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Pulsar Aircraft Corporation Super Pulsar 100 User Manual

Pulsar Aircraft Corporation Super Pulsar 100
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Pulsar Aircraft Corporation Super Pulsar 100 Specifications

General IconGeneral
BrandPulsar Aircraft Corporation
ModelSuper Pulsar 100
CategoryAircrafts
LanguageEnglish

Summary

Super Pulsar 100 Operating Limits

Continental IO-240B7B Maximum Operating Limits

Weight and Balance

First Flight Inspection

Fuselage, Seatbelt & Canopy Inspection

Inspect fuselage shell, seatbelt/harness, and canopy for structural integrity, secure attachment, and proper function.

Wing Attachment Inspection

Check wing attachment fittings, aileron motion, hinges, and control surface security.

Landing Gear Inspection

Verify landing gear bolts, wheel alignment, brake system, and nosewheel security and function.

Empennage Inspection

Inspect empennage motion, stabilizer security, and rudder/elevator control systems.

Control Systems Inspection

Check rudder, aileron, and elevator control systems for proper attachment, motion, and freedom from binding.

Engine Installation & Instruments Inspection

Check engine mount, fuel lines, cowl, exhaust, instruments, and wiring for secure installation and operation.

First Flight Procedure

Preflight Inspections

Perform detailed checks of spinner, prop, cowling, nose wheel, wheel pants, brakes, and control surfaces.

First Flight Operations

Flight Test Procedures

Normal Operating Tests

Conduct initial short flights to test basic functions, systems, and trim within safe operating limits.

Structural and Control Limit Tests

Perform proof tests in smooth air for structural strength, control response, stalls, and roll/yaw characteristics.

Service Tests for Reliability

Conduct extended operations with frequent inspections to identify potential problems and ensure aircraft reliability.