AD 58-04-01

final rule
Data completeness: 60%

Airworthiness Directives; DOUGLAS All DC3 Series Aircraft

AD Number
58-04-01
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Unknown
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company DC3-G102 Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3-G102A Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3-G103A Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3-G202A Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3A-S1C3G Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3A-S1CG Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3A-S4C4G Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3A-SC3G Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3A-SCG Airworthiness Directives; DOUGLAS All DC3 Series Aircraft
aircraft The Boeing Company DC3C-R-1830-90C Airworthiness Directives; DOUGLAS All DC3 Series Aircraft

Unsafe Condition

The passenger entrance door has been altered to hinge at the bottom with installed steps, leading to instances of door opening in flight or inadvertent opening by passengers, resulting in fatal or near fatal incidents.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Install means to safeguard against inadvertent door opening in flight as outlined in CAM 4b.356-2 and -4.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

not later than July 1, 1958

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

Douglas DC3 Series Aircraft with an 'Airstair' type cabin door installation, including models DC3-G102, DC3-G102A, DC3-G103A, DC3-G202A, DC3A-S1C3G, DC3A-S1CG, DC3A-S4C4G, DC3A-SC3G, and others as listed.

AI-generated summary from the source AD text. Verify against the official source before acting.

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for The Boeing Company DC3-G102

Related Airworthiness Directives

98-14-14

final rule

Airworthiness Directives; McDonnell Douglas Model DC-3 and DC-3C Series Airplanes

Unsafe Condition: AFM - Limitations Section - Power Levers

Effective: Aug 11, 1998 Category: aircraft

98-04-35

final rule

Airworthiness Directives; McDonnell Douglas Model DC-3 and DC-4 Series Airplanes

Unsafe Condition: AFM - Limitations Section - Icing

Effective: Mar 25, 1998 Category: aircraft

92-06-15

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DST, Super DC-3, DC-3, DC-3A, DC-3B, DC-3C, and DC-3D series airplanes; all military versions, C-41, C-41A, C-47, C-47A, C-47B, C-48, C-48A, C-49, C-49A, C-49B, C-49C, C-49D, C-49J, C-49K, C-50, C-50A, C-50B, C-50C, C-50D, C-51, C-52, C-52A, C-52B, C-52C, C-53, C-53B, C-53C, C-53D, C-68, C-117A, C-117D, and R4D series airplanes

Unsafe Condition: Prevent Structural Failure Of Wings

Effective: Apr 28, 1992 Category: aircraft

90-05-08

final rule

Airworthiness Directives; MCDONNELL DOUGLAS DC-3, DC-3A, DC-3B, DC-3C, DC-3D, Super DC-3S, C-41, C-47, C-48, C-49, C-50, C-51, C-52, C-53, C-68, C-84, C-117, R4D Series Airplanes

Unsafe Condition: Revise Inspection Program

Effective: Apr 19, 1990 Category: aircraft

View all The Boeing Company ADs →