JASC 5711

Service difficulty reports · 5,587

Reports filed under 5711 · Wing Spar, 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 = '5711'
  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 2001FA0000415Spar · crackedWHILE INSPECTING WING SPARS IN COMPLIANCE WITH AD, THE FRONT SPAR IN THE RIGHT WING WAS FOUND TO HAVE A COMPRESSION CRACK AT THE BUTT END AND THE REAR SPAR IN THE LEFT WING WAS FOUND TO HAVE A LONGITUDINAL CRACK APPROXIMATELY 14 INCHES INBOARD FROM THE TIP.Oct 4, 2001 · N5074X · Bbavia 7GCBCSDR DHL2001742513Spar · crackedAT C-CHECK, CRACK IN FULSE SPAR WEB NR 4 FLAP TRACK, MKD.Oct 4, 2001 · N742DH · Boeing 727225SDR DHL2001742508Spar · corrodedAT C-CHECK- RT WING REAR AUX SPAR AT WS 294. FOUND CORROSION TO FWD/UPPER ANGLE.Oct 4, 2001 · N742DH · Boeing 727225SDR DHL2001742507Spar · corrodedAT C-CHECK, LIGHT CORROSION OF FWD SIDE OF FULSE SPAR ABOVE O/B FLAP POSITION TRANSMITTER MKD.Oct 4, 2001 · N742DH · Boeing 727225SDR QXEA0101670Spar · scratchedPDX - LEFT-HAND WING AT STATION YW133.00 FORWARD SPAR TOWARD THE TOP THERE ARE 3 SMALL LIGHT SCRATCHES. REPAIRED IAW DHC-8 SRM 51-20-26, PAGES 4 AND 5, STEPS 3-A B AND C.Oct 4, 2001 · N353PH · Dhav DHC8202SDR 2002FA0000235Spar · crackedWING MAIN SPAR, TOP OF SPAR OUTBOARD OF STRUT FITTING.Sep 25, 2001 · N8615V · Bbavia 7KCABSDR ASOA01185Spar Cap · crackedDURING HANGAR MAINTENANCE MCN, THE RIGHT WING FORWARD SPAR CAP WAS FOUND TO BE CRACKED. MAINTENANCE IS REPAIRING THE RIGHT WING CRACKED SPAR CAP IAW ASA EO120-57-0115. (M)Sep 25, 2001 · N238AS · Emb EMB120SDR ASOA01184Spar Cap · crackedDURING SCHEDULED MAINTENANCE IN MCN, THE LEFT WING FORWARD SPAR CAP WAS FOUND TO BE CRACKED. MAINTENANCE IS REPAIRING CRACKED LEFT WING SPAR CAP IAW ASA EO120-57-0114. (M)Sep 25, 2001 · N245AS · Emb EMB120SDR AUS20011032Spar · corroded(AUS) LH AND RH WING SPARS PNO 35168-08 (LH) AND PNO 35168-09 (RH)CONTAINED SEVERE EXFOLIATION CORROSION.Sep 24, 2001 · Piper PA28161SDR QXEA0101579Spar · damagedPDX - LEFT-HAND WING INBOARD LEADING EDGE 511AL, LOWER ATTACH FLANGE ON FRONT SPAR, INBOARD NUTPLATE HAS DAMAGED BUSHINGS. REPAIRED IAW HORIZON AIR EA 2-57-139.Sep 21, 2001 · N352PH · Dhav DHC8202SDR AUS20011048Spar · damaged(AUS) ALL FOUR WINGS PNO U2727 MK2 (LT LOWER), PNO U2728 MK2 (RT LOWER), PNO U2729 MK2 (LT UPPER) AND PNO U2730 MK2 (RT UPPER) WERE REJECTED FOLLOWING REBUILD. NUMEROUS HOLES DRILLED IN ALL FOUR WING SPARS WERE OVERSIZE OR DRILLED IN A FIGURE 8. AILERON BELLCRSep 18, 2001 · Dhavxx DH82AROBRTSNSDR DLM11011550Spar Cap · corrodedLH WING / REAR SPAR / UPPER CAP / XORS 725, 745, 790 : CORROSION REPAIR THE LH WING REAR SPAR WAS FOUND CORRODED ON THE UPPER SURFACE OF THE UPPER CHORD AT XORS 725, 745, & 790 COMMON TO TRAILING EDGE PANSep 15, 2001 · N801DE · Doug MD11SDR UPS01236905Spar · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31.Sep 13, 2001 · N912UP · Boeing 72762CSDR QXEA0101496Spar · crackedPDX - LEFT-HAND WING FRONT SPAR TO INBOARD NACELLE CONNECTION ANGLE IS CRACKED IN 2 SPOTS NEAR TOP. REPAIRED IAW DASH-8 SRM 51-40-00 AND SRM 51-40-11.Sep 8, 2001 · N350PH · Dhav DHC8202SDR 2001F00396Spar · crackedWHILE PERFORMING THE MANUFACTURERS EVENT 1 INSPECTION, A CRACK WAS DISCOVERED IN THE RIGHT WING MAIN SPAR 9FS 137) JUST INBOARD OF WING STATION 87.50. THE CRACK WAS APPROXIMATELY .875 INCH LONG AND EXTENDS FROM THE CENTER OF THE SPAR AFT THROUGH A RIVET HOLE.Sep 6, 2001 · N398SP · Piper PA31T1SDR QXEA0101508Spar · chafedPDX- LEFT HAND WING FRONT SPAR BOTTOM FLANGE YW135 TO YW139 IS CHAFED. REPAIRED IAW DHC-8 RD 8-57-1150 AND DHC-8 SRM 51-20-26.Sep 5, 2001 · N350PH · Dhav DHC8202SDR QXEA0101507Spar · chafedPDX- LEFT HAND WING FRONT SPAR FLANGE FROM YW57 TO YW72 IS CHAFED. REPAIRED IAW DHC-8 RD 8-57-811 AND 8-57-1150.Sep 5, 2001 · N350PH · Dhav DHC8202SDR QXEA0101506Spar Cap · corrodedPDX- FRETTING CORROSION AT 15 FASTENER HOLES LOWER SPAR CAP BELOW LEADING EDGE 611AR. REPAIRED IAW DHC-8 RD 8-57-811, 8-57-1150 AND DHC-8 SRM 51-40-11.Sep 3, 2001 · N350PH · Dhav DHC8202SDR MWEA011222Spar · corrodedRIGHT WING AFT SPAR UPPER VERTICAL LEG HAS CORROSION AT STATION XRS 267.0, INBOARD OF UPPER FLAP HINGE BOLT. (XW 251.6) REMOVED CORROSION, INSPECTED, AND BLENDED AREA. ACCEPTABLE PER MWX-ORD-01-004-51H DATED 24 AUGUST 2001.Aug 30, 2001 · N401ME · Doug DC932SDR UPS01236811Spar Cap · corrodedINSPECTION TYPE:C LT WING ON INSPECTION OF LEADING EDGE TO FRONT SPAR JOINT, CORROSION FOUND IN UPPER CAP OF SPAR AT FRONT SPAR STN189. CORROSION REMOVED IAW SRM , HFEC AREA AND NO DEFECTS FOUND, CORROSION BLEND FOUND TO BE OUTSIDE LIMITS, UPPER FRONT SPAR RAug 28, 2001 · N916UP · Boeing 727172CSDR 2001F00582Spar Cap · corrodedDURING FUEL TANK INSPECTION, FOUND CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.25 WAS NOTED. (M)Aug 18, 2001 · N860CA · Beech 1900DSDR UPS01836625Doubler · brokenINSPECTION TYPE:C1,3 RIGHT WING LOWER FRONT SPAR HAS DOUBLER BROKEN AT XS 520. REMOVED, FABRICATED, AND REPLACED DOUBLER IAW SRM 57-2-1 FIG 14A, AND DWG 5802736.Aug 5, 2001 · N809UP · Doug DC873FSDR UPS01836626Spar Cap · crackedINSPECTION TYPE:C1,3 RIGHT WING REAR SPAR LOWER CAP IS CRACKED AT XCW 0. REPAIRED SPAR IAW 8110-3 APPROVED DK SK 809-649.Aug 3, 2001 · N809UP · Doug DC873FSDR 2001F00424Spar · corrodedCENTER TANK UPPER SKIN AT REAR SPAR BS 870 HAS CORRODED AREAS FROM LBL 40 TO RBL 40. ACCOMPLISHED WING CENTER SECTION AFT SPAR UPPER CHORD AND SKIN REPAIR AT RBL 24 IAW AVHM-246RO-1 REV IR. (M)Aug 2, 2001 · N355QS · Boeing 72721SDR 2001FA0000226Spar · crackedCRACK DEVELOPED ON TOP OF LEFT WING. INVESTIGATION REVEALED LOWER FORWARD WING SPAR HINGES AND PINS WORN OUT RESULTING IN EXCESS OF MOVEMENT IN THE LEADING EDGE OF WINGS. NEW WING SPARSJul 28, 2001 · N2764T · Beech 95C55SDR 2001F00585Spar Cap · corrodedDURING FUEL TANK INSPECTION, FOUND CORROSION ON LEFT AND RIGHT WING LOWER SPAR CAP AT WING STATION 124.25 WAS NOTED. (M)Jul 27, 2001 · N83206 · Beech 1900DSDR G60A057Spar Cap · crackedFOUND RIGHT WING REAR SPAR LOWER CAP HAS 3 INCH LONG CRACK IN RADIUS FROM RS 1046.2 TO RS 1049.9. (M)Jul 27, 2001 · N703GC · Doug MD11SDR 2001F00404Spar · corrodedWING CENTER SECTION INTERNAL AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 22L DUE TO CORROSION. INSTALLED WING CENTER SECTION AFT SPAR WEB REPAIR AT STATION 870 BETWEEN LBL 17.2 AND LBL 25.9 IAW AVITAS ENGINEERING REPAIR ORDER AVHM-237RO-1 REV 1R DATED Jul 26, 2001 · N355QS · Boeing 72721SDR 2002F00860Spar · corrodedFOUND WING CENTER SECTION STATION BS 870, REAR SPAR LOWER CHORD, EXTERIOR, RBL 42 HAS CORROSION. (M)Jul 24, 2001 · N356QS · Boeing 72721SDR 2002F00839Spar · crackedRIGHT WING HAS CRACKS AT REAR SPAR UPPER CHORD AT WING STATION 217 INBOARD OF LANDING GEAR. (M)Jul 24, 2001 · N356QS · Boeing 72721SDR 2002F00862Spar · corrodedWING CENTER SECTION FRONT SPAR EXTERIOR LOWER CHORD HAS BULGING AREA AT LEFT BBL 60 INCH. (M)Jul 18, 2001 · N356QS · Boeing 72721SDR 2002FA0000258Spar · crackedWING SPAR, CRACK VISIBLE MIDWAY FROM TOP TO BOTTOM OF NIGHT WING FRONT SPAR FROM 44 INCHES INBOARD ALONG SPAR TO APPROXIMATELY 1130 INCHES FORM INBOARD. WOOD APPEARS TO BE IN GOOD CONDITION OTHERWISE. DEFECT DISCOVERED DURING SPAR INSPECTION IN COMPLIANCE WIJul 18, 2001 · N9898B · Bbavia 7ECSDR 2002FA0000246Spar · defectiveCRACK VISIBLE MIDWAY FROM TOP TO BOTTOM OF RIGHT WING FRONT SPAR FROM 44 INCHES INBOARD ALONG SPAR TO APPROXIMATELY 130 INCHES FROM INBOARD. WOOD APPEARS TO BE IN GOOD CONDITION OTHER WISE. DEFECT DISCOVERED DURING SPAR INSPECTION IN COMPLIANCE WITH AD. AIRJul 18, 2001 · N9898B · Bbavia 7FCSDR 2002FA0000251Spar · crackedDETECTED COMPRESSION CRACK AT TOP OF AFT SPAR ON THE OUTBOARD END OF LIFT STRUT DOUBLER PLATE. CRACK PROGRESSED DOWN AFT SIDE ABOUT 1 INCH. LONGITUDINAL CRACK WAS ALSO FOUND IN AFT SPAR LAST 12 INCHES NEAR TIP. CRACK WAS IN CENTER OF SPAR. WHEN THE WING WJul 17, 2001 · N2546Z · Bbavia 7GCBCSDR DL73K011179Spar Cap · crackedA CRACK WAS FOUND IN THE REAR SPAR UPPER CAP AT RSS 224.14. A REPAIR WAS INSTALLED PER BOEING REWORK DRAWING 65C30105. THE DAMAGE WAS FOUND DURING AN INSPECTION AT HMV.Jul 17, 2001 · N317DL · Boeing 737232SDR ZW0A0105404Spar Cap · crackedDURING CHECK-C MAINT FOUND EYEBROW CRACK IN RT WING UPPER SPAR CAP AT OTBD FLAP HINGE INBD GUIDE PIN. INSTALLED DOUGLAS REPAIR DOUBLER PER DRAWING JO60272-501 AND PER ARA 17773.Jul 17, 2001 · N923TW · Doug DC982SDR CALA0100659Spar · crackedINSPECTION FOUND A CRACK INDICATION IN NR 2 HOLE OF LT WING REAR SPAR UPPER CHORD AT GEAR BEAM CASTING ATTACH POINT. THE HOLE WAS REAMED AND THE CRACK WAS FOUND TO EXCEED 0.500 INCH MAX REAM LIMIT. THE REAR SPAR UPPER CHORD WAS REMOVED AND REPLACED FROM INBOJul 17, 2001 · N14358 · Boeing 7373T0SDR 2001F00205Spar · crackedSPAR CRACKEDJul 12, 2001 · N83233 · Bbavia 7ACSDR 2001F00584Spar Cap · corrodedDURING FUEL TANK INSPECTION, CORROSION ON LEFT AND RIGHT WING SPAR CAP AT WING STATION 124.25 AS NOTED. (M)Jul 11, 2001 · N84703 · Beech 1900DSDR 2001F00423Spar · corrodedWING CENTER SECTION FRONT SPAR BS 740 LOWER CHORD OUTBOARD OF VERTICAL STRINGER F5 HAS TWO RIVETS POPPED OUT AND SKIN BULGING. INSTALLED REPAIR ANGLES AND STRAPS WING CENTER SECTION FRONT SPAR LOWER CHORD AT STATION 740 RBL 42 THROUGH 48.43 IAW AVHM 238R0-1. Jul 11, 2001 · N355QS · Boeing 72721SDR 2001F00422Spar · corrodedWING CENTER SECTION, INTERNAL, AFT SPAR WEB BULGED IN AREA OF UPPER SPAR CHORD BL 45 R. INSTALLED DOUBLER REPAIR AT AFT WEB, STATION BS 870, RBL 50.9 IAW AVHM-23RO-1 REVISION R1. (M)Jul 11, 2001 · N355QS · Boeing 72721SDR 0102786730Spar · corrodedDuring "L" check found corrosion on upper surface of RH wing inboard trailing edge midflap aft spar. Repaired per EA 67-184306.Jul 11, 2001 · N630US · Boeing 7472J9FSDR 2001FA0000080Spar · crackedDURING INSPECTION, FOUND LT WING FORWARD SPAR CRACKED AT UNDERSIDE OF SPAR OUT BOUND OF LIFT STRUT ATTACH POINT. THIS WING WILL BE REPAIRED WITH NEW SPAR INSTALLED.Jul 10, 2001 · N83280 · Bbavia 7ACSDR 2001FA0000387Spar · crackedDURING INSPECTION TO COMPLY WITH AD, CRACKS WERE FOUND INBOARD AND LEFT FRONT SPAR, INBOARD END RIGHT REAR SPAR. .001 FEELER GAGE COULD BE INSERTED .1250 OR MORE INTO CRACKS.Jul 9, 2001 · N2959E · Bbavia 7CCMSDR 2001FA0000131Spar · unsecureAIRCRAFT REGISTERED AS BELLANCA. MODEL IS 7KCAB. DESIGN NOW OWNED BY AMERICAN CHAMPION. WOOD SPAR WING INSPECTED IN ACCORDANCE WITH AD 2000-25-02. SEVERAL RIB/SPAR ATTACHMENT NAILS MISSING. PER SERVICE LETTER SL-417 THE SPAR "DAMAGE" CAUSED BY THE MISSINGJul 3, 2001 · N8680V · Bbavia 7KCABSDR 2001FA0000106Spar · crackedFOUND A SMALL LONGITUDINAL CRACK BETWEEN THE PLYWOOD DOUBLER PLATE AT THE FORWARD LIFT STRUT ATTACH FITTING AND THE NEXT OUTBOARD RIB ALONG THE REAR FACE OF THE SPAR. WITH A MIRROR IN THE NEXT OUTBOARD RIB BAY, THE CRACK PROTRUDED ABOUT THREE INCHES. WHEN THJul 2, 2001 · N1703E · Bbavia 7ACSDR 2002FA0000245Spar · crackedAIRFRAME TOTAL TIME 3161 DURING THE ANNUAL INSPECTION AND WHILE COMPLYING WITH AD INSTRUCTIONS. IT WAS DISCOVERED THAT THE RIGHT WING REAR SPAR HAD AN 8 INCHES LONG LONGITUDINAL CRACK AT THE REAR STRUT ATTACH POINT. ITS SUSPECTED THAT THE AIRFRAME HIGH TIME Jun 30, 2001 · N8643 · Bbavia 7KCABSDR 2001FA0000123Spar · crackedDURING INSPECTION OF RIGHT WING, A CRACK WAS FOUND ON THE AFT SIDE OF THE FORWARD WOOD SPAR, 79 INCHES OUTBOARD FROM THE BUTT RIB. THE 5 INCH LONG, HORIZONTAL CRACK WAS LOCATED AT THE COMPRESSION MEMBER AND RAN THROUGH THE HOLES FOR THE DRAG WIRES. UNDETERMIJun 29, 2001 · N86960 · Bbavia 7KCABSDR 2002FA0000239Spar · crackedDURING ANNUAL INSPECTION, WING SPAR INSPECTION IAW AD., FOUND LONGITUDINAL CRACKS IN THE AREA OF WING STRUT ATTACH POINTS. RIGHT FORWARD SPAR LONGITUDINAL CRACK OBSERVED FROM MISSING CENTER RIB NAIL, INBOARD FROM THE STRUT ATTACH DOUBLER APPROXIMATELY 2 INCH Jun 27, 2001 · N2763G · Bbavia 7ECASDR 2002FA0000256Spar · crackedLONGITUDINAL CRACK LOCATED AT ROOT END OF FRONT WING SPAR IN RIGHT WING. CRACK RUNS FROM BUTT END OF SPAR THROUGH THE TWO TOP BOLT HOLES OF THE SPAR TO FUSELAGE ATTACHMENT BRACKET. CRACK COULD BE SEEN IN THE BUTT END GRAIN AND BY REMOVING THE FUSELAGE ATTACHJun 26, 2001 · N9866Y · Bbavia 7GCB
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