- Registered owner
- Bartlett Robert
- Location
- Cleveland, TX
- Owner type
- Individual
- Serial number
- D-2924
- Year built
- 1951
- Type
- Fixed wing single engine
- Engine
- Reciprocating
- Airworthiness
- Standard, utility
- Airworthiness date
- July 12, 1967
- Certificate issued
- April 22, 2011
- Expires
- April 30, 2030
- Mode S code
- A8A34F
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Continental E225 model are included below.
On this page
Airworthiness directives that may apply · 30
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1967 | 1 |
|---|---|
| 1969 | 2 |
| 1970 | 1 |
| 1972 | 3 |
| 1975 | 2 |
| 1984 | 1 |
| 1989 | 1 |
| 1994 | 1 |
| 1996 | 1 |
| 1997 | 3 |
| 1998 | 1 |
| 1999 | 1 |
| 2000 | 2 |
| 2001 | 2 |
| 2002 | 1 |
| 2003 | 1 |
| 2005 | 1 |
| 2007 | 1 |
| 2022 | 1 |
| 2023 | 1 |
| 2024 | 1 |
See all 35 ADs
Information bulletins that may apply · 6
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N656DMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Beech C35 aircraft
FAA incident reports
No FAA accident or incident reports matched to N656DMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Beech C35 aircraft
Service difficulty reports · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 97ZZZX4453Taper Pin · wornWHILE TAXIING AIRCRAFT, NOTED STEERING RESPONSE USING COPILOT'S PEDALS WAS POOR TRYING TO STEER LEFT. OKAY STEERING TO RIGHT. DURING INSPECTION, TAPER PIN THAT COUPLES PILOT SIDE LT RUDDER PEDAL TO TORQUE TUBE WAS FOUND LOOSE. PIN WAS REMOVED AND FOUND 'NESDR 97ZZZX4452Retract Rod · corrodedDURING ANNUAL INSPECTION, AIRCRAFT RECORDS AND CONDITION INDICATED LANDING GEAR RETRACT SYSTEM BE REMOVED. INSPECT AND RECONDITION AS NEEDED. ROD ENDS WERE REMOVED FROM THE AFT NLG RETRACT ROD AND A LEVEL 3 CORROSION CONDITION WAS FOUND FULL OF HEAVY RUST SCSDR 97ZZZX3888Aileron · out of balanceANNUAL INSPECTION FOUND ELEVATOR AND AILERONS OUT OF BALANCE DUE TO RECENT PAINT JOB. UNITS HAD NOT BEEN STRIPPED PRIOR TO PAINTING OR CHECKED FOR BALANCE. NO REFERENCE TO AD 87-02-02 OR AD 94-20-04 WAS FOUND IN RECORDS.SDR 97ZZZX3887Elevator · out of balanceANNUAL INSPECTION FOUND ELEVATOR AND AILERONS OUT OF BALANCE DUE TO RECENT PAINT JOB. UNITS HAD NOT BEEN STRIPPED PRIOR TO PAINTING OR CHECKED FOR BALANCE. NO REFERENCE TO AD 87-02-02 OR AD 94-20-04 WAS FOUND IN RECORDS.SDR 97ZZZX3886Elevator · out of balanceANNUAL INSPECTION FOUND ELEVATOR AND AILERONS OUT OF BALANCE DUE TO RECENT PAINT JOB. UNITS HAD NOT BEEN STRIPPED PRIOR TO PAINTING OR CHECKED FOR BALANCE. NO REFERENCE TO AD 87-02-02 OR AD 94-20-04 WAS FOUND IN RECORDS.SDR 97ZZZX2898Stab Cuff · misinstalledDURING ANNUAL INSPECTION AND AD 94-20-04 PARA (B) COMPLIANCE FOUND BEECH KIT 35-4016-3 (STAB REINFORCEMENT) LEADING EDGE CUFF ATTACH RIVETS FAULTY. FOUND LT CUFF ON THE RT SIDE AND RT CUFF ON LT SIDE. REVERSAL CAUSED A MISFIT OF CONTOUR AND INADQUATE RIVETINSDR 97ZZZX2897Stab Cuff · misinstalledDURING ANNUAL INSPECTION AND AD 94-20-04 PARA (B) COMPLIANCE FOUND BEECH KIT 35-4016-3 (STAB REINFORCEMENT) LEADING EDGE CUFF ATTACH RIVETS FAULTY. FOUND LT CUFF ON THE RT SIDE AND RT CUFF ON LT SIDE. REVERSAL CAUSED A MISFIT OF CONTOUR AND INADQUATE RIVETIN
STCs that may be installed · 445
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.