Schweizer 269c Manual

  1. Get Free Schweizer 269c Operation Manual gear lycoming fuel-injected Schweizer Model 300CModel 300C - Canyon State Aero Schweizer Series TH-55, 269 A, 269 A-1, 269B, 269C through SN.
  2. Of this and other versions, such as for example the 269C, I shall compile a separate report. h2Performances. In standard atmospheric conditions, at its maximum take-off weight of 703 kg (1'550 lbs), the helicopter has a cruising speed of 136 km/h, while the never exceed speed at sea level is 139 km/h. Above an altitude of 610 m/asl the speed.
  3. Schweizer 300C Model 269C Helicopter Flight Manual (part# CSP-C-1). Aircraft manuals and publications required for any reason other than historical or research.

General SCHWEIZER Pilot's Flight Manual Model 269C-1 Helicopter Sec tion I GEN ERAL IN TRO DUC TION The Pilot’s Flight Manual has been prepared to provide the pilot with information necessary to accomplish the intended mission with the maximum amount of safety and economy possible.

Schweizer 269c 1 Sky Knight

The brilliant career of the Hughes 269A is confirmed by the fact that today, after more than fifty years following its first flight, its the direct successors such as the S-300C and the S-300CBi are still being produced in series!

Schweizer 269c Manual

Civil applications

The Hughes 269A was mainly used for the following tasks: school, business and private flights, photographic and observation missions. It could also be fitted with a special spray system for agricultural applications. Several (american) cities used this two-seater in law-enforcement roles. In this function as an “eye in the sky” it was used to patrol designated areas and support the police units on the ground.
Nowadays the Hughes 269A still flying are mostly used by private users. However there are some aviation schools which are still offering training courses on this historical helicopter.

Technical description*

Schweizer 269c Manual Online

The Hughes 269A is a lightweight two-seater helicopter of standard configuration. The occupants seat side-by-side (the pilot sits in the right seat). The main rotor has three fully articulated blades, and the two-bladed tail rotor is of the teetering type. Its exterior aspect may not appear particularly attractive. Design emphasis is on simplicity in order to keep operating costs to a minimum.