Piper PA-28-236 DAKOTA, Руководство по эксплуатации для пилотов

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PIPER AIRCRAFT CORPORATION
PA-28-236, DAKOTA
ISSUED: JUNE 1, 1978 REPORT: VB-910
2-5
2.21 FUEL LIMITATIONS
(a) Total Capacity 77 U.S. GAL
(b) Unusable Fuel 5 U.S. GAL
The unusable fuel for this airplane has
been determined as 2.5 gallons in each
wing in critical flight attitudes.
(c) Usable Fuel 72 U.S. GAL
The usable fuel in this airplane has
been determined as 36 gallons in each
wing.
(d) Fuel remaining when the quantity indi -
cator reads zero cannot be used safely
in flight.
2.25 NOISE LEVEL
The noise level of this aircraft is 72.9 d B(A).
No determination has been made by the Federal Aviation Administration
that the noise levels of this airplane are or should be acceptable or unacceptable
for operation at, into, or out of, any airport.
The above statement notwithstanding, the noise level stated above has been
verified by and approved by· the Federal Aviation Administration in noise level
test flights conducted in accordance with FAR 36, Noise Standards - Aircraft
Type and Airworthiness Certification. This aircraft model is in compliance with
all FAR 36 noise standards applicable to this type.
2.25 PLACARDS
In full view of the pilot:
THIS AIRPLANE MUST BE OPERATED AS A
NORMAL CATEGORY AIRPLANE IN COMPLIANCE
WITH THE OPERATING LIMITATIONS STATED
IN THE FORM OF PLACARDS, MARKINGS AND
MANUALS.
T H I S A I R C R A F T A P P R O V E D F O R N I G H T
l.F.R. NON-ICING FLIGHT WHEN EQUIPPED IN
ACCORDANCE WITH FAR 91 OR FAR 135.