N650HJ
Registered owner: LAMBRO AIRCRAFT MANAGEMENT LLC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| ACE AVIATION SERVICES CORPORATION (V6NA) | 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.
6 reports on file, 2018-08-20 – 2022-08-11.
Part: SEAT TRACK — CORRODED (FS599) · airframe 6,838 hrs · 4,113 cycles
AT SCHEDULE INSPECTION, DISCOVERED SEAT RAIL UNDER LAVATORY TOILET CORRODED. REPLACED FLOOR RAIL WITH NEW.
Part: SEAT TRACK — CORRODED (BS 574-605) · airframe 5,694 hrs · 3,395 cycles
AT SCHEDULED INSPECTION, DISCOVERED CORROSION ON SEAT RAIL BEAM UPPER SURFACE, FS574.00 TO 605.00, WL73.5. CORROSION WAS REMOVED. DOUBLER REPAIR ANGLES OF 0.063 IN. 2024-T3 WERE INSTALLED WET USING MS20426AD RIVETS AND HL18PB5 HILOKS. REPAIR PERFORMED PER FAA APPROVED DATA IN DRAWING HAJ-GEBD604-5653-M04, REV. I/R FROM FAA DER DERT-605388-NM.
Part: SEAT TRACK — CORRODED (BS 574-605) · airframe 5,694 hrs · 3,395 cycles
AT SCHEDULED INSPECTION, DISCOVERED CORROSION ON SEAT RAIL BEAM UPPER SURFACE, FS574.00 TO 605.00, WL73.5. CORROSION WAS REMOVED. DOUBLER REPAIR ANGLES OF 0.063 IN. 2024-T3 WERE INSTALLED WET USING MS20426AD RIVETS AND HL18PB5 HILOKS. REPAIR PERFORMED PER FAA APPROVED DATA IN DRAWING HAJ-GEBD604-5653-M04, REV. I/R FROM FAA DER DERT-605388-NM.
Part: SKIN — DENTED (FUSELAGE) · airframe 4,943 hrs · 2,874 cycles
AT SCHEDULED INSPECTION, DISCOVERED DENT IN FUSELAGE BELLY SKIN AT FS 646 FRAME 640, TEN INCHES FROM CENTER. DAMAGE DIMENSIONS APPROXIMATELY 3.0 X 8.3. FASTENERS WERE REMOVED IN AREA, SKIN AND STRAP MECHANICALLY FORMED BACK TO ORIGINAL CONTOUR. REFORMED AREA VERIFIED NOT TO BE CRACKED, PER EDDY CURRENT INSPECTION METHOD. BENT SECTION OF FRAME 640 WAS REMOVED, FILLER WAS INSTALLED SANDWICHED BETWEEN TWO REINFORCEMENT DOUBLERS. DOUBLER REPAIR EXTENDING FIVE ROWS OF RIVETS BEYOND SEAM WAS PERFORMED PER STRUCTURAL REPAIR MANUAL 51-70-12, FIGURE 2, SHEET 2.
Part: PIN — MISSING (TORQUE LINK) · airframe 4,222 hrs · 2,412 cycles
AT SCHEDULED INSPECTION DETERMINED NOSE LANDING GEAR UPPER TORQUE LING ATTACHMENT TO LOWER TORQUE LING CASTELLATED NUT MIGRATING OUTWARD OFF OF TORQUE LINK APEX PIN DUE TO SECURING PIN MISSING. INSPECTED OPPOSITE PIN AND DETERMINED EXISTING PIN TO BE WORN. NO DAMAGE TO APEX PIN OR NUT. REPLACED EXISTING PIN AND MISSING PIN WITH NEW.
Part: MOUNT — CORRODED (ASSIST CABLE) · airframe 3,240 hrs · 1,783 cycles
PASSENGER DOOR AFT FRAME AT BS 349, THE DOOR POWER ASSIST CABLE MOUNT WAS CORRODED. CABLE MOUNT WAS REPAIRED IAW DRAWING HAJ-GEBD604-5653-M01-1.