N710EV

Service difficulty reports · 223

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 = 'N710EV' 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 ASOA2014101311404Support Angle · crackedBULKHEAD SUPPORT ANGLE CRACKED AT LBL 26, BS 280. REMOVED AND REPLACED THE BULKHEAD SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01, AND SRM 51-42-06-001-001-A01. MAJOR REPAIR.Sep 20, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014100811392Angle · corrodedPAX DOOR LOWER MID CAP ANGLE IS CORRODED AT INBD AND OTBD SIDE. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Sep 20, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014100811391Angle · crackedANGLE AT BS 280 IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-40-11-001-001-A01 AND SRM 51-12-13-001-001-A01.Sep 20, 2014 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014101511426Floorbeam · crackedLT COCKPIT FLOORBEAM ANGLE CRACKED AT BS 280. REMOVED LT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED LT COCKPIT FLOOR SUPPORT ANGLE. COMPLIED WITH REO 670-53-11-977. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.Sep 19, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014101511425Angle · crackedRT COCKPIT FLOOR SUPPORT ANGLE CRACKED AT BS 280. REMOVED RT COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED RT COCKPIT FLOOR SUPPORT ANGLE. COMPLIED WITH REO 670-53-11-977. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.Sep 19, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014102111462Structure · chafedPAX DOOR FWD OUTER CORNER CHAFED. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. BLENDED CHAFED AREA, FWD OUTER CORNER, OF PAX DOOR IAW SRM 52-11-01-101-001-A01 AND 52-00-01-101-001-A01 AND ASA 51-12-00, REV A.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102111461Fitting · crackedPAX DOOR FWD HAND RAIL STOP FITTING CHAFED AND GROMMET HOLE CRACKED. REMOVE CRACKED STOP FITTING IAW SRM 51-42-21-001-001-A01. LOCATED FASTENER HOLES IN NEW FITTING AND DRILLED TO SIDE IAW SRM 51-42-01-001-001. INSTALLED NEW FITTING IAW SRM 51-42-06-001-0Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014102111460Housing · gougedAFT CARGO DOOR HANDLE HOUSING GOUGED FROM HANDLE ALIGNMENT PIN, UPPER CORNER. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH ECTC REO 670-52-31-031, REV OF NOV 07. BLENDED DAMAGE ON AFT CARGO DOOR HANDLE HOUSING IAW REOSep 17, 2014 · N710EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014102111459Doubler · chafedREPAIR AT BS 977 STRINGER 27 IS CHAFED. REMOVED AND REPLACED THE REPAIR DOUBLER IAW SRM 51-42-20-001-001-A01 AND REO 670-53-00-922, REV-10-03-14.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014101511424Channel · corrodedJ CHANNEL AT BS 280 CORRODED. J CHANNEL REPLACED IAW SB 670BA-53-041.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014101511423Bulkhead Web · corrodedRT FS 280 BULKHEAD WEB IS CORRODED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01 REPAIR IAW REO 670-53-11-594-01. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV-. MAJOR REPAIR.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014101511422Bulkhead Web · corrodedFS 280, LT BULKHEAD WEB IS CORRODED. DAMAGE EXCEEDS ALLOWABLE LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED IAW REO 670-53-11-594-01. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594 REV. MAJOR REPAIR.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014101511421Door Sill · corrodedRBL 36 AT FS 649.0 AT SERVICE DOOR IS CORRODED ON DOOR SILL THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. DAMAGE IS FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-390. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014101511420Frame · corrodedBS 595 FRAME IS CORRODED AT STRINGER 27 IN AVIONICS BAY. REMOVED CORROSION FROM FRAME IAW SRM 51-21-06-001-001-A01.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014101511419Drag Angle · corrodedCRACK ON PAX DOOR AFT DRAG ANGLE. REMOVED PAX DOOR AFT DRAG ANGLE IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01. LOCATED DRILLED AND INSTALLED NEW DRAG ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-13-001-001-A01. MAJOR REPAIR.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014101511418Intercostal · crackedPAX DOOR ACCESS HOLE 832BR INTERCOSTAL CRACKED. REMOVED PAX DOOR INTERCOSTAL IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED FASTENERS HOLES IN NEW INTERCOSTAL IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. RECEIVED AND COMPLIED EO 25-2014-298 10/Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014101511417Stringer · crackedSTRINGER 3L HAS A CRACK AFT OF FS 280, BULKHEAD. COMPLIED EC/TC SB670BA-53-040 01, REV A. COMPLIED WITH REO 670-53-21-493, REV C.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014101311403Floorbeam · corrodedBS 280 FLOORBEAM IS CORRODED. REPLACED ON S/B 670BA-53-041.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014101311402Frame · corrodedBS 319.7 AT STRINGER 27 IS CORRODED IN AVIONICS BAY. BLENDED CORROSION IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014101311401Frame · corrodedBS 310 AT STRINGER 27 IS CORRODED IN AVIONICS BAY. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014100811389Angle · corrodedPAX DOOR UPPER MID CAP ANGLE IS CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00-101-001. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01, 51-41-02-001-001-A01, AND 51-40-11-001-001-A01.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014100811388Angle · corrodedPAX DOOR UPPER AFT CAP ANGLE IS CORRODED. REMOVED AND REPLACED THE CAP ANGLE IAW SRM 51-42-06-001-001-A01, SRM 51-40-11-001-001-A01.Sep 17, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014101311400Frame · corrodedBS 333 AT STRINGER 27 IS FWD AVIONICS BAY IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MAJOR REPAIR.Sep 16, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014101511416Door Frame · corrodedMAIN AVIONICS BAY DOOR CUT OUT FWD SIDE HAS CORROSION BETWEEN STR 25R AND STR 25L WHERE THE DOOR SEAL CONTACTS THE FUSELAGE. REMOVED CORROSION AT FWD SIDE AVIONICS DOOR CUTOUT IAW SRM 51-21-06-001-001-A01.Sep 15, 2014 · N710EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014101311399Rub Strip · debondedLEFT AILERON TEFLON STRIP IS DISBONDED ON OTBD END. REPAIRED IAW REO 670-57-61-006-01, REV E.Sep 15, 2014 · N710EV · Cndair CL6002C10 · AileronsSDR ASOA2014102111465Panel · crackedPAX DOOR AFT SIDE PANEL AT TOP STEP AND MID STEP CORNERS CRACKED. REMOVED AFT SIDE PANEL FROM PAX DOOR IAW SRM 51-42-06-001-001-A01. INSTALLED AFT SIDE PANEL TO PAX DOOR IAW SRM 51-42-06-001-001-A01.Sep 14, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014091011201Handle · crackedINNER PAX DOOR HANDLE CRACKED IN 3 PLACES ON SHAFT FITTING. R & R PAX DOOR INNER PULL HANDLE WITH NEW IAW AMM 52-11-02. MAJOR REPAIR IAW GMM 5-3.Sep 7, 2014 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014072510965Flashlight · inoperativeF/A REPORTS AFT FLASHLIGHT DOES NOT WORK. R & R AFT FLASHLIGHT IAW GMM-3-8.Jul 21, 2014 · N710EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014052910606Retainer · damagedFWD CARGO DOOR LOWER SEAL RETAINER DAMAGE. COMPLIED WITH EC/TC, REO 670-52-35-127-01, PERMANENT REPAIR. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.May 25, 2014 · N710EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014052910605Megaphone · inoperativeMEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-14, REF IPC 25-61-14, FIG 1, ITEM 5.May 25, 2014 · N710EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013111809415Panel · crackedPAX DOOR FWD SIDE PANEL CRACKED AT THE TOP STEP. REPAIRED IAW REO 670R-52-11-705, REV B. MAJOR REPAIR IAW GMM 5-3.Nov 13, 2013 · N710EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013101409221Lamp · burned outAFT INTERIOR CEILING EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP IAW AMM 33-51-09, OPS CHECKED GOOD.Oct 12, 2013 · N710EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012092502290Sill · corrodedAFT CARGO DOOR SILL CORRODED. REPAIRED IAW REO 670-53-61-901.Sep 11, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092602295Stringer · corrodedSTRINGER 18L HAS SEVERAL SMALL AREAS OF LIGHT CORROSION BETWEEN FS 319.7 AND 349. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01, REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 IAW SRM 53-21-23-000-A11.Sep 10, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012092502289Sill · corrodedSERVICE DOOR LOWER SILL ANGLE IS CORRODED FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01 DAMAGE IS MORE THAN 10 PERCENT THICKNESS OF MATERIAL. REMOVED SERVICE DOOR LOWER SILL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. INSTALLED Sep 10, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092502288Floor Support · corrodedFLOOR SUPPORT LBL 11, WC 71.10 AT FS 580 CORRODED. REMOVED FLOOR SUPPORT AT LBL11 IAW SRM 51-42-06-001-001-A01. INSTALLED NEW FLOOR SUPPORT AT LBL 11, FS 280 IAW SRM 51-42-13-001-001.Sep 5, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092502287Angle · corrodedSUPPORT ANGLE RBL 11, WC 71.10 AT FS 280 CORRODED. REMOVED SUPPORT ANGLE AT RBL 11 IAW SRM 51-42006-001-001-A01. INSTALLED SUPPORT ANGLE IAW SRM 51-42-13-001-001.Sep 5, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092502286Floorbeam · corrodedFWD BS 280 FLOORBEAM CORRODED. REMOVED FLOORBEAM AND ANGLE IAW SRM 51-42-06-001-001. LOCATED AND DRILLED NEW FLOORBEAM ANGLE IAW SRM 51-40-11-001-001. INSTALLED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001.Sep 5, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012092602294Frame · corrodedFOUND SIGNS OF CORROSION ON FWD FACE OF FRAME BS 319 BETWEEN STR 26-27L. REMOVED CORROSION IAW SRM 51-21-06-001-001 A01. FOUND BLEND AREA TO BE OUT OF LIMITS AT 12 PERCENT OF MATERIAL THICKNESS IAW SRM 53-21-06-101-002-A01. REO 670-53-21-887 --Sep 4, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012092602293Door Frame · crackedPAX DOOR FRAME FS 327.76 CRACKED, FOUND DURING CMS REMOVAL. REMOVED DOOR FRAME IAW SRM 51-42-06-001-001-A01/51-42-21-001-001-A01. INSTALLED DOOR FRAME IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Sep 4, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2012092502285Sill · corrodedLOWER SILL ANGLES ARE CORRODED. FOUND CORROSION ON SILL ANGLES TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED LOWER SILL ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED ANGLES IAW 51-42-06-001-001-A01 SRM.Sep 4, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092402273Angle · corrodedFOUR ASD HINGE SIDE L ANGLES ARE CORRODED. REMOVED FOUR ASD HINGE L ANGLES IAW SRM 51-42-06-001-001-A01. INSTALLED HINGE L ANGLES IAW SRM 51-42-06-001-001-A01.Sep 4, 2012 · N710EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2012092402272Floor Support · corrodedRT FLOOR SUPPORT FS 280.00 TO 319.70 IS CORRODED IN SERVERAL AREAS. INSTALLED REPAIR DOUBLER IAW SRM 51-42-06-001-001, 51-42- 13-001-001.Sep 4, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092402271Doubler · corrodedTCAS ANTENNA INTERNAL DOUBLER CORRODED AT CONNECTOR FS 303.00, STGR27. FOUND TCAS ANT DOUBLER EXFOLIATED. REMOVED CORRODED TCAS ANTENNA DOUBLER, LOCATED, DRILLED AND INSTALLED NEW SERVICABLE TCAS ANTENNA INTERNAL DOUBLER IAW SRM 51-42-06-001-001-A01. FOUND Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2012092402270Seat Track · corrodedSEAT TRACK HAS CORROSION FS 736.05 RT SIDE. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND INSTALLED SIDE SEAT TRACK IAW AMM 53-00-49-400-801.Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012092402269Seat Track · corrodedSEAT TRACK AT RBL 9, STA 421 CORRODED. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 AND REO 670-53-00-013, REV F. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012092402268Seat Track · corrodedSEAT TRACK AT LBL 9, BS 421 CORRODED. EVALUATED DAMAGE AND FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001-A01 AND REO 670-53-00-13, REF F. R & R NEW SEAT TRACK IAW AMM 53-00-49-400-801.Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012092402267Sill · corrodedAFT CARGO DOOR SILL CORRODED. REMOVED CORROSION IAW SRM 51-21-06-01-001-A01. COMPLIED WITH REO 670-53-61-901.Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092402266Sill · corrodedSERVICE DOOR SILL CORRODED. EVALUATED SERVICE DOOR SILL AND FOUND DAMAGE TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REMOVED SERVICE DOOR SILL ANGLE, MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE ALL WORK DONE IAW SRM 51-42-06-001-00Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012092402265Crossbeam · corrodedBS 280 CROSSBEAM CORRODED AT COCKPIT ENTRANCE. BS 280 CROSSBEAM EXFOLIATED AT CORRODED AREA BEAM FOUND TO BE OUT OF LIMITS IAW SRM 53-11-41-201-002-A01. COMPLIED WITH ECTC REO 670-53-11-047 AND REO 670-53-11-047, REV E.Aug 29, 2012 · N710EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
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