N906EV

Service difficulty reports · 293

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 = 'N906EV' 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 SWI2024F01242Bracket · crackedUPPER PAX DOOR STOP BRACKET ON FUSELAGE AT FS310 CRACKED (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND INSTALLED NEW UPPER PAX DOOR FWD STOP BRACKET AS PER CRJ200 SRM 51-42-21 AND DWG 601R31700 REV-F. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO DFECTS NOTAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202411150812Frame · corrodedFWD FRAME AT FS349 STGR22R HAS CORROSION (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED CORROSION FROM FWD FRAME AT FS 349 STGR 22R,ORIGINAL MATERIAL THICKNESS IS 0.100" REF DRW. 601R320402 REV NC. REMAINING MATERIAL THICKNESS PER NDT IS 0.035". MATERIAL LOSS IAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01042Intercostal · corrodedPASSENGER DOOR INTERCOSTAL DD3 CORROSION (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND INSTALLED NEW PAX DOOR MID DD3 IAW CRJ 200 SRM 51-42-06, CRJ200 SRM 51-42-21 AND DWG 601R31702 REV. N. NO LEAKS NOTED AT THIS TIME SEE CONTINUATION CARD FOR DETAILS AND CAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01041Frame Splice · corrodedFRAME SPLICE FS349 STGR23R HAS CORROSION AND IS BULGING (C-CHECK RO 10/26/2024) (FILED OPEN) FRAME SPLICE FS 349.00 STGR. 23R HAS MULTIPLE SPOTS OF EXFOLATED CORROSION WITH 100% MATERIAL LOSS AND IS OUT OF LIMITS REF CRJ200 SRM 53-00-00. REMOVED AND INSTALLEDAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01040Frame · corrodedFRAME AT FS333 STGR26L-STGR22R HAS AREAS OF CORROSION (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED FRAME AT FS333 STGR26L-22R REF DRW. 601R32004 REV. N, REF DRW. 601R31022 REV. B, REF CRJ200 SRM 51-42-06 AND REF CRJ200 SRM 51-42-21. COMPLIED WITH TAug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWI2024F01039Bracket · crackedUPPER PAX DOOR STOP BRACKET ON FUSELAGE AT FS310 CRACKED (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND INSTALLED NEW UPPER PAX DOOR FWD STOP BRACKET AS PER CRJ200 SRM 51-42-21 AND DWG 601R31700 REV-F. COMPLIED WITH TASK CARD 51-900-1003-SKY. NO DFECTS NOTEDAug 12, 2024 · N906EV · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2024102812Frame · corrodedFWD FRAME AT FS349 STGR22R HAS CORROSION (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED CORROSION FROM FWD FRAME AT FS 349 STGR 22R,ORIGINAL MATERIAL THICKNESS IS 0.100" REF DRW. 601R320402 REV NC. REMAINING MATERIAL THICKNESS PER NDT IS 0.035". MATERIAL LOSS IS Aug 12, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2024111520809Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BETWEEN FS409+118-FS559+10 (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BETWEEN FS409+118-FS559+10 REF CRJ200 SRM 51-21-06Aug 9, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01272Angle · cracked280CLIP CRACKED AT RBL9 (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED 1EA NEW CLIP PN 601R31113-58 AT FS280.00 RBL9 COMMON TO SEAT RAIL REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21.COMPLIED WITH TASK CARD 51-900-1003-SKY.Aug 9, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, StructureSDR SWI2024F01059Floorbeam · cracked280CLIP CRACKED AT RBL9 (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED 1EA NEW CLIP PN 601R31113-58 AT FS280.00 RBL9 COMMON TO SEAT RAIL REF. CRJ200 SRM 51-42-06 AND CRJ200 SRM 51-42-21.COMPLIED WITH TASK CARD 51-900-1003-SKY.Aug 9, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01058Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS409+118-FS559+10 (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS409+118-FS559+10 REF CRJ200 SRM 51-21-06FLAug 9, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA2024102809Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BETWEEN FS409+118-FS559+10 (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED MULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BETWEEN FS409+118-FS559+10 REF CRJ200 SRM 51-21-06ORAug 9, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01251Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON L/H PRESSURE FLOOR SILL (MARKED) BLENDED MULTIPLE SPOTS ON L/H PRESSURE FLOOR SILL PER CRJ200 SRM 51-21-06EVALAUTED MULTIPLE SPOTS OF CORROSION ON L/H PRESSURE FLOOR SILL ORIGINAL THICKNESS IN CHEMILLED POCKET 0.055'' AND Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01250Floorbeam · corrodedFLOOR SUPPORT ANGLE CORRODED COMMON TO 621 BULKHEAD BETWEEN LBL27-L/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED CORROSION ON FLOOR SUPPORT ANGLE COMMON TO FS621 BULKHEAD BETWEEN LBL27-L/H FLOOR SILL. FOUND OUT OF LIMITS. REPAIRED PER RAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01249Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS559+16-FS559+112 (MARKED) REMOVED COROSION FROM MULTIPLE SPOTS ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS559+16-FS559+112 REF CRJ200 SRM 51-21-06 EVALUATED DAMAGE ON FLOOR BEAM TOP CAP ATAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01248Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BTWEN FS559+16-FS559+112 (MARKED) COMPLIED WITH MHIRJ REO 601R-53-51-686 REV -- 2024-09-13 AND DWG# 601R31119 REV H IN THE REMOVAL AND REPLACE OF THE FLOOR BEAM TOP CAP AT RBL9 FS559+16 TO FS559+Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01271Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN LBL27-L/H FLOOR SILL (MARKED) REMOVED AND REPLACED FLOOR SUPPORT STRAP PN 601R31025-29 AT FS559 BETWEEN LBL27 AND LH FLOOR SILL REF CRJ 200 SRM 51-42-06. REV.39A DATE 12/18/202 AND DRAWING 601R31025 REV N SEAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Internal Mounting StructureSDR SWIA2024111510808Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN RBL27-R/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED, LOCATED AND DRILLED NEW FLOOR SUPPORT STRAP AND INSTALLED NEW FLOOR SUPPORT STRAP AT FS559 BTWN RBL27-R/H FLOOR SILL REF CRJ200 SRAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024111501247Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN LBL27-L/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED AND REPLACED FLOOR SUPPORT STRAP PN 601R31025-29 AT FS559 BETWEEN LBL27 AND LH FLOOR SILL REF CRJ 200 SRM 51-42-06. REV.39A DATE 12Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01048Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON L/H PRESSURE FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)BLENDED MULTIPLE SPOTS ON L/H PRESSURE FLOOR SILL PER CRJ200 SRM 51-21-06EVALAUTED MULTIPLE SPOTS OF CORROSION ON L/H PRESSURE FLOOR SILL ORIGINAL THICKNEAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01047Floor Support · corrodedFLOOR SUPPORT ANGLE CORRODED COMMON TO 621 BULKHEAD BETWEEN LBL27-L/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED CORROSION ON FLOOR SUPPORT ANGLE COMMON TO FS621 BULKHEAD BETWEEN LBL27-L/H FLOOR SILL. FOUND OUT OF LIMITS. REPAIRED PER REOAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01046Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS559+16-FS559+112 (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED COROSION FROM MULTIPLE SPOTS ON FLOOR BEAM TOP CAP AT LBL9 BETWEEN FS559+16-FS559+112 REF CRJ200 SRM 51-21-06 EVALUAAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F01045Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON FLOOR BEAM TOP CAP AT RBL9 BTWEN FS559+16-FS559+112 (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)COMPLIED WITH MHIRJ REO 601R-53-51-686 REV -- 2024-09-13 AND DWG# 601R31119 REV H IN THE REMOVAL AND REPLACE OF THE FLOOR BEAMAug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWI2024F10281044Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN LBL27-L/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED FLOOR SUPPORT STRAP PN 601R31025-29 AT FS559 BETWEEN LBL27 AND LH FLOOR SILL REF CRJ 200 SRM 51-42-06. REV.39A DATE 12/1Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA20241028008Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN RBL27-R/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED, LOCATED AND DRILLED NEW FLOOR SUPPORT STRAP AND INSTALLED NEW FLOOR SUPPORT STRAP AT FS559 BTWN RBL27-R/H FLOOR SILL REF CRJ200 SRM Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWI2024F01044Floor Support · corrodedCORROSION NOTED ON FLOOR SUPPORT STRAP AT FS559 BTWN LBL27-L/H FLOOR SILL (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED AND REPLACED FLOOR SUPPORT STRAP PN 601R31025-29 AT FS559 BETWEEN LBL27 AND LH FLOOR SILL REF CRJ 200 SRM 51-42-06. REV.39A DATE 12/1Aug 8, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202411150807Stop Fitting · damagedLH OVERWING EMER DOOR FWD MIDDLE STOP FITTING, ON THE SURROUND, HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 10/26/2024) (FILED CLOSED)FABER, CONNOR - 09/09/2024 05:54 COMPLETE: REPAIRED LH OVERWING EMER DOOR FWD MIDDLE STOP FITTING, ON THE SURROUND, IAW REO 601R-53Aug 7, 2024 · N906EV · Cndair CL6002B19 · Emergency ExitsSDR SWI2024F01038Stop Fitting · damagedLH OVERWING EMER DOOR FWD BOTTOM STOP FITTING, ON THE SURROUND, HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH OVERWING EMER DOOR FWD BOTTOM STOP FITTING, ON THE SURROUND, IAW REO 601R-53-41-3251 REV --, 2024-09-03. SEE CONINUATION Aug 7, 2024 · N906EV · Cndair CL6002B19 · Emergency ExitsSDR SWI2024F01037Stop Fitting · damagedLH OVERWING EMER DOOR AFT BOTTOM STOP FITTING, ON THE SURROUND, HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH OVERWING EMER DOOR AFT BOTTOM STOP FITTING, ON THE SURROUND, IAW REO 601R-53-41-3251 REV --, 2024-09-03. SEE CONTINUATIONAug 7, 2024 · N906EV · Cndair CL6002B19 · Emergency ExitsSDR SWI2024F01036Stop Fitting · damagedLH OVERWING EMER DOOR AFT MIDDLE STOP FITTING, ON THE SURROUND, HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)REPAIRED LH OVERWING EMER DOOR AFT MIDDLE STOP FITTING, ON THE SURROUND, IAW REO 601R-53-41-3251 REV --, 2024-09-03. SEE CONINUATION Aug 7, 2024 · N906EV · Cndair CL6002B19 · Emergency ExitsSDR SWIA2024102807Stop Fitting · damagedLH OVERWING EMER DOOR FWD MIDDLE STOP FITTING, ON THE SURROUND, HAS IMPACT DAMAGE (MARKED) (C-CHECK RO 10/26/2024) (FILED OPEN)FABER, CONNOR - 09/09/2024 05:54 COMPLETE: REPAIRED LH OVERWING EMER DOOR FWD MIDDLE STOP FITTING, ON THE SURROUND, IAW REO 601R-53-4Aug 7, 2024 · N906EV · Cndair CL6002B19 · Emergency ExitsSDR SWI2024F01246Floor Support · corrodedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED CORROSION ON R/H FLOOR SILL FROM FS 409+128 TO FS 559.00. FOUND CORROSION ON R/H FLOOR ANGLE FROM FS449.85- FS473.15 AND ON FLOOR SILL AROUND NUTPLATE HOLE AT FS559.00. CAMP28644789 (C-CHECK RO 10/26/2Aug 6, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202411150806Skin · damagedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED BLOWN OUT HOLE ON FUSELAGE LOCATED AT PANEL 132AL FOUND FREEZE PLUG MISSING. CAMP28644781 (C-CHECK RO 10/26/2024) (FILED CLOSED)FABRICATED AND INSTALLED FREEZE PLUG IAW REO 601R-53-11-162 REV -D 2019-02Aug 6, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWI2024F01043Floor Support · corrodedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED CORROSION ON R/H FLOOR SILL FROM FS 409+128 TO FS 559.00. FOUND CORROSION ON R/H FLOOR ANGLE FROM FS449.85- FS473.15 AND ON FLOOR SILL AROUND NUTPLATE HOLE AT FS559.00. CAMP28644789 (C-CHECK RO 10/26/2Aug 6, 2024 · N906EV · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2024102806Skin · damagedDURING DETAILED VISUAL INSPECTION FOR PREVIOUSLY REPAIRED BLOWN OUT HOLE ON FUSELAGE LOCATED AT PANEL 132AL FOUND FREEZE PLUG MISSING. CAMP28644781 (C-CHECK RO 10/26/2024) (FILED OPEN)FABRICATED AND INSTALLED FREEZE PLUG IAW REO 601R-53-11-162 REV -D 2019-02-0Aug 6, 2024 · N906EV · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202411120802Skin · gougedRIGHT WING OUTBOARD FLAP HAS MULTIPLE GOUGED VANE MOUNTS AND STRUCTURES AS MARKED (C-CHECK RO 10/26/2024) (FILED CLOSED)BLENDED GOUGES ON RIGHT WING OUTBOARD FLAP HAS MULTIPLE VANE MOUNTS AND STRUCTURES. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEAug 2, 2024 · N906EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2024102802Vane · gougedRIGHT WING OUTBOARD FLAP HAS MULTIPLE GOUGED VANE MOUNTS AND STRUCTURES AS MARKED (C-CHECK RO 10/26/2024) (FILED OPEN)BLENDED GOUGES ON RIGHT WING OUTBOARD FLAP HAS MULTIPLE VANE MOUNTS AND STRUCTURES. REF CRJ200 SRM 51-12-00. FOUND TO BE OUT OF LIMITS. RECEIVAug 2, 2024 · N906EV · Cndair CL6002B19 · Trailing Edge FlapsSDR SWI2024F01277Pcu · failedL/H ELEVATOR PCU #3 (INBORD) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK( MX#28623120) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED L/H INBD/ #3 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW/SERVICEABLE L/H INB #3 ELEVATOR PCU REF. CRJ-200 Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01276Pcu · failedL/H ELEVATOR PCU #2 (MIDDLE) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK( MX#28623117) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED L/H MIDDLE #2 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW/SERVICEABLE L/H MIDDLE #2 PCU ELEVATOR REF. CRJ-Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01275Pcu · failedL/H ELEVATOR PCU #1 (OUTBORD) FAILED BEARING BACKLASH CHECK( MX#28623112) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED L/H OTBD/ #1 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW SERVICEABLE L/H OTBD/ #1 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-4Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01274Pcu · failedR/H ELEVATOR PCU #3 (INBORD) FAILED BEARING BACKLASH CHECK (MX#28623011) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED R/H ELEVATOR PCU #3(INBOARD) REF CRJ200 AMM 27-33-01-000-801. INSTALLED REPAIRED RH ELEVATOR PCU #3 PN: 27600-3 SN: MAL-5078 (INBD) WITH NEWAug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01273Pcu · failedR/H ELEVATOR PCU #2 (MIDDLE) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK (MX#28623006) (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED R/H MIDDLE/ #2 PCU ELAVATOR REF CRJ200 AMM 27-33-01-000-801-A01. INSTALLED NEW R/H MIDDLE/#2 PCU ELAVATOR REF CRJ200 AMM 27-Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWIA20240801Pcu · failedR/H ELEVATOR PCU #1 ( OUTBORD) FAILED BACKLASH AND BEARING BACKLASH CHECK (C-CHECK RO 10/26/2024) (FILED CLOSED)REMOVED R/H OTBD/ #1 PCU ELAVATOR REF CRJ200 AMM 27-33-01-000-801-A01. INSTALLED NEW R/H OTBD #1 PCU ELAVATOR REF CRJ200 AMM 27-33-01-400-801-A01.Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01070Pcu · failedL/H ELEVATOR PCU #3 (INBORD) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK( MX#28623120) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED L/H INBD/ #3 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW/SERVICEABLE L/H INB #3 ELEVATOR PCU REF. CRJ-200 AMAug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01069Pcu · failedL/H ELEVATOR PCU #2 (MIDDLE) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK( MX#28623117) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED L/H MIDDLE #2 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW/SERVICEABLE L/H MIDDLE #2 PCU ELEVATOR REF. CRJ-20Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01068Pcu · failedL/H ELEVATOR PCU #1 (OUTBORD) FAILED BEARING BACKLASH CHECK( MX#28623112) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED L/H OTBD/ #1 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-000-801. INSTALLED NEW SERVICEABLE L/H OTBD/ #1 PCU ELEVATOR REF. CRJ-200 AMM 27-33-01-400Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01067Pcu · failedR/H ELEVATOR PCU #3 (INBORD) FAILED BEARING BACKLASH CHECK (MX#28623011) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED R/H ELEVATOR PCU #3(INBOARD) REF CRJ200 AMM 27-33-01-000-801. INSTALLED REPAIRED RH ELEVATOR PCU #3 PN: 27600-3 SN: MAL-5078 (INBD) WITH NEW HAug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWI2024F01066Pcu · failedR/H ELEVATOR PCU #2 (MIDDLE) FAILED PCU BACKLASH AND BEARING BACKLASH CHECK (MX#28623006) (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED R/H MIDDLE/ #2 PCU ELAVATOR REF CRJ200 AMM 27-33-01-000-801-A01. INSTALLED NEW R/H MIDDLE/#2 PCU ELAVATOR REF CRJ200 AMM 27-33Aug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWIA202410280111Pcu · failedR/H ELEVATOR PCU #1 ( OUTBORD) FAILED BACKLASH AND BEARING BACKLASH CHECK (C-CHECK RO 10/26/2024) (FILED OPEN)REMOVED R/H OTBD/ #1 PCU ELAVATOR REF CRJ200 AMM 27-33-01-000-801-A01. INSTALLED NEW R/H OTBD #1 PCU ELAVATOR REF CRJ200 AMM 27-33-01-400-801-A01. PAug 1, 2024 · N906EV · Cndair CL6002B19 · Elevator Control SystemSDR SWIA202163093None · damagedCREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 802696 FOUND CARGO DOOR AFT TRACK STOPPER SEVERELY DAMAGED. (FLIGHT 5762 - FILED CLOSED) REMOVED AND REPLACED CARGO DOOR AFT TRACK STOPPER WITH SERVICEABLE UNIT REF CRJ-200 AMM 52-31-00.Dec 13, 2021 · N906EV · Cndair CL6002B19 · Doors
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