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 DHL2002720508Rib · crackedDURING "C" CHECK, RT WING INTERIOR RIB W.S. 601 LWR. CHORD ST-6 CRACK. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228SDR DHL2002720506Rib · crackedDURING "C" CHECK, RT WING INTERIOR RIB WS 686.5 BS 8 LOWER CHORD PREVIOUS REPAIR CRACK BEYOND STOP HOLE. REPAIRED IAW SRM.Oct 13, 2002 · N720DH · Boeing 727228SDR DHL2002803545Rib · crackedLT WING OUTBD LE FORMER AT STA XRS 597.000 WITH 1/2 INCH CRACK IN IT. STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED RE-INFORCING ANGLE IAW SRM 57-2-0 PG 9-10 CLEANED , TREATED AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9Sep 29, 2002 · N803DH · Doug DC873SDR UPS02839691Rib · crackedINSPECTION TYPE:C2 RT WING LE UPPER RIB IS CRACKED AT XFS 797.5. STOP DRILLED CRACK, NDT VERIFIED CRACK IS TERMINATED AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER I.A.W. SRM. 57-2-0 FIG. 2Sep 29, 2002 · N729UP · Doug DC871FSDR SWAA022216Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING RIB LOWER CHORD CRACKED AT WBL 135.5, BETWEEN STR 2 AND STR 3. REPAIRED RIB LOWER CHORD PER BFG ER.Sep 21, 2002 · N367SW · Boeing 7373H4SDR UIEA200200041Rib · crackedDURING CURRENT C CHECK, FOUND LT WING LEADING EDGE RIB CRACKED, WING STATION ILES1024 AT THE VERTICAL STIFFENER COMMON TO THE UP STOP INTERCOSTAL. DAMAGED AREA TRIMMED OUT. HFEC INSPECTED TRIMMED AREA. NO ADDITIONAL CRACKING FOUND. FABRICATED REPAIR DOUBLESep 20, 2002 · N509MC · Boeing 747230BSDR MWEA020571Rib · tornAFT END OF XCW 42 RIBS IS TORN ABOUT MIDWAY UPPER WEB. FABRICATED FILLER AND REPAIRED DOUBLER, LOCATED AND DRILLED FILLER AND DOUBLER, INSTALLED FILLER AND DOUBLER.Sep 20, 2002 · N900ME · Doug DC915SDR GAIA020129STRib · crackedDURING A LTC INSPECTION, IT WAS DISCOVERED THAT THE RIB CHORD AT FUSELAGE BS 760.95 LEFT WAS CRACKED AT THE FIRST TWO FORWARD HOLES. ACCOMPLISHED REPAIR IAW BOEING 727 SERVICE BULLETIN 727-57-0112, REV 4. THE AIRCRAFT WAS RETURNED TO SERVICE. (M)Sep 19, 2002 · N279US · Boeing 727251SDR ASAA0240101Rib · crackedDURING CHECK FOUND RIB CRACKED AT WBL 135.5 AND BETWEEN STR 2 AND 3. REPAIRED IAW SRM AND EA.Sep 16, 2002 · N786AS · Boeing 7374S3SDR QXEA0201575Rib · crackedCKB-RIGHT HAND CENTER WING LEADING EDGE END RIBS HAS CRACKS ON AFT ENDS. REPAIRED IAW HORIZON AIR EA 6-57-57 AND WVAC EO DH8S-57-0568.Sep 12, 2002 · N406QX · Bombdr DHC8401SDR QXEA0201576Rib · crackedCKB-LEFT HAND CENTER WING LEADING EDGE RIB ENDS ARE CRACKED. REPAIRED IAW HORIZON AIR EA 6-57-57 AND WVAC DH8S 57-0568.Sep 12, 2002 · N406QX · Bombdr DHC8401SDR A6WA200230019Rib · crackedLEFT WING LEADING EDGE 512AL HAS A .25 INCH RIB CRACKED ON FLANGE AT TWO PLACES. DAMAGE LOCATED ON 2ND RIB INBOARD. MAINTENANCE REMOVED DAMAGED AREA FROM LEFT LEADING EDGE 512AL RIB. FABRICATED REPAIR PARTS AND INSTALLED REF DO 328 SRM 51-27-0 AND REPAIR PRSep 7, 2002 · N341PH · Dorner DO328100SDR A6WA200230020Rib · crackedRIGHT LEADING EDGE 612CR HAS CRACKED RIB DAMAGE ON 1ST RIB FROM INBOARD AT UPPER SURFACE. MAINTENANCE REMOVED DAMAGED AREA FROM RIGHT WING LEADING EDGE 612CR RIB. FABRICATED REPAIR PARTS REF D0328 DRM 51-27-0 AND INSTALLED REF DO328 SRM 57-41-23 AND DER REPOSep 7, 2002 · N341PH · Dorner DO328100SDR UPS02439580Rib · crackedDURING C CHECK, RT W 22 V/C FLAP I/B ROTARY ACTUATOR MOUNTING RIB MOUNT BOLT HOLE SURFACE CORROSION REVEALED AT ALL MOUNT HOLES AND BORES. (RHW OLES 1205) RT W 22 V/C FLAP I/B ROTARY ACTUATOR RIB REPAIRED AS PER RS R57-41-34900 & EO B747-5740-17619-A. ROSep 7, 2002 · N683UP · Boeing 747121SDR AUS20020998Rib · cracked(AUS) RH WING RIB CRACKED ALONG RIVET LINE IN THREE PLACES.Sep 6, 2002 · Piper PA32RT300SDR UPS02839330Rib · crackedINSPECTION TYPE:C1 LEFT WING L/E UPPER RIB IS CRACKED AT XS 484.895. STOP DRILLED CRACK, NDT VERIFIED STOP DRILL TERMINATES CRACK, FABRICATED AND INSTALLED ANGLE DOUBLERS IAW SRM 57-2-0 FIG 2.Sep 5, 2002 · N708UP · Doug DC871FSDR DHL2002873508Former · crackedITEM N/R 0716: LH WING OUTBD. LEADING EDGE .500 CRACK IN FORMER UPPER PART STA. XFS885.000CORR: REMOVED DAMAGED FORMER IAW SRM51-1-21 PG.1 FABRICATED NEW FORMER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED FORMER IAW SRM 57-Sep 4, 2002 · N873SJ · Doug DC873FSDR DHL2002873507Panel · crackedITEM N/R 0767: RT. WING T/E UPPER PANEL CRACKED 4" STA. XRS436.000 TO STA. XA475.000CORR: REMOVED AND REPLACED RT. WING T/E UPPER PANEL , STA XRS 436 TO XA475.000 IAW SRM 51-3-0Sep 3, 2002 · N873SJ · Doug DC873FSDR AUS20021134Rib · corroded(AUS) LT AND RT WING OUTER RIBS LOCATED AT STA 191 CORRODED BEYOND LIMITS.Sep 1, 2002 · Beech 95C55SDR AUS20021133Rib · corroded(AUS) LH AND RH WING TRAILING EDGE RIBS CORRODED. RIBS AFFECTED ARE:- LH WING-PNO 95110014-121PNO 95110014-191PNO 95110014-153PNO 95110014-129PNO 95110014-135RH WING-PNO 95110014-122PNO 95110014-192PNO 95110014-154PNO 95110014-130PNO 95110014-120Sep 1, 2002 · Beech 95C55SDR AUS20021123Rib · corroded(AUS) LH WING RIB PNO 9511023-3 AND RH WING RIB PNO 9511023-4 CORRODEDTHROUGH. LH WING RIB CHANNEL PNO 9511023-5 AND RH WING RIBCHANNEL PNO 9511023-6 CORRODED THROUGH. RIBS AND CHANNELS ARE LOCATED AT STN 66.Sep 1, 2002 · Beech 95C55SDR QXEA0201346Rib · crackedCKB - RIGHT HAND CENTER WING LEADING EDGE HAS CRACKED RIBS AT FOUR PLACES, TWO ON INBOARD RIB ENDS AND TWO ON OUTBOARD RIB ENDS. REPAIRED IAW HORIZON AIR EA 6-57-55A AND WVAC EO DHC8S-57-0529A.Aug 23, 2002 · N405QX · Bombdr DHC8401SDR QXEA0201345Rib · crackedCKB - LEFT HAND CENTER WING LEADING EDGE HAS CRACKED RIBS AT FOUR PLACES, TWO ON INBOARD RIB ENDS AND TWO ON OUTBOARD RIB ENDS. REPAIRED IAW HORIZON AIR EA 6-57-55 AND WVAC EO DH8S-57-0529A.Aug 23, 2002 · N405QX · Bombdr DHC8401SDR AUS20020927Rib · cracked(AUS) WING RIB WEB CRACKED DUE TO FLEXING CAUSED BY AILERON PULLEYBRACKET AND FLAP PULLEY BRACKET ATTACHED TO RIB.Aug 21, 2002 · Cessna 550SDR SWAA021880Rib · crackedDURING SCHEDULED D CHECK, FOUND RT WING RIB CRACKED AT WBL 135.5, BETWEEN STR 2R AND STR 3R. REPAIRED RIB PER BFG ER.Aug 18, 2002 · N364SW · Boeing 7373H4SDR UPS02439366Rib · corrodedINSPECTION TYPE:C LT WING L/E RIB AT L/E SLAT 1309.15 ROTARY ACTUATOR MOUNTING HOLES NR 1, 7 BORE CORROSION FOUND. RIB FOUND CORRODED AT LOCATION L/E SLAT 1309.15 TO 1309.15. CORROSION BLEND OUT EXCEEDED SRM LIMIT RIB REPLACED PER SRM 51-10-01, 57-41-34886, Aug 16, 2002 · N672UP · Boeing 747123SDR UPS02839093Pressure Panel · crackedINSPECTION TYPE:PFLT RT W/W UPPER WEB CRACKED STA XW 5.00 FERRY 9151 TO SDF REF D243078. REPAIRED WEB PER SRM 57-2-0 FIGURE 2A.Aug 14, 2002 · N819UP · Doug DC873FSDR L2232Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE RIGHT WING CENTER SECTION CANTED RIB CAP P/N: 5722206-2 (LCWS 26.85") HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45") AND EXTENDING APPROXIMATELY 1" AFT OF THE SPAR. AFTER REMAug 5, 2002 · N666HC · Cessna 441SDR L2240Rib · crackedDURING A SCHEDULED INSPECTION, IT WAS NOTED THAT THE LEFT WING CENTER SECTION CANTED RIBCAP P/N: 5722206-1 (LCWS 26.85 INCH) HAD A CRACK ALONG THE BEND RADIUS AFT OF THE CENTER WING MAIN SPAR (FS 177.45 INCH) AND EXTENDING APPROXIMATELY 1INCH AFT OF THE SPAR. Aug 5, 2002 · N666HC · Cessna 441SDR 0202656743Rib · corrodedDuring "M" check found corrosion on the upper surface of left wing leading edge rib at wing station 1339.75. Repaired per EA 67-191214.Aug 2, 2002 · N643NW · Boeing 747249FSDR BJNA020802Rib · corrodedFOUND LEFT WING LEADING EDGE RIB AT NR 2 SLAT ACTUATOR INBOARD CORRODED. (M)Aug 1, 2002 · N344TM · Boeing 737282SDR UPS02839240Rib · crackedINSPECTION TYPE:C2 LEFT WING L/E LOWER RIB IS CRACKED AT XFS 616.25. STOP DRILLED CRACK, NDT VERIFIED NO CRACKS AT STOP DRILL, FABRICATED AND INSTALLED DOUBLER IAW SRM 57-2-0 FIG 2.Jul 29, 2002 · N806UP · Doug DC873FSDR AUS20021156Rib · corroded(AUS) LT AND RT WING LEADING EDGE RIBS SEVERELY CORRODED. SIXTEEN RIBS AND BOTH BOTTOM OUTBOARD WING SKINS REQUIRED REPLACEMENT. FOUND WHEN RIBS DISMANTLED AFTER FINDING BULGING ALONG THE SPAR INSEVERAL AREAS OUTBOARD OF THE WING STRUTS DURING PERIODIC INSPECTJul 12, 2002 · Cessna 172NSDR DHL2002806844Former · crackedN/R: 1696 RH WING OUTBD L/E UPPER PART FORMER CRACKED .250 XFS647.500CORR: STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE IAW SRM57-2-0 Jul 6, 2002 · N806DH · Doug DC873FSDR DHL2002806852Former · crackedITEM N/R 2281 RH WING CTR L/E UPPER FORMER 1/2" CRACKED , STA XFS 316.000CORR: PERFORMED STOP DRILL IAW SRM 57-2-0 PG. 9-10 FABRICATED DOUBLER WITH 2024T3 AL O.063 IAW SRM57-2-0 PG9-10 , CLEANED , TREATED , AND PRIMED. IAW SRM51-1-8B , INSTALLED DOUBLER ON R/HJul 5, 2002 · N806DH · Doug DC873FSDR DHL8062002847Former · crackedITEM N/R 1964 RH WING OUTBOARD LEADING EDGE UPPER PART FORMER CRACKED 3/4 " XFS616.250CORR: REMOVEED FASTNERS IAW SRM 51-1-21 PG1 PERFORMED STOP DRILL IAW SRM 57-2-0 PG 9-10 FABRICATED DOUBLER IAW 57-2-0 PG 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B ,Jul 5, 2002 · N806DH · Doug DC873FSDR AUS20021035Rib · corroded(AUS) WING RIB CONTAINED GALVANIC CORROSION IN AREA OF LE WS 277.5. FOUND DURING CPCP INSPECTION.Jul 4, 2002 · Boeing 727277SDR DHL2002806851Former · crackedITEM REF N/R 2282 RH WING CTR LEADING EDGE UPPER FORMER .500 CRACK @ STA XFS 322.750CORR: REMOVED FASTNER IAW SRM 51-1-21 PG 1 , FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE ANDJul 4, 2002 · N806DH · Doug DC873FSDR DHL2002806850Former · crackedITEM REF. N/R RH WING CTR L/E FORMER .500 CRACKED XFS329.000CORR: STOP DRILLED CRACK ON RH WING CTR L/E UPPER FORMER , STA. XFS329.000 , IAW SRM57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B, INSTALLEDJul 4, 2002 · N806DH · Doug DC873FSDR DHL2002806849Former · crackedITEM REF N/R 2286 RH WING CTR L/E LOWER FORMER 1" CRACK , STA. XFS360.250CORR: PERFORMED STOP DRILL ON 1" CRACK , STA XFS360.250 IAW SRM 57-2-0 PG. 9-10 FABRICATED DOUBLER IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED , AND PRIMED IAW SRM 51-1-8B INSTALLED DOUBLERJul 4, 2002 · N806DH · Doug DC873FSDR DHL2002806846Former · crackedITEM REF N/R 1317 LT. WING OUTBD L/E FORMER CRACKED AT STA. XFS691.000CORR: STOP DRILLED CRACK IAW SRM 57-2-0 PG. 9-10 FABRICATED REINFORCING ANGLE IAW SRM 57-2-0 PG. 9-10 CLEANED , TREATED AND PRIMED AREA IAW SRM 51-1-8B INSTALLED REINFORCING ANGLE ON OUTBD Jul 4, 2002 · N806DH · Doug DC873FSDR DHL2002806848Former · crackedITEM REF N/R 2233 LH WING CTR. LEADING EDGE LOWER SURFACE FORMER WITH 1" CRACK IN IT STA XFS 335.220 CORR: REMOVED FASTNERS IAW SRM 51-1-21 PG. 1 STOP DRILLED CRACK IAW SRM57-2-0 PG. 9-10FABRICATED REINFORCING ANGLE IAW SRM57-2-0 PG. 9-10 , CLEANED , TREATED ,Jul 3, 2002 · N806DH · Doug DC873FSDR UPS02438972Rib · corrodedINSPECTION TYPE:C, RT WING L/E RIB AT ILES 852.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.065 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT ASJul 2, 2002 · N677UP · Boeing 747123FSDR UPS02438971Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT OLES 1308.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.020 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT Jul 2, 2002 · N677UP · Boeing 747123FSDR UPS02438970Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT OLES 1381.25 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.030 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT Jul 2, 2002 · N677UP · Boeing 747123FSDR UPS02438969Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT OLES 1349.29 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.026 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT Jul 2, 2002 · N677UP · Boeing 747123FSDR UPS02438968Rib · corrodedINSPECTION TYPE: C, RT WING L/E RIB AT OLES 1493.45 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.038 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT Jul 2, 2002 · N677UP · Boeing 747123FSDR AWXA200200640Rib · crackedYVR - MAJOR REPAIR - DURING C-14 CHECK A CRACK WAS FOUND ON THE RT WING T/E, AT THE INBOARD SIDE OF THE AILERON HINGE SUPPORT RIB, WS 340. MAINTENANCE REMOVED THE CRACKED SUPPORT RIB AT WS 340, FABRICATED A NEW RIB, AND INSTALLED REPAIR IAW DWG 65-46460-47, AJul 2, 2002 · N305AW · Boeing 7373G7SDR UPS02438967Rib · corrodedINSPECTION TYPE: C, LT WING L/E RIB AT ILES 755.05 FOUND CORROSION AT ROTARY ACTUATOR MOUNTING BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.008 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AJul 1, 2002 · N677UP · Boeing 747123FSDR UPS02438966Rib · corrodedINSPECTION TYPE: C, LT W L/E RIB AT OLES 1277.15 FOUND CORROSION AT ROTARY ACTUATOR MOUNT BOLT HOLES BORE AND CUTOUT SURFACE. CORROSION BLEND OUT 0.022 INCH X 0.5 INCH X 0.5 INCH EXCEED SRM LIMIT. WING LEADING EDGE RIB INTERMIN CORROSION REPAIR CUTOUT AS PERJun 30, 2002 · N677UP · Boeing 747123F
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