N908EV

Service difficulty reports · 280

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 = 'N908EV' 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 SWIA202157517Panel · crackedSERVICE DOOR SURROUND PANEL 232BZ HAS CRACKED HONEYCOMB AND 1EA ATTACH BRACKET DISBONDED FROM THE BACK SURFACE. (C-CHECK RO 4/12/2021) REPAIRED SERVICE DOOR SURROUND PANEL 232BZ HAS CRACKED HONEYCOMB IAW C&D ZODIAC REPAIR MANUAL 25-6000-1 AND REATTACHEDFeb 1, 2021 · N908EV · Cndair CL6002B19 · Service DoorsSDR SWIA202157563Vane · chafedR/H INBOARD FLAP VANE IS CHAFED AT (3) LOCATIONS ALONG LEADING EDGE. (C-CHECK RO 4/12/2021) RECIEVED NEW SERVICABLE RH IB FLAP WITH SERVICABLE FLAP VANE ATTACHED. REFER TO CAMP 22170380 FOR INSTALLATION OF RH IB FLAP.Jan 31, 2021 · N908EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157562Vane · chafedL/H INBOARD FLAP VANE IS CHAFED AT (3) LOCATIONS ALONG LEADING EDGE. (C-CHECK RO 4/12/2021) RECIEVED NEW SERVICABLE LH IB FLAP WITH SERVICABLE FLAP VANE ATTACHED. REFER TO CAMP 22170380 FOR INSTALLATION OF LH IB FLAP.Jan 31, 2021 · N908EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202157495Skin · dentedADM# N908EV-6732 / DENT LOCATED AT RT AFT FUSELAGE AT F.S. 625.30 BETWEEN STRINGER 18R AND 19 R / PLOT MAP AND EVAL, DAMAGE IF DAMAGE FOUND IN LIMITS ELIMINATE ALL EVIDENCE USING A/C STD PRACTICES/PROCEDURES (C-CHECK RO 4/12/2021) PERFORMED PERMANENT RJan 30, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202057494Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHDec 8, 2020 · N908EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202057490Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA48156-601R-53-61-6986 MXCODEID46346-PR - LEFT SIDE FUSELAGE AREA BELOW CARGO DOOR SCUFF PLATE HAS 6 DENTS BETWEEN FS 605.00 - FS 621.00 AND STGR 17 - STGR 20. PERFORMED TEMP REPAIR PER REO 601R-53-61-6986 REV -- DATEDec 8, 2020 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202057482Landing · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA48158-601R-53-11-2381 -PR1 - LEFT ELECTRONICS BAY TRU ACCESS DOOR AFT LATCH CUT-OUT HAS VISIBLE CRACK ON LOWER RADIUS. COMPLIED WITH TEMPORARY REPAIR PER REO 601R-53-11-2381 REV -- DATED 2013-04-18. PERMANENT REPAIRDec 8, 2020 · N908EV · Cndair CL6002B19 · Hydraulic Compartment DoorsSDR SWIA202081751802Window · crackedHAIRLINE CRACK DEVELOPED IN LEFT WINDOW, CRUISING AT .74 AND FL310. STARTED DESCENT INTO CLARKSBURG, GOT L WINDOW HEAT CAUTION MESSAGE. FOLLOWED QRH, OBVIOUSLY DIDN€™T FIX CRACK. CRACK GOES FROM (INSIDE LOOKING OUT) ABOUT 5-6 INCHES FROM BOTTOM RIGHT CORNER TAug 14, 2020 · N908EV · Cndair CL6002B19 · Flight Compartment WindowsSDR ASOA201811265333Bushing · wornLEFT AILERON, HYDRAULIC SYSTEM NR 3 PRESSURIZED FAILED BACKLASH AT 0.096". MAX ALLOWED IS 0.085". REQUIRES BUSHING REPLACEMENT. REPLACED DAMAGED BUSHING IAW RIL 6208, EC/TC RIL 6208 REV 0, DATED 2018-11-24, REO 601R-57-61-666 REV-, DATED 2018-11-20, EC/TC REO Nov 26, 2018 · N908EV · Cndair CL6002B19 · AileronsSDR ASOA201811205329Bulkhead · crackedFS 621.00 PRESSURE BULKHEAD WEB HAS (2EA) AREAS OF INDICATIONS NOTED IN THE Z-MEMBER HEEL LINE AREA. ONE AT BL 0.00 WL 109-WL112 AT 80% FSH AND ONE AT BL 0.00, WL 130-WL131.5 AT 100% FSH. BOTH AREAS FAIL NDT INSPECTION. REPAIRED DAMAGE IAW REO 601R-53-61-6768 Nov 20, 2018 · N908EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201811205328Skin · dentedFUSELAGE SKIN HAS A SHARP DENT AT FS 591.00 BETWEEN STRINGERS 25R-26R. DENT MEASURES .065" DEEP AND APPROX .758" IN LENGTH. REPAIRED DAMAGE IAW REO 601R-53-61-6773 REV-, DATED 2018-11-15 AND REO 601R-53-61-6773 REV 0, DATED 2018-11-16.Nov 20, 2018 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201811195327Bulkhead · gougedWHILE REPLACING ISOLATORS ON FS 621 BULKHEAD FORWARD SIDE SEVERAL GOUGES AND SCRATCHES WERE FOUND AT THE FOLLOWING LOCATIONS: SCRATCHES AT RBL 4.5 TO 6.5 AND 13.75" TO 27.50" ABOVE WL WITH MAX DEPTH OF .008", GOUGES ARE AT LBL 10, 30.25" AND 13.75" ABOVE WL LBNov 19, 2018 · N908EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201811195326Bracket · crackedPASSENGER DOOR POWER ASSIST MOTOR PULLEY BRACKET ON AFT EDGE APPEARS TO BE PULLING AWAY FROM STRUCTURE. REPAIRED DAMAGE IAW REO 601R-52-11-2638 REV-, DATED 2018-11-01 AND EC/TC REO 601R-52-11-2638 REV 0, DATED 2018-11-05.Nov 19, 2018 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA201811185325Skin · damagedREF: CO# 7654518 JOB# 7765456 OP# 6: WHILE PERFORMING SB 601R-57-046, FOUND (1EA) FASTENER TO BE OVERSIZE IN R/H LOWER BUTTSTRAP AND WINGPLANK.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-57-21-2900 REV.--, DATED 2018-11-12 AND EXPRESSJET EC/TC REO 601R-57-Nov 18, 2018 · N908EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2018120585324Trunnion · crackedREF: CO# 7654518 JOB# 7765456 OP# 7: WHILE PERFORMING SB 601R-57-046 REV.C, FOUND ONE CRACK INDICATION NOTED ON THE L/H SIDE 2ND HOLE FROM FORWARD END OF COLD WORK AREA. INDICATION IS .350" UP FROM BOTTOM END OF STEEL STRAP EXTENDING .100" UP BY 50% FSH ON FWNov 18, 2018 · N908EV · Cndair CL6002B19 · Wing, Landing Gear Attach FittingsSDR ASOA2018120415322Floor Support · corrodedREF: CO# 7654518 JOB# 7765458 OP# 4: CORROSION ON L/H CABIN FLOOR SILL, F.S. 559.00+80 TO F.S. 559.00+96, LBL 45.0. C/A: REPAIRED R/H FLOOR SILL I.A.W. BOMBARDIER REO 601R-53-00-526 REV. --, DATED 22-MAY-2013 AND EXPRESSJET EC/TC REO 601R-53-00-526 01 REV. 0, Nov 10, 2018 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018120415321Floor Support · corrodedREF: CO# 7654518 JOB# 7765458 OP# 5 CORROSION AROUND FASTENER HOLE R/H FLOOR SILL FS 559.00+80, RBL 45.0 C/A:REPAIRED R/H FLOOR SILL I.A.W BOMBARDIER REO 601R-53-00-526 REV -- DATED 22 MAY-2013 AND EXPRESSJET EC/TC REO 601R-53-00-526 01 REV. 0 DATED 2013-05-29Nov 10, 2018 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2018113005320Cargo Track · corrodedREF: CO# 7654518 JOB# 7765458 OP# 2: AFT CARGO SEAT TRACK SEGMENT F.S. 559+110 TO F.S. 570.00+96 RBL 9 IS CORRODED. C/A: REMOVED AND REPLACED CARGO TIE DOWN SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802, AND SRM 51-41-02.Nov 10, 2018 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2018113005319Cargo Track · corrodedREF: CO# 7654518 JOB# 7765458 OP# 6: AFT CARGO SEAT TRACK SEGMENT F.S. 559+80 TO 559.00+96 RBL 27.0 IS CORRODED. C/A: REMOVED AND REPLACED CARGO TIE DOWN SEAT TRACK SEGMENT IAW CRJ200 AMM 53-01-11-000-802, 53-01-11-400-802, AND SRM 51-41-02.Nov 10, 2018 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201811305318Vent · chafedREF: CO# 7654518 JOB# 7765451 OP# 43: PASSENGER DOOR PRESSURE VENT HAS TWO CHAFED STIFFENERS. C/A: REPAIRED CHAFFED STIFFENERS IN PASSENGER DOOR I.A.W. BOMBARDIER REO 601R-52-11-1040 REV. --, DATED 2006/10/30 AND EXPRESSJET EC/TC REO 601R-52-11-1040.Nov 10, 2018 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2018052444713Aileron · crackedRIGHT AILERON APPEARS TO HAVE CRACK SPANNING THE WIDTH OF THE RIGHT EDGE, PERPENDICULAR TO THE TRAINING EDGE. (FLT 2971) CLOSED COMPLIED WITH REO.May 24, 2018 · N908EV · Cndair CL6002B19 · AileronsSDR SWIA201844127Proximity Sensor · failedNOSE GEAR DISAGREE, GEAR DID NOT RETRACT. REMOVED AND REPLACED NLG PROXIMITY SENSOR BRACKET IAW AMM. PERFORMED GEAR SWINGS, GEAR OPERATES NORMALLY, NO MESSAGES.Jan 3, 2018 · N908EV · Cndair CL6002B19 · Landing Gear Position and WarningSDR SWIA2018010444127Unknown · failedGEAR DISAGREE NOSE GEAR DID NOT RETRACT. (FLT#3096) FO: 01/04/2018 WORK IN PROGRESS.Jan 3, 2018 · N908EV · Cndair CL6002B19 · Landing Gear Retraction/Extension SystemSDR SWIA201743213Floorbeam · corrodedFLOORBEAM CAP CORRODED AT BS 409 +5, RBL 9. REMOVED AND REPLACED THE FLOORBEAM CAP IAW SRM.Mar 14, 2017 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743212Skin · dentedRIGHT INBOARD FLAP, BOTTOM SKIN AT INBOARD SIDE HAS A DENT. REPAIRED IAW REO.Mar 2, 2017 · N908EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743211Floor Support · corrodedFLOOR SUPPORT FROM BS 559+86 TO 559+116 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM.Mar 2, 2017 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743209Floor Panel · corrodedFIVE LOCATIONS ON THE LH PRESSURE FLOOR PANEL CORRODED. REPAIRED THE PRESSURE FLOOR PANEL IAW REO.Mar 2, 2017 · N908EV · Cndair CL6002B19 · Fuselage Floor PanelSDR SWIA201743208Floorbeam · corrodedCORROSION ON LEFT PRESSURE FLOORBEAM ANGLE AT BS 517. REPAIR TO LH PRESSURE FLOORBEAM ANGLE IAW SRM.Mar 2, 2017 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201743210Floorbeam · corrodedBS 280 FLOORBEAM ANGLE HAS CORROSION BETWEEN RBL 9 AND LBL 9. REMOVED AND REPLACED FLOORBEAM ANGLE IAW SRM.Mar 1, 2017 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201612101250Engine · smoke"SMOKE TOILET" CAUTION MSG IN FLIGHT. SMOKE SEEN & SMELLED IN MID CABIN. FOLLOWED SMOKE TOILET QRH PROCEDURE. AIRCRAFT RETURNED TO DFW AFTER TO. AIRCRAFT FERRIED TO BTR FOR CORRECTIVE ACTION. MTC REMOVED AND REPLACE RT ENGINE IAW ENGINE CHANGE EC/TC CF34-3. OPDec 10, 2016 · N908EV · Cndair CL6002B19 · Engine (Turbine/Turboprop)SDR ASOA2015092613828Sign · missingEMERGENCY EXIT SIGN MISSING ABOVE SERVICE DOOR. REPLACED THE SIGN IAW AMM 33-51-13. OPS CHECKED GOOD.Sep 26, 2015 · N908EV · Cndair CL6002B19 · Emergency LightingSDR ASOA2015070813285Door · dirtyMAIN CABIN DOOR VERY HARD TO OPEN. CLEAN PAX DOOR PERFORMED, OPS TEST IAW AMM 5-11-00. OPS TEST GOOD NO FURTHER DEFECTS FOUND AT THIS MOMENT.Jul 4, 2015 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015062613187Glowstrip · deterioratedEXIT ROW LUMINESCENT TAPE TORN. R & R RT EMERGENCY EXIT AFT SECTION OF PHOTOLUMINESCENT TRACK IAW AMM 33-51-01.Jun 25, 2015 · N908EV · Cndair CL6002B19 · Emergency EquipmentSDR ASOA2015062613179Door · unknownMAIN DOOR WOULD NOT OPEN. CYCLED MAIN CABIN DOOR SEVERAL TIMES. OPS TEST GOOD IAW AMM 52-11-00. OK FOR SERVICE.Jun 22, 2015 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015061113088Door · stuckMAIN CABIN DOOR STUCK CLOSED ON ARRIVAL. TOOK MULTABLE ATTEMPTS TO OPEN FROM INSIDE AND OUT. PERFORMED OPS CHECK OF PAX DOOR IAW AMM 52-11-00. OPS CHECK GOOD. NO DEFECTS FOUND AT THIS TIME.Jun 7, 2015 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015020512164Cleat · crackedWHILE REMOVING AND REPLACING PAX DOOR SURROUND STRUCTURE CLEAT AT FS 310 BETWEEN INTERCOSTAL AND STRINGERS 15L AND 16L, FOUND SPLICE TAB CRACKED ON FWD LOWER CORNER AF SEAL STRIKER, PN:600-31535-69. COMPLIED WITH EA 12-2015-040. EA 12-2015-040 HAS BEEN ACCOMJan 23, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR ASOA2015020512163Skin · crackedINDICATION NOTED ON RT LOWER WING PLANK ACCESS HOLE 640EB, WS 116.83 LANDING 60 PERCENT FULL SCREEN HEIGHT. FAILED NDT. COMPLIED WITH EC/TC EO 600-57-81. C/W IAW REO 601R-57-21-030, REV L.Jan 16, 2015 · N908EV · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015020512162Floorbeam · corrodedCORROSION ON CARGO FLOORBEAM RBL 9, BS 559+96. BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005. CUTOUT DAMAGED AREA IAW SRM 53-00-43 REPAIR NR 1 STEPS 5A 1 AND 2. FABRICATED REPAIR, LOCATED AND DRILLED IAW SRM 53-00-43, STEP 5A5. C/WJan 14, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015020512161Channel · corrodedCHANNEL UNDER PAX DOOR ANCHOR FITTING AT BS 310 HAS CORROSION. REMOVED AND REPLACED THE CHANNEL IAW SNIEO 601R31096, SNIEO S01.Jan 14, 2015 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015020512160Cargo Track · corrodedCARGO TRACK CORRODED AT BS 559+112 AT RBL 9. REMOVED AND REPLACED THE CARGO TRACK IAW SRM 51-40-11 AND IAW AMM 20-21-00-910-801.Jan 14, 2015 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015020512159Stringer · crackedSTRINGER 3L HAS A CRACK AT FS 280 BULKHEAD. R & R ANGLE AT STRINGER 3L AT FS 280 IAW SRM 51-40-11, 51-42-06 AND 51-77-00, TR 50-32.Jan 14, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR ASOA2015020512158Intercostal · crackedINTERCOSTAL ON AFT SIDE OF BS 621 BULKHEAD AT STRINGER 13L IS CRACKED IN RADIUS. REMOVED CRACKED INTERCOSTAL ON AFT SIDE OF FS 621 BULKHEAD STRINGER 13L IAW SRM TASK 51-42-06 AND 51-42-21. LOCATED, DRILLED NEW SERVICEABLE INTERCOSTAL AT 13L 621FS IAW SRM 51-Jan 14, 2015 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015020512157Skin · crackedRIGHT BOOST PUMP CUTOUT HAS MULTIPLE INDICATIONS ALL AROUND THE VERTICAL & HORIZONTAL LANDINGS 50 PERCENT FSH. FAILED NDT INSPECTION. REMOVED CORROSION ON VERTICAL AND HORIZONTAL LANDINGS IAW SRM 51-21-06. ORIGINAL THICKNESS .150", REMOVED .007" FROM HORIZOJan 13, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015020512156Bearing · deterioratedVERTICAL STABILIZER RUDDER CENTER HINGE FITTING BEARING WORN CAUSING RUDDER TO COME CLOSE TO CONTACTING FITTING. COMPLIED WITH EC/TC RIL 0602, REPAIR TYPE 1 REPLACEMENT OF NESTED BEARING IAW RIL 0602, REV G.Jan 13, 2015 · N908EV · Cndair CL6002B19 · Rudder StructureSDR ASOA2015020512155Shear Tie · corrodedBS 409 FRAME SECTOR TO FUSELAGE SKIN ATTACH CAP ANGLE, HAS CORROSION AROUND FASTENER ON FWD SIDE BL 27. REMOVED CORROSION FROM FS 409.0 FRAME SECTIONS IAW SRM 51-12-00. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-00, TR 53-27. ENGINEERING DISPOSITON REQUIRED. Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR ASOA2015020512154Intercostal · corrodedINTERCOSTAL CORRODED AFT OF AVIONICS DOOR BETWEEN BS 394 - 409, RBL 26. REMOVED CORROSION IAW SRM 51-12-00 AND FOUND INTERCOSTAL TO BE WITHIN LIMITS IAW SRM 53-00-00 TR 53-27, FIGURE 102, SHEETS 1 & 2.Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015020412152Frame · corrodedBS 310 FRAME CORRODED ON AFT SIDE BETWEEN STRINGERS 26L AND 26R. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-06 AND 51-42-21.Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015020412151Isolator · brokenBROKEN ISOLATORS ON BS 621 BULKHEAD FWD FACE. REMOVED AND REPLACED THE ISOLATORS IAW SRM 51-42-13.Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015020412150Floorbeam · crackedBS 460, FLOORBEAM CRACKED, OTBD SIDE OF LBL 9. REMOVED AND REPLACED THE FLOORBEAM ANGLE IAW SRM 51-42-21, SRM 51-40-11, AND SRM 51-42-06.Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015020412149Floorbeam · crackedBS 484, FLOORBEAM REPAIR ANGLE AT RBL 36 IS CRACKED. REPAIRED IAW REO 601R-53-41-1875.Jan 12, 2015 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor Beam
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