Airbus A320-232

Service difficulty reports · 32,652

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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 CALA2025022500443Skin · contaminatedR/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 39IN I/B, 4 1/2IN T/E , 1 1/2IN DIAMETER, "REPAIR PRIOR TO FLIGHT" GEN BY V061632 ON H AECO LCQ NR 9294227/26227Feb 24, 2025 · N463UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025022500442Skin · contaminatedR/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 123 1/2 IN I/B, 6 IN T/E, 3 IN DIAMETER, "REPAIR PRIOR TO FLIGHT". DRILLED WITNESS HOLES IN R/H ELEVATOR TOP SKIN 123.5 IN FROM I/B 6.IN FROM T/E 1.5IN ON IAW A320 AMM 55-20-00-006-A01 PAR4A(7) FO UND NO LIQUID. REPAFeb 24, 2025 · N463UA · Airbus A320232 · Elevator, Plate/SkinSDR CALA2025022500441Skin · contaminatedR/H ELEVATOR TOP SIDE HAS WATER INGRESS AT 200 1/2 IN I/B, 4 1/2 IN T/E, 3 IN DIAMETER, "REPAIR PRIOR TO FLIGHT". REPAIRED R/H ELEVATOR TOP SIDE 200 IN I/B 4.5IN FROM T/F 4.5IN B Y 3IN ZONE C IAW A320 SRM 55-21-11-300-005 CAT A REPAIR.Feb 24, 2025 · N463UA · Airbus A320232 · Elevator, Plate/SkinSDR GTIA2025022438763Apu · odorDURING CLIMB OUT OF BWI, WE BRIEFLY EXPERIENCE A WET SOCK ODOR, BUT WENT AWAY. DESCENDING INTO MCO THE STRONG ODOR RETURN (MODERATE INTENSITY) WE TRY TO ISOLATE PACK #1 FOR FEW MINUTES, THEN PACK #2 AS PER QRH. BUT WE COULDNT ISOLATE THE ODOR. THE INTESITY SLIFeb 24, 2025 · N618NK · Airbus A320232 · Airborne Auxiliary Power Unit (APU) SystemSDR AALA202502272088Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: R/H MLG DOOR FWD HINGE FITTING REQUIRES REPLACEMENT. REF # MIC 3651785. MAINTENANCE REPLACED DOOR HINGE FITTING P/N D288023820301C IAW SRM 51-42-11.Feb 23, 2025 · N650AW · Airbus A320232 · Fuselage, Door HingeSDR CALA2025022602487Seal · missingLOUD SQUEAL COMINGFROM LEFT OVERWING EXITFOUND SEALANT/SEAL MISSING AT LH WING TO FUSELAGE PANELS 191BT AND 191DT NEAR WHERE NOISE REPORTED. SEE ATTACHED PICTURES. INTERIM REPAIR BELLY FAIRING SEALANT/SEALS FOR PANELS 191BT & 191DT IAW MT 53-004, INSPECT TAPEFeb 23, 2025 · N490UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025022500208Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) (ON DOOR STOP FITTING 7 HOLE 1 FR16LH. LENGTH 0.100 INCH. CRACK DIRECTION 9 O’CLOCK ); REF AEROMAN NR 2025 – 29477, W/O: 2025 13/1 PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500207Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 1 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 3 O’CLOCK; REF AEROMAN W/O: 2025 13 / 1, NR 29476, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DOFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500206Door Frame · crackedDURING HEAVY MAINTENANCE:CRACK INDICATION ON DOOR FRAME IN PASSENGER CABIN (1 EA) ON DOOR STOP FITTING 7 HOLE 3 FR16RH. LENGTH 0.100 INCH. CRACK DIRECTION 6 O’CLOCK.; REF AEROMAN W/O: 2025 13 / 1, NR 29478, PERFORMED PERMANENT REPAIR ON INTERCOSTAL AT LEVEL DOFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500205Stringer · corrodedDURING HEAVY MAINTENANCE: CORROSION STRINGER 43L AT LEVEL FR55 IN AFT CARGO COMPARTMENT; REMOVED AND REPLACED STRINGER 43L AND FASTENERS LOC. BTW. FRAME 54 TO FRAME 60 I.A.W. A320 SRM 51-42-11 AND DRAWING E53470342. ALL WORK WAS PERFORMED ON AEROMAN WO2025-13Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Longeron/StringerSDR YENA2025022500204Skin · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND ON FR16 RH SIDE AT HOLE A. CRACK DIRECTION 9 OCLOCK (VIEW FROM OUTSIDE) AND CRACK LENGTH 0.100 INCHES (1EA); PERFORMED PERMANENT REPAIR LOC. ON DOUBLE JOGGLE AREA HOLE A ON FR16 RH SIDE IAW A320 SRM 53-11-12-30Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025022500203Skin · crackedDURING HEAVY MAINTENANCE: CRACK INTERNAL STRUCTURE SECTION CONNECTION FRAME 66 AT LEVEL STR23 L AND BETWEEN Y1292 TO Y1732 AT AFT GALLEY AREA; REMOVED AND REPLACED INTERNAL STRUCTURE SECTION CONNECTION AND FASTENERS LOCATED FRAME 66 AT LEVEL STR23L AND BETWEENFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, Plate/SkinSDR YENA2025022500202Door Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND DOOR STOP 1 HOLE H3 FR68LH. CRACK DIRECTION 11 OCLOCK . CRACK LENGTH 0.100 INCH; REF AEROMAN WO 2025 13/1 NR 2025-29474; ACCOMPLISHED THE REPAIR OF THE CRACK DAMAGE FOUND ON THE REAR FUSELAGE FR68 LHS ( NEAR STRFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500201Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC UPPER CORNER .CRACK DIRECTION 1 O'CLOCK. CRACK LENGTH 0.250 INCH.REF AEROMAN WO 2025 13/1 NR 2025-29453; ACCOMPLISHED THE PERMANENT REPAIR OF THE CRACK DAMAGE ON THE LH WINDSHIFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500200Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND WINDSHIELD CENTER POST LH SIDE LOC LOWER CORNER .CRACK DIRECTION 5 O'CLOCK. CRACK LENGTH 0.500 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29454; ACCOMPLISHED THE PFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500199Window Frame · crackedDURING HEAVY MAINTENANCE: CRACK INDICATION ON WINDSHIELD IN COCKPIT (1 EA) (CRACK INDICATION FOUND CONTINUITY FITTING WINDSHIELD RH SIDE . CRACK DIRECTION VERTICAL. CRACK LENGTH 0.200 INCH.); REF AEROMAN WO 2025 13/1 NR 2025-29455; ACCOMPLISHED THE PERMANENT RFeb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500198Access Panel · damagedDURING HEAVY MAINTENANCE: ELONGATED HOLES ON FUEL ACCESS PANEL 640MB CUT OUT BTW RIB 17 TO RIB 18 ON RH WING (2 EA); (RESOLVED ON W/O: 1348393 TASKCARD: NR-00025 ) REF AEROMAN WO 2025 13/1 NR 2025-29526; PERFORMED PERMANENT REPAIR ON BOTTOM SKIN CUT-OUT BTW RIFeb 23, 2025 · N586JB · Airbus A320232 · Wing, Plate/SkinSDR YENA2025022500197Support · corrodedDURING HEAVY MAINTENANCE: CORROSION LOWER SILL LH LOC. BTW FRAME 66 AND FRAME 68 AT AFT GALLEY AREA (CPCP FINDING ); REF AEROMAN WO 2025 13/1 NR 2025-29665; PERFORMED PERMANENT REPAIR ON LOWER SILL LH LOC. BTW FRAME 66 AND FRAME 68 AT AFT GALLEY AREA I.A.W. A3Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Miscellaneous StructureSDR YENA2025022500196Firewall · not reportedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / SB-53-1500 TAIL CONE / LH/RH FIREWALL / BTWN FR81-83 / DEVIATION - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2025022500195Window Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE/ NOSE FWD FUSELAGE/ FWD WINDSHIELDS / CENTER POST LOWER NODE & CONTINUITY FITTING LH/RH AREAS / CRACK DAMAGE - PERMANENT REPAIR. (CONSIDERED AS A MAJOR REPAIR)Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2025022500194Door Frame · crackedDURING HEAVY MAINTENANCE: FUSELAGE / REAR FUSELAGE / FR 68 LH AND STGR 22 / DOOR STOP FITTING #1 / LOWER INBD HOLE / CRACK DAMAGE - PERMANENT REPAIR (CONSIDERED AS A MAJOR REPAIR)Feb 23, 2025 · N586JB · Airbus A320232 · Fuselage Main, StructureSDR GTIA2025022438761Power Supply · no testREF T/C EO 2562-2423 - EPSU 10WL WILL NOT TEST.-R/R EPSU 10WL IAW AMM 33-51-38. OPS TEST GOOD.Feb 23, 2025 · N611NK · Airbus A320232 · Emergency LightingSDR CALA2025022502469Control Servo · faultedN/W STRG FAULT IN FLIGHT ACPD BSCU1 BITE REF MM 32-46-00-740-001-A, FOUND FAULT "STEERING ELECTRO-HYD MODULE (6GC)". REMOVED NWS SERVO 6GC REF MM 32-51-51-000-001-A. PART ON ORDER REPLACED NLG STEERING CONTROL MODULE (6GC) REF MM 32-51-51-400-001-A STEP 4A-C, Feb 22, 2025 · N439UA · Airbus A320232 · Landing Gear Steering SystemSDR GTIA2025022438760Unknown · odorSTRONG ODOR ON DESCENT STARTING AROUND 25,000 UNPLEASANT MUST GYM SOCK SMELL-PERFORMED TSM 05-50-00-810-831A. INSPECTED PACK# 2 FOR CONTAMINATION. NO EVIDENCE OF CONTAMINATION FOUND. RAN BOTH ENGINES TO DUPLICATE FAULT IAW AMM 71-00-00. NO ODOR DETECTED. R&R RFeb 22, 2025 · N626NK · Airbus A320232 · Air Distribution SystemSDR AALA202502245104Power Supply · inoperativeAIRCRAFT WAS NOT GROUNDED: WHILE PERFORMING PS CHECK, FOUND L2 DOOR EMERGENCY ENTRANCE LIGHTING INOP. MAINTENANCE REPLACED 13WL EPSU AND L2 DOOR EMER LIGHT ASSY OPS CHKS GOOD AMM 33-51-38,Feb 22, 2025 · N604AW · Airbus A320232 · Emergency LightingSDR CALA2025022400428Angle · crackedLH FUSELAGE BELLY FAIRING VERTICAL SUPPPORT AT FR35 CRACKED. REMOVED AND REPLACED CRACKED SUPPORT VERT ANGLE AT LH FUSELAGE F R35 IAW A320 SRM 51-72-11-911-001.Feb 22, 2025 · N463UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025022402435Arming Lever · stiffARMING LEVED DOOR 2R IS JAMMED. DOOR NOT ARMED. OPERATED DOOR, OPS CHECKED GOOD. CLEANED AND LUBED PRECAUTIONARY ARMING LEVER. OK TO FOR SERVICE. OPERATED DOOR, OPS CHECKED GOOD. CLEANED AND LUBED PRECAUTIONARY ARMING LEVER. OK TO FOR SERVICE.Feb 20, 2025 · N464UA · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025022400406Stringer · corrodedAFT CARGO COMP STR 41R CORRODED BETWEEN FR 58 AND FR 59. ACCOMPLISHED REPAIR ON AFT CARGO COMP STR 41R BETWEEN FR 58 AND FR 59 PER HAECO REO-L25363 REV IR WITH NO DEVIATIONS AS DIRECTED BY ECRA 5341-01475.Feb 20, 2025 · N1902U · Airbus A320232 · Fuselage Main, Longeron/StringerSDR GTIA2025022138759Bottle · abnormalL1 DOOR ASSIST BOTTLE LOW -SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 52-10-00. NO OTHER DEFECTS FOUNDFeb 20, 2025 · N634NK · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025022000398Shear Plate · corrodedSUPPORT TASK AFT MAIN CABIN, BETWEEN FR 69 AND FR 70, Y1732 SHEAR PLATE/TRAY, LH SIDE, HAS CORROSION. TRANSCRIBED FROM HAECO GSO NR 9282039 REMOVED AND REPLACED LATERAL SHEAR PLATE BETWEEN LH FR 69 TO FR 70 Y1732 PER AIRBUS DWG 853474180 ISSUE U AND A320-200 SFeb 20, 2025 · N426UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR GTIA2025022138753Flashlight · inoperativeFA D FLASHLIGHT INOP ( FLASHLIGHT AND HOLDERS (FLIGHT DECK OR CABIN) )-R&R CAB ATTENDANT SEATS INST FLASHLIGHT IAW AMM 25-63-00. THIS CLEARS MDDR 105152. MOC NOTFIEDFeb 18, 2025 · N618NK · Airbus A320232 · Emergency EquipmentSDR AALA202502219371Bottle · reads lowAIRCRAFT WAS NOT GROUNDED: L2 PASS/CREW DOOR ASSIST BOTTLE LOW PSI. MAINTENANCE SERVICED L2 PASS/CREW DOOR ASSIST BOTTLE IAW AMM 52-10-00.Feb 17, 2025 · N661AW · Airbus A320232 · Passenger/Crew DoorsSDR CALA2025022000396Seat Track · corrodedFWD CABIN RT SIDE I/B SEAT TRACK CORRODED AT FR 20. REMOVED AND REPLACED SEAT TRACK AT FWD CABIN RT SIDE I/B FROM FR 12 TO FR24 IAW A320 SRM 51-42-11, SRM 51-72-11. SFR NO.1038443.Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR YENA2025021900170Oil System · leakingFLT#613, HPN-FLL. INFLIGHT ADVISED OF A CABIN ODOR THAT RESEMBLED DIRTY SOCKS + WAS NOTICED MAINLY MID CABIN BUT WAS EVIDENT FROM ROW 6 + AFT- SEVERAL CUSTOMERS ALSO COMPLAINED ABOUT THE ODOR - THERE WAS A SLIGHT ODOR ON FLIGHT DECK FOR APPROX 4-5 MIN IN DESCEFeb 17, 2025 · N663JB · Airbus A320232 · APU Oil SystemSDR CALA2025021900381Profile · corrodedFUSELAGE INTERNAL AREA AT FR 67 LST42-RST42 HAS EXFOLIATION. REMOVED AND REPLACED CORRODED FRAME PROFILE AT FR67 WITH A NEW F RAME PROFILE AT FR 67 IAW A320 SRM 51-42-11-001 PARA F.Feb 17, 2025 · N434UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025021800377Floor Support · corrodedFWD CABIN CTR AREA FLOOR SUPPORT Y254 CORRODED AT FR 20 PER HAECO LCQ N/R 9290686/38686 GEN BY. REMOVED AND REPLACED FLOOR BEAM AT FWD CABIN CTR AREA FROM FR 20 -24 IAW A320 SRM 51-72-11.Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage Miscellaneous StructureSDR CALA2025021800379Seat Track · corrodedFWD CABIN RT SIDE O/B SEAT TRACK AT FR 20 CORRODED. REMOVED AND REPLACED SEAT TRACK AT FWD CABIN RT SIDE O/B FROM FR 12 TO FR24 IAW A320 SRM 51-42-11,SRM 51-72-11.Feb 17, 2025 · N459UA · Airbus A320232 · Fuselage, Seat/Cargo Attach FittingsSDR CALA2025021702339Fmc · faultedFMGC 1 FAIL REPORTED BY CREW, RESET UNSUCCESSFUL CFDS ATA 22-83-34 FMGC1 SOURCE EFCS 1 PHASE 5 , SEE TSM 22-83-00-810-859-A, 3 HITS LAST 10 LEGS LOCKED UNLOCKED FOR CORRECTIVE ACTION FOLLOWED TSM 22-83-00-810-859-A, REMOVED AND REPLACED TERMINAL BLOCKS 1831VT4Feb 17, 2025 · N457UA · Airbus A320232 · Flight Management Computing Hardware SystemSDR CALA2025021902379Slide · faultyREPLACED DOOR 2 LEFT EVACUATION SLIDE ASSY PER JOB CARD 31-2561-9-0015 REPLACED DOOR L2 EVACUATION SLIDE ASSY. SER # OFF 7468. SER# ON 7104. REF AMM 25-62-44.PARTS USED: 31-2561-9-0015, QTY :1. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1565986 SN OFF 7468.SLIFeb 16, 2025 · N488UA · Airbus A320232 · Escape SlideSDR YENA2025021900169Filter · odorFLT#808, STT-SJU. ' IN DESCENT BELOW 10,000FT STRONG DIRTY SOCK ODOR DETECTED IN FRONT AND BACK OF PLANE; COMPLIED WITH INFORMATION 2017-T015K,SECTION B2,IDENTIFIED ODOR TO BE APU BLEED SOURCE OF ODOR EVENT,DECONTAMINATION LEVEL B WAS ACCOMPLISHED PER TSM 05-5Feb 16, 2025 · N565JB · Airbus A320232 · Air Distribution SystemSDR CALA2025021902368Butterfly Valve · faultedVENT EXTRACT FAULT, WITH CORRELATED FAULT ISOL V 24HQ WHEN EXTRACT PB/SW SET TO OVRD. REMOVED AND REPLACED AVIONICS VENTILATION SKIN EXCHANGER ISOLATION VALVE. REF AMM TASK 21-26-55-000-002-A. OPS CHECK PERFORMED IN REF TO AMM TASK 21-26-00-710-001-A. OPS CHECFeb 16, 2025 · N452UA · Airbus A320232 · Air Distribution SystemSDR GTIA2025021738751Unknown · odorFA REPORTED A DIRTY SOCK SMELL ON FINAL-PERFORMED AQE INSPECTION IAW TSM 05-50-00-810-831-A NO SOURCE OF ORDOR FOUND AT THIS TIME WITH APU AND ENG'S RUNNING AND ISOLATION OF PACK 1 & 2 NO 3 DAYS AQE HISTORY A/C OK FOR SVC MOC # 106411. DESCRIPTION OF ODOR/FUMFeb 16, 2025 · N613NK · Airbus A320232 · Air Distribution SystemSDR GTIA2025021738750Megaphone · damagedMEGAPHONE VOL. KNOB BROKEN-REMOVED & REPLACED MEGAPHONE, OPS CHECK GOOD. REF. A320 DRAWING EMERG. EQUIP.Feb 16, 2025 · N605NK · Airbus A320232 · Emergency EquipmentSDR YENA2025021800166Unknown · odorFLT#1134, SJU-MCO. 'ON DESCENT COCKPIT HAD DIRTY SOCK SMELL BELOW 10,000 FT, WE UTILIZED THE ISOLATION PROCEDURE BY TURNING OFF PACK 1 & SMELL DISSIPATED CABIN CREW HAD NO SMELL; COMPLIED WITH INFORMATION NOTICE 2017-T015 SECTION B. IDENTIFY ODOR TYPE 1 (APU) Feb 15, 2025 · N505JB · Airbus A320232 · Air Distribution SystemSDR CALA2025021802361Door · contaminatedAPU OIL SMELL IN CABINPACKS RUNNING UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INVESTIGATE AND CONTACT AIRCRAFT MAC METER INITIATED FOR WITH VENDOR ID MAC RELATED WORK ORDER 000000003129638 AND PRTR ACCOMPLISHED ENGINE RUN AT GATE WITH FLIGHT CREW AND WIFeb 15, 2025 · N449UA · Airbus A320232 · Fuselage Structure (General)SDR YENA2025021700161A/C Pack · contaminatedFLT#545, ISP-PBI. 'ON DECENT THROUGH 12K ENTERING VISIBLE MOISTURE FUME / ODOR IN COCKPIT PACK1 OFF/ON/OFF IAW FUME CHECKLIST HP VALVE OPEN AT THRUST IDLE; COMPLIED W/ INFO NOTICE 2017-T015, SECTION B2. IDENTIFIED ODOR TYPE 5 (PACK 1). DECONTAMINATION LEVEL A Feb 15, 2025 · N583JB · Airbus A320232 · Cabin Cooling SystemSDR AALA202506242679Hinge Fitting · crackedAIRCRAFT IN BASE MAINTENANCE: 0.25-INCH CRACK LH MLG DOOR KEAL BEAM HINGE FITTING CONNECTING PLATE. MAINTENANCE REPLACED MLG DOOR KEEL BEAM HINGE FITTING CONNECTING PLATE IAW SRM 51-42-11-801.Feb 14, 2025 · N668AW · Airbus A320232 · Fuselage, Door HingeSDR GTIA2025021738749Ecs · contaminatedDURING DESCENT AROUND 10000FT STRONG FUME ODOR UNABLE TO ISOLATE OR DETERMINE WHCH PACK IT WAS FROM -PERFORMED TSM 05-50-00-810-831-A TO ISOLATE SOURCE. FOUND PACK #2 TO BE THE SOURCE. PERFORMED DECONTAMINATION OF ECS IAW AMM 21-00-00 AND RAN BOTH ENG AT IDLE Feb 14, 2025 · N655NK · Airbus A320232 · Cabin Cooling SystemSDR AALA202502176104Door Latch · inoperativeAIRCRAFT WAS GROUNDED: FLIGHT DECK DOOR IS DIFFICULT TO OPEN AND CLOSE INFLIGHT AND ON THE GROUND. MAINTENANCE REPLACED UPPER LATCH MECHANISM IAW AMM 52-51-00.Feb 14, 2025 · N647AW · Airbus A320232 · Fixed Inner DoorsSDR YENA2025021700163Unknown · odorFLT#1752, SJU-TPA. 'DIRTY SOCK SMELL IN THE COCKPIT AND FWD GALLEY AREA DURING DESCENT STARTING AROUND 12000 FEET; CHECKED APU NO EVIDENCE OF OIL LEAK. COMPLIED WITH INFO NOTICE 2017-T015 SECTION B2. ACCOMPLISHED LEVEL A DECONTAMINATION NO ODOR PRESENT WITH HFeb 14, 2025 · N629JB · Airbus A320232 · Air Distribution System
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