时间：2015-01-22 15:18来源：蓝天飞行翻译公司 作者：民航翻译 点击：次
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To view this page ensure that Adobe Flash Player version 9.0.124 or greater is installed. 31* Navigation data (latitude/longitude, ground speed and drift angle) (Note 9) As installed 1 As installed 32* Landing gear and gear selector position Discrete 4 As installed 33* Groundspeed As installed 1 Data should be obtained from the most accurate system 1 kt 34 Brakes (left and right brake pressure, left and right brake pedal position) (Maximum metered brake range, discretes or full range) 1 1±5% 2% of full range 35* Additional engine parameters (EPR, N1, indicated vibration level, N2; EGT, fuel flow, fuel cut-off lever position, N3) As installed Each engine each second As installed 2% of full range 36* TCAQS/ACAS (traffic alert and collision avoidance system) Discretes 1 As installed 37* Windshear warning Discrete 1 As installed 38* Selected barometric setting (pilot, co-pilot) As installed 64 As installed 0.1 mh (0.01 in-Hg) 39* Selected altitude (all pilot selectable modes of operation) As installed 1 As installed Sufficient to determine crew selection 40* Selected speed (all pilot selectable modes of operations) As installed 1 As installed Sufficient to determine crew selection 41* Selected Mach (all pilot selectable modes of operation) As installed 1 As installed Sufficient to determine crew selection 42* Selected vertical speed (all pilot selectable modes of operation) As installed 1 As installed Sufficient to determine crew selection 43* Selected heading (all pilot selectable modes of operation) As installed 1 As installed Sufficient to determine crew selection 44* Selected flight path (all pilot selectable modes of operation) (course/DSTRK, path angle; final approach path (IRNAV/IAN)) 1 As installed 45* Selected Decision Height As installed 64 As installed Sufficient to determine crew selection 46* EFIS display format (pilot, co-pilot) Discrete(s) 4 As installed 47* Multi-function/engine/ alerts display format Discrete(s) 4 As installed 48* AC electrical bus status Discrete(s) 4 As installed 49* DC electrical bus status Discrete(s) 4 As installed 50* Engine bleed valve position Discrete(s) 4 As installed 51* APU bleed valve position Discrete(s) 4 As installed 52* Computer failure Discrete(s) 4 As installed 53* Engine thrust command As installed 2 As installed 54* Engine thrust target As installed 4 As installed 2% of full range 55* Computed centre of gravity As installed 64 As installed 1% of full range 56* Fuel quantity in CG trim tank As installed 64 As installed 1% of full range 57* Head up display in use As installed 4 As installed 58* Para visual display on/off As installed 1 As installed 59* Operational stall protection, stick shaker and pusher activation As installed 1 As installed 60* Primary navigation system reference (GNSS, INS, VOR/DME, MLS, Loran C, localizer glideslope) As installed 4 As installed 61* Ice detection As installed 4 As installed 62* Engine warning each engine vibration As installed 1 As installed 63* Engine warning each engine over temperature As installed 1 As installed 64* Engine warning each engine oil pressure low As installed 1 As installed 65* Engine warning each engine over speed As installed 1 As installed 66* Yaw Trim Surface Position Full range 2 ±3% unless higher accuracy uniquely required 0.3% of full range 67* Roll Trim Surface Position Full range 2 ±3% unless higher accuracy uniquely required 0.3% of full range 68* Yaw or sideslip angle Full range 1 ±5% 0.5% 69* De-icing and/or anti-icing systems selection Descrete(s) 4 70* Hydraulic pressure (each system) Full range 2 ±5% 100 psi 71* Loss of cabin pressure Discrete 1 72* Cockpit trim control input position Pitch Full range 1 ±5% 0.2% of full range or as installed 73* Cockpit trim control input position Roll Full range 1 ±5% 0.2% of full range or as installed 74* Cockpit trim control input position Yaw Full range 1 ±5% 0.2% of full range or as installed 75* All cockpit flight control input forces (control wheel, control column, rudder pedal) Full range (±311 N (±70 lbf), ±378 N (±85 lbf), ±734 N (±165 lbf) 1 ±5% 0.2% of full range or as installed 76* Event marker Discrete 1 77* Date 365 days 64 78* ANP or EPE or EPU As installed 4 As installed Note 1: VSo stalling speed or minimum steady flight speed in the landing configuration. Note 2: VD design diving speed. Note 3: Refer to §7.8.2.2(a)(12) for increased recording requirements. Note 4: Record sufficient inputs to determine power. Note 5: For aeroplanes with control systems in which movement of a control surface will back drive the pilot’s control, ‘‘or’’ applies. For aeroplanes with control systems in which movement of a control surface will not back drive the pilot’s control,‘‘and’’ applies. In aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately. Note 6: Refer to §7.8.2.2(a)(13) for increased recording requirements. Note 7: If signal available in digital form. Note 8: Recording of latitude and longitude from INS or other navigation system is a preferred alternative. Note 9: If signals readily available. If further recording capacity is available, recording of the following additional information should be considered: (a) operational information from electronic display systems, such as electronic flight instrument systems (EFIS), electronic centralised aircraft monitor (ECAM) and engine indication and crew alerting system (EICAS). Use the following order of priority: (1) parameters selected by the flightcrew relating to the desired flight path, e.g. barometric pressure setting, selected altitude, selected airspeed, decision height, and autoflight system engagement and mode indications if not recorded from another source; (2) display system selection/status, e.g. SECTOR, PLAN, ROSE, NAV, WXR, COMPOSITE, COPY, ETC.; (3) warnings and alerts; (4) the identity of displayed pages for emergency procedures and checklists; (b) retardation information including brake application for use in the investigation of landing overruns and rejected take-offs. ICAO Annex I, Part I, Appendix 8, Table A8-1 ICAO Annex I, Part II Section III: Appendix 2.3 Table A2.3 -1 IS: 7.8.2.1(B) FLIGHT DATA RECORDERS—TYPE AND PARAMETERS – HELICOPTERS (a) Flight data records shall be classified as Type IV, Type IVA, and Type V depending upon the number of parameters to be recorded. (1) Type IV FDRs shall be capable of recording, as appropriate to the helicopter, at least the first 30 parameters in Table B below. (2) Type IVA FDRs shall be capable or recording, as appropriate to the helicopter, at least the first 48 parameters in Table B below. (3) Type V FDRs shall be capable of recording, as appropriate to the helicopter, at least the first 15 parameters in Table B below. (4) For all FDR types, if further recording capability is available, recording of the following additional information shall be considered: (5) Additional operational information from electronic displays, such as electronic flight instrument systems (EFIS), electronic centralised aircraft monitor (ECAM) and engine indication and crew alerting system (EICAS); and (6) Additional engine parameters (EPR, N1, fuel flow, etc.). (b) The parameters that satisfy the requirements for a Type IV; Type IVA, and Type V FDRs are listed below. The number of parameters to be recorded shall depend on helicopter complexity. The parameters without an asterisk (*) are mandatory parameters that shall be recorded. The parameters designated by an asterisk (*) shall also be recorded if an information data source for an asterisked parameter is used by helicopter systems or the flightcrew to operate the helicopter. However, other parameters may be substituted with due regard to the helicopter type and the characteristics of the recording equipment. (c) The following parameters satisfy the requirements for flight path and speed: (1) Pressure altitude (2) Indicated airspeed (3) Total or outside air temperature. (4) Heading (primary flightcrew reference) (5) Normal acceleration (6) Lateral acceleration. (7) Longitudinal acceleration (body axis) (8) Time or relative time count (9) Navigation data*: drift angle, wind speed, wind direction, latitude/longitude. (10) Radio altitude* (d) The following parameters satisfy the requirements for attitude: (1) Pitch attitude. (2) Roll attitude. (3) Yaw rate. (e) The following parameters satisfy the requirements for engine power: (1) Power on each engine: free power turbine speed (Nf), engine torque, engine gas generator speed (Ng), cockpit power control position. (2) Rotor: main rotor speed, rotor brake. (3) Main gearbox oil pressure* (4) Gearbox oil temperature*, main gearbox oil temperature, tail rotor gearbox oil temperature (5) Engine exhaust gas temperature (T4)* (6) Turbine inlet temperature (TIT)* (f) The following parameters satisfy the requirements for configuration: (1) Landing gear or gear selector position*. (2) Fuel quality* (3) Ice detector liquid water content* (g) The following parameters satisfy the requirements for operation: (1) Hydraulics low pressure (2) Warnings (3) Primary flight controls —pilot input and/or control output position: collective pitch, longitudinal cyclic pitch, lateral cyclic pitch, tail rotor petal, controllable stabilator, hydraulic selection. |
