N14605
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.
15 reports on file, 1999-08-10 – 2009-09-12.
Part: BEAR STRAP — CORRODED (BS 847 S24R)
DURING SCHEDULED INSPECTION, FOUND AFT CARGO DOOR CUTOUT, INTERNAL BEARSTRAP CORRODED AT 2.5" ABOVE S24R TO 2" BELOW S-24R FWD OF BS 847 FRAME.
Part: SKIN — CORRODED (BS 303-304)
DURING SCHEDULED INSPECTION, NDT INSPECTION OF L1 DOOR LOWER HINGE CUTOUT FASTENER HOLES CORROSION NOTED BS 303.9, W/L 234
Part: FRAME — CRACKED (BS 616)
DURING SCHEDULED INSP, FOUND CABIN, FUSELAGE FRAME AT BS 616, INBD CHORD CRACKED AT LWR (2) FASTENERS, WL 201.6 LT.
Part: STRINGER CLIP — CRACKED (BS 867 S1)
DURING SCHEDULED INSPECTION, FOUND CRACKED STRINGER CLIP ATTACHED TO FRAME AT BS 867 AND STR 1, AFT CABIN CEILING.
Part: SKIN — GOUGED (BS 867)
DURING SCHEDULED INSP, FOUND DEEP GOUGE ON FUSELAGE SKIN AT BS 867, STR 1.
Part: FLOOR SUPPORT — CORRODED
DURING SCHEDULED INSP, FOUND CORRODED CABIN FLOOR SUPPORT ANGLE AT BS 992.8, BL 37 - BL 45 R.
Part: FLOOR SUPPORT — CORRODED (BS 967)
CORROSION AROUND FASTENERS FLOOR SUPPORT CABIN BS 967, RBL 4 TO RBL 25.
Part: UPLOCK SENSOR — INOPERATIVE (RT MLG) · airframe 41,770 hrs · 21,780 cycles
RT MAIN GEAR RED UNSAFE AFTER TAKEOFF, EXTENDED TO NORMAL 3 GREEN. JACKED A/C PERFORMED SEVERAL GEAR SWINGS, ALL INDICATIONS NORMAL. AS PRECAUTIONARY REMOVED AND REPLACED RT GEAR UPLOCK SENSOR REF AMM 32-61-21, FUNCTIONAL CHECKS GOOD.
Earlier reports · 1999–2007 · 7 reports
2007
Part: FRAME — CRACKED (BS 360 S8L) · airframe 36,509 hrs · 19,094 cycles
INSPECTION FOUND A CRACK IN FRAME AT STA 360, S8L. THE FRAME WAS REPAIRED IAW ECRA 5310-04618.
Part: ANGLE — CORRODED (BS 277-344) · airframe 36,510 hrs · 19,094 cycles
INSPECTION FOUND Z-ANGLE CORRODED AT L-1 DOOR, STA 277-344, BL 0. A NEW Z-ANGLE WAS INSTALLED IAW SRM 51-10-02.
2004
Part: THROTTLE CABLE — STIFF (ENGINES) · airframe 30,455 hrs · 15,973 cycles
THE THROTTLES WOULD NOT REDUCE TO CLIMB POWER IN VNAV CAPTAIN SIDE THROTTLES WERE VERY STIFF. TROUBLESHOOTING FOUND BOTH NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES AT FAULT. THE NR 1 & NR 2 ENGINE THRUST CONTROL PUSH-PULL CABLES WERE REMOVED AND REPLACED IAW MM 76-11-07, PAGE 408. BOTH PUSH-PULL CABLES WERE ADJUSTED IAW MM 76-11-01.
Part: KEELBEAM — CORRODED (FUSELAGE) · airframe 30,266 hrs · 15,877 cycles
RIGHT KEEL BEAM HAS TWO NUT PLATES THAT APPEAR TO HAVE CORROSION UNDER THEM AT STATION 724 AND 721. FABRICATED AND INSTALLED REPAIR PER EC/RA 5311-01204.
2003
Part: CHARGER — INOPERATIVE (CABIN) · airframe 26,745 hrs · 14,023 cycles
INSPECTION FOUND FIRST CLASS CABIN SEATS WITH EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE DURING "A" CHECK. THE BATTERY CHARGER WAS REMOVED AND REPLACED AND OPERATION CHECKED GOOD IAW MM 33-51-02.
Part: SKIN — GOUGED (AFT CARGO DR) · airframe 26,563 hrs · 13,926 cycles
INSPECTION FOUND GOUGE AND DENT IN AFT CARGO DOOR SKIN AT AFT SIDE. REPAIRED DOOR IAW SRM 53-00-01 AND 52-30-01.
1999
Part: WIRE HARNESS — FAILED (NR 1 ENGINE)
LT GEN TRIPPED OFF LINE ON T/O FROM ORF. QRH PROCEDURE WAS RUN AND GEN RESET NORM. APPROX 3 MINS LATER CREW WAS NOTIFIED OF LIGHT SMOKE IN FWD PART OF CABIN. THE A/C RETURNED TO ORF. MX FOUND NR 1 TRANSFORMER RECTIFIER C/B POPPED AND NR 1 ENG FIREWALL DISCONNECT PHASE (B) FOR GEN FEEDER BURNT. TRANSFORMER RECTIFIER AND BATTERY/CHARGER WERE REPLACED IAW MM 24-21-31 AND 24-31-21. NR 1 ENG GEN HARNESS WAS R/R'D. NR 1 GEN FEEDER CABLE D3024 RECEPTACLE WAS ALSO REPLACED. RETERMINATED PYLON HARNESS PER BOEING. NR 1 ENG WAS RUN AND GEN FREQ WAS ADJUSTED IAW MM 24-11-11. OPS OF NR 1 GEN WAS GOOD. TEST FLT EVALUATION WAS PERFORMED AND ALL OPS CHECKED GOOD WITH NO DEFECTS NOTED.