N755EV

Service difficulty reports · 255

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 = 'N755EV' 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 SWIA2019120246803Windshield · crackedLEST WINDSHIELD CRACKED IN FLIGHT. FLIGHT 3289 CLOSED THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 19994297 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH WINDSHIELD IAW TASK CARD. OPS CHECK GOOD NO LEAKS NOTED."Dec 2, 2019 · N755EV · Cndair CL6002C10 · Flight Compartment WindowsSDR SWIA2018102345163Frame · crackedRT FS220 FRAME HAS AN INDICATION .1" LONG AT THE 3RD FASTENER HOLE DOWN FROM STGR13A. (C-CHECK) 10/20/2018 REMOVED, DRILLED AND LOCATED, AND INSTALLED THE RT F. S. 220 UPPER FRAME SECTOR IAW SRM. NO LEAKS NOTED AT THIS TIME.Sep 28, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018102345160Frame · crackedLT FS235 FRAME HAS AN INDICATION .15" LONG AT THE INBD FASTENER HOLE ABOVE STGR13A. (C-CHECK) 10/20/2018 REMOVED AND REPLACED THE FS 235 FRAME PN CC670-34133-9 IAW AMM. NO LEAKS NOTED AT THIS TIME.Sep 28, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2018102345164Post · crackedONE CRACK INDICATION NOTED ON LBL30 POST ON FWD SIDE OF FS202 AT THE TOP OF I-BEAM (AFT WEB-FLANGE INTERSECTION) .400" LONG. (C-CHECK) 10/20/2018 REPAIRED ONE CRACK NOTED ON LBL30 POST ON FWD SIDE OF FS202 AT THE TOP OF I-BEAM (AFT WEB-FLANGE INTERSECTION) .40Sep 27, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018102345161Not Reported · dentedFIVE (5) DENTS FROM FS1162 TO 1181 BETWEEN STR 23L AND 25L. (C-CHECK) 10/20/2018 REPAIRED 5 DENTS FROM FS 1162 TO FS 1181 BETWEEN STR 23L AND 25L IAW REO.Sep 14, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WVER201807160245Panel · gougedPANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EC/TC EO CL600-2C-10-54-L05664 AND EO CL600-2C10-54-L05665.May 3, 2018 · N755EV · Cndair CL6002C10 · Standard Practices/StructuresSDR WVER201807160243Panel · gougedPANELS 443BB AND 443BT ARE GOUGED ON AFT END. REPAIRED PANELS 443BB AND 443BT IAW EXPRESS JET EC/TC`S EO CL600-2C10-54 L05664 AND EO CL6002C10-54-L05565.May 3, 2018 · N755EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR WVER201807160242Strap · crackedJOINT BS 909 AND AFT WING TO FUSELAGE FAIRING STRAP WAS CRACKED. FABRICATED A JOINT AND AFT WING TO FUSELAGE FAIRING STRAP IAW SNIEO CC670-39171 S01.May 3, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR 2018FA0000241Skin · damagedRIGHT EXTERNAL FUSELAGE SKIN SCRATCHED AN GOUGED BETWEEN FS 1015 AND FS 1027, STRINGERS 23R AND 26R. REPAIRED EXTERNAL SKIN IAW STS ENGINEERING SOLUTIONS, ENGINEERING AUTHORIZATION 43-2018-068. Apr 27, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR WVER2018FA0000256Stringer · corrodedSTRINGER 26L, FS 349 TO FS 364 CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED STRINGER 26L, FS 349 TO FS 364 IAW SRM TASKS 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01, 51-21-11-001-001-A01, 51-25-01-001-001-A01.Apr 25, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR WVER2018FA0000255Intercostal · corrodedINTERCOSTAL BETWEEN FS 349 TO FS 364 STRINGER 27L CORRODED ON FLANGE. NO DAMAGE ALLOWED IAW SRM 53-21-23-101-003-A01. REMOVED AND REPLACED INTERCOSTAL 27L BETWEEN FS 349 TO FS 364 IAW SRM TASKS 51-42-06-001-001-A01, 51-40-11-001-001-A01, 51-42-21-001-001-A01Apr 25, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WVER2018FA0000254Intercostal · corrodedINTERCOSTAL BETWEEN FS 349 AND FS 364 IS CORRODED. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Apr 24, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR WVER2018FA0000253Frame · corrodedFS 310 FRAME IS CORRODED BETWEEN STRINGERS 25L AND 25R. REPAIRED FRAME STA 310 IAW REO 670-53-21-799 BY COMPLYING WITH EC/TC REO 670-53-21-799-01.Apr 24, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR WVER2018FA0000252Frame · corrodedCORROSION ON FRAME AT FS319.70 BETWEEN STRINGER 27 AND 26L. REPAIRED FS 319 IAW REO 670-53-21-799 REV A BY COMPLYING WITH EC/TC REO670-53-21-799 02.Apr 24, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR WVER2018FA0000250Frame · corrodedFRAME 349 HAS CORROSION BETWEEN STRINGER 27 AND 26R AND BETWEEN 26L AND 25L. REMOVED AND REPLACED FRAME349, PN SH 670-30357-5 IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01.Apr 23, 2018 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR WVER2018FA0000251Intercostal · corrodedINTERCOSTAL BETWEEN FS 340 - FS 364 STRINGER 26L IS CORRODED ON FLANGE. REMOVED AND REPLACED INTERCOSTAL BETWEEN FS 349 - FS 364 AT STRINGER 26L IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-23-00-001-001-A01, 51-25-16-001-001-AApr 7, 2018 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201705291634Relay · brokenEMERGENCY LIGHTS COME ON WHEN IN THE ARM POSITION. REMOVED AND REPLACED THE RELAY K135 PCB5 (JB11) IAW ESPM 20-39-00, AND AMM 24-06-11, OPS CHECKED GOOD.May 29, 2017 · N755EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015110614001Light · malfunctionedSOME EMERGENCY LIGHT WILL NOT TURN OFF REGARDLESS OF EMERGENCY LIGHT SWITCH IN COCKPIT OR CABIN. AFTER BEING ONBOARD FOR 10 MINTS THEY NOW WOULDN'T STAY ON. MORE THAN 15 SECONDS. CHARGED EMERGENCY LIGHT & PERFORMED OPS CHECK IAW MM 33-51-00, OPS CHECK GOOD Nov 6, 2015 · N755EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015061113092Floor Panel · crackedRT COCKPIT FLOOR AT FS280, RBL36, APPROX, WAS FOUND TO BE CRACKED UPON REMOVAL OF RT 280. REPAIRED IAW ECTC EA 32-2015-217.May 31, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015061113091Floorbeam · crackedLEFT COCKPIT FLOORBEAM CRACKED AT LBL 12. REPAIRED IAW ECTC REO 670-53-11-896 AND RERO 670-53-11-896, REV.May 29, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015061913168Structure · corrodedCORROSION FOUND AT BS 333, RBL 9. REMOVED PACKER IAW 51-42-06-001-001-A01. REPLACED IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-25-126-001-001-A01.May 28, 2015 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015062313175Slider · gougedLT UPPER TRANSCOWL INBD & OTBD SLIDERS GOUGED. REMOVED SLIDERS, GOUGED AT LT UPPER INBD AND OTBD SIDES OF TRANSCOWL AND ALL SHARP EDGES AND SMOOTH AREAS IAW SRM 54-21-00-101-001-A01. COMPLIED WITH STS EA 32-2015-222, REV A DATED 6/2/2015, SECTION I PERMANAMEMay 27, 2015 · N755EV · Cndair CL6002C10 · Engine Thrust ReverserSDR ASOA2015061913167Bulkhead Web · corrodedRT BS 280, BULKHEAD WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REMOVED AND REPLACED THE BULKHEAD WEB, IAW SRM 53-11-10-201-003-A01, AND DWG CC67034170.May 27, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015061913166Bulkhead Web · corrodedLT BS 280 BULKHEAD WEB CORRODED. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-11-10-201-003-A01. REMOVED AND REPLACED THE BULKHEAD WEB IAW SRM 53-11-10-201-003-A01, & DWG CC670-34170.May 27, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, BulkheadSDR ASOA2015062313174Frame · corroded549 FRAME HAS CORROSION BETWEEN STR 18LT AND 19LT, JUST BELOW FLOOR. BLENDED AREA IN FRAME BS 549 BETWEEN STR 18 LT AND 19 LT IAW SRM 51-21-06-001-001-A01. FINISHED REMOVING CORROSION IAW SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-06-May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015061913165Seat Track · corrodedRT SIDE SEAT TRACK BS 485-581 HAS CORROSION. FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913164Seat Track · corrodedRIGHT SIDE SEAT TRACK BS 724.08-761.85 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01, FOUND TO BE OUT OF LIMITS IAW REO 670-53-00-013. REMOVED, FABRICATED, AND INSTALLED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-000-801-A03,May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913163Seat Track · corrodedRIGHT SIDE SEAT TRACK BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913162Seat Track · corrodedSEAT TRACK AT LBL 9 BS 485-581 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & AMM 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913161Seat Track · corrodedSEAT TRACK AT LBL 9 BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913160Seat Track · corrodedSEAT TRACK AT LBL 9 677-830.4 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, & AMM 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913159Seat Track · corrodedLT SIDE SEAT TRACK BS 830.4 - 953 HAS CORROSION. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A01.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913158Seat Track · corrodedLEFT SIDE SEAT TRACK AT BS 863 - 985 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND AMM 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913157Seat Track · corrodedSEAT TRACK RBL 9 BS 485-581 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913156Seat Track · corrodedSEAT TRACK, RBL 9, BS 581-677 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913155Seat Track · corrodedSEAT TRACK RBL 9 BS 677 - 830.40 HAS CORROSION. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, AMM 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913154Seat Track · corrodedSEAT TRACK, RBL 9 BS 830.40 - 953 FOUND CORRODED. R & R THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913153Angle · corrodedANGLE HAS CORROSION THAT ATTACHES TO FRAME BS 565, BETWEEN STRINGERS 18 AND 19 LEFT. REMOVED AND REPLACED THE ANGLE IAW SRM 51-42-06-0041-001-A01 AND 51-42-22-001-001-A01, SRM 51-42-06-001-001-A01 & SRM 51-42-22-001-001-A01.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015061913152Floorbeam · corrodedBS 280 FLOORBEAM CORRODED. THE FLOORBEAM WAS R & R IAW SB670BA-53-041.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA2015060913083Seat Track · corrodedLT SIDE SEAT TRACK BS 785.15-863 HAS CORROISON. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015060913082Seat Track · corrodedRT SIDE SEAT TRACK BS 785.15-969 HAS CORROSION. REPLACED IAW AMM 53-00-49-000-801-A03 AND AMM 53-00-49-400-801-A03.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015060913081Seat Track · corrodedSEAT TRACK AT LBL9 BS 364-485 HAS CORROSION. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV L.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015060913080Seat Track · corrodedLT SIDE SEAT TRACK 565-677 HAS CORROSION. REPAIRED IAW EC/TE REO 670-53-00-343 AND GREO 670-53-00-343, REV L.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015060913079Seat Track · corrodedLT SIDE SEAT TRACK BS 761.85-724.08 HAS CORROSION. REPAIRED IAW EC/TC REO 670-53-00-343 AND GREO 670-53-00-343, REV L.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015060913078Frame · corrodedFRAME BS 549 HAS CORROSION BETWEEN STRS 26L AND 25L, FWD CARGO UNDER FLOOR. REPAIRED IAW SRM 51-21-06-001-001-AO1, 51-31-00-101-003-A01 AND 51-21-16-001-001-A01.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015060913077Frame · corrodedBS 565 FRAME HAS CORROSION BETWEEN STRINGERS 18 AND 19LT, JUST BELOW FLOOR. REPAIRED IAW SRM 51-42-06-001-001-A01, SRM 53-37-06-101-002-AO1 AND SRM 51-21-16-001-001-AO1.May 23, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2015061913151Seat Track · corrodedSEAT TRACK, RBL 9, BS 349-495, CORRODED. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND 53-00-49-400-801-A03.May 22, 2015 · N755EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015061913150Floor Support · corrodedAVIONICS FLOOR SUPPORT ANGLE CORRODED AT 280.00. R & R AVIONICS FLOOR SUPPORT IAW DWG CC670-34010, REV J, SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01, 51-25-16-001-A01, 51-21-11-001-001-A01.May 22, 2015 · N755EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2015061913149Skin · chafedPANEL 443BB HAS CHAFE DAMAGE. BLENDED CHAFE DAMAGE TO A SMOOTH CONTOUR ON PANEL 443BB IN REF TO SRM 51-12-00-001-001-A01. BLENDED AREA IS OUT OF ALLOWABLE LIMITS IAW SRM 54-12-01-101-001-A01.May 22, 2015 · N755EV · Cndair CL6002C10 · Standard Practices/StructuresSDR ASOA2015061113090Floorbeam · corrodedAFT FLOORBEAM ANGLE AT FS 280, CORRODED. R & R IAW SRM 42-06-001-001-A01.May 22, 2015 · N755EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
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