JASC 5710

Service difficulty reports · 4,462

Reports filed under 5710 · Wing Main, Frame 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 = '5710'
  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 DHL2003748008Angle · crackedDURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130 FOUND THE OUTBOARD NR 8 SLAT ACTUATOR MOUNT ANGLE TO BE CRACKED. REMOVED NR 8 SLAT ACTUATOR CRACKED O/B MOUNT ANGLE IAW B-727 SRM 51-30-2. FABRICATED NEW ANGLE FROMay 17, 2003 · N748DH · Boeing 727225SDR DHL2003748007Bracket · crackedDURING DROP IN MAINTENANCE DISCREPANCY AS FOLLOWS, UPON REMOVAL OF DOUBLERS FOR SB 727-57-0130, FOUND BOTH NR 1 SLAT ACTUATOR MOUNT ANGLES TO BE CRACKED. REMOVED NR 1 SLAT ACTUATOR ANGLES IAW B-727 51-30-2. FAB NEW ANGLES FROM 7075 T-6 .063 INCH PO 9912495 1May 17, 2003 · N748DH · Boeing 727225SDR 03FDEA00770Hinge · corrodedRT WING- O/B FLAP O/B HINGE (FLAP SIDE) FWD ATTACHMENT POINT I/B CTR BOLT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-69247 - WINGS - OUTBOARD FLAP HINGE FITTINGS OVERSIZE HOLES - REPAIR.May 13, 2003 · N612FE · Doug MD11SDR CA031001003Windshield · cracked(CAN) IN CRUISE, AT FL 300 THE INNER PLY OF THE RT WINDOW CRACKED. THE QRH WAS APPLIED AND THE FLT CONTINUED WITHOUT FURTHER INCIDENT. THE AIRCRAFT WAS FERRIED WHERE THE WINDOW WAS REPLACED.May 8, 2003 · Cndair CL6002B19SDR DHL2003801077Vane · damagedLT WING L/E INBOARD VANE SLOT PLATING HOLES ELONGATED AT STA XILD 0.7095 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL-030412, ED3258. TRIMMED OUT ELONGATED HOLES SKIN AREA IAW EO DHL-030412, ED3258. FABRICATED DOUBLER (7075-T6 0.071) AND INTERNAL DOUBLApr 29, 2003 · N801DH · Doug DC873FSDR 03FDEA00601Hinge · corrodedNR S 32 C/W E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION ON 04/18/03. COMPLIED WITH E.A.8-5740-68784. RT I/B FLAP HINGE ASSY CORROSION REWORK.Apr 24, 2003 · N320FE · Doug DC1030SDR 03FDEA00600Hinge · corrodedNR S 31 C/W E.A.8-5740-68783-L/H I/B FLAP HINGE ASSY CORROSION REWORK. CLOSING ACTION .COMPLIED WITH E.A.8-5740-68783. ON 04/18/03.Apr 24, 2003 · N320FE · Doug DC1030SDR DHL2003801009Vane · damagedLT WING L/E INBOARD VANE SKIN SHOWS ELONGATED HOLES AT STA XS. 247.000 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EODHL 030413, ED3259. REMOVED FASTENERS IAW SRM 51-1-21 PG 2. CUT OUT DAMAGED AREA IAW EODHL 030413, ED3259. CLEANED, TREATED AND PRIMED AREA Apr 19, 2003 · N801DH · Doug DC873FSDR DHL2003801020Vane · damagedLT WING L/E OUTBOARD VANE SHOWS ELONGATED HOLES AT STA XOLDO 67.0 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW EO DHL 030410, ED-3265 CUT OUT DAMAGED AREA IAW EO DHL 030410, ED 3265. CLEANED, TREATED AND PRIMED AREA IAW SRM 51-1-8B. FABRICATED FILLER (7075-T6Apr 18, 2003 · N801DH · Doug DC873FSDR 03FDEA00499Structure · tornLEFT WING AILERON TRIM TAB INBOARD UPPER SURFACE DISBONDED AND TORN ON HONEYCOMB MATERIAL.Apr 17, 2003 · N218FE · Boeing 727200SDR EIA2003066Structure · corrodedRIGHT WING STA 1323 AFT OF NR 23 VARIABLE CAMBER FLAP LOWER T-CHORD CORRODED. REMOVED CORROSION, TRIMMED DAMAGE, INSPECTED AND NDT, FABRICATED REPAIR AND INSTALL PER ECRA 471-57-217-2 REV-A.Apr 17, 2003 · N471EV · Boeing 747273CSDR ASAA0380293Angle · crackedOKC - DURING 30K CHECK, FOUND LEFT WING LEADING EDGE FRAME TIE IS CRACKED AT UPPER AFT END. REPLACED ANGLE PER SRM 51-10-2. (M)Apr 4, 2003 · N931AS · Doug DC982SDR ASAA0380289Shear Tie · crackedOKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2 AND 30-5. (M)Apr 4, 2003 · N931AS · Doug DC982SDR ASAA0380288Shear Tie · crackedOKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M)Apr 4, 2003 · N931AS · Doug DC982SDR ASAA0380287Shear Tie · crackedOKC - DURING 30K CHECK, FOUND RIGHT WING LEADING EDGE FRAME SHEAR TIE IS CRACKED. REPLACED SHEAR TIE CLIP PER SRM 51-10-2, 10-4, 10-2, 30-2, AND 30-5. (M)Apr 4, 2003 · N931AS · Doug DC982SDR UPS03840478Fitting · crackedINSPECTION TYPE: C3, NR 3 FUEL TANK STRINGER 74 STRAP CRACKED STA XRS 22 ACCESS PANEL 506C. REMOVED CRACKED FITTING IAW DC8 SRM 51-1-20D. FABBED 1 EA FITTING P/ N 5616869-2 FROM 7075-T6511 BAR STOCK PO 334935 IAW DAC 5616869. L OCATED DRILLED DEBURRED IAW DApr 2, 2003 · N819UP · Doug DC873FSDR 03FDEA00317Rib · damagedLT WING NR 6 SLAT OUTBOARD RIB REPAIR AT XOS=889.0, PN ABR 1818.Mar 14, 2003 · N68052 · Doug DC1010SDR UPS03840351Fitting · crackedINSPECTION TYPE: C2, NR 2 MAIN FUEL TANK HAS STRINGER END FITTING CRACKED AT OUTBOARD SIDE OF XRS 50 AT STRINGER 51. REMOVED, FABRICATED AND INSTALLED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Mar 12, 2003 · N880UP · Doug DC873FSDR UPS03240295Rib · crackedINSPECTION TYPE:C&SI L/H WING SUSPECT CRACK AT I/B TRACK RIB ON 4 SLAT CRACK STOP DRILLED IAW SRM 51-10-01. HFEC C/O ON L/H WING AT I/B TR ACK RIB ON NO. 4 SLAT INSP. IAW B727 NDTM PT 6 51-00-00 RESULTS CRAC K CONTAINED BY STOP DRILLED HOLEMar 8, 2003 · N949UP · Boeing 72725CSDR 1592SStructure · misrepairedDURING A PHASE 2, 3 & D INSPECTION, IT WAS VISUALLY DISCOVERED UPPER & LOWER RIB CAP STRUCTURE WAS MISSING AT LT WS 128.80 AS WELL AS STRINGER SPLICES WERE NOT ATTACHED TO THE WING SKIN BETWEEN LT WS 120.0 & 148.30 & THE SKIN SPLICE USED WAS THE WRONG MATERIALMar 5, 2003 · N454EA · Cessna 441SDR 03FDEA00305Cap · crackedDURING "C" CHECK, LT WING UPPER CAP AT RIB STATION XORS 402 CRACKED. THE CRACK WAS ALL THE WAY THRU THE CAP AND WAS LOCATED IMMEDIATELY FWD OF STRINGER 15.Mar 4, 2003 · N392FE · Doug DC1010SDR 03FDEA00289Hinge · corrodedRT WING FOUND OUTBOARD HINGE OUTBOARD HOLE CORRODED AFTER BUSHING REMOVAL.Mar 3, 2003 · N585FE · Doug MD11SDR QXEA0300349Structure · crackedCKB - RIGHT HAND WING CRACK FOUND ON STRUCTURE UNDER INBOARD FLIGHT SPOILER. REPAIRED IAW RD 670-57-51-00-4 AND HORIZON AIR EA R-53-77.Feb 27, 2003 · N608QX · Cndair CL6002C10SDR 03FDEA00170Support · crackedLT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE FOUND CRACKED, APPROXIMATELY 1 INCH IN LENGTH. LT WING L/E SLAT TRACK NR 16 RIB SUPPORT REMOVED AND REPLACED AS PER SRM 51-31-01 VOL II.Feb 24, 2003 · N585FE · Doug MD11FSDR 03FDEA00171Support · crackedRT WING L/E SLAT TRACK, NR 16 RIB SUPPORT, INBOARD SIDE, FOUND WITH CRACK APPROXIMATELY 1 INCH IN LENGTH.Feb 24, 2003 · N585FE · Doug MD11FSDR 03FDEA00162Rib · crackedLT WING, FOUND TRACK NR 16 INBOARD STRUCTURAL RIB CRACKED. LT WING LEADING EDGE AND LEADING EDGE DEVICES, RIB INBOARD SLAT TRACK NR 16. SUPPORT FABRICATION CARRIED OUT IAW EA 1-5740-67574. CRACKED RIB REMOVED IAW SRM 51-31-01 VOL. II. AND REPLACED NEW FABFeb 18, 2003 · N613FE · Doug MD11FSDR SWAA030390Rib · crackedDURING SCHEDULED 1/4D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN S2R & S3R. REPAIRED RIB PER SWA EA.Feb 17, 2003 · N613SW · Boeing 7373H4SDR GTIA030201Structure · corrodedFTW - FOUND LEFT WING, WING TO FUSELAGE CORROSION AT FORMER STATION 807. REMOVED DAMAGED SECTION. FORMED REPAIR DOUBLER. INSTALLED REPAIR DOUBLER AND FILLER. (M)Feb 16, 2003 · N809NK · Doug DC983SDR DHL2003804557Vane · damagedLT WING OUTBD VANE SLOT UPPER SKIN HOLE ELONGATED XOLDO58.000 PERFORMED MAJOR REPAIR IAW EO DHL 030109 ED-3222 . REMOVED FASTNERS IAW SRM 51-1-21 PG 1 TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL030109 , ED-3222. FABRICATED AN EXTERNAL REPAIR DOUBLER (7075T6AFeb 10, 2003 · N804DH · Doug DC873FSDR UPS03840182Fitting · crackedINSPECTION TYPE: C1, LT WING STRINGER 51 END FITTING IS CRACKED OUTBOARD OF XRS 74. REMOVED AND REPLACED FITTING IAW DWG 3704841 AND SRM 51-1-20D.Feb 10, 2003 · N811UP · Doug DC873FSDR DHL2003804667Vane · crackedRT WING L/E INBD. VANE SHOWS HOLES ELONGATED , XS247.000 PERFORMED MAJOR REPAIR IAW EO DHL 030104 , ED-3208. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 TRIMMED OUT DAMAGED SKIN SEGEMENT IAW EA DHL 030104, ED-3208 FABRICATED REPAIR DOUBLER. A FILLER 7075T6 AL 0/0Feb 4, 2003 · N804DH · Doug DC873FSDR SWAA030217Frame · crackedDURING SCHEDULED 5Y CHECK, FOUND LT WING T/E SUPPORT FRAME CRACKED, WBL 413.18. REPAIRED FRAME PER SWA EA.Jan 28, 2003 · N719SW · Boeing 7377H4SDR UIEA200300002Beam · crackedDURING CURRENT C-CHECK AT SIA, FOUND RT WING LE BEAM WEB CRACKED AT OLES 1200. CRACK REMOVED BY CUTTING THE WEB AT OLES 1190 AND DISCARDING THE INBOARD SECTION FROM OLES 1190 TO 1200. PERFORMED HFEC INSPECTION OF CUT EDGE TO ENSURE CRACK FREE CONDITION. NO Jan 22, 2003 · N516MC · Boeing 747243BSDR AUS20030050Wing · delaminated(AUS) LH WING DELAMINATED.Jan 20, 2003 · Boeing 7272J4SDR DHL2003804665Vane · damagedRT OUTBD SLOT VANE AT STA XS 520.000 HOLES ELONGATED. PERFORMED MAJOR REPAIR IAW EO DHL 030101 , ED-3211. REMOVED FASTNERS IAW SRM 51-1-21 PG. 1, TRIMMED OUT DAMAGED SKIN SEGMENT IAW EO DHL 030101 , ED-3211 , FABRICATED REPAIR DOUBLER, A FILLER (7075T6AL-0.06Jan 16, 2003 · N804DH · Doug DC873FSDR UPS03840026Fitting · crackedINSPECTION TYPE: C2, RT WING STRINGER END FITTING IS CRACKED I/B OF XRS 74 AT STRINGER 51. REMOVED AND REPLACED FITTING IAW DWG 3704841, AND SRM 51-1-20D.Jan 9, 2003 · N701UP · Doug DC871FSDR 2003FA0000021Bulkhead · crackedINSPECTION IAW AD. CRACK WAS FOUND IN RIGHT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON INBOARD SIDE OF CAP JUST INSIDE OF INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH THE WING, IT WAS LOCATED IN THE AFT OF THE CAP WIDTJan 6, 2003 · N402CA · Cessna 402BSDR 2003FA0000020Bulkhead · crackedWHILE CONDUCTING INSPECTION IAW AD 00-01-16(D)A CRACK WAS FOUND IN THE RIGHT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON THE INBOARD SIDE OF CAP JUST INSIDE OF THE INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH THE WING. Jan 6, 2003 · N402CA · Cessna 402BSDR 2003FA0000019Bulkhead · crackedINSPECTION IAW AD, A CRACK WAS FOUND IN THE RT ENGINE CANTED BULKHEAD CAP. CRACK WAS LOCATED ON THE INBOARD SIDE OF CAP JUST INSIDE OF INBOARD WING LIP. CRACK WAS APPROXIAMATELY 1.5 INCHES AND RAN CHORD WISE WITH WING. IT WAS LOCATED IN THE AFT OF THE CAP WJan 6, 2003 · N402CA · Cessna 402BSDR AUS20021415Structure · cracked(AUS) RT WING COMPONENTS CRACKED. COMPONENTS AFFECTED INCLUDE: TRAILING EDGE RIB LOCATED AT STA 23.625. WING ROOT RT RIB ASSY LOCATED AT STA 23.625, WING SPAR REINFORCEMENT FITTING, WHEN CHANGING TRAILING EDGE RIB LOCATED AT WS 23.625, IT WAS NOTED THAT RDec 12, 2002 · Cessna 182QSDR C2XA02TY170Spar · crackedDuring mtx taxi of the aircraft, the R/H wing outbd. leading edge struck a storage shed causing damage to the R/H leading edge, wing tip, and fwd. spar. Maintenance spliced in a new section of spar 1, replaced rib 25, and replaced the outbd. leading edge and wDec 9, 2002 · N16951 · Emb EMB145LRSDR CA021211004Lock Plate · corroded(CAN) DURING ACCOMPLISHMENT OF AN H02 CHECK. FOUND THAT THE LT AFT LOCKING PLATE FOR THE LT WING TIP FENCE AND THE AFT ATTACH HARDWARE(2) BOLTS WERE FOUND BADLY CORRODED. THERE WAS NO CORROSION INDICATION AT THE LT FWD ATTACHMENT AND THE AFT THAT SHOWS EXTREMDec 3, 2002 · Airbus A320211SDR PCAA0211141Structure · bird strikeMDT-FLIGHT 3800 CREW REPORTED LARGE BIRD STRIKE ON RIGHT WING. DAMAGE CURRENTLY BEING EVALUATED. MAINTENANCE REPAIRED RIGHT WING IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWINGS RD8-57-2481, RD8-57-2482, RD8-53-2483, RD8-57-2484. WORK ACCOMPLISHED BY BOMBARDINov 27, 2002 · N846EX · Dhav DHC8102SDR 0204009915Cap · corrodedDuring HCK in ATL, corrosion was found in the upper flange of the center wing skin cap. Corrosion was out of limits. Repaired per EA 99-190861.Nov 25, 2002 · N965N · Doug DC931SDR UPS02239974Structure · damagedINSPECTION TYPE: C, RT LE, REMOVABLE SECTION, SOME SCREWS HAVE PULLED THROUGH ON UPPER SURFACE AT O/B END (INTERSECTION OF NR 6 KREUGER & NR 5 SLAT). REPAIR CARRIED OUT IAW SMRO EO 2002-057-003.Nov 22, 2002 · N906UP · Boeing 72730CSDR ABXA020304Structure · wornTRAILING EDGE, WING STA. 161, UPPER SURFACE HAD EXCESSIVE WEAR. REPLACED RIB IAW DC-9 SRM 51-30-2 AND 51-30-5.Oct 30, 2002 · N984AX · Doug DC932SDR UPS02839890Strap · crackedINSPECTION TYPE: C2, RT WING HAS A CRACKED LONGERON 64 END FITTING-STRAP, AND LOWER SPAR IS CRACKED 1/2 INCH FROM EDGE OF SPAR TO FASTENER HOLE AT XRS 450. NDT VERIFIED 1/2 INCH CRACK AT XRS 450 FROM EDGE OF SPAR TO FASTENER HOLE, REMOVED, FABRICATED AND INSOct 25, 2002 · N779UP · Doug DC871FSDR F3LA200200358Housing · wornDURING C 4 CHECK, TRACK HOUSING WAS FOUND TO HAVE A HOLE WORN THROUGH IT CAUSING FUEL LEAK. HOUSING IS LOCATED INSIDE THE WING TANK FOR NR 5 OUT BOARD SLAT TRACK, RT WING STA 497. REMOVED DAMAGED NR 5 OUT BOARD SLAT TRACK HOUSING IN ACCORDANCE WITH THE REQUOct 21, 2002 · N578US · Boeing 737301SDR 16214Structure · crackedIN THE WHEEL WELL AREA OF THE P2V-7 THERE ARE 2 FUEL CELL INTERCONNECT ACCESS PANELS. THE FURTHEST INBOARD PANELS ON EACH SIDE ARE PANEL 53L AND 53R. PANEL 53L, THERE IS A CRACK LOCATED AT THE INBOARD FORWARD CORNER, RUNNING FROM THE RADIUS OF THE DOUBLER CUOct 16, 2002 · N139HP · Lkheed P2V7SDR PCAA0210122Structure · bird strikeDCA-ALB FLIGHT 3927, CREW REPORTED THAT DURING DESCENT AIRCRAFT FLEW INTO A FLOCK OF BIRDS AND TOOK SEVERAL BIRD STRIKES ON ENTIRE AIRCRAFT RESULTING IN DAMAGE TO RIGHT WING WITH FUEL LEAKING OUT, AND HOLE IN TAIL SECTION AT BASE OF VERTICAL STABILIZER. MAINTOct 15, 2002 · N847EX · Dhav DHC8102
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