# Service difficulty reports: N712EV

A list on [N712EV](https://openairdocs.org/aircraft/N712EV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 251 reports

- [SDR SWI2024F00903](https://openairdocs.org/sdr/SWI2024F00903.md): Windshield · cracked · Oct 2, 2024 · N712EV · Cndair CL6002C11 · Flight Compartment Windows
  > R 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 1442623
- [SDR SWIA202163792](https://openairdocs.org/sdr/SWIA202163792.md): None · damaged · Dec 7, 2021 · N712EV · Cndair CL6002C10 · Wing Structure
  > LH 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
- [SDR SWIA202163791](https://openairdocs.org/sdr/SWIA202163791.md): None · corroded · Nov 7, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING 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
- [SDR SWIA202163790](https://openairdocs.org/sdr/SWIA202163790.md): None · corroded · Nov 4, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FS409 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 CONTINUATI
- [SDR SWIA202163794](https://openairdocs.org/sdr/SWIA202163794.md): None · corroded · Nov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION 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 TO
- [SDR SWIA202163789](https://openairdocs.org/sdr/SWIA202163789.md): None · dented · Nov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > DENT 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 CONT
- [SDR SWIA202163788](https://openairdocs.org/sdr/SWIA202163788.md): None · dented · Nov 2, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > DENT 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 DISP
- [SDR SWIA202163787](https://openairdocs.org/sdr/SWIA202163787.md): None · damaged · Oct 19, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > CREASE 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 AND
- [SDR SWIA202163786](https://openairdocs.org/sdr/SWIA202163786.md): None · dented · Oct 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > SEVERAL 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 ST
- [SDR SWIA202163785](https://openairdocs.org/sdr/SWIA202163785.md): None · gouged · Oct 12, 2021 · N712EV · Cndair CL6002C10 · Rudder, Plate/Skin
  > AIRCRAFT 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 F
- [SDR SWIA202163784](https://openairdocs.org/sdr/SWIA202163784.md): None · damaged · Oct 3, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME @ 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 51-42-2
- [SDR SWIA202163783](https://openairdocs.org/sdr/SWIA202163783.md): None · damaged · Sep 28, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > REMOVE 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 PAR
- [SDR SWIA202163782](https://openairdocs.org/sdr/SWIA202163782.md): None · corroded · Sep 25, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > REPLACE 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-A
- [SDR SWIA202163781](https://openairdocs.org/sdr/SWIA202163781.md): None · corroded · Sep 24, 2021 · N712EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > REPLACE 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
- [SDR SWIA202163780](https://openairdocs.org/sdr/SWIA202163780.md): None · corroded · Sep 21, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > LEFT 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 CARD
- [SDR SWIA202163779](https://openairdocs.org/sdr/SWIA202163779.md): None · cracked · Sep 20, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > WINDSHIELD 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
- [SDR SWIA202163778](https://openairdocs.org/sdr/SWIA202163778.md): None · cracked · Sep 20, 2021 · N712EV · Cndair CL6002C10 · Fuselage Structure (General)
  > WINDSHIELD 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. / REMO
- [SDR SWIA202163777](https://openairdocs.org/sdr/SWIA202163777.md): None · corroded · Sep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > LEFT 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
- [SDR SWIA202163776](https://openairdocs.org/sdr/SWIA202163776.md): None · corroded · Sep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > ON 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 ACTI
- [SDR SWIA202163775](https://openairdocs.org/sdr/SWIA202163775.md): None · corroded · Sep 18, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 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 CORRECT
- [SDR SWIA202163774](https://openairdocs.org/sdr/SWIA202163774.md): None · corroded · Sep 17, 2021 · N712EV · Cndair CL6002C10 · Doors
  > CORROSION 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, 53
- [SDR SWIA202163773](https://openairdocs.org/sdr/SWIA202163773.md): None · corroded · Sep 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION 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. R
- [SDR SWIA202163772](https://openairdocs.org/sdr/SWIA202163772.md): None · corroded · Sep 17, 2021 · N712EV · Cndair CL6002C10 · Fuselage Main, Keel
  > SURFACE 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
- [SDR SWIA202163771](https://openairdocs.org/sdr/SWIA202163771.md): None · corroded · Sep 17, 2021 · N712EV · Cndair CL600* · Water and Waste System
  > AFT 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 CORR
- [SDR SWIA202163770](https://openairdocs.org/sdr/SWIA202163770.md): None · corroded · Sep 16, 2021 · N712EV · Cndair CL600* · Fuselage Main, Frame
  > BACK 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,
- [SDR SWIA202163795](https://openairdocs.org/sdr/SWIA202163795.md): None · corroded · Sep 9, 2021 · N712EV · Cndair CL6002C10 · Doors
  > ABOVE 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 53-31-06-0
- [SDR SWIA202163793](https://openairdocs.org/sdr/SWIA202163793.md): None · cracked · Sep 2, 2021 · N712EV · Cndair CL6002C10 · Window/Windshield System
  > CAPTAIN 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 AM
- [SDR SWIA202163769](https://openairdocs.org/sdr/SWIA202163769.md): None · dented · Aug 31, 2021 · N712EV · Cndair CL600* · Fuselage Structure (General)
  > FS 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-- DA
- [SDR SWIA202163768](https://openairdocs.org/sdr/SWIA202163768.md): None · dented · Aug 31, 2021 · N712EV · Cndair CL600* · Aileron Tabs
  > LH 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 57-53
- [SDR SWIA202163767](https://openairdocs.org/sdr/SWIA202163767.md): None · cracked · Aug 30, 2021 · N712EV · Cndair CL600* · Fuselage Main, Frame
  > FRAME 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 51-42-21-001-001
- [SDR ASOA201812315008](https://openairdocs.org/sdr/ASOA201812315008.md): Smoke Detector · false activation · Dec 31, 2017 · N712EV · Cndair CL6002C10 · Smoke Detection
  > AFT 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.
- [SDR ASOA201706061667](https://openairdocs.org/sdr/ASOA201706061667.md): Stiffener · cracked · Jun 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FS 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.
- [SDR ASOA201706031640](https://openairdocs.org/sdr/ASOA201706031640.md): Frame · cracked · Jun 3, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 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-
- [SDR ASOA201706021639](https://openairdocs.org/sdr/ASOA201706021639.md): Angle · damaged · Jun 2, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE 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.
- [SDR ASOA201701061033](https://openairdocs.org/sdr/ASOA201701061033.md): Intercostal · corroded · Jan 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND INTERNAL JACKING FITTING, LT INTERCOSTAL CORRODED. REMOVED AND REPLACED THE INTERCOSTAL, DUCT SPLICE & INTERCOSTAL ANGLE IAW EA 30-2017-004 REV.
- [SDR ASOA2017010610231](https://openairdocs.org/sdr/ASOA2017010610231.md): Frame · corroded · Jan 6, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, Frame
  > DURING 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.
- [SDR ASOA2017010510232](https://openairdocs.org/sdr/ASOA2017010510232.md): Hinge · gouged · Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage, Door Hinge
  > DURING 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.
- [SDR ASOA2017010510230](https://openairdocs.org/sdr/ASOA2017010510230.md): Skin · corroded · Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING 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 670-53-21-242
- [SDR ASOA201701051029](https://openairdocs.org/sdr/ASOA201701051029.md): Former · corroded · Jan 5, 2017 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR ASOA201712311009](https://openairdocs.org/sdr/ASOA201712311009.md): Landing · corroded · Dec 31, 2016 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING 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.
- [SDR ASOA201712311003](https://openairdocs.org/sdr/ASOA201712311003.md): Skin · corroded · Dec 31, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > INTERNAL 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.
- [SDR ASOA201712301002](https://openairdocs.org/sdr/ASOA201712301002.md): Seat Track · corroded · Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LT 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.
- [SDR ASOA201612301392](https://openairdocs.org/sdr/ASOA201612301392.md): Stringer · corroded · Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FWD 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.
- [SDR ASOA201612301391](https://openairdocs.org/sdr/ASOA201612301391.md): Seat Track · corroded · Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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.
- [SDR ASOA201612301390](https://openairdocs.org/sdr/ASOA201612301390.md): Seat Track · corroded · Dec 30, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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.
- [SDR ASOA201612291371](https://openairdocs.org/sdr/ASOA201612291371.md): Seat Track · corroded · Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING 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.
- [SDR ASOA201612291370](https://openairdocs.org/sdr/ASOA201612291370.md): Floor Support · corroded · Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING 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 WIT
- [SDR ASOA201612291367](https://openairdocs.org/sdr/ASOA201612291367.md): Seat Track · corroded · Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN 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-
- [SDR ASOA201612291366](https://openairdocs.org/sdr/ASOA201612291366.md): Seat Track · corroded · Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT 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.
- [SDR ASOA201612291365](https://openairdocs.org/sdr/ASOA201612291365.md): Floorbeam · corroded · Dec 29, 2016 · N712EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBEAM 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.

Next page: https://openairdocs.org/aircraft/N712EV/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/aircraft/N712EV/reports

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