Section II
LIMITATIONS
2-1. ROTORCRAFT CERTIFICATION
Certification is based on an Engine Failure Warning System
(including both visual and audio indications), Low Rotor Warning
System, Outside Air Temperature Gauge, and Fuel Low Caution
Light being installed and operable.
2-2. FLIGHT LIMITATIONS
The following are PROHIBITED:
Operation under Instrument Flight Rules (IFR).
Flight into known icing conditions.
Flight exceeding maximum operating pressure altitude of 10,000
feet.
Solo flight from other than the PIC position. (Refer to Section
4 for identification of PIC position.)
NOTE: When three sets of controls are installed in the aircraft, one
of the occupants must possess a helicopter CFI rating. In non-train-
ing operations, it is recommended that the center set of controls be
removed. (Control set includes: cyclic stick, collective stick, and
tail rotor pedals.) Controls may be removed by pilot. Refer to Para-
graph 7-12 for collective stick installation and removal.
Flight following a battery overtemperature of 160°F or above
until the battery has been inspected. (Optional Ni-Cad)
Flight with door(s) off unless equipped with air dams (P/N’s
269D3109-3/-4) beside left and right seats.
Schweizer RSG, LLC.
Model 269D Helicopter
Reissued:
16
Jan 2019
2-1
FAA Approved
Limitations
Pilot's Flight Manual
Book 3.indd 48
8/4/19 1:25 PM
