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 CA000824017Rib · wrong part(CAN) PART IS STAMPED WITH P/N C6W1035-S14 BUT IS NOT THIS PART. PART IS CERTIFIED BY STAN GROTEK OF BOMBARDIER ON 24-0078 FORM. WRONG PART FOR THIS PART NUMBER APPLICATION.May 25, 2000 · Dhav DHC6SDR UPS00832821Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER SPLICE PAN IS CRACKED AT XS 250. REMOVED, FABRICATED AND REPLACED SPLICE PAN IAW DWG 5769859 AND SRM 51-1-21.May 25, 2000 · N730UP · Doug DC871FSDR DHL2000801107Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .5 INCH. STOP DRILLED CRACK PER SRM 57-2-0 PG 12. FABRICATED DOUBLER (ALCLADE 2024.T3.0.50) PER SRM 57-2-0 PG 12. CLEANED, TREATED AND PRIMED PER SRM 51-1-8 B PG 1 & 2. INSTALLED DOUBLER PER SRM 57-2-0 PG 12.May 24, 2000 · N801DH · Doug DC873FSDR RRXA002672Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK ABOUT 9 INCHES LONG ON THE UPPER RIB ON THE L/E SECTION ABOVE NR 2 PYLON AT STA 250, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAMay 23, 2000 · N8084U · Doug DC871FSDR DHL2000801111Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .25 INCH AT STA XFS 631.000. STOP DRILLED PER SRM 57-2-0. FABRICATED DOUBLER PER SRM 57-2-0. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 57-2-0.May 23, 2000 · N801DH · Doug DC873FSDR DHL2000801109Rib · crackedLEFT WING LEADING EDGE RIB CRACKED .25 INCH AT STA XFS 608.000. STOP DRILLED PER SRM 57-2-0 FIG 2. FABRICATED DOUBLER PER SRM 57-2-0 FIG 2. CLEANED, TREATED AND PRIMED PER SRM 51-1-8. INSTALLED DOUBLER PER SRM 57-2-0.May 23, 2000 · N801DH · Doug DC873FSDR UPS00832814Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 366.5 AND 372.75. REPAIRED RIBS IAW SRM 57-2-0 FIG 2.May 21, 2000 · N730UP · Doug DC871FSDR UPS00832885Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E LOWER RIB IS CRACKED AT XFS 335.250. REMOVED, FABRICATED AND REPLACED RIB IAW DWG 5769530 AND SRM 51-1-20D.May 20, 2000 · N730UP · Doug DC871FSDR UPS00832818Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED BEYOND LIMITS AT XS 503.789. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 20, 2000 · N730UP · Doug DC871FSDR UPS00832886Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIB IS CRACKED AT XFS 716.25. REPAIRED RIB IAW SRM 57-2-0 FIG 2.May 18, 2000 · N730UP · Doug DC871FSDR UPS00832670Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 723.75. REPAIRED IAW SRM 57-2-0 FIG 2.May 18, 2000 · N730UP · Doug DC871FSDR UPS00832817Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XOLDI 6.225. REPAIRED IAW SRM 57-2-0 FIG 2.May 17, 2000 · N730UP · Doug DC871FSDR TWAA0008303Rib · crackedLEFT WING AFT END OF REPAIR ON LEADING EDGE RIB HAS A CRACK APPROX 1 INCH LONG XRS 350 AFT OF NUMBER 4 LEADING EDGE SLAT. STOP DRILLED AND CHECKED PER EDDY CURRENT PART 6 51-00-03 FIG 5 SHT 1. OP16 05-17-00 MCI.May 17, 2000 · N921L · Doug DC932SDR RRXA002676Nut Plate · missingDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B AT XFS 483, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM, 57-2-0 AND 51-1-21May 15, 2000 · N8084U · Doug DC871FSDR RRXA002675Rib · crackedDURING A MAINTENANCE VSIIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B AT XFS 477, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 51-1-21 AND 57-2-0.May 15, 2000 · N8084U · Doug DC871FSDR RRXA002673Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE LOWER RIB AT TRAILING EDGE I/B AT CENTER L/E AT STA XFS 467, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 5May 15, 2000 · N8084U · Doug DC871FSDR RRXA002736Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE 3RD LOWER RIB ON THE RT WING MIDDLE L/E AT STA XFS 304, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0May 12, 2000 · N8084U · Doug DC871FSDR RRXA002735Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE 4TH RIB LOWER SURFACE ON THE RT WING MIDDLE L/E AT STA XFS 310, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRMay 12, 2000 · N8084U · Doug DC871FSDR RRXA002731Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 752, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2May 12, 2000 · N8084U · Doug DC871FSDR RRXA002730Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB ON THE RT WING O/B LEADING EDGE AT STA XFS 748, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2May 12, 2000 · N8084U · Doug DC871FSDR RRXA002729Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK AT END OF UPPER RIB ON RT WING OUTBOARD L/E AT STA XFS 741, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0, 5May 12, 2000 · N8084U · Doug DC871FSDR RRXA002728Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACKED NR 12 UPPER RIB ON THE RT WING L/E MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 5May 12, 2000 · N8084U · Doug DC871FSDR RRXA002725Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 11 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR May 12, 2000 · N8084U · Doug DC871FSDR RRXA002724Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 8 UPPER RIB ON THE RT WING LEADING EDGE MIDDLE SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IMay 12, 2000 · N8084U · Doug DC871FSDR RRXA002723Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 7 UPPER RIB ON THE RT WING MIDDLE L/E AT STA XFS 407, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-7 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002722Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE NR 5 UPPER RIB ON RT WING LEADING EDGE MID SECTION AT STA XFS 408, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8May 12, 2000 · N8084U · Doug DC871FSDR RRXA002674Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE UPPER RIB AT TRAILING EDGE I/B ON CENTER L/E AT XFS 477, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-May 12, 2000 · N8084U · Doug DC871FSDR RRXA002708Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 12 RIB UPPER T/E, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-1, 57-2-0, 51May 10, 2000 · N8084U · Doug DC871FSDR RRXA002705Rib · crackedDURING A MAINTENANCE VISIT FOUND A CRACK TO THE RT WING NR 3 STUB WING NR 6 RIB UPPER END, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AND PRIMED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0, 51-1-21 ANDMay 10, 2000 · N8084U · Doug DC871FSDR RRXA001758Rib · crackedDURING A MAINTENANCE VISIT, FOUND A CRACK TO THE RIB AT THE RT STUB WING OVER NR 3 PYLON AT XFS 207.5, DAMAGE EXCEEDED LIMITATIONS IAW DC-8 SRM. REMOVED DAMAGE, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2-0.May 9, 2000 · N2674U · Doug DC873FSDR MALA000316Rib · crackedLEADING EDGE RIBS 3, 4, 5, 6 & 7 CRACKED. 611 BR REFER CELSIUS TASK CARD 6519. MX CUT ALL CRACKED SUPPORT RIBS AS MARKED, FABRICATED REPAIR ANGLE AND SHIMS. ALODINED AND PRIMED ALL BARE SURFACES. NDT PER FFUNDT006EC. NO CRACKS AFTER CUTOUT, INSTALLED REPAIMay 9, 2000 · N407XJ · Saab 340BSDR UPS00832651Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E AUX TANK RIB IS CRACKED AT XFS 13.75. REPAIRED IAW SRM 57-2-0 FIG 2.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832643Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 622.5. REPAIRED IAW SRM 57-2-0 FIG 2.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832640Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 591.25, 616.25, 635, 653.75. REPAIRED IAW SRM 57-2-0 FIG 2.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832637Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E UPPER RIBS ARE CRACKED AT XFS 697.5, 647.5, 635. REPAIRED IAW SRM 57-2-0 FIG 2.May 8, 2000 · N802UP · Doug DC873FSDR UPS00832649Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 354. REPAIRED IAW SRM 57-2-0 FIG 2.May 7, 2000 · N802UP · Doug DC873FSDR UPS00832646Rib · crackedINSPECTION TYPE:C123, LEFT WING L/E RIB IS CRACKED AT XFS 347.7. REPAIRED IAW SRM 57-2-0 FIG 2.May 7, 2000 · N802UP · Doug DC873FSDR UPS00832644Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 461.3. REPAIRED IAW SRM 57-2-0 FIG 2.May 7, 2000 · N802UP · Doug DC873FSDR UPS00832641Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 322.7. REPAIRED IAW SRM 57-2-0 FIG 2.May 7, 2000 · N802UP · Doug DC873FSDR UPS00832638Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E RIB IS CRACKED AT XFS 491.1. REPAIRED IAW SRM 57-2-0 FIG 2.May 7, 2000 · N802UP · Doug DC873FSDR UPS00832758Rib · crackedINSPECTION TYPE:C123, RIGHT WING L/E UPPER RIB IS CRACKED AT XFS 828.750. REPAIRED IAW SRM 57-2-0 FIG 2.May 5, 2000 · N802UP · Doug DC873FSDR 20000517SH013Canopy · crackedDURING A PHASE INSPECTION, FOUND A CRACK IN THE RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD WING SPAR AND RUNS AFT PARALLEL TO THE BEND LINE 1 INCH LONG. STOP DRILLED PER CESSNA INSTRUCTIONS. (X)May 5, 2000 · N555GD · Cessna 441SDR UPS00832604Rib · chafedINSPECTION TYPE:C2, RIGHT WING L/E RIB HAS HOLE CHAFED IN IT AT XS 503.379. REPAIRED IAW SRM 57-2-0 FIG 2.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832568Rib · crackedINSPECTION TYPE:C-2, LEFT WING LEADING EDGE LWR RIB CRACKED STA XFS 360.250. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED ANGLE DOUBLER IAW SRM 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832567Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E UPPER RIB CRACKED STA XS 467.233. STOP DRILLED CRACKED IAW SRM 57-2-0 FIG 2. FAB AND INSTALLED REPAIR DOUBLER IAW SRM 51-1-21 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832563Rib · crackedINSPECTION TYPE:C-2, LEFT WING LEADING EDGE THE I/B UPPER RIB CRACKED STA XS 520.1. STOP DRILLED CRACKED IAW SRM 57-2-0. FAB AND INSTALLED REPAIR ANGLES IAW 51-1-20 & 57-2-0 FIG 2.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832560Rib · crackedINSPECTION TYPE:C-2, RIGHT WING L/E AT STA XOLDI 6.225 THE LWR RIB CRACKED. STOP DRILLED CRACK IAW SRM 57-2-0. FAB AND INSTALLED 2 REPAIR DOUBLERS IAW SRM 51-1-11, 57-3-1 & 51-1-20D.Apr 25, 2000 · N700UP · Doug DC871FSDR UPS00832538Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIB IS CRACKED AT STA XFS 385.00. STOP DRILLED CRACK AND REPAIRED IAW SRM 57-2-0 FIG 2.Apr 22, 2000 · N700UP · Doug DC871FSDR UPS00832537Rib · crackedINSPECTION TYPE:C2, RT WING L/E RIBS ARE CRACKED AT STA XFS 283.00 AND XFS 401.00. STOP DRILLED CRACK AND REPAIRED BOTH RIBS IAW SRM 57-2-0 FIG 2.Apr 22, 2000 · N700UP · Doug DC871FSDR EIAA2000105Fitting · crackedHAECO-HKG - C6/D-CHECK - RIGHT WING WS 669.5 RIB INBD STRUT FITTING MOST UPPER FASTENER HOLES 2 EACH FOUND CRACKED. SUPPORT FITTING REPLACED PER BSB 747-54A2159 REV 2 FIG 45 AND EIA EO 57-747-1386-94 REV F. (X)Apr 21, 2000 · N482EV · Boeing 747212B
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