Piper Malibu PA-46-310P Pilot Operating Handbook page 500

MALfflU POWER & PROPELLER INT'L, LLC
4600 Lake Road
Minneapolis, MN 55422
AFM SUPPLE:rv.lENT for PA-46-31 OP
2.0 LIMITATIONS (Cont'd)
2.13 WEIGHT LIMITS - N/C
2.15 CENTER OF ORA VITY LIMITS - N/C
2.17
MANEUVER LIMITS - N/C
2.19 FLIGHT LOAD FACTORS-N/C
2.21
KINDS OF OPERATION EQUIPMENT LIST- N/C
2.23 FUEL LIMITATIONS - N/C
2.25 OPERATING ALTITUDE LIMITS - N/C
2.27 CABIN PRESSURIZATION LIMITS - N/C
2.29
NOISE LEVEL - N/C
2.31 MAXIMUM SEATING CONFIGURATION - N/C
Page 6 of7
2.33 PLACARDS - N/C EXCEPT THE FOLLOWING PLACARD IS
LOCATED ON THE DE-ICE SWITCH PANEL:
Prop Heat Test- IO Sec. Max
3.0 E:tv.1ERGENCY PROCEDURES - N/C
4.0
NORMAL PROCEDURES - N/C EXCEPT ADD TO GROUND CHECKLIST:
PROP DE-ICE: Push Prop Heat Test switch to
test
prop de-ice (10 sec
max).
5.0
PERFORMANCE:
The performance of this airplane equipped with the TCM TSI0-550-C
engine and the Hartzell PHC-G3YF-1E/7890(K) propeller is equal to or
better than the performance listed in the original FAA-approved Pilot's
Operating Handbook.
6.0 WEIGHT AND BALANCE - N/C EXCEPT AS NOTED BELOW:
The TCM TSI0-550-C engine and the Hartzell 3-blade PHC-GJYF-
1 E/7890(K) propeller installation is 9 LB heavier than the original airplane
powerplant installation and the CG is approx 0.4 inches further forward.
The STC Installation Instructions contain this information and instructions
for revising the airplane weight and balance data.
FAA Approved:---------
Date:
FEB
O 6 2003
Charles L. Smalley
Manager, Systems & Flight Test Branch
Chicago Aircraft Certification Office
2300 E Devon Ave., Des Plains,
a
60018