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.

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.Jul 31, 1996 · N854FT · Boeing 747122SDR 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.Jul 31, 1996 · N501ME · Doug DC932SDR 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.Jul 31, 1996 · N501ME · Doug DC932SDR 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.Jul 31, 1996 · N5521H · Cessna 152SDR 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.Jul 31, 1996 · N5521H · Cessna 152SDR 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 NO15Jul 30, 1996 · Wthrly 620SDR 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)Jul 29, 1996 · N143AA · Doug DC1030SDR 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.Jul 29, 1996 · N195FE · Boeing 72722SDR 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.Jul 25, 1996 · N614US · Boeing 747251BSDR 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)Jul 22, 1996 · N61CX · Doug DC862SDR 96FDEA01280Chord · crackedDISCREPANCY: NR 0305 (21) CRACK IN PLUS CHORD AT BS 760, LBL 70.5, WL 205. CORRECTIVE ACTION: *****S/D *****COMING.Jul 22, 1996 · N287FE · Boeing 7272D4SDR 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.Jul 18, 1996 · N675UP · Boeing 747123SDR 96ZZZX4126Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4125Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4124Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4123Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4122Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4121Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4120Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4119Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4118Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4117Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4116Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4115Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4114Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4113Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4112Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4111Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 96ZZZX4110Stiffener · crackedINSPECTION OF BOTH RIGHT AND LEFT WINGS PER CASA COM LETTER 212-224, FOUND STIFFENER ANGLES AFT OF FALSE SPAR CRACKED.Jul 18, 1996 · N311ST · Casa C212200SDR 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.Jul 17, 1996 · N675UP · Boeing 747123SDR 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.Jul 17, 1996 · N851FT · Boeing 747122SDR 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 AMEJul 16, 1996 · N419JR · Bbavia 8KCABSDR 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 AMEJul 16, 1996 · N419JR · Bbavia 8KCABSDR 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.Jul 15, 1996 · N856FT · Boeing 747132SDR P5CA9600591Bolt · shearedSHEARED BOLT AT APPROX WS 590 LWR ATTACH FOR STRINGER 7 IN NR 3 MAIN TANK. REPLACED BOLT.Jul 15, 1996 · N856FT · Boeing 747132SDR 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.Jul 15, 1996 · N856FT · Boeing 747132SDR P5CA9600559Fastener · missingMISSING FASTENER AT FSSI 950 COMMON TO WING FRONT SPAR CHORD. RIVET REPLACED PER BAC SRM 51-30-02.Jul 15, 1996 · N856FT · Boeing 747132SDR 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.Jul 11, 1996 · N941UP · Boeing 72722CSDR 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.Jul 11, 1996 · N715DH · Boeing 727155CSDR 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.Jul 11, 1996 · N715DH · Boeing 727155CSDR 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)Jul 11, 1996 · N707AA · Boeing 727223SDR 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)Jul 11, 1996 · N707AA · Boeing 727223SDR 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.Jul 10, 1996 · N921UP · Boeing 727180CSDR 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.Jul 9, 1996 · N715DH · Boeing 727155CSDR 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.Jul 8, 1996 · N951UP · Boeing 72725CSDR 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.Jul 8, 1996 · N951UP · Boeing 72725CSDR 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.Jul 8, 1996 · N474DA · Boeing 727232SDR 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.Jul 8, 1996 · N474DA · Boeing 727232SDR 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.Jul 5, 1996 · N408PE · Boeing 737130SDR 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 ANJul 5, 1996 · N408PE · Boeing 737130
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