Figure 10-3. Level Flight Envelopes A1-F18EA-NFM-200 ORIGINAL XI-10-15
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Figure 10-3. Level Flight Envelopes
A1-F18EA-NFM-200
ORIGINALXI-10-15
Phillip
Text Box
NATOPS FLIGHT MANUAL PERFORMANCE DATA NAVY MODEL F/A-18E/F - 165533 AND UP AIRCRAFT
Phillip
Text Box
http://info.publicintelligence.net/F18-EF-200.pdf
LOW ALTITUDE ACCELERATIONF414-GE-400MAXIMUM THRUST
GROSS WEIGHT E 34,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 3/72 3/73 3/74 3/75 3/77 3/79 3/81 3/84 3/87 1.13/1.07 .91/.96
480 6/149 6/152 6/154 6/157 6/160 7/167 7/174 7/181 7/190 1.14/1.08 .90/.95
520 8/202 8/207 8/211 8/216 9/221 9/232 9/244 10/258 11/273 1.15/1.09 .89/.94
550 9/244 10/251 10/257 10/264 10/272 11/288 12/307 12/330 14/357 1.17/1.11 .90/.94
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 3/74 3/75 3/76 3/77 3/78 3/81 3/84 4/87 4/90 1.13/1.06 .91/.95
480 6/152 6/154 6/157 7/161 7/164 7/171 7/179 8/187 8/197 1.14/1.08 .90/.95
520 8/206 8/211 9/216 9/221 9/227 10/239 10/252 11/268 11/286 1.16/1.10 .90/.94
550 10/250 10/257 11/265 11/273 11/282 12/302 13/327 14/358 16/401 1.18/1.12 .89/.93
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 3/75 3/76 3/77 3/79 3/80 4/83 4/86 4/89 4/93 1.12/1.06 .92/.95
480 7/155 7/158 7/161 7/165 7/168 7/176 8/185 8/194 9/205 1.15/1.08 .91/.95
520 9/210 9/215 9/221 9/227 10/233 10/248 11/264 12/283 13/306 1.16/1.10 .90/.94
550 11/255 11/264 11/273 12/284 12/296 13/325 15/365 18/439 --- 1.17/1.11 .88/.92
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/78 4/79 4/81 4/82 4/83 4/87 4/90 4/94 4/98 1.12/1.06 .92/.95
480 7/159 7/162 7/166 8/170 8/174 8/182 9/192 9/203 10/215 1.14/1.08 .91/.95
520 10/216 10/222 10/229 10/236 11/244 11/261 12/282 13/309 15/346 1.17/1.11 .89/.93
550 11/263 12/275 12/288 13/303 14/321 16/375 --- --- --- 1.19/1.13 .87/.91
Figure 10-4. Low Altitude Acceleration - Maximum Thrust (Sheet 1 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-16
LOW ALTITUDE ACCELERATIONF414-GE-400MAXIMUM THRUST
GROSS WEIGHT E 38,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 3/81 3/82 3/83 3/84 3/86 4/88 4/91 4/94 4/97 1.13/1.07 .91/.96
480 7/167 7/170 7/173 7/176 7/179 7/187 8/195 8/203 8/213 1.14/1.08 .90/.95
520 9/227 9/231 9/237 9/242 10/247 10/260 11/273 11/288 12/306 1.15/1.09 .90/.94
550 10/274 11/281 11/288 11/296 12/304 12/322 13/344 14/369 15/400 1.17/1.11 .89/.94
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 3/83 3/84 4/85 4/86 4/88 4/91 4/94 4/97 4/100 1.12/1.07 .91/.95
480 7/170 7/173 7/176 7/180 8/184 8/192 8/200 9/210 9/220 1.14/1.08 .90/.95
520 9/231 9/236 10/242 10/248 10/254 11/267 11/283 12/300 13/320 1.16/1.10 .90/.94
550 11/280 11/288 12/297 12/306 12/316 13/338 14/366 16/401 18/447 1.18/1.12 .89/.93
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/84 4/85 4/87 4/88 4/90 4/93 4/96 4/100 5/104 1.12/1.06 .92/.95
480 7/173 8/177 8/181 8/185 8/189 8/197 9/207 9/218 10/230 1.15/1.08 .91/.95
520 10/235 10/241 10/248 11/254 11/261 12/277 12/295 13/317 14/343 1.16/1.10 .90/.94
550 12/286 12/295 13/306 13/318 14/331 15/363 17/408 20/489 --- 1.17/1.11 .88/.92
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/87 4/89 4/90 4/92 4/94 4/97 5/101 5/105 5/110 1.12/1.06 .92/.95
480 8/178 8/182 8/186 8/190 9/195 9/204 10/215 10/227 11/241 1.14/1.08 .91/.95
520 11/242 11/249 11/256 12/264 12/273 13/292 14/316 15/346 17/386 1.17/1.11 .89/.93
550 13/295 13/207 14/322 15/339 15/359 18/419 --- --- --- 1.19/1.13 .87/.91
Figure 10-4. Low Altitude Acceleration - Maximum Thrust (Sheet 2 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-17
LOW ALTITUDE ACCELERATIONF414-GE-400MAXIMUM THRUST
GROSS WEIGHT E 42,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/90 4/91 4/92 4/94 4/95 4/98 4/101 4/104 4/108 1.13/1.07 .91/.96
480 7/185 7/188 8/191 8/195 8/199 8/207 8/216 9/225 9/236 1.14/1.08 .90/.95
520 10/251 10/256 10/262 10/268 11/274 11/288 12/303 12/319 13/339 1.15/1.09 .90/.94
550 12/303 12/311 12/319 12/327 13/337 14/357 14/380 15/408 17/442 1.17/1.11 .90/.94
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/91 4/93 4/94 4/96 4/97 4/100 4/104 5/107 5/111 1.13/1.07 .91/.96
480 8/188 8/192 8/195 8/199 8/203 9/212 9/222 9/232 10/244 1.14/1.08 .90/.95
520 10/256 11/262 11/268 11/275 11/281 12/296 13/313 13/332 14/354 1.16/1.10 .90/.94
550 12/310 13/319 13/329 13/339 14/350 15/375 16/405 17/443 19/495 1.18/1.12 .89/.93
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/93 4/95 4/96 4/98 4/99 5/103 5/107 5/111 5/115 1.12/1.06 .92/.95
480 8/192 8/196 8/200 9/204 9/209 9/219 10/229 10/241 11/254 1.14/1.08 .91/.95
520 11/261 11/267 11/274 12/282 12/289 13/307 14/327 15/351 16/379 1.16/1.10 .90/.94
550 13/316 14/327 14/339 14/352 15/366 17/402 18/451 22/539 --- 1.17/1.11 .88/.92
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/97 5/98 5/100 5/102 5/104 5/108 5/112 5/117 6/122 1.12/1.06 .92/.95
480 9/197 9/201 9/206 9/211 10/216 10/227 11/239 11/252 12/267 1.14/1.08 .91/.95
520 12/268 12/276 12/284 13/293 13/302 14/324 15/350 17/382 18/427 1.17/1.11 .89/.93
550 14/327 15/341 15/356 16/375 17/397 20/463 --- --- --- 1.19/1.13 .87/.92
Figure 10-4. Low Altitude Acceleration - Maximum Thrust (Sheet 3 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-18
LOW ALTITUDE ACCELERATIONF414-GE-400MAXIMUM THRUST
GROSS WEIGHT E 46,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/98 4/100 4/101 4/103 4/104 4/108 4/111 5/115 5/119 1.13/1.07 .91/.96
480 8/203 8/206 8/210 8/214 9/218 9/227 9/237 10/247 10/259 1.14/1.08 .90/.95
520 11/275 11/281 11/288 11/294 12/301 12/316 13/332 14/351 14/372 1.16/1.09 .89/.94
550 13/333 13/341 13/350 14/359 14/369 15/392 16/417 17/448 18/485 1.17/1.11 .90/.94
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/100 4/102 4/104 4/105 4/107 5/110 5/114 5/118 5/122 1.13/1.07 .91/.96
480 8/206 9/210 9/215 9/219 9/223 9/233 10/244 10/255 11/268 1.14/1.08 .90/.95
520 11/281 12/288 12/294 12/301 12/309 13/325 14/344 15/365 16/389 1.16/1.10 .90/.94
550 14/341 14/350 14/361 15/372 15/384 16/411 18/444 19/486 21/542 1.18/1.12 .89/.93
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/102 5/104 5/106 5/107 5/109 5/113 5/117 5/122 6/127 1.12/1.07 .92/.95
480 9/211 9/215 9/220 10/225 10/230 10/240 11/252 11/265 12/280 1.15/1.08 .91/.95
520 12/286 12/293 13/301 13/309 13/318 14/337 15/359 16/385 17/416 1.16/1.10 .90/.94
550 14/347 15/359 15/372 16/386 17/402 18/441 20/494 24/598 --- 1.18/1.11 .88/.92
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 5/106 5/108 5/110 5/112 5/114 5/118 6/123 6/128 6/134 1.12/1.07 .92/.95
480 10/217 10/221 10/226 10/231 11/237 11/249 12/262 12/277 13/294 1.15/1.08 .91/.95
520 13/294 13/303 14/312 14/321 14/332 15/355 17/384 18/419 20/467 1.17/1.11 .89/.93
550 15/359 16/374 17/391 18/412 19/436 22/507 --- --- --- 1.19/1.13 .88/.92
Figure 10-4. Low Altitude Acceleration - Maximum Thrust (Sheet 4 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-19
LOW ALTITUDE ACCELERATIONF414-GE-400MAXIMUM THRUST
GROSS WEIGHT E 50,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 4/107 4/109 4/111 5/112 5/114 5/117 5/121 5/125 5/129 1.13/1.07 .91/.96
480 9/221 9/225 9/229 9/233 9/238 10/248 10/258 11/270 11/282 1.15/1.08 .90/.95
520 12/300 12/307 12/313 12/321 13/328 13/344 14/362 15/382 16/405 1.16/1.10 .89/.94
550 14/363 14/372 15/381 15/392 15/402 16/427 17/455 19/488 20/528 1.17/1.11 .89/.94
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 5/110 5/111 5/113 5/115 5/117 5/120 5/125 5/129 6/134 1.12/1.07 .91/.96
480 9/225 9/229 10/234 10/239 10/244 10/254 11/266 11/278 12/293 1.14/1.08 .90/.95
520 12/306 13/313 13/321 13/329 14/337 14/355 15/375 16/397 17/424 1.16/1.10 .90/.94
550 15/371 15/382 16/393 16/405 17/418 18/448 19/484 21/529 23/589 1.18/1.12 .89/.93
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 5/112 5/113 5/115 5/117 5/119 5/124 6/128 6/133 6/138 1.13/1.07 .92/.95
480 10/230 10/235 10/240 10/245 11/250 11/262 12/275 12/289 13/305 1.15/1.08 .91/.95
520 13/312 13/320 14/328 14/337 14/346 15/367 16/391 17/419 19/453 1.16/1.10 .90/.94
550 16/379 16/391 17/405 17/421 18/438 20/480 22/538 26/648 --- 1.18/1.11 .88/.92
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 5/116 5/118 5/120 6/122 6/125 6/129 6/134 6/140 7/146 1.12/1.07 .92/.95
480 10/236 11/241 11/247 11/252 11/258 12/271 13/286 13/302 14/320 1.15/1.09 .91/.95
520 14/321 14/330 15/340 15/350 16/361 17/387 18/418 20/456 22/508 1.17/1.11 .89/.93
550 17/391 18/407 18/426 19/448 20/475 23/551 --- --- --- 1.19/1.13 .88/.92
Figure 10-4. Low Altitude Acceleration - Maximum Thrust (Sheet 5 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-20
LOW ALTITUDE ACCELERATIONF414-GE-400MILITARY THRUST
GROSS WEIGHT E 34,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 5/40 5/41 6/42 6/43 6/44 6/47 7/50 7/53 8/57 1.17/1.08 .90/.95
480 11/84 11/87 12/90 12/94 13/97 14/106 15/117 17/130 19/148 1.22/1.13 .87/.92
520 15/117 16/122 17/128 18/135 18/142 21/160 24/184 29/222 39/301 1.23/1.13 .83/.88
550 19/145 20/153 21/162 22/173 24/187 29/224 --- --- --- 1.27/1.17 .84/.91
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 6/41 6/42 6/43 6/44 6/46 7/49 7/52 8/56 8/61 1.17/1.09 .90/.94
480 12/87 12/90 13/93 13/97 14/102 15/112 17/124 19/141 22/163 1.23/1.14 .87/.92
520 16/121 17/127 18/134 19/141 20/150 23/171 27/202 35/258 --- 1.25/1.15 .84/.90
550 20/151 22/161 23/173 25/188 28/207 --- --- --- --- 1.25/1.16 .85/.91
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 6/42 6/43 6/45 7/46 7/48 7/51 8/55 9/60 9/65 1.17/1.09 .90/.94
480 13/90 13/93 14/98 14/102 15/107 17/119 19/134 22/154 26/184 1.25/1.16 .87/.91
520 18/126 19/133 20/140 21/150 22/161 27/191 35/249 --- --- 1.24/1.14 .85/.90
550 22/157 24/171 26/188 30/214 --- --- --- --- --- 1.23/1.14 .85/.90
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 7/44 7/46 7/47 7/49 8/51 8/55 9/59 10/65 11/72 1.17/1.09 .90/.94
480 14/93 14/98 15/102 16/107 17/113 19/127 21/146 25/172 32/215 1.22/1.14 .87/.91
520 19/131 20/140 22/150 24/162 26/178 --- --- --- --- 1.23/1.14 .87/.92
550 24/169 27/191 33/230 --- --- --- --- --- --- 1.24/1.14 .83/.88
Figure 10-5. Low Altitude Acceleration - Military Thrust (Sheet 1 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-21
LOW ALTITUDE ACCELERATIONF414-GE-400MILITARY THRUST
GROSS WEIGHT E 38,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 6/44 6/46 6/47 6/48 7/49 7/52 7/56 8/60 9/64 1.17/1.08 .90/.94
480 12/94 13/98 13/101 14/105 14/109 16/119 17/131 19/146 22/167 1.22/1.13 .87/.92
520 17/131 18/137 19/144 20/151 21/159 23/179 27/207 32/250 44/339 1.23/1.14 .83/.88
550 21/162 22/171 24/182 25/194 27/209 32/252 --- --- --- 1.27/1.17 .85/.91
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 6/46 7/47 7/48 7/50 7/51 8/55 8/59 9/63 10/68 1.17/1.09 .90/.94
480 13/97 14/101 14/105 15/109 16/114 17/126 19/140 22/158 25/183 1.23/1.14 .87/.92
520 18/136 19/143 20/150 21/158 23/168 26/192 31/227 39/289 --- 1.25/1.15 .84/.90
550 23/169 24/180 26/194 28/211 31/232 --- --- --- --- 1.26/1.16 .85/.91
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 7/47 7/48 7/50 8/52 8/53 8/57 9/62 10/67 11/73 1.16/1.09 .90/.94
480 14/101 15/105 16/110 16/115 17/120 19/133 21/150 24/173 29/207 1.25/1.16 .87/.92
520 20/141 21/149 22/158 24/168 25/180 30/214 39/278 --- --- 1.24/1.14 .85/.90
550 25/177 27/192 29/211 33/241 --- --- --- --- --- 1.23/1.13 .85/.90
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/49 8/51 8/53 8/55 9/57 9/61 10/67 11/73 12/81 1.17/1.10 .90/.94
480 15/105 16/110 17/115 18/121 19/127 21/143 24/164 28/193 36/242 1.22/1.14 .87/.91
520 21/147 23/157 24/168 26/182 29/200 --- --- --- --- 1.23/1.14 .87/.92
550 27/189 31/214 37/258 --- --- --- --- --- --- 1.23/1.14 .83/.88
Figure 10-5. Low Altitude Acceleration - Military Thrust (Sheet 2 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-22
LOW ALTITUDE ACCELERATIONF414-GE-400MILITARY THRUST
GROSS WEIGHT E 42,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 7/49 7/51 7/52 7/53 7/55 8/58 8/62 9/67 10/72 1.17/1.08 .90/.94
480 14/105 14/108 15/112 15/117 16/122 17/132 19/146 21/163 24/185 1.23/1.13 .87/.92
520 19/146 20/152 21/159 22/168 23/177 26/199 30/230 36/277 49/377 1.24/1.14 .83/.88
550 23/180 25/190 26/202 28/216 30/232 36/279 --- --- --- 1.27/1.17 .84/.90
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 7/51 7/52 8/54 8/55 8/57 8/61 9/65 10/70 11/76 1.17/1.09 .90/.94
480 15/108 15/112 16/117 17/121 17/127 19/139 21/155 24/176 28/204 1.24/1.14 .87/.92
520 20/151 21/158 23/166 24/176 25/186 29/213 34/252 44/326 --- 1.25/1.15 .84/.89
550 24/188 27/200 29/215 31/234 34/258 --- --- --- --- 1.26/1.16 .85/.91
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/52 8/54 8/56 8/57 9/59 9/64 10/69 11/75 12/82 1.17/1.09 .90/.94
480 16/112 17/117 17/122 18/127 19/133 21/148 24/167 27/193 33/230 1.25/1.16 .87/.92
520 22/156 23/165 24/175 26/186 28/200 33/238 42/304 --- --- 1.24/1.14 .85/.90
550 27/196 29/213 32/234 37/267 --- --- --- --- --- 1.23/1.14 .85/.90
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/55 9/57 9/59 9/61 10/63 10/68 11/74 12/82 14/90 1.17/1.10 .90/.93
480 17/117 18/122 19/128 20/134 21/141 23/159 27/182 32/215 40/270 1.23/1.14 .87/.91
520 24/164 25/174 27/187 29/202 32/222 --- -- --- --- 1.23/1.14 .87/.91
550 30/210 34/237 41/284 --- --- --- --- --- --- 1.24/1.14 .83/.89
Figure 10-5. Low Altitude Acceleration - Military Thrust (Sheet 3 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-23
LOW ALTITUDE ACCELERATIONF414-GE-400MILITARY THRUST
GROSS WEIGHT E 46,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 7/54 7/56 8/57 8/59 8/61 9/64 9/69 10/73 11/79 1.17/1.08 .90/.94
480 15/115 16/119 16/124 17/129 18/134 19/146 21/161 24/180 27/204 1.23/1.13 .87/.92
520 21/160 22/168 23/175 24/184 25/194 29/219 33/253 40/306 54/418 1.24/1.14 .83/.88
550 26/198 27/209 29/222 31/237 33/255 40/307 --- --- --- 1.23/1.13 .84/.90
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/56 8/58 8/59 8/61 9/63 9/67 10/72 11/78 12/84 1.17/1.09 .90/.94
480 16/119 17/123 18/128 18/134 19/140 21/154 23/171 26/194 31/226 1.24/1.14 .87/.92
520 22/166 24/174 25/183 26/193 28/205 32/235 37/278 48/359 --- 1.25/1.15 .84/.89
550 28/207 30/220 32/237 34/257 38/283 --- --- --- --- 1.26/1.16 .85/.91
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/58 9/59 9/61 9/63 9/65 10/70 11/76 12/82 13/90 1.17/1.10 .90/.94
480 17/123 18/128 19/134 20/140 21/147 23/163 26/184 30/213 36/256 1.25/1.16 .87/.91
520 24/172 25/182 27/193 29/205 31/220 36/262 46/334 --- --- 1.24/1.14 .85/.90
550 30/216 32/234 36/258 41/293 --- --- --- --- --- 1.24/1.14 .85/.90
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 9/61 9/63 10/65 10/67 11/70 11/75 12/82 14/90 15/100 1.17/1.10 .90/.93
480 19/128 20/134 21/141 22/148 23/156 26/175 30/201 35/238 44/299 1.23/1.14 .87/.91
520 26/180 28/192 30/206 32/223 35/244 --- --- --- --- 1.23/1.14 .87/.91
550 33/232 38/261 --- --- --- --- --- --- --- 1.24/1.14 .86/.91
Figure 10-5. Low Altitude Acceleration - Military Thrust (Sheet 4 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-24
LOW ALTITUDE ACCELERATIONF414-GE-400MILITARY THRUST
GROSS WEIGHT E 50,000 POUNDS
REMARKS
ENGINE(S): (2) F414-GE-400DATE: 29 OCTOBER 1999 U.S. STANDARD DAY, 1962 FUEL GRADE: JP-5DATA BASIS: FLIGHT DERIVED FUEL DENSITY: 6.8 LB/GAL
TIME TO ACCELERATE (SEC) / FUEL TO ACCELERATE (LBS) TEMP. EFFECTFACTORSSPEED
(KIAS)DRAG INDEX
0 25 50 75 100 150 200 250 300 +10°C -10°C
SEA
LEVEL
(15°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 8/59 8/61 8/63 9/64 9/66 9/70 10/75 11/81 12/87 1.17/1.09 .90/.94
480 17/126 17/130 18/135 18/141 19/146 21/160 23/176 26/197 29/224 1.23/1.13 .87/.92
520 23/175 24/183 25/192 26/202 28/213 31/240 36/277 43/335 59/460 1.24/1.14 .82/.88
550 28/216 30/229 31/243 34/259 36/279 43/335 --- --- --- 1.23/1.13 .84/.90
2000FEET
(11°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 9/61 9/63 9/65 9/67 10/69 10/74 11/79 12/85 13/93 1.17/1.09 .90/.94
480 18/130 18/135 19/140 20/146 21/153 23/168 26/187 29/213 34/247 1.24/1.15 .87/.92
520 25/181 26/190 27/200 29/212 30/224 35/257 41/305 53/394 --- 1.25/1.16 .84/.89
550 30/226 32/241 35/259 38/281 41/310 --- --- --- --- 1.26/1.16 .85/.91
4000FEET
(7°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 9/63 9/65 10/67 10/69 10/72 11/77 12/83 13/91 14/99 1.17/1.10 .90/.94
480 19/135 20/140 21/147 22/153 23/161 25/179 29/202 33/233 40/281 1.26/1.16 .87/.91
520 26/188 28/199 29/211 31/225 34/241 40/286 51/367 --- --- 1.24/1.14 .85/.90
550 32/236 35/256 39/282 44/321 --- --- --- --- --- 1.24/1.14 .85/.90
6000FEET
(3°C
)
360 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0 0/0
420 10/66 10/69 11/71 11/74 12/76 12/83 14/90 15/99 17/110 1.17/1.10 .90/.93
480 21/140 22/147 23/154 24/162 25/171 28/192 32/220 38/261 48/329 1.23/1.14 .87/.91
520 29/197 31/210 33/225 35/243 39/267 --- --- --- --- 1.23/1.14 .87/.91
550 36/253 41/283 --- --- --- --- --- --- --- 1.25/1.15 .86/.91
Figure 10-5. Low Altitude Acceleration - Military Thrust (Sheet 5 of 5)
A1-F18EA-NFM-200
ORIGINALXI-10-25
Figure 10-6. Maximum Thrust Acceleration - 10,000 Feet
A1-F18EA-NFM-200
ORIGINALXI-10-26
Figure 10-7. Maximum Thrust Acceleration - 30,000 Feet (Sheet 1 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-27
Figure 10-7. Maximum Thrust Acceleration - 30,000 Feet (Sheet 2 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-28
Figure 10-7. Maximum Thrust Acceleration - 30,000 Feet (Sheet 3 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-29
Figure 10-7. Maximum Thrust Acceleration - 30,000 Feet (Sheet 4 of 4)
A1-F18EA-NFM-200
CHANGE 2XI-10-30
Figure 10-8. Maximum Thrust Acceleration - 35,000 Feet (Sheet 1 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-31
Figure 10-8. Maximum Thrust Acceleration - 35,000 Feet (Sheet 2 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-32
Figure 10-8. Maximum Thrust Acceleration - 35,000 Feet (Sheet 3 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-33
Figure 10-8. Maximum Thrust Acceleration - 35,000 Feet (Sheet 4 of 4)
A1-F18EA-NFM-200
ORIGINALXI-10-34
Figure 10-9. Maximum Thrust Acceleration - 40,000 Feet (Sheet 1 of 2)
A1-F18EA-NFM-200
ORIGINALXI-10-35
Figure 10-9. Maximum Thrust Acceleration - 40,000 Feet (Sheet 2 of 2)
A1-F18EA-NFM-200
ORIGINALXI-10-36
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