N751EV

Service difficulty reports · 281

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 = 'N751EV' 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 SWIA2026061576242Tru · faultedDC BUSS 2 CAUTION MESSAGE. SMELLED A BURNING ODOR FOR ABOUT A MINUTE BEFORE GOING AWAY. MULTIPLE ASSOCIATED FAILURES INCLUDING CAUTION MESSAGES AS WELL AS MANY STATUS MESSAGES. MEL 24-31-1CAT B. SMOD APPROVEL REQUIRED FOR RTS DUE TO ODI EVENT (FLIGHT 468Jun 15, 2026 · N751EV · Cndair CL6002C11 · DC Power Distribution SystemSDR SWIA2026040375667Control Unit · faultedSTEERING INOPERATIVE CAUTION AFTER PUSHBACK. RAN QRH MESSAGE CLEARED. (FLIGHT 4710) INTERROGATED MDC AND FOUND FAULT CODE B-007456 FOR NWS ECU FAILED DUE TO INTERNAL FAULT. REMOVED AND REPLACED NWS STEERING ECU REFERENCING APPLICABLE STEPS OF AMM 32-51-10. Apr 3, 2026 · N751EV · Cndair CL6002C11 · Landing Gear Steering SystemSDR SWIA20250317120Plate · gougedUPON REMOVAL OF CARGO NET MOUNTING PLATE INTERCOSTAL FOUND DEEP GOUGES IN RADIUS. (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INTERCOSTAL WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-06-001--001-A01,51-42-21-001-001-A01, 51-45-00-001--001-A01, DWG-SH670-335Jan 20, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202503170118Frame · corrodedFOUND CORROSION ON FWD WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS 295 STR24L ( MX# 29494459 JOB OP: HN00214212 ) (C-CHECK RO 3/14/2025) REPAIRED FWD. WEB FACE AND LOWER FLANGE OF FRAME AT FUSELAGE BELOW FLOOR FS295 STR24L IAW REO 670Jan 18, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202503170114Floor Support · corrodedCORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE, RH SIDE AT APPROXIMATELY FS 1088. SEE ATTACHED PIC. (C-CHECK RO 3/14/2025) REMOVED CORROSION ON UPPER SURFACE OF FLOOR SUPPORT STRUCTURE (SILL) REF-CRJ-700 SRM 51-21-06-001-001 A01 AND FOUND AREA REJan 14, 2025 · N751EV · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR SWIA202503170110Landing · crackedRH SIDE TRU BAY DOOR LOWER LANDING HAS A CRACK ON AFT LATCH CUT OUT (C-CHECK RO 3/14/2025) REMOVED AND REPLACED TRU LOWER LANDING WITH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, 51-42-22-001-001-A01 , REO- 670-53-11-2086 REV -- DATE 2025-01-16. (Jan 10, 2025 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F00333Bayonet · crackedRIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET IS CRACKED. 29442720 (C-CHECK RO 3/14/2025) REPAIRED RIGHT OVERWING EXIT DOOR AFT PROXIMITY SWITCH BAYONET BY COMPLYING WITH ALL STEPS OF REO# 670-52-21-106 REV:-- DATE: 2025-02-03. COMPLIED WITH SKYJan 8, 2025 · N751EV · Cndair CL6002C10 · Emergency ExitsSDR SWIA202503170108Bayonet · crackedLEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS ARE CRACKED. 29442703 (C-CHECK RO 3/14/2025) REPAIRED LEFT OVERWING EXIT DOOR FORWARD & AFT PROXIMITY SWITCH BAYONETS REF GREO PL 670-52-21-103 REV:--:DATE:2024-11-06Jan 8, 2025 · N751EV · Cndair CL6002C10 · Emergency ExitsSDR SWIA202503170103Bracket · crackedS/N 0440LH WING, SLAT TRAK CANISTER BRACKET 1-3 IS CRACKED. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED THE LH WING SLAT TRACK CANNISTER BRACKET AT SLAT TRACK 1-3 REF REO 670-57-42-577 REV -- 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS Jan 3, 2025 · N751EV · Cndair CL6002C10 · Wing, Attach FittingsSDR SWIA2025031701231Pitot Tube · scratchedR/H PITOT STATIC PROBE CUTOUT ON THE UPPER SKIN AT FS210.00 BETWEEN STGR 14 AND STGR 15 LOWER AFT HOLE HAS MULTIPLE SCRATCHES AS MARKED (C-CHECK RO 3/14/2025) WET INSTALLED NEW REPLACEMENT R/H PITOT STATIC MOUNTING PLATE AT FUSELAGE SKIN FS.210 BETWEENDec 31, 2024 · N751EV · Cndair CL6002C10 · Pitot/Static SystemSDR SWIA202503171229Drag Angle · crackedRH FWD VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED RH FWD VERTICAL STAB DRAG ANGLE IAW MHI RJ R.E.O. 670-55-31-187 REV. -- DATED 2025-02-18 AND COMPLIED WITH TASK CARD 51-900-1002-SKYDec 29, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWI2025F00334Drag Angle · crackedLH AFT VERTICAL STAB. DRAG ANGLE HAS SUSPECTED CRACK. (C-CHECK RO 3/14/2025) REPAIRED IAW REO 670-55-31-018 REV-A DATE 2016-11-10 AND COMPLIED WITH TASK CARD 51-900-1002-SKYDec 29, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Stabilizer Attach FittingsSDR SWI2025F00335Panel · corrodedTHE RH MLG WHEEL WELL PANEL 642AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 642AZ IN RH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REV E. COMPLIED WIDec 27, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025031701227Panel · corrodedTHE LH MLG WHEEL WELL PANEL 542AZ ATTACHMENT ANGLE IS CORRODED. (C-CHECK RO 3/14/2025) REMOVED AND INSTALLED NEW ATTACHMENT ANGLE, BELOW PANEL 542AZ IN LH MLG WHEEL WELL AREA REF: CRJ 700 SRM 51-42-20-001-001-A01 AND DWG: CC670-10320 REVE. COMPLIED WITDec 27, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA2025031701226Cowling · chafedS/N 0368LH ENGINE INTERNAL. LOWER CORE COWL HAS MULTIPLE CHAFES AND GOUGES. FLAGGED (C-CHECK RO 3/14/2025) REPAIRED LH ENGINE INTERNAL, LOWER CORE COWL AT MULTIPLE CHAFES AND GOUGES. SEE CONTINUATION CARD FOR FURTHER DETAILS. ALL STEPS OF REO 670-54-23Dec 26, 2024 · N751EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/SkinSDR SWI202503170336Deck Plate · dentedS/N 0329UNDER PILOTS SEAT, FLOORING HAS A DENT . FLAGGED (C-CHECK RO 3/14/2025) REPAIRED DENT UNDER PILOTS SEAT, FLOORING REF REO 670-53-11-2081 REV -- DATED 2025-01-23, COMPLIED WITH 51-900-1002-SKYDec 21, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F00343Strap · corrodedFWD BAGGAGE BAY , AFT H STRAP CORRODED @ APROX FS 581 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP WITH NEW ONE AT F.S.581 .REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01 DWG-SH670-33793 REV-A.COMPLDec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F00342Crossbeam · corrodedCROOS BEAM CAP CORRODED AT APROX FS 1051 RBL 40 MARKED (C-CHECK RO 3/14/2025) CORROSION ON CROSSBEAM CAP FS1051 AT APPROX RBL40 FOUND TO BE OUT OF LIMITS, REPAIRED WITH REO 670-53-61-2449 REV -- DATED 2025-01-22, COMPLIED WITH 51-900-1002-SKYDec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA20203171219Mount · corrodedFWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 581 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED FWD BAG BAY CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01, 51-45-00-001-001-ADec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F00340Strap · corrodedFWD BAGGAGE BAY, FWD H STRAP CORRODED @ APROX FS 538 BETWEEN LBL STRGS 25-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED "H" STRAP AT F.S.538.00.REF: CRJ-700 S.R.M.51-42-22-001-001-A01, 51-42-21-001-001-A01.DWG-SH670-33750 REV-Y. COMPLIED WITH 5Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWI2025F00339Floorbeam · crackedFS280 CLIP ON THE OB SIDE OF LBL12 APPEARS TO BE CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CLIP P/N CC670-34099-1 AT FS280 ON THE OUTBOARD SIDE OF LBL12. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# KBA670-30026 REV. J.COMPLIED WITH SKYWEST TDec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWI2025F00338Mount · corrodedFWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 533 BETWEEN LBL STRGS 22-23 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WITH NEW ONE. REF: CRJ-700 S.R.M. 51-42-21-001-001-A01,51-42-06-001-001-A01,51-45-00-00Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWI2025F00341Hinge · gougedFWD BAGGAGE BAY DOOR HINGE ON ACFT SIDE GOUGED AND WORN. REMOVED AND REPLACED DOOR HINGE FITTING WITH NEW ONE. REF: CRJ-700 S.R.M.51-41-04-001-001-A01,SRM 51-40-11-001-001 A01, DWG-SH670-33840 REV-C TUC--5659 CAL DUE 31-MAR-2025.COMPLIED WITH 51-900-1002-SKY Dec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWI2025F00337Mount · corrodedFWD BAGGAGE BAY, CARGO NET MOUNTING PLATE CORRODED @ APROX FS 557 BETWEEN LBL STRG 27-26 MARKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED CARGO NET MOUNTING PLATE WIRTH NEW ONE. REF: CRJ-700 S.R.M.51-42-06-001-001-A01, DWG-SH670-33574 REV-A. SEE CONTIDec 19, 2024 · N751EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202503171214Housing · gougedAFT CARGO DOOR HANDLE HOUSING IS GOUGED (MARKED) (C-CHECK RO 3/14/2025) REMOVED DAMAGED AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 INSTALLED NEW AFT CARGO DOOR HANDLE HOUSING. REF. CRJ700 SRM 51-42-21-001-001-A01 AND DWG# CC670Dec 14, 2024 · N751EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWI2025F00351Stand Off · crackedR/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL I/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00350Stand Off · crackedR/H LWR TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED R/H TRANSCOWL O/B "A" BRACKET (CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY.Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00349Coaming · chafedR/H UPPER TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 3/14/2025) REPAIRED INNER LATCH DOOR COAMING AT FWD. LATCH ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-1028, REV. NC, 2009-06-15 AND REO 670-54-21-1705, REV. --, 2025-01-17. AND OPS TESDec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202503171211Skin · dentedR/H UPPER TRANSCOWL INNER PERFORATED SKIN IS DENTED (C-CHECK RO 3/14/2025) REPAIRED R/H UPPER TRANSCOWL INNER PERFORATED SKIN AT DENTED LOCATION, REF. CRJ700 SRM 54-10-00-201-002-A01, REPAIR SRS704 AND REO 670-54-21-1703, REV. --, 2025-01-14. COMPLIED Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00348Rivet · looseL/H UPPER TRANSCOWL Z STIFFENER RIVETS PULLED LOOSE (C-CHECK RO 3/14/2025) REPAIRED L/H UPPER TRANSCOWL AT LOOSE / PULLED RIVETS ON INNER SKIN COMMON TO ZED STIFFENER, REF. REO 670-54-21-1709, REV. --, 2025-01-24. COMPLIED WITH 51-900-1002-SKY.Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00347Stand Off · crackedR/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARDec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00346Stand Off · crackedR/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON R/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARDec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00345Stand Off · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED INBD STANDOFF P/N CN624-2082-201 ON L/H UPPER TRANSCOWL REF. REO 670-54-21-971 REV. B, 2023-11-28. COMPLIED WITH SKY CARD 51-900-1002-SKY.Dec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWI2025F00344Stand Off · crackedL/H UPPER TRANSCOWL OTBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 3/14/2025) REMOVED AND REPLACED O/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H UPPER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARDDec 11, 2024 · N751EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA202303171016Hinge · gougedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA59692-670-53-21-582 N751EV MXCODEID52126-DTI - PAX DOOR HINGE FUSELAGE SIDE HAS NEW GOUGE ON AFT LUG LANDING. REMOVED GOUGE FROM PAX DOOR HINGE (FUSE SIDE) AFT LUG LANDING, MATERIAL LOSS FOUND TO BE WITHIN ALLOWABLE Oct 16, 2024 · N751EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA202266348None · odorCREW GETTING SMELLS OF BURNING RUBBER. MOSTLY NEAR ROWS 10 AND 16. SEEMS TO BE MORE PROMINENT DURING TAXI. AND EVEN STRONGER DURING BLEED TRANSFERS FROM BOTH ENGINES TO APU AND APU TO ENGINES. (FLIGHT #4959 FILED CLOSED) COMPLIED WITH ADJUSTMENT AND TEST OAug 22, 2022 · N751EV · Cndair CL6002C10 · Air Conditioning SystemSDR SWIA2020080751693Stringer · corrodedSTRINGER 21R BETWEEN BS 349 - 364 WAS CORRODED. REPLACED THE STRINGER IAW SRM, AND DWG.Jul 23, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751692Floor Support · corrodedFLOOR SUPPORT, RBL 9, BS 641- 693 FOUND OUT OF LIMITS CORROSION. REPLACED THE FLOOR SUPPORT IAW SRM AND REO.Jul 2, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751691Floor Support · damagedWHILE PERFORMING A MAJOR REPAIR ON THE FLOOR SUPPORT BETWEEN BS 477 TO 624 AT LBL 9, DAMAGE WAS FOUND AT BS 653, LBL 9. REPAIRED IAW SRM.Jun 22, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751690Stringer · corrodedMAIN AVIONICS BAY STRINGER 27, BS 333 TO 355 HAD DEEP PITTING CORROSION AROUND RIVETS. REPLACED THE STRINGER IAW DWG, AND SRM.Jun 20, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751687Stringer · corrodedMAIN AVIONICS BAY STRINGER 23R CORRODED BETWEEN FS280.00 AND FS333. REPLACED THE STRINGER IAW DWG, AND SRM.Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751686Stringer · corrodedMAIN AVIONICS BAY STR 22R CORRODED BETWEEN BS 280 AND 333. REPLACED THE STRINGER IAW DWG, AND SRM.Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751685Doubler · corrodedTCAS ANTENNA DOUBLER, BS 295 TO 310 HAD SIGNS OF CORROSION. REPLACED THE TCAS ANTENNA DOUBLER IAW DWG, AND SRM.Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020080751684Stringer · corrodedSTRINGER 26R, BETWEEN BS 333 AND 349 HAD SIGNS OF CORROSION. REMOVED AND REPLACED THE STRINGER IAW DWG, AND SRM.Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751683Frame · corrodedBB 295 FRAME, BETWEEN STRINGERS 26L & 26R HAD SIGNS OF CORROSION. SPLICED IN A NEW FRAME SECTION IAW SRM.Jun 18, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA2020080751682Intercostal · corrodedPAX DOOR MID DD3 INTERCOSTAL WAS CORRODED. REPLACED THE INDERCOSTAL IAW SRM AND DWG.Jun 12, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2020080751679Skin · corrodedEVALUATE EVIDENCE OF CORROSION ON EXTERIOR FUSELAGE BETWEEN FS 980 AND FS 988 AND BETWEEN STGR 26L AND STGR 26R. REPAIRED FUSELAGE SKIN BETWEEB FS 977 - 985 BETWEEN STGRS 26L - 26R, BY RERPLACING THE EXISTING DOUBLERS WITH NEW IAW REO. ALL CHECKED GOOD.Jun 9, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2020080751678Support · corrodedCORROSION FOUND ON SILL BACKUP AT STRINGER 21L, BETWEEN BS 310 TO 333. REMOVED AND REPLACED THE SILL BACKUP DUE TO FOUND TO BE OUT OF LIMITS IAW SRM, DWG AND REO.Jun 7, 2020 · N751EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA2020080751677Stringer · corrodedSTRINGER 21R, BETWEEN BS 310 AND 319 WAS CORRODED. REPLACED THE STRINGER IAW DWG, SRM, AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA2020080751676Intercostal · corrodedPAX DOOR DD2 MID INTERCOSTAL CORRODED. INSTALLED A NEW INTERCOSTAL IAW SRM AND DWG.Jun 5, 2020 · N751EV · Cndair CL6002C10 · Passenger/Crew Doors
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