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 IPXA09556741Plate · crackedINSPECTION TYPE: C2 RT WING WIGGLE PLATE CRACKED LWR T/E FIXED PNL AT NACELLE STRUT AFT FAIRING. REMOVED AND REPLACED PLATE IAW SRM 51-40-02.SDR FDEA200906302397Rub Strip · corrodedRT WING/LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT/RUB STRIP CORRODED. RT WING LWR WING FUEL TANK ACCESS DOOR NR 639CB CUTOUT CORRODED. RUB STRIP REMOVED AND REPLACED IAW SRM 51-42-04 VOLUME II REVISION 40. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 RESDR IPXA09156550Skin · misrepairedINSPECTION TYPE:1C REPAIR SURVEY SEQ 126-W4-01 DOES NOT CORRELATE WITH SRM. REMOVED EXISTING REPAIR ON RT ALL SPEED AILERON LOWER SURFACE BETWEEN RIBS 15-16, 7.5 INCHES AFT OF REAR SPAR ON T/E. FABRICATED AND INSTALLED REPLACEMENT REPAIR REF A300-600 SRM 51-SDR FDEA200906232436Skin · dentedRIGHT WING FLAP OUTBOARD UPPER SKIN SURFACE WITH DEEP DENT AT FRICTION PLATE SEATING AREA BETWEEN RIB 2.5 AND RIB 3. REPAIRED IAW E.A. 6-5710-131025.SDR IPXA09656495Rib · crackedINSPECTION TYPE:7C RT WING I/B AILERON I/B HINGE SUPPORT RIB UPPER AFT FLANGE FOUND CRACKED. RT WING I/B AILERON I/B HINGE SUPPORT FIG RIB REPAIR AS PER HX RS NO. 57-55-36355 REV A. THIS IS A PERMANENT REPAIR WITH MATERIAL AND 10133-2002-7075T6511 AS REPAIR SDR IPXA09M56562Doubler · crackedINSPECTION TYPE:2C LT WING L/E CAVITY BEADED DOUBLER IS CRACKED AT BUCKTAIL BEHIND PANEL 519CB JUST I/B AND ABOVE I/B REFUEL PORT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27 SHT 1-4.SDR IPXA09M56561Doubler · crackedINSPECTION TYPE:2C LT WING L/E CAVITY BEADED DOUBLER HAS 5 EA CRACKS EMITTING FROM BUCKTAILS BEHIND PANEL 519CB JUST ABOVE O/B FUEL PORT. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27 SHT 1-4.SDR IPXA09M56560Doubler · crackedINSPECTION TYPE:2C LT WING L/E CAVITY BEADED DOUBLER HAS 4 CRACKS EMITTING FROM BUCKTAILS BEHIND PANEL 519EB. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER, FILLER, AND ANGLES IAW MD-11 SRM 57-10-00 FIG 27 SHT 1-4.SDR FDEA200906091998Beam · corrodedFOUND CORROSION ON BEAM FOR KRUEGER FLAP STRUCTURE RHS. REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.SDR SWIA200921713Winglet · separatedFLT 4807 - LEFT WINGLET TIP DEPARTED AIRCRAFT IN CRUISE. REPLACED WINGLET.SDR 2009F00036Bolt · crackedPOSSIBLE CRACK IN AFT WING BOLTS UPPER (POSSIBLY WAS CAD PLATING ON BOLTS) SHOWING IN THREADS OF BOLTS.SDR IPXA09M55905Doubler · crackedINSPECTION TYPE:C LT WING L/E LOWER ACCESS NR 519CB COMPT FOUND BEADED DOUBLER CRACKED AS MARKED, STA XORS 536 APPROX. DAMAGE AREA AT BEADED DOUBLER TRIM OFF PER SRM 57-10-00, FIG 27, VOL I, REV 40. HFEC INSP C/O ON TRIMMED OUT EDGE AND FOUND NO CRACK EVIDENSDR FDEA200904201357Structure · corrodedLEFT WING, TRAILING EDGE UPPER CAP UPPER SURFACE FOUND CORROSIONS AT XORS 984. COMPLIED WITH EA 1-5710-129201. REPAIR CLASSIFIED AS MINOR AS PER GMM 6-2-100 REV. 107.SDR IPXA09M56751Winglet · damagedRT UPPER WINGLET ASSY HAS DAMAGED COMPOSITE RIB ON BOTTOM END OF ASSY. RIB HAS 2 AREAS CRACKED AT OUTER SKIN ATTACHMENT TO RIB. PART WAS ORIGINALLY INSTALLED ON ACFT. PART WAS TRANSFERRED TO RO SR1417801. REMOVED DAMAGE AND REPAIRED IAW EO C-5720-33537-A.SDR IPXA09M56750Winglet · damagedRT UPPER WINGLET ASSY HAS 3 DAMAGED AREAS ALONG T/E. REMOVED DAMAGE AND REPAIRED IAW EO C-5720-33537-A.SDR IPXA09B55576Fairing · delaminatedINSPECTION TYPE:C LHW - OTBD FORE FLAP INBD L/E AREA DELAMINATION. COMPOSITE HOT BOND REPAIR CARRIED OUT AS PER SRM 51-70-07 PARA 5A FIG 5 REV 52.SDR FDEA200904081214Structure · chafedRIGHT WING DROOP LEADING EDGE UPPER SURFACE INBOARD SIDE FOUND CHAFING MARKS. REPAIRED AS PER EA 1-5730-128683, CLASSIFIED AS MINOR REPAIR PER GMM 6-2-100, REVISION 107.SDR CA090519011Structure · corroded(CAN) DURING A YEARLY INTERNAL WING CORROSION INSP AS REQUIRED BY CHAPTER 5 REQUIREMENTS, EXTENSIVE SPAR/STRINGER/SKIN CORROSION WAS DISCOVERED IN THE INBD SECTION OF THE MAIN TANKS AND THE COLLECTOR TANKS. X-RAY INSP REVEALED UNDISCOVERED SPOTS OF CORROSION BSDR FDEA200903030830Crossbeam · damagedFOUND DEFORMATION ON CROSSBEAM FROM KRUEGER FLAP STRUCTURE REPAIR PERFORMED BY REPLACEMENT OF PART IAW. SRM 51-72-10.SDR 2009FA0000155Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING OTBD TRUSS ASSY PN 5951051-35 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000154Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING OTBD TRUSS ASSY PN 5951051-35 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000153Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000152Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING INBD TRUSS ASSY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000151Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000150Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND LT WING INBD TRUSS ASSY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000149Truss · corrodedDURING SUPPLEMENTAL INSPECTION 54-10-02 FOUND RT WING INBD TRUSS ASSY PN 5951051-38 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR 2009FA0000148Truss · corrodedDURING SUPPLEMENTAL INSP 54-10-02 FOUND LT WING INBD TRUSS ASSLY PN 5951051-37 SEVERELY PITTED. SENT OUT FOR REPAIR.SDR EIAA20090033Beam · damagedRIGHT WING T/E BEAM WEB AT WBL 432 DAMAGED. REPAIRD PER SRM 51-40-02, FIG 1.SDR EIAA20090032ABeam · crackedRIGHT WING T/E BEAM UPPER CHORD FOUND CRACKED. REPAIRED PER SRM 51-40-04, FIG 2.SDR HALA2009022200060Hinge Pin · migratedVIBRATION NOTED OVER LT WING FUSELAGE. RETURNED TO A AIRPORT. LANDING OUT 319.9 NORMAL LANDING. FOUND LT WING EXIT HATCH, DROP DOWN STEP HINGE PIN MIGRATED LOOSE. REINSTALLED HINGE PIN AND SECURED. ACCOMPLISHED ETOPS 1. OPENED AND CLOSED AFT NR 1 ENG CORSDR HALA2009022200059Hinge Pin · migratedVIBRATION NOTED OVER LT WING FUSELAGE. RETURNED TO AIRPORT. NORMAL LANDING. FOUND LT WING EXIT HATCH, DROP DOWN STEP HINGE PIN MIGRATED LOOSE. REINSTALLED HINGE PIN AND SECURED. ACCOMPLISHED ETOPS 1. OPENED AND CLOSED AFT NR 1 ENG CORE COWLS MM 05-51-38 SDR CA100202008Collar · loose(CAN) AT INSPECTION SOME COLLARS ON HIGH SHEAR RIVETS PN NAS1054-6-10 WHICH ATTACH THE STRUT SUPPORT ASSY TO THE WING SPAR WERE FOUND ABLE TO ROTATE. 4 ON LT WING AND 7 ON RT WING. THE RIVETS ARE HIGH SHEAR AND PRESSED FIT AND SHOWED NO SIGNS OF MOVEMENT. THERSDR FDEA200902040446Beam · corrodedIN KRUEGER FLAP AREA, WING LE ON BEAM HEAVY CORROSION. REPAIR PERFORMED BY REPLACEMENT OF PART IAW SRM 51-72-10.SDR 2009FA0000083Structure · crackedREMOVED CRACKED LT AND RT WING TIPS AND REPLACED WITH NEW PN`S 0723205-1 AND 0723205-20. REMOVED CRACKED ELEVATOR RT AND LT TIPS AND REPLACED WITH NEW PN`S 1234640-4 AND 1234640-3. REMOVED CRACKED HORIZONTAL STAB PLASTIC TIP ON RT SIDE & REPLACED WITH NEW. SDR 2009FA0000082Structure · crackedREMOVED CRACKED LT AND RT WING TIPS AND REPLACED WITH NEW PN`S 0723205-1 AND 0723205-20. REMOVED CRACKED ELEVATOR RT AND LT TIPS AND REPLACED WITH NEW PN`S 1234640-4 AND 1234640-3. REMOVED CRACKED HORIZONTAL STAB PLASTIC TIP ON RT SIDE & REPLACED WITH NEW. SDR UPS09554693Wedge · dentedINSPECTION TYPE:C LT WING NR 4 SLAT T/E WEDGE HAS 1 DENT OUT OF LIMITS DUE TO PROXIMITY 6.5 INCHES FROM OTBD END, 6.3 INCHES FROM T/E (MARKED AS GROUP 1). REMOVED TOPCOAT TO PREPARE BOND DOUBLER IAW SRM 57-43-02 AND SRM 51-70-10, REP NR 2, E(C) PG 203, FIG 20SDR CA090209001Attach Bolt · crackedTHIS BOLT WAS INSPECTED DURING THE ANNUAL INSPECTION OF THIS AIRCRAFT. IT WAS VISUALLY SEEN TO HAVE WHAT LOOKED LIKE A CRACK ON THE HEAD SURFACE OF THE BOLT. THIS COULD BE MISTAKEN AS DAMAGE FROM A DRIFT OR HAMMER DONE DURING INSTALLATION. THE PART WAS REMOSDR FDEA200901210303Bracket · corrodedRT WING, OTBD FLAP OTBD FWD HINGE ACTUATOR ATTACH OTBD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127738, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200901210302Bracket · corrodedRT WING, OTBD FLAP OTBD FWD HINGE ACTUATOR ATTACH INBD HOLE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127738. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR FDEA200901210301Bracket · corrodedLT WING OTBD FLAP FWD OTBD HINGE ACTUATOR INBD BORE FOUND WITH CORROSION. REPAIRED AS PER EA 1-5750-127737, REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100.SDR LR7A2009020200012Access Panel · delaminatedDURING SCHEDULED C-9 CHECK, FOUND RT INBD LIFERAFT FWD ACCESS PANEL DELAMINATED. FABRICATED AND REPLACED PANEL IAW LAC MEA 382-57-08-065.SDR FDEA200901100121Support Beam · crackedNR 4 FLAP TRACK AFT MOUNT VISUALLY CRACKED IN 2 PLACES AT WING TRAILING EDGE REPAIRED LT WING SPOILER SUPPORT BEAM LWR CHORD IAW EA 7-5710-124053 BY SPLICING THE LOWER CHORD MAJOR REPAIR RDR AND SDR RII.SDR SWIA200921300Shear Tie · crackedC-CHECK, CRACKED SHEAR CLIP ON RIGHT OUTBOARD WING AT RIB 16. REPLACED CLIP PER SRM.SDR FDEA200812095115Stiffener · gougedLEFT WING VERTICAL STIFFENER LOWER AREA IS GOUGED AFT OF THE FALSE SPAR AND RIB 6A. REMOVED DAMAGED STIFFENER, LOCATED AND DRILLED NEW STIFFENER IAW DWG A57244644. INSTALLED NEW STIFFENER IAW SRM 51-40-21, PARA 7.SDR 08FDEA04934Support Beam · damagedFASTENERS LOOSE LWR SIDE OF NR 7 SPOILER FITTING. UPON FURTHER EVALUATION FOUND IMPROPER REPAIR IAW DRAWING SR27-57-038. REPAIRED LT WING INBD SPOILER SUPPORT BEAM IAW DRAWING SR 27-57-038 REV C, SEE WO NR 00042909, N/R N00197, JPF FOR DETAILS.SDR CA081114007Structure · damaged(CAN) BIRD STRIKE ON LANDING RT WING ENGINE AREA. LE NR 3, ACFT INSPECTED IAW AMM 05-50-26. IMPACT DAMAGE CONCENTRATED AT RT NR 3 LE. RT NR 3 LE REPLACED IAW AMM, LEAK AND FUNCTION CHECKED. SERVICEABLE.SDR AALA200820079Structure · damagedRT WING ROOT LEADING EDGE HAS DAMAGE. REPAIRED IAW SRM 51-70-00-2.SDR KCSA081510Structure · corrodedLT WING STA-680 BOOST PUMP CUT OUT CORRODED. (K)SDR KCSA081511Structure · corrodedRT WING STA-680 BOOST PUMP CUT OUT CORRODED. (K)SDR UPS08M53408Frame · crackedINSPECTION TYPE:1C RT WING L/E LOWER SURFACE PNL FRAME AT WING STA 506 IS CRACKED. REMOVED CRACKED PANEL, FABRICATED AND INSTALLED REPAIR DOUBLER IAW MD-11 SRM 51-35-02 VOL 2 PG 2, AND DWG ARB2933.
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