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 UPS97823152Tripler · crackedINSPECTION TYPE:, RT WING L/E AT STA XOLDI 6.225 TO THE INTERNAL TRIPLER IS CRACKED IN HALF. REMOVED, FABRICATED AND INSTALLED TRIPLER IAW SRM 57-3-1 AND DWG 5769891 AND SRM 51-1-20.SDR UPS97823087Trapezoidal Ftg · crackedINSPECTION TYPE:C/CK, RIGHT HAND MAIN LANDING GEAR TRAPEZOIDAL FITTING IS CRACKED AT FWD SIDE VERTICAL. REPAIRED FITTING IAW UPS EO DC8 5340 0748 PER APPENDIX D AND E USING KIT 78010659-509 IB AND O/B SPLICE RIGHT HAND.SDR SWIA97949Beam · corrodedLBL 27.00 HAS TWO SPOTS OF CORROSION ON WINGS OF BEAM AT FS 325, (ONE SPOT ON INBOARD SIDE, ONE SPOT OUTBOARD SIDE). FABRICATED AND INSTALLED A DOUBLER REPAIR OVER THE CORRODED AREA.SDR ABXA9700968Hat Channel · crackedDURING C-CHECK, FOUND PANEL NR 2206A HAT CHANNEL CRACKED. REPAIRED HAT CHANNEL IAW ABX SSRM DWG K05159.SDR UPS97223125Shear Tie · crackedINSPECTION TYPE:D, SHEAR TIE IN FUEL TANK ADJACENT TO LT MLG FWD TRUNNION FITTING REMOVED FOR INSPECTION. SHEAR TIE REMOVED IAW SRM 51-30-2.SDR HAL9773Web · crackedRIGHT WING TRAILING EDGE SUPPORT STRUCTURE BUCKLED, CRACKED, AND LEVEL 2 CORROSION JUST OUTBOARD OF SPOILER ACTUATOR, STA XRS-189. STOP DRILLED CRACK, FABRICATED DOUBLER AND WEB, AND INSTALLED PER SRM 57-01, FIG 4, SRM'S 51-30-2, 51-10-3, AND 57-01 FIG B. TOSDR 97ZZZX2107Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2106Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR 97ZZZX2105Bracket · rivet shearedDURING A 100 HOUR INSPECTION, MECHANIC NOTICED CRACK IN THE WING SKIN IN MOST AFT OTBD SECTION OF LT WING. MECHANIC ALSO OBSERVED 2 RIVETS SHEARED THAT ATTACH THE OTBD AILERON HINGE BRACKET ASSY (CESSNA P/N 5021002-12) WHICH ARE SAME RIVETS THAT ATTACH THE TSDR MWEA97343Tee · corrosionDURING INSPECT, LT WING TEE STA XCW58 EXCESS CORR. MAINT REPAIRED IAW DAC DRW 5910465 AND SRM 51-22, 51-30.SDR MWEA97341Tee · corrodedDURING INSPECT, RT WING STA XCW 58 TEE EXCESS CORR. MAINT REPAIRED IAW DAC DWG 5910465 AND SRM 51-22, 51-30.SDR MWEA97332Angle · crackedDURING INSPECT, STRING 11 LT AND RT SPLICE ANGLE VERT LEG CRACKED. MAINT REPAIRED IAW DAC DRWG 3919256.SDR UPS97822997Doubler · crackedINSPECTION TYPE:D, NR 3 PYLON TO LWR WING DOUBLER HAS A .75 INCH CRACK AT WING FRONT SPAR LWR CAP 18 INBD OF PYLON. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PARTS IAW DHC SK-894-812 (REF UPS ENRG FILE NR DC8-57-0781).SDR CALA9700659Angle · crackedINSPECTION FOUND A 5.5 INCH CRACK IN LT WING INBOARD ATTACH ANGLE AT WS XCW 118. THE ANGLE WAS REMOVED IAW SRM 51-33-01. A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-00.SDR GAIA2297Stiffener · crackedDURING C-CHECK INSPECTION, A CRACK WAS FOUND IN THE VERTICAL STIFFENER FOR THE LEFT AFT WING SPAR AT STATION 1. TRACOR FURNISHED KHA THE ORIGINAL 240-1610740C DRAWINGS TO MANUFACTURE THE REPLACEMENT PARTS. THE NEW VERTICAL STIFFENER WAS INSTALLED IAW THE GD SDR 97ZZZX2994Jo Bolts · looseATW - DURING GV ZONAL INSPECTION, FOUND EVIDENCE OF LOOSE JO BOLTS AT RIB ZERO AND RIB 2, LT/RT. REPORT FINDINGS TO AVRO/AIR. REPLACEMENT REQUIRED PER RIL HC571H9033. REMOVED AND REPLACED JO BOLTS ON RIB ZERO AND RIB 2, LT AND RT, STRINGERS 1-7 PER RIL HC57SDR AU970456Winglet · collapsed(AUS) WINGLET INNER CORE COLLAPSED - AIRCRAFT IS AMATEUR BUILTSDR 97ZZZX3141Jo Bolts · damagedATW - LEFT WING RIB 2 INBOARD AND OUTBOARD JO-BOLTS, STRINGERS 1-7, NEED REPLACEMENT PER RIL HC571H9033. REF W/C J118. REPLACED ABOVE JO-BOLTS LEFT WING RIB 2 PER RIL HC571H9033.SDR UPS97823070Doubler · crackedINSPECTION TYPE:D, RT L/E STUB WING AT NR 3 PYLON INTERIOR DOUBLER AND ANGLE CRACKED BETWEEN STA XS 246.5 AND 250. REMOVED AND REPLACED ANGLE SUPPORT AND DOUBLER IAW SRM 51-1-20.SDR UPS97222621Beam · damagedINSPECTION TYPE-SI, WHILE WORKING CUST ID C57-581-04-30 DISCOVERED O/B HOLE ON MLG BEAM COMMON TO NR 4 FLAP TRACK O/B HOLE TO HAVE THE UPPER SURFACE DAMAGED. REPAIRED PER EWO 97-2153 AND ENGINEERING FILE NR 727-57-1817 UPS.SDR RAAA97B2024Stiffener · corrodedDURING SCHEDULED S4 STRUCTURAL/CPCP INSPECTION PER CARD S4 14108, FOUND LEFT WING REAR SPAR WEB STIFFENER CORRODED AT WBL 114. REPAIRED PER SRM 51-40-4, FIG 1.SDR RAAA97B2007Stiffener · crackedDURING SCHEDULED C1 CHECK, FOUND NR 3 SPOILER OUTBOARD MOUNT STIFFENER ON REAR SPAR CRACKED AT WS 519. REPLACED STIFFENER PER SRM 51-30-02.SDR CALA9700612Wing Tip · crackedDURING D-CHECK INSPECTION, FOUND CRACK .5 LT WING TIP FASTENER FWD OF AFT NAV LIGHT. STOP DRILLED, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 57-31-01.SDR UPS97822713Splice Plate · crackedINSPECTION TYPE-D, FWD LWR SPAR TANG SPLICE PLATE CRACKED AT WING STA 421 LT WING JUST I/B NR 1 PYLON. FABRICATED AND INSTALLED IAW DC-8 SRM 51-1-21 AND DWG SRO8570014.SDR ABXA9701072Bracket · corrodedDURING D-INSPECTION, FOUND THE RIGHT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REMOVED AND REPLACED WING TIP ATTACH BRACKET IAW DC-9 SRM 51-30-1.SDR ABXA9701071Bracket · corrodedDURING D-INSPECTION, FOUND THE LEFT WING TIP REAR SPAR ATTACH BRACKET CORRODED. REPLACED BRACKET IAW DC-9 SRM CHAPTER 51-30-5.SDR ABXA9700745Angle · crackedDURING C-CHECK, FOUND REAR SPAR TRAILING EDGE RIB ANGLE ADJACENT TO OUTBOARD FLAP HINGE FITTING IS CRACKED. REMOVED AND REPLACED ANGLE IAW DC9 SRM 51-30-1.SDR UPS97222574Stiffener · corrodedINSPECTION TYPE-SI, WHILE WORKING CUST CARD 510847 FOUND ALL STIFFENERS ON THE REAR SPAR WEB TO BE CORRODED. REMOVED CORRODED STIFFENERS, PROCURED NEW STIFFENERS AND INSTALLED IAW SRM 51-30-2.SDR UPS97822656Doubler · crackedINSPECTION TYPE:D, LT WING UPPER FUEL TANK ACCESS DOUBLER, PANEL 505F, LAND OB CORNER DOUBLER CRACKED. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW SRM 57-2-1 FIG 36 AND DHC SK-818-082 (REF UPS ENRG FILE NR DC8-57- 0770.)SDR CALA9700628Angle · corrodedDURING 1/2 D-CHECK INSP, FOUND RT WING L-ANGLE HAS CORROSION. REMOVED CORROSION PER SRM 57-03.SDR CALA9700550Angle · crackedINSPECTION FOUND A .75 INCH CRACK IN LT WING LEADING EDGE RIB ANGLE JUST OUTBOARD OF 8L SLAT TRACK AT STA XRS 276. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2.SDR 97ZZZX3108Stiffener · crackedATW - RIGHT WING UPPER SHROUD SKIN STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 7 AND 8). REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR 97ZZZX3107Stiffener · crackedATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT ITS FORWARD END APPROXIMATELY 1 INCH LONG. LOCATED IN AREA BETWEEN WING RIBS 7 AND 8. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR 97ZZZX3106Stiffener · crackedATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT ITS FORWARD END APPROXIMATELY 1 INCH LONG LOCATED IN AREA BETWEEN WING RIBS 8 AND 9. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR 97ZZZX3059Stiffener · crackedATW - RIGHT WING UPPER SHROUD SKIN OUTER STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 8 AND 9). REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR 97ZZZX3058Stiffener · crackedATW - LEFT WING TOP TRAILING EDGE SHROUD HAS A STIFFENER WITH A CRACK AT FORWARD END APPROXIMATELY 1.25 INCHES LONG LOCATED IN AREA BETWEEN WING RIBS 4 AND 5. REPAIRED TRAILING EDGE STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR UPS97822912Splice · crackedINSPECTION TYPE-D, NR 3 MAIN STA XRS 74.869 STR 51, THE FWD STRINGER SPLICE IS CRACKED IN 3 PLACES. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-1-20, 51-3-0, 57-1-0.SDR UPS97822786Doubler · crackedINSPECTION TYPE:D, L/WING IB SLOT FRAME DOUBLER CRACKED, BETWEEN STA XS 246.519 AND XS 250.089. REMOVED SKIN PER SRM 51-1-20. FABRICATED DOUBLER PER SRM 57-3-0 AND INSTALLED DOUBLER AND SKIN PER SRM 51-1-20 AND 51-1-21.SDR UPS97822773Rib · crackedINSPECTION TYPE:D, RT WING L/E SECTION BETWEEN PYLONS HAS 4 UPPER L/E RIBS CRACKED AT THE AFT END. FABRICATED AND INSTALLED REPAIR PART PER SRM 57-2-0 FIG 2 AND 57-3-3.SDR ABXA9700758Angle · crackedDURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 373. THE ANGLE WAS REPAIRED IAW DC9 SRM.SDR ABXA9700757Angle · crackedDURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 410 AND 424. THE ANGLE WAS REPAIRED IAW DC9 SRM.SDR ABXA9700756Angle · crackedDURING C-CHECK, THE WING LEADING EDGE RIB SUPPORT ANGLE WAS FOUND CRACKED AT STA 385. THE ANGLE WAS REPAIRED IAW DC9 SRM.SDR MWEA97255Doubler · incorect repairFOUND PREV REPAIR RT WING L/E REQ EVAL FOR CORRECT REPAIR. MAINTENANCE COMPLETED A REPAIR IAW DOUGLAS TELEX SVC MSP 0306 GLP DATED 11 MARCH 97.SDR MWEA97232Shear Clip · crackedSHEAR CLIP CRACKED INSIDE RT WING AT STA 164, BETWEEN STRINGER 15, 16. MAINTENANCE INSTALLED A NEW CLIP IAW SRM 51-30-2.SDR DL72S970593Stiffener · crackedFOUND ON F-1 LETTER CK, 2 SPAR STIFFENERS CRACKED 1.5. LOCATED ON INBD SIDES OF NR 2 AND NR 3 SLATS INBD SIDE OF INBD TRACK. REPAIRED PER MM 57-20-21.SDR RRXA97173Doubler · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION ON INTERNAL DOUBLER IN WING LEADING EDGE, AT XFS=17.5 RIGHT WING. FABRICATED AND INSTALLED REPAIR IAW FAA DER TIMCO ENGINEERING SKETCH REO-02979.SDR ABXA9701079Angle · corrodedDURING D-INSPECTION, FOUND THE LEFT WING INBOARD UPPER TRAILING EDGE PANEL, ATTACH ANGLE CORRODED AT LONGERON 20. REMOVED AND REPLACED ATTACH ANGLE IAW DC-9 SRM CHAPTER 51-30-1.SDR AALA970671Angle · crackedTUL - FOUND 3 INCH CRACK IN VERTICAL LEG OF EXTRUSION, STARTS AT INBOARD END. REMOVED AND REPLACED ANGLE ON E58 210 6151. (M)SDR 97ZZZX3055Stiffener · crackedATW - RIGHT WING UPPER SHROUD SKIN STIFFENER CRACKED AT FORWARD FASTENER (BETWEEN RIBS 7 AND 8). REPAIRED T/E STIFFENER IAW SRM AND AVRO FAX JM/RJ0317/97.SDR UPS97822602Angle · crackedINSPECTION TYPE-D, LT WING L/E VERTICAL ANGLE AT AFT OTBD CORNER OF SLOT HOUSING CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-3-0 AND DAC DWG 5769859.
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