NLR rapport TR 74030 C d.d. 18-2-1974. Stress changes measured during the loosening of the skins from attach ribs, wing to fuselage, of the NF5 … NLR rapport Memorandum SB-74-073 d.d. oktober 1974. Acceleration measurements on the NF-5A and NF-5B aircraft of the Royal Netherlands Air Force. (2 exemplaren) TD-204 NLR rapport SB-74-078 (d.d. 21-10-1974). NF-5 multiparameter recording interim report. NLR rapport TR 74112 C d.d. 15-8-1974. A tentative fatigue test load history for fighter aircraft. TD-206 NLR rapport TR 75083 C d.d. mei 1975. Investigation into the cause of cracking of NF-5 wing root ribs. TD-207 NLR rapport TR 75088 C d.d. juni 1975. Stress changes measured during the mounting of new attach ribs, wing to fuselage, of the NF-5 … NLR rapport SB-76-002 d.d. 13-1-1976. Investigations on fin loads for NF-5A/B. (2 exemplaren) NLR rapport TR 76019 C d.d. 13-2-1976. Summary report NF-5A multiparameter usage recordings. NLR rapport SB-76-034 d.d. 1-3-1976. NF-5A/B wing structure; fatigue program status and projected activities. 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.
