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80-11-04: Cracked Nutplates

FAA order 80-11-04 is an airworthiness directive in force since June 2, 1980. The FAA's subject line: Cracked Nutplates. It names Cessna 150, Cessna 152, Cessna A150, Cessna A152: about 9,912 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: other and general.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Cessna Aircraft Company
Models
150F, 150G, 150H, 150J, 150K, 150L, 150M, 152, A150K, A150L, A150M, A152, F150F, F150G, F150H, F150J, F150K, F150L, F150M, F152, FA150K, FA150L, FA152, FRA150L, FRA150M
On this site
Cessna 150 7,995 registered
Cessna 152 1,637 registered
Cessna A150 232 registered
Cessna A152 48 registered

Dates and paperwork

In force since
June 2, 1980
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 (2,427 characters)
80-11-04 CESSNA: Amendment 39-3782. Applies to the following models and serial number airplanes certificated in all categories: \n\n\nModels\n\n\nSerial Numbers \n150F\n15061533\nthrough\n15064532\n150G\n15064533\nthrough\n15067198\n150H\n15067199\nthrough\n15069308\n150J\n15069309\nthrough\n15071128\n150K\n15071129\nthrough\n15072003\n150L\n15072004\nthrough\n15075781\n150M\n15075782\nthrough\n15079405 \nA150K\nA1500001\nthrough\nA1500226 \nA150L\nA1500227\nthrough\nA1500523 \nA150M\nA1500524\nthrough\nA1500734 \n152\n15279406\nthrough\n15284541\nA152\nA1520735\nthrough\nA1520943 \nF150F\nF150-0001\nthrough\nF150-0067\nF150G\nF150-0068\nthrough\nF150-0219 \nF150H\nF150-0220\nthrough\nF150-0389 \nF150J\nF150-0390\nthrough\nF150-0529 \nF150K\nF15000530\nthrough\nF15000658 \nF150L\nF15000659\nthrough\nF15001143 \nF150M\nF15001144\nthrough\nF15001428 \nFA150K\nFA15000O1\nthrough\nFA1500081 \nFA150L\nFA1500082 \nthrough \nFA1500120 \nFRA150L\nFRA1500121\nthrough \nFRA1500261\nFRA150MFRA1500262\nthrough\nFRA1500336\nF152\nF15201429 \nthrough \nF15201803 \nFA152\nFA1520337 \nthrough \nFA1520372 \n\n\tCOMPLIANCE: Required as indicated unless already accomplished. \n\n\tTo detect cracked NAS 1068A4 nutplates which, if allowed to go undetected, could result in separation of the vertical or vertical and horizontal tail assembly from the airplane, within 100 hours time-in-service after the effective date of this AD, and every 100 hours time-in-service thereafter, accomplish the following: \n\n\tA)\tUsing a suitable light and mirror visually inspect the eight NAS 1068A4 nutplates installed on the Part Number 0432004-9 vertical fin aft attach bracket for cracks in the threaded part (nut body) and/or base of the nutplate and replace any cracked nutplates prior to further flight. \n\n\tB)\tCompliance with this AD is no longer required if the NAS 10684A nutplates are replaced with AN365-428, MS20365-428, MS2l042L4 or MS21044N4 nuts. \n\n\tC)\tAny equivalent method of compliance with this AD must be approved by the Chief, Aircraft Certification Program, Room 238, Terminal Building 2299, Mid-Continent Airport, Wichita, Kansas 67209. \n\n\tNOTE: Cessna Single Engine Service Information Letter SE79-49, Revision # 1, dated April 28, 1980, pertains to the subject. \n\n\tThe AD supersedes AD 78-07-10, Amendment 39-3174 (43 FR 14958, 14959). \n\n\tThis Amendment 39-3782 becomes effective June 2, 1980.

Related safety bulletins advice on the same designs, not orders

2025-12-222025-11 · RUDDER CONTROL SYSTEM
2018-11-21SW-18-31 · NAVIGATION, ATTITUDE, AND DIRECTION DATA SYSTEM
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

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/80-11-04.json · aircraft systems.