Aircraft model

HB-23 Hobbyliner

HB Flugtechnik / HB Aircraft Industries

Airworthiness Directives
2
Manufacturer bulletins
00 Service Bulletins
Last live check
2026-10-012 of 2 re-checked
This page is a reference Record, not an airworthiness or compliance determination. Official FAA and manufacturer sources control over our restatement, subject to governing law. Check applicability, current requirements and incorporated documents before acting. The owner or operator remains responsible for airworthiness and required records under 14 CFR 91.403 and 91.417, as applicable. Terms of Use: /terms.

Also known as: HB-23/2400, Scanliner

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What Airworthiness Directives apply to the HB-23 Hobbyliner

The FAA has published 2 Airworthiness Directives that name the HB-23 Hobbyliner (HB Flugtechnik / HB Aircraft Industries), the earliest in 1996 and the newest on 1996-11-06.

Newest

  1. AD 96-22-16 Airworthiness Directives; HB Aircraft Industries AG HB-23 2400 Hobbyliner/Scanliner Sailpl... 1996-11-06
  2. AD 96-10-02 Airworthiness Directives; HB Flugtechnik GmbH Model HB-23/2400 Sailplanes 1996-05-03

See all 2 directives

The ones owners meet again

  1. AD 96-10-02 Airworthiness Directives; HB Flugtechnik GmbH Model HB-23/2400 Sailplanes 1996-05-03 Repetitive inspection or action

We index directives by model, not by serial number or N-number; the record page and the official document say which serials apply.

How to use this page: check the newest directives at every annual, keep the repetitive items on your inspection calendar, and open the official Federal Register text before any work - our summaries are a reading aid, not a determination of compliance.

Airworthiness Directives

2 records
ADAD 96-22-16HB Aircraft Industries AG HB-23 2400 Hobbyliner/Scanliner Sailplanes1996-12-30Active
AD

96-22-16

FR doc 96-27934 · 61 FR 57322

AD 96-22-16Published 1996-11-06Effective 1996-12-30

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

HB Aircraft Industries AG HB-23 2400 Hobbyliner/Scanliner Sailplanes

Requires inspecting the rudder bearing support bracket for cracks, replacing the bracket if cracked, and modifying the bracket with a third bolt, if no cracks are found.

Full official abstract

Airworthiness Directives; HB Aircraft Industries AG HB-23 2400 Hobbyliner/Scanliner Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain HB Aircraft Industries AG HB-23 2400 Hobbyliner/ Scanliner sailplanes. This action requires inspecting the rudder bearing support bracket for cracks, replacing the bracket if cracked, and modifying the bracket with a third bolt, if no cracks are found. Cracks found in the rudder bearing support brackets prompted this action. The actions specified by this AD are intended to prevent cracks in the rudder bearing support bracket, which could cause loss of control of the rudder and possible loss of the sailplane.

Source: Federal Register document 96-27934, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

ADAD 96-10-02HB Flugtechnik GmbH Model HB-23/2400 Sailplanes1996-06-12Active
AD

96-10-02

FR doc 96-10914 · 61 FR 19815

AD 96-10-02Published 1996-05-03Effective 1996-06-12

FAA rule - 14 CFR 39

FAA rule. Compliance with an applicable AD is required under 14 CFR 39.7. Check its effective date, applicability, compliance times and current status.

HB Flugtechnik GmbH Model HB-23/2400 Sailplanes

Requires inspecting (one time) the elevator control push rod tube for dents or bending and replacing the push rod tube, if damaged, inspecting the elevator control system for incorrect rigging, and repetitively inspecting the…

Full official abstract

Airworthiness Directives; HB Flugtechnik GmbH Model HB-23/2400 Sailplanes

This amendment adopts a new airworthiness directive (AD) that applies to certain HB Flugtechnik GmbH (Flugtechnik) Model HB-23/2400 sailplanes. This action requires inspecting (one time) the elevator control push rod tube for dents or bending and replacing the push rod tube, if damaged, inspecting the elevator control system for incorrect rigging, and repetitively inspecting the threaded adjustable extension joints in the push rod to control lever connection for cracks. If cracks are found, replacing the threaded adjustable joints at both ends of the push rod. Cracking of the threaded adjustable extension joints and incorrect rigging of the elevator control system prompted this AD action. The actions specified by this AD are intended to prevent failure of the elevator control system, which, if not detected and corrected, could result in possible loss of elevator control and loss of the sailplane.

Source: Federal Register document 96-10914, retrieved 2026-08-17 · checked against the live Federal Register record on 2026-10-01

Service Bulletins

0 records

No Service Bulletins in our index yet for this airframe. We only list SBs we have individually sourced from the manufacturer — we never invent one.

This page indexes 2 ADs and 0 SBs from primary sources. The FAA may have issued additional directives for this airframe that are not yet included.

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