1
Q
Scope of the NATOPS
A
contains flight clearance information, operating procedures and restrictions necessary for flight crews to effectively operate their aircraftno manual can address every situation completely or be a substitute for sound judgement
2
Q
Takeoff power max
A
4700 hp at temps up to 39.4*C (104*F) at sea level no bleed air
3
Q
max continuous power
A
4700 hp at 28.3*C (83*F) sea level with both a/c packs on
4
Q
Overspeed protection
A
- Np >104.5% the overspeed governor diverts oil from PCU to increase blade angle and control overspeed
- Np >106% fuel flow is decrease
- Np >119% the FADEC shuts down the engine
- Ng >109% the FADEC shuts down the engine
5
Q
AFCS Basic Operation
A
- -Used for 4-,3-engine operation during climb, cruise, descent and approach
- -Capable of intercepts of 90* (75* loc BC) 45*preferred
- -Autothrottles will not allow speed below 1.2 Vs
6
Q
Autopilot Limitations
A
- T/o and LDG
- A/S > Vh
- ILS Below 200’ HAT, Below MDA on NPA, over localizer
- IPRA below 200’ HAT
- At or below 500’ non-app operations
- RVSM ALT plus/minus 65’
- Weight >164,000 lbs below 1,000’ AGL, config changes or approach operations
7
Q
3 distinct phases of emergencies
A
- Establish and maintain A/C control, flt path clear of terrain, identify and verify nature of malfunction and complete memory items
- Complete ACAWS crew action items, engine-out considerations, determine COA (continue, mission abort, return to base/divert, etc.) and brief the plan
- Monitoring/managing degraded systems, prepare fro unscheduled LDG if necessary, employ crewmember at ACS`
8
Q
Immediate actions and stabilization during emergency
A
- Regardless of altitude PF keep controls and maintain safe flight path until immediate action items are completed- <1000 AGL
- PM announce nature of malfunction (engine failure) and perform duties as required
- >1000 AGL PM state precise nature of malfunction (gearbox No. 1 no oil pressure), PF shall verify and verbally confirm malfunction, AC then calls for appropriate checklist/crew action
- AC should assume role of PM
9
Q
Takeoff Abort Criteria<70 kts
A
- Abort if a major condition arises
- Abort with WARNING-CAUTION ACAWS
- Abort with any ADVISORY ACAWS associated with a malfunction
10
Q
Takeoff Abort Criteria>70kts to V1 (Vref)
A
- Abort if a major condition arises
- Abort for a MASTER CAUTION/WARNING AURAL and VISUAL ALERT that threatens takeoff
- Abort for an engine failure, fire or serious directional control problems exists
11
Q
Takeoff Abort Criteria>V1 (Vref)
A
- Continue takeoff unless airworthiness of A/C is in jeopardy
12
Q
Flaps 10
A
220kias
13
Q
flaps 20
A
210kias
14
Q
flaps 30
A
200kias
15
Q
flaps 40
A
190kias
16
Q
flaps 50
A
183kias
17
Q
flaps 60
A
165kias
18
Q
flaps 70
A
155kias
19
Q
flaps 80
A
150kias
20
Q
flaps 90
A
145kias
21
Q
flaps 100
A
145kias
22
Q
ldg gear extended
A
168kias
23
Q
ldg gear lights extended
A
250kias
24
Q
cargo door open and locked, ramp up and locked
A
250kias
25
cargo door (all positions)
250kias
26
ramp (all positions)
250kias
27
paratroop air deflectors open
150kias
28
paratroop doors open and locked
250kias
29
paratroop doors opening/closing
150kias
30
high-speed drogues
185-250kias
31
low-speed drogues
105-120kias
32
low-speed drogues engaged
130kias
33
severe turbulent airspeed
65kias above stall to 180kias
34
inop windshield nesa below 10,000ft
187kias
35
ldg gear door removed max speed, gear up
200kias
36
ldg gear door removed max speed, gear down
168kias
37
Taxi t/o max normal weight
164,000lbs
38
taxi t/o max alternate weight
175,000lbs
39
landing recommended sink rate 540fpm
142,000lbs
40
landing max normal sink rate 300fpm
164,000lbs
41
landing max alternate sink rate 300fpm
175,000lbs
42
sink rate limit with ar podstanks 1/4main tanks
tanks 1/4: 7,320lbs.....main tanks: 28,000lbs
43
sink rate limit with aux tanks
no limit
44
sink rate limit with ext tanks
less than or equal to 500lbs
45
nose gear deflections 20\*
20kts
46
nose gear deflection 60\*
5kts
47
max nose wheel tire speed
139kts
48
max main wheel tire speed
174kts
49
Fuel weight unbalance limits
1. 1,000 pounds between symmetrical pair (main/ext)
2. 1,500 pounds between wings
3. One aux tank full and other aux tank empty, provided all other tanks are symmetrical or unbalanced toward the opposite side
4. #1/#4 always contain 500-1000lbs more than #2/#3 except when total usable fuel is less than 6000lbs
50
T/O landing fuel management
1. each tank is w/in respective weight limit
2. 1/4 have 500-1000 more than 2/3
3. main tanks full except for STTOC, 1/4 greater than or equal to 7060lbs, 2/3 are greater than or equal to 6410lbs when externals have fuel
4. fuel unbalance within limits
5. sink rate limits are in accordance with chart
51
Enroute fuel management
1. each tank w/in respective limit
2. aux/ext contain usable fuel, 1/4 kept at 8310 and 500-1000 more than 2/3
3. W/O usable fuel in aux/ext, 1/4 stay @ 8310, crossfeed 2/3 down to 1520 then crossfeed 1/4 down to 1520
4. fuel unbalance within limits
5. sink rate limits in accordance with sink rate chart if outboards are full
52
eng start limit
70 secs on, 60 secs off for 5 cycles then 20 minute cooling cycle needed
53
apu limit
start duty cycle: 1 minute on and 4 minutes off no limit to duty cycle MAX cont EGT 680\*C If EGT exceeds 710\*C for \>3 sec reduce APU load' APU auto shutdown if RPM exceeds 110
54
Fuel tank limits 1/4
8310lbs
55
fuel tank limits 2/3
7650lbs
56
fuel tank limits aux
5810lbs
57
fuel tank limits ext
8900lbs
58
fuel tank limits fuselage tank
24,390lbs
59
Engine Failure Below Refusal Speed
A. Aborted Takeoff procedures......Perform (PF)
60
Engine Failure After Refusal Speed
A. Takeoff..........Continue (PF) B. Directional Control........Maintain (PF)-Maintain directional control and wings level with rudder and ailerons. At rotation speed: C. Aircraft attitude....Rotate to target pitch (PF)WARNING: Rotating at significantly less than 3 degrees per second or rotating to a pitch attitude significantly below the target may delay liftoff and result in not clearing obstacles.
61
Aborted Takeoff
A. Abort...................Announce (PF) B. Power levers......GND IDLE (PF) C. Brakes and nose wheel steering............As required (PF)
62
Engine Fire Shutdown
A. Fire Handle..............Pull (PM)B. Agent.........Discharge (if required) (PM)C. ENGINE START switch...........STOP (PM)
63
APU Fire (Ground/In Flight)
A. APU Fire Handle.............Pull (P/CP/PM) B. Agent................Discharge (if required) (P/CP/PM)
64
Fire/Smoke/Fumes Elimination
A. Crew/Passengers.................Notify (PF/PM)B. Oxygen....................Emergency, 100%, ON (ALL)
65
Rapid Decompression
A. Oxygen..........................Normal, 100%, ON (ALL)
66
Four Engine Flameout
A. Aircraft attitude.....Adjust to maintain 15-28% NG (PF) B. Power levers (all)..................FLT IDLE (PF) C. CROSS FEED switches......................CLSD (PM/CM) D. #2 and #3 ENGINE START switches.........STOP, START, Release (PM) E. #1 and #4 ENGINE START switches...........STOP, START, Release (PM)
67
Hose Rapid Trail
(-109 Reel) A. RAPID TRAIL......................Announce (CM) B. MASTER POWER LSK..................OFF (CM/PM) (-110 Reel) A. RAPID TRAIL............Announce (CM)
68
Broken Hose
A. Broken Hose/Breakaway.....Announce (as required) (CM/PM) B. HYDRAULIC POWER LSK..............OFF (CM/PM) C. MASTER POWER LSK.............OFF (CM/PM)
69
Hydraulic System Pressure LO/LOSS/LEAK
A. ENGINE PUMPS switches (affected system).............OFF (PM) B. SUCTION BOOST PUMPS switch (affected system)..........OFF (PM)
70
WINDSHEAR/GCAS/TAWS PULL UP Alert Recovery
A. TAKEOFF power..............set (PF) B. Aircraft attitude.............wings level, nose up (PF) C. Radar altitude, airspeed, and sink rate (as appropriate........................Call out (PM)
71
Ground Evacuation
A. Parking Brake......Set (P) B. Tower..................Notify (CP) C. Pressurization.............EMER DEPRESS (CP) D. Exits..........................Open (as required) (CM) E. FIRE Handles for all engines and APU..............Pull (CP) F. Crew/Passengers.............Notify to evacuate the aircraft (CP)
72
Ground evacuation alarm -- abandoned aircraft
one long sustained ring
73
prepare to bailout alarm bailout alarm
3 short rings one long sustained ring
74
ditching/crash imminent brace for impact
6 short rings one long sustained ring
75
how many overhead escape hatches
3 forward, center and aft
76
primary ground exit
crew entrance door
77
primary air exit
cargo door/ramp
78
how many fire extinguishers
4
79
of first aid kits
22
80
of hand axes
2
81
of emergency exit lights
8
82
of life vest stowage
10
83
of escape ropes
3
84
size of liferafts
20 person 30 person max/liferaft we carry four in the wings and one in the cargo compartment
85
how many walk-around O2 bottles
4, 2 up front one by the manual shutoff in the cargo compartment and the 4th by the ramp/door
86
What are the factors for an abort?
1. airspeed 2. seriousness of malfunction/degraded condition some warnings/cautions are inhibited from 70-140KIAS and below 400' AGL
87
Engine fire shutdown
WARNING=== applies if smoke or flames occur WARNING=== agent should only be discharged if condition persists after the fire handle was pulled or if any other indication or malfunction is suspected that requires the fire ext agent
88
Engine shutdown ACAWS
WARNINGS: -START VLV OPEN -ENG FIRE -MGT HI CAUTIONS: -ENG FLAMEOUT -FADEC A & B FAIL -GBOX NO OIL PRESSURE -PRESS HI / PRESS LO -HOT START -NP LO -OIL HOT -OIL LOW -PROP 1 CNTL LOST -PROP NO 119% PROTECT ADVISORIES: -ENG NO LIGHTOFF -ENG STAGNATED START
89
What caution is advised with UTIL SYS PRESS HI (C) or BSTR SYS PRESS HI (C) or for EXCESSIVE HYD SYSTEM PRESSURE?
DON'T shut down an engine! You will lose your pressure relief
90
If bleed air is available an airstart can be accomplished at an airspeed less than \_\_\_KIAS (Ng
250 KIAS \<29% Ng
91
If bleed air is not available, Ng needs to be?
15% \< Ng \< 29%
92
Altitudes for an airstart with what fuel?
25,000' JP-5/JP-8 Jet A 22,500' JP-4
93
What must the MGT be less than for start?
175\*C
94
What would make you not try a restart?
Eng vibration, fire or fluid leak
95
Purpose of the engine system?
monitor operation of engines, complete operations of engine and assist. Primary purpose is to supply power to the four propellers
96
3 major assemblies of the engine
1. power section 2. torquemeter 3. propeller gearbox
97
what does the torquemeter do?
it transmits power from the power section to the PGB
98
what does the PGB do?
transfers shaft horsepower to the Prop and powers power to the GMAD
99
what does the power section do?
provides power to the PGB with the 14 stage compressor, 2 stage gas generator turbine and 2 stage free power turbine
100
GMAD provides drive pads for:
-PCU -overspeed governor -pgb oil pump and scavenge pump -ac generator -hydraulic pump -prop high pressure oil pump
101
Power section accessory gearbox provides drive pads for?
-Fuel pump metering unit (FPMU) -Permanent magnetic alternator (PMA) -oil pressure and scavenge pumps -air turbine starter
102
engine oil tank specs
20 gal reservoir 12 gals liquid and 8 gals air with 0.66 gal reserve for aux feathering
