N708EV

Service difficulty reports · 333

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 = 'N708EV' 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 ASOA2016051314871Intercostal · corrodedINTERCOSTAL BETWEEN BS 349 - 364, STR 27 HAS CORROSION. INTERCOSTAL FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACE THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01, & 51-42-21-001-001-A01.May 13, 2016 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2016051314870Frame · corrodedFRAME BS 319.7 HAS CORROSION BETWEEN STRINGERS 25 - 27R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. BLENDED AREAS ARE OUT OF LIMITS IAW SRM 53-21-06-101-002-A01. COMPLIED WITH EA 32-2016-084.May 13, 2016 · N708EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2016051314869Frame · corrodedFRAME BS 295 HAS CORROSION BETWEEN STRINGERS 24R - 26L. REMOVED CORROISON IAW SRM 51-21-06-001-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 53-21-06-101-002-A01. COMPLIED WITH STS EA 32-2016-083 ECTC REV O.May 13, 2016 · N708EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015112614132Battery Pack · dischargedEMERGENCY LIGHTS WILL NOT COME ON. RE-CHARGED EMERGENCY LIGHTS AND PERFORMED OPS CHECK IAW AMM 33-51-00. OPS CK GOOD.Nov 26, 2015 · N708EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015062613186Angle · chafedFOUND CHAFE DAMAGE TO CLIP, PN: MM670-36913-001, ATTACHED TO FS 1144.00 AND INTERCOSTAL. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3. RECIEVED AND COMPLIED WITH REO 670-53-61-1136, 06/25/2015. CHAFE DAMAGE TO CLIP, PN- MM670-36913-001. REMOVED AJun 25, 2015 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015062613185Intercostal · chafedFOUND CHAFE DAMAGE ON INTERCOSTAL, PN: MM670-36537-011. UPON FURTHER INSPECTION, FOUND DAMAGE TO BE OUTSIDE THE ALLOWABLE PARAMETERS OF GREO 670-53-61-292, REV C. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3. RECIEVED AND COMPLIED WITH REO 670-53-Jun 25, 2015 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015062613184Strap · chafedCHAFING ON FS 1144 AND STR 9L. RECEIVED REO 670-53-61-1135. C/W REO 670-53-61-1135. CUT AWAY DAMAGE AND REMOVED ALL BURRS AND SHARP EDGES AS SHOWN IN REO 670-53-61-1135. THIS HAS BEEN CLASSIFIED AS A MAJOR REPAIR IAW GMM 5-3. FABRICATED 3EA -1 FRAME STRAPJun 25, 2015 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015022512275Stringer · deterioratedSTRINGER 7L DAMAGE BETWEEN FS 1144.00 AND FS 1162.00 AT WATER INJECTION LINE. COMPLIED WITH EC/TC REO 670-53-61-292, REPAIR B LT-SIDE. THIS IS CONSIDERED A MAJOR REPAIR IAW GMM 5-3.Feb 24, 2015 · N708EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2014122211888Megaphone · inoperativeF/A MEGAPHONE INOPERATIVE. R & R MEGAPHONE IAW AMM 25-61-05.Dec 15, 2014 · N708EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014121511883Flashlight · inoperativeF/A FLASHLIGHT INOPERATIVE. REPLACED THE FWD F/A FLASHLIGHT ALL CHECKED GOOD IAW AMM 25-61-00.Dec 11, 2014 · N708EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014070110791Skin · gougedDURING WALK AROUND, FOUND A GOUGE BETWEEN STRINGERS 16 - 17L FWD OF BS 565. REPAIRED IAW REO 670-53-31-328. MAJOR REPAIR.Jun 24, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014070110790Door · lack of lubeRT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBRICATED RT OVERWING EMERGENCY EXIT IAW AMM 12-20-82-640-802. FUNCTIONAL TESTED GOOD IAW AMM 52-21-00-720-801.Jun 17, 2014 · N708EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA2014070110789Door · lack of lubeLEFT OVERWING EMERGENCY EXIT FAILED FUNCTIONAL TEST. CLEANED AND LUBRICATED RT OVERWING EMERGENCY EXIT IAW AMM 12-20-82-640-802. FUNCTIONAL TESTED GOOD IAW AMM 52-21-00-720-801.Jun 17, 2014 · N708EV · Cndair CL6002C10 · Emergency ExitsSDR ASOA2014070110788Skin · damagedLOWER WING PLANK HAS BURNED SKIN APPROX 21.4 FROM CENTERLINE STRAP AND APPROX 27" AFT OF FWD SKIN EDGE. COMPLIED WITH REO 67-57-00-053, REV 8.Jun 14, 2014 · N708EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014070110787Bushing · damagedLT AND RT SIDE STAY OTBD SPINDLE BUSHINGS HAVE GROOVES ON FLAT SURFACE. RECEIVED AND COMPLIED WITH ECTC REO 670-57-11-084 AND REO 670-57-11-084, REV A.Jun 13, 2014 · N708EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR ASOA2014070110786Floor Support · crackedRT COCKPIT FLOOR SUPPORT, RT SIDE, CRACKED. R & R RT COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.Jun 8, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014070110785Floor Support · crackedLT COCKPIT FLOOR SUPPORT, LT SIDE, CRACKED. R & R LT COCKPIT FLOOR SUPPORT IAW SRM 51-42-06-001-001 AND SRM 51-42-21-001-001.Jun 8, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014070110782Angle · corrodedPAX DOOR SILL CAP ANGLE CORRODED. R & R PAX DOOR SILL CAP IAW SRM 51-41-02, TASK 51-41-02-001-A01. REMOVED SILL CAP AT PASS DOOR IAW ARM 51-41-02, TASK 51-41-02-001-001-A01. LOCATED AND DRILLED SILL CAP IAW SRM 51-0-11 AND DWG SH670-31825.Jun 4, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014070110781Shim · corrodedSHIMS CORRODED AT RBL9 AND FS333. REMOVED PACKERS, DRILLED UP NEW PACKERS AND INSTALLED PACKERS IAW SRM 51-42-06-001-001-A01 AND DWG NR SH670-32167.Jun 4, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014063010776Structure · corrodedSHIMS AND TOP PLATE CORRODED AT RBL 9 AND BS 349. R & R PACKER IAW SRM 51-42-06-001-001, 51-23-00-001-001, 51-40-11-001-001, 51-25-16 AND DWG SH670-32167, 53-21-43-101-001.Jun 4, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014063010775Floor Support · corrodedENTRANCE STORAGE COMPARTMENT FLOOR SUPPORT CORRODED AT BS 310 AND RBL19. EVALUATED FLOOR SUPPORT IAW SRM 53-21-43-101-001. R & R FLOOR SUPPORT IAW SRM 51-42-21-001-001-A01 IAW DWG SH670-31754.Jun 4, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014063010774Floor Support · corrodedFLOOR SUPPORT CORRODED BETWEEN FS 280-319 ON RT SIDE. EVAUALTED PER GREO 670-53-00-390 AND FOUND TO BE OUT OF LIMITS. REMOVED FLOOR SUPPORT IAW SRM 51-47-06-001-001. LOCATED, DRILLED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01 AND SWG SH67Jun 4, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014063010773Door Frame · corrodedRT FS 280 DOOR FRAME CORRODED AT BOTTOM AFT CORNER. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-11-950.Jun 1, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014063010772Door Frame · corrodedLT BS 280, DOOR FRAME CORRODED AT BOTTOM AFT CORNER. . COMPLIED WITH ECTC REO 670-53-11-951. MAJOR REPAIRJun 1, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014063010771Angle · corrodedRT FS 280 BULKHEAD ANGLE IS CORRODED . R & R RT BULKHEAD ANGLE IAW SRM 51-42-06-001-001 AND SRM 51-42-13-001-001. MAJOR REPAIR.Jun 1, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014063010770Bulkhead · corrodedLT BS 280 BULKHEAD ANGLE IS CORRODED. R & R LT FS 280 BULKHEAD ANGEL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01.Jun 1, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014063010769Floor Support · corrodedFLOOR SUPPORT CORRODED. REMOVED FLOOR SUPPORT SRM 51-42-06-001-A01. REPAIRED IAW SB670BA-53-041.Jun 1, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014063010768Floor Support · corrodedAVIONICS BAY FLOOR SUPPORT CORRODED. R & R FLOOR SUPPORT IAW SRM 51-42-06-001-001 AND 51-42-21-001-001 AND DWG CC670-34256.May 31, 2014 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014063010767Bulkhead Web · corrodedLT BS 280 LOWER BULKHEAD WEB CORRODED. AND COMPLIED WITH ECTC REO 670-53-11-594 01 AND GREO 670-53-11-594, REV A. MAJOR REPAIR.May 31, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014063010766Bulkhead Web · corrodedRT BS 280 LOWER BULKHEAD WEB CORRODED. COMPLY WITH EVALUATION/REPAIR IAW SRM 53-11-10-201-003. DAMAGE BEYOND ALLOWABLE LIMITS IAW SRM 53-11-10-201-003. COMPLIED WITH EC/TC REO 670-53-11-594 AND GREO 670-53-11-594.May 31, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014063010765Floorbeam · corrodedBS 280 FLOORBEAM CORRODED ON TOP SURFACE. R & R IAW SB670BA-53-041.May 31, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014070110794Bushing · damagedLT AND RT SIDE STAY OTBD SPINDLE BUSHINGS HAVE GROOVES ON FLAT FACE. REPAIRED IAW EC/TC REO 670-57-11-084. MAJOR REPAIR.May 29, 2014 · N708EV · Cndair CL6002C10 · Wing Miscellaneous StructureSDR ASOA2014070110793Skin · damagedLOWER WING SKIN BURNED WS 21.4. REPAIRED IAW EC/TC REO 670-57-00-053. MAJOR REPAIR.May 29, 2014 · N708EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014070110792Skin · dentedDENT IN FUSELAGE BS 250 - 265, STRINGERS 23-24R. REPAIRED IAW EC/TC REO 670-53-11-948 MAJOR REPAIR.May 29, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014063010764Skin · dentedFWD FUSELAGE DENT BY NOSE JACK PAD AREA RT SIDE, OUTER DENTS. DENT/PROTRUSION WITHIN ALLOWABLE UNITS IAW SRM 53-11-01-101-008. PERFORMED EDDY CURRENT INSPECTION IAW NDTM PART 1, 51-20-006, NO INDICATIONS NOTED . MAJOR REPAIRMay 29, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014063010763Track · dentedCARGO DOOR FWD TRACK DENTED UPPER OUTER RAIL AFT. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. RECEIVED AND COMPLIED WITH EC/TC REO 670-53-62-0102.May 29, 2014 · N708EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA2014032610184Lens · misinstalledEMERGENCY EXIT SIGN BY FORWARD PASSENGER BOARDING DOOR HAS ARROW POINTING THE WRONG WAY. R & R EXIT SIGN LIGHT LENS, REF AMM 33-51-05. ACFT OK FOR SERVICE.Mar 22, 2014 · N708EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2014012309793Battery Pack · dischargedF/A FLASHLIGHT INOPERATIVE. R & R BATTERIES. OPS CHECKED GOOD IAW AMM 25-61-00.Jan 19, 2014 · N708EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013112109448Cable · bindingMAIN ENTRANCE DOOR HARD TO OPEN. R & R TOP CABLE ON PAX DOOR SUPPORT WHEEL, OPS CHECK GOOD IAW 52-11-13.Nov 17, 2013 · N708EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013071608686Megaphone · inoperativeMEGA PHONE INOPERATIVE. R & R MEGA PHONE IAW AMM 25-61-14 IPC REF 25-61-14 ITEM 5. NO FURTHER DEFECTS NOTED.Jul 12, 2013 · N708EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012061901812Sill · corrodedPAX DOOR SILL IS CORRODED. REPAIRED IAW REO 670-53-21-855 AND REO 670-53-21-855.Jun 11, 2012 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012061501800Stiffener · crackedBULKHEAD STIFFNER AT RBL 26 BS 280 BULKHEAD CRACKED, FOUND DURING WEB REMOVAL. REMOVED BULKHEAD STIFFENER AT RBL 26 FS280 IAW SRM 51-42-06. DRILLED NEW STIFFENER IAW SRM 51-40-11-001-001. OK TO INSTALL MAC42QC 06/09/12. INSTALLED BULKHEAD STIFFENER AT RBL Jun 11, 2012 · N708EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2012061401796Floorbeam · corrodedFORWARD FLOORBEAM ANGLE AT FS 280 CORRODED. REMOVED FWD FLOORBEAM ANGLE PER IAW SRM 51-42-06-001-001, 51-42-21-001-001, 51-42-22-001-001. INSTALLED NEW SERVICEABLE FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001, 51-42-21-001-001, 51-42-22-001-001.Jun 7, 2012 · N708EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012061901811Angle · corrodedTWO L ANGLES CORRODED INTERIOR SIDE OF PAX DOOR. REMOVED AND INSTALLED NEW L ANGLES IAW SRM 51-42-06-001-001-A01.Jun 6, 2012 · N708EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012061901810Seat Track · corrodedLEFT PAX CABIN SEAT TRACK, LBL 9 AT FS 379 TO FS 485 HAS CORROSION. CORROSION FOUND TO BE OUT OF LIMITS IAW SM 53-21-49-101-001-A01. R & R SEAT TRACK IAW AMM 53-00-49000-801.Jun 5, 2012 · N708EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012061901809Web · corrodedLT LOWER BS 280 WEB HAS MINOR CORROSION ON AFT SURFACE. REMOVED CORROSION IAW SRM 53-11-10-201-003-A01. REPAIR "A" DAMAGE EXCEEDS LIMITS OF THIS REPAIR .016" REMOVED .005 ALLOWED. REPAIRED WEB IAW REO 670-53-11-594.Jun 5, 2012 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012061901808Web · corrodedRT LOWER BS 280 WEB HAS MINOR CORROSION ON AFT FACE. REMOVED CORROSION IAW SRM 53-11-10-201-003-A01, REPAIR "A" DAMAGE EXCEEDS LIMITS OF THIS REPAIR. .009" REMOVED .005" ALLOWED. REPAIRED WEB IAW REO 670-53-11-594.Jun 5, 2012 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012061901807Angle · corrodedPAX DOOR IS CORRODED AND CRACKED ON FWD STEP RISER FAR BOTTOM STEP. REMOVED ASD FWD WEB ALL SUPPORT ANGLES, DRAG ANGLE, CENTER ANGLE, AND NUTPLATES IAW SRM 51-42-06-0001-001-A01, 51-42-21-001-001-A01, 51-45-00-0001-001-A01 AND 51-42-15-001-001-A01. INSTALLEJun 5, 2012 · N708EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012061901806Sill · corrodedSERVICE DOOR FLOOR SILL IS CORRODED. REMOVED CORROSION ON SERVICE DOOR FLOOR SILL. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-A01. REMOVED MOUNTING ANGLE (PN SH670-31996-3) AND LOWER SILL ANGLE (PN SH 670-31986-1) IAW SRM 51-42-06 AND 51-42-21. Jun 5, 2012 · N708EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012061401795Seat Track · corrodedFS 683 TO 834 RBL 9.0 SEAT TRACK CORRODED IN SEVERAL SPOTS. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. REMOVED AND REPLACED SEAT TRACK IAW SRM ASA AMM 53-00-49-000-801AND AMM 53-00-49-400-801.Jun 5, 2012 · N708EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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