N496TM
Registered owner: SDL GULFSTREAM LLC, AZ (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Wheels Up Private Jets LLC (CVGA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
7 reports on file, 2016-09-27 – 2025-02-25.
Part: DIODE — FAILED (ZONE 200) · airframe 9,007 hrs · 7,177 cycles
SMOKE CAME FROM DASH AREA WHEN ENG SYNC LIGHT IS ON - REMOVED AND REPLACED CR119 DIODE WITH NEW DIODE, P/N 1N4007, ON ENGINE FUEL SYNCH ANNUN CIRCUIT IAW BE400 AMM 20-20-02. OPS CHECK GOOD.REMOVED AND REPLACED RH GLARESHIELD INDICATOR PANEL P/N 45AS88843-49 S/N 235 WITH REPAIRED S/N 152 IAW B400 AMM 31-10-00. OPS CHECKED GOOD.
Part: STARTER GEN — FAILED (LEFT ENGINE) · airframe 7,500 hrs · 5,937 cycles
ON DESCENT, PILOT SIDE PFD, MFD AND CDU DISPLAYS STARTED TO HAVE A WAVY APPEARANCE. MASTER CAUTION AND MASTER WARNING LIGHT STARTED TO FLASH, BUT NO CORRESPONDING ANNUNCIATOR. TCAS AND ATC 1 BREAKERS POPPED ALONG WITH PILOT SIDE PFD TURNING OFF. COPILOTS PFD BEGAN TO FLICKER ON AND OFF ALONG WITH BOTH CDUS. SDU 2 STARTED TO TURN ON AND OFF UNTIL SDU2 CIRCUIT BREAKER POPPED. LEFT CDU WENT OFF AND LEFT FUEL GAUGE WENT TO ZERO. LEFT EFC ANNUNCIATOR CAME ON ALONG WITH L GEN, ICE DETECT FAIL, PITOT HEAT OFF, AND ANTI SKID FAIL.
Part: STIFFENER — CRACKED (THRUST REVERSER) · airframe 6,172 hrs · 4,880 cycles
RT UPPER TR BUCKET OUTBOARD STIFFNER IS CRACKED. REMOVED AND REPLACED RT UPPER TR BUCKET OUTBOARD STIFFENER, IAW NORDAM CMM 78-30-07.
Part: INLET — CRACKED (LT ENGINE) · airframe 6,172 hrs · 4,880 cycles
(SUPPLEMENTAL INFORMATION) LT ENGINE INLET HAS A CRACK, ABOVE STARTER/GEN INLET DUCT ON THE INSIDE.
Part: SUPPORT ANGLE — CRACKED (THRUST REVERSER) · airframe 5,845 hrs · 4,615 cycles
DURING SCHEDULED INSPECTION MX FOUND BOTH THE L/H LOWER THRUST REVERSER LEFT AND RIGHT ANGLES CRACKED. MX REMOVED AND REPLACED THE ANGLES WITH NEW ANGLES IAW CMM 78-30-07 REPAIR 1.
Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 4,802 hrs · 3,820 cycles
CRACKS AT FIRST RIB ON THE LT AND RT HORIZONTAL STAB. REPAIRED HORIZONTIAL STABILIZER RIBS.
Part: PAD — BROKEN (DOOR STEP) · airframe 3,216 hrs · 2,625 cycles
DURING INSPECTION IT WAS FOUND THE THE MAIN ENTRY DOOR STEP PAD WAS BROKEN ALLOWING THE STAIR SUPPORT TO DAMAGE THE FUSELAGE SKIN WHEN EXTENDED. PAD WAS REPLACED AND DAMAGED FUSELAGE SKIN WAS REPAIRED AS REQUIRED.