Service difficulty report · Tire · Boeing 737824

Difficulty date
February 20, 2024
Submitted
March 20, 2024
Operation
Air carrier
Aircraft
N14250
Make and model
Boeing 737824
Aircraft serial
28957
Aircraft time
74,562 hours, 28,031 cycles
System (JASC)
3245 · Tire Tube
Part
Tire
Part number
7377899ERMLGCARB
Part serial
F380C20641
Condition
Failed
Location
Rt Mlg
Part time
3,191 hours, 1,300 cycles
Stage of operation
TO
How discovered
O
Nature of condition
O
Precautionary procedure
B

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

What was found

RIGHT MAIN INBOARD TIRE BLOWN, R & R #3 TIRE IAW CAMM 32-45-11. CHANGING RT GEAR #4 OTBD TIRE DUE TO INBOARD #3 TIRE BLOWOUT. R & R #4 TIRE PER AMM 32-11-45. RT INBOARD FIXED T/E LOWER PANEL DAMAGED DUE TO #3 TIRE BLOWN. RT WING INBOARD FIXED T/E LOWER PANEL REMOVED IAW AMM 57-50-02-000-801. INSTALLED A NEW SERVICEABLE PANEL 651FB. IAW TASK 57-50-02-400-801. REMOVED DAMAGED RT WING INBOARD AFT FLAP IAW AMM 27-51-12-000-801. ACP RII INSPECTION OF RT INBD FLAP INSTALL IAW AMM 27-51-12-400-801 STEP 3 H (16) - 3 H (16) (D). CKS OK. . NO DEFECTS NOTED. R/H I/B AFT FLAP COMPLETED TASK AMM 27-51-12-400-801, COMPLETED STEP F1 A THRU G. COMPLIED WITH INSTALLATION OF THE RIGHT INBOARD AFT FLAP AMM TASK 27-51-12-400-801 STEP F (2) UP TO AND INCLUDING STEP H (15). 04 CONTINUED WITH AMM 27-51-12-400-801 STEP 3 H (16) THRU 3 H (16) (D). COMPLETE INSPECTION OF ITEM 3.H.(8) THRU (12) OF AMM 27-51-11-400-801. COMPLETE INSPECTION OF AMM 27-51-11-820-80 1. ACP RII INSPECTION OF RT INBD FLAP MM 27-51-11-400-801 ITEMS 3(H)8 THRU 3(H)11. CKS OK. INSPECTED ADJUSTEMENT PER AMM 27-51-11-820-801 SET THE CARTRIGES ROLLERS TO NOMINAL POSITION , FROM STEP G(3A) TO (2J) ACCOMPLISHED STEPS 3H(8) THRU 3H(11) OF AMM 27-51-11-400-801 R/H INBD TRAILING EDGE FLAP INSTALLATION. ITEM 3H(12) CALLS OUT FOR ACCOMPLISHING AMM TASK 27-51-11-820-801 INBD TRAILING EDGE FLAP ADJUSTMENT. PERFORMED ADJUSTEMENT PER AMM 27-51-11-820-801 SET THE CARTRIGES ROLLERS TO NOMINAL POSITION , FROM STEP G(3A) TO (2J) INSTALLED INBOARD FLAP SUPPORT AFT FAIRING PER AMM 27-51-18. ADD EMP:U348590 VERIFIED I/B AFT FLAP RIG IAW AMM 27-51-11-820-801 STEPS G(3) THRU H(8). OK TO INSTALL I/B AFT FLAP SUPPORT FAIRING. COMPLETED INBOARD TRAILING EDGE FLAP ADJUSTMEN PER AMM 27-51-11-820-801, FROM STEP G(3) TO STEP H(8). INBOARD FLAP SUPPORT AFT FAIRING NEEDS INSTALL. INSTALLED INBOARD FLAP SUPPORT AFT FAIRING PER AMM 27-51-18.