N903EV

Service difficulty reports · 265

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 = 'N903EV' 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 ASOA20160930086Seat Track · corrodedSEAT TRACK HAS CORRODED. REMOVED AND REPLACED THE SEAT TRACK RBL 9, BS 364-394 IAW AMM 53-01-11-000-802 & 53-01-11-400-802.Sep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA20160930036Intercostal · corrodedINTERCOSTAL 27L CORRODED FWD OF AVIONICS DOOR BETWEEN BS 349 & 364. R & R THE INTERCOSTAL IAW SRM 51-42-06, PG 23. BSep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA20160930035Floorbeam · corrodedFLOORBEAM HAS CORROSION AT BS 559+112 AT LBL 27. REPAIRED THE AREA IAW REO 601R-53-00-027 AND EC/TC EO 600-53-0780. THIS IS CLASSIFIED AS A MAJOR REPAIR.Sep 30, 2016 · N903EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2016061414923Sign · brokenEMERGENCY EXIT SIGN OVER GALLEY DOOR IS BROKEN. R & R SERVICE DOOR EMERGENCY SIGN, TOP IAW AMM 33-51-13. NO FURTHER DEFECT NOTED AT THIS TIME.Jun 14, 2016 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2016022314545Bulb · burned outPAX DOOR OUTSIDE EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED THE EMERGENCY LIGHT LENS, TWISTED BULB OUT OF SOCKET, INSTALLED NEW BULB BY TWISTING IT BACK IN THE SOCKET REINSTALLED CORNER OF THE LIGHT ASSY IAW AMM 33-51-21-000-801 & 33-51-21-400-801. EMERGENCY LFeb 23, 2016 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015110714004Light · damagedFLOOR-LEVEL EMERGENCY FLOODLIGHT AT SERVICE DOOR DAMAGED. R & R FLOODLIGHT IAW AMM 33-51-19. SYSTEM OPS CHECKED GOOD. NO FURTHER ACTION.Nov 7, 2015 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015091413762Landing Gear · malfunctionedGEAR UP DISAGREE INDICATION AFTER TAKEOFF. LEFT MAIN GEAR INDICATED UNSAFE. ACFT RETURNED TO DEPARTURE AFTER T/O, EMERGENCY ACTIONS: LANDING GEAR RETRACTION SYSTEM. COMPLIED WITH VISUAL INSPECTION OF LT MLG AND UPLOCK ASSY IAW AMM 32-32-05. COMPLIED WITH Sep 14, 2015 · N903EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR ASOA2015072613387Mechanism · dirtyF/A REPORTS THAT MAIN PAX DOOR LEVER IS STICKING WHEN TRYING TO OPEN DOOR. REMOVED DEBRIS & TRASH FROM DOOR OPERATING MECHANISM. MAIN DOOR OPERATES OPENS AND CLOSES NORMALLY NOW IAW AMM 52-11-03.Jul 26, 2015 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015052612910Door · lack of lubeMAIN CABIN DOOR WOULD NOT OPEN AT GATE. CLEANED AND LUBRICATED PAX DOOR INNER HANDLE IAW AMM 12-2-52. OPS CHECK GOOD.May 22, 2015 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014102011458Skin · crackedCRACK INDICATIONS NOTED AT LT LOWER WING PLANK ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV. L .Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011457Skin · crackedINDICATIONS NOTED AT RT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011456Skin · crackedINDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW 601R-57-21-030, REV L.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011455Skin · crackedINDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011454Skin · crackedINDICATIONS NOTED AT LT LOWER WING SKIN ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011453Skin · crackedINDICATIONS NOTED AT RT WING ACCESS PANEL LANDING. REPAIRED IAW REO 601R-57-21-030 REV.L 2014-02-05.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011452Access Panel · crackedINDICATIONS NOTED AT RT WING ACCESS PANEL. REPAIRED IAW REO 601R-57-21-030, REV L 2014-02-05.Oct 3, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014102011451Skin · crackedLOWER RT WING ACCESS PANEL LANDING HAS MULTIPLE INDICATIONS OF CORROSION NOTED. REMOVED CORROSION IAW EA 15-2014-197, SECTION 1 1A.Sep 30, 2014 · N903EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2014101411415Isolator · crackedFS 621 BULKHEAD HAS SEVEN ISOLATORS FOUND CRACKED AND/OR BROKEN. R & R THE BROKEN ISOLATORS IAW SRM 51-42-06, PT SL2337.3.Sep 30, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014101711450Attach Angle · damagedON REMOVAL OF THE ATTACHMENT ANGLE AT LBL 9.0 WHERE FLOOR SUPPORT ATTACHES TO BS 280 CROSSBEAM, UNDER OTBD ANGLE FOUND TOP HOLE IN FLOORBEAM WEB TO BE ELONGATED. REPAIRED IAW REO 24-2014-559.Sep 26, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2014101411414Angle · corrodedFOUND FWD J-ANGLE, BS 280 BETWEEN LBL 12 AND RBL 12 TO HAVE CORROSION. LOCATED, DRILLED & INSTALLED FWD J CHANNEL IAW SRM 51-40-11, 51-42-06.Sep 25, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014101711449Structure · chafedREPAIRED LT MLG DOOR L/E CHAFED 2.1" LONG, .025" DEEP, .200 WIDE NEXT TO BRUSH ASSEMBLY. REPAIRED LT MLG DOOR L/E IAW STS EA 32-2014-115, REV P2. RECEIVED FINAL EA STS EA 32-2014-115. COMPLIED WITH EC/TC REO 601R-52-82-034 01, REACCOMPLISHMENT, REPAIR TO MLSep 24, 2014 · N903EV · Cndair CL6002B19 · Landing Gear DoorsSDR ASOA2014101711448Seat Track · corrodedCORROSION ON SEAT TRACK AT RBL 9 FS 364 TO 409.00+128 AT VARIOUS LOCATIONS. R & R SEAT TRACK IAW SRM 51-41-02.Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2014101711447Floor Support · corrodedCORROSION ON LT AND RT FLOOR SUPPORT CAPS FROM FS 364 TO FS 409.00+128 AT VARIOUS LOCATIONS LBL 9 AND RBL 9. FOUND CORROSION TO BE FROM FS 409.00+5 TO FS 409.00+128. REMOVED FASTENERS AND DISPLACED LT FLOOR SUPPORT CAP FROM FS 409+5 TO FS 409+128 IAW SRM 51-Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101711446Skin · corrodedFUSELAGE SKIN EXTERIOR SURFACE HAS MINOR CORROSION AROUND FASTENERS FROM FS 559 TO FS 559+10 BETWEEN STRS 25L AND 25R. REMOVED FASTENERS FROM FS 559 TO FS 559+10 BETWEEN STR 25L TO 25R IAW SRM 51-42-21. BLENDED AREA AROUND FASTENER HOLES REMOVING CORROSION ISep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014101711445Floorbeam · crackedFS 280, FLOORBEAM INBD AND OTBD CLIPS AT RBL 9 ARE CRACKED. REMOVED INBD AND OTBD FLOORBEAM CLIPS AT FS 280 IAW SRM 51-42-21. INSTALLED SERVICEABLE OTBD & INBD FLOORBEAM CLIPS AT RBL 9, FS 280 IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2706, REV ISSUE.Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014101711444Floorbeam · crackedFS 280, FLOORBEAM INBD AND OTBD CLIPS AT LBL 9 ARE CRACKED. REMOVED INBD & OTBD CLIPS ON FLOORBEAM, LBL 9 AT FS 280 IAW SRM 51-42-21. INSTALLED SERVICEABLE INBD & OTBD CLIPS ON FLOORBEAM LBL 9 AT FS 280 IAW SRM 51-42-21. COMPLIED WITH REO 601R-53-11-2706, RSep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2014101411413Angle · corrodedCORROSION ON BS 280 J-ANGLE BETWEEN LBL 9 AND RBL 9. FOUND CORROSION TO BE ON AFT J-ANGLE PREVIOUS REPAIR FILTER ANGLE, PN 601R-53-11-136-1 FROM REO:601R-53-11-136, REV A CORROSION IS OM TOPSIDE AND BOTTOMSIDE AT NUTPLATE LOCATIONS AND CORROSION RUNS DOWN ANDSep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101411412Floor Support · corrodedCORROSION ON LT FLOOR SUPPORT AT BS 409+32. REPAIRED THE FLOOR SUPPORT BETWEEN BS 280 - 409+128 IAW REO:601R-53-00-530.Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101411411Floor Support · corrodedCORROSION ON RT FLOOR SUPPORT AT BS 409. REPAIRED THE FLOOR SUPPORT BETWEEN BS 280 - 409+128 IAW REO:601R-53-00-530.Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101411410Skin · corrodedFUSELAGE EXTERIOR SKIN HAS MINOR CORROSION AROUND FASTENERS FROM BS 559+32 - 559+54 STRINGERS 25L-25R. COMPLIED WITH CORROSION REPAIR IAW EA 25-2014-290 PART 1.Sep 24, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014101711443Angle · corrodedPASSENGER DOOR LOWER SILL ANGLE REPLACEMENT. R & R PASSENGER DOOR CAP ANGLE FOR LOWER SILL ANGLE REPLACEMENT BY REMOVING STRUCTURAL FASTENERS COMMON TO THE STRUCTURE. LOWER SILL ANGLE, ITEM 28, REQUIRES REPLACEMENT. REF SRM 53-21-23, FIG 2, FOR LOCATION.Sep 23, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101711442Bushing · deterioratedRIGHT AILERON INBD LUG AT INBD PCU ATTACHMENT POINT HAS MIGRATED BUSHING. REMOVED MIGRATED BUSHING, INSTALLED OVER SIZE BUSHING USING AMS5569 15-5PH H1000, PO 30012 MATERIAL IAW REO 601R-57-61-004, REV C AND DEVIATION, REO 601R-57-61-505, REV B. C/W ECTC REOSep 23, 2014 · N903EV · Cndair CL6002B19 · AileronsSDR ASOA2014101411409Floor Support · corrodedRT FLOOR SUPPORT CORRODED AROUND FASTENER HOLES BS 559+80 - 589. REPAIRED IAW REO 601R-53-00-526 01 AND GREO 601R-53-00-526, REV.Sep 23, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101411408Floor Support · corrodedLEFT FLOOR SUPPORT CORRODED AROUND FASTENER HOLES FROM BS 559+80 - 574. REPAIRED IAW REO 601R-53-00-526 AND GREO 601R-53-00-526, REV.Sep 23, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101711441Floor Support · corrodedCORROSION ON FLOOR SUPPORT BS 409+128 - 424 RBL 9. CORROSION EXCEEDS LIMITS IAW SRM 53-27. REPAIRED IAW REO 601R-55-41-1841.Sep 22, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101711440Floor Support · corrodedRIGHT FLOOR SUPPPORT FROM BS 409+128 - 559 HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW REO 601R-53-41-666 01 & REO 601R-53-41-666, REV C.Sep 22, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101711439Floor Support · corrodedLEFT FLOOR SUPPORT FROM BS 409+128 - 559 HAS SEVERAL AREAS OF CORROSION. REPAIRED IAW REO 601R-53-41-666, REV C.Sep 22, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101411407Angle · crackedLT ANGLE AT BS 484, LBL 27 IS CRACKED AT UPPER CORNER. REPAIRED IAW REO 601R-53-41-059.Sep 22, 2014 · N903EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2014101611434Skin · chafedRT AILERON UPPER SKIN SHROUD IS CHAFED FROM CENTER FITTINGS OF AILERON TO INBD EDGE OF AILERON. DEEPEST DAMAGE MEASURING APPROX. .015". MAX DAMAGE ALLOWED .005". BLENDED TO A SMOOTH CONTOUR RT AILERON UPPER SKIN SHROUD FROM CENTER FITTINGS OF AILERON TO INBD Sep 21, 2014 · N903EV · Cndair CL6002B19 · AileronsSDR ASOA2014101611433Bearing · failedTHE RUDDER MIDDLE HINGE POINT FITTINGS ON THE VERTICAL STABILIZER HAVE WORN BEARINGS. R & R RUDDER MIDDLE HINGE POINT FITTINGS BEARINGS IAW RIL 0602, REV F, TYPE 2. PERFORMED BEARING BACKLASH OF THE RUDDER SYS 1, 2, AND 3 IAW AMM 27-21-00-220-810. SYS 1 WASSep 21, 2014 · N903EV · Cndair CL6002B19 · Rudder StructureSDR ASOA2014101411406Isolator · crackedFWD SIDE OF BS 621, BULKHEAD HAS ONE CRACKED ISOLATOR ON LT SIDE THIRD ROW FROM THE BOTTOM. R & R THE ISOLATOR IAW SRM 51-42-13.Sep 21, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014101411405Isolator · crackedFWD SIDE OF BS 621 BULKHEAD HAS THREE CRACKED ISOLATORS ON RT SIDE MOST OTBD. R & R THE ISOLATORS IAW SRM 51-42-13.Sep 21, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2014101611432Skin · corrodedSKIN HAS LIGHT CORROSION BS 559+84 - 559+96, STRINGER 22R. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-31-01, TR 53-33. BLENDED CORRODED AREAS IAW SRM 51-12-00.Sep 20, 2014 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2014101611431Bearing · failedLEFT ELEVATOR SYS NR 3 FAILED BEARING BACKLASH. BACKLASH IS .240, MAX ALLOWED .210, .030 OUT OF LIMITS. REMOVED THE LT ELEVATOR SYS NR 1, 2 AND 3 BEARINGS, PN MS14103-6, MS14103-5 AND MS14103-4 IAW AMM 20-26-00-910-807. INSTALLED LT ELEVATOR SYSTEM NR 1, NRSep 20, 2014 · N903EV · Cndair CL6002B19 · Elevator StructureSDR SOA2014101611430Drag Angle · crackedPASSENGER DOOR AFT DRAG ANGLE IS CRACKED. COMPLIED WITH REPAIR TO PAX DOOR STAIR AFT DRAG ANGLE IAW REO 601R-52-11-513.Sep 18, 2014 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014072310923Circuit Breaker · trippedEMERGENCY LIGHTS DO NOT ILLUMINATE. SYSTEM SELF RESET IAW MCC NO FURTHER ACTION REQUIRED.Jul 19, 2014 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2014070310806Door · unknownMAIN PASSANGER DOOR DOES NOT OPEN NORMALLY, DIFFICULT TO OPEN, HANGS UP PART WAY THROUGH THE TRAVEL OF THE DOOR OPEN LEVER. PERFORMED VISUAL INSPECTION AND OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECKED GOOD. NO DEFECTS FOUND AT THIS TIME.Jul 1, 2014 · N903EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2014040310262Battery Pack · failedEMERGENCY LIGHT ABOVE ROW 3 INOPERATIVE. R & R EMERGENCY LIGHT NR 1 BATTERY PACK IAW AMM 33-51-04. OPS CHECKED GOOD.Mar 30, 2014 · N903EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2013060503756Skin · damagedFOD DAMAGE TO ACFT BELLY. OPEN.May 11, 2013 · N903EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2012091202195Seat Track · corrodedSEAT TRACK FROM FS 409.128 TO 559.16 CORRODED. REMOVED CORROSION IAW SRM 51-21-06, MAX MATERIAL REMOVED AT LOCATION R3, FIG 101, .012 DEEP. MATERIAL REMOVED WITHIN LIMITS OF SRM 53-21-49. REMOVED AND REPLACED SEAT TRACK IAW AMM 53-01-11-000-802.Aug 30, 2012 · N903EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
Back to N903EV