- Registered owner
- Bidzy Ta Hot Aana Corp
- Location
- Dillingham, AK
- Owner type
- Corporation
- Serial number
- 32R-7680441
- Year built
- 1976
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, normal
- Airworthiness date
- August 18, 1976
- Certificate issued
- September 30, 2004
- Expires
- April 30, 2028
- Mode S code
- A53855
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 31
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1976 | 3 |
|---|---|
| 1977 | 1 |
| 1978 | 1 |
| 1979 | 1 |
| 1980 | 4 |
| 1981 | 2 |
| 1986 | 1 |
| 1989 | 1 |
| 1993 | 1 |
| 1996 | 2 |
| 1998 | 3 |
| 1999 | 1 |
| 2000 | 1 |
| 2005 | 1 |
| 2006 | 2 |
| 2010 | 1 |
| 2013 | 1 |
| 2017 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
Airframe · Piper PA-32R-300
AD 2024-14-03Autopilot SystemAD 2023-09-09Exhaust Turbine System (Recip)AD 2022-03-15Fuel Quantity IndicatorInformation bulletins that may apply · 14
Advisory, not mandatory.
Airframe · Piper PA-32R-300
SAIB 2022-20Wing SparSAIB AIR-21-10Wing, Attach Fittings (JASC 5740)SAIB AIR-21-07WING SPAR, Verification of Correct Washers used with Wing Spar Attach BoltsSAIB SW-18-31Navigation, Attitude, and Direction Data SystemSAIB CE-11-12R1Wings - PA-28, PA-32, PA-34, and PA-44 Rear Spar Corrosion at Fuselage Attach FittingSAIB CE-14-23Powerplant; Air IntakeSAIB CE-11-42Flight Controls: Control Cable/Pulley InspectionsSAIB CE-11-14Stabilizers- Vertical Stabilizer on Piper PA-28, PA-32, PA-34 Forward Attach Point CorrosionSAIB CE-11-13Wings - Piper PA-28, PA-32, PA-34 Forward Spar CorrosionSAIB CE-11-11Wings - Piper PA-28, PA-32, and PA-34 Aileron Hinge Fitting CorrosionSAIB CE-11-10Piper PA-28, PA-32, PA-34, and PA-44 Corrosion on Flap Hinges, Brackets, and RibsSAIB CE-11-01Stabilizers -Horizontal Stabilator TurnbuckleSAIB CE-09-23Fuel: Piper PA-28, PA-32, PA-34SAIB CE-09-12Navigation: CRS/BARO Knob Interference in some G1000/G900X/G950 InstallationsHistorical bulletins · 1
NTSB investigations · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
NTSB ANC17LA014Accident · Serious injuriesLimited investigationFinal reportMcGrath, AKThe failure of the nose landing gear to extend and lock due to the failure of the alternator and reduced battery power due to the cold ambient temperature, which prohibited the electrically-driven hydraulic pump from supplying adequate hydraulic pressure to…NTSB ANC01LA145Accident · No injuriesLimited investigationFinal reportTanana, AKAn unlocked landing gear mechanism during landing roll. A factor associated with the accident was an electrical system failure.
FAA incident reports · 5
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Accident 20161120022569ALanding: Rollout · Mcgrath, AKDuring a on-demand flight from MCG-HRC-panv-SHX-5N1-MCG, the airman was unable to lower the nose landing gear 4 miles out from 5N1 airport. Both main gear indicated down and locked. The airman tried several times to get the nose gear to lock down without…Incident 20011206031619ILevel Off Touchdown · Bettles, AK(-23) Incident #A1012002006 ptrs 2002B0644. Pilot selected gear down on approach to bettels airport. Gear started down then all electrical power was lost. Aircraft landed and l/h gear failed. Aircraft slid around and off to the side of the runway. The l/h…Accident 20010921025089ATanana, AK(-23) Approximately 26 miles east of Tanana, pilot noted loss of electrical power, which resulted in complete electrical power loss. Pilot elected to make emergency landing in Tanana. He selected gear down above airspeed given for emergency gear extension.…Incident 19990909025999IFcd/Prec Ldg From Cruise · Kotzebue, AK(-23) The aircraft was on the return leg of a part 135 flight when the engine had a catastrophic failure. It was discovered that the #2 cylinder had failed causing engine stoppage and the need for an off airport emergency landing.Incident 19940422028769IClimb · Pontiac, MIOn climb to cruise while leaning engines over shot clearance altitude by 700 feet. Traffic conflict created.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR BTH2002F00000Terminal · corrodedAIRPLANE LANDED, LEFT GEAR UNLOCKED AFTER ELECTRICAL POWER FAILURE ON APPROACH TO LAND. INSPECTION OF ELECTRICAL SYSTEM, FOUND BATTERY POST CORRODED ON POSITIVE TERMINAL.SDR 2001FA0000636Brace · brokenINSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.SDR 2001FA0000635Brace · brokenINSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.SDR 2001FA0000634Brace · brokenINSPECTION FOUND RIGHT NOSE GEAR DOOR BRACE BROKEN AT REAR ATTACH POINT. ALSO CRACKED OUT FROM RIVETS AT AFT END OF BRACE.SDR 20010501CW003Arm · wornDURING VALVE CLEARANCE INSPECTION, FOUND NR 6 INTAKE ROCKER ARM FACE WHERE IT CONTACTS ROTATER CAP, WORN SEVERELY .1250 AND BADLY PITTED. ENGINE HAS BEEN ON OIL ANALYSIS SINCE OVERHAUL WITH NO PROBLEMS NOTED. ALL OTHER ROCKER ARMS FOUND NORMAL. PROBABLE CAUSDR BTHA95002Crankcase · crackedDURING ANNUAL INSPECTION, FOUND CRANKCASE CRACKED FROM EDGE OF NR 2 CYLINDER FLANGE TO FORWARD CORNER AT CYLINDER BASE STUD. EDDY CURRENT INSPECTION VERIFIED CRACK TO BE SUBSURFACE. VISUAL INSPECTION SHOWED NO CRACKING ON INSIDE OF CASE. THE CRACK WAS APPRO
STCs that may be installed · 290
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Piper PA-32R-300
STC SA02571SEInstallation of Garmin G500/G600 TXi Integrated Avionics System (Primary Flight Display, Multi-Function Display, and Engine Indicating System Display).STC SA01800SEFabrication and installation of new or replacement of existing instrument panel lights dimmer control.STC SA01861SEFabrication and installation of Landing Light Controller