N818EX1990 Boeing DHC-8-102
This N-number isn't registered right now. Below is its last known registration, canceled Mar 24, 2005.
Safety record in brief:No NTSB accidents or incidents since 19823 ADs may apply30 service difficulty reports
- Registration
- Deregistered
Registration
FAA Aircraft Registry · Oct 18, 2026- Last registered owner
- Amtering Air INC
- Owner type
- Corporation
- City, state
- Wilmington, DE
- Certificate issued
- Mar 23, 2005
- Canceled
- Mar 24, 2005
- Airworthiness
- Standard · Transport
- Airworthiness date
- Oct 15, 1990
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
- Boeing
- Model
- DHC-8-102
- Year
- 1990
- Serial number
- 235
- Aircraft type
- Fixed wing multi engine
- Category
- Land
- Certification
- Type Certificated
- Seats
- 39
- Engines
- 2
- Max takeoff weight
- 20,000 and over lb
- Mode S code
- AB278E
Engine
- Make and model
- P&W Canada Pw120
- Type
- Turbo-prop
- Power
- 1800 hp
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Ownership history
Ownership history from FAA records- 2005Amtering Air INCWilmington, DE
Individual owners are shown by city and state only.
Safety record
NTSB · Oct 15, 2026 · FAA ADs · Oct 18, 2026 · SDRs · Oct 16, 2026NTSB events (0)
No NTSB accidents or incidents found for this airframe since 1982.
ADs published since 1998 that may apply (3)
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 |
|---|---|---|---|
| 2014-14-02 | Pratt & Whitney Canada Corp. Turboprop Engines | Aug 15, 2014 | Engine (PW120)Only with: PW120, PW121, PW121A engines with Post SB21610 configuration; PW124B, PW127, PW127E, PW127F engines with Post SB21607 and/or Post SB21705 configuration; PW127G and PW127M engines unconditionally. |
| 2012-26-08 | Pratt & Whitney Canada Corp. Turboprop Engines | Feb 15, 2013 | Engine (PW120)Serial numbers per P&WC ASB No. PW100-72-A21813 Rev 3, PW100-72-A21802 Rev 4, and PW100-72-A21798 Rev 5. Only with: Engines with propeller shafts having serial numbers listed in the referenced P&WC ASBs. |
| 2003-21-03 | Pratt & Whitney Canada Models PW118, PW120, PW120A, and PW121 Turboprop Engines | Nov 20, 2003 | Engine (PW120) |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Service Difficulty Reports (30)
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.
- Lights · battery pack · failedMar 5, 2004
MAINTENANCE CREATED DISCREPANCY DUE TO THE LEFT HAND AFT EGRESS EMERGENCY LIGHT NOT TESTING. IT WAS FOUND THAT THE ASSOCIATED BATTERY PACK WAS FAULTY. PACK WAS REPLACED AND SYSTEM OPERATIONAL CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · brake assy · leakingMar 4, 2004
FLIGHT 4014 REPORTED AIRCRAFT VIBRATING WHEN USING RIGHT HAND BRAKE. MAINTENANCE FOUND THE INBOARD RIGHT HAND BRAKE ASSEMBLY LEAKING. THE BRAKE ASSEMBLY WAS REPLACED AND THE SYSTEM OPERATIONAL CHECK GOOD, AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · battery pack · faultyDec 14, 2003
WHILE AIRCRAFT WAS IN MAINTENANCE IT WAS DISCOVERED DURING TEST THAT SEVERAL OVERHEAD AND OUTSIDE EMERGENCY LIGHTS DID NOT TEST. MAINTENANCE FOUND POSITION 300 POWER SUPPLY WITH GROUND WIRE BROKEN AND ASSOCIATED BATTERY OVERHEATING. BOTH WERE REPLACED BUT PROBLEM STILL EXISTED. SUSPECT OTHER…
From FAA Service Difficulty Reports; matched by N-number and serial number.
Show all 10 reportsShow fewer reports
- Fuselage · seat track · corrodedDec 26, 2001
DURING C-CHECK INSPECTION INBOARD LEFT SEAT RAIL FOUND TO HAVE EXCESSIVE CORROSION AT STATION X208. FORWARD SECTION OF SEAT RAIL WAS SPLICED AT STATION X260 IN ACCORDANCE WITH DEHAVILLAND REPAIR DRAWING RD8-53-3074, RD8-53-1102, & RD8-53-2295. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Landing gear · link · wornNov 6, 2001
DURING FLEET INSPECTION OF NOSE GEAR FOR WEAR IN TRAILING ARM LINK ASSEMBLY, TRAILING ARM LINK BEARING AND PIN FOUND WORN. REPLACED LOWER LINK BEARING AND PIN. OPERATIONAL CHECK GOOD. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Nacelles and pylons · rivet · missingAug 29, 2001
BGM- DURING FLEET INSPECTION OF NACELLES FOR LOOSE AND MISSING FASTENERS FOUND 4 RIVETS MISSING FROM OUTBOARD RIGHT NACELLE AFT OF FLAP TRACK TRAILING EDGE. MAINTENANCE REPLACED RIVETS ON RIGHT OUTBOARD NACELLE AFT OF FLAP TRACK TRAILING EDGE. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · wire · brokenAug 17, 2001
BGM-DURING ROUTINE MAINTENANCE VISIT TWO FORWARD EMERGENCY LIGHTS ON FLOOR WERE FOUND INOPERATIVE. BROKEN WIRES REPAIRED ON TWO FORWARD EMERGENCY LIGHTS. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Lights · terminal · damagedJul 14, 2001
DURING ROUTINE MAINTENANCE VISIT EMERGENCY LIGHTS FOUND TO FLICKER WHEN SELECTED ON FROM THE FLIGHT ATTENDANTS PANEL. TERMINAL END REPAIRED AT FLIGHT ATTENDANTS LIGHT SWITCH. AIRCRAFT RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Doors · bushing · missingApr 5, 2001
LGA-FLIGHT 3704 CREW REPORTED PASSENGER DOOR WILL NOT OPEN. MAINTENANCE FOUND THREADED BUSHING MISSING ON HANDRAIL ASSEMBLY. INSTALLED INTERIM REPAIR ON DOOR. DOOR OPERATES NORMALLY. AIRCRAFT RETURNED TO SERVICE. CORRECT BUSHING INSTALLED LATER THAT DAY.
From FAA Service Difficulty Reports; matched by N-number and serial number. - Fuselage · structure · crackedAug 9, 2000
MDT - DURING A FLEET INSPECTION THE REAR FUSELAGE STRUCTURE WAS FOUND CRACKED AT FRAME 4, STRINGER 4 ON THE LEFT SIDE. REPAIRS WERE MADE IAW RD8-55-199 AND THE AIRCRAFT WAS RETURNED TO SERVICE.
From FAA Service Difficulty Reports; matched by N-number and serial number.
Showing the 10 most recent of 30 reports.
Sources
- FAA Aircraft RegistryRegistration, owner city and state, airframe, engineupdated Oct 18, 2026
- NTSB accident and incident databaseAccidents and incidents since 1982updated Oct 15, 2026
- FAA Airworthiness Directives (Federal Register)ADs published since 1998updated Oct 18, 2026
- FAA Service Difficulty ReportsReports since 1995updated Oct 16, 2026