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Standard

Full-Format Printer

1998-10-01
HISTORICAL
ARP4102/14A
This document recommends criteria for the installation and operation of a printer on the flight deck, to supply the flight crew with hard copies of information that originates from data sources such as FMS, ELS/EDMS, ACMS, CMS, and Data Link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
Standard

FULL-FORMAT PRINTER

1992-01-30
HISTORICAL
ARP4102/14
This document recommends criteria for the installation and operation of a printer on the flight deck, to supply the flight crew with hard copies of information that originates from data sources such as FMS, ELS, ACMS, CMS, and Data Link. These criteria are in addition to the specifications of the referenced ARINC Characteristic 744A.
Standard

TAKEOFF PERFORMANCE MONITOR (TOPM) SYSTEM, AIRPLANE, MINIMUM PERFORMANCE STANDARD FOR

2007-07-11
HISTORICAL
AS8044
This Aerospace Standard (AS), establishes minimum performance standards for those sensors, computers, transponders, and airplane flight deck controls/displays which together comprise a Takeoff Performance Monitor (TOPM) System. This standard also defines functional capabilities, design requirements, and test procedures. A TOPM system is intended to monitor the progress of the takeoff and to provide advisory information which the crew may use in conjunction with other available cues to decide to continue or abort the takeoff. See Appendix A for supplementary information relating to NTSB, CAA, and ad hoc committee concerns and background information.
Standard

Crew Safety Provisions for Cargo Aircraft

2007-07-10
HISTORICAL
ARP4101/9
This document recommends provisions for crew safety and survival which are intended to apply to cargo or combination aircraft and equipment.
Standard

Communications and Navigation Equipment

2022-03-21
CURRENT
ARP4102/6A
This document recommends criteria for the control and display of communications and navigation equipment on the flight deck.
Standard

COMMUNICATIONS AND NAVIGATION EQUIPMENT

2007-07-10
HISTORICAL
ARP4102/6
This document recommends criteria for the control and display of communications and navigation equipment on the flight deck. The equipment includes: a Communications: Ultra High Frequency (UHF), Very High Frequency (VHF), and High Frequency (HF) Radios, Cabin/Service Interphones, Public Address (PA), Select Call (SELCAL), Call Select (CALSEL), Satellite Communications (SATCOM). b Navigation: Very High Frequency Omnidirectional Range (VOR), Tactical Air Navigation (TACAN), Automatic Direction Finder (ADF), Distance Measuring Equipment (DME), Instrument Landing System (ILS), Markers (MKR), Omega, Very Low Frequency (VLF), Inertial Navigation Systems (INS), Inertial Reference Systems (IRS), Satellite Navigation (SATNAV), Low Range Radio Altimeter (LRRA). c Weather Radar d Data Link: Company, Air Traffic Control (ATC) Transponders (Mode-S) and others.
Standard

Pilot Visibility From the Flight Deck

2019-02-28
WIP
ARP4101/2A
This document recommends criteria to assure adequate visibility from the flight deck. The flight deck windshield must provide sufficient external vision to permit the pilot to perform any maneuvers within the operating limits of the aircraft safely and at the same time afford and unobstructed view of the flight instruments and other critical components and displays from the same eye position.
Standard

Pilot Visibility From The Flight Deck

2003-02-25
CURRENT
ARP4101/2
This document recommends criteria to assure adequate visibility from the flight deck. The flight deck windshield must provide sufficient external vision to permit the pilot to perform any maneuvers within the operating limits of the aircraft safely and at the same time afford an unobstructed view of the flight instruments and other critical components and displays from the same eye position.
Standard

Flight Deck Alerting System (FAS)

2007-07-10
CURRENT
ARP4102/4
This document recommends design criteria for the Flight Deck Alerting System. The FAS shall enhance safety of flight by providing early crew recognition of aircraft system or component status or malfunction as well as of crew operational error. The FAS, therefore, relates to aircraft configuration and flight phase as well as the aircraft systems. To fulfill this objective, the FAS must attract the attention of the crew, must state with clarity the nature and location of the problem, and must be highly reliable and thoroughly responsive to the operational requirements and environment. Wherever possible, it should provide guidance as to the corrective action.
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