The Airworthiness Branch is responsible for safety oversight of aircraft maintenance and continuing airworthiness functions within the PNG Civil Aviation System. The Branch monitors to ensure that Aviation Industry participants conduct their operations in compliance with the regulatory obligations under the Civil Aviation Act (the Act), the Civil Aviation Rules(CAR) and their Expositions.
The Airworthiness Branch provides technical advice to the Director on aircraft maintenance and continuing airworthiness, including but not limited to the following areas:
PNG AD/Gen/003 Generator System Warning Placard Installation
PNG AD/Gen/007 Emergency Exits-Operational Test
PNG AD/Gen/014 Repair Assessment of Pressurized Fuselages
PNG AD/Gen/018 Wing Fuel Tank Skin without Aluminum-Loaded Paint-Alternate Means of Compliance
PNG AD/Gen/020 Pratt & Withney Engine PT6A Failure of Certain First Stage Reduction Sun Gear
PNG AD/Mil8/023 Replacement of Power Supply to Instrument Panels
PNG AD/Mil8/024 Inspection of Main Rotor Hub Axial Sleeves
PNG AD/Mil8/025 Inspection of Tail Rotor Blades
PNG AD 2016-01-Rev 1 Aircraft Primary Flight Control Cable Terminals-Detailed Visual Inspections
PNG AD 2016-02-Rev 2 Review of Mil-8 Component Records
PNG AD 2018-01 Inspection of Hydraulic Actuators
PNG AD 2019-01 Inspection of Vibration System Wiring
PNG AD/DHC8/22 In-flight Selection of Ground Beta-Inspection/Protection
PNG AD/B767/017 Body Station 955 Fail-Safe Straps-Inspection
PNG AD/B767/021 P50 Panel-Electrical Wire Bundles- Inspection and Protection
The Airworthiness Branch is responsible for safety oversight of aircraft maintenance and continuing airworthiness functions within the PNG Civil Aviation System. The Branch monitors to ensure that Aviation Industry participants conduct their operations in compliance with the regulatory obligations under the Civil Aviation Act (the Act), the Civil Aviation Rules(CAR) and their Expositions.
The Airworthiness Branch provides technical advice to the Director on aircraft maintenance and continuing airworthiness, including but not limited to the following areas:
PNG AD/Gen/003 Generator System Warning Placard Installation
PNG AD/Gen/007 Emergency Exits-Operational Test
PNG AD/Gen/014 Repair Assessment of Pressurized Fuselages
PNG AD/Gen/018 Wing Fuel Tank Skin without Aluminum-Loaded Paint-Alternate Means of Compliance
PNG AD/Gen/020 Pratt & Withney Engine PT6A Failure of Certain First Stage Reduction Sun Gear
PNG AD/Mil8/023 Replacement of Power Supply to Instrument Panels
PNG AD/Mil8/024 Inspection of Main Rotor Hub Axial Sleeves
PNG AD/Mil8/025 Inspection of Tail Rotor Blades
PNG AD 2016-01-Rev 1 Aircraft Primary Flight Control Cable Terminals-Detailed Visual Inspections
PNG AD 2016-02-Rev 2 Review of Mil-8 Component Records
PNG AD 2018-01 Inspection of Hydraulic Actuators
PNG AD 2019-01 Inspection of Vibration System Wiring
PNG AD/DHC8/22 In-flight Selection of Ground Beta-Inspection/Protection
PNG AD/B767/017 Body Station 955 Fail-Safe Straps-Inspection
PNG AD/B767/021 P50 Panel-Electrical Wire Bundles- Inspection and Protection