N712EV

Service difficulty reports · 251

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 = 'N712EV' 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 SWI2024F00903Windshield · crackedR WINDSHIELD CRACKED, OUTER LAYER AT 30,000 FT. QRH COMPLIED WITH. (FLIGHT 4251 - FILED CLOSED)INVESTIGATED RT WINDSHIELD CRACK, AND FOUND FIRST OFFICER'S WINDOW SHATTERED. PLEASE REFERENCE AML 1442623Oct 2, 2024 · N712EV · Cndair CL6002C11 · Flight Compartment WindowsSDR SWIA202163792None · damagedLH AILERON CENTER, OB HINGE LUG DAMAGED. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON LEFT HAND AILERON OUTBD HINGE LUG PER MHIRJ REO 670-57-61-379 REV. -- DATED:2021-12-08. NO FURTHER ACTION REQUIRED AT THIS TIME. PLEASE REFER TO CONTINUATION CARD FOR Dec 7, 2021 · N712EV · Cndair CL6002C10 · Wing StructureSDR SWIA202163791None · corrodedDURING THE REMOVAL OF RIGHT HAND SIDE INTERCOASTAL AT STRINGER STR24R FOR CORROSION AT FUSELAGE STATION FS409 THRU FS421 AIRCRAFT SKIN SUFUR DAMAGED. (C-CHECK RO 1/13/2022) PERFORMED SKIN REPAIR AT STGR24R FROM FS394- FS409, IN ACCORDANCE WITH REPAIR Nov 7, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163790None · corrodedFS409 THRU FS421 RIGHT SIDE OF FUSELAGE CORROSION ON INTERCOASTAL AT STRINGER STR24R. (C-CHECK RO 1/13/2022) REMOVED CORRODED SECTION OF STRINGER 24R AT FS 409.00 TO FS 421.00 AND REPLACED WITH NEW SECTION. REF. CRJ700 SRM 53-00-03. REFERENCE CONTINUATINov 4, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163794None · corrodedCORROSION FOUND ON AFT SIDE OF FRAME FS863, STR27. REQUIRES TO BE REPLACED. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LOWER FRAME FS863 FROM SGTR17L TO SGTR17R PER CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01. PLEASE REFER TONov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163789None · dentedDENT FOUND ON LEFT HAND OUTER SKIN FROM FS 533 TO FS 549, BETWEEN STGR 16L AND STGR 17L. (C-CHECK RO 1/13/2022) REPAIRED DENTED AREA AT FUSELAGE STATION FS 533.00 STGR 16L TO STGR 17L PER REO 670-53-31-749 REV -- DATED 2021-12-03. PLEASE REFERENCE CONTNov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163788None · dentedDENT FOUND ON LEFT HAND OUTER SKIN FROM FS 235 TO FS 250, AT BUT JOIN STGR16L. (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON SKIN AT FS235 TO FS250, STGR16L PER MHIRJ REO 670-53-11-1754 REV. -- DATED: 2021-11-24. PLEASE REFER TO CONTINUATION CARD FOR DISPNov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163787None · damagedCREASE IN FUSELAGE SKIN UNDER SERVICE DOOR AT FS 333.00 BETWEEN STGR21R AND STRGR22R . NEEDS TO BE EVALUATED . (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON FUSELAGE SKIN CREASE UNDER SERVICE DOOR AT FUSELAGE STATION FS 333.00 BETWEEN STRINGER STGR21R ANDOct 19, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163786None · dentedSEVERAL DENTS & SKIN DISTORTED AT L/H SKIN SIDE P/N SH670-31151-9 BETWEEN FS 364 & FS 394 & STR 17LH STR 18LH IN AFT SILL ATTACHING ZONE (C-CHECK RO 1/13/2022) PERFORMED A REPAIR ON LEFT HAND OUTER SKIN AT FUSELAGE STATION FS364 UP TO FS394 BETWEEN STOct 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163785None · gougedAIRCRAFT RUDDER MIDDLE HINGE FITTING , HINGE LUG AT STATION 92.94 HAS 2 GOUGES , AS MARKED . (C-CHECK RO 1/13/2022) PERFORMED REPAIR ON RUDDER MIDDLE HINGE FITTING AT STA. 92.94 PER REO 670-55-41-093 REV-- DATED 2021-10-14. REFERENCE CONTINUATION CARD FOct 12, 2021 · N712EV · Cndair CL6002C10 · Rudder, Plate/SkinSDR SWIA202163784None · damagedFRAME @ FS 517.00 BETWEEN STR 18L & STR 19L BLISTERED PAINT /DEBRIS BUILD-UP. CLEAN & RE-INSPECT. (C-CHECK RO 1/13/2022) REMOVED, FABRICATED AND INSTALLED STUB FRAME AT FS517 FROM STGR18L AND SGTR19L. REF CRJ700 SRM 51-42-06-001-001-A01 AND SRM 51-42-2Oct 3, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163783None · damagedREMOVE AND REPLACE FLOOR SUPPORT BEAM AT LBL 9, FROM FS 858.00 - 939.00 (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LONGITUDINAL FLOOR BEAM WITH A NEW SUPPORT AT LBL9 FROM FS858.00 TO FS939.00 PER CRJ700 SRM 53-00-41-201-001-A01. PAGE 207 PARSep 28, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR SWIA202163782None · corrodedREPLACE CORRODED FLOOR SUPPORT BEAM AT RBL9 FROM FS858 TO FS939. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FLOOR BEAM SUPPORT AT RBL9 FROM FS858 TO FS939 PER CRJ700 SRM 53-00-41-201-001-A01, SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-ASep 25, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR SWIA202163781None · corrodedREPLACE CORRODED LONGITUDINAL FLOOR SUPPORT BEAM FROM FS565.00 TO FS661.00, LBL 9 (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LONGITUDINAL FLOOR BEAM WITH A NEW SUPPORT AT LBL9 FROM FS565 TO FS661 PER CRJ700 SRM 53-00-41-201-001-A01. PAGE 207 Sep 24, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting StructureSDR SWIA202163780None · corrodedLEFT SIDE FRAME AT FS565 AND STRINGER 18L IS CORRODED. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED LEFT SIDE FRAME FS565 FROM SGTR18L TO SGTR7L PER CRJ700 SRM 51-42-06-001-001-A01, AND SRM 51-42-21-001-001-A01. PLEASE REFER TO CONTINUATION CARDSep 21, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163779None · crackedWINDSHIELD SUPPORT POST BETWEEN CO- PILOTS LEFT SIDE WINDSHIELD AND FORWARD CO- PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) REMOVED CRACKED CO-PILOT WINDSHIELD SUPPORT POST AND REPLACED WITH NEW WINDSHIELD SUPPORT POST PER Sep 20, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163778None · crackedWINDSHIELD SUPPORT POST BETWEEN PILOTS LEFT SIDE WINDSHIELD AND FORWARD PILOTS WINDSHIELD IS CRACKED AT TOP NUTPLATE HOLE. (C-CHECK RO 1/13/2022) COMPLETED STRUCTURAL MAJOR REPAIR (**RII**) TASK CARD 51-900-1002-SKY MTCM REV: REV DATE:06 OCT 20 . / REMOSep 20, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)SDR SWIA202163777None · corrodedLEFT HAND FRAME AT FS549, STR18L CORRODED BEYOND ALLOWABLE DAMAGE. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FRAME AT FS549, FROM STR18L TO STR7L PER CRJ700 SRM 51-40-11-001-001-A01 AND 51-42-06-001-001-A01. PRIMED EXPOSED FASTENERS REF CRJ Sep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163776None · corrodedON TOP OF FRAME STATION 310 BTW STR 24 RH TO 24 LH, CORROSION FOUND. (C-CHECK RO 1/13/2022) PERFORMED FRAME REPAIR AT FS310 BETWEEN STR24R TO STR24L PER CRJ700 SRM 53-00-06-201-006-A01. REFERENCE CONTINUATION CARD FOR DISPOSITION AND ALL CORRECTIVE ACTISep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163775None · corrodedFS 319 BTW STR 24 RH TO 26LH, CORROSION FOUND. (C-CHECK RO 1/13/2022) REMOVED AND REPLACED CORRODED FRAME AT FS319 FROM STR23R TO STR26L PER CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. REFER TO CONTINUATION CARD FOR DISPOSITION AND CORRECTSep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR SWIA202163774None · corrodedCORROSION ON AFT DOOR LOWER SILL FLANGE (C-CHECK RO 1/13/2022) REMOVED CORRODED AFT CARGO DOOR LOWER SILL AND REPLACED WITH NEW LOWER SILL AT FUSELAGE STATION FS985.00 UP TO FS1051.30 / PER CRJ700 SRM TASKS 53-61-23-001-001-A01, 53-61-23-101-001-A01, 53Sep 17, 2021 · N712EV · Cndair CL6002C10 · DoorsSDR SWIA202163773None · corrodedCORROSION ON STR26R FROM FS1015 TO FS1047 (C-CHECK RO 1/13/2022) REMOVED CORRODED SECTION OF STGR 26R AT FS 1015.00 TO FS 1047.00 AND REPLACED WITH NEW STRINGER SECTION PER CRJ700 SRM53-00-03-201-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001-A01. RSep 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202163772None · corrodedSURFACE CORROSION ON STR26L FROM FS1015 TO FS1047. (C-CHECK RO 1/13/2022) REPAIRED STRINGER STGR26L FROM FS1015 TO FS1047 WITH EXTRUSIONS,SPLICES AND FILLER PER CRJ700 SRM TASK 53-00-03-201-001-A0 PLEASE REFERENCE TO CONTINUATION CARDS FOR DISPOSITION Sep 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, KeelSDR SWIA202163771None · corrodedAFT DRAIN MAST INNER CHANNEL AT FS1030 TO FS1047 CORRODED. (C-CHECK RO 1/13/2022) REMOVED THE AFT DRAIN MAST AT FS 1030.00 TO FS 1047.00 STGR 27 TO FACILITATE THE REMOVAL OF CORRODED MAST CHANNEL PER AMMTASK 38-32-12-000-801 (CONFIG A01). / REMOVED CORRSep 17, 2021 · N712EV · Cndair CL600* · Water and Waste SystemSDR SWIA202163770None · corrodedBACK UP SILL AT FS 319.00 STRG 21L HAS CORROSION (C-CHECK RO 1/13/2022) REMOVED CORRODED BACK UP SILL AT FS 319.00 STGR 21L AND REPLACED WITH NEW BACK UP SILL PER CRJ700 SRM 51-42-06-001-001-A01. PRESSURIZATION CHECK WILL BE PERFORM UNDER CAMP.23531501,Sep 16, 2021 · N712EV · Cndair CL600* · Fuselage Main, FrameSDR SWIA202163795None · corrodedABOVE FWD CARGO DOOR AT FS549 & STR18LH CORROTION FOUND ON FRAME (C-CHECK RO 1/13/2022) REMOVED CORROSION, ORIGINAL MATERIAL .050, .025" MATERIAL LOSS, REMAINING MATERIAL .025" FOUND TO BE OUT OF LIMITS PER CRJ700 SRM 51-21-06-001-001-A01 AND 53-31-06-0Sep 9, 2021 · N712EV · Cndair CL6002C10 · DoorsSDR SWIA202163793None · crackedCAPTAIN WINDSHIELD IS CRACKED LOCATION OUTBOARD UPPER LEFT HAND CONNER, (C-CHECK RO 1/13/2022) REMOVED AND REPLACED BAY ONE SERVICEABLE WINDSHIELD TASK CARD I.A.W 56-220-1000 SKY REMOVED AMM 56-11-01-000-801 INSTALLATION AMM TASK CARD 56-220-1000 SKY AMSep 2, 2021 · N712EV · Cndair CL6002C10 · Window/Windshield SystemSDR SWIA202163769None · dentedFS 608 STR 15R EXTERNAL SKIN HAS DENT/CREASE ON STRINGER (C-CHECK RO 1/13/2022) COMPLETED STRUCTURAL MAJOR REPAIR (**RII**) CARD 51-900-1002-SKY MTCM REV: REV DATE: 06 OCT 20. IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) 670-53-31-716 REVISION-- DAAug 31, 2021 · N712EV · Cndair CL600* · Fuselage Structure (General)SDR SWIA202163768None · dentedLH OUTBOARD FLAP LOWER SKIN AT FLS 210 HAS DENT (C-CHECK RO 1/13/2022) DENT ON LEFT OUTBOARD FLAP LOWER SKIN AT FLS 210 MEASURED L=10.0",W=4.20", D=.025", FOUND TO BE OUT OF LIMITS PER CRJ700 SRM 57-53-01-101-001-A01. FLAP REPAIRED PER CRJ700 SRM 57-53Aug 31, 2021 · N712EV · Cndair CL600* · Aileron TabsSDR SWIA202163767None · crackedFRAME AT FS333, STGR 1R IS CRACKED AS MARKED. (C-CHECK RO 1/13/2022) REMOVE AND REPLACED FS333 FRAME SECTION FROM STGR -0- TO 9R. IAW DWG # SH670-31950 AND CRJ700 SRM 51-23-00-001-001-A01, 51-40-11-001-001-A01, 51-42-06-001-001-A01 AND 51-42-21-001-001Aug 30, 2021 · N712EV · Cndair CL600* · Fuselage Main, FrameSDR ASOA201812315008Smoke Detector · false activationAFT LAVATORY SMOKE WARNING MESSAGE AS AIRCRAFT DESCENDED THRU 9000 FT. THE SYSTEM SELF RESET. THE MESSAGE NO LONGER ACTIVE IAW MCC. NO FURTHER ACTION REQUIRED.Dec 31, 2017 · N712EV · Cndair CL6002C10 · Smoke DetectionSDR ASOA201706061667Stiffener · crackedFS 202.75 FWD SIDE OF BULKHEAD AT RBL 30 & LBL 30 STIFFENERS HAVE AN INDICATION OF 0..25 IN THE UPPER EDGE FLANGE. REPAIRED RBL 30 & LBL 30 STIFFENER IAW SRM 53-11-10-201-005-A01.Jun 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201706031640Frame · crackedFS 220 RT FRAME HAS AN INDICATION OF .5" LONG ON THE FWD FACE 1" BELOW STR 14 JUST ABOVE FASTENER HOLE. FAILED NDT INSPECTION. LOCATED, DRILLED UP AND INSTALLED A NEW SERVICEABLE FS 220 FRAME SECTOR IAW SRM 51-40-11-001-001-A01, 51-42-06-001-001-A01, 51-42-21-Jun 3, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA201706021639Angle · damagedWHILE PERFORMING SERVICE BULLETIN 670BA-53-044 FOUND 11 HOLES GOING THROUGH SKIN AND CAP ANGLE TO BE DIAMETER .191" DIAMETER OF HOLE SHOULD BE .160" TO .164" PER SERVICE BULLETIN. COMPLIED WITH REO 670-53-11-1284 DATED 6-01-2017.Jun 2, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201701061033Intercostal · corrodedDURING C CHECK, FOUND INTERNAL JACKING FITTING, LT INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL, DUCT SPLICE & INTERCOSTAL ANGLE IAW EA 30-2017-004 REV .Jan 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA2017010610231Frame · corrodedDURING C CHECK, FOUND FRAME BS 349 CORRODED BETWEEN STRINGER 26L & 26R. BLENDED CORROSION AND RESTORED FINISH IAW REO 670-53-21-1308 & EC/TC EO 700-53-10-00002.Jan 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, FrameSDR ASOA2017010510232Hinge · gougedDURING C CHECK, FOUND PAX DOOR HINGE GOUGED FROM ANTI-ROTATION PIN (MIGRATED). REMOVED AND REPLACED HINGE IAW SRM 53-21-23-201-001-A01, & 53-21-201-007-A01.Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage, Door HingeSDR ASOA2017010510230Skin · corrodedDURING C CHECK, FOUND MAIN AVIONICS BAY DOOR CUT OUT INTERNAL SKIN CORRODED. BLENDED CORROSION AND INSTALLED SACRIFICIAL STRIPS IAW REO 670-53-21-242, & EC/TC REO 670-53-21-242Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201701051029Former · corrodedDURING C CHECK, FOUND RT FLOOR PAX DOOR FORMER NEAR UPPER END CORRODED. BLENDED CORROSION AND RESTORED FINISH IAW EA 25-2016-334 & EC/TC EA 25-2016-334.Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201712311009Landing · corrodedDURING COMPLIANCE OF MODSUM IS67053210097, 13EA FASTENER HOLES WERE OVERSIZED INADVERTENTLY ON AVIONICS DOOR LAND, LT SIDE. OPENED UP HOLES AND INSTALLED DOUBLE FLUSH SHALLOW HEAD RIVETS PER EC/TC REO 670-53-21-1375.Dec 31, 2016 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201712311003Skin · corrodedINTERNAL FUSELAGE SKIN CORRODED AT FS 397 BETWEEN STRINGERS 25L-26L. BLENDED CORROSION AND RESTORED FINISH IAW EA 30-2016-373 AND EC/TC EA 30-2016-373.Dec 31, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Plate/SkinSDR ASOA201712301002Seat Track · corrodedLT SIDE WALL SEAT RAIL SEGMENT CORRODED AT FS 483.00-572.00 CORRODED IN SEVERAL AREAS. REMOVED AND REPLACED LT SIDE WALL SEAT RAIL SEGMENT AT 483.00-572.00 IAW AMM 53-00-49-000-801-A03, EC/TC REO 670-53-00-343 AND REO 670-53-00-343 REV M AS WRITTEN.Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612301392Stringer · corrodedFWD CARGO BAY STRINGER 24L CORRODED BETWEEN BS 517-533. REMOVED CORROSION, AND FOUND OUT OF LIMITS. REPAIRED IAW EA 25-2016-337 & EC/TC EA 25-2016-337.Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/StringerSDR ASOA201612301391Seat Track · corrodedCABIN SEAT TRACK SEGEMENT CORRODED BS 683.5-836.5, RBL 9. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03, EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M.Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612301390Seat Track · corrodedCABIN SEAT TRACK SEGEMENT CORRODED BS 683.5-836.5 LBL9. REMOVED AND INSTALLED NEW SEAT TRACK IAW AMM 53-00-49-000-801-A03, 53-00-49-400-801-A03, EC/TC REO 670-53-00-343, AND GREO 670-53-00-343 REV M.Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612291371Seat Track · corrodedDURING C CHECK, FOUND SEAT TRACK SEGMENT LBL 9 CORRODED AT BS 517.00 AND 540.00. FOUND TO BE OUT OF LIMITS IAW SRM 53-31-49-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-400-801-A03, REO 670-53-00-343 AND EC/TC REO 670-53-00-343.Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612291370Floor Support · corrodedDURING C CHECK, FOUND LBL 9 SIDE FLOOR SUPPORT SEGMENT FROM BS 476 TO 571.5 CORRODED IN SEVERAL AREAS. REMOVED THE CORROSION. PERFORMED UT THICKNESS INSPECTION. PERFORMED EDDY CURRENT INSPECTION. NO INDICATIONS NOTED. REPAIRED THE FLOOR SUPPORT & COMPLIED WITDec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous StructureSDR ASOA201612291367Seat Track · corrodedCABIN SEAT TRACK SEGMENT CORRODED BS 581 - 683.5, RBL 9. THE SEAT TRACK WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-41-101-001-A01. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03, EC/TC REO 670-53-00-343, GREO 670-53-00-343 REV M AND AMM 53-00-Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612291366Seat Track · corrodedRIGHT SIDE SEAT TRACK CORRODED BS 785 - 861. REMOVED AND INSTALLED A NEW SEAT TRACK IAW AMM 53-00-49-000-801, EC/TC REO 670-53-00-343, GREO 670-53-00-343 REV M AND AMM 53-00-49-400-801.Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA201612291365Floorbeam · corrodedFLOORBEAM CORRODED BS 549, RBL 7.5. BLENDED CORROSION. PERFORMED UT THICKNESS INSPECTION, PERFORMED EDDY CURRENT INSPECTION IAW NDTM PT1 51-20-006-250-A01. NO INDICATIONS NOTED. COMPLIED WITH REO 670-53-13-31-396 AND EC/TC REO 670-53-13-31-396.Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
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