JASC 5710
Service difficulty reports · 4,462
Reports filed under 5710 · Wing Main, Frame 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 = '5710' 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 = '5710' 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 USAA010692Structure · corrodedPIT - FOUND MATING SURFACE CORRODED 1 INCH BY 5 INCH AREA, LT WING 7210L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION ROT PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)SDR USAA0100690Structure · corrodedPIT - FOUND MATING SURFACE CORRODED, 1 INCH BY 6 INCH AREA, LEFT WING 7217L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01, PAGES 213-216. (M)SDR USAA010691Structure · corrodedPIT - FOUND MATING SURFACE CORRODED 1 INCH BY 3 INCHES, LT WING 7214L. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PGS 213-216. (M)SDR IXXA0100058SDoubler · corrodedDURING ROUTINE C-CHECK INSPECTION, CORROSION WAS DETECTED ON THE RIGHT WING LEADING EDGE INTERIOR DOUBLER AT THE LIFT TRANSDUCER, STATION 380. REPAIR ACCOMPLISHED REMOVAL OF DEFECTIVE DOUBLER, FABRICATION AND INSTALLATION OF NEW DOUBLER IN ACCORDANCE WITH DOUGSDR RRXA11022Spar Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT XFS32.5 AND XFS1117, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW SDR RRXA11009Fitting · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RH WING INTERCOSTAL FITTING AT STA XW98, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. RECEIVED PART AND INSTALLED IAW DC-8 SRM 57-1-0, 5SDR RRXA11070Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING O/B L/E LOWER RIB AT STA. XFS653.75, DAMAGE EXCEEDED LIMITATION IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW DC-8 SRM 5SDR RRXA10964Stiffener · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING T/E VERT. STIFFENER AT STA XW 75.31, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// RECEIVED REPAIR AND INSTALLED IAW DC-8 SRM 57-2-0, FIG 2.SDR UPS01835561Structure · crackedCRACK IN WING STRUCTURE AFT OF LEFT MLG REF DC8-5720-14401-A D213157 COMPLETE AT NEXT C CHECK UPS01835548 VOIDED DUE TO DUPLICATION OF MRRSDR UPS01835548Structure · crackedMX INSP-CRACK IN WING STRUCTURE JUST AFT OF LEFT MLG STRUT, MRR FILED AS OPEN.SDR AU010329Drain Valve · clogged(AUS) DRAINS LOCATED IN WING CENTRE SECTION AFT CAVITY AT BS 1241 WERE BLOCKED BY FOREIGN MATERIALS WITH EIGHT TO TEN LITRES OF WATER PRESENT. TIDE MARKS ALSO PRESENT ON SURROUNDING STRUCTURE INDICATING EVIDENCE OF GREATER QUANTITIES OF WATER RETENTION.SDR RRXA10922Angle · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE L/H CENTER L/E SLOT ANGLE, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// FABRICATED AND INSTALLED PART IAW DC-8 SRM 51-1-21 .SDR MWEA010247Splice · nickedREMOVED STRINGER 14 FORWARD SPLICE P/N 3913324-1 TO FACILITATE OTHER MAINTENANCE. FOUND NICKS, DINGS, AND SCRATCHES. LOCATED, DRILLED, FABRICATED AND INSTALLED CENTER FORWARD 14 SPLICE.SDR MWEA010500Shear Tie · crackedRIGHT WING FUEL TANK, SHEAR TIE CRACKED AT XRS 164 OUTBOARD SIDE BETWEEN AFT SPAR AND STRINGER NR 1. REMOVED CRACKED SHEAR TIE, BLENDED OUT DRILL MARKS, FABRICATED, LOCATED, DRILLED AND INSTALLED NEW CLIP.SDR MWEA010499Shear Tie · crackedRIGHT WING FUEL TANK, SHEAR TIE CRACKED AT XRS 111 OUTBOARD SIDE, BETWEEN AFT SPAR AND STRINGER NR 11. REMOVED CRACKED SHEAR TIE, LOCATED AND DRILLED NEW SHEAR TIE AND CLIP, INSTALLED CLIP.SDR MWEA010485Structure · corrodedLIGHT CORROSION ON THE EDGE OF LEFT WING TEE CAP XCW 58 HORIZONTAL LEG AFT OF STRINGER 19. -- BLENDED CORROSION.SDR MWEA010484Structure · corrodedCORROSION AROUND FASTENER ON LOWER RIGHT WING TEE BETWEEN STRINGER 21 AND 20 (3 & 4 FROM FRONT). REMOVED CORROSION.SDR UPS01235565Panel · corrodedINSPECTION TYPE:C & SI, RT WING & NR 1 FUEL PANEL HAS LIGHT SURFACE CORROSION ON LWR SURFACE, PANEL REPLACED IAW MM 28-11-21SDR AALA20010632Structure · corrodedTUL - FOUND RIGHT WING LOWER LEADING EDGE CHORD EXTENSION HAS HEAVY AREA OF CORROSION, UNDER INBOARD END OF STUB ACCESS. REMOVED CORROSION AND REPAIRED PER AARD 57-30-00-2. (M)SDR USAA010408Link · corrodedPIT - FOUND LINK WITH 3 INCH DIAMETER FRETTING, RIGHT WING INBOARD DOG BONE LINK LUG ON AFT SIDE OF SPAR. BLENDED AREA, DAMAGE TREATED AND PRIMED. (M)SDR DHL2001806517Fairing · brokenC-CHECK - LT WING TE LOWER FAIRING BROKEN 1 INCH AT XW 106.000. PERFORMED STOP HOLE AND FABRICATED DOUBLER IAW SRM 57-2-0 PAGE 1B. CLEANED, TREATED, AND PRIMED IAW SRM 51-1-0 PAGE 12-13. INSTALLED DOUBLER IAW SRM 57-2-0 FIG 1B. STATUS-CLOSED.SDR 01FDEA00205Support Fitting · crackedRT WING L/E STA XFS 1004, NR 16 SLAT TRACK SUPPORT FITTING CRACKED. *S/D* REMOVED AND REPLACED PER DWG ARB2850.SDR RRXA11039Spar Cap · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO RH AUX TANK UPPER SPAR CAP AT STA XFS32.5-XFS142, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-SDR ABXA010417Structure · leakingSPAR CAP LEAKED FUEL JUST INBOARD OF NR 1 PYLON AT S - 64 DOUBLER. REMOVED DOUBLER AND TRIPLER. FABRICATED REPAIR DOUBLERS AND INSTALLED IAW ABX REA D857-40311MR AND DAC DWG SRO8570013.SDR MWEA010252Frame · tool damageLEFT WING FRAME AT STATION 137 INBOARD SIDE HAS TOOL MARKS BY THE FASTENER HOLES FOR THE HOURGLASS STIFFENER. FABRICATED AND INSTALLED FILLER AND DOUBLER.SDR RRXA010564Frame · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO THE CENTER WING FRAME FITTING AT STA 860 X+68", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DCSDR RRXA010563Fitting · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE CENTER WING FRAME FITTING AT STA 879 X+69", DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-SDR DHL2001367510Doubler · corrodedC-CHECK--CORROSION AT DOUBLER FITTED TO REAR SPAR AFT OF NR 5 RT DOWN DRIVE GEARBOX. REMOVED CORROSION IAW SRM 51-40-11, REMOVED METAL =0.001, WITHIN LIMITS. RETREATED AREA.SDR QXEA0100071Seal · tornPDX- SEAL IS TORN AND LEFT WING LOWER SURFACE TRAILING EDGE IS DAMAGED AT STATION YW139-00. REPAIRED IAW DHC-8 SRM 51-40-11 AND HORIZON AIR EA 9-57-549.SDR RRXA003596Fastener · missingDURING A MAINTENANCE VISIT FOUND MISSING FASTENER ON THE RT UPPER WING THRU ACCESS HOLE 505C & THROUGH MID SPAR ACCESS HOLE 560C INSIDE TANK I/B BETWEEN STA 252 & 255, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8.SDR 20010525SG005Fitting · defectiveSAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4SDR 20010525SG004Fitting · defectiveSAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4SDR 20010525SG003Fitting · defectiveSAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4SDR SIMA200007201Fitting · defectiveSAW - DURING EDDY CURRENT ROTO TEST INSPECTION OF THE RIGHT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 2, THE FORWARD OUTBOARD HOLE DETECTED A DEFECT AND WAS REAMED AT AN ANGLE. THE LEFT WING FORWARD SPAR WING TO FUSELAGE ATTACH FITTING AT RIB 4SDR R3R2001201BScrew · incorrectTHE OB ATTACH SCREW IN THE HEATED LEADING EDGE IS TOO LONG AND CAN DAMAGE THE WING SKIN BELOW IT. THE IPC CALLS OUT A MS24693-C48 SCREW BUT IT IS TOO LONG.SDR R3R2001201CScrew · incorrectTHE OB ATTACH SCREW IN THE HEATED LEADING EDGE IS TOO LONG AND CAN DAMAGE THE WING SKINBELOW IT. THE IPC CALLS OUT A MS24693-C48 SCREW BUT IT IS TOO LONG.SDR QXEA0003256Shim · crackedPDX- SHIM HAS CRACKS AROUND FASTENER HOLES IN 3 LOCATIONS ON APERTURE OF PANEL 71A. REPAIRED IAW HORIZON AIR EA 4-57-511.SDR 20001227SH015Beam · corrodedLEFT WING REAR BEAM HAD CORROSION UNDERNEATH AILERON. (X)SDR P2EA00449Channel · crackedDURING Q CHECK, FOUND THE RT HAND WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK L/0.50 W/0.005 REPLACED RT HAND WING TE CAVITY LOWER CHORD CHANNEL.SDR RRXA003656Structure · damagedDURING A MAINTENANCE VISIT FOUND A 1/4 INCH HOLE IN THE RIGHT WING TIP CAP RT O/B NEAR THE CENTER, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED HOLE IAW PD 05-57-047.SDR SWIA972059Structure · damagedDAMAGE FOUND ON LEFT WING TIP. OUTBOARD STATIC WICK BRACKET BROKEN AND JAMMED IN LEFT AILERON CAUSING IT NOT TO MOVE. REPAIRED LEFT WING TIP IAW SRM 51-70-02. REPLACED STATIC WICK AND REINSTALLED WING TIP. AILERON OPS CHECKS GOOD.SDR COMA0060857Structure · damagedATA 727 STRUCK RT WING DURING TAXI OPS. AIRCRAFT IS BEING REPAIRED.SDR QXEA0002905Angle · chafedYXX- REAR SPAR WING TO FUSELAGE FAIRING ATTACHMENT ANGLE HAS CHAFE DAMAGE FROM ACCESS PANELS. REPAIRED IAW DHC-8 RD 8-57-1434, DHC-8 SRM 51-20-16, 51-00-06 AND 51-20-36.SDR QXEA0002906Structure · chafedYXX- FRONT SPAR WING TO FUSELAGE FAIRING LANDING STRIP HAS CHAFE DAMAGE FROM PANELS. REPAIRED IAW DHC-8 RD 8-57-1441, DHC-8 SRM 51-20-16, 51-00-06, 51-20-36, AND 51-20-51.SDR QXEA0003036Fastener · missingPDX- FASTENER MISSING AFT END OF RIB INBOARD OF ACCESS 74D. REPAIRED IAW FOKKER SRM 51-31-01.SDR UPS00434238Rib · crackedINSPECTION TYPE:C, RIGHT WING L/E CRACK ON L/E RIB BOLT HOLE AT OLES 1482.85. REPAIR CARRIED OUT IAW QUERY NOTE 61/2000.SDR RRXA003831Former · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LOWER FORMER AT STA. XFS466, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLED IAW DC-8 SRM 51-1-21, 51-1-20D, 51-1-4.SDR QXEA0002845Strap · delaminatedPDX- LEFT HAND WING LOWER SKIN STRAP AT STATION 8200 AND FRONT SPAR STRAP LAMINATIONS ARE DEBONDING. REPAIRED IAW HORIZON AIR EA 4-57-477.SDR AU000958Frame · damaged(AUS) LEFT WING DAMAGED DURING HEAVY LANDING. (X)SDR QXEA0002844Structure · crackedPDX- ONE CRACK COMING FROM THE AFT BUSHED HOLE AT THE 6 O''CLOCK POSITION APPROXIMATELY .5 INCH LONG. REPAIRED IAW HORIZON AIR EA 4-57-471.
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