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175:) was first flown in March 1988, and was certified in November 1996. The aircraft demonstrated docile stall characteristics, rapid roll rates, 125 knot cruise speed (at 75% power) and crisp handling. After 15 aircraft were built at
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for aerial surveillance operations for environmental and fire control. Specifications are identical to the Eagle 150 other than the ability for the aircraft to be remotely flown.
171:
were then engaged to design an aircraft to meet then-current JAR VLA requirements and demonstrate minimal stall characteristics. The resulting prototype (designated
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design consisting of a forward wing (foreplane), main wing (mainplane) and horizontal stabilizer (tailplane). The aircraft was designed and originally built by
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from
Western Australian inventors Neil Graham and his father Deryck Graham. Australian aeronautical engineer Graham Swannell and American aerodynamicist
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206:. The first system, consisting of three aircraft and a ground station, has been purchased by the Malaysian government and other 20 on order.
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The manufacturing rights to the Eagle 150B are now owned by the
Malaysian company Composites Technology Research Malaysia (CTRM).
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841:
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IA135BRM7054 or IA135CRM7057 or 1A135DRM7057, 1.78 m (5 ft 10 in) diameter fixed-pitch metal propeller
273:
Jane's all the World's
Aircraft 2000–01 Eagle 150B Pilots Operating Handbook and FAA Approved Airplane Flight Manual
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was introduced. Roncz was presented with the Prince's
Australian Medal for the design of the Eagle 150 by
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or IO-240-B7B 4-cylinder air-cooled horizontally-opposed piston engine, 93 kW (125 hp)
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658:(91st ed.). Coulsdon, Surrey, United Kingdom: Jane's Information Group.
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Eagle 150B Pilots
Operating Handbook and FAA Approved Airplane Flight Manual
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APFT Eagle and Piper fleet of Asia
Pacific Flight Training on apron
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745:
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73.6 kg/m (15.1 lb/sq ft) mainplane and foreplane
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84 km/h (52 mph; 45 kn) flaps down at sea level
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World
Directory of Leisure Aviation 2005–2006, ISSN 1368-485X
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102 km/h (63 mph, 55 kn) flaps up at sea level
367:
97 L (26 US gal; 21 imp gal) usable
233:
Productionised version of the XT-S, built by Eagle
Aircraft.
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The unmanned or manned version of 150 is being used by the
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Optionally piloted UAV version of the 150B developed by
629:"CRTM - Unmanned Systems Technology Sdn Bhd (The UAS)"
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1,000 km (620 mi, 540 nmi) at 75% power
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222 km/h (138 mph, 120 kn) at 75% power
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255:Composites Technology Research Malaysia (CTRM)
149:Composites Technology Research Malaysia (CTRM)
60:Composites Technology Research Malaysia (CTRM)
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702:CRTM (Composites Technology Research Malaysia
8:
135:, touring and sport aircraft. It utilizes a
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741:McCauley 1A135 Type Certificate Data Sheet
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402:241 km/h (150 mph, 130 kn)
510:Landing run from 15 m (49 ft):
656:Jane's all the World's Aircraft 2000–01
563:
561:
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504:Take-off run to 15 m (49 ft):
827:1990s Malaysian civil utility aircraft
736:TCM IO-240 Type Certificate Data Sheet
499:0.1433 kW/kg (0.0872 hp/lb)
194:Eagle Airborne Reconnaissance Vehicle
7:
837:Unmanned aerial vehicles of Malaysia
375:Teledyne Continental Motors IO-240-A
198:A development of the aircraft as an
305:7.16 m (23 ft 6 in)
125:is an Australian designed two-seat
724:New Zealand Type Acceptance Report
331:3.62 m (39.0 sq ft)
299:6.45 m (21 ft 2 in)
14:
318:2.31 m (7 ft 7 in)
484:5.3 m/s (1,040 ft/min)
324:5.2 m (56 sq ft)
185:His Royal Highness Prince Philip
26:
714:CASA Australia Type Certificate
682:. Eagle Aircraft Pty Ltd. 2001.
239:Further development of the 150
187:at a London ceremony in 2000.
1:
451:4,575 m (15,010 ft)
143:, but is now manufactured in
847:Aircraft first flown in 1997
530:Honeywell KT 97A Transponder
654:Jackson, Paul, ed. (2000).
361:650 kg (1,433 lb)
312:4.88 m (16.01 ft)
863:
527:Honeywell KY 97A VHF radio
512:365 m (1,198 ft)
506:349 m (1,145 ft)
781:
729:27 September 2007 at the
355:430 kg (948 lb)
219:Royal Malaysian Air Force
179:, Western Australia, the
83:Royal Malaysian Air Force
25:
707:23 February 2014 at the
202:has been designated the
163:is a development of the
278:General characteristics
266:Specifications (E-150B)
200:unmanned aerial vehicle
58:Eagle Aircraft Pty Ltd
842:Three-surface aircraft
247:Eagle Aircraft Pty Ltd
214:
155:Design and development
141:Eagle Aircraft Pty Ltd
212:
137:three lifting surface
719:FAA Type Certificate
569:"Neil Deryck Graham
445:5 hours at 60% power
259:Malaysian Government
635:on 10 November 2016
609:on 19 November 2016
579:on 19 November 2016
533:Garmin GNS250XL GPS
359:Max takeoff weight:
165:Eagle Aircraft X-TS
114:Eagle Aircraft X-TS
38:General information
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130:composite material
123:Eagle Aircraft 150
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94:Introduction date
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631:. Archived from
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575:. Archived from
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449:Service ceiling:
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204:Eagle ARV System
81:In service with
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329:Foreplane area:
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696:External links
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665:978-0710620118
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637:. Retrieved
633:the original
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607:the original
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599:"John Roncz
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581:. Retrieved
577:the original
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551:Neil Graham
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412:Stall speed:
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102:First flight
54:Manufacturer
15:
639:18 November
613:18 November
583:18 November
467:1.9 ;
393:Performance
381:Propellers:
371:Powerplant:
251:BAE Systems
821:Categories
601:The Medium
538:References
495:Power/mass
443:Endurance:
322:Wing area:
236:Eagle 150B
181:Eagle 150B
173:Eagle 150A
169:John Roncz
161:Eagle 150B
71:John Roncz
32:Eagle 150B
806:Eagle ARV
801:Eagle 150
571:Biography
522:including
469:Ultimate:
455:g limits:
385:MacCauley
383:2-bladed
349:Roncz 16%
303:Wingspan:
291:Capacity:
271:Data from
230:Eagle 150
177:Fremantle
21:Eagle 150
727:Archived
705:Archived
518:Avionics
458:JAR-VLA:
257:for the
225:Variants
145:Malaysia
133:training
66:Designer
553:Profile
345:Airfoil
316:Height:
297:Length:
89:History
791:X-Wing
662:
437:Range:
78:Status
786:EX-P1
474:8.55
285:Crew:
796:X-TS
660:ISBN
641:2016
615:2016
585:2016
478:4.27
463:3.8
373:1 ×
159:The
121:The
105:1997
97:1998
43:Type
340:9.9
147:by
823::
560:^
151:.
769:e
762:t
755:v
668:.
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617:.
603:"
587:.
573:"
497::
476:-
472:+
465:-
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347::
338::
293:2
287:1
261:.
253:/
249:/
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
