N507AL

ZIPLINE INTERNATIONAL INC P2 ZIP · Hybrid lift · 5 engines · 0 seats · Valid Registration

Registered owner: ZIPLINE INTERNATIONAL INC, CA (owner ≠ operator)

Operators of this aircraft

Who operated this tail, and how firmly we know it.

No operator established for this aircraft.

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.

18 reports on file, 2000-02-16 – 2012-02-01.

OTHER · 2012-02-01 Matched by certificate designator
ATA 6230

Part: MAST — CORRODED (MAIN ROTOR) · airframe 10,573 hrs

CORROSION FOUND ON TUNGSTEN CARBIDE AREA OF MAST POLE. SENT TO HELICOPTER FOR EVALUATION IAW ASB 407-11-94 MANUAL.

Source: SDR ALGA2012020100075
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: GRIP — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012362412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: PITCH HORN — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012332412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: PITCH HORN — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB PITCH HORN HAS CORROSION BEYOND LIMITS.

Source: SDR ALGA2012012322412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: ADAPTER — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012312412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: GRIP — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012382412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: PITCH HORN — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012342412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: ADAPTER — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012392412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: GRIP — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB GRIP CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012372412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: PITCH HORN — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB PITCH HORN CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012352412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: ADAPTER — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012310412
OTHER · 2012-01-23 Matched by certificate designator
ATA 6220

Part: ADAPTER — CORRODED (ZONE 200) · airframe 10,573 hrs

MAIN ROTOR HUB ADAPTER CORRODED BEYOND LIMITS.

Source: SDR ALGA2012012311412
Earlier reports · 2000–2003 · 6 reports

2003

OTHER · 2003-07-21 Matched by certificate designator
ATA 6320

Part: GEAR — SPALLED (GEARBOX) · airframe 14,266 hrs

HEAVY SPALLING ON GEAR TEETH, DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED.

Source: SDR ALGA088163
OTHER · 2003-07-21 Matched by certificate designator
ATA 6320

Part: PINION GEAR — SPALLED (GEARBOX) · airframe 14,266 hrs

HEAVY SPALLING ON GEAR TEETH,DUE TO IMPROPER MESHING OF GEAR TEETH.

Source: SDR ALGA088162
OTHER · 2003-07-21 Matched by certificate designator
ATA 6230

Part: GEAR — SPALLED (GEARBOX) · airframe 14,266 hrs

HEAVY SPALLING ON GEAR TEETH DUE TO IMPROPER MESHING OF GEAR TEETH. REMOVED AND REPLACED.

Source: SDR ALGA088160
OTHER · 2003-07-09 Matched by certificate designator
ATA 6340

Part: INDICATOR — STUCK (DUAL TACH)

DUAL TACH STUCK AT 120 PERCENT.

Source: SDR ALGA088137
FALSE WARNING · 2003-06-25 Matched by certificate designator
ATA 7712

Part: INDICATOR — MALFUNCTIONED (TORQUE)

ON TAKE OFF, DURING CLIMB THE TORQUE INDICATION WENT TO 103 PERCENT FOR 3-5 SECONDS AND (CHECK) INSTRUMENT LIGHT ILLUMINATED. TORQUE WAS REDUCED TO 93 PERCENT WITH MGT OF 650 DEGREES. CLIMB SPEED WAS 500 FPM, AIRCRAFT WAS RETURNED TO BASE. THE MECHANIC TROUBLESHOT THE SYSTEM WITH THE MAINTENANCE COMPUTER, REMOVED AND REPLACED THE TORQUE INDICATOR AND PRESSURE TRANSMITTER. AIRCRAFT WAS RETURNED TO SERVICE.

Source: SDR ALG2003F00098

2000

OTHER · 2000-02-16 Matched by certificate designator
ATA 3212

Part: FUSEABLE PLUG — FAILED (FLOAT)

THE AIRCRAFT WAS IN THE HANGAR AND ALL OF THE AIR LEAKED FROM THE FLOAT BOTTLE. THE FUSELAGE PLUG FAILED, DISCHARGED FLOAT BOTTLE.

Source: SDR 2000ZZZX820