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 CAL950370Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN NR 4 SLAT OUTBOARD SECOND RIB. A REPAIR ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-50-3. (M)SDR CAL950358Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK ON LOWER SIDE OF LEFT WING INTERNAL RIB AT WS 738.5, ABOVE S-8. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-30-2 AND 57-10-5. (W)SDR SWAA950334Rib · crackedDURING SCHEDULED D-CHECK, FOUND RIB UPPER FLANGE CRACKED AT LEFT WING STA 453 AT FWD STRINGER ATTACH. REPAIRED PER BOEING STRUCTURAL REPAIR MANUAL.SDR MWEA95193Rib · crackedDURING ROUTINE MAINTENANCE, 2 CRACKS WERE FOUND ON LT WING LEADING EDGE RIB STA.XIS 137.0. ONE CRACK AT AFT UPPER END 3 FEET IN LENGTH, THE OTHER CRACK AT FWD UPPER END 1.50 INCHES IN LENGTH. BOTH CRACKS TEMPORARILY REPAIRED PER DOUGLAS TELEX 5-57-20-6 AND WSDR MWEA95191Rib · crackedDURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA XIS 129.710 WAS FOUND CRACKED AT LOWER LEG 2.75 INCHES IN LENGTH.SDR MWEA95190Rib · crackedDURING ROUTINE MAINTENANCE, THE LEFT WING LEADING EDGE RIB AT STA.XIS 134.921 WAS FOUND CRACKED AT LOWER AFT END 1.3750 INCHES IN LENGTH.SDR 95ZZZX2422Rib · crackedDURING 100-HOUR INSPECTION UPON REMOVAL OF 95643-07 BRACKET ASSEMBLY, FOUND CRACK IN RIB ASSY AT SPAR ATTACH POINT. SUSPECT CRACKING DUE TO AGE AND MANY SIDE LOAD LANDINGS BY STUDENTS. SUGGEST RIB BE MANUFACTURED FROM THICKER ALUMINUM.SDR 95ZZZX2381Rib · crackedTHIS RIB IS LOCATED AT STA 49.25, IN THE MAIN LANDING GEAR WELLS. FOUND 3 SENECA'S WHERE THIS RIB HAS BEEN CRACKED IN THE RADIUS OF THE OUTBOARD ANGLE UNDER THE DRAG BRACE SUPPORT. PIPER PA-28R HAS THIS SAME PROBLEM. SUSPECT THE CAUSE IS FROM HARD OR GRASS SDR 95ZZZX2380Rib · crackedTHIS RIB IS LOCATED AT STA 49.25, IN THE MAIN LANDING GEAR WELLS. FOUND 3 SENECA'S WHERE THIS RIB HAS BEEN CRACKED IN THE RADIUS OF THE OUTBOARD ANGLE UNDER THE DRAG BRACE SUPPORT. PIPER PA-28R HAS THIS SAME PROBLEM. SUSPECT THE CAUSE IS FROM HARD OR GRASS SDR UPS203078Rib Chord · crackedWHILE IN C-CHECK, MAINTENANCE FOUND A CRACK IN THE RIB UPPER CHORD AT BL 70.5. MAINTENANCE REPAIRED AND MODIFIED THE CHORD IAW UPS EO 727-5710-1271G.SDR 9506899988Rib · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND CRACKS IN THE RIGHT WING LEADING EDGE NOSE RIBS LOWER ENDS, 3RD, 4TH, AND 6TH RIBS OUTBOARD OF THE NR 10 SLAT TRACK. REPAIRED RIBS PER XEA X9-57-19.SDR UPS202974Rib · corrodedWHILE IN 'C' CHECK, MAINTENANCE FOUND CORROSION ON LT WING RIB UPPER CHORD AT LBL 70.5 TEE CLIP AND STRAP. INSTALLED REPAIR UPS EO B727-5710-1271.SDR 95ZZZX2480Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER MID-RIB AT WS 83.00 TO HAVE A CRACK 5 INCHES LONG. THE CRACK WAS LOCATED IN THE TOP BEND RADIUS, EXTENDING DOWN AT AN ANGLE FROM THE FORWARD REINFORCEMENT ATTACH POINT. THE FORWARD REINFORCEMENT, PN 114-SDR 95ZZZX2479Rib · crackedDURING AN INSPECTION, MAINTENANCE FOUND LT WING CENTER SECTION MID-RIB AT WS 83.00 TO HAVE A CRACK 1.1250 INCH LONG. THE CRACK WAS ALONG THE TOP BEND RADIUS AT THE RIB CENTER STIFFENER ATTACH POINT. THE FORWARD REINFORCEMENT PN 114-120033-15 WAS ALSO CRACKEDSDR SWIA95562Rib · crackedLEFT WING (UPPER) IN THIRD CELL OUTBOARD OF NACELLE, ONE EACH RIB ATTACH FLANGE SECOND AFT CRACKED. FABRICATED AND REPLACED ONE EACH RIB ATTACH FLANGE AT UPPER SKIN SECOND AFT IN THIRD CELL OUTBOARD OF LEFT NACELLE.SDR SWIA95561Rib · crackedLEFT WING (UPPER) IN FIRST CELL OUTBOARD OF NACELLE, FOUR EACH RIB ATTACH FLANGE RIVETED TO UPPER SKIN CRACKED. FABRICATED AND REPLACED FOUR EACH RIB ATTACH FLANGES AT UPPER SKIN FIRST CELL OUTBOARD OF LEFT NACELLE.SDR 95ZZZX2062Rib · not rivetedDURING ANNUAL INSPECTION, FOUND LEFT WING, TIP RIB WAS NOT RIVETED TO MAIN SPAR. THIS APPEARS TO HAVE NEVER BEEN RIVETED. THIS HAS APPARENTLY BEEN OVERLOOKED SINCE THE AIRCRAFT WAS BUILT IN 1975. THE DEFECT IS PLAINLY VISIBLE WITH THE WING TIP REMOVED, IT ISDR 95ZZZX2061Rib · not rivetedDURING ANNUAL INSPECTION, FOUND LEFT WING, TIP RIB WAS NOT RIVETED TO MAIN SPAR. THIS APPEARS TO HAVE NEVER BEEN RIVETED. THIS HAS APPARENTLY BEEN OVERLOOKED SINCE THE AIRCRAFT WAS BUILT IN 1975. THE DEFECT IS PLAINLY VISIBLE WITH THE WING TIP REMOVED, IT ISDR 9506009948Bulkhead · crackedDURING ACCEPTANCE CHECK AND PRIOR TO SERVICE, FOUND .375 INCH CRACK IN LEFT BULKHEAD 42 LOWER 'T' EXTRUSION AT AFT END. REPAIRED PER EA 99-092430.SDR DLL17951738Rib · corrodedDURING HMV, THE A HOLE IN THE MLG ATTACH RIB WAS OVERSIZED TO REMOVE CORROSION. ACCOMPLISHED REPAIRS PER DL ERA 270587-14.SDR PAYA95A4017Rib · crackedDURING C-CHECK, FOUND LEFT WING TIP RIB (RIB NR 30,Z516) CRACKED. REPLACED RIB. (X)SDR IXXA9550Rib · crackedDURING ROUTINE C-CHECK INSPECTION, A CRACK WAS FOUND AT XRS-6 RIB. THE RIB WAS REPAIRED IAW DRAWING HSE27-57-169, WHICH WAS FAA DER APPROVED, AND EO 57-DC8-151. (W)SDR 95ZZZX2006Rib · crackedMSP - DURING A SCHEDULED INSPECTION, MECHANICS COMPLETED A REPAIR TO LT WING RIB, PN 27-31240, AT WS 51, DUE TO CRACK AT HYDRAULIC BULKHEAD FITTING. WORK DONE IAW FAC ARP 57-20-9313, REV. A.SDR UPS202680Rib · crackedWHILE IN 'C' CHECK, MAINTENANCE FOUND CRACK INDICATIONS IN THE FWD 2 HOLES IN RIB CHORD AT STA 760, LBL 70.5. MX REPAIRED IAW UPS EO B727-5710-1271-F, APPENDIX F.SDR ABXA9500303Rib · gougedDURING C-CHECK, INSPECTION FOUND DEEP GOUGE ON RIGHT WING ADJACENT TO TELESCOPIC SLAT BLEED AIR DUCT. REPAIRED IAW ABX REA D957-11203-MR.SDR UPS202662Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND CRACKS IN RIB CHORD AT TWO FASTENER HOLES, BS 760, RBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-6789A.SDR UPS202661Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND 3 CRACKS AROUND HOLES IN RIB CHORD BS 760, LBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-1271.SDR CAL950210Le Rib · crackedGSO - INSPECTION FOUND A 1.2 INCH CRACK IN RT WING LEADING EDGE RIB, JUST OUTBOARD OF NR 5 SLAT ACTUATOR. THE CRACKED SECTION WAS REMOVED IAW SRM 51-30-2 AND A REPAIR WAS INSTALLED IAW SRM 51-20-4 AND SRM 51-30-2. (X)SDR UPS802657Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND CRACKS ON LT WING, LWR SURFACE, UPPER RIBS 13, 29, 24, AND 14. REPAIRED PER MM 57-00-00.SDR UPS202598Rib Chord · corrodedWHILE IN 'D' CHECK, MAINTENANCE FOUND CORROSION ON UPPER VERTICAL FLANGE OF THE WING TO BODY RIB UPPER CHORDS AT BS 760, RBL 70.5, AND LBL 70.5. INSTALLED REPAIR PER UPS EO B727-5710-1271F.SDR 9503612705Rib Chord · crackedDURING PCK, MAINTENANCE FOUND WING TO BODY UPPER RIB CHORD, FS 760, RBL 70.5 CRACKED. REPAIRED PER NWA EA 27-096690.SDR MALA954349Rib · crackedMSP - DURING A MAINTENANCE INSPECTION, MECHANICS FOUND TRAILING EDGE OF RT WING RIB (PN 27-31241-076) AT WS 66.58, CRACKED. COMPLETED REPAIR TO THE TRAILING EDGE OF THE RT WING RIB IAW FAIRCHILD LAR 95-MALA-064 AND SRM. (X)SDR 95ZZZW261Rib · crackedMCI - DURING OP-17, FOUND A ONE INCH CRACK IN UPPER RIB CAP I/B SIDE AT STRINGERS 21 AND 24, STA 503.76. REPAIRED UPPER RIB CAP PER DWG. NR 1647070 AND INSTALLED NEW SPLICE PER VIEW K. TOTAL CYCLES 22210.SDR 95ZZZW260Rib · crackedMCI - DURING OP-17, FOUND STA 555 UPPER RIB CRACKED O/B SIDE OF STRINGER 18 AND FOUND A .5 INCH CRACK AT STRINGER 19. INSTALLED NEW SECTION OF UPPER CAP FROM STRING 19 FWD PER DWG NR 1647070. TOTAL CYCLES 22210.SDR DLL16950796Rib Caps · cutAT HMV, RIB CAPS AT IWS 293.38 AND 319.83 WERE CUT TO FACILITATE REMOVAL AND COLD WORK OF FASTENERS IN REAR SPAR REWORK. REF EO 7-59089-3. REPAIRED RIBS PER SRM 57-12-00.SDR CAL950160Rib · crackedGSO - INSPECTION FOUND A .5 INCH CRACK IN O/B RIB AT RT WING NR 4 SLAT O/B TRACK. THE CRACK WAS STOP DRILLED AND REPAIR FITTINGS WERE INSTALLED IAW EC 5710-01660. (W)SDR 95ZZZW230Rib · crackedMCI - DURING SPECIAL CHECK, FOUND CRACKS AT STA 555 UPPER RIB CAP AS FOLLOWS, .75 INCH O/B OF STRINGER 18, 1 INCH IN STRINGER 18 CASTELLATION, .6250 INCH STRINGER 19, 1 INCH I/B SIDE OF STRINGER 19, AND .0625 INCH AT STRINGER 21. REPAIRED SECTIONS OF CAP PER SDR 95ZZZZ132Rib · corrodedDURING THE COURSE OF AN 8000 HOUR INSPECTION, FOUND LOWER WING RIB AT WS 42.3 HAD EXFOLATION IN THE FUEL TANK AREA UNDER PANEL 521AT. THIS AREA IS NORMALLY COVERED BY SEALANT AND IS NOT READILY AVAILABLE FOR INSPECTION. AREA WAS CLEANED AND FOUND CORROSION DSDR UPS802295Ribs · crackedDURING 'C' CHECK, MAINTENANCE FOUND LEFT WING LEADING EDGE RIBS CRACKED AT STATIONS XFS 313, 369, 622, 672, 790, 796 UPPER, AND XFS 790 LOWER. REPAIRED RIBS PER MM 57-00-00.SDR 95ZZZW227Rib · crackedMCI - DURING SPECIAL CHECK, FOUND CRACKS IN UPPER RIB CAP IWS 503, IN CASTELLATION AT FORWARD SIDE OF STRINGERS 13, 24 AND 25, 1.1250 INCH, 1.25 INCH AND ONE INCH, RESPECTIVELY, INTO AND THROUGH RADIUS. REPAIRED BY INSTALLATION OF NEW SECTION OF RIB CAP PER DSDR ARWA0927952Rib · bentDURING INCIDENT INSPECTION, FOUND RIGHT WING RIB SUPPORT FOR WING TIP AT STA XW 761.695 DAMAGED AT LEADING EDGE AREA. FABRICATED NOSE SECTION OF BULKHEAD FROM .071 INCH 7075-0, AND NOSE DOUBLER AND SPLICE DOUBLER FROM .080 INCH 7075-0. HEAT TREATED, PRIMED, SDR 95ZZZZ119Rib · elongatedDURING MAINTENANCE INSPECTION IN MSP, FOUND THE LEFT WING RIB P/N 27-84010-005 TO HAVE ELONGATED HOLE AT HYDRAULIC LINE PASS THROUGH, FORWARD OF MAIN SPAR. COMPLETED REPAIR TO LEFT WING RIB IAW FAIRCHILD ARP 57-20-9313 AND SRM. (Z)SDR UPS802129Rib · crackedDURING 'C' CHECK MAINTENANCE FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STA XFS 660. REPAIRED RIB PER MM 57-00-00.SDR UPS202175Rib Chord · crackWHILE IN 'D' CHECK MAINTENANCE FOUND RIGHT WING RIB CHORD CRACKED AT WS 686.5 LOWER CHORD STRINGER 6. INSTALLED REPAIR IAW SRM 57-10-5, 51-10-1, 51-10-2 AND 51-30-2.SDR UPS202148Rib · crackedWHILE IN 'D' CHECK MAINTENANCE FOUND I/B TRACK O/B RIB FLANGE CRACKED. INSTALLED REPAIR IAW EO727-57-1078.SDR DL72S950585Rib · crackedDURING HMV, FOUND RIB CRACKED ON O/B SIDE OF NR 6 L/E SLAT TAI DUCT AND A RIB CRACKED NEXT RIB O/B OF ITEM NR 1, REPAIRED BYSTOP DRILLING CRACK AND FABRICATING REPAIR DOUBLER PER SRM 57-50-3 PG 25, INSTALLED REPAIR PER SRM 57-50-3 PG 25.SDR UPS802126Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 9, 11, 12, 14, AND 16 UPPER RIBS CRACKED ON UPPER SURFACES. INSTALLED REPAIRS IAW MM 57-00-00, FIG. 801. (P/N 5769589, 5720123).SDR UPS802125Ribs · crackedWHILE IN 'C' CHECK MAINTENANCE FOUND LT WING OUTBOARD LEADING EDGE ASSY. NR 17, 21, 24, AND 27 UPPER RIBS CRACKED IN UPPER SURFACES. INSTALLED REPAIRS IAW MM 27-00-00, FIG. 801. (P/N 5769589, 5720123).SDR 95ZZZX883Rib · crackedMCI - DURING SPECIAL CHECK FOUND A 1.25 INCH CRACK IN RT WING INTERNAL/LOWER RIB CAP AT AFT RADIUS, IWS 555, OUTBOARD SIDE, 6TH STRINGER FROM AFT. REMOVED AND REPLACED LOWER FORWARD RIB CHORD PER SB 093-57-207, AND DWG. NR 1647070. AIRCRAFT TOTAL TIME: 59,5SDR 95ZZZX770Rib · crackedWHILE PERFORMING A 200-HOUR INSPECTION, FOUND RIB CRACKED IN WHEELWELL, RT WING STA 49.0 INCH. FOUND RUBBER BUMPER ASSY, PIPER PN 42746-00, WORN OUT AND LANDING GEAR HITTING RIB WHEN LANDING GEAR SELECTED UP (IN-FLIGHT) COULD NOT DUPLICATE ON GROUND. SUGGEST
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