N621AR
Registered owner: LT DREAM LLC, TX (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Construction Helicopters, Inc. (JTAA) | 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.
20 reports on file, 2014-08-20 – 2015-11-17.
Part: LANDING LIGHT — SHORTED (EXTERIOR) · airframe 14,332 hrs · 16,954 cycles
ON DEPARTURE, SMOKE NOTICED IN THE COCKPIT. DECLARED EMER & RETURNED. R & R LT LANDING LIGHT IAW MM 33-40-10.
Part: UNKNOWN — SMOKE (COCKPIT) · airframe 14,252 hrs · 16,796 cycles
DURING APPROACH, THE FLIGHT CREW SMELLED & OBSERVED A PUFF OF SMOKE THAT CAME FROM THE BOTTOM LT SIDE OF THE INSTRUMENT PANEL. NO ACTION WAS TAKEN AS LANDING WAS IMMINENT & A NORMAL LANDING WAS PERFORMED WITHOUT INCIDENT.
Earlier reports · 2014 · 18 reports
2014
Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,681 hrs · 16,370 cycles
DURING INSPECTION FOUND NR 11 LT & NR 11 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2018 & 14019-2019 INSTRUCTIONS.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 13,681 hrs · 16,370 cycles
DURING INSPECTION FOUND NR 6 LT & NR 6 RT FRAMES DAMAGED. LOCALLY FABRICATED FRAMES. WORK PERFORMED IAW DWG 14019-2013 & 14019-2014 INSTRUCTIONS.
Part: MOUNT FITTING — CORRODED (LT ENGINE) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING NDT OF LT ENG MOUNT FITTING INSPECTION, FOUND AFT UPPER LT ENG MOUNT FITTING TO BE CORRODED. REMOVED UPPER ENG MOUNT FITTING PN 212-13116-01.2 & SENT OUT TO BE LOCALLY FABRICATED. WORK DONE IAW DWG 14019-2026.
Part: MOUNT FITTING — CORRODED (NR 1 ENGINE) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
FOUND CRACK INDICATION ON NR 1 ENG UPPER MOUNT FITTING ON LT WING FWD SPAR NEAR GROUNDING LUG. FURTHER INSPECTION FOUND TO BE LEVEL 2 CORROSION. PART TO BE REPLACED WITH SERVICEABLE.
Part: SKIN — CRACKED (FUSELAGE) · airframe 13,681 hrs · 16,370 cycles
CRACK FOUND AT STATION 3950 LT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.
Part: SKIN — CRACKED (FUSELAGE) · airframe 13,681 hrs · 16,370 cycles
CRACK FOUND AT STATION 3950 RT SIDE OF FUSELAGE. LOCALLY MANUFACTURED FILLER USING .032 X 2024-T3 & DOUBLER USING .040 X 2024-T3. ALL WORK DONE FOLLOWING DWG 14019-2049 REV V1. NO FURTHER ACTION REQUIRED AT THIS TIME.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
RIGHT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
LEFT WING LOWER SURFACE IN AREA OF ENG EXHAUST TRAIL HAS CORROSION DAMAGE FROM ENG EXHAUST PRODUCT. MILITARY TECHNICAL INSTRUCTION 17 TO BE PERFORMED, REPAIR OF EXHAUST AREA THROUGH SKIN REPLACEMENT & DOUBLER PATCH.
Part: SKIN — DENTED (RT HORIZ STAB) · airframe 13,681 hrs · 16,370 cycles
DURING INSPECTION FOUND RT HORIZONTAL STABILIZER UPPER OTBD SKIN TO HAVE A DENT BEYOND LIMITS. FABRICATED SECTION OF SKIN USING ORIGINAL SKIN AS SAMPLE. MATERIAL USED .025 X 2024-T3 LOT 267230. ALL WORK DONE IAW EO 14019-300, REV V8 PAR 8 112. NO FURTHER ACTION REQUIRED AT THIS TIME.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
LEFT SEAT TRACK SUPPORT HAT CHANNEL & SEAT TRACK FROM FS 3150 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.
Part: CHANNEL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
RIGHT SEAT TRACK HAT CHANNEL SUPPORT & SEAT TRACK FROM FS 2400 TO 3950 FOUND CORRODED BEYOND LIMITS & IN NEED OF REPLACEMENT.
Part: MOUNT BRACKET — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT UPPER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2027 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.
Part: RIB — CORRODED (LT HORIZ STAB) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
TOP INNER RIB OF LT HORIZONTAL STABILIZER AT INBD ATTACH FITTING FOUND CORRODED BEYOND LIMITS. REPLACED INNER RIB AS REQUIRED.
Part: MOUNT BRACKET — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING REMOVAL OF HORIZONTAL STABILIZER FOUND LT LOWER MOUNT BAR CORRODED. LOCALLY MANUFACTURED IAW EO 14019-2028 REV 1R. NO FURTHER ACTION REQUIRED AT THIS TIME.
Part: WINDOW FRAME — CORRODED (COCKPIT) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.
Part: WINDOW FRAME — CORRODED (COCKPIT) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME INBD VERTICAL SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.
Part: WINDOW FRAME — CORRODED (COCKPIT) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOTâS WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.
Part: WINDOW FRAME — CORRODED (COCKPIT) · corrosion level 2 · airframe 13,681 hrs · 16,370 cycles
DURING WINDSHIELD REMOVAL AT HEAVY CHECK CORROSION FOUND ON THE COPILOT'S WINDSHIELD FRAME LOWER SECTION. REPAIRED IAW EO 12032-2036 SUPPORTED BY FAA FORM 8110-3.