HK36 Super Dimona - fact sheet

Diamond HK36 Super Dimona · Weight And Balance

Free account — keep the POHs & checklists you reference in one place.

Overview

This document is a fact sheet for the Diamond HK36 Super Dimona, detailing its specifications, performance metrics, and operational capabilities. It is intended for pilots, aviation enthusiasts, and anyone interested in the technical aspects of this aircraft model. The fact sheet provides essential information such as engine types, performance figures, dimensions, and weight limits, which are crucial for flight planning and operational safety.

Max cruise speed: 190 km/h TAS (TC 100), 222 km/h TAS (TTC 115)
Stall speed: 81 km/h CAS (airbrakes extended), 78 km/h CAS (airbrakes retracted)
Rate of climb: 4.9 m/s (TC 100), 5.4 m/s (TTC 115)
Empty weight: 560 kg (TC 100), 568 kg (TTC 115)
Max take-off mass: 770 kg for both models
Fuel capacity: 55 lt (standard), 79 lt (long range)
Max operating altitude: 5,000 m

Document

Source

Originally published by mfgo.ch. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

View original at mfgo.ch

Report a problem or request removal

Document details

Type: Weight And Balance
Year: 2011
Pages: 2
File size: 717 KB
Publisher: mfgo.ch

Documentation completeness

5/7

Most owners only have the POH. Here's the essential set for the Diamond HK36 Super Dimona.

More Diamond HK36 Super Dimonamanuals & documents

In this document

Power Plant

The HK36 Super Dimona is powered by either the Bombardier Rotax 912 S3 engine, producing 100 hp, or the Bombardier Rotax 914 F3 engine, producing 115 hp. Both engines are paired with an MT propeller MTV-21-A-C-F/CF 175-05, which is a 2-blade hydraulic constant speed propeller with a hydro pneumatic feathered pitch.

Performance and Consumption

The maximum cruise speed at 1,800 meters is 190 km/h TAS for the TC 100 and 222 km/h TAS for the TTC 115. The stall speed with airbrakes extended is 81 km/h CAS, and with airbrakes retracted, it is 78 km/h CAS. The rate of climb at ISA sea level is 4.9 m/s for the TC 100 and 5.4 m/s for the TTC 115.

Dimensions and Weight

The HK36 Super Dimona has a length of 7.28 m, a height of 1.90 m, and a wingspan of 16.33 m. It seats two people, with an empty weight of 560 kg for the TC 100 and 568 kg for the TTC 115. The maximum take-off mass (MTOM) is 770 kg for both variants, allowing for a payload of 210 kg for the TC 100 and 202 kg for the TTC 115.

Fuel Capacity

The aircraft can hold 55 liters in the standard tank and 79 liters in the long-range tank. Fuel grades acceptable for use include Avgas 100LL, ROZ 95, and Mogas.

Operational Limits

The maximum demonstrated crosswind for the TC 100 is 16 km/h and for the TTC 115 is 15 km/h. Both models have a maximum operating altitude of 5,000 meters.

Full document text

HK36 Super Dimona - fact sheet HK36 Super Dimona - fact sheet Power plant TC 100 TTC 115 Engine Bombardier Rotax 912 S3 with 100 hp Bombardier Rotax 914 F3 with 115 hp Propeller MT propeller MTV-21-A-C-F/CF 175-05 2-blade hydraulic constant speed propeller with hydro pneumatic feathered pitch Fuel grades Avgas 100LL, ROZ 95, Mogas Performance/ consumption TC 100 (max. mass) TTC 115 (max. mass) Max. cruise speed (1,800 m, MCP) 190 km/h TAS 222 km/h TAS Cruise speed at 65% (1,800 m) 185 km/h TAS 196 km/h TAS Stall speed, airbrakes extended 81 km/h CAS 81 km/h CAS Stall speed, airbrakes retracted 78 km/h CAS 78 km/h CAS Rate of climb (ISA SL) 4.9 m/s 5.4 m/s Range at 55% (1,800 m, standard-/ long range tank) 545/ 775 km 595/ 849 km Consumption at 65% (1,800 m) 16.8 lt/h 17.4 lt/h Take-off distance 50ft (ISA SL) 299 m 274 m Take-off ground roll (ISA SL) 190 m 182 m Max. demonstrated crosswind 16 km/h 15 km/h Max. operating altitude 5,000 m 5,000 m Minimum rate of descent 1.18 m/s 1.19 m/s Glide ratio 1:27 1:27 Dimensions/ mass/ loading TC 100 TTC 115 Length 7.28 m 7.28 m Height 1.90 m 1.90 m Wing span 16.33 m 16.33 m Seats 2 2 Empty weight 560 kg 568 kg MTOM 770 kg 770 kg Payload 210 kg 202 kg Fuel capacity (standard-/ long range tank) 55 lt/ 79 lt 55 lt/ 79 lt Specifications apply to standard equipped aircraft, if not otherwise stated. Specifications may change without notice. 16.33 m 7.28 m 1.90 m Diamond Aircraft Industries GmbH | N. A. Otto-Straße 5 | A-2700 Wiener Neustadt, Austria T +43 2622 26700 | F +43 2622 26700-1199 | www.diamond-air.at Version: February 18 th , 2011 S_30617E © 2011 Diamond Aircraft Industries GmbH

All Diamond HK36 Super Dimona weight and balance