737 MAX
Incident Reports

U.S. based airlines are required to submit safety reports called Service Difficulty Reports (SDRs) for malfunctions involving aircraft systems in accordance with U.S. law. The Federal Aviation Administration (FAA) is required by Department of Transportation policy to investigate these incidents to determine root causes and to ensure corrective action is taken by aircraft manufacturers and airlines to fix the problem(s). These reports are crucial for maintaining and improving aviation safety, as they help to identify potential hazards, evaluate risks, and implement corrective measures to prevent future tragedies.

The foundation believes it is important to highlight select reports involving 737 MAX airplanes. We find the reports listed below concerning because of the history of the MAX and the repetitive and/or serious nature of the reports.

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Airline

ASAA – Alaska Airlines, AALA – American Airlines, CALA – United Airlines, SWAA – Southwest Airlines

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Control Number
CALA2021120102223
Discrepancy Date
12/1/21
Submission Date
12/1/21
Airline Name
CALA
Registry Number
7251
Aircraft Make
BOEING
Aircraft Model
7378
Aircraft Total Time (hrs)
1177
Discrepancy
REFERENCE 7504156 COMPLETED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02...AWAITING AVO/EC/RA FOR FURTHER INSTRUCTIONS. HFEC INSPECTION REQUIRE AROUND THE CUTOUT. HFEC INSPECTION REQUIRE OF ALL REMOVED INITIAL FASTENERS. PERFORMED HFEC OF TRIM OUT REF 737 NDT PART 6 51-00-00 PROCEDURE MATERIAL ID# 2024-T3 .063 PO#9038308 STEP B - FABRICATION STEP 1 INSPECTION REQUIRED FOR MATERIAL ID VERIFIED MATERIAL ID. 23 & AVO 7251-21-11-28-01 STEP 1.A. NO DEFECTS NOTED. PER AVO# 7251-21-11-28-01. MATERIAL NOTED. REF: AVO #: 7251-21-11-28-01A, ITEM A, 9. APPROVED FABRICATION OF -1 REPAIR DOUBLER PER FIGURE 2 OF AVO # VERIFIED ACCOMPLISHMENT OF STEP 7 OF AVO 7251-21-11-28-01A VERIFIED STEPS 2, 5 AND 6 OF AVO # 7251-21-11-28-01A. VERIFIED ACCOMPLISHMENT OF STEP 1 AND 2 SECTION B OF AVO VERIFIED DAMAGE CUTOUT ON DENT R/H SIDE ...REF SRM 51-10-02.. VERIFIED ACCOMPLISHMENT OF STEP 5 AND 6 SECTION B OF AVO VERIFIED ACCOMPLISHMENT OF STEP 7 SECTION B OF AVO INSPECTED DOUBLER OK TO TREAT AND PRIME. CLEARED FOR OK TO INSTALL REPAIR PART AS PER 7251-21-11-28-01. (RE-FORM SKIN DENT TO ORIGINAL CONTOUR) 7251-21-11-28-01A (ENSURE ADDITIONAL DENT INFO AND LOCATION 7251-21-11-28-01A (EXTERNAL VISUAL AND UNDERLYING STRUCTURE 7251-21-11-28-01A (RE-FORM SKIN DENT TO ORIGINAL CONTOUR) AVO#7251-21-11-28-01A MATCH AND MEET CONDITIONS) NO DISCREPANCIES NOTED. INSP) NO DISCREPANCIES NOTED FABRICATED -1 REPAIR DOUBLER AND LOCATED PRODUCTION FASTENER PER PERFORMED HFEC INSPECTION OF REMOVED FASTENERS