Navigation Pitot Static System Maintenance Section 34-10-00 for Beechcraft 60 Aircraft
Condition NE — Condition disclosed — is shown up front on this listing, along with the exact price, current availability, and what certification paperwork ships with the part, so you can confirm fit and airworthiness before you buy. Full specifications and answers to common questions are below.
What does “New” condition mean?
Request certification documents (8130-3 / EASA Form 1 / C of C)
Description
Overview
The Beechcraft Duke 60 Series Pitot and Static Pressure System Maintenance Manual Section (P/N 34-10-00) provides the authoritative technical guidance for the description, operational principles, troubleshooting, and comprehensive maintenance procedures pertaining to the aircraft's critical pitot and static pressure systems. This specific manual section, identified as Chapter 34-10-00, is an essential resource for A&P mechanics, aircraft owners, and FBO maintenance shops seeking to ensure the accurate function and airworthiness of the aircraft's primary airspeed and altitude sensing components. This vital documentation encompasses all necessary steps for the proper upkeep of the pitot-static system, directly contributing to flight safety and compliance. The information contained within P/N 34-10-00 outlines systematic approaches to identifying and resolving issues, thereby minimizing downtime and ensuring the reliability of instruments dependent on these pressure inputs. Adherence to the procedures detailed in this manual section is paramount for maintaining the operational integrity of the Beechcraft Duke 60 series aircraft.Specifications
As a section within an official aircraft maintenance manual, P/N 34-10-00 does not possess physical specifications such as weight, dimensions, material, or electrical properties. Instead, its "specifications" relate to its content scope and structure:- Document Chapter Designation: 34-10-00
- System Covered: Pitot and Static Pressure System
- Content Focus: System Description, Operation, Troubleshooting, Maintenance Procedures, Inspection Practices
- Information Type: Technical instructions, diagrams (conceptual, within the broader manual), procedural steps, inspection criteria
- Format: Written technical documentation (typically digital or printed as part of a
Specifications
| Part number | 34-10-00 |
|---|---|
| Manufacturer | Beechcraft |
| Condition | NE |
| Airworthiness | Condition disclosed |
| Country of origin | — |
| Lead time | days |
Fits these aircraft
Always verify against your aircraft's IPC before installing.
Frequently asked
Does the Navigation Pitot Static System Maintenance Section 34-10-00 for Beechcraft 60 Aircraft include certification paperwork?
This item is supplied as "Condition disclosed" rather than with full 8130-3 traceability — normal for some condition codes, and it does not mean the part is unusable, only that the paperwork profile differs. Check the listing for exactly what documentation is included, and request any available records before you purchase if your installation requires them.
What condition is this part?
This part is listed in condition NE — Condition disclosed. Condition codes describe how a part reached its current state (for example new, overhauled, serviceable, repaired, or as-removed) and directly affect what paperwork ships with it and how it should be installed. See the Glossary for the full definition of every condition code we use.
How fast does it ship?
This item is currently on backorder, meaning demand has temporarily outpaced our stock and a new shipment is inbound from the manufacturer or our supplier. Request a quote and we will confirm the current estimated delivery window before you commit. If your aircraft is grounded, AOG expedited handling is available on request.
Can I return it?
You may return this item within 30 days of delivery if it is unopened, uninstalled, and in its original packaging. Items that have been installed, powered on, opened hazmat, or separated from an attached 8130-3 tag are non-returnable because their airworthiness status can no longer be confirmed once removed from the part. See our Returns policy for the full process.
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