N377PA
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Pathfinder Aviation, LLC. (P3TA) | 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.
17 reports on file, 2002-06-02 – 2003-06-05.
Part: SKIN — CRACKED (FUSELAGE) · airframe 41,224 hrs · 20,611 cycles
FUSELAGE SKIN CRACKED AT AFT SIDE OF E&E EQUIPMENT FAN OUTLET. REPAIRED PER SB 737-53-1117.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,195 hrs · 20,593 cycles
FLOOR PATH LIGHTING INOP ROWS 18-26. REPLACED LAST SECTION OF FLOOR PATH LIGHT STRIP.
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 41,190 hrs · 20,591 cycles
EMERGENCY LIGHTING INOP. ROW 18 AFT. REPAIRED WIRING IAW SP CHPT.20. TEST OK
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,139 hrs · 20,564 cycles
ROW 1 THRU 5 EMERGENCY PATH LIGHTS INOP. REPLACED LAMP CONNECTING STRIP PER MM 33-50-00. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,081 hrs · 20,536 cycles
EMERGENCY FLOOR LIGHTING INOPERATIVE, ROW 20 AFT. REPLACED ROW 17-29 LIGHT STRIP IAW MM 25-60-01. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,059 hrs · 20,524 cycles
EMERGENCY LIGHTS INOPERATIVE, 20 AFT. CLEANED STRIP CONNECTIONS AT AFT END FROM MOISTURE/WATER. LIGHTS CHECK, OK, IAW MM 33-50-00.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 41,009 hrs · 20,500 cycles
ROW 1-4 LOW LEVEL EMERGENCY LIGHTS INOPERATIVE. REMOVED & REPLACED EMERGENCY FLOOR PATH STRIP ELEMENT IAW MM 33-50-00. TESTS OK.
Part: LIGHT — CONTAMINATED (CABIN) · airframe 40,954 hrs · 20,474 cycles
SECTION 1 & 2 EMERGENCY PATH LIGHTING INOP. REPLACED WET SEGMENTS OF LIGHT STRIP. OPS CHK OK PER MM 33-29-00
Earlier reports · 2002 · 9 reports
2002
Part: COMPUTER — FAILED (FMC) · airframe 40,716 hrs · 20,321 cycles
FMC COMPUTER POPS CIRCUIT BREAKER. REMOVED AND REPLACED FMC COMPUTER. BITE CHECK. OK IAW MM.
Part: CONTROL UNIT — MALFUNCTIONED (AUTOPILOT) · airframe 40,518 hrs · 20,195 cycles
CHANNEL B ON AUTO PILOT INOPERATIVE. AUTO THROTTLES RETARD TO IDLE, WOULD NOT DISPLAY MACH SPEED ON MCP. PERFORMED A/P LAND VERIFY BITE CHECK THROUGH FMC. NO FAULTS INDICATED.
Part: INVERTER · airframe 40,475 hrs · 20,170 cycles
Emergency floor path lighting inop at aprox. sta. 500C. Trouble shot & found inverter bad. R&R inverter IAW WDM 33-51-41, Ops chk good.
Part: ENGINE · airframe 40,166 hrs · 19,997 cycles
At rotation had a loud engine vibration on Left engine. Inspected eng. intake, exhaust; opened cowlings & inspected; close cowlings; BITE AVM per MM77-31-00. Eng. Insp. per MM71-00-47. Ran eng. Parameters & fan blade damage within limits.
Part: SKIN — DAMAGED · airframe 40,125 hrs · 19,968 cycles
Fuselage skin damaged by belt loader sta 767 to sta 772 between str27Lt. and str27Rt.
Part: SKIN — DAMAGED · airframe 40,125 hrs · 19,968 cycles
Fuselage skin damaged by belt loader at sta 789 to sta 799 between str26Rt. and str27Rt.
Part: SKIN — DAMAGED · airframe 40,125 hrs · 19,968 cycles
Fuselage skin damaged by belt loader sta 797 to sta 818 at str27Lt.
Part: LIGHT · airframe 40,149 hrs · 19,984 cycles
Emergency floor path will not illuminate from row 6 to row 12. Repaired wiring floor emerg. path and acc. test IAW MM 33-53-00. Test OK
Part: SLIDE — UNSERVICEABLE (L1 DOOR) · airframe 40,103 hrs · 19,953 cycles
L1 DOOR SLIDE PRESSURE LOW. REMOVED AND REPLACED SLIDE.