Technology Briefing Subject: Version 7.1 (ACAS II Version 7.1) Date: December 22, 2015 Distribution: Citation, Beechcraft, and Hawker Operators Revision: 8 Note: Changes since the last version of this document (Rev. 7 July 24, 2015) are highlighted. Definitions Traffic Alert and Collision Avoidance System II An onboard avionics system that alerts crew members via aural and visual display indications to the presence of air traffic in the vicinity that may pose a potential midair collision threat. In addition to Traffic Advisories (TAs), a system also provides Resolution Advisories (RAs). ACAS II Airborne Collision Avoidance System II The ICAO and European designation for. Traffic Advisory (TA) An alert with aural and visual components that notifies the crew of a developing traffic conflict with another aircraft. (e.g., Traffic! Traffic! ) Resolution Advisory (RA) An urgent alert with aural and visual components that includes specific vertical guidance to the flight crew in order to avert an impending collision. (e.g., Traffic! Traffic! Climb! Climb! ) When both aircraft involved in a potential collision situation are equipped with systems, the two systems coordinate to provide complementary guidance to each respective flight crew. (e.g., The TCAS system on one aircraft will issue a climb directive, while the TCAS system on the other aircraft will issue a directive to descend.) Background systems have been in widespread use in airliners and business aircraft since approximately 1990, reliably helping to avert airborne traffic conflicts and midair collision threats. Successive software versions have brought additional enhancements, and up until recently, Version 7.0 software was the latest worldwide standard. However, an airliner near-collision event over Japan in 2001 and an actual airliner collision at approximately FL350 over southern Germany in 2002 have led to sustained efforts to further improve operational procedures as well as to update software to include additional safety enhancements. As a result of these efforts, Version 7.1 software includes the following major improvements: Resolution Advisory (RA) Reversal Capability: The system will now have the capability to issue an RA reversal. This means that if the crew in one of the aircraft involved in a TCAS RA event fails to comply with the RA instruction given (e.g., Traffic! Traffic! Climb! Climb! ) and does the opposite, the TCAS system of the other aircraft can then issue a reversed RA command to avert a collision. Level Off Callout: The system will now issue a Level Off! Level Off! callout in lieu of the former Adjust Vertical Speed Adjust (AVSA) callout. The AVSA callout is intended to prevent a collision when an aircraft climbs or descends at a rate that potentially puts it in conflict with another aircraft. But the AVSA callout is somewhat ambiguous in that it doesn t aurally instruct pilots whether to increase or decrease vertical speed. They must reference their flight displays to determine how to adjust, and crews sometimes have made the mistake of impulsively adjusting vertical speed in the wrong direction. The Level Off callout is more straightforward and eliminates this ambiguity. Page 1 of 8
Key Benefits for Business Aircraft Operators Improved operational safety Continued access to airspace regions that will require aircraft equipped with (or ACAS II) systems to have Version 7.1 software in order to continue operating in those regions Equipment Requirements Upgrading an existing system to the Version 7.1 level is typically a software change only. However, it may be necessary to ship a unit to the supplier to be upgraded or exchanged for an already upgraded unit. Regulatory Status Europe o In December 2011, the European Commission published Implementing Rule 1332/2011, which established the following requirements: Forward-Fit: All aircraft with an individual certificate of airworthiness issued as of 1 March 2012 and having a Maximum Takeoff Mass (MTOM) greater than 5,700 kg (12,500 lb) or a maximum passenger seating capacity of more than 19 are required to be equipped with ACAS II Version 7.1 ( Version 7.1) in order to operate in European airspace. Retrofit: All aircraft with an individual certificate of airworthiness issued prior to 1 March 2012 and having a MTOM greater than 5,700 kg (12,500 lb) or a maximum passenger seating capacity of more than 19 are required to be equipped with ACAS II Version 7.1 ( Version 7.1) as of 1 December 2015 in order to operate in European airspace. Note: Operators who have voluntarily equipped their aircraft with a system (i.e., even if not required by operating rule) are also required to have Version 7.1 software by the applicable deadlines in order to operate in European airspace. United States o There is currently no published deadline for upgrading systems with Version 7.1 software for operation in the United States. Operation in RVSM airspace currently requires -equipped aircraft to have Version 7.0 software or later. Other Regions o ICAO Annex 10 standards specify that systems should have Version 7.1 software on new aircraft as of 1 January 2014 (forward-fit) and on existing aircraft as of 1 January 2017 (retrofit). o Business aircraft operators who fly internationally need to be aware of the current status of any requirements for Version 7.1 in the regions they intend to operate. Compliance Status of Citation, Beechcraft, and Hawker Aircraft Cessna, Beechcraft, and Hawker have offered three primary systems in the past: the (CAS-67) system from, the TCAS system from ACSS, and the TCAS- and TCAS-94 systems from Rockwell-Collins. In addition, Cessna now offers Garmin s GTS system for new G3000 and G5000 aircraft in production. The following tables beginning on page 3 show status and timing for availability of the upgrade to Version 7.1 for the applicable aircraft models. Links FAA Introduction to Version 7.1 FAA Information for Operators (InFO) 12010 - Version 7.1 European Commission Version 7.1 Implementing Rule Contact: For further information, contact your Citation, Beechcraft, or Hawker Sales or Customer Service Representative. Page 2 of 8
Table 1: Compliance Status of Citation Aircraft Models Currently In Production Name Model (Serial Range) Avionics TCAS System Mustang 510 (1 and on) Garmin G1000 M2 525 (800 and on) Garmin G3000 CJ3+ 525B (451 and on) Garmin G3000 CJ4 525C (1 and on) XLS+ 560XL (6001 and on) Latitude 680A (1 and on) Garmin G5000 Sovereign+ 680 (501 and on) Garmin G5000 Citation X+ 750 (501 and on) Garmin G5000 Collins TCAS- Collins TCAS- Service Bulletin/STC Availability for Version 7.1 (Estimated) Service Bulletin Number A couple of Mustangs have had a TCAS system installed in production. This option on the Mustang platform has always had Version 7.1 software. Version 7.1 software included with the GTS factory option since entry into service Version 7.1 software included with the standard GTS system since entry into service SB525C-34-05 Version 7.1 software incorporated in production with the standard TCAS- system on unit - 0073 as well as units -0078 and on SB560XL-34-73 Version 7.1 software incorporated in production with the standard TCAS- system on unit -6100 as well as units -6102 and on Version 7.1 software to be included with the standard GTS system at entry into service Version 7.1 software included with the standard GTS system since entry into service Version 7.1 software included with the standard GTS system since entry into service Page 3 of 8
Models No Longer In Production Name Model (Serial Range) Avionics TCAS System CitationJet 525 (1-359) SPZ- CJ1 525 (360-558) line 21 CJ1+ 525 (600-701) CJ2 525A (1-245) Collins TCAS- CJ2+ 525A (300-492) Collins TCAS- CJ3 525B (1-374, 377) Collins TCAS- Citation II/SP 550 (2-733) Elec/Mech or EDZ-605 (627-733) Citation SII S550 (1-160) Elec/Mech Bravo 550 (801-1136) P1000 Citation V 560 (1-259) EDZ-605 Ultra 560 (260-537) P1000 Encore 560 (539-707) P1000 Encore+ 560 (751-815) Collins TCAS- Service Bulletin/STC Availability for Version 7.1 (Estimated) Service Bulletin Number SB525-34-87 Only a couple of CitationJet aircraft had a system installed. Cessna is not planning a service bulletin for Version 7.1 for this platform. Only a couple of CJ1 aircraft had a system installed. Cessna is not planning a service bulletin for Version 7.1 for this platform. SB525A-34-40 Only a few CJ2 aircraft had a system installed. Cessna is planning a service bulletin for Version 7.1 for this platform. SB525A-34-38 Version 7.1 software included with the TCAS- factory option as of unit -0493 and on SB525B-34-21 Version 7.1 software incorporated in production on units -0375 & -0376 as well as units -0378 and on SB550-34-118 SB550-34-40 SB550-34-118 SB560-34-162 SB560-34-162 SB560-34-162 SB560-34-161 The service bulletin was completed in December 2014 and mailed in January 2015. Page 4 of 8
Excel 560 (5001-5372) P1000 XLS 560 (5501-5830) P1000 Citation III 650 (1-199, 203-206) Elec/Mech or SPZ- Citation VI 650 (200-202, 207-241) EDZ-605 Citation VII 650 (7001-7119) SPZ- Sovereign 680 (1-349) Primus EPIC Citation X 750 (1-313) P SB560XL-34-75 SB560XL-34-72 Rev 1 SB560XL-34-75 SB560XL-34-72 Rev 1 SB650-34-115 SB650-34-115 SB650-34-115 SB680-34-32 SB680-34-30 Rev 1 SB750-34-61 SB750-34-54 Rev 1 Upgrading to version 7.1 also addresses AD 2012-02-08, which is required by March 13, 2015. Upgrading to version 7.1 also addresses AD 2012-02-08, which is required by March 13, 2015. Upgrading to version 7.1 also addresses AD 2012-02-08, which is required by March 13, 2015. Upgrading to version 7.1 also addresses AD 2012-02-08, which is required by March 13, 2015. Page 5 of 8
Table 2: Compliance Status of Beech Aircraft Models Currently In Production Name Model (Serial Range) Avionics TCAS System Availability of Version 7.1 For New Aircraft King Air 250 King Air 350i King Air 350iER King Air 350iC King Air 350iCER B200GT (BY-117, BY- 119 and on) B300 (Various from FL-672 and on) B300 (Various from FL-424 thru FL-888) B300C (Various from FM-1 and on) B300C (Various from FM-14 thru FM-55) (FM- 12 and on) production as of S/N BY-144 production as of S/N FL-798 production as of S/N FL-798 production as of S/N FM-53 production as of S/N FM-53 Service Bulletin/STC Availability TTR-. TTR-. TTR-. TTR-. TTR-. Models No Longer In Production Name Model (Serial Range) Avionics TCAS System Service Bulletin/STC Availability (Estimated) King Air B200 King Air B200C King Air B200GT King Air 350 B200 (Various from BB-734 thru BB-2019) B200C (Various from BL-37 thru BL-171) B200GT (BY-1 thru BY-116, BY-118) B300 (Various from FL-1 thru FL-683) (BB- 1769, BB- 1834, BB- 1843 and on) (BL- 148 and on) (FL- 381, FL-383 and on) 921 or TTR-. 921 or TTR-. 921 or TTR-. 921 or TTR-. Page 6 of 8
Airliner 1900D 1900D (UE-1 thru UE- 439) - Line 2 Premier 1 390 (RB-2 thru RB-101, RB-103 thru RB-134) Premier 1A 390 (RB-102, RB-135 thru RB-295) Beechjet 400A 400A (RK-1 thru RK-353) - Line IV 94 or TCAS- (STC ST00881WI-D) 921 or TTR-. 921 or TTR-. 921 or TTR-. 921 or TTR-. (SB 34-3432 upgrades existing TTR-920 to TTR-) Notes: 1. The above schedule estimates are provided for informational purposes and are based on the best available information as of the date shown at the beginning of this briefing. Schedules are subject to change. 2. Beechcraft does not have specific plans for other out-of-production models not shown in the table above. We will evaluate potential solutions for such models as we are able. It may be impractical for Beechcraft to develop systems with Version 7.1 software solutions for some models. Page 7 of 8
Table 3: Compliance Status of Hawker Aircraft Models No Longer In Production Name Model (Serial Range) Avionics TCAS System Service Bulletin/STC Availability (Estimated) Hawker 400XP 400A (RK-354 thru RK- -Line IV 604) (STC ST00881WI-D) Hawker 750 750 (HB-1 thru HB-74) Hawker 800XP Hawker 800XP Hawker 800XPi Hawker 850XP Hawker 900XP 800XP (Various from 258266 thru 258566) 800XP (Various from 258541 thru 258722) 800XP (Various from 258699 thru 258847) 850XP (Various from 258750 thru 258984) 900XP (HA-0001 thru HA-0213) Various avionics platforms (mainly SPZ-) Hawker (RC-7 thru RC-76) Primus EPIC or 94 (STC ST02406LA or ST00881WI-D) Note: Incorporated in production on HA-0208 and on (SB 34-4109) equipped with TTR-921 or TTR-. ST02406LA: Version 7.1 upgrade for aircraft equipped with. Upgrading to version 7.1 also addresses AD 2012-02-08, which is required by March 13, 2015. ST00881WI-D: Version 7.1 upgrade for aircraft equipped with Collins TTR-921 or TTR-. MANDATORY SB provides upgrade to Version 7.1 and also addresses AD 2012-02- 08, which is required by March 13, 2015. Notes: 1. The above schedule estimates are provided for informational purposes and are based on the best available information as of the date shown at the beginning of this briefing. Schedules are subject to change. 2. Beechcraft s support of Hawker aircraft does not currently include specific plans for other out-of-production Hawker models not shown in the table above. We will evaluate potential solutions for such models as we are able. It may be impractical for Beechcraft to develop TCAS II systems with Version 7.1 software solutions for some Hawker models. Page 8 of 8