Boeing ASB 767-53A0193: Revision 3, part 2 of 2, text

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The step numbers shown below agree with the numbers shown in the circle symbols in the figure.

NOTE: In areas around external features, scribe lines normally follow the periphery of the external feature.

DO NOT BLEND SCRIBE LINES. BLENDING A SCRIBE LINE MAY HINDER INSPECTION

TECHNIQUES NECESSARY TO DETERMINE THE PRESENCE OR ABSENCE OF FATIGUE CRACKS.CAUTION MORE DATA

QTYIDENTIFICATIONNAMETASKSTEP

(a) (b)1S-1L-1R, STA 448Upper Air Traffic Control (ATC) Antenna Inspect1

(a) (c)1S-1L-1R, STA 600Global Positioning System (GPS) Antenna Right

(a) (c)1S-1L-1R, STA 622Global Positioning System (GPS) Antenna Left

(a) (d)1S-1L-1R, STA 1122Automatic Direction Finder (ADF) Antenna

(a) (d)1S-1L-1R, STA 1166Automatic Direction Finder (ADF) Antenna

(a) (e)1S-1L-1R, STA 654+33Upper Very High Frequency (VHF) Antenna

(a) (e)1Lower Fuselage C/L, STA 513Lower Very High Frequency (VHF) Antenna

(a) (e)1Lower Fuselage C/L, STA 1197+99 Lower Very High Frequency (VHF) Antenna

(a) (f)1Lower Fuselage C/L, STA 555Distance Measuring Equipment (DME) Antenna

(a) (g)3Lower Fuselage C/L, STA 577Fwd Radio Altimeter (RA) Antenna

(a) (g)3Lower Fuselage C/L, STA 621Aft Radio Altimeter (RA) Antenna

(a) Do a detailed inspection of the fuselage skin around the external feature for any scribe line. Use a minimum 10X magnifying lens to aid the inspection.

(b) Refer to 767 AMM 34-53-03 as an accepted procedure.

(d) Refer to 767 AMM 34-57-03 as an accepted procedure.

(e) Refer to 767 AMM 23-12-03 as an accepted procedure.

(f) Refer to 767 AMM 34-55-02 as an accepted procedure.

FIGURE 55: FUSELAGE - EXTERNAL FEATURES - ZONE 2 INSPECTION (SHEET 2 OF 3) Export Controlled ECCN: 9E991 BOEING PROPRIETARY - See page 1 for details Original Issue: November 25, 2008 767-53A0193Revision 3 June 27, 2024 247 of 348 BOEING SERVICE BULLETIN 767-53A0193

ALERTALERT

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MORE DATA

QTYIDENTIFICATIONNAMETASKSTEP

(g) Refer to 767 AMM 34-33-02 as an accepted procedure.

FIGURE 55: FUSELAGE - EXTERNAL FEATURES - ZONE 2 INSPECTION (SHEET 3 OF 3) Export Controlled ECCN: 9E991 BOEING PROPRIETARY - See page 1 for details Original Issue: November 25, 2008 767-53A0193Revision 3 June 27, 2024 248 of 348 BOEING SERVICE BULLETIN 767-53A0193

ALERTALERT

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BOEING SERVICE BULLETIN 767-53A0193

ALERT ALERT This Figure applies only to: Group 8.

INSPECTION AREA --=--- EXISTING BUTT JOINT 1241 13219 STA 1175 00000000 STA 1153 1131 STA 1109 STA 786.1 - S-36R • - S-26R • S-26L - S-36L TYPICAL SCRIBE LINES STA 544 632 654+44 STA 654+22 STA 0000000 588 STA This Figure applies to Group 8: 1543362 FIGURE 56: FUSELAGE - EXTERNAL FEATURES - ZONE 2 INSPECTION (SHEET 1 OF 3) Original Issue: November 25, 2008 Revision 3 June 27, 2024 767-53A0193 Export Controlled ECCN: 9E991 BOEING PROPRIETARY - See page 1 for details 249 of 348

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