---
title: "<Письмо> Росавиации от 09.10.2018 N Исх-25445/03"
number: "Исх-25445/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2018-10-09
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-2544503"
---

## <Письмо> Росавиации от 09.10.2018 N Исх-25445/03

# <Письмо> Росавиации от 09.10.2018 N Исх-25445/03

"Информационное письмо ДЛГ-06-2018"


<a id="p100001"></a>МИНИСТЕРСТВО ТРАНСПОРТА РОССИЙСКОЙ ФЕДЕРАЦИИ

<div align="center">

<a id="p100002"></a>**ФЕДЕРАЛЬНОЕ АГЕНТСТВО ВОЗДУШНОГО ТРАНСПОРТА**

</div>


<a id="p100003"></a>**ПИСЬМО**
**от 9 октября 2018 г. N Исх-25445/03**

<div align="center">

<a id="p100004"></a>**ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-06-2018**

</div>


<a id="p100005"></a>**Управление поддержания летной годности воздушных судов информирует эксплуатантов воздушных судов о выпуске иностранными авиационными администрациями следующих Директив летной годности за период 30.07.2018 - 23.09.2018:**


| <a id="p100006"></a>N | <a id="p100007"></a>Номер | <a id="p100008"></a>Выпущено страной | <a id="p100009"></a>Дата выпуска | <a id="p100010"></a>Изготовить ВС | <a id="p100011"></a>Тип ВС (Классификация ВС, страны выпустившей ДЛГ) | <a id="p100012"></a>Краткое содержание |
| --- | --- | --- | --- | --- | --- | --- |
| <a id="p100013"></a>1 | <a id="p100014"></a>2018-0209 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/vGK4af1Oj/img_0.png) | <a id="p100016"></a>21.09.2018 | <a id="p100017"></a>AIRBUS HELICOPTERS | <a id="p100018"></a>SA 330/AS 332/EC 225 | <a id="p100019"></a>Fuselage - Fuel Draining System - Modification |
| <a id="p100020"></a>2 | <a id="p100021"></a>2016-0105R1 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/vGK4af1Oj/img_1.png) | <a id="p100023"></a>21.09.2018 | <a id="p100024"></a>AIRBUS | <a id="p100025"></a>A321 | <a id="p100026"></a>Fuselage - Cabin Floor Beam Junction - Inspection |
| <a id="p100027"></a>3 | <a id="p100028"></a>2016-0035R1 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/vGK4af1Oj/img_2.png) | <a id="p100030"></a>21.09.2018 | <a id="p100031"></a>AIRBUS | <a id="p100032"></a>A340 | <a id="p100033"></a>Fuselage - Structure Frames and Joints - Modification/Reinforcement |
| <a id="p100034"></a>4 | <a id="p100035"></a>US-2018-19-04 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/vGK4af1Oj/img_3.png) | <a id="p100037"></a>20.09.2018 | <a id="p100038"></a>LEARJET, INC. | <a id="p100039"></a>28, 29, 31/35/36, 55, 60 | <a id="p100040"></a>Flight Controls - Flap Nose Roller Fitting, Nose Roller Support Bracket, and Adjacent Rib Support Structure - Replacement |
| <a id="p100041"></a>5 | <a id="p100042"></a>2018-0208 | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/vGK4af1Oj/img_4.png) | <a id="p100044"></a>20.09.2018 | <a id="p100045"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100046"></a>AB139/AW139, AW169, AW189 | <a id="p100047"></a>Emergency Flotation System - Aft Float Assembly Inflation System - Removal/Installation |
| <a id="p100048"></a>6 | <a id="p100049"></a>2018-0206 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/vGK4af1Oj/img_5.png) | <a id="p100051"></a>20.09.2018 | <a id="p100052"></a>AIRBUS HELICOPTERS | <a id="p100053"></a>AS 350/EC 130, AS 355 | <a id="p100054"></a>Main Rotor - Mast Upper Bearing Sealant Bead/Inner Race Retaining Rings - Inspection |
| <a id="p100055"></a>7 | <a id="p100056"></a>2018-0207-E | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/vGK4af1Oj/img_6.png) | <a id="p100058"></a>19.09.2018 | <a id="p100059"></a>HPH SPOL.S R.O. | <a id="p100060"></a>Glasfluegel 304 | <a id="p100061"></a>Equipment/Furnishings - Towing Release Mechanism - Inspection |
| <a id="p100062"></a>8 | <a id="p100063"></a>US-2018-17-15 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/vGK4af1Oj/img_7.png) | <a id="p100065"></a>18.09.2018 | <a id="p100066"></a>HONEYWELL INTERNATIONAL INC. | <a id="p100067"></a>TPE331, TSE331-3U | <a id="p100068"></a>Engine - Combustion Chamber Case Assembly - Inspection/Replacement/Removal Transducers |
| <a id="p100069"></a>9 | <a id="p100070"></a>2018-0205 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/vGK4af1Oj/img_8.png) | <a id="p100072"></a>14.09.2018 | <a id="p100073"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100074"></a>A109/A119 | <a id="p100075"></a>Main Rotor - Floating Ring Assembly - Inspection/Replacement |
| <a id="p100076"></a>10 | <a id="p100077"></a>2018-0204 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/vGK4af1Oj/img_9.png) | <a id="p100079"></a>13.09.2018 | <a id="p100080"></a>AIRBUS HELICOPTERS | <a id="p100081"></a>SA 330/AS 332/EC 225 | <a id="p100082"></a>Air Conditioning - Clearance between Air Conditioning Unit and Landing Light Connectors - Measurement |
| <a id="p100083"></a>11 | <a id="p100084"></a>2018-0203 | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/vGK4af1Oj/img_10.png) | <a id="p100086"></a>12.09.2018 | <a id="p100087"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100088"></a>AW 169 | <a id="p100089"></a>Rotors Flight Control - Pilot Collective Stick Assembly - Check |
| <a id="p100090"></a>12 | <a id="p100091"></a>2017-0105R1 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/vGK4af1Oj/img_11.png) | <a id="p100093"></a>12.09.2018 | <a id="p100094"></a>AIRBUS | <a id="p100095"></a>A340 | <a id="p100096"></a>Exhaust - Thrust Reverser Outer Fixed Structure - Inspection/Replacement |
| <a id="p100097"></a>13 | <a id="p100098"></a>US-2018-17-12 | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/vGK4af1Oj/img_12.png) | <a id="p100100"></a>11.09.2018 | <a id="p100101"></a>GENERAL ELECTRIC | <a id="p100102"></a>GE90 | <a id="p100103"></a>Engine - Full Authority Digital Engine Control - Software Upgrade Installation |
| <a id="p100104"></a>14 | <a id="p100105"></a>US-2018-07-04 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/vGK4af1Oj/img_13.png) | <a id="p100107"></a>11.09.2018 | <a id="p100108"></a>BOEING | <a id="p100109"></a>DC-9, MD-88, MD-90 | <a id="p100110"></a>Ice and Rain Protection - Air Data Heat System - Modification |
| <a id="p100111"></a>15 | <a id="p100112"></a>2018-0202 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/vGK4af1Oj/img_14.png) | <a id="p100114"></a>11.09.2018 | <a id="p100115"></a>ROLLS-ROYCE PLC | <a id="p100116"></a>RB211-535 | <a id="p100117"></a>Engine - Low Pressure Compressor Blades - Inspection |
| <a id="p100118"></a>16 | <a id="p100119"></a>US-2018-17-23 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/vGK4af1Oj/img_15.png) | <a id="p100121"></a>10.09.2018 | <a id="p100122"></a>BOEING | <a id="p100123"></a>737 | <a id="p100124"></a>Fuselage - Number 3 Windshield Assembly Aft Sill Web - Inspection |
| <a id="p100125"></a>17 | <a id="p100126"></a>US-2018-16-09 | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/vGK4af1Oj/img_16.png) | <a id="p100128"></a>10.09.2018 | <a id="p100129"></a>BOEING | <a id="p100130"></a>737 | <a id="p100131"></a>Fuselage - Frame Webs - Inspection |
| <a id="p100132"></a>18 | <a id="p100133"></a>US-2018-18-07 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/vGK4af1Oj/img_17.png) | <a id="p100135"></a>07.09.2018 | <a id="p100136"></a>BOEING | <a id="p100137"></a>757 | <a id="p100138"></a>Fuselage - Skin Longitudinal Lap Splices - Inspection |
| <a id="p100139"></a>19 | <a id="p100140"></a>2018-0201 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/vGK4af1Oj/img_18.png) | <a id="p100142"></a>07.09.2018 | <a id="p100143"></a>AIRBUS | <a id="p100144"></a>A340 | <a id="p100145"></a>Fuel - Fuel Control and Monitoring Computer - Software Update |
| <a id="p100146"></a>20 | <a id="p100147"></a>2018-0199 | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/vGK4af1Oj/img_19.png) | <a id="p100149"></a>06.09.2018 | <a id="p100150"></a>ROLLS-ROYCE PLC | <a id="p100151"></a>RB211 TRENT 900 | <a id="p100152"></a>Engine - Oil Service Pipe Sealing Rings - Replacement |
| <a id="p100153"></a>21 | <a id="p100154"></a>2018-0198 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/vGK4af1Oj/img_20.png) | <a id="p100156"></a>06.04.2018 | <a id="p100157"></a>AIRBUS | <a id="p100158"></a>A330 | <a id="p100159"></a>Nacelles/Pylons - Lower Aft Pylon Fairing Drain Pipe and U-Shapes - Inspection/Modification |
| <a id="p100160"></a>22 | <a id="p100161"></a>2018-0200 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/vGK4af1Oj/img_21.png) | <a id="p100163"></a>06.09.2018 | <a id="p100164"></a>AIRBUS | <a id="p100165"></a>A320 | <a id="p100166"></a>Electrical Power - Wing Electrical Installation - Modification |
| <a id="p100167"></a>23 | <a id="p100168"></a>2016-0247-CN | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/vGK4af1Oj/img_22.png) | <a id="p100170"></a>06.09.2018 | <a id="p100171"></a>ROLLS-ROYCE PLC | <a id="p100172"></a>TRENT XWB | <a id="p100173"></a>CANCELLED: Engine Fuel & Control - P30 Sense Line Air Tube - Drainage/Inspection |
| <a id="p100174"></a>24 | <a id="p100175"></a>2018-0196 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/vGK4af1Oj/img_23.png) | <a id="p100177"></a>05.09.2018 | <a id="p100178"></a>AIRBUS | <a id="p100179"></a>A330 | <a id="p100180"></a>Flight Controls - Flight Control Primary Computer - Modification/Replacement |
| <a id="p100181"></a>25 | <a id="p100182"></a>2018-0197 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/vGK4af1Oj/img_24.png) | <a id="p100184"></a>05.09.2018 | <a id="p100185"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100186"></a>AW 169, AW 189 | <a id="p100187"></a>Windows - Emergency Exit Windows - Modification |
| <a id="p100188"></a>26 | <a id="p100189"></a>2018-0188R1 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/vGK4af1Oj/img_25.png) | <a id="p100191"></a>05.09.2018 | <a id="p100192"></a>ROLLS-ROYCE PLC | <a id="p100193"></a>RB211 TRENT 700 | <a id="p100194"></a>Engine - Low Pressure Compressor Blades - Inspection/Replacement |
| <a id="p100195"></a>27 | <a id="p100196"></a>2018-0194 | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/vGK4af1Oj/img_26.png) | <a id="p100198"></a>04.09.2018 | <a id="p100199"></a>ROLLS-ROYCE DEUTSCHLAND | <a id="p100200"></a>BR700-715 | <a id="p100201"></a>Engine - High Pressure Turbine Stage 1 Turbine Blades and Blade Damper - Replacement |
| <a id="p100202"></a>28 | <a id="p100203"></a>2018-0195 | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/vGK4af1Oj/img_27.png) | <a id="p100205"></a>04.09.2018 | <a id="p100206"></a>APPLIANCES | <a id="p100207"></a>ATA 25 EQUIPMENT/FURNISHINGS | <a id="p100208"></a>ANJOU AERONAUTIQUE - Restraint Systems Rotary Buckle Sub Assembly - Removal from Service |
| <a id="p100209"></a>29 | <a id="p100210"></a>2015-0141R5 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/vGK4af1Oj/img_28.png) | <a id="p100212"></a>04.09.2018 | <a id="p100213"></a>AIRBUS | <a id="p100214"></a>A380 | <a id="p100215"></a>[Correction] Wings - Leading Edge Shear Cleats - Inspection/Replacement |
| <a id="p100216"></a>30 | <a id="p100217"></a>2014-0016R6 | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/vGK4af1Oj/img_29.png) | <a id="p100219"></a>04.09.2018 | <a id="p100220"></a>AIRBUS | <a id="p100221"></a>A380 | <a id="p100222"></a>Wings - Wing Inboard Leading Edge Droop Nose Gooseneck - Inspection/Repair/Replacement |
| <a id="p100223"></a>31 | <a id="p100224"></a>US-2018-16-14 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/vGK4af1Oj/img_30.png) | <a id="p100226"></a>04.09.2018 | <a id="p100227"></a>BELL HELICOPTER TEXTRON Inc. (BHTI) | <a id="p100228"></a>212, 412 | <a id="p100229"></a>Emergency Flotation Section - Emergency Flotation System Tube Assembly - Replacement |
| <a id="p100230"></a>32 | <a id="p100231"></a>2018-0193 | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/vGK4af1Oj/img_31.png) | <a id="p100233"></a>03.09.2018 | <a id="p100234"></a>DASSAULT AVIATION | <a id="p100235"></a>Fan Jet Falcon | <a id="p100236"></a>Time Limits/Maintenance Checks - Supplementary Structural Inspection Program - Amendment |
| <a id="p100237"></a>33 | <a id="p100238"></a>2018-0192 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/vGK4af1Oj/img_32.png) | <a id="p100240"></a>03.09.2018 | <a id="p100241"></a>AIRBUS | <a id="p100242"></a>A340 | <a id="p100243"></a>Aircraft Flight Manual/Engine Bleed Air System - Amendment; Indicating & Recording System - Flight Warning Computer - Modification/Replacement |
| <a id="p100244"></a>34 | <a id="p100245"></a>2018-0191 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/vGK4af1Oj/img_33.png) | <a id="p100247"></a>03.09.2018 | <a id="p100248"></a>AIRBUS | <a id="p100249"></a>A380 | <a id="p100250"></a>Fuel - Fuel Pumps/Outboard Collector Cell Jet Pump - Inspection |
| <a id="p100251"></a>35 | <a id="p100252"></a>2018-0190 | <a id="p100253"></a>![рис. 35](https://i.bukva.ai/vGK4af1Oj/img_34.png) | <a id="p100254"></a>31.08.2018 | <a id="p100255"></a>AIRBUS HELICOPTERS | <a id="p100256"></a>EC175 | <a id="p100257"></a>Landing Gear - Nose Landing Gear A-Frame/Liner - Inspection |
| <a id="p100258"></a>36 | <a id="p100259"></a>2018-0189 | <a id="p100260"></a>![рис. 36](https://i.bukva.ai/vGK4af1Oj/img_35.png) | <a id="p100261"></a>30.08.2018 | <a id="p100262"></a>AIRBUS | <a id="p100263"></a>A318, A319, A320, A321 | <a id="p100264"></a>Navigation - Back Up Speed Scale/Aircraft Flight Manual - Amendment |
| <a id="p100265"></a>37 | <a id="p100266"></a>US-2018-15-04 | <a id="p100267"></a>![рис. 37](https://i.bukva.ai/vGK4af1Oj/img_36.png) | <a id="p100268"></a>30.08.2018 | <a id="p100269"></a>GENERAL ELECTRIC | <a id="p100270"></a>CF6-80A, CF6-80C | <a id="p100271"></a>Engine - High-Pressure Turbine Stage 1 and Stage 2 Disks - Inspection |
| <a id="p100272"></a>38 | <a id="p100273"></a>2018-0186 | <a id="p100274"></a>![рис. 38](https://i.bukva.ai/vGK4af1Oj/img_37.png) | <a id="p100275"></a>24.08.2018 | <a id="p100276"></a>AIRBUS HELICOPTERS | <a id="p100277"></a>EC 120 B | <a id="p100278"></a>Main Rotor - Hub Scissors Attachment Bolts - Inspection/Replacement |
| <a id="p100279"></a>39 | <a id="p100280"></a>2018-0185 | <a id="p100281"></a>![рис. 39](https://i.bukva.ai/vGK4af1Oj/img_38.png) | <a id="p100282"></a>29.08.2018 | <a id="p100283"></a>ROLLS-ROYCE PLC | <a id="p100284"></a>RB211 TRENT 900 | <a id="p100285"></a>Powerplant - Drains Mast - Inspection/Replacement |
| <a id="p100286"></a>40 | <a id="p100287"></a>2018-0187 | <a id="p100288"></a>![рис. 40](https://i.bukva.ai/vGK4af1Oj/img_39.png) | <a id="p100289"></a>29.08.2018 | <a id="p100290"></a>SAAB AB | <a id="p100291"></a>2000 | <a id="p100292"></a>Fuel - Fuel Quantity Reading Probes and Low Level Sensors - Functional Check |
| <a id="p100293"></a>41 | <a id="p100294"></a>2018-0115-CN | <a id="p100295"></a>![рис. 41](https://i.bukva.ai/vGK4af1Oj/img_40.png) | <a id="p100296"></a>29.08.2018 | <a id="p100297"></a>ROLLS-ROYCE DEUTSCHLAND | <a id="p100298"></a>BR700-710 | <a id="p100299"></a>CANCELLED: Engine - Accessory Gearbox Mount Assembly Tie Bolts - Replacement |
| <a id="p100300"></a>42 | <a id="p100301"></a>2018-0184 | <a id="p100302"></a>![рис. 42](https://i.bukva.ai/vGK4af1Oj/img_41.png) | <a id="p100303"></a>28.08.2018 | <a id="p100304"></a>ATR | <a id="p100305"></a>ATR72 | <a id="p100306"></a>Time Limits/Maintenance Checks - Certification Maintenance Requirements and Airworthiness Limitations - Amendments |
| <a id="p100307"></a>43 | <a id="p100308"></a>2018-0182 | <a id="p100309"></a>![рис. 43](https://i.bukva.ai/vGK4af1Oj/img_42.png) | <a id="p100310"></a>28.08.2018 | <a id="p100311"></a>AIRBUS HELICOPTERS | <a id="p100312"></a>AS 350/EC 130 | <a id="p100313"></a>Tail Rotor - Blade - Life Limit/Reidentification |
| <a id="p100314"></a>44 | <a id="p100315"></a>2018-0183 | <a id="p100316"></a>![рис. 44](https://i.bukva.ai/vGK4af1Oj/img_43.png) | <a id="p100317"></a>28.08.2018 | <a id="p100318"></a>AIRBUS HELICOPTERS | <a id="p100319"></a>EC 120 B | <a id="p100320"></a>Tail Rotor - Blade - Life Limit/Reidentification |
| <a id="p100321"></a>45 | <a id="p100322"></a>CF-2018-23 | <a id="p100323"></a>![рис. 45](https://i.bukva.ai/vGK4af1Oj/img_44.png) | <a id="p100324"></a>27.08.2018 | <a id="p100325"></a>BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100326"></a>206 | <a id="p100327"></a>Engine Turbine/Turboshaft - RPM (N2) Steady-State Operation Avoidance Range Limit |
| <a id="p100328"></a>46 | <a id="p100329"></a>US-2018-17-01 | <a id="p100330"></a>![рис. 46](https://i.bukva.ai/vGK4af1Oj/img_45.png) | <a id="p100331"></a>27.08.2018 | <a id="p100332"></a>BELL HELICOPTER TEXTRON Inc. (BHTI) | <a id="p100333"></a>212, 412 | <a id="p100334"></a>Engine Oil/Aircraft Fuel System - Oil/Fuel Check Valves - Replacement |
| <a id="p100335"></a>47 | <a id="p100336"></a>2018-0180 | <a id="p100337"></a>![рис. 47](https://i.bukva.ai/vGK4af1Oj/img_46.png) | <a id="p100338"></a>27.08.2018 | <a id="p100339"></a>AIRBUS | <a id="p100340"></a>A318, A319, A320, A321 | <a id="p100341"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 3 - Certification Maintenance Requirements - Amendment |
| <a id="p100342"></a>48 | <a id="p100343"></a>2018-0181 | <a id="p100344"></a>![рис. 48](https://i.bukva.ai/vGK4af1Oj/img_47.png) | <a id="p100345"></a>27.08.2018 | <a id="p100346"></a>BALONY KUBICEK | <a id="p100347"></a>BB Hot Air Balloons | <a id="p100348"></a>Fuselage - Envelope Vertical Load Tapes - Inspection |
| <a id="p100349"></a>49 | <a id="p100350"></a>2018-0179 | <a id="p100351"></a>![рис. 49](https://i.bukva.ai/vGK4af1Oj/img_48.png) | <a id="p100352"></a>23.08.2018 | <a id="p100353"></a>AIRBUS | <a id="p100354"></a>A350 | <a id="p100355"></a>Time Limits/Maintenance Checks - Certification Maintenance Requirements - ALS Part 3 - Amendment |
| <a id="p100356"></a>50 | <a id="p100357"></a>2018-0178 | <a id="p100358"></a>![рис. 50](https://i.bukva.ai/vGK4af1Oj/img_49.png) | <a id="p100359"></a>23.08.2018 | <a id="p100360"></a>AIRBUS | <a id="p100361"></a>A350 | <a id="p100362"></a>Hydraulic System/Fuel Tank Inerting System - Engine Driven Pump Rapid Overheat - Master Minimum Equipment List Restriction/Software Update/Modification |
| <a id="p100363"></a>51 | <a id="p100364"></a>US-2018-17-03 | <a id="p100365"></a>![рис. 51](https://i.bukva.ai/vGK4af1Oj/img_50.png) | <a id="p100366"></a>22.08.2018 | <a id="p100367"></a>BOEING | <a id="p100368"></a>787 | <a id="p100369"></a>Ice and Rain Protection - Cabin Air Compressor Inlet Ice Protection System Wiring - Modification |
| <a id="p100370"></a>52 | <a id="p100371"></a>2018-0177 | <a id="p100372"></a>![рис. 52](https://i.bukva.ai/vGK4af1Oj/img_51.png) | <a id="p100373"></a>21.08.2018 | <a id="p100374"></a>AIRBUS HELICOPTERS | <a id="p100375"></a>EC175 | <a id="p100376"></a>Rotor Drive - Main Gearbox Magnetic Plugs - Inspection |
| <a id="p100377"></a>53 | <a id="p100378"></a>US-2018-17-04 | <a id="p100379"></a>![рис. 53](https://i.bukva.ai/vGK4af1Oj/img_52.png) | <a id="p100380"></a>21.08.2018 | <a id="p100381"></a>ROLLS-ROYCE CORPORATION (USA) | <a id="p100382"></a>AE 2100, AE 3007 | <a id="p100383"></a>Engine - Turbine Wheels - Removal/Replacement |
| <a id="p100384"></a>54 | <a id="p100385"></a>2018-0176 | <a id="p100386"></a>![рис. 54](https://i.bukva.ai/vGK4af1Oj/img_53.png) | <a id="p100387"></a>21.08.2018 | <a id="p100388"></a>AIRBUS HELICOPTERS | <a id="p100389"></a>SA 365/366/AS 365/EC 155 | <a id="p100390"></a>Main Rotor Drive - Main Gearbox Magnetic Plug - Replacement |
| <a id="p100391"></a>55 | <a id="p100392"></a>US-2018-13-06 | <a id="p100393"></a>![рис. 55](https://i.bukva.ai/vGK4af1Oj/img_54.png) | <a id="p100394"></a>15.08.2018 | <a id="p100395"></a>BOEING | <a id="p100396"></a>767 | <a id="p100397"></a>Wings - Lower Outboard Wing Skin - Inspection |
| <a id="p100398"></a>56 | <a id="p100399"></a>2018-0175-E | <a id="p100400"></a>![рис. 56](https://i.bukva.ai/vGK4af1Oj/img_55.png) | <a id="p100401"></a>15.08.2018 | <a id="p100402"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100403"></a>AB206 | <a id="p100404"></a>Engine - Power Turbine Limitations - Operational Limitation |
| <a id="p100405"></a>57 | <a id="p100406"></a>US-2018-14-06 | <a id="p100407"></a>![рис. 57](https://i.bukva.ai/vGK4af1Oj/img_56.png) | <a id="p100408"></a>15.08.2018 | <a id="p100409"></a>AMERICAN CHAMPION AIRCRAFT CORP | <a id="p100410"></a>8 series | <a id="p100411"></a>Wings - Aileron Hinge Support - Inspection/Installation |
| <a id="p100412"></a>58 | <a id="p100413"></a>CF-2018-22 | <a id="p100414"></a>![рис. 58](https://i.bukva.ai/vGK4af1Oj/img_57.png) | <a id="p100415"></a>15.08.2018 | <a id="p100416"></a>BOMBARDIER | <a id="p100417"></a>BD-700 | <a id="p100418"></a>Electrical Power - Variable Frequency Generator Harness Low Clearance to Hydraulic/Fuel Lines |
| <a id="p100419"></a>59 | <a id="p100420"></a>2018-0174 | <a id="p100421"></a>![рис. 59](https://i.bukva.ai/vGK4af1Oj/img_58.png) | <a id="p100422"></a>14.08.2018 | <a id="p100423"></a>AIRBUS | <a id="p100424"></a>A310 | <a id="p100425"></a>Wings - Top Skin Stringer Joints at Rib 19 - Inspection/Modification |
| <a id="p100426"></a>60 | <a id="p100427"></a>US-2018-16-06 | <a id="p100428"></a>![рис. 60](https://i.bukva.ai/vGK4af1Oj/img_59.png) | <a id="p100429"></a>09.08.2018 | <a id="p100430"></a>BOEING | <a id="p100431"></a>747 | <a id="p100432"></a>Fuselage - Boeing Material Specification (BMS) 8-39 Flexible Urethanc Foam - Inspection/Modification/Replacement |
| <a id="p100433"></a>61 | <a id="p100434"></a>US-2018-16-07 | <a id="p100435"></a>![рис. 61](https://i.bukva.ai/vGK4af1Oj/img_60.png) | <a id="p100436"></a>09.08.2018 | <a id="p100437"></a>GENERAL ELECTRIC | <a id="p100438"></a>GEnx | <a id="p100439"></a>Engine - High-Pressure Turbine (HPT) Stator Cases - Removal/Replacement |
| <a id="p100440"></a>62 | <a id="p100441"></a>2018-0173-E | <a id="p100442"></a>![рис. 62](https://i.bukva.ai/vGK4af1Oj/img_61.png) | <a id="p100443"></a>08.08.2018 | <a id="p100444"></a>AIRBUS HELICOPTERS | <a id="p100445"></a>EC175, SA 330/AS 332/EC 225, SA 365/366/AS 365/EC 155 | <a id="p100446"></a>Equipment & Furnishings - Hoist Carrier Assembly - Inspection |
| <a id="p100447"></a>63 | <a id="p100448"></a>US-2018-15-06 | <a id="p100449"></a>![рис. 63](https://i.bukva.ai/vGK4af1Oj/img_62.png) | <a id="p100450"></a>08.08.2018 | <a id="p100451"></a>HONDA AIRCRAFT COMPANY LLC | <a id="p100452"></a>HA-420 | <a id="p100453"></a>Time Limits - Airworthiness Limitations - Revision |
| <a id="p100454"></a>64 | <a id="p100455"></a>CF-2018-20 | <a id="p100456"></a>![рис. 64](https://i.bukva.ai/vGK4af1Oj/img_63.png) | <a id="p100457"></a>08.08.2018 | <a id="p100458"></a>BOMBARDIER | <a id="p100459"></a>BD-100 | <a id="p100460"></a>Landing Gear - Main Landing Gear Side Brace Actuators Contain Non-Conforming Split Ball Bearing |
| <a id="p100461"></a>65 | <a id="p100462"></a>US-2018-16-05 | <a id="p100463"></a>![рис. 65](https://i.bukva.ai/vGK4af1Oj/img_64.png) | <a id="p100464"></a>07.08.2018 | <a id="p100465"></a>BOEING | <a id="p100466"></a>757 | <a id="p100467"></a>Wings - Wing Skin/Shim - Inspection |
| <a id="p100468"></a>66 | <a id="p100469"></a>2018-0172 | <a id="p100470"></a>![рис. 66](https://i.bukva.ai/vGK4af1Oj/img_65.png) | <a id="p100471"></a>07.08.2018 | <a id="p100472"></a>AIRBUS HELICOPTERS | <a id="p100473"></a>SA 330/AS 332/EC 225 | <a id="p100474"></a>Main Rotor Blade Attachment Pin - Inspection |
| <a id="p100475"></a>67 | <a id="p100476"></a>CF-2018-21 | <a id="p100477"></a>![рис. 67](https://i.bukva.ai/vGK4af1Oj/img_66.png) | <a id="p100478"></a>07.08.2018 | <a id="p100479"></a>BOMBARDIER | <a id="p100480"></a>DHC-8 | <a id="p100481"></a>Wings - Cracked Spoiler Actuator Bracket |
| <a id="p100482"></a>68 | <a id="p100483"></a>2018-0171-E | <a id="p100484"></a>![рис. 68](https://i.bukva.ai/vGK4af1Oj/img_67.png) | <a id="p100485"></a>06.08.2018 | <a id="p100486"></a>AIRBUS | <a id="p100487"></a>A380 | <a id="p100488"></a>Airplane Flight, Manual - Air Conditioning/Engine Bleed Air System - Amendment |
| <a id="p100489"></a>69 | <a id="p100490"></a>2018-0170 | <a id="p100491"></a>![рис. 69](https://i.bukva.ai/vGK4af1Oj/img_68.png) | <a id="p100492"></a>06.08.2018 | <a id="p100493"></a>AIRBUS | <a id="p100494"></a>A300, A300-600, A300-600ST (Beluga) | <a id="p100495"></a>Landing Gear - Main Landing Gear Hinge Arm/Barrel Pin - Inspection |
| <a id="p100496"></a>70 | <a id="p100497"></a>US-2018-14-02 | <a id="p100498"></a>![рис. 70](https://i.bukva.ai/vGK4af1Oj/img_69.png) | <a id="p100499"></a>01.08.2018 | <a id="p100500"></a>BOEING | <a id="p100501"></a>777 | <a id="p100502"></a>Equipment/Furnishings - Foam Insulation on the Dripshield & Overhead Panel Support Structure - Inspection/Replacement |
| <a id="p100503"></a>71 | <a id="p100504"></a>2018-0167R1 | <a id="p100505"></a>![рис. 71](https://i.bukva.ai/vGK4af1Oj/img_70.png) | <a id="p100506"></a>01.08.2018 | <a id="p100507"></a>ROLLS-ROYCE PLC | <a id="p100508"></a>TRENT 1000 | <a id="p100509"></a>Engine - Intermediate Pressure Compressor Blades/Shafts - Inspection |
| <a id="p100510"></a>72 | <a id="p100511"></a>US-2018-14-12 | <a id="p100512"></a>![рис. 72](https://i.bukva.ai/vGK4af1Oj/img_71.png) | <a id="p100513"></a>30.07.2018 | <a id="p100514"></a>GENERAL ELECTRIC | <a id="p100515"></a>GEnx | <a id="p100516"></a>Engine - Air/Oil Extension Duct - Removal/Replacement |


<a id="p100517"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100518"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100519"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

<div align="right">

<a id="p100520"></a>Начальник<br>
Управления поддержания летной<br>
годности воздушных судов<br>
В.В.КУДИНОВ

</div>




<a id="p100521"></a>

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