N424MB
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.
26 reports on file, 1995-03-12 – 2011-09-30.
Part: ENGINE — POWER LOSS · airframe 10,630 hrs · 40,759 cycles
THE PILOT REPORTED, AFTER PREFLIGHT AND CONFIRMATION CHECKS WERE CONDUCTED, LIFTED TO HOVER. USED THE ENGINE BEEP SWITCH TO SLIGHTLY INCREASE THE NR/N2 RPM TO 100 PERCENT. ON CLIMBOUT REACHING 900 FEET MSL, REDUCED COLLECTIVE TO 50 % ENGINE TORQUE TO ASSESS VISIBILITY IN RAIN AND NOTED NR/N2 DECREASED TO 99 %. THIS OUT OF NORM, PILOT TRIED USING THE BEEP SWITCH TO INCREASE THE NR/N2 BACK TO 100 %. WITH NO RESPONSE TO COMMAND AND BY INCREASING COLLECTIVE TO 60 % TORQUE WITH NO RESPONSE. PILOT ELECTED TO ABORT FLIGHT AND RETURNED TO BASE IAW RFM EMERGENCY INSTRUCTIONS UNDER DROOP COMPENSATION FAILURE.
Earlier reports · 1995–2002 · 25 reports
2002
Part: BATTERY — DISCHARGED (MAIN)
LEAD ACID BATTERY WILL NOT HOLD A CHARGE. STAYS AT 20 VOLTS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
2001
Part: TORQUEMETER — ERRATIC (COCKPIT)
TORQUEMETER INDICATOR INOPERATIVE. NR 1 NEEDLE JUMPS ERRATICALLY. RECEIVED NEW WITH A3 AND A4 CONVERSION KIT. THIS UNIT IS BRAND NEW MANUFACTURE, NOT OVERHAULED OR REPAIRED. REPLACED WITH REPAIRED UNIT CORRECTED PROBLEM. (M)
1999
Part: THERMOCOUPLE — SHORTED (ENGINE)
INTERNAL SHORT. REPLACED THERMOCOUPLE WITH NEW UNIT, CORRECTED PROBLEM. (X)
Part: TUBE — LEAKING (FUEL SYSTEM)
TUBE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — WORN (TURBINE SHROUD)
SEAL RING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTIVE PROBLEM.
Part: TUBE — LEAKING (OIL SYSTEM)
TUBE LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SEAL — LEAKING (NR 3 BEARING)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SPRING — WORN (TURBINE SECTION)
SPRING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BLADE — DAMAGED (GAS PRODUCER)
EXCESSIVE GP BLADE TIP RUB. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1998
Part: BEARING — WORN (TAIL ROTOR)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BEARING — WORN (T/R DRIVE)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1997
Part: SEAL — LEAKED (LT ENG NR 2)
LEFT ENGINE NR 2 BEARING SEAL, UPON INSTALLATION, UNIT LEAKED BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: SPEED PICKUP — FAILED (ENGINE)
SPEED PICKUP UNIT FAILED TO TEST UPON INSTALLATION. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1996
Part: BELLOWS — TORN (M/R MAST)
BELLOWS IS TORN AROUND CLAMP AND FOLD AREAS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
1995
Part: ROTOR ASSY — BLADE SHIFT (LT ENG TURB)
FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES, 3788.0.
Part: BOLT — WORN (T/R)
BOLT WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM.
Part: BUSHING — WORN (T/R)
TEFLON LINERS WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH 8 EACH NEW UNITS, CORRECTED PROBLEM.
Part: SEAL — LEAKING (NR 2 BEARING)
NR 2 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT(S) CORRECTED PROBLEM.
Part: SEAL — LEAKING (NR 3 BEARING)
NR 3 BEARING SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNITS(S) CORRECTED PROBLEM.
Part: TRANSDUCER — MALFUNCTION (OIL PRESSURE)
OIL PRESSURE FLUCTUATION. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
Part: RELAY — SHORTED (DC SYS)
SUSPECT RELAY HAS INTERNAL SHORT, UPON INSTALLATION UNIT POPS CIRCUIT BREAKER. REPLACED WITH NEW UNIT(S), CORRECTED PROBLEM.
Part: ROTARY ASSY — DISC DAMAGE (GAS PRODUCER)
DISC HAS EXCESSIVE DAMAGE (WARPED CAUSING LOOSE BLADES) RESULTING FROM LAB SEAL ELEMENT RUBBING INTO DISC KNIFE EDGES. THIS LAB SEAL HAS FEWER WELD POINTS AS COMPARED TO THE MORE RECENT SEAL DESIGN. THE LAB SEAL WAS INSTALLED NEW AS A PART OF SB 126 UPGRADE. HERE ARE THE VIBRATION RESULTS OF THE ENGINE TEST CELL RUN AT THE TIME THE ROTOR WAS INSTALLED NEW. DYNR = 0.16, GB-R = 0.21, AD-A = 0.26, PT-R = 0.15. PART TOTAL CYCLES, 1299.4.
Part: SEAL — LEAKING (NR 3 BEARING)
SEAL LEAKING BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ENGINE TOTAL CYCLES, 7,314.4.
Part: BEARING — WORN (COMPRESSOR NR 1)
BEARING WORN BEYOND SERVICEABLE LIMITS. REPLACED WITH NEW UNIT, CORRECTED PROBLEM. ENGINE TOTAL CYCLES, 7,314.4
Part: ROTOR ASSY — BLADE SHIFT (LT ENG TURB)
FAILED SB LT101-72-10-0153. EXCESSIVE IBPT BLADE SHIFT NR 7, PLUS 0.008 INCH, NR 10, PLUS 0.008 INCH. REPLACED WITH USED UNIT, CORRECTED PROBLEM. PART TOTAL CYCLES 4406.5.