N262JX

EMBRAER EMB-135LR · 2001 · Fixed-wing multi-engine · 2 engines · 37 seats · Valid Registration

Registered owner: DELUX PUBLIC CHARTER LLC, TX (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

OperatorRolePeriodBasis
DELUX PUBLIC CHARTER LLC (4DPA)Certificate holderMatched 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.

4 reports on file, 2021-06-11 – 2024-02-26.

FLUID LOSS; WARNING INDICATION · 2024-02-26 Matched by certificate designator
ATA 2910

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 34,577 hrs · 36,955 cycles

CREW REPORTED ON TAKEOFF ABOUT 7000 FEET, “HYD1 LO QTY” MSG ILLUMINATED ON EICAS. LOOKED AT HYDRAULIC PAGE, AND QUANTITY WAS DECREASING RAPIDLY. THEN “HYD1 PUMP FAIL” MSG ILLUMINATED. HEARD THE GEAR DOOR OPEN. RETURNED TO THE FIELD. CORR ACTION MX REMOVED DAMAGED RH NOSE GEAR DOOR ACTUATOR HYD HOSE ASSY PN OFF: 123-03011-401, NSN. INSTALLED SERVICEABLE RH NOSE GEAR DOOR ACTUATOR HYD HOSE ASSY PN ON : 123-03011-401, NSN. LEAK CHECK PERFORMED. OPS CHECK GOOD.

Source: SDR 4DPA2024022600001
OTHER · 2022-03-31 Matched by certificate designator
ATA 5322

Part: FLOORBEAM — CORRODED (ZONE 900) · airframe 32,361 hrs · 34,676 cycles

DURING ACCOMPLISHMENT OF TASK CARD 53-23-00-220-C04-A00, FOUND CORROSION UNDER LAVATORY AREA FLOOR BEAM CAP, FLOOR ATTACHMENT POINTS. ORIGINAL MATERIAL THICKNESS .040", ALLOWABLE DAMAGE LIMITED TO 30% OF ORIGINAL THICKNESS, MEASURED .031" DEEP, EXCEEDING THE MAX ALLOWABLE. CONTACTED EMBRAER AND REPAIRED UNDER EMBRAER'S ETD 2022-145-011622. NO FURTHER MAINTENANCE REQUIRED.

Source: SDR 2022F00173
WARNING INDICATION; OVER TEMP · 2021-12-13 Matched by certificate designator
ATA 7200

Part: DUCT — BROKEN (ZONE 400) · airframe 32,082 hrs · 34,353 cycles

ISSUE-CREW REPORTED ENGINE 2 ITT WENT TO RED LIMIT RIGHT AFTER V1 ON TAKEOFF ROTATION, AFTER ACCELERATION ALTITUDE REDUCED THE POWER AND DIVERTED BACK TO KBUR, AND EVEN AFTER LANDING ITT SHOWS 720 ON ENGINES IDLE. AMT'S DISCOVERED DISCHARGE TUBE ASSY BROKEN OFF. AND INBOARD INNER CORE COW DELAMINATED AND DAMAGED. ENGINE REQUIRES OFF WING REPAIR AND WILL BE REPLACED.

Source: SDR 4DPA2021121300001
WARNING INDICATION · 2021-06-11 Matched by certificate designator
ATA 2840

Part: INDICATION SYS — UNKNOWN (FUEL QTY) · airframe 31,444 hrs · 33,653 cycles

DISC: ERRONEOUS FUEL INDICATION, TAKE OFF WAS 9200LBS PASSING THROUGH 4000FT “FUEL IMBALANCE” EICAS AND IT SHOWED 10200LBS TOTAL. 5500 LEFT WING 4600 RIGHT WING. CORRECTIVE ACTION: CHECKED ELECTRICAL FUEL INDICATING SYSTEM AND TRANSFERRED FUEL FROM WING TO WING. "FUEL IMBALANCE" EICAS MESSAGE CAME ON AT 800 LBS DIFFERENCE AND WENT OUT AT 80 LB DIFFERENCE. LEVELED OUT FUEL AND DIPPED BOTH TANKS. BOTH TANKS DIPPED THE SAME QUANTITY. REF: EMB 135 AMM 28-41-00. COULD NOT SEE ANY IMBALANCE ISSUE AT THIS TIME.

Source: SDR 4DPA2021061100001