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 LR7A9818Beam · crackedDURING C-CHECK/BRIDGING INSPECTION, FOUND CENTER WING REAR BEAM CRACKED AT CWS 72R, FS 597, APPROX WL 268. INSTALLED NEW INBD SECTION OF WEB, DOUBLER, AUXILIARY DOUBLER, SPACER STRAP, RADIUS BLOCK, REPAIR FINISHED.SDR CALA9800116Angle · crackedINSPECTION FOUND A 2 INCH CRACK THROUGH TWO FASTENER HOLES OF RIB SUPPORT ANGLE AT WING LEADING EDGE SLAT STA 0. THE RIB SUPPORT ANGLE WAS REMOVED AND REPLACED IAW SRM 51-10-1.SDR CALA9800114Angle · crackedINSPECTION FOUND A 6 INCH CRACK AT FASTENERS IN SUPPORT ANGLE INSIDE LT WING INBOARD LEADING EDGE AREA AFT OF NR 1 LEADING EDGE FLAP INBOARD END AT L/E STA 130. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 51-10-1.SDR ABXA9800122Intercostal · crackedLEADING EDGE STUB WING INBOARD, UPPER INTERCOSTAL CRACKED. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 5769859-37.SDR ABXA9800119Angle · crackedLEFT WING OUTBOARD OF NR 2 PYLON UPPER STIFFENER ANGLE IS CRACKED. REPAIRED IAW DC8 SRM 57-2-0.SDR ABXA9800118Bracket · crackedLEFT WING SPAR AREA AT STA XFS 63 HAS CRACKED BRACKET. REPAIRED IAW DC8 SRM 51-1-20D AND DWG 3643636.SDR P5CA9800041Fairing · wornNR 7 FIXED FAIRING CANOE NEEDS COMPOSIT REPAIR. REPAIRED FIXED FAIRING BY USING FIBERGLASS OVERLAYS IAW SRM 51-40-15.SDR DHL98727003Fitting · brokenAIRFRAME VIBRATION AND BUFFETING DURING LEFT TURNS. REPLACED BROKEN CHANNEL FITTING COVE PANEL WING STA 521 I/B SIDE. REPLACED AND ADJUSTED BROKEN ROD END IN LT COVE PANEL ASSY STA 543. INSTALLED MISSING NUT, WASHER, IN RT I/B FLAP CARRIAGE TRACK ROLLER BEARSDR 98ZZZX2762Tip · crackedATW - CLOSE OUT FAIRING AT RIB 20, LT WING TIP AREA CRACKED. PATCHED SAID CRACKED AREA IAW BAE SRM, PAINTED AND FOUND SERVICEABLE.SDR RRXA98026Doubler · misdrilledDURING A MAINTENANCE VISIT, PERFORMED INSPECTION PROCEDURES IAW SB 57-38 ON RIGHT WING AT STA 69.5. FOUND (3) MISDRILLED RIVET HOLES IN DOUBLER AND TRIPLER. REPAIRED RIVET HOLES BY OVERSIZED AND BUSHINGS INSTALLED IAW FAA APPROVED DER TIMCO ENGINEERING SKETCSDR DL72S980281Stiffeners · cracked2 EA WING L/E SPAR STIFFENERS CRACKED AT NR 4 L/E SLAT INBD TRACK ROLLER FITTING ATTACH. REPLACED STIFFENERS PER M/M 57-20-21.SDR UPS98225607Angle · crackedINSPECTION TYPE-D, TEE ANGLE AT FRONT SPAR UPPER CHORD BBL 24.5 RT CRACKED (WING CENTER SECTION INTERIOR). TEE ANGLE REPLACED IAW EO B727-5710-4575.SDR P5CA9800183Brace · crackedLEFT WING L/E RIB TO FRONT SPAR LWR CHORD TUBE BRACE FWD END CRACKED. REPLACED BRACE PER MM 20-51-01.SDR P5CA9800162Stiffener · crackedRIGHT WING STRINGER 22 WINT STA 669.5 VERTICAL STIFFENER CRACKED AT UPPER NR 1 FASTENER HOLE. REPLACED STIFFENER PER SRM 51-10-01.SDR P5CA9800129Angle · crackedRT WING T/E ACCESS PANEL 672 EB INBOARD SUPPORT FRAME AFT MOUNTING ANGLE CRACKED. SUPPORT ANGLE REPAIRED PER SRM 51-10-01.SDR P5CA9800098Chord · crackedLT WING LOWER CHORD FASTENER HOLE CRACK ON WEB AT 4 O'CLOCK POSITION. REPAIRED HOLE TO OVERSIZED TO .562 NDT NO CRACK FOUND PER HAECO RS 57-21-33654.SDR MZZA98074Stiffener · corrosionKUL - C-CHECK - CORROSION FOUND AT RT WING SPAR STIFFENER OF FRONT SPAR NR 2 FROM WS 251 (NR 5 KRUGER FLAP AREA). CORROSION REMOVED AND FOUND BEYOND LIMIT IAW SRM 57-10-1 AREA 3 INCHES BY 1.5 INCHES BY 0.024 INCH. STIFFENER REPLACED IAW SRM 51-30-2. HYDRAULSDR MWEA98072Intercostal · crackedDURING C-CHECK, FOUND RT WING TRAILING EDGE WEB AND INTERCOSTAL ASSY CRACKED AFT OF OUTBD SPOILER PANEL REACTION ARM. MTC INSTALLED DOUBLER REPAIR IAW SRM 57-01 FIG 3 SHEET 2.SDR ABXA9800033Trap Panel · corrodedDURING C-CHECK, FOUND LEFT TRAPEZODIAL PANEL UPPER HORIZONTAL FLANGE EXFOLIATED AND CRACKED. REPLACED TRAPEZODIAL PANEL IAW DC9 S/B 53-182 AND DC9 SRM 51-30-1.SDR DHL9880616CTip · crackedAT C-CHECK, LEFT WING TIP HAS TEMP REPAIR AND CRACK. CUT OUT DAMAGED SECTION AND FABRICATED DOUBLERS PER SRM 51-1-8. 9 X 6.25, FILLERS 2.5 X 5.25.SDR CALA9800078Bracket · crackedINSPECTION FOUND A .2812 INCH CRACK OUTBOARD OF NR 8 SPOILER ACTUATOR IN RT WING INBOARD TRAILING EDGE PANEL SUPPORT BRACKET AT WS 232. THE CRACK WAS STOP DRILLED IAW SRM 51-10-1, AN ANGLE REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND ECRA 5750-0287SDR 98ZZZX2763Stiffener · crackedATW - LT WING TE TOP SKIN STIFFENER CRACKED AT FORWARD BETWEEN RIBS 7 AND 8. REMOVED AND REPLACED WITH NEW PART AT TRAILING EDGE AT SKIN STIFFENERS BETWEEN RIBS 7 AND 8, LT WING.SDR AALA980111Stiffener · corrodedTUL - CORROSION ON VERTICAL STIFFENER ON FRONT SPAR ABOVE MANUAL DEFUELING VALVE. REMOVED CORRODED STIFFENER AND REPLACED WITH NEW STIFFENER AT LES 160. TST: 54,792 HOURS. CYCLES: 33,779. (X)SDR UPS98225450Bracket · corrodedINSPECTION TYPE-SI, CORROSION ON EXPANSION LINK BS 740, RBL 13, WL 165. REMOVED AND REPLACED EXPANSION LINK SRM 51-10-1, 53-10-1, 51-30-2.SDR DL72L980083Stiffener · crackedA .75 INCH CRACK NR 3 SLAT O/B TRACK VERTICAL STIFFENER ON WING FRONT SPAR. REPLACED ANGLE PER M/M 57-20-21 NR 14.SDR ASAA9840004Fitting · wornSEA - DURING C-CHECK, WEAR WAS FOUND ON THE LOWER SURFACE OF THE UPPER FLANGE ON THE RT WING T/E RIB FITTING. REPAIRED PER EA 5750-01269 AND BOEING TELEX M-7200-98-00052. (M)SDR DHL9871521CStiffener · crackedAT C-CHECK, LEFT WING VERTICAL STIFFENER CRACKED AT LOWER END ON FWD SPAR WEB. STOP DRILLED CRACK, HFEC, INSTALLED ANGLE REPAIR PER SRM 51-40-3, 1.125 X 1.125 X 6.5. N/R 1124SDR UPS99828466Doubler · crackedINSPECTION TYPE:C3, RT WING L/E LWR SKIN AT STA XFS379.0-385.25, THE INTERNAL DOUBLER IS CRACKED. REPAIRED AREA IAW SRM 57-2-0.SDR C2XA98IA003Angle · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING TO FUSELAGE FAIRING 194 LOWER ATTACHMENT ANGLE CRACKED AT AFT END. MAINTENANCE STOP DRILLED CRACK AND INSTALLED REPAIR DOUBLER IAW EMB-120 SRM 51-10-02. THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR UPS98225439Bracket · corrodedINSPECTION TYPE-SI, CORROSION (C53-132-01.00-02) ON EXPANSION LINK BS 740, LBL 13, WL 165. REMOVED AND REPLACED IAW SRM 51-10-1, 53-10-01, 51-10-01.SDR DL72W980062Angle · crackedAT HMV, FOUND BOTH O/B AND LWR I/B ANGLES CRACKED NR 6 LE FLAP ACT MNT POINT. REMOVED ACT, STOP DRILLED CRACKS, FABED DOUBLER, INSTALLED PER MM 57-20-21 FIG 807.SDR 98ZZZX344Bearing Block · corrodedRIGHT REAR BLOCK IN REAR CARRY-THROUGH BULKHEAD CORRODED IN BOLT HOLE AND INTERGRANULAR CORROSION IN BLOCK.SDR 97FDEA00908Bracket · corrodedNR 0179 058 - R/W I/B AILERON, TURNAROUND CASTING CORRODED.SDR UPS98825527Angle · crackedINSPECTION TYPE-D, RT WING L/E RIB LWR SUPPORT ANGLE CRACKED BY AFT FASTENER AT STA XOLDI 6.225. REPAIRED IAW SRM 57-2-0.SDR UPS98825510Clip · crackedINSPECTION TYPE-D, RT WING L/E CLIP CRACKED AT STA XOLDI 6.225 (ABOVE PNEUMATIC DUCT). REMOVED, FABRICATED, AND INSTALLED REPLACEMENT CLIP IAW DWG 5769589 AND SRM 51-1-29D.SDR UPS98825387Angle · crackedINSPECTION TYPE:C, LT WING L/E, INBD END, AFT UPPER CORNER, THE L/E ATTACH ANGLE IS CRACKED. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-3-0 AND DWG 5769632.SDR QXEA9800223Nut Plate Strip · crackedRIGHT HAND WING NUT PLATE STRIP FOR FUSELAGE TO WING FAIRING CRACKED JUST IN FRONT OF FORWARD LANDING GEAR LUG FITTING PANEL 92L. INSTALLED PREVIOUSLY FABRICATED DOUBLER IAW FOKKER SRM 51-31-01 AND VERTICAL FASTENER AS PER MM 20-30-5.SDR QXEA9800222Angle · crackedRIGHT HAND WING 2 STRINGER AT 2.19, 2.18, 2.17 HAVE SMALL 2 ANGLE THAT ARE CRACKED. INSTALLED NEW 2 STRINGER CONNECTION ANGLE PER FOKKER SRM 51-31-01.SDR DL72K972700Bracket · misinstalledWHILE ACCOMPLISHING INSPECTIONS MANDATED BY DAL SI 4-59271-12AD, MTC FOUND A .031 GAP BETWEEN THE NR 1 SLAT ACTUATOR AND THE SUPPORT FITTINGS. THE GAP WAS SHIMMED PER THE REQUIREMENTS OF BAC S/B 727-57-0130 AND DOCUMENTED IN ER/A 363526-14AD.SDR ABXA9701987Splice · crackedDURING AIRCRAFT LINE MAINTENANCE FOUND A CRACKED SPLICE AT STA XFS 422 IN THE RT LOWER WING LEADING EDGE. REPAIRED RT WING LOWER LEADING EDGE SPLICE IAW ABX REA D857-22097-MR.SDR ABXA9701986Splice · crackedDURING AIRCRAFT LINE MAINTENANCE FOUND A CRACKED SPLICE AT STA XFS 422 IN THE RT LOWER WING LEADING EDGE. REPAIRED RT WING LOWER LEADING EDGE SPLICE IAW ABX REA D857-22097-MR.SDR AWXA9700697Beam · crackedLEFT TRAILING EDGE BEAM CRACKED BEYOND LIMITS. REMOVED AND REPLACED LEFT TRAILING EDGE BEAM ASSY.SDR AALA972466Support · corrodedTUL - RIGHT WING LE SUPPORT HAS CORROSION. REPAIRED PER ESO30595, DATED 12-12-97. (M)SDR AALA972465Beam · corrodedTUL - RIGHT KRUGER FLAP ACT CROSSBEAM HAS CORROSION ON BEAM. REMOVED AND REPLACED CROSSBEAM PER SRM 57-45-11 PAGE 2 ITEM NR 5. (M)SDR AALA972476Trap Panel · corrodedTUL - THE INBOARD BARREL NUT HALF IN THE TRAPEZOIDAL PANEL FOR THE SIDE BRACE TO TRAPEZOIDAL PANEL ATTACHMENT IS CORRODED. FABRICATED AND INSTALLED BUSHING PER SRM 57-20-00. HOLES WERE REWORKED PER ESO 7349 DATED 12-11-97 PER ENGINEERING. TST: 67,144.30 HOSDR AALA972475Trap Panel · corrodedTUL - INBOARD BOLT HOLE FOR THE SIDE BRACE ATTACHMENT TO THE TRAPEZOIDAL PANEL CORRODED. FABRICATED AND INSTALLED BUSHING PER 57-20-00. REWORKED 4 EACH HOLES PER ESO 7349 DATED 12-11-97. TST: 67,144.30 HOURS. CYCLES: 25,370. (X)SDR DL72S972607Web · crackedA 1 INCH CRACK NR 8 SLAT ACT I/B ATTACH WEB AND .75 INCH CRACK IN O/B ATTACH WEB. REPAIRED PER MM 57-21-21 P 812.SDR AALA980329Bracket · corrodedTUL - SWITCH BRACKET A5351094120000 CORRODED IN KRUEGER WELL. REMOVED CORRODED BRACKET AND INSTALLED NEW SWITCH BRACKET PER A360 SRM 51-72-10. (X)SDR CALA9701740Angle · crackedINSPECTION FOUND A .75 CRACK IN J ANGLE AT LT WING T/E AREA JUST ABOVE AND INBOARD OF NR 7 SPOILER ACTUATOR. THE TOP PANEL WAS REMOVED. A J ANGLE BRACKET REPAIR WAS INSTALLED AND THE PANEL WAS REINSTALLED. WORK WAS PERFORMED IAW SRM 51-10-2, 51-10-1, 51-30-SDR AALA972345Gear Beam · corrodedTUL - FOUND CORROSION ON LOWER MLG BEAM AT AREA. REPAIR PER ESO 11697, DATED 11-17-97. (M)
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