Serial No.
SECTION 4
ENGINE AIRWORTHINESS DIRECTIVE RECORD – Arriel 1
Page No. 1
A.D. No. / Short Title / Compliance Due at A/F Hrs/ Date / E FE NA / RepetitiveYes/No / Remarks / Signature, Name Number † / Date †
DCA/TUR/1 / Condition Monitoring System - Modification
DCA/TUR/3 / Turbine Case – ID Plate Removal and Modification
DCA/TUR/4 / Gas Generator Rear Bearing Oil Pipe - Modification
DCA/TUR/6A / Reduction Gear Module – Inspection
DCA/TUR/7 / Free Wheel Assembly – Modification
DCA/TUR/8C / Second Stage Nozzle Guide Vanes - Inspection
DCA/TUR/9B / Free Power Turbine - Containment Modifications
DCA/TUR/10 / Overspeed Sensor – Inspection
DCA/TUR/11 / Gas Generator Rear Bearing Chip Detector - Installation
DCA/TUR/13 / Power Turbine Nozzle Assembly - Inspection
DCA/TUR/20 / Centrifugal Impeller – Modification
DCA/TUR/22 / Second Stage Turbine Blade - Replacement
DCA/TUR/26B / Arriel 2nd Stage NGV – Inspection
DCA/TUR/37 / Start Electro Fuel Valve Leaks – Inspection
DCA/TUR/47 / Engines Returned to Civil Use – Inspection
DCA/TUR/61 / Reduction Gearbox Intermediate Pinion – Modification
DCA/TUR/65A / Module 04 Power Turbine – Life Limitation
DCA/TUR/67 / Module M05 Reduction Gearbox – Inspection
DCA/TUR/70D / Gas Generator 2nd Stage Turbine – Reduced Life Limit
DCA/TUR/74 / Fuel Ejector Assembly – Inspection
DCA/TUR/75 / Module M03 2nd Stage NGVs – Inspection
If ‘Yes’ placed in Repetitive AD column, enter details of AD on aircraft repetitive AD control card.
† The maintenance recorded has been carried out in accordance with the requirements of New Zealand Civil Aviation
Rule Part 43 and in respect of that maintenance the (aircraft)* (component)* is released to service. * Delete as applicable
Serial No.
SECTION 4
ENGINE AIRWORTHINESS DIRECTIVE RECORD – Arriel 1
Page No. 2
A.D. No. / Short Title / Compliance Due at A/F Hrs/ Date / E FE NA / RepetitiveYes/No / Remarks / Signature, Name Number † / Date †
DCA/TUR/81 / FCU 3-Way Union Plug – Inspection
DCA/TUR/82 / Gas Generator Rotating Assembly - Inspection
DCA/TUR/83 / Gas Generator Rotating Assembly – Inspection
DCA/TUR/87 / Gas Generator 2nd Stage Turbine – Inspection
2012-0187R2 / Engine Cycle Counting Aid System – Modification
2013-0120 / Free Turbine Bearing Plug – Inspection
2014-0036 / Accessory Gearbox (M01) Bevel Gear – Inspection
2015-0064R1 / Engine Front Support Pins – Inspection
2015-0175 / Tachometer Boxes – Inspection
2016-0009 / Gas Generator Module 03 – Modification
2016-0090 / Centrifugal Impeller – Life Limitation
If ‘Yes’ placed in Repetitive AD column, enter details of AD on aircraft repetitive AD control card.
† The maintenance recorded has been carried out in accordance with the requirements of New Zealand Civil Aviation
Rule Part 43 and in respect of that maintenance the (aircraft)* (component)* is released to service. * Delete as applicable