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 UPS05843855Rib · crackedINSPECTION TYPE:C3 RIB CRACKED AT UPPER END, LT WING STA XFS 828.75. STOP DRILLED CRACK AND NDT VERIFIED PER NDT/SPM06-10-01.001. FAB DOUBLER AND FILLER FOM SHT7075T6-.050, TREATED, PRIMED & INSTALLED SAME REF SRM 57-3-0 FIG 20, 57-2-0 FIG 2, 51-1-8, 51-1-2SDR UPS05443718Rib · crackedINSPECTION TYPE:C, RT WING NR 23 O/B ARM I/B RIB O/B FACE -D- POINT AREA SUSPECT CRACK. RIB REPAIRED AS PER RS R-57-41-35223 AND EO B747-5740-21619-A.SDR UPS05843750Rib · crackedINSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB CRACKED AT XFS 847. STOP DRILLED CRACK, VERIFIED STOP DRILL REF NDTSPM06-10-01.001. FAB REPAIR DOUBLER FROM SHT7075T6-.050. INSTALLED REPAIR REF SRM 51-1-21, 51-1-20D, 51-1-8, 57-2-0 FIG 6, 57-3-3, 5SDR DHL2004809500Rib · crackedRIGHT WING CTR L/E FORMER CRACKED 0.250, STA XFS 291.000. PERFORMED STOP HOLE AND FABRICATED ANGLE DOUBLER (AL2024-T3 0.040) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND DOUBLER ANGLE IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER IAW DC8 SDR 2005FA0000696Spar · crackedWHILE REPLACING THE FLAP TRACK ASSY, A CRACK APPROX 2 INCHES IN LENGTH AND RUNNING THROUGH THE LOWER RIVET HOLES, WAS FOUND UNDER THE LT IB FLAP TRACK. PROBABLE CAUSE WAS A FLAP OVERSPEED DURING FLIGHT. (K)SDR IXXA0500101SRib · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND RT WING NR 4 STUB WING INTERNAL RIB CRACKED 3" XS 520.468. MAJOR REPAIR ACCOMPLISHED REMOVAL OF CRACKED RIB IAW DC8 SRM 51-1-20D PAGE 21 DC8 SRM 51-3-0 PG 1. FABRICATED NEW RIB IAW REPAIR SPEC NR 2003-05 DWG 9753297 SDR SWAA043626Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT AND RT WINGS LOWER RIB CHORDS AT WBL 135.5, CRACKED. REPAIRED RIB CHORDS PER ER.SDR A6WA20041213Rib · crackedFOUND RIGHT MLG WHEEL WELL BATT RIB IS CRACKED 1.5 INCHES LONG IN UPPER AFT RADIUS. REPAIRED RIGHT MLG BATTERY RIB IAW CRJ BOMBARDIER REO 601R-57-51-046 REV B. (M)SDR ASOA04999Rib · crackedDURING A C-CHECK IN MCN, THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RIGHT WHEEL WELL BATT RIB AT WS 53.60 IAW ASA EO 600-57-039A. (M)SDR SWAA043556Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.SDR SWAA043555Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.SDR ASOA04946SRib · crackedDURING AN A-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT BATT RIB ASSY AT WS 53.60 IAW EO. (K)SDR ASOA04946Rib · crackedDURING AN A-CHECK IN MCN, THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE PERFORMED A TEMPORARY REPAIR TO THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW BOMBARDIER REO 601R-57-51-195. THIS IS A TEMPORARY REPAIR ISDR 04FDEA03247Rib · crackedDURING AIRPLANE'S CONVERSION FROM P-F/ACF FOUND 2 INCH LONGERON CRACK RIB 402 LT WING AFT OF FUEL TANK FLAPPER DOOR. INSTALL REPAIR DOUBLER -3 PER SRM 57-20-00 FIG 33.SDR 04FDEA03221Rib · crackedLT WING RIB 16 INBOARD FOUND CRACKED. REMOVED AND INSTALLED AS PER SRM 51-33-01 VOL II. REFER TO WORKCARD 27X8403 FOR CABLES ADJUSTMENT.SDR UPS04843579Rib · crackedLT WING CENTER L/E RIB CRACKED AT XW429 UPPER RIB. STOP DRILLED CRACK, NDT VERIFIED TERMINATION PER SPM 06-10-01.001. FABRICATED STACKED ANGLE REPAIR DOUBLERS FROM SHT7075T6/.040 AND .050 THICK REF SRM 57-3-1 FIG 4 ITEM C, 57-2-0 FIG2. INSTALLED PARTS REF SSDR UPS04843548Rib · crackedLEFT WING CENTER L/E RIB CRACKED AT XW408. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG 1, 57-3-1 FIG 4, 51-1-8, 51-1-20D, 51-1-21.SDR UPS04843547Rib · crackedC3 LT WING CENTER L/E RIB CRACKED AT UPPER AFT END STA XW398. STOP DRILLED CRACK NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-2-0 FIG2, 57-3-1, FIG4, 57-3-1 FIG2, 51-1-8.SDR UPS04843544Rib · crackedRT WING O/B L/E RIB CRACKED NEAR XFS722.50. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE REPAIR ANGLE FROM SHT7075T6-.063 AND INSTALLED SAME REF SRM 57-3-3, 57-2-0 FIG2, 51-1-8, 51-1-21.SDR UPS04843543Rib · crackedCRACKED RIB IN LT CENTER L/E NEAR STA XW322. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR FROM SHT7075T6, .040 AND .032 THICK, AND INSTALLED SAME REF SRM 51-1-8, 57-2-0, 57-3-1.SDR UPS04843546Rib · crackedC3 RT WING CENTER L/E RIB CRACKED AT AFT END, STA XFS347. STOP DRILLED CRACK, NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR ANGLES FROM SHT7075T6 .040 AND .032 AND INSTALLED SAME REF SRM 57-3-1, 57-2-0, 51-1-8,SDR UPS04843545Rib · crackedLT WING CENTER L/E LOWER RIB CRACKED AT AFT END, STA XW408. STOP DRILLED CRACK. NDT VERIFIED REF SPM06-10-01.001. FABRICATE STACKED REPAIR DOUBLERS FROM SHT7075T6-.040 AND INSTALLED SAME REF SRM 57-3-1 FIG 4, 57-2-0, 57-3-1, 51-1-21, 51-1-20D.SDR UPS04843530Rib · crackedRT WING L/E RIB CRACKED AT XFS828.75. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 PER SRM 57-2-0 FIG 2. INSTALLED REPAIR PER SRM 57-2-0 FIG 2, 51-1-8, 57-3-1, 51-1-21, 51-1-20D.SDR EIA2004165Rib · crackedRIGHT WING L/E CAVITY RIB UPPER CORD FWD END FOUND CRACKED AT ILES 1056. L/E RIB REPLACED PER SRM 51-30-02.SDR UPS04843532Rib · crackedLT WING L/E RIB CRACKED AT STA 728 UPPER AFT END. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FABBED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D.SDR UPS04843531Rib · crackedLT WING L/E RIB CRACKED AT LOWER AND UPPER ENDS, STA835. STOP DRILLED CRACKS. NDT VERIFIED BOTH REF SPM 06-10-01.001. FABRICATED UPPER REPAIR FROM 7075T6-.050 AND FABRICATED LOWER REPAIR FROM S25972423 EXTRUSION REF SRM57-3-1, 57-2-0. INSTALLED REPAIRS REFSDR UPS04843529Rib · crackedLT WING L/E RIB CRACKED AT LOWER AFT END, STA860. STOP DRILLED CRACK. NDT VERIFIED PER SPM06-10-01.001. FAB REPAIR ANGLE FROM S25972423 EXTRUSION. INSTALLED REPAIR PER SRM 57-2-0, 51-1-8, 51-1-21D, 51-1-20D.SDR UPS04843528Rib · crackedLT WING L/E LOWER RIB CRACKED AT END, STA 753.75. STOP DRILLED CRACK, NDT VERIFIED PER SPM06-10-01.001. FABRICATED REPAIR ANGLE FROM 7075T6-.050 REF SRM 57-3-0 FIG 20. INSTALLED REPAIR REF SRM 57-3-0 FIG 20, 51-1-8, 51-1-20D.SDR MALA040828Rib · crackedDURING 6Y/4Y INSPECTION IN LAN, 512AL 5 CRACKED RIBS, MAINTENANCE REPAIRED IAW SAAB SRM 57-10-30-2. REFER TO NRC NR 218746 FOR ADDITIONAL INFORMATION. AIRCRAFT RETURNED TO SERVICE 11/18/04.SDR DHL2004873519Rib · damagedNR 1 LEFT STUB WING RIB HOLES ELONGATED, STA XS 520.168 (MAJOR REPAIR). PERFORMED MAJOR REPAIR IAW DC8 SRM 57-1-0 PG 1. REMOVED NR 1 LEFT STUB WING RIB IAW DC8 SRM 51-1-21 PG 1, DC8 SRM 51-1-20D PG 21. CLEANED, TREATED AND PRIMED AREA IAW DC8 SRM 51-1-8B. SDR SWAA043315Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RT WING RIB CHORD PER EA.SDR 2005FA0000694Rib · crackedTHE FIRST WING RIB LOCATED IB OF THE AILERONS WAS FOUND CRACKED ALONG THE RADIUS OF THE ATTACH TAB WHERE THE RIB IS SECURED TO THE AFT SPAR. THIS AIRCRAFT WAS SUBJECTED TO YEARS OF PREVAILING WINDS QUARTERING AGAINST THE T/E OF THE LT AILERON. NO GUST LOCKS SDR MALA040930Rib · crackedLEFT O/B LEADING EDGE HAS 2 CRACKED RIBS. RIBS WERE REPAIRED IAW MESABA EO S57026.SDR SWAA043187Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT WING RIB AT WING STATION 135.5, LOWER AFT END CRACKED. REPAIRED RIB PER ER.SDR DHL2004873505Rib · crackedLT OUTER OUTBOARD WING L/E FORMER CRACKED 0.500 AT XFS 885.000. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. PERFORMED STOP DRILL ON CRACK END IAW SRM 57-2-0 PG 8. FABRICATED ANGLE DOUBLER (ALCLAD 2024-T3 0.032) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMSDR SWIA200414226Rib · crackedRIGHT WING, RIB 17 FORWARD OF AUX SPAR, CLEAT IS CRACKED, IN WET BAY AREA, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED RIB IAW EMB 120 SRM 57-20-07 FIG 203 SHEET 1,2,3.SDR SWIA200414225Rib · crackedRIB 19 LEFT SIDE MOST FWD UPPER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW SRM 51-22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05.SDR SWIA200414224Rib · crackedRIB 19 LEFT SIDE MOST FORWARD LOWER CLEAT IS CRACKED. (ITEM FOUND AT C-CHECK INSPECTION.) REPLACED SHEAR CLIP IAW SRM 51-22-00, 51-25-00, 51-40-02, 51-30-01, 51-21-02, 57-20-07, 51-40-02 AND MM 20-30-05.SDR CA041110004Rib · cracked(CAN) THE RIB WAS FOUND CRACKED AROUND ONE OF THE STRENGTHENING DIMPLES OF THE RIB, ABOUT 1.5 INCHES IN LENGTH. A NEW PART WAS INSTALLED AS REQUIRED.SDR UPS04443504Rib · crackedL/E PNL SUPPORT RIB FOUND CRACKED AT WS 1420 JUST O/B OF NR 1 L/E FLAP PDU. L/E PNL SUPPORT RIB REPAIRED AS PER HX RS NR R57-41-35209 JUST AT WS 1420 O/B OF NR 1 L/E FLAP PDU. REFER UPS EO NR B747-5740-21328-ASDR IXXA060082SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING RIB WEB CRACKED AT STATION XRS6. REMOVED DAMAGE. FABRICATED DOUBLER, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR DOUBLER, AND FASTENERS AT RIGHT HAND WING STATION XRS6 IAW DC8 SRM 57-2-0, 51-1-21, 57-SDR SWAA043147Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING UPPER RIB CHORD CRACKED AT WBL 135.5, STR 2. REPAIRED RIB CHORD PER SWA EA.SDR DHL2004873500Rib · crackedLT WING CTR L/E FORMER CRACKED 0.500 AT XFS 447.750. REMOVED FASTENERS IAW SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLERS (AL 2024-T3 0.040) (2EA) IAW SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED AREA AND ANGLE DOUBLER IAW SRM 51-1-8B. INSTALLED ANGLE DOUBSDR A6WA200440163Rib · crackedRT WS 53.60 BATT RIB ASSY IS CRACKED, 1 INCH LONG IN AFT UPPER RADIUS. REPAIRED BATT RIB ASSY BY CUTTING OUT DAMAGED SECTION. FABBED REPAIR ANGLE FROM S6144-0 AND FILLER FROM 7075T62 P.O. NR 35850, INSTALLED REPAIR PARTS WET USING SOLID RIVETS AND HI-LIGHT FSDR A6WA200440162Rib · crackedBATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS.SDR ASOA04835Rib · crackedDURING A C-CHECK, THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REMOVING AND REPLACING THE RT MAIN LANDING GEAR BATT RIB ASSEMBLY AT WS 53.60 IAW EO600-57-039A.SDR SWAA043101Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RT WING RIB CHORD PER EA.SDR SWAA043067Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT WING LOWER RIB CHORD AT WING STATION 135.5, BETWEEN STRINGER 2 AND STRINGER 3, CRACKED. REPAIRED RIB CHORD PER ER.SDR IXXA060058SRib · crackedDURING ROUTINE C CHECK, FOUND LEFT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS 464.000. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PARTS AND NEW FASTENERS AT LEFT WING LEADING EDGE UPPER RIB ASDR MALA040799Rib · crackedDURING 6Y/4Y INSPECTION IN LAN, MAINTENANCE FOUND 611BR HAS 2 CRACKED RIBS. MAINTENANCE REPAIRED IAW SRM 57-10-30-2. AIRCRAFT RETURNED TO SERVICE 10/12/04.
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