TM-55-1510-219-CL Army Model RU-21H(Guardrail V) Avionics Upgrade Aircraft Manual

GENERAL INFORMATION AND SCOPE
REPORTING   ERRORS   AND   RECOMMENDING IMPROVEMENTS - TM-55-1510-219-CL_12
NORMAL PROCEDURES - TM-55-1510-219-CL_13
LEFT WING, AREA 1
LEFT MAIN LANDING GEAR - TM-55-1510-219-CL_15
NOSE SECTION, AREA 2 - TM-55-1510-219-CL_16
RIGHT ENGINE AND PROPELLER
RIGHT WING, AREA 3 - TM-55-1510-219-CL_18
EMPENNAGE, AREA 5
BEFORE STARTING ENGINES - TM-55-1510-219-CL_20
SECOND ENGINE START (BATTERY START) - TM-55-1510-219-CL_21
FIRST ENGINE START (GPU START) - TM-55-1510-219-CL_22
SECOND ENGINE START (GPU START) - TM-55-1510-219-CL_23
ENGINE RUNUP - TM-55-1510-219-CL_24
LINE UP - TM-55-1510-219-CL_25
DESCENT - MAX RATE (CLEAN)
DESCENT-ARRIVAL - TM-55-1510-219-CL_27
AFTER LANDING - TM-55-1510-219-CL_28
BEFORE LEAVING AIRCRAFT - TM-55-1510-219-CL_29
EMERGENCY PROCEDURES
ENGINE MALFUNCTION AFTER LIFTOFF (FLIGHT CONTINUED)
ENGINE MALFUNCTION DURING FLIGHT
ENGINE   MALFUNCTION   DURING   FINAL APPROACH)
ENGINE   RESTART   DURING   FLIGHT   USING STARTER
ENGINE RESTART DURING FLIGHT (NOT USING STARTER) - TM-55-1510-219-CL_35
LOW OIL PRESSURE - TM-55-1510-219-CL_36
BLEED   AIR   FAILURE   LIGHT   ILLUMINATED
SINGLE-ENGINE    DESCENT/ARRIVAL
PROPELLER FAILURE (OVER 2080 RPM) - TM-55-1510-219-CL_39
F I R E
ELECTRICAL FIRE - TM-55-1510-219-CL_41
FUEL SYSTEM - TM-55-1510-219-CL_42
ELECTRICAL SYSTEM - TM-55-1510-219-CL_43
BATTERY CHARGE LIGHT ILLUMINATED - TM-55-1510-219-CL_44
LANDING EMERGENCIES - TM-55-1510-219-CL_45
GEAR-UP LANDING (ALL GEAR UP OR UNLOCKED) - TM-55-1510-219-CL_46
LANDING WITH NOSE GEAR UNSAFE - TM-55-1510-219-CL_47
CRACKED WINDSHIELD (INTERNAL CRACK)
FLIGHT CONTROLS MALFUNCTION - TM-55-1510-219-CL_49
PERFORMANCE CHECKS - TM-55-1510-219-CL_50
ANTI-ICE SYSTEMS - CHECK
FIRE PROTECTION SYSTEM
WAYPOINT SELECTION - TM-55-1510-219-CL_53
TACAN STATION SELECTION
ELECTRIC    ELEVATOR    TRIM    AND    AUTOPILOT/FLIGHT    DIRECTOR OPERATION
4. Select HDG mode
AVIONICS CHECKS
TACAN
AUTOFEATHER - TM-55-1510-219-CL_59
OVERSPEED GOVERNORS - TM-55-1510-219-CL_60
PNEUMATIC PRESSURE - TM-55-1510-219-CL_61
PRESSURIZATION SYSTEM - TM-55-1510-219-CL_62

Western Governors University

Privacy Statement
Press Release
Contact

Integrated Publishing, Inc. - A (SDVOSB) Service Disabled Veteran Owned Small Business