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 9714289610Clip · corrodedDURING M CHECK, FOUND CORROSION ON STRINGER CLIP FITTING AT RIGHT WS 1137 BETWEEN STR 11 AND 12. REPLACED FITTING PER SRM 51-30-5.SDR DL72K971364Stiffener · crackedRIGHT WING L/E SPAR STIFFENERS CRACKED AT THREE LOCATIONS, INBD SPAR STIFFENER CRACKED AT NR 6 SLAT INBD TRACK AND INBD SPAR STIFFENER CRACKED AT NR 7 SLAT INBD TRACK, OTBD SPAR STIFFENER CRACKED AT NR 7 SLAT O/B TRACK. REPAIRED PER MM 57-20-21.SDR CKSA97351Bracket · brokenDURING C1-12 CHECK INSPECTION, FOUND UPPER TRAILING EDGE PANEL SUPPORT BRACKET BROKEN JUST INBOARD OF NR 6 SPOILER APPROX WS 400. REMOVED AND REPLACED WITH NEW PART IAW B747 SRM 51-10-1 AND 51-30-02, (7075-T6). C-CHECK WORK CARD NUMBER 7CI5709. NON-ROUTINE SDR CKSA97339Chord · crackedDURING C1-12 CHECK INSPECTION, FOUND UPPER CHORD OF WING L/E NOSE BEAM ILES 949.55 CRACKED. REPAIRED UPPER CHORD OF WING L/E NOSE BEAM 949.55 IAW B747 SRM 51-40-03, (7075-T6). C-CHECK WORK CARD NUMBER 7CI6010. NON-ROUTINE TASK CARD NUMBER 109841.SDR AALA971222Stiffener · corrodedTUL - CORROSION AT UPPER NUTPLATE ON VERTICAL STIFFENER. REMOVED AND REPLACED CORRODED STIFFENER PER SRM 51-10-4, PAGE 4. TST: 53,888 HOURS. CYCLES, 34,468. (X)SDR MWEA97616T-Angle · corrosionDURING D-CHECK, FOUND CORROSION ON LEFT WING LOWER T-ANGLE STATION 58 ON OUTBOARD LEG BETWEEN STRINGERS 11 AND 12. MTC REPAIRED IAW DAC DRAWING 5910465.SDR MWEA97612Doubler · misrepairedDURING D-CHECK, FOUND PREVIOUS REPAIR ON RIGHT WING LOWER SKIN AFT SPAR DOUBLER STATION XRS 214. MTC REPAIRED IAW DOUGLAS TELEX SVC-ORD-0107 GLP.SDR UPS97824015Angle · crackedINSPECTION TYPE-D, RT WING L/E AT NR 4 PYLON I/B SIDE SLOT ISLAND MOUNT ANGLE ABOVE PYLON IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT ANGLE IAW SRM 51-1-21, AND DWG 9753293.SDR COMA9710323Channel · wornLEFT WING FAIRING COMPOSITE HAS SLIGHT DELAMINATION AT EDGE. REPAIRED WING FAIRING IAW SRM.SDR UPS97824021Angle · crackedINSPECTION TYPE-D, RT WING L/E AT STA XS246.519 TO XS250.089 VERTICAL STIFFENER IS CRACKED AT BOTTOM. REMOVED, FABRICATED AND INSTALLED REPLACEMENT STIFFENER IAW SRM 51-1-21 AND DWG 9753293.SDR UPS97824019Intercostal · crackedINSPECTION TYPE-D, RT WING L/E SECTION BTWN PYLONS AT STA XS454.976 INTERCOSTAL IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT INTERCOSTAL IAW SRM 51-1-21.SDR ABXA9701186Clip · crackedDURING C-CHECK, FOUND SHEAR CLIP AT STRINGER 11 AND W/STS 69 CRACKED. REPLACED SHEAR CLIP IAW DC-9 SRM 51-30-5.SDR AALA971292False Spar · corrodedTUL - CORROSION ON FALSE SPAR, UPPER CAP. BLENDED AND SMOOTHED PER ESO 7349 DATED 7-10-97. TST: 71,127:03 HOURS. CYCLES: 29,268. (X)SDR UPS97223582Web · crackedINSPECTION TYPE:SI, WHILE WORKING CUSTOMER CARD 696188 FOUND VENT BOX WEB TO BE CRACKED. REPLACED WEB/COVER IAW SRM 51-10-1, 51-10-2, 51-20-4, 51-30-2.SDR UPS97824271Tripler · crackedINSPECTION TYPE-D, LT WING L/E, JUST INBD OF THE STA XOLDI 6.225 RIB, THE UPPER SLOT DOOR AFT TRIPLER IS CRACKED IN TWO. REMOVED, FABRICATED, AND INSTALLED REPLACEMENT TRIPLER IAW 51-1-21, 51-9-0, AND DWG 5770409.SDR UPS97824079Doubler · crackedINSPECTION TYPE-D, LT WING LWR L/E SKIN AT THE NR 2 PYLON CUTOUT, INTERNAL AND EXTERNAL REPAIR DOUBLERS ARE CRACKED. FABRICATED AND INSTALLED REPLACEMENT DOUBLERS IAW SRM 57-2-1.SDR UPS97824012Angle · crackedINSPECTION TYPE-D, LT WING L/E AT THE AFT OTBD CORNER OF THE INBD SLOT STA XS250.089 AFT SIDE BOTTOM, THE RIB TO SLOT AFT WEB ATTACH CLIP IS CRACKED. REMOVED, FABRICATED AND INSTALLED REPLACEMENT CLIP IAW SRM 57-3-2, AND 51-1-20D.SDR MWEA97582Splice · gougedDURING D-CHECK, FOUND SEVERAL DEEP TOOL MARKS ON CENTER FUEL TANK STRINGE NUMBER 20 SPLICE. MTC REMOVED AND REPLACED SPLICE IAW DOUGLAS DRAWING 3913324-501 AND 39133241 AND IAW SRM 51-22-1.SDR MWEA97581Splice · gougedDURING D-CHECK, FOUND SEVERAL DEEP TOOL MARKS ON CENTER FUEL TANK STRINGER SPLICE NUMBER 13. MTC REMOVED AND REPLACED SPLICE IAW DOUGLAS DRAWING NUMBER 3919256 AND SRM 51-22-1.SDR MWEA97578Angle Bracket · corrosionDURING D-CHECK, FOUND MODERATE HEAVY CORROSION ON RT WING TRAILING EDGE SECTION AT INBOARD AFT ANGLE BRACKET. MTC REPAIRED IAW SRM 51-30.SDR CKSA97289Angle · crackedDURING ACCOMPLISHMENT OF CPCP CHECK INSPECTION, FOUND LEFT HAND WING INTERNAL STA BL 348.0 SUPPORT ANGLE IS CRACKED, MARKED M6. REMOVED AND REPLACED SUPPORT ANGLE STA BL 348.0 IAW B727 SRM 51-10-01. CORROSION TASK CARD NUMBER C57-571-01. NON-ROUTINE TASK CASDR CKSA97286Doubler · crackedDURING ACCOMPLISHMENT OF CPCP CHECK INSPECTION, FOUND LEFT HAND WING INTERNAL STA 686.50 AFT STRINGER TO RIB ATTACH POINT DOUBLER IS CRACKED, MARKED M3 LOWER. REPAIRED IAW BOEING SRM 57-10-5 AND BSB 727-570127 FIGURE 2. CORROSION TASK CARD NUMBER C57-571-01.SDR W8PA971192Support · crackedT/E SUPPORT BRACKET IS CRACKED. REPLACED WITH NEW PART. (M)SDR UPS97823789Fitting · crackedINSPECTION TYPE:D, WING BOX, INTERCOSTAL/ATTACH FITTING CRACKED F/S 820 RBL 65. REMOVED AND REPLACED FITTING IAW SRM 51-1-20D.SDR ABXA9701406Doubler · crackedDURING C-CHECK, FOUND CRACK EMANATING FROM FASTENER HOLE AT RIGHT WING STATION XFS 518. REPAIRED INTERNAL DOUBLER IAW ABX REA D857-20383MR.SDR AALA971109Stiffener · crackedTUL - UPPER SPAR STIFFENER NR 9 CRACKED, STA 656.50, LEFT WING. CRACK ENDED IN FASTENER HOLE. INSTALLED REPAIR PER BOEING SB 727-57A 159. TST: 55,431 HOURS. CYCLES, 34,330. (X)SDR UPS97824025Chord · corrosionINSPECTION TYPE-D, FS 857 AT LBL 16 CENTER WING BOX UPPER AFT CHORD HAS HEAVY CORROSION. REMOVED AND REPLACED CHORD IAW SRM 51-1-21.SDR TWAA9810108Angle · crackedMCI - DURING OP 15 MAINTENANCE CHECK, FOUND ON RT WING THE SUPPORT ANGLE FROM FRONT SPAR TO NR 35 SLAT OTBD DRIVE TRACK ROLLER SUPPORT CASTING, CRACKED AT OTBD ANGLE. REMOVED AND REPLACED PLATE ON FORWARD SPAR PER SRM 51-01, PAGE 1 ITEM C, AND DAC DWG 991933SDR AU970761Fitting · cracked(AUS) WING STRUT ATTACHMENT FITTING CRACKED - FOUND DURING MAGNETIC PARTICLE INSPECTION IAW AD/CHA22/2 - CRACK ORIGINATED FROM AIRCRAFT TIEDOWN ATTACHMENTSDR MWEA97524Angle · crackedDURING C-CHECK, FOUND CRACK ON LEFT WING OUTBOARD SPOILER SUPPORT RIB T-STATION XTE 342. MTC REMOVED AND REPLACED T-ANGLE IAW SRM 51-30-2 AND 51-30-8.SDR DLL10971145Skate Angle · crackedA CRACK WAS FOUND IN ON OF THE OUTBOARD SKATE FWD ATTACH HOLES ON THE LT WING PYLON. THIS CRACK WAS LOCATED IN THE UPPER MOST FORWARD ROW OF FASTENERS AND EXTENDS HORIZONTALLY TO THE FORWARD FREE EDGE OF THE PART. THE DAMAGE WAS REMOVED.SDR CKSA97274Angle · crackedDURING CPCP CHECK INSPECTION, FOUND INTERNAL RIGHT WING TANK STA WS 519.0 RIB TO STRINGER ATTACH ANGLE CRACKED JUST AFT OF ACCESS PANEL MARKED M1. INSTALLED DOUBLER REPAIR IAW B727 SRM 51-40-4 FIGURE 1. CORROSION TASK CARD NUMBER C57-571-01 PART 2 OF 2. NONSDR 97FDEA00333Rub Strip · grovedDOUBLER AT RT WING TO CENTER SECTION HAS DEEP GOUGE CAUSED FROM WING/FUSELAGE FILLET RUBBING DOUBLER. (ANB 7309 SPLICE PLATE AT SCW = 118.20.) BURNISHED AREA. PERFORMED HFEC, NO CRACKS INDICATION FOUND. MEASURED GOUGE AT FW END .065 DEEP TAPERED AFT TO 0,SDR WRLADRC0267Rub Strip · corrodedLEFT WING UPPER SURFACE, FUEL TANK ACCESS PANEL CUT OUT NR 534 FOUND CORRODED. STRIP RELEASED A PER MD-11 SRM VOL 151-00-01 REV 20. (M)SDR CALA9700934Angle · crackedINSPECTION FOUND A 2.875 INCH CRACK IN RT WING LEADING EDGE RIB ANGLE AND DOUBLER BETWEEN 5R AND 6R SLAT TRACKS AT STA XRS 164. A DOUBLER AND STRAP WERE FABRICATED AND INSTALLED IAW ECRA 5710-01645.SDR CALA9700933Angle · crackedINSPECTION FOUND A .375 INCH CRACK IN RT WING LEADING EDGE RIB AFT ANGLE, LOCATED AT FIRST RIB OUTBOARD OF 8R SLAT TRACK, STA 270 XRS. A .375 INCH CRACK WAS ALSO FOUND IN RT WING LEADING EDGE RIB AFT ANGLE, LOCATED AT SECOND RIB OUTBOARD OF 8R SLAT TRACK, STASDR 97ZZZM724T-Chord · crackedDURING C-CHECK INSPECTION DISCOVERED CRACKED AND BROKEN UPPER 'T' CHORDS OF BOTH THE LEFT AND RIGHT WINGS AT THE TRAILING EDGE BEAM AT WBL 235.2. RIGHT WING HAD AN 2 INCH CRACK AND THE LEFT WING HAD A BROKEN FORWARD EDGE OF THE FORWARD HORIZONTAL FLANGE OF THSDR SCNA97245Angle · crackedDURING HEAVY MAINTENANCE VISIT, FOUND THE RIGHT WING TRAILING EDGE PANEL SUPPORT ANGLES (2 EACH) CRACKED AT SUPPORT STRUTS BETWEEN SPOILER ACTUATORS NUMBER 12 AND 13. REMOVED, FABRICATED, AND INSTALLED NEW ANGLES AND ROD ASSY PER B727 SRM 57-30-0, 51-30-2, 51SDR CALA9700932Angle · crackedINSPECTION FOUND A .378 INCH CRACK IN LT WING LEADING EDGE RIB AFT ANGLE, LOCATED AT FOURTH RIB INBOARD OF 12L SLAT TRACK, STA XRS 424. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-5.SDR CALA9700931Angle · crackedINSPECTION FOUND A 2.75 INCH CRACK IN LT WING LEADING EGDE RIB LOWER ANGLE/DOUBLER BETWEEN 5L AND 6L SLAT TRACKS, STA XRS 164. DOUBLERS WERE INSTALLED IAW ECRA 5710-01645.SDR UPS97823638Rib · crackedINSPECTION TYPE:D, LT WING L/E RIB AT STA XES760.0 IS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW SRM 57-2-0.SDR 97ZZZX2873Stiffener · crackedFOUND .50 INCH CRACK IN STIFFENER ON RIB, PIPER PN 40423-13. REPAIRED IAW AC43.13. CRACK IS LOCATED ADJACENT TO WHEEL BUMPER IN UPPER WHEELWELL AND SUSPECT WAS CAUSED BY FATIGUE FROM GEAR RETRACTION.SDR ZZDA5711397Skin · corrodedDURING C-CHECK, FOUND CORROSION AROUND SCREW HOLES IN LEFT MAIN GEAR SUPPORT STRUCTURE. REMOVED CORROSION AROUND SCREW HOLES AND OVERSIZED 14 EACH HOLES TO .25 INCH IAW AERO CORP E.O. 97-580 AND RES 04452. MATERIAL LOSS LESS THAN .005 INCH. INSTALLED PANEL SDR IXXA9700122Slot Door · crackedDURING ROUTINE C-CHECK INSPECTION, TWO CRACKS WERE FOUND ON THE RIGHT WING INBOARD LEADING EDGE SLOT DOOR. REPAIR ACCOMPLISHED STOP DRILLING THE ENDS OF THE CRACKS, FABRICATION AND INSTALLATION OF AN EXTERNAL REPAIR DOUBLER IN ACCORDANCE WITH DER APPROVED DRASDR CALA9700967Aux Spar Chord · crackedINSPECTION FOUND A 2 INCH CRACK IN LT WING AUX SPAR LOWER CHORD. THE CRACK WAS LOCATED AT INBOARD END FORWARD OF NR 7 SPOILER ACTUATOR SUPPORT FITTING. THE CRACKED SECTION OF CHORD WAS CUT OUT, A REPLACEMENT CHORD AND SPLICE WERE FABRICATED AND INSTALLED IAWSDR IXXA9700111Angle · corrodedDURING ROUTINE C-CHECK INSPECTION, THE WEB SUPPORT ANGLE ON REAR SPAR UPPER CHORD WAS FOUND TO BE CORRODED AT STATION 857. REPAIR ACCOMPLISHED REMOVAL OF DAMAGED ANGLE, FABRICATION AND INSTALLATION OF TWO REPAIR ANGLES IN ACCORDANCE WITH DER APPROVED DRAWING SDR P5CA9700532Support Rod · brokenLT WING FLYING PANEL O/B SUPPORT ROD SHEARED AT LOWER END. REMOVED AND REPLACED ROD ASSY, RIGGED PANEL PER MM 57-22-02.SDR P5CA9700530Wing Tip · corrodedLEVEL 1 CORROSION RT WING TIP, UPPER SKIN PANEL IS CORRODED AND DELAMINATED. FABED AND INSTALLED NEW PANEL PER BOEING SRM 51-30-02.SDR DL757971067Wedge · delaminatedT/E WEDGE UPPER FWD EDGE DELAMINATED. REPLACED T/E WEDGE PER SRM 57-43-02.SDR 97ZZZX2907Cap Angle · crackedDURING PHASE 1-4 INSPECTION, FOUND RT WHEELWELL CAP ANGLE CRACKED AT AFT END. HARD TO TELL WHAT CAUSED CRACK OTHER THAN INSTALLATION OR NORMAL USE.
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