A O M  3  4  I  0  2  2  I  3  VERTICAL SPEED  THOUSAND FT PER MIN  UP  DOWN  .5  .5  33  30  24  2I  I5  I2  6  3  2 MIN TURN  DC ELEC  L R  30.0  29.9  29.8  I 0 0 F E T I  4  5  6  7  9  2  0  8  3  CALIBRATED  TO 20,000 FEET  ALT  20 20 I0 I0 I0 I0 20 20 TEST  STBY PWR  IN Hg ALg. MANIFOLD  PRESS  25 5 15 30 20 10 35 110  100  90  80  70  60  50  110  100  90  80  70  60  50  E R  %RPM  Supporting pitch Primary pitch and supporting bank Supporting bank Supporting pitch Supporting pitch Primary bank Remains constant Common Errors During Instrument Takeoffs Changing Technology Advances in technology have bro ught about changes in  the instrumentation found in all  types of aircraft, including  helicopters. Electronic displays co mmonly referred to as  “glass cockpits” are becoming more  common. Primary flight  displays (PFDs) and multi-functio n displays (MFDs) are  changing not only what informa tion is available to a pilot  but also how that information is displayed. 1.  Failure to maintain heading  2.  Overcontrolling pedals  3.  Failure to use required power  4.  Failure to adjust pitch attitude as climbing airspeed  is reached  8-18 Illustrations of technological  advancements in instru m entati o n  are described as follows. I n  Figure 8-17, a typ ical PF D  depicts an aircraft flying  straight-and-level at 3,000 feet  and 100 knots.  Figure 8-18  illus trates a nose-low pitch attitude in  a right turn. MFDs can be configured to provide navigation  information, such as the moving map in  Figure 8-19 or  information pertaining to aircraft systems as in  Figure 8-20 . Figure 8-16.  Flight instrument indications during an instrument takeoff.