N754EV

Service difficulty reports · 199

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 = 'N754EV' 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 ASOA2014122311945Skin · damagedAFT DRAIN MAST AFT AT MOUNT IN FUSELAGE IS DAMAGED. REPAIRED IAW REO 670-53-61-1108.Nov 26, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014122311944Bulkhead Web · corrodedBULKHEAD WEB BS 280 FOUND CORRODED. REPAIRED IAW REO 670-53-11-954 01 AND GREO 670-53-11-594, REV.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014122311943Bulkhead Web · corrodedBULKHEAD WEB BS 280 FOUND CORRODED. REPAIRED IAW REO 670-53-11-59401 AND GREO 670-53-11-594 REV.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2014122311942Angle · crackedBS 280 BULKHEAD ANGLE IS CRACKED. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01 AND SRM 51-40-11-001-001-A01.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311941Floorbeam · crackedRT COCKPIT FLOORBEAM CORRODED. REPAIRED IAW SRM 51-42-06-001-001-A01, DWG CC670-33052.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2014122311940Angle · crackedCOCKPIT FLOORBEAM ANGLE CRACKED. REPLACED THE ANGLE IAW SRM 51-42-06-001-001-A01.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311939Angle · corrodedKICKPLATE ANGLE BETWEEN S 310 - 349 IS CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE KICKPLATE ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311938Structure · corrodedRBL 9 FLOOR PACKER CORRODED AT BS 333. R & R FLOOR PACKER IAW SRM 51-42-06-001-001-A01.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311937Structure · corrodedRBL 9 FLOOR PACKER CORRODED AT FS 349. R & R FLOOR PACKER AT FS349 AND RBL 9 IAW SRM 51-42-06-001-001-A01.Nov 25, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311936Floor Support · corrodedRT FLOOR SUPPORT FROM BS 280 - 319 IS CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND OUT OF LIMITS IAW REO 670-53-00-390. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311935Floor Support · corrodedFLOOR SUPPORT BS 319 - 349 FOUND CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-002-A01. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311934Floor Support · corrodedFLOOR SUPPORT BS 310 - 349 FOUND CORRODED . REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-000-001-001-A01, 51-42-21-001-001-A01 AND 51-41-02-001-001-A01.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311933Seat Track · corrodedSEAT TRACK AT RBL 9 BETWEEN BS 485 - 581 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311932Seat Track · corrodedSEAT TRACK AT LBL 9 BETWEEN BS 581 - 677 CORRODED. FOUND SKIN BEYOUND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801A-063 AND AMM 53-00-49-400-801-A03, STEPS 4.B, 3,9-C.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311931Seat Track · corrodedSEAT TRACK AT RBL 9 BETWEEN BS 581 - 677 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311930Seat Track · corrodedSEAT TRACK AT RBL 9 BETWEEN BS 611 - 830 CORRODED. FOUND BEYOND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801A-063 AND AMM 53-00-49-400-801-A03, STEPS 4.B, 3, 9-C.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311929Seat Track · corrodedSEAT TRACK AT LBL 9 BETWEEN BS 611 - 830 CORRODED. FOUND BEYOUND ALLOWABLE LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACKIAW AMM 53-00-49-000-801A-063 & 53-00-49-400-801-A03, STEPS 4.B, 3, 9-C.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311928Frame · corrodedFRAME BS 250 S27 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2014122311927Skin · corrodedSKIN BS 280 S27 CORRODED . REMOVED CORROSION IAW SRM 51-21-06-001-001-A01.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014122311926Intercostal · corrodedCENTER RT LATCH PIN INTERCOSTAL BETWEEN BS 349 - 364 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED IAW SRM 51-42-21-001-001-A01 51-42-06-001-001-A01 AND DWG SH670-32075. MAJOR REPAIR.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2014122311925Seat Track · corrodedSEAT TRACK SEGMENT IS CORRDOED BEYOND LIMITS AT BS 349. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A02.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014122311924Skin · corrodedFUSELAGE SKIN UNDER AFT DRAIN MAST FOUND TO BE CORRODED. BLENDED DAMAGE IAW SRM 51-21-06-001-001. REPAIRED IAW EA 32-2014-208. MAJOR REPAIR.Nov 23, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014122311923Floor Panel · crackedLT SIDE FWD EQUIP BAY FLOOR PANEL CRACKED. REPAIRED IAW REO 670-53-11-509 AND GREO670-53-11-509. REV B. MAJOR REPAIR.Nov 21, 2014 · N754EV · Cndair CL6002C10 · Fuselage Floor PanelSDR ASOA2014122311951Skin · damagedAFT DRAIN MAST AFT RT MOUNT IN FUSELAGE IS DAMAGED. REPAIRED IAW REO 670-53-61-1108Nov 20, 2014 · N754EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA2014072510969Battery · inoperativeCABIN MEGAPHONE NOT WORKING. RESEATED AND SECURED LOOSE BATTERIES.Jul 23, 2014 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014030610075Circuit Board · failedEMERGENCY LIGHTS CYCLE ON AND OFF WITH EMERGENCY LIGHTS SWITCH IN THE ARM POSITION R & R PRINTED CIRCUIT BOARD ASSY JB-11, PCB5, IAW AMM 24-06-11, IPC 24-06-11 ITEM 40, OPS CHECK GOOD. PN ON AND OFF E520005-705A, SN ON E0102, SN OFFE0250.Mar 4, 2014 · N754EV · Cndair CL6002C10 · Light System WiringSDR ASOA2014030610072Safety Valve · failedCABIN ALT CAUTION MESSAGE AT FL 340. FOLLOWED QRH. UNABLE TO CONTROL CABIN PRESSURE, DIVERTED EMERGENCY DECLARED. INTEGRATED MDC. SAFETY VALVE 2 POSTED. R & R NR 2 SAFETY VALVE & OPS CHECKED GOOD IAW AMM 21-32-03, REF AIPC 21-32-03, ITEM 5.Mar 2, 2014 · N754EV · Cndair CL6002C10 · Cabin Pressure Control SystemSDR ASOA2013051603569Unknown · odorSTRONG ODOR LIKE BURNING RUBBER, REPORTED BY F/A AND PAX, ONCE DURING FLIGHT, THEN ON APPROACH AS FLAPS DEPLOYED TO 8 AND 45. ODOR ONLY IN FIRST CLASS CABIN. COULD NOT DUPLICATE BURN LIKE ODOR, RAN LT & RT PACKS WITH APU IAW AMM 21-51-00. NO DEFECTS NOTED. May 12, 2013 · N754EV · Cndair CL6002C10 · Air Distribution SystemSDR ASOA2013013102929Unknown · odorBURNING RUBBER OR CHEMICAL ODOR REPORTED IN CABIN DURING FLIGHT. COMPLIED WITH SL-21-028, NO DEFECTS NOTED.Jan 27, 2013 · N754EV · Cndair CL6002C10 · Air Distribution SystemSDR ASOA2012111602482Glowstrip · damagedFOUND GLOWSTRIP DAMAGED BETWEEN ROWS 15-17. REMOVED AND INSTALLED NEW GLOWSTRIP BETWEEN ROWS 15-17 IAW AMM 33-51-01-000-801 (A04) AND 33-51-01-400-801 (A04) NO DEFECTS NOTED.Nov 13, 2012 · N754EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2012111602481Battery Pack · inoperativeSEVERAL EMERGENCY LIGHTS INOPERATIVE. R & R BATTERY PACK IAW AMM 33-51-17-000-801 AND 35-51-17-400-801. PERFORMED OPS TEST OF THE EMERGENGY POWER SUPPLY UNIT IAW AMM 33-51-17-710-801. OPS CHECKED GOOD.Nov 13, 2012 · N754EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2012111602480Angle · corrodedCORROSION FOUND ON SILL ANGLE. BLENDED CORROSION AND FOUND ARE OUT OF LIMITS IAW SRM 53-21-23-001-002-A01. LOCATED AND DRILLED AND INSTALLED IAW SRM 51-40-06-001-001-A01 AND 51-42-06-001-001-A01 AND DWG SH670-31950. REPAIR CLASSIFIED AS MAJOR REPAIR.Oct 29, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012111602479Angle · corrodedLOWER SILL ANGLE CORRODED, GALLEY SERVICE DOOR SURROUND. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED LOWER SILL ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW SILL ANGLE IAW SRM 51-42-06-001Oct 29, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012111602478Sill · corrodedCORROSION ON SILL PLATE, RT SIDE FS 310 TO 319.7. FOUND TO BE OUT OF LIMITS, R & R FOUND TO BE SASTISFACTORY.Oct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012111402469Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT FS 349 TO 364. REMOVED CORROSION IAW SRM 51-21-06-001-01-A01. REMAINING MATERIAL THICKNESS OUT OF LIMITS IAW SRM 53-00-00-101-001-A01. CUT AWAY DAMAGED FLOOR SUPPORT ONLY AS SHOWN IAW REO 670-53-21-899. FOUND TO BE SATISFACTOOct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012110802452Seat Track · corrodedSEAT TRACK AT RBL 9 FS 844 TO 879 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000/400-801.Oct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012110802451Seat Track · corrodedSEAT TRACK AT RBL 9 FS 349 TO 355 CORRODED. R & R SEAT TRACK IAW AMM 53-00-49-000-801 AND AMM 53-00-49-400-801.Oct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012110802450Floorbeam · corrodedFLOORBEAM ANGLE FOR CRAWLWAY FLOOR PANEL 141ALF AT FS 280 CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. REMAINING MATERIAL THICKNESS IN 3 AREAS BEYOND LIMITS OF SRM 53-00-00-101-001. INSTALLED SEVICEABLE FLOORBEAM ANGLE IAW SRM 51-42-21-001-0Oct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012103102414Seat Track · corrodedRT SIDE WALL SEAT TRACK CORRODED AT FS 785. REMOVED CORRODED SEAT TRACK AND REPLACED WITH NEW ONE IAW AMM 53-00-49-000-801(A03) AND 53-00-49-400-801(A03).Oct 24, 2012 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012111402468Striker · corrodedSEAL STRIKER PLATE ON GALLEY SERVICE DOOR SURRROUND HAS CORROSION ON M INBD SURFACE AT WL71.970 BETWEEN FS319.70 AND FS349. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01. REMOVED SEAL STRIKER PLATE IAW SRM 51-42-06-001-001-A01Oct 23, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012110802449Seat Track · corrodedSEAT TRACK AT LBL 9, 477.4 TO 500 HAS CORROSION. AREA FOUND TO BE OUT LIMITS IAW 53-31-49-101-001-A01. REMOVED SEAT TRACK IAW 53-31-49-000-801-A01. INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 23, 2012 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012110802448Seat Track · corrodedSEAT TRACK AT LBL 9, FS 280 TO 477.4 HAS CORROSION ENTIRE LENGTH. REMOVED SEAT TRACK IAW AMM 53-00-49-000-801 (CONFIG A03). INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-400-801-A03.Oct 23, 2012 · N754EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2012111402467Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AT NOT PLATE LOCATION JUST AFT OF CARGO DOOR FS 1048. REMOVED CORROSION, .002 MATERIAL. REMOVED WITH .061 REMAINING IAW SRM 51-21-06-001-001-A01 JUST AFT OF CARGO DOOR FS 1048. COMPLIED WITH REO 670-53-61-915. FOUND TO BE SATOct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012111402466Sill · corrodedAFT CARGO DOOR SILL INBD FACE CORRODED AT 4 LOCATIONS AS MARKED BETWEEN FS 1000.00 TO FS 1045.00. REMOVED CORROSION ON AFT CARGO DOOR SILL AT 4 LOCATIONS WITH .008 BEING THE DEEPEST IAW SRM 51-21-06-001-001-A01. COMPLIED WITH REO 670-53-61-915. FOUND TO BOct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012110802447Floor Support · corrodedRT FLOOR SUPPORT IS CORRODED AT NUTPLATE POSITION FS 1030.00. REMOVED SURFACE CORROSION IAW MM 670-35404-003. DAMAGE DIMESIONS 1"X1.5"X.002" DEEP O .063" - 061" REMAINING. NO DAMAGE ALLOWED IAW SRM 53-61-43-101-001. COMPLIED WITH REO 670-53-61-916. FOUND Oct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2012110802446Floorbeam · corrodedLT SIDE FS 280 FLOORBEAM HAS CORROSION DAMAGE. CORROSION IS BEYOND REPAIRABLE LIMITS IAW SRM 53-00-00-101-001-A01. R & R FLOORBEAM. COMPLIED WITH REO 670-53-11-047, REV E DATED 08/13/2009. FOUND TO BE SATISFACTORY.Oct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012110802445Floorbeam · corrodedRT SIDE FS 280 FLOORBEAM HAS CORROSION DAMAGE. CORRODED BEYOND LIMITS IAW SRM 53-00-00-101-001-A01. REMOVED AND REPLACED FLOORBEAM. COMPLIED WITH REO 670-53-11-047, REV E DATED 08/13/2009. FOUND TO BE SATISFACTORY.Oct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012110802444Bulkhead · corrodedRIGHT SIDE SKID FS 280 BULKHEAD LOWER WEB CORRODED. CORRODED BEYOND LIMITS IAW SRM 53-11-10-201-003-A01. NDT NEW BULKHEAD LOWER WEB IAW REO 670-53-11-594. FOUND TO BE SATISFACTORY.Oct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2012110802443Floorbeam · corrodedFWD FLOORBEAM ANGLE AT FS 280 HAS CORROSION DAMAGE. REMOVED FWD FLOORBEAM ANGLE. LOCATED AND DRILLED FWD FLOORBEAM ANGLE IAW SRM 51-42-06-001-001. REPLACED FWD FLOORBEAM ANGLE IAW SRM 51-42-06 AND 51-42-21.Oct 22, 2012 · N754EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2012111402465Sill · corrodedGALLEY SERVICE DOOR FRAME SILL IS CORRODED FROM THE FWD DOOR FRAME TO THE AFT DOOR FRAME. MOUNTING ANGLE CORROSION FOUND TO BE OUT OF LIMITS. REMOVED OLD MOUNTING ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01. INSTALLED NEW MOUNTING ANGLE IAW SRMOct 20, 2012 · N754EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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