background image

Garmin International  
1200 E. 151

st

 Street Olathe, KS 66062 

USA 

ROTORCRAFT FLIGHT MANUAL SUPPLEMENT  

for STC SR02123SE

 

 

GARMIN GDL 84H/88H ADS-B TRANSCEIVER 

 

 

190-01310-J2 Rev. 1 

Page 15 of 16 

 

Traffic Sources and Alerting 

 
The GDL 84H/88H is capable of receiving ADS-B, ADS-R, and TIS-B traffic 
reports in order to track traffic around the rotorcraft and provide alerts to the 
flight crew to aid in visual acquisition and avoidance.  
 
Traffic alerting is provided via a visual annunciator and audio callouts for these 
alerts.  
 
Rotorcraft which have a Radar Altimeter OR GNS or GTN display interfaced to 
the GDL 84H/88H will truncate traffic aural alerts to not include bearing, 
distance, and relative altitude information when less than 200 ft above the 
surface.  Additionally, the GDL 84H/88H will reduce the protected volume 
around these rotorcraft when operating below 200 ft above the surface and less 
than 60 kts groundspeed to minimize nuisance alerts in the airport area while 
still providing traffic alerts on other eligible ADS-B OUT equipped aircraft. 
 
Aircraft which are ADS-B participants transmitting on the 1090 MHz band do 
not transmit altitude while in the on ground state and thus will not generate 
traffic alerts until becoming airborne. 
 
Due to some aircraft not being required to equip for ADS-B Out, as well as the 
nature of TIS-B, its service volumes, not all traffic will be tracked by the GDL 
84H/88H.  This is much like an active traffic system which does not track non-
transponder equipped aircraft.  The flight crew must use “see and avoid” 
procedures to visually acquire and avoid other aircraft. 

On Scene Mode (OSM)  

 
Rotorcraft which have a GTN display interfaced to the GDL 88H have the 
ability to use On Scene Mode (OSM).  OSM reduces the protected volume 
around the rotorcraft for alerts that would be produced by other ADS-B 
equipped helicopters.  OSM must turned ON and OFF by the pilot using the 
controls in the MENU of the GTN’s traffic page and is intended to be used when 
intentionally operating in close proximity to other helicopters for activities such 
as ENG.  OSM does not affect the protected volume for other airplanes or non-
ADS-B equipped helicopters. 
 

Interfaced Active Traffic System (Optional, GDL 88H Only with GTN) 

 
When an active traffic system is interfaced with a GDL 88H, the GDL 88H 
receives traffic from the active traffic system and attempts to correlate – or 
match – this traffic with ADS-B traffic the GDL 88H has received and is already 
tracking.  When a correlation is made, the active traffic system or ADS-B target 
with the most accurate information is displayed to the flight crew. Any active 

Summary of Contents for GDL 84H

Page 1: ......

Page 2: ...t Olathe KS 66062 USA ROTORCRAFT FLIGHT MANUAL SUPPLEMENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 2 of 17 FAA APPROVED LOG OF REVISIONS Revision Number Date Description 1 07 29 2015 Complete Supplement ...

Page 3: ...L AURAL TRAFFIC ALERT 6 Section 3 EMERGENCY PROCEDURES 6 3 1 Emergency Procedures 6 Section 4 MALFUNCTION PROCEDURES 6 4 1 Malfunction Indications 6 Section 5 PERFORMANCE DATA 7 MANUFACTURER S DATA Section 6 WEIGHT AND BALANCE DATA 8 Section 7 PILOT CHECKLIST 8 Section 8 FUEL AND OIL DATA 8 Section 9 CHARTS AND TABLES 8 GENERAL 9 Garmin GDL 84H 88H UAT Transceiver 9 Capabilities 11 Installation Co...

Page 4: ... following system interfaces fully functional in order to be compliant with the requirements for 14 CFR 91 227 ADS B Out operations Interfaced Equipment Number Installed Number Required GPS Navigator GTN or GNS 1 or more 1 Transponder 1 or more 1 Barometric altitude source 1 or more 1 Table 2 Required Equipment 1 2 ADS B Out The GDL 84H 88H only complies with 14 CFR 91 227 for ADS B Out when all r...

Page 5: ...affic Control 1 6 Traffic Alerting Traffic alerting is an aid to visual acquisition and may not be used as the sole basis for rotorcraft maneuvering 1 7 Rotorcraft with No Heading Source Rotorcraft which do not have a heading source interfaced to the GDL 88H are subject to the following limitations The traffic page is oriented to rotorcraft TRACK which may or may not align with rotorcraft heading ...

Page 6: ...after power up if a fault was present during the previous power cycle This indicates the unit requires service but does not indicate that the unit will not comply with 91 227 The GDL 84H 88H only complies with 14 CFR 91 227 for ADS B Out when all required functions are operational as indicated when the ADS B annunciator is not illuminated 2 2 Before Takeoff GDL 84H 88H Annunciations CONSIDERED TRA...

Page 7: ... external ADS B annunciator panel if installed ADS B annunciator illuminated Transponder VERIFY ON ADS B Circuit Breaker VERIFY CLOSED When the GDL 84H detects a FAULT that does not affect compliance with requirements of 91 227 this will be annunciated to flight crew at the beginning of the next power cycle by flashing the ADS B annunciator on off for approximately 20 seconds after power up Contac...

Page 8: ...MENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 8 of 16 MANUFACTURER S DATA Section 6 WEIGHT AND BALANCE DATA See current weight and balance data Section 7 PILOT CHECKLIST No change Section 8 FUEL AND OIL DATA No change Section 9 CHARTS AND TABLES No change ...

Page 9: ...on Legend Collective Switch Radio Altitude OR ADS B Annunciator Altitude Reporting Switch self interrogation only Bottom UAT Antenna Traffic Mute Switch Optional Altitude Source Transponder GPS Antenna ADS B Annunciator Optional Altitude Reporting On Off Switch self interrogation only Anonymous Mode Switch Optional Audio Panel TRAFFIC Annunciator Traffic Alerting Optional Traffic Aurals On Off Swi...

Page 10: ...ound station o TIS B Broadcast of secondary surveillance radar SSR derived traffic information from a ground station o FIS B Broadcast of aviation data from a ground station Reception of ADS B In data on 1090 MHz o ADS B Data directly from another transmitting aircraft o ADS R Rebroadcast of ADS B data from a ground station Provide ADS B OUT status via an ADS B annunciator lamp GDL 84H Only Provid...

Page 11: ...irements of 14 CFR 91 227 The GDL 88H meets the requirements of TSO C195a Class C1 C2 C3 C5 TIS B Services TSO C166b Class A1 and FIS B TSO C157a for ADS B In Operation and AC 20 172A for Airworthiness Approval for ADS B In Systems and Applications Installation Configuration This rotorcraft is equipped with a GDL 84H 88H system with the following interfaces features appropriate boxes will be check...

Page 12: ...AFT FLIGHT MANUAL SUPPLEMENT for STC SR02123SE GARMIN GDL 84H 88H ADS B TRANSCEIVER 190 01310 J2 Rev 1 Page 12 of 16 Anonymous Mode Not Available External Switch Controlled via display Height Above Terrain Airport Data Source Not Available Radar Altimeter GPS Navigator ...

Page 13: ...uational Awareness ENG Electronic News Gathering FIS B Flight Information Service Broadcast GDL Garmin Datalink GPS Global Positioning System GTN Garmin Touchscreen Navigator LRU Line Replaceable Unit PABI Pressure Altitude Broadcast Inhibit SBAS Satellite Based Augmentation System TCAS Traffic Collision Avoidance System In this document this term is used to refer to TCAS I TAS and TCAD systems TI...

Page 14: ...der or GTN an alternate Flight ID can be entered via those interfaces and will automatically be updated at the GDL 84H 88H Transmitted Air Ground Status The ADS B OUT message includes the air ground status of the rotorcraft Rotorcraft which do not have a Radar Altimeter OR GNS or GTN display interfaced to the GDL 84H 88H will transmit in air any time the collective is raised Rotorcraft which have ...

Page 15: ...ic alerts until becoming airborne Due to some aircraft not being required to equip for ADS B Out as well as the nature of TIS B its service volumes not all traffic will be tracked by the GDL 84H 88H This is much like an active traffic system which does not track non transponder equipped aircraft The flight crew must use see and avoid procedures to visually acquire and avoid other aircraft On Scene...

Page 16: ... system traffic alerts are provided as follows Alerts will be provided by the TCAS system for targets tracked solely via TCAS AND targets that tracked via TCAS and ADS B which are correlated Alerts will be provided by the GDL 84H 88H for targets that are tracked solely by ADS B The optional interfaced display s Pilot s Guides and supplements provide additional information regarding the functionali...

Reviews: