JASC 5341
Service difficulty reports · 489
Reports filed under 5341 · Fuselage, Wing Attach Fittings, newest first.
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 jasc_code = '5341' 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.
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 jasc_code = '5341' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR GTIA2023020136961Rib · wornWEAR ON INTERCONNECTING STRUT FITTING ON RH WING RAF-01 3102842-02 GENERATED-RAF 3102842-02 NOT REQUIRED AS RAF 3102833-02 PREVIOUSLY GENERATED ADDRESSES THIS DISCREPANCY.SDR GTIA2023020136960Stringer · corrodedCORROSION STRINGER 42L LOCATED BTW FR 54 TO FR 55 IN AFT CARGO COMPARTMENT RAF-01 3102842-01 GENERATED-PERFORMED PERMANENT REPAIR ON STRINGER 42L LOCATED BETWEEN FRAME 54 TO FRAME 55 IN AFT CARGO COMPARTMENT IAW EA # 53-0640-22 AND EC NO. EO 5341-2301. REPAIR SDR GTIA2023020136956Stringer · corrodedCORROSION FOUND ON STR 43L BETWEEN FR54 AND FR56 IN AFT CARGO COMPARTMENT. RAF CREATED-PERFORMED PERMANENT REPAIR ON STRINGER 43L LOCATED BETWEEN FRAME 54 TO FRAME 56 IN AFT CARGO COMPARTMENT IAW EA # 53-0640-22 AND EC NO. EO 5341-2301. REPAIR CATEGORY "A" SDR WX0A2023022231737Unknown · unknownNRC 1000-0060: 35199-5 AFT WET AREA, CORROSION FOUND AROUND NUTPLATE OF L2 FLOOR SILL BEAM NEAR FR 68./AFT WET AREA, L2 FLOOR SILL BEAM NEAR FR 68 REPAIRED AS PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 5, REV. 143 / BAC1503-100096 7075, PO 1763364 HL11VSDR VNAA202301298005Attach Fitting · gougedL/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY .009" DEEP AND 3" IN LENGTH. CORRECTIVE ACTION: REPAIRED L/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0110 REV IR, DATED 01/23/2023.SDR VNAA202301298004Fitting · gougedR/H AFT WING TO FUSELAGE ATTACHMENT FITTING IS GOUGED ON THE AFT I/B EDGE APPROXIMATELY .008" DEEP AND 2" IN LENGTH. CORRECTIVE ACTION: REPAIRED R/H AFT WING FUSELAGE ATTACHMENT FITTING IAW OLIVER WYMAN EA 23-C7-57-0111 REV IR, DATED 01/23/2023.SDR WX0A1900010031720None · noneNRC 1000-0127: (338-01) AFT CARGO COMPARTEMENT, CORROSION FOUND ON STRINGER 43L BTW FR 53 AND FR 54 (LOWER FLANGE, UPPER SURFACE)/AFT CARGO COMPARTMENT, STRINGER 43L BTW FR 53-54 FOUND OUT OF LIMITS PER SRM 53-41-13-283-002 REV.143, MORE THAN 10% MATERIAL REMOSDR SWIA202301023None · damagedFRETTING ON WING PLANK AT ACCESS HOLE PANEL LANDING FOR FUEL PANEL 510AB (C-CHECK RO 2/26/2023) BLENDED WITHIN LIMITS, WING PLANK LANDING FOR 510AB PANEL REF REO 601R -57-21-030 REV L DATED 2014-02-05ORIGINAL MATERIAL 0.182" , REMAINING 0.179", REMOVEDSDR WX0A2023020331723Not Entered · not enteredNRC 1000-0060: 35199-5 AFT WET AREA, CORROSION FOUND AROUND NUTPLATE OF L2 FLOOR SILL BEAM NEAR FR 68. / AFT WET AREA, L2 FLOOR SILL BEAM NEAR FR 68 REPAIRED AS PER SRM 53-41-14-300-001, REPAIR PRINCIPLE 5, REV. 143 BAC1503-100096 7075, PO 1763364 HL11VFSDR DALA2023050503527Unknown · unknownSHIP 3241 NEED TO COMPLY WITH DTA MONITOR CRACK INSPECTION. CORRECTIVE ACTION: COMPLIED WITH ERA 602461-14AD REV. A. (2487972)SDR A6WA202210258413Fitting · chafedLEFT WING TO FUSELAGE FITTING HAD WEAR. AIRCRAFT REMOVED FROM SERVICE. BLENDED THE TWO AREAS OF DAMAGE TO A SMOOTH CONTOUR 1.0"L X 0.300"W X 0.002"D AND 1.200"L X 0.090"W X 0.007"D IAW EA AWAC-CRJ252-01927 REV A. ACCOMPLISHED HFEC INSPECTION AT BLEND AREASSDR CALA2022101402815None · crackedWHILE WORKING EA 5340-01724 REV C OP002 STEP 3.1. NDT NOTED A CRACK INDICATION IN DOORSTOP FITTING 1 BOTTOM IB HOLE AT 4:00 POSITION FACING AFT FRAME 68 LH. (REF LP 9682403 ? PREVIOUSLY CLEARED IN ERROR) -12-300-008. INSTALLED FITTING PER SRM 52-13-31-400-022-SDR CALA2022101202775Flange · crackedCRACK INDICATION FOUND ON WEB HORIZONTAL FLANGE RADII LOWER POSITION OF FR.68 STR.22R L=0.787 INCH APPROX. SEE AEROMAN NON ROUTINE 2022-359838 22 PER PART 2A OF THE LATEST REVISION EC/RA 5341-01339 ON OR INSPECTION ON THE FASTENER HOLE AND EXTERNAL SURFACES OFSDR CALA2022101202774Frame · crackedCRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 12 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-359849 PER PART 2.A OF THE LATES REV. EC/RA 5341-0SDR CALA2022101202772Stop Fitting · unknownFOUND DISCREPANT HOLE SIZES CANNOT BE VERIFIED WITH A PREVIOUSLY APPROVED REPAIR ON LH FR 68 AFT DOOR STOP FITTING SEE AEROMAN NON ROUTINE 2022-360056 B. GENERATE A DIP LOGPAGE TO ACCOMPLISH REACHES 50,045 TOTAL A/C (FC) PERFOM REPEAT REVISION OF EC/RA# 5341-0SDR CALA2022101002752Beam · corrodedCORROSION FOUND ON RH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818030010 PERFORMED REMOVAL OF CORROSION PER SRM 51074-00 REV 142. REWORK CATEGORY "A" PER SRM 53-41-14-300-001 REPAIR PRINCIPLE 5 REV 142 DIMENSIONS: L=24.SDR CALA2022101002751Beam · corrodedCORROSION FOUND ON LH AFT PAX DOOR SILL BEAM AT FR.68 (A3NB-53-3-6222) SEQ#932 ZONE:200. LTPR NR0050011818070010. PERFORMED REMOVAL OF CORROSION PER SRM 51-74-00 REV 142. REWORK THICKNESS (1.6MM). PERFORMED PERMANENT REPAIR CATEGORY "A" PER DIMENSIONS.REWORK ISDR CALA2022100602691Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4SDR CALA2022093002565None · crackedCRACK INDICATION ON FRAME 68 WEB HORIZONTAL FLANGE AT STGR22 LEVEL LH SIDE, CRACK LENGHT IS 1.218 INCH APPROX, CONTACT ENGINEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308627 NITIAL INSPECTIONS OF RSDR CALA2022093002562None · corrodedCORROSION LOWER SILL LOCATED FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-308753 MEASURES AFTER REWORK WAS L:2.388 INCH W:1.169 INCH, ELECTRONIC CRACK AND CORROSION INDICATION NOT FOUND, IAW SRM A320 53-41-14-283-002 FIGURE 002 SHEET 01, THIS IS CALIPSDR CALA2022092802539Floor Support · noneCORROSION LOWER SILL LOCATED FR66 AND STR 23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-308750 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.66 AND STR. AREA IS: 0.091", NOMINAL THICKNESS ON AREA IS: 0.150" PERFORMED IAW NTM NTM 51-10-02 AND NTM 51SDR CALA2022092802544None · crackedCRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER OUTBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-308621 NITIAL INSPECTIONS OF REPAIRED FITSDR CALA2022092802543None · crackedCRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA SEE AEROMAN NON ROUTINE 2022-308624 NITIAL INSPECTIONS OF REPAIRED FITTINSDR CALA2022092802542None · crackedCRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 9 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308622 NITIAL INSPECTIONS OF REPAIRED FITTISDR CALA2022092802540None · crackedCRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE UPPER OUTBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION IS 3 OCLOCK. REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-308623 NITIAL INSPECTIONS OF REPAIRED FITTSDR CALA2022092802536None · crackedCRACK INDICATION ON FRAME 68 LH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTION ARE 1 AND 5 OCLOCK REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (2 EA). 2022-308620 ITIAL INSPECTIONS OF REPAIRED FITTING INSTALLED ON FRSDR CALA2022092802538None · noneCORROSION LOWER SILL FR67 TO FR68 AND STR23L IN PASSENGER CABIN SEE AEROMAN NON ROUTINE 2022-308752 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.67 TO FR.68 W:1.971IN NOMINAL THICKNESS ON AREA IS 0.315 IN IAW SRM A320 THIS REPAIR CATEGORY A, PERFORMED DSDR WX0A1900010074278None · noneNRC 2000-0027: (338-05) R2 DOOR, LOWER SILL BEAM, CORROSION FOUND AROUND NUT PLATE AT FR 68/R2 DOOR LOWER SILL BEAM AROUND NUT PLATE AT FR68 PERMANENTLY REPAIR AS PER SRM 53-41-14-300-001, PRINCIPLE 5 REV141, REPAIR CATEGORY: A. NO FURTHER ACTION REQUIRED. SEESDR CALA2022092302466None · corrodedFWD CARGO PIT R/H BETWEEN FR 24-29 STRINGER 43R HAS CORROSION AR OUND FASTENERS PER HAECO LCQ N/R 9290359/30359 GEN BY V919150 REMOVED AND REPLACED STRINGER 43 R/H FR 24-29 IAW A320 SRM 51-72 -11-911-001 BY MECH V052030 INSP BY V061771SDR CALA2022092302461None · crackedCRACK INDICATION ON FRAME 68 WEB HORIZONTAL FLANGE AT STGR22 LEV EL RH SIDE, CRACK LENGHT IS 0.768 INCH APPROX, CONTACT ENGINEERI NG FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-308629. NITIAL INSPECTIONS OSDR GTIA2022091336657None · corrodedINSIDE CABIN- AFT WET AREA- DOOR SILL HAS CORROSION AROUND FASTENER HOLE FR 68 - STR 23R. RAF-01 2923870-01 GENERATED-REMOVED CORRODED FASTENER HOLE AFT WET AREA ON DOOR SILL FR68 STRINGER 23R, FAB REPAIR AND INSTALLED REPAIR IAW A321 SRM 53-41-14-300-001SDR CALA2022091202336None · noneREF INSP EA 5340-01724 REV C, REJECTABLE HOLE INDICATTIONS FOR ALL HOLES FOR DOOR STOP #1-7 ON RH FR 66 AND FR68. DOOR STOP HOLES PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01327. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01327. / ON OR BEFORE SDR CALA2022091202334None · noneREF INSP EA 5340-01724 REV C, REJECTABLE HOLE INDICATTIONS FOR ALL HOLES FOR DOOR STOP #1-7 ON LH FR 66 AND FR68. STOP HOLES PER PART 2 OF THE LATEST REVISION OF ECRA 5341-01327. ACCOMPLISHED INTERIM REPAIR PER PART 1 OF ECRA 5341-01327. ON OR BEFORE MARCH 5, SDR CALA2022091202333None · crackedCRACK INDICATION ON FRAME 68 RH SIDE IN OPEN FASTENER HOLE LOWER INBOARD AT DOOR STOP FITTING 1 POSITION, CRACK DIRECTIONS ARE 12 AND 6 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (2 EA) SEE AEROMAN NON ROUTINE 2022-343066 LEVEL REPAIR AREA AT DOOR SSDR CALA2022091202332None · crackedCRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPASDR CALA2022090502280None · corrodedCORROSION LOWER SILL LOCATED FR66 AND STR 23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-308750 PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.66 AND STR. AREA IS: 0.091", NOMINAL THICKNESS ON AREA IS: 0.150" PERFORMED IAW NTM NTM 51-10-02 AND NTM 51SDR CALA2022090502279None · corrodedCORROSION LOWER SILL FR67 TO FR68 AND STR23L IN PASSENGER CABIN. PERFORMED PERMANENT REPAIR ON LOWER SILL LOC. AT FR.67 TO FR.68 W:1.971IN NOMINAL THICKNESS ON AREA IS 0.315 IN IAW SRM A320 THIS REPAIR CATEGORY A, PERFORMED DETAIL VISUAL INSPECTION ON AND STR.SDR CALA2022083102226None · noneCORROSION LOWER SILL LOCATED FR66 AT AFT GALLEY AREA SEE AEROMAN NON ROUTINE 2022-308753 MEASURES AFTER REWORK WAS L:2.388 INCH W:1.169 INCH, ELECTRONIC CRACK AND CORROSION INDICATION NOT FOUND, IAW SRM A320 53-41-14-283-002 FIGURE 002 SHEET 01, THIS IS CALIPSDR WX0A1900010074258None · noneNRC 2000-0082: 429-90 DURING SPECIAL DETAILED INSPECTION OF THE DOOR STOP FITTINGS HOLES AT AFT PASSENGER/CREW DOOR, ONE CRACKED FOUND AT L2 DOOR FR 68 FITTING NO.1 LOWER I/B HOLE./FR 68, DOOR STOP FITTINGS NO.01, LOWER I/B HOLE REPAIRED AS PER SRM 53-41-12-3SDR YENA2022083000832Frame · corrodedDURING HEAVY MAINTENANCE: FUSELAGE - REAR / AFT LAVATORY VENT / FR 68-70 & STGR 31R-32R / CORROSION DAMAGE. TEMPORARY REPAIR (CONSIDERED AS A MAJOR REPAIR)SDR YENA2022083000845Exhaust Vent · corrodedFLT#1197, PVD-FLL. ' REF L/P 3424078 (ON WALK AROUND FOUND EVIDENCE OF CORROSION AROUND LAV WASTE EXHAUST.). ON WALK AROUND FOUND EVIDENCE OF CORROSION AROUND LAV WASTE EXHAUST; REPAIRED LAV WASTE EXHAUST PER SRM 53-41-11-300-004. AIRCRAFT FOUND TO BE IN AIRWOSDR CALA2022081902119Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 RH SIDE, CRACK LENGHT IS 0.810 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1EA). SEE AEROMAN NON ROUTINE 393710. A32 0 SRM 53-41-12-30SDR CALA2022081902118Frame · crackedCRACK INDICATION ON FRAME 68 AFT FACE HORIZONTAL WEB AT LEVEL OF STGR 22 LH SIDE, CRACK LENGHT IS 0.700 INCH APPROX, CONTACT ENGI NEERING FOR REPAIR INSTRUCTIONS BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA). SEE AEROMAN NON ROUTINE 2022-393711. A32 0 SRM 53-4SDR CALA2022081902124Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.SEE AEROMAN NON ROUTINE 2022-343198 REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA:L=0.604 IN W=0.485 IN;D=0.079 IN, NOMINAL THICKNESS= SILL PERFORMED VISUAL ISDR CALA2022081702112Frame · crackedCRACK INDICATION ON FRAME 66 LH SIDE IN OPEN FASTENER HOLE LOWER IN BOARD AT DOOR STOP 1 POSITION, CRACK DIRECTION IS 2 OCLOCK, REPAIR BEFORE NEXT FLIGHT AT AFT GALLEY AREA (1 EA) SEE AEROMAN NON ROUTINE 2022-343324 INSPECTION THRESHOLD FROM TIME OF ADL/REPASDR CALA2022081602072Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 LEVEL STRG23L IN PASSENGER CABIN.REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 AT LEVEL POINT AREA.SDR CALA2022081202037Frame · corrodedCORROSION LOWER SILL FR 66 RH SIDE AT AFT GALLEY AREA, SEE AEROMAN NON ROUTINE 2022-293845 PERFORMED PERMANENT REPAIR ON LOWER SILL RH SIDE AT AFT GALLEY L=2.755IN, W=1.984IN, D=0.087IN, EDDY CURRENT DONE ON REWORKED ULTRASONIC THICKSNESS MEASURES ON REWORKED SDR CALA2022080501964Beam · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREASDR CALA2022080501959Doubler · misrepairedA3NB-51-4-6001 TOILET VENT DOUBLER LOCATED FR69-70 STR 30-33R DOES NOT COMPLY WITH CFR 121.1109 PER AMM 51-00-80-200-801C1 FLOW CHART 1 STEP 3 NO REPAIR DATA FOUND.() REMOVED AND REPLACED TOILET VENT DOUBLER IAW SRM 53-41-11-300-00 4 CAT A MAJOR REPAIR. EMP# VSDR CALA2022072901913Channel · corrodedCORROSION LOWER SILL LOCATED FR66 TO FR68 R/H SIDE AT AFT GALLEY AREA REMOVED AND REPLACED LOWER SILL LOCATED FR66 TO FR68 R/H SIDE CORRODED AREAS ARE:DEEPEST POINT L=3.980 IN W=2.049 IN D=0.055 IS 9151970.SEE AEROMAN NON ROUTINE 2022-343194 AT AFT GALLEY AREA
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