N575EH
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.
7 reports on file, 2003-02-13 – 2009-01-02.
Part: FIRE WARNING — FALSE INDICATION
DURING FLIGHT, THE FIRE HANDLE LIGHTS AND THE CAUTION FIRE WARNING LIGHT ILLUMINATED WITH THE TONE IN THE HEADSET. NO SECONDARY INDICATIONS ON THE ENGINE. FOLLOWED EMERGENCY PROCEDURE AND LANDED AT BASE.
Part: FIRE DETECTOR — ACTIVATED (FIRE WARNING)
DURING FLIGHT THE FIRE HANDLE LIGHTS AND THE CAUTION FIRE WARNING LIGHT ILLUMINATED WITH THE TONE IN THE HEADSET. NO SECONDARY INDICATIONS ON THE ENGINE. (K)
Part: TIP CAP — DEBONDED (M/R BLADE) · airframe 30,821 hrs
TIP CAP ASSY BOTTOM DISBONDED. SENT TO CTI FOR REPAIR. INSPECTED PER SA4047-76-5 REV11; REPAIRED KEVLAR PER PROCEDURE NR 2 AND NR 18 1 PLY; REFINISHED PER DRWG NO 76150-09043; STATIC BALANCE PER RS-005N-VI.
Part: CAP — CRACKED (M/R BLADE) · airframe 284 hrs
LEADING EDGE ABRASION STRIP AND UPPER OUTER DOUBLER CRACKED. C-CHANNEL DEBONDED AND DAMAGED AS INDICATED. SENT TO FOR REPAIR. INSPECTED IAW SA4047-76-5 REV11; REPLACED ABRASION STRIP IAW RS-005N-III, MODIFIED EXTERNAL DOUBLERS IAW RS-017. INSTALLED STAINLESS STEEL TIP COVER IAW RS-017-II; REPLACED BOTH FORWARD INTERNAL DOUBLERS AND REBOND C CHANNEL IAW DRWG NR 76150-09043 SPEC 38023-15000; REFINISHED IAW DRWG NO 76150-09043; STATIC BALANCE IAW RS-05N-VI.
Part: FIRE BOTTLE — MISREPAIRED (MAIN) · airframe 2,841 hrs
FIRE BOTTLE NEEDS TO BE SERVICED. INCORRECT GAUGE INSTALLED. HYDRO TESTED, OVERHAULED, INSTALLED GAUGE, FILLED, LEA AND WEIGHT CHECKED.
Part: BLADE — DAMAGED (TAIL ROTOR) · airframe 2,841 hrs
POLYURETHANE STRIP ERODED BOTH BLADES, TRAILING EDGE TAB DAMAGED. EROSION NEAR TIP. SENT FOR REPAIR. X RAYED ULTRASONIC INSPECTED IAW QATI 3016 AND 3098, PERFORMED ALL SCHEDULED INSPECTIONS UOP TO AND INCLUDING 1500 HR INSP IAW COMPOSITE MATERIALS MANUAL 4047-76-5 TABLE 2-2 AND MM 4047-76-2, 65-21-00 AND 65-21-01, INSPECTED ELLIPTICAL PLUG FOR DEBONDING IAW AD 94-14-20; COMPLIED WITH ASB 76-65-43 AND 76-65-46; REPLACED SPAR PLUG IAW RS-0221-II; REPAIRED TRAILING EDGE DAMAGE ON PADDLE A IAW RS-018M-IV; REPAIRED GOUGE IN PITCH HORN BUSHING AREA ON BOTH PADDLES IAW OR176100-018 PART VI; REPLACED BOTH PRIMARY POLYURETHANE STRIPS IAW RS-018M-1; REPLACED.
Part: TIP CAP — DEBONDED (M/R BLADE) · airframe 1,956 hrs
DOUBLER DEBONDING, WORN. SENT TO CTI. INSPECTED PER SA 4047-76-5 REV 11; MODIFIED EXTERNAL DOUBLERS PER RS-017-1; REPLACED ABRASION STRIP PER RS-005N-III; REPAIRED KEVLAR PER PROCEDURE NR 2 AND 18 -1 PLY; REFINISHED PER DRAWING NR 76150-09043; STATIC BALANCE PER RS-005N-VI.