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General| Manufacturer | Cessna |
|---|---|
| Type | Business Jet |
| Crew | 2 |
| First Flight | August 1987 |
| Role | Corporate Jet |
| Wingspan | 15.91 m |
| Height | 4.57 m |
| Max Takeoff Weight | 7, 711 kg (17, 000 lb) |
| Powerplant | 2 × Pratt & Whitney Canada JT15D-5A turbofan |
| Thrust per Engine | 2, 900 lbf (12.9 kN) |
| Service Ceiling | 13, 716 m (45, 000 ft) |
Lists the original issue and subsequent revision dates of the service bulletin.
Identifies the subject of the service bulletin.
Specifies the models and serial numbers to which the bulletin applies.
Explains the purpose of the bulletin, mandates, and upgrades.
Outlines the parts and instructions for installing TCAS II and comm units.
Details conditions for recording the service bulletin as completed.
Informs flight crew of operational changes from the service bulletin.
Confirms FAA approval and amendment to the maintenance manual.
Specifies work phase and estimated man-hours.
Lists part numbers, availability, and cost for kits.
Lists necessary test equipment and software for the installation.
Advises to weigh aircraft after modification for updated information.
Lists required engineering drawings and maintenance manuals.
Steps for preparing the aircraft, including power and warning tags.
Instructions for removing specific components for modification or upgrade.
Detailed steps for installing the TCAS II computer and related cable assemblies.
Steps to configure the TCAS II system per engineering drawings.
Steps to configure the transponders for proper operation.
Procedures to perform a functional check of the TCAS II and transponder systems.
Instructions for ground testing the Elementary Surveillance capability.
Verifying aircraft and flight ID transmission during testing.
Recording pressure altitude and Mode A code received by the test set.
Verifying transmission of capability reports and parameter status.
Checking TCAS RA status and recording received values.
Simulating various traffic scenarios to test TCAS resolution advisories.
Performing GPWS aural tests in conjunction with TCAS self-test.
Testing bearing accuracy of directional antennas using a compass rose.
Testing the top TCAS antenna's bearing function in TA/RA mode.
Verifying circuit breaker power supply and isolation.
Testing intruder display without altitude reporting.
Testing intruder display without bearing information.
Verifying the correct Mode S address for the transponder.
Checking audio, bearing, deviation, SNR, and display for various aircraft systems.
Ensuring correct supplements are inserted into the Airplane Flight Manual.
Identifies the supplemental data sheet's subject.
Specifies applicable models and serial numbers for supplemental data.
Lists manpower, cost, and availability for supplemental parts.
