Cessna 402C - Page 312

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POH$ 82-2
Page 3-2
EHER~ENCY l'ROCEDURES
A!UHU:V lAUD CHI::CKL 1ST
SINGLE
ENGINE AlkS~EEDS fOR SAFE OPERATION
Cond1tiun.
1. Takeoff weight 6850 IblO. 2.Landing weight 6850 lb ••
3. Standard Day. Sea-level.
(4) Beat Single Engine Rate of Climb Speed: Flaps Up
Flaps 10
0
() &!f;t Single Engine Angle ot Climb Speed: Flap. Up
Flaps 10
0
(1) Atr Hint •• _ Control Sveed:
(2) Reco!lllRended Saf~ SlnKI~ I:::nglne Sp~('d:
Flapa Up
Flaps
10°
Flaps
30°
Flapa
Up
flapI'
10°
80 KIAS
76 KIAS·
70 KIAS
95 KIAS
86 KlAS.
95 KIAS
89 KIAS
104
lIAS
90 KIAS
ENGINE INOPERATIVE PROCEDURES
:':Ilt!tll1C Securing Proc:edur~s -- No ChanKe.
~.f~Li..lne failure !luring Takeof~:(SVc\'d belo..., 95 tC.IAS with
f~a.rS 0°, or Nvced below 86 KIAS wllh flapll 10°)
I. Thr<)ttl'~!i
2. Ilri:fke~. or
- CLOSE H1HJ!;DIATELY
land dod br.tkea -AS Rl:QUIRfD
t~nk:in.., jo'\llure After TCllu~off: (Speed above 95 KIAS with
nUp!i 0° and with gear up or in tr.:snilit) -- No Change.
£1£::'-' failure ,\I'ta Talr,con With flal's 10°: (Speed
;d,,)v'~ 1:16 KlAS ""ith KeRr up or in transit.)
WARNING
I.e-yet f1 Lght u·, not be pOSllLble for cenain coabinationa
lIt wdght. tt'Il}H!"t'ature and altitude. 1.0 an1 event I do not
"tt~mpt to c.onttnue the takeoff unll"fIB landing s .. ar 18
alrr-ady up Q{" 111 transit and a pollit1vte dll1lb capability
I.ftII been deterll.lned froa page 5-11. 00 NOT ALLOW AIRSPEED
TO fALL BELOW 86 lIAS.
FAA Approyecl: A.PRIL 21, 1980
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