N73385
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.
12 reports on file, 2001-02-17 – 2001-06-01.
Part: MEGAPHONE — INOPERATIVE (CABIN) · airframe 19,187 hrs · 10,009 cycles
INSPECTION FOUND THE FORWARD MEGAPHONE INOPERATIVE. THE MEGAPHONE WAS REMOVED AND REPLACED IAW MM 25-60-00.
Part: SKIN — GOUGED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND FUSELAGE SKIN GOUGED BELOW LT AFT HORIZONTAL LUG FITTING AT STA 1142. NEW SKIN WAS INSTALLED IAW SRM 51-10-02 AND MM 20-10-34.
Part: FRAME — CRACKED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND A 2 INCH CRACK IN BELTFRAME IN AFT CARGO BIN AT STA 807, RBL 2. THE LOWER FRAME SECTION WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: SKIN — DAMAGED (LT ELEVATOR) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND A HOLE IN LT ELEVATOR UPPER SKIN AT STA 39.02 (APPROXIMATELY 21 INCHES I/B AND 4 INCHES FROM AFT SPAR). THE LT ELEVATOR SKIN WAS REPAIRED IAW ECRA 5520-01250.
Part: SKIN — GOUGED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND FUSELAGE SKIN GOUGED JUST AFT OF RIGHT LOWER HORIZONTAL LUG AT STA 1150. THE DAMAGED SKIN WAS REMOVED AND REPLACED IAW SRM 51-40-01.
Part: DOUBLER — CORRODED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND LOWER STRAP DOUBLER CORRODED AT LOWER DOOR JAMB, STA 787 - 796. THE STRAP DOUBLER WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: FITTING — SEPARATED (LT ELEVATOR) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND LT ELEVATOR HORN BEARING FITTING SEPARATED. THE LT ELEVATOR WAS REMOVED AND REPLACED IAW MM 27-31-11.
Part: BRACKET — CRACKED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND A 1 INCH CRACK IN PANEL SUPPORT BRACKET AT PRESSURE BULKHEAD STA 727, JUST ABOVE STRINGER 27R. A FORMED SECTION REPAIR WAS INSTALLED IAW SRM 51-70-11.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND FLOOR SUPPORT CORRODED AT STA 500D BETWEEN S26L AND S26R. THE FLOOR SUPPORT WAS REMOVED AND REPLACED IAW SRM 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND A 1 INCH CRACK IN INTERCOSTAL AT STA 380 - 400, BL 0. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-30-51 AND 51-10-02.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND A 1 INCH CRACK AT NUTPLATE HOLE IN INTERCOSTAL AT STA 927 - 947, BL 0. THE INTERCOSTAL WAS REPLACED IAW SRM 53-60-51, FIGURE 1, SHEET 7.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 18,416 hrs · 9,650 cycles
INSPECTION FOUND FLOOR SUPPORTS CRACKED AT STA 540, LBL 1 AND RBL 1. THE CRACKS WERE 1 INCH LONG. THE FLOOR SUPPORTS WERE REMOVED AND REPLACED IAW SRM 51-10-02.