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时间:2011-02-10 14:53来源:蓝天飞行翻译 作者:admin
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10.5.1 Plane Captain Brief.
1. Connect external power
2. FCS ram air scoop check (manually restow)
3. REFUEL DR check
4. Normal engine starts
5. Alternate engine shutdowns
a. Fuel/air heat exchanger leak check
b. Switching valve checks
c. Crossbleed restarts
6. ECS ram air scoop check
7. Engine runups to check cautions
8. 4 down but only 3 up (launch bar down)
9. Probe light check
10.5.2 Preflight Checks.
1. Exterior Inspection - Perform IAW NATOPS
a. No loose or improperly installed panels.
b. External canopy switch - CHECK
· Canopy opens and closes smoothly.
· Returns to center (hold) position when released.
c. Boarding ladder operation - CHECK
· Ladder electrically deploys.
· Ladder extends, locks, unlocks, and stows correctly.
2. Interior Checks - Perform IAW NATOPS
a. No loose or improperly installed components (both cockpits)
b. Brake accumulator pressure gauge reads 2,600 psi minimum.
c. Canopy and windscreen: No distortion, blemishes, or cracks (both cockpits)
10.5.3 Pre-Start Checks.
1. BATT switch - ON
A1-F18EA-NFM-000
III-10-4 ORIGINAL
2. Battery gauge - CHECK
· Nominal: 23 to 24 vdc
· FCF minimum: 18 vdc
3. ICS - CHECK (F/A-18F)
Apply external electrical power -
4. EXT PWR switch - RESET
5. GND PWR switches 1, 2, 3, and 4 - B ON (hold for 3 seconds)
· Audibly verify avionics cooling fans are on.
6. COMM 1 and 2 knobs - ON/VOLUME AS DESIRED (both cockpits)
7. L(R) DDI, HUD, and MPCD knobs - ON (both cockpits)
a. Display IBIT - PERFORM
· No stuck pushtile indications (small circles).
· Push STOP when complete.
· All displays operative.
· Note DEGD indications if present.
b. All mode (day/night), brightness, and contrast controls for all cockpit displays - CHECK/SET
(both cockpits)
c. Display surfaces - CHECK (both cockpits)
· No burned phosphor spots on HUD or DDIs.
· No lineouts or burned liquid crystals on MPCD, UFCD, or EFD
d. HUD symbology reject - CHECK
(1) Select REJ2
· Heading scale, command heading, heading caret, nav range (if displayed), bank angle, g,
and airspeed and altitude boxes are removed.
(2) Select NORM
e. HUD displayed radar altitude - CHECK
(1) UFCD/RALT - ON
(2) ALT switch - RDR
· HUD displays radar altitude and ²R².
(3) ALT switch - BARO
· HUD displays barometric altitude.
f. AOA indexer brightness - CHECK AND SET
8. LT TEST switch - TEST (both cockpits)
· All warning and caution lights properly illuminate.
· Landing gear warning tone annunciates (front cockpit switch only).
A1-F18EA-NFM-000
III-10-5 ORIGINAL
9. Seat adjustment - CHECK (both cockpits)
· Smooth through full range of travel.
· Do not hold switch against stops (no limit switches).
10. Rudder pedal adjustment - CHECK (both cockpits)
· Smooth through full range of travel.
· Locks securely when RUD PED ADJ lever released.
11. FCC A emergency cooling - CHECK
· Signal: Punch open palm with fist.
a. AV COOL switch - EMERG
· FCS ram air scoop deploys (thumbs up from PC)
b. PC manually restows scoop.
12. REFUEL DR caution - CHECK
· Signal: (refuel cap) twist hand with curled fingers.
· REFUEL DR caution displayed when PC opens door 8R.
· Caution removed when PC closes door 8R.
13. EXT and INTR lights - Check for proper operation to extent possible for ambient conditions (both
cockpits)
14. FIRE warning test
a. FIRE test switch - TEST A (hold until all lights and aural warnings indicate test has been
successfully passed)
b. FIRE test switch - NORM (pause until system resets - 5 to 7 seconds)
c. FIRE test switch - TEST B (hold until all lights and aural warnings indicate test has been
successfully passed)
10.5.4 Engine Start Checks.
APU start -
1. APU ACC caution light - VERIFY OFF
2. APU switch - ON (READY light within 30 seconds)
3. ENG CRANK switch - R
4. Right throttle - IDLE
· RPM 10% minimum
· TEMP 871°C maximum transient
· OIL 10 psi within 30 seconds
5. Battery gauge - VERIFY 28 vdc
· Battery charger failed if £ 24 vdc.
A1-F18EA-NFM-000
III-10-6 ORIGINAL
6. EFD - CHECK
Ground idle -
· RPM 61% minimum
· TEMP 250° to 500°C
· FF 600 to 900 pph
· OIL 35 to 90 psi (warm oil)
· NOZ 77% to 83%
7. External electrical power - DISCONNECT
 
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本文链接地址:NATOPS Flight Manual 飞行手册 1(160)