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 SWIA202157549Anchor Fitting · corrodedPAX DOOR AFT ANCHOR FITTING IS CORRODED. (C-CHECK RO 4/12/2021) REPLACED PAX DOOR ANCHOR FITTING IAW CRJ 200 AMM 52-11-17-400-804. REF CONTINUATION CARD FOR DETAILS AND WORK PERFORMED.Feb 10, 2021 · N908EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202157548Strap · corrodedFLOOR SUPPORT STRAP AT F.S. 559.00 BETWEEN RBL27 AND RBL45 HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOOR SUPPORT STRAP AT FS559 BETWEEN RBL27 AND RBL45 WITH SERVICEABLE UNIT IAW CRJ-200 SRM 51-42-06.Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157547Strap · corrodedFLOOR SUPPORT STRAP AT F.S. 559.00 BETWEEN LBL27 AND LBL45 HAS MULTIPLE SPOTS OF CORROSION, (C-CHECK RO 4/12/2021) REMOVED AND REPLACED THE L/H FLOOR SUPPORT STRAP AT FS559 BETWEEN LBL27 AND LBL45 WITH SERVICEABLE UNIT IAW CRJ-200 SRM 51-42-06.Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157519Floorbeam · crackedF.S. 280 LBL 9 INBOARD AND OUTBOARD SUPPORT CLIPS ARE CRACKED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED I/B AND O/B SUPPORT CLIPS AT FS280 LBL 9 IAW CRJ 200 SRM 51-42-06 & 51-42-21 OPS TEST GOODFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157518Floorbeam · crackedINTERCOSTAL CLIP CRACKED AT F.S. 484.00 BETWEEN LBL27 AND LBL36 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED INTERCOSTAL CLIP AT F.S. 484.00 LBL 27 IAW CRJ 200 SRM 51-40-11, 51-42-06, AND 51-42-21. INTERCOSTAL CLIP AT F.S. 484.00 LBL 36 REFERENCE JOB: 97Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157506Floorbeam · crackedF.S. 280 RBL 9 SUPORT CLIP IS CRACKED. (C-CHECK RO 4/12/2021) REPAIRED FS280 RBL9 IAW REO 601R-53-21-3407 REV. --, DATED 03/02/2021. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE. SEE CONTINUATION CARD FOFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157505Floorbeam · corrodedFLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00 TO F.S. 409.00+128 (C-CHECK RO 4/12/2021). REMOVED AND REPLACED FLOOR BEAM AT LBL9 FROM FS 409.00-409+128 IAW BOMBARDIER REO 601R-53-31-1187 REV -- DATED 2021-03-08. FORM 337 AND MAJOR REPAIRFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157504Floorbeam · corrodedFLOOR BEAM AT RBL9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00 TO F.S. 409.00+128 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOOR BEAM AT RBL 9 BETWEEN FS 409-409+128 IAW CRJ 200 SRM 51-42-36, 51-42-21, BOMBARDIER REO 601R-53-00-005 REV.B, DATED Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157503Floor Support · corrodedRH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00+128 TO F.S. 559.00 (C-CHECK RO 4/12/2021) REPAIRED RH PRESSURE SILL FROM FS409+128 TO FS559 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157502Floor Support · corrodedLH PRESSURE FLOOR SILL HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00+128 TO F.S. 559.00 (C-CHECK RO 4/12/2021) REPAIRED LH PRESSURE SILL FROM FS409+128 TO FS559 IAW REO 601R-53-41-666 REV-C DATED 2012-11-06. COMPLETED TASK CARD 51-900-1003-SKY AND ATFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202157484Door Sill · corrodedPAX DOOR LOWER SILL IS CORRODED FROM F.S. 310 TO F.S. 349. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED PAX DOOR SILL IAW CRJ 200 SRMS 51-42-06, 51-42-21. FORM M337 AND MAJOR REPAIR TASK 51-900-1003-SKY COMPLETED AND ATTACHED. NO WEIGHT CHANGE, PART FOR Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202157476Floorbeam · corrodedFLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00+128 TO F.S. 559.00 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOOR BEAM AT RBL 9 F.S. 409.00+128 TO F.S. 559.00 IAW REO 601R-53-41-2870 REV-- DATED 2021-02-18. FORM 337 AND MAJOR REFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157474Floorbeam · corrodedFLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 409.00+128 TO F.S. 559.00 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOOR BEAM AT LBL9 FROM F.S. 409.00+128 TO F.S. 559.00 AS REQUIRED IAW REO 601R-53-41-2871 REV-- DATED 2/12/2021. FORM 3Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157473Floorbeam · damagedINTERCOSTAL AT F.S. 484.00 BETWEEN RBL27 AND RBL36 HAS 2 EA BROKEN CLIPS. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED CLIPS IAW CRJ 200 SRMS 51-42-21, 51-42-06, 51-40-11, 51-24-36. REFER TO CONTINUE CARD FOR WORK PERFORMED. FORM 337 AND MAJOR REPAIR TAFeb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157472Door Sill · corrodedR/H FLOOR SILL IS CORRODED AT F.S. 349. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED PREVIOUSLY REPAIRED SECTION OF SILL IAW CRJ 200 SRM 51-42-06 REFERENCING PREVIOUSLY COMLETED REO 601R-53-21-2397 REV -- DATED 2013-01-02. REFER TO CONTINUE CARD FOR DETAILS Feb 10, 2021 · N908EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA202157546Crossbeam · corrodedCROSSBEAM CAP AT F.S. 559.00+80 BETWEEN RBL27 AND RBL45 HAS MULTIPLE SPOTS OF CORROSION. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED CROSSBEAM CAP AT FS 559.00 +80 BETWEEN RBL 27 AND RBL 45 IAW CRJ 200 SRM 51-42-06Feb 9, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202157501Floorbeam · corrodedFLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 559.00 TO F.S. 559.00+80 (C-CHECK RO 4/12/2021) REPAIRED FLOOR BEAM AT LBL9 FROM FS 559 TO 559+80 IAW CRJ200 SRM 53-00-43 & 51-42-06, BOTH REV. 38B DATED 25 NOV 2020. FORM M-337 AND MAJOR REPFeb 9, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157500Floorbeam · corrodedFLOOR BEAM AT RBL 9 HAS MULTIPLE SPOTS OF CORROSION FROM F.S. 559.00 TO F.S. 559.00+80 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOORBEAM IAW CRJ200 SRM 51-42-21, 51-42-36 (BOTH REV. 38B, DATED 11/25/20) AND REO 601R-53-51-565 REV. --, DATED 03/09/20Feb 9, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157499Floorbeam · corrodedFLOOR BEAM AT LBL9 HAS MULTIPLE SPOTS OF CORROSION BETWEEN F.S. 574.00 AND F.S. 621.00 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOOR BEAM AT LBL 9 BETWEEN FS 574.00 TO FS 609.00 IAW CRJ 200 SRM 51-42-06, 51-42-21, 51-42-15 AND 51-42-36. FORM 337 ANFeb 9, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202157480Seat Track · corrodedFLLOR BEAM AT LBL 27 HAS MULTIPLE SPOTS OF CORROSION BETWEEN FS 574.00 AND FS 621.00 (C-CHECK RO 4/12/2021) REMOVED AND REPLACED FLOORBEAM CAP IAW REO 601R-53-61-7601 REV -- DATED 2021-03-15, REFER TO CONTINUE CARD FOR DETAILS OF WORK PERFORMED. MAJOR REPAIR TFeb 9, 2021 · N908EV · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202157498Skin · corrodedFUSELAGE OUTER SKIN IS CORRODED UNDER SEALANT BED AND AROUND SCREW HOLES FOR PANELS 191BB AND 192BB (C-CHECK RO 4/12/2021) REPAIRED FUSELAGE OUTER SKIN UNDER SEALANT BED AND AROUND SCREW HOLES FOR PANELS 191BB AND 192BB IAW REO 601R-53-31-1185 REV. --, DATED 0Feb 7, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202157545Bolt · corrodedRH SPOILERON IB AND OB PCU MOUNTING HARDWARE IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED CORRODED MOUNTING HARDWARE FROM R/H I/B AND O/B SPOILERON PCU,S AND INSTALLED NEW HARDWARE IAW CRJ 200 AMM 27-62-01-400-801. REFERENCE CONTINUATION CARD FOR WORK PEFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157544Bolt · corrodedRH SPOILERON HINGE BOLT ANTI-MIGRATION BRACKET BOLTS 8EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED R/H SPOILERON HING BOLTS ANTI-MIGRATION BRACKET BOLTS IAW CRJ-200 AMM TASK'S 27-64-01-000-801, AND 27-64-01-400-801. SEE CONTINUATION CARFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157543Nut · corrodedRH SPOILERON HINGE NUTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVER AND REPACED R/H SPOILERON HINGE NUTS IAW CRJ-200 AMM TASK'S 27-64-01-000-801 AND 27-64-01-400-801. SEE CONTINUATION CARD FOR DETAILS OF WORK PERFORMED.Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157542Bolt · corrodedRH FLIGHT SPOILER IB AND OB HINGE BOLT ANTI-MIGRATION BRACKET BOLTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH FLIGHT SPOILER IB AND OB HINGE BOLT ANTI-MIGRATION BRACKET BOLTS 4EA AS REQUIRED IAW CRJ 200 AMM 27-64-05-000/400-801 & Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157541Nut · corrodedRH FLIGHT SPOILER HINGE NUTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH IB FLIGHT SPOILER HINGE NUTS IAW CRJ200 AMM 27-64-05-000/400-801Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157540Nut · corrodedRH OB GROUND SPOILER IB AND OB HINGE NUTS ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED HADRWARE ON RH OB GROUND SPOILER IB AND OUTBD HINGE POINTS IAW CRJ 200 AMM 27-65-01-400-801Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157539Bolt · corrodedRH OB GROUND SPOILER ACTUATOR MOUNTING HARDWARE IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED RH OB GROUND SPOILER ACTUATOR HARDWARE IAW CRJ200 AMM 27-63-01-400-801 OPS TEST GOODFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157538Nut · corrodedRH IB GROUND SPOILER OB HINGE NUT IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED CORREDED HARDWARE AND PLACED NEW HARDWARE ON RH IB GROUND SPOILER FOR FUTURE INSTALL. REF. CAMP#22267132 FOR INSTALL.Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157537Bolt · corrodedLH SPOILER IB AND OB HINGE BOLT ANTI-MIGRATION BRACKET BOLTS 8EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED 8EA CORRODED BOLTS FROM L/H SPOILERON I/B AND O/B HINGE BOLT ANTI-MIGRATION BRACKETS IAW CRJ-200 AMM TASKS 27-64-01-000-801 AND 27Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157536Bolt · corrodedLH SPOILERON PCU MOUNTING HARDWARE STACKUP IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED PCU MOUNTING HARDWARE IAW CRJ200 AMM 27-62-01-000/400-801 OPS AND LEAK TEST GOODFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157535Nut · corrodedLH SPOILERON HINGE NUTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED 4EA NUTS ON L/H SPOILERON HINGES IAW CRJ-200 AMM TASKS 27-64-01-000-801 AND 27-64-01-400-801.Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157534Nut · corrodedLH FLIGHT SPOILER IB PCU MOUNTING NUT IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND INSTALLED A SERVICABLE LH FLIGHT SPOILER IB PCU MOUNTING NUT IAW CRJ-200 AMM TASK 27-62-01-400-801 STEPS 2B(6)(7).Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157533Bolt · corrodedLH FLIGHT SPOILER IB AND OB HINGE BOLT ANTI-MIGRATION BRACKET BOLTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED L/H FLIGHT SPOILER IB AND OB HINGE BOLT ANTI-MIGRATION BRACKET BOLTS IWA CRJ 200 AMM 27-64-05-400-801. REFERENCE CONTINUATIFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157532Nut · corrodedLH FLIGHT SPOILER HINGE NUTS 4EA ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED L/H FLIGHT SPOILER HINGE NUTS 4EA IAW CRJ 200 AMM 27-64-05-400-801. REFERENCE CONTINUE CARD FOR WORK PERFORMED.Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157531Nut · corrodedLH OB GROUND SPOILER HINGE NUT AND ANTI-ROTATION TAB HARDWARE IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED LH OB GROUND SPOILER HINGE NUT AND ANTI ROTAION TAB HARDWARE IAW CRJ200 AMM 27-65-01-000/400-801 OPS TEST GOODFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157530Nut · corrodedLH OB GROUND SPOILER IB HINGE NUT IS CORRODED. (C-CHECK RO 4/12/2021) DUPLICATE DISCREPANCY, REFER TO CP 22263478 (1 OP 199).Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157529Nut · corrodedLH OB GROUND SPOILER IB HINGE NUT IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED LH OB GROUND SPOILER IB HINGE HARDWARE IAW CRJ 200 AMM27-65-01-400-801Feb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157528Spacer · corrodedLH IB GROUND SPOILER OB HINGE NUT AND ANTI-ROTATION PLATE HARDWARE IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND INSTALLED NEW SERVICABLE LH IB GROUND SPOILER OB HINGE NUT AND ANTI-ROTATION PLATE HARDWARE IAW CRJ 200 AMM 27-65-01-000/400-801. OPS TESTFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157527Link · corrodedLH IB GROUND SPOILER ACTUATOR LINK IS WORN/CORRODED AND HARDWARE STACKUP IS CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED LH IB GROUND SPOILER ACTUATOR LINK AND HARDWARE IAW CRJ 200 AMM 27-65-01-000/400-801 RIG AND OPS CHECK GOOD REF ATTACHED COFeb 6, 2021 · N908EV · Cndair CL6002B19 · SpoilersSDR SWIA202157526Bolt · corrodedLH ELEVATOR HINGE #2 RETAINER BRACKETS HAVE CORRODED HARDWARE. (C-CHECK RO 4/12/2021) REPLACED L/H ELEVATOR HINGE #2 RETAINER BRACKETS. REF CAMP # 22170364 JOB 9765460 OP 567 FOR INSTALL.Feb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157525Spacer · corrodedLH ELEVATOR HINGE ANTI-ROTATION TAB SPACERS AT HINGE BL24.5, #2, AND #3 ARE CORRODED. (C-CHECK RO 4/12/2021) INSTALLED NEW ANTI-ROTATION TAB SPACERS ON LH ELEVATOR AT HINGE BL24.5, #2, AND #3 IAW CRJ200 AMM 27-34-01-400-801Feb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157524Bolt · corrodedLH ELEVATOR HINGE RETAINER BRACKET BOLTS AT HINGE #1, BL24.5, AND #3 ARE CORRODED. (C-CHECK RO 4/12/2021) REPLACED BOLTS ON L/H ELEVATOR HINGE RETAINING BRACKETS AT HINGES #1,#24.5 AND #3 IAW CRJ 200 AMM 27-34-01-400-801.Feb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157523Bolt · corrodedRH ELEVATOR HINGE #2 RETAINER BRACKETS HAVE CORRODED HARDWARE. (C-CHECK RO 4/12/2021) REMOVED REPLACED RETAINER BRACKET HARDWARE R/H ELEVATOR HINGE #2 IAW CRJ 200 AMM 27-34-01-400-801 STEP3 IFeb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157522Spacer · corrodedRH ELEVATOR HINGE ANTI-ROTATION TAB SPACERS AT HINGE BL24.5, #2 AND #3 ARE CORRODED. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED THE RIGHT ELEVATOR HINGE BL24.5, #2 AND #3 ANTI-ROTATION TAB SPACERS IAW CRJ 200 AMM TASK 27-34-01-000-801/400-801.Feb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157521Bolt · corrodedRH ELEVATOR HINGE RETAINER BRACKET BOLTS AT HINGE #1, BL24.5, AND #3 ARE CORRODED. (12EA) (C-CHECK RO 4/12/2021) REMOVE REPLACED R/H ELEVATOR RETAINER BRACKET BOLTS IAW CRJ 200 AMM 27-34-01-400-801Feb 5, 2021 · N908EV · Cndair CL6002B19 · Elevator StructureSDR SWIA202157497Structure · crackedNOSE LANDING GEAR WHEEL WELL FS215 RBL6 VERTICAL "Z" MEMBER IS CRACKED AT TOP FASTENER HOLE. (C-CHECK RO 4/12/2021) REPAIRED DAMAGE BY CUTTING OUT CRACK IAW REO 601R-53-11-3670 REV -- DATED 2021-03-09. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED COFeb 5, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202157496Structure · crackedNOSE LANDING GEAR WHEEL WELL FS215 LBL6 VERTICAL "Z" MEMBER IS CRACKED AT TOP FASTENER HOLE. (C-CHECK RO 4/12/2021) REPAIRED DAMAGE BY CUTTING OUT DAMAGE IAW REO 601R-53-11-3671 REV -A DATED 2021-03-13. COMPLETED TASK CARD 51-900-1003-SKY AND ATTACHED CFeb 5, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202157483Skin · dentedPAX DOOR SURROUND FUSELAGE SKIN IS DENTED AT FS 310.00 AT LHS STR 14 (C-CHECK RO 4/12/2021) REPAIRED IAW REO 601R-53-21-3396 REV -- DATED 2021-03-21. FORM 337 & MAJOR REPAIR TASK 51-900-1003-SKY COMPLETED AND ATTACHED. NET WEIGHT CHANGE IS -.12 LBS. REFeb 5, 2021 · N908EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202157520Bolt · corrodedALL STOP BRACKET BOLTS ON THE R/H AILERON FOR AILERON HINGE BOLTS ARE CORRODED. (12) TOTAL. (C-CHECK RO 4/12/2021) REMOVED AND REPLACED ALL STOP BRACKET BOLTS ON THE RH AILEON FOR THE THE AILERON HINGE BOLTS IAW CRJ 200 AMM 20-21-00-910-801 REF ATTACHEDFeb 2, 2021 · N908EV · Cndair CL6002B19 · Ailerons
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