EasyManuals Logo

Piper SENECA III User Manual

Piper SENECA III
408 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Page #150 background imageLoading...
Page #150 background image
PA-34-220T
LÄÑÒiÑÖ
Ò18ÏAÑÖE
NÒÑMÄLPRÖCEDURE
STANDARD
WHEELS,
TIRES,
AND BRAKES
THROTTLES
CLOSED 40"
WING
FLAPS
FULL
STALL
TOUCHDOWN PAVED,
LEVEL DRY
3000
i i i
i
i
RUNWAY
MAXIMUM BRAKING
-
Example:
2000
O.A.T.:
22°C
30
as
4 82
76
Pressure
altitude: 3000
ft. 2600
Gross
weight: 3655 lbs.
Head wind: 10
knots
2400
Landing
ground roll
1120
ft
Total
lavrlinr stietance
war
Wh
ha
r
er
Dann
ft
no
B
irrier
s
eed: 82 KIAS
T
rl,, en
H-H¯
H
2ooo
2
m
600
soo
2
LTI
-
600
-40 -20
0
20
40
4500 4000 3500
3000
0 5 10 15
OUTSIDE AIR
TEMPERATURE-°C
WEIGHT
-
POUNDS WIND COMPONENTS
-
KTS.

Table of Contents

Questions and Answers:

Question and Answer IconNeed help?

Do you have a question about the Piper SENECA III and is the answer not in the manual?

Piper SENECA III Specifications

General IconGeneral
ManufacturerPiper Aircraft
ModelSeneca III
Engine TypePiston
Engine ModelContinental TSIO-360-KB
Seating Capacity6
Cruise Speed188 knots (216 mph, 348 km/h)
Length28 ft 7 in (8.71 m)
Max Takeoff Weight4, 750 lb (2, 155 kg)
Horsepower220 hp each
Service Ceiling25, 000 ft (7, 620 m)
Height9 ft 11 in (3.02 m)
Propellers2-bladed constant speed

Related product manuals