Torque values for aircraft fasteners are not suggestions. Under-torqued joints lose clamp load under vibration and thermal cycling; over-torqued bolts yield the shank or strip the nut, destroying the clamping ability they're supposed to provide. The values here come directly from FAA AC 43.13-1B, Chapter 7, Table 7-1 — the authoritative reference for AN hardware in general aviation and experimental applications. Post this chart on the shop wall. Cross-reference it against your aircraft's maintenance manual when a specific torque is called out there, since the manual takes precedence for its own hardware.

Where These Numbers Come From

FAA AC 43.13-1B Table 7-1 provides torque ranges for AN standard hardware under clean, dry conditions. The values assume:

These are the dry torque values. If you're torquing into a fuel-wet environment or have applied any lubricant to the threads, see the lubricated adjustment section below before applying these numbers.

AN Bolt Torque Values — Dry, Cadmium-Plated Alloy Steel

Bolt Size Thread Size Min Torque (in-lb) Max Torque (in-lb) Wrench Size
AN310-32 UNF20255/16"
AN41/4-28 UNF50707/16"
AN55/16-24 UNF1001401/2"
AN63/8-24 UNF1601909/16"
AN77/16-20 UNF45050011/16"
AN81/2-20 UNF4806903/4"
AN105/8-18 UNF8001,00015/16"
AN123/4-16 UNF9601,1001-1/8"

Note that the AN7 minimum (450 in-lb) is higher than AN8 minimum (480 in-lb) — this is correct in AC 43.13-1B. The AN7 bolt has a different grip-to-thread geometry than AN8. Always verify against the current revision of the advisory circular for your specific application.

Lubricated Torque Adjustment

AC 43.13-1B specifies that the dry torque values must be reduced when any lubricant is present on the threads. The standard reduction is 20–30% from dry values. Use the lower end of the reduction (20%) for light lubricants like cadmium plating interaction; use the higher end (30%) for heavy grease, wet sealers, or anti-seize compounds.

Special Cases

Several hardware variants require adjusted torque handling beyond the standard table:

Torque Sequence and Technique

How you apply torque matters as much as the value. Thread galling, embedment, and elastic interaction between adjacent fasteners can all cause actual clamp load to differ significantly from what the torque wrench reads. Use a three-step approach:

  1. Snug the bolt finger-tight. Verify the bolt is not cross-threaded, the washer is seated, and the mating surfaces are in full contact.
  2. Apply torque in three equal increments (approximately 30%, 65%, and 100% of the final value). This allows the joint to seat and the bolt to develop consistent tension without shock loading.
  3. Apply final torque. Do not exceed the maximum by backing off and re-applying — if you exceeded maximum, document it and evaluate whether to replace the fastener.

For castle nuts: torque to the low end of the specified range, then advance (never back off) to the nearest cotter pin hole that aligns with the bolt shank hole. If no hole aligns within the torque range, the grip length is wrong — change the bolt, not the torque. Backing off a castle nut to find a cotter pin slot removes the preload you need and creates a joint that will loosen in service.

Use a calibrated torque wrench for final torque on all structural fasteners. An open-end wrench or box wrench gives no indication of applied torque. Snap-action click wrenches are accurate in the middle of their range but lose accuracy at the extremes — for AN3 bolts (20–25 in-lb), use a beam-type wrench in the 0–100 in-lb range for best accuracy.

Torque Wrench Calibration

A torque wrench that hasn't been calibrated is a false confidence instrument. It feels like precision and may be nowhere near it. Calibration requirements:

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