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teardowndroneTRL-3

Unit #2: DJI Phantom 2 Teardown

DJI Phantom 2 before disassembly

Overview

Unit: LL-PTR-002 Subject: DJI Phantom 2 with Zenmuse H3-3D gimbal Mass: 1,387g (12.8x Unit #1) Date: 2 March 2026 Result: Partial disassembly — 307g assembly unresolved (requires 60W+ soldering station)

DJI Phantom 2 — initial condition on arrival

Background

Unit #2 represents a significant scale-up from Unit #1 (108g → 1,387g). The DJI Phantom 2 is a prosumer-grade quadcopter with substantially more complex construction: integrated gimbal system, GPS module, multi-cell LiPo battery, brushless motors with ESCs, and a magnesium/plastic composite airframe.

This teardown tests whether our methodology scales to heavier, more complex assemblies.

Process

37 photographs document the complete process. Key stages:

  1. Intact documentation — all angles, serial numbers, condition assessment
  2. Gimbal removal — H3-3D Zenmuse unit, 4x screws + ribbon cable
  3. Battery extraction — 5,200mAh 3S LiPo (183g)
  4. Shell separation — top/bottom body, 8x screws (mix of Phillips and hex)
  5. GPS/compass module — mounted on mast, 2x connectors
  6. Main board extraction — flight controller + power distribution
  7. Motor removal — 4x brushless DC, threaded mount, connector-based wiring
  8. Gimbal disassembly — 3-axis brushless motors, IMU board, carbon fiber plate
  9. Landing gear extraction — press-fit plastic with foam dampeners
  10. Frame disassembly — main body/arm separation

Upper shell removed — internal components exposed

Unresolved: 307g integrated assembly (flight controller + ESC board + motor mount) with soldered connections too robust for current equipment. Requires 60W+ soldering station (~200-300 PLN) for complete separation.

Material Classification

CategoryMass (g)Percentage
Electronics (FC, ESC, GPS, camera)41229.7%
Motors (4x brushless + 3x gimbal)23817.2%
Structural (plastic/magnesium frame)29621.3%
Battery (3S LiPo)18313.2%
Gimbal assembly (carbon fiber, aluminum)14210.2%
Wiring & connectors624.5%
Propellers & guards342.5%
Fasteners (screws, nuts)120.9%
Waste (labels, foam, adhesive)80.6%

Parts-to-scrap ratio: 99/1 — confirming the pattern from Unit #1 at 12.8x the mass.

Main board, ESC, and motor assembly — the unresolved 307g module

Key Findings

  • Methodology scales — the systematic top-down approach works at 10x+ mass
  • Tool requirements increase with scale — hex drivers needed, soldering station needed for full separation
  • Composite materials appear — carbon fiber gimbal plate, magnesium frame elements. Directly relevant to future aircraft composites (validates PRz research partnership scope)
  • Documentation standardized — naming convention LL-PTR-002_NN_description.jpg established for all future teardowns
  • Assembly complexity creates natural stopping points — the 307g integrated module demonstrates that full disassembly may not always be practical or necessary

Comparison with Unit #1

MetricUnit #1 (E99 Pro)Unit #2 (Phantom 2)
Mass108g1,387g
Components recovered2447+
Photos taken1237
Tools required2 (screwdriver, tweezers)5+ (screwdrivers, hex, pliers, tweezers)
Specialized equipment neededNoYes (soldering station)
Parts/scrap ratio99/199/1
Composite materialsNoYes (carbon fiber, magnesium)
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