Registered owner
Tatonduk Outfitters Ltd
Owner type
Corporation
Serial number
33285
Year built
1944
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard, normal
Airworthiness date
July 13, 1998
Certificate issued
December 9, 1996
Expires
January 31, 2029
Mode S code
A6ED17

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney R-2800 model are included below.

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Airworthiness directives that may apply · 41

Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.

1960In forceSuperseded2026
ADs by the year they took effect: 8 ADs
19602
19631
19651
19662
19741
19791
See all 41 ADs

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations · 1

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

FAA incident reports · 1

FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.

Service difficulty reports · 13

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

SDR FXGA202105282123Skin · cracked6-8 INCH CRACK @ STA 699-704 APPX. RBL 24. REPAIR OF SKIN DAMAGE CAUSED BY CARGO LOADING/UNLOADING. REPAIR DAMAGE TO FUSELAGE SKIN @ STA 699-704 RBL 24 PER STS ENGINEERING AUTHORIZATION 81-2021-039.May 28, 2021 · N54514 · Curtis C46DCURTIS · Fuselage Main, Plate/SkinSDR FXGA201903261930Bulkhead · corrodedBULKHEAD SKIN REPAIR AT F/STA 704. TO REPAIR A CORRODED SKIN SECTION ON THE REAR BULKHEAD. PERFORM BULKHEAD SKIN REPAIR PER SRM AN 01-25LA-3 TABLE 82 AND FIGURE 229 & EAC DRAWING #1930-01.Mar 26, 2019 · N54514 · Curtis C46DCURTIS · Fuselage Main, BulkheadSDR FXGA201903211929Frame · crackedCRACKED FRAME AT F/STA 173.5 STRINGER 9R. TO REPAIR A CRACKED FUSELAGE FRAME. REMOVE AND SAVE MANUFACTURERS SPLICE BETWEEN STRINGER 11L & 12L. CUT DAMAGE FRAME ABOVE STRINGER 10L. MANUFACTURE AND INSTALL NEW FRAME SECTION PER SRM AN 01-25LA-3, FIGURE 69 & 7Mar 21, 2019 · N54514 · Curtis C46DCURTIS · Fuselage Main, FrameSDR FXGA201505121514Skin · damagedLEFT WING LE REPAIR WING STATION 376 TO 412. TO REPAIR DAMAGE TO LE OF LT WING FROM WING STATION 376 TO 412. REPAIR TOP WING SKIN AFT OF LE TO STRINGER U-15. REPLACEMENT OF STRINGER U-18 & REPAIR OF WING RIB LE PORTION AT STATION 412.May 12, 2015 · N54514 · Curtis C46* · Wing, Plate/SkinSDR FXGA2012018003Oil System · fluctuatesDURING FLIGHT SHUTDOWN NR 1 ENGINE DUE TO OIL QUANTITY AND OIL PRESSURE FLUCTUATION.Jan 10, 2012 · N54514 · Curtis C46DFLYTIGER · Engine Oil Indicating SystemSDR FXGA2011112714001Electrical Sys · surgesFLIGHT CREW EXPERIENCED VOLTAGE SPIKES, TURNED OFF ALL GENERATORS, STILL HAD VOLTAGE SPIKES AND THE TURNED OFF ALL ELECTRICAL SYS.Nov 27, 2011 · N54514 · Curtis C46DFLYTIGER · Electrical Power SystemSDR FXGAN54514001Hinge · crackedDURING THE ACCOMPLISHMENT OF THE DETAILED VISUAL INSPECTION REQUIRED BY AD 58-17-02 PARA 2 TWO CRACKS WERE FOUND ON THE ELEVATOR HINGE WEB. BOTH CRACKS ARE ON THE LT HORIZONTAL STABILIZER ONE AT STA 87 HINGE AND ONE AT STA 127 HINGE. REPAIRED IAW EAC EO 1120 Jun 14, 2011 · N54514 · Curtis C46DCURTIS · Horizontal Stabilizer StructureSDR FXGA545142Skin · dentedFUSELAGE SKIN FOUND DENTED FROM FUSELAGE STA 563L TO 583.5L, BETWEEN STR 31 AND 32. REPAIRED IAW EO 1111 AND 8110-3 FORM DATED 04/01/2011.Apr 1, 2011 · N54514 · Curtis C46ACURTIS · Fuselage Main, Plate/SkinSDR FXGA20110401001Frame · buckledFUSELAGE FRAME 583.5 WAS FOUND BUCKLED AT STR 31 LT. REPAIRED IAW EO 1111 AND 8110-3, DATED 04-01-2011.Apr 1, 2011 · N54514 · Curtis C46DCURTIS · Fuselage Main, FrameSDR FXGA514HYDHydraulic Line · crackedCOMPLETE AND TOTAL LOSS OF HYDRAULIC PRESSURE AND FLUID. A/C LANDED UNEVENTFULLY REPLACED HYDRAULIC PRESSURE LINE PART NUMBER 20-575-1209 AT MAIN ACCUMULATOR DUE TO CRACK NEAR FLARED END.Aug 24, 2010 · N54514 · Curtis C46DCURTIS · Hydraulic System, MainSDR FXGAN54514LS1520Governor · overspeedON INITIAL DESCENT LOST CONTROL OF NR 2 PROP, RPM'S ROSE TO 3100 RPM, WAS ABLE TO FEATHER. DECLARED EMERGENCY. LANDED WITHOUT INCIDENT REPLACED PROP GOV WITH SERVICEABLE UNIT AND RETURNED TO SERVICE. NO FURTHER DIFFICULTIES.Jul 9, 2010 · N54514 · Curtis C46RAIRLIFT · Propeller GovernorSDR FXGAN54514Lever · wornLANDING GEAR LEVER STUCK IN THE NEUTRAL POSITION. LANDING GEAR EXTENDED USING EMERGENCY PROCEDURES ACFT DIVERTED FOR UNEVENTFUL LANDING.May 14, 2010 · N54514 · Curtis C46DAIRLIFT · Landing Gear SelectorSDR FXG2003F00000Downlock · inoperativeON TOUCHDOWN AND ROLL OUT, RT GEAR DOWNLOCK DID NOT ENGAGE AS A/C SLOWED DOWN, GEAR RETRACTED SLOWLY. NR 2 ENG AND PROP SUFFERED A PROP STRIKE AND SUDDEN STOPPAGE. RT WING TIP DRUG ON GROUND, DURING THIS, DEICE BOOT, APPROX 4 FT. OF LOWER SKIN AND THE AILERODec 31, 2002 · N54514 · Curtis C46* · Main Landing Gear

STCs that may be installed

No STCs matched this aircraft’s modelsSTCs are matched through the model’s type certificate data sheet, and this registry model isn’t matched to one.

Earlier aircraft with this N-number · 1

This aircraft carried N54514 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.