Mooney M20J - Page 32

SECTION It
LIMITATIONS
MOONEY
MODEL
M20J
1//1111/1/1///1/11/1/
IlJWARNl NGJll
111/11111/11///111/1I
Takeoff maneuvers, prolonged sldeslps or steep descents
when the selected fueI tank contains less than 8 gallons (48.0
Ik., 30.3 IRers, 8.6 IMP. Gal.) of fuel have not been
demonstrated and may cause loss of pow&
---
I NOTE I
---
Up to 290 foot altitude loss may occur durfng stalls at
maxlmum wetght.
Slow throttle movement required at airspeed above 165 KIAS. Above 165
KIAS, rapid throffl~ movement may result momentary propeller RPM over-
speed.
FLIGHT LOAD FACTOR LIMITS
Maximum Positive Load Factor
.............
Flaps Up +3.8 g.
Flaps Down (33 Degrees) ........ + 2.0 g.
Maxlmum Negative Load Factor
.............
Flap Up -1.5 g. '
Flaps Down ............ 0.0 g.
KIMDS OF OPERATION LIMITS
7711s C a Normal Category airplane approved for VFRllFR day or night opera-
tlons when quipped In accordance with FAR 91.
I
00 NOT OPERATE IN KNOWN ICING CONDITIONS.
TAKEOFFS WITH COWL FLAPS INOPERATIVE ARE
PROHIBITED
Autopilot Llmitatlons - See Section IX.
FUEL LlMtTATlONS
A reduced fuel quantity Indleator is I
llrd in each tank.
The bottom tlp of these lndieat ow the 25 U.S. gallon
-4
(94.7 [Hers) (20.8 IMP. Gal.) usable fue level in each tank.
AIRPLANE FLIGHT MANUAL
2-8
FAA APPROVED REV. B 6-1 2-87
ISSUED 6-2-86