R22 Beta Limitations Flashcards
Skid Width
76”
Main Rotor Radius
151”
Mast Height
107”
Vne
102KIAS (only up to 3000’ DA)
Vno (at sea level)
92KIAS
ASI Green Arc
50-102
Max demonstrated cross wind component
17kts in a hover from any direction up to 10,600’DA
Max Gross Weight
1370lbs
Minimum Gross Weight
920lbs
Max Weight Per Seat
240lbs (including baggage compartments)
Max Weight Per Baggage Compartment
50lbs
Minimum Solo Pilot Weight
No Aux Fuel Tank: 130lbs
With Aux Fuel Tank: 135lbs
Max operating DA
14,000’
Max operating ambient temp
ISA +23c
Min operating ambient temp
ISA -18c
Wind limits for start up and shutdown
Rotor must not be started or stopped in stead winds >26kts, or gusting >30kts
Rotor max speeds
Power On: 104%
Power Off: 110%
Rotor Minimum Speeds
Power On: 97%
Power Off: 90%
Rotor Tach Markings
Upper Red Line: 110% Upper Yellow Arc: 104-110% Green Arc: 97-104% Middle Yellow Arc: 90-97% Lower Red Line: 90% Lower Yellow Arc: 60-70%
Engine Tach Limitations
Max RPM: 104%
Normal Op Range: 97-104%
Engine Cylinder Head Temp Limitations
Max: 500F
Norm op Range: 200-500F
Engine Oil Temp Limitations
Max: 245F
Norm Op Range: 75-245F
Engine Oil Pressure Limitations
Max, start and warm up: 100psi
Norm op range: 60-90psi
Min, Idle: 25psi
Manifold Pressure Indications
Red Radial: 25.2”hg
Yellow Arc: 21.0-25.2”hg
Carburetor Air Temp Gauge Indications
Yellow Arc (Caution Range): -15c to +5c Use full carb heat below 18"hg manifold pressure
Oil Capacity
4-6qts
Fuel Capacity
Main tank: 19.8gal, 19.2 usable
Aux Tank: 10.9gal, 10.5 usable
Approved Oil Grade for all temps
SAE 20W-50
Approved Fuel Grade
100/130
MAGGIE LR 14 GOAL
M - Minimum Crew 1 A - Aerobatics Prohibited G - No low G Pushover G - Governor Remains on during flight except for training or when broken I - Icing Prohibited E - Either or both doors removed
L - Left Seatbelt buckled
R - Right seat solo only
14 - 14,000’ max DA
G - Governor
O - OAT Guage
A - Alternator
L - Low RPM recognition system
CAMAFOOTS GOALC (PAILS)
C - Compass A - Altimeter M - MAP A - ASO F - Fuel O - Oil Temp O - Oil Pressure T - Tach S - Seat Belts
G -Governor O - OAT Guage A - Alternator L - Low RPM C - Carb Air Temp
P - Position Lights A - Anti-collision Lights I - Instrument L- Landing Light (only req when for hire) S - Spare Fuse
Required Instruments for Day Flight
CAMAFOOTS GOALC
Required Instruments for Night Flight
CAMAFOOTS GOALC PAILS
Vne and high blade pitch angle is caused from:
Vne
- High blade pitch angle happens
- High DA
- High MGW
- Turbulence
- Abrupt Inputs
- Low Rotor RPM
R22 Operating Limitations
MAGGIE 14 LR GOAL