Airworthiness Directive 02-11803
recurringAirworthiness Directives; Boeing Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F Series Airplanes
What this AD requires
This document corrects information in an existing airworthiness directive (AD that applies to certain Boeing Model 727, 727C, 727-100, 727-100C, 727-200, and 727-200F series airplanes. That AD currently requires repetitive inspections to find cracking of the lower skin panel at the lower row of fasteners in certain lap joints of the fuselage, and repair, if necessary. This document corrects a typographical error in the supplemental type certificate (STC) number specified in paragraph (i) of that AD. This correction is necessary to ensure that the correct STC number is specified and operators of affected airplanes are advised of all applicable actions.
Which aircraft AD 02-11803 applies to
Whether AD 02-11803 actually applies to your aircraft (by serial and installed parts) and whether it’s already complied with comes from that aircraft’s records.
How AD compliance is recorded
A valid compliance record (14 CFR 43.9) states:
Tailplate reads a tail number’s logbooks and matches every applicable AD — including this one — to its compliance evidence, with recurring next-due dates computed.
Look up a tail number →Read the full directive (Federal Register)Applicability is derived from the FAA directive corpus and is advisory, not a legal airworthiness determination. Compliance is established only from an aircraft’s actual records.