JASC 5340
Service difficulty reports · 22,411
Reports filed under 5340 · Fuselage Main, 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 = '5340' 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 = '5340' 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 UPS06846403Fitting · crackedINSPECTION TYPE:C1 ATTACH FITTING CRACKED AT STA 1160 L19R AFT SIDE. REMOVE AND REPLACE FITTING IAW SRM 51-1-20D.SDR UPS06846395Fitting · crackedINSPECTION TYPE:C1 FITTING CRACKED AT STA 834.500 L22R. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR UPS06846355Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA 902.125 L4L. REMOVED AND REPLACED END FITTING AT STA 902.125 L4L IAW SRM 51-1-20D, 51-3-0 AND SRM 51-1-21.SDR UPS06846354Fitting · crackedFOUND FITTING CRACKED AT STA 820 L18L . REMOVED AND REPLACED END FITTING AT STA 820 L18L IAW SRM 51-1-20D, 51-03-02-0 AND SRM 51-01-08-0.SDR UPS06846339Fitting · crackedFOUND ATTACH FITTING CRACKED AT STA 1150 L18R. REMOVED, FABRICATED AND INSTALLED FITTING IAW SRM 51-1-20D.SDR UPS06846334Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA.857.125 L9L. REMOVED AND REPLACED END FITTING IAW SRM 51-1-21 AND 51-1-20D.SDR UPS06846331Fitting · crackedFOUND LONGERON END FITTING CRACKED AT STA 680 L5R. REMOVED AND REPLACED LONGERON END FITTING AT STA 680 L5R IAW SRM 51-01-21, 51-03-02-0 AND SRM 51-01-20D.SDR UPS06846330Fitting · crackedFOUND LONGERON END FITTING AT STA 902.125 L8R IS CRACKED. REMOVED AND REPLACED LONGERON END FITTING AT STA 902.125 L8R IAW SRM 51-1-21, 51-1-20D, AND SRM 51-3-0.SDR UPS06846329Fitting · crackedLONGERON END FITTING CRACKED AT STA 857.125 L7L. REMOVED AND REPLACED LONGERON END FITTING AT STA 857.125 L7L IAW 51-3-2 AND SRM 51-1-20D.SDR 2006UALA00297Support Fitting · crackedAFT CABIN FRAME SUPPORT FITTING HAS CRACK AT STA 727 STR 14R. *S/D* REMOVED DAMAGE, FABRICATED, DRILLED AND INSTALLED REPAIR PARTS REF EA NR I060081.SDR 2006UALA00296Support Fitting · crackedAFT CABIN FRAME SUPPORT FITTING HAS CRACK AT STA 727 STR 14L. *S/D* REMOVED DAMAGE, FABRICATED, DRILLED AND INSTALLED REPAIR PARTS REF EA NR I060082.SDR ASOA06201Clip · crackedDURING C-CHECK, THE CLIP ON RT FS 461, RBL9 OB PRESSURE FLOOR AREA, WAS FOUND TO BE CRACKED.SDR ASOA06200Clip · crackedDURING AC-CHECK, THE CLIP ON THE FORWARD FACE 654 WAS FOUND TO BE CRACKED. THIS MRR WILL REMAIN OPEN PENDING MAINTENANCES DETERMNATION OF AN APPROPRIATE CORRECTIVE ACTION. (K)SDR 06FDEA0700Stringer Clip · corrodedINTERIOR FUSELAGE, STR CLIP 4R HAS CORROSION BS 720A. REMOVED CORRODED STR CLIP & WILL BE REPLACED ON N00343.SDR 06FDEA0699Stringer Clip · corrodedCORROSION ON STRINGER CLIP AT BS 720B STR 4 RT. REPLACED STR CLIP PER SRM 51-30-2.SDR ASAA0640164Stringer Clip · crackedSTRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP PER SRM 51 40 02.SDR 06FDEA0689Stringer Clip · damagedSTRINGER CLIP AT BS 400 STR 7 LT HAS MECHANICAL DAMAGE. REMOVED AND REPLACED STRINGER CLIP AT BS 400 STR 7 LT PER SRM 51-30-2, 51-30-5, 51-30- 6.SDR ABXA060139Fitting · corrodedWHILE REMOVING LONGERON 24 RIGHT AT STA 5 - 25 THE END FITTING AT STA 70 WAS NOTED TO HAVE CORROSION. REMOVED AND REPLACED END FITTING. FITTING FABRICATED IAW ABX REA D853-53189 ON ITEM YY-985.SDR AWXA200600585Stringer Clip · crackedMCN - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED, 0.25 INCHES, AT BS 663 TO STR 10R. MAINTENANCE REMOVED CRACKED CLIP AT BS 663 TO STR 10R IAW BOIENG 737-300 SRM 51-40-02-0G FIGS 8 AND 12. INSTALLED NEW CLIP AT BS 663 TO STR 10R IAW BOEING 73SDR AWXA200600582Clip · crackedMCN - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED, 0.35 INCHES AT BS 639 STR 1. MAINTENANCE REMOVED CRACKED CLIP AT FRAME BS 639 STR 1 IAW BOEING 737-300 SRM 51-40-02-0G FIGS 8 AND 12. INSTALLED NEW CLIP AT FRAME BS 639 STR 1 IAW BOEING 737-30SDR AWXA200600556Stringer Clip · crackedMCN - DURING C22 CHECK DISCOVERED CRACKED STRINGER TIE CLIP, CRACKED .25 INCHES, AT BS 639 STR 2R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP AT BS 639 STR 2R IAW BOEING 737-300 SRM 51-40-02-0G.SDR AWXA200600555Stringer Clip · crackedMCN - DURING C22 CHECK DISCOVERED STRINGER CLIP CRACKED, .400 INCHES IN LENGTH, AT BS 616 AND STR 2L. MAINTENANCE REMOVED AND INSTALLED NEW CLIP AT BS 616 AND STR 2L IAW BOEING 737-300 SRM 51-40-02-0G FIG 8 AND 12.SDR AWXA200600550Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED STRING 10L CLIP CRACKED, .375 INCHES, AT BS 663. MAINTENANCE REMOVED AND REPLACED THE STRINGER TIE CLIP AT STR 10L AND BS 663 IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 6, 7, AND 8.SDR AWXA200600547Stringer Clip · crackedMCN - MAJOR REPAIR - DURING C22 CHECK DISCOVERED STRINGER TO FRAME CLIP CRACKED, .4 INCHES, AT BS 639, STR 4R. MAINTENANCE REMOVED AND INSTALLED NEW STRINGER TIE CLIP ON FRAME AT BS 639 AND STR 4R IAW BOEING 737-300 SRM 51-40-02-0G FIGURES 3, 6, 7, AND 8.SDR UPS06846408Fitting · crackedINSPECTION TYPE:C2 END FITTING IN C-PIT CRACKED AT STA 1150 L35R. REMOVED AND REPLACED END FITTING IAW SRM 51-1-20D.SDR ABXA060092Fitting · crackedFITTING CRACKED FORWARD OF INBOARD DOOR ACTUATOR. REMOVED AND REPLACED FITTING IAW DC9 SRM 51-30-5.SDR ASOA06176Clip · crackedDURING C-CHECK, THE LT FS 484 CLIP, ON THE OB SIDE WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE LT FS 484 CLIP, ON THE OB SIDE IAW EO. (K)SDR ASOA06171Clip · crackedDURING C-CHECK, THE LT AND RT 625 CLIPS, NEAR STR 14, WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE WILL REMOVE AND REPLACED THE LT AND RT 625 CLIPS, NEAR STR 14, IAW REO. (K)SDR UPS06446343Fitting · wornFOUND FUS BS 1000 S39R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 1000 STR 39R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND EO B747-5310-18579-F FIG 10.SDR UPS06446341Fitting · wornFOUND BS 1000 S37R END FTG CROSS MOUNT BOLT AREA WORN OUT. BS 970- BS 983 STR 37R REPAIRED AS PER SRM 53-10-03 FIG 1 AND STR 37R END FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 & EO NR B747-5310-18579 APPENDIX 'F' FIG 10.SDR 06FDEA0648Fitting · crackedCOMPLY WITH AGING 9-AGING-INSP, FWD MDCC UTILITY AREA SUSPECTED OF CRACK AT FLOORBEAM CONNECTION FITTING AT FRAME 12A RT.SDR 06FDEA0647Fitting · crackedFWD MDCC UTILITY AREA SUSPECT A CRACK AT FLOORBEAM CONNECTION FITTING AT FRAME 12A LT.SDR UPS06446311Clip · crackedBS 480 STR 11L FRAME FWD AND AFT FACE ATT CLIP FASTENER HOLES FOUND ELONGATED. CRACK LENGTH 3/8". FWD AND AFT ATT CLIPS 2 REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06446308Stringer Clip · crackedBS 500 STR12L FRAME FWD FACE ATT TIE CLIP FOUND CRACK. CRACK LENGTH 1/4". TIE CLIP REPLACED AS PER SRM 51-10-01 PG9 AND INSTALLED AS PER SRM 51-30 -02.SDR QXEA200600554Bracket · missingYYC C3, FUSELAGE INTERIOR, FUSELAGE STATION 364, STRINGER 15L, BRACKET IS MISSING AT PANEL ATTACHMENT MEMBER. REPAIRED IAW CRJ700 SRM 51-42-06-001-001-A01 AND HORIZON AIR EA R-53-435.SDR F3LA200600007Attach Fitting · corrodedDURING REMOVAL OF FLOOR PANEL 262EF FOR DISCREPANCY REGARDING AFT LAVATORIES, MAINTENANCE REPORTED L-2 DOORWAY FLOOR PANEL AFT ATTACH PLATE CORRODED. FABRICATED NEW ATTACH PLATE PER AIRBUS DRAWING 10D53670099. TREATED, INSTALLED AND INSTALLED ATTACH PLATE PESDR SWAA060490Stringer Clip · crackedDURING SCHEDULED 1/4D CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 277, STR 15R. REMOVED AND REPLACED CLIP PER SRM.SDR A6WA200640073Support Angle · crackedLT FS 621.00 FLOOR SUPPORT ANGLE IS CRACKED .5 INCH LONG ON OB RADIUS. MAINTENANCE REPAIRED LT FS 621.00 FLOOR SUPPORT ANGLE IAW REO. (K)SDR AWXA200600521Attach Angle · corrodedMCN - DURING C22 CHECK DISCOVERED CORROSION ON AFT CARGO FLOOR WEB ATTACH ANGLE AT BS 767+6" TO 785 AND BL 19R. CORROSION WAS REMOVED AND FOUND TO BE OUT OF LIMITS IAW BOEING 737-300 SRM 53-60-15-1A1 FIG 101. MAINTENANCE REMOVED AND INSTALLED NEW ATTACH ANGLSDR UPS06446344Fitting · corrodedFWD CARGO COMPT REF NRC NR 5726 LT BATH FITTING ATT SURFACE FOUND HEAVY CORROSION AT STA 983 STR 38L PRESSURE BULKHEAD (AFTER FTG REMOVED ). CORROSION BLEND OUT 0.100" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, BS 1000 STR 38L UPPER BATH TUB FTG REPLACED SDR AWXA200600364Attach Angle · crackedMCN - DURING C4 CHECK DISCOVERED LEFT A/C BAY FRAME 39 STR 35L INSIDE AND OUTSIDE ATTACH ANGLE ON WEB CRACK 2.6" IN LENGTH. REMOVED AND INSTALLED NEW ATTACH ANGLES IN LT A/C BAY FS 39 STR35L IAW AIRBUS A320 SRM 51-72-11 PG 2 AND AIRBUS A320 SRM 51-42-11 PGS 2SDR ABXA060085Fitting · crackedRIGHT CANTED KEEL WEB TO WING SPAR FITTING WAS CRACKED. REPLACED FITTING ON NON ROUTINE 0366 IAW DC9 SRM.SDR 2006UALA00256Attach Angle · crackedFLOORBEAM TO WEB ATTACH ANGLE AT BS 246 APPROX LBL 48, COCKPIT ENTRY STEP IS CRACKED. CRACKED ANGLE REPLACED PER SRM. ANGLE FOUND DURING ROUTINE INSPECTION PROGRAM PER BOEING SERVICE BULLETIN 767-53-0093.SDR 2006UALA00252Fastener · misinstalledSTRINGER CLIP AT STA 867 STRINGER 20R INSTALLED WITH LOCK FASTENER THAT FAIL MAXIMUM PROTRUSION TEST ON GO-NO GO GAGE. REMOVED & INSTALLED NEW STRINGER CLIP & FASTENERS REF 51-40-02.SDR 2006UALA00247Support · crackedCABIN BS 827 AFT SIDE OF FRAME IS CRACKED BETWEEN S8L & S9L AT PSU RAIL SUPPORT. INSTALLED REPAIR REF MM 53-10-84.SDR 06FDEA0599Tee Fitting · corrodedFOUND TEE FITTING CORRODED STA 740 RBL 4 CORROSION ON LOWER EDGE OF BULKHEAD. REPLACED BULKHEAD LOWER CHORD PER SRM 51-30-5 AND 51-30-2.SDR SWAA060484Stringer Clip · crackedDURING SCHEDULED 8Y CHECK, FOUND FUSELAGE STRINGER CLIP CRACKED AT BS 293, STR 16R. REMOVED AND REPLACED CLIP PER SRM.SDR WTXR10549Attach Bracket · crackedFOUND CRACK AT LT AND RT FUSELAGE FRAME 20 AT THE WING ATTACH POINT. LT CRACK IS APPROX 1.0 INCHES IN LENGTH, RT CRACK IS APPROX .75 INCHES IN LENGTH.SDR ABXA060137Fitting · corrodedFOUND LOWER AFT CARGO, STA 1230, LONGERON 28 RIGHT, LONGERON BATHTUB FITTING CORRODED OUT OF LIMITS. REMOVED AND REPLACED BATHTUB FITTING IAW DC8 SRM 51-1-21, 51-1-20D, 51-1-8, 51-3-1 AND LWR 200302015.SDR ABXA060100Clip · corrodedLOWER AFT CARGO STA 1000 BETWEEN LONGERON 33 RIGHT AND 32 RIGHT, FRAME CLIP CORRODED OUT OF LIMITS. REMOVED CORROSION IAW DC8 SRM 51-1-8. MADE REPAIR IAW REA D853-53274, AND INSTALLED FASTENERS IAW DC8 SRM 51-1-20.
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