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Atlas / NTSB / DCA24LA110

NTSB CAROL · Event

Event DCA24LA110

2024-02-25 San Francisco, California, United States Airport · SFO None 1 aircraft Status: Completed

Registry · N13138

FAA Aircraft Registry record.

Make / Model

BOEING 757-224

Year of manufacture

1999 · 25 years old at event

Engine

ROLLS-ROYC RB-211 SERIES

Seats / Engines

178 seats · 2 engines

Last airworthiness date

19991207

ADS-B equipped

Yes — Mode-S A081CA

Registrant of record

UNITED AIRLINES INC

Source: FAA Aircraft Registry (releasable master file).

Aircraft involved

Probable cause & findings

The crew’s over-rotation of the aircraft pitch during takeoff which resulted in a tailstrike.

Factual narrative

United Airlines (UA) flight 3872 experienced a tailstrike while taking off from San Francisco International Airport (SFO), San Francisco, California. The flight was a local maintenance test flight. The purpose of the test flight was to validate maintenance conducted after a write-up for abnormal flight deck noises that occurred on a previous flight. According to the flight crew, they conducted a flaps 5, reduced power takeoff from runway 28R. The captain recalled the aircraft accelerated faster than normal and had the propensity to lift off prior to the rotation speed of 127 knots. At rotation speed, the captain began a normal aft pull on the control yoke and the pitch attitude increased faster than expected. The captain just called “positive rate” when the crew heard and felt a “boom.” As this flight was a test flight, it was not loaded with passengers and cargo to a takeoff weight typical of flights the pilot flying normally flew. The pilot flying rotated at a rate “normal” to his experience, however because the accident aircraft was loaded lighter than normal, the normal rotation inputs resulted in an over-rotation. The crew assessed the instruments and controllability and decided to continue their climb to flight level (FL) 190 [19,000 feet] where they conducted the tailstrike checklist. They returned to SFO and conducted a flaps 30 landing with no further incident. Prior to leaving the flight deck after the flight, the first officer received the pitch report for takeoff which showed that tail contact occurred about 12.2 degrees during departure and the actual pitch for this departure reached 15.3 degrees. Inspection of the aircraft showed that the tail strike damaged the chord, web, and stiffeners of the auxiliary power unit firewall bulkhead. Because the damage would adversely affect the structural strength of the bulkhead and require major repair or replacement, the damage was considered substantial. The investigation determined that the maintenance conducted prior to this test flight was not related to the accident. Source: NTSB Aviation Accident Database Retrieved: 2026-02-12

NTSB Findings

Hierarchical cause / factor breakdown from the FAA bulk avdata database. Each finding tagged C (Cause) or F (Factor).

  • Personnel issues-Action/decision-Action-Incorrect action performance-Pilot

Verbatim from NTSB's published report. Source file NTSB_2024_DCA24LA110.txt. Findings + structured fields enriched from FAA avall.mdb. Full investigation docket on data.ntsb.gov ↗.

Related research

What the literature says.

Academic papers and agency reports matching this event's aircraft type or causal vocabulary (maintenance). Sourced from NASA NTRS, NTSB Safety Studies, FAA CAMI, AOPA Air Safety Institute, Embry-Riddle Scholarly Commons, arXiv, and the Semantic Scholar academic graph.

Browse the full corpus — academia portal ↗