Super King Air 300 and 350 B300 Maintenance Training Manual – FlightSafety PDF

Description

The Super King Air 300 and 350 B300 Maintenance Training Manual from FlightSafety International is a chapter-by-chapter training text built for the technician who maintains the Beechcraft Super King Air 300 series airframe and its installed systems. It is written in the ATA 100 chapter format, so the chapter and subject numbering a mechanic already works with in the Aircraft Maintenance Manual carries straight across into this study material. Content is drawn from the manufacturer’s Airplane Flight Manual, Pilot Manual and Maintenance Manuals, and the manual was assembled at the Hawker Beechcraft Maintenance Learning Center in Wichita, Kansas.

File Details

• Manual type: Maintenance Training Manual
• Publisher: FlightSafety International
• Subject aircraft: Beechcraft Super King Air 300 and 350 (B300)
• Edition: Second Edition, November 2011
• Revision history: Revision 0.1 January 2012; Revision 0.2 February 2013; Revision 0.3 December 2013
• Chapter format: ATA 100
• Language: English
• File format: PDF

Chapters Covered

• Introduction (ATA 100) – general aircraft description, external familiarization, cabin seating arrangements, flight deck layout, control wheels, fuel panels, instrument markings, engine instruments, center pedestal, subpanels, right side panel, overhead light control panel, T-tail configuration, flight control locks
• ATA 100 / Publications – ATA numbering system, page and block guide, chapter/system index guide, assignment of subject material, list of effective pages, revision bars, and the supporting publications set including the POH/AFM, MMEL, AMM, Wiring Diagram Manual, Airworthiness Limitations Manual, Illustrated Parts Catalog, Component Maintenance Manual, Structural Repair Manual, RVSM Data Package and Service Bulletins
• Aircraft General (ATA 5-12) – Time Limits/Maintenance Checks with the 200-hour phase inspection program, extended range and alternate phase programs, biennial inspection program, high utilization inspection program, special inspection requirements, overhaul and replacement schedule, unscheduled maintenance checks and continuous corrosion control; Dimensions and Areas with Super King Air 350 and 300 specifications, airplane stations, zone locations and access panels; Lifting and Shoring; Leveling and Weighing; Towing and Taxiing with turn radius and danger areas; Parking and Mooring including ground points and tie-downs; Placards and Markings; Servicing with lubrication charts
• Standard Practices (ATA 20) – standard torque values for fine and coarse thread fasteners, torque wrench adapters and calculation, electrostatic discharge sensitivity classification and ESDS handling, packaging and marking, electrical bonding methods for pipes, tubing and conduit, control cable inspection, tension check, storage and pulley inspection, bearing installation by retaining compound and by staking, tube and hose assemblies and fittings, flared fitting torque chart, tubing bending limits, tube damage limits, fastener locking devices, aircraft finish care, corrosion types and control, sealing and bonding, and electrical wiring routine inspections
• Air Conditioning (ATA 21) – electronic flow control units with ambient temperature sensor, electronic controller, firewall shutoff valve, bleed-air flow control modulating valve and transducers; distribution for both the Keith Products system and earlier configurations; cooling including compressor, condenser, receiver/dryer, expansion valve and evaporators; temperature control in auto, manual heat and manual cool modes; electric heat; pressurization system with pressure differential, outflow valve, safety valve, cabin altitude limiters, controller, preset valve and the full phase-by-phase operating sequence; air conditioning refrigerant servicing and troubleshooting charts
• Avionics (ATA 22/23/34) – Pro Line 21 electrical power and lighting systems, DC electrical load distribution, DC-DC converter power supply, light dimmer power supply, electronic flight instrument system including PFD, MFD, DCP and reversionary control panel, air data systems, attitude heading system, electronic standby instrument system, flight guidance system, ground proximity warnings, RVSM and its airworthiness inspection requirements, Pro Line II avionics units, pitot-static system, gyro horizon, EFIS, attitude and heading systems, flight director/autopilot, cockpit voice recorder, and underwater acoustic locating beacon
• Electrical Power (ATA 24) – wiring diagram conventions, wire code description and electrical symbols, DC electrical power and bus distribution system for the 350 and 300, bus-tie printed circuit board and control schematics, Hall Effect devices, starter-generator description, function, controls and indications, generator control units, paralleling, reverse current and overvoltage protection, cross-start overload current limiting, generator control relay, starter-generator brush wear, external power receptacle, DC-DC converter power supply, AC power for earlier serial ranges, inverters, bus-transfer relays, AC power monitor PCB, circuit breakers, emergency and abnormal indications, and electrical panel locations
• Equipment and Furnishings (ATA 25) – flight compartment crew seats and seat attach fittings with wear limits, passenger compartment seats, ottomans, armcaps, seat track wear limits, acoustics and insulation, rail system, interior trim panels, cabin partitions, passenger tables, lavatory, baggage compartment cargo web and cabinetry, plus the Artex 110-4 and Artex 110-406 emergency locator transmitters with components, controls, operation, diagnostics and maintenance considerations
• Fire Protection (ATA 26) – engine fire detection system with temperature sensor element and responder unit, fire detection zones and activation conditions, fire detection system testing, engine fire extinguishing system with bottle, gage, explosive squib and spray tube routing, extinguisher circuit operation and testing, bleed-air warning system description and operation, and portable fire extinguishers

Read as a whole, this training manual gives a technician a continuous narrative of how the Super King Air 300 series is put together and how each system behaves. Rather than presenting isolated procedures, it explains the architecture behind the airframe and its systems, then walks through the components, controls, indications, operation and maintenance considerations for each. The ATA chapter structure means a subject can be found the same way it would be found in the maintenance manual, and the recurring figure references, schematics and tables make the explanations usable at the aircraft rather than only in a classroom.

What the Training Manual Covers in Practice

Airframe and ground handling subjects are covered in depth. The Aircraft General material walks through inspection program structure, including the 200-hour phase inspection program with its four-phase 800-hour cycle, the alternate phase and biennial programs, the high utilization inspection program for aircraft flying 400 hours or more annually, the overhaul and replacement schedule, unscheduled maintenance checks, and the continuous corrosion control inspection. Airplane stations, zone locations, fuselage access panels, floorboard access panels and wing access panels are all diagrammed, along with hoisting, jacking, leveling, weighing, towing and mooring, placards, markings and lubrication points.

Air conditioning and pressurization receive particularly thorough treatment. The electronic flow control units are broken down into their individual components, and the pressurization control system is explained phase by phase, from engine start on the ground through lift off, climb out, cruise, descent and landing, with separate coverage of dump and unpressurized ventilation, the cabin altitude and differential warning annunciators, and cabin leakage testing. The Keith Products environmental system installed from FL-500 and after is covered alongside the earlier configuration, including the dual zone temperature control, the servo driven air valves, and the maximum cooling, transition and heating modes.

Electrical power is documented at the level of individual circuit paths. Bus distribution for both the 350 triple-fed system and the 300 arrangement is presented with condition diagrams showing what happens as the battery switch, battery bus switch, generator ties and bus sense switch are operated, and what changes during engine start, generator online and external power. Generator control unit functions including voltage regulation, paralleling, reverse current protection, overvoltage protection and cross-start current limiting are explained along with a fault isolation example table. A separate section covers the AC system for the earlier inverter-equipped serial ranges.

Avionics coverage spans both the Pro Line 21 and Pro Line II installations. Display components, control panels, air data computers, attitude heading computers, flux detector units, external compensation units, electronic standby instrument systems, flight guidance computers, servos and servo mounts, autopilot panel and flight control panel are all described, together with the RVSM airworthiness inspection requirements and the static port step height measurement and log.

Model and Serial Number Coverage

The manual addresses the following Beechcraft models and serial number groups:

• 300 (300LW) – FA-1 through 230
• B300 (350) – FL-1 and subsequent
• B300 – FN-1 and subsequent (camera modification)
• B300C – FM-1 and subsequent (cargo door)

Where the 300 and 350 differ, those differences are called out throughout the text and in the schematics and tables. The manual also distinguishes the configurations tied to specific serial groups, including the Pro Line 2 and Pro Line 21 avionics splits, the Keith environmental system from FL-500 and subsequent, and the lead acid battery installation from FL-215 and subsequent.

Understanding the Role of This Manual

This is training and familiarization material rather than a substitute for the approved maintenance publications. Where data in this manual conflicts with the manufacturer’s or FAA publications, the manufacturer’s or FAA publications take precedence. It is at its most useful alongside the Aircraft Maintenance Manual, the Wiring Diagram Manual and the applicable Component Maintenance Manuals, and it is well suited to technicians new to the Super King Air 300 series who need the systems explained before they work on them, as well as to experienced personnel who want a consolidated reference across the airframe, avionics, electrical and environmental systems.

Get the Super King Air 300 and 350 B300 Maintenance Training Manual

This Super King Air 300 and 350 B300 maintenance training manual supports real work on the aircraft: reading and interpreting the ATA chapter structure, understanding how the pressurization and air conditioning systems respond through every phase of flight, tracing bus distribution and generator control circuits, working through avionics and flight guidance architecture, following lubrication and corrosion control schedules, and servicing the ELT and fire protection systems. Having the correct explanations and the correct values in front of you matters, because an incorrectly set bypass valve, a misinterpreted bus tie condition or a missed inspection interval all lead to unnecessary troubleshooting time and avoidable damage.

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