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 CAL950772Rib · crackedHOU - INSPECTION FOUND A 3 INCH CRACK IN RT WING RIB. A DOUBLER WAS INSTALLED IAW SRM 57-06, FIGURE 5. (X)SDR S2YA950020Rib · crackedDURING AN SCHEDULED INSPECTION, MAINTENANCE FOUND THE LEFT WING CENTER MID RIB AT WS 83.00 TO HAVE A CRACK AT THE TOP APPROXIMATELY FIVE INCHES ACROSS. THE CRACK WAS LOCATED BETWEEN THE FORWARD AND AFT POWER PACK MOUNTS AND A REPAIR WAS MADE. THE RIB REINFORSDR DLL13953416Rib · crackedTHE LT AND RT WING RIB UPPER CAPS AT IWS 503 WERE FOUND WITH SEVERAL CRACKS IN THE TYPICAL LOCATIONS AT THE ATTACH TABS AT AIRCRAFT HMV. THESE CAPS WILL BE REPLACED PER DL ERA 271522-14.SDR UPS204130Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND THE RT WING RIB AT WS 546.5 WAS CRACKED AT S-6 LOWER AND S-9 UPPER. MAINTENANCE REPLACED THE RIB IAW UPS EO B727-5710-1325-6 AND MM 28-10-00.SDR UPS204126Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK AT RT WING RIB AT WS 546.5. MAINTENANCE REMOVED AND INSTALLED A NEW RIB IAW EO B727-5710-13256.SDR UPS204115Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 SLAT I/B TRACK SUPPORT FITTINGS AND RIBS CRACKED BEYOND STOP DRILL. MAINTENANCE REMOVED AND REPLACED THE RIBS PER SRM 51-30-2.SDR UPS804099Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 778.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.SDR UPS804098Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 653.75. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.SDR UPS804097Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 641.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.SDR UPS804096Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB STA XFS 660.0 WAS CRACKED. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.SDR UPS804095Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 728.75 WAS CRACKED. STOP DRILLED CRACK AND FABRICATED REPAIR PARTS AND INSTALLED PER SRM 57-20-0.SDR UPS804094Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 566.25 WAS CRACKED AT THE AFT UPPER END. STOP DRILLED CRACK AND FABRICATED REPAIR DOUBLERS AND INSTALLED PER SRM 57-20-0.SDR UPS804093Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 610.0 WAS CRACKED AT THE AFT LWR END. REPAIRED PER SRM 57-2-0.SDR UPS804092Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0.SDR UPS804091Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 766.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-00-00.SDR UPS804090Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE LWR END. REPAIRED PER SRM 57-2-0.SDR UPS804089Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 791.25 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.SDR UPS804088Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 797.5 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.SDR UPS804087Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB AT STA XFS 810.0 WAS CRACKED AT THE UPPER END. REPAIRED PER SRM 57-2-0.SDR UPS804084Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 760.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00.SDR UPS804083Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT LWR END. REPAIRED IAW MM 57-00-00.SDR UPS804082Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E AT STA XFS 672.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00.SDR UPS804081Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD L/E RIB AT STA XFS 785.0 WAS CRACKED AT THE AFT UPPER END. REPAIRED IAW MM 57-00-00 PG 801.SDR UPS804080Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT OTBD WING, STA XFS 747.5 RIB WAS CRACKED AT THE AFT UPPER END. REPAIRED RIB IAW MM 57-00-00 PG 801.SDR UPS8040100Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND RT WING L/E RIB WAS CRACKED STA XFS 816.25. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 57-20-0.SDR UPS204075Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W INBD MIDFLAP, OB CENTER TRACK RIB FITTING WAS CRACKED. INSTALLED NEW TRACK RIB FITTING IAW SRM 51-30-2 AND SRM 51-10-1.SDR UPS204038Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W STA 171.5 UPPER RIB CHORD CRACKED AT STRINGER 5 TO 20 ATTACH POINT. REMOVED FASTENERS AND CUT OUT DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-2, 51-30-2.SDR DLL13953342Rib · crackedTHE LT WING RIB UPPER CAP AT IWS 503 HAS SEVERAL CRACKS IN THE ATTACH TABS. DUE TO STRUCTURAL CONSTRAINTS IT IS DESIRABLE TO REPLACE THE UPPER CAP RATHER THAN REPAIR SUBJECT DAMAGED PART. REPAIRED PER DL ERA 271522-14AD.SDR DLL13953321Rib · crackedLT/RT WING RIB LOWER CAP AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPAIRED PER DL ERA 271518-14AD. FOUND AT HMV.SDR UPS 803947Le Rib · crackedWHILE IN DALFORT FOR C-MAINT, FOUND UPPER LEADING EDGE RIBS CRACKED AT STA XSF 416, XSF 410, XFS 373, XFS 304, AND XFS 310, UPPER AND LOWER. REPAIRED PER MM 57-00-00, FIG 801.SDR PAYA95A4032Rib · chafedLEFT WING RIB NR 30 CHAFED AT THE STROBE POWER SUPPLY MOUNTING LOCATION. REPAIRED IAW AN 8110-3. (M)SDR 95ZZZX4518Rib · crackedDURING ANNUAL INSPECTION, CRACKS FOUND AT RIB REAR ATTACHMENT AREA. ALSO, FOUND INBOARD FLAP ATTACHMENT CRACKED. AIRCRAFT WAS DAMAGED AT APPROX 500 HOURS. RT WING WAS REBUILT WITH NEW RIBS. LT WING REPLACED WITH USED WING. LT WING WAS FROM A PA22-135. RT SDR UPS803906Rib · crackedWHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND RT WING OUTBOARD LEADING EDGE 4 EACH UPPER RIBS CRACKED AT STA XFS 735, XFS 791, XFS 811, AND XFS 817. REPAIRED RIBS PER MM 57-00-00, FIG. 801.SDR UPS803905Rib · crackedWHILE IN DALFORT FOR C-CHECK, MAINTENANCE FOUND LT WING LEADING EDGE 7 EACH RIBS CRACKED AT STA XFS 835, XFS 817, XFS 804 LOWER, XFS 823, XFS 804 UPPER, XFS 720, AND XFS 763. REPAIRED RIBS PER MM 57-00-00, FIG 801.SDR SWAA950548Chord · crackedDURING SCHEDULED 1/2 D-CHECK, FOUND RIGHT WING RIB LOWER CHORD CRACKED AT WBL 135.5, FWD OF S2 AT RADIUS. REPAIRED PER SWA ACO 587-57.SDR UPS203873Rib · crackedWHILE IN FOR SI CHECK, MAINTENANCE FOUND CRACKED RIB ON SLAT TRACK ON O/B SIDE. REPLACED IAW SRM 57-51-31 AND 51-30-2.SDR DL72L953064Rib · crackedFOUND DURING A-2 LETTER CHECK, .25 INCH CRACK NR 2 L/E SLAT ACT ATTACH I/B RIB. REPAIRED PER MM 57-54-0.SDR Y2PA950011Rib · brokenYIP - DURING A ROUTINE MAINTENANCE INSPECTION, IT WAS NOTED THAT THE LEFT WING OUTBOARD SPOILER SUPPORT UPPER RIB ASSEMBLY WAS BROKEN, AND A SECTION OF THE RIB WAS MISSING. REMOVED AND REPLACED RIB ASSEMBLY. NEW RIB WAS PROCURED PRE-DRILLED AND THE HOLES DIDSDR UPS203810Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED UPPER RIB CHORD AT FWD VENT BOX FWD FLANGE 7 INCHES AFT OF FRONT SPAR ON LEFT WING AT STA 171.5. REPAIRED IAW SRM 51-40-04.SDR 96ZZZM544Rib · crackDURING D-CHECK, RIB INSIDE RIGHT WING HAS 5 INCH CRACK AS SEEN THROUGH ACCESS HOLE NR 8811. REMOVED FASTENERS AND OPENED LOWER SKIN FOR ACCESS PER SRM 51-30-2. STOP DRILLED AT END OF CRACKS PER SRM 51-10-1. FABRICATED ANGLE REPAIR 2024-T3 .063 12 INCH BY 1 SDR 96ZZZM543Rib · crackedDURING D-CHECK, FOUND WING LEADING EDGE INTERIOR UPPER RIB REPAIR ANGLE IS CRACKED AT AFT END STATION 349.6 OUTBOARD SIDE. INSTALLED FAB CHANNEL 2024-T3 .040 INCH 14 INCHES LONG BY 3 INCHES WIDE PER SRM 51-40-3. LOCATION, WING L/E STATION 349.6 OUTBOARD SIDESDR 96ZZZM542Rib · crackedDURING D-CHECK, FIXED WING LEADING EDGE STATION 130.7 INNER RIB HAS LOWER INBD INNER REPAIR ANGLE CRACKED 5 INCHES FROM FWD END. REMOVED FASTENERS FROM REPAIR ANGLE. REMOVED FASTENERS FROM ANGLE AND CUT OUT ANGLE PER SRM 51-40-4. FABRICATED ANGLE 2024-T3 .0SDR 96ZZZM541Rib · crackedDURING D-CHECK, FIXED WING LEADING EDGE AT WBL 92.8 INNER VERTICAL SUPPORT 2ND FROM AFT END IS CRACKED AT TOP FASTENER. STOP DRILLED CRACK AS PER SRM 51-10-1. FABRICATED DOUBLER AND FILLER 2024-T3 .050 5 INCH BY 5 INCH AND INSTALLED PER SRM 51-40-2.SDR DLL13953322Rib · crackedLT/RT WING RIB UPPER CAPS AT IWS 555 HAVE SEVERAL CRACKS IN THE TYPICAL LOCATION AT THE ATTACH TABS. REPLACED CAP PER ERA 271319-14AD.SDR P5CA9500537Rib · crackedCRACKED FORGED RIB LEFT WING LEADING EDGE CAVITY WS 800. (2 CRACKS ON AFT UPPER LEFT SIDE CHORD). MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03 INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500536Rib · crackedCRACKED UPPER LEFT CHORD ON FORGE RIB AT WS 930 LEFT WING LEADING EDGE CAVITY. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.SDR P5CA9500535Rib · crackedCRACKED FORGE RIB LEFT WING LEADING EDGE CAVITY WS 960 AFT RIGHT SIDE UPPER CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER SRM 51-30-02.SDR P5CA9500534Rib · crackedCRACK ON LEFT WING LEADING CAVITY WS 850 FORGED RIB AT THE AFT UPPER LEFT SIDE CHORD. MANUFACTURED REINFORCEMENT PER BOEING SRM 57-20-03, INSTALLED PER BOEING SRM 51-30-02.SDR P5CA9500585Rib · crackedCRACK ON LEFT WING LEADING CAVITY WS 950 FORGED RIB AFT UPPER CHORD. REPAIRED PER BOEING SRM 57-20-03.SDR CAL950585Rib · crackedGSO - INSPECTION FOUND A .25 INCH CRACK IN RADIUS OF RT RIB AT LOWER FORWARD ATTACH HOLE, STA 738. THE CRACK WAS STOP-DRILLED. DOUBLER AND FILLER WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 57-10-5. (X)
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