BEECHCRAFT
BonanzaS35
Section IX
Supplements
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The 1nformat1ou in this document 1• PM Appl'OYed u.ter1al wh1ch, toptber with
the approprtue basic CAA/PM Approved Airplane nt,i-bt lfanual. 1a applicabl•
aDd muat be carried in the basic manual when airplane 1a modified by t.be
1mtaJ.lat1on o! the Beech Pneumatic Pitch Assist Model PC•l (and Altitude Bold
Model AB-1, s.:r installed) in accord&Dce with S'l'C SA269WE.
The information in this document supersedes the basic manual 011l1 where covered
in the items contained 111 this Supplement. .For l.1aitat1ou &D.d Proced~a. not
cont&1Ded in thia Suppleaent, consult thll aanual proper.
1. LlXITATIONS SEC'l'IOK
l.. Pneumatic Pitch Aaaist ahall be duri=c take-off and laadiq.
2. Plleumat1c Pitch Aaaist ahall be OF'P whea aircraft 1a operated below
800 feet above tbe terrain. -
3. Pzae1-t1c Pitch Aui~t _!?! to be operated above V~ (Green Arc).
4. Brittain Pneumatic Pitch Assist PC-1 and Altitude AH-1 ahall be installed
for use only in conjunction with an FAA Approved 1ustallat1on. of Br1 tta1n-
Clarksob Autopilot or 'l"actair .IIodel B1O1 Autopilot.
11. OPEKATiml PRO:EDURES SECT I OK - KOlU1AL
A. l. A pilot ccmaarid "SXNS .. adJust111en.t is provided to T&rJ' the pitch
:re•poDM.
2. Set "SE!CS" knob full COUDter-clocJnriae befo.N- engacibl: autopilot
... tar.
3. lDcre&N or decre&N "SENS" u required for optimua performance.
(Clockwi .. to incre ... NDa1tivity, counter-clockwi- to dkre ... ).
4. ec..and airl:n.ft attitude with aaAual elevator tria tab.
$. Piteh As•1•t trill. indicator gives •1•ual reference of tria status.
(w:ben. tria• 1bd1cator bar is above aid-mark. &1rcra:f1: bas DO- u.p
eleYator tria &Ad Y1ce Tera&.)
IIOl'Z: C&bin t-perature• below 20°F. will cauM a de<:N&M ill the
aoraal n•po.aae of the i'Deuaat1c Pitch Aa•i•t.
l'M~ed
(B) Da~: September 20, 1963
(B) Paplof2~
11401
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