AVIATION / Airframe & controls / REVIEWED 2026-09-11
Provide stability and control at the tail.
The tail combines fixed or trimmable stabilizers with separate elevators and rudder. Structural capability is concentrated in program-specific work packages.
Program applicability is stated for each listing. 737NG, 737 MAX, and other aircraft examples are distinct configurations; listed products are not automatically interchangeable or approved for installation.
The aerostructures portfolio names empennage work on Gulfstream G650 and HondaJet. [1]
Other aircraft — business jets; no 737 applicability established [1]
Contact the manufacturer or aircraft OEM for the applicable approved program and configuration. This is an inquiry route, not an assertion of stock, price or installation eligibility.
Designs and manufactures horizontal and vertical stabilizer assemblies. [2]
General empennage capability; 737 applicability unverified [2]
Contact the manufacturer or aircraft OEM for the applicable approved program and configuration. This is an inquiry route, not an assertion of stock, price or installation eligibility.
The cited disclosure identifies 787 horizontal-stabilizer and A220 horizontal/vertical-tail work. [3]
Other aircraft — 787/A220; no 737 applicability established [3]
Contact the manufacturer or aircraft OEM for the applicable approved program and configuration. This is an inquiry route, not an assertion of stock, price or installation eligibility.
A company address is shown separately from a published factory location. Request the manufacturing site and lot traceability for the exact part when sourcing.
Separate tail structure, trim mechanism, rudder and elevator responsibilities.
Area, sweep and incidence must match the aircraft configuration.
Compare vertical, lateral and torsional load cases at fuselage hard points.
Tail dynamics depend on hinge balance and the entire aircraft.
Confirm stabilizer travel, clearances and stops where trim is provided.
Compare balance weights and delivered mass distribution.
Review composite protection, metal joints and corrosion control.
Check access to internal structure, hinges and approved repair schemes.
Specifications belong to the named product and configuration.
Public source establishes the product/work package, but does not publish comparable component mass, load limits or envelope. Request controlled drawings and configuration data through the aircraft program.
Public source establishes the product/work package, but does not publish comparable component mass, load limits or envelope. Request controlled drawings and configuration data through the aircraft program.
Manufacturer pages and technical documents support the linked claims. A review date is not a publication date or stock check.
Fuselage, wing, control-surface and empennage capabilities; named business-jet tail references.
Accessed 2026-09-10Fuselage, wing, stabilizer and secondary-structure engineering and production.
Accessed 2026-09-10787 fuselage and stabilizer, 767 wing movables and empennage, ATR structures; historical program disclosure.
Accessed 2026-09-10