N14652
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.
13 reports on file, 2007-07-07 – 2009-12-21.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 31,477 hrs · 16,703 cycles
FWD EMERGENCY FLASHLIGHT NO CHARGE INDICATED. REPLACED BATTERY IN FLASHLIGHT, OPS CHECKED NORMAL.
Earlier reports · 2007–2008 · 12 reports
2008
Part: STRINGER — DAMAGED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
STRINGER DAMAGED AT STATION 867 S-1 BL-0. CUT OUT DAMAGED SECTION OF STRINGER AND INSTALLED STRINGER SPLICE REPAIR PER ECRA 5310-04876.
Part: SKIN — WORN (VERTICAL STAB) · airframe 28,873 hrs · 15,348 cycles
FUSELAGE UPPER SURFACE WHERE DORSAL FIN SEAL BLADE TOUCHES THE SKIN IS WORN. REPAIRED THE UPPER SKIN OF THE DORSAL PER ECRA 5331-01433.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGERS 8 AND 9 IS CRACKED AROUND RIVET AT STA 787L. TRIMMED OUT CRACKED AREA OF FRAME AND INSTALLED REPAIR DOUBLERS AND FILLERS PER ECRA 5311-01439. INITIATED DIP 91636 TO READ AS FOLLOWS, BEFORE THE ACCUMULATION OF 71598 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5311-014 39.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
VERTICAL WEB AT STATION 178 BULKHEAD STRUCTURE HAS A CRACK RBL 17.1 WL-119.5. REPAIRED VERTICAL WEB STATION 178 BULKHEAD RBL 17.1 WL-119.5 PER ECRA 5311-01438.
Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
CORROSION ON SHEAR TIE AT STATION 747, STR 27R (BILGE AREA). REMOVED AND INSTALLED REPAIRED SHEAR TIE AND DOUBLER AT STATION 747 STR-27R (BILGE) REF SRM 53-00-07.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 AND 9 CRACKED AROUND HOLE STA 360 L. REPAIRED CRACK AROUND HOLE AT STA 360 L, REMOVED DAMAGED AREA (CUT OUT IN ITEM 1, 2, 3) AND MADE REPAIR ANGLES "A" & AMP; "B" AND INSTALLED AS REF EA5310-04498.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 AND 9 CRACKED AROUND RIVET HOLE STA 827L. CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED ALL REPAIR PARTS PER ECRA 5311-01435.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGERS 8 & AMP; 9 CRACKED AROUND RIVET STA 747L. FABRICATED AND INSTALLED REPAIR DOUBLERS PER ECRA 5310-04498.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
CABIN BETWEEN STA 340 AND 360 BL 0 FLOOR SUPPORT CRACKED. REMOVED AND REPLACED FLOOR SUPPORT REF 51-40-02.
Part: FRAME — CRACKED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
AIR CONDITIONING SUPPORT BRACKET ATTACHED TO THE FRAME BETWEEN STRINGER 8 & AMP; 9 CRACKED AROUND RIVET HOLE STA 867L. REPAIRED FRAME AT STA 867L STRINGER 8 & AMP; 9 PER EA 5310-04498.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 28,873 hrs · 15,348 cycles
MINOR CORROSION ON FLOORBEAM, STA 986 AT FASTENER HOLES, RBL 40-RBL 50. BURNISHED CORROSION FOUND TO BE OUT OF LIMITS AT RBL 40 AND INSTALLED REPAIR STRAP AT RBL 40 REF SRM 53-00-51 REPAIR 3.
2007
Part: LIGHT — INOPERATIVE (CABIN) · airframe 25,209 hrs · 13,486 cycles
EMERGENCY EXIT LIGHT AT SEAT 19C WAS INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT AT SEAT 19C REF AMM 33-51-81. OPS CHECK GOOD.