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AEROSPACE TECHNOLOGIES
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Location
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Latin America
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- Contact Us
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Onboard Systems - HUMS
Onboard Systems
Honeywell’s onboard systems collect, process and interpret data generated by various helicopter components including engines and gearboxes. This data provides detailed analysis to skilled technicians with access to a computer.
Honeywell Health and Usage Monitoring Systems (HUMS) are industry-proven, unify our ground-based carry-on products and meet current regulatory requirements. They are also designed to support future HUMS functions.
Honeywell’s onboard systems feature:
- Health monitoring, diagnostics and recording
- Advanced drive train diagnostics
- Greater than 100db dynamic range
- Advanced rotor track and balance
- Event processing and recording
- Flight regime recognition
- Engine health monitoring
- Helicopter operation monitoring program support
- Global positioning system (GPS)
- Wireless communication interface
- Integrated inertial system using micro electromechanical systems (MEMS) and GPS sensors
- Three embedded processors support partitioned DO 178B software functions and systems growth
- Up to 8GB of compact flash (non-crash survivable) for vehicle or flight data recording
Note: Models include 1134, 1209, 1230 and Onboard VXP. Features may change based on model.
If you are interested in purchasing or learning more about our HUMS, vibration monitoring, or rotor track and balance products and services, please contact an authorized distributor in your region.
Introducing the Next Evolution in Condition-Based Maintenance - RECON
Honeywell is introducing the next-generation in Health Usage and Monitoring System (HUMS). Codenamed RECON the system is designed to help commercial and military helicopter operators increase safety, operational availability and reliability while reducing operational and maintenance costs. CLICK HERE to learn more.
Onboard Systems Comparison Table
| Onboard Systems | ONBOARD VXP | MODEL 1209 | MODEL 1134 | MODEL 1239 |
|---|---|---|---|---|
| ACCELEROMETERS (SIMULTANEOUS MEASUREMENT) | 26 (6) |
36 (6) |
24* (6) | 48 (8) |
| TACHOMETERS / TRACKERS | 4 /4 | 8/2 | 5*/1 | 10/2 |
| GENERAL PURPOSE ANALOG & DISCRETE IN | 8 | 32 | 48 | |
| GENERAL PURPOSE DISCRETE OUT (LOW/HIGH) | 0/2 | 16/4 | ||
| DIGITAL COMMUNICATION – USB – CAN – ETHERNET – RS232 / 422 / 485 – 1394 FIREWIRE – ARINC 429 TRANSMIT/RECEIVE – MIL-STD-1553B DUAL REDUNDANT BUSES |
1 |
1 1* 2 2 1 1/2 1 (OPTIONAL) |
2 1 4 4 1 2/4 4 |
|
| INTERNAL STORAGE (STANDARD /OPTIONAL) | 512MB | 128MB | 512MB / 8GB | 512MB / 8GB |
| QUICK ACCESS RECORDER (NOT CRASH SURVIVABLE) | - | - | OPTIONAL | OPTIONAL |
| DIMENSIONS: – L x W x H INCHES (WITH MOUNTING PLATE) – L x W x H MM (WITH MOUNTING PLATE) |
12.2 x 7.1 x 3.0 304 x 180 x 76 |
3.0 x 5.75 x 7.575 76 x 146 x 192 |
7.6 x 6.2 x 1.8 193 x 158 x 46 |
8.8 x 4.7 x 2.5 224 x 119 x 64 |
| WEIGHT (W/O MOUNTING PLATE) | 6.2 lbs / 2.82 kg | 4lbs 5oz / 1.95 kg | 2.5 lb / 1.13 kg | 4.0 lbs / 1.81 kg |
| TEMPERATURE (DEGREES C) | -30 to +60 | -20 to +55 | -40 to +71 | -40 to +71 |
| SOFTWARE: RTCA/DO-178B | LEVEL E | LEVEL D | ||
| REGULATIONS: – CAP-739 (FDM), HOMP/FOQA – JAR-OPS3 – CAP-753 (VHM) |
LIMITED YES YES |
YES YES YES |
*Reconfigurable options using internal jumper selection. Total number is dependent on jumper configuration.
Platforms
| COMMERCIAL |
MILITARY | |||||
|---|---|---|---|---|---|---|
| PLATFORM | PLATFORM |
PRODUCT | FAA STC | CANADA STC | EASA STC | ANAC STC |
| Aerospatiale AS-365 | VXP |
SR01949NY-D | 10017018 |
|||
| Agusta S.p.A. AB139 | CH47C/D, HH60G/UH60A/L, C130E/H | SR02120NY-D | SH07-1 | |||
| Airbus Helicopters AS365 | SR01949NY-D | |||||
| Airbus Helicopters BK117/EC145 | SR02535LA | 2016S10-07 | ||||
| Airbus Helicopters EC135 | SR02114NY-D | 10034246 |
||||
| Bell 206L | SR01972NY-D | 2016S10-08 | ||||
| Bell 212 | SH03-26 | |||||
| Bell 407 | SR01613NY-D | |||||
| Bell 412, 412CF, 412EP | SR01591NY-D | 2006S05-05 | ||||
| Bell 427 | SR01953NY-D | |||||
| Bell 430 | SR01957NY-D | |||||
| Leonardo A109E | SR01970NY-D | |||||
| Sikorsky S-61L/N | SR01401NY | SH01-55 |
||||
| Sikorsky S-76A/S-76C S76A ≥ S/N 760511, S76C W/STC SH568NE |
SR02110NY-D | SH01-13 | 10016864 |
2008S10-07 | ||
| Sikorsky S-76C ≥ S/N 760511 |
SR01135NY-D | O-LSH08-236/D | 10016863 |
|||
| Bell 429 | 1134 | OH58D, AH6/MELB | SR09536RC-D | SH11-17 | 10034699 | |
| Leonardo AW139 | SR03260NY | 10049905 | ||||
| Bell 212 | OH58D, MH47G/F, CH47C/D/F, AH64A/D/D Block II/D Block III, UH60A/L, MH60M |
1209 | SR02818NY | 10048070 | ||
| Bell 412 |
SR09373RC-D | 10016920 | ||||
| Sikorsky S-76C ≥ S/N 760511 |
CH47C/D, MH60M/L/T, S70A/B, S76C/C+/C++ | 1239 | SR02602NY-D | 10056180 |
