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 0104079868Spar · corrodedDuring an Mck in ATL, corrosion was found in the left wing front spar web, around station XCW 32. THe corrosion is around two holes in the web for the two harness leads. Material .090 7075-t6 aluminum clad sheet. Repaired per EA 98-185058SDR UPS01236690Stringer · crackedINSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2SDR C2XA01BT159Strut · wornYUL---DURING 4C INSPECTION YUL MAINTENANCE FOUND RT WING REAR SPAR FITTING AT RIB 16, TRAILING EDGE STRUT HOLE TO BE ELONGATED. MAINTENANCE REMOVED AND REPLACED RT WING REAR SPAR FITTING AT RIB 16, TRAILING EDGE STRUT IAW ATR42 STANDARD PRACTICE 20-21-12. OKSDR CA010817002Bolt · damaged(CAN) BOLT FOUND WITH MECHANICAL THREAD DAMAGE UPON INSPECTIONSDR SWAA012329Spar · crackedDURING SCHEDULED D CHECK, FOUND LH REAR SPAR UPPER CHORD CRACKED AT WBL 157. R&R REAR SPAR UPPER CHORD SECTION PER BFG ER .SDR SWAA012322Beam · corrodedDURING SCHEDULED D CHECK, FOUND RH MLG STABILIZER BEAM CORRODED AT AFT INBD SIDE. R&R STAB BEAM PER MM.SDR 01FDEA00729Bushing · corrodedN 970 LH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER 57-41-011-4.SDR 01FDEA00728Bushing · corrodedN 971 RH FWD TERMINAL PIN BUSHING CORRODED. R&R BUSHING PER IAW 57-41-011-4.SDR SWAA012327Fitting · corrodedDURING SCHEDULED D CHECK, FOUND LH MLG SUPPORT BEAM AFT HANGER FITTING CORRODED. R&R FITTING PER MM.SDR SWAA012130Fitting · crackedDURING SCHEDULED C3 CHECK, FOUND LH MLG BEAM HANGER FITTING CRACKED AT FWD END. R&R FITTING PER ALM INV. # SWA 10410.SDR SWAA012131Fitting · crackedDURING SCHEDULED D CHECK, FOUND RH MLG BEAM FITTING CRACKED AT D HOLE. REPAIRED FITTING PER BFG ER.SDR SWAA012071Support Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND LH & RH MLG WALKING BEAM SUPPORT FITTINGS CORRODED. R&R MLG SUPPORT FITTINGS PER MM.SDR MWEA011048Cap · cracked3 1/2" CRACK FOUND ON LEFT UPPER FORWARD SPAR CAP 2 1/2" OUTBOARD OF XCW 58.5 AS VIEWED THROUGH ACCESS PANEL. -- TRIMMED OUT CRACK, TRIMMED AND LOCATED FILLERS, NESTED ANGLE, STIFFNER, INSTALLED FILLER AND ANGLE.SDR RRXA11403Clip · crackedDURING A MAINTENANCE VISIT FOUND R/H CTR WING L/E HAS A CRACKED CLIP XOLDI 6.225. *** CORRECTIVE ACTION *** REMOVED DAMAGED CLIP, FOUND FRAM CRACKED, STOP DRILLED CRACK. FABRICATED CLIP AND DOUBLER IAWIAW DC8 DRW 5754701 AND SRM 57-2-0 FIG 2. INSTALLED CLIPSDR RRXA11392Clamp · crackedDURING A MAINTENANCE VISIT FOUND R/H WING O/B L/E STA XRS 761 PNEUMATIC DUCT LOWER BRACKET CRACKED, FOUND 2 NUT PLATE BROKEN. *** CORRECTIVE ACTION *** REMOVED AND REPLACED NUT PLATES, REMOVED AND REPLACED BRACKETS IAW SRM 51-1-21 AND 51-30 AND 51-1-20D.SDR SWAA011885Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND MLG WALKING BEAM SUPPORT FITTING CORRODED AT LH FWD. R&R FITTING PER MM.SDR RRXA11379Fitting · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CTR L/E STA XFS 404-400 FITTING CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED FITTING IAW DWG # 5770409, SRM 51-1-20, 51-1-21 AND 51-1-21ASDR RRXA11373Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H CTR L/E XFS 329.0 LWR WAS CRACKED. *** CORRECTIVE ACTION *** REMOVED AND REPLACED RIB AND REINSTALLED IAW SRM 51-1-20D AND DWG 5769530-54.SDR ERKR200100143Splice Plate · damagedWING REAR SPAR LOWER SPLICE PLATE - HOLE - K COUNTERBORED.SDR RRXA11369Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA 480. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2. NDT DETERMINED CRACK TEMINATED AT STOP DRILL PER SPM 06-10-01.001, FABRICATSDR RRXA11368Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED STA XS 473.5. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21 STOP DRILLED CRACK PER SRM 57-2-0 FIG 2, NDT DETERMINED CRACK TERMINATES AT STOP DRILL PER SRM 06-10-01.001. FABSDR RRXA11367Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING MID L/E UPPER RIB TIP CRACKED AT STA XS461. *** CORRECTIVE ACTION *** REMOVED FASTENER PER SRM 51-1-21. STOP DRILLED CRACK PER SRM 57-2-0 FIG 2 PG 9 NOT VERIFIED CRACK TERMINATES AT STOP DRILL PER SPM0G10-01.001. FASDR RRXA11364Rib · crackedDURING A MAINTENANCE VISIT FOUND L/H WING CENTER L/E STA XFS 310 RIB CRACKED AFT UPPER END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2SDR RRXA11313Panel · delaminatedDURING A MAINTENANCE VISIT FOUND DELAMINATION DAMAGE TO L/H WING LWR T/E PANEL INBOARD OF FLAP HINGE AT STA.219, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART AND INSTALLSDR RRXA11360Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E XFS 393 RIB CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2SDR RRXA11359Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E STA XFS 372 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2SDR RRXA11358Rib · crackedDURING A MAINTENANCE VISIT FOUND R/H WING CENTER L/E RIB STA XFS 397 CRACKED UPPER AFT END. *** CORRECTIVE ACTION *** REPAIRED RIB IAW DC8 SRM 57-2-0 FIG 2SDR ERKR200100135Splice · corrodedLEFT AND RIGHT BS 1241 REAR SPAR- ANGLE SPLICE. THIS ECRA SPLICES IN A NEW SECTION OF 65B10821-1 ANGLE ON BOTH SIDES UP TO THE INBOARD EDGES OF THE BULKHEAD FITTINGS. REPAIR IS ACCOMPLISHED USING A SPLICE ANGLE AT LBL 80 AND RBL 80. ADDITIONALLY THE TAPERSHSDR SWAA011742Attach Fitting · corrodedDURING SCHEDULED SERVICE CHECK, FOUND LH MLG WALKING BEAM ATTACH FITTING CORRODED. R&R BEAM ATTACH FITTING PER MM.SDR RRXA11280Skin · corrodedDURING A MAINTENANCE VISIT FOUND CORROSION DAMAGE TO R/H UPPER WING SKIN AT STA. XRS22.750 AND STR#3, 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-8SDR RRXA11253Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H I/B L/E PNEUMATIC DUCT SUPPORT BRACKET, 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 51-1SDR RRXA11245Panel · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO RT WING LOWER T/E PANEL I/B OF #1 SPOILER AT STA.XW3, 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 SWAA011699Support Fitting · corrodedDURING SCHEDULED A2 CHECK, FOUND RH MLG WALKING BEAM SUPPORT FITTING CORRODED. R&R MLG SUPPORT FITTING PER ALM WORK CARD 3371.SDR RRXA11238Bracket · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING I/B AND O/B FIRE BOTTLE BRACKET, 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 51-1-2SDR QXEA0100945Structure · damagedYYC - RIGHT-HAND STUBWING TRAILING EDGE HAS PLAY. REPAIED IAW HORIZON AIR EA 4-54-130 AND FOKKER MM 54-10-02, PAGE 3.SDR AUS20010684Structure · delaminated(AUS) INTERNAL DELAMINATION OF WING/FUEL TANK. SEVERE FUEL LEAKAGE. THE AIRCRAFT IS A HOMEBUILT AND IT IS SUSPECTED THAT INCORRECTTECHNIQUES WERE USED IN THE CONSTRUCTION.SDR RRXA11203Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING L/E RIB AT STA. XFS785, 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 57-2-0 FIG.2, 5SDR RRXA11202Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E RIB AT STA. XFS778.25, 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 57-2-0 FSDR RRXA11201Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIBS AT STA. XFS716.25, 728.75, 735, 741.25, 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 51-1-20DSDR RRXA11194Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO LT WING O/B L/E LOWER RIBS AT STA. XFS660-641.25-653.75, 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, SDR RRXA11193Doubler · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING CENTER L/E INTERNAL DOUBLER LOCATED AT DRAIN HOLE AT STA. XFS337, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED PART SDR RRXA11192Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING L/E LOWER RIB AT STA. XFS653.75, 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 57-2-0SDR RRXA11191Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIB AT STA.XFS616.25-622.5, 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 SSDR RRXA11186Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E RIBS AT STA. XFS672.5-678.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. NDT HFCC INSP IAW SPM06-10-01.001. FABRICATEDSDR RRXA11180Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO R/H WING O/B L/E UPPER RIB AT STA.XFS610-566.25, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. /////CORRECTIVE ACTION///// REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. HFCC INSPECTION IAW SPM 06-10-01.001. FABRSDR RRXA11178Rib · crackedDURING A MAINTENANCE VISIT FOUND CRACK DAMAGE TO L/H WING L/E UPPER RIB AT STA.XFS691.25, 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 DC-8 SRM 57-2-SDR USAA010697Structure · corrodedPIT - FOUND CORROSION 1 INCH BY 6 INCH, LT WING 7211 OPENING. CORROSION LEVEL 1, TASK NR C53-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGE 213-216. (M)SDR USAA010696Structure · corrodedPIT - FOUND CORROSION 1 INCH BY 4 INCH AREA, LT WING 7204L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)SDR USAA010695Structure · corrodedPIT - FOUND MATING SURFACE 1 INCH BY 3 INCH, LT WING 7213L OPENING. CORROSION LEVEL 1, TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216.SDR USAA010693Structure · corrodedPIT - FOUND MATING SURFACE 1 INCH BY 4 INCH AREA OF CORROSION, LT WING 7202L OPENING. CORROSION LEVEL 1 TASK NR C57-300-01. CLEANED CORROSION, ROTO PEENED, TREATED PER SRM 57-20-01 PAGES 213-216. (M)
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