Operation of Aircraft

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Attachment D Annex 6 — Operation of Aircraft Serial number Parameter Measurement range Recording interval (seconds) Accuracy limits (sensor input compared to FDR read-out) 19 Pitch trim position Full range 1 ±3% unless higher accuracy uniquely required 20 Radio altitude –6 m to 750 m (–20 ft to 2 500 ft) 1 ±0.6 m (±2 ft) or ±3% whichever is greater below 150 m (500 ft) and ±5% above 150 m (500 ft) 21 Glide path deviation Signal range 1 ±3% 22 Localizer deviation Signal range 1 ±3% 23 Marker beacon passage Discrete 1 24 Master warning Discrete 1 25 NAV 1 and 2 frequency selection (Note 5) 26 DME 1 and 2 distance (Notes 5 and 6) 27 Landing gear squat switch status 28 GPWS (ground proximity warning system) Full range 4 As installed 0 – 370 km 4 As installed Discrete 1 Discrete 1 29 Angle of attack Full range 0.5 As installed 30 Hydraulics, each system (low pressure) 31 Navigation data (latitude/longitude, ground speed and drift angle) (Note 7) 32 Landing gear or gear selector position Discrete 2 As installed 1 As installed Discrete 4 As installed Note.— The preceding 32 parameters satisfy the requirements for a Type I FDR. Notes.— 1. V S o stalling speed or minimum steady flight speed in the landing configuration. 2. V D design diving speed. 3. Record sufficient inputs to determine power. 4. For aeroplanes with conventional control systems ‘‘or’’ applies. For aeroplanes with non-mechanical control systems ‘‘and’’ applies. In aeroplanes with split surfaces, a suitable combination of inputs is acceptable in lieu of recording each surface separately. 5. If signal available in digital form. 6. Recording of latitude and longitude from INS or other navigation system is a preferred alternative. 7. If signals readily available. ATT D-5 1/11/01
Annex 6 — Operation of Aircraft Part I 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 centralized aircraft monitor (ECAM) and engine indication and crew alerting system (EICAS). Use the following order of priority: 1) parameters selected by the flight crew 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; and c) additional engine parameters (EPR, N 1 , EGT, fuel flow, etc.). 1/11/01 ATT D-6
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International Standards and Recomme
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TRANSMITTAL NOTE NEW EDITIONS OF AN
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AMENDMENTS The issue of amendments
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Annex 6 — Operation of Aircraft P
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Annex 6 — Operation of Aircraft C
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INTERNATIONAL STANDARDS AND RECOMME
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Chapter 1 Emergency locator transmi
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Chapter 1 Operator. A person, organ
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CHAPTER 3. GENERAL Note 1.— Altho
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CHAPTER 4. FLIGHT OPERATIONS 4.1 Op
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Chapter 4 a) the type, performance
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Chapter 4 Note.— It is the practi
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Chapter 4 4.4.1.2 An instrument app
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Chapter 4 Note 1.— Guidance on th
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Annex 6 — Operation of Aircraft c
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Annex 6 — Operation of Aircraft -
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CHAPTER 7. AEROPLANE COMMUNICATION
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CHAPTER 8. AEROPLANE MAINTENANCE No
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Page 61 and 62: CHAPTER 9. AEROPLANE FLIGHT CREW 9.
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Page 65 and 66: CHAPTER 10. FLIGHT OPERATIONS OFFIC
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Page 69 and 70: CHAPTER 13. SECURITY* 13.1 Domestic
Page 71 and 72: APPENDIX 1. LIGHTS TO BE DISPLAYED
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Page 77 and 78: APPENDIX 3. ADDITIONAL REQUIREMENTS
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Page 81 and 82: APPENDIX 5. SAFETY OVERSIGHT OF AIR
Page 83 and 84: ATTACHMENT A. FLIGHT TIME AND FLIGH
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Page 87 and 88: Annex 6 — Operation of Aircraft N
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Page 115 and 116: ATTACHMENT F. AIR OPERATOR CERTIFIC
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Page 119 and 120: Attachment F 4.3 Operations and mai
Page 121 and 122: ATTACHMENT H. FLIGHT SAFETY DOCUMEN
Page 123 and 124: ATTACHMENT I. ADDITIONAL GUIDANCE F
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