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.

SDR 06FDEA2478Finger Doubler · crackedFOUND LT WING LEADING EDGE CAVITY THRU ACCESS PANEL 525AB CEILING AREA FINGER DOUBLER CRACKED AT XOS 699. REPAIRED AS PER FEDEX E.A. 1-5730-100701. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.Jul 8, 2006 · N614FE · Doug MD11SDR UPS06247569Structure · corrodedINSPECTION TYPE:C SURFACE CORROSION AT BOTH I/B STATIC DISCHARGERS LEFT WING TIP T/E. CORROSION REMOVED IAW SRM 51-10-01 AND FASTENERS REMOVED IAW SRM 51-3 0-02. AREA O/B FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01. DAMAGED AREA REPAIRED IAW SRM 57-20-05. Jul 6, 2006 · N935UP · Boeing 7271A7CSDR AWXA200601243Cylinder · corrodedSAL - MAJOR REPAIR - CHECK NO. C7. NR NO. 5909891. CORROSION AROUND THE HOLE NR 53 OF ACTUATING CYLINDER ANCHORAGE LT WING. CORROSION AROUND THE HOLE NR 53 OF ACTUATING CYLINDER ANCHORAGE ON THE LEFT WING WAS REMOVED IAW PART A OF AWA ER NR 26 - 5721 - 06181 -Jul 2, 2006 · N605AW · Airbus A320232SDR QXEA200601340Web · chafedPDX: C3. CHAFE ON WEB AT WING STATION YW 136.3, 5 INCHES FROM AFT AND SPARE, 5 INCHES FROM TOP SKIN OB SIDE. MAINTENANCE REPAIRED IAW Q400 SRM 51-12-00, NDTM 51-00-01-250-801, NDTM PART 1, 51-00-04-910-801, AMM TASK 51-25-40-370-801 AND HORIZON EA 6-57-484.May 19, 2006 · N406QX · Bombdr DHC8402SDR AWXA200600831Beam · crackedSAL - DURING C5 CHECK DISCOVERED CRACK ON SUPPORT ANGLE LOCATED AT THE TRAILING EDGE BETWEEN RIB 23 AND RIB 24 OF THE LEFT WING. MAINTENANCE REMOVED AND REPLACED THE BEAM ASSEMBLY ON THE TRAILING EDGE OF THE LT WING RIB 23 TO RIB 24 IAW AIRBUS 320 SRM 51-72-1May 18, 2006 · N624AW · Airbus A320231SDR 06FDEA1959Repair · unknownFOUND PREVIOUSLY REPAIR ON LT INBD MID FLAP LOWER SURFACE INBD OF INBD CARRIAGE FAIRING IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND REINSTALLED REPAIR PARTS IAW EA 7-5710-92428. REPAIR IS CLASSIFED AS MAJOR PER FEDEX GMM 6-2-100.May 18, 2006 · N270FE · Boeing 72722SDR 06FDEA1934Strut · corrodedRIGHT WING, OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING AFT HOLE FOUND CORRODED. COMPLIED WITH FEDEX EA 1-5750-97760, WINGS OUTBOARD TRAILING EDGE FLAP RT INBD SUPPORT STRUT CORROSION REPAIR. REPAIR CLASSIFIED AS MINOR AS PER FEDEX GMM 6-2-100.May 16, 2006 · N599FE · Doug MD11FSDR 06FDEA1933Strut · corrodedRIGHT WING OUTBOARD FLAP, INBOARD FLAP HINGE, AFT FITTING FORWARD HOLE FOUND CORRODED. RIGHT WING, OUTBOARD FLAP INBOARD FLAP HINGE AFT FITTING FORWARD HOLE CORROSION REPAIRED AS PER FEDEX EA NR 1-5750-97760, TITLE, WINGS OUTBOARD TRAILING EDGE FLAP. RIGMay 16, 2006 · N599FE · Doug MD11SDR QXEA200601361Plate · corrodedPDX: C3. LIGHT CORROSION BY SCREW HOLE AT AFT EDGE OF LADDER PLATE UNDER PANEL 522BT. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-03 AND HORIZON EO 6-57-317.May 15, 2006 · N406QX · Bombdr DHC8402SDR QXEA200601362Plate · corrodedPDX: C3. LIGHT CORROSION ON LADDER PLATE BY SCREW HOLE (FWD EDGE) UNDER PANEL 522AT. MAINTENANCE REPAIRED IAW RD 8/4-57-441, NDTM PART 6, 51-00-02 AND HORIZON EO 6-57-317.May 12, 2006 · N406QX · Bombdr DHC8402SDR USAA060682Support · crackedFOUND STA 135.50 LT WING INSIDE ACCESS HOLE 7202L CRACKED. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW EA 97692, DEFECT SIZE: 2 INCHES.May 10, 2006 · N531AU · Boeing 7373B7SDR 06FDEA1686Support Fitting · corrodedRIGHT WING O/B FLAP I/B HINGE SUPPORT FITTING (P/N ARC4008) O/B NR 2 BOLT HOLE FOUND CORRODED. CORROSION REPAIRED AS PER FEDEX EO 1-5750-7-5008. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100.May 3, 2006 · N618FE · Doug MD11SDR QXEA200601646Structure · chafedYYC C3 RIGHT HAND WING OUTBOARD FLAP CHAFED FROM YW210 TO YW246. REPAIRED IAW RD 8/4-57-648, ISSUE 1 AND EA 6-57-463.Apr 28, 2006 · N425QX · Bombdr DHC8402SDR VNAA0604013Wing · lightning strikeTHE AIRCRAFT WAS STRUCK BY LIGHTNING DURING CRUISE FLIGHT. THE FLIGHT LANDED WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE LT WINGLET, SEVERAL ANTENNAS, AND NUMEROUS SPOTS ON THE FUSELAGEApr 26, 2006 · N247JS · Cndair CL6002B19SDR QXEA200601574Panel · damagedYYC - C3 LEFT WING FUEL PANEL REBATES AT 521BT, 521AT AND 621AT HAS SCRATCHES AROUND HOLES. REPAIRED IAW RD 8/4-57-441, ISSUE 1.Apr 21, 2006 · N425QX · Bombdr DHC8402SDR VNAA0604011Structure · lightning strikeTHE CREW REPORTED A POSSIBLE LIGHTNING STRIKE DURING CLIMBOUT FROM TYS. THE FLIGHT LANDED IN CLT WITHOUT INCIDENT. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR DAMAGE WAS FOUND ON THE LEFT WINGLET, RIGHT ELEVATOR, AND RIGHApr 21, 2006 · N244PS · Cndair CL6002B19SDR VNAA0604009Structure · lightning strikeDURING POSTFLIGHT INSPECTION THE CREW REPORTED EVIDENCE OF A LIGHTNING STRIKE ON THE RIGHT WINGLET. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. DAMAGE WAS FOUND ON THE RIGHT WINGLET, NR 2 VHF ANTENNA, AND THE LOWER TAIL NAVIGATIApr 20, 2006 · N209PS · Cndair CL6002B19SDR QXEA200601573Panel · damagedYYC - C3 RIGHT WING PANEL BEHIND REAR SPAR AT STATION 371-389 WAS DRILLED OFF TO FACILITATE ACCESS TO OUTBOARD SPOILER, NEED TO BE RIVETED BACK ON. INSTALLED IAW DHC-8-400 SRM TASK 51-42-45-330-801 AND 51-42-35-330-801.Apr 18, 2006 · N425QX · Bombdr DHC8402SDR VNAA0604007Structure · lightning strikeAFTER LANDING THE CREW REPORTED THE AIRCRAFT HAD TAKEN A LIGHTNING STRIKE. MAINTENANCE PERFORMED EN ROUTE AND DETAILED LIGHTNING STRIKE INSPECTIONS. MINOR PITTING DAMAGE WAS FOUND ON THE TOP FUSELAGE AND RIGHT WING. ALL DAMAGE WAS REPAIRED. THE AIRCRAFT WAApr 17, 2006 · N260JS · Cndair CL6002B19SDR QXEA200601095Structure · corrodedPDX - C4 CORROSION ON MATING SURFACE OF WING STRUCTURE, AROUND OUTBOARD FASTENER HOLES OF PANEL 624AT. REPAIRED IAW RD 8-57-611.Apr 13, 2006 · N356PH · Dhav DHC8202SDR 06FDEA1418Doubler · crackedLEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA FOUND FORMER DOUBLER AT STA XIS 562 WITH CRACKED. LEFT HAND WING - FIXED LEADING EDGE COMPARTMENT CANTED AREA AT STA XIS 562 CRACKED DOUBLER. REMOVED AND REPLACED AS PER SRM 51-33-01 VOLUME II. NEWApr 12, 2006 · N582FE · Doug MD11SDR HNAA0600025Fire · detectedAFTER TAKEOFF NR 1 RUDDER FULL PRESSURE AND ROLL SPOILER INBOARD HYDRAULIC CAUTION LIGHT ILLUMINATED. CREW DECLARED EMERGENCY RETURNED TO AIRFIELD. MAINTENANCE REMOVED FLAP WELL PANEL 532AB AND FOUND AREA UNDER PANEL WAS CHARRED FROM FIRE. FIRE WAS HOT ENOUApr 12, 2006 · N808EX · Dhav DHC8102SDR 06FDEA1326Stringer · crackedHFEC INSPECTION CARRIED OUT, FOUND CRACK ON RIGHT WING STRINGER-12 END. RIGHT WING STRINGER 12 END CRACKED AREA REPAIR CARRIED OUT AS PER SRM 57-20-00 FIGURE 10 VOLUME I. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100.Apr 7, 2006 · N595FE · Doug MD11SDR USAA060546Fastener · looseON TOP OF RT WING JUST I/B OF PYLON ON L/E 7 LOOSE FASTENERS. REMOVED 7 FASTENERS AND REPLACED WITH NEW FASTENERS IAW SRM 51-40-02.Apr 3, 2006 · N505AU · Boeing 7373B7SDR P5CA0601469Structure · corrodedRIGHT WING TRAILING EDGE STA 710.0 - 718.0 CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-014.Mar 31, 2006 · N921FT · Boeing 747283BSDR 06FDEA1143Bracket · corrodedRT WING OB FLAP IB AFT HINGE BRACKET FWD ATTACHMENT OB CENTER HOLE CORRODED. COMPLIED WITH FEDEX EA 1-5750-95793. THIS REPAIR CLASSIFIED AS MAJOR AS PER FEDEX GMM 6-2-100.Mar 17, 2006 · N612FE · Doug MD11SDR 06FDEA1012Angle · crackedRIGHT HAND FIXED L/E RIG ANGLE FOUND CRACKED AT XORS 475. REMOVED AND REPLACED AS PER SRM 51-33-01 VOL.II. ANGLE FABRICATED AS PER DWG ARB2931.Mar 13, 2006 · N612FE · Doug MD11SDR AMWA76315Structure · bird strikeON APPROACH INTO MHK AIRCRAFT STRUCK MULTIPLE GEESE. AIRCRAFT DAMAGE TO RIGHT STUB WING AND RIGHT WING OUTBOARD NACELLE. MAINTENANCE REMOVED AND REPLACED THE ENTIRE RT LEADING EDGE IAW FR-CO-01332,01333,01334.Mar 10, 2006 · N166YV · Beech 1900DSDR TAMF20060016SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON RT WING T/E INBOARD SPOILER SUPPORT BEAM, STA 375.8. CHORD WAS FABRICATED IAW BOEING SMAL (SPARE MATERIAL AUTHORIZATION LICENSE) PO BOEING CONTROL 206706 & BOEING DRAWING 113T1407 AND INSTALLED IAW SRM 51-40-Mar 9, 2006 · N767QT · Boeing 767200SDR TAMF20060015SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON LT WING T/E INBOARD SPOILER SUPPORT BEAM, STA WS 250.0. CHORD WAS FABRICATED IAW BOEING SMAL (SPARE MATERIAL AUTHORIZATION LICENSE) PO BOEING CONTROL 206705 & BOEING DRAWING 113T1407 AND INSTALLED IAW SRM 51-Mar 9, 2006 · N767QT · Boeing 767200SDR TAMF20060014SSupport Beam · corrodedDURING C-INSPECTION CHECK WAS FOUND A CORROSION ON LT WING T/E OUTBOARD SPOILER SUPPORT BEAM, BETWEEN STA WS 431.97 TO WS 394.92. CHORD WAS BE FABRICATED IAW BOEING SMAL PO 206740 (SPARE MATERIAL AUTHORIZATION LICENSE) & BOEING DRAWING 113T1407 AND INSTALLED Mar 9, 2006 · N767QT · Boeing 767200SDR 06FDEA0856Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=683. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=683 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954Feb 27, 2006 · N615FE · Doug MD11SDR 06FDEA0855Doubler · crackedRIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER FOUND CRACKED AT XORS=562. RIGHT HAND WING FIXED LEADING EDGE RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PER DRAWING ARB3954Feb 27, 2006 · N615FE · Doug MD11SDR 06FDEA0854Doubler · crackedLEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER FOUND CRACKED AT XORS=562. LEFT HAND WING FIXED LEADING EDGE INTERNAL RIB DOUBLER AT XORS=562 REMOVED AND REPLACED WITH NEW FABRICATED DOUBLER AS PER SRM 51-33-01 VOLUME II. NEW DOUBLER FABRICATED AS PERFeb 27, 2006 · N615FE · Doug MD11SDR 06FDEA0709Duct · crackedRIGHT HAND WING LEADING EDGE ANTI-ICE TELESCOPIC DUCT CUTOUT AT XORS372 FOUND CRACKED AS MARKED. REPAIRED AS PER FEDEX EA 1-5730-90763.Feb 17, 2006 · N602FE · Doug MD11SDR DHL2006804549Doubler · crackedRT WING NR3 MAIN TANK 505F ACCESS DOOR INTERNAL DOUBLER FLANGE CRACKED 0.750 XRS 12.000 S-5 (MAJOR REPAIR). REMOVED FASTENERS. CUT OUT DAMAGED SECTION IAW DWG AA66-57-R09. PERFORMED NDT INSP USING DYE PENETRANT IAW NDT SPM. APPLIED YELLOW COATING TO TANK INTEFeb 16, 2006 · N804DH · Doug DC873FSDR 06FDEA0628Doubler · crackedRT WING L/E FOUND 1 CRACK 5" LONG ON INTERNAL DOUBLER AT STA XORS 562. INSTALLED DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F166195/N00195 AND IAW SRM 57-10-00 FIG 71 VOL 1.Feb 9, 2006 · N68054 · Doug DC1010SDR 06FDEA0621Structure · corrodedMAIN DECK COMPARTMENT, DURING SLANT PANEL DRAIN INSPECTION FOUND CORROSION, NEAR DRAIN AREA AT LT STA 1361. REMOVED AND FOUND EXCEEDED LIMITS PER SRM 57-20-00 VOLUME I, FIGURE 12. COMPLIED WITH FEDEX EA 1-5710-90740.Feb 9, 2006 · N593FE · Doug MD11SDR 2006FA0000193Bolt · damagedDURING FIRST PHASE INSPECTION (49 HOURS SINCE NEW)FOUND LEFT WING TO UPPER STRUT BOLT HEAD DAMAGED FROM FACTORY, APPARENTLY INSTALLED WITH VISE-GRIP TYPE TOOL. NO TORQUE SEAL FOUND ON NUT. DAMAGE EXTENSIVE ENOUGH THAT TORQUE COULD NOT BE CHECKED WITH SOCKET. PFeb 9, 2006 · N410BS · Cessna 172SSDR 2006FA0000192Bolt · damagedDURING FIRST PHASE INSPECTION (49 HOURS SINCE NEW)FOUND LEFT WING TO UPPER STRUT BOLT HEAD DAMAGED FROM FACTORY, APPARENTLY INSTALLED WITH VISE-GRIP TYPE TOOL. NO TORQUE SEAL FOUND ON NUT. DAMAGE EXTENSIVE ENOUGH THAT TORQUE COULD NOT BE CHECKED WITH SOCKET. PFeb 9, 2006 · N410BS · Cessna 172SSDR UPS06446320Tank · crackedINSPECTION TYPE:C LT WING SURGE TANK WS 1516 LWR AREA STR 5 & 6 FOUND CRACKED, CRACK LENGTH .4375 INCH AND PIECE BROKEN. LT WING SURGE TANK WS 1516 FULL LENGTH LOWER CHORD REPAIRED AS PER HX RS R57-22-35446 AND UPS ENGINEER FILE 747-57-20088.Feb 7, 2006 · N522UP · Boeing 747200SDR DHL2006804538Cap · corrodedLT WING INBOARD L/E UPPER PART SLANT PANEL UPPER CAP CORRODED XFS 7.500 - XFS 26.250 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW SRM 57-1-0, BOEING MESSAGE 1-156506024-2. REMOVED CORROSION IAW SRM 51-1-8 PG 17-18. FOUND OUT OF LIMITS IAW SRM 57-2-1 FIG 37. Feb 6, 2006 · N804DH · Doug DC873FSDR 06FDEA0544Hinge · crackedFOUND LT WING L/E XOS 792 FOUND ACCESS PANEL TEE/HINGE CRACK 1" LONG AND EXT SKIN LOWER SECTION CRACK 2" LONG. REPAIRED L/E SKIN IAW SRM 57-10-00 FIG 68 VOL 1 AND SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER F163378/N00378 AND IAW SRFeb 6, 2006 · N68056 · Doug DC1010SDR MALA060051Structure · ground damageRIGHT WING TRAILING EDGE FAIRING PLUG PART NUMBER 601R10872-62 SUSTAINED DAMAGE BY CONTACT WITH A GROUND SUPPORT VEHICLE. THE DAMAGE STARTS JUST INBOARD OF THE MOST INBOARD STATIC WICK ON THE FAIRING. IT THEN EXTENDS 21 INCHES OUTBOARD, THE TRAILING EDGE HASFeb 5, 2006 · N602XJ · Cndair CL6002B19SDR MWEA060010Vane · gougedLEFT WING INBOARD FIXED VANE HAS GOUGE ON LOWER SIDE, OUTBOARD EDGE. FABRICATED AND INSTALLED DOUBLER.Jan 30, 2006 · N808ME · Doug DC982SDR 06FDEA0390Fastener · damagedRT WING AFT/LOWER INBOARD PANEL HAS ONE SCREW HEAD MISSING (LOG BOOK ENTRY REQUIRED). RT WING AFT LOWER I/B PANEL REPAIRED HOLE, AT #5 FLAP TRACK ATTACHMENT. IAW FED -EX EA 7- 5710-96555Jan 26, 2006 · N490FE · Boeing 727200SDR QXEA200600426Bushing · migratedPDX: RT WING LEADING EDGE LWR FLANGE HAS SLEEVE/BUSHING MIGRATING OUT OF SCREW HOLE .15 INBOARD OF NACELLE. MAINTENANCE REPAIRED IAW NDTM PART 6, 51-00-02, Q400 SRM 51-21-10-380-801 SUB TASK 51-21-10-380-001, SRM 51-25-10-370-801 AND HORIZON EA 6-57-431.Jan 24, 2006 · N400QX · Bombdr DHC8402SDR QXEA200600314Fastener · brokenYYC - C3 RIGHT WING TRAILING EDGE HAS BROKEN FASTENER AT STATWION WS199.40. REPAIRED IAW CRJ700/900 SRM 51--42-06-001-001-A01.Jan 21, 2006 · N606QX · Cndair CL6002C10SDR 2006FA0000204Cover · chafedCOVER IS CHAFING LOWER FWD LT AND RT WING ATTACH PORT SPART CAP AND WING SKIN. THE COVER HAS NO ANTI-CHAFE PROTECTION. RECOMMEND RUBBER EDGE SEAL OR FAY SEALED EDGE TO AVOID METAL TO METAL CONTACT WITH SPAR AND WING SKIN. (K)Jan 21, 2006 · N6812W · Beech 300BEECHSDR VNAA0601018Structure · lightning strikeLIGHTNING DAMAGE WAS DISCOVERED ON THE LEFT WINGLET TIP DURING PERFORMANCE OF A ROUTINE INSPECTION. MAINTENANCE PERFORMED DETAILED LIGHTNING STRIKE INSPECTIONS AND FOUND NO OTHER DAMAGE. THE WINGLET WAS REPAIRED IAW BOMBARDIER REO 601R-57-31-065 AND THE AIRCJan 21, 2006 · N206PS · Cndair CL6002B19
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