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 EISA96024Rib · crackedLEFT WING INTERNAL RIB CRACKED AT WS 601 SECOND LOWER STRINGER FWD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-05. (M)SDR AALA960331Rib · crackedTUL - LEFT 656.5 RIB CRACKED AT LOWER NR 8 STRINGER. STOP DRILLED CRACK AND INSTALLED DOUBLER PER SRM 57-10-5, PAGE 6. TST: 74,632 HRS. CYCLES, 51,110. (X)SDR EISA96021Rib · crackedRIGHT WING INTERNAL RIB CRACKED AT WS 656 SECOND LOWER STRINGER AFT OF FRONT SPAR. STOP DRILLED CRACK, FABRICATED REPAIR PER SB 727-57-0127 AND INSTALLED REPAIR PER SRM 57-10-05. (M)SDR EISA96023Rib · crackedLEFT WING INTERNAL RIB CRACKED AT WS 738 FIRST LOWER STRINGER FORWARD OF REAR SPAR. FABRICATED AND INSTALLED DOUBLER PER SRM 57-10-5. (M)SDR DLL13960378Rib Cap · crackedTHE RT WING IWS 529 UPPER CAP IS CRACKED IN TYPICAL LOCATIONS. THE REF ERA AUTHORIZES REPLACEMENT OF THE SUBJECT CAP CONTAINING CRACKS PER LAC L1011 S/B 093-57-207, REF DL ERA 272877 AD REV A.SDR 96ZZZX1133Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACKS EXTEND FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACKS AND REINSPECT AT 200-HOUR INTERVALS.SDR 96ZZZX1132Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACKS EXTEND FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACKS AND REINSPECT AT 200-HOUR INTERVALS.SDR 96ZZZX1134Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN THE LT WING CANTED RIB, PN 5722206-1. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCH. CESSNAS' REPAIR IS TO STOP-DRILL THE ENDS OF THE CRACK AND REINSPECT EACH 20SDR 96ZZZX1131Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL END OF CRACK AND REINSPECT EACH 200 HOURS ACCORDING TO THE SUSDR 96ZZZX1130Rib · crackedWHILE DOING A PHASE INSPECTION, FOUND A CRACK IN WING CANTED RIBS. CRACK EXTENDS FROM THE AFT SIDE OF THE FORWARD SPAR, REARWARD ALONG THE BEND RADIUS, 1.0 INCHES. CESSNA'S REPAIR IS TO STOP-DRILL END OF CRACK AND REINSPECT EACH 200 HOURS.SDR UPS405425Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND 2 CRACKS IN UPPER CHORD OF L/E RIB AT O/B LEADING EDGE STATION 1534.95, 1462.85, 14653.35, 1309.15, 1237.05, 1195.55 AND 1483.95. REPAIRED PER SRM 57-20-03 FIG 1.SDR UPS405424Rib · crackedWHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK IN UPPER CHORD FLANGE L/E RIB AT I/B LEADING EDGE STATION 802.5, 852.45 AND 886.5. REPAIRED IAW SRM 57-20-03 FIG 1.SDR 9604672716Rib Chord · crackedDURING PERIODIC CHECK, FOUND CRACKS IN THE BS 760 WING TO BODY UPPER RIB CHORD, UPPER AND LOWER FORWARD FASTENER HOLES. REPAIRED CHORD (P/N 65-18522-16) PER EA 27-103441.SDR 96ZZZM501Rib · crackedDURING C-CHECK, FOUND RT WING LOWER FLANGE OF WING RIB CRACKED AT WS 629 AT LOWER STRINGER 8 PER PENETRANT INSPECTION PER SB 727-57-0127 REV 3 ENDS OF CRACK MARKED. STOP DRILLED CRACK PER SRM 51-10-1 AT WS 629 LOWER STRINGER 8 OF WING RIB. INSTALLED WING INSSDR 96ZZZM500Rib · crackedDURING C-CHECK, FOUND RIGHT WING LOWER FLANGE OF WING RIB CRACKED AT WS 686 AT STRINGER 8 TWO PARALLEL CRACKS AND AT STRINGER 6 AT PREVIOUS REPAIR. PENETRANT INSPECTION PER BOHM 20-20-2 PER SB 727-57-0127. ENDS OF CRACKS MARKED. REMOVED RT WING RIB AT WS 68SDR 96ZZZM499Rib · crackedDURING C-CHECK, FOUND STATION 601 WING RIB LOWER FLANGE HAS CRACKS AT NR 6 AND NR 8 STRINGER LOCATIONS. STOP DRILLED CRACKS AT NR 6 AND NR 8 STRINGER TO RIB LOCATION, ON RIB LOWER FLANGE STATION 601.5 PER SB 727-57-0127 FIG 2. NO CRACKS PROGRESSED AFTER STOPSDR 96ZZZM490Rib · crackedDURING C-CHECK, FOUND LEFT WING, LOWER FLANGE OF WING RIB AT WS 686 CRACKED AT STRINGER 6 AND STRINGER 8. MARKED PENETRANT INSPECTION PER OHM 20-20-2 PER SB 727-57-0127. STOP DRILLED EACH END OF CRACKS AS PER SRM 51-10-1. INSTALLED WING RIB REPAIR AS PER SRSDR 96ZZZM489Rib · mis repairedDURING C-CHECK, FOUND WING RIB STATION 656 HAS PREVIOUS REPAIR WITH CUTOUT EXCEEDING 3 INCH LIMIT ON SRM 57-10-5 FIG 2. REMOVED AND REPLACED WING RIB AT STATION 656 PER SB 727-57-0127.SDR MWEA96031Rib · crackedDURING C-CHECK, FOUND TWO LEADING EDGE RIBS AT STA XIS 134.9 AND 137.0 ON LT WING CRACKED. REPLACED LEADING EDGE RIBS IAW SRM 51-30-2 AND RETURNED A/C TO SERVICE.SDR AU960113Rib · cracked(AUS) WING RIB LOCATED IN WHEEL WELL CRACKED FROM RIVET HOLESSDR 96ZZZX1505Rib · crackedDURING C/W AD 95-20-07, FOUND AFT RIB ASSEMBLIES, LEFT AND RIGHT, CRACKED AFTER REMOVING MAIN GEAR SIDE BRACE STUD BRACKET, PN 75643-06. SUBMITTER REPORTED SAME PROBLEM WITH SEVERAL OTHER ARICRAFT.SDR 96ZZZX1504Rib · crackedDURING C/W AD 95-20-07, FOUND AFT RIB ASSEMBLIES, LEFT AND RIGHT, CRACKED AFTER REMOVING MAIN GEAR SIDE BRACE STUD BRACKET, PN 75643-06. SUBMITTER REPORTED SAME PROBLEM WITH SEVERAL OTHER AIRCRAFT.SDR C2XA96IA039Rib · crackedIAH - DURING C-CHECK INSPECTION, FOUND RIGHT WING NOSE RIB NR 17 WEB CRACKED AT UPPER SURFACE ATTACHMENT. MAINTENANCE REMOVED AND REPAIRED THE UPPER FLANGE WITH 'L' ANGLE PER FAX NR EST 023/96. AIRCRAFT APPROVED FOR RETURN TO SERVICE. (M)SDR UPS805406Rib · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, RT WING L/E UPPER RIBS CRACKED AT STA XFS 501. REPAIRED PER MM 57-00-00 FIG 801.SDR UPS805407Rib · crackedWHILE IN FOR C-CHECK MAINTENANCE REPORTED, LT WING L/E ASSY HAS 8 RIBS CRACKED AT STA XFS 691, 672, 666, 660, 647, 641, 635 AND 629. REPAIRED PER MM 57-00-00 FIG 801.SDR 9602409970Rib · crackedDURING M-CHECK, FOUND A CRACK IN THE LEFT WING FUEL TANK RIB TO LOWER WING ATTACH FITTING, XRS 69 AT STR 11. REPLACED FITTING PER SRM 51-30-2.SDR C2XA96IA029Rib · crackedIAH - DURING 1C CHECK INSPECTION, FOUND RIGHT WING RIB NR 19 (NOSE RIB WEB) TO BE CRACKED. MAINTENANCE INSTALLED L-PROFILE. (M)SDR AALA960097Rib · crackedTULE - FOUND CRACK IN RADIUS OF LOWER RIB CHORD WING STATION 738.5 RIGHT WING (FWD CHORD) IN FUEL TANK. STOP DRILLED BOTH ENDS OF CRACK, NDT CHECKED BOTH STOP DRILLS. INSTALLED DOUBLER PER SRM 57-10-5 PAGE NR 4. (M)SDR AALA960096Rib · crackedTULE - FOUND LOWER RIB CHORD CRACKED AT STRINGER 5 AT STATION 601.5 INSIDE RIGHT WING FUEL TANK. REMOVED RIB AND INSTALLED NEW BUILT UP RIB PER SB 727-57-0127 FOR STATION 601.5R. COVER PLATE ON ES8 1517971. (M)SDR UPS805384Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, LT WING L/E, 3 EACH, RIBS CRACKED AT STA. XFS 767, 846, 679. REPAIRED RIBS PER MM 57-00-00, FIG. 801.SDR UPS805379Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E 2 EACH RIBS CRACKED AT STA XFS138, XFS 328. REPAIRED RIBS PER MM 27-00-00, FIG. 801.SDR CAL960053Rib · crackedHOU - INSPECTION FOUND A .625 INCH CRACK IN LOWER RADIUS OF LEFT WING LEADING EDGE RIB, LOCATED OUTBOARD OF NR 8 SLAT TRACK. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 57-04. (M)SDR CAL960268Rib Web · crackedSTATION 31J - INSPECTION FOUND A 1.5 INCH CRACK IN LEFT WING LEADING EDGE RIB WEB. THE CRACK WAS STOP DRILLED. A DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 51-40-2. (M)SDR UPS805381Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA. XFS 608, 596, 871, 827, 803, 785, 779, AND 749. REPAIRED RIBS PER MM 57-00-00, FIG. 801.SDR UPS805380Ribs · crackedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED, RT WING L/E ASSY, 8 EACH, RIBS CRACKED AT STA XFS 841, 836, 817, 797, 771, 652, 620, AND 626. REPAIRED RIBS PER MM 57-00-00, FIG. 801.SDR CAL960144Rib · crackedSTATION 31J - INSPECTION FOUND TWO .5 INCH CRACKS AT THE TWO MOST AFT SCREW HOLES IN RIGHT WING LEADING EDGE RIB UPPER CHORD. THE CHORD WAS REMOVED. AN ANGLE WAS FABRICATED AND INSTALLED IAW SRM 57-20-2, 51-10-2, 51-30-2, AND MM 51-20-2. (M)SDR 96ZZZM193Rib · crackedMCI - DURING C-CHECK, FOUND A CRACK AT WS 629 RIB LOWER HOLE, STRINGER 2. STOP DRILLED PER SRM 57-10-5 AND REPAIRED PER SRM 57-10-5, FIGURE 2 AND TWA STANDARD PRACTICES. (M)SDR EISA95524Rib · crackedFOUND 1 INCH CRACK IN LEFT WING RIB NEAR LOWER FASTENER HOLE AT WS 738.5 AND FIRST STRINGER AFT OF FRONT SPAR. FABRICATED AND INSTALLED RIB DOUBLER PER SRM 57-10-05 AND 51-30-01. (M)SDR EISA95519Rib · cracksHFEC INDICATES TWO CRACKS AT LEFT WING RIB AT WS 546.5 LOWER FASTENER HOLE SECOND STRINGER FORWARD OF REAR SPAR. REPLACED RIB ASSY PER SRM 51-10-01 AND 51-30-02. (M)SDR EISA95511Rib · crackedTWO INCH CRACK IN RIGHT WING RIB NEAR LOWER FASTENER HOLE WS 656.5 AND SECOND STRINGER AFT OF FRONT SPAR. FABRICATED REPAIR CHANNEL AND INSTALLED CHANNEL AND SHIM PER SRM 53-10-5. (M)SDR EISA95508Rib · crackedRIGHT WING RIB CRACKED WHERE IT ATTACHES TO LOWER STRINGER AT WS 486.5. FABRICATED REPAIR CHANNEL AND INSTALLED PER SRM 51-10-05. (M)SDR 96ZZZM186Rib · crackedMCI - DURING C-CHECK, FOUND BOTTOM FLANGE OF RIB CRACKED ABOVE STRINGER 5, STATION 6865. STOPPED DRILLED CRACKS PER SRM 51-10-01 AND REPAIRED PER SRM 57-10-15, FIGURE 2 SHEET, 1 AND FIGURE 1, SHEET 3. (M)SDR 96ZZZM185Rib · crackedMCI - DURING C-CHECK, FOUND BOTTOM LEG OF RIB CRACKED ABOVE STRINGER 6, STATION 601.5. STOP DRILLED PER SRM 51-10-1 AND REPAIRED PER SRM 57-10-5.SDR 96ZZZM183Rib · crackedMCI - DURING C-CHECK, FOUND RIGHT WING TANK RIB CRACKED, LOWER STRINGER, 2ND STRINGER, STATION 629, FROM REAR. STOP DRILLED AND INSTALLED REPAIR PER SRM 57-10-5.SDR 95FDEA01865Rib · crackedWHILE WORKING INSP CARD 7-5710-7-2308H PT 1 NOTED CRACK INDICATIONS IN THE FWD UPPER AND LOWER HOLES OF THE 70.5 CHORD BS 760 RT. CRACK INDICATIONS IN THE FWD UPPER ARE IN THE 1 AND 6 O'CLOCK POSITION, LWR FWD HOLE IN 2 O'CLOCK POSITION. TRIMMED OUT CRACKED FSDR C2XA95IA383Rib · crackedIAH - DURING C-CHECK INSPECTION, THE LEFT WING NOSE RIB NR 20 WAS FOUND TO BE CRACKED. MAINTENANCE REMOVED AND REPLACED THE AFFECTED NOSE RIB, AND THE AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE. (M)SDR AALA952036Riblet · crackedTUL - CRACK IN LOWER ANGLE OF LEADING EDGE FORMER/RIBLET OUTBOARD OF KRUEGER FLAP ACTUATOR BAY. STOP DRILLED CRACK AND INSTALLED REINFORCING ANGLE PER SRM 57-41-11 AND ESO 30595, DATED 10-5-95. TST, 21,241.57 HOURS. CYCLES, 8,851. (X)SDR EISA95488Rib · crackedTWO CRACKS IN LEFT WING RIB WS 601.5. REPLACED RIB PER SB 727-57-0127. (M)SDR EISA95471Rib · crackedTWO CRACKS RIGHT WING INTERNAL RIB AT WS 546.50 LOWER FLANGE. INSTALLED DOUBLER PER SRM 57-10-05. (M)SDR EISA95470Rib · crackedTHREE CRACKS IN LEFT WING INTERNAL RIB AT WS 546.5. STOP DRILLED CRACKS FABRICATED DOUBLER PER SRM 57-10-5 AND INSTALLED DOUBLER PER SRM 57-10-5. (M)
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