N2269A
Registered owner: SHIELD AI INC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
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.
26 reports on file, 1995-11-07 – 1999-04-06.
Part: ENCODER — FAILED (COCKPIT)
ALTIMETER ENCODER NOT FUNCTIONING.
Part: TORQUE GAUGE — READS LOW (ENGINE)
TORQUE GAUGE READS LOW.
Part: SENSOR — DEFECTIVE (FUEL CELL)
FLOAT LEAKING. UNIT WAS PURCHASED ON 6-7-89.
Earlier reports · 1995–1998 · 23 reports
1998
Part: TANK UNIT — OUT OF TOLERANCE (FUEL SYSTEM)
TRANSMITTER IN FUEL TANK TRANSMITS HIGH OUT OF TOLERANCE.
Part: MOUNT — FAILED (TRANSMISSION)
CAUSED YELLOW TEMP INDICATOR ON INPUT SHAFT TO TURN BLACK.
Part: REGULATOR — DEFECTIVE (DC SYS)
VOLTS REG DEFECTIVE. NOT ADJUSTABLE ABOVE 270 FEET.
Part: ACTUATOR — FAILED (M/R CONTROL)
ACTUATOR MOTOR WILL NOT RUN.
1997
Part: VALVE — FAILED (FUEL SYS)
VALVE STAYS OPEN INTERMITTENTLY.
Part: FUEL PUMP — LEAKING (SEAL DRAIN)
FUEL LEAKING FROM SEAL DRAIN.
Part: BEACON — WONT TEST (ULB UNIT)
BEACON WILL NOT TEST.TIME SINCE REPAIR 253:50.
Part: INDICATOR — PRECESSES (COCKPIT ATTITUDE)
ATTITUDE INDICATOR PRECESSES EXCESSIVELY.
Part: TRANSCEIVER — INOPERATIVE (COCKPIT ATC)
MODE "C" INOPERATIVE. PERFORMED PRELIMINARY INSPECTION, TESTED, ADJUSTED PULSE WIDTH AND FREQUENCY. REPLACED MISSING PHOTOCELL LENS P/N 088-00655-0000. BENCH CHECK GOOD.
Part: INDICATOR — FAILED (COCKPIT ATTITUDE)
ATTITUDE INDICATOR WOULD NOT ERECT.
Part: ACTUATOR — FAILED (M/R CONTROL)
ACTUATOR DOES NOT OPERATE.
Part: AIRSPEED IND — LEAKS (COCKPIT)
AIRSPEED INDICATOR LEAKS DURING STATIC SYSTEM CHECK.
Part: TRANSPONDER — INOPERATIVE (COCKPIT)
TRANSPONDER MODE C INOPERATIVE. PERFORMED PRELIMINARY INSPECTION. FOUND POWER OUT LOW, ADJUSTED V101. NO HELP. REPLACED V101 CAVITY TUBE P/N C2080A. REPAIRED. BENCH CHECK GOOD.
1996
Part: SCROLL ASSY — OVERSIZE (PROBE ELBOW)
UPON PRE-ASSEMBLY INSPECTION OF PART NOTED THE FOLLOWING: I.D. OVERSIZED ON SCROLL PROBE ELBOW BORE AS MARKED. REPLACED DISCREPANT PART. PART RETURNED TO DALLAS AIRMOTIVE FOR 100% WARRANTY REPAIR PER ROB HALDEMEN'S INSTRUCTIONS.
Part: TRANSCEIVER — FAILED (COCKPIT)
WILL NOT REPORT. FOUND UNIT DRAWS EXCESSIVE CURRENT. REPLACED CAVITY OSCILLATOR V101. REPAIRED. ADJUSTED PULSE WIDTH AND FREQUENCY. BENCH CHECK GOOD.
Part: TRANSCEIVER — DEFECTIVE (COCKPIT VHF)
READOUT STAYS DIM IN BRIGHT LIGHT. FOUND THAT DISPLAY LENS HAD LOST IT'S TINT. REPLACED DISPLAY LENS - REPAIRED PROBLEM. ADJUSTED SIDETONE. BENCH CHECK GOOD.
Part: SERVO — LEAKING (FLT CONTROL)
SERVO LEAKING AT PISTON SHAFT.
Part: SERVO — LEAKING (FLT CONTROL)
SERVO LEAKING AT PISTON SHAFT.
Part: STRAP — CRACKED (AFT CABIN)
PART IS CRACKED. AFT CABIN OVERHEAD BOX BEAM R/H STRAP P/N 206-031-200-076 CRACKED OUT AT CENTER R/H SUPPORT. INSTALLED NEW STRAP ASSEMBLY.
1995
Part: TRANSCEIVER — DEFECTIVE (COCKPIT ATC)
TWO YEAR INSPECTION REQUIRED. FOUND V101 CAVITY OSCILLATOR WEAK AND V301 PHOTODETECTOR INOPERATIVE. REPLACED BOTH ITEMS. ADJUSTED POWER OUT AND FREQUENCY TO SPECS. BENCH CHECK GOOD.
Part: SPAR ASSY — CORRODED (HORIZ STAB)
SPAR ASSY IS CORRODED. (CORROSION AND WORN BEYOND LIMITS) REPLACED WITH SERVICEABLE SPAR ASSY.
Part: FITTING — MIS MFG (BOX BEAM)
PILOT HOLES ON VERTICAL FLANGE OF FITTING DO NOT ALIGN WITH EXISTING FASTENER HOLES ON BOX BEAM.
Part: CROSSTUBE — CORRODED (AFT SKID)
CROSSTUBE IS CORRODED. (CORROSION AT MOUNT PAD .011 BEYOND LIMITS.)