N241CH

GULFSTREAM AEROSPACE GIV-X (G450) · 2011 · Fixed-wing multi-engine · 2 engines · 22 seats · Valid Registration

Registered owner: TTX 2 LLC, NV (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
Columbia Helicopters Peru, S.A.C.Operatoron 2013-01-07Operator named in NTSB report

Accident & incident history

Accident · 2013-01-07 Operator named in NTSB report
BOEING-VERTOL 234 Fatal injury NUSCColumbia Helicopters Peru, S.A.C.

Operated by Columbia Helicopters Peru, S.A.C. (per NTSB report)

Source: NTSB case ERA13RA106

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.

3 reports on file, 1997-09-30 – 1998-06-13.

OTHER · 1998-06-13 Matched by certificate designator
ATA 7314

Part: PUMP — WORN (NR 2 ENGINE)

DURING TAKEOFF CHECK, PILOT NOTICED NR 2 FUEL PRESS 12 PSI LOWER THAN NR 1. THIS IS LOWER THAN IT NORMALLY OPERATES WITH ENG AT FLY AND BOTH FUEL TANK BOOST PUMPS ON. PILOT VERIFIED FUEL TANK BOOST PUMPS OPERATIONAL. VERIFIED FUEL PRESS IND READING PROPERLY. WHEN BOTH NR 2 FUEL TANK BOOST PUMPS WERE TURNED OFF, NR 2 FUEL PRESS WENT INTO YELLOW. REMOVED NR 2 ENG DRIVEN FUEL PUMP AND FND INPUT SHAFT COULD BE TURNED WITH NO MOVEMENT OF PUMP IMPELLER. REMOVED AND REPLACED FUEL PUMP. SHAFT SPLINES WORN ALLOWING IT TO DISENGAGE. MALE SPLINES OF THE SHAFT HAD SMALL AREA OF WEAR. LENGTH OF FEMALE SPLINES OF THE PUMP ARE SMALLER THAN LENGTH OF MALE SPLINES CAUSING WEAR TO BE CONCENTRATED ON A SMALL AREA. (X)

Source: SDR CHIA3099
OTHER · 1998-03-17 Unresolved
ATA 6220

Part: SHOULDER BOLT — FAILED (ROTOR HEAD)

AFT ROTOR HEAD SHOULDER BOLT FAILED. SUBMITTER STATED 114R22012 IS THE IMPROVED BOLT THAT IS SUPPOSED TO PREVENT THIS TYPE OF FAILURE.

Source: SDR CHI2077
FLT CONT AFFECTED · 1997-09-30 Unresolved
ATA 6710

Part: ACTUATOR — MALFUNCTION (STICK BOOST)

ON START-UP, PILOT WAS DOING CONTROL CHECK AND NOTICED HE COULD NOT GET THE FULL TRAVEL AFT THAT IS NORMAL WHILE DOING THE CONTROL CHECKS. TROUBLESHOOTING REVEALED THAT IF ONLY ONE HYDRAULIC SYSTEM WAS SELECTED, THE ACTUATOR WOULD START BINDING AND NOT PERMIT FULL TRAVEL OF THE CYCLIC STICK FORWARD OR AFT. IF BOTH HYDRAULIC SYSTEMS WERE SELECTED, THERE WAS NO BINDING IN THE ACTUATOR. THERE WAS NO INDICATION OF A JAMMED ACTUATOR ACCORDING TO THE JAM INDICATOR BUTTONS. REPLACED ACTUATOR, CONTROL AND TRAVEL CHECKS WERE GOOD.

Source: SDR CHI1921