# SDR HEEA955737

- Type: Service difficulty report (as reported; unverified)
- Difficulty date: September 12, 1995
- Submitted: March 26, 2000
- Operation: General aviation
- Make and model: Bell 212
- Registry model: [Bell 212](https://openairdocs.org/model/bell-212) (OpenAirDocs)
- System (JASC): [5330 · Fuselage Main, Plate/Skin](https://openairdocs.org/jasc/5330)
- Part: Panel Assy
- Part number: 205032814051
- Condition: Mis Mfg
- Location: Boom Sta 101
- Stage of operation: IN
- Nature of condition: W
- Precautionary procedure: K
- FAA source: FAA Service Difficulty Reporting System (https://sdrs.faa.gov/)
- Page: https://openairdocs.org/sdr/HEEA955737

## Discrepancy

CORE ON PANEL IS TOO NARROW LEAVING APPROXIMATELY 1/2" TO 5/8" SPACE BETWEEN CORE TRANSITION AREA AND LOWER LONGERON FLANGES ON BOTH L/H AND R/H SIDES.  PANEL OUTER DIMENSION IS TOO SHORT, NOT LEAVING ENOUGH MATERIAL TO GET PROPER EDGEDISTANCE ON RIVETS FOR TOP FLANGES OF L/H AND R/H LONGERONS.  CORE AREAS ON INSIDE OF PANEL ARE MISPOSITIONED CAUSING PANEL TO NOT FIT BETWEEN ATTACHMENT FLANGES AT BOOM STATION 101.38.

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