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61-101-00802.EF1 Revision J                                                                                      

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(48) Rotate the TEST FUNCTION switch to IND AMP. 

(49) Verify the indicator reads 900 ± 35 lbs. 

(50) Set the 28 VDC power supply to OFF. 

(51) Set the T/S ON / OFF to OFF. 

 

D.  Disconnecting/Reconfiguring 

(1)  Disconnect 28 VDC power supply. 

(2)  Disconnect the T/S from the Indicator. 

 

3.  ALTERNATE CALIBRATION (WET TANKS) 

 

Note:

  The Alternate Calibration should only be used as a temporary measure when draining  

facilities are not available. Recalibrate the aircraft using the Preferred Calibration 
method at the first opportunity. 

 

Note:

  The Alternate Calibration applies the nominal empty tank capacitance value to the  

system by the T/S for the indicator zero reading. A second capacitance value, (equal 
to the combined value of nominal empty tank plus the equivalent quantity of fuel in the 
tanks), is applied to the system. The indicator is then adjusted to show the substituted 
fuel quantity. 

 

Note:

  Accuracies, close to the Preferred Calibration, may be obtained if the measured dry 

capacitance for specific serial number aircraft is known and used instead of EMPTY 
values referenced in Table 2 (Tank Capacitance Empty). The ADD FOR FULL values 
listed in Table 4 should be added to the known values to obtain the CAP SIM value 
for FULL. 

 

A.  Test Set Preparation 

 

 

Note:

  Refer to Precautions and Preliminary in General Information section. 

(1)  Ensure aircraft battery is disconnected. 

CAUTION:

 WHEN LOWERING OR RAISING THE PILOT FUEL PANEL, ENSURE  

 

 

  THAT THE AIRCRAFT BATTERY IS DISCONNECTED. OBSERVE ALL  

 

 

  SAFETY PRECAUTIONS. 

(2)  Access the applicable indicator. 

(3)  Ensure circuit breakers are open. 

(4)  Ensure aircraft wiring plug at Indicator is disconnected. 

 

B.  Connecting Test Set  

(1)  Ensure T/S switch is OFF. 

(2)  Rotate the TEST FUNCTION switch to CAP SIM CAL (NORM SYS). 

(3)  Set the INSULATION / SYSTEM switch to SYSTEM. 

(4)  Set the MAIN / TOT-AUX / NAC switch to MAIN / TOT. 

(5)  Set the 200 (pF) / 1000 (pF) switch to 200 (pF). 

 

C.  Connecting the Test Set 

(1)  Connect the T/S as depicted in Figure 11 or Figure 12 (whichever is applicable). 

 

 

Summary of Contents for DC400

Page 1: ...101 00802 Doc P N 61 101 00802 EF1 Revision J September 4 2020 _________________________________________ MOD C used with DC400 or DC400A P N 101 00800 or P N 101 00850 Digital DC Fuel Quantity Test S...

Page 2: ...nformation contained herein is the sole property of Barfield Inc No intellectual property rights are granted by the delivery of this document or the disclosure of its content This entire document is p...

Page 3: ...this manual Inquiries should include specific questions and reference the publication title number chapter page figure paragraph and effective date Please send comments to TECHNICAL CUSTOMER SUPPORT...

Page 4: ...r to obtain the list of approved repair facilities worldwide ensuring that this equipment will be serviced using proper procedures and certified instruments BARFIELD PRODUCT SUPPORT DIVISION Telephone...

Page 5: ...inal 101 00814 adapter cable D 260 00729 January 22 2009 Updated Company Logo E 260 00779 April 29 2010 Added List of Approved Repair Facilities and Recertification Information page vii F 260 00788 Se...

Page 6: ...IES 1 3 PANEL CONTROLS 1 4 AIRCRAFT SYSTEM DESCRIPTION 1 6 PRECAUTIONS 2 7 PRELIMINARY 2 8 DISCLAIMER 2 9 RECERTIFICATION 3 CHAPTER 1 OPERATION 4 1 INSULATION MEASUREMENT TEST 4 2 CAPACITANCE MEASUREM...

Page 7: ...LA 1 thru LA 225 F F90 1 S N LA 226 and after G A100 B100 S N B 152 B 156 and after BE 2 and after H 200 All 200 200C 200CT and 200T I B200 GT GTi 250 All J 300 All 300 and 300C K 350 350i 360 All 2...

Page 8: ...made 4 Ensure power remains OFF unless otherwise specified 7 PRELIMINARY 1 To ensure the integrity of all system components perform the Insulation Capacitance tests first Then perform one of the Indi...

Page 9: ...has a one year recertification requirement Qualified technicians in a shop equipped with the necessary tooling facilities and Barfield approved procedures must perform the maintenance required by this...

Page 10: ...ONNECTIONS ENSURE APPLICABLE CIRCUIT BREAKER S ARE OPEN 4 Disconnect aircraft wiring plug at the indicator B Test Set Preparation 1 Set T S ON OFF switch to OFF 2 Rotate the TEST FUNCTION switch to IN...

Page 11: ...the T S reading is less than 50 nS Note The display reading is in nS nano Siemens To get an equivalent M megaohms measurement divide 1000 by the T S display reading T S DISPLAY READING EQUIVALENT M 1...

Page 12: ...h position except SIG RTN 14 With switch rotated to SIG RTN verify a T S reading of 1 15 Return fuel panel select switch to MAIN TOTAL a If a test does not comply with specification repeat test to ver...

Page 13: ...connect aircraft wiring plug at the indicator B Test Set Preparation 1 Set T S ON OFF switch to OFF 2 Rotate the TEST FUNCTION switch to PROBE S 3 Set the INSULATION SYSTEM switch to SYSTEM 4 Set the...

Page 14: ...ON 2 Set the aircraft fuel panel select switch to MAIN or TOTAL 3 Push and hold the T S PRESS TO READ CAP pF pushbutton 4 Verify that the tanks value is within tolerances as specified in Table 2 Tank...

Page 15: ...T GTi GTx C99 Aircraft Type Total Nacelle Only Min Nom Max Min Nom Max C90 C90 B GT GTi GTx 224 6 249 5 274 5 79 3 88 1 96 9 C99 219 4 243 7 268 0 74 1 82 3 90 5 E90 A100 B100 with 100 380006 15 17 In...

Page 16: ...plug to Indicator 4 Return the aircraft to its original configuration 3 INDICATOR TEST Note Refer to Precautions and Preliminary in General Information section Note Failure to calibrate the system aft...

Page 17: ...e P N 101 00831 for conversion to systems with circular style connectors 2 Connect T S IND connector to Indicator 3 Connect T S ACFT connector to aircraft wiring plug Figure 5 Indicator Test With 101...

Page 18: ...15 Release the pushbutton 16 Rotate the TEST FUNCTION switch to IND AMP 17 Verify the indicator reads 1200 lbs 18 If the indicator does not show 1200 lbs adjust FULL 19 If the indicator still does not...

Page 19: ...CAP pF pushbutton while adjusting the CAP SIM pF control knob to obtain a test display of 231 pF 41 Rotate the TEST FUNCTION switch to IND AMP 42 Verify the indicator reads 600 35 lbs 43 Rotate the T...

Page 20: ...efueled Drain pumps 2 Disconnect aircraft battery CAUTION WHEN RAISING OR LOWERING THE PILOT FUEL PANEL ENSURE AIRCRAFT BATTERY IS DISCONNECTED 3 Gain access to applicable Indicator 4 Open the circuit...

Page 21: ...the indicator does not read 1300 lbs use the F FULL adjustment to obtain correct reading 11 Rotate the TEST FUNCTION switch to CAP SIM CAL NORM SYS Note FULL adjustments may affect the EMPTY setting E...

Page 22: ...s are made to the harness following this test then the Preferred Calibration must be repeated and subsequently this integrity test A Aircraft Preparation 1 Disconnect aircraft battery CAUTION WHEN LOW...

Page 23: ...CAUTION DO NOT TAP BEZEL OF INSTRUMENT TO VIBRATE TO REMOVE FRICTION GENTLY TAP ADJACENT PANEL OR REAR HOUSING OF INDICATOR BEFORE TAKING READINGS 17 Verify the indicator reads the same as in step 15...

Page 24: ...24 40 lbs 32 Failure to obtain the correct indication may indicate the possibility of in line resistance in the aircraft wiring between the Indicator and the probes a If this condition exists disconne...

Page 25: ...t fuel panel select switch to AUX NAC and hold if applicable CAUTION DO NOT TAP BEZEL OF INSTRUMENT TO VIBRATE TO REMOVE FRICTION GENTLY TAP ADJACENT PANEL OR REAR HOUSING OF INDICATOR BEFORE TAKING R...

Page 26: ...ect Note When cleaning the connectors be sure to include the T S s connectors 60 Set the T S ON OFF switch to OFF E Disconnecting Reconfiguring 1 Open the circuit breakers turn the battery switch OFF...

Page 27: ...14 to the T S PROBES receptacle as shown per Figure 7 3 Determine the part number and physical makeup of the probe under test 4 Connect the color coded wires sockets from the probe adapter to the matc...

Page 28: ...25 5 27 5 29 5 Leading Edge Outboard 100 380006 13 67 103 187 23 0 24 6 26 5 Inboard Aft 100 380006 37 71 107 141 145 173 15 0 17 7 19 0 Integral Inboard 100 380006 93 121 179 20 2 22 2 24 2 Integral...

Page 29: ...bles and probes Aircraft C90 C90A B GT GTi GTx C99 Tank Unit Beech Probe P N Min Nom Max Leading Edge Inboard 100 380006 11 69 105 139 143 175 40 3 44 8 49 3 Leading Edge Outboard 100 380006 13 67 103...

Page 30: ...ote The probes and harnesses in Table 12 were installed in aircraft with S N LW17 LW69 through LW214 B152 B156 through B234 BE1 through BE24 and BB2 through BB220 Note The 59 harness has diodes mounte...

Page 31: ...owing setps Figure 8 Probe Discrete Level Interface 2 Ensure the test leads P N 101 01012 banana plugs are connected to the DISCRETE LEVEL SENSOR jacks 3 Connect the clip ends of test leads to probe D...

Page 32: ...F 2 Rotate the TEST FUNCTION switch to CAP SIM CAL NORM SYS 3 Set the INSULATION SYSTEM switch to SYSTEM 4 Set the MAIN TOT AUX NAC switch to MAIN TOT 5 Set the 200 pF 1000 pF switch to 200 pF B Conne...

Page 33: ...OF INDICATOR BEFORE TAKING READINGS 7 Verify the indicator reads zero lbs 8 If reading is not zero adjust EMP 1 E 1 9 If the indicator will not give a zero reading replace the indicator 10 Rotate the...

Page 34: ...C 2 through C 28 until an accurate gage adjustment is obtained 30 Set the MAIN TOT AUX NAC switch to MAIN TOT 31 Rotate the TEST FUNCTION switch to CAP SIM CAL NORM SYS 32 Set the 200 pF 1000 pF swit...

Page 35: ...ity Note Accuracies close to the Preferred Calibration may be obtained if the measured dry capacitance for specific serial number aircraft is known and used instead of EMPTY values referenced in Table...

Page 36: ...sted in Table 2 for the aircraft under test 3 Press and hold the PRESS TO READ CAP pF pushbutton while adjusting the CAP SIM pF control knob to obtain a T S reading for the aircraft as per Table 2 4 C...

Page 37: ...to adjust the T S display to an AUX NAC EMPTY nominal value referenced in Table 2 for the aircraft under test 21 Press and hold PRESS TO READ CAP pF pushbutton while adjusting CAP SIM pF control knob...

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