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 ASOA201201730Sill · corrodedAFT CARGO BAY, RT FLOOR SILL SCREW HOLES CORRODED FROM 1000 TO 1051.3. 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 .058" ORIGINAL IS .063" MJun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201729Sill · corrodedAFT CARGO BAY RT FLOOR SILL SCREW HOLES CORRODED FROM FS 1051.3 TO 1088.2. 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 .057" ORIGINAL IS .0Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201728Sill · corrodedAFT CARGO BAY , LT FLOOR SILL SCREW HOLES CORRODED FROM FS 1051.3 TO 1088.2. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF BLENDED AREA IAW MAC NDT INSPECTION PROCEDURE UT 3. MIN MATERIAL REMAINING IS .061" ORIGINAL Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201727Seat Track · corrodedSEAT TRACK RBL 27.00, FS 978 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802 AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201726Seat Track · corrodedSEAT TRACK LBL 9.0 FS 898 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201725Seat Track · corrodedSEAT TRACK RBL 9.0, FS 978 TO 1005 IS CORRODED. REMOVED SEAT TRACK IAW AMM 53-00-49-000-802, INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-802.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201201724Floor Support · corrodedRT FS 280.00 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. MATERIAL REMOVED 0.002" LESS 10 PERCENT IN LIMITS. PERFORMED LPI TYPE1 METHOD C ON BLEND AREA IAW SRM 51-12-00-001-001-A01 IAW MAC NDT PROCEDURE PT-1. NO INDICATIONS Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201723Web · corrodedRT FS 280.00 WEB AFT FACE HAS CORROSION. REPLACED BS 280 WEB IAW EC/TC REO 670-53-11-594 01.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201722Floor Support · corrodedCOCKPIT CENTER FLOORBOARD AFT SUPPORT FWD OF FS 280.00 HAS CORROSION. REMOVED FLOOR SUPPORT AND INSTALLED SERVICEABLE SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201721Web · corrodedLEFT FS 280.00 WEB AFT FACE HAS CORROSION. REPLACED WEB IAW EC/TC REO 670-53-11-594.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201720Floorbeam · corrodedFS 280.00 CROSSBEAM HAS CORROSION. REPLACED 280 CROSSBEAM IAW EC/TC REO 670-53-11-047.Jun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201201719Intercostal · corrodedCORROSION FOUND ON INTERCOSTAL AT FS 349-364 BETWEEN AND S26 AND 27R. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. LOCATED & DRILLED SERVICEABLE INTERCOSTAL IAW SRM TASK 51-40-11-001-001. TREATED & PRIMED HOLES IAW SRM 51-21-16-001-001. INSTALLED INTERCOSJun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201718Intercostal · corrodedCORROSION FOUND ON INTERCOSTAL AT FS 364 AND S26L. REMOVED INTERCOSTAL IAW SRM 51-42-06-001-001. LOCATED & DRILLED SERVICEABLE INTERCOSTAL IAW SRM TASK 51-40-11-001-001. TREATED & PRIMED HOLES IAW SRM 51-21-16-001-001. INSTALLED INTERCOSTAL IAW SRM TASKS DJun 1, 2012 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201201705Wire · brokenEMERGENCY LIGHT AT SERVICE DOOR EXIT, INOPERATIVE. FOUND BROKEN WIRE AT CONNECTOR BEHIND PANEL 232JZ. REPAIRED IAW ESPM 20-12-00. OPS TESTED GOOD IAW AMM 33-51-00-710-801.May 29, 2012 · N741EV · Cndair CL6002C10 · Light System WiringSDR ASOA201201362Connector · disconnectedEMERGENCY EXIT SIGN ON LT WINDSCREEN INOPERATIVE. CONNECTED CONNECTOR FOR THE EMERGENCY LIGHT IAW AMM 25-24-01. OPS CHECKED GOOD.Apr 23, 2012 · N741EV · Cndair CL6002C10 · Light System WiringSDR ASOA201201251Lamp · burned outRT OVERWING EMERGENCY EXIT DOOR LOWER EXIT SIGN HAS SEVERAL LIGHTS BURNED OUT. RELAMPED RT OVERWING EMERGENCY DOOR EXIT SIGN IAW AMM 33-51-11.Apr 11, 2012 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201200009Lamp · burned outRT AFT MOST EXTERNAL EMERGENCY LIGHT INOPERATIVE. RELAMPED RT AFT MOST EXTERNAL EMERGENCY LIGHT. OPS CHECKED GOOD IAW AMM 33-51-15.Dec 30, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201102437Lamp · burned outAFT MOST CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED AFT MOST CABIN CEILING EMERGENCY LIGHT. OPS CHECKED GOOD.Dec 27, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201102436Stop Fitting · crackedFWD STOP BRACKET CRACKED ON MAIN CABIN DOOR. REINSPECTED FWD STOP BRACKET ON MAIN CABIN DOOR IAW REO 670-53-21-765. NO FURTHER DEFECTS NOTED AT THIS TIME.Dec 25, 2011 · N741EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201102229Lens · missingEMERGENCY FLOOD LIGHT COVER MISSING. REPLACED LIGHT COVER IAW AMM 33-51-11.Nov 23, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201102061Connector · miswiredCEILING EMGENCY LIGHT AT ROW 4 OUT. REPINNED CONNETOR P357 IAW ESPN 20-26-00 OPS CHECKED GOOD. ACFT OK FOR SERVICE.Oct 30, 2011 · N741EV · Cndair CL6002C10 · Light System WiringSDR ASOA201101543Lamp · burned outNR 2 CABIN CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED NR 2 CABIN CEILING EMERGENCY LIGHT IAW AMM 33-51-09, OP'S CHECKED GOOD.Aug 20, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201101337Lamp · burned outRT SIDE AFT EXTERNAL EMEGENCY LIGHT IS OUT. RELAMPED RT SIDE AFT EXTERNAL EMEGENCY LIGHT. OPS CHECK GOOD IAW AMM 33-51-02. ACFT OK FOR SERVICE.Jul 15, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201100856Battery Pack · inoperativeNUMEROUS EMERGENCY LIGHTS OUT, INTERIOR/EXTERIOR. R & R THE NR 3 EPSU BATTERY PACK IAW AMM 33-51-17. OPS CHECKED GOOD.Apr 30, 2011 · N741EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201001714Crossbeam · corrodedFS 280 CROSSBEAM CORRODED IN SEVERAL PLACES. INSTALLED TEE BRACKETS AND COMPLIED WITH STEPS 9 TO 17 OF REO 670-53-11-047. ALL WORK DONE IAW REO 670-53-11-047. COMPLIED WITH EC/TC REO 670-53-11-047 AND REO 670-53-11-047, REV E.Nov 2, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001709Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. INSTALLED SIDE SEAT RAIL IAW 53-00-49-400-801.Nov 1, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001687Floorbeam · corrodedTEE ANGLES AT 280 RBL9 & LBL9 FWD FLOORBEAM TO 280 ATTACHED ANGLES CORRODED. REMOVED UNSERVICEABLE TEE ANGLES AND REPLACED WITH SERVICEABLE TEE ANGLES. ALL WORK DONE IAW SRM 51-42-21-001-001-A01 AND SRM 51-42-22-001-001-A01.Oct 28, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001686Floorbeam · crackedSUPPORT ANGLE FOR RT WEB AT FS 280, RBL26 FOUND CRACKED. R & R SUPPORT ANGLE FOR RT WEB AT FS280, RBL 26 IAW SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. (CLOSED)Oct 28, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001651Floor Support · corrodedCOCKPIT FLOOR SUPPORT CORRODED BEYOND LIMITS. REMOVED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01. INSTALLED COCKPIT FLOOR SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001650Web · corrodedRT FS 280 WEB CORRODED AT RBL 12. REMOVED WEB DAMAGED FROM CORROSION IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. RESTORED FINIOct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001649Web · corrodedLT FS 280 WEB CORRODED AT LBL 12. REMOVED DAMAGED WEB IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. DRILLED NEW WEB IAW SRM 51-40-11-001-001-A01. WEB. INSTALL LT FS280, AT INSTALLED WEB IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-13-001-001-A01. Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001648Crossbeam · corrodedFS 280, CROSSBEAM CORRODED IN SEVERAL PLACES. REMOVED DAMAGED CROSSBEAM IAW SRM 51-42-06 AND 51-42-21. CUT NEW CROSSBEAM IAW SRM 51-40-11-001-001-A01. COMPLIED WITH STEP 2 OF REO 670-53-11-047. NO INDICATIONS NOTED. COMPLIED WITH STEPS 3-7 OR REO 670-53-Oct 25, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001630Stringer · corrodedSTRINGER 26R CORRODED AT FS 303. REMOVED COATING. MEASURED CORROSION DAMAGE WITH DEPTH GUAGE (.033" MATERIAL LOSS) AND FOUND CORRODED AREA OUT OF LIMITS IAW SRM 51-21-00-AND SRM 53-00-00-101-001-A01. R & R STRINGER 26 RT FS 303.00 IAW SRM 51-42-06-002-001-AOct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201001629Frame · corrodedFRAME HAS CORROSION AT FS 310 AND BETWEEN STR 27 AND 26L. REMOVED COATINGS AND CORROSION IAW SRM 51-21-00-001-A01. BLENDED CORRODED AREAS IAW SRM 51-21-00-001-A01. PERFORMED UT THICKNESS MEASUREMENT ON BLEND AREA IAW MAC NDT INSP PROCEDURE UT-3 MINIMUN MATOct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001628Angle · corrodedANGLE HAS CORROSION AT FS 364.00 AND STR 26R. REMOVED CORROSION FROM ANGLE IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01. BLENDED AREA WITHIN ALLOWABLE DAMAGE LIMITS SRM 53-21-23-101-003-A01.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001627Intercostal · corrodedCORROSION ON INTERCOSTAL AT FS 364 AND STR 27RT. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01. BLENDED AREA FS 364 & STR 27R IS WITHIN ALLOWABLE DAMAGE LIMITS IAW SRM 53-21-23-101-003-A01.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201001626Intercostal · corrodedCORROSION ON INTERCOSTAL AT FS 364 AND STR 27L. REMOVED CORROSION FROM INTERCOSTAL IAW SRM 51-21-00-001-A01, SRM 51-42-06-001-A01.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201001625Floorbeam · corrodedCORROSION AT FS 280 ON FLOORBEAM ANGLE THAT SECURES THE FWD END OF FLOOR BOARD PANEL 131 ALF. REMOVED CORRODED SUPPORT ANGLE IAW SRM 51-42-06-001-001-A01 FOR SOLID RIVETS, IAW SRM 51-42-20-001-001-A01 FOR LOCK FASTENER, REMOVED NUT PLATES FROM CORRODED SUPPOROct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201001624Seat Track · corrodedSEAT TRACK HAS CORROSION FROM FS680-693 LBL 9.00 ON THE INSIDE AND OUTSIDE OF TRACK. REMOVED SEAT TRACK. TRIMMED NEW SEAT TRACK TO DIMENTIONS OF OLD SEAT TRACK & MATCH DRILLED SEAT TRACK IAW REO 670-53-00-074. INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001623Seat Track · corrodedSEAT TRACK HAS CORRSION FROM FS581-680 LBL 9.00 ON INSIDE AND OUTSIDE OF TRACK. REMOVED SEAT TRACK. TRIMMED TO FIT NEW SEAT TRACK AND CUT BACK SCALLOP FLANGE IAW THE ORIGINAL TRACK. LOCATED, DRILLED AND COUNTERSTRUCK. INSTALLED NEW SEAT TRACK IAW AMM 53-00Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001622Seat Track · corrodedSEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF SEAT TRACK FROM FS 581-693.00 RBL 9.00. REMOVED SEAT TRACK. TRIMMED TO FIT NEW SEAT TRACK AND, CUT BACK SCALLOP FLANGE IAW THE ORIGINAL TRACK. LOCATED, DRILLED AND COUNTERSUNK. INSTALLED NEW SEAT TRACK IAW Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001621Seat Track · corrodedSEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF SEAT TRACK FROM FS 485-FS 581 RBL 9.00. REMOVED SEAT TRACK. FITTED, TRIMMED, DRILLED & COUNTERSUNK IAW REPAIR EO 670-53-00-074, PARA 3. INSTALLED SEAT TRACK AT FS 485-FS 581 IAW AMM 53-00-49-000-801.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001620Seat Track · corrodedSEAT TRACK HAS CORRISON AT FS 364.00, RBL 9.00. SEAT TO BE REPLACED. (CLOSED)Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001619Seat Track · corrodedSEAT TRACK HAS CORROSION ON INSIDE AND OUTSIDE OF TRACK AT FS 349.00, RBL 9.00. REMOVED & INSTALLED SEAT TRACK AT FS 350-485, RBL 9.00 IAW AMM 53-00-49-400-801.Oct 19, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001613Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN FS 677.00 AND FS 712.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B)1. REMOVED & INSTALLED NEW SEAT TRACK 51-670-37509-1 IAW AMM 53-00-49-400-801.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001612Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN FS 712.00 AND FS 761.00 HAS CORROSION. CORROSION NOT WITHIN LINITS IAW SRM 53-31-49. REMOVED SEAT TRACK & INSTALLED AT RT FS 712-FS 761 IAW AMM 53-49-400-801.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001611Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49 PARA 3(B). REMOVED AND REPLACED SEAT TRACK IAW AMM 53-00-49-000-801.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001610Seat Track · corrodedRT SIDE SEAT RAIL BETWEEN FS 863.00 AND FS 969.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3(B) I. REPLACE SEAT TRACK IAW AMM 53-00-49-000-801.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001609Seat Track · corrodedLT SIDE SEAT RAIL BETWEEN FS 863.00 AND FS 969.00 HAS CORROSION. CORROSION ON SEAT TRACK IS NOT WITHIN LIMITS IAW SRM 53-31-49. REMOVED & INSTALLED SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201001608Seat Track · corrodedLEFT SIDE SEAT RAIL BETWEEN FS 785.00 AND FS 863.00 HAS CORROSION. CORROSION NOT WITHIN LIMITS IAW SRM 53-31-49, PARA 3 (B) REMOVED LT SIDE SEAT RAIL AND REPLACED IAW AMM 53-00-49-400-801.Oct 18, 2010 · N741EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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