N11656
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, 2004-01-22 – 2006-07-21.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 22,348 hrs · 11,667 cycles
EMERGENCY PATH LIGHTING INOP BULB IN FIRST CLASS. REPLACED LENSE AND OPS CHECKS NORMAL.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 18,540 hrs · 9,673 cycles
THE OVERHEAD EMERGENCY EXIT LIGHT AT OVERWING HATCHES FAILED TO REMAIN ILLUMINATED WHEN ACTIVATED DURING TEST. THE BATTERY PACK FOR ZONE UNDER LT OVERWING EXIT WAS REMOVED AND REPLACED IAW SRM 33-51-51.
Part: SKIN — DELAMINATED (NR 2 SLAT) · airframe 16,190 hrs · 8,448 cycles
INSPECTION FOUND O/B CORNER OF NR 2 SLAT SKIN DELAMINATED. REPAIRED IAW SRM 51-70-10.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 16,190 hrs · 8,448 cycles
INSPECTION FOUND FUSELAGE SKIN DAMAGED ON FORWARD CURVED SIDE AT RIGHT AFT HORIZONTAL STABILIZER ATTACH POINT. THE SKIN WAS REPLACED IAW SRM 51-40-2.
Part: ANGLE — CORRODED (FUSELAGE) · airframe 16,190 hrs · 8,448 cycles
INSPECTION FOUND R-1 DOOR Z-ANGLE CORRODED FROM STA 270-360. THE Z-ANGLE WAS REMOVED AND REPLACED IAW SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 16,190 hrs · 8,448 cycles
INSPECTION FOUND A 1 INCH CRACK IN FLOOR SUPPORT WEB BETWEEN STA 348 AND 360, BL 0. THE WEB WAS REMOVED AND A NEW WEB WAS INSTALLED IAW SRM 51-10-02.