Title 14

PART 135 APPENDIX D


Appendix D to Part 135 - Airplane Flight Recorder Specification

14:3.0.1.1.11.14.3.1.39 : Appendix D

Appendix D to Part 135 - Airplane Flight Recorder Specification
Parameters Range Accuracy sensor input to DFDR readout Sampling interval (per second) resolution 4 read out
Time (GMT or Frame Counter) (range 0 to 4095, sampled 1 per frame) 24 Hrs ±0.125% Per Hour 0.25 (1 per 4 seconds) 1 sec.
Altitude −1,000 ft to max certificated altitude of aircraft ±100 to ±700 ft (See Table 1, TSO-C51a) 1 5′ to 35′ 1.
Airspeed 50 KIAS to Vso, and Vso to 1.2 VD ±5%, ±3% 1 1kt
Heading 360° ±2° 1 0.5°
Normal Acceleration (Vertical) −3g to + 6g ±1% of max range excluding datum error of ±5% 8 0.01g
Pitch Attitude ±75° ±2° 1 0.5°
Roll Attitude ±180° ±2° 1 0.5°.
Radio Transmitter Keying On-Off (Discrete) 1
Thrust/Power on Each Engine Full range forward ±2% 1 (per engine) 0.2% 2.
Trailing Edge Flap or Cockpit Control Selection Full range or each discrete position ±3° or as pilot's indicator 0.5 0.5% 2.
Leading Edge Flap on or Cockpit Control Selection Full range or each discrete position ±3° or as pilot's indicator 0.5 0.5% 2.
Thrust Reverser Position Stowed, in transit, and reverse (discretion) 1 (per 4 seconds per engine)
Ground Spoiler Position/Speed Brake Selection Full range or each discrete position ±2% unless higher accuracy uniquely required 1 0.22 2.
Marker Beacon Passage Discrete 1
Autopilot Engagement Discrete 1
Longitudinal Acceleration ±1g ±1.5% max range excluding datum error of ±5% 4 0.01g.
Pilot Input And/or Surface Position-Primary Controls (Pitch, Roll, Yaw) 3 Full range ±2° unless higher accuracy uniquely required 1 0.2% 2.
Lateral Acceleration ±1g ±1.5% max range excluding datum error of ±5% 4 0.01g.
Pitch Trim Position Full range ±3% unless higher accuracy uniquely required 1 0.3% 2.
Glideslope Deviation ±400 Microamps ±3% 1 0.3% 2.
Localizer Deviation ±400 Microamps ±3% 1 0.3% 2.
AFCS Mode And Engagement Status Discrete 1
Radio Altitude −20 ft to 2,500 ft ±2 Ft or ±3% whichever is greater below 500 ft and ±5% above 500 ft 1 1 ft + 5% 2 above 500′.
Master Warning Discrete 1
Main Gear Squat Switch Status Discrete 1
Angle of Attack (if recorded directly) As installed As installed 2 0.3% 2.
Outside Air Temperature or Total Air Temperature −50 °C to + 90 °C ±2° c 0.5 0.3° c
Hydraulics, Each System Low Pressure Discrete 0.5 or 0.5% 2.
Groundspeed As installed Most accurate systems installed (IMS equipped aircraft only) 1 0.2% 2.
If additional recording capacity is available, recording of the following parameters is recommended. The parameters are listed in order of significance:
Drift Angle When available. As installed As installed 4
Wind Speed and Direction When available. As installed As installed 4
Latitude and Longitude When available. As installed As installed 4
Brake pressure/Brake pedal position As installed As installed 1
Additional engine parameters:
EPR As installed As installed 1 (per engine)
N 1 As installed As installed 1 (per engine)
N 2 As installed As installed 1 (per engine)
EGT As installed As installed 1 (per engine)
Throttle Lever Position As installed As installed 1 (per engine)
Fuel Flow As installed As installed 1 (per engine)
TCAS:
TA As installed As installed 1
RA As installed As installed 1
Sensitivity level (as selected by crew) As installed As installed 2
GPWS (ground proximity warning system) Discrete 1
Landing gear or gear selector position Discrete 0.25 (1 per 4 seconds)
DME 1 and 2 Distance 0-200 NM; As installed 0.25 1mi.
Nav 1 and 2 Frequency Selection Full range As installed 0.25