N752EV

Service difficulty reports · 365

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 = 'N752EV' 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 SWI2024F01002Slat Track · damagedLEFT SLAT TRACK 2-3 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED SLAT TRACK 2-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1648 REV -- DATE 2024-07-31. COMPLIED WITH 51-900-10Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F01001Slat Track · damagedLEFT SLAT TRACK 2-2 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-2 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED THE LJun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F01000Slat Track · damagedLEFT SLAT TRACK 2-1 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK 2-1Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00999Slat Track · damagedLEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1643 REV -- DATE 2024-07-25. COMPLIED WITH 51-Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00998Slat Track · damagedLEFT SLAT TRACK 1-2 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LH SLAT TRACK 1-2 - REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED LEFT SLAT TRACK 1-2 - REO 670-57-Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00997Slat Track · damagedRIGHT SLAT TRACK 3-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 3-2, LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK REPAIRED PER REO 670-57-42-1638Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00996Striker · bentPASSENGER DOOR SURROUND STRUCTURE SEAL STRIKER BENT AT FORWARD LOWER CENT ROLLER ASSY (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIR OF PAX DOOR SURROUND SEAL STRIKER AT LOWER CENT ROLLER ASSY AREA ACCOMPLISHED PER REF CRJ 700 SRM 53-21-23-201-006-A01. ALL LEAK ANDJun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024F00995Slat Track · damagedRIGHT SLAT TRACK 2-2 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) 28399060 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 2-2, UPPER AND LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-00Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00994Slat Track · damagedRIGHT SLAT TRACK 2-1 HAS PITTING IN 2AREAS, 1 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON RIGHT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REMOVED SLAT Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00993Fitting · gougedPASSENGER DOOR SURROUND STRUCTURE FORWARD HANDRAIL FITTING GOUGED (C-CHECK RO 10/7/2024) (FILED OPEN)BLENDED FITTING AND FOUND OUT OF LIMITS. REPLACED WITH NEW FITTING REF. CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-31810 REV AE. COMPLIED WITH ALJun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024F00992Slat Track · damagedRIGHT SLAT TRACK 1-3 HAS PITTING IN 2 AREAS ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON RIGHT SLAT TRACK 1-3 ON LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIR ACCOMPLISHED PER COMPLIED WITH REO 670-57-4Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00991Slat Track · damagedRIGHT SLAT TRACK 1-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 1-2, UPPER AND LOWER SURFACE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1640 REV. -- DATJun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00990Skin · chafedCHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)CHAFE ON EXTERNAL SKIN INSIDE OF A PREVIOUS BLEND OR DENT. FS969.0 - FS985.00 STGR27 FOUND TO BE OUT OF ALLOWABLE LIMITS DUJun 17, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWI2024F00989Slat Track · damagedLEFT SLAT TRACK 3-1 HAS PITTING IN 2 AREAS ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED PITTING ON THE LH SLAT TRACK 3-1 REF REO 670-57-42-1639 REV -- DATED 2024-07-24. SEE CONTINUATION FOR DETAILS. COMPLIED WITH 51-900-100Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00988Slat Track · damagedLEFT SLAT TRACK 2-3 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED SLAT TRACK 2-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1648 REV -- DATE 2024-07-31. COMPLIED WITH 51-900-10Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00987Slat Track · damagedLEFT SLAT TRACK 2-2 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-2 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED THE LJun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00986Slat Track · damagedLEFT SLAT TRACK 2-1 HAS PITTING IN 4 AREAS, 2 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LEFT SLAT TRACK 2-1 ON UPPER AND LOWER SURFACE REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK 2-1Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00985Slat Track · damagedLEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED LEFT SLAT TRACK 1-3 HAS PITTING IN 3 AREAS REF REO 670-57-42-1643 REV -- DATE 2024-07-25. COMPLIED WITH 51-Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00984Slat Track · damagedLEFT SLAT TRACK 1-2 HAS PITTING IN 3 AREAS,1 ON THE LOWER SURFACE - 2 ON THE UPPER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON LH SLAT TRACK 1-2 - REF CRJ700 SRM 51-21-06-001-001-A01. REPAIRED LEFT SLAT TRACK 1-2 - REO 670-57-Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00983Slat Track · damagedRIGHT SLAT TRACK 3-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 3-2, LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-001-A01. SLAT TRACK REPAIRED PER REO 670-57-42-1638Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00982Striker · bentPASSENGER DOOR SURROUND STRUCTURE SEAL STRIKER BENT AT FORWARD LOWER CENT ROLLER ASSY (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIR OF PAX DOOR SURROUND SEAL STRIKER AT LOWER CENT ROLLER ASSY AREA ACCOMPLISHED PER REF CRJ 700 SRM 53-21-23-201-006-A01. ALL LEAK ANDJun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024F00981Slat Track · damagedRIGHT SLAT TRACK 2-2 HAS PITTING IN 3 AREAS, 2 ON THE LOWER SURFACE - 1 ON THE UPPER SURFACE. (MARKED IN RED) 28399060 (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 2-2, UPPER AND LOWER SURFACE - REF CRJ700 SRM 51-21-06-001-00Jun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00980Fitting · gougedPASSENGER DOOR SURROUND STRUCTURE FORWARD HANDRAIL FITTING GOUGED (C-CHECK RO 10/7/2024) (FILED OPEN)BLENDED FITTING AND FOUND OUT OF LIMITS. REPLACED WITH NEW FITTING REF. CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-31810 REV AE. COMPLIED WITH ALJun 17, 2024 · N752EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWI2024F00979Slat Track · damagedRIGHT SLAT TRACK 1-2 HAS PITTING IN 1 AREA ON THE LOWER SURFACE. (MARKED IN RED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED DAMAGE ON THE RIGHT-HAND SLAT TRACK 1-2, UPPER AND LOWER SURFACE. RECEIVED AND COMPLIED WITH ALL STEPS OF REO 670-57-42-1640 REV. -- DATJun 17, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F01108Bracket · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED BRACKET (SH670-33852-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED CLOSED) INSTALLED NEW FITTING IAW BOMBARDIER DRAWING SH670-33600 REV AD AND CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001Jun 16, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01107Fitting · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED CLOSED)FORWARD BAGGAGE BAY, INTERNAL STRUCTURE, MACHINED FITTING AT LBL24 (SH670-33390-1) REPLACED IAW CRJ 700 SRM 51-42-Jun 16, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA20240616Door Frame · gougedAVIONICS BAY DOOR SURROUND STRUCTURE STGR26L AFT OF FS333.00 GOUGED (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED GOUGE FROM STRINGER SPLICE AT FS333.00 STGR26L AND FOUND OUT OF LIMITS DUE TO NO PUBLISHED LIMITS FOR THE CIRCUMFERENTIAL JOINT AT FS333.00. REMOVEJun 16, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA20241009616Door Frame · gougedAVIONICS BAY DOOR SURROUND STRUCTURE STGR26L AFT OF FS333.00 GOUGED (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED GOUGE FROM STRINGER SPLICE AT FS333.00 STGR26L AND FOUND OUT OF LIMITS DUE TO NO PUBLISHED LIMITS FOR THE CIRCUMFERENTIAL JOINT AT FS333.00. REMOVED Jun 16, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2024F00958Bracket · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED BRACKET (SH670-33852-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED OPEN) INSTALLED NEW FITTING IAW BOMBARDIER DRAWING SH670-33600 REV AD AND CRJ700 SRM 51-42-21-001-001-A01 AND 51-42-22-001-001-AJun 16, 2024 · N752EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWI2024F00957Fitting · corrodedFORWARD BAGGAGE BAY INTERNAL STRUCTURE MACHINED FITTING (LBL24) (SH670-33390-1) CORROSION AROUND SCREW HOLES (C-CHECK RO 10/7/2024) (FILED OPEN)FORWARD BAGGAGE BAY, INTERNAL STRUCTURE, MACHINED FITTING AT LBL24 (SH670-33390-1) REPLACED IAW CRJ 700 SRM 51-42-21Jun 16, 2024 · N752EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWI2024F01090Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT LBR 9 AT APPROX. FS485.40 TO FS565.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED FLOOR BEAM CAP AT RBL 9.0 BETWEEN F/S 476.55 TO F/S 571 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01089Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT RBL 9 AT APPROX. FS565.40 TO FS677.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED CLOSED)INSTALLED NEW FLOOR BEAM FROM RBL 9 FS 565 TO FS 677. REF CRJ700 SRM 53-00-41-201-001-A01 , REO 670-53-31-913 REV-A DJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01088Floor Support · corrodedR/H FLOOR SILL BETWEEN FS677.00 TO FS693.00 HAS CORROSION (MARKED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED AND REPLACED WITH NEW R/H FLOOR SILL BETWEEN FS677.00 TO FS693.00 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-32170 REV V. COMPLIED WITH SKJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01087Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS477.40 TO FS565.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS477.40 TO FS565.00 IAW CRJ-700 SRM 53-00-41-201-001-A01 REV. 38 DAJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01086Mount · corrodedGALLEY 1 STRUCTURE MOUNT BOLT FITTING FWD INBOARD CORROSION (MARKED) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED, REPLACED AND INSTALLED NEW GALLEY 1 FWD INBOARD MOUNTING BOLT FITTING P/N SH670-32149 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. SH670-32Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage, Equipment Attach FittingsSDR SWI2024F01093Floor Support · corrodedMULTIPLE SPOTS OF CORROSION ON T-CAP AT RBL9 AT APPROXIMATELY FS855.00 - FS960.00 AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED FLOOR BEAM AT RBL 9.0 FROM F/S 854.45 TO F/S 977.00 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-51-298 REV. -- DATJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01092Floor Support · corrodedMULTIPLE SPOTS OF CORROSION ON T-CAP AT LBL9 AT APPROXIMATELY FS855.00 - FS977.00 AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)PERFORMED A BEAM REPAIR FROM FS855.00 TO FS904.00 PER CRJ 700 SRM 53-00-41-201-001-A01 AND REO# 670-53-51-301 REV:-- DATE:2024-08-1Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F01091Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED ON AFT SIDE, LOCATED AT FS879.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)EVALUATED CORROSION ON FRAME AT FS879.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202411040615Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED CLOSED)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024F00936Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT LBR 9 AT APPROX. FS485.40 TO FS565.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED FLOOR BEAM CAP AT RBL 9.0 BETWEEN F/S 476.55 TO F/S 571 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-31Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00935Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT RBL 9 AT APPROX. FS565.40 TO FS677.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)INSTALLED NEW FLOOR BEAM FROM RBL 9 FS 565 TO FS 677. REF CRJ700 SRM 53-00-41-201-001-A01 , REO 670-53-31-913 REV-A DATJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00934Floor Support · corrodedR/H FLOOR SILL BETWEEN FS677.00 TO FS693.00 HAS CORROSION (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED AND REPLACED WITH NEW R/H FLOOR SILL BETWEEN FS677.00 TO FS693.00 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-32170 REV V. COMPLIED WITH SKYWJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00933Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS477.40 TO FS565.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED L/H FLOOR BEAM CAP AT LBL 9 AT APPROX. FS477.40 TO FS565.00 IAW CRJ-700 SRM 53-00-41-201-001-A01 REV. 38 DATEJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00932Fitting · corrodedGALLEY 1 STRUCTURE MOUNT BOLT FITTING FWD INBOARD CORROSION (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)REMOVED, REPLACED AND INSTALLED NEW GALLEY 1 FWD INBOARD MOUNTING BOLT FITTING P/N SH670-32149 REF CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. SH670-3212Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00952Frame · corrodedREAR FUSELAGE INTERNAL STRUCTURE CORROSION ON FS1015.00 FORWARD SIDE BETWEEN STGR22L TO STGR23L AS MARKED (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED CORROSION ON FRAME AT FS1015.00 STGR22L-STGR23L FWD SIDE AND FOUND OUT OF LIMITS PER CRJ700SRM 53-61-06-101-0Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024F00950Floor Support · corrodedMULTIPLE SPOTS OF CORROSION ON T-CAP AT LBL9 AT APPROXIMATELY FS855.00 - FS977.00 AS MARKED (C-CHECK RO 10/7/2024) (FILED OPEN)PERFORMED A BEAM REPAIR FROM FS855.00 TO FS904.00 PER CRJ 700 SRM 53-00-41-201-001-A01 AND REO# 670-53-51-301 REV:-- DATE:2024-08-12 Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00949Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED ON AFT SIDE, LOCATED AT FS879.00 BETWEEN STGR26L AND STGR26R AS MARKED (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION ON FRAME AT FS879.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A0Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024F00948Frame · corrodedAFT INTERNAL FUSELAGE FRAME IS CORRODED, LOCATED AT FS863.00 BETWEEN STGR26L AND STGR26R AS MARKED MX (C-CHECK RO 10/7/2024) (FILED OPEN)EVALUATED CORROSION AT FS863.00 STGR26L-STGR26R AND FOUND OUT OF LIMITS PER CRJ700SRM 53-51-06-101-003-A01. RECEIVED AND COJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWI2024F00947Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT LBR 9 AT APPROX. FS485.40 TO FS565.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED FLOOR BEAM CAP AT RBL 9.0 BETWEEN F/S 476.55 TO F/S 571 IAW CRJ 700 SRM 53-00-41-201-001-A01 AND REO 670-53-31Jun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2024F00946Floor Support · corrodedMULTIPLE SPOTS OF CORROSION NOTED ON R/H FLOOR BEAM CAP AT RBL 9 AT APPROX. FS565.40 TO FS677.00 (MARKED) (C-CHECK RO 10/7/2024) (FILED OPEN)INSTALLED NEW FLOOR BEAM FROM RBL 9 FS 565 TO FS 677. REF CRJ700 SRM 53-00-41-201-001-A01 , REO 670-53-31-913 REV-A DATJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
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