TBM Debuts the 960 at Sun N Fun

Lightspeed Tango Headset

ByHank Gibson March 29, 2016June 2, 2016

I recently purchased the new, wireless, Lightspeed Tango headset.  I’m a little OCD, so when a headset wire is banging against my shoulder while I’m trying to tune a radio or point something out, it’s a little annoying. A headset without the wires caught my eye.

As I’ve stated before in a previous article, I really like Lightspeed headsets.  They are more comfortable than Bose, and a little bit more affordable too.  The noise canceling quality is very high in the different Lightspeed models.  I personally believe it got even better with the Lightspeed Tango.

Let’s talk about the obvious first.  Not having a wire connecting you to the headset jacks is really nice.  You’re not tethered to anything, so your head is free to move anywhere without getting yanked back in place. Lightspeed developed a new technology, called Lightspeed Link, which bypasses Bluetooth or Wifi and connects the Panel Interface to the headset wirelessly.

The Link technology works pretty well.  The only problem I have noticed is in certain airplanes, I occasionally lose one ear, but after I wiggle the input wires around, the deaf ear comes back up.  It may be a loose connector in the plane itself.

The really nice thing about the Lightspeed Tango is the fact that it doesn’t need AA batteries anymore. Lightspeed put rechargeable lithium ion batteries in both the Panel Interface and the headset.  You get 12 hours of battery life out of both, far surpassing any length of time you would want to be in an airplane.  If the battery dies, there is a handy aux cable that can connect the Panel Interface directly to the headset (the ion batteries recharge with the included wall charger and USB cables in 2 hours).

Though the Lightspeed Tango is slightly heavier than the Zulu 2 due to the Link hardware and the lithium ion battery, it is still extremely comfortable.  The ear cups actually fit better over my ears and give me a better seal with glasses on then the Zulu 2 did.  As with all Lightspeed products, there is no squeezing of my head and the cushions on top of the headset sit very comfortably on top of my head.

The Bluetooth is much simpler to use than the Zulu 2 and definitely simpler than the Bose A20.  Sound quality is very good for phone calls and music.  The volume control on the headset itself is set to make smaller adjustments so you don’t have to deal with wide swings in volume.

Overall, I’m a big fan of the Lightspeed Tango.  I am recommending them to all the pilots I talk to.  Rolling in at $400 cheaper than the Bose, you can’t go wrong.

Cirrus CAPS Pull in Arkansas

ByHank Gibson December 9, 2015December 21, 2015

Cirrus CAPS pull #55 took place at the beginning of November over Fayatteville, AR.  From initial reports, it appears a clamp broke on the oil cooler, causing a loss of oil pressure.  It does not appear that the engine immediately quit, but an annunciator alerted the pilot that the engine was losing oil pressure.  At this point, it appears the pilot elected to do an emergency descent to an airport below him, but ended up not timing it right, missing the airport and pulling the parachute.

As an experienced Cirrus flight instructor, there appears to be some suspect decision making in handling this operation.  I teach in a Cirrus that if an oil light comes on, given that a pilot has some altitude to work with, it is a better option to physically shut the engine down, leaving control of the situation in the pilot’s hands.  This way, the pilot knows when the engine is stopping and is prepared for it, instead of the engine acting erratically and causing problems on the descent.

After checking the engine gauges and shutting the engine down, a pilot should establish best glide first, not nose down and descend at a high rate trying to make an airport.  Best glide gives the pilot many more options and a lot more altitude to work with, further allowing him/her to plan how to make an airport directly underneath the airplane.

To pontificate, it seems that if the pilot had adjusted the plane to best glide, instead of performing an emergency descent, there is the possibility that Drake Field would have been reachable, the chute would not have been needed, and the driver of the truck would not have had to visit the hospital.  Hindsight is 20-20, but this may be an overall training and decision making issue that may need further emphasis.

The initial NTSB report as well as a link to the CBS story is below.

http://www.cbsnews.com/live/video/pilot-forced-to-deploy-emergency-parachute-in-arkansas/

NTSB Identification: CEN16LA026
14 CFR Part 91: General Aviation
Accident occurred Tuesday, November 03, 2015 in Fayetteville, AR
Aircraft: CIRRUS DESIGN CORP SR22T, registration: N857SW
Injuries: 3 Minor, 1 Uninjured.
This is preliminary information, subject to change, and may contain errors. Any errors in this report will be corrected when the final report has been completed. NTSB investigators may not have traveled in support of this investigation and used data provided by various sources to prepare this aircraft accident report.
On November 3, 2015, at 0950 central standard time, a Cirrus SR22T airplane, N857SW, descended under the canopy of the cirrus airframe parachute system (CAPS) and landed on a road in Fayetteville, Arkansas. The pilot, pilot rated passenger and one person on the ground received minor injuries. One passenger in the back right seat was uninjured. The airplane was substantially damaged. The airplane was registered to WG Aviation LLC, Rogers, Arkansas, and operated by a private individual under the provisions of 14 Code of Federal Regulations Part 91 as a personal flight. Visual meteorological conditions prevailed at the time of the accident and an instrument flight rules (IFR) flight plan was filed. The flight departed from the Bentonville Municipal Airport (VBT), Bentonville, Arkansas, at 0934 and was en route to the Waco Regional Airport (ACT), Waco, Texas.

According to the pilot, after departure from ACT he leveled off around 10,000 ft mean sea level (MSL) and was in “VFR on top” conditions. The pilot noticed that the crew alerting system (CAS) flashed a yellow caution light for oil pressure; the engine was still producing power. The pilot notified air traffic control (ATC) of the issue and received vectors to the nearest airport, Drake Field Airport (FYV), Fayetteville, Arkansas. The pilot descended and maneuvered toward FYV as the CAS indicated a red warning light for oil pressure, which had dropped below 10 psi. The engine was producing inconsistent power as the airplane descended to 3,300 ft and FYV was still not in sight due to cloud coverage. The pilot was unable to maintain altitude and the airplane’s stall warning horned sounded. The pilot deployed the Cirrus airframe parachute system (CAPS) and descended to the ground. During the landing the airplane collided with a truck and then came to rest on a four lane road.

At 0953, the weather observation at FYV reported wind from 190 at 9 knots, gusting to 17 knots, 10 miles visibility, clear sky, temperature 61° F, dew point 57° F, and altimeter setting 30.11 inches of mercury.

An initial postaccident examination was conducted on November 4, 2015, in Fayetteville. Engine oil was observed on the underside of the fuselage. The oil cooler cross fitting was broken and oil was observed in the engine compartment.

The airplane’s recoverable data module and three data cards were removed and sent to the NTSB Vehicle Recorders Laboratory for download.

The airplane has been retained for further examination.

ViBAN IFR Hood

ByHank Gibson February 8, 2017

The first task I give my new instrument students before we start training is to find a view limiting device that they like.  There’s the hood that everyone hates (which has been used since the beginning of instrument training,though it isn’t that uncomfortable) or foggles, which usually end up becoming very uncomfortable very quickly.  The headset ends up pressing the sides of the foggles into the side of your head, leaving lumps and scars that hurt for days.

Well, there is finally another solution that combines the hood and foggles.  Meet the ViBAN.

ViBAN brags that it is the most comfortable IFR view limiting device out there.  I have a customer who has one and he loves it.  It’s easy to put reading glasses on underneath while still blocking the view of the exterior of the plane.  It doesn’t leave bruises against the side of your head, either.

If you’re looking for something different for your IFR training, give ViBAN a try.

Mooney Enters the Training Market with the Mooney M10

ByHank Gibson November 19, 2014December 5, 2014

Earlier this week, Mooney announced they would be following competitors Piper (with their Archer DX) and Redbird (with their retrofitted 172 known as the Redhawk) into the training market with the Mooney M10 T and Mooney M10 J.  Mooney, which hasn’t manufactured a primary trainer since the Mooney M10 Cadet in 1970, is planning on putting Jet A burning Continental Engines in the new aircraft.  The mockup was unveiled at Airshow China.

The Mooney M10 T is a 3 seat, fixed gear trainer sporting a Continental CD-135 engine.  At 135 HP, the initial design data claims the Mooney M10 T will be able to cruise at 140 KTAS at 75% power, allowing the Jet A engine to burn between 4-5 gallons per hour while holding 42 gallons of fuel.  As with other Jet A piston powered airplanes, the Mooney M10 T will have a Fully Automated Digital Engine Control (or FADEC) system.  This leaves just a single power lever in the cockpit, allowing the pilot to set a percent power and the FADEC computer will set the manifold pressure, prop speed, and mixture.

The Mooney M10 J has a slightly bigger engine, the 155 HP Continental CD-155.  It also is equipped with retractable gear.  Initially, Mooney is predicting 160 KTAS at 75% power for the Mooney  M10 J.  The airplane will come as a two-seater, but will have a third seat as an option.  Mooney says that the Mooney M10 J will allow pilots to make an easy transition to the bigger and faster M20J that has been popular for many years amongst “Mooniacs.”

In a new direction for Mooney, the Mooney M10 T Mooney M10 J will both be composite airplanes with side sticks, instead of the traditional sheet metal exterior with a yoke as Mooney aircraft have been in the past. Also venturing from the more powerful Mooney aircraft is the fact that the Mooney M10 T and Mooney M10 J will have two doors.  Remaining, though, is the swept tail that Mooney aircraft are known for.  Both airplanes will be equipped with Garmin G1000 panels, while the Mooney M10 J will also have the GFC 700 autopilot, marketing more toward aircraft owners rather than students.

The only downside that I read about was the time between replacements for the engines.  For the CD-135 engine in the Mooney M10 T, time between replacement is 1,500 hours, whereas the CD-155 only has a 1,200 hour replacement time.

Mooney expects certification and deliveries to begin for the Mooney M10 T and Mooney M10 J in 2017.

Information courtesy of AOPA and Mooney International.  Images courtesy of Mooney International.

After Market Ice Protection

ByHank Gibson December 16, 2017December 23, 2017

It’s winter time, so that means winter weather for the aviation community.  For single engine piston pilots, that means dealing with icing conditions.  For us Texan flyers, ice only presents an issue for maybe a week out of the year (the exception being for those Panhandle residents!), but it’s nice to have some protection.

Most single engine pistons do not come with ice protection from the factory and, of those that do, most are not Flight Into Known Icing (FIKI) approved.  The systems are “get out of jail” systems that can reduce the amount of ice you pick up if you accidentally get into icing conditions and you are on your way out.  The Cirrus SR22 line of aircraft has had the TKS system option since 2006, with the new FIKI system being available since 2010.  The Cessna TTx has a FIKI option that was debuted in 2014.

The above mentioned airplanes use TKS systems.  There are a handful of single engine pistons that use boots that are FIKI certified:  the Piper PA46 line (Malibu, Mirage, and Matrix) and the Cessna P210 and T210 line (though not all are equipped with boots).

If you find yourself flying into wintry conditions often and want some protection for your clean wing airplane, there are some aftermarket options for a lot of airplanes now.  Do note that all these systems do come with a pretty hefty price tag, but can be worth it if you fly into icing a good bit.

CAV Ice Protection TKS Systems

CAV Ice Protection is a TKS system outfitter.  What is TKS fluid?  According to Flying Magazine:

“TKS systems dispense an ethylene glycol-based fluid with a freezing point below minus 70 degrees F through porous titanium panels attached to the leading edge of the wing and empennage. The fluid is released through thousands of the panels’ laser-drilled holes, which are not much larger than the size of a human hair. As air flows over the wing and empennage, it disperses the fluid, coating the surfaces, and preventing the formation and adherence of ice.”

The advantages of a TKS system are the whole entire wing gets coated to get rid of any extra ice that adheres to the top or bottom of the wing surface.  The disadvantage is there is only a finite amount of fluid, so when it runs out, you don’t have any more protection.  The fluid also adds extra weight agains the useful load of the airplane.

CAV Offers a Basic TKS system for the following single engine piston aircraft:

• Beech Bonanza
• Cessna 182, 206, 210, 350, & 400
• Columbia 350 & 400
• Piper PA32
• Mooney M20

CAV Offers a full FIKI System for the following single engine piston aircraft:

• Beech A36 & G36 Bonanza, and Baron
• Cessna 210 & TTx
• Commander 114
• Mooney M20

For more information, check out CAV Ice Protection’s Website.

Ice Shield De-Icing Boots

Ice Shield is another after market de-ice option.  Ice Shield makes boots for wing leading edges.  The advantage of boots is they activate instantaneously, getting rid of ice where it builds up first, on the wing leading edge.  No running out of fluid and only the added weight of the system.  Ice Shield also offers heated windscreens for several the Piper Saratoga line and the A36, B36, and G36 Bonanza line.

Ice Shield has boots for the following single engine piston aircraft:

• Beech Bonanza F33A and -36 line
• Cessna 210 line
• Piper Pa46 line

For more information, check out Ice Shield’s Website.

Pitch + Power = Performance

ByHank Gibson October 10, 2016October 17, 2016

My first chief flight instructor had an addage he would impart to his flight instructors when we began working at that flight school. “Pitch + Power = Performance” he would tell us. Then he’d glare at us and follow up with, “nobody teaches that right, so make sure your students know it.”

Now, having been a CFI for seven years, I would tend to agree with him. I have moved on from doing mostly primary training to transition training. Transition training is taking someone who is already a pilot and teaching them how to fly a different type of airplane. In jets, you get a type rating. In piston engine airplanes, there is no FAA requirement to go through any type of extra training as long as you are rated in category and class (eg. single engine piston). But, insurance companies know that Mr. Fresh Private Pilot can’t just hop from a Cessna 172 into a Cirrus SR22 or a Bonanza, so they require transition training before insuring those pilots.

What did my chief instructor mean when he imparted his wisdom? He was speaking about a particular phase of flight, the final approach phase, regardless of whether it’s a VFR approach or an IFR approach. The pitch of the airplane and the power setting of the airplane have to be utilized together to achieve the proper speed and descent rate (performance).

VFR

On the final approach leg of a VFR pattern, most piston engine aircraft are configured with landing gear down and flaps down in the landing position. This puts the airplane on the back side of the power curve in the region of reverse command. In the region of positive command, in cruise, for example, the more power you add, the faster you are going to go and, if you pitch up, you will go up and you pitch down, you will go down. But, they work together (if you point the nose down, you will accelerate unless you reduce the power); remember, Pitch + Power = Performance.

In the region of reverse command, the pitch controls the airspeed and the power controls your rate of descent, but, again, they work together. Let’s say the airplane is 5 knots above it’s approach speed on final. Initially, the pilot will need to pitch up slightly to bleed off that airspeed. The airplane will want to climb, so as he is pitching up, he’ll need to make a slight power reduction to stay on glide slope.

Alternatively, let’s say the airplane is high, but is on speed. The pilot will make a power reduction to descend to the glide path, but he’ll also need to pitch down to maintain the proper airspeed.

What you don’t want to do is this: if the airplane is high on final, don’t push the nose down to try and get down. This does cause the airplane to lose altitude quickly, but the airspeed increases quickly. With a higher airspeed, the airplane has a lot more energy to dissipate when it gets to the runway, meaning you’ll float longer which can lead to forcing the airplane down or using up too much runway and not being able to get the airplane stopped in time.

IFR

On an instrument approach, you are on the front side of the power curve. When trying to stay on glide slope, the power is controlling the speed of the airplane and the pitch is keeping the airplane on glide slope. This can be a little bit confusing for VFR pilots transitioning to instrument approaches as they are not used to being on the front side of the power curve.

Keeping in mind that Pitch + Power = Performance, let’s put the airplane above the glide slope on an ILS approach. In order to get down to the glide slope, the pitch needs to be lowered as much as needed (it’s always better to pick a pitch attitude to fly and see if it is working to bring the glide slope back to center. If it doesn’t work, pick a new one. Don’t just push the nose down until the glide slope moves) and the power needs to be reduced to maintain airspeed (again, pick a specific power setting). Once the glide slope centers, then the pitch will be raised slightly and the power will need to be increased to hold glide slope and speed respectively.