HT-18 Standardization Training TH-57 Autorotation Variables and Procedure

HT-18 Standardization Training TH-57 Autorotation Variables and Procedure

HT-18 Standardization Training TH-57 Autorotation Variables and Procedure Review January 20th, 2015 LT Brian Tips Carnes- Stan Ofiicer LT Johnny Dozer Kane- B Stage Stan LT Cole Fancy Weideman Form Stan Capt Ryan White- Night Tactics Stan LT Brendan McGunigle Low Level Stan / Training Officer Reference

NAVAIR 01-H57BC - NATOPS CNATRA P-457 CONTACT FTI COMTRAWINGFIVEINST 3710.8S RWOP CNATRA P402 (Rev. 04-11) Systems Workbook OH-58 Flight Manual Objectives Review autorotation variables. Drive a discussion of autorotation standards in training and associated techniques for instruction.

Provide expectations of making fields. Identify not often discussed hazards. Review course rules North of Tree Field. Outline Auto Variables Review

Auto Geometry FTI Procedures First Auto Other Hazards Make the Field North of Tree Field Course Rules Variables Controlled Airspeed Nr Reaction Time Uncontrolled

Gross Weight DA Wind Temperature Reaction Time TH-57 Glide Characteristics FTI vs. NATOPS

FTI: Nr maintained at or above 94% => Larger ROD & GS. NATOPS: Assumes 90% Nr Rate of Descent: 1360 1760 fpm (50kias) (72kias) Glide Ratio: 4.1 3.3 (72kias)

(50kias) 02/24/2020 "Warriors Train Here" 6 Auto Geometry 50 KIAS 72 KIAS Glide Slope Ratio: 3.25

19 DEG 600 AGL = 1,950 OTG (0.37 Miles) 300 AGL = 975 OTG (0.18 Miles) Glide Ratio: 4.08 14 DEG 600 AGL = 2,448 OTG (0.46 Miles) 300 AGL = 1224 OTG (0.23 Miles) Normal Approach Geometry

Glide Slope 2:1 600 AGL = 1200 (.23 Miles) OTG 300 AGL = 600 (.11 Miles) OTG Entry FTI 70 KTS / 600 AGL Enter the autorotation by smoothly lowering the collective to the full down position and simultaneously adding right pedal to maintain balanced

flight. Reduce twist grip to the flight idle position and turn to the course line. Verbals PAC: Lane, Lock, Sock PAC: Altitude 600 FT, 70 KIAS, VSI AT OR BELOW ZERO, AIRCRAFT IN TRIM PAC: Down, Right, IDLE, Turn. Transition to Final

FTI Transition to 50 to 60 KTS descending attitude. Monitor Nr and control between 90 and 107 % with collective (optimum 94 to 95%). NATOPS PAC: Attitude, Nr, Ball Final FTI Intercept the course line

and establish crosswind correction as necessary. Maintain the 50 to 60 KTS descending attitude. Ensure Collective is full down by 150 feet AGL Verbals PAC: 200 On Courseline PAC: 150 Collective Full Down Flare FTI

At 75 to 100 AGL flare with cyclic in order to reduce rate of descent, reduce groundspeed, and increase Nr. Adjust flare as required to achieve desired groundspeed and minimal rate of descent. Verbals Power Recovery PAC: 100 Flare, Twist Grip Full Open

PNAC: Roger Twist Grip Full Open Full Auto PAC: 100 Flare,Twist Grip Flight Idle. PNAC: Roger, Twist Grip is Flight Idle Recovery FTI 10 to 15 AGL, coordinate up collective and forward cyclic to slow the rate of descent and lower the

noce to level attitude. Maintain heading with the pedals. Verbals PAC: 10-15 Pull, Pause, Level Power Recovery PAC: 5 Taxi, Taxi, Taxi Full Auto PAC:5 Cushion, Cushion, Cushion. Low Rotor RPM Recovery

At 15 to 20, crack open the throttle slightly, lower the nose toward a level attitude and simultaneously increase the collective, bleeding rotor rpm no lower than 90%; smoothly rotate the twist grip to the full open position. Hazards Spike Knock Low RPM, Poor Auto Landing, Low G (+.5) Pylon Whirl Blade Flapping/Mast

Bumping. Touchdown after an Auto Tailboom Dynamic Modes Touchdown after auto (~64% N%) Highspeed auto (68-73%Nr) First Auto Controlled

Airspeed Nr Trim Reaction Time Uncontrolled Gross Weight DA

Wind Temperature Self Critique Debrief: Conditions DA Effects Winds Flare Pull Aim Points RWOP 3-6 para 3.5 #5 : Practice autorotations to a specific point are prohibited.

Webster. A point is geometric element that has zero dimensions and a location determinable by an ordered set of coordinates Lane 1500x400 Landing Area/Zone 200x200 Point Undefined Size Auto @ 200 AGL Calculated at

90% Nr 50 KIAS Min Descent 72 KIAS Max Glide Glide Slope 3.25 4.08

Distance OTG (Ft) 650 816 Rate of 1558 Descent (FPM) 1780 Time

(Sec) 6.7 7.7 *Does not account for flare. Expect longer distances at higher airspeeds. 650 50 KIAS @ 200 AGL 816 72 KIAS

@200 AGL 400 900 1400 1800 2450 72 KIAS @600 AGL 1950 50 KIAS

@ 600 AGL 400 2800 1900 1950 3550 3950 650 50 KIAS @ 200 AGL

816 72 KIAS @200 AGL 1100 4500 2200 816 72 KIAS @200 AGL

1000 650 50 KIAS @ 200 AGL 500 1900 500 650 50 KIAS @ 200 AGL

816 72 KIAS @200 AGL 1250x 300 1450x 550 1800 1050

650 650 50 KIAS @ 200 AGL 1200 816 72 KIAS @200 AGL 2190

540 650 50 KIAS @ 200 AGL 816 72 KIAS @200 AGL Conclusion

Know your variables. Instruct to the variables for that day. Relate FTI procedures through technique. Make the Field, Calibrate your eyes. Questions? Future Auto Fly Day March/April Time Frame HT-18 Standardization Training North of Tree Field No longer the wild west 20 January 2015

LT Jonny DOZER Kane CAT 1 STAN O North of Tree Field Why? At least 17 HAZREPs documenting slow to spool events Causal factor in recent Class-B mishap The fields in the channel suck Tree Field unavailable for simulated engine failures at altitude R+I 14-17 (Dated 14 NOV 14)

This is how we do it now Clarifying wave-off procedures 02/24/2020 "Warriors Train Here" 36 North of Tree Field Proficiency: When was the last time you flew a full auto? Are you targeting specific areas or the field in general or rolling it to Flight Idle and hoping for the best?

Are you sure you can make the field? If you are not confident, snivel for a QIP in a Bravo or with someone who is comfortable operating up there 02/24/2020 "Warriors Train Here" 37 North of Tree Field Normal flow of traffic or The Loop Fly North from Tree Field to Pistol Field East to Antenna Field

South to Utah Field West to intercept the power lines and then turn south When abeam Tree Field, turn west to split Tree Field Dont worry there will be a picture soon Peanut field is not a thing Dropping in Aircraft shall only execute one EP to each field then move to the next in the rotation Working Antenna is not a thing

02/24/2020 "Warriors Train Here" 38 North of Tree Field Wave-offs (power on or off does not matter) Wave-offs from fields after Simulated Emergencies at Altitude shall be executed away from the flow of traffic Once safe lateral separation has been attained and interval IDed, turn to parallel but heading the opposite direction Re-intercept course rules from a perpendicular heading behind your interval

Aircraft shall only execute one EP to each field then move to the next in the rotation. 02/24/2020 "Warriors Train Here" 39 Antenna Field North of Tree Field Pistol Field

Utah Field Peanut Field (Not a thing) 02/24/2020 Power Lines Tree Field "Warriors Train Here"

Normal Flow Blue line Flight at altitude Green arrows Wave-off routes Peanut Field Not a thing Wave-offs will be to the outside of The Loop (to the left) in order to remain predictable 40

Questions? 02/24/2020 "Warriors Train Here" 41

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