E2-C2, ADV, & IUT RIFP-04
Airways Navigation Flight Procedures
Sg 7, fr 4
Sg 7, fr 2
PLANNING FOR AIRWAYS NAVIGATION MISSION
* FLIPs required for flight planning
STANDARD T-45A FUEL PLANNING DATA
Based on T-45A preliminary NATOPS flight manual, 1 MAY 1992 Change 5. Actual performance
* Check items for destination airfield
will vary with nonstandard temperature, winds, and varying gross weights. For initial planning only.
. 29. 8 lbs
. 3. .
Total usable fuel . . . . . . . . . . .
.
.
.
.
* Weather criteria
. .200 .
Start/Taxi/Takeoff . . . . . . . . . . .
.
.
.
.
. .
. .250 .
Penetration approach . . . . . . . . .
.
.
.
.
. .
* Takeoff minimums
. .250 .
GCA . . . . . . . . . . . . . . . . . .
.
.
.
.
. .
. .3.00 .
Reserve (20 min @ 10,000 FT MSL) .
.
.
.
.
.
* Planning for alternate
LOW LEVEL
360 KGS, 12K GW = 6.6 lbs/NM and 2,375 PPH
* Planning route of flight
300 KGS, 12K GW = 5.0 lbs/NM and 1500 PPH
JP-4 = 6.5 lbs/Gal
JP-5 = 6.8 lbs/Gal
JP-8 = 6.7 lbs/Gal
* Determining fuel requirements
CLIMB OUT (Using climb schedule: 250 KIAS to 10K, 300 KIAS to intercept .72 IMN)
* Preparing single-engine jet flight log
NM
KIAS
TIME
ALTITUDE
FUEL USED
5,000
0+01
* Military flight plan
250
04
60 lbs
10,000
0+02
250
10
120
15,000
0+04
300
20
190
* Criteria determining type of approach
20,000
0+06
300
28
260
25,000
0+08
292/.72
38
360
30,000
0+10
263/.72
53
440
* Additional airways navigation review topics
35,000
0+12
235/.72
70
540
40,000
0+16
209/.72
80
600
Sg 7, fr 5
ENROUTE (Max range @ 12K GW)
IMN
CAS
#/HR
TAS
#/NM
ALTITUDE
5,000
5.21
.43
260
1460
280
10,000
4.72
.45
250
1345
285
4.08
.49
245
1245
305
15,000
3.69
.52
240
1180
320
20,000
3.46
.56
230
1160
335
25,000
3.24
.61
225
1165
360
30,000
2.90
.65
220
1090
375
35,000
2.84
.68
200
1110
390
40,000
DESCENT (12K GW idle w/spd brakes in @ max range)
FUEL USED
NM
TIME
ALTITUDE
KIAS
25 lbs
5,000
195
12
0+03
80
10,000
195
28
0+07
90
15,000
195
39
0+10
125
20,000
195
53
0+14
150
25,000
195
68
0+17
175
30,000
195
85
0+21
210
35,000
195
100
0+24
225
40,000
195
116
0+26
OPTIMUM ALTITUDE and SPEED
GROSS WEIGHT
IMN
ALT
#/NM
3.08
13,000
.68
36,800 ft
2.86
12,000
.68
38,400 ft
2.63
11,000
.68
39,600 ft
VII. Determining fuel requirements for stages of flight 2.9.4.1.2, 2.1.8.1
A.
NATOPS performance data, Section XI for nonstandard conditions
B.
T-45A fuel planning data, above, for standard conditions during initial
planning. (Data is not current NATOPS values and is to be used for
training purposes only. DO NOT USE FOR FLIGHT.)
1.
Optimum altitude and speed
2.
Start, taxi, takeoff fuel
3.
Fuel to climb
(8-97) Original
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