# N244YV: 1996 Beech 1900D, registration cancelled 2012-07-10

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: July 10, 2012
- Exported to: Egypt
- Status when cancelled: Valid registration
- Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162)
- Engine: [Pratt & Whitney PT6A series](https://openairdocs.org/engine/pratt-whitney-pt6a-series) (registry code 52032)
- Data sheets: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Serial number: UE-244
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, normal
- Airworthiness date: September 28, 1996
- Certificate issued: May 2, 2012
- Last registry action: May 2, 2012
- Mode S code: A24115
- Owners when cancelled: [Raytheon Space And Airborne Systems](https://openairdocs.org/faa-owner/RAYTHEON%20SPACE%20AND%20AIRBORNE%20SYSTEMS), [Attn: Andy Hattam](https://openairdocs.org/faa-owner/ATTN%3A%20ANDY%20HATTAM)
- Location: [El Segundo, CA](https://openairdocs.org/faa-place/CA/El%20Segundo)
- Owner type: Corporation
- Owner's area on the map: 33.9171° N, 118.4016° W: Placed by OpenAirDocs at the center of ZIP code 90245, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N244YV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=244YV
- Page: https://openairdocs.org/deregistered/N244YV-2012-07-10

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Beech 1900D: https://openairdocs.org/model/beech-1900d.md

## Service difficulty reports (22)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR AMWA071001017](https://openairdocs.org/sdr/AMWA071001017), Dec 6, 2007: SKIN. CHAFED. FRICTION CHAFING DURING ENGINE OPERATION CREATED WORN SEGMENTS ON THE RT ENGINE NACELLE. CHAFING WAS ALONG THE ENTIRE LENGTH AND SHAPE OF THE NACELLE. OBTAINED 
- [SDR AMWA1001010A](https://openairdocs.org/sdr/AMWA1001010A), Nov 9, 2007: SPAR. DAMAGED. AT RT WING WS 54.75 FOUND 0.50 INCH HOLE THROUGH SUB SPAR. HOLE HAD EVIDENCE OF POSSIBLE ELECTRICAL ARCING AT WIRING GROUNDING ATTACHMENT. REPAIRED IAW APPROVED
- [SDR AMWA87546](https://openairdocs.org/sdr/AMWA87546), Sep 19, 2007: BATTERY. CORRODED. AFTER ARRIVING, THE CREW CALLED MAINT CONTROL TO WRITEUP THE BATTERY CHARGE ANNUNCIATOR ILLUMINATED IN FLT. THIS BATTERY CHARGE ANNUNCIATOR WRITEUP IS A NUISANC
- [SDR AMWA86034](https://openairdocs.org/sdr/AMWA86034), Jul 13, 2007: SWITCH. MALFUNCTIONED. DURING FLT LT PROPS WENT INTO AUTOFEATHER. LANDED WITH NO FURTHER INCIDENT. PERFORMED CHECK FLT AND WAS UNSATISFACTORY. REMOVED AND REPLACED LOW AND HIGH TQ SWI
- [SDR AMWA84318BC](https://openairdocs.org/sdr/AMWA84318BC), Apr 30, 2007: BATTERY CABLE. CORRODED. BATT CHARGE ANNUNCIATOR ILLUMINATED ON DEPARTURE JUST AFTER GEAR RETRACTION. THIS BATTERY CHARGE ANNUNCIATOR LIGHT ILLUM IS CONSIDERED A NUISANCE WARNING, CAUSI
- [SDR AMWA078811](https://openairdocs.org/sdr/AMWA078811), Aug 7, 2006: EADI. ODOR. AFTER TAKEOFF, CREW NOTICES SMELL (ELECTRICAL ODOR) IN FLIGHT DECK. DECLARED AN EMERGENCY W/EQUIP LANDED AND TAXIED OFF RUNWAY. SHUT ENGINES DOWN ON TAXI WAY. N
- [SDR AMWA078595](https://openairdocs.org/sdr/AMWA078595), Jul 25, 2006: BRAKE. WEAK. CREW REPORTED AFTER LANDING, THAT THE LT BRAKE WAS WEAK. MAINTENANCE WAS CALLED AND FOUND LT BRAKE WEAR TO BE WITHIN LIMITS. BLED BRAKES AND OPS CHECKED NORMAL.
- [SDR AMWA078586](https://openairdocs.org/sdr/AMWA078586), Jul 24, 2006: ENGINE. MALFUNCTIONED. AFTER TAKEOFF RT ENGINE TORQUE DROPPED TO 2000 FTLBS A/C RTF WITHOUT FURTHER INCIDENT. MAINTENANCE WAS CALLED AND ADJUSTED THE RT ENGINE LOW TORQUE SETTINGS. OP
- [SDR 1060504022A](https://openairdocs.org/sdr/1060504022A), May 23, 2006: SPAR CAP. CORRODED. BIO-CORROSION RT MAIN SPAR CAP AT WS 124.588. REPAIRED IAW MFG FR-CO-01350 REV.1
- [SDR 1060504022](https://openairdocs.org/sdr/1060504022), May 23, 2006: SPAR CAP. CORRODED. BIO-CORROSION LT MAIN SPAR CAP AT WS124.588. REPAIRED IAW MFG FR-CO-01350 REV.1
- [SDR AMWA77016](https://openairdocs.org/sdr/AMWA77016), Apr 17, 2006: WINDSCREEN. CRACKED. DURING DECENT INTO PIT AT APPROX 14,000 FT. CREW HEARD CAPTIANS WINDSHIELD CRACK. LANDED IN PIT WITH NO FURTHER INCIDENT. MAINTENANCE THEN REMOVED AND REPLACED 
- [SDR 76399](https://openairdocs.org/sdr/76399), Mar 15, 2006: FIRE LOOP. WARNING LIGHT. RT FIRE LOOP WARNING ILLUMINATED IN FLIGHT WITH RT FIRE HANDLE ILLUMINATION MORE INFO TO BE ADDED LATER. CONTROL NR 76398.
- [SDR 76398](https://openairdocs.org/sdr/76398), Mar 15, 2006: FIRE LOOP. OUT OF POSITION. RIGHT FIRE LOOP WARNING ILLUMED IN FLIGHT WITH RIGHT FIRE HANDLE ILLUMINATION. MAINTENANCE WAS CALLED AND REPOSITIONED FIRELOOP OPS CHECKS NORMAL. NO PARTS WERE
- [SDR AMWA76380](https://openairdocs.org/sdr/AMWA76380), Feb 14, 2006: CONNECTOR. LOOSE. RIGHT FIRE LOOP CAUSES MASTER WARNING TO ILLUMINATE IN FLIGHT. MAINTENANCE CAME AND RESECURED A LOOSE CONNECTION AT THE FORWARD CONNECTOR. OPS CHECK NORMAL.
- [SDR 68755](https://openairdocs.org/sdr/68755), Jan 28, 2005: BRAKE ASSY. WEAK. ON CREWS FIRST FLIGHT CHECKS LEFT BRAKE WAS WEAK. A/C RETURNED TO THE HANGAR. MTC BLED BRAKES AND A/C RETURNED TO SERVICE. BLED BRAKES.
- [SDR 57827](https://openairdocs.org/sdr/57827), Jan 11, 2004: AUTOFEATHER SYS. MALFUNCTIONED. ON TAXI OUT CREW BEGAN STARTING LT ENGINE, AFTER GETTING IT STARTED PROPS WOULDN'T COME OUT. ALSO THE AUTOFEATHER WOULDN'T TEST. CREW RETURNED TO THE GATE WITH 
- [SDR AMW2002F00003](https://openairdocs.org/sdr/AMW2002F00003), Sep 16, 2002: PUMP. FAILED. WHILE FLIGHT WAS ENROUTE, THE LT LOW FUEL PRESSURE ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CREW THEREFORE RETURNED THE AIRCRAFT TO THE FIELD WITHOUT ANY FURTHER 
- [SDR 98ZZZM257](https://openairdocs.org/sdr/98ZZZM257), Jan 22, 1998: BULKHEAD. CRACKED. ICT MAINTENANCE FOUND SMALL CRACK IN DOVETAIL BULKHEAD. REPAIRED IAW AMWA TO 1900-27-00-0001. ICT MAINTENANCE FOUND 2 CRACKS IN TOP SKIN. REPAIRED IAW AMWA TO 1
- [SDR 98ZZZM258](https://openairdocs.org/sdr/98ZZZM258), Jan 15, 1998: SKIN. CRACKED. ICT MAINTENANCE FOUND SMALL CRACK IN TOP SKIN OF LEFT OUTBOARD FLAP AT INBOARD ATTACH BRACKET. REPAIRED IAW AMWA TO 1900-27-00-0001. (M)
- [SDR 97ZZZM1202](https://openairdocs.org/sdr/97ZZZM1202), Oct 11, 1997: SKIN. CRACKED. AT ICT OVERNIGHT MAINTENANCE, THE RT OUTBOARD FLAP WAS FOUND TO HAVE A .5 INCH LONG CRACK 8 INCHES FROM OUTBOARD EDGE AND 4 INCHES FROM LE BOTTOM SKIN. FLAP WAS
- [SDR 97ZZZX4168](https://openairdocs.org/sdr/97ZZZX4168), Jun 19, 1997: BRACKET. CHAFED. REMOVED AND REPLACED RIGHT TRAILING EDGE FLAP ATTACH BRACKET IAW SRM 51-40 DUE TO CHAFING, P/N 3516505031.
- [SDR 97ZZZX4169](https://openairdocs.org/sdr/97ZZZX4169), Jun 10, 1997: FLAP. CRACKED. RIGHT INBOARD FLAP WAS FOUND TO HAVE A CRACK INBOARD OF DOVETAIL. STOP DRILLED AND INSTALLED DOUBLER.

## FAA accident and incident reports (4)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20020916027309I](https://openairdocs.org/incident/20020916027309I), Sep 16, 2002: Beech 1900D (N244YV), MO. (-23) On September 16, 2002 at 11:40 local time, aircraft N244YV'S left low fuel pressure annunciator illuminated in flight. The crew switched on the left…
- [Incident 20020610011279I](https://openairdocs.org/incident/20020610011279I), Jun 10, 2002: Beech 1900D (N244YV), Pittsburgh, PA. (-23) Flight departed 28L at 1352 local. Upon reaching 2,500 MSL crew noticed pax claiming smoke in the cabin. Aircraft landed runway 32 at 1357 local.…
- [Incident 20020411008429I](https://openairdocs.org/incident/20020411008429I), Apr 11, 2002: Beech 1900D (N244YV), Pittsburgh, PA. (-23) On April 11, 2002, at 11:00 local time, aircraft N244YV on approach to pit lowered the landing gear, and the nose down and lock indicator didn't…
- [Incident 19970518017979I](https://openairdocs.org/incident/19970518017979I), May 18, 1997: Beech 1900D (N244YV), Kansas City, MO. Narrative: air midwest inc. (amwa) flight AMWA727, enroute to dsm from mci had to abort take-off for low torque indications. Amwa line maintenance was…

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