For those interested the following was obtained from the RCAF Argonaut Pilot Operating Notes. This is what you would call a crib sheet so you get the base safe numbers and techniques which the aircraft required. This was a pressurised hull with liquid cooled RR Merlin engines with a two speed supercharger system. It was heavier than the DC-4 and the C-54.
Overall you will need from 4000 ft to 6500 ft of runway for take offs and landings at ISA temperatures and from being light to heavy.
Fuel planning (in Lbs) - Reserve allow 2100 lbs, Approach Fuel allow 350 lbs and for holding allow for 1400 lbs per hour.
Fuel consumption MS Gear (Below F130) S/L - 250 -450 lbs per engine (500-1000 BHP)
A100 - 240-450 lbs per engine
F150 - 230-580 lbs per engine
FS Gear (Above F130) F150 - 270-470 lbs per engine
F200 - 270-495 lbs per engine
F250 - 340-540 lbs per engine
As can be seen fuel consumption was fairly constant and power was generally set to have about 900 BHP output. So basically your looking at about 500 lbs per hour per engine on the climb.
Stall Speeds: Vs F0 -95 knots
Vs F15 -82 knots
Vs F30 -76 knots
Vs F40 -69 knots
Normal Operating weights were between 55,000 lbs and 78,000 lbs. NOTE Maximum Landing Weight is 66,000 lbs.
V SPEEDs V Rudder Control - 43 knots
Weight | V1 (kts) | V2 (Kts) |
55000 lbs | 70 | 89 |
60000 lbs | 75 | 92 |
65000 lbs | 81 | 96 |
70000 lbs | 87 | 99 |
72000 lbs | 90 | 101 |
74000 lbs | 92 | 103 |
76000 lbs | 94 | 106 |
78000 lbs | 97 | 107 |
TKOF Full throttle 71.5"MP 2900 -3000 RPM Rudder effective from 43 knots VR - Allow acceleration 110 knots - GEAR UP Pitch Attitude 8 degrees
Set 1st Segment Climb to 120 knots Flaps Up then power to 54"MP and 2800 RPM
2nd Segment Climb above 1000ft MS Gear 54"2650 RPM (Maintain these power settings throughout climb
Normal Climb 134 - 147 knots.
F130 Change to FS Supercharger Settings by reducing power on 1 and 4 engines to 30" -Set FS Advance throttles to 54"or 50" Minimum, repeat for engine 2 and 3. Supercharger warning lights should now be ON.
Notes- At max weight Max AOC is 107 knots and about 200 FPM
At 75000 lbs Max AOC is 104 knots and about 300 FPM
At 70,000 lbs Max AOC is 99 knots and about 600 FPM
Rate of Climb is modest and generally about 650 FPM but relatively constant.
Initial Descent - No greater than 217 kts IAS. 2350 RPM 35"MP to 10,000 feet then set MS Gearing on Superchargers
Below 10,000 ft can reduce RPM to between 2250 and 2000 RPM and 35"MP
Landing Gear Vle - 169 knots Vf1 (1st Stage Flap) - 169 knots - RESET RPM to 2350 if required.
Initial Approach - 112 knots Final Approach 112 knots. Flap 30 and 40 degrees not until on final.
Hope this helps some of you Argonaut drivers. This data was not in the Argonaut manual which otherwise was excellent.
Cheers