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 UPS08652300Angle · crackedINSPECTION TYPE:C RIGHT WING LES 679 FRONT SPAR SUPPORT ANGLE FOUND CRACK. CRACK LENGTH .375 INCH APPROX. RIGHT WING LES 679 FRONT SPAR SUPPORT ANGLE REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02.SDR MALA080094Structure · damagedJET WAY HIT LT OUTBD WING LEADING EDGE. INSPECTED AIRCRAFT, ONLY DAMAGE FOUND WAS NR 7 POSITION LT OUTBD WING LEADING EDGE. REPLACED NR 7 LT LEADING EDGE IAW SAAB AMM 57-20. OPS CHECKED IAW SAAB AMM 30-10/ PN ON 7257211-515, SEALANT NOT APPLIED SEE BELOW FOSDR UPS08652358Web · crackedINSPECTION TYPE:N/A RIGHT WING LES664 FWD D-NOSE WEB FOUND CRACKED AT LWR AREA. CRACK LENGTH 2 TO 2.5 INCHES APPROX. RIGHT WING FWD D-NOSE SUPPORT WEB REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02, JUST BETWEEN OSS648 AND 694. REFER NRC5062SDR UPS08652338Web · crackedINSPECTION TYPE:N/A RIGHT WING LES 679 FWD D-NOSE SUPPORT WEB FOUND CRACK AT LOWER AREA. CRACK LENGTH 2 INCHES TO 2.5 INCHES APPROX. RIGHT WING FWD D-NOSE SUPPORT WEB REPLACED AND INSTALLED AS PER SRM 51-10-02 AND 51-40-02 JUST BETWEEN OSS648 AN 694 AREA.SDR 08FDEA01846Fitting · crackedFOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION HORIZONTAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE C, E, G). REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5356 AND NSA5350, APPROVED BY RAS/70503969/045/200SDR 08FDEA01845Fitting · crackedFOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION VERTICAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE H, I, W, N). REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5351 AND EN6115, APPROVED BY RAS/70503969/045/20SDR 08FDEA01844Fitting · crackedFOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION HORIZONTAL FLANGE C 47 WITH DAMAGE AND CRACKS (HOLE A, D, E, G). REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING BUSHINGS, APPROVED BY RAS/70503969/045/2008 ISS A AND EA 6SDR 08FDEA01843Fitting · crackedFOUND ON SEVERAL HOLES IN CENTER WING BOX LOWER JUNCTION VERTICAL FLANGE C47 WITH DAMAGE AND CRACKS (HOLE H, I, M, N, V) REPAIR PERFORMED BY OVERSIZING THE HOLES UNTIL DAMAGE REMOVAL AND INSTALLING FASTENER NSA5351-9 AND NSA5479, APPROVED BY RAS/70503969/045/2SDR UPS08M52313Structure · crackedINSPECTION TYPE:2C LEFT WING L/E SLAT TRACK NR 14 CUTOUT CRACKED. TRIMMED OUT CRACK, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALL DOUBLER AND FILLER IAW MD-11 SRM 57-10-00 VOLUME 1 FIG 21.SDR CWQR200804Stiffener · chafedAC WAS IN SCHEDULED MAINTENANCE, AN INSP NOTICED THAT THE LT MAIN GEAR ACTUATOR WAS CHAFING ON THE WING SPAR WHEEL WELL STIFFENER, PN 6621211-26. UPON FURTHER INVESTIGATION WE FOUND THAT THE -26 STIFFENER WAS INSTALLED ON THE WRONG SIDE FROM THE FACTORY. SINCSDR UIEA200800194Beam · crackedLEFT WING LEADING EDGE "D" BEAM UPPER CHORD CRACKED ILES 1120. D' BEAM UPPER CHORD FABRICATED AND REPLACED IAW DRAWING 65B07895-139.SDR UPS08M52317Doubler · crackedINSPECTION TYPE:2C LEFT WING FIXED L/E BEADED DOUBLER BETWEEN SLAT TRACK 10 AND 11 FOUND CRACKED. CUT OUT DAMAGE, FABRICATED FILLER, ANGLES, AND DOUBLER, AND INSTALLED IAW MD-11 SRM 57-10-00 FIG 27, 51-33-01, 51-31-01, AND 51-21-01.SDR P5CA0801567Tie Rod · brokenON WALKAROUND FOUND A TIE ROD AND CLEVIS BROKEN ON THE RT WING GEAR WHEEL WELL AT WBL 238.38 FIXED TRAILING EDGE UPPER RIB. REMOVED DAMAGED PARTS AND VISUALLY INSPECTED AREA IN ACCORDANCE WITH EO 4457A140. (A)SDR UPS08852248Angle · crackedINSPECTION TYPE:C3 NR 1 STUBWING INBOARD WEB "L" ANGLE CRACKED IN LOWER RADIUS. FABRICATED AND REPLACED NR 1 STUBWING INBOARD WEB L-ANGLE IAW SRM 51- 01-20D, SRM 51-03-00 AND SRM 51-1-21.SDR 08FDEA01747Deflector · delaminatedFOUND DELAMINATION ON DEFLECTOR DOOR 672LB, INNER SIDE. REPAIR PERFORMED BY BONDING REPAIR IAW SRM 51-77-12, APPROVED BY RADS/BAE/1006487/2008 IIS A AND EA 6-5755-115272.SDR ABXR080170Angle · crackedCENTER WING TO FUSELAGE ANGLE CRACKED AND SEPERATED ABOVE REPAIR STRAP FORWARD SPAR AREA AT APPROX. RIGHT BUTT LINE 48. REMOVED AND REPLACED FITTING IAW DC9 SRM. (A)SDR 08FDEA01717Support Angle · crackedRIGHT WING LEADING EDGE CAVITY PANEL SUPPORT ANGLE IS CRACKED, OUTBD OF THE NR 8 SLAT TRACK. REMOVED FORMER IAW SRM 51-35-01 & 51-33-01; VOL II. FABRICATED PER DWG ARB1162, REV "S". ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PGS 21 - 24. INSTSDR UPS08M52459Doubler · crackedINSPECTION TYPE:C RT WING FIXED L/E COMPT AT STA XORS 538 APPROX FOUND UPPER DOUBLER CRACKED AS MARKED. DAMAGED AREA AT RT WING FIXED L/E COMPT STA 538 UPPER DOUBLER AREA TRIMMED OFF AS PER SRM 57-10-00 VI FIG 27 R40. NEW REPAIR DOUBLER, REPAIR FILLER & 03EASDR 08FDEA01642Angle · crackedAFT OF R/WING REAR SPAR, CRACKED ANGLE AT T/E TOP PANEL SUPPORT ANGLE, OUTBD SIDE OF RIB 9, FWD OF SPOILER NR 3 INBD HINGE PIN. REMOVED CRACKED ANGLE IAW A300-600 SRM 51-40-21. RECEIVED NEW BRACKET P/N A5724007120100, P/O NR 617032.1. INSTALLED NEW BRACKET SDR 08FDEA01623Retainer · crackedNR 1 PYLON PANEL 437HL HAS A CRACKED SEAL RETAINER. REMOVED AND REPLACED THE SEAL RETAINER IAW SRM 51-31-01 VOL II.SDR 08FDEA01622Retainer · crackedNR 1 PYLON PANEL 437AR SEAL RETAINER IS CRACKED. REMOVED & REPLACED THE SEAL RETAINER IAW SRM 51-31-01; VOL II.SDR UPS08852197Intercostal · crackedINSPECTION TYPE:C3 RIGHT WING CENTER L/E INTERCOSTAL CRACKED AT OUTBOARD PERI-SEAL STAND-OFF BRACKET AT XFS 434. FABRICATED AND REPLACED RIGHT WING CENTER L/E INTERCOSTAL AT XFS 434 IAW DWG 5769857 AND SRM 51-01-20D.SDR 08FDEA01486Fairing · crackedRT WING NR 6 FLAP TRACK FWD FAIRING HAS SEVERAL CRACKS REMOVED FASTENERS AND FABRICATED NEW REPAIR DOUBLER. INSTALLED NEW DOUBLER REF SRM 57-20-4 FIG 1. TREATED AND PRIMED AND PAINTED REF SRM 51-10-2 P2. THIS IS CLASSIFIED AS A MINOR REPAIR.SDR UPS08852297Fitting · crackedINSPECTION TYPE:C3 LEFT WING CENTER L/E SLOT STRESS PANEL TO ROD END FITTING HAS 8 INCH CRACK AT OUTBOARD END. REMOVED AND REPLACED LT CENTER L/E FITTING IAW SRM 51-3-0 AND SRM 51-1- 24.SDR UPS08852222Web · gougedINSPECTION TYPE:C3 SEVERAL DEEP GOUGES IN INBOARD WEB AT NR 1 STUB WING. REPAIRED NR 1 STUB WING INBOARD WEB IAW SRM SRM 57-02-00, DWG 9753297, SRM 51-01-08 AND SRM 51-01-21.SDR UPS08852198Angle · gougedINSPECTION TYPE:C3 LEFT WING CENTER L/E OUTBOARD UPPER Z-ANGLE GOUGED AND HAS 2 EA OVERSIZED HOLES. REPAIRED LEFT WING CENTER L/E OUTBOARD Z-ANGLE IAW DWG 5769857, SRM 57-02-00-0 FIG 2A AND SRM 57-02-00 FIG 007.SDR UPS08M52506Support Bracket · crackedINSPECTION TYPE:C LEFT WING L/E TOP PANEL 516ET INTERNAL SUPPORT BRACKETS 03 EA FOUND CRACKED. NR 516ET PANEL INTERNAL (3EA) SUPPORT BRACKETS REMOVED. REPAIR BRACKETS 6EA FAB & HEAT-TREATED. FASTENER HOLES PICK-UP ON 6EA REPAIR SUPPORT BRACKETS. SIX EA REPSDR A6WA200840330Angle · crackedRIGHT WING, L/E EDGE 630JL, ANGLE CRACKED AT WS 149.58. (M) ANGLE REPLACED IAW SRM 51-41-02.SDR 08FDEA01699Frame · crackedRT WING, FAIRING 632BB WITH FRAME ATTACHMENT SIDE LOAD CRACK. FRAME REPAIRED IN ACCORDANCE WITH FEDEX EA 6-5720-117327.SDR DHL2008760505Web · crackedREMOVED AND REPLACED NR 1 K-FLAP INBOARD AND OUTBOARD ACTUATOR MOUNT SUPPORT WEBS BY FABRICATION, LWS 307.5 TO 315.2, PER B727 SRM 51-10-2, 51-30-2, 51-20-1 FIG 3, 51-30-5, AND BAC DWG 65-16275 REV D.SDR DHL2008760502Beam · crackedL/WING T/E "J" BEAM CRACKED AT LWBL 128. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BEAM FROM WBL 70.5 TO 154.0, PER ASTAR J/C EC-00873-001 AND B727 SRM 51-30-2.SDR DHL2008760501Beam · crackedR/WING T/E "J" BEAM CRACKED AT RWBL 128. REMOVED, FABRICATED, AND INSTALLED NEW SUPPORT BEAM FROM WBL 70.5 TO 154.0, PER ASTAR J/C EC-00874-001 AND B727 SRM 51-30-2.SDR UPS08852128Angle · brokenINSPECTION TYPE:C1 LT WING T/E STA 436, RIB JUST O/B OF AILERON BUS CABLE SPRING ASSY HAS APPROX 4 INCHES BROKE OFF. FABBED AND INSTALLED REPAIR ANGLE 51-1-21, 51-1-20D, 51-1-8.SDR ASAA0872849Fitting · damagedL N WING RSS 260 FITTING FOUND WITH DRILL HOLD. REPLACED WITH NEW PART.SDR UPS08M52629Duct · chafedINSPECTION TYPE-C, LT WING ANTI-ICE TELESCOPIC DUCT LOWER DOOR FWD AREA FOUND CHAFING MARK. LT WING ANTI-ICE TELESCOPIC DUCT LWR DOOR PANEL REMOVED IAW AMM 20-50-02R53. CHAFING MARK REMOVED FOUND EXCEED LIMIT IAW SRM 57-00-01 VIR 35. NEW PANEL FABRICATED IAW SDR 08FDEA01648Plate · crackedLT WING, L/E ACCESS PANEL ATTACHMENT CHORD (LANDING PLATE) CRACKED 523BB BETWEEN RIB 8 AND 9. REPAIRED IN ACCORDANCE WITH FEDEX ENGINEERING AUTHORIZATION 6-5720-117325.SDR A6WA200840296Skin · crackedCRACK FOUND ON RT WING, AFT OF LANDING EDGE AT WS 343, BTWN ACCESS PANEL 603 LZ AND 630 KZ. (K) RT WING L/E ON THE REAR SIDE AT WEB FABRICATED IAW SRM 51-24-16. RT WING L/E ON THE REAR SIDE AT WS 343 WEB INSTALLED IAW SRM 51-42-13. (A)SDR 08FDEA01215Fitting · crackedSTRINGER BUTTERFLY FITTING NR 43 IS CRACKED APPROX 1/2 TOTAL LENGTH ON THE RIGHT WING, STA XORS 372. THE FITTING IS INSIDE THE FUEL TANK AT STRINGER 43, RIB XORS 372. REMOVED & REPLACED FITTING REF SRM 51-33-01; VOL IISDR SWAA081693Stiffener · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING VERTICAL STIFFENER CRACKED AT RIB WBL 542. REPAIRED STIFFENER PER ER.SDR 08FDEA01189Rub Strip · chafedLEFT WING SPOILER T/E RUB STRIP IS CHAFED. REMOVED T/E RUB STRIP IAW AIRBUS CMM 57-73-11. RECEIVED NEW RUB STRIP P/N A5777020920400, PO 612493.2. LOCATED AND DRILLED IAW AIRBUS CMM 57-73-11. INSTALLED RUB STRIP IAW AIRBUS CMM 57-73-11. PRIMED AND TOP COATSDR HALA0800466Skate Angle · crackedCRACK ON LT PYLON/WING, OUTBD SKATE ANGLE FWD EDGE,CRACK AT ATTACH FASTENER. REPAIR CARRIED OUT IAW SB 767-57-0023.SDR HALA0800464Fitting · corrodedLT WING DRY BAY FRONT SPAR BULKHEAD FITTING AND MATING SURFACE HAS PITTING CORROSION. FITTING REPLACED, MATING SURFACE BLENDED WITHIN LIMITS IAW SRM 57-20-10 REV 76.SDR UPS08M52229Structure · crackedINSPECTION TYPE:4C LEFT WING LE ACCESS PANEL LANDING AT NR 9 SLAT TRACK CRACKED. FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 57-10-00 FIG.18.SDR UIEA200800094Rub Strip · wornRT WING INBOARD AILERON UPPER SURFACE HAS RUB STRIP WORN THROUGH. REPAIRED RUB STRIP IAW ATLAS EO 4457A136 AND SRM 57-60-01 FIG 201 AND SRM 51-70-09 AND 51-70-10.SDR A6WA200840258Angle · crackedRIGHT WING AT WS 148 INBOARD AND OUTBOARD ANGLE CRACKED 1 INCH BY 2 INCH. (M) RT WING AT W/S 148 IB AND OB ANGLE REPLACED IAW SRM 51-41-02. (K)SDR A6WA200840271Angle · crackedLT WING OUT AND INBOARD ANGLES AT WS 148 CRACKED 1 INCH BY 2 INCH. (M) ANGLES REPLACED IAW SRM 51-40-11.SDR 08FDEA01110Beam · crackedRT WING I/B T/E "J " BEAM AT WING STATION 92 CRACKED, WING T/E SUPPORT BEAM FOR NR 7 SPOILER. TRIMMED OUT CRACKED AREA LENGTH 0.75" IAW SRM 51-10-1. TREATED AND PRIMED AREA "J" BEAM IAW SRM 51-10-2 DRAWING SR27-57-025.SDR 08FDEA01109Shim · migratedMIGRATING SHIMS AND LOOSE HARDWARE AT LWR SIDE OF NR 8 SPOILER ACTUATOR SUPPORT BEAM FITTING, WS 198. REPAIRED SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".SDR 08FDEA01108Support Beam · crackedMIGRATING SHIMS AND LOOSE HARDWARES AT LWR SIDE OF NR 7 SPOILER SUPPORT BEAM FITTING WS 198. REPAIRED NR 7 SPOILER ACTUATOR SUPPORT BEAM FITTING IAW DRAWING SR27-57-038 REV "C".SDR 2008FA0000193Support Bracket · crackedWHILE COMPLYING WITH AD 79-22-04 ON AILERON CONTROL SYS INSP AND SB 165A, 100 HOUR REPETITIVE INSP, FOUND LT OB AILERON HINGE SUPPORT BRACKET, 902010-501 CRACKED. CRACKED VISUALLY SEEN WITH OUT DISASSEMBLY USING A STRONG LIGHT AND SYSTEM LOADING. HOWEVER, WHE
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