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LUH 72 Study Progression > LUH72 Progression Deck > Flashcards

LUH72 Progression Deck Flashcards

1
Q

Engine Failure at OGE Hover steps

A

CACRASS

  1. Collective- adjust to maint. rotor
  2. A/S- increase if possible
  3. Collective- adjust OEI limit or below (12FLI)
  4. Rotor speed- trim to MAX
  5. A/S- gain 65kts (Vy)
  6. Collective- reduce to OEI MCP / blw (11FLI)
  7. Aff Eng - ID
  8. SE/ES - Perform
  9. Land - ASA Practicable
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2
Q

Engine Failure at OGE Hover Procedures

A
  1. collective adjust, rotor trim to max, 20 deg nose down, maintain trim/heading.
  2. excel through 30 KIAS, adjust collective 2.5 min OEI (12FLI); excel through 45 KIAS.
  3. 200’ AGL and/or clear of obstacles, adjust to 65 KIAS, adjust to OIC MCP or below
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3
Q

Engine Failure Low Altitude/Low Airspeed/Cruise Flight Steps

A

ORAS

  1. OEI Flt- Est
  2. Rotor Speed- Trim to MAX
  3. Aff Eng - ID
  4. SE/ES - Perform
  5. Land
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4
Q

Engine Failure Low Altitude/Low Airspeed/Cruise Flight Procedures

A
  1. announce engine failure, collective adjust to maintain RPM R, trim rotor to max, and adjust to OEI flight, maintain trim
  2. near landing adjust to 65KIAS, shallow approach, trim
  3. 50’ AGL and 40KIAS, running landing, NTE 300fpm descent, land w/ max FLI min fwd a/s
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5
Q

Autorotation Steps

A

CADB

  1. COL - reduce to maintain rotor speed
  2. A/S - maintain 70-90kts
  3. Dual Eng / ES - Perform
  4. Batt Mstr swtch- Off
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6
Q

Autorotation Procedures

A
  1. lower collective until engine and Rotor RPM split, maintain (60-90) 75* KIAS, trim
  2. NLT 200’ AGL ensure steady state auto is attained:
    - RPM R in limits
    - Airspeed
    - Trim
    - Landing area assured
  3. Terminate with one of the 2 options:
    - Power Recovery - abort
    - Terminate with Power - continue w/ maneuver
  4. 100’ AGL aft cyclic to deccel flare 15-20deg nose up, maintain alignment w/ landing
  5. 10’-15’ AGL collective to control descent/ground speed, reduce flare to 7deg, estab landing attitude
  6. come to stop at 5’ AGL, hover
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7
Q

Perform Manual Throttle (low side failure) Underspeed Steps

A

OBVANT

  1. OEI Flt- Est
  2. Bleed air consumers - Off
  3. VARNR - Chk Man
  4. Aff Eng- ID
  5. N2 Trim- comp NRO / Match TQ
  6. Twist Grip (aff eng)- Rels Stop - Rotate toward flt, stabilize Normal rng /FLI needles match
  7. Land - ASA Practical (perform VMC App. w/ man throttle. twist grip Idle before lowering COL)
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8
Q

Perform Manual Throttle (high/low side failures) Procedures

A
  1. confirm condition, identify malfunction, announce corrective action
  2. after landing, rotate twist grip to fly prior to placing collective in the full down position
    Warning* - do not let limiting stop fall into place when #2 throttle is in the EMER area.
    Caution* - releasing #1 safety throttle latch is difficult, will take longer to release
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9
Q

Fixed Pitch Steps

A

CASSALAA

  1. COL - reduce to min SS
  2. A/S - 70kts or >
  3. Suit land area - SEL
  4. Shall app w/ nose left (perform is 40kts w/ nose left)
  5. A/S - Reduce to aligne nose with FLT direction
  6. Landing - Perform
    * (If nose right above 40kts:)
  7. A/S - Increase
  8. App - Abort/climb
  9. Auto - perform
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10
Q

Fixed Pitch Procedures

A
  1. airspeed 70 KIAS or above, intercept and maintain approach angle, slow to 40 KIAS, <300fpm rate of descent, nose left - continue (right - abort)
  2. arrive over the first 1/3 of the landing area approx 5’ AGL w/ nose left
  3. maintain altitude while decreasing a/s until aligned w/ landing direction, apply fwd cyclic
    * collective increase will increase right yaw*
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11
Q

Perform Manual Throttle (high side failure) Overspeed Steps

A

CVNAT
1.COL - raise to maint. N2/NRO w/in limits
2. VARNR - Chk Man
3. N2 trim - NRO to 101 w/ match TQ
(If not possible:)
4. Aff Eng - ID
5. Twist grip - rotate toward Idle stabilize in Normal Rng/FLI needles match
6. Land - ASA Practical (perform VMC app w/ man throttle. Twist grip Idle before lowering COL)

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12
Q

Single Engine Emergency Shutdown

A

will situation allow for OEI flight?
1. Twist grip (aff eng) - Rotate slowly to Idle, check indications, then OFF
2. Rotor Speed - Trim to MAX
(Bleed air heating - will be shutdown automatically, depending on power margin of remaining eng - may be turned back on as follows:)
2. BLD HTG EMER/NORM sw - EMER
3. BLD HTG rheostat - ON

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13
Q

OEI Flight Conditions Establish in case power of Aff Eng Tends to Zero:

A
  1. Maintain ENG w/in Safe OEI Limits (12FLI or blw)
  2. Maintain A/C w/in Safe OEI limits (Airspeed: Max A/S 110kts below 12FLI……. OR……. Max 65kts between 12-14 FLI)
    NOTE: If a climb is necessary to reach safe flt altittude, attempt to obtain 65 Vy (best rate of climb) or 45 Vx (best climb gradient speed). Then establish A/S between 65-110kts.
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14
Q

OEI Flight Conditions Establish in case power of AFF ENG Still Delivers Power:

A
  1. Establish steady level flight and determine if the situation will allow for OEI flight by setting AFF ENG to IDLE and maintaining the Normal ENG w/in appropriate OEI limits.
  2. *If ENG PWR is sufficient for OEI flight (w/ 1 ENG Idle and 1 ENG Normal) continue w/ remaining steps of the relevant procedure and Land ASA Practical.
  3. *If ENG PWR is NOT sufficient for OEI flight: Land ASA POSSIBLE
  4. Then perform SE/ES
    * If necessary try to escape from danger w/ both ENGs operating
    * To determine if the situation will allow for OEI flight - rule of thumb - check that the sum of individual ENG TQs is lower than the OEI TQ limit
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15
Q

Land Immediately

A

The urgency of the landing is paramount. Primary considerations is to assure survival of the occupants. Landing in water, trees or other unsafe areas should be considered only as a last resort.

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16
Q

Land as soon as POSSIBLE

A

Land w/out delay at the nearest adequate site (i.e. open field) at which a safe approach and landing can be made.

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17
Q

Land as soon as practical

A

The landing site and duration of flight are at the discretion of the pilot. Extended flight beyond the nearest approved landing area where appropriate assistance can be expected is not recommended.

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18
Q

Resetting tripped Circuit Breakers

A

A tripped CB shall not be reset In-Flight unless doing so is consistent with EP. No attempt should be made to reset a CB if it trips a second time.

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19
Q

Basic Rules for Emergency Procedures

A
  1. Maintain Aircraft Control
  2. Analyze the Situation
  3. Take Proper Action
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20
Q

FLI: Starting Maximum (red hollow triangle)

A

FLI : 8.5
Time: N/A
TQ: NA
TOT: 785

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21
Q

FLI: Starting Transient (red solid triangle)

A

FLI: 11
Time: 5 sec
TQ: N/A
TOT: 865

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22
Q

FLI: Starting Normal Range (white band)

A

FLI: 6-7
Time: N/A
TQ: N/A
TOT: 650-700

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23
Q

FLI: AEO T/O Pwr Rng (yellow band)

A

FLI: 8.5-10
Time: 5 min
TQ: 71-88%
TOT: 845

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24
Q

FLI: AEO Max T/O Pwr (red vertical rectangle)

A

FLI: 10
Time: 5 min
TQ: 88%
TOT: 845

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25
Q

FLI: AEO Transient (red dot)

A

FLI: 10.5
Time: 12 sec (unintentional use)
TQ: 97%
TOT: N/A

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26
Q

FLI: OEI Max Cont. Pwr (MCP) (yellow vertical 2 blocks)

A

FLI: 11
Time: N/A
TQ: 91.5%
TOT: 845

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27
Q

FLI: OEI Transient Pwr (2.5 min) (red vertical 2 blocks)

A

FLI: 12
Time: 2.5 min (unintentional use)
TQ: 125%
TOT: 885

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28
Q

FLI: OEI Transient (red split dot)

A

FLI: 14
Time: 12 sec (unintentional use)
TQ: 140%
TOT: N/A

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29
Q

FLI Starting limits

A

FLI: 6-7
TOT: 650-700c (white range, normal start)

FLI: 8.5 - 11
TOT: 785-865c (Transient - 5 seconds / Red triangles)

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30
Q

AEO FLI/TQ/Airspeed Limits

A 
FLI:
0-8.5 : cont. ops 
            0-71% TQ
8.5 : MCP
             71% TQ
8.5-10 : T/O Pwr Rng (5 minutes)
             71-88% TQ
**A/S limited to 65kts above 8.5 FLI**
10 : MAX (red line)
             88% TQ
10-10.5 : Transient (12 sec unintentional)
             88-97% TQ
10.5 : MAX (red dot)
              97% TQ
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31
Q

OEI FLI/TQ/Airspeed Limits

A 
FLI:
0-11 : Cont. Ops *(MCP)*
       0-91% TQ
11-12 : Transient (2.5 min)
       91.5-125% TQ
A/S : limited to 110kts or 65kts if >12 FLI
12 : MAX (red line)
        125% TQ
12-14 : Transient (12 sec unintentional)
        125-140% TQ
14 : MAX (red dot)
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32
Q

AEO Over-Torque Limits

A
  1. Anytime greater than 8.5-10 FLI for over 5 min
  2. Anytime greater than 10-10.5 FLI for over 12 sec
  3. Anytime greater than 10.5 FLI
  4. Anytime A/S >65kts if FLI is over 8.5
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33
Q

OEI Over-Torque Limits

A
  1. Anytime greater than 11-12 FLI for over 2.5 min
  2. Anytime greater than 12-14 FLI for over 12 sec
  3. Anytime above 14 FLI
  4. Anytime A/S >65kts if FLI is over 12
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34
Q

Triple Tach Limits: ENG RPM Limits (N2: outer scale: #1/#2 needles)

A

N2 Eng / Rotor Limits:

  1. 96-104% - cont. operations (green arc)
  2. 96% - Min (red line)
  3. 104% - Max (red line)
  4. 106% - max over speed transient (12 sec or 5 min depending on pwr)
    * 12 sec if high pwr / eng TQ >2 x 30%
    * 5 min if low pwr / Eng TQ < 2 x 30%
  5. 85% - Max Underspeed transient (20 sec)
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35
Q

Triple Tach Limits: Rotor RPM Limits (inner scale: “R” needle, pwr ON)

A

Rotor Limits (PWR ON) are same as N2 Limits (PWR ON)

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36
Q

Triple Tach Limits: Rotor RPM Limits (inner scale “R” needle, pwr OFF)

A

Rotor Limits (PWR OFF)

  1. 80-104% (GM2000kg / 4410 lbs) - cont. Ops
  2. 104% - Max (red line)
  3. 110% - MAX, 12 sec transient (red dot)
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37
Q

Describe NRO Warning Light / Audio Sys.

A

NRO <95% : steady RPM light, low beeping tone
NRO 106-110% : Flashing RPM light w/ Warning Gong every 3 sec
NRO > 110% : Flashing RPM light w/ high steady pitch tone

EP for “Rotor RPM” Warning light:

  1. Rotor RPM Indicator - check
  2. COL Lever - Adjust as necessary to maintain NRO w/in normal range
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38
Q

What is the N2 overspeed Caution?

A

N2 over-speed over 123.1% may result in an engine over-speed trip (auto eng shutdown)

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39
Q

What rotor speed is maintained by VARTOMS?

A

The VARTOMS will control rotor speed automatically.
A/S /_ 55kts - rotor RPM will be controlled between 96.5-102%
*Note: If TQ split exceeds 15%, the VAR NR caution lgt appears and the MAN pb is yellow illum. TQ can be sync’d w/ the 4-way beep sw on the COL. Once TQ split less than 15% VARTOMS should return automatically to norm.
**Note: if N1 indicators show a difference of 10% or more ENG SPLIT caution lgt will appear on CAD.

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40
Q

Main Rotor Mast Moment Limits

A 
Normal Range: left side of yellow 
            >50%
Caution Range: Yellow region
            50-64%
Maximum: Red bar/red circle region
             64%
Transient (25 sec): >64-77%
Transient (7 sec): >77-90%
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41
Q

Mast Moment Caution

A

Mast Moment limitations can be exceeded while on the ground and collective is in the full down and locked position. Crewmembers must exercise extreme caution when entering and exiting the pilot stations to avoid contact w/ the cyclic w/ main rotor turning.

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42
Q

Mast Moment Exceeding the Red bar/Circle “Limit Lgt” / “Exceed Lgt”

A

A warning gong and a red box with “Limit” will come on at >64%.
All these indications disappear upon leaving the red bar/circle.
If >77% the MM “Exceed” light will come on and will NOT disappear.
Logbook entry and maintenance action is required whenever “Limit” or “Exceed” caution light has been exceeded.

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43
Q

MM maintenance action required if Total Accumulated Time Exceeds:

A

> 64% for 25 sec or >77% for 7 sec

Check log book form for accumulative time for each.

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44
Q

EP for MM EXCEED

A

MM >77% “Exceed” caution light will remain ON.
Land ASA practical
(avoid maneuvers causing high MM. Logbook entry required.)

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45
Q

What are limits for ENG Oil Pressure?

A

Min: 1.3 bar
Caution rng: 1.3 -1.5 bar
Cont.: 1.5-5.0 bar
Max: 5.0 bar

*NOTE: ENG Oil Pressure may exceed 5.0 bar during start must stay at idle until normal pressure.

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46
Q

What are limits for ENG Oil Temperature?

A

Min: -10c
Mac: 115c

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47
Q

What are limits for Transmission Oil Pressure?

A

Min: 1.0 bar
Caution rng: 1.0-1.5 bar
Cont.: 1.5-5.0 bar
Max: 5.0 bar

*NOTE: XMSN Oil Press Lgt “ON” between 1.0 to 1.4 bar during eng Idle /low RPM is acceptable.

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48
Q

What are limits for Transmission Oil Temperature?

A

Min: -10c
Max: 105c

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49
Q

EP for “ENG OIL P” (low)

A
  1. ENG Oil Press - Check
  2. OEI Flt cond - Estab
  3. Aff ENG - ID
  4. SE / ES - Perform
  5. LASA Practical
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50
Q

EP for “ENG OIL T” (high)

A
  1. OEI Flt cond - Estab
  2. Aff ENG - ID
  3. Twist Grip aff eng - Adjust TQ to 20-30% / oil temp monitor
    * 4. If temp below limits: LASA Practical
    * 4. If temp above limits: SE/ ES - Perform
  4. LASA Practical
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51
Q

EP for “XMSN OIL P” (low)

A 
Warning gong will acitvate
If ONE XMSN Oil Press Lgt:
1. Power - Reduce
2. LASA Practical
If BOTH XMSN Oil Press Lgts:
1. LAND IMMEDIATELY
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52
Q

EP for “XMSN OIL T” (high)

A
  1. XMSN (P) / XMSN (T) - Check
    * If w/in limits:
  2. LASA Practical
    * If above limits:
  3. Power - Reduce as much as possible
    * If remains above limits:
  4. LASA POSSIBLE
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53
Q

EP for “ENG CHIP Lgt”

A
  1. OEI Flt - Estab
  2. Aff ENG - ID
  3. *Alternate #1: SE/ES - Perform
  4. *Alternate #2: Twist Grip aff eng - Rotate slowly to Idle, check indications
  5. LASA Practical
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54
Q

Airspeed limitations (0-50kts limits - 10 total)

A
  • 15kts: Max rearward flight w/ hinged doors spoiled position
  • 17kts: Hover - IGE - X wind limitations (>7000DA), Controllability assured
  • 30kts: Hover - IGE - X wind limitations (
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55
Q

Airspeed Limitations (55-110kts limits)

A
  • 55kts: Pre-landing check - check RPM 101 when A/S below 55kts (VARTOMS = A/S <55kts = 101-103.5% / A/S >/_ 55kts = 96.5-102%)
  • 60kts: Front doors must be spoiler positions with sliding doors open
  • 65kts: Vy, best rate of climb A/S (Vne is 65kts when above AEO 8.5 or OEI 12)
  • 70kts: Min A/S (T/R Malf) until final then - 40kts w/ nose left
  • 90 kts: MAX for AUTOs (60-90kts / recommend 75kts)
  • 100kts: Max w/ hinged doors in spoiler positions
  • 100kts: Max A/S FIRE
  • 100kts: Max A/S w/ Cargo hook
  • 110kts: Max A/S for OEI Flt (limited to 65kts if above 12FLI)
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56
Q

Airspeed Limitations NOTE

A

NOTE: Flying with doors open/removed is “Prohibited” during IMC flights.
(If doors open - max X wind Hvr = 30kts, Front doors spoil >60kts, Vne 100kts Cruise)

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57
Q

Airspeed Automatic Flight Control System (AFCS)

A
  • 25kts: Max X wind for ILS App
  • 30kts: min for Indicated A/S Mode (IAS) Engaged - acceptable is 30kts - Vne
  • 30kts: Follow-Up Trim Activates <30kts (Decelerating) & Disengages >40kts (Accelerating)
  • 60kts: Use of Go-Around (GA) mode Prohibited w/ IAS mode engaged & A/S <60kts
  • 60kts: Min A/S req to engage Upper Modes; will disengage <20kts
  • 70kts: Min A/S (Vmiml) app. is 60kts (AFCS); for IFR app (AFCS) is 70kts
  • 80kts: Recommended A/S range for IMC app is 80-125kts
  • 120kts: Hands-On operation (Cruise) after (AFCS) failure max; ILS app max is 100kts
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58
Q

Minimum Hands-Off Flying Altitudes?

A

T/O is 200ft AGL

Other times is 500ft AGL

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59
Q

FIRE WARNING LIGHT (ON GROUND)

A
  1. FIRE sw (aff eng) - Raise Guard - PRESS
    NOTE: Aff ENG will shut down automatically, ACTIVATE indicator light, BOT 1 legend (both EMER OFF switch pnl), and F VALVE CL caution indication (CAD) come on. FIRE legend remains on as long as overheat condition exists)
  2. Both FUEL PRIME PUMPS - Check OFF
  3. BOT1/BOT2 pb - Press (BOT1 activated) - EXT ind. lgt comes on EMER OFF SW pnl)
    NOTE: Extinguisher bottle will begin discharging when N1<50%. After discharge of bottle contents, BOT1 legend and EXT light go off; BOT2 pb legend comes on.
  4. Clock stop watch - start
  5. Double ENG ES - Perform
  6. Passengers - alert/evac
  7. If situation permits and FIRE warning is still on after 1 min:
  8. BOT1/BOT2 pb - Press (BOT2 Activated)
  9. BAT MSTR switch - OFF
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60
Q

FIRE WARNING LIGHT IN FLIGHT

A
  1. OEI Flt cond - Estab
  2. Airspeed - Reduce if IAS is exceeding 100kts
  3. FIRE sw (aff eng) - Raise guard - Press
    NOTE: Aff ENG will shut down automatically, ACTIVATE indicator light, BOT 1 legend (both EMER OFF switch pnl), and F VALVE CL caution indication (CAD) come on. FIRE legend remains on as long as overheat condition exists)
    NOTE: Extinguisher bottle will begin discharging when N1<50%. After discharge of bottle contents, BOT1 legend and EXT light go off; BOT2 pb legend comes on.
  4. BOT1/BOT2 pb - Press (BOT1 activated) - EXT ind. lgt comes on EMER OFF SW pnl)
  5. Clock stop watch - start
  6. AFF ENG - ID
  7. SE / ES - Perform
  8. Passengers - Alert
  9. LASA POSSIBLE
    If FIRE warning is still on after 1 minute:
  10. BOT1/BOT2 pb - Press (BOT2 activated)
    If FIRE warning remains on:
  11. LAND IMMEDIATELY
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61
Q

WARNING LIGHT CABIN FIRE ON GROUND

A
  1. Double ENG ES - Perform
  2. Passenger - Alert/Evac
  3. Fire - Extinguish if possible
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62
Q

WARNING LIGHT CABIN FIRE IN FLIGHT

A
  1. A/S - 65kts recommended
  2. Passengers - alert
  3. Heating/air conditioning - OFF
  4. Fire - Extinguish if possible
  5. Fumes, smoke - eliminate, open sliding doors, windows and vents
  6. LAND AS SOON AS POSSIBLE
  7. After landing - Double ENG ES - Perform
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63
Q

LOW FUEL WARNING LIGHT IN FLIGHT

A 
1. Fuel Quantity indication - Check
If positive fuel indication in the main tank:
2. Both Fuel Pump XFER sw (FWD+AFT) - Check IN
3. Both Fuel Pum XFER CBs - Check IN
If BOTH FUEL LOW warning lgts remain on:
4. LAND W/IN 10 MINUTES
If One FUEL LOW warning lgt remains on:
5. Expect SE failure
64
Q

Which Emergency Procedures have LAND IMMEDIATELY?

A
  1. ENG Fire if FIRE warning remains ON

2. XMSN OIL PRESS warning with both indications below 1.0 bar

65
Q

Which Emergency Procedures have LAND AS SOON AS POSSIBLE?

A
  1. ENG FIRE if warning light goes OFF
  2. Cabin Fire
  3. Electrical Fire if fire/smoke continues
  4. BAT TEMP warning
  5. XMSN OIL PRESS if it remains above limits after reducing pwr
  6. GEN DISC (both) if unable to restore
  7. SHED EMER after going thru dual GEN DISCON procedure
  8. Total Electrical Pwr Loss
  9. FUEL FILT (both)
  10. ROTOR BKE
  11. 2nd AHRS failure (IFR) continue on stvy inst. if VFR
  12. Pedal Vibrations
  13. Wire Strike
66
Q

PPC Rules of Thumb

A 
Lbs to Kgs = 2.205
Zero fuel wt = (-) 1534 lbs
Low fuel = 24kgs / 53lbs
1% TQ = 90 lbs
1% TQ = (0-20c)
1% TQ = (20-40c)
2% TQ = 1000 PA
1% TQ = (5kts wind)
3% TQ = (6-10kts wind)
7% TQ = (>10kts wind)
7% TQ = (IGE - OGE)

VARTOMS: <55kts = 96.5 - 102 Nr
VARTOMS: >_55kts = 101 - 103.5 Nr

Charts that apply to “OEI” conditions are marked on the upper corner with a black color triangle

67
Q

When must a PPC be recomputed?

A

Increase of:
+5c
+500ft PA
+200lbs wt

68
Q

How do you convert Kg to lbs for PPC Gross Weight?

A

Use multiplier x 2.205

example: 3585kg x 2.205 = 7905 lbs

69
Q

Max PA & Max Temp will be used for all computations EXCEPT?

A

Go NO/GO Torque

Predicted Hover TQ

70
Q

How is Zero Fuel Wt computed on PPC?

A

Total Fuel is (112.3 gals).
Total Fuel Wt is 1530 lbs
*Subtract 1530 lbs from Aircraft GWT - Block (1) and enter into Zero Fuel Wt - Block (4)

71
Q

Why should you be concerned if Max TQ Avail AEO is above/below 97% TQ?

A

This number will allow you to know ahead-of-time (if) the Aircraft is capable of achieving Max TQ (AEO) - I/A/W Operator’s Sup Max TQ AEO (88% for 5 min or 97% for 12 sec)

72
Q

When computing GO NO/GO TQ (IGE/OGE) should you use Max or current Temp/PA?

A

Must use current Temp and PA

73
Q

During hover pwr check if “3ft hover TQ” is above or below GO NO/GO (IGE) TQ, what does that mean for you?

A

If above GO NO/GO (IGE) TQ: over Max GWT
If below GO NO/GO (IGE) TQ: below Mx GWT

If above GO NO/GO (OGE) TQ: aircraft is to heavy to perform OGE

74
Q

What is the significance of knowing Max GWT OGE w/ MCP?

A

If the actual Aircraft GWT is above this weight you can expect to be in the 5 min PWR T/O range (>8.5 FLI) while performing OGE maneuvers. (1% TQ = approx, 90 lbs)

75
Q

What is the significance of knowing the H/V Altitude (AGL)?

A 
Hovering OGE (w/ zero airspeed) at or above this ALT a safe landing can be expected after SEF.
Hovering OGE (w/ zero airspeed) below this ALT a safe landing may not be possible after a SEF. Avoid or stay minimum time.
(drawing a boundary curve on the HV diagram will reveal varying airspeed and altitude combinations from which a safe landing can be expected after a SEF and help determine areas that should be avoided if possible.
76
Q

Cruise Data on PPC:

What A/S and TQ will you use to stay on station as long as possible?

A

use Max Endurance Arirpeed and Max Endurance TQ

77
Q

What A/S and TQ will you use to climb as fast as possible?

A

Use Max TQ Avail (AEO): Red line - TQ = 88% / FLI = 10 (5 min)
Use A/S between 45kts (Vx) and 65kts (Vy) for best climb (A/S>65kts = over TQ)

78
Q

What is the significance of “OEI IAS - MIN/MAX”?

A

the Min A/S number should = 12 FLI (Max TQ 2.5 min)
When doing Practice SELs (OEI) attempting to land at Min A/S with Max FLI - this recorded A/S should be close to your touchdown speed.

the Max A/S nuber should = 12 FLI, (Max TQ 2.5 min)
This recorded A/S is your Max OEI IAS you can expect at 12 FLI.

(Remember: Vne for OEI flight is limited to 110kts)

79
Q

When does “Arrival Data” have to be computed?

A 
Must be computed if there is an increase of:
\+5c
\+500ft PA
\+200 lbs
Between departure and landing locations
80
Q

What Publications are required for flight?

A

RFM
FAA Airworthiness Cert
Logbook (DA Form 2408-12,13,14,18, Wt/Balance)
Checklist
PPC
Freq Card
Form 1891 inside ALSE Vest
Pubs for mission (IFR/VFR/Airfield)
Maps, Charts, Approach Plates, Supplement
FIH
IPAD and Electronic pubs, plus battery charged

81
Q

Flight Equipment Required for Flight?

A 
Per 95-1:
Flight Helment
ID Tags
Under Clothing (cotton/nomex/wool)
Flight suit
Flight Gloves
Flight Boots
82
Q

Inadvertant IMC Procedures

A

Pilot on the Controls:
A - Announce IMC: (maintain a/c control, transition to ins., initiate climb)
A - Attitude: Level the wings on Att Ind.
H - Heading: maintain heading, turn only to avoid known obstacles
T - TQ: Adjust TQ as necessary
T - Trim: Trim a/c as necessary
A - A/S: Adjust a/s as necessary
A - Altitude: Adjust to desired alt after estab a/c control

Pilot not on the Controls:
will monitor the cockpit instr. to assist in recovery, adjust transponder to emergency, tune radios, make approp. radio calls and perform other tasks as directed by the PC.

The most important action is to climb while estab. a/c control

The crew brief states local area specifics.

ATM states: Level Att, 65kts, Positive RoC, then complete IMC Procedurs

WARNING: do NOT use upper modes until a/c is under control.

83
Q

What is the Weight & Balance Classification of the UH-72?

A

Class II : a/c where Wt. /CG limits can readily be exceeded by loading arrangements (troops/pax). a/c whose Wt. and Bal Class is not stated in the Op. Man will be considered Class II.

84
Q

What are Pilot Responsibilities for Wt. & Bal I/A/W AR 95-1 and RFM?

A

95-1: Pilot must ensure a current & accurate Wt. & Bal Form is on board the ACFT.

95-1/RFM:Pilot must ensure the ACFT stays w/in Wt. & Bal limits for the entire flight.

RFM: ensure cargo is stowed properly (proper tie downs) & cargo will not shift in flight.

85
Q

What is a/c Max GWT?

A

3585kgs / 7905lbs

86
Q

What is Min GWT?

A

1750kgs / 3859lbs

87
Q

What is Max allowable floor loading?

A

600kg/m2 / 123lbs/sq ft

88
Q

What is Max allowable load per tie down?

A

70kg / 154.3lbs

89
Q

How do you compute a/c GWT?

A

ACFT Basic Wt + Crew Wt + Internal Load + Total Fuel on Board

90
Q

How do you compute ACFT Zero Fuel WT?

A

Total planning ACFT GWT at T/O - Total Fuel on Board at T/O

91
Q

How do you compute “useful load” for the mission? (how much additional wt in cargo & people can you carry)

A

Max Allowable GWT IGE / OGE - Total Planning ACFT GWT at T/O

92
Q

How can GO NO/GO TQ be used to verify Wt & Bal?

A

Exceeding Max GWT IGE during 3ft hover PWR check may overgross the ACFT or exceed other limitations.

Exceeding Max GWT OGE TQ during 3ft hover PWR check indicates ACFT is to heavy to perform OGE maneuvers.

93
Q

During preflight and ENG run up while following the checklist, what does the * mean?

A
  • means check shall be completed before each flight. Items not marked with * need only be checked before 1st flight of the day.
94
Q

Wind limitations for starting/shutdown high winds:

A

50kts Max

95
Q

What voltage on VMED would require the use of the EPU for starting?

A

less than 23.5 volts

96
Q

How are messages displayed on the CAD?

A

CAD is divided into 3 different sections:
System 1: (L/S) represents left power plant
System 2: (R/S) represents right power plant
MISC System: (center) includes operation of the non-redundant systems.

Messages are displayed as they are received - once acknowledged messages are displayed in order of importance.

97
Q

During the Bat HOR test Green LED / Red LED means?

A

Green LED - ensures 30 min of Emer PWR to Stby ATT
Red LED - Emer batt pack is empty, must be replaced

*IMC Flight is PROHIBITED because no Standby Horizon

98
Q

What are Engine Starter Energizer Time Limits?

A

EXT PWR:
20-On / 60 OFF
20 ON / 60 OFF
20 ON / 30 MIN OFF

BATT PWR:
30 ON / 60 OFF
30 ON / 60 OFF
30 ON / 30 MIN OFF

99
Q

What are Starter Energize Time Limits for Ventilation?

A

EXT PWR:
15 ON / 60 OFF
15 ON / 23 MIN OFF

BATT PWR:
20 ON / 60 OFF
20 ON / 23 MIN OFF

*NOTE: Do not vent both ENGs at the same time.

100
Q

What are the ABORT START CRITERIA?

A

Ignition - doe not take place w/in 15 sec
TOT - rise above limits
Oil Press ENG/XMSN not positive by ground IDLE
N2 & Rotor Needles not matched by ground IDLE
*CAUTION: If abort start must Vent Engine to prevent “hot start” on 2nd attempt start on same engine

101
Q

What are ABORT START PROCEDURES?

A

(P*) Twist Grip - (aff eng) OFF
(P) ENG START sw - (aff eng) OFF
(P) Engine Ventilation (aff eng) - Perform

102
Q

During engine start check Eng Starter sw OFF by _____% N1?

A

40% N1

103
Q

What 5 things must be accomplished Prior to initiating AFCS test?

A 
C - Coll - Locked
H - Hyd test complete
A - AP1 and AP2 - OFF
M - Mast Moment - Minimized
P - P/CP off the controls
*AFCS must be performed prior to the first flight of the day (once a day).
104
Q

After completing the Auto Pilot Test the “ON” light remains blinking, what is this an indication of and what are your actions?

A

Indicates a minor failure.

Attempt autopilot test a second time.

105
Q

During HYD test which system WILL NOT provide HYD boost to T/R?

A

HYD Sys #1 will NOT provide HYD boost to T/R

HYD Sys #2 will provide HYD boost to T/R

106
Q

What is maximum movement of cyclic during Run-up on the ground?

A

Not more than 3cm from nuetral

107
Q

During Bleed Air Heating check - what indication should you get on the CAD when BLD HTG rheostat is Turn On? What problem could result if No Light?

A

Green heating advisory light should appear on the CAD. (Below 10c no Green Lgt Defog system may not work properly to DeFog / DeIce front wind screens.)

108
Q

The VARTOMS will automatically become “Active” as soon as both engines reach _____

A

> 20% TQ

109
Q

Rotor RPM Light should go “OFF” as Rotor RPM passes through what %?

A

95%

110
Q

Before T/O check can be performed by memory at the Stage Field:

A 
Hover Flight -Perform
VarNR caution - OFF
N2 Rotor RPM - 101%
FLI Needles - Check
Hover PWR - Note
All Warn/Caut/CAD/VMED - Check 
Cabin Area - Crew/Pass/Mission Equip - Secure
111
Q

Before landing Check can be performed by memory at the Stage Field:

A

All Instruments - Check
All Warn/Caut/CAD/VMED - check
N2 / Rotor - check 101% below 55kts
Cabin Area - Crew/Pass/Mission Equip - Secure

112
Q

During Engine Shut Down:

A

Rotor RPM Lgt and Audio will com eon as Rotor RPM decreases <95%

Eng Fail Lgt and Gong will come on as N1 speed decreases <50%

113
Q

Engine must remain at idle for ____ seconds before shutdown.

A

30 seconds

Caution: Signal Eng Ldg with FLI above MCP (11FLI) requires 3 min cooling before S/D

114
Q

When closing Twist Grips decel time for N1 is ____ seconds to travel from ___%N1 to ____%N1.

A

40 seconds
30%
0%

115
Q

Rotor Brake may be applied when:

A

Both engines OFF & Rotor RPM <50%

NOTE: Allow min cooling period of 10 min before next application of rotor brake.

116
Q

VMC T/O Standards:

A

Determine and “announce” the type of T/O that requires min power to clear obstacles. Taking into account Gross WT, Power avail, and Distance from Obstacles.

117
Q

Normal T/O (VMC)

A

(Take Off on the “5’s”)
Perform hover flight - 3ft

Adjust cyclic to attain an accelerative attitude (5 deg nose below horizon)

Smoothly increase Collective to attain desired climb attitude (approx. 0.5 FLI above hover pwr)

A/S -PWR - Trim climb / maintain 50kts (in trim) until 50ft or clear of obstacles

After clearing obstacles or 50ft, place a/c in trim and accel to 65kts (Vy) then adjust to attain desired rate of climb (500fpm)

118
Q

Level Acceleration T/O (VMC)

A

Use when heavy or high pwr is required to Hover

slowly hover fwd while maintaining hover pwr.
Achieve ETL IGE, dont let settle to ground or increase pwr or abort
apply fwd cyclic to prevent blow back while maintaining pwr setting
as passes through ETL, A/C will climb at current pwr setting

119
Q

Constant Angle / Vertical T/O (VMC)

A

ALT over A/S T/O - confined area T/O
maintain constant angle from Hover or Gnd to a point in space to clear obstacles. demands more power than hover power.
After clearing obstacles, adjust controls for normal climb 65kts (Vy), 500fpm
in small confined areas a Vertical T/O (ALT over A/S) will require OGE pwr.

WARNING: Avoid steep right turns below 45kts

120
Q

VARTOMS:
Variable Rotorspeed and Torque Matching System
What two things does VARTOMS provide?

A

In the NORM mode: VARTOMS will adjust the “Rotor Speed” to its optimum range and perform “TQ Matching” of both engines.

In the MAN mode: the 4 way beep switch controls the “Rotor Speed” and “Match TQ” from the Collective heads.

121
Q

After startup, the VARTOMS will always be inactive for system check reasons but will automatically become activated as soon as both engines reach ___% TQ?

A

20% TQ

122
Q

The VARTOMS will adjust the Rotor Speed automatically to its optimum range depending on what 3 things?

A

Pressure altitude
air temperature
dynamic pressure from the airspeed and TQ of the engines

123
Q

VARTOMS A/S - Rotor RPM controlled at?

A

A/S <55kts : Rotor RPM 101-103%

A/S >55kts : Rotor RPM 96.5-102%

124
Q

If a TQ split exceeds ___% will cause the VAR NR caution on CAD & MAN pb Yellow Lgt to illuminate.
When will VAR NR return to normal from TQ split?

A

> 15%

<15%

125
Q

Central Panel Display System:
CAD -
VMED - Lane #1 and Lane #2

A

CAD: Caution and Advisory Display
- cautions and advisories, and onboard fuel information
VMED: Vehicle and Engine Monitoring Display
-Lane #1 displays FLI Needles (TQ, TOT or N1 that is nearest the limit)
-Lane #2 displays engine and dynamic system parameters related to on-board systems: Eng/XMSN, HYD Press/Temps, OAT, Vne, electrical (batt/GEN), optional equipment

126
Q

If VMED fails what displays selected parameters from it?

A

CAD

127
Q

If CAD fails, what displays selected cautions from it?

A

VMED Lane #1 or #2 (both are capable)

128
Q

How is stabilization of the aircraft from random P/R/Y excursions caused by wind and turbulence through what systems?

A

AFCS Auto-Pilot / Upper Modes, provide a high degree of stabilization through fiber optic gyros (FOG), computers, and magnetometers, SEMA’s and SAS systems enabling “Hands-Off” flight and even full autopilot w/ navigation.

129
Q

The basic function of AFCS/Autopilot is accomplished by using a mix of:

A

Sensors: OAT, FOG, magnetometers, air data computer (ADC), records changes in attitude P/R/Y and sends data to the “Brains”
Brains: 2 ea. Autopilot Modules (APM), 2 ea. Attitude & Hold Reference Systems (AHRS) which interpret and then calculate from aircraft sensors, a response to the movements of the aircraft through the use of systems “Muscles”
Muscles: Hyd assist - 5 ea. SEMA’s and SAS

130
Q

What are the 5 levels of Stabilization?

A
  1. Unstabilized: no AFCS and No autopilot
  2. Back-up SAS: Only SAS actuators ON
  3. Digital SAS: Autopilot On / Trim motor (s) Off
  4. Attitude Hold / Retention: Autopilot
  5. Upper Modes + Coupled Nav: Autopilot
131
Q

What is level 1 of Stabilization?

A

Unstabilized: use SAS/AP cut (cyclic)

- only basic force trim (FTR) is avail.

132
Q

What is level 2 of Stabilization?

A

Back-Up SAS: Use SAS On (cyclic)

  • both autopilots off
  • uses FOGs as sensors in P/R/Y axis (brains)
  • uses single SEMA as actuator in P/R/Y controlled by FOGs (muscles)
  • requires hands-on flight ops
  • 3 ea. SEMA’s / 3 ea. FOG’s + FTR is avail.
133
Q

What is level 3 of Stabilization?

A

Digital SAS: an autopilot mode provides attitude retention of a/c only:

  • a/c operates in this mode only when both autopilots are on and cyclic an/or yaw trim motors are off
  • uses AHRS sensors in P/R/Y axis (brains)
  • uses duplex SEMSs as actuators in P/R axis and single SEMA in Y axis (muscles)
  • all 5 SEMAs / FOG’s and FTR are avail*
134
Q

what is level 4 of Stabilization?

A

Basic Autopilot: Attitude hold. provides stable platform for upper modes:

  • both autopilots on, cyclic & yaw trim motors on, NO upper modes engaged
  • uses AHRS in P/R/Y axes
  • uses duplex SEMA in P/R and single SEMA in Y axes controlled by APM
  • Autopilots engaged, all 5 SEMAs / FOG’s and FTR avail.*
  • FTR switch releases cyclic control forces
  • BEEP TRIM moves P attitude 2deg/sec for and aft, and roll attitude 4deg/sec laterally
  • left/right pedal temporarily overrides Y trim
135
Q

What is level 5 of Stabilization?

A

Auto Pilot Upper Modes: Upper modes ops provide the following:

  • ALT hold
  • HDG acquisition/hold
  • IAS hold
  • VS hold
  • ALT Acquire
  • GA (go around)
  • GS (Glide Slope)
  • LOC (localizer)
  • VOR A (VOR Approach)
  • VOR (VOR Navigation)
  • BC (back course)
  • NAV (coupling to nav computer)
136
Q

AP MD DCPL sw In-Flight will ________ Upper Modes and Place AC into level 4.

A

disengage

137
Q

AP MD DCPL sw on-ground will do what?

A

center the cyclic

138
Q

What does the Follow-Up Trim provide for?

A

short term stabilization and wind gust disturbance through auto trimming functions to reduce cyclic stick forces especially during Hover Flight.

139
Q

When will Follow-Up Trim disengage (IAS)?

A

above 40kts when acceleration and active below 30kts when decelerating

140
Q

What overrides the Follow-Up Trim?

A

FTR if pressed and held while flying

141
Q

How can you improve the Yaw control in Hover Flight?

A

Turn off the Yaw Trim function

142
Q

What is the definition of NMS? (Navigation Management System)

A

pure GPS stand along system that is approved for IFR enroute, terminal and approach procedures. Use of NMS as a primary nav source is permitted only when a current and approved data base is used. IFR enroute, terminal and approach nav is PROHIBITED unless the pilot verifies the currency of the data base.
Traditional nav equip (VOR, DME…) are installed and serviceable, to provide an alternate means of nav. Approaches not approved as GPS overlay may be conducted with NMS only until reaching FAF, but approaches must be conducted with relevant traditional IFR equip.

143
Q

What is the min A/S to engage Upper Modes?

A

60kts

144
Q

At what A/S will Upper Modes disengage?

A

less than 20kts

145
Q

What is the AFCS “Safety Feature”?

A

If helicopter descends too low w/ vertical modes engaged, the AFCS will automatically revert back to ALT Mode and will Level-Off at 65ft AGL

146
Q

When using ALT Mode what control is used to maintain A/S?

A

Collective must be used to maintain A/S when using ALT Mode or changing ALT w/ ALT. A Mode
monitor A/S closely is A/S is less than 80kts

147
Q

At what A/S can you engage HDG Mode?

A

above 60kts

148
Q

At what A/S is GA Mode prohibited?

A

less than 60kts

149
Q

What is GA Mode used for?

A

in case of missed approach, will acquire and hold a predefined vertical speed of 1000ft/min for 10 sec, then automatically revert to VS mode. a loss of 60ft may be encountered during GA

150
Q

What must be selected to NAV (VOR)?

A

VLOC must be selected as NAV source, a route or direct-to must be established and screens on VOR.

151
Q

What must be selected to NAV (NMS)?

A

GPS must be selected as NAV source, a route or direct-to must be established and screens on NMS.

152
Q

How does APP Mode work (Approach)?

A

used to capture/track inbound course of approach.

  • rotate HDG bug to intercept course
  • set course selected for approach
  • press APP pb as copter nears selected track - the AFCS will disengage APP arm and HDG and the APP C will illuminate, course will be Captured and copter will turn inbound on course
  • Collective must be used to maintain desired A/S when ALT Mode is used for Step-Down altitudes*
153
Q

What is important to know about IAS Mode?

A
  • Collective must be used to maintain desired altitude.
  • reference limit is 30kts to VNE
  • IAS Mode must be engaged above 60kts
  • Fore/Aft motion of Beep-Trim sw will slew IAS reference at 8kts
  • IAS mode may be used during PAR while using COLL for glide slope and Hdg knob for course
154
Q

Is BC mode used?

A

no

155
Q

What is important to know about VS Mode?

A
  • COLL used to maintain A/S
  • at low height the Mode reverts to ALT mode, leveling off at 65ft AGL
  • Fwd/Aft motion of Beep Trim will slew the VS reference 200ft/min for each sec of Beep

LUH 72 Study Progression (1 decks)

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