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 08FDEA03004Fairing · chafedLEFT WING INBD FAIRING PANEL 535 DL IS CHAFED. REPAIRED THE LT WING INBD FLAP FAIRING PANEL 535 P/N ARC 0740-501 BY FABRICATING & BONDING THE SKINS; CORE; DOUBLERS; PHENOLIC FILLERS & INSTALLED HARDWARE IAW EA 8-5750-116997; DWG ARC 0740 & TPS - 1001; RESDR 08FDEA02987Structure · corrodedFOUND CORROSION UNDER STATIC DISCHARGER RT WING TIP. REPAIR PERFORMED BY BLEND OUT THE CORROSION, CUT THE AREA AND PERFORM A PATCH REPAIR IAW RAS/FOK/008/2008 ISS A, APPROVED BY EA 6-5730-120120.SDR 08FDEA02983Retainer · corrodedLEFT MLG W/W LOWER FWD WING PANEL HAS CORROSION ON SEAL RETAINER STRIP NEAR LOWER MLG SUPPORT BEAM, WSS 217. REMOVED AND REPLACED LEFT MLG W/W LOWER FWD WING PANEL SEAL RETAINER AT WSS 217 REF SRM 51-30-2 PG 2 AND DWR 65-21656. THIS IS CLASSIFIED AS A MINOR SDR UPS08652869Web · crackedRT WING L/E NOSE BEAM LOWER SUPPORT WEB FOUND CRACKED AT ILS 676 (CRACK LENGTH 1.25") RT WING L/E NOSE BEAM SUPPORT WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 648 AND OSS 694.SDR UPS08652868Web · crackedLT WING L/E STA 525 FWD NOSE BEAM WEB LT WING AREA CRACK. (CRACK LENGTH .7500" APPROX). LT WING L/E FWD NOSE BEAM WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6, AND OSS 565.9 REF HX NRC NR 50462 FOR WORKING DETAIL.SDR UPS08652867Web · crackedLT WING L/E STA 504 FWD NOSE BEAM WEB LWR AREA CRACK (CRACK LENGTH 1" APPROX). LT WING L/E FWD NOSE BEAM WEB REPLACED IAW SRM 51-10-02 AND INSTALLED IAW SRM 51-40-02 JUST BETWEEN OSS 499.6 AND OSS 565.9.SDR UPS08M52865Structure · crackedINSPECTION TYPE-C, RT WING LWR WINGLET FOUND CRACKED AT AFT FITTING. DURING BOROSCOPE INSPECTION. RT WING LOWER WINGLET CRACKED AFT FITTING REPLACED IAW EO MD11-5720-276 80-A APPENDIX E.SDR UPS08M52864Structure · crackedINSPECTION TYPE-C, LT WING LOWER WINGLET FOUND CRACKED AT AFT FITTING DURING BOROSCOPE INSPECTION. LT WING LOWER WINGLET CRACKED AFT FITTING REPLACED IAW EO MD11-5720- 27680-A APPENDIX D.SDR 08FDEA02864Support · crackedLEFT WING OUTBD FLAP, INBD HINGE, FAIRING ATTACH BRACKET IS CRACKED AFT OF THE FLAP TRANSMITTER IN THREE LOCATIONS. REMOVED FAIRING TO FOM REF DC/MD-10 SRM 51-31-01; VOL II. REMOVED THE -1 TEE, -19 CLIP, -51 CLIP AND -1 CRACKED BRACKET REF DC/MD-10 SRM 51-31SDR 08FDEA02838Channel · crackedGENERATED BY EO NR 7-5710-7-4322 RT WING, STA 686.5 WEB FWD ATTACH "Z" CHANNEL CRACKED, OUTBD. REMOVED DAMAGED "Z" CHANNEL, LOCATED AND DRILLED NEW "Z" CHANNEL AND INSTALLED. REFERENCE SRM 51-30-2. CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02837Bracket · misalignedRIGHT WING TANK UNIT (PROBE) CONTACTING STRINGER 11 REPAIR AT WS 686.5. FABRICATED NEW QUANTITY INDICATOR BRACKET AND INSTALLED. REF EA NR 7-5710-114010. THIS IS CLASSIFIED AS A MAJOR.SDR 08FDEA02832Intercostal · crackedLEFT WING TIP INSIDE PANEL NR 528 DB INTERCOSTAL UPPER ANGLE IS CRACKED IN NUMEROUS PLACES. REMOVED LEFT WING TIP IAW MD-10 AMM 57-23-01-2. REPAIRED THE WING TIP IAW DC/MD-10 SRM 57-00-01, FIG 4, VOL I AND SRM 57-20-00, VOL I. COMPLIED WITH FEDEX EA 8-572SDR 08FDEA02778Retainer · corrodedRT WING REAR SPAR LWR CHORD, APPROX 12" IB OF FWD MLG TRUNNION, SEAL RETAINER CORRODED AT OB END. REMOVED FAIRING AND SEAL RETAINER REF SRM PG 2 LOCATED AND DRILLED NEW SEAL RETAINER REF SRM 51-30-5 PG 1, INSTALLED SEAL RETAINER AND FAIRING REF SRM 51-30-2SDR 08FDEA02713Retainer · corrodedLT WING LOWER T/E PANEL SEAL RETAINER IS CORRODED WS 167 TO 222 JUST AFT OF AFT SPAR LWR CHORD FABRICATED NEW, 2 EA SEAL RETAINERS ON LT WING LOWER T/E PANEL FROM WS 162 TO 222. REF DWG 65-21656-88, TREATED, PRIMED, AND INSTALLED REF SRM 51-10-2 PG 1-7, 51-3SDR UPS08852790Structure · damagedINSPECTION TYPE-C2, RT WING LE AUX TANK UPPER T CAP HAS DOUBLE DRILLED HOLE STA. XFS 92. FABBED AND INSTALLED REPAIR DOUBLER IAW SRM, 51-1-8, 51-1-26, 57-2-1 F IG37.SDR 08FDEA02633Web · crackedLEFT WING INBD T/E NR 4 JACKSCREW/ELEPHANT EAR FAIRING. CRACKED AT UPPER AFT INBD CLOSER WEB INSTALLED DOUBLER AND FILLER REF SRM 51-40-2 PG 6, THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02579Bracket · corrodedSEAL RETAINER ON SNRM NR N00362 IS CORRODED. FOUND BRACKET UNDER RETAINER CORRODED AT WS 167 TO 222 AFT OF SPAR LOWER CHORD. REPLACED BRACKET (STIFFENER) ON NON ROUTINE W/U NR N00362. SEE ITEM NR 16 ON JPF. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA02568Support Angle · crackedRT WING LWR FIXED T/E PANEL BELOW NR 14 SPOILER ACTUATOR. FLAP TRACK SUPPORT ANGLE CRACKED. REMOVED AND MANUFACTURED NEW O/B ANGLE FOR NR 8 FLAP TRACK SUPPORT BRACKET REF BOEING DRAWING 69-22894-9 AND SRM 51-20-1. INSTALLED NEW MANUFACTURED ANGLE ON BRACKETSDR UPS08852749Fitting · gougedINSPECTION TYPE-C2, LT WING FLAPWELL FITTING BENT AND GOUGED BELOW FLAP STA 98 ACTUATOR. REMOVED AND INSTALLED FITTING AT FLAP STA 98 IAW SRM 51-3-0, 51-1-8, 5 1-3-1.SDR 08FDEA02467Angle · crackedRT WING L/E STA 90 VERTICAL ANGLE CRACKED LWR SIDE. FABRICATED REPAIR ANGLE FILLER FROM 7075-T6 .050 PO NR 9007294 DIMS 7 INCH BY 2 1/2 INCH, FILLER 2 INCH BY 1 INCH. INSTALLED REPAIR PARTS AT RT WING LE STA 90 IAW SRM 51-40-3 FIG 1, SRM 57-20-2 FIG 1 AND SRSDR UALA2008111303552Structure · damagedDAMAGE TO LWR CHORD IN LT AC BAY ABOVE PLENUM. MAJOR REPAIR ACCOMPLISHED. AFTER HEAT TREAT AND CAD PLATING INSTALLED ANGLES, STRAP AND CHORD SECTION. LOWER CHORD REPAIRED PER UA-EVA-71685.SDR 08FDEA02383Channel · damagedFOUND A DOUBLE HOLE IN LT WING TIP END RIB CHANNEL. REPAIR PERFORMED BY OVERSIZING, PLUGGED THE HOLE AND FASTENER INSTALLATION AT ORIGINAL LOCATION IAW RAS /BAE/1007232/2008 ISS A, APPROVED BY EA 6-5730-120058.SDR 08FDEA02372Web · crackedCRACK ON LEFT WING TRAILING EDGE WEB JUST OUTBOARD OF NR 7 SPOILER FITTING. CUT-OUT DAMAGED AREA, FABRICATED NEW DOUBLER, FABRICATED WEB, & INSTALLED REPAIR PARTS IAW SRM 51-30-2, AND DRAWING SR27-57-038.SDR 08FDEA02294Stiffener · corrodedRT MLG STRUT WELL LWR FIXED PNL SEAL RETAINER ASSY IS CRACKED/CORRODED ALONG WING SPAR CHORD WS 190-220 REMOVED 4 HYD STANDOFFS AND 2 SEAL DEPRESSORS FROM STA 180-220. REMOVED DRAIN TUBE, TE FAIRING PANEL, TE FIXED PANEL RT. FABRICATED 2 NEW SEAL RETAINERS OSDR 08FDEA02293Support · crackedLEFT WING T/E SPAR AREA; NR 4 SPOILER OUTBD HINGE INNER WEB HAS A REPAIR INSTALLED THAT IS CRACKED IN THE RADIUS. THE NR 4 SPOILER IS REALLY THE NR 2 OUTBD. REMOVED SKIN SUPPORT IAW A300-600 SRM 51-40-21; PG 7. LOCATED; DRILLED AND DEBURRED SKIN SUPPORT P/NSDR 08FDEA02292Stiffener · corrodedSEAL RETAINER STIFFENER RT WING AFT LWR SPAR WS 181-220 IS CORRODED REMOVED CORROSION FROM STIFFENER AT STA 181-220 RT WING ORIGINAL MATERIAL .040 MATERIAL LOSS .010 REMAINING MATERIAL .030 OUT OF LIMITS. REMOVED STIFFENER AND FABRICATED NEW STIFFENER MATERIASDR IXX2008F00080Stiffener · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER.SDR IXX2008F00049Stiffener · crackedDURING ROUTINE C CHECK INSPECTION, FOUND RT WING TRAILING EDGE STIFFENER CRACKED AT STATION XW 19.000. REMOVED CRACKED STIFFENER. FABRICATED STIFFENER. PERFORMED NDT INSPECTION. NO CRACK, NO CORROSION FOUND. CLEANED, TREATED AND PRIMED AREA AND STIFFENER.SDR CA080617001Support · damaged(CAN) THE OTBD HOLE IN THE SPEED BRAKE TRUNNION SUPPORT IS ABOUT .5 HOLE MISALIGNED WITH THE HOLE IN THE RIB WHERE THE UPPER OTBD AILERON CABLE PASSES THROUGH ON BOTH THE LT AND RT WING. THE AILERON CABLES WERE WORN AND HAD WORN INTO THE AFT SIDE OF THE HOLE ISDR 2008FA0000416Tape · peelingSTUDENT PILOT DECLARED AN EMERGENCY AS HE THOUGHT NOISE HE WAS HEARING WAS HIS ENGINE COMING APART. AFTER SAFELY LANDING IT WAS FOUND THAT THE NOISE WAS THE ANTI-SLIP WINGWALK MATERIAL SLAPPING THE WING, IN THE SLIP STREAM. WIND GOT UNDER THE MATERIAL AND LISDR 08FDEA02177Angle · crackedLT WING L/E, FOUND 1 CRACK 1" LONG ON ANGLE INT WING TIP. REPAIR ANGLE IAW SRM 57-00-01 VOL.1 FIG.10 SHT 1.SDR 08FDEA02165Bracket · brokenRIGHT WING NR 7 SLAT TRACK CLOSE OUT PANEL HAS A BROKEN BRACKET.SDR UPS08852570Support Angle · chafedINSPECTION TYPE:C2 RT WING INBD SLOT VANE HAS A DEEP CHAFING MARK AT SUPPORT ANGLE AT OTBD SIDE. REMOVED AND REPLACED SUPPORT ANGLE IAW AMM, 51-1-24, 27-80-00.SDR 08FDEA02114Fitting · damagedFOUND TOOLING MARKS ON PICK UP FITTING GANTRY 5 LT, C 47 REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 08FDEA02089Angle · damagedLEFT WING INBD UPPER L/E PANEL 516 DT HAS A BROKEN ANGLE. REMOVED THE BROKEN ANGLE ON THE LEFT WING L/E PANEL 516 DT IAW DC/MD-10 SRM 51-31-01; VOL II. RECEIVE MATERIAL ID 7075-0, 0.050, PO 606256.5 IAW DAC DWG ARB 1261, REV IFOR THE FAB OF A NEW ANGLE. HEASDR C2XAA08TY057Panel · corrodedTYS - DURING A CURRENT 3C INSPECTION THE BONDIND STRIP ON PANEL 197CL WAS FOUND CORRODED. MAINTENANCE REPAIRED THE PANEL IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145 XR AMM 2 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE ESDR C2XAA08TY056Panel · corrodedTYS - DURING A CURRENT 3C INSPECTION PANEL 197 CL WAS FOUND CORRODED AT THE BONDING STRAP. MAINTENANCE REPAIRED THE PANEL IAW EMB 135/145 EC 5750-01315 AND PAINTED IAW EMB 145XR AMM 51-21-02. ALL WORK WAS ACCOMPLISHED AND AIRCRAFT WILL BE RELEASED AT THE ENDSDR 08FDEA02068Stiffener · crackedLEFT MLG WHEEL WELL; AFT OUTBD CORNER HORIZONTAL FRAME SUPPORT, INBD ANGLE IS CRACKED AT THE BOTTOM. REMOVED ACCESS PANELS IAW DC/MD-10 SRM 51-31-01; VOL II AND ANGLE IAW DC/MD-10 SRM 51-35-01; 51-33-01; VOL II. MATERIAL ID FOR THE ANGLE IS 7075-0, 0.063; POSDR 08FDEA02067Stiffener · crackedLEFT MLG WHEEL WELL; LEFT WING INBD WEB; 4TH ANGLE AFT OF THE MLG CUTOUT IS CRACKED. THIS SDR WAS GENERATED IN ERROR. FOR DETAILS OF THIS DISCREPANCY SEE NON-ROUTINE NR N00205 AND SDR TRACKING NUMBER 08-2066.SDR 08FDEA02066Stiffener · crackedLEFT MLG WHEEL WELL; LEFT WING INBD WEB; 4TH ANGLE AFT OF THE MLG CUTOUT IS CRACKED. REMOVED STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II. MATERIAL ID FOR THE STIFFENER 7075-0, 0.040 PO 606256.4. FABRICATED STIFFENER IAW DAC DWG ANB 7203, REVSDR 08FDEA02065Stiffener · crackedLEFT MLG WHEEL WELL; LEFT WING INBD WEB 2ND AFT ANGLE AFT OF THE MLG CUTOUT IS CRACKED. REMOVED STIFFENER IAW DC/MD-10 SRM 51-35-01 AND 51-33-01; VOL II. MATERIAL ID FOR THE STIFFENER 7075-0, 0.040. FABRICATED STIFFENER IAW DAC DWG ANB 7208, REV "AB". ALOSDR 08FDEA02064Stiffener · crackedLEFT MLG WHEEL WELL LEFT WING INBD WEB AFT OF THE MLG GEAR CUTOUT; THE FIRST ANGLE IS CRACKED AT THE BOTTOM. REMOVED COVERS IAW DC/MD-10 SRM 51-31-01; VOL II AND STIFFENER IAW DC/MD-10 SRM 51-31-01 AND 51-33-01 VOL II. MATERIAL ID FOR STIFFENER 7075-0, 0.06SDR UPS08652342Web · crackedINSPECTION TYPE:N/A LEFT WING LES 694 FWD D-NOSE FAIRING SUPPORT WEB LOWER AREA FOUND CRACKED. CRACK LENGTH 2.5 INCHES APPROX. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02, JUST BETWEEN OSS648 AND 694 AREA.SDR UPS08652341Web · crackedINSPECTION TYPE:N/A LEFT WING LES 675 FWD OF REFUEL PANEL LOWER CHORD FOUND CRACK. LEFT WING FWD D-NOSE FAIRING SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694 REFER NRC50623 FOR WORKING DETAIL.SDR UPS08M52449Strap · crackedINSPECTION TYPE:2C RIGHT WING L/E SPLICE STRAP XFS 669 CRACKED. REMOVED, FABRICATED, AND INSTALLED SPLICE STRAP IAW MD11 SRM 51-21-01, 51-33-01, AND DWG ARB3954.SDR 08FDEA01923Angle · crackedLEFT WING INBD LE CAVITY NR 2 FLAP ACTUATOR AFT MOUNT, UPPER CORNER ANGLE IS CRACKED REMOVED AND REPLACED WEB REF SRM 51-30-2. OPS CHECKED ACCOMPLISHED ON W/C 70C003-00 THIS CLASSIFIED AS A MINOR REPAIR.SDR 08FDEA01884Stiffener · crackedLEFT WING SPAR AREA, TOP SKIN STIFFENER AT WIAX 13-9 HAS A CRACK. MATERIAL ID FOR THE REPAIR IS 7075-T6 0.110 60-7018 EXTRUSION PO 566980.6 IAW A300-600 SRM 57-51-11, FIG 207 AND DWG NR A57241059. FABBED REPAIR ANGLE IAW A300-600 SRM 57-51-11, FIG 207. ALODSDR HALA0800591Seal · tornBLADE SEAL TORN ON RIGHT WING O/B AILERON UPPER BLADE. REPLACED UPPER BLADE SEAL ON RIGHT WING O/B AILERON AT TORN AREA IAW SRM 51-40-02-OG-0.SDR ASAA0873019Web · crackedBS 663.75 WING CENTER SECTION REAR SPAR LOWER RIGHT WEB (COMPOSITE PANEL) CRACKED. WING CENTER SECTION REAR SPAR AT BS 663.75 LOWER RIGHT WEB CRACK REPAIRED IAW B737 700 SRM 51 70 04 REPAIR NR 10.SDR 2008FA0000360Stiffener · misinstalledFOUND RT STIFFENER (PN 662121126) INADVERTENTLY INSTALLED IN LT POSITION. WITH LANDING GEAR IN THE STOWED POSITION, THE ACTUATOR CONTACTED THE STIFFENER AND CAUSED MINOR CHAFFING. NEITHER THE ACTUATOR NOR THE STIFFENER WERE DEFORMED/ DAMAGED. (K)
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