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 SWI2024F00945Floor 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 SWI2024F00944Floor 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 SWI2024F00943Fitting · 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 SWI2024F00942Frame · 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 SWIA20241009615Floorbeam · corrodedMULTIPLE SPOTS OF CORROSION ON T-CAP AT RBL9 AT APPROXIMATELY FS855.00 - FS960.00 AS MARKED (C-CHECK RO 10/7/2024) (FILED OPEN)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. -- DATEDJun 15, 2024 · N752EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2024F00940Floor 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 SWI2024F00938Frame · 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 SWI2024F00941Floorbeam · 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 Main, Floor BeamSDR SWI2024F00931Floorbeam · 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 Main, Floor BeamSDR SWI2024F00930Floor 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 SWI2024F00929Floorbeam · 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 Main, Floor BeamSDR SWI2024F00928Fitting · 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 · Buffet/GalleysSDR SWI2024F00927Frame · 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 SWI2024F00925Floorbeam · 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 Main, Floor BeamSDR SWI2024F00924Frame · 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 SWI2024F00937Frame · 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 SWI2024F01085Bracket · crackedL/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 10/7/2024) (FILED CLOSED):INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANS COWL . REF. REO 670-54-21-971, REV. B, 2023-11-28 AND COMPLIED WITH 51-900-1002-SKY.Jun 12, 2024 · N752EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024F01084Bracket · crackedL/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 10/7/2024) (FILED CLOSED)INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28, AND COMPLIED WITH 51-900-1002-SKYJun 12, 2024 · N752EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA20240612Stiffener · pulledR/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED/SHEARED (C-CHECK RO 10/7/2024) (FILED CLOSED)REPAIRED R/H UPPER TRANSCOWL AT FASTENER HOLES COMMON TO ZED STIFFENER, REF. REO 670-54-21-1655, REV. --, 2024-08-05. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 5Jun 12, 2024 · N752EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA20241009612Stiffener · pulledR/H UPPER TRANSCOWL Z STIFFENER RIVETS ARE PULLED/SHEARED (C-CHECK RO 10/7/2024) (FILED OPEN)REPAIRED R/H UPPER TRANSCOWL AT FASTENER HOLES COMMON TO ZED STIFFENER, REF. REO 670-54-21-1655, REV. --, 2024-08-05. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-Jun 12, 2024 · N752EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024F00923Stand Off · crackedL/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 10/7/2024) (FILED OPEN)INSTALLED 1 EA. NEW STANDOFF P/N CN624-2082-201 ON L/H LOWER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28, AND COMPLIED WITH 51-900-1002-SKYJun 12, 2024 · N752EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2024F00975Roller · wornL/H WING SLAT TRACK 3-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SIDE ROLLER 4EA IAW CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL TEST PASSED.Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00974Roller · wornL/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WORN BEYOND LIMITS (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW L/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WITH NEW SHIMS AS NEEDED; REF CRJ-700 AMM 27-81-44-000-802-A01. GAP AND FREEDOM OF MOVEMENTJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00973Roller · wornL/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 2EA NEW/SERVICEABLE AFT SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT LH SLAT-TRACK 1-2 REF CRJ700 AMM 27-81-44-400-801 A01. GAPS AND MOVEJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00972Roller · wornR/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 4EA NEW/SERVICEABLE SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT RH SLAT-TRACK 1-2 - REF CRJ700 AMM 27-81-44-400-801 A01, GAP AND MOVEMENJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00971Roller · wornR/H WING SLAT TRACK 3-2 2EA FWD SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 3-2 FWD SIDE ROLLERS P/N CC670-12027-3. REF - CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL CHECKJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00970Roller · wornR/H WING SLAT TRACK 2-2 3EA SIDE ROLLERS WORN BEYOND LIMITS (FWD OTBD, FWD INBD, AFT OTBD) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 2-2 SIDE ROLLERS (FWD OTBD, FWD INBD, AFT OTBD). CRJ700 AMM 27-81-44-Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00969Roller · wornL/H WING SLAT TRACK 3-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SIDE ROLLER 4EA IAW CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL TEST PASSED.Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00968Roller · wornL/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WORN BEYOND LIMITS (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW L/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WITH NEW SHIMS AS NEEDED; REF CRJ-700 AMM 27-81-44-000-802-A01. GAP AND FREEDOM OF MOVEMENTJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00967Roller · wornL/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 2EA NEW/SERVICEABLE AFT SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT LH SLAT-TRACK 1-2 REF CRJ700 AMM 27-81-44-400-801 A01. GAPS AND MOVEJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00966Roller · wornR/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 4EA NEW/SERVICEABLE SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT RH SLAT-TRACK 1-2 - REF CRJ700 AMM 27-81-44-400-801 A01, GAP AND MOVEMENJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00965Roller · wornR/H WING SLAT TRACK 3-2 2EA FWD SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 3-2 FWD SIDE ROLLERS P/N CC670-12027-3. REF - CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL CHECKJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00964Roller · wornR/H WING SLAT TRACK 2-2 3EA SIDE ROLLERS WORN BEYOND LIMITS (FWD OTBD, FWD INBD, AFT OTBD) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 2-2 SIDE ROLLERS (FWD OTBD, FWD INBD, AFT OTBD). CRJ700 AMM 27-81-44-Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00963Roller · wornL/H WING SLAT TRACK 3-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SIDE ROLLER 4EA IAW CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL TEST PASSED.Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00962Roller · wornL/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WORN BEYOND LIMITS (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW L/H WING SLAT TRACK 2-2 4EA SIDE ROLLERS WITH NEW SHIMS AS NEEDED; REF CRJ-700 AMM 27-81-44-000-802-A01. GAP AND FREEDOM OF MOVEMENTJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00961Roller · wornL/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 2EA NEW/SERVICEABLE AFT SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT LH SLAT-TRACK 1-2 REF CRJ700 AMM 27-81-44-400-801 A01. GAPS AND MOVEJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00960Roller · wornR/H WING SLAT TRACK 1-2 4EA SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED 4EA NEW/SERVICEABLE SIDE ROLLERS WITH NEW SHIMS AS REQUIRED AT RH SLAT-TRACK 1-2 - REF CRJ700 AMM 27-81-44-400-801 A01, GAP AND MOVEMENJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWI2024F00959Roller · wornR/H WING SLAT TRACK 3-2 2EA FWD SIDE ROLLERS WORN BEYOND LIMITS. (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 3-2 FWD SIDE ROLLERS P/N CC670-12027-3. REF - CRJ700 AMM 27-81-44-400-803-A01. OPERATIONAL CHECKJun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA20240608Slat Track · wornR/H WING SLAT TRACK 2-2 3EA SIDE ROLLERS WORN BEYOND LIMITS (FWD OTBD, FWD INBD, AFT OTBD) (C-CHECK RO 10/7/2024) (FILED CLOSED)REMOVED WORN AND INSTALLED NEW SERVICEABLE RH WING SLAT TRACK 2-2 SIDE ROLLERS (FWD OTBD, FWD INBD, AFT OTBD). CRJ700 AMM 27-81-44-Jun 8, 2024 · N752EV · Cndair CL6002C10 · Leading Edge DevicesSDR SWIA2021081960465Seat Track · crackedUPON INSTALLATION ON PAX SEAT 16BA, NEW FLOOR SEAT TRACK CRACKED AND RAISED UP AT FWD FOOT MOUNT. SEAT TRACK IS LBL9 AT APPROX FS830.40 TO FS985.00 (C-CHECK RO 8/18/2021) REMOVED AND INSTALLED NEW LBL9 SEAT TRACK AT FS830.40 TO FS985.00. REF: CRJ700 AMMJul 31, 2021 · N752EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021081960435Stringer · corrodedSTRINGER 23R JOINT SPLICE AT FS333 HAS CORROSION (C-CHECK RO 8/18/2021) INSTALLED NEW SERVICEABLE STRINGER JOINT SPLICE AT FS333, STGR 23R REF. CRJ700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG NO. SH670-32420 REV. E. LEAK CHECK GOOD. COMPLIED WITH SKYJul 26, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960434Stringer Splice · corrodedSTRINGER 24R JOINT SPLICE AT FS333 HAS CORROSION (C-CHECK RO 8/18/2021) INSTALLED NEW STRINGER 24R JOINT SPLICE AT FS333 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG SH670-32420 REV E. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYJul 24, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960433Stringer · corrodedSTRINGER 23R HAS CORROSION BETWEEN FS 280.00 AND FS 333.00 (C-CHECK RO 8/18/2021) INSTALLED NEW SERVICEABLE STRINGER 23R BETWEEN FS280-FS333 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG NO. SH670-31630 REV. FJul 24, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960432Stringer · corrodedSTRINGER 24R BET. FS280 TO FS333 HAS CORROSION (C-CHECK RO 8/18/2021) INSTALLED NEW SERVICEABLE STRINGER 24R BETWEEN FS280-FS333 REF. CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG NO. SH670-31630 REV. F. LEAK CHECKJul 22, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960431Vane · out of limitsLEFT OUTBOARD FLAP VANE RIB AT LEFT WING WS 296.07 OUT OF LIMITS (C-CHECK RO 8/18/2021) REMOVED AND REPLACED LEFT OUTBOARD VANE RIB WITH NEW RIB. REF: CRJ700 SRM 57-53-02-201-002-A01 TYPE1 / COMPLIED WITH SKY WEST TASK CARD 51-900-1002-SKYJul 20, 2021 · N752EV · Cndair CL6002C10 · Trailing Edge FlapsSDR SWIA2021081960430Stringer · corrodedCORROSION ON STRG26R BETWEEN FS280 AND FS333 (C-CHECK RO 8/18/2021) INSTALLED NEW STGR 26R BETWEEN FS 280.00 AND FS 333.00 REF CRJ 700 SRM 51-42-21-001-001-A01, CRJ 700 SRM 51-42-06-001-001-A01 AND DWG. NO. SH670-31630 REV.F. LEAK CHECK GOOD. COMPLIEDJul 15, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960429Stringer · corrodedCORROSION ON STRG25R SPLICE AT FS333 (C-CHECK RO 8/18/2021) INSTALLED NEW STGR.25R JOINT SPLICE AT FS 333 REF CRJ 700 SRM 51-42-06-001-001-A01 AND DWG. NO. SH670-32420 REV. E. LEAK CHECK GOOD COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKYJul 15, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960428Stringer · corrodedCORROSION ON STRG25R BETWEEN FS280 AND FS333 (C-CHECK RO 8/18/2021) INSTALLED NEW STRINGER 25R BETWEEN FS 280.00 AND FS333.00 REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND DWG. NO. SH670-31630 REV. F. LEAK CHECK GOOD. TASK CJul 15, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202160427Stringer · corrodedCORROSION ON STRG24L BETWEEN FS349 AND FS333 (C-CHECK RO 8/18/2021) REMOVED AND REPLACED STGR24L BETWEEN FS349 AND FS333. REF: CRJ 700 SRM 53-00-03-201-001 (A01) AND DWG SH690-31350 REV M. COMPLIED WITH TASK CARD 51-900-1002 SKY (CL600-2C10) STRUCTURAL Jul 15, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2021081960426Doubler · corrodedCORROSION AT THE LOWER FWD TCAS ANTENNA, INTERNAL DOUBLER, AROUND DOME NUTS (C-CHECK RO 8/18/2021) INSTALLED NEW LNTERNAL DOUBLER AT THE LOWER FWD TCAS ANTENNA REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-41-02-001-001-A01 AND DWG SH670-32364 REJul 15, 2021 · N752EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
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