# Service difficulty reports: N709EV

A list on [N709EV](https://openairdocs.org/aircraft/N709EV.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 4 · 197 reports

- [SDR SWIA202512080006](https://openairdocs.org/sdr/SWIA202512080006.md): Proximity Sensor · out of rig · Dec 6, 2025 · N709EV · Cndair CL6002C11 · Landing Gear Position and Warning
  > NOSE DOOR OPEN WARNING MESSAGE ON CLIMB OUT. QRH COMPLETED. (FLIGHT 3574) INTERROGATED MDC AND FOUND B1-007721 INDICATING NLG RT DOOR OUT OF RIG OR PROX SENSOR PX 31 OUT OF RIG. PERFORMED GEAR SWINGS IN REFERENCE AMM 32-30-00, COULD NOT DUPLICATE FAULT. MEAS
- [SDR SWIA202264018](https://openairdocs.org/sdr/SWIA202264018.md): None · malfunctioned · Jan 22, 2022 · N709EV · Cndair CL600* · Landing Gear Door Actuator
  > GEAR DISAGREE WARNING MESSAGE UPON GEAR RETRACTION AFTER TAKEOFF. RAN QRH. WARNING MESSAGE WENT AWAY, BUT THE MOTOR CONTINUED TO RUN FOR THE DURATION OF THE FLIGHT. ALL THREE GEAR INDICATED DOWN AND LOCKED. (FLIGHT 3251 FILED CLOSED) T/S GEAR DISAGREE
- [SDR SWIA202161757](https://openairdocs.org/sdr/SWIA202161757.md): None · dented · Sep 22, 2021 · N709EV · Cndair CL6002C10 · Wing, Fuselage Attach Fittings
  > RH OUTBOARD FLAP VANE LEADING EDGE HAS TWO DENTS AT WING STATION 185.10 (C-CHECK RO 10/9/2021) REPAIRED THE RIGHT HAND OUTBOARD VANE LEADING EDGE AT WING STATION WS185.10 IN ACCORDANCE WITH REPAIR ENGINEERING ORDER (REO) 670-57-53-001 REV A DATED:201
- [SDR SWIA202161768](https://openairdocs.org/sdr/SWIA202161768.md): None · cracked · Aug 27, 2021 · N709EV · Cndair CL6002C10 · Window/Windshield System
  > FIRST OFFICER WINDSHIELD CONTAINS MINOR CRACKS IN THE (STRUCTURAL) GLASS PLIES ALL AROUND EDGES. (C-CHECK RO 10/9/2021) REMOVED OF THE FIRST OFFICER WINDSHIELD PER AMM TASK 56-11-01-000-801 (CONFIG A01) / REMOVAL OF THE WINDSHIELD SIDE STRAP AMM TASK
- [SDR SWIA202161756](https://openairdocs.org/sdr/SWIA202161756.md): None · dented · Jul 28, 2021 · N709EV · Cndair CL6002C10 · Fuselage Structure (General)
  > DENT ON FUSELAGE SKIN AT LEFT HAND FS517, STR16 (C-CHECK RO 10/9/2021) PERFORMED REPAIR ON LEFT HAND FUSELAGE SKIN AT FS517, STR16L IAW MHIRJ REO 670-53-31-689. IAW CRJ700 NDTM 51-20-006, CRJ700 SRM 51-24-36,51-24-16,51-21-16,51-23-00,51-40-11,51-42-21
- [SDR SWIA202161755](https://openairdocs.org/sdr/SWIA202161755.md): None · damaged · Jul 8, 2021 · N709EV · Cndair CL6002C10 · Fuselage Structure (General)
  > FUSELAGE EXTERNAL SKIN, FS 501, BETWEEN STR 20R & STR21R COUNTERSINK UNEVEN, RIVET HEAD NOT FLUSH WITH SURFACE AFT OF HOLE. (C-CHECK RO 10/9/2021) REPAIR OF FASTENER HOLE ON EXTERNAL FUSELAGE SKIN AT FS 501.00 BETWEEN STGR 20R AND STGR 21R PER STRUCTURA
- [SDR SWIA202161754](https://openairdocs.org/sdr/SWIA202161754.md): None · corroded · Jul 6, 2021 · N709EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > INTERCOSTAL AT STR20R, BETWEEN FS300-FS310 UNDER SERVICE DOOR CORRODED. (C-CHECK RO 10/9/2021) REMOVED CORRODED INTERCOSTAL AT STGR 20R FS 300.00 TO FS 310.00 AND REPLACED WITH NEW INTERCOSTAL IAW CRJ700 SRM 53-21-23, 51-24-21, 51-24-06, 51-40-11, 51-25
- [SDR SWIA202161767](https://openairdocs.org/sdr/SWIA202161767.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 978.00 TO FS. 1005.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) SEAT TRACK DAMAGE AT FS. 978.00 TO FS. 1005.00 RBL27 FOUND TO BE OUT OF LIMIT AS PER CRJ700 SRM 53-51-49. REMOVED AND OBTAINED NEW SEAT TRACK, LOC
- [SDR SWIA202161766](https://openairdocs.org/sdr/SWIA202161766.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 1005.00 TO 1041.00 AT LBL 9 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 1005.00 TO FS 1041.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 20276 7075T6511 LOT#
- [SDR SWIA202161765](https://openairdocs.org/sdr/SWIA202161765.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SIDEWALL SEAT TRACK, LH SIDE FS. 853.00 TO 960.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED AND REPLACED SIDE WALL SEAT TRACK L/H SIDE FS 853.00 TO 960.00 IAW CRJ 700 SRM 51-41-02. AND AMM 53-00-49.
- [SDR SWIA202161764](https://openairdocs.org/sdr/SWIA202161764.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SIDEWALL SEAT TRACK, RH SIDE FS. 853.00 TO FS. 960.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS (C-CHECK RO 10/9/2021) REMOVED AND REPLACED DAMAGED R/H SIDEWALL SEAT TRACK FROM FS853 TO FS960 IAW CRJ700 SRM 53-51-49, 51-41-02, 51-24-36, 51-40-11 AN
- [SDR SWIA202161763](https://openairdocs.org/sdr/SWIA202161763.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 684.00 TO FS.724.00 AT RBL 9.00 FOUND PITTING CORROSION (C-CHECK RO 10/9/2021) REMOVED AND REPLACED DAMAGED SEGMENT OF RBL 9.00 SEAT TRACK FROM FS684 TO FS724 IAW MHIRJ REO 670-53-00-589. NO FURTHER ACTION REQUIRED AT THIS TIME.
- [SDR SWIA202161762](https://openairdocs.org/sdr/SWIA202161762.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 581.00 TO FS. 685.00 AT RBL 9.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED CORROSION AND EVALUATED SEAT TRACK AT RBL9.00 FROM FS581.00 TO FS 685.00 IAW CRJ700 SRM 51-21-06 FOUND TO BE OUT OF LIMITS. RE
- [SDR SWIA202161761](https://openairdocs.org/sdr/SWIA202161761.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 581.00 TO FS. 684.00 AT LBL 9.00 FOUND PITTING CORROSION AND NICKS AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 581.00 TO FS 684.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 202767075
- [SDR SWIA202161760](https://openairdocs.org/sdr/SWIA202161760.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK FS. 376.00 TO FS. 485.00 AT LBL 9 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS. (C-CHECK RO 10/9/2021) REMOVED DAMAGED SEAT TRACK AT FS 376.00 TO FS 485.00 LBL 9.00 IAW CRJ700 AMM 53-00-49. INSTALLED NEW SEAT TRACK P/N 202767075T6511 LOT# R
- [SDR SWIA202161759](https://openairdocs.org/sdr/SWIA202161759.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage, Powerplant Attach Fittings
  > SEAT TRACK AT FS. 364.00 TO FS 485.00 AT LBL 27.00 FOUND PITTING CORROSION AT MULTIPLE LOCATIONS (C-CHECK RO 10/9/2021) REMOVED CORROSION ON SEAT TRACK AT FS. 364.00 TO FS 485.00 AT LBL 27.00, MATERIAL REMOVED IS GREATER THAN 0.035" EXCEEDING ALLOWABLE
- [SDR SWIA202161753](https://openairdocs.org/sdr/SWIA202161753.md): None · corroded · Jun 16, 2021 · N709EV · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > FLOOR SUPPORT FS. 525.00 TO FS. 575.00, RBL 9.00 HAS CORROSION ON UPPER SECTION (C-CHECK RO 10/9/2021) REMOVED AND REPLACED CORRODED FLOOR SUPPORT FROM FS 525 TO FS575, RBL 9.00 IAW CRJ700 SRM 53-00-41. NO FURTHER ACTION REQUIRED.
- [SDR SWIA202161758](https://openairdocs.org/sdr/SWIA202161758.md): None · corroded · Jun 15, 2021 · N709EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > SILL/INTERCOSTAL AT STR21L BETWEEN FS310 AND FS333, SHOWS EVIDENCE OF CORROSION. (C-CHECK RO 10/9/2021) REMOVED AND REPLACED CABIN SILL/INTERCOSTAL AT STR 21L BETWEEN F.S. 310 AND F.S. 333 IAW CRJ 700 AMM 51-42-06 AND SRM 51-42-21
- [SDR SWIA202161752](https://openairdocs.org/sdr/SWIA202161752.md): None · corroded · Jun 15, 2021 · N709EV · Cndair CL6002C10 · Fuselage Structure (General)
  > FS280 SKIN JOINT SPLICE CORRODED BETWEEN STR 20R & 22R. (C-CHECK RO 10/9/2021) COMPLIED WITH MHIRJ REPAIR ENGINEERING ORDER#670-53-21-2092 FASTENERS REMOVED 3 AREAS BLENDED AT FS280.00 SKIN JOINT SPLICE BETWEEN STR20R AND STR22R ALL FASTENERS REINSTALLE
- [SDR SWIA202161751](https://openairdocs.org/sdr/SWIA202161751.md): None · corroded · Jun 9, 2021 · N709EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FS310.00 THRU FS333.00 RIGT SIE FUSELAGE STGR20R CORRODED UNERFLOOR BELOW SREVICE DOOR. (C-CHECK RO 10/9/2021) AFTER FURTHER INVESTIGATION STR20R STRINGER NOT CORRODED, CORROSION IS ON INTERCOSTAL ON STR20R FROM FS310-333. REMOVED AND REPLACED CORRODED
- [SDR SWIA202161750](https://openairdocs.org/sdr/SWIA202161750.md): None · dented · Jun 1, 2021 · N709EV · Cndair CL6002C10 · Fuselage Structure (General)
  > DENT LOWER OUTER BOTTOM REAR FUSELAGE SKIN RBL 8, F.S. 1053 (C-CHECK RO 10/9/2021) REPAIRED DENT OF LOWER OUTER FUSELAGE SKIN AT RIGHT BUTT LINE 8 AT FUSELAGE STATION 1035. PER MHIRJ REO 670-53-61-1923 REV. -- DATED: 18 AUG 2021. ANALYSIS TO BE COMPLETE
- [SDR ASOA201702181248](https://openairdocs.org/sdr/ASOA201702181248.md): Frame · cracked · Feb 18, 2017 · N709EV · Cndair CL6002C10 · Fuselage Main, Frame
  > FOUND RT FS 235.00 UPPER FRAME SECTOR TO BE VISUALLY CRACKED. REMOVED AND REPLACED RT FS 235.00 FRAME SECTOR IAW SRM 51-40-11-001-001-A01, 51-42-21-001-001-A01 AND 51-42-06-001-001-A01.
- [SDR ASOA201702121187](https://openairdocs.org/sdr/ASOA201702121187.md): Stiffener · cracked · Feb 12, 2017 · N709EV · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > DURING A C CHECK, FOUND THE BS 202.75 FWD SIDE OF BULKHEAD RBL 30 STIFFENER HAS AN INDICATION OF.15 INCH LONG CRACK IN THE UPPER EDGE OF FLANGE. REPAIRED IAW SRM 53-11-10-201-005-A01.
- [SDR ASOA201702121186](https://openairdocs.org/sdr/ASOA201702121186.md): Stiffener · cracked · Feb 12, 2017 · N709EV · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > DURING A C CHECK, FOUND THE BS 202.75 FWD SIDE OF BULKHEAD LBL 30 STIFFENER HAS AN INDICATION OF.15" LONG CRACK IN THE UPPER EDGE OF FLANGE. REPAIRED IAW SRM 53-11-10-201-005-A01.
- [SDR ASOA201611050910](https://openairdocs.org/sdr/ASOA201611050910.md): Beam · cracked · Nov 5, 2016 · N709EV · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT APRON STRUCTURE MACHINED BEAM BS 821.31 IS CRACKED. COMPLIED WITH STS EA 32-2016-240 AND EC/TC EA 32-2016-240.
- [SDR ASOA20161105090](https://openairdocs.org/sdr/ASOA20161105090.md): Beam · cracked · Nov 5, 2016 · N709EV · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT APRON STRUCTURE, MACHINED BEAM BS 821.31 IS CRACKED. COMPLIED WITH EA 32-2016-237 AND EC/TC EA 32-2016-237.
- [SDR ASOA20161102109](https://openairdocs.org/sdr/ASOA20161102109.md): Angle · corroded · Nov 2, 2016 · N709EV · Cndair CL6002C10 · Passenger/Crew Doors
  > DURING C CHECK, FOUND KICK PLATE ANGLE AT PAX DOOR SURROUND CORRODED. R & R PAX DOOR KICK PLATE ANGLE IAW SRM 53-21-23-101-001-A01, 51-42-06-001-001-A01, 51-42-21-001-001-A01, AMM 52-70-04-400-802-A01, & 52-70-04-820-802-A02.
- [SDR ASOA20161101108](https://openairdocs.org/sdr/ASOA20161101108.md): Fitting · corroded · Nov 1, 2016 · N709EV · Cndair CL6002C10 · Passenger/Crew Doors
  > DURING C CHECK FOUND PAX DOOR HANDRAIL CUPS CORRODED. R & R PAX DOOR HINGE CUPS IAW SRM 51-42-15-001-001-A01, 51-42-06-001-001-A01, & 51-42-15-001-001-A01.
- [SDR ASOA20161101107](https://openairdocs.org/sdr/ASOA20161101107.md): Seat Track · corroded · Nov 1, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 995-1015. R & R THE SEAT TRACK IAW AMM 53-00-49-000-802-A02, & 53-00-49-400-802-A02.
- [SDR ASOA20161101106](https://openairdocs.org/sdr/ASOA20161101106.md): Seat Track · corroded · Nov 1, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK CORRODED AT RBL 9 BS 985 & 1015. R & R THE SEAT TRACK IAW AMM 53-00-49-400-802-A02
- [SDR ASOA20161101105](https://openairdocs.org/sdr/ASOA20161101105.md): Floor Support · cracked · Nov 1, 2016 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND TRU FLOOR SUPPORT CRACKED AT AFT LATCH ON LEFT SIDE. R & R THE FLOOR SUPPORT IAW SRM 51-42-06-001-001, 51-42-13-001-001, & EC/TC SNIEO CC670-33040 S05.
- [SDR ASOA20161022020](https://openairdocs.org/sdr/ASOA20161022020.md): Seat Track · corroded · Oct 22, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE LEFT SEAT TRACK AT BS 565-677 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021027](https://openairdocs.org/sdr/ASOA20161021027.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT RBL9 BETWEEN BS 677-830 CORRODED. REMOVED AND REPACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.
- [SDR ASOA20161021026](https://openairdocs.org/sdr/ASOA20161021026.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND SEAT TRACK CORRODED AT LBL 9 BETWEEN BS 893 - 977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.
- [SDR ASOA20161021025](https://openairdocs.org/sdr/ASOA20161021025.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND SEAT TRACK CORRODED AT RBL 9 BETWEEN BS 847-977. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000-801-A03 AND COMPLIED WITH EC/TC REO 670-53-00-343 AND GREO 670-53-00-343 REV M.
- [SDR ASOA20161021024](https://openairdocs.org/sdr/ASOA20161021024.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND SEAT TRACJ AT BS 379-485 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021023A](https://openairdocs.org/sdr/ASOA20161021023A.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT BS 485-565 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021022](https://openairdocs.org/sdr/ASOA20161021022.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE RIGHT SIDE SEAT TRACJ AT BS 785-863 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021021](https://openairdocs.org/sdr/ASOA20161021021.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT BS 677-708 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021019](https://openairdocs.org/sdr/ASOA20161021019.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE RIGHT SEAT TRACK AT BS 485-565 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400/801/A03.
- [SDR ASOA20161021018](https://openairdocs.org/sdr/ASOA20161021018.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT BS 469-581, LBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021017](https://openairdocs.org/sdr/ASOA20161021017.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT BS 349-469 RBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021016A](https://openairdocs.org/sdr/ASOA20161021016A.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > DURING C CHECK, FOUND THE SEAT TRACK AT BS 581-677 LBL 9 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161021015](https://openairdocs.org/sdr/ASOA20161021015.md): Seat Track · corroded · Oct 21, 2016 · N709EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RIGHT SEAT TRACK BS 379-485 CORRODED. FABRICATED A NEW SEAT TRACK IAW EC/TC REO 670-53-00-343. REMOVED AND REPLACED THE SEAT TRACK IAW AMM 53-00-49-000/400-801-A03.
- [SDR ASOA20161019095A](https://openairdocs.org/sdr/ASOA20161019095A.md): Floor Support · corroded · Oct 19, 2016 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RBL 9 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT FROM BS 1015 - 1070 IAW REO 670-53-0369, EC/TC EO700-53-0369 AND EC/TC REO 670-53-61-1287.
- [SDR ASOA20161019094A](https://openairdocs.org/sdr/ASOA20161019094A.md): Floor Support · corroded · Oct 19, 2016 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LBL 9 FLOOR SUPPORT CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT FROM BS 1015 - 1070 IAW REO 670-53-61-1288, EC/TC EO700-53-0360 AND EC/TC REO 670-53-61-1288.
- [SDR ASOA20161019031](https://openairdocs.org/sdr/ASOA20161019031.md): Floor Support · corroded · Oct 19, 2016 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING C CHECK FOUND RT FLOOR SUPPORT CORRODED FROM BS 280-319. R & R THE FLOOR SUPPORT IAW SRM 51-40-11-001-001-A01 AND 51-42 13-001-001-A01.
- [SDR ASOA20161019028](https://openairdocs.org/sdr/ASOA20161019028.md): Floor Support · corroded · Oct 19, 2016 · N709EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > DURING C CHECK, FOUND FLOOR SUPPORT AT BS 349 RBL9 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-21-06-001-001-A01, 51-42-06-002-002-A01, AND 51-40-11-001-001-A01
- [SDR ASOA20161016096](https://openairdocs.org/sdr/ASOA20161016096.md): Skin · chafed · Oct 16, 2016 · N709EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > SKIN CHAFED BY FAIRING AT BS 969 - 985. COMPLIED WITH REO 670-53-00-476 AND EC/TC REO 670-53-00-476.
- [SDR ASOA2016062314982](https://openairdocs.org/sdr/ASOA2016062314982.md): Sign · broken · Jun 23, 2016 · N709EV · Cndair CL6002C10 · Emergency Lighting
  > EMERGENCY EXIT SIGN HOUSING ABOVE SERVICE DOOR IS BROKEN, HANGING LOOSE. R & R EMERGENCY EXIT SIGN HOUSING ABOVE SERVICE DOOR IAW AMM 33-51-05. OPS CHECKS GOOD.

Next page: https://openairdocs.org/aircraft/N709EV/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 = 'N709EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N709EV/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.