RECENT PROJECTS

Main companies expertise is development of unique modification and upgrade solutions for commercial and business aviation. This includes concept definition, engineering design and substantiation, on-field engineering support during integration, followed by EASA certification. Necessary local CAA validations can be also provided, if necessary and requested by the customer.

With our Expert Team, all highly experienced aviation experts, ALAMO Engineering flexibly involves necessary experts, whole Design, Production and Maintenance approved organizations for affordable, fast and successful project completion.

ALAMO Engineering offers complete integration solution including:

  • On-field engineering support during installation, configurations and ground and flight tests
  • System upgrade proposal and definition
  • Delivery of all Hardware and Installation Kits
  • Complete engineering design
  • Corresponding EASA certification
  • Engineering after-sale support during aircraft commercial operation
DescriptionThe installation covers installation of new Satcom Direct Plane Simple Ku-Band SATCOM system, consisting of a Satcom Direct Modem Unit (SMU), installed in the AFT equipment bay LH side on Equipment Rack, and a KU-Band Advanced Tail Mounted Antenna (ATMA), installed on the top of vertical stabilizer. New LHT TIOS+ SATCOM Radome/Installation Kit/STC 10060445 is concurrent requirement for this upgrade.
TC HolderBoeing
TypeB737
ModelA16WE
Variant-700/-800
ApprovalEASA 10083889
DescriptionThe installation covers the upgrade of the existing satellite communication system by a Satcom Direct Plane Simple KU-Band SATCOM system, consisting of a Satcom Direct Modem Unit (SMU), installed in the AFT equipment bay LH side, and a KU-Band Advanced Tail Mounted Antenna (ATMA), installed on existing antenna frame assembly on the vertical stabilizer. Existing SATCOM Radome is reused. If the obsolete AMT-50 Antenna system is installed, it shall be removed and replaced on its position by ATMA. If AMT-700 antenna system is installed, it remains. Dual Antenna system installation (AMT-700 and ATMA) is covered.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
BD-700-1A11
VariantGlobal Express
Global Express XRS
Global 5000 (classic & GVFD)
Global 6000
ApprovalEASA 10078957
ValidationsFAA ST00167IB
DescriptionRemoval of originally installed, obsolete parts:

  • CTU Aerocom 3000,
  • ICS-100/-200 Iridium/Voice,
  • wireless DECT Handsets, Cradle, Base Station

installation of all new equipment and parts:

  • SDR Gateway, 2ch Iridium/Voice,
  • WiFi/4G cabin antennas,
  • WIFI AVIATOR Handset with Cradle
  • WiFi/4G-LTE cabin activation.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
BD-700-1A11
VariantGlobal Express, XRS
Global 5000 (classic and GVFD)
Global 6000
ApprovalMCA20A13AE-01
MCA21A41AE-01
Validations
DescriptionRemoval of OEM originally installed ICG ICS-1XX/-2XX Satcom Iridium/Voice with Collins SAT-2100-6100, or Honeywell MCS-6000/-7000 SATCOM Inmarsat with AMT-50 Antenna System (incl. AMT-50, ACU, DLNA). Installation of FOI – FANS1A+ Over Iridium, 1ch Iridium Transceiver (TSO-159a/b)
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
VariantGlobal Express, XRS
ApprovalEASA 10083557
ValidationsFAA ST00190IB
DescriptionInstallation of one or two single-channel SATCOM Iridium Antenna on rear/top fuseladge, STA 767.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
BD-700-1A11
VariantGlobal Express, XRS
Global 5000
ApprovalEASA 10075263
Validations ST04591NY
DescriptionRemoval of originally installed Collins CES – Cabin Electronic System with Galley TSE and two Cabin Standard Definition bulkhead LCD, as well as CD/DVD players and installation of Collins VENUE High-Definition CMS/IFE with Galley HD TSE and two Cabin HD LCD, 3D HD Airshow, AS-Mobile, Blueray Player and Cabin HDMI ports.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A11
VariantGlobal 5000
ApprovalMCA21A12AE-01
Validations
DescriptionRemoval of OEM originally installed CTU Aerocom 3000 with wireless DECT Handsets, Cradle and Base Station and installation of Collins Advanced Data Router ADR-2100 with cabin WiFi/4G-LTE functionalities.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A11
VariantGlobal 5000
ApprovalMCA20A24AE-01
Validations
DescriptionInstallation of Collins single Aircraft Interface Device (AID) with dual Tablet Interface Modules (TIM), providing aircraft data in peer-to-peer communication and electrical power to Pilot and Co-Pilot portable iPAD/EFB.
TC HolderBombardier
TypeBD700
ModelBD-700-1A11
VariantGlobal 5000
ApprovalEASA 10078637
DescriptionUpgrade of Honeywell Flight Management System FMZ-2000 (Software Version 6.1, NZ-2010) ) on a Bombardier CL-600-2B16 / 601-3R Variant, introducing RNP1 operational capability.
TC HolderBombardier
TypeCL600
ModelCL-600-2B16
Variant601-3R
ApprovalEASA 10074604
DescriptionRemoval of all originally installed and obsolete cabin wash lights with ballast units and installation of all new LED Wash Lights with dimmers from Aircraft Lighting International in Crew Rest, Galley, Passenger Cabin and Lavatory.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
VariantGlobal Express, XRS
ApprovalMCA22A01AE-01
Validations
DescriptionRemoval of Avionica Mini QAR and installation of L3 HARRIS QAR200 – Micro Quick Access Recorder with removable storage card
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
VariantGlobal Express, XRS
ApprovalMCA20A24AE-01
Validations
DescriptionRemoval orinally installed placards in Galley, Lavatories, Passenger Cabin and AFT Baggage Compartment and installation, manufacturing and installation of all new, bilingual EN/RU placards.
TC HolderBombardier
TypeBD-700
ModelBD-700-1A10
BD-700-1A11
VariantGlobal 6000
Global 5000
ApprovalMCA21A29AE-01
MCA21A40AE-01
Validations
DescriptionThis ADS-B out upgrade solution is fully integrated into EMB145/135 Honeywell Primus II avionics. It may be performed independently from any EMB SB, by upgrading corresponding Honeywell NAV/COM equipment directly with Honeywell (dealer involvement is required). ADS-B out information is displayed on Pilot/Co-Pilot RMUs. Basically, upgrade consists of NAV/COM units removal, upgrade/replacement by Honeywell and re-installation. Just six new wires to be installed in forward avionic compartment.
TC HolderEmbraer
TypeEMB135 (all)
EMB145 (all)
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalEASA 10077196
DescriptionRemoval of OEM originally installed DU-870 Display Unit and their replacement by LCD DU-875. One-by-one upgrade/replacement is possible, no new hardware or wire installation is required. Estimated labour – 4MH. Estimated a/c ground time: 5 hours.
TC HolderYabora
(ex-Embraer)
TypeEMB135BJ
EMB145
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalEASA 10058644
DescriptionInstallation of FOI – FANS Over Iridium, 1ch Iridium Transceiver (TSO-159a/b) with corresponding Iridium Antenna (TSO-159a/b). This EASA STC is an alternative solution to Embraer SB145LEG-23-0052 (HSD SATCOM Installation), concurrently required for SB145LEG-23-0040 (FANS-1A Activation).
TC HolderYabora
(ex-Embraer)
TypeEMB135BJ
EMB145
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalEASA 10075546
DescriptionRemoval of OEM originally installed VT Miltope CA/WAP with corrresponding WiFi Antenna and installation of GDR Router with cabin internal WiFi and 4G-LTE Antenna
TC HolderYabora
(ex-Embraer)
TypeEMB135BJ
EMB145
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalMCA20A10AE-01
Validations
DescriptionRemoval of OEM Embraer originally installaed SATCOM Swift 64 (SDU-7300 and HPA-7400) and installation of new SATCOM Swift Broadband (SDU-7330 and HPA-7450) Single-channel or Multi-channel SATCOM Swift BB/SBB.
TC HolderYabora
(ex-Embraer)
TypeEMB135BJ
EMB145
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalMCA20A16AE-01
Validations
DescriptionRemoval of OEM originally installed cabin placards and installation of new placards i.a.w. customer request.
TC HolderEmbraer
TypeEMB135BJ
EMB145
ModelEASA.IM.A.032
VariantLegacy 600/650
ApprovalMCA21A01AE-01
Validations

Description

OSD-SIM Data for AW169 Full Flight Simulators

Document Nr.TitleRevisionA/C ModelVariant/ConfigurationNotes
AW169_VDRVALIDATION DATA ROADMAP AW 1695.0AW169Core Avionics SW Phase 3.0 / Fixed Landing Gear(a)
AW169P8_VDRVALIDATION DATA ROADMAP AW169 P83.0AW169Core Avionics SW Phase 8.0 / Fixed Landing Gear(b)

(a) Devices to be assessed and validated with reference to the above listed data are eligible for Interim Qualification only (see CS SIMD.100(b) ).
(b) Devices to be assessed and validated with reference to the above listed data are eligible for Full Objective Qualification.

TC HolderTypeModelVariantApprovalValidations
LEONARDO S.p.AAW169AW16910076972 REV. 2
without
https://alamo-engineering.com/wp-content/themes/hazel/
https://alamo-engineering.com/
#164f80
style1
paged
Loading posts...
/home/customer/www/alamo-engineering.com/public_html/
#
on
none
loading
#
Sort Gallery
on
no
off
off
off