2 MANDATORY INSPECTIONS The following mandatory inspections as specified in TADS have been complied with, or are next due at: Periodicity (whichever occurs first) Carried Out Next Due Description Reference Hours Calendar Hours Date Hours Date CAA AD Mandatory life limits 2804 PRE 80/ n/a 12 months n/a (X-refer G-2012-0001) TNS 138 CAA AD Wing to fuselage attachment 2806 PRE 80/ Next wing removal Next wing removal links TNS 161 CAA AD 12 years Undercarriage mounting 2807 PRE 80/ n/a (x-refer n/a casting X-ray TNS 165 to TNS) CAA AD Dependent on Fuselage centre section tie 007-09-85/ mod state n/a n/a bar TNS 175 (x-refer to TNS 138) CAA AD Engine frame attach points in 009-09-85/ n/a 36 months n/a fuselage TNS 180 Fuselage rear bulkhead 200 hours 12 months (original) CAA AD 005-05-90/ TNS 183 Fuselage rear bulkhead 600 hours 36 months (repaired or replaced) CAA AD Tail unit assembly 021-08-91/ n/a 7 years n/a (struts X-ray) TNS 186 CAA AD Engine frame joint 003-08-94/ 600 hours n/a n/a examination TNS 190 CAA AD Flap operating cable failure 001-03-95/ 150 hours 12 months TNS 184 6 months CAA AD Replace brackets at inspection Tail unit assembly 014-11-97/ 9984 fatigue hours (pre mod TNS 176 H.357) Page 3 of 5
2 MANDATORY INSPECTIONS The following mandatory inspections as specified in TADS have been complied with, or are next due at: Description Reference Periodicity (whichever occurs first) Carried Out Next Due Hours Calendar Hours Date Hours Date Mandatory life limits (X-refer G-2012-0001) CAA AD 2804 PRE 80/ TNS 138 n/a 12 months n/a Wing to fuselage attachment links CAA AD 2806 PRE 80/ TNS 161 Next wing removal Next wing removal Undercarriage mounting casting X-ray CAA AD 2807 PRE 80/ TNS 165 n/a 12 years (x-refer to TNS) n/a Fuselage centre section tie bar CAA AD 007-09-85/ TNS 175 Dependent on mod state (x-refer to TNS 138) n/a n/a Engine frame attach points in fuselage CAA AD 009-09-85/ TNS 180 n/a 36 months n/a Fuselage rear bulkhead (original) CAA AD 005-05-90/ TNS 183 200 hours 12 months Fuselage rear bulkhead (repaired or replaced) 600 hours 36 months Tail unit assembly (struts X-ray) CAA AD 021-08-91/ TNS 186 n/a 7 years n/a Engine frame joint examination CAA AD 003-08-94/ TNS 190 600 hours n/a n/a Flap operating cable failure CAA AD 001-03-95/ TNS 184 150 hours 12 months Tail unit assembly CAA AD 014-11-97/ TNS 176 Replace brackets at 9984 fatigue hours 6 months inspection (pre mod H.357) Page 3 of 5