N825H

BELL 214ST · 1984 · Rotorcraft · 2 engines · 18 seats · Valid Registration

Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
Erickson Helicopters, Inc. (9EKA)Certificate holder—Matched 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.

10 reports on file, 1998-07-21 – 2018-10-30.

OTHER · 2018-10-30 Matched by certificate designator
ATA 5320

Part: SUPPORT — CRACKED (NOT REPORTED) · airframe 9,614 hrs · 7,529 cycles

PN 214-031-240-173 SUPPORT FOUND CRACKED DURING AIRFRAME INSPECTION.

Source: SDR 9EKA2018110810003
OTHER · 2017-05-26 Matched by certificate designator
ATA 6210

Part: EROSION SHIELD — DEBONDED (MAIN ROTOR BLADE) · airframe 9,556 hrs · 7,453 cycles

DURING PREVENTATIVE TOUCH UP PAINT ON MAIN ROTOR BLADE, DISCOVERED LOWER BLADE EROSION PLATE DEBONDED AT BOND LINE

Source: SDR 9EKA20170527002
OTHER · 2016-08-07 Matched by certificate designator
ATA 5320

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 9,131 hrs · 6,578 cycles

DURING POST FLIGHT DISCOVERED A 4" SKIN CRACK IN FUSELAGE AFT OF RT PILOT DOOR. DURING HIDDEN DAMAGE INSPECTION, FOUND CRACKED BULKHEAD DOOR POST SUPPORT AT STA 142.50, WL 22.00, BL 40.0.

Source: SDR 9EKA20160808010
VIBRATION/BUFFET · 2016-04-20 Matched by certificate designator
ATA 5310

Part: BEAM — CRACKED (FUSELAGE) · airframe 9,044 hrs · 6,377 cycles

DURING INSPECTION OF AIRFRAME FOR SUSPECTED CAUSE FOR TWO REV VIBRATIONS, FOUND A 4.9 INCH X1.25 INCH CRACK IN THE LT BAGGAGE COMPARTMENT & ENG DECK AT FS STATION 278 - 280. FUSELAGE LT UPPER BEAM CAP IS CRACKED IN LT BAGGAGE COMPARTMENT & UNDER ENG DECK.

Source: SDR 9EKA20160420005
OTHER · 2013-11-01 Matched by certificate designator
ATA 6320

Part: CASE — CRACKED (XMISN RING GEAR) · airframe 8,402 hrs · 5,135 cycles

DURING INVESTIGATION OF AN OIL LEAK, A CRACK WAS FOUND IN THE MAIN TRANSMISSION UPPER LEFT HAND RING GEAR CASE .

Source: SDR 2013FA0000625
OTHER · 2001-11-02 Matched by certificate designator
ATA 5302

Part: HANGER ASSY — MISMANUFACTURED

WILL NOT FIT IN SUPPORT ON AIRCRAFT. HOLES MILLED IN WRONG AREA.

Source: SDR HEEA077036
OTHER · 1998-08-17 Matched by certificate designator
ATA 5330

Part: PANEL — MISMANUFACTURED (FUSELAGE)

THREE EACH DOUBLER RINGS ON BOTTOM OF PANEL BONDED ON 180 DEGREES OUT - SLOT ON RING NEEDS TO BE FACING OUTBOARD AND AFT CENTER ACCESS HOLE SEPARATED.

Source: SDR HEEA0015627
INADEQUATE Q C · 1998-07-30 Matched by certificate designator
ATA 5347

Part: TRACK — MISMANUFACTURED (FUSELAGE)

LOWER OUTBOARD FLANGE TOO NARROW TO PICK UP FASTENERS.

Source: SDR HEEA0015413
INADEQUATE Q C · 1998-07-21 Matched by certificate designator
ATA 5320

Part: STIFFENER — MISMANUFACTURED (FUSELAGE)

STIFFENER MISMANUFACTURED. PART DOESN'T FIT THE POSITION ON THE AIRFRAME.

Source: SDR HEEA0015206
INADEQUATE Q C · 1998-07-21 Matched by certificate designator
ATA 5347

Part: TRACK — MISMANUFACTURED (FUSELAGE)

LOWER OUTBOARD FLANGE TOO NARROW TO PICK UP FASTENERS.

Source: SDR HEEA0015205