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(1) DELETE THIRD PARAGRAPH.
(2) ADD:
THE F-14 MUST BE FLOWN OFF THE CATAPULT BY THE PILOT. AT
SHUTTLE RELEASE, THE ENERGY STORED IN THE NOSE STRUT IS
RELEASED, ROTATING THE AIRCRAFT TO THE INITIAL FLYAWAY
ATTITIDE OF APPROXIMATELY 12-15 DEGREES NOSE-UP ON THE VDI
AND HUD. THE AIRCREW SHOULD PLAN FOR THE STANDARD EXCESS
ENDSPEED OF 15 KNOTS, UNLESS NOTIFIED OTHERWISE. LOWER
EXCESS ENDSPEED THAN ANTICIPATED OR A LOWER PITCH TRIM
SETTING THAN RECOMMENDED WILL REQUIRE THE PILOT TO USE
BACKSTICK AT THE END OF THE CATAPULT STROKE TO CAPTURE AND
MAINTAIN THE DESIRED CLIMBOUT PITCH ATTITUDE OF 10 DEGREES.
HIGHER ENDSPEED THAN EXPECTED OR A HIGHER PITCH TRIM SETTING
THAN RECOMMENDED WILL REQUIRE THE PILOT TO STOP THE ROTATION
AT 10 DEGREES WITH SLIGHT FORWARD STICK. WHILE ROTATING TO
THE FLYAWAY ATTITUDE, THE FLIGHTCREW WILL FEEL THE AIRCRAFT
SETTLE APPROXIMATELY 5 FEET BEFORE COMMENCING A CLIMB. FOR
CATAPULT LAUNCHES WITH EXCESS ENDSPEED LESS THAN 15 KNOTS,
THE AOA WILL RISE ABRUPTLY TO 17 UNITS AND THEN GRADUALLY
DECREASE AS AIRSPEED INCREASES DURING THE FLYAWAY.
AIRCREW COORDINATION IS PARTICULARLY CRITICAL IN THIS
REGIME, SINCE THE AIRCREW MUST ENSURE THAT INITIAL FLYAWAY
PARAMETERS ARE MAINTAINED WHILE REMAINING ALERT FOR ANY
ABNORMAL LAUNCH CHARACTERISTICS AND ENGINE MALFUNCTIONS.
HIGH ENDSPEED AND/OR SINGLE-ENGINE FLYAWAY WITH TRIM
SETTINGS ABOVE 2 DEGREES MAY REQUIRE SIGNIFICANT FORWARD
STICK PRESSURE. IN ALL CONFIGURATIONS, THE USE OF
AFTERBURNER AND/OR LEVEL RAPID ACCELERATION WILL REQUIRE
REDUCED NOSE TRIM SETTINGS. THE RIO SHALL SCAN AIRSPEED,
ALTITUDE AND ATTITUDE TO CONFIRM A POSITIVE RATE OF CLIMB.
THE AVIA DISPLAY MAY BE USED TO PROVIDE ADDITIONAL
INFORMATION (AOA AND POSITIVE RATE OF CLIMB) DURING THE
INITIAL FLYAWAY, THOUGH, THE VSI AND AOA INFORMATION
DISPLAYED ON THE AVIA IS PARTICULARLY SUSCEPTIBLE TO LAG AND
INACCURACIES, AND SHOULD BE USED ONLY AS A SECONDARY SOURCE
OF INFORMATION. THE RIO'S PRIMARY SCAN SHOULD BE AIRSPEED,
ALTITUDE AND ATTITUDE FROM THE CONVENTIONAL INSTRUMENTS.
ADDITIONAL CONSIDERATIONS EXIST FOR NIGHT/IFR CATAPULT
LAUNCHES. AIRCRAFT ACCELERATION AND THE LACK OF EXTERNAL
VISUAL CUES WILL CAUSE THE AIRCREW TO SENSE THAT THE NOSE IS
HIGHER THAN ACTUAL AND CAN RESULT IN SPATIAL DISORIENTATION.
UNDER THESE CONDITIONS A VIGILANT INSTRUMENT SCAN IS REQUIRED
TO ENSURE THAT THE PROPER ATTITUDE IS MAINTAINED THROUGHOUT
THE LAUNCH AND SUBSEQUENT CLIMBOUT. THE AIRCREW SHOULD ALSO
BE ALERT FOR POWER TRANSIENTS, WHICH CAN TEMPORARILY DISABLE
THE PILOT'S PRIMARY ATTITUDE DISPLAY (VDI) DURING AND AFTER
THE CATAPULT STROKE, AND REQUIRE TRANSITION TO THE STANDBY
GYRO FOR ATTITUDE INFORMATION.
5. CHANGE REF C (F-14D NFM), CHAPTER 8, PAGE 8-4, PARA 8.4.2,
CATAPULT LAUNCH:
A. DELETE THIRD (LAST) PARAGRAPH.
B. ADD:
THE F-14 MUST BE FLOWN OFF THE CATAPULT BY THE PILOT. AT
_____________________________________________________________________________
CNO 300001Z MAR00 Page 4 of 4 NA 01-F14AAA-1 IC 143
NA 01-F14AAP-1 IC 41
NA 01-F14AAD-1 IC 21
SHUTTLE RELEASE, THE ENERGY STORED IN THE NOSE STRUT IS RELEASED,
ROTATING THE AIRCRAFT TO THE INITIAL FLYAWAY ATTITIDE OF
APPROXIMATELY 12-15 DEGREES NOSE-UP ON THE VDI AND HUD. THE
AIRCREW SHOULD PLAN FOR THE STANDARD EXCESS ENDSPEED OF 15 KNOTS,
UNLESS NOTIFIED OTHERWISE. LOWER EXCESS ENDSPEED THAN
ANTICIPATED OR A LOWER PITCH TRIM SETTING THAN RECOMMENDED WILL
REQUIRE THE PILOT TO USE BACKSTICK AT THE END OF THE CATAPULT
STROKE TO CAPTURE AND MAINTAIN THE DESIRED CLIMBOUT PITCH
ATTITUDE OF 10 DEGREES. HIGHER ENDSPEED THAN EXPECTED OR A
HIGHER PITCH TRIM SETTING THAN RECOMMENDED WILL REQUIRE THE PILOT
TO STOP THE ROTATION AT 10 DEGREES WITH SLIGHT FORWARD STICK.
WHILE ROTATING TO THE FLYAWAY ATTITUDE, THE FLIGHTCREW WILL FEEL
THE AIRCRAFT SETTLE APPROXIMATELY 5 FEET BEFORE COMMENCING A
CLIMB. FOR CATAPULT LAUNCHES WITH EXCESS ENDSPEED LESS THAN 15
KNOTS, THE AOA WILL RISE ABRUPTLY TO 17 UNITS AND THEN GRADUALLY
DECREASE AS AIRSPEED INCREASES DURING THE FLYAWAY.
AIRCREW COORDINATION IS PARTICULARLY CRITICAL IN THIS REGIME,
SINCE THE AIRCREW MUST ENSURE THAT INITIAL FLYAWAY PARAMETERS ARE
MAINTAINED WHILE REMAINING ALERT FOR ANY ABNORMAL LAUNCH
CHARACTERISTICS AND ENGINE MALFUNCTIONS. HIGH ENDSPEED AND/OR
SINGLE-ENGINE FLYAWAY WITH TRIM SETTINGS ABOVE 2 DEGREES MAY
REQUIRE SIGNIFICANT FORWARD STICK PRESSURE. IN ALL
CONFIGURATIONS, THE USE OF AFTERBURNER AND/OR LEVEL RAPID
ACCELERATION WILL REQUIRE REDUCED NOSE TRIM SETTINGS. THE RIO
SHALL SCAN A REPEAT OF THE PILOT'S HEADS UP DISPLAY AND
ASSOCIATED STANDBY FLIGHT INSTRUMENTS TO ENSURE THE CORRECT
　
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