ROTORCRAFT FLIGHT MANUAL

EASA TIP Rev.7, Section III, §3.2 (sub §3.2.2) and §3.3 (sub §3.3.2). (ref. MAF 109G0257A427 dated 29 January 2024) Revised pages Title page, A-4 and B-1 thru B-4. Manufacturer’s Data 21 Revised page 1-14. EASA Approval N° 10083793 dated 29 January 2024; Acceptance i.a.w. FAA- EASA TIP Rev.7, Section III, §3.2 (sub§ 3.2.1) and §3.3 (sub§3.3.1) - Design change classified as Basic. (ref. MAF 109G0257A427 dated 29 January 2024) Revised pages Title page, A-4 and B-1 thru B-4. Manufacturer’s Data REVISION No. SUBJECT APPROVALPrinted copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM List of Document No. 109G0040A017 Effective Pages October 22, 2007 B-1 LIST OF EFFECTIVE PAGES Note Revised text is indicated by a black vertical line in the outer margin of the page and the approval revision number is printed in the lower margin. Note The yellow pages (marked with *) apply to FAA registered AW119 MKII helicopters only and supersede the corresponding pages of the Rotorcraft Flight Manual. The holders of the Rotorcraft Flight Manual who are affected shall replace the corresponding pages of the basic Rotorcraft Flight Manual. Page Revision N° *Title page 21 *A-1 8 *A-2 16 *A-3 19 *A-4 21 *B-1 thru *B-4 21 i and ii 0 iii 4 iv thru viii 0 PART I — EASA Approved 1-i 0 1-ii 13 1-iii and 1-iv 0 1-1 1 1-2 0 1-3 and 1-4 4 1-5 15 1-6 0 1-7 thru 1-13 0 1-14 21 1-15 thru 1-19 0 1-20 4 1-21 13 1-22 thru 1-25 0 1-26 and 1-27 4 1-28 thru 1-40 0 2-i 4 2-ii thru 2-iv 0 2-1 thru 2-3 0 2-4 1 2-5 17 2-6 13 Page Revision N° Printed copy not contractually maintained by Leonardo Helicopters List of AW119 MKII RFM Effective Pages Document No. 109G0040A017 B-2 October 22, 2007 LIST OF EFFECTIVE PAGES (Cont.d) 2-7 and 2-8 0 2-9 13 2-10 0 2-11 and 2-12 1 2-13 and 2-14 2 2-15 and 2-16 8 2-17 thru 2-21 0 2-22 4 2-23 0 2-24 17 2-25 thru 2-29 0 2-30 and 2-31 8 2-32 thru 2-34 0 3-i thru 3-iv 0 3-1 thru 3-9 0 3-10 7 3-11 19 3-12 and 3-13 0 3-14 and 3-15 0 3-16 thru 3-35 0 3-36 4 3-37 19 3-38 0 3-38A and 3-38B 19 3-39 thru 3-46 0 3-47 and 3-48 8 3-49 and 3-50 1 3-51 and 3-52 0 4-i thru 4-iv 0 4-1 thru 4-4 0 4-5 4 4-6 thru 4-8 0 Page Revision N° 4-9 thru 4-12 4 4-13 thru 4-19 0 4-20 4 4-21 0 4-22 4 4-23 thru 4-36 0 5-1 2 5-2 0 5-3 14 5-4 6 5-5 14 5-6 2 Supplement 1 (Refer to the applicable List of Effective Pages) Supplement 2 (Refer to the applicable List of Effective Pages) Supplement 3 (Refer to the applicable List of Effective Pages) Supplement 4 (Refer to the applicable List of Effective Pages) Supplement 5 (Refer to the applicable List of Effective Pages) Supplement 6 (Refer to the applicable List of Effective Pages) Supplement 7 (Refer to the applicable List of Effective Pages) Page Revision N° Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM List of Document No. 109G0040A017 Effective Pages October 22, 2007 B-3 LIST OF EFFECTIVE PAGES (Cont.d) Supplement 8 (Refer to the applicable List of Effective Pages) Supplement 9 (Refer to the applicable List of Effective Pages) Supplement 10 (Refer to the applicable List of Effective Pages) Supplement 11 (Refer to the applicable List of Effective Pages) Supplement 12 (Refer to the applicable List of Effective Pages) Supplement 13 (Refer to the applicable List of Effective Pages) Supplement 14 (Refer to the applicable List of Effective Pages) Supplement 15 (Refer to the applicable List of Effective Pages) Supplement 16 (Refer to the applicable List of Effective Pages) Supplement 17 (RESERVED) Supplement 18 (Refer to the applicable List of Effective Pages) Supplement 19 (Refer to the applicable List of Effective Pages) Page Revision N° Supplement 20 (Refer to the applicable List of Effective Pages) Supplement 21 (Refer to the applicable List of Effective Pages) Supplement 22 (Refer to the applicable List of Effective Pages) Supplement 23 (Refer to the applicable List of Effective Pages) Supplement 24 Reserved Supplement 25 (Refer to the applicable List of Effective Pages) PART II — MANUFACTER’S DATA C-1 18 C-2 0 6-i 18 6-ii thru 6-iv 0 6-1 thru 6-3 0 6-4 18 6-5 thru 6-7 0 6-8 and 6-9 4 6-10 0 6-11 thru 6-13 4 6-14 0 6-15 thru 6-17 4 6-18 thru 6-32 0 Page Revision N° Printed copy not contractually maintained by Leonardo Helicopters List of AW119 MKII RFM Effective Pages Document No. 109G0040A017 B-4 October 22, 2007 LIST OF EFFECTIVE PAGES (Cont.d) 7-i 2 7-ii 9 7-iii and 7-iv 0 7-1 and 7-2 0 7-3 and 7-4 9 7-4A and 7-4B 9 7-5 thru 7-14 0 7-14A thru 7-14D 2 7-15 thru 7-21 0 7-22 17 7-23 thru 7-32 0 8-i thru 8-iv 0 8-1 thru 8-10 0 9-i thru 9-iv 4 9-1 thru 9-48 4 * pages FAA only Page Revision N°Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Table of Contents Document No. 109G0040A017 11-06-07 Page i TABLE OF CONTENTS Page LIST OF REVISIONS...................................................................... A-1 LIST OF EFFECTIVE PAGES ........................................................ B-1 TABLE OF CONTENTS ....................................................................... i INTRODUCTION ................................................................................iii PART I — EASA APPROVED SECTION LIMITATIONS ...................................................................................... 1 NORMAL PROCEDURES .................................................................. 2 EMERGENCY AND MALFUNCTION PROCEDURES ....................... 3 PERFORMANCE ............................................................................... 4 OPTIONAL EQUIPMENT SUPPLEMENTS....................................... 5 PART II — MANUFACTURER’S DATA Page LIST OF REVISIONS...................................................................... C-1 SECTION WEIGHT AND BALANCE ................................................................... 6 SYSTEMS DESCRIPTION ................................................................ 7 HANDLING, SERVICING AND MAINTENANCE ................................ 8 SUPPLEMENTAL PERFORMANCE INFORMATION......................... 9 Printed copy not contractually maintained by Leonardo Helicopters Table of Contents AW119 MKII RFM Document No. 109G0040A017 Page ii 11-06-07 This Page Intentionally Left Blank Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Introduction Document No. 109G0040A017 11-06-07 Page iii Rev. 4 INTRODUCTION GENERAL It is responsibility of the flight crew to be familiar with the contents of this manual. REVISIONS (REISSUES) This manual is subject to revisions (reissues) which will be automati- cally distributed to all holders of the manual. It is the responsibility of the operator to assure that the revisions (reissues) are incorporated into the manual upon receipt. At the beginning of the manual there is the “List of Revisions” table that shows all pages of the manual which have been revised as well as number 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 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. Temporary Revision pages are not written in the “List of Effective Pages”. A complete list of active and inactive Temporary Revision are written in the “List of Temporary Revisions” page.Printed copy not contractually maintained by Leonardo Helicopters Introduction AW119 MKII RFM Document No. 109G0040A017 Page iv 11-06-07 TERMINOLOGY WARNINGS, CAUTIONS AND NOTES WARNING An operating procedure, practice, etc., which, if not correctly 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 rec- ommended. “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. “Secured” has been used to determine if the item under examination is correctly locked; mainly referred to doors and disconnectable items. “Security” has been used to determine if the item under examination is correctly positioned and installed. Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Introduction Document No. 109G0040A017 11-06-07 Page v ABBREVIATION The use of capitol letters in the text, apart from normal grammatical usage indicates the actual wording or marking of indicators, controls or control positions on the helicopters. Abbreviations and acronyms used throughout this RFM are defined as follows: — A/C : AirCraft — a.c. / AC : Alternating current — ADI : Attitude Data Indicator — AGL : Above Ground Level — AWG : Aural Warning Generator — A/F : Airframe — CCW : CounterClockWise — CG : Center of Gravity — CW : ClockWise — d.c. / DC : Direct current — EDU : Electronic Display Unit — EEC : Engine Electronic Control — EMM : Engine Maintenance Manuall — GW : Gross Weight — Hd : Density altitude — Hp : Pressure Altitude — HSI : Horizontal Situation Indicator — IAS : Indicated AirSpeed — ICS : InterCommunication System — I.D.S. : Integrated Display System — IGE : In Ground Effect — ISA : International Standard Atmosphere Printed copy not contractually maintained by Leonardo Helicopters Introduction AW119 MKII RFM Document No. 109G0040A017 Page vi 11-06-07 — ITT : Inter-Turbine Temperature — KCAS : Knots Calibrated AirSpeed — KIAS : Knots Indicated AirSpeed — LH : Left hand — MAN : MANual override system — MCL : Master Caution Light — MCP : Maximum Continuous Power — MEC : MEChanical — MFR : ManuFactureR — MGB : Main Gear Box — MWL : Master Warning Light — N1 : Gas generator speed — N2 : Power turbine speed — NR : Rotor speed — OAT : Outside Air Temperature — OGE : Out of Ground Effect — PLA : Power Lever Angle (throttle) — QTY : QuantiTY — RFM : Rotorcraft Flight Manual — RH : Right Hand — RMI : Radio Magnetic Indicator — ROC : Rate Of Climb in ft/min — RPM : Revolutions Per Minute — SAS : Stabilization Augmentation System — TAS : True AirSpeed in knots — TOP : Take-Off Power — TQ : Engine TorQue Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Introduction Document No. 109G0040A017 11-06-07 Page vii — VFR : Visual Flight Rules — VHF : Very High Frequency — V NE : Velocity Never Exceed — VSI : Vertical Speed Indicator — V Y : Best rate of climb speed — Xfer : Transfer — WCA : Warning Caution Advisory Printed copy not contractually maintained by Leonardo Helicopters Introduction AW119 MKII RFM Document No. 109G0040A017 Page viii 11-06-07 Figure 1. Helicopter — Three views WL STA STA 1666 DIA 10830 DIMENSIONS IN MILLIMETERS BL 0 9930 0 WL 0 WL 2531 STA 3380 1765 ICN-19-A-150000-G-A0126-00001-A-01-1 DIA 1940 3598 11144 12984 2100 Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Table of Contents EASA Approved 11-06-07 Page 1-i SECTION 1 LIMITATIONS TABLE OF CONTENTS Page GENERAL ....................................................................................... 1-1 BASIS OF CERTIFICATION ........................................................... 1-1 TYPE OF OPERATION ................................................................... 1-1 FLIGHT CREW ................................................................................ 1-1 NUMBER OF SEATS ...................................................................... 1-1 AIRSPEED LIMITATIONS (IAS) ..................................................... 1-2 FLIGHT WITH PASSENGER CABIN DOORS OPEN OR REMOVED ........................................................................... 1-2 GROUND SPEED LIMITATIONS .................................................... 1-2 SLOPE TAKE-OFF AND LANDING LIMITATIONS........................ 1-5 WEIGHT LIMITATIONS................................................................... 1-5 CENTER OF GRAVITY LIMITATIONS ........................................... 1-5 ALTITUDE LIMITATIONS ............................................................. 1-10 AMBIENT AIR TEMPERATURE LIMITATIONS ........................... 1-10 POWER PLANT LIMITATIONS..................................................... 1-11 GAS GENERATOR SPEED (N1) ............................................. 1-11 POWER TURBINE SPEED (N2) .............................................. 1-11 INTER-TURBINE TEMPERATURE (ITT) ................................. 1-12 ENGINE TORQUE (TQ) ........................................................... 1-12 Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Table of Contents Document No. 109G0040A017 Page 1-ii 11-06-07 EASA Approved Rev. 13 Page ROTOR LIMITATIONS (NR)..........................................................1-13 POWER-ON ..............................................................................1-13 POWER-OFF ............................................................................1-13 FUEL SYSTEM LIMITATIONS ......................................................1-14 FUEL PRESSURE ....................................................................1-14 ENGINE LUBRICATION SYSTEM LIMITATIONS ........................1-15 OIL PRESSURE........................................................................1-15 OIL TEMPERATURE ................................................................1-15 MAIN TRANSMISSION LUBRICATION SYSTEM LIMITATIONS 1-17 OIL PRESSURE........................................................................1-17 OIL TEMPERATURE ................................................................1-17 TAIL ROTOR GEARBOX LUBRICANT LIMITATIONS.............1-18 ENGINE STARTER LIMITATIONS................................................1-19 GENERATOR LOAD LIMITATIONS .............................................1-19 HYDRAULIC SYSTEM LIMITATIONS ..........................................1-20 FLUID PRESSURE ...................................................................1-20 APPROVED FLUID...................................................................1-20 MISCELLANEOUS LIMITATIONS ................................................1-21 ENGINE CONTROL SYSTEM LIMITATIONS ..........................1-21 BAGGAGE COMPARTMENT LIMITATIONS ...........................1-21 LANDING LIGHTS OPERATION VS MAGNETIC COMPASS INDICATION LIMITATIONS......................................................1-21 UPPER DECK WINTER KIT LIMITATIONS (IF INSTALLED) ..1-21 NORMAL IDS MODE OF OPERATION....................................1-21 INSTRUMENT MARKINGS ...........................................................1-22 ELECTRONIC DISPLAY UNIT FORMAT .....................................1-24 PLACARDS ...................................................................................1-38 Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Table of Contents EASA Approved 11-06-07 Page 1-iii LIST OF FIGURES Page 1-1. Airspeed Limitation - VNE (power on/off) ............................ 1-3 1-2. Weight and Longitudinal CG Envelope (metric units) ........................................................................ 1-6 1-3. Weight and Longitudinal CG Envelope (imperial units) ..................................................................... 1-7 1-4. Weight and Lateral CG Envelope (metric units) ........................................................................ 1-8 1-5. Weight and Lateral CG Envelope (imperial units) ..................................................................... 1-9 1-6. Airspeed Indicator.............................................................. 1-23 1-7. Back-up Dual Tachometer Indicator .................................. 1-23 1-8. EDU1 Primary Mode - START format (typical) .................. 1-26 1-9. EDU1 Primary Mode - CRUISE format (typical) ................ 1-26 1-10. EDU2 Secondary Mode - MAIN format (typical) ................ 1-27 1-11. EDU1 & EDU2 - REVERSIONARY format (typical)........... 1-27 1-12. EDU 1 - InterTurbine Temperature (ITT) ........................... 1-28 1-13. EDU 1 - Torque (TQ) ......................................................... 1-29 1-14. EDU 1 - Gas Generator Speed (N1).................................. 1-30 1-15. EDU 1 - Power Turbine Speed (N2) .................................. 1-31 1-16. EDU 1 - Rotor Speed (NR) ................................................ 1-32 1-17. EDU 2 - Engine Oil (Pressure and Temperature) .............. 1-33 1-18. EDU 2 - Transmission Oil (Pressure and Temperature) ............................................. 1-34 1-19. EDU 2 - Ammeter .............................................................. 1-35 1-20. EDU 2 - Fuel Pressure....................................................... 1-36 1-21. EDU 2 - Hydraulic Pressure............................................... 1-37 1-22. Placards in Clear View of the Pilot..................................... 1-38 Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Table of Contents Document No. 109G0040A017 Page 1-iv 11-06-07 EASA Approved LIST OF TABLES Page 1-1. Approved fuel.....................................................................1-14 1-2. Approved lubricating oils....................................................1-16 1-3. Approved lubricating oils....................................................1-17 1-4. Approved lubricating oils....................................................1-18 1-5. EDU parameters ................................................................1-24 1-6. EDU mode .........................................................................1-25 1-7. EDU revisionary mode .......................................................1-25 Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-1 Rev. 6 SECTION 1 LIMITATIONS GENERAL Compliance with the operating limitations in section 1 of this manual is mandatory. The helicopter must also be operated in accordance with the appropri- ate operating rules. BASIS OF CERTIFICATION The helicopter is certified under JAR 27 Small Rotorcraft Category, with the exemption of a limited number of paragraphs for which com- pliance has been demonstrated with CS 27 and FAR part 27. TYPE OF OPERATION This helicopter is approved for day and night VFR operation, in non- icing condition. The helicopter equipped with only the Radio COMM KY196B (as alter- native to Radio NAV/COMM KX165A) is approved for day VFR opera- tion only. No aerobatic maneuvres are permitted. FLIGHT CREW The minimum flight crew consists of one pilot who shall operate the helicopter from the right crew seat. NUMBER OF SEATS Eight (pilot included). Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-2 11-06-07 EASA Approved AIRSPEED LIMITATIONS (IAS) V NE (Power-ON/OFF).................................................. : See Figure 1-1 Minimum airspeed in autorotation (without close external references) ........................................: 60 KIAS Maximum airspeed with torque between 100 and 108.5% (take-off power range).................................: 75 KIAS FLIGHT WITH PASSENGER CABIN DOORS OPEN OR REMOVED V NE with one or both doors open or removed ........................: 85 KIAS V NE during doors opening and closing operation...................: 70 KIAS Note When passenger cabin doors are open or removed check the Weight and Balance of the helicopter. GROUND SPEED LIMITATIONS Maximum forward speed at touchdown after engine failure .................................................................... : 50 kts Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-3 Rev. 4 Figure 1-1. Airspeed Limitation - VNE (power on/off) -30 -20 -10 0 10 20 30 160 150 140 130 120 110 100 50 40 -6000 -4000 -2000 0 2000 4000 6000 8000 10000 12000 14000 16000 18000 20000 -50 -40 -30 -20 -10 0 10 20 30 40 50 60 70 80 90 100 110 120 OUTSIDE AIR TEMPERATURE - °C INDICATED AIRSPEED - KNOTS DENSITY ALTITUDE - FEET -1000 0 1000 2000 OAT LIMIT OAT LIMIT PRESSURE ALTITUDE - FEET 3000 4000 5000 6000 7000 8000 9000 10000 11000 12000 13000 14000 15000 ICN-19-A-151000-G-A0126-00003-A-01-1 109G0290T149/2 ISSUE A Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-4 11-06-07 EASA Approved Rev. 4 This Page Intentionally Left Blank Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-5 Rev. 15 40 SLOPE TAKE-OFF AND LANDING LIMITATIONS Nose-up operations.................................................................. : 12 deg Side-up operations................................................................... : 10 deg Nose-down operations ............................................................... : 2 deg WEIGHT LIMITATIONS Maximum Gross Weight for ground operations (towing and Take off prohibited) .............................. : 2900 kg (6393 lb) Maximum Gross Weight......................................... : 2850 kg (6283 lb). Minimum Gross Weight for flight ............................ : 1725 kg (3803 lb). CENTER OF GRAVITY LIMITATIONS Longitudinal CG limits .................................. : See Figures 1-2 and 1-3 Lateral CG limits .......................................... : See Figures 1-4 and 1-5 Note In some loading conditions the longitudinal limitation (aft limit) can be exceeded. Refer to Section 6 for loading instructions. Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-6 11-06-07 EASA Approved Note Longitudinal Station ”0” is 1785 mm forward of the front jack point. Figure 1-2. Weight and Longitudinal CG Envelope (metric units) 2531 2850 2160 1725 1812 3528 3580 3392 3284 3457 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200 3200 3300 3400 3500 3600 3700 119G0290T149/2 ISSUE A ICN-19-A-151000-G-A0126-00001-A-01-1 Minimum flying weight Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-7 40 Note Longitudinal Station “0” is 70.2 in forward of the front jack point. Figure 1-3. Weight and Longitudinal CG Envelope (imperial units) 5580 4762 6283 3803 3995 129.3 133.5 140.9 138.9 136.1 3000 3500 4000 4500 5000 5500 6000 6500 7000 127 129 131 133 135 137 139 141 143 145 119G0290T149/2 ISSUE A ICN-19-A-151000-G-A0126-00006-A-01-1 Minimum flying weight Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-8 11-06-07 EASA Approved Note Lateral Station “0” is 450 mm inboard from each main jack point and coincides with the helicopter longitudinal plane of symmetry. Figure 1-4. Weight and Lateral CG Envelope (metric units) 2450 1725 2450 2850 -53 60 -60 53 1400 1600 1800 2000 2200 2400 2600 2800 3000 3200 -100 -80 -60 -40 -20 0 20 40 60 80 100 119G0290T149/2 ISSUE A ICN-19-A-151000-G-A0126-00002-A-01-1 Minimum flying weight 1725 Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-9 40 Note Lateral Station “0” is 17.7 in inboard from each main jack point and coincides with the helicopter longitudinal plane of symmetry. Figure 1-5. Weight and Lateral CG Envelope (imperial units) 3803 5401 5401 6283 2.4 -2.4 2.1 -2.1 3000 3500 4000 4500 5000 5500 6000 6500 7000 -4 -3 -2 -1 0 1 2 3 4 ICN-19-A-151000-G-A0126-00007-A-01-1 Minimum flying weight 119G0290T149/2 ISSUE A 3803 Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-10 11-06-07 EASA Approved ALTITUDE LIMITATIONS Maximum operating altitude .............................. : 15000 ft (4572 m) Hp AMBIENT AIR TEMPERATURE LIMITATIONS Refer to Figure 1-1. Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-11 40 POWER PLANT LIMITATIONS The helicopter is powered by a Pratt & Whitney Canada PT6B-37A Build Specification 1242 turboshaft engine. GAS GENERATOR SPEED (N1) Minimum ...................................................................................... : 51% Cautionary (autorotation only)............................................. : 51 to 60% Continuous operation..................................................... : 60 to 100.1% Take-off (5 minutes) .................................................. : 100.1 to 103.2% Maximum take-off (5 minutes)................................................. : 103.2% Transient (30 seconds) ........................................................... : 103.8% Note Transient must not be used intentionally. POWER TURBINE SPEED (N2) Minimum ...................................................................................... : 95% Cautionary......................................................................... : 95 to 101% Continuous operation...................................................... : 101 to 103% Maximum ................................................................................... : 103% Transient (10 seconds) .............................................................. : 108% Note Transient must not be used intentionally. Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-12 11-06-07 EASA Approved INTER-TURBINE TEMPERATURE (ITT) Maximum continuous ............................................................... : 755 °C Take-off (5 minutes) ...................................................... : 755 to 810 °C Maximum take-off (5 minutes).................................................. : 810 °C Transient (5 seconds)............................................................... : 860 °C Maximum unlimited at starting ................................................. : 870 °C Transient at starting................................................................ : 1090 °C two second between 980 °C and 1090 °C. Note A linear variation applies above 870 °C, ten seconds, and 980 °C, two seconds. Note Transient must not be used intentionally. ENGINE TORQUE (TQ) Maximum continuous .................................................................: 100% Take-off (5 minutes) .....................................................: 100 to 108.5% Maximum take-off (5 minutes).................................................: 108.5% Transient (6 seconds)................................................................. : 115% Note Transient must not be used intentionally. Printed copy not contractually maintained by Leonardo Helicopters AW119 MKII RFM Section 1 Document No. 109G0040A017 Limitations EASA Approved 11-06-07 Page 1-13 40 ROTOR LIMITATIONS (NR) POWER-ON Minimum ...................................................................................... : 95% Cautionary......................................................................... : 95 to 101% Continuous operation...................................................... : 101 to 103% Maximum ................................................................................... : 103% Transient (10 seconds) .............................................................. : 108% Note Transient must not be used intentionally. POWER-OFF Transient (10 seconds) ................................................................ : 80% Minimum ...................................................................................... : 90% Continuous operation........................................................ : 90 to 110% Maximum ................................................................................... : 110% Printed copy not contractually maintained by Leonardo Helicopters Section 1 AW119 MKII RFM Limitations Document No. 109G0040A017 Page 1-14 11-06-07 EASA Approved Rev. 21 FUEL SYSTEM LIMITATIONS FUEL PRESSURE Cautionary............................................................................ : 0 to 7 psi Continuous operation ......................................................... : 7 to 25 psi Maximum................................................................................... : 25 psi (*) Contains fuel system icing inhibitor (FSII) (for JP-8, MIL-T-83133C allows two grades. The grade meeting NATO code F-34 has FSII while the grade meeting code F-35 has no FSII without prior agreement). (**) Use of TS-1 fuel complying with GOST 10227-86 specification, but not complying with Decree 118, is prohibited. (***) Use of Jet B fuel, alone or mixed with other approved fuels, is limited to operation with ambient temperature up to +15 °C. (****) Use of No. 3 Jet Fuel with additives T1502 or T1602 is prohibited. Note Any mixture of approved fuels may be used. Note For operation below 4 °C the use of anti-ice additive is author- ized but not mandatory since the engine oil system is provided with an oil-to-fuel heater where, depending upon the tempera- ture of the fuel, the engine oil is utilized to preheat the fuel. For additive requirements and blending procedures refer to EMM. Table 1-1. Approved fuel Type Specification JET A ASTM D1655 JET A-1 ASTM D1655 JET B (***) ASTM D1655 JP-5 (*) MIL-T-5624 JP-8 (*) MIL-T-83133 No. 3 Jet fuel (RP-3) (****) GB 6537-2018 TS-1 (**) GOST 10227-86, in addition complying to Decree 118 Printed copy not contractually maintained by Leonardo Helicopters