---
title: "<Письмо> Росавиации от 25.05.2017 N Исх-11516/03"
number: "Исх-11516/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2017-05-25
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-1151603"
---

## <Письмо> Росавиации от 25.05.2017 N Исх-11516/03

# <Письмо> Росавиации от 25.05.2017 N Исх-11516/03

"Информационное письмо ДЛГ-04-2017"


<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 25 мая 2017 г. N Исх-11516/03**

<div align="center">

<a id="p100004"></a>**ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-04-2017**

</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 с 09 апреля по 19 мая 2017 года:**


| <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>Изготовитель ВС | <a id="p100011"></a>Тип ВС<br>(Классификация ВС, страны выпустившей ДЛГ) | <a id="p100012"></a>Краткое содержание |
| --- | --- | --- | --- | --- | --- | --- |
| <a id="p100013"></a>1 | <a id="p100014"></a>2017-0092-E | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/bOpVNoIpH/img_0.png) | <a id="p100016"></a>19.05.2017 | <a id="p100017"></a>DUC, SOCIETE | <a id="p100018"></a>FLAIR-2 | <a id="p100019"></a>Propellers - Removal from Service |
| <a id="p100020"></a>2 | <a id="p100021"></a>2017-0091 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/bOpVNoIpH/img_1.png) | <a id="p100023"></a>19.05.2017 | <a id="p100024"></a>AIRBUS | <a id="p100025"></a>A318, A319, A320, A321, A330, A340 | <a id="p100026"></a>Navigation - Traffic Collision Avoidance System Processor - Modification (Software Update)/Replacement |
| <a id="p100027"></a>3 | <a id="p100028"></a>CF-2017-17 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/bOpVNoIpH/img_2.png) | <a id="p100030"></a>19.05.2017 | <a id="p100031"></a>VIKING AIR LTD | <a id="p100032"></a>DHC-2 | <a id="p100033"></a>Wing - Cracking of Flap and Aileron hinge arm support brackets and Rear Spar Web |
| <a id="p100034"></a>4 | <a id="p100035"></a>CF-2016-36R1 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/bOpVNoIpH/img_3.png) | <a id="p100037"></a>17.05.2017 | <a id="p100038"></a>BOMBARDIER | <a id="p100039"></a>DHC-8 | <a id="p100040"></a>Landing Gear - Main Landing Gear Retraction Actuator Rod-End Failure |
| <a id="p100041"></a>5 | <a id="p100042"></a>CF-2017-15 | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/bOpVNoIpH/img_4.png) | <a id="p100044"></a>17.05.2017 | <a id="p100045"></a>BOMBARDIER | <a id="p100046"></a>DHC-8 | <a id="p100047"></a>Landing Gear - Main Landing Gear Up-Lock Assembly Latch Wear - Introduction of One-Star Certification Maintenance Requirement Task 323100-102 |
| <a id="p100048"></a>6 | <a id="p100049"></a>2017-0089 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/bOpVNoIpH/img_5.png) | <a id="p100051"></a>17.05.2017 | <a id="p100052"></a>AIRBUS HELICOPTERS | <a id="p100053"></a>AS 350/EC 130, AS 355 | <a id="p100054"></a>Main Rotor - MR Mast Upper Bearing Lubrication/MR Mast Jet Oil Hose - Inspection |
| <a id="p100055"></a>7 | <a id="p100056"></a>US-2017-08-01 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/bOpVNoIpH/img_6.png) | <a id="p100058"></a>17.05.2017 | <a id="p100059"></a>GULFSTREAM AEROSPACE CORPORATION | <a id="p100060"></a>GV | <a id="p100061"></a>Fuel - Fuel Boost Pump - Inspection/Replacement - Airplane Maintenance Program - Revision |
| <a id="p100062"></a>8 | <a id="p100063"></a>2017-0090 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/bOpVNoIpH/img_7.png) | <a id="p100065"></a>17.05.2017 | <a id="p100066"></a>DIAMOND AIRCRAFT INDUSTRIES | <a id="p100067"></a>DA 42/62 | <a id="p100068"></a>Engine Exhaust - Exhaust Pipes - Modification/Inspection |
| <a id="p100069"></a>9 | <a id="p100070"></a>2017-0088 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/bOpVNoIpH/img_8.png) | <a id="p100072"></a>16.05.2017 | <a id="p100073"></a>ROLLS-ROYCE PLC | <a id="p100074"></a>TRENT XWB | <a id="p100075"></a>Engine - Intermediate Pressure Turbine Stage 2 Locking Plates - Inspection |
| <a id="p100076"></a>10 | <a id="p100077"></a>CF-2017-07R1 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/bOpVNoIpH/img_9.png) | <a id="p100079"></a>16.05.2017 | <a id="p100080"></a>BOMBARDIER | <a id="p100081"></a>CL-600 (Challenger) | <a id="p100082"></a>Cold Weather Operations - Introduction of Low Temperature Ground Wing Anti-Ice System |
| <a id="p100083"></a>11 | <a id="p100084"></a>2016-0036-CN | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/bOpVNoIpH/img_10.png) | <a id="p100086"></a>15.05.2017 | <a id="p100087"></a>ROLLS-ROYCE PLC | <a id="p100088"></a>TRENT XWB | <a id="p100089"></a>CANCELLED: Engine - Low Pressure Compressor/Shaft Attachment - Inspection |
| <a id="p100090"></a>12 | <a id="p100091"></a>US-2017-08-07 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/bOpVNoIpH/img_11.png) | <a id="p100093"></a>15.05.2017 | <a id="p100094"></a>LEARJET, INC. | <a id="p100095"></a>60 | <a id="p100096"></a>Fuselage - Fuselage Skin - Inspection |
| <a id="p100097"></a>13 | <a id="p100098"></a>US-2017-07-06 | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/bOpVNoIpH/img_12.png) | <a id="p100100"></a>15.05.2017 | <a id="p100101"></a>GULFSTREAM AEROSPACE CORPORATION | <a id="p100102"></a>G-1159 | <a id="p100103"></a>Flight Controls - Rudder Assembly - Inspection/Replacement - Modification |
| <a id="p100104"></a>14 | <a id="p100105"></a>2017-0087 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/bOpVNoIpH/img_13.png) | <a id="p100107"></a>12.05.2017 | <a id="p100108"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100109"></a>AW189 | <a id="p100110"></a>Main Rotor - Main Rotor Slip Ring - Inspection/Replacement |
| <a id="p100111"></a>15 | <a id="p100112"></a>2017-0086 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/bOpVNoIpH/img_14.png) | <a id="p100114"></a>12.05.2017 | <a id="p100115"></a>DIAMOND AIRCRAFT INDUSTRIES | <a id="p100116"></a>DA 40 | <a id="p100117"></a>Engine Controls - Electronic Control Unit - Modification |
| <a id="p100118"></a>16 | <a id="p100119"></a>2017-0084 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/bOpVNoIpH/img_15.png) | <a id="p100121"></a>12.05.2017 | <a id="p100122"></a>CFM INTERNATIONAL | <a id="p100123"></a>CFM56-5, CFM56-5B | <a id="p100124"></a>Engine - Radial Drive Shaft - Replacement |
| <a id="p100125"></a>17 | <a id="p100126"></a>2017-0085-E | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/bOpVNoIpH/img_16.png) | <a id="p100128"></a>12.05.2017 | <a id="p100129"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100130"></a>A109/A119 | <a id="p100131"></a>Stabilizers - Elevator Assembly - Inspections |
| <a id="p100132"></a>18 | <a id="p100133"></a>US-2017-07-09 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/bOpVNoIpH/img_17.png) | <a id="p100135"></a>10.05.2017 | <a id="p100136"></a>SIKORSKY | <a id="p100137"></a>S-92 | <a id="p100138"></a>Tail Rotor Drive - Tail Gearbox Center Housing - Removal from Service (Retirement Life) |
| <a id="p100139"></a>19 | <a id="p100140"></a>2017-0083 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/bOpVNoIpH/img_18.png) | <a id="p100142"></a>10.05.2017 | <a id="p100143"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100144"></a>AB139/AW139 | <a id="p100145"></a>Main Rotor - Main Rotor Slip Ring - Inspection/Replacement |
| <a id="p100146"></a>20 | <a id="p100147"></a>US-2017-09-06 | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/bOpVNoIpH/img_19.png) | <a id="p100149"></a>08.05.2017 | <a id="p100150"></a>GENERAL ELECTRIC | <a id="p100151"></a>GEnx | <a id="p100152"></a>Engine Controls - Full Authority Digital Engine Control (FADEC) Software |
| <a id="p100153"></a>21 | <a id="p100154"></a>2017-0081 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/bOpVNoIpH/img_20.png) | <a id="p100156"></a>08.05.2017 | <a id="p100157"></a>AIRBUS | <a id="p100158"></a>A310 | <a id="p100159"></a>Wing - Wing Top Skin Panel Attachments at Rib 2 and Rib 3 - Inspection/Repair/Modification |
| <a id="p100160"></a>22 | <a id="p100161"></a>2017-0082 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/bOpVNoIpH/img_21.png) | <a id="p100163"></a>08.05.2017 | <a id="p100164"></a>AIRBUS | <a id="p100165"></a>A300, A300-600, A310 | <a id="p100166"></a>Fuselage - Bulk Cargo Door - Inspection/Repair |
| <a id="p100167"></a>23 | <a id="p100168"></a>2007-0242R1 | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/bOpVNoIpH/img_22.png) | <a id="p100170"></a>08.05.2017 | <a id="p100171"></a>AIRBUS | <a id="p100172"></a>A310 | <a id="p100173"></a>Wings - Outer Wings Structural Fatigue - Inspection/Modification |
| <a id="p100174"></a>24 | <a id="p100175"></a>2017-0080 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/bOpVNoIpH/img_23.png) | <a id="p100177"></a>05.05.2017 | <a id="p100178"></a>AIRBUS HELICOPTERS | <a id="p100179"></a>AS 350/EC 130 | <a id="p100180"></a>Fuselage - Tail Boom/Fenestron Junction Frame - Inspection |
| <a id="p100181"></a>25 | <a id="p100182"></a>2017-0075R1 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/bOpVNoIpH/img_24.png) | <a id="p100184"></a>05.05.2017 | <a id="p100185"></a>ROLLS-ROYCE PLC | <a id="p100186"></a>RB211 TRENT 900 | <a id="p100187"></a>Powerplant - Drains Mast - Inspection/Replacement |
| <a id="p100188"></a>26 | <a id="p100189"></a>2017-0077 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/bOpVNoIpH/img_25.png) | <a id="p100191"></a>03.05.2017 | <a id="p100192"></a>AIRBUS HELICOPTERS | <a id="p100193"></a>SA 330/AS 332/EC 225 | <a id="p100194"></a>Rotorcraft Flight Manual/Emergency Procedures - Amendment |
| <a id="p100195"></a>27 | <a id="p100196"></a>2017-0078 | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/bOpVNoIpH/img_26.png) | <a id="p100198"></a>03.05.2017 | <a id="p100199"></a>AIRBUS | <a id="p100200"></a>A330 | <a id="p100201"></a>Stabilizers - Horizontal Stabilizer/Center Box Top Skin - Inspection/Repair |
| <a id="p100202"></a>28 | <a id="p100203"></a>2017-0076 | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/bOpVNoIpH/img_27.png) | <a id="p100205"></a>03.05.2017 | <a id="p100206"></a>AIRBUS | <a id="p100207"></a>A380 | <a id="p100208"></a>Time Limits / Maintenance Checks - System Equipment Maintenance Requirements - ALS Part 4 - Amendment |
| <a id="p100209"></a>29 | <a id="p100210"></a>CF-2017-14 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/bOpVNoIpH/img_28.png) | <a id="p100212"></a>02.05.2017 | <a id="p100213"></a>BOMBARDIER | <a id="p100214"></a>CL-600 (Regional Jet) | <a id="p100215"></a>Landing Gear - Failure of Main Landing Gear Shimmy Damper Belleville Washers |
| <a id="p100216"></a>30 | <a id="p100217"></a>US-2017-08-08 | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/bOpVNoIpH/img_29.png) | <a id="p100219"></a>28.04.2017 | <a id="p100220"></a>CFE COMPANY | <a id="p100221"></a>CFE738 | <a id="p100222"></a>Engine - High-Pressure Compressor (HPC) Impeller - Removal/Replacement |
| <a id="p100223"></a>31 | <a id="p100224"></a>2017-0074 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/bOpVNoIpH/img_30.png) | <a id="p100226"></a>28.04.2017 | <a id="p100227"></a>DIAMOND AIRCRAFT INDUSTRIES | <a id="p100228"></a>DA 42/62 | <a id="p100229"></a>Flight Controls - Flap Control System/Bell Crank Assembly - Inspection/Modifcation |
| <a id="p100230"></a>32 | <a id="p100231"></a>2015-0234-CN | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/bOpVNoIpH/img_31.png) | <a id="p100233"></a>28.04.2017 | <a id="p100234"></a>AIRBUS | <a id="p100235"></a>A319, A320, A321 | <a id="p100236"></a>CANCELLED: Doors - Main Landing Gear Door Tie Rod Assembly - Inspection |
| <a id="p100237"></a>33 | <a id="p100238"></a>2017-0073 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/bOpVNoIpH/img_32.png) | <a id="p100240"></a>27.04.2017 | <a id="p100241"></a>BAE SYSTEMS (OPERATIONS) LTD | <a id="p100242"></a>JETSTREAM3100, JETSTREAM3200 | <a id="p100243"></a>Time Limits / Maintenance Checks - Corrosion Prevention and Control Programme - Amendment |
| <a id="p100244"></a>34 | <a id="p100245"></a>2017-0071 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/bOpVNoIpH/img_33.png) | <a id="p100247"></a>26.04.2017 | <a id="p100248"></a>ROLLS-ROYCE PLC | <a id="p100249"></a>RB211 TRENT 700 | <a id="p100250"></a>Engine - Compressor Intermediate Case - Inspection/Repair |
| <a id="p100251"></a>35 | <a id="p100252"></a>2017-0072-E | <a id="p100253"></a>![рис. 35](https://i.bukva.ai/bOpVNoIpH/img_34.png) | <a id="p100254"></a>26.04.2017 | <a id="p100255"></a>STEMME AG | <a id="p100256"></a>S10, S12 | <a id="p100257"></a>Propeller - Gearbox - Replacement/Modification |
| <a id="p100258"></a>36 | <a id="p100259"></a>2013-0306-CN | <a id="p100260"></a>![рис. 36](https://i.bukva.ai/bOpVNoIpH/img_35.png) | <a id="p100261"></a>26.04.2017 | <a id="p100262"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100263"></a>EC135/635 | <a id="p100264"></a>CANCELLED: Fuel - Fuel System/Supply Tank Indication - Check |
| <a id="p100265"></a>37 | <a id="p100266"></a>2006-0318R2 | <a id="p100267"></a>![рис. 37](https://i.bukva.ai/bOpVNoIpH/img_36.png) | <a id="p100268"></a>25.04.2017 | <a id="p100269"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100270"></a>EC135/635 | <a id="p100271"></a>Rotorcraft Flight Control - Tail Rotor Control Linear Transducer (LVDT Collective) Bearing - Inspection/Replacement and Rod and Floor Modification |
| <a id="p100272"></a>38 | <a id="p100273"></a>2017-0069 | <a id="p100274"></a>![рис. 38](https://i.bukva.ai/bOpVNoIpH/img_37.png) | <a id="p100275"></a>25.04.2017 | <a id="p100276"></a>AIRBUS | <a id="p100277"></a>A330, A340 | <a id="p100278"></a>Wings - Centre Wing Box Fastener Holes at Frame 40 Vertical Web - Inspection/Modification |
| <a id="p100279"></a>39 | <a id="p100280"></a>US-2017-05-51 | <a id="p100281"></a>![рис. 39](https://i.bukva.ai/bOpVNoIpH/img_38.png) | <a id="p100282"></a>25.04.2017 | <a id="p100283"></a>AIR COMM CORPORATION, BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100284"></a>EASA STC 10028717, STC SR00693DE, 429 | <a id="p100285"></a>[Final Rule] Air Conditioning - Condenser Blower-to-Motor Attachment - Inspection/Deactivation |
| <a id="p100286"></a>40 | <a id="p100287"></a>2011-0070 | <a id="p100288"></a>![рис. 40](https://i.bukva.ai/bOpVNoIpH/img_39.png) | <a id="p100289"></a>25.04.2017 | <a id="p100290"></a>SAFRAN HELICOPTER ENGINES | <a id="p100291"></a>ARRIUS 2 | <a id="p100292"></a>Engine Fuel & Control - Pipe Injector Preferred Assembly - Replacement |
| <a id="p100293"></a>41 | <a id="p100294"></a>CF-2016-01R2 | <a id="p100295"></a>![рис. 41](https://i.bukva.ai/bOpVNoIpH/img_40.png) | <a id="p100296"></a>25.04.2017 | <a id="p100297"></a>BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100298"></a>429 | <a id="p100299"></a>Tail Rotor - Pitch Link Corrosion |
| <a id="p100300"></a>42 | <a id="p100301"></a>2017-0067 | <a id="p100302"></a>![рис. 42](https://i.bukva.ai/bOpVNoIpH/img_41.png) | <a id="p100303"></a>24.04.2017 | <a id="p100304"></a>SAAB AB, AERONAUTICS | <a id="p100305"></a>340 | <a id="p100306"></a>Flight Controls - Stall Warning and Identification System/Stall Warning Computer - Modification/Replacement |
| <a id="p100307"></a>43 | <a id="p100308"></a>2017-0068 | <a id="p100309"></a>![рис. 43](https://i.bukva.ai/bOpVNoIpH/img_42.png) | <a id="p100310"></a>24.04.2017 | <a id="p100311"></a>FOKKER SERVICES | <a id="p100312"></a>F28 | <a id="p100313"></a>Landing Gear - Landing Gear Handle Teleflex Mechanism - Inspection/Lubrication |
| <a id="p100314"></a>44 | <a id="p100315"></a>BR-2017-04-01 | <a id="p100316"></a>![рис. 44](https://i.bukva.ai/bOpVNoIpH/img_43.png) | <a id="p100317"></a>24.04.2017 | <a id="p100318"></a>EMBRAER | <a id="p100319"></a>ERJ-190 | <a id="p100320"></a>Nacelles/Pylons - Pylon Lower Link Fittings - Modification |
| <a id="p100321"></a>45 | <a id="p100322"></a>2017-0066-E | <a id="p100323"></a>![рис. 45](https://i.bukva.ai/bOpVNoIpH/img_44.png) | <a id="p100324"></a>21.04.2017 | <a id="p100325"></a>AIRBUS HELICOPTERS | <a id="p100326"></a>AS 350/EC 130 | <a id="p100327"></a>Fuselage - Tail Boom/Fenestron Junction Frame - Inspection |
| <a id="p100328"></a>46 | <a id="p100329"></a>2017-0048 | <a id="p100330"></a>![рис. 46](https://i.bukva.ai/bOpVNoIpH/img_45.png) | <a id="p100331"></a>20.04.2017 | <a id="p100332"></a>AIRBUS | <a id="p100333"></a>A300-600, A310 | <a id="p100334"></a>[Correction] Fuselage - Aft Cargo Door Sill Beam Area - Inspection/Modification |
| <a id="p100335"></a>47 | <a id="p100336"></a>2017-0065 | <a id="p100337"></a>![рис. 47](https://i.bukva.ai/bOpVNoIpH/img_46.png) | <a id="p100338"></a>19.04.2017 | <a id="p100339"></a>CFM INTERNATIONAL | <a id="p100340"></a>CFM56-5, CFM56-5B | <a id="p100341"></a>Engine Fuel and Control - Hydro-Mechanical Units - Operational Limitations |
| <a id="p100342"></a>48 | <a id="p100343"></a>US-2017-07-04 | <a id="p100344"></a>![рис. 48](https://i.bukva.ai/bOpVNoIpH/img_47.png) | <a id="p100345"></a>18.04.2017 | <a id="p100346"></a>GENERAL ELECTRIC | <a id="p100347"></a>GE90 | <a id="p100348"></a>Engine - High Pressure Compressor (HPC) Rotor Stage 2-5 Spools - Removal |
| <a id="p100349"></a>49 | <a id="p100350"></a>US-2017-08-06 | <a id="p100351"></a>![рис. 49](https://i.bukva.ai/bOpVNoIpH/img_48.png) | <a id="p100352"></a>18.04.2017 | <a id="p100353"></a>GENERAL ELECTRIC | <a id="p100354"></a>GE90 | <a id="p100355"></a>Engine Oil - Fuel/Oil Lube/Servo Coolers (Main Fuel Oil Heat Exchangers") - Replacement" |
| <a id="p100356"></a>50 | <a id="p100357"></a>US-2017-08-05 | <a id="p100358"></a>![рис. 50](https://i.bukva.ai/bOpVNoIpH/img_49.png) | <a id="p100359"></a>18.04.2017 | <a id="p100360"></a>GENERAL<br>ELECTRIC | <a id="p100361"></a>GE90 | <a id="p100362"></a>Engine - High-Pressure Compressor (HPC) Stage 8-10 Spool - Inspection |
| <a id="p100363"></a>51 | <a id="p100364"></a>2013-0170R1 | <a id="p100365"></a>![рис. 51](https://i.bukva.ai/bOpVNoIpH/img_50.png) | <a id="p100366"></a>18.04.2017 | <a id="p100367"></a>SAFRAN HELICOPTER ENGINES | <a id="p100368"></a>ARRIEL 2 | <a id="p100369"></a>Engine Fuel & Control - Hydro-Mechanical Metering Unit - Inspection/Replacement |
| <a id="p100370"></a>52 | <a id="p100371"></a>2017-0064-E | <a id="p100372"></a>![рис. 52](https://i.bukva.ai/bOpVNoIpH/img_51.png) | <a id="p100373"></a>12.04.2017 | <a id="p100374"></a>SAFRAN HELICOPTER ENGINES | <a id="p100375"></a>ARRIEL 1 | <a id="p100376"></a>Engine Fuel & Control - Drain Valve Assembly - Inspection/Replacement |
| <a id="p100377"></a>53 | <a id="p100378"></a>US-2017-07-10 | <a id="p100379"></a>![рис. 53](https://i.bukva.ai/bOpVNoIpH/img_52.png) | <a id="p100380"></a>12.04.2017 | <a id="p100381"></a>AMERICAN CHAMPION AIRCRAFT CORP | <a id="p100382"></a>8 series | <a id="p100383"></a>Placards - Acrobatic Flight Prohibited - Installation//Wings - Aileron Hinge Rib and Support - Inspection |
| <a id="p100384"></a>54 | <a id="p100385"></a>2017-0063 | <a id="p100386"></a>![рис. 54](https://i.bukva.ai/bOpVNoIpH/img_53.png) | <a id="p100387"></a>12.04.2017 | <a id="p100388"></a>AIRBUS | <a id="p100389"></a>A330, A340 | <a id="p100390"></a>Fuselage - Frame 40 Skin Panel Junction - Inspection |
| <a id="p100391"></a>55 | <a id="p100392"></a>CF-2015-16R2 | <a id="p100393"></a>![рис. 55](https://i.bukva.ai/bOpVNoIpH/img_54.png) | <a id="p100394"></a>11.04.2017 | <a id="p100395"></a>BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100396"></a>429 | <a id="p100397"></a>Tail Rotor - Pitch Link Spherical Bearing Accelerated Wear |
| <a id="p100398"></a>56 | <a id="p100399"></a>US-2017-06-09 | <a id="p100400"></a>![рис. 56](https://i.bukva.ai/bOpVNoIpH/img_55.png) | <a id="p100401"></a>11.04.2017 | <a id="p100402"></a>BOEING | <a id="p100403"></a>787 | <a id="p100404"></a>Equipment/Furnishings - Closets/Video Stations - Fire Blok Installation Fuselage - Main Passenger Cabin Floor Panel Openings - Fire Blocking Tape Installation |
| <a id="p100405"></a>57 | <a id="p100406"></a>2017-0062 | <a id="p100407"></a>![рис. 57](https://i.bukva.ai/bOpVNoIpH/img_56.png) | <a id="p100408"></a>11.04.2017 | <a id="p100409"></a>AIRBUS HELICOPTERS | <a id="p100410"></a>AS 350/EC 130 | <a id="p100411"></a>Rotors Flight Control - Collective Pitch Control - Inspection |


<a id="p100412"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100413"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100414"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

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<a id="p100415"></a>Начальник Управления<br>
поддержания летной годности<br>
воздушных судов<br>
В.В.КУДИНОВ

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