Beechcraft King Air 100 — Other Documents

This Type Acceptance Report provides detailed information regarding the Beechcraft King Air C90A and its variants, including the C90GT and C90GTi, as accepted for operation in New Zealand. The report outlines the basis for type acceptance, including compliance with FAA Type Certificate number 3A20, and specifies the requirements for airworthiness certification under New Zealand regulations. It includes details on the aircraft's specifications, operational requirements, and any additional conditions necessary for compliance. The document serves as a reference for operators and maintenance personnel involved with these aircraft models, ensuring they meet the necessary standards for safety and performance in New Zealand airspace.

• Maximum Takeoff Weight (MCTOW) for C90A is 9650 lb (s/n LJ-1063 thru LJ-1137) and 10100 lb (s/n LJ-1138 thru LJ-1755).
• The C90A is equipped with Pratt & Whitney Canada PT6A-21 engines.
• The aircraft must have a cabin altitude pressure switch that activates at 10,000 ft AMSL for compliance with New Zealand regulations.
• The C90GT and C90GTi models have increased power and avionics upgrades compared to the C90A.
• The report includes compliance with FAA Type Certificate number 3A20, which covers multiple models.