N711SY, cancelled Mar 3, 2020
Service difficulty reports · 99
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. 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 n_number = 'N711SY' AND deregistration_id = 'N711SY-2020-03-03' 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.
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 n_number = 'N711SY' AND deregistration_id = 'N711SY-2020-03-03' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR SCNA201910019183Skin · wornRH LE SLAT #7 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #7 SLAT REF AMM 27-81-21. INSPECTED INTERFACE, OK TO INSTALL. INSTALLED NEW SLAT IAW AMM 27-81-21-400-801. SSDR SCNA2019100194182Structure · worn#1 SLAT UNDER TRAILING EDGE HAS WORN ANTI ABRASION PAINT NUMEROUS SPOTS. OUTBOARD TRAILING EDGE WEAR IS BEYOND ALLOWABLE LIMIT AND WILL REQUIRE REPAIR PER SRM 57-42-01-2R-6 REPAIR 6. REPAIRED REF SRM 57-42-01-2R-6SDR SCNA2019100194181Skin · damagedRH LE SLAT #6 BARE METAL SHOWING ON UNDERSIDE ALONG AFT EDGE. FOUND TRAILING EDGE WEAR BEYOND SRM REPAIRABLE LIMITS PER SRM 57-42-01-2R-6 REPAIR 6. REMOVED #6 SLAT REF AMM 27-81-21. PERFORMED INTERFACE INSPECTION AND OK TO INSTALL NEW SLAT. INSTALLED NEW SLAT SDR SCNA2019100194180Structure · corrodedAFT CARGO DOOR, CORROSION ON LOWER AFT INSIDE CORNER NEXT TO INSULATION BUTTON. SEE SRM 52-30-01/1A01 FOR LIMITS. METAL THICKNESS .071 MATERIAL 7075T6. REMOVED CORROSION AT 2 LOCATIONS WITH CUTOUTS AT LOWER AFT CORNER AND LOWER INNER SKIN FWD OF AFT STOP FITTISDR SCNA2019100192179Fastener · looseLEFT WING, UPPER L/E 16 LOOSE FASTNERS FROM THE PYLON INBD. ALONG THE AFT SIDE OF PANEL. REMOVED 16 EA LOOSE FASTENERS ON L/H WING UPPER SKIN JUST INBD OF # 1 PYLON. REAMED HOLES TO 1ST OVER 3/16. .199" OPEN HOLE AND COUNTER SINK HFEC ACCOMPLISHED BY NDI. NO CSDR SCNA2019100194178Spar · cracked11" CRACK ON WING CENTER SECTION REAR SPAR BETWEEN 45.64 AND 31.83 STIFFENERS. COMPLETED INTERIM REPAIR IAW SRM 57-10-10-2R-2 PARAGRAPH 6. ITEM WILL BE PLACED ON GMM/MTI FOR TRACKING PURPOSES FOR A DETAILED VISUAL INSPECTION EVERY 3,000 FLIGHT CYCLES. IF ADDITSDR SCNA201906219072Support · damagedRIGHT MLG SIDE STAY IS RUBBING INTO THE LOWER BEAM SUPPORT AND INTO THE THIRD ROD END SUPPORT MOUNT. REF TASK CARD FOR FIXED T/E PANEL WEAR. REMOVED AND REPLACED ROD SUPPORT AND RECONNECTED ROD.SDR SCNA201902152027Battery · inoperativeFWD WINDSCREEN EMERGENCY PATH LIGHT INOP. R+R'D FORWARD L/A PWR SUPPLY BATTERY. OPS CHECK OK.SDR SCNA201809176108Battery · dischargedEMERGENCY EXIT LIGHT L2, OVERHEAD INOP. R&R BATTERY L2 DOOR AND OVERHEAD EXIT LIGHT. OPS CHECK GOOD.SDR SCNA20180830103Battery Pack · dischargedRT AFT EXTERIOR EMG LIGHT AND INTERER EXIT LIGHT INOP. R/R BATTERY PACK. OPS CHK GOOD.SDR SCNA20180426080Structure · crackedFOUND A CRACK ON THE NR 2 LT LE SLAT. LENGTH OF CRACK IS 1.125 INCH. THE CRACK IS ACCEPTABLE TO FLY FOR 50FC. REMOVED AND REPLACED THE NR 2 LT L/E SLAT. OK FOR SERVICE.SDR SCNA20180330074Light · inoperative9ABC EMERGENCY LIGHT INOP. PLACED 9ABC EMERGENCY AISLE LIGHT ON MEL. R&R THE INOP EMER LIGHT BULB AT 9ABC. OP CHECK GOOD. THIS CLEARS MEL.SDR 2018F00062Pump · failedLOST OF HYDRAULIC SYSTEM "B" INFLIGHT. POP OUT CIRCUIT BREAKERS ENGINE 2 PUMP DEPRESS VALVE 1 AND SYST "B" STANDBY RUDDER. (QRF RETURN TO AIRPORT). CORRECTIVE ACTION:HAS BEEN CHANGED EDP SYST "B" ENGINE 2 AND CHANGED FILTER SYSTEM B.SDR SCNA20170901160Skin · dentedFUSELAGE DENT LOCATED NEAR LAV SERVICE DOOR. REMOVED DENT DAMAGE AT LAV SERVICE DOOR STA 834 BELOW STR 22L AND REPAIRED.SDR SCNA20161001231Light · inoperativeAFT EMERGENCY LIGHT IN HORSESHOE PANEL INOPERATIVE. REMOVED AND REPLACED AFT AISLE EMERGENCY LIGHT. OPS CHECKED GOOD.SDR SCNA20161001230Floorboard · corrodedFLOORBOARD IS CORODED AT RBL 16, BS 966.SDR SCNA20161001229Floor Panel · damagedFORWARD CABIN FLOOR PANEL 141A5810-56 HAS CORNER BROKEN OFF. REPAIRED THE FLOOR PANEL.SDR SCNA20161001228Floor Panel · damagedFORWARD CABIN FLOOR PANEL 141A5810-484 HAS TWO AREAS WHERE THE UPPER LAYER OF FIBERGLASS IS MISSING. REPAIRED THE FLOOR PANEL.SDR SCNA20161001227Floor Panel · damagedFORWARD CABIN FLOOR PANEL 141A5810-464 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED THE CABIN FLOOR PANEL.SDR SCNA20161001226Floor Panel · damagedFWD CABIN FLOOR PANEL 141A5810-185 HAS EDGE DAMAGE. REPAIRED FWD CABIN FLOOR PANEL.SDR SCNA20161001225Insert · corrodedFORWARD CABIN FLOOR PANEL 141A5810-185 HAS SEVERAL MISSING AND CORRODED INSERTS. REPAIRED FORWARD CABIN FLOOR PANEL 141A5810-185.SDR SCNA20161001224Insert · corrodedFORWARD CABIN FLOOR PANEL 141A5810-245 HAS SEVERAL CORRODED INSERTS. REPLACED THE INSERTS.SDR SCNA20161001223Crease Beam · corrodedCREASE BEAM CORRODED IN SEVERAL PLACES FROM BS 947.5 TO 986.5. REMOVED THE CORROSION AND FOUND TO BE OUT OF LIMIT. INSTALLED A NEW CREASE BEAM.SDR SCNA20161001222Nut Plate · missingBL 0 INTERCOSTAL MISSING ONE NUTPLATE BS 927 TO 947. INSTALLED A NEW NUT PLATE.SDR SCNA20161001221Floor Support · corrodedFLOOR SUPPORT CORRODED LBL 20 UPPER FLANGE AFT HOLE BS 967 TO 947. REMOVED CORROSION, ORIGINAL T= .090, AFTER BLENDING T=.059, .031 MATERIAL LOSS OUT OF LIMITS. REMOVED AND REPLACED FLOOR SUPPORT.SDR SCNA20161001220Floorbeam · corrodedBS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO LBL 45. REMOVED CORROSION IAW EA.SDR SCNA20161001219Floorbeam · corrodedBS 986 FLOORBEAM CORRODED ON UPPER SURFACE UPPER FLANGE PREVIOUS REPAIR BL 0 TO RBL 45. REMOVED CORROSION IAW EA.SDR SCNA20161001218Floorbeam · corrodedBS 966 FLOORBEAM CORRODED AT RBL 27. REPAIRED THE FLOORBEAM.SDR SCNA20161001217Floorbeam · damagedFLOORBEAM BS 312 UPPER FLANGE HAS SCRIBE LINES AND CORROSION FROM LBL 5 TO 52. REPAIRED THE FLOORBEAM.SDR SCNA20161001214Intercostal · crackedINTERCOSTAL AT RBL 32 STA 312 TO 328 IS CRACKED ON UPPER FLANGE AT FWD HOLE INTO THE RADIUS. REMOVED AND REPLACED INTERCOSTAL AT RBL 32 STA. 312 TO 328.SDR SCNA20161001213Intercostal · crackedINTERCOSTAL AT STA 328 TO 312 AT RBL16 IS CRACKED AT AFT HOLE ON UPPER FLANGE. REMOVED AND REPLACED INTERCOSTAL AT STA 312 TO 328 RBL 16.SDR SCNA20160930212Window Frame · crackedR1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REMOVED DAMAGE TO R/H FLIGHT DECK #1 WINDOW FRAME AND REPAIRED.SDR SCNA20160930211Window · crackedR1 WINDOW HAS A CRACK INDICATION ON UPPER RIGHT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK ON FLIGHT DECK SIDE. RESTORED R/H #1 WINDOW FRAME CRACK ON UPPER R/H CORNER. OPS AND LEAK CHECK GOOD.SDR SCNA20160930210Window Frame · crackedL1 WINDOW FRAME, UPPER O/B CORNER AT MOST UPPER I/B ATTACH FASTENER HOLE TO #2 WINDOW FRAME, CRACK INDICATION IN HOLE, HOLE MARKED IN BLACK. REPAIRED L/H FLIGHT DECK #1 WINDOW FRAME UPPER O/B CORNER.SDR SCNA20160930209Window Frame · crackedL1 WINDOW FRAME HAS A CRACK INDICATION ON UPPER LEFT HAND CORNER. END OF CRACK INDICATION MARKED IN BLACK. RESTORED L/H #1 WINDOW FRAME CRACK ON UPPER LEFT HAND CORNER. OPS AND LEAK CHECK GOOD.SDR SCNA20160930208Skin · delaminatedRT WING LEADING EDGE PANEL 621CB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621CB.SDR SCNA20160930207Skin · damagedRIGHT WING LEADING EDGE PANEL 621DB DELAMINATED ON LEADING EDGE. REPAIRED RH WING LEADING EDGE PANEL 621DB.SDR SCNA20160930206Bracket · crackedPULLEY BRACKET AFT OF BS 1016 FOR THE LEFT HORIZONTAL STAB CABLE "STA", FAIRLEAD ON PULLEY BRACKET IS CRACKED. REMOVED CRACKED FAIRLEAD AFT OF STA 1016 FOR LH HORIZONTAL STAB CABLE & REPLACED WITH NEW.SDR SCNA20160930205Support · corrodedR1 DOOR THRESHOLD SUPPORT ATTACH TO CREASE BEAM IS CORRODED AT STA. 320 RBL 61. REMOVED CORROSION FROM R1 DOOR THRESHOLD SUPPORT ATTACH ANGLE ORIG. "T" 0.090 REMOVED 0.022 REMAINING "T" 0.068 OUT OF LIMITS. SUPPORT ANGLE WAS INSTALLED AS PART OF THE CREASE BSDR SCNA20160930204Crease Beam · corrodedR1 DOOR CREASE BEAM IS CORRODED RBL 60 STA 320 TO 358. REMOVED AND REPLACED R1 DOOR CREASE BEAM.SDR SCNA20160930203Floor Support · corrodedFLOOR SUPPORT AT STA 309.9 RBL 5 CORRODED AFT OF GALLEY MOUNT. REMOVED FLOOR SUPPORT AT STA - 294.5 RBL 5. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT.SDR SCNA20160930202Strap · corrodedRIGHT HAND CREASE BEAM STRAP CORRODED AT STA 291. REMOVED & REPLACED RT CREASE BEAM STRAP STA 277 TO 312.SDR SCNA20160930201Skin · wornRT A/C BAY, GROUND PNEUMATIC DOOR INNER SURFACE HAS AREAS OF WEAR AND MISSING PAINT. BLENDED DAMAGE ON GROUND PNEUMATIC DOOR, ORIGINAL T=.100 AFTER BLENDING T=.075, .025 MATERIAL LOSS, OUT OF LIMITS. FABRICATED NEW DOOR AND INSTALLED.SDR SCNA20160930200Beam · looseNR 6 FLAP FAIRING LOOSE AT AFT CENTER ATTACHMENT. REMOVED & REPLACED NR 6 FLAP FAIRING AFT ATTACH BEAM ASSY.SDR SCNA20160929199Skin · damagedLEFT WING AILERON UPPER SURFACE HAS SEVERAL AREAS OF EXPOSED COMPOSITE. REPAIRED THE LEFT WING AILERON UPPER SURFACE.SDR SCNA20160929198Trunnion · looseLEFT WING MAIN LANDING GEAR, FWD TRUNION RETENTION NUTS SEALENT DISBONDED OR MISSING 4 EA. NUTS. APPLIED FILLET SEAL TO SPECIAL WASHERS NUTS ON LH WINGS MLG, FWD TRUNION RETENTION NUTS.SDR SCNA20160929197Nose Cowl · damagedRT WING NR 2 ENGINE NOSE COWL, THUMBNAIL MATTING SURFACE HAS LIGHT WEAR AND MISSING PAINT. AREAS FROM 10 TO 2 O`CLOCK MARKED. REPAIRED NR 2 RIGHT WING ENGINE NOSE COWL.SDR SCNA20160929196Panel · looseRIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. FOUND HOLES TO BE ELONGATED ON UPPER SUPPORT BEAM AT RIGHT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL, CUT OUT DAMAGE AND ACCOMPLISHED REPAIR.SDR SCNA20160929195Panel · looseLEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL IS LOOSE. REMOVED 2 EACH RETAINERS ON LEFT WING TRAILING EDGE DEFLECTION CONTROL RIB PANEL. INSTALLED SERRATED PLATE AND REINSTALLED 2EACH RETAINERS.SDR SCNA20160929194Skin · delaminatedLEFT OUTBOARD AFT FLAP, INBOARD TRAILING EDGE CORNER HAS A SMALL AREA OF DELAMINATION. REPAIRED LEFT OUTBOARD AFT FLAP INBOARD TRAILING EDGE CORNER.
Back to N711SY, cancelled Mar 3, 2020