N740EV

Service difficulty reports · 282

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 = 'N740EV' 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 ASOA2014081411064Bracket · corrodedFWD LOWER BRACKET AT SERVICE DOOR BS 319.7 IS CORRODED. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED ANGLE IAW SRM 51-42-06-001-001-A01.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081411063Floorbeam · corrodedRT FLOORBEAM BS 280 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS. REPAIRED IAW ECTC REO 670-53-21-139.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081411062Floorbeam · corrodedBS 280 FLOORBEAM CORRODED AT MULTIPLE AREAS. FLOORBEAM WAS REPLACED.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081411061Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. R & R FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG CC670-34256.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014081411060Retainer · bentFWD CARGO DOOR OUTER SEAL RETAINER IS BENT AT FWD AND AFT LOWER CORNERS. REPAIRED IAW EC/TC REO 670-52-35-127 01 REV STEP 11.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014081411059Floor Panel · crackedLT SIDE BS 193, ELECTIRCAL BAY FLOOR PANEL CRACKED. REPAIRED IAW ECTC REO 670-53-11-509 AND GREO 670-53-11-509, REV B.Jul 18, 2014 · N740EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014081511089Skin · dentedDENT FOUND ABOVE AND LT OF FWD CARGO DOOR BETWEEN TWO REINFORCING PLATES. REPAIRED IAW EA 12-2014-171.Jul 16, 2014 · N740EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2013031303165Lamp · burned outAFT CEILING EMERGENCY FLOOD LIGHT INOPERATIVE. R & R LAMP. OPS CHECKED GOOD.Mar 9, 2013 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012072501969Bulb · burned outFWD FUSELAGE, EMERGENCY LIGHTS INOPERATIVE. R & R TWO FWD LIGHT ASSY BULBS. PERFORMED OPS TEST IAW AMM 33-51-15-710-801. OPS CHECKED GOOD.Jul 19, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012071901944Handle · out of adjustPASSENGER DOOR RELEASE HANDLE EXCEEDS MAXIMUM FORCE. ADJUSTED PASSENGER DOOR WITHIN SPECIFIED LIMITS IAW AMM 52-11-04-710-801 A01, 52-11-02-820-801 A01. 52-11-00-710-701-A01.Jul 16, 2012 · N740EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2012071901943Frame · corrodedCORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT.Jul 16, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012071901941Intercostal · corrodedCORROSION AT FS 364 RT INTERCOSTAL BETWEEN STRINGERS 27 & 26R. INSTALLED INTERCOSTAL AT FS 364 RT INTERCOSTAL IAW SRM 51-42-21-001-001.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801921Intercostal · corrodedCORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 26 & 27L.Jul 13, 2012 · N740EV · Cndair CL2151A10 · Fuselage Miscellaneous StructureSDR ASOA2012071801920Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 349-364.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801919Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 295 & 310.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801918Stringer Splice · corrodedSTRINGER SPLICE 26R FS 333, FOUND CORRODED OUT OF LIMITS. REMOVED AND REPLACED STRINGER SPLICE IAW SRM 51-42-06-001-001.Jul 13, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071901940Stringer · corrodedCORROSION ON STRINGER 25 RIGHT FROM FS 349 - 333. REMOVED CORROSION ON STRINGER AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED STRINGER 25R IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED & DRILLED NEW STRINGER IAW SRM 51-Jul 9, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071901939Frame · corrodedCORROSION ON FS 349 FRAME FROM STRINGERS 24-26 RIGHT. BLENDED CORROSION AND FOUND FRAME TO BE OUT OF LIMITS REF SRM 51-21-06-001-001 & SRM 53-21-06-101-006. REMOVED FRAME IAW SRM 51-42-06-001-001-A01 & 51-42-21-001-001-A01. LOCATED AND DRILLED NEW FRAMEJul 9, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012071801917Stringer · corrodedCORROSION AT FS 364 STRINGER 26L. INSTALLED NEW STRINGER 26L IAW SRM 51-42-06-001-001, A01 & DWG SH670-31372.Jul 9, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071901938Floor Support · corrodedLT AFT CARGO FLOOR SUPPORT UNDER PANEL 281JLF HAS SURFACE CORROSION BETWEEN FS 1015 TO 1045. REMOVED DAMAGE IAW SRM 51-12-00-001-001-A01. MEASURED AREA, ORIGINAL MATERIAL THICKNESS .063" BLEND DIMENSIONS : 5.3"X2.1X.035", .028" REMAINING; 2.7" X 1.4"X .005",Jul 5, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071901937Sill · crackedFWD EQUIPMENT COMPARTMENT RT SIDE, SILL UNDER THE ADG HYD PUMP IS CRACKED. REPAIRED IAW GREO 670-53-11-504 AND ECTC REO 670-53-11-509.Jul 3, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012072501968Frame · corrodedCORROSION ON FRAME AT FS 319 AND FROM STRINGERS 26L TO 26R. REMOVED CORROSION ON FRAME IAW SRM 53-21-06-101-002-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .042"7, ORIGINAL IS .050" MJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012072501967Support · corrodedCORROSION ON NLG NOSE JACK FITTING SUPPORTS (LT AND RT) BETWEEN FS 265.00 AND FS 280.00. BLEND DAMAGE FROM FITTING SUPPORTS DETERMINE REMAINING MATERIAL & SUBMIT TO THD REF SRM 51-21-06-001-001. STARTED BLENDING LT AND RT SIDE OF NOSE JACK SUPPORT FITTING IAJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071901936Frame · corrodedCORROSION AT FS 333 BETWEEN STRINGERS 26 AND 27 LEFT. BLENDED DAMAGE ON FRAME. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT PROCEDURE UT-3. MIN MATERIAL REMAINING IS .040" ORIGINAL IS .050" MATERIAL REMOVED IS .010" . REPAIRED IAW REO 670-Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2012071901935Intercostal · corrodedCORROSION AT FS 364 RT INTERCOSTAL BETWEEM STRG27 AND 26R. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801916Stringer · corrodedCORROSION AT FS 364 STRINGER 26L. CORROSION OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER IAW SRM 51-42-06-001-001-A01. DRILLED NEW STRINGER AND INSTALLED IAW SRM 51-42-06-001-001.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801915Intercostal · corrodedCORROSION AT FS 364 INTERCOSTAL BETWEEN STRINGERS 27 AND 26L. BLENDED CORROSSION AND FOUND OUT OF LIMITS REF SRM 53-21-23-101-003-A01 & SRM 51-21-06-001-001. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001 & SRM 51-42-21-001-001. INSTALLED NEW INTERCOSTAL IAJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801914Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 349 TO 364. CORROSION FOUND OUT OF LIMITS IAW SRM 53-21-03-101-006-A01. REMOVED STRINGER SPLICE AND SECTION OF STRINGER IAW SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER IAW SRM 51-40-11-001-001. INSTALLED STRIJul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012071801913Channel · corrodedCHANNEL CORRODED AT FS 305 AND S27 ABOVE ANTENNA. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-01-101-002-A01. R & R CHANNEL IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012071801912Stringer · corrodedCORROSION ON STRINGER 26R BETWEEN FS 295 AND 310. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND OUT OF LIMITS IAW SRM 53-21-03-101-003-A01. REMOVED STRINGER REF SRM 51-42-06-001-001. DRILLED NEW SECTION OF STRINGER 26R REF SRM 51-40-11-001-001.Jul 2, 2012 · N740EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA2012070901868Light · brokenLIGHT, AISLE WITH ARROW BROKEN AT END OF TRACK. RECEIVED NEW TRACK LIGHTING SEGMENT,Jul 2, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201201681Battery · dischargedEMERGENCY LIGHTS WILL NOT STAY ON WHEN SELECTED ON. CHARGED THE EMERGENCY LIGHT BATTERIES, OPS CHECKED GOOD IAW AMM 33-51-00, ACFT OK FOR SERVICE.May 24, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201200841Glowstrip · missingPHOTOLUMINESCENT FLOOR STRIP MISSING FROM GALLEY. INSTALLED SERVICEABLE EMERGENCEY FLOOR PATH MARKING AT GALLEY AREA IAW AMM 33-51-01 NO FURTHER DEFECTS NOTED.Mar 8, 2012 · N740EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201200839Placard · missingEMERGENCY EXIT PLACARD ON PAX DOOR MISSING. INSTALLED PLACARD IAW GMM 3-8.6Mar 8, 2012 · N740EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA201200268Warning Message · false activationON FINAL APPROACH IN MODERATE ICING CONDITIONS, RECEIVED LT WING ANTI ICE CAUTION MESSAGE. FOLLOWED QRH AND MESSAGE DID NOT EXTINGUISH. EMERGENCY DECLARED. PERFORMED RESET OF WING ANTI ICE SYSTEM IAW FIM 30-12-00, COULD NOT DUPLICATE MESSAGE. NO FURTHER Jan 23, 2012 · N740EV · Cndair CL6002C10 · Airfoil Anti/De-ice SystemSDR ASOA201200170Light · looseA SECTION OF THE EMERGENCY FLOOR LIGHTING RIPPED UP. R & R EMERGENCY LIGHT IAW AMM 33-51-11. ACFT OK FOR SERVICE.Jan 16, 2012 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100869Lamp · burned outEMERGENCY LIGHT ON CEILING PANEL ROW 15 INOP. R & R LAMP IAW CRJ 700 33-51-09. OPS CHECK GOOD PLACARD REMOVED DEFER CLEARED. (ITEM RESOLVE UNDER MDDR: 639804-2) R & R LAMP IAW CRJ 700 33-51-09. OPS CHECK GOOD PLACARD REMOVED DEFER CLEARED. (CLOSED)May 2, 2011 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100852Lamp · inoperativeEMERGENCY LIGHT ON CABIN CEILING INOPERATIVE, ROW 15. RELAMPED IAW 33-51-09, OPS CHECKED GOOD.Apr 28, 2011 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100033Lamp · burned outNR 6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT INOP. RELAMPED NR6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD. RELAMPED NR 6 AFT MOST CABIN CEILING EMERGENCY FLOOD LIGHT IAW AMM 33-51-09, OPS CHECK GOOD.Jan 5, 2011 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100032Lamp · burned outRT AFT EXTERIOR EMERGENCY LIGHT INOP. RELAMPED RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD. RELAMPED RT AFT EXTERIOR EMERGENCY LIGHT IAW AMM 33-51-15, OPS CHECK GOOD.Jan 5, 2011 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001708Glowstrip · damagedPHOTOLUMINESCENT TRACK ON LT SIDE JUST AFT OF EXIT ROW 12AB DAMAGED. R & R PHOTOLUMINESCENT TRACKS ON LT SIDE JUST AFT EXIT ROW 12AB IAW AMM 33-51-01.Nov 1, 2010 · N740EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA201001562Bulb · burned outLT AFT ENTERIOR EMERGENCY LIGHT INOP. R & R BULB IAW AMM 33-51-15, OPS CHECK GOOD IAW AMM 33-51-15. (CLOSED)Oct 13, 2010 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001495Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE, R & R FWD EXT BATTERY PACK IAW AMM 33-51-01. OPS CK GOOD. DEFER CLEAR, MCC NOTIFIED.Oct 3, 2010 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001494Battery Pack · inoperativeFWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. R & R FWD EXT BATTERY PACK IAW AMM 33-51-04 OPS CK GOOD DEFER CLEARED MCC NOTIFIED.Oct 3, 2010 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001493Light · inoperativeFWD EMERGENCY LIGHTS WILL NOT ILLUMINATE. ITEM TRANSFERRED TO ASA DMIL NR 568377-2 IAW CUSTOMER.Oct 3, 2010 · N740EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001473Doubler · corrodedSURFACE CORROSION ON UPPER FS 280.00 MODSUM DOUBLER PN BA670-30069-8. BLENDED CORROSION DAMAGE IS GREATER THAN 10 PERCENT OUT OF LIMITS REF SRM 53-00-00. FABRICATED NEW DOUBLER OUT OF 7075T62 .050 PO T000004626 IAW DWG BA670-30069, REV A. PRIMED & APPLIED PROSep 29, 2010 · N740EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001429Floorbeam · corrodedUPPER MODSUM DOUBLER AT LT FS 280 FLOORBEAM CORRODED. BLENDED CORROSION DAMAGE IS GREATER THAN 10 PERCENT OUT OF LIMITS REF SRM 53-00-00. FABRICATED NEW DOUBLER OUT OF 7075T62 .050 P/O T000004626 IAW DWG BA670-30069, REV A. PRIMED & APPLIED PROTECTIVE TOPCSep 21, 2010 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001428Stiffener · crackedRT LOWER FS 280 BULKHEAD WEB STIFFENER PN:CC670-34117-6 IS CRACKED AT LOWER FASTENER LOCATION. REMOVED STIFFINER AT RT FS 280.00 LOWER BULKHEAD RBL 26.00 IAW SRM 51-42-06. LOCATED AND DRILLED NEW STIFFENER REF SRM 51-40-11. REMOVED PNL 221BRF IAW AM 53-00-47-Sep 21, 2010 · N740EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA201001409Floorbeam · crackedFS 280.00, LT FLOORBEAM CRACKED. REMOVED LT FS280 FLOORBEAM IAW SRM 51-42-06 & 51-42-13. DRILLED-UP NEW FOORBEAM REF SRM 51-40-11-001-001-A01. NDT FLOORBEAM LT CUT LINE IAW NDTM 51-20-06. NO DEFECTS NOTED REF ATTACHED NDT REPORT. INSTALLED FLOORBEAM IAW SRMSep 19, 2010 · N740EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001408Intercostal · crackedPAX DOOR AFT INTERCOSTAL CRACKED LOWER AFT. REMOVED AFT DOOR CENTERING PLATE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01, PERFORMED GVI, NO DEFECTS NOTED. REMOVED LWR AFT INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. LSep 19, 2010 · N740EV · Cndair CL6002C10 · Passenger/Crew Doors
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