N714P

No registry detail on file · not in current registry

Operators of this aircraft

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

OperatorRolePeriodBasis
PHI Aviation, LLC (HEEA)Certificate holderMatched by certificate designator

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.

11 reports on file, 1999-02-14 – 2024-07-23.

SMOKE/FUMES/ODORS/SPARKS · 2024-07-23 Matched by certificate designator
ATA 2170

Part: MOTOR — INOPERATIVE (EVAP BLOWER) · airframe 7,440 hrs

15 MINUTES FROM HOUMA, SMOKE WAS OBSERVED COMING OUT OF A/C VENTS. AIR CONDITIONER AND FAN WERE TURNED OFF AND SMOKE IMMEDIATELY STOPPED.

Source: SDR HEEA202407240001
WARNING INDICATION · 2023-02-10 Matched by certificate designator
ATA 2400

Part: CONTACTOR — INOPERATIVE · airframe 10,583 hrs · 13,679 cycles

DURING CRUISE IN IMC NO 2 DC GENERATOR FAILED AND DID NOT RESET AFTER EMERGENCY PROCEDURE WAS PERFORMED.

Source: SDR 2023FA0000085
OTHER · 2019-05-21 Matched by certificate designator
ATA 3200

Part: BOLT — WORN (LANDING GEAR) · airframe 9,182 hrs

SUPPLEMENTAL ISSUE FOR REVISED SDR. LEFT MAIN LANDING GEAR WOULD NOT EXTEND. REPAIRED LANDING GEAR. AIRCRAFT PLACED ON JACK, PERFORMED OPERATION CHECK OF LANDING AND THE GEAR WOULD NOT EXTEND. FOUND LEFT MAIN LANDING GEAR TIE DOWN RING IN THE UP POSITION CAUSING THE GEAR NOT TO EXTEND DOWN. REMOVED TIE DOWN CLEVIS AND BUSHINGS, CLEANED AND INSPECTED AND FOUND THE BOLT WORN. REPLACED THE BOLT AND REINSTALLED THE CLEVIS. ALSO REPLACED WORN LEFT HAND MAIN LANDING GEAR DOOR LINK SWIVEL FITTING.

Source: SDR HEER20190521985
SMOKE/FUMES/ODORS/SPARKS · 2011-04-01 Matched by certificate designator
ATA 2197

Part: WIRE — BURNED (AIR CON) · airframe 3,586 hrs

UPON DESCENDING FOR A NORMAL LANDING TO ST300 AT ABOUT 3000 FT PIC AND SIC NOTICED A VERY STRONG ODOR OF FUMES (ELECTRICAL FIRE) IN THE COCKPIT. COCKPIT STARTED TO GET HAZY FROM ALL THE SMOKE. TRIED TO ISOLATE BY TURNING OFF AIR CONDITIONER TO NO AVAIL. NOTICED BOTH PILOT AND CO-PILOT AP1 AND AP2 CYCLIC LIGHT FLICKERING ALONG WITH "FD" FLAG FLASHING ON THE ADI. TEMPORARILY TURNED OFF CO-PILOT CRT SCREENS TO SEE IF SMOKE CLEARED. PULLED OUT CHECK LIST AND FOLLOWED EMERGENCY PROCEDURES. WITH SECONDARY INDICATIONS AND UNABLE TO ISOLATE, LANDED AS SOON AS POSSIBLE WHICH WAS ON SS259. MX FOUND THE GROUND WIRE FOR THE AIR CONDITIONER TO HAVE BURNED AND PULLED OUT OF THE TERMINAL END THAT CONNECTS TO THE STRUCTURE. THIS CAUSED THE AIR CONDITIONER TO SEEK GROUND THROUGH THE MOUNTING BOLTS FOR THE AIR CONDITIONER PALLET.

Source: SDR HEEA130629
WARNING INDICATION · 2010-09-28 Matched by certificate designator
ATA 2211

Part: TRANSDUCER — DEFECTIVE · airframe 2,904 hrs

ENGINE OUT LIGHT AND AUDIO WITH ASSOCIATED YAW KICK ON TAKEOFF. TROUBLESHOT AND FOUND TRANSDUCER DEFECTIVE. REPLACED TRANSDUCER.

Source: SDR HEEA129496
SMOKE/FUMES/ODORS/SPARKS · 2010-03-02 Matched by certificate designator
ATA 2150

Part: MOTOR — FAILED (EVAPORATOR) · airframe 1,965 hrs

ON CLIMB OUT OFF OF MCY AT 400 FEET BOTH PILOTS SMELLED ACRID ODOR. ACFT RETURNED TO BASE. CAUSE OF PROBLEM, EVAPORATOR MOTOR, PN 85-02-250-1, SN K31045. REPLACED.

Source: SDR HEEA127665
NO TEST · 2001-09-07 Matched by certificate designator
ATA 3350

Part: LIGHT — LOOSE (CABIN) · airframe 15,412 hrs · 5,110 cycles

THE EGRESS LIGHT WAS INOPERATIVE AT SEAT 14D. SECURED LIGHT STRIP.

Source: SDR ZW0A0108201
PARTIAL RPM/PWR LOSS · 2001-05-31 Unresolved
ATA 7230

Part: STATOR VANE — FRACTURED (NR 1 ENGINE) · airframe 14,318 hrs · 4,802 cycles

JUST AFTER TAKEOFF CREW HEARD LOUD NOISE FROM NUMBER 1 ENGINE, FOLLOWED BY EGT GOING TO 653. CREW SHUT DOWN THE ENGINE AND RETURNED TO STL. METAL WAS FOUND IN THE TAIL PIPE AND THE ENGINE WAS REPLACED. FOUND VANES FROM THE 10TH AND 11TH STAGE COMPRESSOR, QUADRANT NUMBER 4, HAD FRACTURED AT THE 10 O'CLOCK POSITION AND MOVED INTO THE GAS PATH STRIKING THE C-10 BLADES. THE DAMAGE THEN MULTIPLIED.

Source: SDR ZW0A0102704
NO TEST · 2001-01-07 Unresolved
ATA 3350

Part: LIGHT — CONTAMINATED (CABIN) · airframe 12,724 hrs · 4,313 cycles

THE EGRESS LIGHT STRIP IN FIRST CLASS WAS INOPERATIVE. DRIED MOISTURE FROM LIGHT TRACK IN FIRST CLASS. CHECK-C 8-16-00 LAX.

Source: SDR TWAA0100504
OTHER · 1999-09-26 Unresolved
ATA 2565

Part: SLIDE — WORN (R4 DOOR)

WHILE PARKED AT THE GATE THE NUMBER 4 CABIN DOOR ON THE RT SIDE OF THE AIRCRAFT WAS OPENED WHILE THE ESCAPE SLIDE WAS ARMED. THE ESCAPE SLIDE DID NOT FULLY DEPLOY. REPLACED THE ESCAPE SLIDE. CHECK-C 2-20-99 LAX.

Source: SDR TWAA9913204
OTHER · 1999-02-14 Unresolved
ATA 5753

Part: PANEL — DAMAGED (LT TE FLAP)

DURING CHECK-C MAINT, FOUND THE LT WING I/B FLAP TRAILING EDGE AFT FLAP BOTTOM SIDE, LOWER WEDGE PANEL WITH A .375 INCH TEAR LOCATED APPROXIMATELY 4 FT O/B BY 11 INCHES HIGH FROM I/B END. REPAIRED PER SRM 51-70-17 (REFERRED FROM SRM 57-53-01) WITH MINIMUM OF 2 PLYS PER NOTE B OF FIG 24, WITH 2 LAYERS OF ADHESIVE TOP AND BOTTOM. COOKED AT 200 DEG, SEALED AND PAINTED.

Source: SDR TWAA9902707