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ENSTROM 480 - Chapter 1: Operating Limitations; General Operating Limitations; Altitude Limits; Engine and Fuel Operation Limits

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ENSTROM 480/480B RFM SUPPLEMENT 1-1
FAA Approved: Jan 24/11
Report No. 28-AC-041 Dec 17/10
CHAPTER 1. OPERATING LIMITATIONS
1-1. General
1. Refer to the basic RFM.
2. In addition to the operating limitations set forth in the
basic RFM, the following limitations must be observed during
ground and flight operations.
1-2. Altitude Limits
1. Maximum operating pressure altitude without
supplement oxygen equipment is 2,400 m (8,000 ft) with
passengers on board or 3,000 m (10,000 ft) without
passengers on board.
2. Oxygen equipment must be approved by CAA of Ukraine.
1-3. Engine Limits
1. Fuel Operation Limits
a. Primary Fuel is defined as fuel conforming to MIL-T-5624
Grade JP-4 or JP-5, MIL-G-83133 Grade JP-8, ASTM D
1655 Jet A/A1 or Jet B, GOST 10227 Grade RT or TS-1,
GSTU 320.00149943.007-97 Grade RT and GSTU
320.00149943.011-99 Grade TS-1.
NOTE
At temperatures below 4°C (40°F), fuels RT
and TS-1 shall contain Anti-Icing Additive
Fluid I or Fluid I-M with a concentration of
0.1 - 0.3% by volume.
This electronic document is not linked to a subscription for revision control or distribution. Refer to the Optional Equipment
Supplement Publications Status link under the Technical Support Page of the Enstrom Helicopter website for the current revision
level of this Rotorcraft Flight Manual Supplement.
UNCONTROLLED COPY WHEN DOWNLOADED OR PRINTED

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