JASC 5712
Service difficulty reports · 6,970
Reports filed under 5712 · Wing, Rib/Bulkhead, 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 = '5712' 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 = '5712' 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 07FDEA04582Rib · crackedLEFT WING LEADING EDGE CAVITY AREA RIB ANGLE AT STATION XOS 584 FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB ANGLE (FORMER) AS PER SRM 51-31-01 VOLUME II AND FABRICATED FORMER AS PER DOUGLAS DRAWING ARB2931 AND INSTALLED FORMER AT LEFT HAND WING LEADINGSDR 07FDEA04581Rib · crackedRIGHT WING LEADING EDGE CAVITY RIB DOUBLER AT STATION XOS 789 (XORS 683) FOUND CRACKED. 10-29-07 REMOVED CRACKED RIB DOUBLER AS PER SRM 51-31-01 VOLUME II AND FABRICATED RIB DOUBLER AS PER DOUGLAS DRAWING ARB3954 AND INSTALLED AT RIGHT HAND WING LEADINSDR 2007FA0000907Bulkhead · misalignedCONTROL CABLE, (P/N 0510105-308), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7. IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT. MSDR 2007FA0000906Bulkhead · misalignedCONTROL CABLE, (P/N 0510105-308), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7. IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT. MSDR 2007FA0000898Bulkhead · misalignedCONTROL CABLE, (P/N 0510105-339), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7. IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT. CSDR 2007FA0000904Bulkhead · misalignedCONTROL CABLE, (P/N 0510105-339), FOUND WORN TO REPLACE LIMITS IAW AC43.13-1A, CABLE INSPECTION. CABLE WAS WORN DUE TO CONSTANT CONTACT WITH LANDING GEAR BULKHEAD FAIRLEAD P/N S338-7. IT IS BELIEVED THAT THE HOLE MISALIGNMENT CAUSED THIS CONSTANT CONTACT. MSDR 07FDEA04555Rib · crackedDURING COMPLIANCE WITH EO NR 6-5750-7-5000 P1, LT INBOARD FLAP RIB NR 25 WAS FOUND TO BE CRACKED. REPLACEMENT OF DAMAGED RIB NR 25.SDR DLM88071460Rib · crackedCRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=455. REPLACED ANGLE PER DWG 9919329.SDR DLM88071459Rib · crackedCRACK ON RT WING FIXED LEADING EDGE RIB ANGLE AT STA XOS=448. REPLACED ANGLE PER DWG 9919329.SDR ASAA0792116Bulkhead · crackedLEFT WING TRAILING EDGE BULKHEAD AT WBL 201 90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-40-02.SDR CA071009002Rib · dented(CAN) REMNANTS OF A BIRD WAS FOUND ON ARRIVAL. INSP REVEALED A DENT IN THE RT WING LEADING EDGE AT WING. THE DENT WAS APPROXIMATELY 4 INCHES BY 2 INCHES AND .25 INCHES DEEP. MAINTENANCE REMOVED THE DENT AND REPLACED RIB AT WING STATION 167.00 AND THE L/E WAS RSDR ASAA0792117Bulkhead · crackedRIGHT WING TRAILING EDGE BULKHEAD AT WBL 201.90 WEB ASSY CRACKED. WEB ASSY REPLACED WITH NEW PART IAW B737 900 SRM 51-40-02.SDR 07FDEA04491Rib · crackedLT WING INBOARD FLAP RIB 25 FOUND CRACKED. REPLACED FLAP RIB 25 AND RUB AND ROLLER TRACK.SDR 07FDEA04512Skin Panel · corrodedFOUND CORROSION AT RT WING LOWER SKIN RIB 10-12, REAR SPAR AND AFT REPAIR PERFORMED BY BLEND OUT CORROSION AND REPROTECTION IAW EA 6-5720-112459 AND RAS/BAE/1005247/2007 ISS A.SDR 07FDEA04507Rib · crackedFOUND UPPER RIB CAP CRACKED ON RT WING PNL 634AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.SDR 07FDEA04506Rib · crackedFOUND UPPER RIB CAP CRACKED ON LT WING PNL 534AT. REPLACED RIB IAW SRM 57-20-00 FIG 38 SHT 1-2-3 VOL I.SDR UIEA200700448Spar Cap · corrodedRIGHT WING FRONT SPAR LOWER CHORD AREA FSSO 1356 CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 AND BOEING MESSAGE 1-638497220-2.SDR 07FDEA04372Rib · crackedDURING SCHEDULED B CHECK, RT INBOARD FLAP RIB 25, P/N A5796011320100 WAS FOUND TO HAVE A 3 INCH CRACK IN THE FWD UPPER RADIUS, REF: N00030. REMOVED AND REPLACED DAMAGED RIB REF: A300 SRM 51-40-21.SDR 07FDEA04373Rib · crackedDURING SCHEDULED B CHECK, LT INBOARD FLAP RIB 25, P/N A 5796011320000 WAS FOUND TO CRACKED IN TWO PLACES, A 1.5 INCH CRACK WAS FOUND IN THE FWD UPPER RADIUS AND A 1.5 INCH CRACK WAS FOUND IN THE AFT UPPER RADIUS AND FLANGE, REF: N00029. REMOVED AND REPLACESDR 07FDEA04340Rib · crackedRT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.SDR 07FDEA04339Rib · crackedRT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.SDR 07FDEA04338Rib · crackedRT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.SDR 07FDEA04337Rib · crackedRT WING L/E INT STRUCTURE FOUND CRACK ON UPPER RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.SDR 2007FA0000815Rib · crackedCRACKS FOUND DURING INSPECTION, CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY. WITH NEW MFG PART 78475-004 (AN IMPROVED PART). HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THSDR 2007FA0000813Rib · crackedCRACKS FOUND DURING INSPECTION. CRACKS FOUND IN LOWER RELIEF EDGE MADE USE OF REPAIR KIT P/N: 767 - 397 NOT POSSIBLE. THE CRACK REQUIRED REPLACEMENT OF ENTIRE RIB ASSY WITH NEW PART 78475-004 (AN IMPROVED PART). HAVE DIGITAL PHOTOS OF THE CRACKED RIB, THE CRASDR 07FDEA03887Rib · damagedFOUND DAMAGE (NICK) ON RT WING TRAILING EDGE AILERON HINGE RIB (INBOARD), WITH A MINIMUM REMAINING THICKNESS OF 1,7MM (NOMINAL 2,3MM). REPAIR PERFORMED BY BLEND OUT DAMAGE, HFEC INSPECTION AND FLAP PEENING IAW EA 6- 5751-81123 AND RAS/BAE/1272/2004 ISSUE A.SDR 07FDEA03885Rib · damagedFOUND DAMAGE (NICK) ON RT WING TRAILING EDGE AILERON HINGE RIB, WITH MINIMUM REMAINING THICKNESS OF 2,2MM. REPAIR PERFORMED BY BLEND OUT DAMAGE, HFEC INSPECTION AND FLAP PEENING IAW EA 6-5751-81123 AND RAS/BAE/1272/2004 ISSUE A.SDR 07FDEA03816Rib · crackedRT WING L/E INT STRUCTURE FOUND CRACK ON RIB. REPAIRED AREA IAW SRM 57-20-00 FIG 1 SHT 1 VOL I.SDR 07FDEA03697Rib · corrodedFOUND ON LT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISDR 07FDEA03696Rib · corrodedFOUND ON RT MLG FWD LUG INNER BORE RIB 5 THE BUSHING TO BE OUT OF ROUND, AFTER REMOVAL OF BUSHING FOUND CORROSION ON THE LUG REPAIR PERFORMED BY CORROSION REMOVAL AND REAM UP THE HOLE IAW DRAWING R572-49121, APPROVED BY EA 6-5751-8106 AND RAS/BAE/0979/2004 ISSDR 2007FA0000931Bulkhead · misalignedCONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A. THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE. IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGSDR 07FDEA03596Rib · chafedFOUND CHAFING MARK ON LT WING INTERMEDIATE RIB AT WIAX 21.9. REPAIR PERFORMED BY BLEND OUT TO SMOOTH CONTOUR IAW EA 6-5751-112495 AND RAS/BAE/1005322/2007 ISS A.SDR 07FDEA03562Rib · corrodedFOUND CORROSION IN MLG RIB 5 FWD LUG ON BOTH WINGS. REPAIR PERFORMED BY SPOT FACING AND OVERSIZING WITH NEW BUSHES IAW REPAIR DRW R572-40221 ISSUE E, APPROVED BY EA 6-5751-95903 AND RAS/BAE/1002238/2006 ISSUE A.SDR 07FDEA03472Rib · crackedFOUND CRACK (3MM) ON MLG RIB 5, LHS, AT HOLE 47 (RAS/BAE/1001321/2005 GIVES A LIMIT OF 10 FC). REPAIR PERFORMED BY REAM UP UNTIL CRACK REMOVAL IAW EA 6-5710-92236 AND RAS/BAE/1001952/2005 ISS B.SDR 07FDEA03336Rib · crackedRT WING TIP CRACKS, 1.5" LONG ON EXTERNAL SKIN XW 928, YW 799. CONTINUED CRACK ON INT OLD REPAIR ON FRAME XW 928, YW 799. REPAIRED AREA IAW SRM 57-00-01 FIG 10 VOL I.SDR 07FDEA03315Rib · crackedCRACK DAMAGE ON LT WING LEADING EDGE CLOSING RIB WOFX-277.9. REPAIR PERFORMED BY TRIMMING OUT THE DAMAGED AREA, LOCALLY MANUFACTURING AND INSTALLING AN INFILL PACKER AND REPAIR ANGLE USING EXISTING AND NEW FASTENER POSITIONS IAW TD/J1/02572/2006 ISSUE A APPSDR 07FDEA03295Rib · chafedFOUND AT ALL SPEED AILERON HINGE RIBS LT/RT DEEP CHAFING MARKS, ON THE INTERMEDIATE RIB 6A POSITIONS ON BOTH WINGS. REPAIR PERFORMED BY BLENDING AND REPROTECTION AT POSITIONS RIB 6A AS PER TD/J1/S1/0234/2006 ISSUE B APPROVED BY EA 6-5751-99137 AND RAS/BAE/1SDR DHL2007746534Rib · crackedNR 5 SLAT AT ACTUATOR ATTACH HAS O/B FRAME CRACKED ON FWD LOWER CORNER. REMOVED AND REPLACED RIB AT NR 5 SLAT O/B IAW B-727 SRM 51-30-5 AND 51-30-2, RIB P/N 65-17276-9, PO: 7268244.SDR 07FDEA03143Rib · crackedLT WING INTERNAL L/E ON UPPER RIB FOUND CRACK 0.70" LONG. REPAIRED RIB IAW SRM 57-20-00 FIG 1 VOL I.SDR 07FDEA03142Rib · crackedLT WING INT L/E ON UPPER RIB FOUND CRACK 0.60" LONG. REPAIRED RIB IAW SRM 57-20-00 VOL 1 FIG 1.SDR 07FDEA03025Rib · chafedCHAFING MARK AT END OF RIB 6-A, OUTBOARD SIDE RT WING T/E. REPAIR PERFORMED BY BLEND IAW EA 6-5751-103339 AND RAS/BAE/1003495/2006 ISS "A".SDR UPS07M50623Rib · crackedINSPECTION TYPE:4C RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED RIGHT WING NR 16 SLAT TRACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01.SDR UPS07M50622Rib · crackedINSPECTION TYPE:4C LEFT WING NR 16 SLAT TRACK I/B FITTING (RIB) IS CRACKED. REMOVED AND REPLACED LEFT WING NR 16 SLAT TRACK I/B FITTING (RIB) IAW MD-11 SRM 51-33-01 AND 51-35-01.SDR 07FDEA02903Rib · crackedRIGHT WING SLAT TRACK NR 16 RIB FOUND CRACKED. 08-31-07 REMOVED AND REPLACED AS PER SRM 51- 35-01 VOLUME II AND SRM 51-33-01 VOLUME II. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR 07FDEA02858Rib · crackedLEFT WING LEADING EDGE CAVITY INBOARD OF NR 2 SLAT OUTBOARD TRACK RIB AT SLAT STATION 318 IS CRACKED AT FORWARD LOWER ATTACH FASTENER. REMOVED RIB AND HAD CRACK NDT AND STOP DRILLED CRACK, FORMED DOUBLER AND INSTALLED. REPAIR DOUBLER TO RIB ALODINED, PRIMED SDR SWAA074024Rib · crackedDURING SCHEDULED SPV CHECK, FOUND LT WING RIB CRACKED AT STA 135.5. REPAIRED RIB PER ACO.SDR 07FDEA02856Rib · corrodedCORROSION FOUND ON LT MLG RIB 5 FWD LUG REPAIR PERFORMED BY OVERSIZING THE BORE AND CORROSION REMOVAL IAW DRAWING R572-40221, APPROVED BY EA 6-5751-112446 AND RAS/BAE/100519/2007 ISS A.SDR 2007FA0000926Bulkhead · wornCONTROL CABLE, ( P/N 0510105-308), FOUND WORN TO REPLACEMENT LIMITS IAW CABLE WEAR INSPECTION GUIDELINES IN AC43.13-1A. THE CABLE CONSTANTLY RUBS THE S338-7 FAIRLEAD IN THE LANDING GEAR BULKHEAD HOLE. IT IS BELIEVED THAT A HOLE MISLOCATION CAUSES THE MISALIGSDR 07FDEA02819Rib · wornLT WING L/E AT STA XOS 460 ON LOWER RIB AREA DOOR 513AB FOUND DEEP WEAR REPAIRED TEE IAW SRM 57-00-01 VOL I FIG 9. FABRICATED PARTS IAW SRM 57-00-01 FIG 9 VOL 1.SDR UPS07M50927Rib · crackedINSPECTION TYPE:C LEFT WING LEADING EDGE HAS NOSE RIB CRACKED BETWEEN SLAT TRACKS 12 AND 13 STICKER 7058. CRACKED RIB REMOVED. NEW RIB FABBED USING MAT'L 7075-0-0.040" PER DWG ARB2922. RIB HEAT TREATED AS PER DPS 7.00-1 & HARDNESS VALUES HRB 83.1 AS PER DPS
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