TM TECHNICAL MANUAL OPERATOR'S MANUAL FOR ARMY RC-12N AIRCRAFT NSN HEADQUARTERS, DEPARTMENT OF THE ARMY 29 APRIL 1994

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TECHNICAL MANUAL OPERATOR'S MANUAL FOR ARMY RC-12N AIRCRAFT NSN 1510-01-361-5016 WARNING DATA TABLE OF CONTENTS INTRODUCTION DESCRIPTION AND OPERATION AVIONICS MISSION EQUIPMENT OPERATING LIMITS AND RESTRICTIONS WEIGHT/BALANCE AND LOADING PERFORMANCE DATA NORMAL PROCEDURES EMERGENCY PROCEDURES DISTRIBUTION STATEMENT A: distribution is unlimited Approved for public release; REFERENCES HEADQUARTERS, DEPARTMENT OF THE ARMY 29 APRIL 1994 ABBREVIATIONS AND TERMS ALPHABETICAL INDEX A93BC00C0115

TECHNICAL MANUAL No. 1-1510-223-10 Operator s Manual ARMY MODEL RC-12N HEADQUARTERS DEPARTMENT OF THE ARMY Washington, D.C., 29 April 1994 REPORTING OR ERRORS AND RECOMMENDING IMPROVEMENTS You can help improve this manual. If you find any mistakes or if you know of any way to improve the procedures, please let use know. Mail your letter, DA Form 2028 (Recommended Changes to Publications and Blank Forms), or DA Form 2028-2 located in the back of this manual directly to: Commander, U.S. Army Aviation and Missile Command, ATTN: AMSAM- MMC-LS-LP, Redstone Arsenal, AL 35898-5230. A reply will be furnished directly to you. You may also send in your comments electronically to our E-mail address at <Is-lp@redstone.army.mil>, or by fax at (205) 842-6546 or DSN 788-6546. Instructions for sending an Electronic DA Form 2028 may be found at the back of this manual immediately preceding the hard copy DA Forms 2028. TABLE OF CONTENTS CHAPTER 1 INTRODUCTION... Section I. General... l-l CHAPTER 2 AIRCRAFT AND SYSTEMS DESCRIPTION AND OPERATION... 2-1 Section I. Aircraft... 2-1 Section II. Emergency Equipment... 2-20 Section III. Engines and Related Systems... 2-21 Section IV. Fuel System... 2-34 Section V. Flight Controls... 2-41 Section VI. Propellers... 2-45 Section VII. Utility Systems... 2-48 Section VIII. Heating, Ventilation, Coding, and Environmental Control System... 2-58 Section IX. Electrical Power Supply and Distribution System... 2-63 Section X. Lighting... 2-73 Section XI. Flight Instruments... 2-76 Section XII. Servicing, Parking, and Mooring... 2-84 CHAPTER 3 AVIONICS... 3-l Section I. General... 3-l Section II. Communications... 3-2 Section III. Navigation... 3-20 Section IV. Radar and Transponder... 3-77 CHAPTER 4 MISSION EQUIPMENT... 4-1 Section I. Mission Avionics... 4-1 Section II. Aircraft Survivability Equipment... 4-4 CHAPTER 5 OPERATlNG LIMITS AND RESTRICTIONS... 5-1 Section I. General... 5-1 Section II. System Limits... 5-1 Section III. Power Limits... 5-7 Section IV. Loading Limits... 5-7 Section V. Airspeed Limits, Maximum and Minimum... 5-9 Section VI. Maneuvering Limits... 5-9 DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited. l-l Change 1 i

Section VII. Environmental Restrictions... 5-10.1 Section VIII. Other Limitations... 5-12 Section IX. Required Equipment for Various Conditions of Flight... 5-12 CHAPTER 6 WEIGHT / BALANCE AND LOADING... 6-1 Section I. General... 6-1 Section II. Weight and Balance... 6-1 Section III. Fuel/Oil... 6-3 Section IV. Center of Gravity... 6-5 Section V. Cargo Loading... 6-5 Section VI. Survivability Equipment... 6-7 CHAPTER 7 PERFORMANCE... 7-1 CHAPTER 8 NORMAL PROCEDURES... 8-1 Section I. Mission Planning... 8-1 Section II. Operating Procedures and Maneuvers... 8-2 Section III. Instrument Flight... 8-27 Section IV. Flight Characteristics... 8-28 Section V. Adverse Environmental Conditions... 8-30 Section VI. Crew Duties... 8-35 CHAPTER 9 EMERGENCY PROCEDURES... 9-1 Section I. Aircraft Systems... 9-1 ii Change 1

CHAPTER 1 INTRODUCTION 1-1. GENERAL. These instructions are for use by the operator(s). They apply to the RC-12N aircraft. 1-2. WARNINGS, CAUTIONS, AND NOTES. Warnings, cautions, and notes are used to emphasize important and critical instructions. Explanatory examples are as follows: WARNING An operating procedure, practice, etc., which, if not correctly followed, could result in personal injury or loss of life. ÈÈÈÈÈ 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. 1-3. DESCRIPTION. a. This manual contains the best operating instructions and procedures for the RC-12N aircraft under most circumstances. The observance of limitations, performance, and weight/balance data provided is mandatory. The observance of procedures is mandatory except when modification is required because of multiple emergencies, adverse weather, terrain, etc. Your flying experience is recognized, and therefore, basic flight principles are not included. THIS MANUAL SHALL BE CARRIED IN THE AIRCRAFT AT ALL TIMES. b. The RC-12N is a pressurized, low wing, all metal aircraft and is powered by two turboprop engines. The basic mission of the aircraft is radio reconnaissance. 1-4. APPENDIX A, REFERENCES. Appendix A is a listing of official publications cited within the manual applicable to and available for flight crews. 1-5. APPENDIX B, ABBREVIATIONS AND TERMS. Appendix B is a listing of abbreviations and terms used throughout the manual. 1-6. INDEX. The index lists in alphabetical order, titled paragraphs, figures, and tables contained in this manual. 1-7. ARMY AVIATION SAFETY PROGRAM. Reports necessary to comply with the safety program are prescribed in AR 385-40. 1-8. DESTRUCTION OF ARMY MATERIEL TO PRE- VENT ENEMY USE. For information concerning destruction of Army materiel to prevent enemy use, refer to TM 750-244-1-5. 1-9. FORMS AND RECORDS. Army aviators flight record and aircraft maintenance records which are to be used by crew members are prescribed in DA PAM 738-751 and weight and balance manual TM 55-1500-342-23. 1-10. EXPLANATION OF CHANGE SYMBOLS. Except as noted in this paragraph, changes to the text and tables, including new material on added pages, are indicated by a vertical line in the outer margin extending close to the entire area of the material affected. Exception: pages with emergency markings, which consist of black diagonal lines around three edges, may have the vertical line or change symbol placed along the inner margins. Symbols show current changes only. A miniature pointing hand symbol is used to denote a change to an illustration. However, a vertical line in the outer margin, rather than miniature pointing hands, is utilized when there have been extensive changes made to an illustration. Change symbols are not utilized to indicate changes in the following: a. Introductory material. b. Indexes and tabular data where the change cannot be identified. c. Blank space resulting from the deletion of text, an illustration or a table. d. Correction of minor inaccuracies, such as spelling, punctuation, relocation of material, etc., unless correction changes the meaning of instructive information and procedures. 1-10.1 EFFECTIVITY CODES. The designator symbol CA is used throughout this manual to identify text, illustrations, and performance data Change 3 1-1

for aircraft equipped with the Improved Constant Area Exhaust Stacks. The designator symbol IR identifies text, illustrations, and performance data for aircraft equipped with the Infra Red Reducing Exhaust Stacks. Data which has no icons applies to both. 1-11. AIRCRAFT DESIGNATION SYSTEM. The designation system prescribed by AR 70-50 is used in aircraft designations as follows: EXAMPLE RC-12N R - Modified mission symbol (Reconnaissance) 1-12. USE OF WORDS SHALL, SHOULD, AND MAY. Within this technical manual the word shall is used to indicate a mandatory requirement. The word should is used to indicate a nonmandatory but preferred method of accomplishment. The word may is used to indicate an acceptable method of accomplishment. 1-13. PLACARD ITEMS. Where applicable, placarded items (switches, control, etc.) are shown throughout this manual in capital letters. C - Basic mission and type symbol (Cargo) 12 - Design number N - Series symbol 1-2 Change 3