62-22-01: Vacuum Pump Modification
FAA order 62-22-01 is an airworthiness directive in force since October 31, 1962. The FAA's subject line: Vacuum Pump Modification. It names Cessna 150, Cessna 175 Skylark: about 8,921 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: heating, ice protection and utility systems.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- Cessna Aircraft Company
- Models
- 150, 175, 175A, 175B, 175C
- On this site
- Cessna 150 7,995 registered
Cessna 175 Skylark 926 registered
Dates and paperwork
- In force since
- October 31, 1962
- Docket
- Unknown
- Status
- Current
- The FAA's document
- Read the order on the FAA's site
The order itself the regulatory text, as published
Show the full text (1,266 characters)
62-22-01 CESSNA: Amdt. 494 Part 507 Federal Register October 16, 1962. Applies to All Models 150, 175, 175A, 175B, and 175C Aircraft Equipped with Continental Engines O-200-A, GO-300-A and GO-300-C Modified to Incorporate Airborne Mechanisms Model 113A5 Vacuum Pumps (Supplemental Type Certificates Nos. SA1-630 and SA1-610 Amended March 13, 1962, Issued to Airborne Mechanisms Division of Randolph Manufacturing Co.).
Compliance required within the next 10 hours' time in service after the effective date of this AD.
In order to prevent failure of the Airborne Mechanisms Model 113A5 vacuum pump because of improper installation, remove and reinstall the pump as follows:
Mount the pump and then remove it from the engine drive pad. The coupling will remain in the engine spline and the separation will occur between the pump shaft and the coupling. The coupling must then be pressed 1/16 inch further into the engine spline. Reinstall the pump, and insure that the steel cross vanes protrude approximately 1/16 inch from the hub of the coupling.
(Airborne Mechanisms Service Letter No. 4 dated May 15, 1962, entitled "Installation Interference of Model 113A5 Drive Splines" covers this same subject.)
This directive effective October 31, 1962.
Related safety bulletins advice on the same designs, not orders
2017-08-25CE-17-25 · ELEVATOR TORQUE TUBE Inspections for cracks and corrosion in elevator torque tubes
2017-05-11CE-17-12 · Horizontal Stabilizer Elevator Attach Points
2015-10-09CE-16-03 · VERTICAL TAIL Aft Fin Attachment Fitting
2012-01-25CE-12-14 · Three Alternative Methods of Compliance for AD 2011-10-09
2010-07-30CE-10-40R1 · Aircraft Fuel System; water contamination of fuel tank systems on Cessna single engine airplanes
Source: FAA Dynamic Regulatory System, airworthiness directives. The FAA's document is the authority; the register counts are this site's, from the FAA register of October 8, 2026. Connections as data: /graph/directive/62-22-01.json · aircraft systems.