N709EV

Service difficulty reports · 197

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 = 'N709EV' AND registry_match = 'registration'
  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 ASOA2016040114679Battery Pack · dischargedEMERGENCY LIGHTS NOT WORKING, CHARGED AND PERFORMED OPS CHECK OF EMERGENCY LIGHTS IAW AMM 33-51-00. NO FURTHER DEFECT.Apr 1, 2016 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015101013879Battery Pack · dischargedCAPTAIN'S SIDE FLASHLIGHT IS NOT WORKING. R & R THE FLASHLIGHT BATTERIES IAW GMM. OPS CHECKED GOOD.Oct 10, 2015 · N709EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015050412733Glowstrip · missingON SERVICE DOOR, 6 IN GLOWSTRIP MISSING. R & R SERVICE DOOR AFT GLOWSTRIP IAW AMM 20-60-04.Apr 29, 2015 · N709EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015031912425Battery · inoperativeMEGAPHONE INOPERATIVE. R & R MEGAPHONE BATTERIES IAW 25-61-14, OPS CHECK GOOD.Mar 15, 2015 · N709EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2015020512153Battery Pack · dischargedEMERGENCY LIGHTS INOPERATIVE. CHARGED BATTERYS WITH SWITCH IN ARM POSTION. EMERGENCY LIGHTS CHECKED GOOD.Feb 1, 2015 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014110711611Flashlight · inoperativeF/A REPORTS FORWARD FLASHLIGHT IS INOPERATIVE. REPLACED FLASHLIGHT IAW AMM 25-61-00. OPS CHECKED GOOD.Nov 3, 2014 · N709EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014103111591Battery Pack · inoperativeFOUND AFT EMERGENCY LIGHTS INOPERATIVE. R & R NR 4 EMERGENCY POWER PACK & OPS CHECK GOOD IAW AMM 33-51-17, NO FURTHER FAULTS IPC 33-51-17, ITEM 6.Oct 30, 2014 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014102811525Connector · damagedFIRE SYSTEM FAULT STATUS MESSAGE MDC REPORTS LT ENGINE FIRE LOOP B OPEN. FOUND PUSHED BACK CONTACT ON CONNECTOR J551 PIN EE R & R CONTACT IAW ESPM 20-16-43, FIRE SYS FAULT IS GONE, COMPLIED WITH OPS TEST OF THE FIRE EXINGUISHER SYSTEM IAW AMM 21-10-00-710-80Oct 18, 2014 · N709EV · Cndair CL6002C10 · Fire Protection System WiringSDR ASOA2014102811526Tab · deterioratedTAB DETERIORATED. REPAIRED HORIZONTAL STABILIZER PIVOT FITTING ANTI-ROTATION TABS. REPAIRED IAW SB 670BA-55-012.Oct 15, 2014 · N709EV · Cndair CL6002C10 · Horizontal Stabilizer StructureSDR ASOA2014102811523Stringer · corrodedSTRINGER 27 CORRODED AT BS 280. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-03-101-002-A01. REMOVED AND REPLACED THE STRINGER IAW SRM 51-42-20-001-001-A01 AND 51-42-06-001-001-A01. MAJOR REPAIR.Oct 1, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014102811522Frame · corrodedCORROSION ON INTERIOR SIDE OF DOOR FRAME BS 311.75, 15 INCHES BELOW LOWER TENSION TIE BAR FWD FITTING TO 13 INCHES ABOVE LOWER TENSION TIE BAR FWD FITTING. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF LIMITS IAW SRM 52-00-01-001-Oct 1, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014102711519Skin · damagedRT WING LOWER SKIN INCOMING HOLE DIAMETER 0.398" AND 0.402" DO NOT AGREE WITH HOLE DIAMETER REQUIREMENT OF 0.3910"-0.3940" IAW SB670BA-53-020. COMPLIED WITH REO 670-57-21-742 REV P2 DATED SEP 29,2014.Sep 30, 2014 · N709EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014102711518Skin · corrodedASD DOOR INNER SKIN IS CORRODED OUT OF LIMITS IAW SRM 52-00-001-101-001-A01. REMOVED AND REPLACED IAW REO 670-52-11-793, REV.Sep 30, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102711517Skin · crackedFOUND A CRACK INDICATION IN RT WING LOWER SKIN. REPAIRED IAW REO 670-57-21-742, REV P1, P2, P3, P4, P5, P6, P7.Sep 25, 2014 · N709EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014102711516Skin · crackedONE CRACK INDICATION IN RT WING LOWER SKIN. REPAIRED IAW IAW REO 670-57-21-742, REV P1, P2, P3, P4, P5, P6, P7 AND P8.Sep 25, 2014 · N709EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014102711514Angle · corrodedAFTER REMOVAL OF PAX DOOR SILL ANGLE, TOP ANGLE FOUND LOWER CAP ANGLE TO BE CORRODED ALONG THE NUTPLATE HOLES AND NUTPLATES. CORROSION ON PAX DOOR LWR SILL ANGLE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01, REMOVE LOWER SILL ANGLE. REMOVED 2EA DOOSep 24, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711513Angle · crackedCRACK ON INNER ANGLE OF ATTACHMENT STRUCTURE FOR INNER DOOR LEVER. REMOVED AND REPLACED THE ANGLE, IAW PJ162163, SRM 51-42-06-001-001-A01, AND SRM 51-40-11-001-001-A01.Sep 23, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102711512Floorbeam · crackedFLOORBEAM ANGLE CRACKED BS 280 LBL 26. R & R CRACKED ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34117. MAJOR REPAIR.Sep 19, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102711511Plate · crackedFWD CARGO BAY DOOR LOWER PLATE IS CRACKED. REMOVED LOWER PLATE IAW AMM 52-35-07-000-802-A01. FITTED AND DRILLED NEW LOWER PLATE IAW DRN LE670-39647, SRM 51-40-11-001-001-A01. INSTALLED SERVICEABLE LOWER PLATE IAW AMM TASK 52-35-04-410-802.Sep 19, 2014 · N709EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014102711510Floorbeam · corrodedCORROSION ON FLOORBEAM AT BS 280, LBL 35. BLENDED DAMAGE AREA AND FOUND TO BE IN LIMITS IAW SRM 51-21-06-001-001.Sep 18, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102711509Bulkhead Web · corrodedLEFT BS 280, LOWER WEB IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REPAIRED IAW REO 670-53-11-594, DATED APR. 27, 2011.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014102711508Bulkhead Web · corrodedRIGHT BS 280 LOWER WEB IS CORRODED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CORROSION DAMAGE IAW SRM 51-21-06-001-001-A01. REPAIRED BLENDED AREA AT RT 280, LOWER WEB IAW SRM 53-11-10-201-003-A01, PARA 3.B (1)-3.C.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014102711507Door Frame · corrodedAVIONICS BAY DOOR CUT-OUT, ENTIRE CUTOUT, CORRODED. BLENDED CORROSION ALONG THE FWD EDGE OF THE AVIONICS BAY DOOR CUT OUT IN REF TO SRM 51-21-06-001-001-A01, CORROSION IN A NON DAMAGEABLE AREA. THIS REPAIR IS CLASSIFIED AS MAJOR REPAIR IAW SOP 5702. COMPLSep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014102711506Intercostal · corrodedINTERCOSTAL CORRODED AT S27R, BETWEEN BS 349 & 364. REMOVED CORROSION IAW 51-21-06-001-001-A01.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711505Frame · corrodedFRAME BS 333 CORRODED AFT SIDE AT STR 27. REMOVED CORROSION FROM FRAME 333 AT AFT SIDE OF FRAME ON STR 27 LOCATION IAW SRM 51-21-06-001-001-A01.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014102711504Frame · corrodedFRAME 319.70 CORRODED FWD SIDE BETWEEN STR 26RT-26LT. BLENDED OUT CORROSION ON FRAME ATTACH FLANGE AND IN RADIUS IAW SRM 51-21-06-001-001-A01 FRAME OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. BLENDED CORROSION ON FRAME 319.70 BETWEEN STR 27 AND 26L IAW SRM 5Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014102711503Skin Splice · corrodedCIRCUMFERENTIAL SPLICE JOINT AT FS 280 INNER SKIN CORRODED BETWEEN STR 24LT-24RT. REMOVED CORROSION AT FS 280 BETWEEN STR 27-26R AND BETWEEN STR 25R-24R IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION FROM FS 280, ST 26L-25L AND STR 26R-25R IAW SRM 51-21-06-Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014102711502Floor Support · corrodedFLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE CORRODED ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01 AND 51-42-21-001-001-A01.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711501Floorbeam · corrodedCOCKPIT FLOORBOARD 221ALF AFT FLOORBEAM ANGLE AT BS 280 CORRODED. REMOVED CORRODED ANGLE AND REPLACED IAW SB 670BA-53-041.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102711500Floorbeam · corrodedBS 280 FLOORBEAM RT SIDE CORRODED. REMOVED CORRODED FLOORBEAM AND REPLACED IAW SB670BA-53-041.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102711499Floorbeam · corrodedBS 280 FLOORBEAM LT SIDE CORRODED. REMOVED CORRODED FLOORBEAM AND REPLACED IAW SB670BA-53-041.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102711498Cover · damagedAPU STARTER POWER CABLES ABRADABLE SHEATH TORN. WRAPPED APU POWER CABLES WITH ELECTRICAL INSULATING TAPE IAW GREO 670-24-22-001, REV A. COMPLIED WITH GREO REO 670-24-22-001, REV A DATED 11-25-2010. REPAIRED APU POWER OUTPUT CABLE IAW REO 670-24-22-001, REVSep 17, 2014 · N709EV · Cndair CL6002C10 · APU System WiringSDR ASOA2014102711497Attach Angle · crackedPANEL 194AB, ATTACH ANGLE CRACKED LT MLG W/W. REMOVED ANGLE FROM ACFT AND FABRICATED NEW ANGLE IAW EA 32-2014-120, SECTION 1. COMPLIED WITH EA 32-2014-120, REV P1.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA2014102711496Doubler · gougedREPAIR DOUBLER GOUGED AT BS 977. REPAIRD IAW REO 670-53-00-421 REV-A MAJOR REPAIR.Sep 17, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711495Door Sill · corrodedDURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 349, LBL 35 SILL STRUCTURE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND DWG SH670-31810.Sep 16, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711494Door Sill · corrodedDURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 340 LBL 35.SILL STRUCTURE REMOVED AND REPLACED IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND DWG SH670-31810.Sep 16, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711493Door Sill · corrodedDURING AVDEC INSPECTION, FOUND CORROSION AT PAX DOOR AT BS 315, LBL 35 ON SILL STRUCTURE. REMOVED AND REPLACED THE DOOR SILL IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01 AND DWG SH670-31810.Sep 16, 2014 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014102711492Housing · gougedAFT CARGO DOOR HANDLE HOUSING GOUGED. REMOVED HANDLE IAW AMM 52-31-03-000-801 A01, DRILLED NEW SERVICEABLE HANDLE ASSY AND INSTALLED IAW SRM 52-31-03-400-801 A01 AND SRM 51-42-21-001-001-A01. MAJOR REPAIR .Sep 16, 2014 · N709EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014102311483Fitting · crackedREINFORCEMENT FITTING ON ASD FS 338.963 HAS CRACK ON REINFORCEMENT FITTING INSIDE PANEL 832AR. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CRACKED PULL IN CAM DOUBLER, PN 601R31-8094-2 IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01Sep 16, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102311482Vent · gougedASD VENT FLAP GOUGED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED GOUGED AREA OF ASD VENT FLAP IAW SRM 51-12-00-001-001-A01, TEMP REV 51-12-00-001-001-A01, TEMP REV 51-005D. REPAIR OF THE DAMAGE ON THE PRESSURE VENT ON PAX DOOOR IS COSep 16, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102311481Panel · crackedASD UPPER MID STEP AFT SIDE PANEL CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED AFT SIDE PANEL, PN 601R-31707-7 IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. NEW SIDE WALL PANEL TO BE INSTALLED.Sep 16, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102311480Panel · crackedASD BOTTOM STEP FWD SIDE PANEL CRACKED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. FWD SIDE PANEL, PN 601R317071-8, REMOVED IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. REMOVED SUPPORT STRUCTURE FROM SIDE PANEL SKIN IAW SRM 51-42-06-0Sep 16, 2014 · N709EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102311479Frame · gougedLEFT AFT CORE COWL MID FRAME GOUGED. REMOVED DAMAGE IAW SRM 54-13-00-101-001-A01. FROM AFDL 520336, Z MID JOINT OUT OF LIMITS DUE TO BLEND AREA WITHIN 2D OF FASTENER NEEDS TO BE SUBMITTED FOR REPAIR. RECEIVED AND COMPLIED WITH STS EA 32-2014-102, SECTION I-Sep 16, 2014 · N709EV · Cndair CL6002C10 · Nacelle/Pylon, Frame/Spar/RibSDR ASOA2014102211472Light · damagedEMERGENCY LIGHT BROKEN AND DEBONDED. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-01-000-801-A03 AND AMM 33-51-01-400-801-A03.Sep 15, 2014 · N709EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014102211471Skin · damagedRT ENGINE CORE COWL HAS CHAFE DAMAGE DUE TO CONTACT WITH GREEN HARNESS. REPAIRED IAW REO 670-54-23-959. MAJOR REPAIR.Sep 15, 2014 · N709EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR ASOA2014102211470Floor Panel · crackedFORWARD EQUIPMENT COMPARTMENT FLOOR CRACKED AT SIDE FS 193. REPAIRED IAW ECTC REO 670-53-11-509, REV A, REV. MAJOR REPAIR.Sep 15, 2014 · N709EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014102211469Floor Panel · crackedFORWARD EQUIPMENT COMPARTMENT FLOOR CRACKED LT SIDE, FS 193.00. REPAIRED IAW REO 670-53-11-509, REV B. MAJOR REPAIR.Sep 15, 2014 · N709EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014102411489Skin · dentedLEFT ENGINE LOWER FWD COWL DOOR DENTED. REPAIRED IAW EA 32-2014-098, REV 1R.Sep 14, 2014 · N709EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR ASOA2014102411488Attach Angle · crackedVERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED LT SIDE AT APPROX STR DATUM 55.62 PERCENT. FOUND TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. INSTALLED NEW SERVICEABLE ATTACH ANGLE IAW DWG JBA 670-23103, & SRM 51-42-06-001-001-A01 & 51-42-21-001-001-Sep 14, 2014 · N709EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR ASOA2014102411487Attach Angle · crackedVERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE CRACKED RT SIDE AT APPROX STG DATUM 55.62 PERCENT. EVALUATED DAMAGES TO BE OUT OF LIMITS IAW SRM 55-00-00-101-001. SUMITTED TO ENGINEERING FOR PERMANENT REPAIR DISPOSITION. THIS REPAIR IS CLASSIFIED AS A MAJOR RESep 14, 2014 · N709EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
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