1976 Cessna U206F

• Max Takeoff Weight: 3,600 lb

Engine

• CONTINENTAL IO520F 
• S/N: 1011513

Prop

• HARTZELL
• PHC-C3YF-1RF
• 975.1 SOH 

Modifications/Conversions

• Installation of the Split Forward Cargo Door Window must be in accordance with Transport Canada Civil Aviation (TCCA) approved Airworthiness Resources Corporation (ARC) Installation Instruction P0220-08, Revision IR dated June 1, 2020, or later TCCA approved Revision.
• Operation of the Split Forward Cargo Door Window must be in accordance with TCCA Approved ARC Flight Manual Supplement FMS-2061-01, Issue 1 dated June 30, 2020, or later TCCA approved Issue.
• Maintenance of the Split Forward Cargo Door Window must be in accordance with TCCA accepted ARC Instructions for Continued Airworthiness P0220-29, Revision IR dated May 1, 2020, or later TCCA accepted Revision.
• Basis of Certification: As per original basis of certification defined in TCDS ACE and A-212. Compliance with FAR 23.807 at amendment 23-10 has been shown when the aircraft has six (6) or fewer occupants on board.
• Definition of the Type Design Change: TCCA Approved ARC Master Data List MDL-2061-01, Issue 1 dated June 30, 2020, or later TCCA approved Issue.
• Note: This Supplemental Type Certificate enables Cessna 206H and 206H models to operate with six (6) or fewer occupants on board when configured with an approved 6 seat interior.

• Split Rear door (STC SA-34)
• Two ICom A210s
• One Kenwood VHF
• One Artex 406 ELT
• Transponder removed as per tech log entry

• Maintained to commercial standards 
• Last Flown July 3, 2022
• Last W/B April 1,2021
• Empty- 2050.0 LB
• C-of-G 34.8
• Last C-of-A April 30, 2022