N336SA
Registered owner: BANK OF UTAH TRUSTEE, UT (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| BAKER MARINE CONSTRUCTION CORP | Operator | on 1982-01-19 | Operator named in NTSB report |
Accident & incident history
Operated by BAKER MARINE CONSTRUCTION CORP (per NTSB report)
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.
8 reports on file, 2014-07-04 – 2019-01-23.
Part: HYDRAULIC LINE — BLOWN (ZONE 700) · airframe 31,081 hrs · 39,441 cycles
DURING APPROACH, AFTER GEAR DOWN AND LOCKED "HYD" WARNING CAME ON. HYD. QTY. AND PRESSURE READ 0. MAINTENANCE PERSONNEL FOUND BLOWN HOSE ASSY. AT THE NOSE GEAR RETRACT ACTUATOR.
Part: BRACKET — CRACKED (RT MLG) · airframe 30,741 hrs · 38,937 cycles
UNSAFE GEAR INDICATION ON RT MAIN LANDING GEAR.
Part: WINDSHIELD — CRACKED (COCKPIT) · airframe 27,802 hrs · 34,661 cycles
WHEN ENROUTE, CAPTAIN WINDSHIELD CRACKED. DECLARED EMERGENCY AND LANDED. THE WINDSHIELD WAS REPLACED.
Part: SKIN — DENTED (BS 580) · airframe 27,679 hrs · 34,467 cycles
DENT AT RT FUSELAGE UNDER 11TH CABIN WINDOW. EVALUATED DAMAGE AT FUSELAGE BS 580.0, WATERLINE 100. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.
Part: SKIN — DENTED (BS 512-520) · airframe 27,679 hrs · 34,467 cycles
DENT ON SEAM AFT OF 9TH WINDOW RT SIDE. EVALUATED DAMAGE AT FUSELAGE BS 516. REPAIRED IAW SRM 53-70-10-205, FIG 203. NDT INSPECTED IAW NDT MANUAL 51-06-00. PRIMED AND PAINTED TO MATCH ACFT COLORS. NO CHANGE IN ACFT WEIGHT AND BALANCE.
Part: SOCKET — OVERHEATED (CABIN LIGHTS) · airframe 26,989 hrs · 33,283 cycles
BURNING ODOR IN FWD CABIN REPORTED BY F/A DURING CRUISE AT 15,000 FT. NO ABNORMAL COCKPIT INDICATIONS. ODOR WAS EVIDENT IN ALL OF ZONE A, GALLEY. OPENED BOTH ENGINE COWLS FOR VISUAL INSPECTION, NO DEFECTS NOTED. INSPECTED CABIN COMPARTMENT FOR ANY SIGNS OF BURNING NO DEFECTS NOTED. UNABLE TO DUPLICATE BURNING ODOR. ACFT OK TO CONTINUE SERVICE. FOUND ONE CABIN LIGHT HOLDER AT SEAT 8CD WITH SIGNS OF HEAT DAMAGE AND BURNED ODOR. REPLACED LIGHT HOLDER IAW AMM 20-20-10 AND OPS CHECKS PERFORMED IAW AMM 33-21-05 AND NO FURTHER DEFECTS NOTED.
Part: WIRE HARNESS — FAILED (WOW) · airframe 26,550 hrs · 32,599 cycles
LANDING GEAR HANDLE STUCK IN THE DOWN POSITION, USED OVERRIDE TO PULL IT UP. LANDED. REPLACED WOW HARNESS IAW AWM 32-31-10. SWUNG GEAR AND FOUND EVERYTHING SATISFACTORY, TEST FLIGHT REQUIRED.
Part: LINE — LEAKING (ENGINE FUEL) · airframe 26,412 hrs · 32,416 cycles
STRONG ODOR OF OIL & FUEL IN CABIN. LANDED, INSPECTED ALL FUEL LINES AND OIL COMPONENTS THE LT ENGINE FOR ANY POSSIBLE LEAKAGES THAT MAY CAUSE THE ODOR IN THE CABIN. FOUND AGB TO HMU LINE LEAKING AFTER INITIAL ENGINE RUN. TIGHTEN LINE IAW MM 730000, STEP 9A. PERFORMED SECOND ENGINE RUN AND NO LEAKS FOUND, OR ODOR IN THE CABIN.