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 QXEA200500425Plate · corrodedYYC - RIGHT WING LADDER PLATE FOR PANEL 622AT HAS FRETTING CORROSION. REPAIRED IAW Q400 SRM 57-10-30-320-002 AND HORIZON AIR EA 6-57-301.SDR UPS05443676Splice · crackedINSPECTION TYPE: C, RIGHT WING STA 1241 UPPER REAR SPAR SIDE - OF - BODY SPLICE PLATE AREA FOUND HOLE NR 3 CRACKED AT WING UPPER SKIN AND INTERNAL SPLICE FITTING APPROX 0.040 INCH REFER ATTACHED SKETCH. HOLE REPAIRED AS PER SB 747-57A2314.SDR 05FDEA00056Structure · corrodedLT WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 FOUND CORRODED. REPAIR CARRIED OUT AT LEFT HAND WING, TRAILING EDGE UPPER CHORD AT XORS= 1042 AS PER FEDEX EA 1-5710-81589, FOUND EXCEEDED LIMITS AS PER SRM 57-20-00 VOLUME I, FIGURE 16.SDR QXEA200500050Pan · crackedPDX - RIGHT HAND STUB WING PRESSURE PAN HAS TWO CRACKS WHERE THE NR 2 PRESSURE HYDRAULIC LINE PASSES THROUGH. REPAIRED IAW SRM 51-42-06-001-0001-A01, SRM 51-23-00 AND SRM 51-42-06.SDR QXEA200400885Structure · corrodedPDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT HAND WING, BETWEEN STATION YW 155.2-173.2. REPAIRED IAW HORIZON AIR EA 6-57-268 AND RD 8/4-57-399.SDR QXEA200400875Structure · corrodedPDX - FRETTING CORROSION AROUND NUMEROUS BOLT HOLES, LEFT WING, BETWEEN STATION YW117.5-136.3. REPAIRED IAW RD 8/4-57-399 AND HORIZON AIR EA 6-57-268.SDR 04FDEA03314Support Bracket · corrodedRIGHT HAND WING OUTBOARD FLAP OUTBOARD HINGE (FLAP SIDE), ACTUATOR PIN ATTACHMENT OUTBOARD BORE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMATER=1.191, FINAL DIAMETER=1.219, AND FABRICATED BUSHING INSTALLED AS PER FEDEX EA SDR 04FDEA03253Panel · delaminatedRIGHT WING INBOARD FLAP AREA LEFT HAND FALSE SPAR CEILING PANEL INBOARD OF MAIN LANDING GEAR STRUT DELAMINATED/DENTED. REMOVED FILLET PANELS 152FT, 152ET AND SMALL PANEL OUTBOARD OF DAMAGED PANEL IAW DC10 SRM 51-31-01 VOL 2, TO FOM. REMOVED DELAMINATED PANELSDR 04FDEA03140Panel · delaminatedPANEL NR 641 LB, RIGHT WING INBOARD TRAILING EDGE HAS DELAMINATION IN NUMEROUS AREAS. REPAIRED PANEL NR 641LB BY FABRICATING AND BONDING NEW SKINS, DOUBLER AND CORE IAW TPS 1001 REV E AND DAC DWG ARC0357 ANF FEDEX EA 8-5710-81521, WINGS, RIGHT HAND LOWER AILESDR QXEA200400773Panel · corrodedPDX - FUEL PANEL 522AT HAS ALL COUNTERSINK THAT HAVE PITTING CORROSION. REPLACED IAW WORK CARD 500ME2860266.SDR USAA040891Stiffener · crackedPIT- Q6 - VERTICAL STIFFENER, 1.2500 INCH CRACK, AT RBBL 6.15, STA 663.75. REPLACED VERTICAL STIFFENER IAW EA 79313 AND EO 5704V245 (RAFT).SDR WX0400050Structure · bird strikeLAS - CREW REPORTED BIRD STRIKE LEFT WING TRAILING EDGE. MAINTENANCE PERFORMED BIRD STRIKE INSPECTION IAW AMM 05-51-08. NO DAMAGE FOUND. AIRCRAFT RETURNED TO SERVICE.SDR VNAA0411002Structure · bird strikeAFTER SHUTDOWN IN DAY EVIDENCE OF A BIRD STRIKE ON THE RT WING INBOARD LEADING EDGE WAS REPORTED BY THE CREW OF FLIGHT 2461. PSA MAINTENANCE INSPECTED THE AREA AND FOUND THE DAMAGE TO BE OUT OF LIMITS FOR CONTINUED SERVICE. PSA MAINTENANCE THEN REMOVED & REPSDR EIA2004134Support Beam · crackedRT WING STA 665-685, TRAILING EDGE SUPPORT BEAM, LOWER CHORD CRACKED ON FORWARD SIDE. REPAIRED RT WING TRAILING EDGE SUPPORT BEAM, LOWER CHORD BETWEEN WS 665-685, PER ECRA 470-57-227-2, REV A.SDR 05FDEA00379Cap · crackedLEFT WING RIB UPPER CUP CRACK AT XORS 372. TRIMMED OUT CRACKED PORTION AND SPLICE REPAIRED IAW FEDEX EA 8-571-80005.SDR UPS04443321Splice · crackedINSPECTION TYPE-C, LT WING UPPER BS 1241 WL 180 REAR SPAR SPLICE PLATE FASTENER HOLE NR 7 FOUND CRACKED AT SPAR CHORD UPPER LAYER RUNNING AFT APPROX .0625 INCH LONG. HOLE REWORKED AND OVERSIZED IAW EO B747-5740-17032.SDR UPS04443330Splice · crackedINSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT INTERNAL SPLICE FITTING AT 7 O'CLOCK POSITION APPROX 0.080 INCH LONG. CRACKED HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032.SDR UPS04443329Splice · crackedINSPECTION TYPE: C, RT BS 1241 STR R28 UPPER WING REAR SPAR SPLICE PLATE HOLE NR 4 FOUND CRACK AT SPLICE PLATE AT 12 O'CLOCK POSITION APPROX 0.080 INCH LONG. HOLE REWORKED AND OVERSIZED AS PER EO B747-5740-17032 & RIGHT SPLICE PLATE REPLACED AS PER EO B747-57SDR MALA040749Shroud · damagedDURING C1 INSPECTION IN YYC, RT O/B WING SHROUD TRAILING EDGE DAMAGED. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04.SDR MALA040751Seal · wornDURING C1 INSPECTION IN YYC, LEFT O/B WING SHROUD TRAILING EDGE SEAL WORN. MAINTENANCE REPAIRED IAW EO A57013. AIRCRAFT RETURNED TO SERVICE 10/7/04.SDR EIA2004077Structure · corrodedRT WING GEAR WELL HAS SURFACE CORROSION AROUND FASTENER HOLES AT BS 1336-1338 AND OVERWING LONGERON. REPAIRED RT OVERWING LONGERON BS 1326-1345 PER ECRA 480-53-170-2.SDR GAIA04120Panel · crackedDURING C-CHECK INSPECTION, FOUND RT WING L/E STA 349 WEB PANEL CRACKED. REF FASI NR 86603, STOP DRILLED WEB AREA AND INSTALLED DOUBLER REPAIR IAW SRM 51-40-2, FIG 1.SDR UPS04243216Plate · corrodedINSPECTION TYPE: C, LIGHT SURFACE CORROSION AROUND FASTENER HEAD ON HORIZ FLANGE OF LT WING UPPER SPLICE PLATE AT BS 848. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-021. HFEC CARRIED OUT ON ABOVE AREA IAW B727 NDTM 51-00-00 PT6 FIG 4SDR UPS04243238Frame · crackedINSPECTION TYPE:C, SUSPECT CRACK ON WING CENTER SECTION AT BS 775 RBL 45 ON LOWER FLANGE. HFEC CARRIED OUT IAW NDT M 51-00-00. RESULT - CRACKS CONFIRMED. FWD SECTION OF CHORD REMOVED AT BS 740 - BS 780 RBL 45 IAW 51-30-2. CENTER SECTION CHORD FWD SECTION ASDR UPS04243208Structure · crackedINSPECTION TYPE: C, LOWER LEFT WING, FIXED WING STRUCTURE WHICH SECURES NR 3 FLAP TRACK FAIRING IS CRACKED ON BOTH I/B AND O/B SIDES. HFEC CARRIED OUT ON SUSPECT CRACKS IAW B727 NDTM 51-00-00 PT 6 FIG 4. CRACKS CONFIRMED ENDS MARKED. DAMAGED AREA REMOVES IASDR EIA2004078Structure · corrodedLT WING GEAR W/W STA. 1241 LBL 40-80 CORROSION BETWEEN CANTED WEB AND LWR CHORD. REMOVED CORROSION AND REPAIRED IAW ECRA 480-53-167-2SDR USAA040572Beam · wornCLT - FOUND BEAM WITH APPROXIMATELY 5 INCHES OF WEAR, LOWER FLANGE OF LEAD BEAM, AFT END OF BEAM. BLENDED AND TREATED PER EA 95815. (M)SDR 2004F00283Fairing · departedLEFT CENTER WING FAIRING PANEL DEPARTED AIRCRAFT WHILE DESCENDING THROUGH FL13 EN ROUTE FROM SAT-HOU. NO PASSENGERS ON BOARD. PILOTS REDUCED SPPED ON DESCENT PRIOR TO LANDING WHEN LOUD NOISE WAS HEARD. (M)SDR CA040817008Structure · frayed(CAN) DURING THE POST FLIGHT INSPECTION THE RT AND LT WINGLET TIPS WERE FOUND TO BE DAMAGED BY STATIC DISCHARGE. THE RESIN MATERIAL WAS WAS BLOWN AWAY EXPOSING THE CARBON FIBERS AND LEAVING THE TRAILING EDGE FRAYED. CREW DID NOT EXPERIENCE LIGHTNING ON THE LASSDR 04FDEA02376Hinge Bracket · corrodedLT WING, OB FLAP, IB AFT HINGE OB PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502. MATERIAL REMOVED = 0.004 REMAINING THICKNESS = 0.498. COMPLIED WITH FEDEX EA 1-5750-76807, LEFT AND RIGHT OUTBOARD FLASDR 04FDEA02374Hinge Bracket · corrodedLT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.006, REMAINING THICKNESS = 0.0.396 COMPLIED WITH FEDEX EA 1-5750-76808SDR 04FDEA02373Hinge Bracket · corrodedLT WING, OB FLAP, OB AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE IB CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LEFT AND RIGHT OUTBOARD FLAP - SDR 04FDEA02372Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11- 02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.402, MATERIAL REMOVED = 0.004, REMAINING THICKNESS = 0.398. COMPLIED WITH FEDESDR 04FDEA02371Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH ACTUATOR ROD END ATTACHING HOLE OUTBOARD CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2-4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.192. COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOASDR 04FDEA02370Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE INBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.500, MATERIAL REMOVED = 0.001, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA# 1-5750-76808, WINGS SDR 04FDEA02368Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE FLANGE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL THICKNESS = 0.502, MATERIAL REMOVED = 0.003, REMAINING THICKNESS = 0.0.499. COMPLIED WITH FEDEX EA 1-5750-76808, WSDR 04FDEA02367Hinge Bracket · corrodedLT WING, OUTBOARD FLAP, OUTBOARD AFT HINGE WITH OUTBOARD PIVOT HOLE CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.071 COMPLIED WITH FEDEX EA 1-5750-76808, WINGS - LT AND RT OUTBOARD FLAP - OUTBSDR 04FDEA02163Stop Fitting · crackedRT WING OUTBOARD FLAP STOP FITTING FOUND CRACKED 2 PLACES. REMOVED CRACKED STOP FITTING AS PER SRM 51-31-01, VOLUME II AND INSTALLED NEW FITTING AT RIGHT HAND WING OUTBOARD FLAP AS PER SRM 51-33-01, VOLUME II.SDR A6WA200440104Bushing · migratedAT LEFT MLG MOUNTING TRUNNION BUSHING IS MIGRATED .004 WS 66. PERFORMED A MAJOR REPAIR BY REMOVING MIGRATED LEFT MLG AFT TRUNNION BUSHING AND INSTALLED FIRST OVERSIZE BUSHING P/N 601R5720113-21, IAW BOMBARDIER REO 601R-57-21-003 REV B. (M)SDR UPS04242853Frame · corrodedINSPECTION TYPE: C, EVIDENCE OF CORROSION ON CENTER SECTION OF NR 2 TANK UPPER CHORD AT RBL 63.5 APPROX. ON INVESTIGATION CORROSION WAS FOUND TO BE EXTENSIVE. UPPER CHORD FWD SPAR CENTER SECTION REMOVED PER SRM 51-30-2, NEW CHORD SECTION CUT TO ACC INSTL IAWSDR 04FDEA02007Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOASDR 04FDEA02015Beam · crackedRIGHT WING INBOARD AILERON LOWER BEAM CRACKED AT END. REMOVE TEE-CAP IAW DC10 SRM 51-35-01 VOL I, FABRICATED -4 TEE CAP IAW DCA DWG ARC 3012 AND DC10 SRM 51-10-01 FIG 13 VOL 3. TRIMMED, LOCATED, DRILLED AND DEBURRED -4 TEE CAP IAW DC10 SRM 57-31-01 VOL 2 ANDSDR 04FDEA01978Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093", FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARSDR 04FDEA01830Bracket · corrodedRIGHT WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE FOUND CORRODED. RIGHT HAND WING, INBOARD FLAP OUTBOARD HINGE (FLAP SIDE), OUTBOARD PIVOT HOLE BORE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442 TO 443 AND FOUND EXCEEDED LIMITS, SDR 04FDEA01778Structure · corrodedLEFT HAND WING LOWER WINGLET WING SIDE - AFT INTERNAL MOUNT BOLT HOLE AREAS HAVE MINOR SURFACE CORROSION.SDR QXEA200400424Attach Bracket · crackedPDX - LEFT HAND WING LEADING EDGE UPPER ATTACH BRACKET CRACKED YW384.5, YW137. REPAIRED IAW DHC-8-200 SRM 51-40-00.SDR 04FDEA01259Support Bracket · crackedRT WING FUEL TANK VENT LINE SUPPORT BRACKET IS CRACKED AND BROKEN AT XORS 683 INBOARD SIDE. REMOVED AND REPLACED BRACKET IAW SRM 51-31-01 AT MAE.SDR AUS20040346Skin · corroded(AUS) WING TRAILING EDGE CONTAINED CORROSION ON BOTH SIDES.SDR IXXA0400076SVane · damagedDURING A ROUTINE C-CHECK INSPECTION FOUND RT WING VANE SLOT HOLES ELONGNATED AT SX 515.720. REPAIR WAS ACCOMPLISHED. REMOVED ALL FASTENERS WITH THE REPAIR AREA AND REMOVED DAMAGED AREA PER APPLICABLE MANUALS, PERFORMED NDT INSPECTION PER NDT SPM PART 06-10-0SDR CA040423005Spar · crackedDURING REPLACEMENT OF A BRACKET ON THE RT AILERON, A CRACK APPOXIMATELY .075 INCH WAS DISCOVERED UNDER THE BRACKET AT ONE OF THE ATTACH POINT BOLT HOLES ON THE SPAR LEADING EDGE. THE CRACK WAS REPAIRED IN ACCORDANCE WITH APPROVED DATA AND THE FAIRCHILD SRM.
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