Folks... from an aero's perspective:
In large/critical structures we typically specify the following:
Install temporary fasteners or clamps to pull structure TIGHTLY together.
Install all threaded fasteners "finger tight".
Install rivets [and swagged-collar lock-bolts] undriven, between temp fasteners/clamps. NOTE: tape-over heads to prevent pop-out, allowing rivet to stabilize hole.
Torque To final value [or frangible-collar-break] in (3) stages [50%, 75% and 100%, MIMIMUM] using a typical crossing pattern (perhaps the term "criss-cross pattern" is more "friendly/descriptive"

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Note: wait at least 10-miuntes between torquing stages for joint settling and any "sealant squeeze-out].
NOTE: FINAL-TORQUE value is determined by adding the "free-running-torque" of the nut on the male threads to the theoretical required torque value [shear or tension from charts for each thread style]... resulting in a value that will be different for each fastener combination: especially with self-locking hardware!!!
Drive rivets & swagged-collar lock-bolts AFTER securing all threaded fasteners.
Fillet-seal around edges of nuts/washers and structure using sealant-squeeze-out; or apply tamper-evident paint across thread, nut, washer and structure [evidence of movement]. If necessary [IE: vibration environments], we also use cotter-pins and/or lock-wire.
NOTE: for some joints where installed torques are deliberately low but critical [IE: bearings on shafts, small-headed bolts, etc], we allow a "slight over-torque" to settle parts, wait a short-while, then back-off and final-torque to value. A theme-and-variation to this is "over-torque and back-off slightly concept" is to back-off until a thru-hole in male threads aligns to a "nearest" castelated cut-out in the nut... then install a cotter-pin or lock-wire.
Note: The concept of "checking torque" in a joint is alien... we use indicator mechanisms and inspections to verify that a "job" is finished.... and indicators that joint may have become loosen in-service.
Regards, Wil Taylor