N467TW
Registered owner: SIERRA AMERICAN CORP, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
112000 LBS TAKEOFF, FLAPS 1, V1=144 VR=147 V2=153, RIGHT SEAT TAKEOFF. AFTER NORMAL START AND TAXI OUT FROM WILSON AIR CENTER TO RUNWAY 18L WE PROCEEDED TO TAKE THE RUNWAY AS CLEARED. ROLL OUT WAS NORMAL WITH NORMAL ENGINE SPOOL UP TO STABILIZE ENGINE PARAMETERS, PROCEEDED TO ADVANCE THROTTLES TO TAKE OFF POWER (2.13 EPR). ACCELERATION WAS NORMAL AND CONTINUED. AT APPROXIMATELY 130 KIAS A LOUD BANG WAS HEARD ON THE RIGHT SIDE OF THE AIRCRAFT; AN ABORTED TAKE OFF WAS EXECUTED AND PROCEEDED BACK. THE ATC TOWER REPORTED DEBRIS ON THE RUNWAY. THE FLIGHT ATTENDANTS REPORTED A FLAME COMING FROM THE RIGHT ENGINE AT ABOUT THE TIME OF THE "BANG". INITIAL VISUAL INSPECTION DOES NOT SHOW DAMAGE TO INLET FAN BLADES, TURBINE BLADES IN EXHAUST AREA SHOW MAJOR DAMAGE.
CUTOUT OIL CANNED AREA (1.25" DIAMETER) ON L/H AFT FUSELAGE SKIN EXTERIOR BETWEEN FS 967 AND FS 986.5 AND STR 24L AND STR 25L IAW AERO DESIGN SERVICES EO #ADS-N467TW-01 REVISION IR DATED 02/OCT/2023. ACCOMPLISHED HFEC NDT INSPECTION AROUND CUTOUT AREA WITH NO INDICATIONS IAW BOEING 737 NDT MANUAL PART 6 51-00-00 REVISION 139. REMOVED 23 EA EXISTING FASTENERS COMMON TO STR 24L, STR 25L, AND STR 26L WITHIN REPAIR AREA AT FS 967 AND FS 986.5 AERO DESIGN SERVICES EO #ADS-N467TW-01 REVISION IR DATED 02/OCT/2023. ACCOMPLISHED NDT OPEN HOLE ROTARY PROBE INSPECTION AT 23 EA OPEN HOLES FROM PREVIOUSLY REMOVED FASTENERS WITH NO INDICATIONS IAW BOEING 737 NDT MANUAL PART 6 51-00-00 REVISION 139. FABRICATED REPAIR DOUBLER OUT OF .050" 2024-T3 AND LOCATED AND DRILLED HOLES COMMON TO REPAIR DOUBLER AND REPAIR AREA IAW AERO DESIGN SERVICES EO #ADS-N467TW-01 REVISION IR DATED 02/OCT/2023. INSTALLED REPAIR DOUBLER (9.50" LENGTH X 8.750" WIDTH) TO REPAIR AREA ON L/H AFT FUSELAGE SKIN EXTERIOR BETWEEN FS 967 AND FS 986.5 AND STR 24L AND STR 25L IAW AERO DESIGN SERVICES EO #ADS-N467TW- 01 REVISION IR DATED 02/OCT/2023. RESTORED PROTECTIVE AND DECORATIVE FINISH TO REPAIR AREA AND COMPLETED ALL POST-REPAIR REQUIREMENTS IAW AERO DESIGN SERVICES EO #ADS-N467TW- 01 REVISION IR DATED 02/OCT/2023.
DURING CRUISE FLIGHT PORTION ENROUTE FROM KCKB TO KEWR WE EXPERIENCED AN A SYSTEM HYDRAULIC LOSS. AS SOON AS THE ADVISORY LIGHT ILLUMINATED BOTH THE F.O. AND MYSELF VERIFIED 0 (ZERO) QUANTITY ON HYDRAULIC SYSTEM A. THE LOSS OF SYSTEM A CHECKLIST WAS PERFORMED. THE LOSS OF SYSTEM A CHECKLIST WAS COMPLETED AND LANDING WAS ACCOMPLISHED WITH NO FURTHER DIFFICULTIES. INSPECTION REVEALED A HYDRAULIC HOSE P/N BACH8A08NN0180 HAD BURST IN THE R/H MLG WHEEL WELL FWD SIDE NEAR THE FWD LANDING GEAR TRUNION. REFERENCE 737-200 IPC 29-12-00-01 PAGE 3, ITEM #7 FOR THE LOCATION OF THE HOSE AND PART NUMBER.
FLAP ASYMMETRY ISSUE AFTER TAKE OFF. DECLARED AN EMERGENCY AND LAND AT ALTERNATE AIRPORT. AFTER TROUBLESHOOTING IT WAS DISCOVERED THAT THE RT FLAP TRANSMITTER AND THE FLAP INDICATOR WERE FAULTY. REPLACED FAULTY UNITS AND THE DISCREPANCY WITH THE FLAP ASYMMETRY WAS RESOLVED.
DURING CLIMB, THE PILOT TRIED TO SELECT FLAP UP WITH NO RESPONSE. THE FLAP INDICATION SHOWED THE RT FLAP AT 1 DEGREE AND THE LT FLAP AT 5 DEGREES. WITH NO RESPONSE TO THE FLAP HANDLE POSITION. DECLARED AN EMERGENCY AND LANDED AT AN ALTERNATE AIRPORT. THE AIRCRAFT WAS ALWAYS UNDER CONTROL AND NO ROLL OR CONTROL ISSUES. REPLACED THE RT FLAP POSITION TRANSMITTER AND THE FLAP POSITION INDICATOR CORRECTED THE DISCREPANCY.
RT STABILIZER, TOP SIDE SKIN WITH CORROSION SURROUNDING FASTENERS NEAR T/E.