---
title: "<Письмо> Росавиации от 19.10.2017 N Исх-24084/03"
number: "Исх-24084/03"
issuer: "Федеральное агентство воздушного транспорта"
issued_on: 2017-10-19
status: действует
canonical: "https://bukva.ai/docs/pismo-ish-2408403"
---

## <Письмо> Росавиации от 19.10.2017 N Исх-24084/03

# <Письмо> Росавиации от 19.10.2017 N Исх-24084/03

"Информационное письмо ДЛГ-09-2017"


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

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

<a id="p100003"></a>ПИСЬМО
от 19 октября 2017 г. N Исх-24084/03

<a id="p100004"></a>ИНФОРМАЦИОННОЕ ПИСЬМО ДЛГ-09-2017

<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 11 сентября по 8 октября 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 (Классификация ВС, страны, выпустившей ДЛГ) | <a id="p100012"></a>Краткое содержание |
| --- | --- | --- | --- | --- | --- | --- |
| <a id="p100013"></a>1 | <a id="p100014"></a>2017-0197 | <a id="p100015"></a>![рис. 1](https://i.bukva.ai/x46OfPoJL/img_0.png) | <a id="p100016"></a>06.10.2017 | <a id="p100017"></a>ROLLS-ROYCE PLC | <a id="p100018"></a>VIPER MK 601-22 | <a id="p100019"></a>Engine - Oil Pump Assembly/Oil Pressure Filter - Inspection/Replacement |
| <a id="p100020"></a>2 | <a id="p100021"></a>US-2017-20-06 | <a id="p100022"></a>![рис. 2](https://i.bukva.ai/x46OfPoJL/img_1.png) | <a id="p100023"></a>06.10.2017 | <a id="p100024"></a>HONEYWELL INTERNATIONAL INC. | <a id="p100025"></a>AS907 | <a id="p100026"></a>Engine - Second Stage Low-Pressure Turbine (LPT2) Blade - Inspection |
| <a id="p100027"></a>3 | <a id="p100028"></a>2017-0196 | <a id="p100029"></a>![рис. 3](https://i.bukva.ai/x46OfPoJL/img_2.png) | <a id="p100030"></a>05.10.2017 | <a id="p100031"></a>AEROCONSEIL, AIRBUS, BRITISH AIRWAYS plc, FOKKER SERVICES, H4 AEROSPACE (UK) LTD, PMV ENGINEERING, SCANDINAVIAN AVIONICS DESIGN ApS | <a id="p100032"></a>EASA STC 10045396, A318, A319, A320, A321, A330, A340, EASA STC 10039421, EASA STC 10047494, EASA STC 10051008, EASA STC 10047157, EASA STC 10047744, EASA STC 10050434, EASA STC 10050942, EASA STC 10051659, EASA STC 10051519, EASA STC 10054797 | <a id="p100033"></a>Navigation - Traffic Collision Avoidance System Processor - Modification (Software Update)/Replacement |
| <a id="p100034"></a>4 | <a id="p100035"></a>2017-0195 | <a id="p100036"></a>![рис. 4](https://i.bukva.ai/x46OfPoJL/img_3.png) | <a id="p100037"></a>04.10.2017 | <a id="p100038"></a>AIRBUS | <a id="p100039"></a>A340 | <a id="p100040"></a>Exhaust - Thrust Reverser Outer Fixed Structure - Inspection/Replacement |
| <a id="p100041"></a>5 | <a id="p100042"></a>2016-0166-Е | <a id="p100043"></a>![рис. 5](https://i.bukva.ai/x46OfPoJL/img_4.png) | <a id="p100044"></a>04.10.2017 | <a id="p100045"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100046"></a>AB204/AB205, AB212/AB412 | <a id="p100047"></a>[Correction] Main Rotor Drive - Spiral Bevel Gear - Inspection |
| <a id="p100048"></a>6 | <a id="p100049"></a>US-2017-20-05 | <a id="p100050"></a>![рис. 6](https://i.bukva.ai/x46OfPoJL/img_5.png) | <a id="p100051"></a>04.10.2017 | <a id="p100052"></a>BOEING | <a id="p100053"></a>757 | <a id="p100054"></a>Fuselage - Crown Skin Panel - Inspection/Repair/Replacement |
| <a id="p100055"></a>7 | <a id="p100056"></a>US-2017-19-02 | <a id="p100057"></a>![рис. 7](https://i.bukva.ai/x46OfPoJL/img_6.png) | <a id="p100058"></a>02.10.2017 | <a id="p100059"></a>BOEING | <a id="p100060"></a>727 | <a id="p100061"></a>Doors - Main Cargo Door Cam Support Assemblies - Inspection |
| <a id="p100062"></a>8 | <a id="p100063"></a>US-2017-17-19 | <a id="p100064"></a>![рис. 8](https://i.bukva.ai/x46OfPoJL/img_7.png) | <a id="p100065"></a>29.09.2017 | <a id="p100066"></a>BOEING | <a id="p100067"></a>DC-9, MD-88 | <a id="p100068"></a>Fuselage - Bulkhead Structures - Inspection |
| <a id="p100069"></a>9 | <a id="p100070"></a>US-2017-20-01 | <a id="p100071"></a>![рис. 9](https://i.bukva.ai/x46OfPoJL/img_8.png) | <a id="p100072"></a>29-09.2017 | <a id="p100073"></a>HONEYWELL INTERNATIONAL INC. | <a id="p100074"></a>TFE731-20/-40/-50/-60 | <a id="p100075"></a>Turbine Engine Compressor Section - Fan Disks - Removal/Replacement |
| <a id="p100076"></a>10 | <a id="p100077"></a>CF-2017-33 | <a id="p100078"></a>![рис. 10](https://i.bukva.ai/x46OfPoJL/img_9.png) | <a id="p100079"></a>29.09.2017 | <a id="p100080"></a>VIKING AIR LTD | <a id="p100081"></a>DHC-2 | <a id="p100082"></a>Airframe - Corrosion |
| <a id="p100083"></a>11 | <a id="p100084"></a>2017-0193 | <a id="p100085"></a>![рис. 11](https://i.bukva.ai/x46OfPoJL/img_10.png) | <a id="p100086"></a>29.09.2017 | <a id="p100087"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100088"></a>MBB-BK 117 | <a id="p100089"></a>Main Rotor Drive - Main Rotor Mast - Inspection |
| <a id="p100090"></a>12 | <a id="p100091"></a>US-2017-17-18 | <a id="p100092"></a>![рис. 12](https://i.bukva.ai/x46OfPoJL/img_11.png) | <a id="p100093"></a>29.09.2017 | <a id="p100094"></a>GENERAL ELECTRIC | <a id="p100095"></a>CF34-8 | <a id="p100096"></a>Turbine Engine - Fan Blades - Life Limit Reduction |
| <a id="p100097"></a>13 | <a id="p100098"></a>2017-0194-E | <a id="p100099"></a>![рис. 13](https://i.bukva.ai/x46OfPoJL/img_12.png) | <a id="p100100"></a>29.09.2017 | <a id="p100101"></a>AIRBUS HELICOPTERS | <a id="p100102"></a>EC175 | <a id="p100103"></a>Stabilizers - Horizontal Stabilizer Attachment Bolts - Inspection/Modification/Clearance Check Rotorcraft Flight Manual - Amendment |
| <a id="p100104"></a>14 | <a id="p100105"></a>2017-0192 | <a id="p100106"></a>![рис. 14](https://i.bukva.ai/x46OfPoJL/img_13.png) | <a id="p100107"></a>28.09.2017 | <a id="p100108"></a>APPLIANCES | <a id="p100109"></a>ATA25 EQUIPMENT/FURNISHINGS | <a id="p100110"></a>RECARO Aircraft Seating Gmbh & Co. KG - Passenger Seats - Modification |
| <a id="p100111"></a>15 | <a id="p100112"></a>CF-2017-32 | <a id="p100113"></a>![рис. 15](https://i.bukva.ai/x46OfPoJL/img_14.png) | <a id="p100114"></a>28.09.2017 | <a id="p100115"></a>BOMBARDIER | <a id="p100116"></a>BD-700 | <a id="p100117"></a>Flight Controls - Elevator Control System Bracket Cracking |
| <a id="p100118"></a>16 | <a id="p100119"></a>US-2017-19-20 | <a id="p100120"></a>![рис. 16](https://i.bukva.ai/x46OfPoJL/img_15.png) | <a id="p100121"></a>26.09.2017 | <a id="p100122"></a>GENERAL ELECTRIC | <a id="p100123"></a>CT7-8, CT7-9 | <a id="p100124"></a>Turbine Engine - High-Pressure Compressor Impeller - Removal |
| <a id="p100125"></a>17 | <a id="p100126"></a>US-2017-19-10 | <a id="p100127"></a>![рис. 17](https://i.bukva.ai/x46OfPoJL/img_16.png) | <a id="p100128"></a>26.09.2017 | <a id="p100129"></a>BOEING | <a id="p100130"></a>757 | <a id="p100131"></a>Doors - Main Cargo Door Cam Support Assemblies - Inspection/Replacement |
| <a id="p100132"></a>18 | <a id="p100133"></a>CF-2017-31 | <a id="p100134"></a>![рис. 18](https://i.bukva.ai/x46OfPoJL/img_17.png) | <a id="p100135"></a>25.09.2017 | <a id="p100136"></a>BOMBARDIER | <a id="p100137"></a>BD-700 | <a id="p100138"></a>Fuselage - Attachments for Belly Fairing Access Panels - Replacement |
| <a id="p100139"></a>19 | <a id="p100140"></a>2017-0190 | <a id="p100141"></a>![рис. 19](https://i.bukva.ai/x46OfPoJL/img_18.png) | <a id="p100142"></a>25.09.2017 | <a id="p100143"></a>AIRBUS HELICOPTERS | <a id="p100144"></a>EC175 | <a id="p100145"></a>Fuel System - Additional Fuel Tank 4 - Inspection |
| <a id="p100146"></a>20 | <a id="p100147"></a>2017-0191-E | <a id="p100148"></a>![рис. 20](https://i.bukva.ai/x46OfPoJL/img_19.png) | <a id="p100149"></a>25.09.2017 | <a id="p100150"></a>AIRBUS HELICOPTERS | <a id="p100151"></a>SA 330/AS 332/EC 225 | <a id="p100152"></a>Main Rotor - Rotating Swashplate Yokes - Inspection/Rework |
| <a id="p100153"></a>21 | <a id="p100154"></a>US-2017-16-10 | <a id="p100155"></a>![рис. 21](https://i.bukva.ai/x46OfPoJL/img_20.png) | <a id="p100156"></a>22.09.2017 | <a id="p100157"></a>BOEING | <a id="p100158"></a>777 | <a id="p100159"></a>Wings - Underwing Longerons - Inspection |
| <a id="p100160"></a>22 | <a id="p100161"></a>2017-0189 | <a id="p100162"></a>![рис. 22](https://i.bukva.ai/x46OfPoJL/img_21.png) | <a id="p100163"></a>22.09.2017 | <a id="p100164"></a>AIRBUS HELICOPTERS | <a id="p100165"></a>SA 330/AS 332/EC 225 | <a id="p100166"></a>Time Limits/Maintenance Checks - Main Gearbox Suspension Bar Pins/Fittings - Re-calculation of Life Limits/Replacement |
| <a id="p100167"></a>23 | <a id="p100168"></a>2017-0187 | <a id="p100169"></a>![рис. 23](https://i.bukva.ai/x46OfPoJL/img_22.png) | <a id="p100170"></a>22.09.2017 | <a id="p100171"></a>BAE SYSTEMS (OPERATIONS) LTD | <a id="p100172"></a>JETSTREAM4100 | <a id="p100173"></a>Time Limits/Maintenance Checks - Fatigue and Environmental Damage Inspections - Amendment |
| <a id="p100174"></a>24 | <a id="p100175"></a>2017-0188 | <a id="p100176"></a>![рис. 24](https://i.bukva.ai/x46OfPoJL/img_23.png) | <a id="p100177"></a>22.09.2017 | <a id="p100178"></a>AIRBUS | <a id="p100179"></a>A380 | <a id="p100180"></a>Fuselage - Frame 94 Upper Shell - Inspection |
| <a id="p100181"></a>25 | <a id="p100182"></a>2017-0185 | <a id="p100183"></a>![рис. 25](https://i.bukva.ai/x46OfPoJL/img_24.png) | <a id="p100184"></a>22.09.2017 | <a id="p100185"></a>AIRBUS | <a id="p100186"></a>A330, A340 | <a id="p100187"></a>Landing Gear - Parts with 300M Material Properties outside of Specification Requirements - Identification/Replacement [Life Limit] |
| <a id="p100188"></a>26 | <a id="p100189"></a>CF-2017-05R1 | <a id="p100190"></a>![рис. 26](https://i.bukva.ai/x46OfPoJL/img_25.png) | <a id="p100191"></a>22.09.2017 | <a id="p100192"></a>BOMBARDIER | <a id="p100193"></a>DHC-8 | <a id="p100194"></a>Fuel System - Motive Flow Line Fouling and Motive Flow Line and Pressure Relief Line Broken P-Clamps |
| <a id="p100195"></a>27 | <a id="p100196"></a>2017-0186 | <a id="p100197"></a>![рис. 27](https://i.bukva.ai/x46OfPoJL/img_26.png) | <a id="p100198"></a>21.09.2017 | <a id="p100199"></a>AIRBUS | <a id="p100200"></a>A380 | <a id="p100201"></a>Electrical Power - Ram Air Turbine Uplock Assembly - Modification |
| <a id="p100202"></a>28 | <a id="p100203"></a>2017-0184 | <a id="p100204"></a>![рис. 28](https://i.bukva.ai/x46OfPoJL/img_27.png) | <a id="p100205"></a>20.09.2017 | <a id="p100206"></a>MECAER AVIATION GROUP SpA | <a id="p100207"></a>NH-300C | <a id="p100208"></a>Main Rotor Drive - Lower Coupling Drive Shaft - Inspection |
| <a id="p100209"></a>29 | <a id="p100210"></a>US-2017-16-01 | <a id="p100211"></a>![рис. 29](https://i.bukva.ai/x46OfPoJL/img_28.png) | <a id="p100212"></a>20.09.2017 | <a id="p100213"></a>APPLIANCES | <a id="p100214"></a>ATA25 EQUIPMENT/FURNISHINGS | <a id="p100215"></a>AMERI-KING CORPORATION - Emergency Locator Transmitters - Inspection |
| <a id="p100216"></a>30 | <a id="p100217"></a>2017-0183 | <a id="p100218"></a>![рис. 30](https://i.bukva.ai/x46OfPoJL/img_29.png) | <a id="p100219"></a>20.09.2017 | <a id="p100220"></a>AIRBUS | <a id="p100221"></a>A380 | <a id="p100222"></a>Nacelles/Pylons - Inboard and Outboard Pylon Drain System - Inspection |
| <a id="p100223"></a>31 | <a id="p100224"></a>2017-0161R1 | <a id="p100225"></a>![рис. 31](https://i.bukva.ai/x46OfPoJL/img_30.png) | <a id="p100226"></a>20.09.2017 | <a id="p100227"></a>AIRBUS | <a id="p100228"></a>A319, A320, A321 | <a id="p100229"></a>[Correction] Electric and Electronic Common Installation - Battery Retaining Rods - Identification/Replacement |
| <a id="p100230"></a>32 | <a id="p100231"></a>2017-0182 | <a id="p100232"></a>![рис. 32](https://i.bukva.ai/x46OfPoJL/img_31.png) | <a id="p100233"></a>19.09.2017 | <a id="p100234"></a>AIRBUS | <a id="p100235"></a>A380 | <a id="p100236"></a>Fuel - Fuel Pumps/Outboard Collector Cell Jet Pump - Functional Check/Inspection |
| <a id="p100237"></a>33 | <a id="p100238"></a>US-2017-18-14 | <a id="p100239"></a>![рис. 33](https://i.bukva.ai/x46OfPoJL/img_32.png) | <a id="p100240"></a>19.09.2017 | <a id="p100241"></a>ROLLS-ROYCE CORPORATION (USA) | <a id="p100242"></a>250 Series II | <a id="p100243"></a>Engine - 3rd and 4th Stage Turbine Wheels - Inspection/Removal |
| <a id="p100244"></a>34 | <a id="p100245"></a>US-2017-18-06 | <a id="p100246"></a>![рис. 34](https://i.bukva.ai/x46OfPoJL/img_33.png) | <a id="p100247"></a>18.09.2017 | <a id="p100248"></a>BOEING | <a id="p100249"></a>747 | <a id="p100250"></a>Wings - Leading Edge Area - Modification |
| <a id="p100251"></a>35 | <a id="p100252"></a>US-2017-18-05 | <a id="p100253"></a>![рис. 35](https://i.bukva.ai/x46OfPoJL/img_34.png) | <a id="p100254"></a>18.09.2017 | <a id="p100255"></a>BOEING | <a id="p100256"></a>747 | <a id="p100257"></a>Wings - Fuse Pin of the Landing Gear Beam End Fitting - Replacement/Inspection |
| <a id="p100258"></a>36 | <a id="p100259"></a>2017-0179 | <a id="p100260"></a>![рис. 36](https://i.bukva.ai/x46OfPoJL/img_35.png) | <a id="p100261"></a>18.09.2017 | <a id="p100262"></a>BAE SYSTEMS (OPERATIONS) LTD | <a id="p100263"></a>ATP | <a id="p100264"></a>Wings - Front Spar/C-Channels - Inspection |
| <a id="p100265"></a>37 | <a id="p100266"></a>2017-0181 | <a id="p100267"></a>![рис. 37](https://i.bukva.ai/x46OfPoJL/img_36.png) | <a id="p100268"></a>18.09.2017 | <a id="p100269"></a>EADS CASA | <a id="p100270"></a>C-295, CN-235 | <a id="p100271"></a>Doors - Nose Landing Gear Door Actuator Shaft Assembly - Inspection |
| <a id="p100272"></a>38 | <a id="p100273"></a>2017-0180 | <a id="p100274"></a>![рис. 38](https://i.bukva.ai/x46OfPoJL/img_37.png) | <a id="p100275"></a>18.09.2017 | <a id="p100276"></a>AIRBUS | <a id="p100277"></a>A350 | <a id="p100278"></a>SUPERSEDED BY EASA AD 2017-0200 |
| <a id="p100279"></a>39 | <a id="p100280"></a>2017-0178 | <a id="p100281"></a>![рис. 39](https://i.bukva.ai/x46OfPoJL/img_38.png) | <a id="p100282"></a>15.09.2017 | <a id="p100283"></a>AIRBUS, SHORT BROTHERS PLC | <a id="p100284"></a>A319, A320, A321, EASA STC 10029547 | <a id="p100285"></a>Power Plant - Monolithic Fan Cowl Doors - Modification |
| <a id="p100286"></a>40 | <a id="p100287"></a>2017-0017R2 | <a id="p100288"></a>![рис. 40](https://i.bukva.ai/x46OfPoJL/img_39.png) | <a id="p100289"></a>15.09.2017 | <a id="p100290"></a>ROLLS-ROYCE PLC | <a id="p100291"></a>TRENT 1000 | <a id="p100292"></a>Engine - Intermediate Pressure Compressor Rotor Seal - Inspection |
| <a id="p100293"></a>41 | <a id="p100294"></a>2011-0164R2 | <a id="p100295"></a>![рис. 41](https://i.bukva.ai/x46OfPoJL/img_40.png) | <a id="p100296"></a>15.09.2017 | <a id="p100297"></a>AIRBUS HELICOPTERS | <a id="p100298"></a>AS 350/EC 130, AS 355 | <a id="p100299"></a>Rotors Flight Control - Tail Rotor Control Stop Screws - Inspection |
| <a id="p100300"></a>42 | <a id="p100301"></a>2017-0177 | <a id="p100302"></a>![рис. 42](https://i.bukva.ai/x46OfPoJL/img_41.png) | <a id="p100303"></a>14.09.2017 | <a id="p100304"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100305"></a>MBB-BK 117 | <a id="p100306"></a>Equipment & Furnishing - Outboard Load System - Inspection/Replacement |
| <a id="p100307"></a>43 | <a id="p100308"></a>2017-0176-E | <a id="p100309"></a>![рис. 43](https://i.bukva.ai/x46OfPoJL/img_42.png) | <a id="p100310"></a>14.09.2017 | <a id="p100311"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100312"></a>A109/A119 | <a id="p100313"></a>Main Rotor - Main Rotor Blades - Inspection/Replacement |
| <a id="p100314"></a>44 | <a id="p100315"></a>2017-0175-E | <a id="p100316"></a>![рис. 44](https://i.bukva.ai/x46OfPoJL/img_43.png) | <a id="p100317"></a>13.09.2017 | <a id="p100318"></a>LEONARDO S.p.A. HELICOPTERS | <a id="p100319"></a>AB139/AW139 | <a id="p100320"></a>Main Rotor - Main Rotor Blades - Inspection/Replacement |
| <a id="p100321"></a>45 | <a id="p100322"></a>US-2017-16-05 | <a id="p100323"></a>![рис. 45](https://i.bukva.ai/x46OfPoJL/img_44.png) | <a id="p100324"></a>12.09.2017 | <a id="p100325"></a>BOEING | <a id="p100326"></a>737 | <a id="p100327"></a>Wings - Krueger Flap Bullnose Attachment Hardware - Inspection |
| <a id="p100328"></a>46 | <a id="p100329"></a>US-2017-18-12 | <a id="p100330"></a>![рис. 46](https://i.bukva.ai/x46OfPoJL/img_45.png) | <a id="p100331"></a>12.09.2017 | <a id="p100332"></a>APPLIANCES | <a id="p100333"></a>ATA 35 OXYGEN | <a id="p100334"></a>B/E AEROSPACE - Protective Breathing Equipment - Inspection/Replacement |
| <a id="p100335"></a>47 | <a id="p100336"></a>US-2017-18-11 | <a id="p100337"></a>![рис. 47](https://i.bukva.ai/x46OfPoJL/img_46.png) | <a id="p100338"></a>12.09.2017 | <a id="p100339"></a>BEECHCRAFT CORPORATION | <a id="p100340"></a>390 | <a id="p100341"></a>Hydraulic Power - Engine Driven Pumps - Inspection/Replacement |
| <a id="p100342"></a>48 | <a id="p100343"></a>2017-0162 | <a id="p100344"></a>![рис. 48](https://i.bukva.ai/x46OfPoJL/img_47.png) | <a id="p100345"></a>12.09.2017 | <a id="p100346"></a>ROLLS-ROYCE PLC | <a id="p100347"></a>RB211-22B, RB211-524 | <a id="p100348"></a>[Correction] Engine - Low Pressure Turbine Roller Bearing - Replacement |
| <a id="p100349"></a>49 | <a id="p100350"></a>2017-0174 | <a id="p100351"></a>![рис. 49](https://i.bukva.ai/x46OfPoJL/img_48.png) | <a id="p100352"></a>12.09.2017 | <a id="p100353"></a>AIRBUS HELICOPTERS DEUTSCHLAND | <a id="p100354"></a>MBB-BK 117 | <a id="p100355"></a>Time Limits/Maintenance Checks - Airworthiness Limitations - Amendment |
| <a id="p100356"></a>50 | <a id="p100357"></a>2013-0192-CN | <a id="p100358"></a>![рис. 50](https://i.bukva.ai/x46OfPoJL/img_49.png) | <a id="p100359"></a>12.09.2017 | <a id="p100360"></a>POWERJET S.A. | <a id="p100361"></a>SaM146 | <a id="p100362"></a>CANCELLED: Engine - Accessory Gearbox Integrated Drive Generator Spur Gearshaft - Identification/Replacement |
| <a id="p100363"></a>51 | <a id="p100364"></a>US-2017-17-06 | <a id="p100365"></a>![рис. 51](https://i.bukva.ai/x46OfPoJL/img_50.png) | <a id="p100366"></a>12.09.2017 | <a id="p100367"></a>BOEING | <a id="p100368"></a>737 | <a id="p100369"></a>Fuselage - Fuselage Frame - Inspection |
| <a id="p100370"></a>52 | <a id="p100371"></a>US-2017-17-09 | <a id="p100372"></a>![рис. 52](https://i.bukva.ai/x46OfPoJL/img_51.png) | <a id="p100373"></a>11.09.2017 | <a id="p100374"></a>BOEING | <a id="p100375"></a>737 | <a id="p100376"></a>Wings - Fuel Tank Access Door - Replacement/Check/Maintenance or Inspection Program Revision |


<a id="p100377"></a>Тексты Директив летной годности находятся на интернет-ресурсах соответствующих авиационных администраций и разработчиков АТ.
<a id="p100378"></a>Руководителям Межрегиональных территориальных управлений воздушного транспорта Федерального агентства воздушного транспорта довести данную информацию до подконтрольных авиапредприятий Российской Федерации.
<a id="p100379"></a>Организациям, эксплуатирующим указанные ВС, принять меры по своевременному выполнению требований применимых директив летной годности.

<a id="p100380"></a>Начальник Управления
поддержания летной годности
воздушных судов
В.В.КУДИНОВ



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