90-26-05: Seat Pan
FAA order 90-26-05 is an airworthiness directive in force since December 26, 1990. The FAA's subject line: Seat Pan. It names Boeing 737, Boeing 757: about 3,336 aircraft on the U.S. register today across them, though an order usually covers particular versions or serial numbers rather than every one. System: cabin, seats and restraints.
What it applies to as the FAA lists it
- Kind of product
- Aircraft
- Makes
- The Boeing Company
- Models
- 737-300 Series, 737-400 Series, 737-500 Series, 757-200 Series
- On this site
- Boeing 737 2,896 registered
Boeing 757 440 registered
Dates and paperwork
- In force since
- December 26, 1990
- Docket
- 90-NM-261-AD
- 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 (2,765 characters)
90-26-05 BOEING: Amendment 39-6832. Docket No. 90-NM-261-AD. \n\n\tApplicability: Model 737-300, 737-400, and 737-500 series airplanes, and Model 757- 200 series airplanes; equipped with Transaero P/N 91466 series double flight attendant seats; certificated in any category. \n\n\tCompliance: Required as indicated, unless previously accomplished. \n\n\tTo prevent injury to flight attendants, accomplish the following: \n\n\tA.\tWithin 21 days after the effective date of this AD, inspect the front edge of the affected seat pans for areas of abnormal flexibility when hand pressure is applied perpendicular to the seat pan, and for permanent deflection or misfair of the seat pan edge when stowed.\n\n\t\t1.\tIf no obvious damage is detected, repeat the inspection at intervals not to exceed 30 days.\n\n\t\t2.\tIf any of the above conditions are found, prior to further flight, accomplish one of the following: \n\n\t\t\ta.\tInstall a placard stating that the damaged seat is not to be occupied; orb.\tReplace the seat pan with a new seat pan of the same part number, and continue to inspect at intervals not to exceed 30 days thereafter in accordance with paragraph A. of this AD; or \n\n\t\t\tc.\tRepair the seat pan in a manner approved by the Manager, Seattle Aircraft Certification Office, and continue to inspect at intervals not to exceed 30 days in accordance with paragraph A. of this AD. \n\n\tB.\tThe actions required by paragraph A. of this AD may be terminated upon replacement of affected seat pans with seat pans that have been approved by the Manager, Seattle Aircraft Certification Office, FAA, Transport Airplane Directorate. \n\n\tC.\tAn alternate means of compliance or adjustment of the compliance time, which provides an acceptable level of safety, may be used when approved by the Manager, Seattle Aircraft Certification Office (ACO), FAA, Transport Airplane Directorate. \n\n\tNOTE: The request should be submitted directly to the Manager, Seattle ACO, and a copy sent to the cognizant FAA Principal Inspector (PI). The PI will then forward comments or concurrence to the Seattle ACO. \n\n\tD.\tSpecial flight permits may be issued in accordance with FAR 21.197 and 21.199 to operate airplanes to a base in order to comply with the requirements of this AD. \n\n\tAll persons affected by this directive who have not already received the appropriate service information from the manufacturer may obtain copies upon request to Boeing Commercial Airplane Group, P.O. Box 3707, Seattle, Washington 98124. This information may be examined at the FAA, Northwest Mountain Region, Transport Airplane Directorate, 1601 Lind Avenue S.W., Renton, Washington. \n\n\tThis amendment (39-6832, AD 90-26-05) becomes effective on December 26, 1990.
Related safety bulletins advice on the same designs, not orders
2026-10-232026-18 · NOSE/TAIL LANDING GEAR, Installation of AeroControlex STC ST01255CH may allow water to leak and freeze on...
2026-10-032026-17 · VNAV Approach Disconnect Following Missed Approach, Anomaly on Airplanes with FMC U14.0/14.1
2026-04-062026-09 · HYDRAULIC POWER, Hydraulic Power Transfer Unit System
2026-01-082026-01 · PITOT/STATIC ANTI-ICE SYSTEM
2025-09-082025-08 · INDICATING/RECORDING SYSTEM, Erroneous Illumination of Cabin Altitude Warning Lights in High Altitude Landing Mode
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 November 6, 2026. Connections as data: /graph/directive/90-26-05.json · aircraft systems.
