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Piper M350 · Weight And Balance

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Overview

This document is a flight test report for the Piper M350, a pressurized single-engine piston aircraft. It provides an in-depth look at the aircraft's performance, features, and handling characteristics. The report is intended for pilots and aviation enthusiasts, detailing the M350's specifications, operational capabilities, and unique attributes compared to other aircraft in its class. Key highlights include the aircraft's engine performance, cruising capabilities, and safety features, making it a suitable option for both business and leisure travel.

  • Basic empty weight: 3,150 lbs (1,429 kg)
  • Maximum takeoff weight: 4,340 lbs (1,969 kg)
  • Fuel capacity: 120 US gallons (454 liters)
  • Maximum cruising speed: 213 KTAS (395 km/h)
  • Range: 1,343 nautical miles (2,487 km) with 45 minutes reserve
  • Takeoff distance over 50 ft obstacle: 2,090 ft (637 m)
  • Service ceiling: 25,000 ft (7,620 m)

Document

Source

Originally published by www.kcac.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
Weight And Balance
Year
2017
Pages
6
File size
1.0 MB
Publisher
www.kcac.com

Specifications & performance

Extracted from this document.

Specifications

Range (nm)
1,343
Engine (hp)
350
Height (ft)
11.4
Length (ft)
28.11
Propeller
Hartzell constant speed
Wingspan (ft)
43
Engine model
Lycoming TIO-540-AE2A
Max speed (kt)
213
Cruise speed (kt)
190
Empty weight (lb)
3,150
Fuel capacity (gal)
120
Rate of climb (fpm)
1,000
Service ceiling (ft)
25,000
Max takeoff weight (lb)
4,340

Performance

Fuel burn (gph)
24.1
Landing over 50ft
1,968
Takeoff over 50ft
2,090
Landing distance (ft)
1,968
Takeoff distance (ft)
2,090
Stall speed clean (kt)
63

V-speeds

VR
85
VY
120
VNE
198
VSO
63
VREF
85

Weight & balance

Useful load (lb)
1,190
Basic empty weight (lb)
3,150
Max takeoff weight (lb)
4,340
Documentation completeness
4/7

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In this document

Aircraft Overview

The Piper M350 is a pressurized single-engine piston aircraft, derived from the PA-46 Malibu lineage. It features a 350 HP Lycoming TIO-540-AE2A engine and a three-blade Hartzell constant speed propeller. The M350 is designed for comfort and efficiency, with a maximum takeoff weight of 4,340 pounds and a range of 1,343 nautical miles.

Performance Specifications

The M350 has a maximum cruising speed of 213 KTAS and a service ceiling of 25,000 feet. It can achieve a takeoff distance of 2,090 feet over a 50-foot obstacle and a landing distance of 1,968 feet over the same obstacle. The aircraft's fuel capacity is 120 US gallons, providing flexibility in range and payload.

Cockpit and Avionics

Equipped with the Garmin G1000 avionics suite, the M350 includes dual primary flight displays and a multifunction display. It features advanced flight envelope protection and a hypoxia recognition system, enhancing safety and ease of operation for pilots.

Handling Characteristics

The M350 exhibits responsive handling qualities, with a smooth autopilot disengagement and effective control surfaces. The aircraft is designed for ease of operation, making it suitable for pilots with varying experience levels.

Safety Features

The M350 includes several safety features such as Electronic Stability Protection and a Coupled Go-Around Mode, which simplifies the go-around procedure. The pressurized cabin allows for comfortable cruising at higher altitudes without the need for supplemental oxygen.

Safety notes

  • Ensure proper weight and balance calculations before flight.
  • Monitor cabin pressure differential to avoid hypoxia.
  • Follow recommended procedures for go-arounds and descents.

Full document text

74 SKIES Magazine | March/April 2017 flight test / Piper M350 obility is a highly prized commodity for some busy people, both in business and in leisure. If you’re a pilot “on the go,” Piper Aircraft’s M350 pressurized piston- powered single-engine airplane may be a solution. Aviation Unlimited, Piper’s Canadian sales dis- tributor, brought a brand new demonstrator air- craft, registration C-GBTB, to Ottawa on a sunny autumn day. Isaac Capua and Conrad Hatcher flew the airplane from Aviation Unlimited’s base at Oshawa Airport. As it happened, their arrival for our flight proved a good test of the airplane, as the Ottawa airport was under a blanket of fog. It was encouraging indeed to see, or rather hear, the aircraft complete a tough instrument approach and taxi out of the mist for our meeting. The M350 is the latest development of what was originally Piper’s popular PA-46 Malibu; a design introduced in 1983 which ushered in the age of the cabin-class single. The original Continental engine- powered, 310 horsepower (HP) Malibu suffered a number of high-profile engine failures, so Piper rebooted the design with the 350 HP Lycoming- powered Mirage in 1989. The concept for the M PiPer’s M350 fares well against the coMPetition, occuPying its unique niche as the only new Pressurized Piston- engine aircraft on the Market. By RoBeRt eRdos cruiser Pressurized Piston flight test / Piper M350 74 SKIES Magazine | March/April 2017 SKIES Magazine | March/April 2017 75 SKIES Magazine | March/April 2017 75 The M350 is the latest iteration in Piper’s successful PA-46 model line. Jim Barret/Piper Aircraft Photo Download this as a wallpaper here! Watch the video here! 76 SKIES Magazine | March/April 2017 flight test / Piper M350 Important for the owner-pilot, the M350 has ramp appeal. Peter Handley Photos The PA-46 ushered in the age of the cabin-class single. The Garmin G1000 avionics suite incorporates impressive flight envelope protection features. There are six seats and room for baggage in what Rob Erdos dubs a “serious travelling machine.” SKIES Magazine | March/April 2017 77 turboprop-powered Meridian was introduced in 1997, featuring a 500 HP Pratt & Whitney Canada PT6A-42A turboprop engine. In recent years, Piper has invested heav- ily in its M-Class models, which include the M500 and M600 turboprops, developed from the Meridian, and the M350 piston derivative of the Mirage. The M350 was introduced in 2015, certified as the PA-46- 350P, and powered by a dual-turbocharged, fuel-injected 350 HP Lycoming TIO-540- AE2A engine driving a three-blade Hartzell constant speed propeller. The Matrix is the unpressurized version of the M350. Meet the M-ClAss I was pleasantly surprised by the fit and finish of the airplane, perhaps having been biased by so many forlorn old Piper trainers that I’ve seen parked behind flying clubs. Not so the M350, which looked solid and robust. To my eye, it was swoopy and attractive on the ramp; not a trivial impression for what is almost entirely an owner-flown design. The pre-flight inspection revealed an airplane that was thoroughly modern and well-conceived. The exterior lights are all light emitting diodes (LED) for improved service life. A small storage compartment in the under-wing radome and another in the tail provide convenient externally- accessible storage for light items. Capua extolled the merits of the M350’s optional pneumatic deicing system over competing fluid-based systems. Cabin access is quite dignified for a light airplane, with entry via a two-part clamshell door and stairs. I settled into the left seat. Hatcher was my adult supervision in the right seat. The cockpit seats were thoroughly adjustable, and after some fiddling I found it quite comfortable. The headroom was the only disappointment— even for my quite average 5’9” frame, my headset just touched the cabin roof. Hatcher mentioned that a seat modification kit is available to allow up to three more inches of headroom, if one desires. I would. Our demonstrator aircraft had a basic empty weight of 3,150 pounds, which, thanks to its generous optional equipment, was 100 pounds over the published standard equipped weight. Adding two pilots, one human and some gear brought the zero fuel weight to 3,730 pounds. The fuel gauges indicated 76 gallons, or about two-thirds fuel quantity, bringing the gross takeoff weight to 4,186 pounds. That left us 154 pounds below the maximum takeoff weight of 4,340 pounds. Clearly you cannot fill the seats and fill the tanks, but with a published maximum range of 1,343 nautical miles (plus reserve), the 720 pound (120 US gallon) maximum fuel load provides considerable flexibility to trade range for payload. The pre-flight inspection revealed solid construction and quality workmanship. “WheRe tO, BOYs?” We obtained a clearance for a round- robin flight to Kingston, Ont. The start procedure was straightforward for a fuel- injected engine. Nosewheel steering was a bit stiff, with light centering forces, but I quickly made friends with it. The earlier fog had cleared, and we departed Ottawa’s Runway 07 under a clear blue sky with light winds. Normal takeoffs are performed with 10 degrees of flaps, using a rotation speed of 85 knots indicated airspeed (KIAS). Engaging the Coupled Go-Around feature on the ground preset the flight director for a wings-level, seven degree pitch attitude. Assuming maximum takeoff weight, the published takeoff distance over a 50-foot obstacle was a respectable 2,090 feet. Hatcher recommended a 120 KIAS cruise-climb airspeed, which resulted in just over a 1,000 feet per minute rate of climb. Thanks to the turbocharger, one can expect the M350 to maintain its climb performance to nearly cruise altitude. COMfORtABle CRUiseR We levelled off at 14,000 feet under ISA+12 degree Celsius conditions and set High Speed Cruise power: 32.0 inches manifold pressure; 2,470 RPM; with the mixture leaned to 1,560F turbine inlet

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temperature. The result was 190 knots true airspeed (KTAS) sipping 24.1 gallons per hour fuel flow. Piper quotes a maximum cruising speed of 213 KTAS, but that would occur at the airplane’s 25,000 foot certified ceiling. Hatcher described “the mid-teens” as good cruising altitudes for the M350. I mused that it was a pleasant novelty to be so high in a piston single-engine airplane with a cabin altitude of only 1,620 feet, owing to the 5.5 pounds per square inch maximum cabin pressure differential. If that appeals, then your airplane search narrows to the M350, since it’s the only pressurized pis- ton-engine aircraft currently in production. Hatcher agreed, offering that buyers are often attracted to the pressurization for their passengers’ comfort, as it affords higher, smoother cruise altitudes without need of an oxygen mask. “It trumps the parachute,” Capua added, in reference to the ballistic recovery chute in the competing Cirrus. The M350 can maintain sea level cabin pressure to 12,000 feet. The cockpit environment in cruise left little to be desired. Owing to the pressur- ization, air conditioning is standard equip- ment. Heating and ventilation seemed quite adequate. Under my noise cancelling head- set, the big Lycoming purred contentedly. With Garmin’s GFC 700 autopilot smooth- ly doing the steering, I idly poked my finger into the pulse oximeter on the instrument panel, and was rewarded with the knowl- edge that I had 98 per cent blood oxygen saturation. Oh, I apparently also had a pulse of 69 beats per minute. Reassuring. In the event that I wasn’t adequately pressurized with oxygen, a hypoxia recognition system would detect the absence of pilot interaction with the avionics and commence an automated descent to a safer altitude. The now nearly ubiquitous Garmin G1000 avionics suite includes dual 10.4-inch primary flight displays and one 12.1-inch multifunc- tion display—and a whole lot of capability. Standard equipment in the M350 includes synthetic vision and a yaw damper. I took a stab at loading the RNAV RWY 19 instru- ment approach in Kingston, stumbling slightly due to my unfamiliarity. Hatcher, coming to my rescue, noted that computer- savvy pilots seem to expect to understand the complex G1000 immediately, musing that, “If you recall fixed-card ADF approaches, I’m surprised that pilots expect to master the G1000 in an hour.” Fair enough. From there, the avionics simply steered us through the procedure and delivered us at the missed approach point. I just monitored our progress through the synthetic vision system, and was left to manage configuration and power. 78 SKIES Magazine | March/April 2017 flight test / Piper M350 Hope Aero Propeller & Components Inc. 7605 Bath Road, Mississauga, ON L4T 3T1 Canada t | 905-677-8747 or 800-268-9900 f | 905-677-5935 goodtogo@hopeaero.com | HOPEAERO.COM CusTOMeR dRiveN, CusTOMized seRviCe sOLuTiONs. OuR wORk is dONe CORReCTLy The fiRsT TiMe, eveRy TiMe. CONTiNuOus fLOw pROduCTiON fOR eveN fasTeR TuRN TiMes. R408 photo faMiLy-OwNed siNCe 1969, wORLd-CLass faCiLiTy HOPE AERO PROPELLERS WHEELS & BRAKES NDT SERVICES DYNAMIC BALANCING 80 SKIES Magazine | March/April 2017 flight test / Piper M350 Commencing the missed approach is typically a high-workload moment requiring disengagement of the autopilot, but the M350’s Coupled Go-Around Mode made it push-button simple. In concert with the Underspeed Protection System, the autopilot remains engaged and protects against excessively low speed while the pilot applies power and cleans up the flaps and undercarriage. hANDliNg, APPROACh AND lANDiNg En route back to Ottawa, I took the opportunity to sample the M350’s handling qualities. Autopilot disengagements were smooth, typically leaving the airplane in trim. The controls were pleasant, responsive and tight, and would present no undue challenges for a minimally experienced pilot. I found configuration changes transparent, requiring only small trim corrections. Having extended the undercarriage and full flaps, I sampled a few very benign stalls. At our operating weight, the low- speed audio warning activated at 63 KIAS, with only a small and easily corrected left wing drop at 59 KIAS. The Electronic Stability Protection system provides additional flight envelope protection from roll upsets while hand- flying by automatically engaging servos to input corrective forces should the pilot encroach upon safe limits. A further neat Garmin innovation is the big, blue “LVL” (level) button on the instru- ment panel, which serves as a sort of panic button to quickly return the aircraft to a wings-level attitude with zero vertical speed. Aircraft owner-pilots rarely fly as much as they would like, and maintaining proficiency is often a challenge. The comprehensive safety features in the M350 go a long way to matching the aircraft to its target demographic. If my opinion on these safety features isn’t clear: “Yay, Piper!” Returning to Ottawa it was quickly time for descent, which is usually a limitation of tur- bocharged aircraft, as power reductions need to be performed very slowly to avoid shock- cooling the expensive parts. I was pleased to see that the M350 could achieve better than a 2,000 foot-per-minute rate of descent without reducing power, thanks to the combination of wing-mounted speed brakes and the rela- tively high maximum airspeed (Vne) of 198 KIAS. Likewise, the generous undercarriage and approach flap (10 degrees) extension speed of 165 KIAS help the M350 to slow down when the airport appears. Far too soon we were landing back on Ottawa’s Runway 07, using full flaps and an approach speed (Vref) of 85 KIAS. Turning onto the taxiway, I noticed that I was smil- ing. That’s the best endorsement that I can imagine for an owner-flown airplane design. the eNVelOPe, PleAse It is heartening to report that there are once again a number of single-engine airplanes on the market. Options include four- to six-place designs, piston and turboprop models, high- and low-wings, with fixed and retractable undercarriage. The market hasn’t been so well served since the 1980s, although today’s airplanes are far better in every regard. Piper’s new M350 fares well against the competition, occupying its unique niche as the only pressurized six- place single-engine piston aircraft. The M350 is a light airplane, but it’s also a serious travelling machine. Armed with the G1000’s impressive capabilities, weather radar and certification for flight into known icing, the result is a virtually “go anywhere any time” airplane for pilots on the go. Mobility problem solved. Robert Erdos is a contributing editor for Skies magazine. He is a graduate of the U.S. Naval Test Pilot School and a professional test pilot. Also an aviation enthusiast, his spare time activities include displaying vintage airplanes and flying his RV-6 kitplane. 120 US gal 454 litres Usable fuel capacity Hartzell constant speed propeller Lycoming TIO-540-AE2A, 350 hp Engine 4,340 lbs 1,969 kg Max. takeoff weight 5.6 psid Max. cabin differential 213 ktas 395 km/h Max. cruising speed 1,343 nm 2,487 km Range with 45 minutes reserve 2,090 ft 637 m Takeoff distance (over 50 ft obstacle) 1,968 ft 600 m Landing distance (over 50 ft obstacle) 25,000 ft 7,620 m Max. approved altitude wingspan: 43 ft (13.1 m) height: 11.4 ft (3.4 m) length: 28.11 ft (8.6 m) Jim Barret/Piper Aircraft Photo