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 UPS04843456Rib · crackedINSPECTION TYPE: C3, RIGHT CENTER L/E RIB (LOWER) CRACKED AT XFS 335. FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW DC-8 SRM 57-3-0 AND 51-1-20D.Oct 11, 2004 · N755UP · Doug DC873FSDR UPS04843455Rib · crackedINSPECTION TYPE:C3, RIGHT WING O/B LEADING EDGE UPPER RIB IS CRACKED AT XFS 753.750. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-21 & 51-20D.Oct 10, 2004 · N755UP · Doug DC871FSDR UPS04843454Rib · crackedINSPECTION TYPE:C3, RIGHT WING CENTER L/E INTERNAL DOUBLER AND L/E SKIN IS CRACKED AT DRAIN HOLE XFS 335.250. REMOVED INTERNAL DOUBLER AND STOP DRILLED 2 CRACKS IAW DC-8 SRM 51-1-21 & 57-2-0 FIG 6. REMOVED, FABRICATED AND INSTALLED EXTERNAL IAW 51-1-20D, 51-Oct 10, 2004 · N755UP · Doug DC871FSDR UPS04843453Rib · crackedINSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB IS CHAFED THROUGHT AT XS 515-720. BLENDED CHAFED AREA IAW DC-8 SRM 57-2-0 FIG 2. FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2, 57-3-1 & 51-1-20D.Oct 10, 2004 · N755UP · Doug DC871FSDR UPS04843452Rib · crackedINSPECTION TYPE: C3, RIGHT WING O/B L/E RIB IS CRACKED WITH CORROSION AT XFS 772.500. REMOVED FASTENERS AND CORROSION IAW DD-8 SRM 51-1-21 & 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-3-0 FIG 19 & 57-2-0 FIG 2.Oct 10, 2004 · N755UP · Doug DC871FSDR UPS04843448Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE TWO LOWER RIBS CRACKED AT XFS 622.500 AND XSF 616.250. INSTALLED REPAIR DOUBLERS ON TWO RIBS AT XFS 622.500 AND XSF 616.250 IAW SRM 57-3-2 FIG 6 SHEET 2.Oct 10, 2004 · N755UP · Doug DC871FSDR SWAA042940Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING TANK UPPER RIB CHORD AT WING STATION 114, STRINGER 1, CRACKED. REPAIRED RIB PER ER.Oct 10, 2004 · N396SW · Boeing 7373H4SDR IXXA060091SRib · crackedDURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 404. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT STATOct 5, 2004 · N825BX · Doug DC871FSDR IXXA060090SRib · crackedDURING ROUTINE C-CHECK, FOUND RIGHT WING LEADING EDGE CAVITY RIB CRACKED AT STATION XFS 397.75. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RIGHT WING LEADING EDGE CAVITY AT SOct 5, 2004 · N825BX · Doug DC871FSDR IXXA060095SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT WING TRAILING EDGE UPPER RIB CRACKED AT STATION XW65. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED RIB. FABRICATED NEW RIB. LOCATED, DRILLED TRIMMED, TREATED, PRIMED, INSTALLED NEW RIB AND FASTENERS AT RIGHT WING TRAILINOct 4, 2004 · N825BX · Doug DC871FSDR IXXA060096SRib · crackedDURING ROUTINE C-CHECK, FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS360. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS360. IAW SRM 57-2-0,Oct 3, 2004 · N825BX · Doug DC871FSDR IXXA060012SRib · crackedDURING ROUTINE C CHECK, FOUND RIGHT HAND WING LEADING EDGE CAVITY AT STATION XFS410.25 AND 416.500 UPPER RIBS CRACKED. REMOVED NEEDED FASTENERS. REMOVED DAMAGE. FABRICATED REPAIR PARTS, LOCATED, TRIMMED, TREATED, PRIMED, AND INSTALLED REPAIR PARTS AND NEW FOct 3, 2004 · N825BX · Doug DC871FSDR IXXA060102SWeb · crackedDURING ROUTINE C-CHECK FOUND RT WING LEADING EDGE UPPER WEB CRACKED AT STATION XFS610. REMOVED FASTENERS AS NEEDED TO REMOVE DAMAGED WEB. FABRICATED NEW WEB, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED NEW WEB AND NEW FASTENERS AT RT WING UPPER LEADIOct 2, 2004 · N825BX · Doug DC871FSDR IXXA060100SRib · crackedDURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS735. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS735. IAW SRM 57-2Oct 2, 2004 · N825BX · Doug DC871FSDR IXXA060099SRib · crackedDURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS722.500. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TRIMMED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING UPPER LEADING EDGE STATION XFS722.Oct 2, 2004 · N825BX · Doug DC871FSDR IXXA060098SRib · crackedDURING ROUTINE C CHECK FOUND RT WING LEADING EDGE UPPER RIB CRACKED AT STATION XFS672. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LOWER LEADING EDGE STATION XFS672. IAW SRM 57-2Oct 2, 2004 · N825BX · Doug DC871FSDR IXXA060097SRib · crackedDURING ROUTINE C CHECK FOUND RT WING LEADING EDGE LOWER RIB CRACKED AT STATION XFS635. REMOVED DAMAGE. FABRICATED REPAIR PART, LOCATED, DRILLED, TREATED, PRIMED, INSTALLED REPAIR PART AND NEW FASTENERS AT RT WING LEADING EDGE STATION XFS635. IAW SRM 57-2-0, 5Oct 2, 2004 · N825BX · Doug DC871FSDR IXXA0500037SRib · crackedDURING A ROUTINE C CHECK INSPECTION, FOUND LT STUB WING NR 1 STRUCTURE RIB WITH CRACK DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED CRACKED RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED ARESep 27, 2004 · N606AL · Doug DC873FSDR UPS04443381Rib · crackedINSPECTION TYPE: C, LEFT WING: CTR WING L/E SUPPORT RIB FOUND CRACKED AT ILES 964.55 AS MARKED. LEFT WING CTR WING L/E SUPPORT RIB AT ILES 964.55 REPLACED AS PER SRM 51-10-01 PG 8.Sep 24, 2004 · N681UP · Boeing 747121SDR UPS04443331Rib · crackedINSPECTION TYPE: C, RT WING L/E NR 17 VC FLAP O/B ARM O/B ROTARY ACTUATOR SUPPORT RIB AT ILES 764 APP. FOUND UPPER CHORD MID SPAN AREA CRACK AS MARKED. L/E RIB REPAIRED AT ILES 764 AS PER SRM 57-20-03 FIG 3.Sep 24, 2004 · N681UP · Boeing 747121SDR UPS04443380Rib · crackedINSPECTION TYPE: C, RIGHT WING L/E OLES 1421 NR 25 VC FLAP I/B ROTARY O/B SUPPORT RIB FWD MOUNT HOLE CRACKED. SUPPORT RIB REPLACED AS PER SRM 51-10-01 PG 8. NR 25 VC FLAP REF MM 27-81-02 RIGGING & OPERATION CHECK CUTOUT PER MM 27-81-00.Sep 23, 2004 · N681UP · Boeing 747121SDR UPS04443377Rib · crackedINSPECTION TYPE-C, RT WING L/E OLES 1453 NR25 VC FLAP OB ROTARY IB SUPPORT RIB FWD MOUNT HOLE CRACKED. RT WING L/E OLES NR25 VC FLAP OB ROTARY ACTUATOR IB SUPPORT RIB REPAIRED IAW HX RSNR R-57-41-35205, DVI THE AFFECTED AREA AT C- CHECK INTERVALS NOT TO EXCESep 23, 2004 · N681UP · Boeing 747121SDR IXXA0500035SRib · wornDURING A ROUTINE C CHECK INSPECTION, FOUND RT STUB WING NR 4 STRUCTURE RIB WEAR DAMAGE AT STA XS 520.000. REPAIR ACCOMPLISHED, REMOVED WORN RIB. FABRICATED RIB AND PERFORMED HEAT TREATMENT. PERFORMED NDT INSPECTION. CLEANED, TREATED AND PRIMED. INSTALLED Sep 22, 2004 · N606AL · Doug DC873FSDR UPS04443354Rib · crackedINSPECTION TYPE: C, RIGHT WING L/E OLES 1409 APPROX NR 25 V/C FLAP I/B ROTARY I/B SUPPORT RIB FWD MOUNT HOLE CRACK. RIGHT WING L/E OLES 1409 APPROX NR 25 VC FLAP I/B ROTARY ACTUATOR I/B SUPPORT RIB REPAIRED AS PER HX RS R-57-41-35202, DVI THE AFFECTED AREA ATSep 21, 2004 · N681UP · Boeing 747121SDR USAA040635Rib · crackedPIT - FOUND RIB CRACKED .5 INCH, RIGHT WING AT RIB STATION 135.5, LOWER CHORD. DOUBLER INSTALLED PER EA 79058. (M)Sep 19, 2004 · N514AU · Boeing 7373B7SDR UPS04243199Rib · corrodedINSPECTION TYPE: C, EXFOLIATION CORROSION FOUND ON FIXED WING L/E RIB LOWER CHORDS AT LES 236.217 AND LES 243.977. REMOVED CHORDS ON ABOVE AREA IAW SRM 51-30-02. FABRICATED AND INSTALLED CHORDS ON ABOVE AREA IAW BOEING DRAWING NR 65-16269.Sep 17, 2004 · N938UP · Boeing 727173CSDR UPS04843252Rib · chafedINSPECTION TYPE: C3, RT WING I/B STUB WING RIB XILD 42 HAS A DEEP CHAFF. REMOVED DAMAGED AREA. NDT VERIFIED NO CRACKS NOTED AROUND CUTOUT. FABRICATED REPAIR ANGLES (2 EA) & FILLER AND INSTALLED IAW DC-8 SRM 57-2- 0.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843229Rib · crackedINSPECTION TYPE: C3, WING LT LEADING EDGE AT STA XFS 672.500 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843227Rib · crackedINSPECTION TYPE:C3 WING LEFT L/E RIB IS CRACKED AT STA 785. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843225Rib · crackedINSPECTION TYPE:C3, WING LT OUTBOARD LEADING EDGE AT STA 778.250 APROX RIB CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843224Rib · crackedINSPECTION TYPE:C3 WING LT LEADING EDGE AT STA 735 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED SHIM & REPAIR DOUBLER AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843223Rib · crackedINSPECTION TYPE:C3 UPPER RIB CRACKED IN LT CENTER L/E ABOVE OPENING FOR PANEL 520B. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED TWO REPAIR DOUBLERS AND INSTALLED IAW DC-8 SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843148Rib · crackedC3 RT WING NR 4 STUB WING HAS TWO RIBS CRACKED ABOVE NR 4 PYLON FOOT STOOL. STOP DRILLED ONE CRACK AND CUT OUT ONE CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK AND NO CRACKS NOTED AT CUT OUT. FABRICATED REPAIR ANGLES AND INSTALLED IAW SRM 57-2-0 FIG 2Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843147Rib · crackedC3 WING RT L/E AT STA XFS 335.250 DRAIN HOLE DOUBLER IS CRACKED. NDT VERIFIED CRACK IS APPROX. .3750 INCH LONG. REMOVED INTERNAL DOUBLER ON RT WING L/E, FABRICATED REPLACEMENT DOUBLER IAW DWG 5769589-27. INSTALLED REPLACEMENT DOUBLER ON RT L/E AT STA XFS 335.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843145Rib · crackedC3 WING RT L/E AT APPROX. STA XFS 465 HAS CRACKED RIB. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLER AND INSTALLED IAW SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843144Rib · crackedC3 LT WING L/E AT STA. XFS 716.250 RIB IS CRACKED. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND INSTALLED IAW SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843143Rib · crackedC3 WING LT L/E RIB IS CRACKED AT STA XFS 816.250. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843142Rib · crackedINSPECTION TYPE: C3, WING LT L/E AT STA XFS 578 RIB IS CRACKED. NDT VERIFIED CRACK .5 INCH LONG. STOP DRILLED CRACK. NDT VERIFIED CRACK TERMINATES AT STOP DRILL. FABRICATED REPAIR ANGLE AND SHIM AND INSTALLED IAW SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843139Rib · crackedC3 WING LT L/E AT STA. XFS 591.250 RIB IS CRACKED. REPAIRED LT WING L/E RIB AT STA. XFS 591.250 IAW SRM 57-2-0 FIG 2.Sep 9, 2004 · N772UP · Doug DC871FSDR UPS04843228Rib · crackedINSPECTION TYPE:C3 CRACKED RIB AT APPROX STA XFS 728 RIGHT WING LEADING EDGE. REMOVED PREVIOUS REPAIR AND TRIMMED OUT CRACK. NDT VERIFIED NO CRACKS NOTED AT TRIM OUT. REINSTALLED REPAIR PARTS IAW DC-8 SRM 51-1-21 AND 51-1-20D.Sep 8, 2004 · N772UP · Doug DC871FSDR UPS04843146Rib · crackedC3 RT WING MID L/E XFS 335 UPPER RIB IS CRACKED AT AFT END. STOP DRILLED CRACK. NDT VERIFIED STOP DRILL TERMINATES CRACK. FABRICATED REPAIR ANGLE DOUBLERS AND INSTALLED IAW SRM 57-2-0 FIG 2.Sep 8, 2004 · N772UP · Doug DC871FSDR DHL2004801504Rib · crackedLT WING CTR L/E UPPER FORMER CRACKED 1.000, STA XFS 354.000. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALSep 1, 2004 · N801DH · Doug DC873FSDR DHL2004801502Rib · crackedRT WING CTR L/E UPPER FORMER CRACKED 0.500, STA. XFS 435.789. REMOVED FASTENERS IAW DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.040) IAW DC8 SRM 57-2-0 PG 10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED ANGLE DOUBLER AND NEWSep 1, 2004 · N801DH · Doug DC873FSDR DHL2004801503Rib · crackedRT WING CTR L/E UPPER FORMER CRACKED 0.500, STA XFS 360.250. REMOVED FASTENERS IAW DC8 SRM 51-1-20D PG 21, DC8 SRM 51-1-21 PG 1. FABRICATED ANGLE DOUBLER (AL 2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALSep 1, 2004 · N801DH · Doug DC873FSDR DHL2004801501Rib · crackedLEFT INNER WING OUTBOARD L/E FORMER CRACKED 0.750, STA XFS 703.750. PERFORMED STOP HOLE AND FABRICATED (2EA) REINFORCING ANGLES (AL2024-T3 0.032) IAW DC8 SRM 57-2-0 PG 9-10. CLEANED, TREATED AND PRIMED IAW DC8 SRM 51-1-8B. INSTALLED REINFORCING ANGLES IAW DAug 28, 2004 · N801DH · Doug DC873FSDR SWAA042485Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LT WING LOWER RIB AT WBL 135.5, CRACKED. REPAIRED LT WING RIB CHORD PER SB, ERO.Aug 26, 2004 · N350SW · Boeing 7373H4SDR ASOA04645Rib · crackedDURING A C-CHECK IN MCN, THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 WERE FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE LEFT AND RIGHT WHEEL WELL BATT RIB ASSEMBLIES AT WS 53.60 IAW ASA EO 600-57-039A. (M)Aug 25, 2004 · N857AS · Cndair CL6002B19SDR 04FDEA02556Rib · crackedLEFT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT LEFT HAND WING LEADING EDGE NR 16 SLAT TRACK AREA AS PER SRM 51-33-01 VOL II.Aug 24, 2004 · N593FE · Doug MD11FSDR 04FDEA02555Rib · crackedRIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK RIB FOUND CRACK. REMOVED CRACKED RIB AS PER SRM 51-31-01 VOL II AND INSTALLED NEW RIB AT RIGHT HAND WING LEADING EDGE NR 16 SLAT TRACK AS PER DRAWING ARB7565 AND SRM 51-33-01 VOL II.Aug 24, 2004 · N593FE · Doug MD11FSDR SWAA042450Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND LEFT WING RIB LOWER CHORD CRACKED AT WBL 135.5. REPAIRED RIB PER SWA EA.Aug 24, 2004 · N351SW · Boeing 7373H4
Back to JASC 5712