NLR rapport SB-76-035 d.d. 1-3-1976. NF-5A/B vertical tail structure; fatigue program status and projected activities. TD-212 NLR rapport TR 76049 C d.d. 5-5-1976. Fractographic investigation of a cracked NF-5 wing root rib. NLR rapport TR 76080 C part I d.d. 9-9-1976. The calibration of the RNLAF NF-5A instrumented wing; Part I: Description and results. NLR rapport TR 76080 C part II d.d. 9-9-1976. The calibration of the RNLAF NF-5A instrumented wing; Part II: Influence coefficient plots. TD-215 NLR rapport TR 76115 C d.d. 9-9-1976. Development of fatigue test specimen for the NF-5 wing lower skin. TD-216 NLR rapport TR 77088 C d.d. 29-7-1977. Flight load tests on NF-5 wing skin specimens. NLR rapport Memorandum SC-77-172 d.d. 21-12-1977. Comparison of measured and calculated strains near the critical radius in the vertical tail of the NF-5A. NLR rapport TR 79008 C d.d. januari 1977. Investigation of the load distribution in the NF-5A vertical tail section and of the stress in the … NLR rapport MP 79008 U d.d. 23-2-1979. Re-assesment of service life by comparative specimen tests. NLR rapport Memorandum VG-79-017 C d.d. 30 april 1979. Handleiding voor het opmeten van target- en vliegtuig-referentiepunten en de openingshoeken van een fotocamera t.b.v. DIAS. NLR rapport TR 79032 C d.d. 1-3-1979. NF-5A vertical stabilizer flight loads survey. TD-222 NLR rapport TR 79075 C d.d. 3-8-1979. Investigation into the cause of cracking of NF-5 fuselage frames at STA. 487.22.
