N576EH
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.
10 reports on file, 1999-03-16 – 2008-07-31.
Part: CIRCUIT BREAKER — SMOKE (SEARCH LIGHT)
RT SIDE HSI FAILED FOUND CB ABOVE THE SEARCH LIGHT CONTROL BREAKER POPPED AND THE PILOTS CLOCK DISPLAY BLANK RESET CIRCUIT BREAKER THEN DETECTED SMOKE OPENED CIRCUIT SMOKE ODOR WENT AWAY. ACFT LANDED SAFELY.
Part: SEARCH LIGHT — SMOKE (COCKPIT)
SEARCHLIGHT CIRCUIT BREAKER POPPED, RESET AND PILOTS DETECTED SMOKE. OPENED CIRCUIT CONTINUED FLIGHT WITH NO FURTHER ODOR OF SMOKE. NORMAL ACFT SHUTDOWN.
Part: ELECTRICAL SYS — FAILED
RT SIDE HSI FAILED, FOUND CB ABOVE THE SEARCH LIGHT CONTROL BREAKER POPPED AND THE PILOTS CLOCK DISPLAY BLANK RESET CIRCUIT BREAKER THEN SMELLED SMOKE OPENED CIRCUIT SMOKE SMELL WENT AWAY, ACFT LANDED SAFELY. (K)
Part: CIRCUIT BREAKER — POPPED (SEARCHLIGHT)
SEARCHLIGHT CIRCUIT BREAKER POPPED, RESET AND PILOTS SMELLED SMOKE. OPENED CIRCUIT CONTINUED FLIGHT WITH NO FURTHER SMELL OF SMOKE. NORMAL AIRCRAFT SHUTDOWN. (K)
Part: BLADE — PEELING (MAIN ROTOR) · airframe 14,691 hrs
TRIM TAD PEALING/SEPARATED. INSPECTED, PERFORMED X RAY ULTRASONIC INSPECTIONS PER QATI 3048, 3016, SS8806 & 3095, PERFORMED ALL INSPECTIONS UP TO AND INCLUDING 900 HOUR INSPECTIONS, COMPLIED WITH AD 884-10-02 & ASB 76-65-18C; REPLACED TRIM TAB 1 ER PER RS-006K-III; REPLACED NICKEL STRIP PER RS-007J-1; REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9; REPLACED 4 EA ROOT END THROUGH BUSHINGS PER RS-004N-VII; REINSTALLED TIP CAP SN A175-03282; REFINISHED WITH HIGH VIS SCHEME 2 PER SA 4047-76-5 DRWG 76150-09000 AND 76150-09100; STATIC BALANCED PER CTI-DAL-DA-026 @ TT 9172.0
Part: BLADE — DAMAGED (MAIN ROTOR) · airframe 14,078 hrs
M/R BLADE SEPARATION BETWEEN TIP RIB AND BLADE ASSY. INSPECTED, PERFORMED X RAY, ULTRASONIC INSPECTIONS PER QATI3048-3016, SS8806 & 6095, PERFORMED ALL INSPECTIONS UP TO AND INCLUDING 900 HOUR INSPECTIONS CMPLIED WITH AD 84-10-02, ASB 76-65-18C &N ASB 76-65-57. REPLACED SHIMS PER SA4047-76-5 PROCEDURE NO 9 REV 9 REPLACED 4 ROOT END THROUGH BUSHINGS PER RS-004N-VII; REPLACED STIFFNERS PER RS-003C; REPAIRED VOID ON UPPER SURFACE AT TIP PER PROCEDURE NR 18-1PLY; REPLACED NICKEL STRIP PER RS-007J-I; INJECTED SHEATH VOID AT TIP PER SA4047-76-5 PROCEDURE 2; REINSTALLED TIP CAP SN A175-03746; REFINISHED PAINT WITH HIGH VIS SCHEME 02 PER S76 SRM SA4047-76-5 DRWG 76150-09000 AND 76150-09100; STATIC BALANCED PER CTI-DAL-
Part: ALTIMETER — FAILED (RADAR) · airframe 12,485 hrs
RADAR ALTIMETER WAS OVERHAULED BY FREESCAN 2 / 2001 AND RET'D TO ERA . INSTALLED ON AIRCRAFT AND HAD TO REMOVE DUE TO BEING TOTALLY INOPERABLE. RETURNING TO FREESCAN ON ERA REPAIR ORDER RW-884523 REQUESTING WARRANTY REPAIR.
Part: INDICATOR — FAILED (N1 TACH)
N1 TACH INDICATOR PURCHASED FROM TURBOMECA 9/13/99. LED DIGITS WILL NOT ILLUMINATE.
Part: OVERSPEED BOX — FAILED (NR 1 ENGINE)
NR 1 ENGINE FAILED IN-FLIGHT. INVESTIGATION AND TROUBLESHOOTING INDICATED THAT THE OVERSPEED BOX FAILED.
Part: RECEIVER — MALFUNCTIONED (COCKPIT NAV)
UNIT RECEIVER ORIGINAL WITH AIRCRAFT WHEN PURCHASED. KNR634 CAUSES DME TO CYCLE.