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 TAOA109615Rib · crackedAD NR 94-07-08 INSPECTION OF THE LEFT SIDE BL 70.5 WING RIB UPPER CHORD REVEALED CRACKS IN THE FORWARD TWO FASTENER HOLES COMMON TO THE BS 760.95 FRAME. THE CRACK EXTENDS SLIGHTLY INTO THE HORIZONTAL FLANGE. CORROSION WAS ALSO DETECTED ON THE INNER SURFACE OOct 31, 1996 · N923TS · Boeing 727225SDR CALA9601698Rib · crackedINSPECTION FOUND A 2 INCH CRACK AT UPPER EDGE OF RT WING LEADING EDGE RIB, SLAT STA 0. THE CRACK WAS STOP DRILLED, A WEB REPAIR WAS FABRICATED AND INSTALLED IAW SRM 57-20-1.Oct 31, 1996 · N17407 · Boeing 727243SDR DHL9672009CRib · crackedAT C-CHECK, CRACK INDICATION FOUND AT LEFT WING RIB STA 656.5 AT S-2 LOWER ATTACH FASTENER HOLE OLD REPAIR. REMOVED OLD REPAIR, INSTALLED ANGLE REPAIR AT WING RIB PER SRM 57-10-5.Oct 30, 1996 · N720DH · Boeing 727228SDR DHL9672022CRib · crackedAT C-CHECK, INSPECTION FOUND CRACK AT WING RIB STA 738.5 STRINGER 2 LOWER AT ATTACH FASTENER HOLE. STOP DRILLED CRACK, HFEC STOP DRILL, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-127. ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-0127, REPAIR 7 BY 3 .Oct 29, 1996 · N720DH · Boeing 727228SDR DHL9672008CRib · crackedAT C-CHECK, FOUND CRACK AT WING RIB STA 601.5 AT S-3 LOWER FASTENER ATTACH HOLE. STOP DRILLED CRACK, HFEC OF STOP DRILL OK. ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127, ACCOMPLIHED REPAIR PER SRM 57-10-5, REPAIR 9 BY 3.125.Oct 29, 1996 · N720DH · Boeing 727228SDR CALA9700018Rib · crackedINSPECTION FOUND A 1 INCH CRACK IN FORWARD SHEAR TIE AT LT WING NR 2 MAIN TANK WS 670, UPPER STRINGER 27 AND A .5 INCH CRACK WAS FOUND AT SHEAR TIE OF RIB CHORD, LOWER STRINGER 19. THE RIB CHORD AT UPPER STRINGER 27 WAS REPAIRED IAW SB 57-2273. THE RIB CHORDOct 28, 1996 · N17025 · Boeing 747238BSDR DHL9672007CRib · crackedAT C-CHECK, INSPECTION OF LEFT WING REVEALED CRACK AT WING RIB STA 686.5 S-2 LOWER ATTACH FASTENER HOLE. STOP DRILLED CRACK, HFEC OF HOLE, ENLARGED HOLE ADDITIONAL .062 PER S/B 57-0127 AND ACCOMPLISHED REPAIR PER SRM 57-10-5 AND S/B 57-0127, REPAIR 9 BY 3.125Oct 26, 1996 · N720DH · Boeing 727228SDR DHL9672006CRib · crackedAT C-CHECK, LEFT WING INSPECTION REVEALED CRACK AT WING RIB STA 629, ATTACH FLANGE AT S-2 LOWER SIDE. STOP DRILLED CRACK, ACCOMPLISHED HFEC OF STOP HOLE, ENLARGED STOP HOLE ADDITIONAL .062 PER S/B 57-0127. INSTALLED ANGLE REPAIR PER SRM 57-10-5 AND S/B 57-0Oct 25, 1996 · N720DH · Boeing 727228SDR 96ZZZX5587Rib · crackDURING A PHASE INSPECTION, FOUND A 1.5 INCH CRACK IN RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FWD WING SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. STOP DRILLED CRACK PER CESSNA INSTRUCTIONS.Oct 25, 1996 · N81WS · Cessna 441SDR DHL9672033CRib · crackedAT C-CHECK, RIGHT WING RIB STA 629, LOWER FLANGE AT STR 6 CRACKED. STOP DRILLED CRACK, HFEC INSTALLED REPAIR PER SRM 57-10-5, 3 BY 10.Oct 24, 1996 · N720DH · Boeing 727228SDR MALA965169Rib · crackedDURING AN INSPECTION IN MSP, MAINTENANCE FOUND AT RIGHT WS 39 WING RIB FORWARD LOWER CUTOUT A .250 CRACK ON AFT SIDE AND .50 CRACK ON LOWER SIDE OF CUTOUT, P/N 27-31020. REPAIRS COMPLETED BY INSTALLATION OF A REPAIR DOUBLER PER AEROTECH DESIGNS EA01-96108 DATOct 23, 1996 · N2692P · Swrngn SA227ACSDR DHL9672032CRib · crackedAT C-CHECK, RIGHT WING RIB AT STA 686.5 HAS CRACK AT ATTACH POINT. STOP DRILLED CRACK AND PERFORMED HFEC ISNP. INSTALLED RIB REPAIR PER SRM 57-10-5, REPAIR 3 BY 10.Oct 22, 1996 · N720DH · Boeing 727228SDR DHL9672013CRib · crackedAT C-CHECK, INSPECTION REVEALED CRACK INDICATION AT WING RIB STA 601.5 AT S-2 LOWER ATTACH FASTENER HOLE. STOP DRILLED CRACK PER 57-0127. HFEC INSPECTION OF STOP HOLE, ENLARGED HOLE AN ADDITIONAL .062 PER S/B 57-0127. INSTALLED WING RIB REPAIR 10 BY 2 PER Oct 21, 1996 · N720DH · Boeing 727228SDR DHL9672011CRib · crackedAT C-CHECK, RIB CRACKED JUST FWD OF TOP CHORD FWD SPAR AT STA 349, RIGHT WING. STOP DRILLED CRACK, DYE PEN INSP. INSTALLED ANGLE REPAIR PER SRM 51-40-3, REPAIR 6 BY 1.5.Oct 21, 1996 · N720DH · Boeing 727228SDR DLL15962450Rib · crackedTHE LT WING IWS 555 RIB UPPER CAP AT STR 10 HAS A CRACK APPROX .875 INCH LENGTH. THE CRACK WAS STOP DRILLED, COLD WORKED AND EDDY CURRENT INSPECTED. REV B PROVIDES FAA APPROVAL TO ER/A.Oct 16, 1996 · N753DA · Lkheed 10113853SDR ABXA9700713Rib · crackedDURING ACCEPTANCE INSPECTION, FOUND THE OUTBOARD LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 10 CRACKED. REMOVED AND REPLACED LEADING EDGE RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Oct 14, 1996 · N964AX · Doug DC941SDR DL73E962387Rib · crackedTHE WING RIB UPPER CHORD AT RBL 70.5 AND BS 851 HAS TWO CRACKS IN THE VERTICAL FLANGE. ONE CRACK EXTENDS FROM THE AFT END OF THE PART IN THE BOTTOM FASTENER ROW. THE SECOND CRACK EXTENDS FROM THE MIDDLE OF THE AFT EDGE OF THE VERTICAL FLANGE TO THE END FASTEOct 12, 1996 · N376DL · Boeing 737247SDR MWEA96558Rib · crackedDURING D-CK, FOUND LEADING EDGE SECTION ON LT WING HAS TWO CRACKED RIBS, 6TH FROM INBD END AND MOST OUTBOARD. BOTH CRACKED AT UPPER ENDS. INSTALLED DOUBLE ANGLE REPAIR IAW SRM 57-01 FIG 2, SHEET 3.Oct 11, 1996 · N80ME · Doug DC914SDR MWEA96551Rib · crackedDURING D-CK, FOUND RT WING L/E SECTION NR 4 HAS THREE CRACKED RIBS. INSTALLED ANGLE REPAIRS IAW SRM 57-01, FIG 2.Oct 11, 1996 · N80ME · Doug DC914SDR 96ZZZM1524Rib · crackedMCI - DURING OP-16, FOUND A 1 INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB U PPER END, STATION 312. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES.Oct 11, 1996 · N959U · Doug DC982SDR 96ZZZM1521Rib · crackedMCI - DURING OP-16, FOUND A ONE INCH CRACK IN UPPER RADIUS OF RIGHT WING LE RIB AFT UPPER END, STATION 331. REPLACED LE RIB PER SRM 51-01 AND TWA STANDARD PRACTICES. (M)Oct 11, 1996 · N959U · Doug DC982SDR DHL9672043CRib · crackedAT C-CHECK, CRACKS NOTED ON RIGHT WING UPPER CHORD BL 70.5. STOP DRILLED CRACK, HFEC STOP HOLE AND HOLES COMMON TO FASTENERS. INSTALLED WING REPAIR PER S/B 57-112.Oct 8, 1996 · N720DH · Boeing 727228SDR DHL9672042CRib · crackedAT C-CHECK, HFEC ON LEFT WING RIB UPPER CHORD, CRACKS AT BL 70.5. STOP DRILLED HOLE, HFEC ON STOP HOLE AND COMMON FASTENERS HOLES, NOT CRACKS NOTED. INSTALLED PREVENTATIVE MODIFICATION PER S/B 57-0112 AND DRAWING 65-33202.Oct 8, 1996 · N720DH · Boeing 727228SDR ABXA9700714Rib · crackedDURING ACCEPTANCE INSPECTION, FOUND THE LEFT WING LEADING EDGE RIB AT SLAT TRACK NR 2 CRACKED. REMOVED AND REPLACED RIB IAW DC-9 SRM CHAPTERS 51-30-2 AND 51-30-5.Oct 8, 1996 · N964AX · Doug DC941SDR 96ZZZX5720Rib · crackedDURING A 100-HOUR INSPECTION, FOUND CRACK IN RIB/FORMER AT LOCATION LT WING STA 136.188. SUSPECT CAUSE DUE TO VIBRATION. REPLACE RIB/FORMER.Oct 8, 1996 · N4494A · Beech 58SDR 96ZZZX5718Rib · crackedDURING A 100-HOUR INSPECTION, FOUND LT WING STA 45 RIB ASSY HAS 3 CRACKS ALONG UPPER SKIN RIVET ROW ON RIB, 1 PULLED RIVET AT FORWARD LOWER CORNER ATTACH TO SPAR. RIB IS DEFORMED IN THE CENTER AREA AT RIB. AILERON TRIM CABLES WEARING HOLES IN RIB. SUSPECT COct 8, 1996 · N4494A · Beech 58SDR UPS96221522Rib · crackedINSPECTION TYPE-D, RIB AT LEFT WING STA 686 CRACKED AT LOWER STR 8 ATTACH HOLE. REPLACED RIB ASSY STA 686 PER EO B727-5710-1325 APPENDIX C.Oct 3, 1996 · N942UP · Boeing 72722CSDR EISA96189Rib · crackedDURING A SCHEDULED D-CHECK, FOUND RIGHT WING RIB CRACKED AT STATION 629. REPAIRED RIB PER SB 727-57-127. (M)Sep 28, 1996 · N313NE · Boeing 727223SDR EISA96188Rib · crackedDURING A SCHEDULED D-CHECK, FOUND LEFT WING RIB CRACKED AT STATION 601.5. REPAIRED RIB PER SB 57-127. (M)Sep 28, 1996 · N313NE · Boeing 727223SDR UPS96821348Rib · crackedINSPECTION TYPE-C/CK, LEFT WING UPPER IB RIB CRACKED AT XRS 139 BARREL NUT END IN NR 2 MAIN TANK. REMOVED UPPER CAP, SPLICED RIB CAP AND REINSTALLED FWD SECTION OF RIB CAP IAW TIMCO REO 02311.Sep 27, 1996 · N867UP · Doug DC873FSDR MALA965152Rib · crackedDURING SCHEDULED MAINTENANCE IN MSP, MECHANICS FOUND RIGHT INBOARD FLAP END COVE RIB AT WS 27.103 CRACKED IN BEND AT UPPER AFT CORNER ABOVE FLAP POT MOUNT. COMPLETED REPAIR BY INSTALLING A DOUBLER IAW AERO TECH DESIGNS EO 01-96097 DATED SEPT 27, 1996. (M)Sep 27, 1996 · N26863 · Swrngn SA227ACSDR 96ZZZX5113Rib · crackedDURING PHASE INSPECTION, FOUND 1.5 INCH CRACK IN RT WING CANTED RIB TOP CAP. CRACK STARTS AT AFT SIDE OF FORWARD SPAR AND RUNS AFT PARALLEL TO THE BEND RADIUS. STOP DRILL CRACK PER CESSNA INSTRUCTIONS.Sep 23, 1996 · N441LL · Cessna 441SDR DHL9672234CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 629.0 HAS A CRACK IN PREVIOUS REPAIR DOUBLER ON LOWER CHORD IN AREA OF STR 6. REMOVED CRACKED REPAIR AT LEFT WING, STOP DRILLED END OF CRACK, INSTALLED REPAIR AT WING RIB PER SRM 57-10-5, 9 BY 4.Sep 21, 1996 · N722DH · Boeing 727228SDR DHL9672235CRib · crackedAT C-CHECK, LEFT WING RIB AT STA 656.5 CRACKED AT LOWER CHORD AT STR 8 ATTACH BOLT AREA. STOP DRILLED END OF CRACK, INSTALLED WING RIB REPAIR PER SRM 57-10-5, 9 BY 4.Sep 19, 1996 · N722DH · Boeing 727228SDR DHL9672228CRib · crackedAT C-CHECK, RIGHT WING RIB HAS PREVIOUS REPAIR DOUBLER CRACKED AT LOWER CHORD STA 656.5 AT STR 6. REMOVED REPAIR, REAMED STOP HOLE, CONDUCTED HFEC, INSTALLED REPAIR PER SRM 57-10-5.Sep 19, 1996 · N722DH · Boeing 727228SDR DHL9672227CRib · crackedAT C-CHECK, RT WING RIB STA 686.5 HAS LOWER CHORD CRACKED AT STR 8. STOP DRILLED, HFEC AND INSTALLED REPAIR PER SRM 57-10-5, 9 BY 4.Sep 19, 1996 · N722DH · Boeing 727228SDR AALA961368Stringer · crackedTUL - FOUND TOP WING STRINGER 9 CRACKED AT RIB ATTACHMENT. REPAIRED DAMAGE AREA PER SRM 57-10-4 FIG 2, PAGE 4. (M)Sep 19, 1996 · N847AA · Boeing 727223SDR UPS96821231Rib · crackedINSPECTION TYPE-CS2, RT WING LEADING EDGE WING 3 RIBS CRACKED AT STA XFS212, XFS242 AND XFS285. REPAIRED RIBS PER MM 57-00-00 FIG 801.Sep 18, 1996 · N813UP · Doug DC873FSDR DHL9672229CRib · crackedAT C-CHECK, RIGHT WING RIB STA 629 CRACKED AT LOWER CHORD IN AREA OF STR 8 ATTACH BOLT. STOP DRILLED, HFEC AND INSTALLED DOUBLER PER SRM 57-10-5, 10.5 BY 3.5.Sep 18, 1996 · N722DH · Boeing 727228SDR DHL9672236CRib · crackedAT C-CHECK, WING RIB STA 686.5 HAS PREV REPAIR CRACKED AT LOWER CHORD STR 6. REMOVED PREVIOUS REPAIR, INSTALLED NEW REPAIR PER SRM 57-10-5, CHANNEL 8.5 BY 2.5.Sep 17, 1996 · N722DH · Boeing 727228SDR DHL9672230CRib · crackedAT C-CHECK, WING RIB STA 656.5 CRACKED AT PREVIOUS REPAIR DOUBLER AT STR 6 LOWER CHORD. REMOVED EXISTING REPAIR, INSTALLED WING REPAIR PER SRM 57-10-5, 9 BY 2.25.Sep 17, 1996 · N722DH · Boeing 727228SDR EISA96263Rib · crackedFOUND RIB CRACKED AT FORWARD SIDE OF UPPER VENT BOX AT WING STATION 686.5. INSTALLED REPAIR PER SRM 57-10-05. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96262Rib · crackedFOUND 2 CRACKS FROM FASTENER HOLES IN RIGHT WING RIB CHORD UPPER VERTICAL FLANGE WS 70.5 RT SIDE. INSTALLED REPAIR PER SB 727-57-0112. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96258Rib · crackedFOUND WING RIB CRACKED IN TWO PLACES AT RIGHT WS 629.5. INSTALLED REPAIR PER SRM 57-10-05. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96257Rib · crackedFOUND RIB CRACKED IN THREE PLACES AT LT WS 629.5. INSTALLED NEW RIB PER SB 57-017. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96256Rib · crackedFOUND WING RIB CRACKED AT RT WS 601.5. REMOVED AND REPLACED DAMAGED RIB PER SB 727-57A-159. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96255Rib · crackedFOUND WING RIB CRACKED AT RT WS 546.5. FABRICATED AND INSTALLED REPAIR CHANNEL PER 57-10-05. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96253Rib · crackedFOUND THREE CRACKS IN WING RIB AT LEFT WS 601.5. FABRICATED AND INSTALLED REPAIR PER SRM 57-10-00. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96248Rib · crackedFOUND RIGHT WING LEADING EDGE RIB CRACKED AT WS 330. FABRICATED AND INSTALLED DOUBLER PER SRM 51-30-02. (M)Sep 15, 1996 · N300NE · Boeing 72725SDR EISA96244Rib · crackedFOUND LEFT WING RIB CRACKED AT WS 656.5, 2ND LOWER STRINGER FROM REAR SPAR. INSTALLED RIB REPAIR PER SRM 57-10-05. (M)Sep 15, 1996 · N300NE · Boeing 72725
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