N699DA
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.
8 reports on file, 2003-02-27 – 2006-10-03.
Part: COMPRESSOR WHEEL — CRACKED (LT ENGINE)
(REF NR: 6841.5.30) DURING A SCHEDULED INSPECTION, EDDY CURRENT NDT REVEALED A CRACK IN THE LT ENGINE HP COMPRESSOR STAGE 1 ROTOR. (K)
Part: ACTUATOR — DEFECTIVE (NLG) · airframe 1,305 hrs · 1,097 cycles
LT MAIN UNSAFE INDICATION, RAN ALT GEAR EXT CHECKLIST. ENDED UP WITH LT MAIN AND NOSE GEAR UNSAFE INDICATION ADN FLAPS WOULD NOT EXTEND BEYOND 20 DEGREES. FLIGHT CREW DID A BLOW DOWN CYCLE OF THE LANDING GEAR TO SEE IF THAT WOULD CLEAR THE INDICATION. IT DID NOT. LT MAIN GEAR ACTUATOR AND DOWN AND LOCKED SWITCH (PN P624007) WERE REPLACED IAW MFG. MAINT CHECKS WERE CARRIED OUT IAW MM, NO FURTHER DEFECTS NOTED. AC WAS RETURNED TO SERVICE. (PA-04-004 CNTRL NR) (K)
Part: AXLE — CORRODED (NLG)
DURING NOSE WHEEL TIRE CHANGE THE INNER BORE OF THE NOSE AXLE WAS FOUND TO BE CORRODED. PART HAD TO BE ORDERED TRIP WAS CANCELLED. REMOVED CORRODED AXLE (PN 2342117002) SN R274 AND INSTALLED NEW AXLE IAW MFG MM. AIRCRAFT WAS RETURNED TO SERVICE.
Part: INDICATOR — MALFUNCTIONED (CABIN PRESSURE)
PRESSURIZATION SYSTEM LIGHT ON. CABIN ALTITUDE RATE GAUGE FLUCTUATING WILDLY. CABIN PRESSURE INDICATOR INOPERATIVE. TROUBLESHOT PRESSURIZATION SYSTEM IAW MM CHAPTER 21-30-00 PAGE 216 STEPS 1 THROUGH 25. FOUND NO DEFECTS WITH PRESSURIZATION CONTROLLING SYSTEM. OBSERVED CABIN PRESSURE INDICATOR FLUCTUATING FROM PLUS 2000 FEET TO -2000 FEET WITH ONLY APU OPERATING. INSTALLED SERVICEABLE CABIN PRESSURE INDICATOR AND PERFORMED SUCCESSFUL OPERATIONAL CHECK OF THE CABIN PRESSURIZATION SYSTEM IAW THE MM CHAPTER 21-30-00 PATE 201 STEP A. RETURNED AIRCRAFT TO SERVICE. (M)
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)
CABIN PRESSURE CONTROLLER MALFUNCTIONING IN AUTO MODE. AIRCRAFT ABORTED ITS TAKEOFF. DEFER PER MEL SECTION 21-1. MO410-1, AFL NR 00817. AIRCRAFT RETURNED TO SERVICE. (M)
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)
CABIN PRESSURE CONTROLLER MALFUNCTIONING IN AUTO MODE. AIRCRAFT ABORTED ITS TAKEOFF. FAILURE OF THE PRESSURIZATION SYSTEM TO OPERATE IN AUTO MODE. REPLCED FLOW CONTROL VALVE. REPLACED LEFT EMERGENCY PRESSURIZATION VALVE. REPLACED CABIN PRESSURIZATION CONTROLLER. SYSTEM OPERATIONAL TEST PER LEARJET MM. THIS CLEARED DMI LOG M0410-1. AIRCRAFT WAS RETURNED TO SERVICE. (M)
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)
CABIN PRESSURIZING AS THROTTLES ARE ADVANCED FOR TAKEOFF. UNABLE TO DETERMINE CAUSE. CONTRACTED AN OUTSIE AGENCY FOR ASSISTANCE. AN OPERATIONAL CHECK OF THE CABIN PRESSURIZATION SYSTEM WAS COMPLIED WITH PER LEAR 60 MM 21-30-00. NO DEFECTS NOTED. AIRCRAFT WAS RETUREND TO SERVICE, AND RETURNED TO HOME BASE. (M)
Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE)
THE AIRCRAFT BEGAN ITS TAKEOFF ROLL, AT TAKEOFF POWER THE WHEELS BROKE GROUND AND THE PRESSURIZATION BEGAN TO DRIVE THE CABIN TO SEA LEVEL. THE CABIN BEGAN TO PRESSURIZE AT A RAPID RATE WITH BLEED AIR FORM THE ENGINES ON POWER UP. NO POSITIVE REASON WAS IDENTIFIED. THE AIRCRAFT RETURNED TO THE DEPARURE RAMP AND THE MX DEPARTMENT PERFORMED A CABIN PRESSURIZATION OPERATIONAL CHECK IAW THE LEAR 60 MX MANUAL, 21-30-00, PAGE 215. NO DEFECTS WERE NOTED, AND THE DISCREPANCY COULD NOT BE DUPLICATED. THE AIRCRAFT WAS RELEASED AND RETURNED TO SERVICE. (M)