N413JG
Registered owner: TRANS EXECUTIVE AIRLINES OF HAWAII INC DBA, HI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Trans Executive Airlines of Hawaii (TXHA) | 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.
19 reports on file, 2007-04-26 – 2023-01-07.
Part: FRAME — CRACKED (BS 360 S20-21R) · airframe 61,842 hrs · 55,460 cycles
STA 360 FRAME BETWEEN S20R-S21R FOUND CRACK AT THE EDGE OF FASTENER HOLE (0.31" IN LENGTH)
Earlier reports · 2007–2022 · 18 reports
2022
Part: BEAM — CORRODED (HORIZONTAL STAB) · airframe 61,842 hrs · 55,460 cycles
BULGES AT RT HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM AT HSS 68, 120, 130, AND 137.5.
Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 61,842 hrs · 55,460 cycles
BULGE AT RT HORIZONTAL STABILIZER REAR SPAR HSS 136.5.
Part: SPAR — CORRODED (HORIZONTAL STAB) · airframe 61,842 hrs · 55,460 cycles
BULGES AT LEFT HORIZONTAL STABILIZER REAR SPAR CHORD AT HSS 126.
Part: BEAM — CORRODED (HORIZONTAL STAB) · airframe 61,842 hrs · 55,460 cycles
BULGES AT LH SIDE HORIZONTAL STABILIZER UPPER TRAILING EDGE BEAM AT STAB 83 (3.0" X 1.5" IN AREA) & STA 116 (0.8" X 0.4" IN AREA)
Part: SKIN — CORRODED (LT WING) · airframe 61,842 hrs · 55,460 cycles
CORROSION AT LWR LT WING SKIN SURFACE INSPAR WS 583.
2007
Part: SKIN — CRACKED (CARGO DOOR) · airframe 60,395 hrs · 54,138 cycles
AFT CARGO DOOR/CRACKED SKIN NEAR OF LATCH HANDLE, ACO NR 0753101 PROVIDE INSTRUCTIONS ON REPAIRING CRACK IN AFT CARGO DOOR SKIN NEAR HANDLE, SRM 52-30-2 FIG 3.
Part: SKIN — CRACKED (BS 957-966) · airframe 54,138 hrs
SKIN IS CRACKED AT THE LOWER FWD CORNER OF THE L-2 DOOR CUT OUT. ACO NR 075397 REV 0 PROVIDES INSTRUCTIONS ON REPAIR OF L-2 DOOR CRACK SRM 53-30-3 FIGURE 46.
Part: FLOORBEAM — CORRODED (BS 941) · airframe 60,395 hrs · 54,138 cycles
PASSENGER CABIN/CORRODED UPPER SURFACE ON FLOORBEAM BS 941.5 AND LBL-16 TO RBL-7ACO NR 075378 REV. 0 PROVIDE INSTRUCTION ON REPAIR OF FLOOR BEAM AT BS-947.5, LBL 36-RBL 12, SRM 53-10-9 FIGURE 9.
Part: SHEAR TIE — CORRODED (BS 787) · corrosion level 2 · airframe 60,395 hrs · 54,138 cycles
LIGHT SURFACE CORROSION AT SHEAR TIE ON BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R, ACO NR 075370 REV 1. PROVIDE INSTRUCTIONS ON REPAIR AT BS 787, LOWER LOBE, BETWEEN STR 27L AND STR 27R SRM 53-10-4 FIGURE 7.
Part: FRAME SPLICE — ACTIVE (BS 767 S14R) · airframe 60,395 hrs · 54,138 cycles
PASSENGER CABIN/CRACKED FRAME AT BS 767 NEAR STRINGER 14R. PROVIDE INSTRUCTIONS ON REPAIR OF CRACKED FRAME AT BS 767 STR 14R, BOEING SB 737-53A-1261 PART 3 REPAIR.
Part: FRAME — CRACKED (BS 663) · airframe 60,395 hrs · 54,138 cycles
PASSENGER CABIN/CRACK ON FRAME BS-663 AND STRINGER-2L, ACO NR 075365 PROVIDES INSTRUCTION ON REPAIR OF CRACKED FRAME AT BS-663, STRINGER 2L SRM 53-10-4.
Part: SKIN — DENTED (BS 420) · airframe 60,395 hrs · 54,138 cycles
DENT ON FUSELAGE SKIN BETWEEN STR 26R TO STR 25R AT BS 420 R, ACO NR 075366, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 420 R STR-25R-26R, SRM 53-30-3.
Part: SKIN — DAMAGED (BS 777) · corrosion level 3 · airframe 60,395 hrs · 54,138 cycles
LOWER LOBE/FUSELAGE SKIN SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BSTA-777 BBL-0. FOUND CORROSION AT FASTENER REMOVAL, ACO NR 075380. PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS-777,FROM STR-27L TO STR-27R SRM 53-30-3 FIGURE 5.
Part: SKIN — DAMAGED (BS 807-827) · corrosion level 3 · airframe 60,395 hrs · 54,138 cycles
LOWER LOBE/FUSELAGE SKIN, SHOWS SIGNS OF HAVING LOOSE ATTACH RIVETS FROM BS 807 TO BS 827 AT BBL-0. FOUND CORROSION AT THE TIME FASTENER REMOVAL. ACO NR 075369 PROVIDE REPAIRS INSTRUCTIONS ON SKIN REPAIR AT BS 807-827 BBL 0, SRM 53-10-4 FIGURE 6.
Part: SKIN — CANNING (BS 480-500) · airframe 60,395 hrs · 54,138 cycles
FWD CARGO PIT OIL CAN EFFECT ON SKIN BETWEEN STR 22R AND STR-21R. ALSO BETWEEN STA 480R AND STA 500R ACO NR 075363, PROVIDE INSTRUCTIONS ON REPAIR OF SKIN AT BS 480-500, STR 21R-22R SRM BOEING 53-30-3.
Part: SKIN — DENTED (BS 328-360) · airframe 60,395 hrs · 54,138 cycles
DENT ON FUSELAGE SKIN AT BS 358/STR-17L NEAR DOOR L-1. ACO NR 075398 REV. 0, PROVIDE INSTRUCTIONS ON REPAIR OF GOUGE FWD OF BS 360 SRM 53-30-3 AND BOEING MESSAGE 1-326794229-26 AND FAA 8100-9.
Part: SKIN — DENTED (BS 995-1000) · airframe 60,395 hrs · 54,138 cycles
UPPER LOBE/SEVERAL DENTS ON FUSELAGE SKIN FROM BS 995 TO BS1000 BETWEEN S-15L TO S-16L, NEAR DOOR L2.ACO NR 075385 REV 0. PROVIDES INSTRUCTIONS ON REPAIR OF FUSELAGE SKIN AFT OF L2 DOOR, SRM 53-30-3 FIG 46 AND FIG 48 BOEING MESSAGE 1-377247518-4 WITH FAA 8100-9.
Part: SKIN — CANNING (BS 360-420) · airframe 60,395 hrs · 54,138 cycles
OIL-CAN EFFECT ON FUSELAGE SKIN AT BS 384 BETWEEN STR-16L/17L, ACO NR 0753100 REV.0, PROVIDE INSTRUCTIONS ON REPAIR OF DAMAGE SKIN, BETWEEN BS 360L TO BS 420L SRM 53-30-3 AND BOEING MESSAGE 1-326794229-28 AND FAA 8100-9.