N911ZCBeechcraft C90A
Safety record in brief:No NTSB accidents or incidents since 19827 ADs may apply2 service difficulty reports
Registration
FAA Aircraft Registry · Oct 20, 2026- Registered owner
- Valiair Lc Trustee
- Owner type
- LLC
- City, state
- Casper, WY
- Certificate issued
- May 4, 2026
- Expires
- May 31, 2033
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Airframe & engine
FAA Registry + type dataAirframe
- Manufacturer
- Beechcraft
- Model
- C90A
- Serial number
- LJ-1557
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 9
- Engines
- 2
- Max takeoff weight
- Up to 12,499 lb
- Mode S code
- AC9CA4
Engine
- Type
- Turbo-prop
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2026 – nowValiair Lc TrusteeCasper, WY · current
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 20, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
Accident history for this modelADs published since 1998 that may apply (7)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2007-12-06 | Hawker Beechcraft Corporation (Type Certificate (TC) No. 3A20 and TC No. A24CE Formerly… | Jul 16, 2007 | Airframe (C90A)Certain serial numbers: C90A LJ-1697–LJ-1726; C90A LJ-1728; C90A LJ-1729; C90A LJ-1731–LJ-1739; C90A LJ-1741–LJ-1743; B200 BB-1827–BB-1912; … |
| 2004-17-02 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, and 1900 Series Airplanes | Oct 4, 2004 | Airframe (C90A)Certain serial numbers: 65-A90, B90, C90, C90A LJ-76; 65-A90, B90, C90, C90A LJ-114–LJ-1691; E90 LW-1–LW-347; F90 LA-2–LA-236; 99, 99A, A99A, B99, C99 U-1–U-239; 100, A100 B-1–B-94; … |
| 2002-09-12 | Raytheon Aircraft Company Beech Model C90 Airplanes | Jun 21, 2002 | Airframe (C90A)Certain serial numbers: C90A LJ-1157–LJ-1276; C90A LJ-1278–LJ-1537; C90A LJ-1540 |
| 2002-01-10 | Raytheon Aircraft Company Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-4, B90, C90… | Feb 22, 2002 | Airframe (C90A)Certain serial numbers: 65-90 LJ-1–LJ-1559; 65-A90 LJ-1–LJ-1559; B90 LJ-1–LJ-1559; C90 LJ-1–LJ-1559; C90A LJ-1–LJ-1559; 65-A90-1 LM-1–LM-141; … |
| 99-10-07 | Raytheon Aircraft Corporation Beech Models 65-90, 65-A90, 65-A90-1, 65-A90-2, 65-A90-3… | Jun 8, 1999 | Airframe (C90A) |
Show all 7 ADsShow fewer ADs
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 97-25-03 | Raytheon Aircraft Company 65, 90, 99, 100, 200, 300, 1900, and 2000 Series Airplanes | Jan 21, 1998 | Airframe (C90A) |
| 97-23-17 | Raytheon Aircraft Company 90, 100, 200, and 300 Series Airplanes (Formerly Known as… | Dec 29, 1997 | Airframe (C90A)Certain serial numbers: C90 LJ-683–LJ-1463; C90A LJ-683–LJ-1463; E90 LW-177–LW-347; F90 LA-1–LA-236; H90 LL-1–LL-61; A100 B-228–B-247; … |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (2)
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
- Landing gear · drag brace · damagedAug 6, 2022
CLEARED FOR VISUAL APPROACH, CONDUCTED BEFORE LANDING ITEMS. MLG WAS LOWERED. MLG INDICATORS DISPLAYED NOSE & RT MAIN GEAR DOWN & LOCKED. NO LT MAIN INDICATION & MLG HANDLE WAS INDICATING RED IN TRANSIT. COULD NOT DETECT ANY SUBSEQUENT NOISE THAT GEAR WAS STILL IN TRANSIT. ATTEMPTED TO CYCLE GEAR…
From FAA Service Difficulty Reports; matched by N-number and serial number. - Wings · flap track · brokenJun 30, 2021
DURING FINAL APPROACH, THE LH OTBD FLAP I/B FLAP TRACK BROKE INTO TWO PIECES ALLOWING THE FLAP TO CANT CAUSING IT TO JAM AND NOT ALLOW TRAVEL TO THE APPROACH POSITION. BECAUSE THE FLAP WAS CANTED IT ALSO ALLOWED IT TO CONTACT THE LH AILERON INDUCING A RESISTANCE IN THE YOKE IN A SMALL RANGE OF…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 20, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 20, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026