Safety record in brief:2 NTSB accidents (substantial damage at worst, latest Mar 2022)7 ADs may apply9 service difficulty reports
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The pilot’s failure to maintain adequate clearance during landing on a rooftop helipad.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for CEN22LA147)
The improper securing of the exhaust duct bolts, which resulted in the duct becoming unseated and substantial heat damage to the tail rotor drive shaft.
From NTSB records; matched by N-number.Read NTSB report (search CAROL for CEN19LA146)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2026-16-13 | Turbine Section | Aug 31, 2026 | Engine (PW210S) |
| 2022-03-09 | Sikorsky Aircraft Corporation Helicopters | Mar 17, 2022 | Airframe (S-76D)Only with: Thales GPS TopStar 200 LPV receiver P/N C17149HA01 installed. |
| 2021-15-12 | Turbine Engine Compressor Section | Sep 9, 2021 | Engine (PW210S) |
| 2017-19-01 | Sikorsky Aircraft Corporation Helicopters | Jan 2, 2018 | Airframe (S-76D)Certain serial numbers: …–761075. Only with: Main rotor servo pushrod assembly P/N 76400-00034-059, 76400-00014-074, 76400-00014-076, or 76400-00014-077 installed. |
| 2016-23-10 | Sikorsky Aircraft Corporation Helicopters | Dec 12, 2016 | Airframe (S-76D) |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2015-19-51 | Sikorsky Aircraft Corporation Helicopters | Nov 10, 2015 | Airframe (S-76D)Only with: Main rotor servo input control pushrod assembly P/N 76400-00034-059 or tail rotor pushrod assembly P/N 76400-00014-071 installed. |
| 2000-11-52 | Sikorsky Aircraft Corporation Model S-76 Series Helicopters | Aug 31, 2000 | Airframe (S-76D) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
ON OUTBOUND LEG OF HEMS FLIGHT #1 VMM FAILED WITH LOSS OF COPILOTS INSTRUMENTS. TRIP ABORTED AND AIRCRAFT RETURNED TO KLIT
From FAA Service Difficulty Reports; matched by N-number and serial number.FORWARD AND AFT VIBRATION FELT IN THE CYCLIC DURING HOVER AND FLIGHT.
From FAA Service Difficulty Reports; matched by N-number and serial number.NR 1 & NR 2 ENGINE BLEED VALVE SUPPORT BRACKETS BOTH CRACKED THROUGH SUPPORT SADDLES.
From FAA Service Difficulty Reports; matched by N-number and serial number.AIR MEDICAL PUMP WILL NOT OPERATE. UPON POWER APPLIED TRIPS CIRCUIT BREAKER PROTECTION
From FAA Service Difficulty Reports; matched by N-number and serial number.#2 NAV HAS FAILURE CODE WHEN ON FREQS ABOVE 109
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING AIRCRAFT RUN-UP, NR 2 AUTOPILOT WOULD NOT COMPLETE BIT TEST DURING AP TEST. UNABLE TO CLEAR OR RESET.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT MLG DOWN INDICATION INTERMITTENT. LEG HAS BROKEN WIRES IN HARNESS.
From FAA Service Difficulty Reports; matched by N-number and serial number.LEFT MLG DOWN INDICATION INTERMITTENT. FOUND WIRE HARNESS BROKEN.
From FAA Service Difficulty Reports; matched by N-number and serial number.DURING LANDING APPROACH TO HOSPITAL LANDING PAD, LT MAIN LANDING GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH AND GREEN SAFE LIGHT NOT ILLUMINATED. APPROACH ABORT AND TRANSITIONED TO THE AIRPORT WHERE A VISUAL OF THE LANDING GEAR WAS COMPLETED TO ENSURE DOWN. LT SEGMENT OF MAIN GEAR HARNESS WIRE BROKEN.…
From FAA Service Difficulty Reports; matched by N-number and serial number.