Weight Limits; Center Of Gravity; Maneuvers; Maneuver Load Factors - Cub Crafters CC18-180 Pilot Operating Handbook

SECTION 2
LIMITATIONS
* Only applicable to Sensenich Propeller 76EM8 when used
with Lycoming O-360-C1G engine per AD 69-09-03.
* *A yellow low oil temperature indication below 100ºF is a
cautionary indication provided to emphasize when the
engine is operating outside the normal range.
must not be initiated when the oil temperature is below
100ºF unless the engine accelerates smoothly when the
2.6

WEIGHT LIMITS

Maximum weight ................................................... 2300 lbs.
Minimum operating weight .................................... 1300 lbs.
2.7

CENTER OF GRAVITY

Forward
Rearward (at all weights) .................... 81.0 in. aft of Datum
The datum is 60 in. forward of wing leading edge.
2.8

MANEUVERS

This is a normal category airplane. All acrobatic
maneuvers, including spins, are prohibited.
2.9

MANEUVER LOAD FACTORS

Maximum positive load factor, flaps up ........................ 3.8 g
Maximum positive load factor, flaps down .................... 2.0 g
Maximum negative load factor .................................... -1.5 g
No inverted maneuvers approved
REPORT TC10000AFM
Page Number: 2-4
NOTE
NOTE
throttle is opened.
(at 2300 lb.) ................. 79.1 in. aft of Datum
(at 1600 lb. or less) ...... 70.5 in. aft of Datum
Straight line variation between points given
CUB CRAFTERS
Issued: 05/31/05
Date of Revision: 06/20/14
CC18-180
Takeoff