AD 75-23-07
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Cessna Aircraft Company | 310Q | Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes |
| aircraft | Cessna Aircraft Company | 310R | Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes |
| aircraft | Cessna Aircraft Company | T310Q | Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes |
| aircraft | Cessna Aircraft Company | T310R | Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes |
Unsafe Condition
Failure of the emergency exit window to function properly due to inadequate design or installation.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Accomplish the window modification, screw inspection, trim modification, and placard installation as per Cessna Service Letter ME75-26 or an approved equivalent method.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
within the next 50 hours' time in service after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Cessna Models 310Q/T310Q (Serial Numbers 310Q0401 thru 310Q1160) and 310R/T310R (Serial Numbers 310R0001 thru 310R0330)
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
Emergency Exit Window
Applicability Source Text
Show captured applicability text from the source AD
AD Final Rules - DRS_75-23-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-23-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes Subject: Emergency Exit Window Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/13/1975 Make: Cessna Aircraft Company Model: 310Q | 310R | T310Q | T310R Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-23-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2418 AD NUMBER: 75-23-07 SUBJECT HEADING: Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes ACTION: SUMMARY: DATES: ; Effective November 13, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-23-07 CESSNA: Amendment 39-2418. Applies to Models 310Q/T310Q (Serial Numbers 310Q0401 thru 310Q1160) and 310R/T310R (Serial Numbers 310R0001 thru 310R0330) airplanes. Compliance: Required as indicated, unless already accomplished. To assure proper operation of the emergency exit window, within the next 50 hours' time in service after the effective date of this AD, accomplish the window modification, screw inspection, trim modification and placard installation, as applicable, in accordance with Cessna Service Letter ME75-26 or later approved revision or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective November 13, 1975. FOOTER:
Document Text
Show stored source text (verify against official source)
AD Final Rules - DRS_75-23-07.html Copy URL Print/Save as PDF Document Versions Feedback Details AD Number: 75-23-07 Document Type: AD Final Rules Docket Number: Unknown Subject Heading: Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes Subject: Emergency Exit Window Status: Current Citation: This information is not available. Citation Publish Date: Effective Date: 11/13/1975 Make: Cessna Aircraft Company Model: 310Q | 310R | T310Q | T310R Product Type: Aircraft Product Subtype: Small Airplane Affected AD: Superseded AD: Affected By: Superseded By: Service/Office: Office of Primary Responsibility: CFR Part Reference: Part 39 Comments: AIRWORTHINESS DIRECTIVES FINAL RULES: 75-23-07 CITATION: This information is not available. PAGE NUMBER: DOCKET NUMBER: Unknown AMENDMENT: 39-2418 AD NUMBER: 75-23-07 SUBJECT HEADING: Airworthiness Directives; Cessna Models 310Q, 310R, T310Q, T310R Airplanes ACTION: SUMMARY: DATES: ; Effective November 13, 1975. ADDRESSES: FOR FURTHER INFORMATION CONTACT: SUPPLEMENTARY INFORMATION: REGULATORY TEXT: 75-23-07 CESSNA: Amendment 39-2418. Applies to Models 310Q/T310Q (Serial Numbers 310Q0401 thru 310Q1160) and 310R/T310R (Serial Numbers 310R0001 thru 310R0330) airplanes. Compliance: Required as indicated, unless already accomplished. To assure proper operation of the emergency exit window, within the next 50 hours' time in service after the effective date of this AD, accomplish the window modification, screw inspection, trim modification and placard installation, as applicable, in accordance with Cessna Service Letter ME75-26 or later approved revision or by any equivalent method of compliance approved by the Chief, Engineering and Manufacturing Branch, FAA, Central Region. This amendment becomes effective November 13, 1975. FOOTER:
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.
Related Airworthiness Directives
2014-03-03
final ruleAirworthiness Directives; Cessna Aircraft Company Airplanes
Unsafe Condition: Accretion of ice on protected and unprotected surfaces during inadvertent icing encounters can result in large increases in stall speed and changes to handling characteristics, leading to aerodynam...
2005-18-20
final ruleAirworthiness Directives; Goodrich De-icing and Specialty Systems “FASTprop” Propeller De-icers
Unsafe Condition: Goodrich De-icing and Specialty Systems 'FASTprop' propeller de-icers becoming loose or debonded, and detaching from propeller blades during operation.
2004-25-16 R1
final ruleAirworthiness Directives; Kelly Aerospace Power Systems Part Number (P/N) 14D11, A14D11, B14D11, C14D11, 23D04, A23D04, B23D04, C23D04, or P23D04 Fuel Regulator Shutoff Valves (Formerly Owned by ElectroSystems, JanAero Devices, Janitrol, C&D Airmotive Products, FL Aerospace, and Midland-Ross Corporation)
Unsafe Condition: Failure of the fuel regulator shutoff valve could result in fuel leakage in aircraft with these combustion heaters, which could result in an aircraft fire.
2005-01-19
final ruleAirworthiness Directives; GARMIN International Inc. GTX 33, GTX 33D, GTX 330, and GTX 330D Mode S Transponders
Unsafe Condition: The GTX 33/33D/330/330D Mode S transponders may detect the S1 (suppression) interrogating pulse below the minimum trigger level (MTL) and, in some circumstances, not reply. This could lead to inacc...