Airbus A320-232

Service difficulty reports · 32,648

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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 YENA2026021800220Unknown · odorFLT 259, BDL-FLL. AFTER PARKING. FO INFORMED THAT THE TWO INFLIGHT IN THE REAR OF THE AIRCRAFT EXPERIENCED A FUME EVENT WHICH CAUSED THEM TO FEEL LIGHT HEADED. THE EVENT OCCURRED ON FINAL APPROACH. FRONT CABIN DID NOT EXPERIENCE ANYTHING. THE COCKPIT ALSO WAFeb 17, 2026 · N615JB · Airbus A320232 · Air Distribution SystemSDR YENA2026021800217Oil System · leakingFLT 1247, LGA-TPA. BOTH AFT FA'S SAID THEY SMELLED A DIRTY SOCKS ODOR AT 7000 FT DURING DESCENT. SCRATCHY THROAT & BURNING EYES.; ACCOMPLISHED INFO NOTICE 2017-T015M REFER TSM 05-50-00-810-831-A, FOUND DIRTY SOCKS ODOR ACTIVE DURING APU BLEED ON AND PACKS Feb 17, 2026 · N558JB · Airbus A320232 · APU Oil SystemSDR CALA2026021813859Cover · missingDURING WALK AROUND FOUND PANEL COVER MISSING FROM RT WING LEADING EDGE. OTBD OF RT ENGINE. OPEN.Feb 17, 2026 · N493UA · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021700208Apu · odorFLT 438, MCO-BDL . STRONG OIL ODOR DURING CLIMBOUT & CRUISE, WENT AWAY FROM 35000 FT TO LANDING ,SMELLED A LEVEL 2 OIL ODOR. THIS PLANE HAS HISTORY. ( APU BLEED AIR SUPPLY SYSTEM ). RESOLVED ON W/O: 1477336 TASKCARD: NR-00002 PREVIOUSLY C/W ON LOGPAGE 44629Feb 17, 2026 · N643JB · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR GTIA2026021939281Ecs · contaminatedAFTER LANDING FUMES SMELL FROM THE AFT OF AIRCRAFT POSSIBLY FROM PACK 2. FA STATES THAT THE SMELL CAME AROUND THE TIME THE GEAR CAME DOWN ON APPR. APU WAS OFF DURING THAT TIME.-REF TSM 05-50-00-810-831-A. ACCOMPLISHED LEVEL A DECONTAMINATION PROCEDURE AND R+R Feb 16, 2026 · N652NK · Airbus A320232 · Cabin Cooling SystemSDR YENA2026021800219Ecs · contaminatedFLT 968, PBI-HPN. CABIN/COCKPIT FUMES MOMENTARILY ON ASCENT B/T 5000-8000. THEN PROLONGED ON DESCENT FROM UPPER TEENS (17-19000) TO GROUND ALL CREW SMEELED IT. AIR SMELLS CLEAN ON APU BLEED.; C/W LEVEL A DECONTAMINATION PER INFO NOTICE 2017-T015M. REF LP 4458Feb 16, 2026 · N663JB · Airbus A320232 · Air Conditioning SystemSDR CALA2026022013944Fuel Cap · missingFUELER REPORTS MISSING FUEL CAP REQUESTING CDL FOR MISSING FUEL CAP. COMPLIED WITH CDL ITEM PLACED ON CDL REPLACED FUEL CAP, OPS CHECK GOOD.Feb 15, 2026 · N481UA · Airbus A320232 · Fuel StorageSDR CALA2026021813868Antenna · faultedWX RADAR R/T ON LOWER RIGHT OF ND WHEN WX RADAR TURNED ON AT TOP OF DESCENT, RADAR IN OPPOSITE, FLIGHT REPORT OPENED RADOME & CHECKED FOR WATER INTRUSION & DAMAGE. NO EVIDENCE OF ANY DAMAGE IAW AMM 53-15-991-00400-00-A. REPLACED THE WEATHER RADAR ANTENNA IAFeb 15, 2026 · N442UA · Airbus A320232 · Weather Radar SystemSDR YENA2026021700209Control Panel · overheatedFLT 1338, MCO - BDL, ON DECENT, SMELLED A FAINT ELECTRICAL ODOR SHORT HINT LATER NOTICED BROWN SPOTS ON AUTO BRAKE PANEL WAS VERY HOT TO THE TOUCH ELECTRIC ODOR WENT IN WAVES TURNED OFF LIGHTS TO PANEL PANEL ALSO HAD LIGHT START BURNING OUT IN DESAT. COMPLFeb 15, 2026 · N519JB · Airbus A320232 · Landing Gear Brake SystemSDR YENA2026021700207Ecs · contaminatedFLT 38, SJO-FLL. DIRTY SOCK SMELL WHEN BOARDING.; COMPLIED WITH IFORMATION NOTICE 2017-T015, STEP 1, ISOLATED FAULT TO TYPE 10 MISCELLANEOU ODOR. PER TSM 05-50-00-810-085-B/ SM O5-00-810-085-D. ACFT OK FOR SERVICE. PERFORMED LEVEL A ECS DECONTAMINATION IAW SFeb 15, 2026 · N629JB · Airbus A320232 · Air Distribution SystemSDR GTIA2026021639280Battery · inoperativeR2 DOOR FLASHLIGHT INOPERATIVE. R & R R2 DOOR FLASHLIGHT BATTERY IAW DRAWING EMER-EQUIPFeb 15, 2026 · N656NK · Airbus A320232 · Emergency EquipmentSDR YENA2026021800216Post · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE UPPER AREA VERTICAL MEMBER -Y254 AT FRAME 24A ON FWD CA RGO BAY REF AEROMAN NR 2026-39977 WO 2026 25/1 REMOVED AND REPLACED VERTICAL MEMBER -Y254 AT FRAME 24A IAW AMM 25-54-81-000-801-A AND AMM 25-54-81-400-801-A. THISFeb 14, 2026 · N632JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026021800214Post · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE UPPER AREA VERTICAL MEMBER Y765 AT FRAME 24A ON FWD CARGO COMPARTMENT; REF AEROMAN NR 2026-39978 WO 2026 25/1 REMOVED AND REPLACED VERTICAL MEMBER Y765 AT FRAME 24A IAW AMM 25-54-81-000-801-A AND AMM 25-54-81-400-801-A.Feb 14, 2026 · N632JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026021800213Post · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE UPPER AREA VERTICAL MEMBER -Y765 AT FRAME 24A ON FWD CARGO BAY, REF AEROMAN NR 2026-39979 WO 2026 25/1 REMOVED AND REPLACED VERTICAL MEMBER -Y765 AT FRAME 24A IAW AMM 25-54-81-000-801-A AND AMM 25-54-81-400-801-A. THIS Feb 14, 2026 · N632JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026021800212Post · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE UPPER AREA VERTICAL MEMBER Y254 AT FRAME 24A ON FWD CARGO BAY, REF AEROMAN NR 2026-39980 WO 2026 25/1. REMOVED AND REPLACED VERTICAL MEMBER Y254 AT FRAME 24A IAW AMM 25-54-81-000-801-A, AND AMM 25-54-81-400-801-A. THIFeb 14, 2026 · N632JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2026021800211Skin · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLE EXTERNAL SKIN LOWER SURFACE OF CUT OUT FUEL TANK AREA BT W RIB16 TO RIB17 ON RH WING; REF AEROMAN NR 2026-39866 WO 2026 25/1 JB NR-0042 WO 1441774 FUR A320-57-02978.Feb 14, 2026 · N632JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2026021800210Skin · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLES AT 2 LOCATION, BOTTOM SKIN EXTERNAL SURFACE OF CUT OUT FUEL TANK AREA BTW RIB 16 TO RIB 17 ON RT WING; REF AEROMAN NR 2026-40034 WO 2026 25/1 JB NR-0043 WO 1441774 FUR A320-57-02979.Feb 14, 2026 · N632JB · Airbus A320232 · Wing, Plate/SkinSDR AALA202604281730Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: REPLACE CONTINUITY FITTING LH SIDE IAW EA 372184. MAINTENANCE REPLACED CONTINUITY FITTING LOCATED Y0 AND FR2 LH SIDE BY EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR AALA202604249438Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: MAINTENANCE: WINDSHIELD FRAMING CENTER POST FITTING LOWER FITTING FOUND CRACKED AT Y0 AND FR2. MAINTENANCE REPLACE LOWER FITTING YO AND FR2 IAW EA 372184.Feb 13, 2026 · N653AW · Airbus A320232 · Fuselage Main, StructureSDR YENA2026021600198Ecs · contaminatedFLT 1030, RSW-JFK. INFLIGHT NR 4 FA REPORTED A MIGRAINE HEADACHE AND SMELLED BURNED HYDRAULIC FLUID ODOR AT CRUISE. TURNED HYDRAULICS OFF & ON, ON THE GROUND TO RESET COMPUTERS.; COMPLIED WITH INFORMATION NOTICE 2017-T015 STEP 1. IDENTIFIED ODOR A TYPE 10 MIFeb 13, 2026 · N583JB · Airbus A320232 · Air Distribution SystemSDR CALA2026022314023Plate · wornLEFT PYLON AT LOWER RIB 5 SPAR AND CHAFE STRIP IS WORN. LEFT PYLON LOWER RIB 5 SPAR CHAFED WAS BLENDED PER SRM 54-51-12-283-003, AREA OF CHAFE IS 1 INCH FWD OF FASTENER ROW AND 6 INCHES FROM INBD EDGE. POST BLENDING AREA MEASURES: D=0.010, W-0.500, L=0.250.Feb 12, 2026 · N448UA · Airbus A320232 · Nacelle/Pylon, Main FrameSDR CALA2026021613779Lug · brokenLEFT ELEVATOR OTBD SERVO HAS A MISSING LOCKING LUG. BROKEN LUG PER AAR LCQ N/R 9294030/38030 GEN BY V923643 ESFR COMPLETED REPAIRED L/H ELEVATOR O/B SERVO LOCKING LUG IAW SRM 55-26- 47-300-001-A. PERFORMED OPS CHECKED GOOD IAW 27-34-00-710-001-A.Feb 12, 2026 · N497UA · Airbus A320232 · Elevator StructureSDR AALA202602139260Power Supply · failedAIRCRAFT WAS GROUNDED: EMERGENCY LIGHT FAILED, INTERNAL FAULT. MAINTENANCE REPLACED FWD EPSU IAW 33-51-38 OPS AND BITE TEST GOOD.Feb 12, 2026 · N651AW · Airbus A320232 · Emergency LightingSDR AALA202602135890Flashlight · out of positionAIRCRAFT WAS NOT GROUNDED: CABIN FLASHLIGHT AT JUMPSEAT 5 APPEAR TO BE INSTALLED INCORRECTLY, AND IS NOT CHARGING. MAINTENANCE INSTALLED UNDER FA SEAT 5 NEW TAMPER SEALS, REPLACED BATTERIES AND PUT IN THE CORRECT POSITION IAW AMM 25-60-00.Feb 12, 2026 · N658AW · Airbus A320232 · Emergency EquipmentSDR AALA202602129327Light · no testAIRCRAFT WAS GROUNDED: DURING R1 SLIDE REPLACEMENT EMERGENCY LIGHT TEST 33-51-00-710-001 FAILED. MAINTENANCE REPLACED EMERGENCY LIGHT AND TESTED OK IAW 33-51-00.Feb 12, 2026 · N651AW · Airbus A320232 · Emergency LightingSDR GTIA2025021239279Flashlight · inoperativeFWD GALLEY FLASHLIGHT INOP -INSTALLED NEW FLASHLIGHT PER SPIRIT A320 EMERGENCY DRAWING LAYOUT TEST . OK THIS CLOSES DMI PLC RMVD, MOC NOTIFIED DMI LOG UPDATEDFeb 12, 2026 · N636NK · Airbus A320232 · Emergency EquipmentSDR YENA2026021700202A/C Pack · odorFLT 839, JFK-BQN, PASSING 10000FT WE BOTH SMELLED OIL. COMPLIED WITH THE PROCEDURE AND AFTER 3 MINS, TURNED ON THE NR 1 PACK AND OODR CAME BACK. MUSTY ACID ODOR. COMPLIED WITH INFO NOTICE 2017-T015 STEPS 1 & 2 INDENTIFIED ODOR AS A TYPE 5. NO 30 DAY HISTOFeb 11, 2026 · N828JB · Airbus A320232 · Cabin Cooling SystemSDR CALA2026021313768Proximity Sensor · damagedFOUND BOTH LT FWD & AFT PROX DETECTOR ASSY ACTUATING RODS BENT IAW AMM 25-62-43. REMOVED LT FWD & AFT PROX SWITCHES, REMOVED RELEASE MECHANISM ASSEMBLIES. INSTALLED NEW ASSEMBLIES IAW AMM 52-73-11. LT FWD & AFT EMERGENCY EXIT DOORS REMOVED. COMPLETED LT FWFeb 11, 2026 · N447UA · Airbus A320232 · Emergency EquipmentSDR CALA2026021213743Release Mech · damagedFOUND BOTH LEFT FWD, & AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS DAMAGED IAW AMM 52-21-11. R & R BOTH LT FWD AND AFT EMERGENCY OVERWING EXITS SLIDE RELEASE MECHANISMS IAW AMM 52-21-11.Feb 11, 2026 · N447UA · Airbus A320232 · Escape SlideSDR CALA2026021213722Elec Connector · disconnectedL2 DOOR EMERGENCY LIGHT DID NOT TEST, FOUND CONNECTOR 7245VC DISCONNECTED ENTIRELY IAW AIPC 24-92-04-46M, ITEMS 10, AND 20, AWM 33-51-03 PAGE 8, AND ESPM 20-44-29-01. RECONNECTED & OPS CHECKED PERFORMED IAW AMM 31-51-00-710-007-A. OPS CHKD NORMAL.Feb 11, 2026 · N457UA · Airbus A320232 · Light System WiringSDR AALA202604241668Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOOR BEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N2 FR 36. CRACK L= 0.530 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOOR BEAM Y765 VERTICAL STRINGER #2 AT FR 36 Feb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604226871Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N3 FR 36. CRACK L= 0.550 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM Y254 VERTICAL STRINGER #3 AT FR 36 IAWFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604225191Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N5 FR 36. CRACK L= 0.875 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y765 VERTICAL STRINGER #5 AT FR 36 IFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR AALA202604220542Floorbeam · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION FOUND ON HORIZONTAL FLOORBEAM RADIUS BACKSIDE OF THE SPAR VERTICAL STRINGER N4 FR 36. CRACK L= 0.610 INCH. MAINTENANCE ACCOMPLISHED PERMANENT REPAIR INSTRUCTIONS ON FLOORBEAM -Y254 VERTICAL STRINGER #4 AT FR 36 IAFeb 10, 2026 · N653AW · Airbus A320232 · Fuselage Main, Floor BeamSDR CALA2026021213744Flap · out of adjustDOOR L AFT EMER EXIT ECAM. ADJUSTED LEFT AFT OVERWING EXIT COVER FLAP, ECAM INDICATION NO LONGER REMAINS REF AMM 25-23-47.Feb 10, 2026 · N447UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2026021113695Cover Plate · crackedL1 DOOR UPPER PLATE APPEARS TO HAVE A CRACK ALONG THE AFT EDGE. REMOVED AND REPLACED L1 DOOR UPPER COVER PLATE IAW A320 SRM 51- 72-11-911-001.Feb 10, 2026 · N447UA · Airbus A320232 · Passenger/Crew DoorsSDR AALA202604282565Frame · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK INDICATION ON FRAME 68 RH SIDE IN WEB AFT FACE RADIUS WITH STGR 8 HORIZONTAL FLANGE, AT AFT GALL EY AREA CRACK LENGTH IS 0.430 INCH. MAINTENANCE ACCOMPLISHED TIME LIMITED REPAIR INSTRUCTIONS ON FR68 BTW STR7 AND STR9 RH SIDFeb 9, 2026 · N653AW · Airbus A320232 · Fuselage Main, FrameSDR AALA202602184795Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N4 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #4 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602189094Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N3 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #3 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602188638Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N2 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #2 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602188350Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: REPLACE HINGE ARM END FITTING ELEVATOR N5 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #5 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR AALA202602184281Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N6 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #6 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Emergency LightingSDR AALA202602189099Hinge Fitting · excess playAIRCRAFT IN BASE MAINTENANCE: EXCESSIVE PLAY HINGE ARM END FITTING ELEVATOR N1 ON LH HORIZONTAL STABILIZER. MAINTENANCE REPLACED HINGE ARM END FITTING ELEVATOR #1 ON LH HORIZONTAL STABILIZER IAW AMM 55-16-42-000-001-A AND AMM 55-16-42-400-001-A.Feb 9, 2026 · N653AW · Airbus A320232 · Elevator StructureSDR GTIA2025021239278Flashlight · expiredR2 F/A FLASHLIGHT EXPIRED ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R R2 FLASHLIGHT IAW AMM 25-65-00. OPS CK OK. THIS CLEAR DMI 6050545-1. MOC NOTIFIED. PLACARD REMOVEDFeb 9, 2026 · N646NK · Airbus A320232 · Emergency EquipmentSDR GTIA2025021239277Flashlight · expiredR1 F/A FLASHLIGHT EXPIRED ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R R1 FLASHLIGHT IAW AMM 25-65-00. OPS CK OK. THIS CLEAR DMI 6050544-2. MOC NOTIFIED. PLACARD REMOVEDFeb 9, 2026 · N646NK · Airbus A320232 · Emergency EquipmentSDR GTIA2025021239276Flashlight · expiredL1 F/A FLASHLIGHT EXPIRED ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R L1 FLASHLIGHT IAW AMM 25-65-00. OPS CK OK. THIS CLEARS DMI 6050544-1. MOC NOTIFIED. PLACARD REMOVED.Feb 9, 2026 · N670NK · Airbus A320232 · Emergency EquipmentSDR YENA2026021100166Unknown · odorFLT 1199, LGA - MCO. ON DESCENT THROUGH 15000 FT. STRONG ODOR IN COCKPIT, MAGIC MARKER & OILY. COMPLIED WITH INFORMATION NOTICE 2017-T015, STEPS 1 AND 2. DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER EC A2122043-01. A/C IS OK FOR SVC.Feb 9, 2026 · N827JB · Airbus A320232 · Air Distribution SystemSDR YENA2026021100164None · noneFLT 54, PBI - PBI. FUEL ODOR UPON LANDING IN AFT SECTION ODOR DECIPATED WHEN MX CAME ABOARD. PERFORMED INFO-NOTICE 2017-T015M ISOLATED FAULT TO TYPE 10 ODOR WAS DUE TO OTHER ACFT EXHAUST FUME IAW TSM 05-50-00-810-085-B TSM 05-50-00-810-085-D, ACFT FOR SERVICEFeb 9, 2026 · N593JB · Airbus A320232 · Standard Practices/StructuresSDR AALA202602103572Cylinder · no testAIRCRAFT IN BASE MAINTENANCE: DO NOT PASS OPERATIONAL TEST DOOR DAMPER DAMPING FUNCTION AT PASSENGER CREW DOOR 841. MAINTENANCE REPLACED DOOR DAMPER AT PASSENGER CREW DOOR 841 I.A.W A320 FAM AMM 52-11-14-000-001-B AND A320 FAM AMM 52-11-14-400-001-B.Feb 9, 2026 · N667AW · Airbus A320232 · Passenger/Crew DoorsSDR YENA20260210001Skin · corrodedDURING HEAVY MAINTENANCE: RT WING TOP SKIN PANEL CORRODED /1/ - AIRBUS DOSSIER 81709907 /2/ - AIRBUS RDAF REF. & ISSUE.: 81709907/003/2025 ISSUE A /3/ - AIRBUS RI R572-44701 ISSUE B /4/ - AIRBUS RI R572-58616 ISSUE N /5/ - AIRBUS RI R572-58926 ISSUE E /6/ - AFeb 8, 2026 · N613JB · Airbus A320232 · Wing, Plate/Skin
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