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Seneca V - New Arrival

Max. range 828 NM

Max. speed 205 kt

Passengers 5 person

Intro:

The Piper Seneca V is a high-performance, twin-engine light aircraft, widely used for personal, business, and charter flying. Featuring twin turbocharged 220-hp Continental engines and counter-rotating propellers, it offers a 200-knot max cruise speed, seating for six, and excellent short-field performance with a 25,000 ft service ceiling.

Key Performance & Specifications

Engines: Two Continental TSIO-360-RB5B engines with 220 hp each.
Cruise Speed: Up to 200 ktas.
Range: Approximately 828 nm to 900 nm.
Service Ceiling: 25,000 ft.
Maximum Takeoff Weight (MTOW): 4,750 lbs.
Useful Load: Approx. 1,331 lbs.
Propellers: Counter-rotating McCauley props to eliminate critical engine factors.

The Seneca V is recognized as a versatile and "tough" light twin often used for regional corporate transport, cargo, and training.

Cessna 172 (AP-BJZ)

Max. range 750 NM

Max. speed 125 kts

Passengers 3 person

Intro:

The Cessna 172 is a four-seat, single-engine, high-wing aircraft, widely recognized as the most produced and successful aircraft in history with over 45,000 built since 1956. Renowned for its stability and reliability, it is the primary trainer for flight schools worldwide

Key Specifications:

Engine: Lycoming IO-360-L2A.
Maximum Speed: 125 knots (144 mph / 230 km/h).
Range: Approx. 600-750 NM (with 50 gal usable fuel).
Max Takeoff Weight: 2,550 lbs.
Service Ceiling: 14,000–14,200 ft
Design: Known for its high-wing design, which provides excellent visibility and stability, making it ideal for training.

Cessna 172 (AP-BIX)

Max. range 750 NM

Max. speed 125 kts

Passengers 3 person

Intro:

The Cessna 172 is a four-seat, single-engine, high-wing aircraft, widely recognized as the most produced and successful aircraft in history with over 45,000 built since 1956. Renowned for its stability and reliability, it is the primary trainer for flight schools worldwide

Key Specifications:

Engine: Lycoming IO-360-L2A.
Maximum Speed: 125 knots (144 mph / 230 km/h).
Range: Approx. 600-750 NM (with 50 gal usable fuel).
Max Takeoff Weight: 2,550 lbs.
Service Ceiling: 14,000–14,200 ft
Design: Known for its high-wing design, which provides excellent visibility and stability, making it ideal for training.

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Rawalpindi Flying Club was established in 1957, and since then the academy has supplied flight companies with professional pilots and high-quality training services.

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