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 GTIA2022011036211None · noneFA "C" FLASHLIGHT INOP-REMOVED AND REPLACED FLASHLIGHT AT FA "C" POSITION IAW AMM 25-65-00.Jan 7, 2022 · N632NK · Airbus A320232 · Escape SlideSDR GTIA2022011036210None · dentedDENT CAUSED BY BIRD STRIKE ON FUSELAGE BELOW F.O.S SLIDING WINDOW BETWEEN FRAM 5&6 ,ZONE 1, CODE C. RAF 01 CREATED-REPAIRED DENTED FUSELAGE SKIN BELOW FO'S SLIDING WINDOW FR 5-6 IAW A320 SRM 53-11-11-300-011, REPAIR REQUIRES RE INSP AT 60,000/120,000 FH SUBSIQJan 7, 2022 · N617NK · Airbus A320232 · Fuselage Structure (General)SDR AALA202201100284Power Supply · inoperativeAIRCRAFT WAS NOT GROUNDED: EMERGENCY LIGHTS INOPERATIVE AFT GALLEY. REPLACED AFT GALLEY EMERGENCY POWER SUPPLY UNIT AND ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK PER AMM 33-50-00.Jan 7, 2022 · N660AW · Airbus A320232 · Emergency LightingSDR CALA2022011000080None · crackedL/H FR 16 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A AFT REACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPEC " REFF VT MAE NRC 0020933 FOR WORK PERFORMED. 2A OF LATESJan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000079None · crackedR/H FR 16 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #3 D AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2A OF ACHES 39,510 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONS VT MAE NRC 0020971 FOR WORK PERFORMED. LATEST REVISION OF EC/RAJan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000078None · none(A3NB-21-3-6032) WATER FOUND COMING FROM LAV DRAINS BETWEEN FR 8 THRU FR21.() ACCOMPLISHED ECRA 2011-01000 "SPILLAGE WAS ONLY POTABLE WATER" E MP# V936637 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOB ILE AT BFM ON NR# 0021202.Jan 7, 2022 · N466UA · Airbus A320232 · Cabin Equipment/FurnishingsSDR CALA2022011000077None · crackedL/H FR 20 DOORSTOP FITTING #1 HAS CRACK INDICATION NOTED IN HOLE #1 & #3 READ AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B REACHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTION FF VT MAE NRC 0020973 FOR WORK PERFORMED. OF LATEST REVISJan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000076Fitting · crackedWHILE AT VT AREOSOACE BFM DURING C-1 CHECK REF NR0021094 ROTO PROBE OF RH FR66 #5 DOOR STOP FITTING HOLE D1 FOUND CRACK INDICA TION. PLUG & WASHER IAW SRM 53-73-12-001. RE-INSTALLED DOORSTOP FITTIN EMBODIMENT 33000FC (FH NOT RELAVENT) SUBSEQUENT INSP AT INTERVJan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000075Intercostal · corrodedL/H FR 20 DOORSTOP FITTING #7 HAS CRACK INDICATION NOTED IN HOLE #3 AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L AS FOLLOWS: "ACCOMPLISH INSPECTION REQUIREMENTS PER PART 2B OF L CHES 40,010 TOTAL FLIGHT CYCLES. ACCOMPLISH REPEAT INSPECTIONSJan 7, 2022 · N466UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000074None · none(AD 2018-03-12) L/H FR66 DOOR STOP #6 TOP I/B HOLE HAS OVALITY.( ) REPAIRED LH FR66 DOOR STOP #6 IAW EC/RA 5341-01293 EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBILE AT BFM O N NR#0018943Jan 7, 2022 · N471UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022011000073None · none(AD 2018-03-12) L/H FR66 DOOR STOP #7 TOP AND BOTTOM O/B HOLES H AVE OVALITY. DOOR STOP #3 BOTTOM I/B HOLE HAS A REJECTABLE DAMAG E INDICATION. DOOR STOP #1 TOP O/B HOLE HAS A CRACK INDICATION,B OTTOM O/B HOLE HAS OVALITY REPAIRED L/H FR66 DOOR STOPS IAW EC/RAJan 7, 2022 · N471UA · Airbus A320232 · Fuselage Structure (General)SDR CALA2022011000068None · cracked(AD 2018-03-12) R/H SIDE FR66 DOOR STOP #7 TOP I/B HOLE HAS A CR ACK INDICATION. DOOR STOP #3 BOT I/B HOLE HAS REJECTABLE DAMAGE INDICATION.() REPAIRED R/H FR66 DOOR STOP #7 IAW EC/RA 5341-01293 EMP# V935774 WORK ACCOMPLISHED AT ST ENGINEERING AEROSPACE OF MOBJan 7, 2022 · N471UA · Airbus A320232 · Fuselage Structure (General)SDR AALA202201119522Hinge Fitting · corrodedAIRCRAFT IN BASE MAINTENANCE: LEFT HORIZONTAL STABILIZER REAR SPAR AREA - # 5 ELEVATOR HINGE BEARING IS CORRODED. REPLACED HINGE FITTING PER AMM 55-16-42-400-001-A.Jan 6, 2022 · N604AW · Airbus A320232 · Horizontal Stabilizer StructureSDR YENA2022010700014Oil System · leakingFLT 1796, CUN-FLL. INFLIGHT REPORTED A CHEMICAL OR FUME-TYPE SMELL. IT WAS INTERMITTENT ON GROUND AND ON DESCENT AT 6000 MSL AT LEAST 3 SEPARATE TIMES ; PERFORMED INSPECTION IAW INFO NOTICE 2017-T015I. FOUND EVIDENCE OF APU OIL LEAK AND SOURCE OF ODOR EVENT. RJan 6, 2022 · N561JB · Airbus A320232 · APU Oil SystemSDR YENA2022010700013Coffeemaker · failedFLT 379, DCA-FLL. VERY FAINT BURNING SMELL FROM FORWARD GALLEY BY COFFEE MAKER DURING DESCENT. DISSIPATED AFTER LANDING COFFEE MAKER WAS ON (MX-270 ATTACHED). ( COFFEE MAKERS ) ; INSP FOUND FWD COFFEE MAKER 106 HEATING PLATE BURNT OUT CAUSING ODOR PLACED ON NEJan 6, 2022 · N535JB · Airbus A320232 · Buffet/GalleysSDR CALA2022010700066Stop Fitting · crackedRH-FR66, DOOR STOP #1, LOWER INBOARD HOLE HAS CRACK INDICTION.() SUPPORT TASK AD 2018-03-12. R/H FR66 #1 LOWER I/B HOLE. REPAIED AND REAMED IAW SRM 53-41-12- ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERING AEROSP 300-10. ORG REAMED .394 FINAL DIA. .4Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700065Stop Fitting · crackedRH-FR66, DOOR STOP #4, UPPER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #4 DOOR STOP UPPER I/B HOLE. REPAIRED AND REAMED IAW SR FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI M 53-41-12-300-10. ORG. REAMED .394 Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700064Drain · leakingWITHIN 36 MONTHS, ACCOMPLISH ECRA 2011-01000, CARGO COMPARTMENT SPILL SECTION 2.C. SUPPLEMENTAL INSPECTION,IN THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRINGERS 10 AND STRINGER 12. THE AREA FROM BODY STATION 8 TO BODY STATION 21 BETWEEN STRINGJan 6, 2022 · N466UA · Airbus A320232 · Ice/Rain Protection SystemSDR CALA2022010700063Stop Fitting · crackedRH-FR66, DOOR STOP #5, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12 R/H FR66 #5 DOOR STOP LOWER HOLE. REPAIRED AND REAMED IAW SRM 53 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGINEERIN -41-12-300-10. ORG. REAMED .394 FIN Jan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700062Stop Fitting · crackedRH-FR68, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION.( ) SUPPORT TASK AD 2018-03-12. R/H FR68 #6 DOOR STOP LOWER I/B HOLE REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED EMP# V934344 WORK ACCOMPLISHED AT ST ENGIN 53-41-12-300-10 ORG. REAMED .394 FIJan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700061Stop Fitting · crackedRH- FR66, DOOR STOP #6, LOWER INBOARD HOLE HAS CRACK INDICATION. () SUPPORT TASK AD 2018-03-12 R/H FR66 #6DOOR STOP LOWER I/B HOLE. REPAIRED AND REAMED IAW SRM FORM 44-0008 ATTACHED. EMP# V934344 WORK ACCOMPLISHED AT ST ENGI 53-14-12-300-10. ORG. REAMED .394 FJan 6, 2022 · N466UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700060Frame · corrodedFWD CARGO FR33 STR40L-STR41L HAS CORRODED CLEAT REMOVED AND REPLACED CLEAT AT FR33 STR40L-STR41L IAW ARM 51-75-1 2-911-001 ADD EMP:V052030Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022010700058Stringer · crackedLH SIDE FRAME 68 AT STR22 INNER CAP AND WEB FLANGEIS CRACKED. CR ACK ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, AFT SIDE, I N AND ABOVE RADIOUS. CRACK APPROX 2.25" WITH ENDS MARKED IN BLAC K. L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE. ACCOMPLJan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022010700057Stringer · crackedL/H FR35 STR30L HOLE #3 HAS CRACK INDIACTIONS AT THE 2:00. 3:00, AND 4:00 POSITIONS. REF HAECO N/R 9294150 FOR REFERENCE. #3 FINIAL HOLE SIZE .199". ACCOMPLISH INITIAL INS THE LATEST OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE 59,68 HOURS, WHICHEVER COMES Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, Longeron/StringerSDR CALA2022010700056Frame · crackedL/H FR35 STR 30 HOLES #2 HAS CRACK INDACTIONS AT THE 5:00, 6:00, AND 11:00 POSITIONS CONTACT ENGINEERING FOR REPAIR INSTRUCTION BEFORE NEXT FLIGHT. FOR A REFERENCE FOR #2 HOLE. FINIAL HOLE SIZE .250". ACCOMPLISH OF THE REVISION OF ECRA 5331-02825 ON OR BEFORE Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022010700055Door Frame · crackedL2 DOOR FRAME 68 DOOR STOP FITTING #1 LOWER INBOARD HOLE IS CRAC KED IN THE FRAME WEB AT 5:00 AND 10:00 POSITION. REO-L23516 REV IR IS INCLUDED AS APPENDIX A FOR REFERENCE.#3 HOL REPAIR ON THE FR68 DOOR STOP #1 AND STR 22 FLANGE PER PART 3 OF E START DIA .269"Jan 6, 2022 · N484UA · Airbus A320232 · Fuselage Main, StructureSDR CALA2022010700049Shear Tie · corrodedFWD CARGO FR29 STR43R-STR42R CLEAT IS CORRODED. REMOVED AND REPLACED CLEAT IN FWD CARGO FR 29 STR43R-STR42R IAW S RM 51-42-17.Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2022010700048Shear Tie · corrodedFWD CARGO FR33 STR41R-STR42R HAS CORRDED CLEAT. REMOVED AND REPLACED CLEAT IN FWD CARGO FR 33 STR41R-STR42R IAW ARM 51-77-11.Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2022010700047Shear Tie · corrodedFWD CARGO FR33 STR40R-41R HAS CORRDED CLEAT. REMOVED AND REPLACED CLEAT IN FWD CARGO FR33 STR40R-STR41R IAW 5 1-72-11.Jan 6, 2022 · N435UA · Airbus A320232 · Standard Practices/StructuresSDR CALA2022010700046Shear Tie · corrodedFWD CARGO FR33 STR41L-STR42L HAS CORRODED CLEAT. REMOVED AND REPLACED VLEAT AT FR 33 STR41L AND STR42L IAW SRM 51 -42-11-511-001.Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2022010700045Shear Tie · corrodedFWD CARGO FR33 STR42L-STR43L HAS CORRODED CLEAT. REMOVED AND REPLACED CLEAT AT FR 33 STR42L-STR43L IAW SRM 51-75- 12-911-001.Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR CALA2022010700043Shear Tie · corrodedFWD CARGO FR33 STR40L-STR41L HAS CORRODED CLEAT REMOVED AND REPLACED CLEAT AT FR33 STR40L-STR41L IAW ARM 51-75-1 2-911-001 ADD EMP:V052030Jan 6, 2022 · N435UA · Airbus A320232 · Fuselage Internal Mounting StructureSDR YENA2022031400192Window Post · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING RH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1EA); REMOVED AND REPLACED CONTINUITY FITTING RH (1E/A) AND FASTENERS LOC. BTW FR1 TO FR2 WIJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2022031400191Pressure Blkhd · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 35 TO PRESSURE BULKHEAD ATTACHMENT AREA FWD FACE AT FASTENER HOLE LOCATED 1 INCH BELOW ST30LH LEVEL, CRACK DIRECTIONS ARE 3 AND 9 OCLOCK, CRACK LENGTH ARE L1=0.375 INCH APPROX, L2=0.28 0 INCH APPROX IN FWD CAJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2022031400190Frame · crackedDURING HEAVY MAINTENANCE, CRACK INDICATION ON FRAME 2 WINDSHIELD CENTER POST LOWER ATTACHMENT CONTINUITY FITTING LH SIDE, CRACK LENGTH IS 0.250 INCH APPROX IN COCKPIT (1 EA); ACCOMPLISHED THE REPAIR OF THE (1) CRACK IN THE LH WINDSHIELD FRAMING NEAR THE CENTERJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, StructureSDR YENA2022031400189None · noneDURING HEAVY MAINTENANCE, (E/C A21-1370-01) WINGS / CENTER WING BOX / UPPER SKIN PANEL / UPPER SURFACE / FRAME 41-42 / STIFF 17 / CORROSION DAMAGE - PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)Jan 5, 2022 · N506JB · Airbus A320232 · Wing SparSDR YENA2022031400188Bulkhead · crackedDURING HEAVY MAINTENANCE, (E/C A21-1362-01) FUSELAGE / CENTER FUSELAGE / FR 35 & STR 30L / BULKHEAD / CRACKS AT FASTENER HOLES – PERMANENT REPAIR (CLASSIFIED AS A MAJOR REPAIR)Jan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, BulkheadSDR YENA2022031400187Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN LOC. BTW FR41 TO FR42 ON STIFFENER 17 L/H SIDE IN CENTER FUEL TANK (CPCP RELATED MPD TASK; "EVALUATED REWORKED AREA LOCATED ON EXTERNAL SKIN BTW FR41 TO FR42 ON STIFFENER 17 LH IN CENTER FUEL TANK AND FOUND OUTJan 5, 2022 · N506JB · Airbus A320232 · Wing Main, Frame StructureSDR YENA2022031400186Skin · corrodedDURING HEAVY MAINTENANCE, CORROSION EXTERNAL SKIN LOC. AT LEVEL FR42, 1.500 IN OUTBOARD SIDE OF Y1292 IN CENTER FUEL TANK (CPCP RELATED MPD); ACCOMPLISHED REPAIR OF CORROSION AFFECTED AREA FOUND ON RH WING BOTTOM SKIN UPPER SURFACE AROUND RIB.Jan 5, 2022 · N506JB · Airbus A320232 · Wing Main, Frame StructureSDR YENA2022031400185Tie Clip · corrodedDURING HEAVY MAINTENANCE, CORROSION INTERNAL STRUCTURE TIE CLIP LOCATED AT FR 32 AND BTW STR 41R AND 42R IN FWD CARGO COMPARTMENT; REMOVED AND REPLACED TIE CLIP IAW A32O SRM 51-72-11-911-001 AND DWG D53232982Jan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, FrameSDR YENA2022031400184Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y464.8 BTW FR 64-67 AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y464.8 LOCATED BTW FR64-67 AT AFT GALLEY AREA IAW SRM A320-51-72-11 & DWG D53472040 SHEETS 2;10;12. REF. AEROMAN WO 1138762 NR 2021-499923 Jan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022031400183Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM -Y765 BTWN FR 64-66 AT AFT GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y765 BTWN FR 64-66 AT AFT GALLEY IAW SRM A320-51-72-11 AND DRWG D534 72816 SHEET 2; SHEET 3; DWG D53472000 SHEET 24. REF. AEROMAN W/O 113876Jan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022031400182Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM - Y1292 LOCATED BTW FR 12-24 AT FWD. GALLEY AREA; REMOVED AND REPLACED FLOOR BEAM -Y1292 LOCATED BTWN FR 12-24 AT FWD. GALLEY AREA IAW A320 SRM 51-72-11 & DWG. D53110984 SHEET 1; DWG. D53112812 SHEET 2;D53110876 SJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022031400181Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y1292 LOCATED BTWN FR 12-24 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01); REMOVED AND REPLACED FLOORBEAM+Y1292 LOCATED BTWN FR12-24 AT FWD. GALLEY AREA IAW A320 SRM 51-42-11;SRM 51-72-11 AND DWG D5311281Jan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022031400180Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOOR BEAM +Y503.2 LOCATED BTWN FR 12-16 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01); REMOVED AND REPLACED FLOOR BEAM +Y 503.2 LOCATED BTWN FR 12-16 AT FWD FWD. GALLEY AREA IAW A320 SRM 51-42-11 AND SRM 51-72-11 ANJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022031400179Floorbeam · corrodedDURING HEAVY MAINTENANCE, CORROSION FLOORBEAM +Y765 LOCATED BTWFR12-24 AT FWD. GALLEY AREA (CPCP RELATED MPD TASK 531189-01; REMOVED AND REPLACED FLOORBEAM +Y765 LOCATED BTWN FR12-24 AT FWD. GALLEY AREA IAW A320SRM 51-42-11;51-72-11 AND DRWG D53112812. REF. AEJan 5, 2022 · N506JB · Airbus A320232 · Fuselage Main, Floor BeamSDR YENA2022010700011Transfer Valve · closedFLT 1434, SJU-FLL (DIVERTED TO MCO). NOTICED DURING CRUISE THAT THE FUEL TRANSFER VALVES HAD LATCHED CLOSED, AS PER MEL 28-15-01C, THOSE VALVES WERE LATCHED OPEN AND SHOULD HAVE STAYED OPEN FOR THE DURATION OF THE FLIGHT.; REF MDDR C/N 460173, ACCOMPLISHED MX Jan 5, 2022 · N653JB · Airbus A320232 · Aircraft Fuel Distribution SystemSDR CALA2022010700037Frame · crackedLH SIDE FRAME 68 AT STR 22 INNER CAP AND WEB FLANGE IS CRACKED. CRACK LOCATED ABOVE THE LOWER MOUNT HOLES OF THE #1 DOOR STOP, A FT SIDE, IN AND ABOVE RADIUS. CRACK APPROX 2.25" WITH ENDS MARKE D IN BLACK. L2 DOOR DRAME 68 DOOR STOP FITTING #1 LOWER I/B HOLE IJan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR CALA2022010700036Frame · crackedL/H FR35 STR30L HOLE #2 HAS CRACK AT THE 5:00, 6:00, AND 11:00 P OSITIONS. HOLE #3 HAS CRACK INDICATIONS AT 2:00, 3:00, AND 4:00. #1 HAS CRACK INDICATIONS AT 5:30 AND 6:30 POSITIONS. PER HAECO LCQ NR 9294149/22149, 9294150/22150, 9294148/22148. GENERATED BY V0Jan 5, 2022 · N484UA · Airbus A320232 · Fuselage Main, FrameSDR GTIA2022010636207Bottle · low pressureL1 DOOR EMER ASSIST BOTTLE REQ SERVICING-SERVICED L1 DOOR EMER ASSIST BOTTLE IAW AMM 52-10-00.Jan 5, 2022 · N640NK · Airbus A320232 · Emergency Equipment
Back to Airbus A320-232