTOR AT 19 LH, OPS CHECK NORMAL IAW AMM 33-51-19.Sep 10, 2024 · N647AW · Airbus A320232 · Light System WiringSDR YENA2024091101263Oil System · leakingFLT#580, MBJ-JFK. (AIRCRAFT PERFORMED AN AIR TURN BACK TO MBJ) 'LOW OIL QTY AFTER #1 TAKE OFF 4 SQT 7QT ON DOWN WIND 12 QT AFTER GATE; INSP # 1 ENG FOR AC7NE OIL LEAK IAW AMM 79-00-00 NO LEAK NOTED. SVC #1 ENG OIL IAW AM 12-13-79 AS PRECAUTION CREW PERFORMED ESep 10, 2024 · N763JB · Airbus A320232 · Turbine Engine Oil SystemSDR YENA2024091101261Slide · no testFLT#40, MDE-FLL. 'REF. LOGPAGE 4059972 ITEM #1. FWD EPSU INTERIOR / EXTERIOR LIGHT FAULT; PERFORMED TSM TASK 33-51-00-810-808-A. REPLACED FWD R/H ESCAPE SLIDE PER M/M 25-62-44. OPS CHECK GOOD OF EPSU 10WL PER M/M 33-51-00.'Sep 9, 2024 · N623JB · Airbus A320232 · Escape SlideSDR YENA2024091101260Slide · no testFLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 10 WL NEEDS REPLACEMENT; REPLACED EMERGENCY BATTERY ON FIN 10WL IN REF TO AMM 33-51-8 TEST FAILED P/N TRANS C/W UNDER W.O # 1358429 FURTHER T/S REQUIRED.'Sep 9, 2024 · N623JB · Airbus A320232 · Escape SlideSDR YENA2024091101259Slide · no testFLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST & LP 4059972-1 (REFERRED TO LOG PAGE 4059975-1 FOR R/R R1 SLIDE & LOGPAGE 4059975-2 (PERFORMED TSM, TASK 33-51-00-310-808-A, REPLACED AFT L/H L2 ESCAPE SLIDE PER AMM 25-62-44 OPS CHSep 9, 2024 · N623JB · Airbus A320232 · Escape SlideSDR YENA2024091101258Landing Gear · malfunctionedFLT#365, BOS- RSW.' (AIRCRAFT DECLARED AN EMERGENCY AND PERFORMED AN AIR TURN BACK TO BOS). 'AFTER T/O: L/G NOT UPLOCKED WHEELS SD PAGE INDICATED AMBER " L/G CTRL" GEAR DID NOT RETRACT; TS PER TSM 32-31-00-810-808-A REPLACED RELAY 62GA PERFORMED MULTIPLE EXTENSep 9, 2024 · N746JB · Airbus A320232 · Landing Gear Retraction/Extension SystemSDR YENA2024091101256Slide · no testFLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 11WL NEEDS REPLACEMENT; REPLACED EMERGENCY BATTERY ON FIN 11WL IN REF TO AMM 33-51-38 TEST OK P/N TRANS C/W UNDER W.O 1358429.'Sep 9, 2024 · N623JB · Airbus A320232 · Escape SlideSDR YENA2024091101255Slide Raft · no testFLT#40, MDE-FLL. 'WHILE PERFORMING TASK # A320-33-51-00-710-003 CHECK OF EMERGENCY BATTERY CHK FOUND AFT & FWD EPSU INTERIOR,EXTERIOR LIGHT FAULT; REFERED TO LOG PAGE 4059975-1 FOR REMOVED AND REPLACED R1 SLIDE & LOGPAGE 4059975-2 (PERFORMED TSM, TASK 33-51-00Sep 9, 2024 · N623JB · Airbus A320232 · Escape SlideSDR YENA2024091101254Battery · no testFLT#40, MDE-FLL. 'REF TASK CARD # A320-33-51-00-710-003 EMERGENCY BATTERY TEST FIN 12WL NEEDS REPLACED; REPLACED EMERGENCY BATTERY ON FIN 12WL IN REF TO AMM 33-51-38 TEST OK P/N TRANS C/W UNDER WO # 1358429.'Sep 9, 2024 · N623JB · Airbus A320232 · Emergency LightingSDR AALA202409112375Attach Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT SLAT TRACK 3 (FORWARD BOLT) ON LEFT-HAND WING. REPLACED BOLT PER JOB CARD 26C51057005.Sep 9, 2024 · N604AW · Airbus A320232 · Leading Edge DevicesSDR YENA2024091001250Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 LH DOOR STOP FITTING 7 UPPER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00014) REF AEROMAN WO: 2024 253/1 WCC# 2024-501345. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FISep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001249Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 LH DOOR STOP FITTING 7 LOWER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00015) REF AEROMAN WO: 2024 253/1 WCC# 2024-501346. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 LH DOOR STOP FISep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001248Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 RH DOOR STOP FITTING 7 LOWER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00016) REF AEROMAN WO: 2024 253/1 WCC# 2024-501347. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FISep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001247Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR.16 RH DOOR STOP FITTING 7 UPPER I/B HOLE; (RESOLVED ON W/O: 1321520 TASKCARD: NR-00017) REF AEROMAN WO: 2024 253/1 WCC# 2024-501348. PERFORMED REPAIR INTERCOSTAL FITTING LOC. AT LEVEL FR.16 RH DOOR STOP FISep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001246Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENT 1 (FWD AND AFT) OF THE E MERGENCY EXIT HATCH DOOR 843 . FWD RH SIDE. CRACK LENGTH = 0.152 INCH APROX; REF: ARM W/O 2024 253/1 N/R 2024-501289 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXSep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001245Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 833 FWD LH SIDE. CRACK LENGTH = 0.177 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501290 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXSep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001244Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 834 AFT LH SIDE. CRACK LENGTH = 0.164 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501291 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXSep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001243Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON INNER FRAME SEGMENTS 1, (FWD AND AFT) OF THE EMERGENCY EXIT HATCH DOOR 844 AFT RH SIDE. CRACK LENGTH = 0.100 INCH A PROX; REF: ARM W/O 2024 253/1 N/R 2024-501292 PERFORMED EC A320-52-1144 DOORS / EMERGENCY EXSep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001242Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON FRAME 35 PRESSURE BULKHEAD FWD FACE LH SIDE, FROM LOWER OUTBOARD FASTENER AT LEVEL OF STGR30, CRACK LENGTH IS 0.095 INC H APROX, IN FWD CARGO COMPARTMENT (1 EA); REF AEROMAN N/R 2024-501382, ACCOMPLISHED REPAIR HOLSep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024091001241Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR 68 LH LOWER INBD HOLEN OF DOOR STOP FITTING N1 AREA CRACK D = 0.135INCH; REF AEROMAN N/R 2024- 501342, PERFORMED REPAIR IAW A320 SRM 53-41-12-300-011. REF FUR A320 -53-1712.Sep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001240Bulkhead · crackedDURING HEAVY MAINTENANCE, PRESSURE BULKHEAD FWD SIDE AT FR35 & STGR30L CRACKED FASTENER HOLES REFERENCE: /1/ AEROMAN EA 53-9036-24 REV. 0 (COVER + PART 1-3) /2/ AIRBUS RDAF 81452909/003/2024#A /3/ AIRBUS RI R533-70268 ISSUE C /4/ AIRBUS RI R533-70269 ISSUE D.Sep 9, 2024 · N595JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2024091101264Transducer · failedFLT#296, JFK-SKB. (AIRCRAFT PERFORMED AN AIR TURN BACK TO JFK) 'AIR ENG BLEED ABNORMAL RAN ALL CK LOSTS AND CONTACTED MX -ADV AIR RETURN JFK; REMOVED AND REPLACED #1 ENG 10HA1 IAW AMM 36-11-43, RAN ENG #1 OPS CHECK NO GOOD. FUTHER T/S REQ.' (SUPPLEMENTAL TO FOSep 8, 2024 · N763JB · Airbus A320232 · Engine Bleed Air SystemSDR YENA2024091101253Unknown · odorFLT#101, FLL-JFK. 'CUSTOMERS NOTED IN CRUISE AT FL320 A STRONG GAS SMELL IN ROWS 9-13 LASTING FOR APROX 20 MIN. FLIGHT CREW DID NOT SMELL. ONLY ONE INFLIGHT NOTED TRANSIENT SMELL FOR A BRIEF TIME; COMPLIED WITH INFORMATION NOTICE 2017-T015. SECTION A, ISOLATEDSep 8, 2024 · N964JT · Airbus A320232 · Air Distribution SystemSDR GTIA2024090938365A/C Pack · odorFLIGHT ATTENDANTS REPORTED A MUSTY DIRTY SOCK SMELL ON DESCENT AT AROUND 11,000 FT PACK 2 WAS ISOLATED AND THE SMELL DISSAPATED-TROUBLE SHOT PER TSM 05-50-00 ISOLATED PACK 2 SEE ITEM #2 OF THIS LOG PAGE FOR DEFERAL OF PACK 2 MOC # 65847Sep 8, 2024 · N646NK · Airbus A320232 · Cabin Cooling SystemSDR YENA2025070700684Unknown · odorFLT#1454, SJU-FLL. 'ON DESCENT BELOW 10000 FT FORWARD FA CALLED AND SAID THEY HAD A BURNT RUBBER SMELL IN FORWARD GALLEY AND FIRST FEW ROWS; COMPLIED WITH INFORMATION NOTICE 217-T015L SECTION B2 IDENTIFIED ODOR TYPE 10 TRANSIENT ENVIRONMENT SYS ODORS ACCOMPLISSep 7, 2024 · N807JB · Airbus A320232 · Air Distribution SystemSDR AALA202409231684Pump · inoperativeAIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **SUPPLEMENTAL REPORT FOR AALA2Sep 7, 2024 · N657AW · Airbus A320232 · Fuel Boost PumpSDR AALA202409239557Contact · failedAIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA20240Sep 7, 2024 · N657AW · Airbus A320232 · Fuel System WiringSDR AALA202409236181Pump · inoperativeAIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA20240Sep 7, 2024 · N657AW · Airbus A320232 · Fuel Boost PumpSDR AALA202409231856Pump · inoperativeAIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. **ORIGINAL REPORT WAS AALA20240Sep 7, 2024 · N657AW · Airbus A320232 · Fuel Boost PumpSDR AALA202409111684Pump · inoperativeAIRCRAFT WAS NOT GROUNDED: CENTER TANK PUMP 1 INOPERATIVE. VALVE INDICATES CLOSED IN THE AMBER POSITION WHEN THE PUMP IS IN THE ON POSITION AND WITH FUEL IN THE CENTER TANK. CENTER TANK FUEL DOES NOT FEED TO THE NUMBER 1 ENGINE. (OPEN)Sep 7, 2024 · N657AW · Airbus A320232 · Fuel Boost PumpSDR AALA202409235424Coupling · wornAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON SPLICE LOCATED BETWEEN FR 66 AND STR 23L IN AFT GALLEY AREA. REPLACED SPLICE COUPLING PER SRM 53-41-14-22A.Sep 6, 2024 · N604AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202409236605Coupling · wornAIRCRAFT IN BASE MAINTENANCE: ELONGATED HOLE ON SPLICE LOCATED BETWEEN FR 66 AND STR 23L IN AFT GALLEY AREA. REPLACED SPLICE COUPLING PER SRM 53-41-14-22A.Sep 6, 2024 · N604AW · Airbus A320232 · Fuselage Miscellaneous StructureSDR AALA202409114290Hinge Arm · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #4. REPLACED ELEVATOR LEFT HINGE ARM END FITTING #4Sep 6, 2024 · N604AW · Airbus A320232 · Elevator StructureSDR AALA202409110684Hinge Arm · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #1. REPLACED ELEVATOR LEFT HINGE ARM END FITTING #1Sep 6, 2024 · N604AW · Airbus A320232 · Elevator StructureSDR AALA202409116894Hinge Arm · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #2. REPLACED ELEVATOR LEFT HINGE ARM END FITTING #2Sep 6, 2024 · N604AW · Airbus A320232 · Elevator StructureSDR AALA202409114657Hinge Arm · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #3. REPLACED ELEVATOR LEFT HINGE ARM END FITTING #3Sep 6, 2024 · N604AW · Airbus A320232 · Elevator StructureSDR AALA202409117435Hinge Arm · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #5. REPLACED LEFT HINGE ARM END FITTING #5Sep 6, 2024 · N604AW · Airbus A320232 · Elevator StructureSDR AALA202409102296Hinge Fitting · excess playAIRCRAFT WAS IN BASE MAINTENANCE: EXCESSIVE PLAY ON BEARING ELEVATOR LEFT HINGE ARM END FITTING #6. REPLACED ELEVATOR LEFT HINGE ARM END FITTING #6 I.A.W AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Sep 6, 2024 · N604AW · Airbus A320232 · Horizontal Stabilizer StructureSDR AALA202409102786Release Pin · shearedAIRCRAFT WAS GROUNDED: ON NORMAL LANDING IN ILM THE AIRCRAFT LEFT OVERWING DOOR AT 11A EMERGENCY EXIT ECAM MESSAGE POPPED UP ON ROLL OUT AND THE DOORS PAGE SHOWED OPEN. WE STOPPED THE AIRCRAFT TO CONFER WITH FLIGHT ATTENDANT WHO VERIFIED THE HANDLE COVER WAS OSep 6, 2024 · N654AW · Airbus A320232 · Emergency ExitsSDR AALA202409106932Proximity Sensor · bentAIRCRAFT WAS GROUNDED: ON NORMAL LANDING IN ILM THE AIRCRAFT LEFT OVERWING DOOR AT 11A EMERGENCY EXIT ECAM MESSAGE POPPED UP ON ROLL OUT AND THE DOORS PAGE SHOWED OPEN. WE STOPPED THE AIRCRAFT TO CONFER WITH FLIGHT ATTENDANT WHO VERIFIED THE HANDLE COVER WAS OSep 6, 2024 · N654AW · Airbus A320232 · Door Warning SystemSDR YENA2024091001239Frame · crackedDURING HEAVY MAINTENANCE: FR 20 DOUBLE JOGGER AREA HOLE "C" WITH CRACK INDICATION ON FRAME; REF MEXICANA WO#1316755 S/N 00329 FOR WORK PERFORMED; FUSELAGE LH FR20 DOUBLE JOGGLE AREA, HOLE "C" CRACK ON FRAME WAS REPAIRED, IAW A320 SRM TASK 53-11-12-300-012 REVSep 6, 2024 · N516JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024091001238Door Frame · crackedDURING HEAVY MAINTENANCE: LH FR68 DOOR STOP FITTING HOLE 1 WITH CRACK INDICATION; REF MEXICANA WO# 1316755 S/N 0328; LH FR68 DOOR STOP FITTING HOLD 1 WAS REPAIRED IAW A320 SRM 53-41-12-300-011 REV 150, THIS REPAIR IS CAT B INSP THRESHOLD FROM EMBODIMENT OF THSep 6, 2024 · N516JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2024091001237Frame · crackedDURING HEAVY MAINTENANCE: RH FR20 DOUBLE JOGGER AREA HOLDS "A" AND "C" WITH CRACK INDICATION ON FRAME; REF MEXICANA WO#1316755 S/N 0330 FOR WORK PERFORMED; RH FR20 DOUBLE GOGGER AREA HOLD "A" CACK ON FR WAS REPAIRED IAW A320 SRM 52-11-12-300-012 MAY 01/24 RESep 6, 2024 · N516JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2024091001236Hinge Arm · damagedDURING HEAVY MAINTENANCE: VERTICAL STABILIZER, HINGE ARM FITTING NO 7 WITH ELONGATED HOLES; REF MEXICANA WO# 1316755 S/N 00332; VERTICAL STABILIZER HINGE ARM FITTING NO 7 WAS REPAIRED IAW TRE2055026 DATE AUG 08/2024, TEMP REPAIR, LIMITATIONS 6 MOS. IAW RDAF 8Sep 6, 2024 · N516JB · Airbus A320232 · Vertical Stabilizer Miscellaneous StructureSDR YENA2024091001235Seat Track · corrodedDURING HEAVY MAINTENANCE: CPCP FINDING: PASSENGER CABIN, FWD AREA, BTW FR22 AND FR24, RH SEAT TRACK -Y765 WITH CORROSION; CORROSIONS AT SEAT TRACK BETWEEN FR22 /FR24 AND -Y765 WERE REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS. THIS REPAIR IS CAT (A) ISep 6, 2024 · N516JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2024091001234Seat Track · corrodedDURING HEAVY MAINTENANCE: CPCP FINDING: PASSENGER CABIN, FWD AREA, BTW FR22 AND FR24, RH SEAT TRACK -Y1292 WITH CORROSION; "CORROSIONS AT SEAT TRACK BETWEEN FR22 /FR24 AND -Y1292 WERE REWORKED, EVALUATED AND FOUND WITHIN ALLOWABLE LIMITS. THIS REPAIR IS CAT (ASep 6, 2024 · N516JB · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR AALA202409097505Flashlight · inoperativeAIRCRAFT WAS NOT GROUNDED: AFT LEFT HAND INBOARD FLIGHT ATTENDANT FLASHLIGHT INOPERATIVE, REPLACED FLASHLIGHT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 25-22-41.Sep 6, 2024 · N661AW · Airbus A320232 · Emergency EquipmentSDR CALA2024090900602Control Servo · faultySPLR FAULT DISPLAYED ON UPPER ECAM SCREEN. - F-CTL ON DEPARTURE FLT CONTROLSPLR FAULT ON UPPER ECAM SPOKE TO FLIGHT CREW. SPOILER FAULT OCCURED ON TAXI OUT, RESET SEC 1 2 AND 3, FAULT CLEARED. ONCE AIRBORNE, AFTER 5-10 SECONDS OF GEAR UP, FAULT RETURNED. PILOTSep 6, 2024 · N487UA · Airbus A320232 · Drag Control SystemSDR AALA202409090682Bottle · low pressureAIRCRAFT WAS NOT GROUNDED: DURING PS CHECK FOUND L1 DOOR DAMPER LOW PRESSURE. REPLACED L1 DOOR DAMPER FILLING VALVE AND SERVICED DOORSep 6, 2024 · N663AW · Airbus A320232 · Passenger/Crew Doors
Back to Airbus A320-232