---
title: "<Письмо> Росавиации от 19.11.2018 N Исх-29656/03"
number: "Исх-29656/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2018-11-19
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-2965603"
---

## <Письмо> Росавиации от 19.11.2018 N Исх-29656/03

# <Письмо> Росавиации от 19.11.2018 N Исх-29656/03

"Информационное письмо ДЛГ-07-2018"


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

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

<div align="center">

<a id="p100003"></a>**ПИСЬМО**<br>
**от 19 ноября 2018 г. N Исх-29656/03**

</div>


<a id="p100004"></a>ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-07-2018

<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 24.09.2018 - 04.11.2018:


| <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>US-2018-19-21 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/qVoB5aLBh/img_0.png) | <a id="p100016"></a>02.11.2018 | <a id="p100017"></a>BOEING | <a id="p100018"></a>707, 720 | <a id="p100019"></a>Fuel - Maintenance or Inspection Program - Revision |
| <a id="p100020"></a>2 | <a id="p100021"></a>US-2018-20-05 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/qVoB5aLBh/img_1.png) | <a id="p100023"></a>02.11.2018 | <a id="p100024"></a>BOEING | <a id="p100025"></a>727 | <a id="p100026"></a>Fuselage - Bulkhead Frame Web - Repetitive Inspections |
| <a id="p100027"></a>3 | <a id="p100028"></a>US-2018-19-32 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/qVoB5aLBh/img_2.png) | <a id="p100030"></a>02.11.2018 | <a id="p100031"></a>BOEING | <a id="p100032"></a>707, 720 | <a id="p100033"></a>Nacellies/Pylons - Nacelle Strut Spar and Overwing Fittings, Diagonal Braces and Associated Fittings - Repetitive Inspections/Replacement |
| <a id="p100034"></a>4 | <a id="p100035"></a>US-2018-20-13 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/qVoB5aLBh/img_3.png) | <a id="p100037"></a>02.11.2018 | <a id="p100038"></a>BOEING | <a id="p100039"></a>737, 757, 767 | <a id="p100040"></a>[Correction] Fuel - Motor-Operated Valve Actuators - Replacement/Maintenance or Inspection Program - Revision |
| <a id="p100041"></a>5 | <a id="p100042"></a>2018-0237-E | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/qVoB5aLBh/img_4.png) | <a id="p100044"></a>02.11.2018 | <a id="p100045"></a>ALLSTAR PZL GLIDER | <a id="p100046"></a>SZD-54 Perkoz | <a id="p100047"></a>Flight Controls - Elevator Control System - Inspection |
| <a id="p100048"></a>6 | <a id="p100049"></a>2018-0236-E | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/qVoB5aLBh/img_5.png) | <a id="p100051"></a>02.11.2018 | <a id="p100052"></a>AIRBUS HELICOPTERS | <a id="p100053"></a>EC175 | <a id="p100054"></a>Landing Gear - Emergency Flotation Unit - Inspection/Replacement Rotorcraft Flight Manual/Master Minimum Equipment List - Temporary Revision |
| <a id="p100055"></a>7 | <a id="p100056"></a>US-2018-20-22 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/qVoB5aLBh/img_6.png) | <a id="p100058"></a>30.10.2018 | <a id="p100059"></a>GENERAL ELECTRIC | <a id="p100060"></a>GE90 | <a id="p100061"></a>Engine - Combustor Assembly - Removal/Replacement |
| <a id="p100062"></a>8 | <a id="p100063"></a>US-2018-20-23 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/qVoB5aLBh/img_7.png) | <a id="p100065"></a>30.10.2018 | <a id="p100066"></a>GENERAL ELECTRIC | <a id="p100067"></a>GE90 | <a id="p100068"></a>Engine - High Pressure Compressor Rotor Stage 2-5 Spools - Removal/Replacement |
| <a id="p100069"></a>9 | <a id="p100070"></a>GA8-10 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/qVoB5aLBh/img_8.png) | <a id="p100072"></a>30.10.2018 | <a id="p100073"></a>GIPPSLAND | <a id="p100074"></a>GA8 | <a id="p100075"></a>Time Limits/Maintenance Cheeks - Airworthiness Limitations Sction - Amendment |
| <a id="p100076"></a>10 | <a id="p100077"></a>2018-0234 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/qVoB5aLBh/img_9.png) | <a id="p100079"></a>30.10.2018 | <a id="p100080"></a>AIRBUS | <a id="p100081"></a>A350 | <a id="p100082"></a>Exhaust - Thrust Reverser Actuators - Greasing/Master Minimum Equipment List Restriction - Amendment |
| <a id="p100083"></a>11 | <a id="p100084"></a>US-2018-22-06 | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/qVoB5aLBh/img_10.png) | <a id="p100086"></a>30.10.2018 | <a id="p100087"></a>PRATT & WHITNEY | <a id="p100088"></a>PW2000 | <a id="p100089"></a>Engine Fuel & Control - Metering Valve Pilot Valve - Removal / Replacement |
| <a id="p100090"></a>12 | <a id="p100091"></a>US-2018-19-09 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/qVoB5aLBh/img_11.png) | <a id="p100093"></a>30.10.2018 | <a id="p100094"></a>SIKORSKY | <a id="p100095"></a>S-92 | <a id="p100096"></a>Landing Gear - Components - Life Limit/Inspection |
| <a id="p100097"></a>13 | <a id="p100098"></a>2018-0233 | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/qVoB5aLBh/img_12.png) | <a id="p100100"></a>26.10.2018 | <a id="p100101"></a>AIRBUS | <a id="p100102"></a>A319, A320. A321 | <a id="p100103"></a>Fuselage - Cargo Compartment Fitting Brackets, Tack and Rivet Holes - Inspection/Repair |
| <a id="p100104"></a>14 | <a id="p100105"></a>2018-0218 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/qVoB5aLBh/img_13.png) | <a id="p100107"></a>26.10.2018 | <a id="p100108"></a>AIRBUS | <a id="p100109"></a>A318. A319. A320, A321 | <a id="p100110"></a>[Correction] Wings - Center and Outer Wing Box at Level of Rib I Junction - Inspection |
| <a id="p100111"></a>15 | <a id="p100112"></a>US-2018-21-13 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/qVoB5aLBh/img_14.png) | <a id="p100114"></a>25.10.2018 | <a id="p100115"></a>HONDA AIRCRAFT COMPANY LLC | <a id="p100116"></a>HA-420 | <a id="p100117"></a>Airplane Flight Manual Temporary Revision/Landing Gear - Power Brake Valves - Replacement |
| <a id="p100118"></a>16 | <a id="p100119"></a>2018-0231 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/qVoB5aLBh/img_15.png) | <a id="p100121"></a>25.10.2018 | <a id="p100122"></a>AIRBUS | <a id="p100123"></a>A318, A319, A320. A321 | <a id="p100124"></a>Time Limits/Maintenance Checks - Airworthiness Limitations Section Part 5 - Fuel Airworthiness Limitations - Amendment |
| <a id="p100125"></a>17 | <a id="p100126"></a>CF-2018-21R1 | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/qVoB5aLBh/img_16.png) | <a id="p100128"></a>25.10.2018 | <a id="p100129"></a>BOMBARDIER | <a id="p100130"></a>DHC-8 | <a id="p100131"></a>Wings - Cracked Spoiler Actuator Bracket |
| <a id="p100132"></a>18 | <a id="p100133"></a>US-2018-22-04 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/qVoB5aLBh/img_17.png) | <a id="p100135"></a>25.10.2018 | <a id="p100136"></a>BOEING | <a id="p100137"></a>787 | <a id="p100138"></a>Flight Controls - Trailing Edge Flap Rotary Actuator - Inspection/Replacement |
| <a id="p100139"></a>19 | <a id="p100140"></a>CF-2018-27 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/qVoB5aLBh/img_18.png) | <a id="p100142"></a>24.10.2018 | <a id="p100143"></a>VIKING AIR LTD | <a id="p100144"></a>CL-215 | <a id="p100145"></a>Flight Controls - Excess Fiberglass Content in Aileron Control System and Flap Interconnect System Components |
| <a id="p100146"></a>20 | <a id="p100147"></a>US-2018-20-04 | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/qVoB5aLBh/img_19.png) | <a id="p100149"></a>24.10.2018 | <a id="p100150"></a>GULFSTREAM AEROSPACE CORPORATION | <a id="p100151"></a>GVI | <a id="p100152"></a>Flight Controls - Normal and Abnormal Procedures Sections of the Airplane Flight Manual - Revisions |
| <a id="p100153"></a>21 | <a id="p100154"></a>2018-0229 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/qVoB5aLBh/img_20.png) | <a id="p100156"></a>23.10.2018 | <a id="p100157"></a>AIRBUS | <a id="p100158"></a>A300-600, A300-600ST (Beluga) | <a id="p100159"></a>Wings - Centre Wing Box Frame 47 Angle Fittings - Inspection/Modification |
| <a id="p100160"></a>22 | <a id="p100161"></a>2018-0230 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/qVoB5aLBh/img_21.png) | <a id="p100163"></a>23.10.2018 | <a id="p100164"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100165"></a>MBB-BK 117 | <a id="p100166"></a>Integrated Modular Avionics - Aircraft Management Computer Software - Modification |
| <a id="p100167"></a>23 | <a id="p100168"></a>2018-0227 | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/qVoB5aLBh/img_22.png) | <a id="p100170"></a>22.10.2018 | <a id="p100171"></a>AIRBUS | <a id="p100172"></a>A330 | <a id="p100173"></a>Exhaust - Thrust Reverser Latch Beam Gussets - Inspection/Modification |
| <a id="p100174"></a>24 | <a id="p100175"></a>2018-0228 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/qVoB5aLBh/img_23.png) | <a id="p100177"></a>22.10.2018 | <a id="p100178"></a>AIRBUS | <a id="p100179"></a>A330 | <a id="p100180"></a>Power Plant - Engine Air Inlet Cowl Inner Barrel Lower Panels - Inspection / Replacement |
| <a id="p100181"></a>25 | <a id="p100182"></a>2018-0226 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/qVoB5aLBh/img_24.png) | <a id="p100184"></a>22.10.2018 | <a id="p100185"></a>AIRBUS | <a id="p100186"></a>A330, A340 | <a id="p100187"></a>Stabilizers - Horizontal Stabilizer Centre Box Top Skin - Inspection/Repair |
| <a id="p100188"></a>26 | <a id="p100189"></a>2018-0222 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/qVoB5aLBh/img_25.png) | <a id="p100191"></a>19.10.2018 | <a id="p100192"></a>PILATUS AIRCRAFT LTD | <a id="p100193"></a>PC-6 | <a id="p100194"></a>Flight Controls - Rudder Shaft Assembly Rivet Configuration - Inspection |
| <a id="p100195"></a>27 | <a id="p100196"></a>2018-0224 | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/qVoB5aLBh/img_26.png) | <a id="p100198"></a>19.10.2018 | <a id="p100199"></a>AIRBUS | <a id="p100200"></a>A340 | <a id="p100201"></a>Exhaust - Thrust Reverser Outer Fixed Structure - Inspection/Replacement |
| <a id="p100202"></a>28 | <a id="p100203"></a>2018-0225-E | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/qVoB5aLBh/img_27.png) | <a id="p100205"></a>18.10.2018 | <a id="p100206"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100207"></a>MBB-BK 117 | <a id="p100208"></a>Equipment & Furnishings - Hook Mount Assembly - Inspection |
| <a id="p100209"></a>29 | <a id="p100210"></a>US-2018-20-15 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/qVoB5aLBh/img_28.png) | <a id="p100212"></a>17.10.2018 | <a id="p100213"></a>BOLING | <a id="p100214"></a>787 | <a id="p100215"></a>Electrical Power - New Software for the Generator Control Unit - Installation |
| <a id="p100216"></a>30 | <a id="p100217"></a>2018-0223 | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/qVoB5aLBh/img_29.png) | <a id="p100219"></a>17.10.2018 | <a id="p100220"></a>APPLIANCES | <a id="p100221"></a>ATA 25 EQUIPMENT/FURNISHINGS | <a id="p100222"></a>B/E AEROSPACE FISCHER GmbH - Seat Energy Absorber Assembly - Modification |
| <a id="p100223"></a>31 | <a id="p100224"></a>CF-2018-28 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/qVoB5aLBh/img_30.png) | <a id="p100226"></a>16.10.2018 | <a id="p100227"></a>VIKING AIR LTD | <a id="p100228"></a>DHC-6 (Twin Otter) | <a id="p100229"></a>Flight Controls - Worn Elevator Cables - Inspection |
| <a id="p100230"></a>32 | <a id="p100231"></a>2018-0221 | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/qVoB5aLBh/img_31.png) | <a id="p100233"></a>16.10.2018 | <a id="p100234"></a>AIRBUS | <a id="p100235"></a>A380 | <a id="p100236"></a>Wings - Aileron Actuator Fittings - Inspection |
| <a id="p100237"></a>33 | <a id="p100238"></a>2018-0167R2 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/qVoB5aLBh/img_32.png) | <a id="p100240"></a>16.10.2018 | <a id="p100241"></a>ROLLS-ROYCE PLC | <a id="p100242"></a>TRENT 1000 | <a id="p100243"></a>Engine - Intermediate Pressure Compressor Blades/Shafts - Inspection |
| <a id="p100244"></a>34 | <a id="p100245"></a>US-2018-19-22 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/qVoB5aLBh/img_33.png) | <a id="p100247"></a>15.10 2018 | <a id="p100248"></a>GENERAL ELECTRIC | <a id="p100249"></a>CF34-10 | <a id="p100250"></a>Engine - High-Pressure Turbine Front Rotating Air Seal - Replacement |
| <a id="p100251"></a>35 | <a id="p100252"></a>US-2018-20-04 | <a id="p100253"></a>![рис. 35](https://i.bukva.ai/qVoB5aLBh/img_34.png) | <a id="p100254"></a>15.10.2018 | <a id="p100255"></a>GULFSTREAM AEROSPACE CORPORATION | <a id="p100256"></a>GVI | <a id="p100257"></a>NOT ADOPTED - LASA DECISION ATTACHED |
| <a id="p100258"></a>36 | <a id="p100259"></a>CF-2018-26 | <a id="p100260"></a>![рис. 36](https://i.bukva.ai/qVoB5aLBh/img_35.png) | <a id="p100261"></a>15.10.2018 | <a id="p100262"></a>BOMBARDIER | <a id="p100263"></a>CL-600 (Challenger) | <a id="p100264"></a>Landing Gear - Main Landing Gear Side Stay Actuators Contain Non-Conforming Split Ball Bearing |
| <a id="p100265"></a>37 | <a id="p100266"></a>2018-0220 | <a id="p100267"></a>![рис. 37](https://i.bukva.ai/qVoB5aLBh/img_36.png) | <a id="p100268"></a>12.10.2018 | <a id="p100269"></a>AIRBUS | <a id="p100270"></a>A350 | <a id="p100271"></a>Wings - Wing Rib Foot to Wing Lower Cover Clearance - Inspection/Temporary Operational Restrictions |
| <a id="p100272"></a>38 | <a id="p100273"></a>2018-0219 | <a id="p100274"></a>![рис. 38](https://i.bukva.ai/qVoB5aLBh/img_37.png) | <a id="p100275"></a>12.10.2018 | <a id="p100276"></a>M&D FLUGZEUGBAU | <a id="p100277"></a>AVO 68 (Samburo) | <a id="p100278"></a>Flight Controls - Elevator Mass Balance - Inspection |
| <a id="p100279"></a>39 | <a id="p100280"></a>2018-0218 | <a id="p100281"></a>![рис. 39](https://i.bukva.ai/qVoB5aLBh/img_38.png) | <a id="p100282"></a>11.10.2018 | <a id="p100283"></a>AIRBUS | <a id="p100284"></a>A318, A319, A320, A321 | <a id="p100285"></a>Wings - Center and Outer Wing Box at Level of Rib I Junction - Inspection |
| <a id="p100286"></a>40 | <a id="p100287"></a>CF-2018-25 | <a id="p100288"></a>![рис. 40](https://i.bukva.ai/qVoB5aLBh/img_39.png) | <a id="p100289"></a>10.10.2018 | <a id="p100290"></a>BOMBARDIER | <a id="p100291"></a>CL-600 (Regional Jet) | <a id="p100292"></a>Fuselage - AFT Fuselage Fitting Not Heat Treated |
| <a id="p100293"></a>41 | <a id="p100294"></a>2018-0217 | <a id="p100295"></a>![рис. 41](https://i.bukva.ai/qVoB5aLBh/img_40.png) | <a id="p100296"></a>10.10.2018 | <a id="p100297"></a>PILATUS AIRCRAFT LTD | <a id="p100298"></a>PC-6 | <a id="p100299"></a>Stabilizers - Horizontal Stabilizer Hinge Bracket Assembly/Front Spar Attachment Area - Inspection |
| <a id="p100300"></a>42 | <a id="p100301"></a>US-2018-18-03 | <a id="p100302"></a>![рис. 42](https://i.bukva.ai/qVoB5aLBh/img_41.png) | <a id="p100303"></a>09.10.2018 | <a id="p100304"></a>BOEING | <a id="p100305"></a>737 | <a id="p100306"></a>Doors/Fuselage - Floor Beam Lower Chord and Door Stop Fittings - Inspection |
| <a id="p100307"></a>43 | <a id="p100308"></a>US-2018-19-20 | <a id="p100309"></a>![рис. 43](https://i.bukva.ai/qVoB5aLBh/img_42.png) | <a id="p100310"></a>09.10.2018 | <a id="p100311"></a>BOEING | <a id="p100312"></a>737 | <a id="p100313"></a>Fuselage - Frames and Stub Beams - Inspection/Repair |
| <a id="p100314"></a>44 | <a id="p100315"></a>US-2018-18-13 | <a id="p100316"></a>![рис. 44](https://i.bukva.ai/qVoB5aLBh/img_43.png) | <a id="p100317"></a>09.10.2018 | <a id="p100318"></a>BOEING | <a id="p100319"></a>737 | <a id="p100320"></a>Wings - Outboard Flap Tracks - Inspection |
| <a id="p100321"></a>45 | <a id="p100322"></a>US-2018-17-14 | <a id="p100323"></a>![рис. 45](https://i.bukva.ai/qVoB5aLBh/img_44.png) | <a id="p100324"></a>09.10.2018 | <a id="p100325"></a>GENERAL ELECTRIC | <a id="p100326"></a>CF34-8 | <a id="p100327"></a>Engine Exhaust - Thrust Reverser - Inspection |
| <a id="p100328"></a>46 | <a id="p100329"></a>2018-0216 | <a id="p100330"></a>![рис. 46](https://i.bukva.ai/qVoB5aLBh/img_45.png) | <a id="p100331"></a>08.10.2018 | <a id="p100332"></a>CFM INTERNATIONA L | <a id="p100333"></a>LEAP-1 | <a id="p100334"></a>Engine - Full Authority Digital Electronic Control Software - Replacement |
| <a id="p100335"></a>47 | <a id="p100336"></a>2018-0215 | <a id="p100337"></a>![рис. 47](https://i.bukva.ai/qVoB5aLBh/img_46.png) | <a id="p100338"></a>05.10.2018 | <a id="p100339"></a>AIRBUS | <a id="p100340"></a>A380 | <a id="p100341"></a>Aircraft Flight Manual - Fuel Quantity Indication System Procedure - Amendment |
| <a id="p100342"></a>48 | <a id="p100343"></a>US-2018-19-23 | <a id="p100344"></a>![рис. 48](https://i.bukva.ai/qVoB5aLBh/img_47.png) | <a id="p100345"></a>04.10.2018 | <a id="p100346"></a>BOEING | <a id="p100347"></a>747, 757 | <a id="p100348"></a>Doors - Cargo Door Control Switches - Replacement/Installation |
| <a id="p100349"></a>49 | <a id="p100350"></a>2018-0214 | <a id="p100351"></a>![рис. 49](https://i.bukva.ai/qVoB5aLBh/img_48.png) | <a id="p100352"></a>04.10.2018 | <a id="p100353"></a>DIAMOND AIRCRAFT INDUSTRIES | <a id="p100354"></a>DA 42 | <a id="p100355"></a>Flight Controls - Rudder Pedal Gust Lock Mounts - Removal |
| <a id="p100356"></a>50 | <a id="p100357"></a>CF-2017-04R2 | <a id="p100358"></a>![рис. 50](https://i.bukva.ai/qVoB5aLBh/img_49.png) | <a id="p100359"></a>03.10.2018 | <a id="p100360"></a>BOMBARDIER | <a id="p100361"></a>DHC-8 | <a id="p100362"></a>Fuel System - Corrosion and Wear of Hydraflow Couplings and Sleeves, Fuel Tube End Ferrules, and Fuel Component End Ferrules |
| <a id="p100363"></a>51 | <a id="p100364"></a>ISR-I-24-2018-09-7 | <a id="p100365"></a>![рис. 51](https://i.bukva.ai/qVoB5aLBh/img_50.png) | <a id="p100366"></a>01.10.2018 | <a id="p100367"></a>GULFSTREAM (GALP) | <a id="p100368"></a>G150 | <a id="p100369"></a>Electrical Power - Upper and Lower Front Relay Box Replacement |
| <a id="p100370"></a>52 | <a id="p100371"></a>2018-0213 | <a id="p100372"></a>![рис. 52](https://i.bukva.ai/qVoB5aLBh/img_51.png) | <a id="p100373"></a>01.10.2018 | <a id="p100374"></a>AIRBUS | <a id="p100375"></a>A350 | <a id="p100376"></a>Flight Controls - Inboard Aileron - Modification // Aircraft Flight Manual - Amendment |
| <a id="p100377"></a>53 | <a id="p100378"></a>CF-2018-24 | <a id="p100379"></a>![рис. 53](https://i.bukva.ai/qVoB5aLBh/img_52.png) | <a id="p100380"></a>01.10.2018 | <a id="p100381"></a>BOMBARDIER | <a id="p100382"></a>CL-600 (Challenger) | <a id="p100383"></a>Cold Weather Operations - Introduction of Low Ground Temperature Wing Anti-Ice Procedure |
| <a id="p100384"></a>54 | <a id="p100385"></a>2018-0212 | <a id="p100386"></a>![рис. 54](https://i.bukva.ai/qVoB5aLBh/img_53.png) | <a id="p100387"></a>28.09.2018 | <a id="p100388"></a>AIRBUS | <a id="p100389"></a>A319, A320 | <a id="p100390"></a>Powerplant - CFM56-5A Engine Mount Titanium Crossbeam - Replacement [Life Limitation] |
| <a id="p100391"></a>55 | <a id="p100392"></a>2018-0211 | <a id="p100393"></a>![рис. 55](https://i.bukva.ai/qVoB5aLBh/img_54.png) | <a id="p100394"></a>28.09.2018 | <a id="p100395"></a>CFM INTERNATIONA L | <a id="p100396"></a>CFM56-7B | <a id="p100397"></a>Engine - Fan Blades - Inspection |
| <a id="p100398"></a>56 | <a id="p100399"></a>2018-0199 | <a id="p100400"></a>![рис. 56](https://i.bukva.ai/qVoB5aLBh/img_55.png) | <a id="p100401"></a>26.09.2018 | <a id="p100402"></a>ROLLS-ROYCE PLC | <a id="p100403"></a>RB211 TRENT 900 | <a id="p100404"></a>[Correction] Engine - Oil Service Pipe Sealing Rings - Replacement |
| <a id="p100405"></a>57 | <a id="p100406"></a>US-2018-18-12 | <a id="p100407"></a>![рис. 57](https://i.bukva.ai/qVoB5aLBh/img_56.png) | <a id="p100408"></a>25.09.2018 | <a id="p100409"></a>AIRBUS HELICOPTERS, DONALDSON COMPANY INC. | <a id="p100410"></a>AS 350/EC 130, EASA STC 10017072. STC EASA.IM.R.S.01509, STC SR02393CH | <a id="p100411"></a>Engine Air intake System - Rotorcraft Flight Manual Supplement - Revision |
| <a id="p100412"></a>58 | <a id="p100413"></a>US-2018-17-20 | <a id="p100414"></a>![рис. 58](https://i.bukva.ai/qVoB5aLBh/img_57.png) | <a id="p100415"></a>25.09.2018 | <a id="p100416"></a>BOLING | <a id="p100417"></a>727 | <a id="p100418"></a>Fuel - Airworthiness Limitations/Maintenance or Inspection Program - Revision |
| <a id="p100419"></a>59 | <a id="p100420"></a>US-2018-14-10 | <a id="p100421"></a>![рис. 59](https://i.bukva.ai/qVoB5aLBh/img_58.png) | <a id="p100422"></a>25.04.2018 | <a id="p100423"></a>PRATT & WHITNEY | <a id="p100424"></a>PW2000 | <a id="p100425"></a>Fuel Control Turbine Engines - Electronic Engine Control Software - Installation |
| <a id="p100426"></a>60 | <a id="p100427"></a>2018-0202R1 | <a id="p100428"></a>![рис. 60](https://i.bukva.ai/qVoB5aLBh/img_59.png) | <a id="p100429"></a>25.09.2018 | <a id="p100430"></a>ROLLS-ROYCE PLC | <a id="p100431"></a>RB211-535 | <a id="p100432"></a>Engine - Low' Pressure Compressor Blades - Inspection |
| <a id="p100433"></a>61 | <a id="p100434"></a>2018-0118R1 | <a id="p100435"></a>![рис. 61](https://i.bukva.ai/qVoB5aLBh/img_60.png) | <a id="p100436"></a>25.09.2018 | <a id="p100437"></a>BELL HELICOPTER TEXTRON Inc. (BHTI) | <a id="p100438"></a>212, 412 | <a id="p100439"></a>Main Rotor Drive - Engine-to-Transmission Drive Shaft Line Nuts - Inspection/Replacement |
| <a id="p100440"></a>62 | <a id="p100441"></a>2018-0210-E | <a id="p100442"></a>![рис. 62](https://i.bukva.ai/qVoB5aLBh/img_61.png) | <a id="p100443"></a>25.09.2018 | <a id="p100444"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100445"></a>EC135/635 | <a id="p100446"></a>Equipment & Furnishings - Hoist Carrier Assembly - Inspection |
| <a id="p100447"></a>63 | <a id="p100448"></a>US-2018-23-51 | <a id="p100449"></a>![рис. 63](https://i.bukva.ai/qVoB5aLBh/img_62.png) | <a id="p100450"></a>07.11.2018 | <a id="p100451"></a>BOENG | <a id="p100452"></a>737-8, 737-9 | <a id="p100453"></a>Airplane Flight Manual - Runaway Horizontal Stabilizer Trim Limitations / Procedures - Amendment |


<a id="p100454"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100455"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100456"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

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<a id="p100457"></a>Начальник Управления<br>
поддержания летной годности<br>
воздушных судов<br>
В.В.КУДИНОВ

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<a id="p100458"></a>

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