Piper Aircraft Corporation Seneca II PA-34-200T User Manual

FAA APPROVED IN N ORMAL CATEGORY BASED ON
FAR 23 AND FAA PART 21 . SUBPART J. THIS
HANDBOOK INCLUDES THE MATERIAL REQUIRED
TO BE FUR NI SHED TO THE Pl LOT BY FAR 23 AND
FAR PART 21 . SUBPART J AND CONSTIT UTE S THE
APPROVED Al RP LANE FUG HT MANUAL ANO MUST
BE CARRIED IN THE AIRPLANE AT ALL TIME S.
Al RPLANE SER IA L NQ __ J_ 1± _- _7 _B _7_ 0_0_
6
_
6
__ _
PILOT'S
OPERATING
HANDBOOK
1999 Kg. SENECA II
PA-34 - 200T
REPORT. VB- 1140
FAAAPPROVEDBY : LJJ ~
WARD EVANS
D.O.A. NO. S0-1
PIPER AJRCRAFT CORPORATI ON
VERO BEACH, FLORIDA
AIRPLANE REGI STRATION NO. 9 H -RE B ¥ DATE
0
0F APPROVAL: SEP TEMB ER 12 . i 980

Piper Aircraft Corporation Seneca II PA-34-200T Specifications

General

Type	Light twin-engine aircraft
Manufacturer	Piper Aircraft Corporation
Model	Seneca II PA-34-200T
Crew	1
Length	28 ft 7 in (8.71 m)
Height	9 ft 11 in (3.02 m)
Max takeoff weight	4, 570 lb (2, 073 kg)
Rate of climb	1, 340 ft/min (6.8 m/s)
Powerplant	2 × Continental TSIO-360EB turbocharged flat-six engines, 200 hp each
Service ceiling	25, 000 ft (7, 620 m)
Capacity	Up to 6 passengers