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.

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, 51-1-2Jan 4, 2005 · N868UP · Doug DC873FSDR 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.Jan 4, 2005 · N675UP · Boeing 747123SDR 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, 5Dec 30, 2004 · N868UP · Doug DC873FSDR 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 Dec 22, 2004 · N809DH · Doug DC873FSDR 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)Dec 15, 2004 · N7892N · Cessna R172ESDR 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 Dec 14, 2004 · N602AL · Doug DC873FSDR SWAA043626Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT AND RT WINGS LOWER RIB CHORDS AT WBL 135.5, CRACKED. REPAIRED RIB CHORDS PER ER.Dec 14, 2004 · N604SW · Boeing 7373H4SDR 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)Dec 13, 2004 · N408AW · Cndair CL6002B19SDR 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)Dec 9, 2004 · N860AS · Cndair CL6002B19SDR SWAA043556Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.Dec 6, 2004 · N506SW · Boeing 7375H4SDR SWAA043555Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RIB CHORD PER ACO.Dec 6, 2004 · N506SW · Boeing 7375H4SDR 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)Nov 29, 2004 · N860AS · Cndair CL6002B19SDR 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 INov 29, 2004 · N860AS · Cndair CL6002B19SDR 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.Nov 29, 2004 · N559FE · Doug DC1010SDR 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.Nov 25, 2004 · N577FE · Doug MD11SDR 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 SNov 19, 2004 · N744UP · Doug DC871FSDR 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.Nov 19, 2004 · N744UP · Doug DC871FSDR 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.Nov 19, 2004 · N744UP · Doug DC871FSDR 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.Nov 19, 2004 · N744UP · Doug DC871FSDR 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.Nov 19, 2004 · N744UP · Doug DC871FSDR 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,Nov 18, 2004 · N744UP · Doug DC871SDR 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.Nov 18, 2004 · N744UP · Doug DC871FSDR 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.Nov 18, 2004 · N744UP · Doug DC871FSDR 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.Nov 17, 2004 · N481EV · Boeing 747132SDR 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.Nov 17, 2004 · N744UP · Doug DC871FSDR 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 REFNov 17, 2004 · N744UP · Doug DC871FSDR 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.Nov 17, 2004 · N744UP · Doug DC871FSDR 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.Nov 17, 2004 · N744UP · Doug DC871FSDR 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.Nov 16, 2004 · N453XJ · Saab 340BSDR 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. Nov 14, 2004 · N873SJ · Doug DC873FSDR SWAA043315Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING LOWER RIB CHORD AT WBL 135.5, CRACKED. REPAIRED RT WING RIB CHORD PER EA.Nov 11, 2004 · N505SW · Boeing 7375H4SDR 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 Nov 5, 2004 · N83258 · Bbavia 7ACSDR MALA040930Rib · crackedLEFT O/B LEADING EDGE HAS 2 CRACKED RIBS. RIBS WERE REPAIRED IAW MESABA EO S57026.Nov 2, 2004 · N454XJ · Saab 340BSDR SWAA043187Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT WING RIB AT WING STATION 135.5, LOWER AFT END CRACKED. REPAIRED RIB PER ER.Nov 2, 2004 · N601WN · Boeing 7373H4SDR 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 PRIMNov 1, 2004 · N873SJ · Doug DC873FSDR 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.Nov 1, 2004 · N57734 · Emb EMB120ERSDR 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.Nov 1, 2004 · N57734 · Emb EMB120ERSDR 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.Nov 1, 2004 · N57734 · Emb EMB120ERSDR 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.Oct 29, 2004 · Cessna 150LSDR 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-AOct 29, 2004 · N521UP · Boeing 747200SDR 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-Oct 28, 2004 · N825BX · Doug DC871FSDR 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.Oct 28, 2004 · N503SW · Boeing 7375H4SDR 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 DOUBOct 27, 2004 · N873SJ · Doug DC873FSDR 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 FOct 25, 2004 · N404AW · Cndair CL6002B19SDR A6WA200440162Rib · crackedBATT RIB ASSY IS CRACKED 1.2500 INCH LONG IN AFT UPPER RADIUS. CORRECTIVE ACTION IN PROGRESS.Oct 25, 2004 · N404AW · Cndair CL6002B19SDR 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.Oct 25, 2004 · N877AS · Cndair CL6002B19SDR 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.Oct 25, 2004 · N503SW · Boeing 7375H4SDR 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.Oct 22, 2004 · N397SW · Boeing 7373H4SDR 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 AOct 17, 2004 · N825BX · Doug DC871FSDR 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.Oct 11, 2004 · N449XJ · Saab 340B
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