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"

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SDR USAA050802Rib · gougedCLT - C4 - RIB, 4 INCHES X .5 INCH, GOUGE, RT WING, WBL 417 JUST OB OF OB FOREFLAP. CUTOUT DAMAGE AND INSTALLED DOUBLER IAW EA. (K)Jun 27, 2005 · N421US · Boeing 737401SDR UPS05844901Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 671. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873FSDR UPS05844900Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 721. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLE IAW DC-8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873FSDR UPS05844899Rib · crackedINSPECTION TYPE C-1, RT WING L/E UPPER RIB CRACKED AT XFS 734. STOP DRILL CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE DOUBLER IAW DC -8 SRM 57-2-0 FIG 2 AND 57-3-3 FIG 7.Jun 27, 2005 · N851UP · Doug DC873FSDR UPS05844892Rib · crackedINSPECTION TYPE C-1, RT WING UPPER L/E RIB CRACKED 0.5 IN LONG AT XFS 584. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLES IAW DC-8 SRM 57-2-0 FIG 2.Jun 25, 2005 · N851UP · Doug DC873FSDR VTZA200500123Rib · crackedLT BATTERY RIB CRACKED.Jun 23, 2005 · N642BR · Cndair CL6002B19SDR VTZA200500120Rib · crackedRT BATTERY RIB CRACKED BETWEEN ATTACHING FASTENERS.Jun 23, 2005 · N642BR · Cndair CL6002B19SDR ASAA0510170Rib · wornYXX - FOUND LEFT WING RIB BETWEEN AILERON AND FORE FLAP T/E ANGLE SUPPORT CHANNEL HAS WEAR DAMAGE. REMOVED AND REPLACED SUPPORT ANGLE IAW B737-200 SRM. (M)Jun 14, 2005 · N742AS · Boeing 737290CSDR VTZA200500112Rib · crackedLEFT BATT RIB IS CRACKED 1.5 INCH.Jun 13, 2005 · N628BR · Cndair CL6002B19SDR VTZA200500114Rib · crackedRIGHT BATT RIB IS CRACKED .750 INCH BETWEEN THE ATTACHING FASTENERS.Jun 13, 2005 · N628BR · Cndair CL6002B19SDR SWAA051719Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SRM & SWA TASKCARD.Jun 12, 2005 · N508SW · Boeing 7375H4SDR SWAA051647Rib · crackedDURING SCHEDULED D-CHECK, FOUND LT WING RIB UPPER FLANGE CRACKED AT WS 453, STR 12. REMOVED AND REPLACED RIB PER SRM.Jun 5, 2005 · N311SW · Boeing 7373H4SDR SWAA051646Rib · crackedDURING SCHEDULED D-CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER BFG ER.Jun 5, 2005 · N311SW · Boeing 7373H4SDR ASOA05531Rib · crackedDURING A C-CHECK IN HOT, THE RIGHT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RIGHT BATTERY RIB ASSEMBLY AT WS 53.60 IAW ASA EO 600-57-039A. (M)Jun 4, 2005 · N909EV · Cndair CL6002B19SDR VTZA200500106Rib · crackedRT BATTERY RIB CRACKED .750 IN. BETWEEN ATTACHING FASTENERS.Jun 4, 2005 · N627BR · Cndair CL6002B19SDR VTZA200500105Rib · crackedLT BATTERY RIB CRACKED.Jun 4, 2005 · N627BR · Cndair CL6002B19SDR ASOA05486Rib · crackedDURING A C-CHECK, THE RT BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE IS REPAIRING THE RT BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)Jun 2, 2005 · N850AS · Cndair CL6002B19SDR UPS05844700Rib · crackedLT WING CENTER L/E AT XFS 335 RIB CRACKED ON L/E LOWER SURFACE. STOP DRILLED CRACK. FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-20D, AND 51-1-21.Jun 1, 2005 · N840UP · Doug DC873FSDR COMA0560322Rib · crackedLT AND RT BATT RIB CRACKED. REPAIRED I/A/W REO 601R-57-51-046 AND REO 601R-57-51-211.Jun 1, 2005 · N932CA · Cndair CL6002B19SDR VTZA200500089Rib · crackedRT BATT RIB IS CRACKED .750 INCH BETWEEN ATTACHING FASTENERS.May 26, 2005 · N659BR · Cndair CL6002B19SDR VTZA200500088Rib · crackedLT BATT RIB IS CRACKED 1.5 INCH.May 26, 2005 · N659BR · Cndair CL6002B19SDR UPS05844697Rib · chafedRT CENTER WING L/E RIB CHAFED THROUGH AROUND PNEUMATIC DUCT SUPPORT ROD CONNECTION AT XFS 513. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57 -2-0 FIG 2 AND 51-1-20D.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844696Rib · crackedRT CENTER WING L/E PNEUMATIC DUCT ATTACH POINT UPPER RIB CRACKED 3 INCH LONG AT XFS 304. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR IAW DC-8 SRM 57-2 -0 FIG 2, 51-1-15, AND 51-1-20D.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844573Rib · crackedINSPECTION TYPE:C3 RIGHT WING CENTER L/E UPPER RIB CRACKED AT XFS 454. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844572Rib · crackedINSPECTION TYPE:C3 RIGHT WING O/B LEADING EDGE LWR RIB CRACKED AT XFS 623.500. CRACK TERMINATES AT FASTENER HOLE, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844566Rib · crackedINSPECTION TYPE:C3 RIGHT CENTER WING L/E LWR RIB CRACKED AT XFS 304. CUT OUT DAMAGED AREA, FABRICATED, AND INSTALLED REPAIR FILLER & ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844565Rib · crackedINSPECTION TYPE:C3, RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 495. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844564Rib · crackedINSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 416. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844560Rib · crackedINSPECTION TYPE:C3 RT CENTER WING L/E UPPER RIB CRACKED AT XFS 297. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844558Rib · crackedINSPECTION TYPE:C3 RIGHT CENTER WING L/E UPPER RIB CRACKED AT XFS 291. CRACK TERMINATES AT FASTENER HOLE. FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 25, 2005 · N840UP · Doug DC873FSDR UPS05844563Rib · crackedINSPECTION TYPE:C3, RIGHT OUTBOARD L/E LWR RIB CRACKED AT XFS 822.500. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844557Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE UPPER RIB CRACKED AT XFS 603.750. STOP DRILLED CRACK, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 57-2-0 FIG 2 AND 51-1-20D.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844556Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 609. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844555Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 778. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844554Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 772.250. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844553Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE LWR RIB CRACKED AT XFS 660. STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR UPS05844552Rib · crackedINSPECTION TYPE:C3 RIGHT O/B LEADING EDGE RIB CRACKED AT XFS 678.750 (LOWER RIB). STOP DRILLED CRACK, FABRICATED REPAIR ANGLE, AND INSTALLED REPAIR ANGLE IAW DC-8 SRM 57-2-0 FIG 2, 51-1-20D, AND 51-1-21.May 24, 2005 · N840UP · Doug DC873FSDR SWIA200515778Rib · crackedLEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF LEFT BAT RIB IAW REO 601R-57-51-046.May 23, 2005 · N409SW · Cndair CL6002B19SDR SWIA200515777Rib · crackedLEFT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. RIB INSTALLED IAW CRJ200 SRM 51-42-21 AND 51-25-16.May 23, 2005 · N409SW · Cndair CL6002B19SDR SWIA200515776Rib · crackedRIGHT BAT RIB CRACKED ITEM FOUND AT C-CHECK INSPECTION. INSTALLED REPAIR OF RIGHT BAT RIB IAW REO 601R-57-51-046 AND REO 601R-57-51-217.May 23, 2005 · N409SW · Cndair CL6002B19SDR SWIA200515775Rib · crackedRIGHT BAT RIB CRACKED, ITEM FOUND AT C-CHECK INSPECTION. INSTALLED NEW RIB AT RIGHT BAT IAW SRM 51-42-21.May 23, 2005 · N409SW · Cndair CL6002B19SDR SWAA051504Rib · crackedDURING SCHEDULED 1/2D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 & STR 3. REPAIRED RIB PER SWA ACO.May 23, 2005 · N353SW · Boeing 7373H4SDR UPS05444656Rib · crackedINSPECTION TYPE:C RIGHT WING BS 1241 UPPER REAR SPAR SPLICE BOLT HOLE NR 9 FOUND CRACKED AT RIB CHORD (CRACK LENGTH 0.040 INCH). HOLE REWORKED AS PER EO B747-5740-17032-C.May 19, 2005 · N677UP · Boeing 747123FSDR 05FDEA01308Rib · crackedRT WING LEADING EDGE SLAT TRACK NR 16 INBOARD RIB FOUND CRACKED. CRACKED RIB REMOVED AND REPLACED AS PER SRM 51-33-01 AND SRM 51-35-01 VOLUME II. THIS REPAIR CLASSIFIED AS MAJOR REPAIR AS PER GMM 6-2-100.May 16, 2005 · N580FE · Doug MD11SDR UPS05444660Rib · crackedINSPECTION TYPE:C RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLES FOUND CRACKED (CRACK LENGTH 1 INCH). RT WING NR 19 VC FLAP I/B ARM O/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307. DETAIL VISUAL INSPECMay 14, 2005 · N677UP · Boeing 747123FSDR UPS05444659Rib · crackedINSPECTION TYPE:C LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE FASTENER HOLE CRACKED (CRACK LENGTH 1 INCH). LT WING NR 7 VC FLAP O/B ARM I/B SUPPORT RIB FWD VERTICAL FLANGE REPAIRED AS PER HX RS R57-41-35307 DETAIL VISUAL INSPECT AT 6 MONTMay 14, 2005 · N677UP · Boeing 747123FSDR UPS05444658Rib · crackedINSPECTION TYPE:C LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B FACE D-HOLE CRACKED. (CRACK LENGTH .5 INCH). LT WING NR 5 VC FLAP O/B ARM O/B SUPPORT RIB I/B AREA REPAIRED AS PER HX RS R57-41-35308 DETAIL VISUAL INSPECT AT EALIER OF C-CHECK OR 18 MONTH INMay 14, 2005 · N677UP · Boeing 747123FSDR UPS05444582Rib · crackedINSP TYPE: C, LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD CRACKED REVEALED AT WBL 445.8 INCHES FWD OF I/B AILERON I/B EDGE (CRACK LENGTH 0.5 INCH). LT WING UPPER T/E PANEL SUPPORT RIB UPPER CHORD REPLACED AS PER SRM 51-10-01 PG 9.May 14, 2005 · N677UP · Boeing 747123FSDR EIA2005122Rib · crackedLT WING SURGE TANK WS 1516, RIB LOWER CHORD AT STRINGER 6 AREA FOUND CRACKED AS MARKED. LT WING SURGE TANK, WS 1516 RIB LOWER CHORD REPLACED AT STRINGER 6 AREA PER SRM 57-10-05, FIG 4.May 13, 2005 · N482EV · Boeing 747212BSDR ASOA05473Rib · crackedDURING A C-CHECK, THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 WAS FOUND TO BE CRACKED BEYOND LIMITS. MAINTENANCE REPAIRED THE RT MAIN LANDING GEAR WHEEL WELL BATT RIB ASSEMBLY AT WS 53.60 IAW EO. (K)May 11, 2005 · N829AS · Cndair CL6002B19
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