1983 - 2029.pdf

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 MOJAVE PA 31P-350 <, HOW IT COMPARES Piper Beech 5BP Cessna 340 Cessna 414 Cessna 421 Cabin Width (ft/in) Height (ft/in) Passengers Weights (lb) Typical empty Max i o Max fuel (US gal) Power (h.p.) Performance Max cruise fkt) Take off distance (ft) Max range (n.m.) : (48rn in reserve) Base price (IFR,S) These figures are intended  4/2 4 /  i 5/6 5 070 7 200 240 2 x 350 234 2,800 1,300 3/6 4/2 4,020 6 200 166/190 2x325 241 2 643 1,235 3/10J 4/1 5 4,184 5 990 207 2 x 310 229 2,175 1,405 4/7 4/3 5 4,543 6 750 213 2 x3 10 224 2 595 1 327 561,500 04,500 474,810 442,300 , i gujde; consult manufacturers far detailed quotations 4/7 4/3 5/es 4 883 7 450 213/270 2 x 375 241 2 323 1,485 655 200 50in -»-j Manufacturer s performance figures Climb rate—two engines —one engine Certificated altitude Single-engine service ceiling Pressurisation Cruise. 75% power, mid weight Cruise, 55% power, mid weight Take-off distance (50ft) 1 490ft/min 293ft/min 25.000ft 15,300ft 6lb/in  234kt 201kt 2,800ft Maximum  weights Ramp Take-off Landing Zero fuel 7.245lb 7.200lb 7.000lb 6.7001b 5901b Manufacturer: Piper Aircraft Corp, Lock Haven, PA, USA 1745,  telephone (717)  748-6711;  UK distributor: CSE  Avi ation.  Oxford, telephone 108675) 43 21 . FLIGHT International 5 Novemb er 1983 1235

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MOJAVE PA 31P-350

<,

HOW IT COM PARE S

Piper

B e e c h

5 B P

C e s s n a

3 4 0

C e s s n a

4 1 4

C e s s n a

4 2 1

Cabin

W idth ( f t /in )

Height ( f t / in)

Passengers

W e i g h t s ( lb )

T y p i c a l e m p t y

Max i o

Max fuel (US gal)

Power (h.p.)

P e r f o r m a n c e

Ma x c ru ise fk t )

Take off distance (f t )

Max range (n.m.)

: (48rn in reserve)

Base price (IFR,S)

These f igures are in tended  

4 / 2

4 /   i

5 / 6

5 070

7 200

2 4 0

2 x 3 5 0

2 3 4

2 , 8 0 0

1,300

3 / 6

4 / 2

4 , 0 2 0

6 200

1 6 6 / 1 9 0

2 x 3 2 5

2 4 1

2 6 4 3

1,235

3 / 1 0 J

4 / 1

5

4 , 1 8 4

5 990

2 0 7

2 x 3 1 0

2 2 9

2 , 1 7 5

1,405

4 /7

4 /3

5

4 , 5 4 3

6 750

2 1 3

2 x 3 1 0

2 2 4

2 5 9 5

1 327

5 6 1 , 5 0 0

0 4 , 5 0 0 4 7 4 , 8 1 0 4 4 2 , 3 0 0 ,

i gu jde ; consu l t manufac turers fa r de ta i led quota t ions

4 / 7

4 / 3

5 / e s

4 8 8 3

7 450

2 1 3 / 2 7 0

2 x 375

2 4 1

2 3 2 3

1,485

6 5 5 2 0 0

50in -»- j

Manufacturer s performance figures

Climb rate—two engines

—one engine

Certificated altitude

Single-engine service ceiling

Pressurisation

Cruise. 75% power, mid weight

Cruise, 55% power, mid weight

Take-off distance (50ft)

1 490ft/min

293f t /m in

25.000f t

15,300ft

6 lb / in

 

234k t

201k t

2,800ft

M a x i m u m   weights

Ramp

Take-off

Landing

Zero fuel

7.245lb

7.200lb

7.000lb

6.7001b

5901b

Manufacturer: Piper Aircraft Corp, Lock Haven, PA, USA

1 7 4 5 ,

  telephone (717)   7 4 8 - 6 7 1 1 ;   UK distributor: CSE   Av i

ation.

 Oxford, telephone 108675) 43 21 .

FLIGHT International 5 Novemb er 1983

1235