AD 96-07-14
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | EADS CASA | C-212-CB | CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF Series Airplanes |
| aircraft | EADS CASA | C-212-CC | CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF Series Airplanes |
| aircraft | EADS CASA | C-212-CD | CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF Series Airplanes |
| aircraft | EADS CASA | C-212-CE | CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF Series Airplanes |
| aircraft | EADS CASA | C-212-CF | CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF Series Airplanes |
Unsafe Condition
Reduced structural integrity of the airplane due to potential cracking in the horizontal stabilizer-to-fuselage attach fittings and Principal Structural Elements (PSE) as defined in CASA SID C-212-PV-01-SID.
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Required Actions
Replace horizontal stabilizer-to-fuselage attach fittings with specified part numbers for Model C-212-CB series. Incorporate a revision into the maintenance inspection program for all models to inspect PSE at the later of 20,000 total landings/20,000 hours or 9 months after AD effective date. Report inspection results to CASA within 10 days. Repair or replace cracked structure before further flight.
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Compliance Time
Required as indicated, unless accomplished previously. For Model C-212-CB: prior to 16,500 total landings or within 6 months after AD effective date, whichever is later. For inspections: by later of 20,000 total landings/20,000 hours or 9 months after AD effective date.
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Affected Aircraft
CONSTRUCCIONES AERONAUTICAS, S.A. (CASA) Model C-212-CB, -CC, -CD, -CE, and -CF series airplanes, certificated in any category.
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
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