- Registered owner
- B29258 LLC
- Location
- Estero, FL
- Owner type
- LLC
- Serial number
- 29258
- Year built
- 1999
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 25, 1999
- Certificate issued
- November 19, 2020
- Expires
- November 30, 2027
- Mode S code
- A276D3
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every GE CF6-80 model are included below.
On this page
Airworthiness directives that may apply · 61
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1985 | 1 |
|---|---|
| 1986 | 1 |
| 1989 | 1 |
| 1990 | 2 |
| 1991 | 6 |
| 1992 | 1 |
| 1993 | 1 |
| 1994 | 3 |
| 1995 | 2 |
| 1996 | 1 |
| 1997 | 1 |
| 1998 | 2 |
| 1999 | 4 |
| 2000 | 6 |
| 2001 | 2 |
| 2002 | 2 |
| 2003 | 4 |
| 2004 | 3 |
| 2005 | 2 |
| 2006 | 3 |
| 2007 | 5 |
| 2008 | 3 |
| 2009 | 7 |
| 2011 | 1 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2020 | 2 |
| 2021 | 2 |
| 2022 | 2 |
| 2023 | 1 |
| 2025 | 1 |
Engine · GE CF6-80 series
AD 2024-24-03Engine ExhaustAD 2023-20-08Engine (Turbine/Turboprop)AD 2021-26-22Turbine SectionInformation bulletins that may apply · 5
Advisory, not mandatory.
Engine · GE CF6-80 series
SAIB 2023-15Falsified Forms from AOG TechnicsSAIB NE-11-27Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel NozzlesSAIB NE-10-37Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback FaultsSAIB NE-08-44Engine Thrust Reverser Transcowl Clevis PinSAIB NE-07-01Dual engine flameouts on twin engine airplanesNTSB investigations · 1
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
FAA incident reports
No FAA accident or incident reports matched to N258SNMatched 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 Boeing 747-47UF aircraft
Service difficulty reports · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9WGA2026052225807Shear Tie · crackedDURING HEAVY CHECK, CRACK FOUND ON THE CENTER TANK STA 1000 FRONT SPAR SHEAR TIE RBL 33.99, (NR 041074, SEQ 874). REMOVED AND REPLACED SHEAR TIE AT CENTER TANK STA. 1000 FRONT SPAR RBL 33.99, IAW SRM 51-40-02 AND SB 747-53A2904.SDR 9WGA2026052225806Shear Tie · crackedDURING HEAVY CHECK, CRACK FOUND ON THE CENTER TANK STA 1000 FRONT SPAR SHEAR TIE, LBL 33.99, (NR 041073, SEQ 873). REMOVED AND REPLACED SHEAR TIE AT CENTER TANK STA. 1000 FRONT SPAR, LBL 33.99, IAW SRM 51-40-02 AND SB 747-53A2904.SDR 9WGA2026052225808Shear Tie · crackedDURING HEAVY CHECK, CRACK FOUND ON THE CENTER TANK STA 1000 FRONT SPAR SHEAR TIE RBL 75.92, REMOVED AND REPLACED SHEAR TIE CENTER TANK STA. 1000 FROM SPAR RBL 75.92, IAW SRM 51-40-02, AND SB 747-53A2904.SDR 9WGA2026052225805Shear Tie · crackedDURING HEAVY CHECK, CRACK FOUND ON THE CENTER TANK STA 1000 FRONT SPAR SHEAR TIE LBL 11.33, (NR 041072, SEQ 872). REMOVED AND REPLACED SHEAR TIE AT CENTER TANK STA. 1000 FRONT SPAR LBL 11.33, IAW B747-400 SRM 51-40-02 AND REQUIREMENTS SERVICE BULLETIN 747-53SDR 9WGA2026052125804Doubler · corrodedLH WING REAR SPAR NO. 2 MAIN TANK STRUCTURE JUMPER POINT AROUND FORWARD OVERRIDE/JETTISON PUMP HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED DOUBLER AT LT WING REAR SPAR NR 2 MAIN TANK STRUCTURE OVERRIDE / JETTISON PUMP PER SRM 51-40-02.SDR 9WGA2026052125803Doubler · corrodedLH WING REAR SPAR NO. 2 MAIN TANK STRUCTURE JUMPER POINT FUEL BOOST PUMP HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED DOUBLER ON LT WING, REAR, SOAR #2 MAIN TANK STRUCTURE FUEL BOOST PUMP IAW SRM 51-40-02,SDR 9WGA2026042725802Skin · corrodedRIGHT HAND WING UPPER SURFACE TRAILING EDGE SIDE WAS FOUND WITH CORROSION FROM STA ERSS 1646.716 TO WBL 1247, DURING HEAVY CHECK, PER WO 15698, NRC 940659, SEQ 459, PERFORMED BLEND AREA RH WING UPPER SURFACE T/E SIDE FROM STA ERSS 1646.716 TO WBC 1241 (1687 -SDR 9WGA2026040925801Pump · corrodedFUEL OVERRIDE JETTISON PUMP CENTER TANK-RIGHT M225 BEHIND OF THE BONDING JUMPER WAS FOUND CORROSION OF STRUCTURE. REPAIRED AREA AT FUEL OVERRIDE JETTISON PUMP CENTER TANK RIGHT M225, IAW B747-400 SRM 51-10-02, SRM 57-10-10, SOPM 20-10-03, WGN-WGN-26-0022-03B,SDR 9WGA2023091525801Cylinder · shearedDISCREPANCY: DIVERTED DUE TO GEAR NOT RETRACTING. EICAS "GEAR TILT" STATUS MESSAGE "GEAR MONITOR". CORRECTIVE ACTION: FOUND LH IB BODY GEAR LEVELING CYLINDER SHEARED. REMOVED AND REPLACED LEVELING CYLINDER IAW AMM 32-13-15.SDR 9WGA2022050925801Actuator · lockedDISCREPANCY: EICAS GEAR DISAGREE UNABLE TO RETRACT LEFT BODY GEAR AFTER TAKEOFF. CORRECTIVE ACTION: REPLACED LH BODY GEAR RETRACT ACTUATOR, LEAK CHECKS GOOD. REF AMM 32-33-01-004-001/404-009.SDR 9WGA2021102125801None · noneAIR RETURN FOR COMPRESSOR STALL #3 ENGINE. RAN ENGINE LIMITER SURGE OR STALL CHECK, ENGINE CONTINUED TO RUN AT REDUCED THRUST AND WOULD NOT RESPOND TO THRUST LEVER MOVEMENT.SDR 9WGA2021071125801Warning Message · illuminatedENGINE 4 OVERHEAT LOOP A (CLIMBOUT) (STATUS) EICASSDR 9WGA2021062825801Cabin Pressure · faultedATB DUE TO RAPID CLIMB ALT APPROX 9900.
STCs that may be installed · 6
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Engine · GE CF6-80 series
STC SE01543CHReplace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve.STC SE01478CHInstallation of Cook Airtomic alignment joint p/n AIR 22912.STC SE00969CHInstall AeroControlex P/N 2605290-001 variable stator feedback control cable.STC SE01471ATReplace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine.STC SE00463LAInstall fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220STC SA2227SOInstallation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES