flyingcheesehead
Taxi to Parking
- Joined
- Feb 23, 2005
- Messages
- 28,186
- Location
- UQACY, WI
- Display Name
- iMooniac
- Home Airfield
- KUES/KMKE
I've been getting the itch to upgrade to a twin again lately. My sons are getting bigger and the Mooney isn't going to hold all of us forever.
Several years ago I was looking hard at 310s and did a bit of a deep dive learning about them, which I posted as the All About Cessna 310s thread.
Well, I've wanted and loved the Twin Comanche for a much longer time - At least back to 2004 when AOPA's sweepstakes airplane was a Twin Comanche, but I liked them even before that. I am a fan of efficiency, and living next to a big ice bucket of a lake that has swallowed one airplane in my logbook, an efficient twin has been very high on my list for as long as I can remember, and when I started flying the Twinkie was probably the best. It's still the best of the affordable ones, the Tecnam P2006 and the Diamond DA42 are too new to really be in the affordable category just yet, with starting used prices for both still north of half a million dollars.
So, thinking about buying again and thinking about that other thread got me thinking that I should probably make another "brain dump" post with all of the knowledge I've collected on Twin Comanches over the past 25ish years, since I probably won't remember it all for another 25! Maybe Comanche expert @Kristin will fill in any gaps I leave here. As with the other thread, I'll update this first post with any new information. Also, in the course of verifying the information here I found a really well written, thorough article about the Twin Comanche by Tom Horne in the September 1980 issue of AOPA Pilot that's very much worth a read if you're really interested in the Twinkie.
The Basics
The Twin Comanche built on Piper's success with the single-engine Comanche line that started in 1958; the Twin Comanche was introduced in the latter half of 1963. The PA-30 "A" model (which was never so named, just the PA-30) was sold from 1963-65 and can be distinguished from the others by having only two side windows, it also had "four" seats with the two rear seats being a single bench seat. The PA-30B model was sold from 1966-68 and added the third side window and optionally two more seats (6 total) where the last two pretty much took up the baggage compartment and had little to no legroom, really they're kid seats. The PA-30C model was sold in 1969, gained a standard 6-pack panel layout instead of the earlier models' "shotgun" panel, and moved engine switches from the bottom row of the panel to the left-hand side and changed them to rocker switches. Finally, the PA-39 "C/R" was sold from 1970-72 and had counter-rotating props for extra safety. There were also turbonormalized models of the B, C, and 39/CR. On June 23rd, 1972, the remnants of Hurricane Agnes dumped up to 19 inches of rain in the area of the Piper factory in Lock Haven, PA and the adjacent Susquehanna River crested at over 31 feet, destroying and sweeping away airframes, parts, and tooling from the Comanche lines. Piper made the decision to continue producing the Arrow and Seneca in Vero Beach and end production of the entire Comanche line, a sad day in aviation history.
One other historical note on the Twin Comanche series: At the time they were being produced, the FAA required multi checkrides to do a Vmc demo at as low an altitude as possible to maximize thrust on the remaining engine as well as some other foolishness like keeping the ball centered and not banking into the good engine at all, and some instructors and examiners requiring things like OEI power on stalls! As a result, a lot of light twins spun into the ground with students, instructors, and examiners on board. The Twin Comanche was by far the most popular training twin at the time and took the blame. The FAA flight tests found nothing wrong with the airplane, but they raised the Vmc on the Twin Comanche from 80mph to 90mph. There's more on the history of the issue in general here: https://www.aopa.org/news-and-media...gazine/replace-multiengine-myths-with-reality
Capability
Performance: A basic normally aspirated Twinkie with no speed mods is usually going to be about a 160-knot bird. Really clean ones with some speed mods might hit 170. Turbo models can push 200 at altitude. Speed increase with the Miller (200hp) engine version is claimed to be 13% over the 160hp ones.
Load and range: Useful load is in the neighborhood of 1200* pounds, and standard fuel is 90 gallons without tip tanks and 120 gallons with; tip tanks also allow for an increased gross weight of 3725 provided the last 125 is fuel in the tips. Factory config lets you take about 650 pounds on about a 750-mile trip with reserves. Tip tanks allow for taking 750+ pounds on the 750-mile trip (leaving the aux tanks empty and fueling the tips instead), or 480 pounds on a 1,000+ mile leg. Filling the mains alone lets you take around 850 pounds for 450 nm. * Numbers are, of course, approximate and may vary significantly on more heavily modified birds.
Systems
Engines: The entire Twin Comanche line came from the factory with 160hp fuel injected Lycoming IO-320s, with the CR version having one LIO-320 and the turbo versions having a Rajay turbo bolted on. There were aftermarket 200hp IO-360s available for both the N/A and turbo versions, and these tend to get snapped up on the used market quite quickly.
Turbos: Turbo models came from the factory with tip tanks and oxygen systems, but the turbo was also offered as an aftermarket mod so there are a few turbonormalized airframes that don't have tip tanks or O2. The turbo system on models so equipped is pretty simple. It's a turbonormalizer with a manual wastegate. Thus, the engine maintains the same 8.5:1 compression ratio and is not any different from the normally aspirated version. In fact, you can run the turbo model as if it were normally aspirated by simply not closing the wastegates at all. The wastegate controls are a pair of vernier knobs under the throttle quadrant, normal operation is to leave the throttles wide open after takeoff and then slowly twist the wastegate controls in as you climb to maintain the desired manifold pressure; descending is done in the opposite order, with MP reduction starting with twisting the wastegate controls out until they're fully open (no boost) and then working the throttle as you would with a normally aspirated plane. This keeps the operation simple, and ensures that the turbos are very well cooled down prior to landing. Critical altitude is 20,000 feet, single engine ceiling is 19,000 feet and service ceiling with both engines is 30,000.
Fuel system: Standard from the factory, the Twin Comanche had a 90 gallon fuel system, 60 gallons in the mains and 30 in the wing aux tanks. 30 gallon tip tanks were standard on factory turbo models and optional on the normally aspirated ones. All of the factory tanks are direct-feed to the engines. Additional aftermarket tanks could consist of 38 gallon wet wing aux tanks (Miller), 40 gallon nacelle tanks (Phill-Air), and a 10 gallon tank that went in the bottom of the baggage compartment. It's also rare to see more than one aftermarket tank type fitted, as the Twinkie is quite efficient and burns around 16gph total, so even the factory tip tank setup is good for 7+ hours; adding the Miller or nacelle tanks gives you an endurance of around 10 hours! At least one airplane so fitted has crossed the Atlantic.
De-ice: This was available in a couple of ways, including an aftermarket system from Wiggins Airways that inflated boots with an on-board nitrogen tank! There were also more traditional de-ice boot systems available long ago, but none of them can be retrofitted now and there are only a handful of Twinkies left that are de-iced due to a very high cost to maintain the systems.
Well, I've wanted and loved the Twin Comanche for a much longer time - At least back to 2004 when AOPA's sweepstakes airplane was a Twin Comanche, but I liked them even before that. I am a fan of efficiency, and living next to a big ice bucket of a lake that has swallowed one airplane in my logbook, an efficient twin has been very high on my list for as long as I can remember, and when I started flying the Twinkie was probably the best. It's still the best of the affordable ones, the Tecnam P2006 and the Diamond DA42 are too new to really be in the affordable category just yet, with starting used prices for both still north of half a million dollars.
So, thinking about buying again and thinking about that other thread got me thinking that I should probably make another "brain dump" post with all of the knowledge I've collected on Twin Comanches over the past 25ish years, since I probably won't remember it all for another 25! Maybe Comanche expert @Kristin will fill in any gaps I leave here. As with the other thread, I'll update this first post with any new information. Also, in the course of verifying the information here I found a really well written, thorough article about the Twin Comanche by Tom Horne in the September 1980 issue of AOPA Pilot that's very much worth a read if you're really interested in the Twinkie.
The Basics
The Twin Comanche built on Piper's success with the single-engine Comanche line that started in 1958; the Twin Comanche was introduced in the latter half of 1963. The PA-30 "A" model (which was never so named, just the PA-30) was sold from 1963-65 and can be distinguished from the others by having only two side windows, it also had "four" seats with the two rear seats being a single bench seat. The PA-30B model was sold from 1966-68 and added the third side window and optionally two more seats (6 total) where the last two pretty much took up the baggage compartment and had little to no legroom, really they're kid seats. The PA-30C model was sold in 1969, gained a standard 6-pack panel layout instead of the earlier models' "shotgun" panel, and moved engine switches from the bottom row of the panel to the left-hand side and changed them to rocker switches. Finally, the PA-39 "C/R" was sold from 1970-72 and had counter-rotating props for extra safety. There were also turbonormalized models of the B, C, and 39/CR. On June 23rd, 1972, the remnants of Hurricane Agnes dumped up to 19 inches of rain in the area of the Piper factory in Lock Haven, PA and the adjacent Susquehanna River crested at over 31 feet, destroying and sweeping away airframes, parts, and tooling from the Comanche lines. Piper made the decision to continue producing the Arrow and Seneca in Vero Beach and end production of the entire Comanche line, a sad day in aviation history.
One other historical note on the Twin Comanche series: At the time they were being produced, the FAA required multi checkrides to do a Vmc demo at as low an altitude as possible to maximize thrust on the remaining engine as well as some other foolishness like keeping the ball centered and not banking into the good engine at all, and some instructors and examiners requiring things like OEI power on stalls! As a result, a lot of light twins spun into the ground with students, instructors, and examiners on board. The Twin Comanche was by far the most popular training twin at the time and took the blame. The FAA flight tests found nothing wrong with the airplane, but they raised the Vmc on the Twin Comanche from 80mph to 90mph. There's more on the history of the issue in general here: https://www.aopa.org/news-and-media...gazine/replace-multiengine-myths-with-reality
Capability
Performance: A basic normally aspirated Twinkie with no speed mods is usually going to be about a 160-knot bird. Really clean ones with some speed mods might hit 170. Turbo models can push 200 at altitude. Speed increase with the Miller (200hp) engine version is claimed to be 13% over the 160hp ones.
Load and range: Useful load is in the neighborhood of 1200* pounds, and standard fuel is 90 gallons without tip tanks and 120 gallons with; tip tanks also allow for an increased gross weight of 3725 provided the last 125 is fuel in the tips. Factory config lets you take about 650 pounds on about a 750-mile trip with reserves. Tip tanks allow for taking 750+ pounds on the 750-mile trip (leaving the aux tanks empty and fueling the tips instead), or 480 pounds on a 1,000+ mile leg. Filling the mains alone lets you take around 850 pounds for 450 nm. * Numbers are, of course, approximate and may vary significantly on more heavily modified birds.
Systems
Engines: The entire Twin Comanche line came from the factory with 160hp fuel injected Lycoming IO-320s, with the CR version having one LIO-320 and the turbo versions having a Rajay turbo bolted on. There were aftermarket 200hp IO-360s available for both the N/A and turbo versions, and these tend to get snapped up on the used market quite quickly.
Turbos: Turbo models came from the factory with tip tanks and oxygen systems, but the turbo was also offered as an aftermarket mod so there are a few turbonormalized airframes that don't have tip tanks or O2. The turbo system on models so equipped is pretty simple. It's a turbonormalizer with a manual wastegate. Thus, the engine maintains the same 8.5:1 compression ratio and is not any different from the normally aspirated version. In fact, you can run the turbo model as if it were normally aspirated by simply not closing the wastegates at all. The wastegate controls are a pair of vernier knobs under the throttle quadrant, normal operation is to leave the throttles wide open after takeoff and then slowly twist the wastegate controls in as you climb to maintain the desired manifold pressure; descending is done in the opposite order, with MP reduction starting with twisting the wastegate controls out until they're fully open (no boost) and then working the throttle as you would with a normally aspirated plane. This keeps the operation simple, and ensures that the turbos are very well cooled down prior to landing. Critical altitude is 20,000 feet, single engine ceiling is 19,000 feet and service ceiling with both engines is 30,000.
Fuel system: Standard from the factory, the Twin Comanche had a 90 gallon fuel system, 60 gallons in the mains and 30 in the wing aux tanks. 30 gallon tip tanks were standard on factory turbo models and optional on the normally aspirated ones. All of the factory tanks are direct-feed to the engines. Additional aftermarket tanks could consist of 38 gallon wet wing aux tanks (Miller), 40 gallon nacelle tanks (Phill-Air), and a 10 gallon tank that went in the bottom of the baggage compartment. It's also rare to see more than one aftermarket tank type fitted, as the Twinkie is quite efficient and burns around 16gph total, so even the factory tip tank setup is good for 7+ hours; adding the Miller or nacelle tanks gives you an endurance of around 10 hours! At least one airplane so fitted has crossed the Atlantic.
De-ice: This was available in a couple of ways, including an aftermarket system from Wiggins Airways that inflated boots with an on-board nitrogen tank! There were also more traditional de-ice boot systems available long ago, but none of them can be retrofitted now and there are only a handful of Twinkies left that are de-iced due to a very high cost to maintain the systems.



