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N741

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1946 Grumman G-21A · Pratt & Whitney R-985 series

Open in FAA registry

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Registered owner
Damico Samuel P
Location
Pittsford, NY
Owner type
Individual
Serial number
B-97
Year built
1946
Type
Fixed wing multi engine
Engine
Reciprocating
Airworthiness
Standard
Airworthiness date
April 17, 1957
Certificate issued
January 7, 2010
Expires
July 31, 2029
Mode S code
A9F640
Grumman G-21AAirframe model · 8 seats · 2 engines · 34 registeredTCDS TC 654Airframe · Grumman G-21AEngine modelPratt & Whitney R-985 series

From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Pratt & Whitney R-985 model are included below.

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Airworthiness directives that may apply · 10

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

1964In forceSuperseded2026

Information bulletins that may apply

Advisory, not mandatory.

No bulletins matched this aircraft’s models

NTSB investigations · 2

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

NTSB ANC08FA050Accident · Serious injuriesField investigationFinal reportUnalaska, AKThe pilot's failure to maintain clearance from a truck while landing, and the vehicle operator's decision to ignore runway warning signals. Contributing to the accident was an inoperative vehicle gate system and the failure of airport management to adequately…Apr 10, 2008 · Substantial damageNTSB ANC94GA041Accident · Minor injuriesFinal reportMt. Fairweather, CanadaThe pilot's improper decision in attempting to outclimb the rising terrain with the existing airplane climb performance. Factors which contributed to the accident were: the pilot's inadequate preflight of the airplane, the over maximum gross weight of the…Mar 21, 1994 · Substantial damage

FAA incident reports · 2

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

Accident 20080409831909ALevel Off Touchdown · Unalaska, AK(-23) At approximately 1630 adt on April 9, 2008, a Grumman goose (G-21A), N741, operated by peninsula airways under 14 CFR part 135 as a commuter, flight number 325, struck a container trailer of a truck while landing at dutch harbor, Alaska. The airplane…Apr 9, 2008 · Substantial damageAccident 19940321006189AGustauvs, AKAircraft crashed after encountering downdraft. (-4)the state-operated amphibian was unable to outclimb rising terrain and impacted the margerie glacier, coming to rest at 9,650 ft MSL. Pilot had not flown since last proficiency check on 11/27/93. Pilot's…Mar 21, 1994 · Substantial damage

Service difficulty reports · 4

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

SDR PNSA050301Coupling · brokenLT MAIN LANDING GEAR WOULD NOT RETRACT OR EXTEND. HUNG UP IN MID TRAVEL. DOVE AIRCRAFT AND PERFORMED SUDDEN PULL UP AND LANDING GEAR WENT TO DOWN AND LOCK POSITION. AIRCRAFT RETURNED TO DUT AND MADE A NORMAL LANDING. MAINTENANCE FOUND LT WORM GEARBOX COUPLMar 9, 2005 · N741 · Grumav G21A · Landing Gear Retraction/Extension SystemSDR DHL2001741004Windshield · failedCAPT WINDSHIELD SHATTERED AT FLIGHT LEVEL 350. ABNORMAL PROCEDURES ACCOMPLISHED. R&R L-1 WINDOW WITH SERVICABLE UNIT PER M/M 56-11-11. A/C OK FOR SERVICE. STATUS - CLOSED.Mar 27, 2001 · N741 · Grumav G21A · Flight Compartment WindowsSDR PNSA990202Valve · out of positionDURING CLIMB, PILOT NOTICED FUEL WAS NOT BURNING EVENLY FROM BOTH TANKS. UPON SELECTING THE RT TANK (THE FULLEST TANK) BOTH ENGINES LOST POWER. THE FUEL SELECTOR WAS RETURNED TO THE BOTH POSITION AND THE ENGINES STARTED. AFTER LANDING IT WAS DISCOVERED THEFeb 23, 1999 · N741 · Grumav G21A · Aircraft Fuel Distribution SystemSDR PNSA980204Cylinder · separatedLT ENGINE STARTED RUNNING ROUGH AND LOST POWER, RETURNED TO BASE. FOUND CYLINDER SEPARATED FROM CASE. REPLACED ENGINE.Feb 20, 1998 · N741 · Grumav G21A · Reciprocating Engine Cylinder Section
Reports on N741 not matched to an aircraft · 2

They name N741, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

SDR DHL2005741576Frame · corrodedFRAME CORRODED AT STA 1166 AT STR 29R. FRAME AT BS 1166 FROM STR 25L-STR 25R IS CORRODED BEYOND ALLOWABLE LIMITS. CUT OUT DAMAGE SECTION FROM 25L- STR 25R IAW B727 SRM 53-10-4 FIG 13. FABRICATED NEW SECTION FROM 25L TO 25R 76 BY 10 IN. 7075-T6 .063 PO NR 509Apr 26, 2005 · N741 · Boeing 7272Q9 · Fuselage Main, FrameSDR DHL2005741575Seat Track · corrodedSEAT TRACK 24L AT BS 760 TO 848 CORROSION. REMOVED SEAT TRACK AT BS 760-848 LBL 24 IAW B727 RSM 51-30-2 FIG 7. REPLACED, LOCATED AND DRILLED FASTENER HOLES IN PN BAC 1520-841 PO NR 9002155 (8FT) IAW B727 SRM 51-30-2. TREATED AND PRIMED AREA AND PART IAW B72Apr 25, 2005 · N741 · Boeing 7272Q9 · Fuselage, Seat/Cargo Attach Fittings

STCs that may be installed · 40

Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.

See all 40 STCs

Earlier aircraft with this N-number · 1

This aircraft carried N741 before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.

1930Curtiss Wright JN4C · S/N 71128Cancelled Mar 20, 1930 · Built 1918 · Work E Clyde, Fort Worth, TX