MD Helicopters MDHI MD900 Technical specifications

Log of EASA Revisions By Date
REVISION NUMBER AND DATE EASA Approval Number
Revision 7 13 January 2003............... 2004-2053
Revision 8 8 July 2005.................... 2004-2053
TR6-001 5 June 2006..................... E02686
TR6-002 22 December 2006................ E02686
Revision 9 21 August 2007................ E02686
Revision 10 20 February 2008............. E02686
Revision 11 11 April 2008................. E02686
Reissue #1 2 December 2008............ E02686
Revision 1 21 July 2009................... E02686
Reissue #2 6 November 2009............ E02686
Reissue #2
EASA−i
CSP−902RFM207E−1
As of 28 September 2003, the EASA began approving FAA rotorcraft
flight manuals. Operators of MD900 series helicopters registered in a
European Union member state are required to place this approval page
after the cover page in their flight manual.
European Aviation Safety Agency approved
Rotorcraft Flight Manual for Model MD900
(902 Configuration with PW 207E)

CSP−902RFM207E−1ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
EASA−ii
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CSP−902RFM207E−1
Model MD900 (902 Configuration with PW 207E)
F90−001
R O T O R C R A F T F L I G H T M A N U A L
REGISTRATION NO: _________________
SERIAL NO: _________________
Cover

CSP−902RFM207E−1
Copyright E1999-2014 by MD Helicopters, Inc.
All rights reserved under the copyright laws.
F−i
Type Certificate No. H19NM
Approved By: _____________________________________
Manager, Flight Test Branch, ANM-160L
Federal Aviation Administration
Los Angeles Aircraft Certification Office
Transport Airplane Directorate
Original Approval Date: July 28, 2000
Reissue #1: December 2, 2008
Reissue #2:
THE FAA APPROVED ROTORCRAFT FLIGHT MANUAL CONSISTS OF THE FOLLOWING SECTIONS.
SECTION II −LIMITATIONS
SECTION III −EMERGENCY PROCEDURES
SECTION IV −NORMAL PROCEDURES
SECTION V −PERFORMANCE DATA
SECTION X −OPTIONAL EQUIPMENT
SECTION XI −CATEGORY−A OPERATIONS
The helicopter must be operated in compliance with the operating limitations as set forth in section II of
this manual and any additional limitations from Section X as a result of an installed optional equipment
item.
Sections III, IV, V, X and XI contain recommended procedures and data and are FAA approved.
THIS MANUAL MUST BE KEPT IN THE HELICOPTER AT ALL TIMES.
Title Page
(902 Configuration with PW 207E)
FAA APPROVED
ROTORCRAFT
FLIGHT MANUAL
for
Model MD900

CSP−902RFM207E−1ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Revision 5
F−ii
Reissue 2
LOG OF REVISIONS BY DATE
FAA / NON−FAA REVISIONS
REVISION NUMBER AND DATE
Original Issue 28 July 2000.
Revision 1 30 May 2001......
Revision 2 02 November 2001......
Revision 3 26 December 2002......
Revision 4 13 February 2003......
Revision 5 23 April 2003......
Revision 6 22 September 2003......
Revision 7 13 January 2004......
Revision 8 8 July 2005......
Revision 9 21 August 2007......
Revision 10 20 February 2008.....
Revision 11 11 April 2008.....
Reissue #1 2 December 2008.....
Revision 1 21 July 2009......
Reissue #2 06 November 2009.....
Revision 1 03 February 2012......
Revision 2 03 August 2012......
Revision 3 10 January 2013......
Revision 4 28 January 2014......
Revision 5 30 September 2014......
Approved By
Manager, Flight Test Branch, ANM-160L
Federal Aviation Administration
Los Angeles Aircraft Certification Office
Transport Airplane Directorate

CSP−902RFM207E−1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Original F−iii
Reissue 2
APPROVING AUTHORITIES
Joint Aviation Authorities (JAA)
This manual was approved by the JAA.
European Aviation Safety Authority (EASA)
The MD900 and this manual were accepted by EASA based on the JAA approval
listed above. Subsequent revisions of this manual are approved by EASA who
issues a four-digit approval number. See MDHI web page http://www.mdhelicop
ters.com, publications link for EASA approval number and instructions.
National Agency of Civil Aviation (Brazil)
This Aircraft Flight Manual is approved by the FAA on behalf of the National
Agency of Civil Aviation for Brazilian registered aircraft, in accordance with
the Regulamentos Brasileiros de Homologação Aeronáutica” (RBHA) 21, Section
21.29.
/
(Initial FAA Approval Signature/Date)
Manager, Flight Test Branch, ANM-160L
Federal Aviation Administration
Los Angeles Aircraft Certification Office
Transport Airplane Directorate

CSP−902RFM207E−1ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Original
F−iv
Reissue 2
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CSP−902RFM207E−1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
F−vRevision 4
Reissue 2
TABLE OF CONTENTS
PARAGRAPH PAGE
Cover 1......................................................................
Title Page F-i..................................................................
Log of Revisions By Date F-ii....................................................
Approving Authorities F-iii......................................................
Summary of Revisions to the Rotorcraft Flight Manual F-v........................
List of Effective Pages F-vi......................................................
Section I −General
1-1.Introduction 1-1...........................................................
1-2.Scope 1-1..................................................................
1-3.Organization 1-1...........................................................
1-4.Method of Presentation 1-3.................................................
1-5.Definition of Terms 1-3.....................................................
1-6.Abbreviations 1-4..........................................................
1-7.Multi-Purpose Utility Operations 1-7........................................
1-8.Technical Publications 1-7..................................................
1-9.Rotorcraft Certification 1-9.................................................
1-10.Pilot's Briefing 1-9........................................................
1-11.Dimensions 1-10...........................................................
1-12.Conversion Charts 1-12.....................................................
Section II −Limitations
2-1.Flight Restrictions 2-1......................................................
2-2.Environmental Operating Conditions 2-2....................................
2-3.Airspeed Limitations 2-4....................................................
2-4.Weight Limitations 2-6.....................................................
2-5.Center of Gravity (CG Envelope) 2-7.........................................
2-6.Rotor Brake Limitations 2-8................................................
2-7.Rotor Speed Limitations 2-8................................................
2-8.Transmission Limitations 2-8...............................................
2-9.Power Plant Limitations 2-9................................................
2-10.Generator Limitations 2-11.................................................

ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
CSP−902RFM207E−1
F−vi Revision 4
Reissue 2
PARAGRAPH PAGE
2−11. Starter limitations 2−11.......................................................
2-12.Fuel System Limitations 2-11...............................................
2-13.Integrated Instrumentation Display System (IIDS) 2-12.......................
2-14.Decals and Placards 2-16...................................................
Section III −Emergency and Malfunction Procedures
3-1.General 3-1................................................................
3-2.Caution and Warning Annunciators and Audio Tones 3-2......................
3-3.Engine Emergencies 3-3....................................................
3-4.Emergency Landing Procedures 3-6..........................................
3-5.EEC Malfunctions 3-8......................................................
3-6.Engine Starting - Manual 3-11...............................................
3-7.Engine/Aircraft Shutdown - Manual 3-14.....................................
3-8.Fire Emergencies 3-15.......................................................
3-9.Flight Control Malfunctions 3-19.............................................
3-10. Pitot/Static System Malfunction: Single or Dual Pitot Tube Installation 3-26....
3-11.Engine and Generator Malfunction Indications 3-27...........................
3-12.Transmission Malfunction Indications 3-31...................................
3-13.Fuel System Display Advisories 3-34........................................
3-14.Caution and Warning Advisories 3-38........................................
3-15.Other Malfunction/Advisories 3-42..........................................
3-16.Vibrations 3-44............................................................
3-17.Emergency Egress 3-45.....................................................
3-18.Emergency Equipment 3-46.................................................
Section IV −Normal Procedures
4-1.Preflight Requirements 4-1.................................................
4-2.Pilot's Daily Preflight Check 4-4.............................................
4-3.Pilot's Preflight Check 4-15..................................................
4-4.Engine Pre-Start Cockpit Check 4-22.........................................
4-5.Engine Starting - Automatic 4-24............................................
4-6.Engine Runup 4-25..........................................................
4-7.Before Takeoff 4-25..........................................................
4-8.Normal Takeoff 4-26.........................................................

CSP−902RFM207E−1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
F−viiRevision 5
Reissue 2
PARAGRAPH PAGE
4-9.Cruise 4-26.................................................................
4-10.Slow Flight/Approach 4-26..................................................
4-11.Landing 4-27..............................................................
4-12.Engine/Aircraft Shutdown - Normal 4-28....................................
4-13.Post Flight 4-30............................................................
4-14.Noise Impact Reduction Procedures 4-31.....................................
4-15.Flight With Doors Removed or Cabin Doors Open 4-32........................
4-16.One Engine Inoperative Training 4-33.......................................
4-17.Fuel System 4-34..........................................................
Section V −Performance Data
5-1.General 5-1................................................................
5-2.Noise Characteristics 5-2...................................................
5-3.Density Altitude Chart 5-3..................................................
5-4.Airspeed Calibration 5-5....................................................
5-5.Best Rate of Climb Speed 5-7................................................
5-6.Rate of Climb and Descent - OEI 5-9........................................
5-7.Rate of Climb - AEO 5-25....................................................
5-8.Hover Ceiling, AEO 5-44.....................................................
5-9.Hover Ceiling, OEI 5-54.....................................................
5-10.Height Velocity Diagram 5-57..............................................
5-11.Power Assurance Check - Automatic 5-58....................................
5-12.Power Assurance Check - Manual 5-60......................................
Section VI −Weight and Balance Data
6-1.Weight and Balance Characteristics 6-1......................................
6-2.Load Limits and Balance Criteria 6-7........................................
6-3.Equipment Removal or Installation 6-7......................................
6-4.Longitudinal Weight and Balance Determination Passenger Configuration 6-8..
6-5.Longitudinal Loading of Cargo 6-9...........................................
6-6.Permissible Lateral Loadings - Passenger Configuration 6-10...................
6-7.Lateral Loading of Cargo 6-11................................................
6-8.Internal Loading of Cargo 6-11...............................................

ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
CSP−902RFM207E−1
F−viii Revision 4
Reissue 2
PARAGRAPH PAGE
Section VII −Systems Description
7-1.Helicopter Exterior Description 7-1..........................................
7-2.Fuselage 7-3...............................................................
7-3.Tailboom and Empennage 7-5...............................................
7-4.Landing Gear 7-6..........................................................
7-5.Main Rotor System 7-8.....................................................
7-6.Flight Controls 7-10.........................................................
7-7.Hydraulic Systems 7-20.....................................................
7-8.Propulsion System 7-24......................................................
7-9.Engine Air Intake and Inlet Particle Separator (IPS) 7-28......................
7-10.Engine Power Management System 7-29.....................................
7-11.Fuel System 7-31...........................................................
7-12.Fire Extinguishing System 7-34.............................................
7-13.Electrical System 7-36......................................................
7-14.Environmental Control 7-39................................................
7-15.Integrated Instrumentation Display System (IIDS) 7-41.......................
7-16.IIDS Data Storage 7-49.....................................................
7-17.Balance Monitoring System 7-52............................................
7-18.IIDS Menu Structures 7-53.................................................
Section VIII −Handling, Servicing, and Maintenance
8-1.Hoisting, Lifting, and Jacking 8-1...........................................
8-2.Towing and Moving 8-1.....................................................
8-3.Parking and Storage 8-4....................................................
8-4.Access and Inspection Provisions 8-10.........................................
8-5.Servicing 8-21..............................................................
8-6.Aircraft Cleaning 8-33.......................................................
8-7.Cockpit Door Removal 8-34..................................................
8-8.Cabin Seats: Removal/Installation 8-36.......................................
8-9.Copilot Flight controls 8-37..................................................
8-10.Engine Charts 8-38........................................................
8-11.Special Operational Checks and Procedures 8-41..............................

CSP−902RFM207E−1
ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
F−ixRevision 4
Reissue 2
PARAGRAPH PAGE
Section IX −Additional Operations and Performance Data
9-1.Abbreviated Checklists 9-1..................................................
9-2.Fuel Flow vs Airspeed 9-4..................................................
9-3.International Civil Aviation Information 9-26.................................
Section X −Optional Equipment
10-1.General Information 10-1...................................................
10-2.Listing - Optional Equipment 10-1..........................................
10-3.Compatibility - Combined Optional Equipment 10-2..........................
10-4.Optional Equipment Performance Data 10-2.................................
10-5. Operating Instructions: Air Conditioning (P/N900P7250302-103) 10-3.........
10-6.Operating Instructions: Controllable Landing/Search Light 10-7...............
10-7.Operating Instructions: Rotorcraft Cargo Hook Kit 10-13.......................
10-8.Operating Instructions: Windscreen Wipers 10-21..............................
10-9.Operating Instructions: Supplemental Fuel System 10-25......................
10-10.Operating Instructions: Rescue Hoist 10-35..................................
10-11.Operating Instructions: Removable CoPilot Controls 10-49.....................
10-12.Operating Instructions: Airframe Fuel Filter 10-55...........................
10-13.Operating Instructions: SX-16 Night Sun with Aft Mount 10-59...............
10-14.Operating Instructions: RDR-1400C Weather Radar 10-65....................
10-15.Operating Instructions: LEO-II-A5 Observation System 10-71................
10-16.Operating Instructions: Annunciator panel 10-75.............................
10-17.Operating Instructions: Moving Map Navigation Systems 10-77................
10-18.Operating Instructions: W.E.S.T Battery Protection System 10-81..............
10-19.Operating Instructions: SX-16 Night Sun with EPMS mount and
Laser Pointer 10-83...........................................................
10-20.Operating Instructions: Smoke Detector 10-89................................
10-21.Operating Instructions: Crew Door Modification with
Quick Release Mechanism 10-93...............................................

ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
CSP−902RFM207E−1
F−x Revision 5
Reissue 2
PARAGRAPH PAGE
Section XI −Category A Operations
Part I −General 11−1............................................................
11-1.1.General 11-1.............................................................
11-1.2.Definitions - Category A Takeoff 11-1......................................
11-1.3.Definitions - Category A Landing 11-3.....................................
Part II −Limitations 11−5........................................................
11-2.1.Clear Airfield, Heliport and Elevated Helipad 11-5..........................
11-2.2.Maximum Takeoff and Landing Weight Limits 11-6.........................
11-2.3.6501 - 6700 LBS Clear Airfield Operations Only 11-9.......................
Part III −Takeoff and Landing Procedures 11−11...................................
11-3.1.Clear Airfield Takeoff Procedures 11-11.....................................
11-3.2.Heliport/Elevated Helipad Takeoff Procedures 11-15..........................
11-3.3.Landing Procedures - Clear Airfield, Heliport and Elevated Helipad 11-17.....
11-3.4.Confined Heliport/Helipad Takeoff procedures 11-20..........................
11-3.5.Takeoff Decision Point (TDP) 11-21.........................................
11-3.6.Rejected Takeoff - Confined heliport 11-22...................................
11-3.7.Continued Takeoff - Confined Heliport 11-24................................
11-3.8.Short field Takeoff Procedures 11-26........................................
11-3.9.Confined heliport and Balked landing Procedures 11-29......................
11-3.10.Equipment Malfunctions 11-33............................................
Part V −Takeoff and Landing Procedures 11−35....................................
11-5.1.Takeoff Performance 11-35.................................................
11-5.2.Takeoff Distance Required 11-35............................................
11-5.3.Continued Takeoff Flight Path 11-39........................................
11-5.4.Landing Performance - Open Airfield 11-43.................................
11-5.5.Landing Performance - Heliport/Elevated Helipad 11-43......................
Part IX −Additional Operations and performance data 11−45........................
11-9.1.Category A OEI Training 11-45.............................................

CSP−902RFM207E−1ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
Revision 5 F−xi
Reissue 2
SUMMARY OF REVISIONS
TO THE ROTORCRAFT FLIGHT MANUAL
NOTE:Revisions are listed below by number with appropriate remarks.
Section II pages marked [C]* indicate FAA approved color pages.
Black−and−white reproductions of color pages are not considered to be “FAA
Approved”.
REVISION
NUMBER REMARKS
Revision 5 Section V: Paragraph 5-1, corrected the metric conversion of the
maximum gross weight within the NOTE.
Paragraph 5-2, corrected the metric conversion in Table 5-1 and
added Table 5-2 for noise characteristics of max. gross weight of 6500
lb.
Section IX: Paragraph 9-3, added Tables 9-1 and 9-2 for ICAO Noise
Level data at max. gross weight of 6770 lb. and 6500 lb.

ROTORCRAFT FLIGHT MANUAL
MD900 (902 Configuration with PW 207E)
CSP−902RFM207E−1
F−xii Revision 5
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MD900 (902 Configuration with PW 207E)
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