N409
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
6 reports on file, 2006-06-28 – 2006-11-08.
Part: RAIL — DAMAGED (FUSELAGE) · airframe 27,591 hrs · 4,240 cycles
FWD CARGO SIDE RAIL CRACKED DUE IMPACT DAMAGE.
Part: STRUCTURE — DELAMINATED (FORE FLAP) · airframe 26,339 hrs · 4,065 cycles
DELAM & PUNCTURE DAMAGE TO RT I/B FORE FLAP 60 INCHES FROM I/B EDGE & 12 INCHES FROM TE.
Part: SKIN — GOUGED (T/E FLAP) · airframe 26,339 hrs · 4,065 cycles
2 AREAS OF DAMAGE TO UPPER SURFACE LEADING EDGE LT O/B TE AFT FLAP CAUSED BY MID FLAP COVE PANEL SUPPORT BRACKETS, 0.050 DEPTH X .5 DIA. 15 IN FROM O/B EDGE AND 0.040 DEPTH X .5 DIA. 35 IN FROM O/B EDGE, PANEL THICKNESS .120
Part: SKIN — PUNCTURED (TE FLAP) · airframe 25,763 hrs · 3,987 cycles
LEFT AFT T/E FLAP LOWER SKIN HAS A PUNCTURE MARK LOCATED 125 INCHES FROM I/B & 9 INCHES FWD OF AFT EDGE. PUNCTURE MARKS REPAIRED IAW ATLAS AIR SRM 747-400F 57-53-01 PG 102 REF D & F REVISION 43 FIG 101.
Part: SKIN — CRACKED (FLAP) · airframe 25,763 hrs · 3,987 cycles
LEFT TRAILING EDGE I/B MID FLAP HAS PREVIOUS REPAIR THAT HAS CRACKED ON I/B END 6 INCHES FROM EDGE. DAMAGE REMOVED & REPAIR LAYED UP 7 CURED IAW B747-400F SRM 51-70-06 REPAIR 5A (1), PARA 4 A, C, E (1) (D) PG 13 REVISION 43.
Part: SKIN — PUNCTURED (TE FLAP) · airframe 25,763 hrs · 3,987 cycles
RIGHT I/B FORE FLAP LOWER SKIN 4 PUNCTURE MARKS ALL APPROX .100 DIA LOCATED AT 1) 65.5 INCHES FROM I/B EDGE & 6.75 INCHES FROM AFT. 2) 64.5 INCHES FROM I/B EDGE & 9.5 INCHES FROM AFT EDGE. 3) 60 INCHES FROM I/B EDGE & 14 INCHES FROM AFT EDGE. 4) 56.5 INCHES FROM I/B EDGE & 25 INCHES FROM AFT EDGE. PUNCTURE MARKS RECTIFIED IAW ATLAS AIR 747-400F SRM 57-53-01 PG 102 REF D & F REV 43.