AW 1 3 9 R F M

Document N°
139G0290X002

ROTORCRAFT
FLIGHT MANUAL
AgustaWestland S.p.A. Publication Code 502500032
 AW139 - RFM - 4D
Document N°
139G0290X002

ROTORCRAFT FLIGHT MANUAL

Copy assigned to rotorcraft:
S/N . . . . . . . . . . . . . . . . . . . . . . . . .
Registration Marks . . . . . . . . . . . . .

ISSUE 2 : 10-11-2010
Rev. 22 : 19-10-2017
AW139 and AB139 are two names of the same product.
They identify two batches of aircraft manufactured in conformity
with a unique Type Certificate Data Sheet
Where not specifically declared, the content of this document is
applicable to both AW139 and AB139 helicopters.

Continuing airworthiness criteria for the AW139 is developed and maintained

by Agusta, who is the holder of the type certificate in the state of design.

E.A.S.A. Approval Date:

10 November 2010.

Publication Code: 502500032

 AW139 - RFM - 4D
Document N°
139G0290X002

This Page Intentionally Left Blank

 AW139 - RFM - 4D
Document N°
139G0290X002

This publication contains information proprietary to Finmeccanica

S.p.A. Reproduction and/or resale of the information or illustrations
contained herein is not permitted without the written approval of CUS-
TOMER SUPPORT & SERVICES - ITALY - Product Support Engi-
neering Dept. Additional copies of this publication and/or change
service may be obtained from:

FINMECCANICA S.p.A.
HELICOPTER DIVISION
CUSTOMER SUPPORT & SERVICES - ITALY
Via Giovanni Agusta, 520
21017 Cascina Costa di Samarate (VA) Italy
Tel.: 0039-0331 225036 - Fax.: 0039-0331 225988
e-mail: GestPubs@finmeccanica.com

Rev. 18
 AW139 - RFM - 4D
Document N°
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This Page Intentionally Left Blank

 AW139 - RFM - 4D Table of Contents
Document N°
139G0290X002

TABLE OF CONTENTS

Page
Record of Temporary Revisions TR-1
Record of Revisions A-1
Record of Effective Pages B-1
Introduction I-1

PART I - E.A.S.A. APPROVED

Section
Limitations 1-1
Normal Procedures 2-1
Emergency and Malfunction Procedures 3-1
Performance Data 4-1
Optional Equipment Supplements 5-1

E.A.S.A. Approved TOC-1

Table of Contents AW139 - RFM - 4D
Document N°
139G0290X002

PART II - MANUFACTURER’S DATA

Section
Weight and Balance 6-1
System Description 7-1
Handling, Servicing and Maintenance 8-1
Supplemental Performance Information 9-1

TOC-2 E.A.S.A. Approved

 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

Record of Revisions
REVISION
SUBJECT APPROVAL
No.
--- Issue 2 is equivalent to Issue 1 Rev Approval No. EASA
21 with the following changes: 10032486
Dated: November 10,
• All page headings updated with 2010
the new product logo.
• Editorial corrections and non
sequential pages added in pre-
vious revisions incorporated
into RFM.
• Altitude limitations and perfor-
mance data presented in feet
and meters.
• Groundspeed presented in
knots and km/hr.
• Windspeed limits presented in
knots and meters per second.
Section 2 Optional standby Approval No. EASA
instrument MEGGITT included. 10032487
Dated:
November 10, 2010
Section 5 Updated Incompatibility Approval No. EASA
Table. 10032485
Supplement 71 Section 1, Placard Dated:
page updated IAW 139G3000A001 November 10, 2010
Icing Compatibility Handbook
1 Section 5 Pages: 5-i, 5-2 thru 5-4, 5-7 Approval No.
thru 5-16. EASA 10033123
Section 5 Supp. 12 Pages: S12-A17, Dated:
S12-B14, S12-C19, December 20, 2010
and S12-C20,
S12-D24 and
S12-D25, S12-E2 and
S12-E3, S12-E11 and
S12-E12, S12-E17
and S12-E18,

Page A-1
Rev. 16
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
1 (cont.) S12-E20 and
S12-E21, S12-E25,
S12-E27, S12-E29,
S12-E31, S12-F14,
S12-G16, S12-H15
and S12-H16, S12-J8,
S12-I1 thru S12-I8,
S12-I12 thru S12-I44,
S12-L2, S12-L7,
S12-L11 thru S12-L17.
Section 3 Pages: 3-35 and 3-36. Approval No.
Section 5 Supp. 1 Page: S1-5. EASA 10033121
Section 5 Supp. 2 Page: S2-16. Dated:
Section 5 Supp. 5 Pages: S5-iii, S5-16 December 20, 2010
and S5-17, S5-19.
Section 5 Supp. 11 Page: S11-17.
Section 5 Supp. 17 Page: S17-i.
Section 5 Supp. 29 Pages: S29-iv,
S29-1 thru S29-3,
S29-6, S29-28.
Section 5 Supp. 31 Pages: S31-1,
S31-5.
Section 5 Supp. 36 Page: S36-i.
Section 5 Supp. 41 Pages: S41-18,
S41-26.
Section 5 Supp. 44 Pages: S44-i,
S44-5.
Section 5 Supp. 49 Page: S49-20.
Section 5 Supp. 50 Pages: S50-5,
S50-84, S50-84A and
S50-84B, S50-113,
S50-115, S50-117,
S50-119, S50-121 thru
S50-126.
Section 5 Supp. 54 Pages: S54-iii,
S54-3 thru S54-14.
Section 5 Supp. 65 Pages: S65-1,
S65-3 thru S65-8.
Section 5 Supp. 67 Pages: S67-14 thru
S67-17.

Page A-2
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Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
1 (cont.) Section 5 Supp. 68 Pages: S68-17 and
S68-18.
Section 5 Supp. 69 Pages: S69-14 thru
S69-21.
Section 5 Supp. 70 Pages: S70-12 thru
S70-15.
Section 5 Supp. 71 Page: S71-8.
Section 5 New Issue Supplement 74.
Section 5 Supp. 23 Page: S23-24. Manufacturer’s Data
Section 7 Pages: 7-iii thru 7-vi, 7-136
thru 7-138.
2 Section 5 Supp. 11 Pages: S11-iii and Approval No.
S11-iv, S11-12 thru EASA 10037547 and
S11-18, S11-18A and EASA 10037548
S11-18B, S11-25 and Dated:
S11-26, S11-29.
December 5, 2011
Section 5 Supp. 41 Pages: S41-iii and
S41-iv, S41-12,
S41-17, S41-29 and
S41-30, S41-33.
Section 5 Supp. 49 Pages: S49-iii and
S49-iv, S49-14,
S49-19, S49-29 and
S49-30, S49-32.
Section 5 Supp. 50 Page: S50-6.
Section 1 Pages: 1-iii, 1-8, 1-32, 1-36. Approval No.
QRH Revision required EASA 10037551,
Section 2 Pages: 2-6 thru 2-9, 2-26, EASA 10037550 and
2-31. EASA 10037545
QRH Revision required
Dated:
Section 5 Supp. 50 Pages: S50-iii,
December 5, 2011
S50-v thru S50-vii,
S50-ix and S50-x,
S50-2A and S50-2B,
S50-4, S50-19 and
S50-20, S50-20A and
S50-20B, S50-21,
S50-139 thru
S50-146.

Page A-3
Rev. 16
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
2 (cont.) Section 5 Supp. 38 Pages:
S38-i, S38-iii, S38-1
and S38-2, S38-10.
Section 5 Supp. 31 Pages: S31-iii,
S31-3, S31-5.
Section 5 Supp. 54 Pages: S54-9 and
S54-10.
Section 5 Supp. 65 Page: S65-4.
Section 3 Pages: 3-49, 3-126, 3-141,
3-145, and 3-146,
3-151, 3-163 and
3-164, 3-167, 3-173
thru 3-176, 3-178.
QRH Revision required
Section 5 Supp. 74 Page: S74-1.
Section 5 Supp. 12 Pages: S12-B6,
S12-D27, S12-F7.
QRH Revision required
Section 5 Supp. 51 Pages: S51-iii,
S51-1 thru S51-4,
S51-6, S51-6A and
S51-6B.
Section 5 Supp. 71 Pages: S71-18,
S71-48.
Section 5 Supp. 11 Pages: S11-9 thru
S11-11.
Section 5 Supp. 41 Pages: S41-9 thru
S41-11, S41-13 thru
S41-16, S41-18,
S41-18A and
S41-18B, S41-29 thru
S41-31, S41-33.
Section 5 Supp. 49 Pages: S49-11 thru
S49-13, S49-15 thru
S49-18, S49-20, S49-
20A and S49-20B,
S49-29 and S49-30,
S49-32.
Section 5 Supp. 16 Pages: S16-i,
S16-iii, S16-1 thru
S16-3.

Page A-4
Rev. 16
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
2 (cont.) Section 5 Supp. 29 Pages: S29-i,
S29-iv, S29-2 thru
S29-4, S29-6 thru
S29-8, S29-28.
Section 5 Pages: 5-2 thru 5-7, 5-9 thru
5-15.
Section 5 Supp. 58 Page: S58-1.
Section 5 Supp. 19 Page: S19-2.
Section 5 Supp. 20 Page: S20-2.
Section 5 Supp. 17 Pages: S17-1,
S17-4 and S17-5.
Section 5 Supp. 37 Page: S37-2. Manufacturer’s Data
Section 5 Supp. 5 Page: S5-109 and
S5-110.
Section 5 Supp. 7 Page: S7-3 and
S7-4.
Section 5 Supp. 23 Page: S23-16.
Section 5 Supp. 25 Pages: S25-iii,
S25-7 thru S25-9.
Section 5 Supp. 33 Page: S33-4.
Section 5 Supp. 35 Page: S35-6.
Section 5 Supp. 52 Page: S52-5.
Section 5 Supp. 59 Page: S59-4.
Section 5 Supp. 61 Page: S61-6.
Section 5 Supp. 66 Page: S66-6.
Section 2 Page: 2-41.
Section 7 Pages: 7-iii, 7-118, 7-138.

3 Section 5 Pages: 5-7, 5-9 thru 5-16. Approval No.

Section 5 Supp. 9 Pages: S9-i, S9-iv, EASA 10040469
S9-1 thru S9-3, S9-5 Dated: July 18, 2012
and S9-6, S9-13,
S9-16, S9-19.
Section 5 New Issue Supplement 77.
Section 2 Page: 2-12. Approval No.
Section 5 Supp. 67 Pages: S67-25. EASA 10040467
Section 5 Supp. 69 Pages: S69-28. Dated: July 18, 2012
Section 5 Supp. 70 Pages: S70-21.

Page A-5
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Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
3 (cont.) Section 5 Supp. 56 Pages: S56-i thru Approval No.
S56-iv, S56-1 thru EASA 10040464
S56-12. Dated: July 5, 2012
Section 1 Page: 1-33.
Section 2 Pages: 2-ii, 2-11, 2-13, 2-21
thru 2-24, 2-32, 2-36,
2-49 and 2-50.
QRH Revision required
Section 3 Pages: 3-iii thru 3-viii, 3-55,
3-75, 3-95 thru 3-98,
3-104, 3-110, 3-115,
3-117 and 3-118.
QRH Revision required
Section 5 Supp. 1 Page: S1-2.
Section 5 Supp. 23 Page: S23-5.
Section 5 Supp. 10 Page: S10-4.
Section 5 Supp. 11 Page: S11-13.
Section 5 Supp. 12 Pages: S12-B2,
S12-B29, S12-C2 and
S12-C3, S12-C21,
S12-C29, S12-C31,
S12-D3 and S12-D4,
S12-D27, S12-D35,
S12-D37, S12-E25,
S12-E27, S12-E29,
S12-F2, S12-F14,
S12-F27, S12-F29,
S12-F31, S12-J8,
S12-L3, S12-L11.
Section 5 Supp. 50 Pages: S50-iii and
S50-iv, S50-viii and
S50-ix, S50-4 and
S50-5, S50-13,
S50-109, S50-113,
S50-115, S50-117.
Section 5 Supp. 34 Pages: S34-22,
S34-32.
Section 5 Supp. 40 Pages: S40-20,
S40-30.
Section 5 Supp. 67 Pages: S67-35.

Page A-6
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Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
3 (cont.) Section 5 Supp. 69 Page: S69-40.
Section 5 Supp. 70 Page: S70-32.
Section 4 Pages: 4-7, 4-29 and 4-30.
Section 5 Supp. 60 Page: S60-7.
Section 5 Supp. 74 Page: S74-1.
Section 5 New Issue Supplement 78.
Section 5 New Issue Supplement 75. Approval No.
Section 5 Supp. 71 Page: S71-8. EASA 10040466
Dated: July 18, 2012
Section 6 Chart E Page: 1. Manufacturer’s Data
Chart D Page: 1
Section 7 Pages: 7-iii, 7-4, 7-89 and
7-90, 7-134.
4 Section 5 New Issue Supplement 83. Approval No.
EASA 10042530
Dated: December 06,
2012
Section 5 Supp. 9 Pages: S9-iv, S9-1 Approval No.
and S9-2, S9-5 and EASA 10042531
S9-6, S9-6A and Dated: December 06,
S9-6B. 2012
Section 1 Page: 1-ii, 1-29 thru 1-32. Approval No.
Section 2 Pages: 2-13, 2-21 thru 2-23. EASA 10042529
Section 3 Pages: 3-40, 3-52, 3-68, Dated: December 06,
3-72, 3-103, 3-132. 2012
Section 4 Pages: 4-63, 4-65.
Section 5 Pages: 5-2, 5-5 thru 5-7, 5-11
thru 5-16.
Section 5 Supp. 1 Page: S1-5.
Section 5 Supp. 9 Pages: S9-8 thru
S9-15, S9-17 and
S9-18, S9-20 and
S9-21.
Section 5 Supp. 28 Pages: S28-1 and
S28-2.
Section 5 Supp. 50 Pages: S50-iv and
S50-v, S50-23 and
S50-24, S50-24A and
S50-24B, S50-63.

Page A-7
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Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
4 (cont.) Section 5 Supp. 51 Pages: S51-17,
S51-47.
Section 5 Supp. 52 Pages: S52-i,
S52-1.
Section 5 Supp. 66 Page: S66-3.
Section 5 Supp. 68 Page: S68-14.
Section 5 Supp. 69 Pages: S69-49,
S69-51, S69-53.
Section 7 Pages: 7-iii, 7-vi, 7-129, Manufacturer’s Data
7-139 and 7-140.
Section 8 Page: 8-1.
Section 9 Page: 9-7.
5 Section 5 Pages: 5-4 thru 5-7, 5-10 Approval No.
thru 5-16. EASA 10043778
Section 5 Supp. 37 Pages: S37-i, Dated: February 25,
S37-1. 2013
Section 5 Supp. 67 Pages: S67-i thru
S67-vi, S67-1 thru
S67-50.
Section 5 Supp. 68 Pages: S68-i thru
S68-iv, S68-1 thru
S68-28.
Section 5 Supp. 69 Pages: S69-i thru
S69-vi, S69-1 thru
S69-58.
Section 5 Supp. 70 Pages: S70-i thru
S70-vi, S70-1 thru
S70-42.
Section 5 Supp. 74 Pages: S74-2,
S74-7.
Section 5 New Issue Supplements 79,
80 and 81.
Section 5 Supp. 24 Page: S24-1. Approval No.
Section 5 New Issue Supplement 82. EASA 10043780
Dated: February 25,
2013

Page A-8
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 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
5 (cont.) Section 1 Pages: 1-34 and 1-35. Approval No.
Section 2 Pages: 2-i, 2-12 thru 2-18, EASA 10043781
2-18A and 2-18B, Dated: February 25,
2-19. 2013
Section 3 Pages: 3-viii, 3-68, 3-72,
3-178.
Section 5 Supp. 9 Pages: S9-9 and
S9-10, S9-12, S9-14,
S9-17, S9-20 and
S9-21.
Section 5 Supp. 11 Page: S11-23.
Section 5 Supp. 17 Page: S17-5.
Section 5 Supp. 19 Page: S19-3.
Section 5 Supp. 20 Page: S20-3.
Section 5 Supp. 34 Pages: S34-i,
S34-iii and S34-iv,
S34-1.
Section 5 Supp. 40 Pages: S40-i,
S40-iii and S40-iv,
S40-1 and S40-2.
Section 5 Supp. 71 Pages: S71-31,
S71-36, S7-41.
Section 7 Pages: 7-iii thru 7-vi, 7-114 Manufacturer’s Data
thru 7-116.
Section 8 Page: 8-1.
Section 9 Page: 9-7.
6 Section 5 New Issue Supplement 76. Approval No.
Section 5 Pages: 5-4, 5-7, 5-9 thru EASA 10044323
5-18. Dated: April 5, 2013
Section 5 Supp. 71 Page: S71-7.
Section 1 Page: 1-35. Approval No.
EASA 10044327
Dated: April 5, 2013
Section 4 Pages: 4-i thru 4-iii, 4-62, Approval No.
4-65, 4-67 thru 4-70. EASA 10044324
Section 5 Supp. 5 Pages: S5-iv thru Dated: April 5, 2013
S5-viii, S5-109 thru
S5-114.
Section 5 Supp. 50 Pages: S50-63.
Section 5 Supp. 51 Pages: S51-47.

Page A-9
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Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
6 (cont.) Section 5 Supp. 69 Pages: S69-53,
S69-55.
Section 5 Supp. 43 Pages: S43-i, Approval No.
S43-iii, S43-1 and EASA 10044322
S43-2, S43-5 thru Dated: April 5, 2013
S43-10.
Section 3 Page: 3-128. Approval No.
Section 5 Supp. 38 Pages: S38-iii and EASA 10044329
S38-iv, S38-3, S38-8. Dated: April 5, 2013
Section 5 Supp. 50 Pages: S50-5.
Section 5 Supp. 67 Pages: S67-9 and
S67-10.
Section 5 Supp. 69 Pages: S69-8 thru
S69-10, S69-22 and
S69-23.
Section 5 Supp. 70 Pages: S70-7 thru
S70-9.
Section 7 Page: 7-109. Manufacturer’s Data
7 Section 2 Page: 2-12. Approval No.
Section 5 Supp. 67 Page: S67-1. EASA 10046273
Section 5 Supp. 69 Page: S69-1. Dated: September 05,
Section 5 Supp. 70 Page: S70-1. 2013
Section 5 Supp. 79 Pages: S79-1,
S79-7, S79-9.
Section 5 Supp. 80 Pages: S80-5,
S80-9.
Section 5 Supp. 81 Pages: S81-1,
S81-4.
Section 5 Supp. 11 Pages: S11-iii, Approval No.
S11-15. EASA 10046275
Section 5 Supp. 41 Pages: S41-iii and Dated: September 05,
S41-iv, S41-15. 2013
Section 5 Supp. 49 Pages: S49-17.
Section 5 Supp. 46 Page: S46-5.
Section 1 Page: 1-31. Approval No.
Section 5 Pages: 5-5 thru 5-8, 5-10 EASA 10046279
thru 5-13, 5-15. Dated: September 05,
Section 5 Supp. 25 Page: S25-2. 2013

Page A-10
Rev. 16
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Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
7 (cont.) Section 5 Supp. 43 Pages: S43-iii,
S43-1 thru S43-12.
Section 5 Supp. 45 Pages: S45-i,
S45-iii and S45-iv,
S45-1 thru S45-10.
Section 5 Supp. 74 Page: S74-1.

Introduction Pages: I-3 thru I-11. Approval No.

Section 3 Pages: 3-78, 3-120. EASA 10046282
Section 5 Supp. 9 Pages: S9-iv, S9-2. Dated: September 05,
Section 5 Supp. 10 Page: S10-4. 2013
Section 5 Supp. 11 Pages: S11-iii,
S11-20, S11-23 thru
S11-28.
Section 5 Supp. 13 Page: S13-20.
Section 5 Supp. 35 Pages: S35-iii,
S35-3 and S35-4.
Section 5 Supp. 41 Pages: S41-20 thru
S41-32.
Section 5 Supp. 49 Pages: S49-22,
S49-24 thru S49-30.
Section 5 Supp. 71 Page: S71-35.
Section 5 Supp. 80 Pages: S80-1 thru
S80-3, S80-6, S80-10,
S80-13, S80-15.
Section 5 Supp. 82 Pages: S82-iii and
S82-iv, S82-1 thru
S82-4, S82-4A and
S82-4B, S82-5 thru
S82-7, S82-10 thru
S82-12, S82-17 thru
S82-19, S82-22,
S82-25, S82-27,
S82-29 and S82-30.
Section 5 Supp. 41 Pages: S41-45 and Manufacturer’s Data
S41-46.
Section 7 Pages: 7-iii thru 7-vi, 7-141
thru 7-146.

Page A-11
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Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
8 Section 5 Pages: 5-11, 5-13, 5-16. Approval No.
Section 5 Supp. 41 Pages: S41-14 and EASA 10046811
S41-15. Dated: October 25,
Section 5 Supp. 49 Pages: S49-16, 2013 &
S49-20B.
Approval No.
EASA 10046812
Dated: October 25,
2013
9 Section 3 Pages: 3-ii, 3-40 and 3-41. Approval No.
EASA 10048407
Dated: March 07, 2014
Section 5 New Issue Supplement 84 Approval No.
EASA 10048408
Dated: March 07, 2014
Section 5 New Issue Supplement 85 Approval No.
EASA 10048410
Dated: March 07, 2014
Section 1 Page: 1-31. Approval No.
QRH Revision required EASA 10048409
Section 2 Pages: 2-49 and 2-50. Dated: March 07, 2014
Section 3 Page: 3-75.
QRH Revision required
Section 4 Page: 4-70.
Section 5 Pages: 5-7 thru 5-17.
Section 5 Supp. 1 Pages: S1-7 and
S1-8.
Section 5 Supp. 49 Page: S49-20B.
Section 5 Supp. 50 Page: S50-145.
Section 5 Supp. 71 Pages: S71-iv thru
S71-vi, S71-40,
S71-40A and
S71-40B, S71-41.
QRH Revision required
Section 5 Supp. 74 Pages: S74-i,
S74-1.

Page A-12
Rev. 16
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Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
10 Section 3 Pages: 3-25, 3-28, 3-67, Approval No.
3-76, 3-80, 3-89, EASA 10049631
3-169. Dated: June 26, 2014
Section 5 Pages: 5-7 thru 5-18.
Section 5 Supp. 2 Page: S2-19.
Section 5 Supp. 23 Page: S23-6.
QRH Revision required
Section 5 Supp. 81 Page: S81-8.
Section 2 Pages: 2-11, 2-19. Approval No.
QRH Revision required EASA 10049632
Section 5 Supp. 34 Pages: S34-iv, Dated: June 26, 2014
S34-28, S34-36.
Section 5 Supp. 40 Pages: S40-iv,
S40-26, S40-33.
Section 5 Supp. 67 Pages: S67-iv,
S67-36.
Section 5 Supp. 69 Pages: S69-iv,
S69-39.
Section 5 Supp. 70 Pages: S70-iv,
S70-30.
QRH Revision required
Section 5 Supp. 84 Page: S84-6.
Section 5 Supp. 85 Pages: S85-i,
S85-5, S85-7.
Section 2 Page: 2-12. Approval No.
Section 5 Supp. 67 Page: S67-1. EASA 10049633
Section 5 Supp. 68 Page: S68-1. Dated: June 26, 2014
Section 5 Supp. 69 Page: S69-1.
Section 5 Supp. 70 Page: S70-1.
Section 5 Supp. 74 Pages: S74-2,
S74-7.
Section 5 Supp. 79 Pages: S79-i,
S79-1, S79-7, S79-9.
Section 5 Supp. 80 Pages: S80-5,
S80-9.
Section 5 Supp. 81 Pages: S81-1,
S81-4.
Section 5 Supp. 11 Pages: S11-11 thru Approval No.
S11-13. EASA 10049634
Dated: June 26, 2014

Page A-13
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Revisions Document N°
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REVISION
SUBJECT APPROVAL
No.
10 (cont.) Section 5 Supp. 12 Pages: S12-9,
S12-13 and S12-14,
S12-A9 thru S12-A11,
S12-B6 thru S12-B8,
S12-C8 thru
S12-C10, S12-D8 thru
S12-D10, S12-D10A,
S12-D10D thru
S12-D10F, S12-D11,
S12-E9 thru S12-E12,
S12-E12A thru
S12-E12F, S12-F7
thru S12-F9, S12-G8,
S12-G8A and
S12-G8B, S12-H2,
S12-H6, S12-H10 thru
S12-H12, S12-H12A
and S12-H12B,
S12-I9 and S12-I10,
S12-I17 and S12-I18,
S12-J5 and S12-J6.
Section 5 Supp. 13 Pages: S13-8,
S13-26, S13-37.
Section 5 Supp. 30 Pages: S30-iii,
S30-1, S30-4A and
S30-4B.
Section 5 Supp. 41 Pages: S41-11 thru
S41-15.
Section 5 Supp. 49 Pages: S49-iii,
S49-13 theu S49-17.
Section 5 Supp. 50 Pages: S50-2,
S50-5, S50-21,
S50-65.
Section 5 Supp. 51 Pages: S51-2,
S51-4, S51-6, S51-6A,
S51-17.
Section 5 New Issue Supplement 87.
Section 9 Pages: 9-i, 9-iii thru 9-vi, 9-1 Manufacturer’s Data
thru 9-4, 9-63 thru
9-136.

Page A-14
Rev. 16
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
11 Section 2 Pages: 2-7 thru 2-10. Approval No.
Section 3 Page: 3-97. EASA 10051365
Section 5 Pages: 5-7 and 5-8, 5-10 thru Dated: November 26,
5-13, 5-15 thru 5-17. 2014
Section 5 Supp. 38 Pages: S38-iii and
S38-iv, S38-3,
S38-8.
Section 5 Supp. 71 Pages: S71-iv,
S71-20, S71-31 and
S71-32, S71-32A and
S71-32B.
Section 5 Supp. 72 Pages: S72-i thru
S72-iv, S72-1 thru
S72-10.
Section 5 Supp. 76 Pages: S76-1,
S76-15.
Section 7 Pages: 7-iii, 7-vi, 7-146 thru
7-148.
Section 9 Pages: 9-i thru 9-v, 9-136
thru 9-138.
Section 1 Pages: 1-30 and 1-31. Approval No.
Section 4 Page: 4-37. EASA 10051367
Section 5 Supp. 50 Page: S50-65. Dated: November 26,
Section 5 Supp. 9 Page: S9-11. 2014
Section 5 Supp. 49 Page: S49-10.
Section 5 Supp. 67 Page: S67-9.
Section 5 Supp. 69 Page: S69-7.
12 Section 5 Pages: 5-8 thru 5-18. Approval No.
Section 5 Supp. 11 Pages: S11-iii, EASA 10052093
S11-11 thru S11-15. Dated: January 30,
Section 5 Supp. 12 Pages: S12-A3 thru 2015
S12-A5, S12-A19 and
S12-A20, S12-A32A
and S12-A32B,
S12-A55 thru
S12-A60, S12-B2 and
S12-B3, S12-B17 and
S12-B18, S12-B22,
S12-B28A and
S12-B28B, S12-C3,

Page A-15
Rev. 16
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
12 (cont.) S12-C5, S12-C21 and
S12-C22, S12-C28,
S12-C22, S12-C28,
S12-D3 and S12-D4,
S12-D4A and
S12-D4B, S12-D5,
S12-D27 and
S12-D28, S12-D34A
and S12-D34B,
S12-D57 thru
S12-D62, S12-E3,
S12-E6, S12-E20 and
S12-E21, S12-E24A
and S12-E24B,
S12-E30A and
S12-E30B, S12-F2
thru S12-F5, S12-F16
and S12-F17,
S12-F20A and
S12-F20B, S12-F26A,
and S12-F26B,
S12-F32A and
S12-F32B, S12-F51
thru S12-F56,
S12-G5, S12-G20 and
S12-G21, S12-H3,
S12-H21 and
S12-H22, S12-I3 and
S12-I4, S12-I6,
S12-I35 and S12-I36,
S12-I45 and S12-I46,
S12-J3, S12-J12 thru
S12-J14, S12-K2,
S12-K4, S12-K30 thru
S12-K36, S12-L2,
S12-L7, S12-L11,
S12-L15, S12-L21 and
S12-L22.

Page A-16
Rev. 16
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
12 (cont.) Section 5 Supp. 13 Pages: S13-iv thru
S13-viii, S13-8 thru
S13-10, S13-36A thru
S13-36D, S13-64 thru
S13-74.
Section 5 Supp. 41 Pages: S41-iii and
S41-iv, S41-11 thru
S41-16, S41-16A and
S41-16B, S41-17 and
S41-18.
Section 5 Supp. 49 Pages: S49-13 thru
S49-17.
Section 5 Supp. 50 Pages: S50-iii thru
S50-xii, S50-2, S50-
2A and S50-2B, S50-5
and S50-6, S50-18,
S50-21, S50-32A thru
S50-32D, S50-58A
thru S50-58J,
S50-80A thru
S50-80F, S50-81 thru
S50-84, S50-84A,
S50-108A thru
S50-108F, S50-145
thru S50-158.
Section 5 Supp. 51 Pages: S51-2 and
S51-3.
Section 5 New Issue Supplement 86.
Section 5 New Issue Supplement 88. Approval No.
EASA 10052091
Dated: January 30,
2015
Section 2 Page: 2-9. Manufacturer’s Data

13 Section 5 Pages: 5-12 and 5-13, 5-15. Approval No.

Section 5 New Issue Supplement 90. EASA 10052459
Section 5 Supp. 50 Pages: S50-iii thru Dated: March 03, 2015
S50-xi, S50-1 and
S50-2, S50-2A, S50-4
thru S50-6, S50-11,

Page A-17
Rev. 16
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
13 (cont.) S50-13, S50-21,
S50-85, S50-89,
S50-93, S50-108A.
Section 5 Supp. 86 Pages: S86-v and Approval No.
S86-vi, S86-31, EASA 10052462
S86-42, S86-58, Dated: March 03, 2015
S86-66.
Section 5 Supp. 12 Page: S12-C13.
Section 5 Supp. 50 Page: S50-2A.
Section 5 Supp. 9 Pages: S9-iii, S9-1, Approval No.
S9-5, S9-6B, S9-13, EASA 10052460
S9-16, S9-19. Dated: March 03, 2015
Section 5 Pages: 5-8, 5-18. Approval No.
Section 5 Supp. 45 Pages: S45-iii, EASA 10052461
S45-1, S45-7. Dated: March 03, 2015
Section 5 Supp. 81 Page: S81-30. Manufacturer’s Data
14 Section 5 Pages: 5-2, 5-8 thru 5-18. Approval No.
Section 3 Page: 3-71. EASA 10053555
Section 5 Supp. 50 Page: S50-4. Dated: June 05, 2015
Section 5 New Issue Supplement 89. Approval No.
EASA 10053551
Dated: June 05, 2015
Section 5 New Issue Supplement 92. Approval No.
EASA 10053552
Dated: June 05, 2015
Section 5 Supp. 10 Pages: S10-i, Approval No.
S10-4. EASA 10053557
Dated: June 05, 2015
15 Section 2 Pages: 2-40, 2-40A and Approval No.
2-40B, 2-41 and 2-42. EASA 10054259
Section 3 Page: 3-40. Dated: July 30, 2015
Section 5 Pages: 5-8, 5-17.
Section 5 Supp. 14 Pages: S14-iii,
S14-3.
Section 5 Supp. 16 Pages: S16-iii,
S16-4.

Page A-18
Rev. 16
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
15 (cont.) Section 5 Supp. 21 Pages: S21-iii,
S21-4.
Section 5 Supp. 27 Pages: S27-iii,
S27-4.
Section 5 Supp. 28 Pages: S28-iii,
S28-6.
Section 5 Supp. 36 Page: S36-8.
Section 5 Supp. 38 Page: S38-6.
Section 5 Supp. 42 Page: S42-11.
Section 5 Supp. 43 Page: S43-11.
Section 5 Supp. 46 Page: S46-6.
Section 5 Supp. 50 Pages: S50-85,
S50-89, S50-93,
S50-103 thru
S50-108, S50-108A,
S50-133 and S50-134.
Section 5 Supp. 52 Page: S52-8.
Section 5 Supp. 58 Page: S58-4.
Section 5 Supp. 64 Page: S64-8.
Section 5 Supp. 72 Page: S72-9.
Section 5 Supp. 73 Page: S73-7.
Section 5 Supp. 78 Pages: S78-iii,
S78-7 thru S78-10.
Section 5 Supp. 84 Pages: S84-iii,
S84-7 thru S84-10.
Section 5 Supp. 90 Pages: S90-123,
S90-131, S90-135,
S90-145, S90-147,
S90-149, S90-153.
Section 5 Supp. 92 Page: S92-11.
Section 5 Supp. 13 Pages: S13-vii, Approval No.
S13-64 thru S13-76. EASA 10054260
Section 5 Supp. 86 Pages: S86-5, Dated: July 30, 2015
S86-15, S86-33 thru
S86-68.
Section 5 Supp. 81 Pages: S81-i thru Approval No.
S81-iv, S81-1 thru EASA 10054261
S81-30. Dated: July 30, 2015

Page A-19
Rev. 16
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
15 (cont.) Section 5 Supp. 17 Pages: S17-i, Approval No.
S17-iii, S17-1 thru EASA 10054262
S17-3, S17-5 and Dated: July 30, 2015
S17-6.
Section 5 Supp. 89 Page: S89-i.
Section 5 New Issue Supplement 91.
16 Section 5 Pages: 5-i, 5-6, 5-8 thru 5-20. Approval No.
Section 5 New Issue Supplement 93. EASA 10055268
Dated: October 27,
2015
Section 5 Supp. 87 Pages: S87-i, Approved with
S87-iv, S87-1 thru NDC-139G2100-002
S87-4. dated October 23,
2015 under the
authority of DOA ref.
EASA.21J.005
Section 5 Supp. 9 Page: S9-6B. Approved with
Section 5 Supp. 13 Pages: S13-vi and NDC-139G0257-011
S13-vii, S13-68 and dated October 19,
S13-69. 2015 under the
Section 5 Supp. 34 Page: S34-32.
authority of DOA ref.
Section 5 Supp. 40 Page: S40-30.
EASA.21J.005
Section 5 Supp. 56 Pages: S56-i,
S56-iv, S56-1, S56-6
and S56-7, S56-9,
S56-11 thru S56-14.
Section 5 Supp. 67 Page: S67-40.
Section 5 Supp. 69 Pages: S69-9,
S69-26 thru S69-28,
S69-43.
Section 5 Supp. 70 Page: S70-34.
Section 5 Supp. 76 Pages: S76-4,
S76-6, S76-9, S76-50.
Section 5 Supp. 86 Pages: S86-11,
S86-18.
Section 7 Pages: 7-25, 7-110.

Page A-20
Rev. 16
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
17 Section 5 Supp. 43 Pages: S43-i, Approval No.
S43-iii, S43-1 and EASA 10056113
S43-2, S43-7 and Dated: December 18,
S43-8. 2015
Section 5 Supp. 28 Pages: S28-i thru Approved with
S28-iv, S28-1 thru NDC-139G9310-003
S28-6. dated December 21,
2015 under the
authority of DOA ref.
EASA.21J.005
Section 5 Pages: 5-3 and 5-4, 5-9, Approved with
5-13, 5-15, 5-19. NDC-139G6700-002
Section 5 New Issue Supplement 94. dated December 21,
2015 under the
authority of DOA ref.
EASA.21J.005
Section 5 Supp. 42 Pages: S42-i thru Approved with
S42-iv, S42-1 thru NDC-139G3441-003
S42-12. dated December 21,
2015 under the
authority of DOA ref.
EASA.21J.005
Section 2 Pages: 2-42 and 2-43. Approved with
Section 5 Supp. 71 Pages: S71-iii, NDC-139G0257-013
S71-20. dated December 21,
Section 5 Supp. 86 Pages: S86-iv thru 2015 under the
S86-vi, S86-15,
authority of DOA ref.
S86-16A and
EASA.21J.005
S86-16B.
Section 5 Supp. 91 Page: S91-3.
Section 7 Pages: 7-112 and 7-113.
18 Section 5 Supp. 43 Page: S43-7. Approval No.
EASA 10058289
Dated: May 31, 2016

Page A-21
Rev. 18
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
18 (cont.) Section 1 Page: 1-29. Approved with
Section 2 Pages: 2-i and 2-ii, 2-4 and NDC-139G0257-016
2-5, 2-7, 2-9, 2-27 and dated May 27, 2016
2-28. under the authority of
Section 1 Pages: 1-33, 1-66.
DOA ref.
Section 5 Supp. 12 Page: S12-H23.
EASA.21J.005
Section 5 Supp. 67 Page: S67-44.
Section 5 Supp. 69 Pages: S69-7,
S69-26, S69-47.
Section 5 Supp. 70 Page: S70-37.
Section 7 Pages: 7-iii, 7-91, 7-92A and
7-92B.
Section 5 Supp. 19 Pages: S19-i, Approved with
S19-iii, S19-1 and NDC-139G3271-001
S19-2. dated May 27, 2016
Section 5 Supp. 20 Pages: S20-i, under the authority of
S20-1.
DOA ref.
Section 5 Pages: 5-2 thru 5-9.
EASA.21J.005
19 Section 1 Page: 1-34. Approval No.
Section 5 Pages: 5-12, 5-15. EASA 10059049
Section 5 Supp. 50 Pages: S50-iii, Dated: August 5, 2016
S50-5 and S50-6,
S50-6A and S50-6B.
Section 5 Pages: 5-9, 5-19. Approval No.
Section 5 Supp. 9 Page: S9-21. EASA 10059083
Section 5 New Issue Supplement 95. Dated: August 31,
2016
Section 1 Page: 1-29. Approved with
Section 2 Pages: 2-34 and 2-35. NDC-139G0257-017
Section 3 Page: 3-2. dated July 29, 2016
Section 5 Page: 5-8. under the authority of
Section 5 Supp. 87 Page: S87-i.
DOA ref.
Section 7 Page: 7-109.
EASA.21J.005
Section 8 Page: 8-13.
20 Section 5 Supp. 77 Pages: S77-6, Approval No.
S77-8. EASA 10060192
Dated: November 24,
2016

Page A-22
Rev. 20
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
20 (cont.) Section 2 Pages: 2-6, 2-9 and 2-10, Approved with
2-33. NDC-139G0257-019
Section 5 Supp. 93 Pages: S93-1, dated November 8,
S93-6. 2016 under the
Section 9 Pages: 9-v, 9-125 thru 9-127.
authority of DOA ref.
EASA.21J.005
Section 5 Supp. 89 Pages: S89-i, Approved with
S89-iii, S89-1 thru NDC-139G1830-004
S89-6. dated November 10,
2016 under the
authority of DOA ref.
EASA.21J.005
21 Section 1 Page: 1-8. Approval No.
EASA 10061566
Dated: April 12, 2017
Section 5 New Issue Supplement 96. Approval No.
Section 5 Pages: 5-9, 5-13 thru 5-19. EASA 10061568
Dated: April 12, 2017
Section 5 Supp. 87 Pages: S87-i, Approval No.
S87-1. EASA 10061562
Dated: April 12, 2017
Section 5 Supp. 90 Page: S90-3. Approval No.
EASA 10061564
Dated: April 12, 2017
Section 5 New Issue Supplement 97. Approval No.
EASA 10061563
Dated: April 12, 2017
Section 1 Pages: 1-1 and 1-2. Approved with
Section 5 Supp. 68 Page: S68-25. NDC-139G0257-020
Section 5 Pages: 5-2, 5-8. dated April 5, 2017
under the authority of
DOA ref.
EASA.21J.005

Page A-23
Rev. 21
Record of AW139 - RFM - 4D
Revisions Document N°
139G0290X002

REVISION
SUBJECT APPROVAL
No.
22 Section 3 Pages: 3-ii, 3-39, 3-41 and Approval No.
3-42, 3-42A and EASA 10063465
3-42B, 3-97. Dated: October 17,
2017
Section 2 Page: 2-12. Approval No.
Section 5 Page: 5-8. EASA 10063521
Section 5 Supp. 37 Pages: S37-iii, Dated: October 19,
S37-1 thru S37-4. 2017
Section 5 Supp. 67 Pages: S67-1,
S67-9 and S67-10.
Section 5 Supp. 68 Pages: S68-iii,
S68-1, S68-20A and
S68-20B.
Section 5 Supp. 69 Pages: S69-1,
S69-8 and S69-9,
S69-26.
Section 5 Supp. 70 Pages: S70-1,
S70-7 and S70-8.
Section 5 Supp. 74 Pages: S74-2,
S74-7.
Section 5 Supp. 79 Pages: S79-i,
S79-iii, S79-1 and
S79-2, S79-4, S79-7
thru S79-14.
Section 5 Supp. 80 Pages: S80-iii and
S80-iv, S80-1 thru
S80-13, S80-15,
S80-17 thru S80-21.
Section 5 Supp. 81 Pages: S81-1,
S81-4.
Section 5 Supp. 60 Pages: S60-iii, Approval No.
S60-5, S60-11. EASA 10063530
Dated: October 19,
2017
Section 5 Supp. 86 Pages: S86-iii, Approval No.
S86-4, S86-12. EASA 10063535
Dated: October 19,
2017

Page A-24
Rev. 22
 AW139 - RFM - 4D Record of
Document N° Revisions
139G0290X002

REVISION
SUBJECT APPROVAL
No.
22 (cont.) Section 5 Supp. 58 Pages: S58-i thru Approved with
S58-iv, S58-1 thru NDC-139G9750-004
S58-4. dated October 13,
2017 under the
authority of DOA ref.
EASA.21J.005
Section 5 Supp. 73 Pages: S73-i thru Approved with
S73-iv, S73-1 thru NDC-139G3441-004
S73-8. dated October 19,
2017 under the
authority of DOA ref.
EASA.21J.005
Section 1 Pages: 1-8, 1-27, 1-33. Approved with
Section 3 Pages: 3-14, 3-26, 3-32, NDC-139G0257-021
3-54. dated October 13,
Section 5 Pages: 5-3, 5-6 and 5-7, 5-9, 2017 under the
5-13, 5-15 thru 5-17.
authority of DOA ref.
Section 5 Supp. 11 Pages: S11-iii and
EASA.21J.005
S11-iv, S11-19 thru
S11-28.
Section 5 Supp. 26 Pages: S26-i,
S26-1.
Section 5 Supp. 41 Pages: S41-iii and
S41-iv, S41-2 thru
S41-3, S41-19 thru
S41-42.
Section 5 Supp. 49 Pages: S49-iii and
S49-iv, S49-1 thru
S49-3, S49-22 thru
S49-38.
Section 5 Supp. 84 Page: S84-1.
Section 5 Supp. 93 Page: S93-1.
Section 7 Pages: 7-iv thru 7-vi, 7-58,
7-92A and 7-92B.

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139G0290X002 Pages

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NOTE: A black vertical line in outer margin of the page indicates
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A-24 and A-25 22 1-30 and 1-31 11
A-26 blank 22 1-32 4
B-1 thru B-30 22 1-33 22
I-1 and I-2 0 1-34 19
I-3 thru I-11 7 1-35 6
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2-26 2 3-33 and 3-34 0
2-27 and 2-28 18 3-35 and 3-36 1
2-29 and 2-30 0 3-37 and 3-38 0
2-31 2 3-39 22
2-32 3 3-40 15
2-33 20 3-41 and 3-42 22
2-34 and 2-35 19 3-42A 22
2-36 3 3-42B blank 22
2-37 thru 2-39 0 3-43 thru 3-48 0
2-40 15 3-49 2
2-40A and 2-40B 15 3-50 and 3-51 0
2-41 15 3-52 4
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3-90 thru 3-94 0 3-165 and 3-166 0
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3-98 3 3-169 10
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3-109 0 4-i thru 4-iii 6
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INTRODUCTION

GENERAL
It is the responsibility of the flight crew to be familiar with the contents
of this manual.

REVISIONS (RE-ISSUES)
This manual is subject to revisions (re-issues) which will be automati-
cally distributed to all holders of the manual. It is the responsibility of
the operator to assure that the revisions (re-issues) are incorporated
into the manual upon receipt.
At the beginning of the manual there is the ”Record of Revision” table
that shows all pages of the manual which have been revised as well
as number, subject and approval reference of each revision.

REVISION SYMBOL
Revised text is indicated by a black vertical line on the outer margin of
the page, adjacent to the affected text and the revision number is
printed in the lower inner margin. The revision symbol identifies the
addition of new information, a change of procedure, the correction of
an error, or a rewording of the previous information.

TEMPORARY REVISIONS
Temporary Revisions are issued when immediate data is to be
included in the manual. The Temporary Revision data can add to or
cancel the initial data in the manual. They are numbered progressively
for each section of the manual and are printed on blue paper. Tempo-
rary Revision pages are not written in the ”Record of Effective Pages”.
A complete list of active and inactive Temporary Revisions is written
in the ”Record of Temporary Revisions” page.

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TERMINOLOGY

WARNINGS, CAUTIONS AND NOTES

Warnings, Cautions and Notes are used throughout this manual to
emphasize important and critical instructions and are used as follows:

WARNING
An operating procedure, practice, etc., which, if not cor-
rectly followed, could result in personal injury or loss of life.

CAUTION

An operating procedure, practice, etc., which, if not strictly

observed, could result in damage to, or destruction of,
equipment.

Note
An operating procedure, condition, etc., which is essential
to highlight.

USE OF PROCEDURAL WORDS

The concept of procedural word usage and intended meaning which
has been adhered to in preparing this RFM is as follows:
”Shall” or ”Must” have been used only when application of a proce-
dure is mandatory.
”Should” has been used only when application of a procedure is re-
commended.
”May” has been used only when application of a procedure is optional.
”Will” has been used only to indicate futurity, never to indicate a man-
datory procedure.
”Condition” has been used to determine if the item under examination
presents external damage which could jeopardize its safe operation.

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”Secure” has been used to determine if the item under examination is

correctly locked, referring to doors and disconnectable items, or cor-
rectly positioned and installed.

DEFINITIONS
The level of alertness required by the pilots is a function of the flight
regime.
The following definitions are used in the manual:
Fly Attentive - Pilot to maintain close control of the flight path using
hands on when required.
Fly Manually - Pilot to control directly the flight path using hands on.
QFE - Atmospheric pressure at aerodrome elevation (or runway
threshold).
QNH - Altimeter subscale setting to obtain elevation when on the
ground.

ABBREVIATION
The use of capital letters in the text, apart from normal grammatical
usage, indicates the actual wording of marking of indicators, controls
or control positions on the helicopter.
Abbreviations and acronyms used throughout this RFM are defined as
follows:

— a.c./AC : Alternating Current

— ACLCD : Active Liquid Crystal Displays

— ADC : Air Data Computer

— ADF : Automatic Direction Finder

— ADLP : Data Link Processor

— ADM : Air Data Module

— ADS : Air Data System

— AEO : All Engines Operative

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— A/F : Airframe

— AFCS : Automatic Flight Control System

— AG : Accessory Gearbox

— AGL : Above Ground Level

— AHRS : Attitude Heading Reference System

— ALS : Ambient Light Sensor

— AMSL : Above Mean Sea Level

— AP : AutoPilot

— ATT : Attitude hold

— ATC : Air Traffic Control

— AWG : Aural Warning Generator

— BFO : Beat Frequency Oscillator

— BL : Buttock Line

— BOD : Bottom Of Descent

— BOW : Basic Operating Weight

— CAS : Calibrated Air Speed

— CAT : Category

— C/B : Circuit Breaker

— CCD : Cursor Control Devices

— CCW : Counter Clock Wise

— CCP : Cockpit Control Panel

— CG : Center of Gravity

— CLTV : Collective

— CPI : Crash Position Indicator

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— CS : Centistoke

— CVR : Cockpit Voice Recorder

— CW : Clock Wise

— DAU : Data Acquisition Unit

— d.c./DC : Direct Current

— DEOS : Digital Engine Operating System

— DCU : Data Collection Unit

— DFDAU : Digital Flight Data Acquisition Unit

— DGPS : Differential Global Positioning System

— DH : Decision Height
— DICP : Display Instrument Control Panel
— DME : Distance Measuring Equipment
— EAPS : Engine Air Particle Separator
— EASA : European Aviation Safety Agency
— ENAC : Ente Nazionale Aviazione Civile
— ECL : Engine Control Lever
— ECS : Environmental Control System
— ECU : Engine Control Unit
— EDU : Electronic Display Unit
— EEC : Electronic Engine Control
— EFIS : Electronic Flight Instrument System
— EGPWS : Enhanced Ground Proximity Warning System
— ELT : Emergency Locator Transmitter
— EMM : Engine Maintenance Manual
— EOP : Engine Oil Pressure

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— EPU : Estimated Position Uncertainty

— ESIS : Electronic Standby Instrument System
— EXT : External
— FAA : Federal Aviation Administration
— FAF : Final Approach Fix
— FCC : Flight Control Circuit
— FCU : Fuel Computer Unit
— FD : Flight Director
— FDR : Flight Data Recorder
— FMCW : Frequency-Modulated Continuous Wave
— FMM : Fuel Management Module
— FMS : Flight Management System
— FOD : Foreign Object Damage
— FOM : Figure of Merit
— FTR : Force Trim Release
— FWD : Forward
— GA : Go-Around

— GC : Guidance Controller

— GI : Ground Idle

— GPS : Global Positioning System

— GS : GroundSpeed

— G/S : GroundSpeed

— GS : Glide Slope

— GW : Gross Weight

— HCB : Heating Control Box

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— Hd : Density altitude

— HF : High Frequency

— HIGE : Hover In Ground Effect

— HOGE : Hover Out of Ground Effect

— Hp : Pressure altitude

— HPS : Hydraulic Power Supply

— HSI : Horizontal Situation Indicator

— H-V : Height Velocity

— IAS : Indicated Air Speed

— ICS : Inter Communication System

— IDS : Integrated Display System

— IGB : Intermediate Gear Box

— IFR : Instrumental Flight Rules

— IGE : In Ground Effect

— IGS : Instrument Guidance System

— ILS : Instrument Landing System

— IR : Infrared

— ISA : International Standard Atmosphere

— ITT : Inter Turbine Temperature

— JAR : Joint Aviation Requirements

— KCAS : Knots - Calibrated Air Speed

— KIAS : Knots - Indicated Air Speed

— LAT : Lateral

— LCF : Low Cycle Fatigue

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— LDA : Landing Directional Aid

— LG : Landing Gear

— LGCP : Landing Gear Control Panel

— LH : Left Hand

— LOC : Localizer

— LONG : Longitudinal

— LSS : Lightning Sensor System

— MAN : Manual Override System

— MAU : Modular Avionic Unit

— MCDU : Multifunction Control Display Unit

— MCL : Master Caution Light

— MCP : Maximum Continuous Power

— MDA : Minimum Descent Altitude

— MEC : MEChanical

— MFD : Multifunction Flight Display

— MFR : Manufacturer

— MGB : Main Gear Box

— MLG : Main Landing Gear

— MLS : Microwave Landing System

— MPOG : Minimum Pitch On Ground

— M/R : Main Rotor

— MRC : Modular Radio Cabinet

— MWL : Master Warning Light

— NF : Power turbine speed

Page I-8 E.A.S.A. Approved

Rev. 7
 AW139 - RFM - 4D Introduction
Document N°
139G0290X002

— NG : Gas generator speed

— NLG : Nose Landing Gear

— NR : Rotor speed

— NVG : Night Vision Goggle

— OAT : Outside Air Temperature

— OEI : One Engine Inoperative

— OGE : Out Of Ground Effect

— OR : Operational Range

— PAX : Passengers

— PCM : Power Control Module

— PCMCIA : Personal Computer Memory Card Interface Association

— PEP : Peak Envelope Power

— PFD : Primary Flight Display

— PI : Power Index

— PLA : Power Lever Angle (throttle)

— PMS : Power Management Switch

— PSU : Passenger Station Unit

— PWR : Power

— RAIM : Receiver Autonomous Integrity Monitor

— RCP : Reconfiguration Control Panel

— RFM : Rotorcraft Flight Manual

— RH : Right Hand

— RICP : Remote Instrument Control Panel

— RNP : Required Navigation Performance

E.A.S.A. Approved Page I-9

Rev. 7
Introduction AW139 - RFM - 4D
Document N°
139G0290X002

— ROC : Rate Of Climb

— RPM : Revolutions Per Minute

— SAS : Stability Augmentation System

— SID : Standard Instrument Departure

— SOV : Shut-Off Valve

— S/N : Serial Number

— STA : Station

— STAR : Standard Terminal Arrival Route

— TA : Terrain Awareness

— TAD : Terrain/Obstacle Awareness Display

— TAS : True Air Speed

— TAWS : Terrain Awareness and Warning System

— TBD : To Be Defined

— TCAS : Traffic Collision and Alert System

— TOC : Top Of Climb

— TOD : Top Of Descent

— TOP : Take Off Power

— TQ/TRQ : Engine torque

— TRSOV : Tail Rotor Shut Off Valve

— TVC : Temperature Control Valve

— VDR : VHF - Data Radio

— VFR : Visual Flight Rules

— VIDL : VOR/ILS/Data Link

— VMS : Vehicle Monitoring System

Page I-10 E.A.S.A. Approved

Rev. 7
 AW139 - RFM - 4D Introduction
Document N°
139G0290X002

— VLO : Maximum landing gear operating speed

— VLE : Maximum landing gear extended speed

— Vmini : Minimum airspeed for flight under IFR

— VNE : Never exceed speed

— VOR : Very high frequency Omni-directional Range

— VSI : Vertical Speed Indicator

— Vy : Speed for best rate of climb

— W.A.T. : Weight/Altitude/Temperature

— WGT : Weight

— WOW : Weight On Wheel

— WX : Weather radar

— Xfer : Transfer

— XPDR : Trasponder

E.A.S.A. Approved Page I-11

Rev. 7
Introduction AW139 - RFM - 4D
Document N°
139G0290X002

2.25m (7.40ft)

3.04m (9.98ft)

3.50m ( 11.48ft)

.27ft)
m (45
Ø13.8

4.98m (16.36ft)

8.40m (27.57ft)

3.57m ( 11.71ft)

2.7m
(8.86ft)

4.34m (14.24ft)

13.53m (44.40ft)

16.62m (54.55ft)

ICN-39-A-156000-A-00003-00030-A-03-1

Figure 1-1 Helicopter - Three Views

Page I-12 E.A.S.A. Approved

 AW139 - RFM - 4D Introduction
Document N°
139G0290X002

2.25m (7.40ft)

3.04m (9.98ft)

3.50m ( 11.48ft)

4.22m (13.85ft)

ft)
m (45.27
Ø13.8

4.98m (16.36ft)

8.40m (27.57ft)
3.57m ( 11.71ft)

2.7m
(8.86ft)

4.34m (14.24ft)

13.77m (45.18ft)

16.62m (54.55ft)

ICN-39-A-156000-A-00003-00209-A-02-1

Figure 1-2 Helicopter - Three Views (Long Nose Version)

E.A.S.A. Approved Page I-13

Introduction AW139 - RFM - 4D
Document N°
139G0290X002

1.48m 0.96m
(4.86ft) (3.15ft)
1.32m 0.61m 0.54m
(4.33ft) (2.00ft) (1.77ft)

ICN-39-A-000000-A-00003-00266-A-01-1

Figure 1-3 Cabin and Baggage Door Dimensions

Page I-14 E.A.S.A. Approved