Ops Limits Flashcards
EGT max/AB (Ground steady state)
630-650
EGT mil (Ground steady state)
630-650
EGT start (flight steady state)
925 max
EGT mil (FLT steady state)
630-650
EGT max/AB (FLT steady state)
630-650
Abort start when EGT reaches ____
845
Abort AC during ground start if EGT reaches _____
925
Total fluctuations in EGT of ______ are acceptable if EGT is between ___ and ____
15 (+/- 7.5), 630-650
RPM idle (Ground steady state)
46-50
RPM mil (Ground steady state)
99-101
RPM max/AB (Ground steady state)
99-101
RPM mil (FLT steady state)
99-104
RPM max/AB (FLT steady state)
99-104
RPM fluctuations idle
46-50
RPM fluctuations mil/max (GRD)
99-101
RPM fluctuations mil/max (FLT)
+/- 1
Nozzle idle (Ground steady state)
77-92
Nozzle mil (Ground steady state)
0-20
Nozzle max/AB (Ground steady state)
50-85
Nozzle mil (FLT steady state)
0-20
Nozzle max/AB (FLT steady state)
50-85
Nozzle fluctuations idle GRD
None allowed
Nozzle fluctuations mil/AB (GRD)
+/- 3
Nozzle fluctuations mil/AB (FLT)
+/- 3
Fuel flow start (Ground steady state)
360
Fuel flow idle (Ground steady state)
400-600
Fuel flow mil (Ground steady state)
2100-2700
Fuel flow start (FLT steady state)
360 (max)
Fuel flow idle (FLT steady state)
200
Oil pressure idle (Ground steady state)
5-20
Oil pressure mil (Ground steady state)
20-55
Oil pressure max/AB (Ground steady state)
20-55
Oil pressure idle (FLT steady state)
5 (min)
Oil pressure mil (FLT steady state)
20-55
Oil pressure max/AB (FLT steady state)
20-55
Fuel flow idle fluctuations (GRD)
+/- 25
Fuel flow fluctuations mil/AB (GRD)
+/- 50
Fuel flow fluctuations mil/AB (FLT)
+/- 50
Oil pressure fluctuations idle (GRD)
+/-2
Oil pressure fluctuations mil/max GRD
+/-2
Oil press fluctuations mil/max FLT
+/-2
Time durations mil (Ground steady state)
5
Time durations max/AB (Ground steady state)
5
Time durations mil (FLT steady state)
30
Time durations max/AB (FLT steady state)
15
EGT start (Ground steady state)
925 (max) 845
Following rapid throttle movements, nozzle position should stabilize within permissible fluctuation range within _______ seconds
10
During engine start the indicated fuel flow may momentarily transit above ______ LB/HR after advancing the throttle to idle during engine sequence but should return to equal to or less than ______ LB/HR prior to EGT rise during actual engine start
360 / 360
Do not exceed ___ minutes in military power with oil pressure above ________. If a sudden change of _______ or greater in oil pressure indication occurs at any stabilized RPM, follow engine oil system malfunction procedures in Section III of DASH 1
5 / 55 PSI / 10 PSI
Flaps 1% - 45%
300 KCAS
Flaps 46% - 60%
240 KCAS
Flaps over 60%
220 KCAS
Canopy
50 KCAS
Gear / gear doors
240 KCAS
Nose wheel steering
65 kts GS
Main wheel tire
214 (14 ply) kts GS
195 (12 ply) kts GS
Nose wheel tire
174 kts GS
Min PSI hydraulic pressure
1500
Max PSI hydraulic pressure
3200
Normal range hydraulic pressure
2850 PSI to 3200 PSI
WSSP Sym
0 to +4.0
WSSP Asym
0 to +3.0
WSSP normal capacity
140 LBS
Airspeed limits Max
400 KCAS
Airspeed limits SB open / turbulence
350 KCAS
Airspeed limits abrupt control
240 KCAS
DASH-1 prohibited maneuvers
1.
Vertical stalls
DASH-1 prohibited maneuvers
2.
Intentional Spins
DASH-1 prohibited maneuvers
3.
Continuous aileron rolls (more than one complete roll) will be accomplished only at 1.0 G and 3/4 or less stick deflection.
Oxygen pressure normal range
50 PSI to 120 PSI
Load factor 3500 Sym G
-2.3 to +5.7
Load factor 3000 Sym G
-2.4 to +5.9
Load factor 2000 Sym G
-2.6 to +6.5
Load factor 1000 Sym G
-2.9 to 7.2
Load factor 3500 Asym G
0 to +4.1
Load factor 3000 Asym G
0 to +4.3
Load factor 2000 Asym G
0 - +4.7
Load factor 1000 Asym G
0 to +5.0
Caution: Extension / retraction of landing gear at bank angles greater than _____ degrees or at load factors greater than _____ G can result in overs tress failure of the main landing gear sidebrace trunnion
45 / 1.5
Maximum allowable transient RPM ______ %
107
