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 UPS202119Rib Mount Tab · crackedWHILE IN 'D' CHECK, MAINT FOUND VENT BOX STR 12 RIB MOUNT TAB CRACKED AT WS 656.5 (KIT P/N 65C26139-16), LT WING. INSTALLED REPAIR IAW SRM 57-10-4 AND SB 57A159.SDR 95FDEA00104Rib · crackedHFECI OF FASTENER HOLES AT BS 760 LBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED IN RIB CHORD, AND BOTTOM HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760 LBL 70.5 PER FEDEX EA 7-5710-23684.SDR 95FDEA00103Rib · crackedHFECI OF FASTENER HOLES AT BS 760, RBL 70.5 SHOW CORROSION THROUGHOUT ALL SIX HOLES. TOP FWD HOLE IS CRACKED THREE PLACES IN RIB CHORD, AND BOTTOM FWD HOLE HAS A CRACK IN THE RIB CHORD. REPAIRED FASTENER HOLES AT BS 760, RBL 70.5 PER FEDEX EA 7-5710-2368A.SDR 95ZZZX848Rib · crackedMCI - DURING SPECIAL CHECK, FOUND A 1 INCH CRACK IN IWS 555 RIB UPPER CAP CASTELLATION, AT 14 STRINGERS FORWARD OF REAR SPAR ABOVE RIB CUT OUT, LT WING. REPAIRED UPPER RIB CAP AT IWS 555 ST STR 18 AND STR 19, PER ARA 867. AIRCRAFT TOTAL TIME: 59,628 HOURS; SDR UPS202082Rib · crackedWHILE IN 'D' CHECK, MAINTENANCE FOUND RIGHT WING RIB CHORD WAS CRACKED AT WING STA 656.5, LOWER CHORD S-8. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-2, 51-20-1, 51-30-2.SDR UPS202074Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND L/W RIB CHORD IS CRACKED WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.SDR UPS202073Rib · crackedDURING 'D' CHECK, MAINTENANCE FOUND R/W RIB CHORD IS CRACKED AT WS 629 LOWER CHORD 5-6. INSTALLED REPAIR IAW SRM 57-10-5.SDR 95ZZZX849Rib · crackedMCI - DURING SPECIAL CHECK - FOUND .75 INCH CRACK IN RT WING INTERNAL UPPER RIB CAP, IN AFT RADIUS, IWS 555, OUTBOARD SIDE, SIXTH STRINGER FROM AFT STR 13. INSTALLED UPPER CHORD ANGLE PER DWG. NR. 1647070. AIRCRAFT TOTAL TIME 59,628 HOURS; 23,327 CYCLES.SDR 95ZZZX595Rib · damagedUPON 100-HOUR INSPECTION, FOUND WING SURFACE DISTORTED, SKINS CREASED ON LOWER SURFACE WS 93.00 AT MAIN SPAR. REMOVAL OF SKIN REVEALED LOWER SPAR CAP BENT, SPAR WEB CREASED AND RIBS DAMAGED. CAUSE UNKNOWN. SPAR CAP TOO WEAK AT JACK POINTS.SDR 95ZZZX594Rib · damagedUPON 100-HOUR INSPECTION, FOUND WING SURFACE DISTORTED, SKINS CREASED ON LOWER SURFACE WS 93.00 AT MAIN SPAR. REMOVAL OF SKIN REVEALED LOWER SPAR CAP BENT, SPAR WEB CREASED AND RIBS DAMAGED. CAUSE UNKNOWN. SPAR CAP TOO WEAK AT JACK POINTS.SDR 95ZZZX499Rib · crackedDURING 100-HOUR INSPECTION, FOUND RIB INSIDE RT WHEELWELL CRACKED. ALSO, FOUND RT LANDING GEAR UPPER BUMPER ASSY, PN 43016-01, CRACKED, AND, SKIN ABOVE THE BUMPER ASSY CRACKED. SUSPECT CAUSE - LANDING GEAR COMING INTO UPLOCK TOO HARD AND HITTING UPPER BUMPERSDR 9500809856Rib · crackedDURING PERIODIC CHECK, FOUND CRACK IN THE LEFT WING RIB, WS 485.5. REPAIRED PER EA 98-094922.SDR DLL16950131Rib · modifiedREF EO 7-59089-3 AT RIGHT WING IWS 319 RIB CAP BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE WITH THE RIB CAP. CUT RIB CAP AND REPAIRED PER SRM 57-12-00 PG 805.SDR DLL16950130Rib · modifiedREF EO 7-59089-3 IN COMPLIANCE OF VA 31733 AT RIGHT WING IWS293 BOTTOM HOLE ON VERTICAL RIB FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE TO RIB CAP. CUT RIB CAP FOR CLEARANCE AND REPAIRED PER SRM 57-12-00 P805.SDR DLL16950129Rib · modifiedREF EO 7-59089 AT LEFT WING IWS 319, BOTTOM HOLE ON VERICAL FLANGE CANNOT BE REAMED OR COLD WORKED DUE TO INTERFERENCE OF RIB CAP. CUT RIB FLANGE FOR TOOL CLEARENCE AND REPAIRED PER SRM 57-12-00 PG 805.SDR DLL16950128Rib · modifiedREF EO 7-59089 IN COMPLIANCE OF VA 31733AT LEFT WING RIB CAP AT IWS 293, BOTTOM HOLE ON VERTICAL FLANGE CANNOT BE REAMED OR COLD WORKED, DUE TO INTERFERENCE FROM RIB CAP. CUT RIB CAP FOR TOOL CLEARANCE AND REPAIR PER SRM 57-12-00 PG805.SDR DL72L950170Rib · crackedDURING HMV, FOUND NR 2 L/E SLAT ACTUATOR ATTACH RIBS CRACKED, REPAIRED PER MM 57-54-0.SDR UPS801932Le Ribs · crackedWHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING OUTBOARD OF NR 1 PYLON NR 4, NR 5, NR 6, NR 9, NR 10 RIBS ON LEADING EDGE CRACKED ON UPPER SURFACE. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801.SDR UPS801931Le Ribs · crackedWHILE IN 'C' CHECK, MAINTENANCE REPORTED LEFT WING LEADING EDGE NR 11, NR 12, NR 13, NR 16, NR 17 RIBS CRACKED ON UPPER SIDE COUNTING OUTBOARD OF NR 1 PYLON. INSTALLED REPAIR IAW MM 57-00-00, FIG. 801.SDR 95ZZZX932Rib · crackedDURING A ROUTINE 100-HOUR INSPECTION, CRACKS WERE FOUND IN THE RIB AT THE AILERON HINGE DOUBLER.
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