# Airworthiness Directives; Boeing Model 747-100, -200B, -200F, -200C, -100B, -300, -100B SUD, -400, -400D, and -400F Series Airplanes; and Model 747SR Series Airplanes
> **Rule** · Final rule; request for comments. · Published 2003-04-23 · Effective 2003-05-08 · 68 FR 19937
## Document
- **Document number:** 03-9691
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 68 FR 19937
- **Publication date:** 2003-04-23
- **Effective date:** 2003-05-08
- **FAA docket:** Docket No. 2003-NM-15-AD
## Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to all Boeing Model 747-100, -200B, -200F, -200C, -100B, -300, -100B SUD, -400, -400D, and -400F series airplanes; and Model 747SR series airplanes. This action requires repetitive inspections to detect discrepancies of the actuator attach fittings of the inboard and outboard flaps, and follow-on and corrective actions as necessary. This action is necessary to detect and correct cracking and other damage of the actuator attach fittings of the trailing edge flaps, which could result in abnormal operation or retraction of a trailing edge flap, and possible loss of controllability of the airplane. This action is intended to address the identified unsafe condition.

## Source
- [Federal Register document](https://www.federalregister.gov/documents/2003/04/23/03-9691/airworthiness-directives-boeing-model-747-100--200b--200f--200c--100b--300--100b-sud--400--400d-and)
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