N719EV

Service difficulty reports · 269

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 = 'N719EV' 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 SWIA2024F00654Hinge · damaged10 EA LUG HOLES ON AFT SIDE OF PAX DOOR HINGE (FUSELAGE SIDE) HAVE REACHED AN INSIDE DIAMETERS .290" (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW HINGE HALF (FUSELAGE SIDE) PN SH670-31876-13 REF CRJ 700 SRM 53-21-23-201-007-A01 AND DWG SH670-31810 REMay 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA20240808516Hinge · gougedPAX DOOR HINGE (DOOR SIDE) HAS GOUGES ON NUMEROUS LANDS, GOUGES TO NUMEROUS LUGS, ELONGATED ROLL PIN HOLE, AND 1 EA LUG WALL THICKNESS LESS THAN .100" (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR HINGE. REF: CRJ-700 SRM 52-11-01-201-002-A01May 16, 2024 · N719EV · Cndair CL6002C10 · Fuselage, Door HingeSDR SWIA2024F00617Torque Box · gougedEVALUATE GAUGE ON THE LEFT ENG. TR TORQUE BOX AT THE 2 O'CLOCK POSITION. (MARKED) (C-CHECK RO 8/4/2024) REMOVED GAUGE AND PERFORMED STEP 1 AND 2, ENSURED BLEND IS TO SMOOTH CONTOUR AND ENSURED DEPTH IS NO LESS THAN REPORTED , ENSURED NO BLENDED OVER FAMay 15, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2024F00616Depressor · damagedPASSENGER DOOR SEAL DEPRESSOR IS NICKED AND BENT. FS310.00 STGR7L. (FLAGGED) (C-CHECK RO 8/4/2024) REPAIRED PASSENGER DOOR SEAL REF CRJ700 SRM 53-21-23-201-006-A01 REPAIR TYPE IV. COMPLIED WITH 51-900-1002-SKY AND PRESSURE CHECK GOOD . SEE CONTINUATIOMay 15, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2024F00615Floorbeam · crackedLH COCKPIT FLOOR BEAM AT LBL12 IS CRACKED AT FS280 (C-CHECK RO 8/4/2024) REPAIRED LH COCKPIT FLOOR BEAM AT LBL12 REF CRJ700 SRM 53-11-43-201-003-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKYMay 15, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2024F00614Skin · gougedEXTERNAL SKIN GOUGED AND DENTED BETWEEN FS969.00 AND FS985.00 AT STGR27 AS MARKED (C-CHECK RO 8/4/2024) REPAIRED EXTERNAL SKIN BETWEEN FS 969 AND FS 985 AT STGR27 REF REO 670-53-00-290 REV -F 2019/04/26. COMPLIED WITH 51-900-1002-SKY AND PRESSURE CHECK May 15, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA2024F00613Floorbeam · crackedRH COCKPIT FLOOR BEAM AT RBL12 IS CRACKED AT FS280 (C-CHECK RO 8/4/2024) REPAIRED RH COCKPIT FLOOR BEAM AT RBL12 REF CRJ700 SRM 53-11-43-201-003-A01 REV 38 JUL 25/2020. COMPLIED WITH TASK CARD 51-900-1002-SKYMay 15, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Floor BeamSDR SWIA2024F00643Bracket · crackedL/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/4/2024) INSTALLED NEW L/H UPPER TRANSCOWL "A" BRACKET (PN CN624-2082-201) REF REO# 670-54-21-971, REV B, DATED 11/28/23. COMPLIED FULLY W/SKYCARD 51-900-1002-SKY. SEE CONTINUATION May 14, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2024F00642Skin · dentedR/H UPPER TRANSCOWL INNER PERFORATED SKIN IS DENTED (C-CHECK RO 8/4/2024) USING A ROTARY FILE REMOVED DAMAGED AREA OF THE METAL PERFORATE LINER AND HONEYCOMB CORE. REMOVED 0.25"OF THE HONEYCOMB CORE FROM THE EDGE OF CUTOUT TO ALLOW THE ADHESIVE TO GO BMay 14, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2024F00641Stiffener · shearedR/H UPPER TRANSCOWL Z STIFFENER HAS SHEARED RIVETS (C-CHECK RO 8/4/2024) ON R/H UPPER TRANSCOWL, REPAIRED 2 EA. FASTENER HOLES IN UNDERLYING PERFORATED SKIN COMMON TO ZED STIFFENER AND COMPLIED WITH ALL APPLICABLE STEPS OF REO 670-54-21-1643, REV. --, May 14, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2024F00640Stiffener · looseL/H LWR TRANSCOWL Z STIFFENER FASTENERS ARE LOOSE/PULLED (C-CHECK RO 8/4/2024) REPAIRED UNDERLYING FASTENER HOLES COMMON TO ZED STIFFENER P/N CN624-2038-204 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-1641, REV. --, 2024-06-05 AND COMPLIED WITH SKYWESMay 14, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA20240808513Stiffener · shearedR/H LWR TRANSCOWL Z STIFFENER HAS SHEARED RIVETS (C-CHECK RO 8/4/2024) REPAIRED R/H LOWER TRANSCOWL INNER SKIN UNDER "Z" STIFFENER REF. REO 670-54-21-1645 REV. --, 2024-06-11.COMPLIED WITH SKYCARD 51-900-1002-SKY.May 13, 2024 · N719EV · Cndair CL6002C10 · Engine Thrust ReverserSDR SWIA2024F00612Intercostal · corrodedPAX DOOR INTERCOSTAL DD3 FS320.00 - FS 338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD3 FS320.00 - FS 338.00. REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWINGMay 12, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2024F00611Intercostal · corrodedPAX DOOR INTERCOSTAL DD2 FS320.00 - FS 338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD2 FS320.00 - FS 338.00 . REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWINMay 12, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA2024F00610Intercostal · corrodedPAX DOOR INTERCOSTAL DD4 FS320.00 - FS 338.00 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR INTERCOSTAL DD4 FS320.00 - FS 338.00 . REF: CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01 AND DRAWINGMay 12, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA20240808512Former · corrodedPAX DOOR FWD. FORMER FS311.75 HAS INTERGRANULAR CORROSION (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW PAX DOOR FWD FORMER FS311.75. REF:CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-21-001-001-A01, AND DRAWING 601R31702 REV N. COMPLIED WITH 5May 12, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA20240808508Skin · chafedRIGHT WING AILERON UPPER LEADING EDGE CHAFFED BETWEEN WS282.00 TO WS353.00 AS MARKED (C-CHECK RO 8/4/2024) REMOVED AND INSTALLED NEW UPPER LEADING EDGE SKIN ON RH AILERON REF CRJ700 SRM 51-42-06-001-001-A01 REF CRJ700 SRM 51-42-21-001-001-A01, DWG CC670May 8, 2024 · N719EV · Cndair CL6002C10 · AileronsSDR SWIA20240808507Roller · wornPASS DOOR ON AFT SIDE OF DOOR AT LOWER ROLLER GUIDE WORN (C-CHECK RO 8/4/2024) REMOVED AND REPLACED PAX DOOR CENTERING (GUIDE) PLATE. REF: CRJ-700 SRM 51-42-13-001-001-A01 AND DRAWING 601R31702 REV N. COMPLIED WITH 51-900-1002-SKY AND SEE CONTINUATIONMay 7, 2024 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR SWIA20240808504Skin · dentedADM # 8219- FWD FUSELAGE BELOW CA SIDE WINDOW. JUST FWD FS280.00. DENT 1.81" LONG .71" HIGH .018" DEEP JUST FWD FS 280.00. SRM 53-00-01-101-A01. PLOT, MAP, AND EVALUATE DAMAGE IF WITHIN ACCEPTABLE LIMITS OR REWORKED, ELIMINATE EVIDENCE USING STANDARD AMay 4, 2024 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR SWIA202401110008Unknown · burnedWINDSHIELD HEAT BURNING ON CAPTAIN SIDE WINDSHIELD (FLIGHT 4942 FILED CLOSED)THIS DISCREPANCY WAS TRANSFERRED TO CAMP ITEM 27657328 WITH THE FOLLOWING CORRECTIVE ACTION: "REMOVED AND REPLACED LH WINDSHIELD IN REF CRJ 700 AMM 56-11-01. ALL OPS, AND PRESSURIZATJan 8, 2024 · N719EV · Cndair CL6002C10 · Windshield/Door Rain/Ice RemovalSDR SWIA202158457Structure · damagedL/H AFT HOLE OF AFT DRAIN MAST IS ELONGATED (C-CHECK RO 5/23/2021) REMOVED DAMAGE AND INSTALLED DOUBLER PER REO 670-53-61-1870 IAW CRJ700 SRM 51-40-11, CRJ700 SRM 51-24-36 , CRJ700 SRM 51-24-16 AND 51-23-00, 51-42-06,51-42-21, REO 670-53-61-1256Apr 8, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202158460Stringer Clip · corrodedATTACHING STRINGER CLIP (GROUNDING CLIP) FWD OF FS333 AT STR21R/H SPLICE CORRODED. (C-CHECK RO 5/23/2021) EVALUATED CORRODED CLIP, FOUND TO BE OUT OF LIMITS, REMOVED AND REPLACED DAMAGED STINGER CLIP FROM FS333 AT STGR21R/H WITH FABRICATED CLIP IAW CRJ7Mar 11, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, Attach FittingsSDR SWIA202158459Floor Panel · corrodedFS 280.00 AVIONICS FLOOR PANEL 141ALF FORWARD SUPPORT ANGLE HAS CORROSION ON TOP SURFACE. (C-CHECK RO 5/23/2021) FS 280 AVIONICS FLOOR PNL 141ALF FWD SUPPORT ANGLE CORR. REMOVED AND REPLACED WITH NEW SERVICABLE ANGLE P/N CC670-34256-3 IAW CRJ-700-SRM-Feb 18, 2021 · N719EV · Cndair CL6002C10 · Fuselage Floor PanelSDR SWIA202158456Frame · corrodedFRAME AT FS 379 BETWEEN STR 22R AND STR21R CORRODED. REQUIRES REPLACEMENT. (C-CHECK RO 5/23/2021) REMOVED, FABRICATED AND INSTALLED FRAME SEGMENT FS379, STR22R IAW BOMBADIER DRAWING # SH670-32118 AND SRM 51-42-06. REFER TO CAMP #22270919 FOR PRESSURIZATFeb 18, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202158455Frame · corrodedCORROSION ON F/S 379 L/H SIDE AT STR 22 (C-CHECK RO 5/23/2021) EVALUATED CORROSION, 100% MATERIAL LOSS, FOUND TO BE OUT OF LIMITS. REMOVED, FABRICATED AND REPLACED FRAME SEGMENT AT FS379 L/H P/N SH670-32101-1 PER DRAWING SH670-32101.SEE CAMP 22549325 FOFeb 18, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202158466Seat Track · out of limitsRH SIDE WALL SEAT TRACKS NEED CLEANING AND EVALUATION FROM FS 379.00 TO FS 977.00 (C-CHECK RO 5/23/2021) CLEANED AND EVALUATED R/H SIDEWALL SEAT TRACK FROM F.S 379 TO F.S 977.00. FOUND 2 SECTIONS OUT OF LIMITS AND WAS REPLACED. SECTION 1 F.S 379 TO F.S Feb 10, 2021 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158465Seat Track · out of limitsLH SIDE WALL SEAT TRACKS NEED CLEANING AND EVALUATION FROM FS 379.00 TO FS 977.00 (C-CHECK RO 5/23/2021) CLEANED AND EVALUATED L/H SIDEWALL SEAT TRACKS F.S 364 TO F.S 485, F.S 785 TO F.S 852 AND F.S 863 TO F.S 953, FOUND OUT OF LIMITS AND REMOVED AND REFeb 10, 2021 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158454Rib · crackedRH RIB AT FS 677.00 HAS A CRACK AT THE END OF THE METAL , IN THE BEND RADII, 1/4" IN LENGTH. UNDER THE WING-TO -BODY FAIRING. (C-CHECK RO 5/23/2021) REMOVED, FABRICATED AND INSTALLED NEW SUPPORT ANGLE IAW SHORT BROS/BOMBARDIER DWG PL SH670-39072 AND CRJFeb 7, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR SWIA202158453Stringer · corrodedCORRISION ON STRINGER AND BRACKET FS 364.00 AND STGR 21RH LONG THE JOINT PIECE, 6" EITHER SIDE OF STRINGER. (C-CHECK RO 5/23/2021) REMOVED AND REPLACED CORRODED STRINGER STR21 R/H FROM FS 333 TO FS 379 IAW CRJ700 SRM51-42-21, CRJ700 SRM 51-42-06,CRJ700 Feb 7, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202158463Fitting · chafedFORWARD CARGO DOOR FORWARD LOWER GUIDE FITTING HAS CHAFE MARK/CHIPPED MISSING PAINT. (C-CHECK RO 5/23/2021) REMOVED AND REPLACED FORWARD LOWER GUIDE FITTING P/N SH670-33846-5 IAW CRJ700 SRM 53-31-23 AND GAP CHECK GOOD REF. CRJ-700 AMM 52-35-00 OPERATIONFeb 4, 2021 · N719EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202158462Fitting · chafedFORWARD CARGO DOOR AFT LOWER GUIDE FITTING HAS CHAFE MARK/CHIPPED MISSING PAINT. (C-CHECK RO 5/23/2021) REMOVED AND REPLACED LOWER AFT GUIDE FITTING FOR FWD CARGO BAY DOOR IAW CRJ 700 SRM 53-31-23Feb 4, 2021 · N719EV · Cndair CL6002C10 · Cargo/Baggage DoorsSDR SWIA202158452Seat Track · damagedSEAT TRACK AT RBL 9 FS 863.50 TO FS 977 NEEDS CLEANED AND EVALUATED (C-CHECK RO 5/23/2021) REMOVED SEAT TRACK AT RBL9 FS 863.5 TO FS 977.0 AND REPLACED WITH NEW SEAT TRACK IAW REO 670-53-00-589.Feb 4, 2021 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158467Seat Track · out of limitsSEAT TRACKS ON THE FLOOR, LH SIDE FROM FS 349.00 TO FS 1039.00, AT STGR9 LH AND STGR27 LH, NEED CLEANING AND EVALUATION. (C-CHECK RO 5/23/2021) REMOVED AND REPLACED SEAT TRACKS ON THE FLOOR, LH SIDE FROM FS 349.0 TO FS 1039.0 AT LBL9 AND LBL27, EVALUATEFeb 3, 2021 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158464Seat Track · out of limitsSEAT TRACKS ON THE FLOOR, RH SIDE FROM FS 349.00 TO FS 1039.00, AT STGR9 RH AND STGR27 RH NEED CLEANING AND AVALUATION. (C-CHECK RO 5/23/2021) EVALUATED AND CLEANED SEAT TRACKS FOUND 4 TRACKES OUT OF LIMITS REMOVED AND REPLACED TRACKS FROM FS485-581,FS5Feb 3, 2021 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202158458Support Angle · corrodedSERVICE DOOR SILL PROTECTOR PLATE COVER SUPPORT ATTACH ANGLES, TOTAL 4 ANGLES BETWEEN FS310.00 THRU FS349.00 HAVE SURFACE CORROSION. (C-CHECK RO 5/23/2021) REPLACED ANGLES IAW CRJ700 SRM 51-42-06.Feb 2, 2021 · N719EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR SWIA202158451Stringer · corrodedSEVERAL AREAS OF CORROSION BELOW SERVICE DOOR CUT-OUT ON STRINGER 20 BETWEEN FS295.00 THRU 349.00. (C-CHECK RO 5/23/2021) REPLACED RIGHT SIDE FUSELAGE STRINGER 20 BETWEEN FS295.00 THRU FS349.00 IAW CRJ700-SRM 51-42-06,CRJ700-51-42-21 CRJ700-51-42-20,CRJFeb 2, 2021 · N719EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR SWIA202158461Cover Plate · chafedGALLEY SERVICE DOOR LOWER SILL PROTECTOR PLATE HAS TWO CHAFE MARKS ON UPPER SURFACE, NEEDS TO BE REPLACED. (C-CHECK RO 5/23/2021) REMOVED AND REPLACED GALLEY DOOR LOWER SILL PROTECTOR PLATE IAW CRJ700 SRM 51-40-11 AND SRM 51-21-11.Feb 1, 2021 · N719EV · Cndair CL6002C10 · Galley DoorsSDR ASOA201805292009Charger · no testBATTERY CHARGER NR 4 FAILED AN OPS CHECK IAW TC 700-33-900-701-A01. MAINTENANCE REMOVED AND REPLACED THE BATTERY CHARGER IAW AMM 33-51-17. AIRCRAFT WAS APPROVED FOR RETURN TO SERVICE.May 29, 2018 · N719EV · Cndair CL6002C10 · Emergency LightingSDR ASOA201708221863Door Frame · corrodedPAX DOOR FWD FRAME HAS CORROSION AROUND LOWER LATCH ARM. REMOVED CORROSION, PERFORMED NDT UT THICKNESS INSPECTION. COMPLIED WITH EA 43-2017-125, AND EC/TC EA 43-2017-125.Aug 22, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201708221862Door Frame · corrodedPAX DOOR FRAME CORRODED AT BS 329.41. REMOVED CORROSION, PERFORMED NDT UT THICKNESS INSPECTION. COMPLIED WITH EA 25-2017-090 AND EC/TC EA 25-2017-090.Aug 22, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201708221861Door Frame · corrodedPAX DOOR FWD FRAME HAS CORROSION AT THE TOP LATCH MECHANISM. REMOVED CORROSION, PERFORMED NDT UT THICKNESS INSPECTION. COMPLIED WITH EA 43-2017-125 AND EC/TC EA 43-2017-125.Aug 22, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, StructureSDR ASOA201708201869Skin · chafedFUSELAGE SKIN CHAFFED FS 96900-FS 985.00 STR 27. COMPLIED WITH EC TC REO 670-53-00-290 REV D DATED 09-10-2015 AS WRITTEN. PERFORMED UT THICKNESS INSPECTION IAW BSC NDT INSPECTION PROCEDURE 4.3, MIN MATERIAL REMAINING IS .091", ORIGINAL IS .188", REMOVED IS .0Aug 20, 2017 · N719EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201708151867Doubler · gougedRT INBOARD FLAP INTERNAL DOUBLER GOUGED UNDER OUTBOARD MOST VANE ACTUATOR. COMPLIED WITH EC/TC REO 670-57-52-352 AND REO 670-57-52-352 REV - DATED 03/28/2017 AS WRITTEN.Aug 15, 2017 · N719EV · Cndair CL6002C10 · Trailing Edge FlapsSDR ASOA201708111868Angle · crackedASD ANGLE CRACKED AT THE PRESSURE VENT FLAP/LATCH MECHANISM SUPPORT STRUCTURE. REMOVED AND REPLACED ASD ANGLE AT VENT FLAP AREA REF SRM 51-42-06-001-001-A01 AND DRAWING 601319050.Aug 11, 2017 · N719EV · Cndair CL6002C10 · Passenger/Crew DoorsSDR ASOA201708101826Seat Track · corrodedLBL9 CABIN SEAT RAIL SEGMENT FS375-485 CORRODED SEVERAL AREAS. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND REPLACED SEAT RAIL SEGMENT IAW REO 670-53-00-343 REV K, COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343 REV M AS WRITTEN.Aug 10, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708091825Seat Track · corrodedRBL 9 CABIN SEAT TRACK SEGMENT BS 349 - 385, CORRODED IN SEVERAL PLACES. BLENDED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED AND REPLACED THE SEAT TRACK SEGMENT IAW REO 670-53-00-343, REV K, COMPLIED WITH ECTC REO 670-53-00-343 AND GREO 670-53-00-343,Aug 9, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708081870Seat Track · corrodedLEFT SIDE WALL SEAT TRACK SEGMENT FROM FS 677-712 CORRODED OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK AT FS 677-712 LT SIDE IAW AMM 53-00-49-801-A17 AND 53-00-49-400-801-A17 AND EC/TC REO 670-53-00-343 AND REO-670-53-00-343.Aug 8, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708081824Seat Track · corrodedRIGHT SIDE WALL SEAT TRACK SEGMENT FROM BS 675 TO 713 HAS CORROSION AROUND SEVERAL SCREW HOLES. REMOVED CORRODED RIGHT SIDE WALL SEAT TRACK IAW AMM 53-00-49-000-801-A03. FABRICATED NEW SEAT TRACK IAW ECTC REO 670-53-00-343 AND REO 670-53-00-343. INSTALLEAug 8, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201708081823Seat Track · corrodedLEFT SIDE WALL SEAT TRACK SEGMENT FROM BS 677 TO 712 IS CORRODED OUT OF LIMITS. INSTALLED A NEW LT SIDEWALL SEAT TRACK IAW AMM 53-00-49-400-801-A17.Aug 8, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA08081821Seat Track · corrodedLEFT SIDE WALL SEAT TRACK SEGMENT FROM BS 677 - 712 CORRDED OUT OF LIMITS. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801-A17, 53-00-49-400-801-A17, EC/TC REO 670-53-00-343, AND REO-670-53-00-343.Aug 8, 2017 · N719EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
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