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SDR SROM2011007

Open the Markdown

Service difficulty report · Skin · Boeing 737205

FAA SDR system

Difficulty date
July 19, 2011
Submitted
July 19, 2011
Operation
General aviation
Aircraft
N736BP
Make and model
Boeing 737205
Aircraft serial
23465
Aircraft time
41,369 hours, 38,886 cycles
System (JASC)
5330 · Fuselage Main, Plate/Skin
Part
Skin
Condition
Nicked
Location
Fuselage
Part time
41,369 hours, 38,886 cycles
Stage of operation
IN
How discovered
V
Nature of condition
O
Precautionary procedure
K

As reported to the FAA. Reports are unverified, and codes are left as the FAA publishes them.

What was found

NICK ON FUSELAGE SKIN AT BS 847 S-25R REPAIRED IN ACCORDANCE WITH MESSAGE NOS. KFC-ATR-11-0004-01C, DATED JUNE 24, 2011, KFC-ATR-11-0004-05B, DATED JUNE 29, 2011, KFC-ATR-11-0004-06C, DATED JULY 13, 2011 AND BOEING APPROVED FAA FORM 8100-9, DATED JULY 14, 2011. UT THICKNESS CARRIED OUT IN ACCORDANCE WITH BOEING 737 NDT MANUAL D6-37239, PART 4, 51-00-00, FIGURE 3 ON BLEND-OUT AREA OF FUSELAGE SKIN AT BS 847 S-25R, NOMINAL OF 0.036, LOWEST READING 0.022 (NDT11-0819). HFEC INSPECTION OF OPEN HOLES COMMON TO THE REPAIR IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011; SECTION 53-30-3, FIGURE 46 AND BOEING 737 NDT MANUAL D6-37239, PART 6, 51-00-00, FIGURE 16. NO DEFECTS EVIDENT ( NDT11-0854). HFEC INSPECTION OF CUT OUT EDGES IN ACCORDANCE WITH BOEING 737-200 STRUCTURAL REPAIR MANUAL (SRM), REV 103, DATED MAR 10, 2011; SECTION 53-30-3, FIGURE 46 AND BOEING 737 NDT MANUAL D6-37239, PART 6, 51-00-00, FIGURE 23. NO DEFECTS EVIDENT (NDT11-0853). REFERENCE NON-ROUTINE WORK ORDER NR. 1014377, DATED 14 JULY 2011.