Flight Maneuvering Load Factors; Types Of Operation; Fuel Limitations; Noise Level - Piper PA-44-180 Seminole 1979 Pilot's Operating Handbook And Faa Approved Airplane Flight Manual

SECTION 2
LIMITATIONS
PIPER AIRCRAFT CORPORATION
PA-44-180, SEMINOLE
. 2.17 FLIGHT MANEUVERING LOAD FACTORS
(a) Positive Load Factor (Maximum)
(I)
Flaps Up
(2) Flaps Down
(b) Nega,we Lond Factor (Maximum)
2.19 TYPES OF OPERATION
3.8 G
2.0 G
No inverted maneuvers
approved.
The airplane is approved for the following operations when equipped
in accordance with FAR 91 or FAR 135.
(a) Day V.F.R.
(b) Night V.F.R.
(c) Day I.F.R.
(d) Night 1.F.R.
(e) Non Icing
2.21 FUEL LIMITATIONS
(a) Total Capacity
(b) Unusable Fuel
The unusable fuel for this airplane has
been determined as 1.0 gallon in each
nacelle in critical flight attitudes.
(c) Usable Fuel
The usable fuel in this airplane has
been determined as 54 gallons in each
nacelle or a total of 108 gallons.
2.23 NOISE LEVEL
110 U.S. GAL.
2 U.S. GAL.
108 U.S. GAL.
The corrected noise level of this aircraft is 74. 7 d
B(A)
with the two blade
propeller and 75.6 d B(A) with the three blade propeller.
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.
REPORT: VB-860
2-6
ISSUED: MARCH 23, 1978
REVISED: JANUARY 22, 1982