Pilatus PC-9

Twin-Seat, Single-Engine Basic Trainer Aircraft

Switzerland | 1984

"Developed from the Pilatus PC-7, the PC-9 serves as a basic and advanced two-seat trainer for many global operators."

Authored By: Staff Writer | Last Edited: 09/30/2020 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.

Image from the Untied States Department of Defense DVIDS imagery database.

The Pilatus PC-9 is a successful twin-seat basic training aircraft used in military circles to provide future pilots and combat airmen their first taste of flight. The aircraft emerged from Swiss-based Pilatus Aircraft in the mid-1980s and has found global respect from flyers despite its modest production total of 265 units. The type, developed from the earlier PC-7 model of similar form and function, went on to form the basis of the American Beechcraft / Raytheon T-6 "Texan II" basic trainer (detailed on this site) currently used by the U.S. military.

A first-flight of the PC-9 was had on May 7th, 1984 and certification followed in September of 1985. Production has been ongoing since 1984. Military operators have ranged from Angola and Australia to Thailand and the United States.

The arrangement of the PC-9 is conventional with a straight-wing mainplane configuration used. The mainplanes are seated at midships as is the tandem-seat cockpit sporting a large, curved canopy offering excellent vision out-of-the-cockpit. The cockpit sits aft of a long nose section housing the single engine installation. The tail unit showcases a single vertical tail fin and low-set horizontal planes. The undercarriage, wholly-retractable, utilizes two single-wheeled main legs (under each wing element) and a single-wheeled nose leg. Internally, the cockpits are a mix of steam-style gauges and display units. The control stick is at center, between the knees, and the throttle is set to portside. Controls are doubled for student and instructor positions. Both airmen are afforded ejection seats.

Variants include the basic, and original, PC-9 model. The PC-9/A became a basic trainer for the Royal Australian Air Force (RAAF) and was built locally under license by Hawker de Havilland. The PC-9B was a two-seat target-tower for the German Air Force and the PC-9M followed in 1997. The M-model introduced a revised tail fin and wingroots as well as other subtle changes.

The PC-9M featured an empty weight of 3,805lb against an MTOW of 5,180lb. Power is from a Pratt & Whitney Canada PT6A-62 turboprop engine developing 1,150 horsepower providing speeds of 370 miles per hour with a range out to 955 miles and a service ceiling up to 38,000 feet. Rate-of-climb is 4,100 feet-per-minute.

Pilatus then teamed with American-based Beechcraft to offer the PC-9 Mk.2 for the JPATS program. This model became the T-6A Texan II in service with the USAF and USN.

While typically unarmed, the PC-9 has three hardpoints under each wing and can carry various load outs for training purposes or light strike sorties.

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September 2020 - The Royal Thai Air Force has committed to the purchase of 12 T-6C basic trainers. The order includes training and spare parts for the fleet. These will be used to succeed an aging fleet of Pilatus PC-9M aircraft in same role. The deal was announced on September 28th, 2020.

Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Pilatus PC-9 Twin-Seat, Single-Engine Basic Trainer Aircraft.

1 x Pratt & Whitney Canada PT6A-62 turboprop engine developing 1,150 horsepower driving a four-bladed propeller unit at the nose.
Propulsion

370 mph
595 kph | 321 kts
Max Speed

37,992 ft
11,580 m | 7 miles
Service Ceiling

957 miles
1,540 km | 832 nm
Operational Range

4,100 ft/min
1,250 m/min
Rate-of-Climb

City-to-City Ranges
Operational range when compared to distances between major cities (in KM).

NYC

LON

PAR

BER

MOS

TOK

SYD

LAX

NYC

Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Pilatus PC-9 Twin-Seat, Single-Engine Basic Trainer Aircraft.

2
(MANNED)
Crew

33.3 ft
10.15 m
O/A Length

33.2 ft
(10.12 m)
O/A Width

10.7 ft
(3.25 m)
O/A Height

3,803 lb
(1,725 kg)
Empty Weight

7,055 lb
(3,200 kg)
MTOW

Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.

RANGE

ALT

SPEED

Armament
Available supported armament and special-mission equipment featured in the design of the Pilatus PC-9 Twin-Seat, Single-Engine Basic Trainer Aircraft .

OPTIONAL:
Conventional drop stores and gunpods across six underwing hardpoints (three to a wing).

Variants
Notable series variants as part of the Pilatus PC-9 family line.

PC-9 - Base Series Designation; original production model.

PC-9/A - Basic trainer for the RAAF; 48 examples by Hawker de havilland.

PC-9B - Target-tower for German Air Force

PC-9M - Model of 1997; revised tail fin and wingroots.

Beech Pilatus PC-9 Mk.2 - Joint marketing for the JPATS program, becoming the Raytheon Texan II trainer for the USAF and USN services.

Operators
Global customers who have evaluated and/or operated the Pilatus PC-9. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 265 Units
Contractor(s): Pilatus - Switzerland / Hawker de Havilland - Australia

National flag of the Kingdom of Saudi Arabia

[ Angola; Australia; Bulgaria; Croatia; Chad; Cyprus; Germany; Iraq; Ireland; Mexico; Myanmar; Oman; Saudi Arabia; Slovenia; Switzerland; Thailand; United Kingdom; United States ]

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