MAULE M-5-210C Model Guide
MAULE M-5-210C · Model Guide
Overview
MAULE M-5-210C is a single-engine piston aircraft from Maule. The supplied documents give no variant-specific performance, weights or seat count. They cover a wing lift strut airworthiness directive and a sunvisor kit. The M-5 family is listed at up to 4 passengers, up to 500 nm range, up to 150 kt cruise and up to 20000 ft ceiling.
- Wing lift struts are the main inspection item: the AD covers the M-5-210C, all serial numbers, with strut P/N 2079E or 2080E fitted.
- Strut inspections repeat at intervals not to exceed 24 calendar months, unless sealed struts P/N 2200E and 2201E are fitted with no holes drilled.
- No variant-specific specs, weights or seat count were supplied. Verify these against the aircraft's own documents.
- A Rosen sunvisor kit under STC SA01251SE lists the M-5-210C as an applicable aircraft.
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.
Document details
- Type ·
- Model Guide
- Year ·
- 2026
- File size ·
- 46 KB
- Copy found at ·
- sprinkle.com
Does the wing strut AD apply to the MAULE M-5-210C?
Yes. The MAULE M-5-210C is named in the AD, all serial numbers, if it has strut P/N 2079E or 2080E (or FAA-approved equivalents). The AD does not apply to airplanes with four sealed struts, P/N 2200E and 2201E.
How often must the MAULE M-5-210C struts be inspected?
For the MAULE M-5-210C, repeat inspections are due at intervals not to exceed 24 calendar months if no dents or corrosion are found. They may end after new sealed struts are installed, provided no holes are drilled in them.
How many people does the MAULE M-5-210C carry?
The documents give no seat count for the MAULE M-5-210C itself. The M-5 family is listed at up to 4 passengers, so confirm the exact figure in the aircraft's own documents.
What is the MAULE M-5-210C Model Guide?
The MAULE M-5-210C Model Guide is a model guide for the MAULE M-5-210C, dated 2026.
What year was the MAULE M-5-210C Model Guide published?
The MAULE M-5-210C Model Guide — the MAULE M-5-210C model guide on file — is dated 2026.
Common. More common than 92% of the aircraft models we track.
Most owners only have the POH. Here's the essential set for the MAULE M-5-210C.
- Pilot's Operating Handbook / AFM
- Checklist
- Maintenance Manual
- Parts Catalog (IPC)
- Systems & Wiring
- Service Bulletins on file
- Type Certificate (TCDS)
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In this document
Wing lift strut AD
Czech AD CAA-AD-3-062R1/98 reissues FAA AD 98-15-18, effective 9 September 1998. It aims to prevent corrosion failure of the struts, which could let the wing separate. Struts are removed and inspected per Maule SB No. 11 of October 30, 1995. A dent or external corrosion means installing airworthy inspected struts or new sealed struts.
What to check when buying
Ask for the logbook entry of the strut inspection, which the AD requires. Confirm the strut part numbers. Sealed struts P/N 2200E and 2201E show two raised weld spots on the upper end, below the serial number plate. The upper cuff must be removed to see them. Holes drilled for cuffs or door clips bring back the 24-month inspections.
Sunvisor kit option
The Rosen Tube Mount NSA Sunvisor System (kit R1710000, STC SA01251SE) lists the M-5-210C as an applicable aircraft. Installation takes approximately 1/2 to 1 hour. The manual lists no airworthiness limitations. Attaching hardware should be checked for security at least at each annual inspection.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Safety notes
- Corrosion of the wing lift struts could eventually result in the wing separating from the airplane, according to the AD.
- An ultrasonic strut reading of 0.024 inch or less requires strut replacement before further flight.
- The AD applies even if the airplane has been modified, altered or repaired. An affected owner must request approval of an alternative method of compliance.
Summary written by AI from the source document. Check the original before relying on it. See which parts of Sprinkle are written by AI.
Full document text
MAULE M-5-210C Model Guide MAULE M-5-210C is a single-engine piston aircraft from Maule. The supplied documents give no variant-specific performance, weights or seat count. They cover a wing lift strut airworthiness directive and a sunvisor kit. The M-5 family is listed at up to 4 passengers, up to 500 nm range, up to 150 kt cruise and up to 20000 ft ceiling. • Wing lift struts are the main inspection item: the AD covers the M-5-210C, all serial numbers, with strut P/N 2079E or 2080E fitted. • Strut inspections repeat at intervals not to exceed 24 calendar months, unless sealed struts P/N 2200E and 2201E are fitted with no holes drilled. • No variant-specific specs, weights or seat count were supplied. Verify these against the aircraft's own documents. • A Rosen sunvisor kit under STC SA01251SE lists the M-5-210C as an applicable aircraft. Wing lift strut AD Czech AD CAA-AD-3-062R1/98 reissues FAA AD 98-15-18, effective 9 September 1998. It aims to prevent corrosion failure of the struts, which could let the wing separate. Struts are removed and inspected per Maule SB No. 11 of October 30, 1995. A dent or external corrosion means installing airworthy inspected struts or new sealed struts. What to check when buying Ask for the logbook entry of the strut inspection, which the AD requires. Confirm the strut part numbers. Sealed struts P/N 2200E and 2201E show two raised weld spots on the upper end, below the serial number plate. The upper cuff must be removed to see them. Holes drilled for cuffs or door clips bring back the 24-month inspections. Sunvisor kit option The Rosen Tube Mount NSA Sunvisor System (kit R1710000, STC SA01251SE) lists the M-5-210C as an applicable aircraft. Installation takes approximately 1/2 to 1 hour. The manual lists no airworthiness limitations. Attaching hardware should be checked for security at least at each annual inspection. Safety notes: • Corrosion of the wing lift struts could eventually result in the wing separating from the airplane, according to the AD. • An ultrasonic strut reading of 0.024 inch or less requires strut replacement before further flight. • The AD applies even if the airplane has been modified, altered or repaired. An affected owner must request approval of an alternative method of compliance.