TruTrak Automatic Pitch Trim User Manual
Page 2
IT IS THE INSTALLERS RESPONSIBILITY TO ENSURE
THAT THE TRIM SYSTEM DOES NOT EXCEED THE
ABILITY OF THE PILOT TO CONTROL THE AIRCRAFT AT
ANY SPEED WITH THE TRIM TAB AT FULL DEFLECTION
IN EITHER POSITION.
IF UNABLE TO MAINTAIN FLIGHT CONTROL WITH THE
TRIM TABS AT FULL DEFLECTION THEN STOPS WILL BE
NEEDED IN THE AIRCRAFT TRIM SYSTEM.
See also other documents in the category TruTrak Air equipment:
- ADI (16 pages)
- ADI Pilot I (28 pages)
- AFS Pilot (16 pages)
- Altrak Mounting (1 page)
- Altrak VS (16 pages)
- AP I (2 pages)
- AP II (2 pages)
- AP III (2 pages)
- AP IV (2 pages)
- DFC Install Manual (16 pages)
- DFC Operating Manual (17 pages)
- Digiflight II Instal Manual (24 pages)
- Digiflight II Operating Manual (16 pages)
- Digiflight Install Manual (19 pages)
- Digiflight Operation Manual (15 pages)
- Digitrak Install and User Guide (20 pages)
- Digitrak Ref (2 pages)
- EFIS AP (8300-057C) (36 pages)
- EFIS (8300-056) (24 pages)
- EFIS Pilot’s Guide (2 pages)
- EMS BU (8300-065) (32 pages)
- Gemini ADI (20 pages)
- Gemini PFD (26 pages)
- GPS Configuration (6 pages)
- GX Pilot (16 pages)
- KRT2 Comm Radio IR (36 pages)
- Pictorial Pilot (20 pages)
- Sorcerer (20 pages)
- Sorcerer – Outdated (20 pages)
- Sorcerer RV10 AP100 (24 pages)
- TS-83 Rev C (20 pages)
- Vizion 380-385 Install manual (20 pages)
- Vizion 380-385 Operation Manual (48 pages)
- Yaw Damper (12 pages)