N676TX

CESSNA 560XL · 2004 · Fixed-wing multi-engine · 2 engines · 13 seats · Valid Registration

Registered owner: TVPX AIRCRAFT SOLUTIONS INC TRUSTEE, UT (owner ≠ operator)

Operators of this aircraft

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

OperatorRolePeriodBasis
RED WING AEROPLANE COMPANY (R3WA)Certificate holderMatched 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.

3 reports on file, 2021-12-24 – 2024-01-08.

OTHER · 2024-01-08 Matched by certificate designator
ATA 5753

Part: SKIN — DELAMINATED (RT TE FLAP) · airframe 14,450 hrs · 11,278 cycles

RH O/B FLAP TRAILING EDGE OF FLAP FOUND TO HAVE DELAMINATION SEPARATION AFTER POST FLIGHT INSPECTION.

Source: SDR R3WA2024010800010
OTHER · 2022-04-27 Matched by certificate designator
ATA 3410

Part: DATA BOX — DIRTY (ZONE 100) · airframe 13,449 hrs · 10,636 cycles

CREW WAS DESCENDING TO KMDW WHEN ADC #2 ALTITUDE TAPE FAILED ON FO SCREEN. CREW DECLARED AN EMERGENCY AS THEY WERE APPROACHING CLASS B AIRSPACE. CREW RAN CHECKLIST AND PERFORMED A REVERSION TO THE #1 ADC. LANDED WITHOUT INCIDENT. MAINTENANCE WENT TO AIRCRAFT POWERED UP ALL SYSTEMS AND COULD NOT DUPLICATE AN ERROR. CLEANED ELECTRICAL CONNECTORS.

Source: SDR R3WA 22.02
WARNING INDICATION · 2021-12-24 Matched by certificate designator
ATA 2750

Part: CONNECTING ROD — BINDING (TE FLAPS) · airframe 13,278 hrs · 10,537 cycles

DURING INITIAL APPROACH & LANDING TO KLEX (ABOUT 10-15NM FROM THE RUNWAY / ILS RUNWAY 22 APPROACH), FLAPS 7 WAS SELECTED. THEN GEAR DOWN WAS SELECTED. IMMEDIATELY, THE STAB MISCOMPARE ANNUNCIATOR ILLUMINATED, THE FLAPS DID NOT EXTEND NORMALLY, AND THE GEAR UNLOCKED...BUT DID NOT EXTEND. THE CE560XL CHECKLIST, PAGE Q1 WAS REFERRED TO. THE PROCEDURE WAS COMPLETED TO THE LETTER OF THE CHECKLIST WHICH LED TO THE GEAR BEING DOWN & LOCKED AND THE FLAPS EXTENDING NORMALLY. MAINTENANCE FOUND THAT THE RIGHT OUTBOARD FLAP WAS BINDING IN TRACK WHICH WAS CAUSING THE HYDRAULIC SYSTEM TO REMAIN ON. WHEN LANDING GEAR WAS SELECTED THE HYDRAULIC SYSTEM COULD NOT ACCOMMODATE BOTH SYSTEMS. FLAP CONNECTING RODS WERE ADJUSTED. AIRCRAFT WAS RECENTLY PAINTED. SURMISE THAT THE FLAPS WERE INSTALLED AND CONNECTING RODS WERE SLIGHTLY OUT OF ADJUSTMENT WHEN FLAPS WERE REINSTALLED.

Source: SDR R3WA202112300007