---
title: "<Письмо> Росавиации от 20.04.2017 N Исх-8707/03"
number: "Исх-8707/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2017-04-20
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-870703"
---

## <Письмо> Росавиации от 20.04.2017 N Исх-8707/03

# <Письмо> Росавиации от 20.04.2017 N Исх-8707/03

"Информационное письмо ДЛГ-03-2017"


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

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

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<a id="p100003"></a>**ПИСЬМО**
**от 20 апреля 2017 г. N Исх-8707/03**

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<a id="p100004"></a>**ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-03-2017**

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<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 12 марта по 09 апреля 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>2017-0060 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/318ZVcmBJ/img_0.png) | <a id="p100016"></a>2017-04-07 | <a id="p100017"></a>AIRBUS | <a id="p100018"></a>A330, A340 | <a id="p100019"></a>Wings - Slat Track Front Stop Attachment - Inspection |
| <a id="p100020"></a>2 | <a id="p100021"></a>2010-0227R1 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/318ZVcmBJ/img_1.png) | <a id="p100023"></a>2017-04-07 | <a id="p100024"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100025"></a>EC 135/635 | <a id="p100026"></a>Rotorcraft Flight Control - Tail Rotor Rod and Ball Pivot - Inspection/Replacement |
| <a id="p100027"></a>3 | <a id="p100028"></a>2010-0058R1 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/318ZVcmBJ/img_2.png) | <a id="p100030"></a>2017-04-07 | <a id="p100031"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100032"></a>EC135/635, MBB-BK 117 | <a id="p100033"></a>Rotor Flight Controls - Tail Rotor, Cyclic and Collective Control Levers - Inspection/Repair |
| <a id="p100034"></a>4 | <a id="p100035"></a>2017-0061 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/318ZVcmBJ/img_3.png) | <a id="p100037"></a>2017-04-07 | <a id="p100038"></a>SAFRAN HELICOPTER ENGINES | <a id="p100039"></a>ARRIEL 1 | <a id="p100040"></a>Engine - Front Support Pins - Inspection/Replacement |
| <a id="p100041"></a>5 | <a id="p100042"></a>2017-0059 | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/318ZVcmBJ/img_4.png) | <a id="p100044"></a>2017-04-06 | <a id="p100045"></a>AIRBUS HELICOPTERS | <a id="p100046"></a>AS 350/EC 130 | <a id="p100047"></a>Engine Controls - Switches 53Ka, 53Kb and 65K - Inspection/Modification |
| <a id="p100048"></a>6 | <a id="p100049"></a>2017-0058 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/318ZVcmBJ/img_5.png) | <a id="p100051"></a>2017-04-06 | <a id="p100052"></a>WSK PZL - SWIDNIK S.A. | <a id="p100053"></a>PZL W-3A | <a id="p100054"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section - Amendment |
| <a id="p100055"></a>7 | <a id="p100056"></a>2017-0057 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/318ZVcmBJ/img_6.png) | <a id="p100058"></a>2017-04-06 | <a id="p100059"></a>WSK PZL - SWIDNIK S.A. | <a id="p100060"></a>PZL W-3A | <a id="p100061"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section - Amendment |
| <a id="p100062"></a>8 | <a id="p100063"></a>2017-0056 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/318ZVcmBJ/img_7.png) | <a id="p100065"></a>2017-04-05 | <a id="p100066"></a>ROLLS-ROYCE PLC | <a id="p100067"></a>TRENT 1000 | <a id="p100068"></a>Engine - Intermediate Pressure Turbine Blades - Inspection/Replacement |
| <a id="p100069"></a>9 | <a id="p100070"></a>CF-2011-41R1 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/318ZVcmBJ/img_8.png) | <a id="p100072"></a>2017-04-04 | <a id="p100073"></a>BOMBARDIER | <a id="p100074"></a>BD-100 | <a id="p100075"></a>Hydraulic Accumulators - Screw Cap/End Cap Failure |
| <a id="p100076"></a>10 | <a id="p100077"></a>US-2017-07-02 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/318ZVcmBJ/img_9.png) | <a id="p100079"></a>2017-04-04 | <a id="p100080"></a>SIKORSKY | <a id="p100081"></a>269 | <a id="p100082"></a>Main Rotor Drive - Drive Shaft - Inspection/Life Limitation |
| <a id="p100083"></a>11 | <a id="p100084"></a>US-2017-06-03 | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/318ZVcmBJ/img_10.png) | <a id="p100086"></a>2017-04-04 | <a id="p100087"></a>APPLIANCES | <a id="p100088"></a>ATA 21 AIR CONDITIONING | <a id="p100089"></a>MEGGITT (TROY) INC. - Combustion Heaters - Inspection/Pressure Test/Deactivation/Removal |
| <a id="p100090"></a>12 | <a id="p100091"></a>2015-0124R3 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/318ZVcmBJ/img_11.png) | <a id="p100093"></a>2017-04-04 | <a id="p100094"></a>AIRBUS | <a id="p100095"></a>A330, A340 | <a id="p100096"></a>Flight Controls - Flight Control Primary Computer - Modification/Replacement |
| <a id="p100097"></a>13 | <a id="p100098"></a>US-2017-07-01 | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/318ZVcmBJ/img_12.png) | <a id="p100100"></a>2017-04-03 | <a id="p100101"></a>M7 AEROSPACE LLC | <a id="p100102"></a>SA226, SA227 | <a id="p100103"></a>Engine Controls - Engine-Propeller Pitch Control Assembly - Inspection/Replacement/Rework |
| <a id="p100104"></a>14 | <a id="p100105"></a>US-2017-05-07 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/318ZVcmBJ/img_13.png) | <a id="p100107"></a>2017-03-31 | <a id="p100108"></a>BOEING | <a id="p100109"></a>777 | <a id="p100110"></a>Engine Exhaust - Thrust Reverser (T/R) Halves - Installation |
| <a id="p100111"></a>15 | <a id="p100112"></a>2017-0055 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/318ZVcmBJ/img_14.png) | <a id="p100114"></a>2017-03-31 | <a id="p100115"></a>AIRBUS HELICOPTERS | <a id="p100116"></a>SA 365/366/AS 365/EC 155 | <a id="p100117"></a>Fuselage - Cowlings and Fairings - Inspection |
| <a id="p100118"></a>16 | <a id="p100119"></a>US-2017-06-01 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/318ZVcmBJ/img_15.png) | <a id="p100121"></a>2017-03-30 | <a id="p100122"></a>BOEING | <a id="p100123"></a>737 | <a id="p100124"></a>Fuselage - Aft Lower Lobe Skins - Inspection/Repair/Replacement |
| <a id="p100125"></a>17 | <a id="p100126"></a>US-2017-06-14 | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/318ZVcmBJ/img_16.png) | <a id="p100128"></a>2017-03-30 | <a id="p100129"></a>BOEING | <a id="p100130"></a>737 | <a id="p100131"></a>Stabilizers - Horizontal Stabilizer Lower Skin - Inspection |
| <a id="p100132"></a>18 | <a id="p100133"></a>CF-2014-45R2 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/318ZVcmBJ/img_17.png) | <a id="p100135"></a>2017-03-30 | <a id="p100136"></a>BOMBARDIER | <a id="p100137"></a>DHC-8 | <a id="p100138"></a>Nacelle - A-Frame Structure - Insufficient Fillet Radius and Fouling with Main Landing Gear Stabilizer Brace and the Electrical Wiring Harnesses |
| <a id="p100139"></a>19 | <a id="p100140"></a>US-2017-06-13 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/318ZVcmBJ/img_18.png) | <a id="p100142"></a>2017-03-29 | <a id="p100143"></a>TEXTRON AVIATION INC. | <a id="p100144"></a>680 | <a id="p100145"></a>Fuselage - Aft Canted Bulkhead - Inspection/Modification |
| <a id="p100146"></a>20 | <a id="p100147"></a>2017-0054 | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/318ZVcmBJ/img_19.png) | <a id="p100149"></a>2017-03-27 | <a id="p100150"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100151"></a>AW189 | <a id="p100152"></a>Windows - Bubble Window Kit - Modification/Inspection |
| <a id="p100153"></a>21 | <a id="p100154"></a>CF-2016-31R1 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/318ZVcmBJ/img_20.png) | <a id="p100156"></a>2017-03-27 | <a id="p100157"></a>BOMBARDIER | <a id="p100158"></a>DHC-8 | <a id="p100159"></a>Landing Gear - Dynamic Response of Main Landing Gear System to External Loads |
| <a id="p100160"></a>22 | <a id="p100161"></a>US-2017-04-01 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/318ZVcmBJ/img_21.png) | <a id="p100163"></a>2017-03-27 | <a id="p100164"></a>GULFSTREAM AEROSPACE CORPORATION | <a id="p100165"></a>GV1 | <a id="p100166"></a>Flight Controls - Flight Control Computer (FCC) Software - Update |
| <a id="p100167"></a>23 | <a id="p100168"></a>2017-0052 | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/318ZVcmBJ/img_22.png) | <a id="p100170"></a>2017-03-24 | <a id="p100171"></a>AIRBUS HELICOPTERS | <a id="p100172"></a>AS 350/EC 130 | <a id="p100173"></a>Engine Controls - Switches 53Ka, 53Kb and 65K - Inspection/Modification |
| <a id="p100174"></a>24 | <a id="p100175"></a>2017-0051 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/318ZVcmBJ/img_23.png) | <a id="p100177"></a>2017-03-24 | <a id="p100178"></a>AIRBUS | <a id="p100179"></a>A300, A300-600, A300-600ST (Beluga), A310 | <a id="p100180"></a>Fuel - Fuel Pump Canister Hood - Inspection/Replacement/Modification |
| <a id="p100181"></a>25 | <a id="p100182"></a>2017-0053 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/318ZVcmBJ/img_24.png) | <a id="p100184"></a>2017-03-24 | <a id="p100185"></a>BAE SYSTEMS (OPERATIONS) LTD | <a id="p100186"></a>JETSTREAM3100, JETSTREAM3200 | <a id="p100187"></a>[Correction] Landing Gear - Main Landing Gear/Pintle to Cylinder Interface - Inspection |
| <a id="p100188"></a>26 | <a id="p100189"></a>ISR-I-52-2017-03-28 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/318ZVcmBJ/img_25.png) | <a id="p100191"></a>2017-03-23 | <a id="p100192"></a>GULFSTREAM (GALP) | <a id="p100193"></a>G150 | <a id="p100194"></a>Doors - Adjustment of the Main Entrance Door Closed and Locked Indication Microswitch - Inspection |
| <a id="p100195"></a>27 | <a id="p100196"></a>CF-2017-12 | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/318ZVcmBJ/img_26.png) | <a id="p100198"></a>2017-03-23 | <a id="p100199"></a>BOMBARDIER | <a id="p100200"></a>BD-100 | <a id="p100201"></a>Fuselage - Incorrect Installation of Fasteners on Rear Spar Fitting |
| <a id="p100202"></a>28 | <a id="p100203"></a>ISR-I-52-2017-03-29 | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/318ZVcmBJ/img_27.png) | <a id="p100205"></a>2017-03-23 | <a id="p100206"></a>GULFSTREAM (GALP) | <a id="p100207"></a>ASTRA, G100 | <a id="p100208"></a>Doors - Adjustment of the Main Entrance Door Closed and Locked Indication Microswitch - Inspection |
| <a id="p100209"></a>29 | <a id="p100210"></a>BR-2017-03-01 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/318ZVcmBJ/img_28.png) | <a id="p100212"></a>2017-03-20 | <a id="p100213"></a>EMBRAER | <a id="p100214"></a>ERJ-170, ERJ-190 | <a id="p100215"></a>Fuselage - Forward Pressure Bulkhead - Repetitive Inspections/Modification |
| <a id="p100216"></a>30 | <a id="p100217"></a>2017-0050-E | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/318ZVcmBJ/img_29.png) | <a id="p100219"></a>2017-03-17 | <a id="p100220"></a>AIRBUS HELICOPTERS | <a id="p100221"></a>SA 330/AS 332/EC 225 | <a id="p100222"></a>Time Limits/Maintenance Checks - Main Gearbox Particle Detector/Oil Filter/Oil Cooler - Inspection Main Rotor Drive - Epicyclic Module - Replacement/Reduced Service Life Limit |
| <a id="p100223"></a>31 | <a id="p100224"></a>2017-0049 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/318ZVcmBJ/img_30.png) | <a id="p100226"></a>2017-03-16 | <a id="p100227"></a>EADS CASA | <a id="p100228"></a>C-212 | <a id="p100229"></a>Fuel - Fuel Distribution.System/Fuel Tube - Modification |
| <a id="p100230"></a>32 | <a id="p100231"></a>2017-0048 | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/318ZVcmBJ/img_31.png) | <a id="p100233"></a>2017-03-15 | <a id="p100234"></a>AIRBUS | <a id="p100235"></a>A300-600, A310 | <a id="p100236"></a>Fuselage - Aft Cargo Door Sill Beam Area - Inspection/Modification |
| <a id="p100237"></a>33 | <a id="p100238"></a>US-2017-05-05 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/318ZVcmBJ/img_32.png) | <a id="p100240"></a>2017-03-13 | <a id="p100241"></a>PRATT & WHITNEY | <a id="p100242"></a>PW4070, PW4080, PW4090 | <a id="p100243"></a>Engine - High-Pressure Turbine 1st Stage Hub - Inspection/Replacement |
| <a id="p100244"></a>34 | <a id="p100245"></a>2017-0047 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/318ZVcmBJ/img_33.png) | <a id="p100247"></a>2017-03-13 | <a id="p100248"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100249"></a>MBB-BK 117 | <a id="p100250"></a>Hydraulic Power - Module Plate Assembly - Inspection/Modification |


<a id="p100251"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100252"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100253"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

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<a id="p100254"></a>И.о. начальника Управления<br>
поддержания летной годности<br>
воздушных судов<br>
С.И.СУСЛОВ

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<a id="p100255"></a>

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