JASC 5740
Service difficulty reports · 3,003
Reports filed under 5740 · 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 = '5740' 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 = '5740' 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 B3OR20041029Attach Fitting · damagedON 22 SEPTEMBER 2004 A 5 YEAR WING BOLT INSPECTION WAS COMPLIED WITH ON A BEECHCRAFT A200 AIRCRAFT. THREE OF THE WING ATTACH FITTINGS WERE FOUND TO HAVE DAMAGE TO THE FLAT FACE PORTION OF THE FITTINGS, THE AREA WHERE THE WASHER RESTS ON THE FITTING. THE DAMAGESDR UIEA200400167Fitting · corrodedWHILE PERFORMING EO 4757A087, REAR SPAR UPPER CHORD AND SIDE BODY INSPECTION. CORROSION STILL EXIST ON THE UPPER REAR SPAR INTERNAL SPLICE FITTING AFTER INCORPORATING NR 5 HOLE DIA MAX OF 1.40 INCHES WITH SLEEVED BOLT REPAIR. LEVEL 1 MINOR. REAMED HOLE NR 5SDR 2004UALA00910Support Fitting · crackedRIGHT WING INBOARD MAIN FLAP REAR SIDE LINKAGE SUPPORT FITTING CRACKED, INBOARD AND OUTBOARD SIDES. MAJOR REPAIR ACCOMPLISHED. REPAIRED & INSTALLED SUPPORT FITTING.SDR USAA040675Hinge Fitting · wornHINGE FITTING WORN .0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69-39228.SDR COOSDR040030Fitting · corrodedRT AND LT WING TRAILING EDGE SUPPORT, CANOE FITTING OB/IB HOLES ID CORRODED AT STA XF=97.906, STA XF=219.498 AND STA XF=399.723.SDR CA040817006Attach Fitting · chafed(CAN) THE STRUT ATTACH FITTING ON FORWARD SPAR OF THE RH WING WAS CHAFED BY THE LEADING EDGE SKIN, WHICH HAD NOT BEEN TRIMMED ADEQUATELY DURING MANUFACTURE. THE CHAFING LEFT A SMALL DIMPLE THAT COULD LEAD TO CRACKING OF THE FITTING.SDR USAA040472Attach Angle · crackedFOUND ATTACH ANGLE WITH .375 INCH CRACK, STATION 1620-1640 BL 0. REPLACED CRACKED ANGLE WITH FABRICATED LIKE PART PER SRM 53-00-51. (M)SDR AALA20040882Fitting · damagedAFW - LEFT HAND WING TERMINAL FITTING AT SPAR AT STATION 155 HAS BLENDOUT. AREA IS 0.30 AND DEPTH IS 0.135 INCH. DAMAGED AREA WAS BLENDED SMOOTH, VISUALLY INSPECTED, AND REFINISHED PER THE SRM. A REPLACEMENT FASTENER WITH 0.050 INCH CRES WASHER WAS INSTALLESDR USAA040381Fitting · corrodedPIT - FOUND FITTING CORRODED .25 INCH AREA, RIGHT WING AFT SPAR AND LG BEAM GEAR DOOR HINGE POINT OUTBOARD. REAMED AND COUTNERSINK NEW FITTING PER MM 20-50-11-2-912-002 FIG 202. (M)SDR USAA040374Fitting · crackedFOUND AFT SPAR ATTACH FITTING CRACKED .25 INCH, LANDING GEAR BEAM AFT SPAR ATTACH FITTING, RIGHT WING AFT SPAR. MODIFIED PART INSTALLED PER EO 5702V054. (M)SDR 2004UALA00703Fitting · brokenNR 5 GROUND SPOILER OB ACTUATOR ATTACH LUG BROKEN. NR 5 GROUND SPOILER ACTUATOR WAS FOUND FRACTURED AT THE BEARING END DURING ROUTINE HMV MAINTENANCE INSPECTION. THE ACTUATOR WAS SENT TO THE SHOP FOR INITIAL EVALUATION BEFORE BEING SENT TO BOEING FOR A FULL FSDR USAA040378Fitting · galledPIT - FOUND GALLED FITTING, MLG WALKING BEAM, RIGHT WING REAR SPAR, STATION 200. DEFECTIVE PART REPLACED WITH IDENT PART NR PER BMM 20-50-11-2-912-002 FIG 202. (M)SDR USAA040372Fitting · crackedPIT - FOUND FITTING CRACKED .75 INCH, RIGHT WING REAR SPAR STATION 224. INSTALLED NEW SUPPORT FITTING PER EA 78781. (M)SDR 04FDEA02162Fitting · crackedLT WING - OUTBOARD FLAP STOP FITTING CRACKED 2 PLACES. REPLACED AS PER MM 27-50-30- 4. ON P/N: NRC6753-503 AND ON S/N: 047. OFF P/N: NRC6753-503 AND OFF S/N: 006. FUNCTIONAL CHECK REFER TO SNRM N0508 FOR WORK DETAILS.SDR UPS04842901Fitting · crackedINSPECTION TYPE: C1, NR 4 ALT BOOST PUMP BRACKET AND STRINGER 59 END FITTING AT XW 408 ARE CRACKED. REMOVED, FABRICATED AND REPLACED FITTING AND REPLACED BRACKET IAW DWG 3645611 AND 5644972 AND SRM 51-1-20D.SDR 04FDEA02100Fitting · corrodedC/W EA 8-5720-79541 WINGS INBOARD FLAP SIDE LOAD SUPPORT FITTING CORROSION REPAIR P/N ANB7434. COMPLIED WITH EA 8-5720-79541.SDR 04FDEA2099Fitting · corrodedC/W EA 8-5750-79553 WINGS OUTBOARD AILERON, ACTUATOR ATTACH FITTING REWORK. COMPLIED WITH EA 8-5750-79553.SDR 04FDEA02097Fitting · corrodedC/W EA 8-5740-79557 WINGS RIGHT AILERON SUPPORT ASSY CORROSION REPAIR P/N ARC0317- 502. COMPLIED WITH EA 8-5740-79557.SDR UPS04842913Support · crackedINSPECTION TYPE:C1 RIGHT WING FLAP HINGE 3 SUPPORT FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5642342 AND SRM 51-1-20D, 51-1-21.SDR 04FDEA02032Fitting · crackedLEFT WING, OUTBOARD FLAP ATTACHING RIB STOP FITTING FOUND CRACKED. REMOVED AND REPLACED AS PER SRM 51-31-01 VOLUME II.SDR IXXA060410SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING OUT BOARD FLAP HINGE FITTING CORRODED AT STATION XF97. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060408SFitting · corrodedDURING ROUTINE C CHECK, FOUND LEFT WING FLAP HINGE BASE FITTINGS CORRODED AT STATIONS XW219 AND XW97. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060402SFitting · crackedDURING ROUTINE C CHECK, FOUND LEFT WING RIGHT CENTER FUEL TANK FITTING PLATE CRACKED AT STATION XWC23 BETWEEN STRINGERS 1 AND 2. REPLACED PER ALL APPLICABLE DATA.SDR 04FDEA01768Fitting · crackedRIGHT HAND WING OUTBOARD FLAP INBOARD HINGE INTERNAL RIB FITTING (FORWARD OUTBOARD SIDE) FOR HINGE ATTACHMENT CRACKED APPROXIMATELY 2 INCHES IN LENGTH. RIGHT HAND WING OUTBOARD FLAP REMOVED AND REPLACED AS PER MM 27- 50-30-4 AND FLAPS RIGGING AND OPERATIONAL SDR IXXA060438SFitting · crackedDURING ROUTINE C CHECK, FOUND NUMBER 4 MAIN FUEL TANK FITTING CRACKED AT STATION 239.793 BETWEEN FRONT SPAR AND STRINGER 18. REPAIRED PER ALL APPLICABLE DATA.SDR IXXA060123SAttach Angle · crackedDURING ROUTINE C-CHECK FOUND RIGHT WING INTERIOR OF PANEL NUMBER 546 FORWARD INBOARD VERTICAL ANGLE CRACKED. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED ANGLE. FABRICATED NEW ANGLE, LOCATED, DRILLED, DEBURRED, TRIMMED, TREATED, PRIMED, INSTALLED NEW ANGLE SDR UPS04842653Fitting · corrodedINSPECTION TYPE:C2 LEFT WING FLAP HINGE 98 CANOE FITTING IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED FITTING IAW DWG 5614372 AND M/M 27-51-12.SDR UPS04842648Bracket · crackedINSPECTION TYPE:C2 BOOST PUMP BRACKET IS CRACKED IN NR 4 ALT BETWEEN XRS 463-XRS 428, ON STRINGER 58 AND 59. REMOVED AND REPLACED BRACKET IAW DWG 3645611 AND SRM 51-1-20D AND DWG 3645612.SDR UPS04842647Fitting · crackedINSPECTION TYPE:C2, NR 1 ALT TANK BOOST PUMP FITTING IS CRACKED AT STRINGER 58 BETWEEN XRS 463-XRS428. REMOVED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D.SDR QXEA200400422Attach Bracket · crackedPDX - RIGHT HAND WING AT BOTTOM LEADING EDGE 611E ATTACH BRACKET CRACKED, YW138, BOTTOM SPAR CAP. REPAIRED IAW SRM 51-40-00.SDR IXXA060423SAngle · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TEE ANGLE CRACKED AT STATION XRS162. REPAIRED PER ALL APPLICABLE DATA.SDR 2004FA0000567Mount · crackedFOUND AT 100 HOUR INSPECTION. NOSE GEAR ACTUATOR MOUNT, CRACKED AFT OF NOSE GEAR ACTUATOR.SDR UPS04242555Tee Fitting · crackedINSPECTION TYPE: C, TEE FITTING CRACKED ON UPPER I/B T-EDGE PANEL FOR APU EXHAUST 70.5 WBL. REPAIR CARRIED OUT IAW SRM 51-40-4 & 51-10-2.SDR 04FDEA01255Stop · gougedLT WING O/B FLAP, O/B FLAP TRACK STOP GOUGED. REMOVED AND REPLACED TRACK STOP IAW MM 20-50-02-2.SDR DHL2004754008Mount Bracket · crackedDURING C-CHECK, RT WING NR 6 KRUEGER FLAP ACTUATOR MOUNT IS CRACKED AT LOWER CORNERS. REMOVED ACTUATOR MOUNT, FABRICATED REPLACEMENT PART 7075-T6, .063 PO 900861 (8 X 3) IAW B727 SRM 57-20-2 RM171 FIG 1. TREATED AND PRIMED IAW B727 SRM 51-10-2 AND INSTALLED SDR UPS04842390Fitting · crackedINSPECTION TYPE: C1, INSIDE NR 1 ALT FUEL TANK STATION XRS 440 STRINGER 58 BOOST PUMP FITTING IS CRACKED. REMOVED, FABRICATED AND REPLACED FITTING IAW DWG 3645611 AND SRM 51-1-20D.SDR UPS04842402Fitting · crackedINSPECTION TYPE: C1, NR 2 MAIN TANK STRINGER 51 AT XRS 50 IS CRACKED. REMOVED AND REPLACED FITTING IAW DWG 4614391 AND SRM 51-1-20D.SDR UPS04842394Fitting · crackedINSPECTION TYPE: C1, NR 3 MAIN FUEL TANK HAS STRINGER 51 END FITTINGS CRACKED AT XRS 74. REMOVED AND REPLACED FITTINGS IAW DWG. 3704841 AND SRM. 51-1-20D, 51-3-0SDR DHL2004802004Fitting · crackedLT X3 WING TO FUSELAGE FITTING CRACKED. REMOVED AND REPLACED LT STA. X3 WING TO FUSELAGE FITTING IAW DOUGLAS DRAWING 589477 AND DC-8 SRM 51-1-20.SDR SROM200400049Fitting · crackedDURING D CHECK INSPECTION RT WING REAR SPAR TO MLG SUPPORT BEAM FITTING CRACKED AT IB UPPER CORNER. REMOVED DAMAGED MLG SUPPORT BEAM FITTING AND INSTALLED A NEW MLG SUPPORT BEAM FITTING IAW ASA EA 5720-01238 AND EA 10325.SDR SROM200400046Fitting · crackedDURING D CHECK INSPECTION COMPLIED WITH EA 10324 AND ASA EA 5720-01237 (LT WING MLG SUPPORT BEAM FITTING INSPECTION AND REPLACEMENT, SB 737-57-1216 REV. 2) REMOVED AND REPLACED LT WING SUPPORT BEAM FITTING IAW ASA EA 5720-01237 AND AAR EA 10324.SDR UPS04842121Fitting · corrodedINSPECTION TYPE: C3, LEFT WING FLAP HINGE 219 CANOE FITTING HAS PITTING CORROSION. MILLED OUT CORROSION, FABRICATED AND INSTALLED REPAIR FILLERS IAW SB 27-164.SDR AUS20040215Fitting · corroded(AUS) LT WING AFT LOWER ATTACHMENT FITTING PN 5011024-2, LT WING AFT UPPER ATTACHMENT FITTING PN 5011023-1, RT WING AFT LOWER FITTING PN 5011024-2 AND RT WING AFT UPPER FITTING PN 5011023-1 ALL CONTAINED INTERGRANNULAR CORROSION.SDR 2004FA0000400Attach Bracket · crackedDURING AN ANNUAL INSPECTION THE WELD JOINT THAT ATTACHES THE UPPER WING SKIN ATTACH BRACKET TO THE UPPER MAIN WING SPAR CENTER SECTION JUST ABOVE THE UPPER LT WING ATTACHMENT FITTING WAS CRACKED. MANUFACTURER WAS CONTACTED AND REPAIR INSTRUCTIONS WERE PROVIDESDR SWAA040824Attach Angle · crackedDURING SCHEDULED SPV, FOUND LT WING LOWER ATTACH ANGLE AT WBL 135.5, S2, CRACKED. REMOVED AND REPLACED LT WING ATTACH ANGLE PER SRM.SDR DHL2004750024Bracket · crackedDURING -C- CHECK, NR 1 LEADING EDGE FLAP ACTUATOR BRACKETS TRUNNION SUPPORT CRACKS BOTH SIDES I/B & O/B. REMOVED AND REINSTALLED NR 1 L/E FLAP ACTUATOR IAW B727 MM 27-81-22. REMOVED BRACKETS FROM NR 1 L/E FLAP ACTUATOR IAW B727 SRM 51-30-2, 2EA LEFT & RIGHTSDR DHL2004809003Fitting · crackedRIGHT-HAND WHEEL WELL STA 931 FALSE SPAR STA 1.50 FITTING IS CRACKED 1.50 INCH LONG FORWARD TO AFT. DEFERRED IAW GMM 3.5 CAT 1. REF BOEING SERVICE ENGINEERING TECH & FLEET SUPPORT LETTER DHL-CVG-04-00024H 15MAR04. ENTERED AS DMI 16041E. ONLY 2 REVENUE FLIGSDR 04FDEA00588Fitting · crackedLEFT WING O/B FLAP STOP FITTING FOUND CRACKED. LT WING O/B FLAP CRACKED STOP FITTING REMOVED AND REPLACED AS PER SRM 51-33-01 VOL. II.SDR ABO2004F00000Fitting · crackedWHILE PERFORMING ROUTINE 36 MONTH/1000 HOUR WING BOLT INSPECTION, A CRACK WAS DISCOVERED USING DYE PENETRANT INSPECTION METHOD. THE CRACK WENT FROM WING BOLT HOLE, THROUGH THE RADIUS UP TO THE FITTING (FLAT AREA).SDR UPS04442042Fitting · crackedINSPECTION TYPE: C, CRACK FOUND AT NR 1 DIA BRACE UNDERWING ATTACHED FITTING'S MOST AFT HOLE OF THE O/B ROW, CRACK LENGTH .125 INCH LONG APPROX AT THE UPPER SURFACE. CRACKED HOLE REPAIRED PER RS R57-04-35118 AND EO B747-5740-20132-A.
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