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The purpose of this Supplement is to provide the maintenance technician with the information necessary to ensure the correct functionality and performance of the Avionics Standby System Update on the Cessna Model 525B until this information gets incorporated into the next revision to the manuals listed in the "REVISIONS" section of this supplement.
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ATA 34-18-05, EFD-750 Electronic Flight Display - Removal/Installation. ATA 34-18-10, DCM-750 Configuration Module - Removal/Installation. ATA 34-18-15, MAG-500 Magnetometer - Removal/Installation. Model 525B (Airplanes -0057 and -0135 and On) Wiring Diagram Manual Chapter 31, Indicating/Recording Systems ATA 31-10-01, Figure 03, Switch Panels (Airplanes 0665 & On).
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Continuous Inspection Program This ICA Supplement does not affect the current inspection program. Airworthiness Limitations Cessna Aircraft Company Model 525B, Chapter 4, Airworthiness Limitations, contains the system and airframe limitations for the Model 525B. NOTE: The Airworthiness Limitations section is FAA-approved and specifies maintenance required under Section 43.16 and 91.403 of Title 14 Code of Federal Regulations, unless...
SUPPLIER PUBLICATION LIST General This section gives you a list of some of the supplier publications for the Model 525B Airplane. Use the supplier publication list to cross reference the component part number and the applicable supplier publication part number to find the correct supplier publication. It can be necessary to have special tools and equipment to complete some of the maintenance procedures in the supplier publications.
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Airplanes -0610 and On and Airplanes -0057 and -0451 thru -0609 that incorporate SB525B-34-40 General This section provides the electrical load analysis for the Cessna Model 525B (Airplanes -0610 and On and Airplanes -0057 and -0451 thru -0609 that incorporate SB525B-34-40).
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This section gives the maintenance practices for the cleaning of the pitot-static systems. The Model 525B has three separate and independent pitot-static systems, the pilot (left), copilot (right) and standby. For more information about the system, refer to Pitot-Static System - Description and Operation.
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(Garmin ADC) General This section gives the adjustment and test procedures for the Model 525B airplane pitot-static system. The inspections given in this section include a Pitot-Static System Functional Check and a Reduced Vertical Separation Minimums (RVSM) Skin Waviness Inspection. The checks and inspections given in this section are also satisfactory return to service tests for most of the pitot-static system and air data computers.
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Make sure the full inspection area meets the requirements of Zone 1 local contour. Refer to Model 525B Structural Repair Manual, Chapter 51, Aerodynamic Surfaces. Repair any differences with the standard procedures found in the Model 525B Structural Repair Manual, Chapter 51, Aerodynamic Surfaces.
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For troubleshooting data to assist in the correction of L3Harris Electronic Flight Display System problems, refer to the Model 525B Wiring Diagram Manual (Airplanes -0057 and -0135 and On) and the newest revision of the L3Harris Aviation Products, Electronic Flight Display System, EFD-750, 0040-15751-01 Installation Manual, found in the Supplier Publication List.
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CONFIG File are as follows: The Version value is the new configuration file version. The Aircraft value is Model 525B. (18) Cycle power to the EFD-750 while holding the rotary knob. (19) Make sure that the ADEC option in the pilots menu shows a green check mark.
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Management And Transmit - Maintenance Practices, Inhibit Logging During Ground Maintenance Operations. Start and taxi the airplane to a compass rose on the airport. Refer to the Model 525B FAA Approved Airplane Flight Manual for the engine starting and taxi instructions.
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Wait 15 seconds to let the EFD-750 save the changes. (20) Taxi the airplane back to the maintenance facility and stop the engines. Refer to the Model 525B FAA Approved Airplane Flight Manual for the taxi and engine shutdown instructions.
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Install the DCM-750 Configuration Module (Refer to Figure 401). Put the configuration module (PI065) in its correct position at the electrical connector (PI062). Connect the DCM to the rear of the electrical connector. Refer to the Model 525B (-0057 and -0135 and On) Electrical Wiring Diagram Manual.
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL NOTES: AN ASTERISK(*) PRECEDING A LETTER INDICATES LOWER CASE. ADD PROTECTIVE SLEEVING (M23053/5-1XX-X) TO COVER SWITCH TERMINALS. JI117 PI117 CABIN REV/DIM PNL SI125 RI004 PILOT PI118 JI118...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DI089 S3106-6 DIODE ASSEMBLY 0057 - 0057 0135 & ON...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL PI109 JI109 JI108 PI108 POWER PANEL CABIN CABIN POWER PANEL (20) (20) (20) SI019 (20) (20) (20) LH GEN SWITCH (20) (REF POWER DISTRIBUTION) (20) (20) (20)
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY FI110 9912808-2 LED PANEL - POWER 0057 - 0057 0451 &...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JI111 PI111 CABIN LH TILT PNL PI113 JI113 LH TILT PNL CABIN SI047 SI045 SI046 LH BOOST (REF LH FUEL CONTROL) FUEL TRANSFER RH BOOST PUMP REFER TO 28-20-01...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DI054 S3106-3 DIODE ASSEMBLY 06090 0665 & ON...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY SI046 S3506-1 SWITCH - FUEL TRANSFER 0057 - 0057 0135 &...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DI018 S3106-3 DIODE ASSEMBLY 06090 0057 - 0057 0135 &...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JI122 PI122 FI122 (WHT) (VEND)RED AFT PED (BLU) (VEND)BLK LED PANEL (REF INTERIOR LIGHTS) REFER TO 33-10-01 FI126 (WHT) (VEND)RED TRIM TAB LT (BLU) (VEND)BLK LED PANEL...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DI091 S3106-4 DIODE ASSEMBLY 0665 & ON DI092...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JI125 PI125 CABIN LNDG GEAR PNL GEAR UP SI141 GEAR SEL SW PI127 JI127 GEAR DOWN SI006 (REF LANDING GEAR MONITOR) LNDG GEAR PNL CABIN REFER TO 32-60-01...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY FI003 LIGHT ASSEMBLY - LANDING GEAR (ZONE 245)
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JC522 PC522 JC115 PC115 CABIN LH CONSOLE LH CONSOLE CABIN SC008 JC507 (WHT) (REF POWER DISTRIBUTION) INTERIOR (BLU) REFER TO 24-30-01 PILOT PHONE MASTER SW NORMAL (ORN)
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY FC101 LED PANEL - LEFT CONSOLE JC115 SJS830250...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JF522 PF522 CABIN RH CONSOLE JF507 (WHT) (BLU) COPILOT PHONE (ORN) JACK JF509 COPILOT HEADSET MIC JACK JF506 COPILOT OXY (BLU) MASK MIC JACK (WHT) (REF DUAL AUDIO)
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY FF101 LED PANEL - RIGHT CONSOLE JF116 SJS830250...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL JI111 PI111 CABIN LH TILT PNL PI113 JI113 LH TILT PNL CABIN SI047 SI045 SI046 LH BOOST (REF LH FUEL CONTROL) FUEL TRANSFER RH BOOST PUMP REFER TO 28-220-01...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DI054 S3106-3 DIODE ASSEMBLY 06090 0665 & ON...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SWITCH PANELS AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY SI047 M8805/93-001 SWITCH - LEFT BOOST PUMP 81640 0665 &...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL NOTES: AN ASTERISK(*) PRECEDING A LETTER INDICATES LOWER CASE. TERMINATE SHIELD WITH 22AWG WIRE. SLEEVE 16AWG WIRE WITH S4057-3 PROTECTIVE SLEEVING FROM 11PN017-1HN002. ***REFER TO 91-10-01 FOR GROUND INFORMATION...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SECONDARY FLIGHT DISPLAY AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY DC007 S3106-3 DIODE ASSEMBLY 06090 0665 & ON...
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® CESSNA MODEL 525B (SERIALS -0057 AND -0135 AND ON) WIRING DIAGRAM MANUAL SECONDARY FLIGHT DISPLAY AIRPLANES 0665 & ON UNITS NOMENCLATURE PART NUMBER 1 2 3 4 5 6 7 EFFECTIVITY ASSY PB031 MS3475L22-41S CONNECTOR 96906 0665 & ON S3074-22 .
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