N797PA

AMAZON.COM SERVICES LLC MK30 · Rotorcraft · 6 engines · 0 seats · Valid Registration

Registered owner: AMAZON.COM SERVICES LLC, WA (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
PAN AMERICAN WORLD AWYS INC.Operatoron 1965-01-31Operator named in NTSB report

Accident & incident history

Accident · 1965-01-31 Operator named in NTSB report
BOEING 707 321C Serious injuryPAN AMERICAN WORLD AWYS INC.

Operated by PAN AMERICAN WORLD AWYS INC. (per NTSB report)

Source: NTSB case NYC65I0101

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.

3 reports on file, 2005-04-20 – 2009-09-30.

OTHER · 2009-09-30 Unresolved
ATA 5753

Part: MOUNT BRACKET — UNKNOWN (TE FLAP)

WORK PERFORMED: 6,000 HR TIME CHANGE ON FLAP SECTORS AND SB 60-27-29 R2 INSTALLATION OF LT AND RT IMPROVED FLAP SECTOR MOUNTING BRACKETS. DURING RIGGING CHECKS OF FLAP SYS. FOUND SECTORS TO BE CONTACTING SPAR 8 ON BOTH WINGS. MM 27-50-00, PAGE 202 REQUIRES .030-.040" CLEARANCE BETWEEN SECTORS AND SPAR 8. CONTACTED MFG AND RECEIVED APPROVAL TO BLEND A MAX OF .040" FROM SECTORS TO OBTAIN PROPER CLEARANCES

Source: SDR 2009FA0000972
OTHER · 2009-09-30 Unresolved
ATA 2750

Part: FLAP — OBSTRUCTED (TE FLAPS)

WORK PERFORMED: 6,000 HR TIME CHANGE ON FLAP SECTORS AND SB 60-27-29 R2 INSTALLATION OF LT AND RT IMPROVED FLAP SECTOR MOUNTING BRACKETS. DURING RIGGING CHECKS OF FLAP SYS. FOUND SECTORS TO BE CONTACTING SPAR 8 ON BOTH WINGS. MM 27-50-00, PAGE 202 REQUIRES .030-.040" CLEARANCE BETWEEN SECTORS AND SPAR 8. CONTACTED MFG AND RECEIVED APPROVAL TO BLEND A MAX OF .040" FROM SECTORS TO OBTAIN PROPER CLEARANCES.

Source: SDR 2009FA0000971
OTHER · 2005-04-20 Unresolved
ATA 3230

Part: UNKNOWN — MALFUNCTIONED (NLG)

DURING DEPARTURE, AFTER MAINTENANCE (ENGINE AND THRUST REVERSER) THE NOSE LANDING GEAR DID NOT RETRACT. THE AC RETURNED TO DEPARTURE FOR REPAIR. PROBABLE CAUSE: THE AC WAS JACKED, THE LANDING GEAR WAS FUNCTIONALLY TESTED IAW MM. THE DISCREPANCY COULD NOT BE DUPLICATED. SUSPECTED AN AIR LOCK IN THE NOSE LANDING GEAR RETRACTION SYSTEM. A CHECK FLIGHT WAS PERFORMED WITHOUT FURTHER INCIDENT. (EA09200504998) (K)

Source: SDR 2005FA0000716