You see, here's the problem:
I'm no Ernie Gann. Nor am I the only DC6 pilot on this board. Not only that, but I'm afraid I'm not infused with the proper amount of nostaglia necessary to wax poetic about the big Doug.
Is it just a job? No, it's an adventure too. I honestly never know where I'm going to spend the night. There are far too many variables in a regular DC6 operation. I suppose I could list them but you can probably guess the big ones.
So to the question about lifestyle, well, it can be tough but what flying job isn't tough on lifestyle.
When we work, we work hard and fast.
All right, I feel "A Day in the Life" coming on. Maybe we can start a new thread about that...?
Here's the deal. About an hour and a half before departure the FE shows up for the preflight and fueling. He'll start in the cockpit and check things like the fire warning system, electrical system, hydraulic system. He'll also check all of the fuel boost pumps and the warning horns (takeoff and gear). After the cockpit is finished he'll go outside for the walk around. Obvious stuff: gear pins, hydraulics, uplocks, lights, tires, brakes, etc.
All that should take about 30 minutes. By then the FO and Capt should be sauntering in the door. Have a look at the release and the weather and the load and give a fuel load to the engineer...who goes back out to the plane, unless one of us was cool enough to go out there and tell him what the fuel load was.
The FE will take the planes 14' ladder and climb on top of the wing (in every weather condition, it doesn't matter. If it's snowing he'll also take a broom with him--if he's smart). The plane has 4 main fuel tanks and 4 aux tanks for a total capacity of 5404 gals of 100LL. That's 32,424# of fuel at a high power cruise setting of 1200bhp at 2400#/hr that's roughly 13.5 hours endurance. A more typical fuel load for our flights is between 9,500# and 12,500#.
The old joke about running out of oil before running out of fuel is a true comment. Each engine carries 30 gals of oil. We figure a 10 gal burn for the first hour and then 4 gals for every hour or leg after that.
And then there's the water/methanol mix: 10 gals per engine. That'll give you about 3 to 4 "wet" takeoffs depending on temperature and technique.
A lot of this airplane's weight, as you can tell, is just carrying itself around. It has an empty weight of about 59,000#. It'll carry a cabin load of about 28,000# and has a max takeoff weight of 103,800# when using water injection and auto-feather.
The engines will develop a max 2400bhp at takeoff. Max 2800RPM. Max 59.5"MP. There's a formula for calculating bhp from BMEP and RPM but I don't remember it off the top of my head.
Bottom line with the BMEP gauge is that it's basically a torque gauge measuring power at the prop but they're not even calibrated. So we only use them for leaning (12 drop) and as a general power instrument. I usually take a nice scan of the BMEPs, MPs, RPMs and oil and fuel pressures after the 60 knot call but before V1.
The unusual thing about the DC6 (maybe other large recips too, I don't know) is that the FE handles the throttles except during the flare on landing. During takeoffs the pilot's hand is on the throttles until V1 in case of an abort but the FE is setting MP and monitoring RPMs, water, oil and fuel pressures.
After takeoff the FE will be busy looking at all 144 spark plugs (one at a time) on a scope. He'll be looking for patterns that will indicate shorted leads, fouled plugs, low compression, etc. Simultaneously he'll also be adjusting cowl flaps to maintain 170 degrees on the CHTs and maintaining climb power with the throttles.
This airplane belongs rightfully so to the engineer and then the Capt. It is really a huge responsibility for someone who is typically new to the company. In fact, I understand Air Atlantique, a British operator, puts new hires in the right seat and then upgrades them to engineer and then Capt. It seems like a pretty good idea to me as I've come to believe that the most useless person in a three person cockpit is the FO.
The FO is basically just responsible for paperwork, flying every other leg (usually the light one) and trying to stay out of the way of the engineer.
The cockpit wasn't originally designed for an FE. But after a few crashes in the 50's and after some pressure from ALPA (I understand) Douglas was forced to install an FE seat, facing forward between the pilots stradling the center console where they put the trims, mixes, carb heats, flap and gear handles.
The cockpit is huge but it's often an orgy of shoulders, hands and elbows.
Anyway, once leveled in cruise, the FE will lean out the engines and this is usually when a cracked cylinder will rear its ugly head with a nice firm backfire. When that happens the FE will re-enrichen the mix, turn to the scope and determine which cylinder is the offender. At that point the engine is usually feathered (as a Capt once told me: There are no mandatory shut downs when I'm on board) and we return to base to wait for the four to six hour jug change which has made our already long day that much longer.
One of the charming things about working in Alaska is that we operate under 121 supplemental. That's right. There's no "duty day" limits per se. Twelve hours of flying in a 24 hour period. That's it. I was on duty for 20 hours once after a diversion to an airport with no fuel.
Don't ask. Long story.
What else? I don't know. When it's light it flys like a seminole. When it's heavy it flys like a big boat. It has a real fat straight wing so it can handle big loads on crappy strips. The gear is stout--very stout. The systems are redundant. The beautiful thing about the Six is that if something breaks there's usually another way to get it to work.
All of the heaters (3 wing, 1 cabin) have dual ignition and cross feed capability.
The carbs have heat and alcohol.
The windscreen has heat and alcohol.
Pressurization is automatic/manual or...coffee-grinder (nevermind). Two cabin super-chargers.
Electrical: One GEN can handle the entire load. Three inverters. Engine instruments get power from two. The third is for emergencies when on BATT power.
Two engine driven HYD pumps and one elect. aux pump. In case of total loss of HYD the brakes have an emer air press tank.
The props are reversible up to METO power and quite effective but they get tempermental when it gets really cold. Blade switches stick and sometimes they get stuck in reverse or just go to feather when coming out of reverse. This is where an experienced and knowledgeable FE comes in very handy. Talk about arm pits and elbows...
It is an amazing airplane considering it was designed only 40 years after the Wright Flyer. It was, at one point, state of the art. You can see those guys in Santa Monica actually sat down and thought about what they were gonna build. The design is a proven success no doubt about it. And I've been accused of being bitter and twisted but the truth of the matter is that I'm proud to work for a company that has been operating DC6s longer than anyone else in the world. We've had two hull losses (one fatal) in 48 years of business. And it's not like these things get pampered. They work all year-round, all around the clock in every conceivable condition. The fact of the matter is we abuse them.
We've de-clutched the high-blowers and run the lowest possible octane while making full power wet take offs. We have the least experienced crews ever. Every take off and almost every landing is overweight--and not always greased, let me tell you. And then we'll take this poor machine that was designed to cross an ocean and we'll do 10 shuttles a day to an airport that's 15 mins away when it's -30F. Tell me that's not tough on the structure and the engines.
Is it no wonder she smokes, spits, coughs, squeaks, rattles, moans and slowly shudders everytime she gets off.
It's the moaning and shudders I like best.
There. That's flying a DC6.