Manufacturer North American Aviation
Aircraft P-51 Mustang
NAA Part Number 73-33112
Bendix Part Numbers 66584 & 161271
Proper Description Landing Gear Pivot Shaft and Ring Assembly
Location One assembly is located at the top of each P-51 Landing Gear Assembly (P/N 73-33102)
Nickname Pivot Shaft
AC.A. 01-151-L2, 26-April-2017
Nobody wants to witness, participate in, or collapse a landing gear on a Mustang. It is a costly and intensive repair resulting in damage to wing, fuselage, and major components. While the most common reason a Mustang ends up on its belly is pilot error, another factor can be the failure of a landing gear pivot shaft. Fortunately, there are inspections, preventative measures and solutions that almost eliminate the likelihood of this failure mode. AirCorps Aviation in Bemidji MN has compiled a comprehensive explanation of the failure modes of this critical component, with the belief that it is something every pilot and mechanic involved with a Mustang should thoroughly understand.
Read on to learn why…
Pivot shaft is an abbreviated description from the actual component properly named Landing Gear Pivot Shaft and Ring Assembly. This critical component can be described as the point at which the gear leg attaches and rotates for retraction of landing gear into the wing. It also bears the stress of attachment of a landing gear to wing and absorbs the impact of the main wheel tires making contact with the ground upon landing.
The pivot shaft was designed and engineered by North American as P/N 73-33112 on July 5, 1940 and checked / approved about a month later. The NAA drawing identifies two were used per ship on on all P-51 variants, F-51 & A-36 Series aircraft A thru K. On June 6, 1943 the drawing was made inactive and production was handed over to Bendix who produced the part as part number 66584 – a “light shaft” and as 161271 – a “heavy shaft” subsequently discussed.
Mustang expert Mark Tisler explains the three generations of pivot shafts commonly referred to as light, light cut, and heavy.
A light landing gear pivot shaft (P/N – 73-33112 & 66584) has two different generations of production, both of which share a light wall on the interior of the shaft. The first generation “light” pivot shaft has a sharp radius on the thrust face anda 90 degree corner around the radius of the chrome bearing. The second generation “light cut” pivot shaft has had the 90 angle undercut to give it a radius and reduce stress concentration. Tech Order 01-60JE-47 outlines replacement of light shafts with heavy shafts.
A heavy landing gear pivot shaft (P/N 161271) is machined differently on the inside bore of the pivot tube and has increased wall thickness. The pivot shaft thrust face has a large radius cut away to make a symmetrical sloping edge. There are also diagonal bands called “cheeks” on each side of the pivot shaft and an additional bead around the base to reduce the propensity to crack.
In overhauling 10 sets of landing gear over the past two years, AirCorps has established a standard process of handling these increasingly rare, high-value components. The importance of recording serial numbers, inspecting for airworthiness by checking for cracks, straightness, twist, and re-plating, if necessary, cannot be understated.
To ensure proper inspection, the pivot shaft must be removed from the aircraft to see cracks in the radius. Dye penetrant has been found to be insufficient in locating cracks meaning the pivot shaft must undergo magnetic particle inspection. A thorough dimensional analysis should be done to check the straightness and location of splines relative to the angle of the gear leg receptacle hole. Also measure for elongation of the top and bottom of the gear leg receptacle hole and the outer diameter (O.D.) of chromed surfaces, along with checking for flaking of chrome which is an indication of rust underneath.
Therefore, AirCorps recommends, Following guidance given Military T.O. 01-60JE-47 to replace “light weight” shafts 73-33112 & 66584 as soon as possible or at next inspection. If “light weight” shafts are operated, we recommend immediate magnaflux inspection if not previously inspected by removal and magnaflux. We also recomm
Pivot shafts are prone to cracks in a number of areas and require consistent inspection regardless of type. Experience in inspecting pivot shafts has identified the propensity for cracking in a few select areas:
Cracking location # 1 – Exterior Corner at intersection of pivot and landing gear receptacle on both light and heavy pivot shafts.
Location of external Pivot Shaft Cracking – photo – AirCorps Aviation
Heavy landing gear pivot shaft cracking circled in red. Thank you to Gary Norville for photo contribution
Cracking location #2 – Radius of thrust face can be up to ¼” from face edge of internal radius.
To ensure the landing gear outer cylinder piston tube (Bendix Part numbers 67428 / 67427) will fit the pivot shaft landing gear leg receptacle hole, measure for elongation of the internal dimensions.
Twist of spline shafts is an often overlooked element of inspection that can affect the landing gear not properly engaging and uplocking when retracted. Splines will twist under 73-33116 bushing which is not visible without careful inspection.
Heavy shafts are interchangeable with lights, but the bearings in the gear casting in the wing need to be chamfered to accept heavy shafts. Heavy pivot shafts (161271) require the use of bushing 122-33109 in the landing gear casting in wing. Damage to casting and shaft will occur if a 161271 shaft is installed in a casting with 73-33109 bushing.
If you’re looking for replacement shafts, prior to purchasing any original Bendix components ensure airworthiness by inspecting for cracks, straightness, and that the bore for the gear leg is not out of round. While original pivot shafts are quite difficult source right now, Roush Aviation has completed PMA approval and production of replacement pivot shafts that have improvements in failure areas.
AirCorps is available to perform inspections, answer questions, and perform modifications and services related to pivot shafts and landing gear. AirCorps has overhauled countless sets of P-51 landing gear and has the P-51 Landing gear on its Repair Station Capabilities list.
Contact us for more info on ways we can assist with your project!
Vice President of Restoration
Mark Tisler achieved his Airframe & Powerplant in 1985 after graduating college with a degree in Agricultural Mechanization. In 1988, Mark began working with Gerry Beck at Tri-State Aviation in Wahpeton. His love of warbirds didn’t stop at just airframes, his humble and technical expertise make him a favorite of operators, veterans, and aircraft owners. Tisler has worked on 13 major P-51 restorations and everything from a Stearman to a Corsair. This AirCorps co-owner helps lead the award winning Restoration & Maintenance departments which work not only on resurrecting historic aircraft but also prepping restored aircraft for flight readiness. This capable team does inspections, light and heavy maintenance, and component overhaul / repair for a variety of aircraft.
This week Mark got a TBM-3E Avenger ready for a successful ferry flight to Bemidji. Next week he will fly out to the East Coast to assist in rigging landing gear in a P-51D.
Contact us for more info on ways we can assist with your project!
AirCorps Library – P-51 Mustang Resources
Aircraft Inspection & Maintenance Guide – P-51, 00-20A-2-P-51, 7-Nov-1947
T.O. 01-60JE-2, Maintenance Instructions for F-51D, F-51M, ZF-51K, and TF-51D, T.O. No. 1F-51D-2 (AN 01-60JE-2), 30-Nov-1956)
Maintenance Instructions – Cavalier Mustang – F-51D, T.0. 1F-51D-2, 27-Sept-1968
WHILE AIRCORPS (VENDOR) BELIEVES THAT THE INFORMATION CONTAINED THEREIN IS ACCURATE AND CORRECT, VENDOR DOES NOT WARRANT THE ACCURACY OR THE CORRECTNESS OF ANY DRAWINGS, MANUALS, OR THE INFORMATION CONTAINED THEREIN. THE INFORMATION, DRAWINGS AND REFERENCE MATERIAL ARE SUPPLIED TO THE CUSTOMER ON AN “AS IS” BASIS WITHOUT ANY WARRANTIES, EXPRESS OR IMPLIED, INCLUDING, BUT NOT LIMITED TO, ANY WARRANTIES OF MERCHANTABILITY OR FITNESS FOR ANY PARTICULAR PURPOSE. ALL WORK SHOULD BE COMPLETED IN ACCORDANCE WITH FAA REGULATIONS AND APPROVED DATA.