Issued: December 01, 2010 226-56-011

Page 1 of 8

SERVICE BULLETIN

SA226 SERIES

Windows

Inspection of Cockpit Heated Windshields (P/N 26-21126 and 27-19442)

1. PLANNING INFORMATION

A. Effectivity:

All SA226 Series Aircraft

B. Reason:

Over a 2.5 year calendar period, the window manufacturer and repair facility has

repaired 19 windows with inner glass ply fracture. The manufacturer deems inner

glass ply failure as critical to the structural integrity of the window.

C. Description:

This service bulletin implements repetitive inspections on heated glass windshields (P/N 26-21126, 27-19442) and if noted damage is found, replacing the

affected window.The inspections defined in this service bulletin are intended to

identify glass shear and / or interlayer cracking that may be present in the

windshield assembly. These inspections are focused on the areas adjacent to the

windshield metal insert with particular attention to areas not directly adjacent to

the windshield heating grid. (See Figures 1 and 2)

D. Compliance:

Mandatory

E. Approval:

FAA Approved for Engineering Design.

F. Manpower:

M7 Aerospace estimates 2 manhours (1 manhour per window) to accomplish this

service bulletin. This estimate is for direct labor only accomplished by an experienced

crew. Adjust the estimate with operator task hour data if necessary.

G. Material-Cost and Availability:

(1) Cost:

Because of pricing fluctuations, individual cost estimates should be obtained from

your normal material procurement outlet.

(2) Availability:

Not applicable.
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SERVICE BULLETIN

SA226 SERIES

H. Tooling-Price and Availability:

Not applicable

I. Weight and Balance:

Not affected

J. Reference:

None

NOTE: References are for manufacturers’ use only.

K. Other Publications Affected:

SA226 Series Maintenance Manual.

2. ACCOMPLISHMENT INSTRUCTIONS

A. Perform inspections in 2.B. in accordance with intervals called out in Table 001.

B. Inspection:

(1) Determine Time in Service of the LH and RH cockpit heated windshields.

(2) With the use of maintenance stands or ladders, obtain adequate access to

perform a detailed visual inspection of the entire periphery of the LH and RH

cockpit heated windshields from the outside of the aircraft.

(3) Ensure that the surface of the glass is free from dirt, oil, or other contaminants.

Remove dirt and other substances from glass surface with clean water. Wash with

mild soap and water or a 50/50 solution of isopropyl alcohol and water. Do not use

any abrasive materials or any strong acids or alkalines. When wiping the surface,

use a soft cloth or sponge and use a straight rubbing motion. Rinse thoroughly and

dry; do not apply wax.

(4) With the use of a flashlight and 10X magnification, perform a detailed visual

examination of the inner glass ply, the interlayer, and the outer glass ply in an area

defined by the inner edge of the metal insert (see Figure 2) and extending inward

3.0 inches toward the center of the windshield. Inspect for indications of delamination, interlayer cracking, and / or glass shear. The viewing angle for the

inspection should extend from a line of sight that is perpendicular to the surface

of the glass to an angle extending approximately 45 degrees to either side of this

plane as shown in Figure 4.

(5) For indications of glass shear or interlayer cracking, the windshield must be

repaired / replaced by an FAA approved vendor prior to further flight.
Issued: December 01, 2010 226-56-011

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SERVICE BULLETIN

SA226 SERIES

(6) For removal and installation instructions for heated windshields refer to chapter

56-10-00 of the SA226 Series Maintenance Manual.

C. Complete aircraft records according to 14 CFR 43.9.

D. Complete and mail Service Bulletin compliance form.

3. DEFINITIONS AND ACCEPTANCE CRITERIA - WINDSHIELDS

A. Definitions

Delamination Delamination - The disbonding of either the inner and / or the outer

glass component from the adjacent interlayer material. It appears as

a clear bubble that is flat and smooth with a circular or irregular shape.

Glass Shear A fracturing of portions of the glass material adjacent to the interlayer

material. It can extend to significant areas of failure parallel to the

glass surface. Glass shear can be similar in appearance to delamination, but can be differentiated from delamination by "rainbow"

colors, distinct shear planes and crushed contours displayed as a

white "frosting" in appearance. Inspection for glass shear can be

aided by the use of and LED type flashlight, particularly in highlighting

the "rainbow" colors associated with glass shear.

THRESHOLD/REPETITIVE INSPECTION INTERVALS

FOR 26-21126 AND 27-19442 HEATED WINDSHIELDS

TABLE 001

 * TIME IN SERVICE

 B 1100 to 5000 3 weeks from publish Every 100 hours *TIS until

 date of SB. window reaches category C.

 C Greater than 5000 3 weeks from publish Every 50 hours *TIS.

 date of SB.

 Category Hours *TIS on each Threshold Inspection Repetitive Inspection date/

new or repaired date/time (on or before) time (on or before)

windshield

 A Less than 1100 3 weeks from publish Every 150 hours *TIS until

 date of SB. window reaches category B.
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SERVICE BULLETIN

SA226 SERIES

Interlayer Cracking A narrow break, fissure, or separation in the interlayer material.

Interlayer cracking normally occurs adjacent to the glass components

along the inboard edge of the metal insert and also at the interlayer

release boundary. When viewed from the edge of the crack (see

Figure 3), interlayer cracking is indicated as a prominent black line

type crack / tear through the thickness of the interlayer. When viewed

looking at the plane of the crack (see Figure 3), striations in the

interlayer can be observed.

B. Critical Area Inspection – Glass Windshields

NOTE: The critical area is the area of the laminated glass windshields used for

taxiing, takeoff, climb, cruise, and landing measured 2.0 in (50.8 mm) from

inner edge of retainer, around entire periphery towards center of windshield,

except measured 0.5 in (12.7 mm) around the temperature sensors.

(1) Delamination

(a) Cloudy or milky appearance in the delamination indicates moisture or solvent penetration. Windshields with this condition should be replaced at

the earliest opportunity.

(b) Delaminated areas characterized by irregular or jagged boundaries indi- cate uneven separation of the vinyl and glass.

(c) Replace windshield if one of the following conditions are noted:

1 Area of vision required for safe operation is affected (pilot's discretion).

2 Windshield heat system inoperative.

(2) Glass Shear

(a) Glass Shear in any portion of the windshield requires replacement prior to further flight.

(3) Interlayer Cracking

(a) Interlayer Cracking in any portion of the windshield requires replacement prior to further flight.

C. Semi-Critical Area Inspection – Glass Windshield

NOTE: Semi-Critical areas are the perimeter of the glass windshield, within the 2.0 in

(50.8 mm) region from the inner edge of the retainer.

(1) Delamination

(a) Cloudy or milky appearance in the delamination indicates moisture or solvent penetration.

(b) Delamination areas characterized by irregular or jagged boundaries indi- cate uneven separation of the vinyl and glass.

(c) Replace windshield if one of the following conditions is noted:

1 Area of vision required for safe operation is affected (pilot's discretion).
Issued: December 01, 2010 226-56-011

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SERVICE BULLETIN

SA226 SERIES

2 Windshield heat system inoperative.

(2) Glass Shear

(a) Glass Shear in any portion of the windshield requires replacement prior to further flight.

(3) Interlayer Cracking

(a) Interlayer Cracking in any portion of the windshield requires replacement prior to further flight.
Issued: December 01, 2010 226-56-011

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SERVICE BULLETIN

SA226 SERIES

COCKPIT HEATED WINDSHIELD

FIGURE 1

COCKPIT HEATED WINDSHIELD COMPONENTS

FIGURE 2

Heating Grid

Outer Edge of 

Windshield & 

Metal Insert

Metal Insert

Inner Edge

View Looking Forward

at RHS Windshield

Outer glass

Inner glass

Interlayer

Metal

Retainer

Metal

Insert

Inner Edge of 

Metal Insert

Sealant

3.0 inch 
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SERVICE BULLETIN

SA226 SERIES

INTERLAYER CRACKING

FIGURE 3

Outer glass

Inner glass

Interlayer

Metal

Retainer

Metal

Insert

When viewed from edge, crack appears 

as a black line or a series of short 

disconnected black lines

Interlayer crack

Outer glass

Inner glass

Interlayer

Metal

Retainer

Metal

Insert

When viewed from side,

 striations are visible Interlayer crack
Issued: December 01, 2010 226-56-011

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SERVICE BULLETIN

SA226 SERIES

INSPECTION VIEWING ANGLES

FIGURE 4

Outer glass

Inner glass

Interlayer

Metal

Retainer

Metal

Insert

Plane perpendicular to 

plane of glass

45o 45o

Extent of viewing 

angle for inspection