Service difficulty report · Slat Track · Boeing 7377H4

Difficulty date
September 27, 2021
Submitted
October 27, 2021
Operation
Air carrier
Aircraft
N263WN
Make and model
Boeing 7377H4
Aircraft serial
32520
Aircraft time
46,043 hours, 27,465 cycles
Part
Slat Track
Condition
Corroded
Location
Rt Wing Nr 5
Stage of operation
NR
How discovered
9
Nature of condition
O
Precautionary procedure
O

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

What was found

RH L/E #5 SLAT; INBOARD MAIN TRACK UPPER SURFACE; PLATING WORN; PITTING AND LIGHT CORROSION ; / [01] DEACTIVATED LEADING EDGE FLAPS AND SLATS IAW AMM 27-81-00-040-801.; [02] DISCONNECTED #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-000-802 STEPS 4.E.(1)-(5); [03] COMPLETED REMOVAL OF #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-000-801 STEP 4.E. (6); [04] VERIFIED PARTIAL STEP 1.; [05] VERIFIED CLEARANCE OF #5 MAIN SLAT TRACK SIDE GUIDES AND STOPS IAW AMM 27-81-21-400-802 STEP 5F.(3)(C); CHECKED OUT GOOD.; [06] VERIFIED COMPLETE STEP 2.; [07] REINSTALLED #5 I/B MAIN SLAT TRACK IAW AMM 27-81-21-400-802 STEPS 5G (1);(2)(A)1)-3); STEPS 5G(3)-(5)(D)2) & (6)(C)1)&2); [08] CAL. TOOLS USED:<BR>I.D. ATS2321<BR>S/N: 0119121014<BR>DUE: 05/2022<BR><BR>I.D. PER2148<BR>S/N: 0420503937<BR>DUE:02/2022; [09] VERIFIED UPDATED STEP 1.; [10] ADJUST #5 I/B SLAT AS REQUIRED AND PERFORM LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL.; [11] ENTERED PART AND MEASURMENT INFORMATION; [12] CHECKED ADJUSTMENT OF #5 SLAT AND PERFORMED LEADING EDGE FLAP AND SLAT SYSTEM OPERATION WITH PRIMARY CONTROL PER AMM 21-81-21-400-802 STEP 5G(7)-(10). CHECKS GOOD; [13] COMPLETED STEPS 1-3; [14] TAK COMPLETE

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