N413LX
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, 2007-10-03 – 2012-05-01.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHEDULED INSPECTION, MX TECH FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSP, MX TECH FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, MX FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. CRACKS WERE FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW KIT 128-6200-1.
Part: RIB — CRACKED (ZONE 300) · airframe 10,137 hrs · 8,460 cycles
DURING SCHEDULED INSPECTION, MX TECH FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, FOUND 12 RIBS CRACKED IN THE HORIZONTAL STAB. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSP, MX TECH FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, MX FOUND 12 RIBS CRACKED IN THE HORIZONTAL STAB. CRACKS WERE FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, MX FOUND 12 RIBS CRACKED IN THE HORIZONTAL STAB. CRACKS WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSP, MX FOUND 12 RIBS CRACKED IN THE HORIZONTAL STAB. CRACKS WERE FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSP, MX TECH FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 10,137 hrs · 8,460 cycles
DURING SCHDULED INSPECTION, MX FOUND 12 RIBS CRACKED IN THE HORIZ STABILIZER. EACH CRACK WAS FOUND TO BE EMINATING OUTWARD FROM A FASTENER HOLE ON THE ATTACHEMENT FLANGES OF THE RIBS WHERE THE BLIND FASTENERS WERE INSTALLED ON THE LOWER SKIN. ALL 12 RIBS WERE REPLACED IAW MFG KIT 128-6200-1.
Earlier reports · 2007–2009 · 3 reports
2009
Part: CONTROL CABLE — BROKEN (TE FLAPS) · airframe 8,151 hrs · 6,835 cycles
WHILE INSPECTING FLIGHT CONTROL CABLES FOR A REPORTED VIBRATION DISCREPANCY, MX DISCOVERED THE FWD (EXTENSION) FLAP FOLLOW-UP CABLE BROKEN AT THE CRIMPED FERRULE FOR THE CENTER BELL CRANK. INSP OF THE BREAKAGE REVEALED SEVERE CORROSION CONCENTRATED IN THE AREA OF THE CABLE BENEATH THE FERRULE. THE CABLE WAS REMOVED AND REPLACED.
2007
Part: HOSE — RUPTURED (HYD SYSTEM) · airframe 7,292 hrs · 6,100 cycles
ON APPROACH CREW EXPERIENCED COMPLETE HYDRAULIC FAILURE AT 4000' ON APPROACH INTO KDAL, LOST ALL HYDRAULIC PRESSURE WITHIN ABOUT 20 SEC. AFTER FIRST INDICATION OF A PROBLEM, DECLARED AN EMERGENCY, RAN THE EMERGENCY CK LIST FOR GEAR EXTENSION, ZERO FLAP LANDING, AND EMERGENCY BRAKING. LANDED AND USED EMERGENCY BRAKING. CREW FOUND HYDRAULIC RESERVOIR COMPLETELY EMPTY. MAINTENANCE DISCOVERED HYDRAULIC PUMP PRESSURE HOSE RUPTURED. THERE WAS NO EVIDENCE OF CHAFFING OR OTHER DAMAGE TO THE HOSE AT THE POINT WHERE IT RUPTURED HOSE WAS REPLACED.
Part: RIB — CRACKED (HORIZONTAL STAB)
DURING A SCHEDULED MAINTENANCE VISIT WHILE PERFORMING A HORIZONTAL STABILIZER ROLLER INSPECTION OF THE HORIZONTAL STABILIZER IB RIB AND BRACKET ASSEMBLIES, THE LT IB ROLLER BRACKET WAS FOUND CRACKED. DETAILED INSPECTION INSTRUCTIONS OF THIS AREA ARE OUTLINED IN MFG COMMUNIQUE' NR 70. MAINTENANCE REPLACED THE RIB.