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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 14 of 16 

 

 

 

SYSTEM DESCRIPTIONS 

Pilot’s Guide 

 
The Garmin GDL 84/88 Pilot’s Guide, part number and revision listed below, 
contain additional information regarding GDL 84H/88H system description, 
control, and function. Cockpit Reference Guides and Pilot Guides for interfaced 
displays provide additional operating information.  
 

 

GDL 84/88 ADS-B Transceiver Pilot’s Guide 
P/N 190-01122-03 Rev E or later 

 

Mode 3/A Code, IDENT, and Emergency Status 

 
Mode 3/A Code, IDENT, and Emergency Status data that is included in the 
ADS-B OUT message is obtained automatically by the GDL 84H/88H.  No pilot 
action except normal use of the transponder is required. 

Flight ID 

 
Flight Identification will default to the aircraft registration.  If interfaced with a 
Garmin transponder 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 a Radar Altimeter OR GNS or GTN display 
interfaced to the GDL 84H/88H will transmit “in air” any time the height above 
the surface is more than 25 feet or groundspeed is in excess of 15 knots. 

Pressure Altitude Broadcast Inhibit 

 
For rotorcraft with an interfaced Garmin GTX 33/330/32/327 or SL 70 
transponder the broadcast of pressure altitude is controlled by the transponder 
mode.  Turning the transponder to ALT will also broadcast pressure altitude in 
the ADS-B output.  Turning the transponder to ON will inhibit pressure altitude 
from being broadcast. 
 
For rotorcraft without a Garmin GTX 33/330/32/327 or SL 70 transponder 
pressure altitude broadcast is controlled via a separate switch or interfaced GNS 
or GTN display. 
 
 

Summary of Contents for GDL 88H

Page 1: ......

Page 2: ...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 Descr...

Page 3: ...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 Sec...

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 G...

Page 5: ...ffic 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 whi...

Page 6: ...fter 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 compl...

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 w...

Page 8: ...ENT 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 CHE...

Page 9: ...n 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...

Page 10: ...und 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...

Page 11: ...rements 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...

Page 12: ...FT 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 Ter...

Page 13: ...ational 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...

Page 14: ...er 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 st...

Page 15: ...c 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 Th...

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 wil...

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