---
title: "<Письмо> Росавиации от 09.04.2019 N Исх-11086/03"
number: "Исх-11086/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2019-04-09
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-1108603"
---

## <Письмо> Росавиации от 09.04.2019 N Исх-11086/03

# <Письмо> Росавиации от 09.04.2019 N Исх-11086/03

"Информационное письмо ДЛГ-03-2019"


<div align="center">

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

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

<a id="p100003"></a>**ПИСЬМО**<br>
**от 9 апреля 2019 г. N Исх-11086/03**

<a id="p100004"></a>**ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-03-2019**

</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 25.02.2019 - 24.03.2019:


| <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>US-2019-03-07 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/oQZdiK7Xs/img_0.png) | <a id="p100016"></a>22.03.2019 | <a id="p100017"></a>BOEING | <a id="p100018"></a>737 | <a id="p100019"></a>Wings - Krueger Flap Bullnose Attachment Hardware - Inspection |
| <a id="p100020"></a>2 | <a id="p100021"></a>US-2019-03-06 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/oQZdiK7Xs/img_1.png) | <a id="p100023"></a>22.03.2019 | <a id="p100024"></a>BOEING | <a id="p100025"></a>737 | <a id="p100026"></a>Equipment/Furnishings - Passenger Service Units - Installation |
| <a id="p100027"></a>3 | <a id="p100028"></a>2018-0164R1 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/oQZdiK7Xs/img_2.png) | <a id="p100030"></a>21.03.2019 | <a id="p100031"></a>ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG | <a id="p100032"></a>TRENT 1000 | <a id="p100033"></a>[Correction] Engine - High Pressure Turbine Disc Front Cover Plate - Replacement [Life Limitation] |
| <a id="p100034"></a>4 | <a id="p100035"></a>2019-0057 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/oQZdiK7Xs/img_3.png) | <a id="p100037"></a>20.03.2019 | <a id="p100038"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100039"></a>A109/A119 | <a id="p100040"></a>Rotors Flight Control - Collective Stick Torque Tube Assembly - Inspection/Replacement |
| <a id="p100041"></a>5 | <a id="p100042"></a>2019-0060 | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/oQZdiK7Xs/img_4.png) | <a id="p100044"></a>20.03.2019 | <a id="p100045"></a>AIRBUS HELICOPTERS | <a id="p100046"></a>AS 350/EC 130, AS 355 | <a id="p100047"></a>Rotors Flight Control - Tail Rotor Gearbox Actuating Rod - Inspection |
| <a id="p100048"></a>6 | <a id="p100049"></a>2019-0058 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/oQZdiK7Xs/img_5.png) | <a id="p100051"></a>20.03.2019 | <a id="p100052"></a>ROLLS-ROYCE DEUTSCHLAND Ltd & Co KG | <a id="p100053"></a>TRENT 1000 | <a id="p100054"></a>Time Limits/Maintenance Checks - Time Limits Manual/Maintenance Programme - Amendment |
| <a id="p100055"></a>7 | <a id="p100056"></a>2019-0059 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/oQZdiK7Xs/img_6.png) | <a id="p100058"></a>20.03.2019 | <a id="p100059"></a>AIRBUS | <a id="p100060"></a>A330 | <a id="p100061"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 2 - Damage Tolerant Airworthiness Limitation Items - Implementation |
| <a id="p100062"></a>8 | <a id="p100063"></a>US-2019-01-03 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/oQZdiK7Xs/img_7.png) | <a id="p100065"></a>19.03.2019 | <a id="p100066"></a>BOEING | <a id="p100067"></a>737 | <a id="p100068"></a>Landing Gear - Trunnion Pin Assemblies - Inspection/Lubrication/Replacement |
| <a id="p100069"></a>9 | <a id="p100070"></a>US-2019-01-06 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/oQZdiK7Xs/img_8.png) | <a id="p100072"></a>19.03.2019 | <a id="p100073"></a>BOEING | <a id="p100074"></a>737 | <a id="p100075"></a>Fuselage - Frame Web and Doubler - Inspection |
| <a id="p100076"></a>10 | <a id="p100077"></a>2019-0056 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/oQZdiK7Xs/img_9.png) | <a id="p100079"></a>19.03.2019 | <a id="p100080"></a>AIRBUS | <a id="p100081"></a>A318, A319, A320, A321 | <a id="p100082"></a>Time Limits/Maintenance Checks - Safe Life Airworthiness Limitation Items - ALS Part 1 - Amendment |
| <a id="p100083"></a>11 | <a id="p100084"></a>2019-0055-E | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/oQZdiK7Xs/img_10.png) | <a id="p100086"></a>19.03.2019 | <a id="p100087"></a>BRP-ROTAX GmbH & Co KG | <a id="p100088"></a>912 S, 915 | <a id="p100089"></a>[Correction] Engine fuel and Control - Fuel Pump Assembly - Inspection/Replacement |
| <a id="p100090"></a>12 | <a id="p100091"></a>2019-0054 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/oQZdiK7Xs/img_11.png) | <a id="p100093"></a>18.03.2019 | <a id="p100094"></a>SAAB AB | <a id="p100095"></a>2000 | <a id="p100096"></a>Nacelles/Pylons - Engine Mounting Structure - Modification |
| <a id="p100097"></a>13 | <a id="p100098"></a>US-2019-01-08 | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/oQZdiK7Xs/img_12.png) | <a id="p100100"></a>18.03.2019 | <a id="p100101"></a>BOEING | <a id="p100102"></a>777 | <a id="p100103"></a>Equipment - Galley Mounted Seat Fittings - Modification |
| <a id="p100104"></a>14 | <a id="p100105"></a>2019-0052 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/oQZdiK7Xs/img_13.png) | <a id="p100107"></a>14.03.2019 | <a id="p100108"></a>WSK PZL - SWIDNIK S.A. | <a id="p100109"></a>SW4 | <a id="p100110"></a>Exhaust - Exhaust Ducts and Clamps - Inspection/Modification |
| <a id="p100111"></a>15 | <a id="p100112"></a>2019-0053 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/oQZdiK7Xs/img_14.png) | <a id="p100114"></a>14.03.2019 | <a id="p100115"></a>SAAB AB | <a id="p100116"></a>2000 | <a id="p100117"></a>Fuel $\text{в}€'$ Magnetic Fuel Level Indicator $\text{в}€'$ Inspection |
| <a id="p100118"></a>16 | <a id="p100119"></a>US-2019-05-01 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/oQZdiK7Xs/img_15.png) | <a id="p100121"></a>13.03.2019 | <a id="p100122"></a>PRATT & WHITNEY | <a id="p100123"></a>PW2000 | <a id="p100124"></a>Engine - Diffuser & High Pressure Turbine Case - Inspection |
| <a id="p100125"></a>17 | <a id="p100126"></a>2019-0049 | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/oQZdiK7Xs/img_16.png) | <a id="p100128"></a>11.03.2019 | <a id="p100129"></a>AIRBUS | <a id="p100130"></a>A330 | <a id="p100131"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 3 - Certification Maintenance Requirements - Amendment |
| <a id="p100132"></a>18 | <a id="p100133"></a>2017-0209R1 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/oQZdiK7Xs/img_17.png) | <a id="p100135"></a>11.03.2019 | <a id="p100136"></a>AIRBUS | <a id="p100137"></a>A380 | <a id="p100138"></a>Integrated Modular Avionics - Internal Timer - Power Cycle (Reset) |
| <a id="p100139"></a>19 | <a id="p100140"></a>2019-0050 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/oQZdiK7Xs/img_18.png) | <a id="p100142"></a>11.03.2019 | <a id="p100143"></a>AIRBUS | <a id="p100144"></a>A340 | <a id="p100145"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 3 - Certification Maintenance Requirements - Amendment |
| <a id="p100146"></a>20 | <a id="p100147"></a>2019-0048 | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/oQZdiK7Xs/img_19.png) | <a id="p100149"></a>11.03.2019 | <a id="p100150"></a>AIRBUS | <a id="p100151"></a>A340 | <a id="p100152"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 4 - System Equipment Maintenance Requirements - Amendment |
| <a id="p100153"></a>21 | <a id="p100154"></a>2019-0046 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/oQZdiK7Xs/img_20.png) | <a id="p100156"></a>11.03.2019 | <a id="p100157"></a>AIRBUS HELICOPTERS | <a id="p100158"></a>SA 365/366/AS 365/EC 155 | <a id="p100159"></a>Rotor Drive(s) - Tail Rotor Drive Flange - Modification |
| <a id="p100160"></a>22 | <a id="p100161"></a>2019-0047 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/oQZdiK7Xs/img_21.png) | <a id="p100163"></a>11.03.2019 | <a id="p100164"></a>AIRBUS | <a id="p100165"></a>A330 | <a id="p100166"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 4 - System Equipment Maintenance Requirements - Amendment |
| <a id="p100167"></a>23 | <a id="p100168"></a>CF-2019-10 | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/oQZdiK7Xs/img_22.png) | <a id="p100170"></a>08.03.2019 | <a id="p100171"></a>BOMBARDIER, ROCKWELL COLLINS | <a id="p100172"></a>CL-600 (Challenger), EASA STC 10041712, STC ST01505WI-D | <a id="p100173"></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="p100174"></a>24 | <a id="p100175"></a>CF-2019-09 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/oQZdiK7Xs/img_23.png) | <a id="p100177"></a>08.03.2019 | <a id="p100178"></a>BOMBARDIER, ROCKWELL COLLINS | <a id="p100179"></a>BD-100, STC ST01611WI-D | <a id="p100180"></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="p100181"></a>25 | <a id="p100182"></a>CF-2019-07 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/oQZdiK7Xs/img_24.png) | <a id="p100184"></a>08.03.2019 | <a id="p100185"></a>VIKING AIR LTD | <a id="p100186"></a>CL-215 | <a id="p100187"></a>Wing - Cracking of the Wing Lower Skin at Wing Station 51 under the Drag Angle |
| <a id="p100188"></a>26 | <a id="p100189"></a>2019-0044 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/oQZdiK7Xs/img_25.png) | <a id="p100191"></a>07.03.2019 | <a id="p100192"></a>AIRBUS | <a id="p100193"></a>A300-600 | <a id="p100194"></a>Wings - Centre Section Frame 40 Forward Fitting Radius at Tension Bolt Junction - Inspection/Repair |
| <a id="p100195"></a>27 | <a id="p100196"></a>2019-0045-E | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/oQZdiK7Xs/img_26.png) | <a id="p100198"></a>07.03.2019 | <a id="p100199"></a>WSK PZL - SWIDNIK S.A. | <a id="p100200"></a>SW4 | <a id="p100201"></a>Tail Rotor - Rotor Blade Bearing(s) - Inspection |
| <a id="p100202"></a>28 | <a id="p100203"></a>2019-0043 | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/oQZdiK7Xs/img_27.png) | <a id="p100205"></a>06.03.2019 | <a id="p100206"></a>TECNAM, Costruzioni Aeronautiche | <a id="p100207"></a>P2006T | <a id="p100208"></a>Landing Gear - Nose Landing Gear Piston Tube - Replacement |
| <a id="p100209"></a>29 | <a id="p100210"></a>CF-2019-08 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/oQZdiK7Xs/img_28.png) | <a id="p100212"></a>06.03.2019 | <a id="p100213"></a>BELL HELICOPTER TEXTRON CANADA (BHTC) | <a id="p100214"></a>505 (Jet Ranger X) | <a id="p100215"></a>Engine Fuel and Control - Change of Flight Manual Limitation for Jet B and JP-4 Fuels |
| <a id="p100216"></a>30 | <a id="p100217"></a>CF-2019-06 | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/oQZdiK7Xs/img_29.png) | <a id="p100219"></a>01.03.2019 | <a id="p100220"></a>BOMBARDIER | <a id="p100221"></a>DHC-8 | <a id="p100222"></a>Fuselage - Non-Conforming Keel Tension Fittings and Stringer End Fittings |
| <a id="p100223"></a>31 | <a id="p100224"></a>BR-2019-02-02 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/oQZdiK7Xs/img_30.png) | <a id="p100226"></a>28.02.2019 | <a id="p100227"></a>EMBRAER | <a id="p100228"></a>ERJ-170, ERJ-190 | <a id="p100229"></a>Fuselage - Ram Air Turbine Compartment Door Seal Attachment - Inspection/Rework |
| <a id="p100230"></a>32 | <a id="p100231"></a>2019-0042 | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/oQZdiK7Xs/img_31.png) | <a id="p100233"></a>27.02.2019 | <a id="p100234"></a>AIRBUS | <a id="p100235"></a>A330 | <a id="p100236"></a>Power Plant - Engine Air Inlet Cowl Acoustic Panels - Inspection/Repair/Replacement |
| <a id="p100237"></a>33 | <a id="p100238"></a>2017-0103R1 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/oQZdiK7Xs/img_32.png) | <a id="p100240"></a>25.02.2019 | <a id="p100241"></a>AUSTRO ENGINE GMBH | <a id="p100242"></a>E4 | <a id="p100243"></a>Engine - Timing Chain - Replacement/Aircraft Flight Manual - Limitations Section - Amendment |
| <a id="p100244"></a>34 | <a id="p100245"></a>US-2019-02-01 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/oQZdiK7Xs/img_33.png) | <a id="p100247"></a>25.02.2019 | <a id="p100248"></a>GENERAL ELECTRIC | <a id="p100249"></a>GEnx | <a id="p100250"></a>Engine - High-Pressure Turbine Stator Cases - Removal/Replacement |
| <a id="p100251"></a>35 | <a id="p100252"></a>2019-0041 | <a id="p100253"></a>![рис. 35](https://i.bukva.ai/oQZdiK7Xs/img_34.png) | <a id="p100254"></a>25.02.2019 | <a id="p100255"></a>AUSTRO ENGINE GMBH | <a id="p100256"></a>E4 | <a id="p100257"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section - Amendment |


<a id="p100258"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100259"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100260"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

<div align="right">

<a id="p100261"></a>Начальник Управления<br>
поддержания летной<br>
годности воздушных судов<br>
В.В.КУДИНОВ

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<a id="p100262"></a>

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