| SPCL |
SPECIAL TEST FEATURES |
FUEL COMPATIBILITY JET A,JP-4 JP-5 MIL-F-5624H |
| CXCY |
PART NAME ASSIGNED BY CONTROLLING AGENCY |
FUEL FLOW TRANSMITTER |
| ABKW |
OVERALL HEIGHT |
4.530 INCHES NOMINAL |
| ABMK |
OVERALL WIDTH |
3.050 INCHES NOMINAL |
| ABHP |
OVERALL LENGTH |
7.300 NOMINAL INCHES |
| BGNL |
MEASUREMENT RANGE |
+400.0/+33000.0 POUNDS PER HOUR |
| FEAT |
SPECIAL FEATURES |
TRANSMITTER IS ALUMINUM BODY WITH CYLINDRICAL BORE;A TURBINE DRIVER,FLOW STRAIGHTENER AND MEASUREMENT ASSY ARE PUT ON A SHAFT AND INSTALLED IN THE BORE;FOR USE IN AIRCRAFT FLOW MEASURING SYSTEMS;OPERATES WITH A FUEL FLOW INDICATOR TO SHOW RATE OF FUEL FLOW,TOTAL FUEL USED, OR BOTH;NO EXTERNAL POWER IS NECESSARY FOR THE TRANSMITTER;COMPONENT MAINTENANCE MANUAL 73-35-36 PAGES 1 AND 2 FEB 15/02 FIGURE 1;SUPPLIED MOUNTING IS A FLAT SURFACE I A RECTANGULAR ELECTRONICS COMPARTMENT ON THE TRANSMITTER FOR 2 MAGNETICV PICKOFF COILS AND A SKEW (SWIRL) RUDDER;ELECTRICAL CONNECTOR RECEPTACLE KEYWAY IS ON OUTSIDE OF ELECTRONICS COMPARTMENT AND A COVER FITS ON THE ELECTRONICS COMPARTMENT |
| AGAV |
END ITEM IDENTIFICATION |
AIRCRAFT;AIRBUS A330,A340 |