Skip to main content

Type Certificate Data Sheet

Cessna 152 Aerobat · Type Certificate

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

Overview

This document serves as the Type Certificate Data Sheet for the Cessna 152, detailing the aircraft's specifications, performance data, and operational limitations. It is intended for use by pilots, maintenance personnel, and aviation enthusiasts who require comprehensive information about the Cessna 152. The document outlines critical data such as weight limits, engine specifications, and performance characteristics, ensuring that users have access to essential information for safe operation and maintenance of the aircraft.

  • Maximum takeoff weight: 1,670 lbs (757 kg)
  • Useful load: 490 lbs (222 kg)
  • Stall speed: 47 knots (54 mph)
  • Maximum cruise speed: 107 knots (123 mph)
  • Service ceiling: 14,700 feet (4,480 meters)
  • Range: 415 nautical miles (478 miles)
  • Maximum demonstrated crosswind component: 15 knots

Document

Source

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

Report a problem or request removal

Document details

Type
Type Certificate
Pages
30
File size
20 MB
Publisher
www.chloratech.ca
How rare is it?
20Cessna 152 Aerobat registered worldwide · 0 active

Common. Rarer than 4% of the aircraft models we track.

Documentation completeness
4/7

Most owners only have the POH. Here's the essential set for the Cessna 152 Aerobat.

More Cessna 152 Aerobatmanuals & documents

See all 24
Similar aircraft

If you fly the Cessna 152 Aerobat, you may also be researching these.

In this document

Aircraft Specifications

The Cessna 152 is a two-seat, single-engine, high-wing aircraft. It has a maximum takeoff weight of 1,670 lbs (757 kg) and a useful load of 490 lbs (222 kg). The aircraft is powered by a Lycoming O-235-L2C engine, producing 110 horsepower.

Performance Data

The Cessna 152 has a stall speed of 47 knots (54 mph) and a maximum cruise speed of 107 knots (123 mph). The service ceiling is 14,700 feet (4,480 meters), and the range is approximately 415 nautical miles (478 miles) with standard fuel.

Operational Limitations

The aircraft is certified for day VFR operations and has specific limitations regarding weight and balance, which must be adhered to for safe flight. The maximum demonstrated crosswind component is 15 knots.

Safety notes

  • Ensure weight and balance are within limits before flight.
  • Adhere to operational limitations for safe flight.