---
title: "<Письмо> Росавиации от 17.01.2019 N Исх-943/03"
number: "Исх-943/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2019-01-17
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-94303"
---

## <Письмо> Росавиации от 17.01.2019 N Исх-943/03

# <Письмо> Росавиации от 17.01.2019 N Исх-943/03

"Информационное письмо ДЛГ-01-2019"


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

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

<a id="p100003"></a>ПИСЬМО
от 17 января 2019 г. N Исх-943/03

<a id="p100004"></a>ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-01-2019

<a id="p100005"></a>Управление поддержания летной годности воздушных судов информирует эксплуатантов воздушных судов о выпуске иностранными авиационными администрациями следующих Директив летной годности на период 17.12.2018 - 13.01.2019:


| <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>2018-0276R1 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/jSzuKemxC/img_0.png) | <a id="p100016"></a>11.01.2019 | <a id="p100017"></a>AIRBUS | <a id="p100018"></a>A330 | <a id="p100019"></a>Fuselage - Structural Parts/Joints - Modification - Reinforcement |
| <a id="p100020"></a>2 | <a id="p100021"></a>US-2018-26-05 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/jSzuKemxC/img_1.png) | <a id="p100023"></a>11.01.2019 | <a id="p100024"></a>BOEING | <a id="p100025"></a>777 | <a id="p100026"></a>Fuel - Motor-Operated Valve Actuators/Maintenance or Inspection Program - Inspection/Replacement/Revision |
| <a id="p100027"></a>3 | <a id="p100028"></a>US-2018-26-06 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/jSzuKemxC/img_2.png) | <a id="p100030"></a>11.01.2019 | <a id="p100031"></a>BOEING | <a id="p100032"></a>737 | <a id="p100033"></a>Doors - Main Landing Gear Center Door Assemblies - Inspection |
| <a id="p100034"></a>4 | <a id="p100035"></a>US-2018-26-03 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/jSzuKemxC/img_3.png) | <a id="p100037"></a>11.01.2019 | <a id="p100038"></a>BOEING | <a id="p100039"></a>757 | <a id="p100040"></a>Equipment/Furnishings - IPECO 3A090 and 3A258 Flight Crew Seats - Inspection |
| <a id="p100041"></a>5 | <a id="p100042"></a>US-2018-22-07 | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/jSzuKemxC/img_4.png) | <a id="p100044"></a>11.01.2019 | <a id="p100045"></a>ENGINE ALLIANCE LLC | <a id="p100046"></a>GP7200 | <a id="p100047"></a>Engine - High Pressure Compressor Stages 2-5 Spool - Inspection/Replacement |
| <a id="p100048"></a>6 | <a id="p100049"></a>2019-0002 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/jSzuKemxC/img_5.png) | <a id="p100051"></a>11.01.2019 | <a id="p100052"></a>AIRBUS | <a id="p100053"></a>A380 | <a id="p100054"></a>Nacelles/Pylons - Inboard and Outboard Pylon Drain System - Inspection |
| <a id="p100055"></a>7 | <a id="p100056"></a>US-2018-23-12 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/jSzuKemxC/img_6.png) | <a id="p100058"></a>11.01.2019 | <a id="p100059"></a>APPLIANCES | <a id="p100060"></a>ATA 25 EQUIPMENT/FURNISHINGS | <a id="p100061"></a>[Correction] ZODIAC AERO EVACUATION SYSTEMS - Fusible Plugs - Replacement |
| <a id="p100062"></a>8 | <a id="p100063"></a>2019-0004 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/jSzuKemxC/img_7.png) | <a id="p100065"></a>11.01.2019 | <a id="p100066"></a>APPLIANCES | <a id="p100067"></a>ATA 34 NAVIGATION | <a id="p100068"></a>THALES AVS FRANCE SAS - Global Navigation Satellite System - Operational Limitations |
| <a id="p100069"></a>9 | <a id="p100070"></a>2019-0003 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/jSzuKemxC/img_8.png) | <a id="p100072"></a>11.01.2019 | <a id="p100073"></a>AIRBUS HELICOPTERS | <a id="p100074"></a>EC175 | <a id="p100075"></a>Rotor Drive - Main Gearbox Top Sensor - Inspection |
| <a id="p100076"></a>10 | <a id="p100077"></a>CF-2019-02 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/jSzuKemxC/img_9.png) | <a id="p100079"></a>10.01.2019 | <a id="p100080"></a>VIKING AIR LTD | <a id="p100081"></a>DHC-6 (Twin Otter) | <a id="p100082"></a>Time Limits/Maintenance Checks - Airworthiness Limitations - Implementation |
| <a id="p100083"></a>11 | <a id="p100084"></a>CF-2019-01 | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/jSzuKemxC/img_10.png) | <a id="p100086"></a>10.01.2019 | <a id="p100087"></a>AIRBUS HELICOPTERS, BELL HELICOPTER TEXTRON CANADA (BHTC), BELLIS INVESTMENTS LTD, MD HELICOPTERS INC (MDHI) | <a id="p100088"></a>AS 350/EC 130, AS 355, 206, 407, STC SH98-35, 369, 500N | <a id="p100089"></a>Standard Practices - Helicopter External Transport System (HETSв., ![формула](https://i.bukva.ai/jSzuKemxC/img_11.png) ) - Unapproved Parts, Inadequate Service Life Limits and Maintenance Requirements |
| <a id="p100090"></a>12 | <a id="p100091"></a>CF-2018-36 | <a id="p100092"></a>![рис. 13](https://i.bukva.ai/jSzuKemxC/img_12.png) | <a id="p100093"></a>10.01.2019 | <a id="p100094"></a>BOMBARDIER | <a id="p100095"></a>CL-600 (Challenger) | <a id="p100096"></a>Navigation - Flight Instruments - Unreliable Air Data in the Cockpit |
| <a id="p100097"></a>13 | <a id="p100098"></a>2019-0001 | <a id="p100099"></a>![рис. 14](https://i.bukva.ai/jSzuKemxC/img_13.png) | <a id="p100100"></a>10.01.2019 | <a id="p100101"></a>AIRBUS HELICOPTERS | <a id="p100102"></a>AS 350/EC 130 | <a id="p100103"></a>Doors - Sliding Door Opening Mechanism - Inspection |
| <a id="p100104"></a>14 | <a id="p100105"></a>2018-0265R1 | <a id="p100106"></a>![рис. 15](https://i.bukva.ai/jSzuKemxC/img_14.png) | <a id="p100107"></a>10.01.2019 | <a id="p100108"></a>BRP-ROTAX GmbH & Co KG | <a id="p100109"></a>914 F, 915 | <a id="p100110"></a>[Correction] Engine - Exhaust Valve - Replacement |
| <a id="p100111"></a>15 | <a id="p100112"></a>2018-0137R1 | <a id="p100113"></a>![рис. 16](https://i.bukva.ai/jSzuKemxC/img_15.png) | <a id="p100114"></a>09.01.2019 | <a id="p100115"></a>AIRBUS | <a id="p100116"></a>A318, A319, A320, A321 | <a id="p100117"></a>Nacelles/Pylons - Pylon Aft Fixed Fairings - Inspection |
| <a id="p100118"></a>16 | <a id="p100119"></a>CF-2018-37 | <a id="p100120"></a>![рис. 17](https://i.bukva.ai/jSzuKemxC/img_16.png) | <a id="p100121"></a>08.01.2019 | <a id="p100122"></a>BOMBARDIER | <a id="p100123"></a>BD-100 | <a id="p100124"></a>Recording System - Cockpit Voice Recorder (CVR) and Flight Data Recorder (FDR) power supply modification |
| <a id="p100125"></a>17 | <a id="p100126"></a>US-2018-25-17 | <a id="p100127"></a>![рис. 18](https://i.bukva.ai/jSzuKemxC/img_17.png) | <a id="p100128"></a>07.01.2019 | <a id="p100129"></a>AIR COMM CORPORATION, AIRBUS HELICOPTERS, BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100130"></a>CAA UK AAN 25273, EASA STC 10029555, STC EASA.IM.R.S.01173, STC EASA.IM.R.S.01537, STC SH2750NM, STC SR00222DE, STC SR00543DE, STC SR00643DE, AS 350/EC 130, 206, 407 | <a id="p100131"></a>Air Conditioning - Electrical Connectors - Replacement |
| <a id="p100132"></a>18 | <a id="p100133"></a>2018-0292 | <a id="p100134"></a>![рис. 19](https://i.bukva.ai/jSzuKemxC/img_18.png) | <a id="p100135"></a>28.12.2018 | <a id="p100136"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100137"></a>AB139/AW139 | <a id="p100138"></a>Tail Rotor - Tail Rotor Slider Assembly - Inspection |
| <a id="p100139"></a>19 | <a id="p100140"></a>2018-0290 | <a id="p100141"></a>![рис. 20](https://i.bukva.ai/jSzuKemxC/img_19.png) | <a id="p100142"></a>21.12.2018 | <a id="p100143"></a>AIRBUS | <a id="p100144"></a>A350 | <a id="p100145"></a>Stabilizer - Vertical Stabilizer Tension Bolts - Modification |
| <a id="p100146"></a>20 | <a id="p100147"></a>2018-0291 | <a id="p100148"></a>![рис. 21](https://i.bukva.ai/jSzuKemxC/img_20.png) | <a id="p100149"></a>21.12.2018 | <a id="p100150"></a>ROLLS-ROYCE PLC | <a id="p100151"></a>RB211 TRENT 700 | <a id="p100152"></a>Engine - High Pressure Turbine Blades - Replacement |
| <a id="p100153"></a>21 | <a id="p100154"></a>CF-2018-33 | <a id="p100155"></a>![рис. 22](https://i.bukva.ai/jSzuKemxC/img_21.png) | <a id="p100156"></a>21.12.2018 | <a id="p100157"></a>BOMBARDIER, ROCKWELL COLLINS | <a id="p100158"></a>CL-600 (Regional Jet), EASA STC 10041711, STC ST01514WI-D | <a id="p100159"></a>Avionic System - Airplane Flight Manual Navigation System Limitations - Prohibit Editing CLIMB TO Altitudes and Use of Temperature Compensation on Flight Management System |
| <a id="p100160"></a>22 | <a id="p100161"></a>2018-0288 | <a id="p100162"></a>![рис. 23](https://i.bukva.ai/jSzuKemxC/img_22.png) | <a id="p100163"></a>21.12.2018 | <a id="p100164"></a>AIRBUS | <a id="p100165"></a>A318, A319, A320, A321 | <a id="p100166"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 2 - Damage Tolerant Airworthiness Limitation Items - Implementation |
| <a id="p100167"></a>23 | <a id="p100168"></a>2018-0289 | <a id="p100169"></a>![рис. 24](https://i.bukva.ai/jSzuKemxC/img_23.png) | <a id="p100170"></a>21.12.2018 | <a id="p100171"></a>AIRBUS | <a id="p100172"></a>A318, A319, A320, A321 | <a id="p100173"></a>Fuselage - Service Door Stop Fitting Hole - Inspection/Repair |
| <a id="p100174"></a>24 | <a id="p100175"></a>2018-0283 | <a id="p100176"></a>![рис. 25](https://i.bukva.ai/jSzuKemxC/img_24.png) | <a id="p100177"></a>20.12.2018 | <a id="p100178"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100179"></a>MBB-BK 117 | <a id="p100180"></a>Rotors Flight Control - Main Rotor Actuator - Inspection |
| <a id="p100181"></a>25 | <a id="p100182"></a>2018-0286 | <a id="p100183"></a>![рис. 26](https://i.bukva.ai/jSzuKemxC/img_25.png) | <a id="p100184"></a>20.12.2018 | <a id="p100185"></a>ENSTROM HELICOPTER CORPORATION | <a id="p100186"></a>280, 480, F-28 | <a id="p100187"></a>Main Rotor - Hydraulic Damper/Belt Tension Shaft Rod End Assembly - Inspection |
| <a id="p100188"></a>26 | <a id="p100189"></a>2016-0106R1 | <a id="p100190"></a>![рис. 27](https://i.bukva.ai/jSzuKemxC/img_26.png) | <a id="p100191"></a>20.12.2018 | <a id="p100192"></a>AIRBUS | <a id="p100193"></a>A321 | <a id="p100194"></a>Fuselage - Frame 35.2A - Inspection |
| <a id="p100195"></a>27 | <a id="p100196"></a>2018-0284 | <a id="p100197"></a>![рис. 28](https://i.bukva.ai/jSzuKemxC/img_27.png) | <a id="p100198"></a>20.12.2018 | <a id="p100199"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100200"></a>EC135/635 | <a id="p100201"></a>Rotors Flight Control - Main Rotor Actuator - Inspection |
| <a id="p100202"></a>28 | <a id="p100203"></a>CF-2018-35 | <a id="p100204"></a>![рис. 29](https://i.bukva.ai/jSzuKemxC/img_28.png) | <a id="p100205"></a>20.12.2018 | <a id="p100206"></a>BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100207"></a>429 | <a id="p100208"></a>Tail Rotor Drive - Tail Rotor Gearbox - Introduction of Attachment Hardware Recurring Torque Check |
| <a id="p100209"></a>29 | <a id="p100210"></a>2018-0287 | <a id="p100211"></a>![рис. 30](https://i.bukva.ai/jSzuKemxC/img_29.png) | <a id="p100212"></a>20.12.2018 | <a id="p100213"></a>AIRBUS HELICOPTERS | <a id="p100214"></a>AS 350/EC 130, AS 355 | <a id="p100215"></a>Rotors Flight Control - Tail Rotor Gearbox Actuating Rod - Inspection |
| <a id="p100216"></a>30 | <a id="p100217"></a>CF-2018-34 | <a id="p100218"></a>![рис. 31](https://i.bukva.ai/jSzuKemxC/img_30.png) | <a id="p100219"></a>20.12.2018 | <a id="p100220"></a>BOMBARDIER | <a id="p100221"></a>DHC-8 | <a id="p100222"></a>Flight Controls - Elevator Power Control Unit Bracket Cracking |
| <a id="p100223"></a>31 | <a id="p100224"></a>2018-0285 | <a id="p100225"></a>![рис. 32](https://i.bukva.ai/jSzuKemxC/img_31.png) | <a id="p100226"></a>20.12.2018 | <a id="p100227"></a>PILATUS AIRCRAFT LTD | <a id="p100228"></a>PC-6 | <a id="p100229"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section - Amendment |
| <a id="p100230"></a>32 | <a id="p100231"></a>2018-0282 | <a id="p100232"></a>![рис. 33](https://i.bukva.ai/jSzuKemxC/img_32.png) | <a id="p100233"></a>19.12.2018 | <a id="p100234"></a>AIRBUS HELICOPTERS | <a id="p100235"></a>SA 330/AS 332/EC 225 | <a id="p100236"></a>Fuselage - Main Gearbox Suspension Bar Rear Attachment Fitting Screws - Inspection |
| <a id="p100237"></a>33 | <a id="p100238"></a>DCA-750XL-32A | <a id="p100239"></a>![рис. 34](https://i.bukva.ai/jSzuKemxC/img_33.png) | <a id="p100240"></a>19.12.2018 | <a id="p100241"></a>PACIFIC AEROSPACE LTD | <a id="p100242"></a>750XL | <a id="p100243"></a>Landing Gear - Nose and Main Landing Gear Attachment Bolts - Inspection |
| <a id="p100244"></a>34 | <a id="p100245"></a>DCA-750XL-33 | <a id="p100246"></a>![рис. 35](https://i.bukva.ai/jSzuKemxC/img_34.png) | <a id="p100247"></a>19.12.2018 | <a id="p100248"></a>PACIFIC AEROSPACE LTD | <a id="p100249"></a>750XL | <a id="p100250"></a>Aileron Pivot Fork Assembly - Inspection |
| <a id="p100251"></a>35 | <a id="p100252"></a>2018-0281 | <a id="p100253"></a>![рис. 36](https://i.bukva.ai/jSzuKemxC/img_35.png) | <a id="p100254"></a>18.12.2018 | <a id="p100255"></a>PIPISTREL VERTICAL SOLUTIONS d.o.o. | <a id="p100256"></a>Virus SW 121 | <a id="p100257"></a>Fuel - Fuel Pressure Sensor - Inspection/Replacement |
| <a id="p100258"></a>36 | <a id="p100259"></a>2018-0264 | <a id="p100260"></a>![рис. 37](https://i.bukva.ai/jSzuKemxC/img_36.png) | <a id="p100261"></a>17.12.2018 | <a id="p100262"></a>DASSAULT AVIATION | <a id="p100263"></a>Falcon 7X | <a id="p100264"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section - Amendment |
| <a id="p100265"></a>37 | <a id="p100266"></a>2018-0280 | <a id="p100267"></a>![рис. 38](https://i.bukva.ai/jSzuKemxC/img_37.png) | <a id="p100268"></a>17.12.2018 | <a id="p100269"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100270"></a>A109/A119 | <a id="p100271"></a>Rotors Flight Control - Mixing Control System Rigid Connecting Link - Inspection |


<a id="p100272"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100273"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100274"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

<a id="p100275"></a>Начальник Управления
поддержания летной годности
воздушных судов
В.В.КУДИНОВ



<a id="p100276"></a>

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