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FAA orders · airworthiness directive · historical

2003-19-14: Fuselage

FAA order 2003-19-14 is an airworthiness directive in force since October 20, 2003. The FAA's subject line: Fuselage. It names Burkhart Grob G-103: about 71 aircraft on the U.S. register today, though an order usually covers particular versions or serial numbers rather than every one. System: instruments and avionics.

What it applies to as the FAA lists it

Kind of product
Aircraft
Makes
Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und; Burkhart Grob Luft-Und
Models
G103 Twin Astir, G103 Twin II, G103A Twin II Acro, G103C Twin III Acro
On this site
Burkhart Grob G-103 71 registered

Dates and paperwork

In force since
October 20, 2003
Published
September 30, 2003 (signed September 19, 2003)
Docket
2003-CE-35-AD
Replaced by
2003-19-14 R1
Status
Historical
The FAA's document
Read the order on the FAA's site

The FAA's summary their words, unchanged

The FAA is adopting a new airworthiness directive (AD) for all BURKHART GROB LUFT--UND RAUMFAHRT GmbH & CO KG (GROB) Models G103 TWIN ASTIR, G103 TWIN II, G103A TWIN II ACRO, and G103C TWIN III ACRO sailplanes. This AD requires you to modify the airspeed indicators and install a flight speed reduction placard and an aerobatic maneuver restriction placard (as applicable). This AD also requires you to revise the flight and maintenance manual. This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the possibility of damage to the fuselage during limit load flight due to inadequate safety margins designed into the fuselage. Such a condition could result in reduced structural integrity of the fuselage and lead to loss of control of the sailplane.

The order itself the regulatory text, as published

Show the full text (3,158 characters)
2003-19-14 Burkhart Grob Luft--und Raumfahrt Gmbh & Co KG: Amendment 39-13317; Docket No. 2003-CE-35-AD. When Does This AD Become Effective? (a) This AD becomes effective on October 20, 2003. What Other ADs Are Affected By This Action? (b) None. What Sailplanes Are Affected by This AD? (c) This AD affects the following sailplane models and serial numbers that are certificated in any category: Model Serial Nos. G103 TWIN ASTIR G103 TWIN II G103A TWIN II ACRO G103C TWIN III ACRO All All All All What Is The Unsafe Condition Presented in This AD? (d) This AD is the result of mandatory continuing airworthiness information (MCAI) issued by the airworthiness authority for Germany. We are issuing this AD to prevent the possibility of damage to the fuselage during limit load flight due to inadequate safety margins designed into the fuselage. Such a condition could result in reduced structural integrity of the fuselage and lead to loss ofcontrol of the sailplane. What Must I Do To Address This Problem? (e) To address this problem, you must accomplish the following: Actions Compliance Procedures Modify the airspeed indicators; install flight speed, aerobatic maneuver, and load limit restriction placards (as applicable); and revise the flight and maintenance manual (as applicable). Within the next 10 hours time-in-service (TIS) after October 20, 2003 (the effective date of this AD). Per GROB Alert Service Bulletin No. ASB315-63/2, dated June 2, 2003, and Alert Service Bulletin No. ASB315-64, dated June 30, 2003. What About Alternative Methods of Compliance? (f) You may request a different method of compliance or a different compliance time for this AD by following the procedures in 14 CFR 39.13. Send your request to the Manager, Standards Office, Small Airplane Directorate, FAA. For information on any already approved alternative methods of compliance, contact Gregory A. Davison,Aerospace Engineer, FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 64106; telephone: (816) 329- 4130; facsimile: (816) 329-4090. Is There Material Incorporated by Reference? (g) You must do the actions required by this AD must be done in accordance with GROB Alert Service Bulletin No. ASB315-63/2, dated June 2, 2003, and GROB Alert Service Bulletin No. ASB315-64, dated June 30, 2003. The Director of the Federal Register approved the incorporation by reference of this service bulletin in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. You may get a copy from GROB Luft-und Raumfahrt, Lettenbachstrasse 9, D-86874 Tussenhausen- Mattsies, Germany; telephone: 011 49 8268 998139; facsimile: 011 49 8268 998200; email: [email protected]. You may review copies at FAA, Central Region, Office of the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 64106; or at the Office of the Federal Register, 800 North Capitol Street, NW., suite 700, Washington, DC. Is There Other Information That Relates to This Subject? (h) German AD 2003-185, dated May 30, 2003, and German AD 2003- 231, dated July 16, 2003 also address the subject of this AD.

Related safety bulletins advice on the same designs, not orders

2007-10-18CE-08-01 · Fuselage, Wing, & Stabilizer Structure
2006-06-21CE-06-49 ·

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/2003-19-14.json · aircraft systems.