N753EV

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 = 'N753EV' 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 SWIA2018112945287Structure · dentedONE DENT LOCATED RT SIDE FORWARD FUSELAGE. (C-CHECK) RO: 11/26/2018. REPAIRED DENT LOCATED AT RT SIDE FORWARD FUSELAGE REFERENCING REO 670-53-11-1451.Oct 22, 2018 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018112945286Structure · dentedONE DENT LOCATED RT SIDE FORWARD FUSELAGE. (C-CHECK) RO: 11/26/2018. REPAIRED DENT ON RT FWD FUSELAGE REF REO 670-21-1574.Oct 22, 2018 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2018112945291Access Panel · damagedLEFT WING LEADING EDGE ACCESS PANEL HAS DAMAGED SCREW HOLE. (C-CHECK) RO: 11/26/2018. REPAIRED SCREW HOLE ON LT LE WING PANEL REF REO 670-57-41-396.Oct 14, 2018 · N753EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2018062045155Bulb · inoperativePILOT REPORTED THE BACK OF EXIT SIGN WAS NOT ILLUMINATING ON THE INDICATOR PANEL. MX REMOVED AND REPLACED THE EXIT SIGN BULB AND OPS CHECKED GOOD. ACFT WAS APPROVED FOR RETURN TO SERVICE.Jun 15, 2018 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201706191698Support Fitting · corrodedRT SUPPORT FOR JACK PAD FITTING FOUND CORRODED BEYOND LIMITS WHILE GAINING ACCESS TO NLG JACK PAD FITTING. REMOVED AND REPLACED NOSE JACK PAD FITTING SUPPORT PER SRM 51-42-06-001-001-A01, 51-42-001-001-A01 AND DRAWING CC670-32050.Jun 19, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR ASOA201706181697Frame · corrodedFS 310.00 FRAME, STG 26L-26R CORRODED FWD & AFT. COMPLIED WITH EC/TC REO 670-53-21-1308 AND REO 670-53-21-1308 FOR REPAIR.Jun 18, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201706171695Angle · corrodedFS 265 FRAME, STR 26L - 26R CORRODED. EVALUATED DAMAGE AND DETERMINED CORROSION TO BE CONTAINED TO STIFFENING ANGLE AT FS 265. DAMAGE IS OUT OF LIMITS. REF SRM 53-00-00-101-001 A01. REMOVED STIFFENING ANGLE REF SRM 51-42-06-001-001 A01. DRILLED UP NEW STIFFENIJun 17, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, FrameSDR ASOA201706171692Angle · corrodedLOWER FS 280 FRAME FLOOR SUPPORT ANGLE CORRODED. REMOVED AND REPLACED UNSERVICEABLE 280 LOWER FRAME SUPPORT ANGLE WITH NEW SUPPORT ANGLE IAW SRM 51-42-06-001-001 A01 AND DRAWING CC670-34010. RESTORED CIC TO REPAIR AREA. REFERENCE: SRM 51-21-11-001-001 A01.Jun 17, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706171691Fitting · crackedSTUB FITTING CRACKED BY NOSE JACKPAD FITTING. REMOVED AND INSTALLED NEW STUB ASSY IAW SRM 51-42-13-001-001-A01.Jun 17, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706171690Fitting · crackedNOSE JACKPAD FITTING CRACKED. REMOVED AND INSTALLED NEW NOSE JACK PAD FITTING IAW SRM 51-42-21-001-001-A01, AMM 51-41-10-960-801-A01, AND DRAWING NR CC670-32050.Jun 17, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, Attach FittingsSDR ASOA201706171689Support · corrodedNOSE JACKING FITTING LT SUPPORT, FS265-FS280, CORRODED. REMOVED AND INSTALLED NEW SUPPORT FOR NOSE JACK PAD FITTING IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, AND DRAWING NR CC670-32-050Jun 17, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, Attach FittingsSDR ASOA201706161694Support Channel · corrodedIN FWD CARGO AREA STRUCTURE AROUND LOWER BEACON IS CORRODED. REMOVED CORROSION IN SUPPORT CHANNEL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF REWORK AREA IAW NDTM PT 1, 51-20-004-270-A01 MIN THICKNESS IS .054". NO DAMAGE ALLOWED. PERFORMJun 16, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706161693Support Channel · corrodedIN FWD CARGO AREA STRUCTURE AROUND ADF ANTENNA IS CORRODED. REMOVED CORROSION IN SUPPORT CHANNEL IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS INSPECTION OF REWORK AREA IAW NDTM PT 1, 51-20-004-270-A01 MIN THICKNESS IS .069". NO DAMAGE ALLOWED. PERFORMEJun 16, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706151680Frame · corrodedFS 364 FRAME STR 26L-25R CORRODED. REPAIRED FRAME BY COMPLYING WITH EC/TC REO 670-53-21-687 AND GREO 670-53-21-687 REVB DATED 06-06-2016.Jun 15, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, FrameSDR ASOA201706151679Panel · corrodedPAX DOOR FWD SIDE PANEL CORRODED SEVERAL AREAS. REMOVED AND REPLACED PAX DOOR FWD SIDE PANEL IAW SRM 51-42-06-001-001-A01 AND 51-42-13-001-001-A01.Jun 15, 2017 · N753EV · Bombdr CL6002D15 · Passenger/Crew DoorsSDR ASOA201706151678Skin · not reportedPERMANENT REPAIR REQUIRED ON LT LOWER WING PLANK FWD EDGE (FUR-57-00-00923). COMPLIED WITH PERMANENT REPAIR OF WING PLANK BY COMPLYING WITH EC/TC EA 20-2017-081, STS EA 20-2017-081, AND EC/TC FUR-57-00-00923.Jun 15, 2017 · N753EV · Bombdr CL6002D15 · Wing, Plate/SkinSDR ASOA201706141677Doubler · corrodedATC LOWER ANTENNA INTERNAL DOUBLER, FS 349 - FS 364 STR 26R CORRODED. REMOVED ATC 1 LOWER ANTENNA IAW AMM 34-54-04-000-801 A01. REMOVED ATC ANTENNA DOUBLER IAW SRM 51-42-06-001-001A01. ATC DOUBLER OUT OF LIMIT IAW SRM 53-21-01-101-006 A01. DRILLED NEW ATC ANTEJun 14, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, Plate/SkinSDR ASOA201706141676Landing · crackedRT TRU DOOR AFT LATCH ANGLE CRACKED ON THE TRU FLOOR. REMOVED AND REPLACED RT AVIONIC DOOR LANDING IAW SRM 51-42-06-001-001-A01, AND 51-42-13-001-001-A01. MAJOR REPAIR.Jun 14, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201706101655Crossbeam · corrodedFLOOR CROSSBEAM CORRODED AT FS 1051 RBL 27-RBL 40. BLENDED CORROSION IAW EA 38-2017-091 AND EC/TC EA 38-2017-091.Jun 10, 2017 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201706101654Stringer · corrodedSTR 27 CORRODED AT FS280-300. REMOVED CORRODED STRINGER AND INSTALLED NEW STRINGER IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, 51-25-06-001-001-A01 AND 51-25-16-001-001-A01.Jun 10, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201706081653Intercostal · corrodedINTERCOSTAL FS 349 - FS 364 STR 27 LT CORRODED. LOCATED & DRILLED NEW INTERCOSTAL & INSTALLED IAW SRM 51-40-11-001-001-A01 & SRM 51-42-06-001-001 & DRAWING SH670-32075.Jun 8, 2017 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201706061646Splice · corrodedSPLICE ANGLE, STG 26R, FS333 CORRODED. REMOVED AND REPLACED CORRODED SPLICE ANGLE STG 26R, FS333 IAW SRM 51-42-06-001-001-A01. ALL DEFECTS CORRECTED.Jun 6, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706061645Door Sill · corrodedLT FLOOR SILL CORRODED FROM FS 985-1000. COMPLIED WITH E/C T/C EA 32-2017-140 AND EA 32-2017-140 FOR REPAIR OF FLOOR SILL AT FS 985-1000 LT.Jun 6, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Miscellaneous StructureSDR ASOA201706041644Stringer · corrodedSTRINGER 26 RT FS 280 - FS 333 CORRODED. REMOVED AND INSTALLED NEW SERVICEABLE STRINGER 26 RT FS 280- FS 333 PER SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01,51-40-11-001-001-A01 AND DAW SH670-31634. THIS IS A MAJOR REPAIR.Jun 4, 2017 · N753EV · Bombdr CL6002D15 · Fuselage Main, Longeron/StringerSDR ASOA201706041643Intercostal · corrodedSUPPORT, FS 349- FS 364 STR 26 RT CORRODED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-40--11-001-001-A01 AND 51-42-06-001-001-A01 THIS IS A MINOR REPAIR.Jun 4, 2017 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201706031642Door Sill · corrodedSILL CORRODED AT FS319.70 TO 310.00 AND BETWEEN RBL40-43. REMOVED FLOOR SILL FROM FS280-319, RBL40 IAW SRM 51-42-06-001-001-A01. LOCATED AND DRILLED HOLES IN NEW FLOOR SILL IAW SRM 51-42-06-001-001-A01, 51-40--11-001-001-A01. ASSEMBLED AND INSTALLED RT FLOOR SJun 3, 2017 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201706031641Housing · crackedHOUSING AROUND CARGO DOOR HANDLE CRACKED (AFT). REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING IAW SRM 51-42-21-001-001-A01 AND 52-31-03-400-801-A01.Jun 3, 2017 · N753EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR ASOA201705311630Floorbeam · corrodedCORROSION FOUND ON THE FLOORBEAM ANGLE BS 280 BETWEEN LBL 9 AND RBL 9. R & R THE FLOORBEAM ANGLE IAW SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, & 51-40-11-001-001-A01.May 31, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR ASOA201705311631Seat Track · corrodedLEFT SEAT TRACK CORRODED, BS 785 - 863. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 31, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705311629Seat Track · corrodedLEFT SEAT TRACK CORRODED, BS 677 - 708. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 31, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705281628Seat Track · corrodedRIGHT SEAT TRACK CORRODED, BS 485 - 565. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 28, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705281627Seat Track · corrodedRIGHT SEAT TRACK CORRODED, BS 785 - 863. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 28, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705281626Seat Track · corrodedLEFT SEAT TRACK CORRODED, BS 485 - 565. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343, & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 28, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705281625Seat Track · corrodedLEFT SEAT TRACK CORRODED, BS 863 - 953. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 28, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705271624Seat Track · corrodedRIGHT SEAT TRACK CORRODED BS 349-485. FABRICATED A NEW SEAT TRACK IAW REO 670-53-00-343 & EC/TC REO 670-53-00-343. R & R THE SEAT TRACK IAW AMM 53-00-49-000/400-801.May 27, 2017 · N753EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201705241623Angle · corrodedCORROSION FOUND ON DOOR THRESHOLD ANGLE AT BS 280, RBL 9. R & R DOOR THRESHOLD ANGLE IAW SRM 51-42-06-001-001-A01, & 51-42-13-001-001-A01.May 24, 2017 · N753EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201705231621Post · corrodedLEFT FS 280 COCKPIT DOOR POST CORRODED AT THE LOWER CORNER. R & R THE POST AND REPAIRED ADDITIONAL DAMAGE IAW EA 32-2017-128, & EC/TC EA 32-2017-128. MAJOR REPAIR.May 23, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201705231620Post · corrodedRIGHT BS 280 COCKPIT DOOR POST CORRODED AT THE LOWER CORNER. R & R THE POST AND REPAIRED ADDITIONAL DAMAGE IAW EA 32-2017-129, & EC/TC EA 32-2017-129. MAJOR REPAIR.May 23, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201705191619Frame · corrodedBS 349 FRAME, STRINGERS 27 - 26R CORRODED, AFT SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK. FINISHED REPAIR IAW REO 670-53-21-1308 & EC/TC REO 670-53-21-1308.May 19, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201705191618Frame · corrodedBS 319.7 FRAME, STRINGERS 26L - 26R CORRODED, FWD & AFT SIDE. REMOVED CORROSION IAW SRM 51-21-06-001-001-A01. PERFORMED UT THICKNESS CHECK. FINISHED REPAIR IAW REO 670-53-21-1308 & EC/TC REO 670-53-21-1308.May 19, 2017 · N753EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA20160901002Light · wornEMERGENCY FLOOR LIGHT NEAR CLOSET IS WORN OUT. MAINTENANCE R & R EMERGENCY FLOOR LIGHT STRIP AT FWD CLOSET IAW AMM 33-51-01. AIRCRAFT OK FOR RETURN TO SERVICE.Sep 1, 2016 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016090115331Light · deterioratedEMERGENCY FLOOR LIGHT NEAR CLOSET IS WORN OUT. R & R EMERGENCY FLOOR LIGHT STRIP AT FRONT CLOSET IAW AMM 33-51-01.Sep 1, 2016 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2016080115150Lens · brokenLEFT AFT EXTERIOR EMERGENCY LIGHT LENS BROKEN. REMOVED AND REPLACED THE EXTERIOR EMERGENY LIGHT LENS IAW CMM 33-52-07.Jul 28, 2016 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015120514144Lens · brokenRIGHT OVERWING EMERGENCY EXIT LIGHT COVER BROKEN. R & R RT AFT OVERWING EMERGENCY EXIT LIGHT COVER AND PERFORMED OPS CHECK IAW AMM 33-51-15. OPS TEST GOOD AT THIS TIME.Dec 5, 2015 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015111414033Light · inoperativeROW 9 CEILING EXIT LIGHT INOPERATIVE. R & R CEILING EXIT LIGHT IAW AMM 33-51-09. OPS CHECK GOOD.Nov 14, 2015 · N753EV · Cndair CL6002C10 · Emergency LightingSDR ASOA2015100613870Latch · out of adjustSERVICE DOOR WILL NOT CLOSE, HARD TO OPEN. COMPLIED WITH INSPECTION OF SERVICE DOOR LATCH ASSY FOUND UNLOCK CRANK LOOSE. RECONNECTED UPLOCK CRANK TO PUSH ROD CW, OPS OF DOOR LOCKING MECHANISM CHECK GOOD IAW AMM 52-41-02. OPS IAW 52-41-00, ITEM CLEARED PLACAOct 6, 2015 · N753EV · Cndair CL6002C10 · Service DoorsSDR ASOA2014102311476Megaphone · intermittentMEGAPHONE WORKING INTERMITTENTLY. R & R MEGAPHONE IAW AMM 25-61-14, IPC REF 25-61-14 FIG 1C, ITEM 5. ACFT OK FOR SERVICE.Oct 18, 2014 · N753EV · Cndair CL6002C10 · Emergency EquipmentSDR ASOA2014091611223Tab · chafedCHAFE DAMAGE ON LT AND RT ANTI-ROTATION TABS OF THE HORIZONTAL STABILIZER. COMPLIED WITH EC/TC SB 670BA-55-012 01,02,03.Sep 6, 2014 · N753EV · Cndair CL6002C10 · Horizontal Stabilizer, Tab StructureSDR ASOA2014091611222Skin · crackedRT WING LOWER PLANK HAS 1 EA FASTENER HOLE WITH CRACK INDICATION. REPAIRED IAW REO 670-57-21-733 P1. MAJOR REPAIR.Aug 22, 2014 · N753EV · Cndair CL6002C10 · Wing, Plate/SkinSDR ASOA2014091611221Skin · crackedLT WING LOWER PLANK HAS THREE FASTENER HOLES WITH CRACK INDICATIONS. REPAIRED IAW REO 670-57-21-733 P1. MAJOR REPAIR.Aug 22, 2014 · N753EV · Cndair CL6002C10 · Wing, Plate/Skin
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