N758EV

Service difficulty reports · 295

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 = 'N758EV' 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 ASOA2015020412141Light · damagedEMERGENCY LIGHT DAMAGED AT SEAT 5AB & 6AB. R & R THE LIGHT IAW AMM 33-51-01.Jan 31, 2015 · N758EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2013120309521Frame · corrodedCORROSION ON FRAME, LBL 9 FS 286 UNDER TOP STRAP. REMOVED CORROSION IAW ASRM 51-21-06-001-001-A01. MAJOR REPAIR.Nov 14, 2013 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2013120309520Bulkhead · corrodedRT LOWER BULKHEAD WEB AT FS 280 IS CORRODED. REMOVED CORROSION ON RT LOWER BULKHEAD IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-11-594.Nov 14, 2013 · N758EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2013121609652Skin · chafedSKIN CHAFED AT BS 977, STRINGER 27, REPAIRED IAW EC/TC, REO 670-53-00-290 AND MODSUMIS 670538200021.Nov 11, 2013 · N758EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2013120309519Floorbeam · corrodedFS 280 FLOORBEAM CORRODED ON LT SIDE AT DRIP TRAYS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-43-101-001-A01. REPAIRED IAW SB670BA-53-041. MAJOR REPAIR.Nov 11, 2013 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2013120309518Floorbeam · corrodedFS 280 FLOORBEAM CORRODED ON RT SIDE AT DRIP TRAYS. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01 AND 53-21-43-101-001-A01. REPLACED FLOORBEAM IAW SB670BA-53-041. MAJOR REPAIR.Nov 11, 2013 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2013120309517Latch · lack of lubeDOOR FAILED FUNCTIONAL TEST OF THE PAX DOOR COMPLETE UNLOCK CYCLE, FORCE GAUGE WAS AT 20LB. AT END OF CYCLE. LUBRICATED PAX DOOR LATCH PINS AND LATCH CAMS IAW AMM 12-20-52-640-809. PERFOMED FUNCTIONAL CHECK OF PAX DOOR IAW AMM 52-11-00-720-801, FUNCTIONAL CHNov 9, 2013 · N758EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013120309516Handle · no testRT OVERWING EMERGENCY EXIT FAILED HANDLE PULL TEST. REMOVED SHOOT BOLT TO INSPECT LINK RODS IAW AMM 52-21-02-000-801. CLEANED AND INSPECTED SHOOT BOLTS AND LINK RODS WITH CONTACT CLEANER INSTALLED SAME SERVICEABLE SHOOT BOLTS IAW AMM 52-21-02-400-801 FUNCTIONov 9, 2013 · N758EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA2013091208986Lamp · burned outNR 5 EXTERIOR EMERGENCY LIGHT IS OUT. RELAMPED NR 5 EXT EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECKED GOOD.Sep 8, 2013 · N758EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2013082308905Hinge · chafedDURING PAX DOOR HINGE INSPECTION, FOUND CHAFING DAMAGE. REPAIRED IAW REO 670-52-11-511. MAJOR REPAIR IAW GMM 5-3.Aug 21, 2013 · N758EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2013071908737Megaphone · unserviceableMEGAPHONE UNSERVICEABLE. R & R MEGAPHONE IAW AMM 25-61-14.Jul 18, 2013 · N758EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013060603760Adc · malfunctionedEFIS COMPUTER MONITOR, IAS, ALT, HDG ON BOTH SIDES, STBY AIRSPEED ALSO FAILED, STALL FAIL, MACH TRIM CAUTION. R & R BOTH ADC'S IAW AMM 34-13-01-000-801, 400-801. R & R ISI IAW AMM 34-12-01-000-801, 400-801.Mar 18, 2013 · N758EV · Cndair CL6002C10 · Attitude and Direction Data SystemSDR ASOA2013012402899Door · bindingGATE ON ARRIVAL F/A UNABLE TO OPEN DOOR. HANDLE STUCK/DIFFICULT TO MOVE. OPENED AFTER MULTIPLE ATTEMPTS: HANDLE STICK BINDING. OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECK GOOD, NO FURTHER ISSUES AT THIS TIME.Jan 21, 2013 · N758EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012111402463Bracket · crackedFWD STOP BRACKET ON DOOR SURROUND STRUCTURE IS CRACKED. R & R FWD STOP BRACKET ON DOOR SURROUND STRUCTURE IAW SRM 51-41-20.Nov 10, 2012 · N758EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012110902456Lamp · burned outCEILING EMERGENCY LIGHT AT ROW 6 INOPERATIVE. RELAMPED CEILING EMERGENCY LIGHT AT ROW 6 IAW AMM 33-51-09, OPS CHECKED GOOD.Nov 6, 2012 · N758EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201200490Megaphone · unserviceableMEGAPHONE MISSING HARDWARE. R & R MEGAPHONE IAW AMM 25-61-14. OPS CHECKED GOOD.Feb 13, 2012 · N758EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201200488Lamp · burned outCABIN CEILING EMERGENCY LIGHT NR 5 INOPERATIVE. RELAMPED CABIN CEILING EMERGENCY LIGHT NR 5 AS REQUIRED. OPS CHECKED GOOD IAW AMM 33-51-00.Feb 13, 2012 · N758EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201200486Connector · disconnectedCABIN CEILING EMERGENCY LIGHT NR 1 INOPERATIVE. FOUND NR 1 EMERGENCY CEILING LIGHT ELECTRICAL CONNECTER DISCONNECTED ON THE CEILING PANEL. RECONNECTED CABIN CEILING EMERGENCY CONNECTOR ON THE CEILING PANEL IAW AMM 25-26-05. OPS CHECKED GOOD.Feb 13, 2012 · N758EV · Cndair CL6002C10 · Light System WiringSDR ASOA201102402Control Unit · failedAFTER GEAR RETRACTION, RECEIVED AN ANTI-SKID OTBD CAUTION MESSAGE AND AN OTBD GROUND SPOILER FAULT STATUS MESSAGE. RAN QRH CHECKLIST. DECLARED EMERGENCY AND LANDED NORMAL. R & R RT OTBD TRANSDUCER IAW AMM 32-44-01.Dec 20, 2011 · N758EV · Cndair CL6002C10 · Brake Anti-Skid SectionSDR ASOA201102107Connector · looseRT MIDDLE EXTERIOR EMERGENCY LIGHT IS NOT LIGHTING DURING OPS CHECK. REPLACED LIGHT BULB IAW AMM 33-51-15-000-801 & 33-51-15-400-801. OPS CHECKED FAILED. FOUND LOOSE CONNECTION. RECONNECTED IAW ESPM 20-26-00, OPS CHECKED GOOD IAW AMM 33-51-00-710-801-A01.Nov 2, 2011 · N758EV · Cndair CL6002C10 · Light System WiringSDR ASOA201102089Battery Pack · intermittentEMERGENCY LIGHTS ILLUMINATE UNCOMMANDED. TROUBLESHOT EMERGENCY LIGHTS & VERIFIED DISCREPANCY TO BATTERY PACK NR 2 DISCONNECTED THEN RECONNECTED. CONNECTOR PL124P1/P2 PERFORMED SUCCESSFUL OPS TEST OF EMERGENCY LIGHTS SYS REF SSM 33-50-00; SCHEM 2 SHEET 3 AND ANov 1, 2011 · N758EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201102058Floorboard · crackedFWD EQUIPMENT COMPARTMENT RT FLOOR CRACKED ADJACENT TO ADG PUMP. REPAIRED IAW REO 670-57-11-509 AND GENERIC REO 670-53-15-509 REV--, DATED 07/06/2010 AS WRITTEN.Oct 29, 2011 · N758EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA201102045Seat Track · corrodedSEAT TRACK IS CORRODED BETWEEN FS 667.00 - 708.00. REPAIRED IAW REO 670-53-00-343 AND REO 670-53-00-343 REV.Oct 26, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201102033Stringer · corrodedSTRINGER 6RT BETWEEN FRAMES 333-349 CORRODED. REPAIRED IAW REO 670-53-21-744.Oct 24, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201102020Intercostal · corrodedINTERCOSTAL AT FS 364 S27R CORRODED. INSTALLED INTERCOSTAL IAW SRM 51-42-21-001-001 & 51-42-06.Oct 21, 2011 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201102014Stringer Splice · corrodedSTRINGER SPLICE 25R FS 319.70-333.00 CORRODED. REMOVED STRINGER SPLICE IAW SRM 51-42-06-001-001. INSTALLED NEW STRINGER SPLICE IAW SRM 51-42-00-001-001-A01.Oct 20, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201102011Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. REPAIRED IAW REO 670-53-11-047.Oct 19, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201102010Intercostal · corrodedINTERCOSTAL AT FS 364.00 S27L CORRODED. REMOVED CORRODED INTERCOSTAL, DRILLED AND INSTALLED NEW IAW SRM 51-42-06-001-001.Oct 19, 2011 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201102009Floor Support · crackedMAIN AVIONICS BAY FLOORBEAM ANGLE WHICH ATTACHES TO FS 280 CRACKED. REMOVED AND INSTALLED A SERVICEABLE FLOORBEAM ANGLE IAW SRM 51-42-06-0014-001-A01 AND 51-42-21-001-001-A01.Oct 19, 2011 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201101929Seat Track · corrodedSEAT TRACK AT 9 LBL BETWEEN FS 379 - 485 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-807. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101928Stringer · corrodedSTRINGER 26 RT BETWEEN FRAMES 333 AND 349 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINOct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201101927Stringer · corrodedSTRINGER 25 RT BETWEEN 319.7-333 HAS CORROSION AT SEVERAL RIVET SHANKS. REMOVED CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-21-06-001-001-A01. .018 MATERIAL REMOVED, NO DAMAGE ALLOWED IN THIS AREA IAW SRM. R & R STRINGER IAW SRM 51-42-06-001-001.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201101926Stringer · corrodedSTRINGER 26 RT BETWEEN FRAMES 295.00 AND 310.00 HAS CORROSION AROUND SEVERAL RIVET SHANKS. REMOVED CORROSION IAW 51-42-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING OS .042. DAMAGE Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201101925Frame · corrodedFS 319.70 FRAME CORRODED BETWEEN STR 26 AND 27 RT. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRMOct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201101924Frame · corrodedFS 275 FRAME CORRODED AT S29R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .048. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101-002-AOct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201101923Frame · corrodedFRAME CORRODED AT FS 319.70 AND BETWEEN STR 27 AND 26L. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MINIMUM MATERIAL REMAINING IS .046. BLENDED AREA FOUND TO BE WITHIN LIMITSOct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201101922Frame · corrodedFRAME CORRODED AT FS 310 AND ON BOTH SIDES OF STR 27. CORROSION REMOVED IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .047. BLENDED AREA FOUND TO BE WITHIN LIMITS IAW SRM 53-21-06-101Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201101921Web · corrodedRT 280 WEB IS CORRODED. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. REMOVED DAMAGED WEB IAW REO 670-53-11-594. INSTALLED WEB IAW REO 670-570-53-11-594.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201101920Attach Angle · corrodedATTACH ANGLE AT FS 280.00 BULKHEAD CORRODED. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND WITH IN LIMITS IAW SRM 53-00-00-101-001. APPLIED PRIMER AND PAINT IAW SRM 51-21-11-001-A01.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA201101919Web · corrodedLEFT BS 280, WEB CORRODED. FOUND TO BE OUT OF LIMITS. CUT-OUT AREA IAW REO 670-53-11-594. PERFORMED EDDY CURRENT INSPECTION IAW REO 670-53-11-594 & NDTM PART 1, 51-20-006. NO INDICATIONS NOTED. INSTALLED NEW WEB IAW REO670-53-11-594, STEPS 5-7.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201101918Floorbeam · corrodedCOCKPIT FLOORBEAM AT FS 280.00 IS CORRODED. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM 51-42-06-001-001.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201101917Floorbeam · corrodedBS 280 CROSSBEAM IS CORRODED. REMOVED AND REPLACED CROSSBEAM IAW SRM CH 51-42-06-001-001, 51-42-21-001-001 & REO 670-53-11-047.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201101916Seat Track · corrodedCABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 863-977. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101915Seat Track · corrodedCABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 708-761. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101914Seat Track · corrodedCABIN LT SIDE SEAT TRACK IS CORRODED BETWEEN FS 785-863. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101913Seat Track · corrodedLEFT SIDE SEAT TRACK IS CORRODED BETWEEN FS 677-708. REMOVED SEAT TRACK IAW AMM 53-0-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101912Seat Track · corrodedRIGHT SIDE SEAT TRACK IS CORRODED BETWEEN FS 863-977. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101911Seat Track · corrodedCABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 785-863. REMOVED IAW AMM 53-00-49-000-801. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101910Seat Track · corrodedCABIN RT SIDE SEAT TRACK IS CORRODED BETWEEN FS 708-761. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201101909Seat Track · corrodedRIGHT SIDE SEAT TRACK IS CORRODED BETWEEN FS 677-708. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801-A03. INSTALLED NEW SEAT TRACK IAW AMM 55-00-49-400-801.Oct 10, 2011 · N758EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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