Instruction Manual

G1000 / GFC 700 System Maintenance Manual - 200/B200 Series King Air Page 7-57
190-00915-01 Revision 8
7.24.3 Safe Flight Lift Computer Flight Calibration
NOTE
This procedure is required only for aircraft with the optional Electronic Stability
and Protection (ESP) feature.
1. Disable the STABILITY & PROTECTION item via the MFD AUX – SYSTEM SETUP 2 page.
Verify that the message “ESP OFF” is present.
2. Perform the “Flight Test and Calibration” procedure in accordance with the King Air 200 Series
Maintenance Manual, listed in Table 1-2, Section 27-31-00.
3. If the stall warning points for the new lift computer were set to match the lift computer that was
removed, adjustments to the new lift computer may not be necessary in flight. If the stall warning
points are adjusted in flight, verify the LAA output per Section 7.24.2.
4. Enable the STABILITY & PROTECTION item via the MFD AUX – SYSTEM SETUP 2 page.
Verify that the message “ESP OFF” is not present.
7.25 ESP Functional Check
NOTE
This procedure is required only for aircraft with the optional Electronic Stability
and Protection (ESP) feature.
1. Apply power to the aircraft and avionics systems by placing the aircraft AVIONICS MASTER
PWR and BATT switches to ON. Ensure G1000 system and components are powered and
operating normally.
2. Verify the DISPLAY BACKUP button on the audio panel is pushed in so that the GDUs will not
operate in reversionary mode.
3. Verify no AHRS, ADC, Autopilot, PFD, AFCS Mode Controller, GCU alert messages or monitor
flags (HDG MISCOMP etc) are present on PFD1 or PFD2.
4. On initial power up verify that the MFD splash screen includes a graphic similar to the following: