An-24

1. Implementation of works in according with Industry Bulletins, except of works on the structural components of the airplane.

2. Implementation of works in according with Service Bulletins by Supplemental Type Certificates.

Installation of the 'СРППЗ-2000', 'СН-3301', GPS-155XL systems and А813-0409 indicator

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Installation of the Terrain Awareness and Warning System (EGPWS/TAWS)

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Installation of the Air Data Display AD32

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Installation of the Traffic Alert And Collision Avoidance System CAS-67A

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Installation of the Satellite Navigation System with flight operations in B-RNAV

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Installation of the Distance Measuring Equipment (DME) KN-63

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Installation of the Emergency Locator Transmitter 'КОСПАСС-САРСАТ'

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Installation of the satellite equipment Skynode S200-021 Iridium

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Installation of the satellite equipment Aero-C Inmarsat system

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Installation of the backup attitude indicator and roll limits warnings

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Installation of a separate power supply of the left and right attitude indicator with two independent channels

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Installation of the flight crew restraint system

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Installation of 'БКК-18' and autopilot switch off according to warnings 'GYRO FAULT', 'ROLL LIMIT'. Ensuring the protection of wire harnesses

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Replacement of the radioisotope ice detector 'РИО-3' with vibration type detector EW-164

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Installation of the Solid State Flight Data Recorder (SSFDR) "БУР-4-1"

byr-4-1-new

Type design approval of the aircraft modification:
Supplemental Type Certificate № DTL0179 issued by State Aviation Administration of Ukraine.

Documentation for the implementation of modification:
Performed in accordance with design documentation № 24.СТ8.001.ПТК-16 approved by State Aviation Administration of Ukraine.

Documentation for operation of the aircraft with modification:
Supplements to Flight Manual, Maintenance Manual and Maintenance Program approved by State Aviation Administration of Ukraine and issued by separate books.

List of equipment for modification of the aircraft:
• «БСИ-4» – data collector unit;
• «БР-4Т» – Solid State Recorder;
• «ПУ-4» – control panel.
DK-120/90 – underwater location beacon.

Requirements for design of the aircraft:
There are no specific requirements for design of the aircraft for installation and operation of the Solid State Flight Data Recorder (SSFDR) «БУР-4-1».

Additional information:
Par. 6.3.1 ICAO Annex 6 to the Convention on International Civil Aviation.

Installation of the Solid State Cockpit Voice Recorder (SSCVR) "ОРТ"

opt-new

Type design approval of the aircraft modification:
Supplemental Type Certificate № DTL0180 issued by State Aviation Administration of Ukraine.

Documentation for the implementation of modification:
Performed in accordance with design documentation № 24.СТ9.001.ПТК-16 approved by State Aviation Administration of Ukraine.

Documentation for operation of the aircraft with modification:
Supplements to Flight Manual, Maintenance Manual and Maintenance Program approved by State Aviation Administration of Ukraine and issued by separate books.

List of equipment for modification of the aircraft:
• «ОРТ» - Solid State Cockpit Voice Recorder (SSCVR);
• Control panel «ОРТ»;
• Microphone;
DK-120/90 – underwater location beacon.

Requirements for design of the aircraft:
There are no specific requirements for design of the aircraft for installation and operation of the Solid State Cockpit Voice Recorder (SSCVR) «ОРТ».

Additional information:
Par. 6.3.2 ICAO Annex 6 to the Convention on International Civil Aviation.

Replacement of the altimeter 'РВ-5 (РВ-УМ)' with 'РВ-5М'

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