UPS FLIGHT FORWARD INC
Also recorded as: UPS FLIGHT FORWARD INC
Accident & enforcement record
Events that happened, regardless of the operator's own reporting. Each links to its public source.
NTSB accidents & incidents
No NTSB accidents or incidents linked to this operator.
FAA enforcement actions
No FAA enforcement actions linked to this operator.
Maintenance disclosure history
Service Difficulty Reports are self-reported maintenance findings. The NUMBER of reports is not a measure of reliability — diligent operators file more, not fewer. These are shown for transparency, not as a negative signal. To verify a report, search its control number at the FAA SDRS site.
Reports span 2022–2022. Most-reported systems: Navigation (34) — 7; Nacelles / pylons (54) — 4; Fuselage (53) — 3; Auto flight (22) — 1; Electrical power (24) — 1. Most-common natures of condition, as filed: OTHER — 16.
16 reports on file.
Part: CAP — DETACHED (ZONE 200) · airframe 59 hrs · 972 cycles
PARACHUTE CAP DEPARTED FLIGHT
Part: CAP — DEPARTED (ZONE 200) · airframe 64 hrs · 1,194 cycles
PARACHUTE CAP DEPARTED FLIGHT
Part: CAP — DEPARTED (ZONE 200) · airframe 54 hrs · 1,079 cycles
PARACHUTE CAP DEPARTED FLIGHT ON TWO SEPARATE OCCASIONS (JUNE 21, 2021 & MAY 23, 2022)
Part: ARM — SEPARATED (ZONE 400) · airframe 43 hrs · 865 cycles
#4 ELECTRONIC SPEED CONTROLLER SEPARATING FROM ARM ASSEMBLY DUE TO FAILED SCREW INSERTS
Part: AVIONICS UNIT — FAILED (UNKNOWN) · 217 cycles
INTERNAL HARDWARE FAILURE. VEHICLE WILL NOT POWER OFF.
Part: GPS — UNKNOWN (ZONE 200)
VEHICLE HAD AN INCIDENT DUE TO GPS ISSUES.
Part: AVIONICS UNIT — UNKNOWN (ZONE 200) · airframe 27 hrs · 286 cycles
ELECTRICAL FAILURE DURING BATTERY INSTALLATION.
Part: ARM — FAILED (PYLON) · airframe 31 hrs · 838 cycles
ELECTRONIC SPEED CONTROLLER SEPARATING FROM ARM ASSEMBLY DUE TO FAILED SCREW INSERTS.
Part: AVIONICS UNIT — UNKNOWN (ZONE 200)
INTERNAL HARDWARE ISSUE.
Part: ARM — FAILED (NACELLE) · airframe 26 hrs · 376 cycles
ELECTRONIC SPEED CONTROLLER SEPARATING FROM ARM ASSEMBLY DUE TO FAILED SCREW INSERTS.
Part: GPS — MALFUNCTIONED (ZONE 200)
GPS ISSUES
Part: AVIONICS UNIT — FAULTED (ZONE 200) · airframe 39 hrs · 691 cycles
AVIONICS PLANE POWER ANOMALY
Part: ELECTRICAL SYS — UNKNOWN (UNKNOWN) · airframe 14 hrs · 183 cycles
ELECTRICAL FAILURE DURING BATTERY INSTALLATION.
Part: ARM — FAILED (NACELLE) · airframe 22 hrs · 304 cycles
ELECTRONIC SPEED CONTROLLER SEPARATING FROM ARM ASSEMBLY DUE TO FAILED SCREW INSERTS.
Part: GPS — FAULTED (ZONE 200) · airframe 11 hrs · 68 cycles
GPS ISSUES
Part: CONTROLLER — DEFECTIVE (FLIGHT) · airframe 20 hrs · 180 cycles
DEFECTIVE FLIGHT CONTROLLER
Linked aircraft
| N-number | Make / model | Year | Status | Link basis |
|---|---|---|---|---|
| NFA33LTNTHA | — | — | Matched by certificate designator | |
| NFA39ETNFCC | — | — | Matched by certificate designator | |
| NFA3LETKH4N | — | — | Matched by certificate designator | |
| NFA3MT99NCA | — | — | Matched by certificate designator | |
| NFA3MTAHNNW | — | — | Matched by certificate designator | |
| NFA3MTALKRL | — | — | Matched by certificate designator |