JASC 5720
Service difficulty reports · 13,638
Reports filed under 5720 · Wing Miscellaneous Structure, 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 = '5720' 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 = '5720' 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 P5CA9600415Hilock Fastener · head shearedHEAD SHEARED ON HILOCK RIGHT WING AFT SPAR, LOWER CHORD, JUST OUTBOARD OF WING GEAR AFT TRUNNION. REPLACED HILOCK PER BOEING SRM 51-10-01.SDR MWEA96387Angle · corrodedDURING D-CHECK, A T/E PANEL RIB UPPER ANGLE CORRODED, RT WING STA XRS 380. FABRICATED AND INSTALLED A NEW ANGLE WITH RIB IAW SRM 51-40-0.SDR MWEA96361Angle · crackedDURING D-CHECK, LT WING TRAP PANEL AFT OUTBD FLANGE REPAIR HAD AN ANGLE CRACK AT THE AFT FLANGE. INSTALLED ANGLE REPAIR IAW SRM 57-09, FIG 71 SHEET 2.SDR 96ZZZX4397Channel · corrodedWHEN LEFT DOORPOST TRIM WAS REMOVED FOR WINDSHIELD CHANGE, CORROSION WAS FOUND AT LEFT WING FORWARD SPAR CARRY-THROUGH AREA. WING WAS REMOVED. BRACE AND CHANNEL WERE REPLACED.SDR 96ZZZX4396Channel · corrodedWHEN LEFT DOORPOST TRIM WAS REMOVED FOR WINDSHIELD CHANGE, CORROSION WAS FOUND AT LEFT WING FORWARD SPAR CARRY-THROUGH AREA. WING WAS REMOVED. BRACE AND CHANNEL WERE REPLACED.SDR AU961165Pin · mismanufactured(AUS) WING HINGE PINS FAULTY - DEPTH OF THREADED HOLES VARIES BETWEEN 21.463MM AND 21.844MM (0.845IN AND 0.860IN) - MAXIMUM DEPTH OF HOLE IS 21.336MM (0.840IN) - FOUND DURING INSPECTION IAW WEATHERLY SERVICE NOTE NO15SDR AALA961128Angle · corrodedTUL - FOUND EXFOLIATION CORROSION ON LOWER WING SPLICE ANGLE WITH A CRACK BETWEEN 1ST AND 2ND HOLES OUTBOARD OF GEAR TRUNNION CASTING TOP OF LOWER WING. INSTALLED A NEW SPLICE ANGLE PER SRM 51-01-00-05 PG 1. (M)SDR 96FDEA01293Chord · corrosionNR 0231 042. CORROSION C53-132-02(1) ON STA 870, UPPER CHORD LBL 58-60, 46, 36-38, 26-28, 17-19, RBL 55, 45, 10, 0 WL 172. REMOVED AND REPLACED 870 UPPER CHORD LBL 70 - RBL 70, WL 172 PER FEDEX EA 7-5710-29709.SDR 9616576614Fitting · crackedDURING P-CHECK, FOUND A CRACK IN THE CENTER WING VERTICAL SUPPORT FRAME UPPER TIE FITTING BS 1000 AT LBL 35. REPLACED FITTING PER SA 5715-01014-3.SDR IXXA96141Fitting · crackedDURING ROUTINE C-CHECK INSPECTION, THE RIGHT MAIN LANDING GEAR TORQUE TUBE SUPPORT FITTING WAS FOUND TO BE CRACKED. THE FITTING WAS REPLACED IAW THE STRUCTURAL REPAIR MANUAL. (M)SDR 96FDEA01280Chord · crackedDISCREPANCY: NR 0305 (21) CRACK IN PLUS CHORD AT BS 760, LBL 70.5, WL 205. CORRECTIVE ACTION: *****S/D *****COMING.SDR UPS96420914Skirt Angle · crackedINSPECTION TYPE: C. FOUND LT SKIRT ANGLE CRACKED APPROXIMATELY 6 INCHES AFT OF LAST TRAILING EDGE DOOR HINGE. ALSO, 2 INCHES FORWARD ATTACHMENT HOLES WORN OUT. REPAIRED SKATE ANGLE IAW TO KLM DFX 96-171 ISSUE NR 3 AND IAW EFN 747-54-0131.SDR 96ZZZX4126Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4125Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4124Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4123Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4122Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4121Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4120Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4119Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4118Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4117Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4116Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4115Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4114Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4113Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4112Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4111Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR 96ZZZX4110Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.SDR UPS96420791Chord · crackedINSPECTION TYPE-C, RT WING LOWER CHORD CRACKED AT RT ILES 1117.00 INSIDE L/E AREA. REMOVED BROKEN OFF PIECE AND TRIMMED CHORD. REPAIR ANGLE PLACED, APPROVED UPS AMS 96-0172RE.SDR P5CA9600380False Spar · corrodedRT FALSE SPAR FORWARD SIDE FROM WING GEAR TRUNNION ATTACH I/B TO END HAS BARE METAL WITH MINOR SURFACE CORROSION. REMOVED LEVEL ONE CORROSION, TREATED IAW SRM 51-10-02.SDR 96ZZZX4032Strut Fitting · crackedINSPECTED THE LIFT STRUT FITTINGS (PN 3-1632-1 AND PN 316322) IAW AD 96-03-11 PER AMERICAN CHAMPION SERVICE LETTER NR 408. FOUND TWO OF THE FOUR FITTINGS CRACKED AT THE RADIUS AS SHOWN IN THE ILLUSTRATION. INSTALLED THE NEW STYLE FITTINGS (PN 3-1691) PER AMESDR 96ZZZX4031Strut Fitting · crackedINSPECTED THE LIFT STRUT FITTINGS (PN 3-1632-1 AND PN 316322) IAW AD 96-03-11 PER AMERICAN CHAMPION SERVICE LETTER NR 408. FOUND TWO OF THE FOUR FITTINGS CRACKED AT THE RADIUS AS SHOWN IN THE ILLUSTRATION. INSTALLED THE NEW STYLE FITTINGS (PN 3-1691) PER AMESDR P5CA9600592Fasteners · shearedTWO SHEARED RIVETS (FASTENERS) AT FRONT SPAR LOWER CHORD AT APPROX WS 660 IN NR 3 MAIN TANK. REPLACED FASTENERS PER BAC SRM 51-30-02.SDR P5CA9600591Bolt · shearedSHEARED BOLT AT APPROX WS 590 LWR ATTACH FOR STRINGER 7 IN NR 3 MAIN TANK. REPLACED BOLT.SDR P5CA9600589Stiffener · crackedCRACK AT OTBD FRONT SPAR VERTICAL RIB STIFFENER IN NR 3 MAIN TANK AT WS 670. TEMP REPAIR, STOP DRILLED CRACK AND INSTALLED A REPAIR STRAP PER HAECO REPAIR SCHEME R-57-21-32967 AND BOEING FAX APPROVAL.SDR P5CA9600559Fastener · missingMISSING FASTENER AT FSSI 950 COMMON TO WING FRONT SPAR CHORD. RIVET REPLACED PER BAC SRM 51-30-02.SDR UPS96220755Clamp Rings · corrodedINSPECTION TYPE-C, FRETTING SURFACE CORROION ON LT AND RT WING FUEL TANK DOOR CLAMP RINGS. FUEL TANK DOOR CLAMP RINGS REPLACED IAW MM 28-11.SDR DHL9671524DAngle · crackedAT D-CHECK, LT LEADING EDGE CAVITY WBL 92.8 SECOND VERTICAL SUPPORT ANGLE IS CRACKED AT BOTTOM FASTENER. STOP DRILLED CRACK, INSTALLED ANGLE REPAIR, 9 INCHES BY 1 INCH BY 1 INCH, PER SRM 51-40-3.SDR DHL9671521DAngle · crackedAT D-CHECK, LT WING LEADING EDGE CAVITY STA 130.7 LOWER SUPPORT ANGLE CRACKED AFT OF MIDDLE SUPPORT ANGLE AT ATTACH BOLT. INSTALLED SUPPORT ANGLE PER SRM 51-40-3, 9 INCHES BY 1 INCH BY 1 INCH.SDR AALA961033Stiffener · corrodedTUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER, FSS 245. REPLACED VERTICAL STIFFENER PER SRM 51-10-4, PAGE 4. TST: 41,665 HOURS. CYCLES: 21,768. (X)SDR AALA961032Stiffener · corrodedTUL - LEFT WING FORWARD SPAR, CORROSION ON VERTICAL STIFFENER FSS 255. REPLACED STIFFENER PER SRM 51-10-4. TST: 41,665 HOURS. CYCLES: 21,768. (X)SDR UPS96220637Angle · crackedINSPECTION TYPE-C, LT WING ANGLE FOR PANEL 8107 CRACKED. REMOVED FAB'D AND INSTALLED ANGLE PER BOEING DWG NR 65-19275 AND 51-30-2.SDR DHL9671522DAngle · crackedAT D-CHECK, LT WING LEADING EDGE LOWER SUPPORT ANGLE AT WS 121.5 CRACKED AT ATTACH BOLTS. STOP DRILLED AND INSTALLED ANGLE REPAIR, 4 INCHES BY 1 INCH, PER SRM 51-10-1.SDR UPS96221018Stiffener · crackedINSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - OTBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, 51-30-2 AND SEALED PER SRM 50-20-4.SDR UPS96221017Stiffener · crackedINSPECTION TYPE: C. RT WING L/E AT NR 6 SLAT INBD TRACK - INBD VERTICAL STIFFENER FOR TRACK MOUNT IS CRACKED. REMOVED FABRICATED AND INSTALLED REPLACEMENT STIFFENER PER SRM'S 51-10-1, ,51-30-2 AND SEALED PER SRM 51-20-04.SDR DL72K961717Stiffener · crackedFOUND 1 CRACK IN WING L/E SPAR STIFFENERS OF NR 2 O/B TRACK. REPAIRED PER M/M 57-20-21 PG 813.SDR DL72K961715Stiffener · crackedFOUND 1.25 INCH CRACKS AT WING L/E SPAR STIFFENERS AFT OF NR 3 SLAT I/B TRACK TWO EACH. REPAIRED BY REPLACING STIFFENERS PER M/M 57-20-21 PG 813.SDR CALA9601005Stiffener · crackedINSPECTION FOUND A .25 INCH CRACK IN RT WING VERTICAL STIFFENER AT LEADING EDGE UNDER PANEL 6526. THE STIFFENER WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND 51-10-5.SDR CALA9600999Stiffener · damagedTWO STIFFENERS AND AFT SIDE OF WEB ON RT WING AT STA 180.36 SUSTAINED DAMAGE FROM TOOLING. THE STIFFENERS WERE REMOVED AND THE DAMAGED AREA WAS BLENDED IAW SRM 51-30-2 AND 57-10-1. STIFFENERS AND REPAIR PLATES WERE FABRICATED AND INSTALLED IAW SRM 57-10-2 AN
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