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Beechcraft 95 Travel Air Model Guide

Beechcraft 95 Travel Air · Model Guide

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Overview

The Beechcraft 95 Travel Air is a four-seat, twin-engine piston airplane built from 1958 to 1968. The type certificate lists two Lycoming O-360-A1A engines at 180 hp each. It also lists a five-place layout when optional equipment is installed. This guide uses only the supplied documents for limits and inspection points.

  • Two Lycoming O-360-A1A engines, 180 hp each, 2700 rpm limit; fuel is 91/96 minimum grade aviation gasoline.
  • Maximum weight is 4000 lb on the Model 95 and 4100 lb on the B95; each baggage compartment is limited to 270 lb.
  • Wing forward spar carry-thru cracking is the headline inspection item; a clean airplane is re-inspected every 500 flight hours.
  • Check cabin door latching: accidents followed doors opening because pilots did not confirm the latch before takeoff.

Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.

Reference only, not for flight. Use the current approved manual for your aircraft. See terms, section 5.

Document

Source

Copy found at sprinkle.com. Sprinkle hosts a reference copy with an added summary, specifications and searchable full text.

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Document details

Type
·
Model Guide
Year
·
2026
File size
·
50 KB
Copy found at
·
sprinkle.com

Specifications & performance

Extracted from this document.

Specifications

Engine power (hp)
·
180
Main tank usable (gal)
·
22
Aux tank capacity (gal)
·
17
Main tank capacity (gal)
·
25
Optional aux tank capacity (gal)
·
31

V-speeds

MANEUVERING_SPEED_KTS
·
139
NEVER_EXCEED_SPEED_KTS
·
208
GEAR_EXTENDED_SPEED_KTS
·
130
FLAPS_EXTENDED_SPEED_KTS
·
113
MAX_STRUCTURAL_CRUISE_SPEED_KTS
·
161

Weight & balance

Max weight (lb)
·
4,000
Max weight b95 (lb)
·
4,100
Rear baggage max (lb)
·
270
Forward baggage max (lb)
·
270
About this document
What engines does the Beechcraft 95 Travel Air use?

The Beechcraft 95 Travel Air is certificated with two Lycoming O-360-A1A engines. Each is limited to 180 hp at 2700 rpm. Minimum fuel grade is 91/96 aviation gasoline.

What is the biggest inspection item on a Beechcraft 95 Travel Air?

The wing forward spar carry-thru structure. For the Beechcraft 95 Travel Air, SB 53-2269 Rev. 2 requires any crack to be repaired with the P/N 58-4008 kit. If no cracks are found, re-inspect every 500 flight hours.

How much can the Beechcraft 95 Travel Air carry in baggage?

On the Beechcraft 95 Travel Air, the forward and rear compartments are each limited to 270 lb. Maximum weight is 4000 lb on the Model 95 and 4100 lb on the B95.

What is the Beechcraft 95 Travel Air Model Guide?

The Beechcraft 95 Travel Air Model Guide is a model guide for the Beechcraft 95 Travel Air, dated 2026.

What year was the Beechcraft 95 Travel Air Model Guide published?

The Beechcraft 95 Travel Air Model Guide — the Beechcraft 95 Travel Air model guide on file — is dated 2026.

Documentation completeness
5/7

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In this document

Limits and loading

Model 95: maximum weight 4000 lb. CG range is +79.4 to +83.0 at 4000 lb and +75.0 to +83.0 at 3480 lb or less. Fuel per side: 25 gal main (22 usable) and 17 gal aux, with an optional 31 gal aux. Oil is 8 qt per engine. Speed limits are CAS: never exceed 208 kt, gear extended 130 kt, flaps extended 113 kt.

Airframe: spar and door

Mandatory Service Bulletin 2269 (SB 53-2269 Rev. 2, incorporated in AD 90-08-14) covers the wing forward spar carry-thru frames on Travel Airs, serials TD-1 through TD-721. Any crack must be repaired with the P/N 58-4008 kit. If there are no cracks, re-inspect every 500 flight hours. The brief ties the cracking to nose gear loads in landing and ground handling. Service Bulletin 2190 requires a cabin door latching placard and a door rigging check.

Gear, brakes and fuel system

Check nose gear and main gear down-lock tension; on twins the positive downlock must be disconnected to test the main gear. Mandatory SB 32-4125 asks Model 95 owners to review records for P/N 35-825094-4 nose gear plunger parts delivered between March 1, 2012 and March 31, 2013. Dukes electric boost pumps with carbon vanes can shatter; check the pump for Nylatron vanes. The D95A uses 7.00-6 main tires and 5.00-5 nose tires.

Safety notes

  • Cabin door opening after takeoff led to loss of control or low-altitude stalls; confirm the door is latched before every takeoff.
  • BPPP recommends against soft-field takeoffs in Travel Airs: lift-off into ground effect is below VMCA, and any power loss means losing directional control.
  • Shattered carbon vanes in older Dukes boost pumps can reach the engine fuel pump and cause reduced or lost engine power.

Full document text

Beechcraft 95 Travel Air Model Guide The Beechcraft 95 Travel Air is a four-seat, twin-engine piston airplane built from 1958 to 1968. The type certificate lists two Lycoming O-360-A1A engines at 180 hp each. It also lists a five-place layout when optional equipment is installed. This guide uses only the supplied documents for limits and inspection points. • Two Lycoming O-360-A1A engines, 180 hp each, 2700 rpm limit; fuel is 91/96 minimum grade aviation gasoline. • Maximum weight is 4000 lb on the Model 95 and 4100 lb on the B95; each baggage compartment is limited to 270 lb. • Wing forward spar carry-thru cracking is the headline inspection item; a clean airplane is re-inspected every 500 flight hours. • Check cabin door latching: accidents followed doors opening because pilots did not confirm the latch before takeoff. Limits and loading Model 95: maximum weight 4000 lb. CG range is +79.4 to +83.0 at 4000 lb and +75.0 to +83.0 at 3480 lb or less. Fuel per side: 25 gal main (22 usable) and 17 gal aux, with an optional 31 gal aux. Oil is 8 qt per engine. Speed limits are CAS: never exceed 208 kt, gear extended 130 kt, flaps extended 113 kt. Airframe: spar and door Mandatory Service Bulletin 2269 (SB 53-2269 Rev. 2, incorporated in AD 90-08-14) covers the wing forward spar carry-thru frames on Travel Airs, serials TD-1 through TD-721. Any crack must be repaired with the P/N 58-4008 kit. If there are no cracks, re-inspect every 500 flight hours. The brief ties the cracking to nose gear loads in landing and ground handling. Service Bulletin 2190 requires a cabin door latching placard and a door rigging check. Gear, brakes and fuel system Check nose gear and main gear down-lock tension; on twins the positive downlock must be disconnected to test the main gear. Mandatory SB 32-4125 asks Model 95 owners to review records for P/N 35-825094-4 nose gear plunger parts delivered between March 1, 2012 and March 31, 2013. Dukes electric boost pumps with carbon vanes can shatter; check the pump for Nylatron vanes. The D95A uses 7.00-6 main tires and 5.00-5 nose tires. Safety notes: • Cabin door opening after takeoff led to loss of control or low-altitude stalls; confirm the door is latched before every takeoff. • BPPP recommends against soft-field takeoffs in Travel Airs: lift-off into ground effect is below VMCA, and any power loss means losing directional control. • Shattered carbon vanes in older Dukes boost pumps can reach the engine fuel pump and cause reduced or lost engine power.