N741EV

Service difficulty reports · 325

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 = 'N741EV' 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 ASOA2014080611013Floorbeam · corrodedRIGHT & LEFT 280 FLOORBEAM CORRODED. REMOVED RT 280 CORRODED FLOORBEAM AND REPLACED WITH SERVICEABLE RT 280 FLOORBEAM AS NEEDED IAW SB670BA-53-041, REV D. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014080611012Doubler · crackedASD PULL IN LEVER DOUBLER CRACKED INSIDE ACCESS PANEL, 832AR. R & R ASD PULL IN LEVER DOUBLER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01 AND AMM 51-42-21-001-001-A01 IAW DWG 601R318097. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014080411006Seat Track · corrodedRT SEAT TRACK BS 349-485 HAS CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-49-101-001, 51-21-00-001-001. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411005Seat Track · corrodedLT INBD SEAT TRACK BS 677-830 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411004Seat Track · corrodedLEFT INBD SEAT TRACK BS 581-677 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411003Seat Track · corrodedLT INBD SEAT TRACK BS 379-485 HAS CORROSION. R & R SEAT TRACKIAW SRM 53-00-49-001-001-A001 & AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411002Seat Track · corrodedRT SIDE SEAT TRACK BS 711-761 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-400-801 AND 53-00-49-000-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411001Seat Track · corrodedRT SIDE SEAT TRACK BS 677-711 HAS CORROSION. FOUND TO BE OUT-OF-LIMITS IAW SRM 53-41-49-11-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-001-801/53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080411000Seat Track · corrodedRT SIDE SEAT TRACK AT BS 485-578 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW SR, 53-31-49-101-001-A01. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801, AND 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080410999Seat Track · corrodedLT SIDE SEAT TRACK AT BS 573-708 HAS CORROSION. REMOVED & INSTALLED SERVICEABLE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080410998Seat Track · corrodedLT SIDE SEAT TRACK AT BS 677-708 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801 & 53-00-49-400-807.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080410997Seat Track · corrodedLT SIDE SEAT TRACK BS 708-752 HAS CORROSION. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080410996Seat Track · corrodedLT SIDE SEAT TRACK AT FS 785 - 863 CORRODED. REMOVED THE SEAT TRACK IAW AMM 53-00-49-000-801. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-49-101-001-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801.Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014080410995Hinge · gougedASD HINGE ACFT SIDE GOUGED AT AFT END BY ROLL PIN. ALL WORK ACCOMPLISHED IAW REO 670-53-21-582. RESTORED FINISH TO ASD HINGE IAW REO 670-53-21-582 AND ECTC REO 670-53-21-582. REPAIRED PASSENGER DOOR HINGE, FUSELAGE SIDE, IAW REO 670-53-21-582, REV A. THIS Jul 16, 2014 · N741EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2014080410994Intercostal · crackedASD INTERCOSTAL CRACKED INSIDE ACCESS PANEL 832BR. R & R ASD INTERCOSTAL IAW SRM 51-42-06-001-001-A01, SRM 51-42-06-13-001-001-A01 AND 51-42-21-001-001-A01 IAW DWG 601R31902. RESTORED FINISH IAW SRM 51-21-16-001-001-A01. THIS REPAIR IS CLASSIFIED AS A MAJORJul 16, 2014 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2014081311046Angle · corrodedSERVICE DOOR UPPER ANGLE CORRODED. REMOVED ANGLE IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED NEW ANGLE IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-15-001-001-A01. INSTALLED ANGLE IAW SRM 51-42-06-001-001-A01 AND DWG SH670-31996. MAJJul 15, 2014 · N741EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014081311045Intercostal · corrodedINTERCOSTAL CORRODED BETWEEN BS 310-319.70 STRINGER 20R. REMOVED CORROSION IAW SRM 51-21-03-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081311044Intercostal · corrodedINTERCOSTAL CORRODED BETWEEN BS 349-364 AT STRINGER 26 RT. FOUND TO BE OUT OF LIMITS. REMOVED THE INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 AND DWJul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081311043Frame · corrodedFRAME AT BS 310 CORRODED BETWEEN STRINGERS 25L-25R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014081311042Frame · corrodedFS 280 FRAME CORRODED BETWEEN STRINGERS 23RT-23LT. REMOVED CORROISON FROM FRAME IAW SRM 57-21-06-001-001-A01. MAJOR REPAIR.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014081311041Support · corrodedRT SIDE FWD SUPPORT JUST AFT OF BS 280 HAS CORROSION. CLEANED CORROSION AND FOUND AREA OUT OF LIMITS IAW SRM 51-21-06-001-001-A01. CUT AWAY DAMAGE IAW SRM 53-21-43-201-002-A01. MAJOR REPAIR.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014081311040Angle · corrodedASD SILL KICK PLATE ANGLE CORRODED. FOUND OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 AND 52-06-00-101-001-A01. REMOVED KICKPLATE ANGLE IAW SRM 51-42-06-001-001. DRILLED KICKPLATE ANGLE IAW SRM 51-40-11-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080611011Striker · corrodedSERVICE DOOR UPPER SEAL STRIKER CORRODED AT DRAIN HOLES. R & R CORRODED SERVICE DOOR LOWER SEAL STRIKER IAW SRM 51-42-06. LOCATED AND DRILLED NEW STRIKER SEAL IAW SRM 51-40-11-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA2014080611010Angle · corrodedCORRODED ANGLE AT BS 349, STR 20 RT. REMOVED CORROSION FROM ANGLE IAW SRM 53-21-101-002-A01. FOUND DAMAGE IS BEYOND THE ALLOWABLE LIMITS OF SRM 53-00-00-101-001-A01, ANGLE REPLACED.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080410993Frame · corrodedFRAME BS 333 CORRODED AFT SIDE BETWEEN S26L-26R. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014080410992Doubler · corrodedTCAS DOUBLER CORRODED BETWEEN FRAMES 295-310 AT STR 27. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR IAW SOP 5702. REMOVED CORRODED DOUBLER IAW SRM 51-42-06-001-001-A01. TRANSFERED HOLES TO NEW DOUBLER IAW SRM 51-42-06-001-001-A01. INSTALLED TCAS DOUBLER IAJul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014080410991Floorbeam · corrodedFWD FLOORBEAM ANGLE CORRODED AT BS 280. REMOVED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. INSTALLED NEW FLOORBEAM ANGLE IAW DWG PL CC670-34256 AND SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014080410990Stand Off · unsecureTWO STAND OFFS ARE UNSECURE ON FRAME BS 265 BETWEEN S24L-24R. BONDED THE STAND OFFS IAW SRM 51-22-00-001-001-A01. MAJOR REPAIR.Jul 15, 2014 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014080611009Skin · dentedLEFT ENGINE INLET COWL DENTED AT BOTTOM. FOUND DENTS TO BE OUT OF LIMITS IAW 54-11-01-101-A01. FINISHED MAPPING AND SUBMITTED FOR PERMANMENT REPAIR TO STS ENGINEERING. RECEIVED AND COMPLIED WITH EC/TC AND EA 32-2014-014.Jul 13, 2014 · N741EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR ASOA2014080410989Floor Panel · crackedFWD EQUIPMENT BAY FLOOR PANEL CRACKED RT SIDE BY ADG STOW PUMP APPROXIMATELY BS 193. REPAIRED IAW REO 670-53-11-509. MAJOR REPAIR.Jul 13, 2014 · N741EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014080410988Floor Panel · crackedFWD EQUIPMENT BAY FLOOR PANEL CRACKED LT SIDE APPROXIMATELY, BS 193. REPAIRED IAW EC/TC REO-670-53-11-509 AND GRO 670-53-11-509, REV B. MAJOR REPAIR.Jul 13, 2014 · N741EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014080611025Rub Strip · deterioratedLT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. COMPLIED WITH EC/TC, REO 670-57-61-006 PERMANENT REPAIR. COMPLIED WITH REO 670-57-61-006, REV D OF PERMANENT REPAIR. RECEIVED AND COMPLIED WITH ECTC REO 670-57-61-006-01.Jul 12, 2014 · N741EV · Cndair CL6002C10 · AileronsSDR ASOA2014080611024Rub Strip · deterioratedRT AILERON OTBD RUB STRIP REQUIRES PERMANENT REPAIR. PERMANENT REPAIR TO RT AILERON OTBD RUB STRIP IAW SRM 51-22-00. COMPLIED WITH REO 670-57-61-006, REV D FOR PERMANAENT REPAIR TO RT AILERON RUB STRIP.Jul 12, 2014 · N741EV · Cndair CL6002C10 · AileronsSDR ASOA2014041610356Megaphone · damagedMEGAPHONE SCREW RETAINERS DAMAGED. R & R THE MEGAPHONE IAW AMM 25-61-14 AND AIPC 25-61-14, FIG 1C, ITEM 5.Apr 12, 2014 · N741EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2013101409219Drag Angle · crackedPAX DOOR DRAG ANGLE CRACKED AT ASSIST PULLEY. REMOVED DAMAGED DRAG ANGLE (AFT SIDE) ON PAX DOOR IAW SRM 51-42-06 AND 51-42-13. DRILLED UP AND INSTALLED NEW DRAG ANGLE IAW SRM 51-42-13 AND 51-42-22.Oct 11, 2013 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA2013052403656Battery Pack · dischargedEMERGENCY LIGHTS LEFT ON, AND WILL NOT POWER UP. CHARGED BATTERY PACKS WITH APU POWER.May 20, 2013 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2013012502905Battery · dischargedAFT F/A FLASHLIGHT INOPERATIVE. R & R BATTERIES IAW AMM 25-60-00. OPS CHECKED GOOD AT THIS TIME.Jan 22, 2013 · N741EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012110902453Lamp · burned outCEILING EMERGENCY LIGHT AT ROW 15 INOPERATIVE. RELAMPED EMERGENCY LIGHT IAW AMM 33-51-09, OPS CHECKED GOOD.Nov 5, 2012 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012101702357Light · unsecureFLOOR LIGHT STRIP AT ROW 14 UNSECURE. R & R FLOOR LIGHT STRIP AT ROW 14 A & B IAW AMM 33-51-01.Oct 14, 2012 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012090502165Placard · missingPHOTOLUMINESCENT PLACARD ON THE RT SIDE OF GALLEY EMERGENCY EXIT DOOR IS MISSING INSTALLED PHOTOLUMINECENT PLACARD ON GALLEY SERVICE DOOR IAW AMM 11-30-00.Sep 1, 2012 · N741EV · Cndair CL6002C10 · Placards and MarkingsSDR ASOA2012061501802Wire · brokenG-1 GALLEY EMERGENCY LIGHT INOPERATIVE. TROUBLESHOT AN FOUND WIRE AT FORWARD EDIT LIGHT AT FWD SERVICE DOOR IS BROKEN. REPAIRED IAW ESPM 20-33-00. OPS TESTED GOOD IAW AMM 33-51-00-710-801.Jun 12, 2012 · N741EV · Cndair CL6002C10 · Light System WiringSDR ASOA2012061401798Frame · crackedFRAME 320.10 CRACKED. LOCATED, DRILLED, AND INSTALLED IAW SRM 51-42-06-001-001-A01.Jun 7, 2012 · N741EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201201763Floor Support · corrodedCABIN LT FLOOR SUPPORT JUST AFT OF FS 280.00 IS CORRODED. REMOVE CORROSION IAW SRM 51-21-06-001-001-A01. REMOVED CORROSION AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 53-21-43-101-001-A01. ALODINED, PRIMED AND PAINTED TREATED AREA AS REQUIRED IAW SRM 51-21-06Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201762Floor Support · corrodedRT FLOOR SUPPORT JUST AFT OF FS 349.00 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT 3. FOUND OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. REPAIRED REO 670-5Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201736Angle · corrodedVERTICAL ANGLE AT PAX DOOR IS CORRODED AROUND NUTPLATES ON INBD AND OTBD SIDES. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND IT TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 AND 51-21-06-001-001-A01. REMOVED ANGLE ANGLE IAW SRM 51-42-06-001-00Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201735Seat Track · corrodedSEAT TRACK RBL 9, FS 835 TO 980 IS CORRODED. R & R SEAT TRACK IAW AMM'S 53-00-49-000-801 AND 53-00-49-400-801.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201734Seat Track · corrodedSEAT TRACK LBL 9, FS 835 TO 990 IS CORRODED. R & R WITH NEW FLOOR SEAT TRACK IAW AMM 53-00-49-000-801-A01 AND 53-00-49-400-801-A03.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201733Angle · corrodedAFT CARGO DOOR LOWER SILL ANGLE CORRODED FROM BS 1000.00 - 1051.30. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURE UT-3. MIN MATERIAL REMAINING IS .034", ORIGINAL IS .063" MAJun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201732Sill · corrodedAFT CARGO BAY, LT FLOOR SILL SCREW HOLES CORRODED FROM FS 985 TO 1000. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063" Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201731Floor Support · corrodedAFT CARGO COMPT, RT FLOOR SILL SCREW HOLES CORRODED FROM FS 985 TO 1000. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLEND AREA IAW MAC NDT INSPECTION PROCEDURES UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL IS .063Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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