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Engine Reference
Engine Monitors:
H384 Series H598 Series Engine Monitors Reference List
H484 SERIES

The Howell Instruments' microprocessor-based engine monitors combine accuracy and dependability with multi-channel monitoring capability. Engine management with state-of-the-art technology enhances fleet operations and safety, while reducing operating costs.

In addition to allowing the operator to view engine and airframe parameters in real time, the unit can be programmed to display data in any of the following modes.
  • Identification and Usage Data
  • Exceedance Monitoring
  • Trend Monitoring
  • Flight Profile Data
Display
The digital display includes one, thirty (30) character line of green alphanumeric characters.

Data Access Connector
The Data Access Connector is provided for uploading and downloading data.

Exceedance Monitoring
The H484 can monitor selected parameters for out-of-limit conditions. The engine manufacturer's operating limits are programmed into the unit, which tracks engine operation in real time under operational conditions. When an exceedance is detected, a latching ball flag on the face of the unit is set, informing maintenance personnel that an out-of-limit event has occurred. The unit also has the capability of providing an output signal to a cockpit Advisory/Warning Panel. The H484 normally records the date and time of the event, a frame (or frames) of all parameters pertinent to the event, the duration of the exceedance, the peak value of the offending parameter and, if applicable, the level of maintenance required based upon the severity of the event.

Flight Profile Data
Flight profile data can be collected in a Timed Recording Mode or a Profile All Mode. The Timed Recording Mode collects a frame of data at a selectable fixed time interval. The Profile All Mode collects start and shutdown records at a rate of one per second. All other operational data is gathered using data compression techniques to minimize the space of data collected.

Data Reduction
A menu-driven ground station software package helps operators reduce flight data using an IBM compatible PC. Data file management is straightforward, easy to interpret, and it provides storage for data records.

Input Signals
Four cards are dedicated to the processing of input signals.
  1. The frequency card can monitor up to five frequency inputs. The frequency range is 3.5 Hz to 30 KHz.
  2. The low level analog card is capable of monitoring two thermocouples and two RTDs.
  3. The high level analog card can monitor three high level DC analog signals.
  4. The discrete card monitors up to six discrete inputs. These discrete inputs can be voltage or ground. This card also has the capability of outputting two 28 VDC@1 Amp discrete signals that are software programmable.
Expansion
Expansion card slot number 1 is addressable and is capable of accommodating any of the cards listed above as well as cards of special design.

Expansion card slot number 2 is addressable and is capable of monitoring four dedicated signals such as synchro and pulse displacement fuel flow meters. This expansion slot also has the capability of interfacing with ARINC 429, MIL STD 1553, and RS 232 data busses. This capability allows the H384 to interface with:

  • Howell Automatic Engine Data Acquisition System (AEDATS)
  • Howell JETCAL2000® Analyzer
  • Aircraft Air Data Computers
  • Personal Computers
  • Air Frame Data Buss
Vibration measurement capability is also available as an option.

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Howell Instruments, Incorporated
8945 South Freeway • Fort Worth, Texas  76140
Phone: (817) 336-7411
Fax: (817) 336-7874