Section 2 Placards Flashcards
Emergency Exit / Pilots Side Window
EMERGENCY EXIT - PULL HANDLE - PUSH BOTTOM OF WINDOW OUT WITH SUSTAINED FORCE
Emergency Exit / Below Aft Lower Corner of Pilots Side Window
EMERGENCY WINDOW RELEASE - PULL
Adjacent to Left Engine Fuel Selector
a. 50 GAL - LEFT MAIN - (Green Sector)
b. 50 GAL - RIGHT MAIN - (Yellow Sector)
c. LEFT ENGINE - OFF - (Red Sector)
d. 31.5 GAL - LEFT AUX (Yellow and Green Sector)
Adjacent to Right Engine Fuel Selector
a. 50 GAL - RIGHT MAIN - (Green Sector)
b. 50 GAL - LEFT MAIN - (Yellow Sector)
c. RIGHT ENGINE - OFF - (Red Sector)
d. 31.5 GAL - RIGHT AUX (Yellow and Green Sector)
On Floor Between Fuel Selectors
a. SET FUEL SELECTOR VALVE TO LEFT MAIN TANK FOR LEFT ENGINE AND RIGHT MAIN TANK FOR RIGHT ENGINE IN TAKEOFF, LANDING, AND EMERGENCY
b. TAKEOFF AND LAND WITH AUX FUEL PUMPS ON
c. USE FULL RICH MIXTURE AND AUXILIARY FUEL PUMPS ON ‘LOW’ WHEN SWITCHING FUEL TANKS (FEEL FOR DETENTS)
d. n/a
e. TO EXTEND GEAR MANUALLY , PULL OUT THE CRANK TO ENGAGE AND TURN CLOCKWISE. CAUTION: 1. GEAR SWITCH SHOULD BE IN NEUTRAL BEFORE OPERATING MANUAL SYSTEM. 2. PUSH BUTTON AND STOW CRANK BEFORE OPERATING ELECTRICALLY.
f. USE MAIN TANKS FOR TAKEOFF, LANDING, AND FIRST 90 MINUTES OF FLIGHT
Above Wire Tunnel Trim Above Circuit Breaker Panel
a. THIS AIRCRAFT MUST BE OPERATED AS A NORMAL CATEGORY AIRCRAFT IN COMPLIANCE WITH THE OPERATING LIMITATIONS STATED IN THE FORM OF PLACARDS, MARKINGS, AND HANDBOOKS (PILOT’S CHECKLIST)
b. NO AEROBATIC MANEUVERS INCLUDING SPINS ALLOWED
c. AIR MINIMUM CONTROL SPEED: 80 KIAS
d. MAXIMUM GEAR OPERATING SPEED: 138 KIAS
e. MAXIMUM GEAR EXTEND SPEED: 138 KIAS
f. MAXIMUM FLAP EXTEND SPEED: (15 FLAP): 158 KIAS
(35 FLAP): 139 KIAS
g. MAXIMUM MANUEVERING SPEED: 148 KIAS
Idle Power Stall Speeds: Gear Up/Flaps Up
Bank 0: 79
Bank 20: 82
Bank 40: 91
Bank 60: 112
Idle Power Stall Speeds: Gear Down/Flaps 15
Bank 0: 77
Bank 20: 79
Bank 40: 88
Bank 60: 109
Idle Power Stall Speeds: Gear Down/Flaps 35
Bank 0: 72
Bank 20: 74
Bank 40: 82
Bank 60: 101
On Instrument Panel
a. OPEN DEFROST OR CABIN AIR DURING HEATER OPERATION
b. HEATER OVERHEAT - PUSH - TEST T AND B - LOW VOLT
c. Near the fuel tank quantity indicator selector switch:
MAIN AUX - L.H. AUX - R.H. AUX
On Rudder Horn
a. If optional rudder mounted rotating beacon installed:
ANTI-COLLISION LIGHT REQ’D FOR PROPER RUDDER MASS BALANCE. DO NOT REMOVE
On Wing Locker Doors
MAXIMUM BAGGAGE - 120 LBS
On Baggage Door
MAXIMUM BAGGAGE CAPACITY - STATION 89 TO STATION 109 - 200 LBS. STATION 109 TO STATION 132 - 160 LBS. SEE WEIGHT AND BALANCE DATA FOR DETAILED LOADING INSTRUCTIONS
In Nose Baggage Area
MAXIMUM BAGGAGE XX.X
MAX CAPACITY 350 LBS LESS XX.X OPERATIONAL EQUIPMENT
On Engine Control Pedestal
a. T.O. - T.O. (takeoff) range on elevator trim tab indicator (nose up 4 deg to nose up 11 deg) NOSE DN NOSE UP
b. Above Rudder Trim Tab: L NOSE R
c. Above Aileron Trim Tab: L ROLL R
d. ENGINE ALTERNATOR AIR - PULL OUT - LOCK R - LOCK L
e. If Propeller unfeathering accumulators are installed: PROPELLER UNFEATHERING ARE INSTALLED ON THIS AIRPLANE
f. COWL FLAPS - PULL TO CLOSE - LOCK LOCK
