# N182YV: 1995 Beech 1900D, registration cancelled 2012-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2012
- Exported to: South Africa
- 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-182
- Year built: 1995
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: November 17, 1995
- Certificate issued: January 3, 2012
- Last registry action: January 3, 2012
- Mode S code: A14A54
- Owner when cancelled: [Specialized Aircraft Services Inc](https://openairdocs.org/faa-owner/SPECIALIZED%20AIRCRAFT%20SERVICES%20INC)
- Location: [Wichita, KS](https://openairdocs.org/faa-place/KS/Wichita)
- Owner type: Corporation
- Owner's area on the map: 37.7038° N, 97.2793° W: Placed by OpenAirDocs at the center of ZIP code 67208, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N182YV
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=182YV
- Page: https://openairdocs.org/deregistered/N182YV-2012-03-08

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 (50)

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

- [SDR GLBA20111003H](https://openairdocs.org/sdr/GLBA20111003H), Oct 1, 2011: UPLOCK SWITCH. INOPERATIVE. PILOT REPORTED THAT THE GEAR INTRANSIT LIGHT REMAINED ILLUMINATED AFTER THE GEAR WAS RETRACTED. MX REPLACE THE RT LANDING GEAR UPLOCK SWITCH PN: H11-1541GLA IAW
- [SDR GLBA20110930F](https://openairdocs.org/sdr/GLBA20110930F), Sep 29, 2011: LINE. LEAKING. PILOT REPORTED THAT FUEL WAS DRIPPING FROM HYD LINES IN LT WHEEL WELL. MX CLEANED AND INSPECTED THE AREA, NO LEAK FOUND.
- [SDR GLBA20110927F](https://openairdocs.org/sdr/GLBA20110927F), Sep 26, 2011: HANDLE. UNSECURE. PILOT REPORTED THAT THE DOOR HANDLE ON THE FWD RT EMERGENCY EXIT DOOR APPEARS TO BE RECESSED. MX RESECURED THE EMER EXIT DOOR IAW BMM 52-20-00, OK FOR SERVICE.
- [SDR GLBA20110926K](https://openairdocs.org/sdr/GLBA20110926K), Sep 24, 2011: EXTINGUISHER. OVERSERVICED. PILOT REPORTED THAT THE PASSENGER FIRE EXTINGUISHER READ OUT IN THE RED, OVER CHARGED. MX REPLACED THE FIRE EXTINGIUSHER.
- [SDR GLBA20110915F](https://openairdocs.org/sdr/GLBA20110915F), Sep 14, 2011: PCB. INOPERATIVE. PILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. REPLACED THE AUTOFEATHER PCB REF BMM 20-00-01, OPS CHECKED GOOD.
- [SDR GLBA20110914001](https://openairdocs.org/sdr/GLBA20110914001), Sep 14, 2011: ANNUNCIATOR. INOPERATIVE. PILOT REPORTED THAT AUTOFEATHER ANNUNCIATOR IS INOPERATIVE. OPEN
- [SDR GLBA20110816G](https://openairdocs.org/sdr/GLBA20110816G), Aug 15, 2011: LANDING GEAR. MALFUNCTIONED. PILOT REPORTED THAT WHILE ON A CHECK FLIGHT THE LANDING GEAR WAS SELECTED DOWN, NOTHING HAPPENED AND HAD TO MANUALLY EXTEND THE GEAR, GOT 3 GREENS AND LANDING. 
- [SDR GLBA20110722F](https://openairdocs.org/sdr/GLBA20110722F), Jul 21, 2011: CABLE. BROKEN. PILOT REPORTED THAT THE SNUBBER CABLE BROKE UPON OPENING THE AS DOOR. MX REPLACED THE CABLE IAW BMM 52-10-01-201, PN: 129-514119-1GLA.
- [SDR GLBA20110718G](https://openairdocs.org/sdr/GLBA20110718G), Jul 15, 2011: BULB. MISSING. DURING PREFLIGHT THE PILOT FOUND THE INST EMERGENCY LIGHT BULB MISSING. MX REPLACED THE EMERGENCY LIGHT BULB, PN: 1864 IAW BMM 33-10-04.
- [SDR GLBA20110621F](https://openairdocs.org/sdr/GLBA20110621F), Jun 20, 2011: UPLOCK SWITCH. FAILED. "SUP" - SIG EVENT - PILOT REPORTED THAT WHEN THE RETRACTED THE GEAR, THE INTRANSIT LIGHT WOULD NOT EXTINGUISH, LANDING GEAR EXTENDED WITH 3 GREENS WITH NO INTRA
- [SDR GLBA20110525G](https://openairdocs.org/sdr/GLBA20110525G), May 24, 2011: PUMP. WORN. PILOT REPORTED THAT THE RT FUEL PSI LOW LIGHT ILLUMINATED DURING FLIGHT, TURNED STANDBY PUMP ON AND LIGHT EXTINGUISHED. MX R & R THE RT LOW PRESS FUEL PUMP IAW 
- [SDR GLBA20110524F](https://openairdocs.org/sdr/GLBA20110524F), May 23, 2011: SWITCH. OUT OF RIG. PILOT REPORTED THAT THE CABIN DOOR ANNUNCIATOR ILLUMINATED AT FLIGHT LEVEL 240, MAX DIFF WAS 4.7, MAX DIFF DIDN'T CHANGE. PUT ON MEL. MAINTENANCE FOUND THE PRES
- [SDR GLBA20110516G](https://openairdocs.org/sdr/GLBA20110516G), May 15, 2011: PLACARD. MISINSTALLED. - SIG EVENT - PILOT REPORTED THAT THE EMERGENCY EXIT PLACARD IS AT THE WRONG SEAT. PLACARD IS IN 7C AND SHOULD BE IN 5C. MX INSTALLED THE PLACARD IN THE PROPER 
- [SDR GLBA20110420J](https://openairdocs.org/sdr/GLBA20110420J), Apr 19, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 500 AND STRINGERS 4L & 5L CRACKED AT THE STRUT MOUNT
- [SDR GLBA20110420H](https://openairdocs.org/sdr/GLBA20110420H), Apr 19, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 456 AND STRINGER 3L & 4L AT THE GAS STRUC
- [SDR GLBA20110420F](https://openairdocs.org/sdr/GLBA20110420F), Apr 19, 2011: SPAR. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK RADIATING FROM THE DEICE TUBING HOLE IN THE HORIZONTAL STAB MAIN SPAR CENTER WEB
- [SDR GLBA20110418F](https://openairdocs.org/sdr/GLBA20110418F), Apr 18, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 9AR CRACKED .15" IN LENGTH. MAINTENANCE R
- [SDR GLBA20110418G](https://openairdocs.org/sdr/GLBA20110418G), Apr 18, 2011: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED .2" IN LENGTH. MAINTENANCE RE
- [SDR GLBA201007121](https://openairdocs.org/sdr/GLBA201007121), Jul 12, 2010: SPLINE. STRIPPED. PILOT REPORTED THAT DURING TAKEOFF (CLIMB OUT) ENROUTE, NR 1 ENGINE FAILED & AUTOFEATHERED, ENGINE SHUTDOWN BY ITSELF, THE AIRCRAFT LANDED BACK AT FIELD WITHOUT
- [SDR GLBA20100628F](https://openairdocs.org/sdr/GLBA20100628F), Jun 27, 2010: SWITCH. DIRTY. SMOKE/SMELL - PILOTS REPORTED THAT WITH THE BATTERY ON, ALL OF THE ANNUNCIATORS REMAINED ILLUMINATED WITH A SLIGHT BURNING SMELL BEING NOTICED. MX REMOVED AND C
- [SDR GLBA20100324F](https://openairdocs.org/sdr/GLBA20100324F), Mar 23, 2010: SKIN. DENTED. MAJOR REPAIR - PILOTS REPORTED THAT A BIRD STRIKE OCCURRED ON SHORT FINAL ON THE LT WING, LT OTBD SECTION OF THE WING. BETWEEN WING SIDE 249.5 & WING SIDE 261.5
- [SDR GLBA20100129F](https://openairdocs.org/sdr/GLBA20100129F), Jan 25, 2010: SKIN. DAMAGED. COMPONENT REPAIR - DURING A LIGHTINING STRIKE INSP OF THE ACFT AN EXIT HOLE WAS FOUND ON THE LT ELEVATOR. THE ELEVATOR WAS REMOVED AND REPLACED. IAW MM 27-30-00
- [SDR GLBA20091104H](https://openairdocs.org/sdr/GLBA20091104H), Nov 4, 2009: SKIN. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE A CRACK WAS FOUND IN THE RIGHT HAND FUSELAGE SKIN AT F.S. 498.25 ABOVE STRINGER 10R. THE CRACK RADIATES THROUGH A RIVET HOL
- [SDR GLBA20091104J](https://openairdocs.org/sdr/GLBA20091104J), Nov 4, 2009: FRAME. BENT. DURING ROUTINE SCHEDULED MAINTENANCE A FRAME WAS FOUND BENT AT F.S. 451 BETWEEN STRINGER 6R & 7R. DAMAGE FOUND UNDER PREVIOUS REPAIR TO FUSELAGE SKIN. MAINTENAN
- [SDR GLBA20091104G](https://openairdocs.org/sdr/GLBA20091104G), Nov 4, 2009: SKIN. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE THE FUSELAGE SKIN WAS FOUND CRACKED AT F.S. 447 BETWEEN STRINGERS 6R AND 7R. CRACK LOCATED AT UPPER FORWARD CORNER OF A PRE
- [SDR GLBA20091030G](https://openairdocs.org/sdr/GLBA20091030G), Oct 29, 2009: FRAME. BENT. SCHEDULED MAINTENANCE A FUSELAGE FRAME WAS FOUND BENT AT FS 198.25 ON THE LEFT HAND SIDE OF THE FUSELAGE AT STRINGER 6L. MAINTENANCE REPAIRED THE FRAME AND PERF
- [SDR GLBA20091030J](https://openairdocs.org/sdr/GLBA20091030J), Oct 29, 2009: FRAME. BENT. DURING ROUTINE SCHEDULED MAINTENANCE STRINGER 6L WAS FOUND BENT JUST AFT OF FUSELAGE FRAME AT F.S. 198.25. MAINTENANCE REPAIRED STRINGER 6L AND PERFORMED THE RE
- [SDR GLBA20091030L](https://openairdocs.org/sdr/GLBA20091030L), Oct 26, 2009: ANGLE. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE A PREVIOUS REPAIR WAS FOUND CRACKED ON THE RIGHT HAND HEAVY ANGLE AT F.S. 303.25. CRACK LENGTH APPROXIMATELY 1". MAINTENANC
- [SDR GLBA20091030H](https://openairdocs.org/sdr/GLBA20091030H), Oct 26, 2009: ANGLE. CRACKED. DURING ROUTINE SCHEDULED MAINTENANCE A RIGHT HAND HEAVY ANGLE WAS FOUND CRACKED IN BEND RADIUS AT F.S. 303.25 AFT OF FUSELAGE FRAME. CRACK LENGTH APPROXIMATELY 
- [SDR GLBA20090928G](https://openairdocs.org/sdr/GLBA20090928G), Sep 25, 2009: SKIN. DAMAGED. UPON INSPECTION OF THE ACFT A LIGHTNING STRIKE WAS FOUND ON THE RT ELEVATOR TOP SKIN. MAINTENANCE REMOVED AND REPLACED THE ELEVATOR I.A.W. 27-30-00. MX REMOVED 
- [SDR GLBA2009](https://openairdocs.org/sdr/GLBA2009), Sep 9, 2009: SKIN. CRACKED. MAJOR REPAIR - WHILE PERFORMING OTHER MAINTENANCE RELATED TO AN ANTENNA REPLACEDMENT A RIVET HEAD WAS FOUND MISSING AND TWO SMALL CRACKS WERE FOUND THAT WERE AP
- [SDR GLBA20090424F](https://openairdocs.org/sdr/GLBA20090424F), Apr 21, 2009: SKIN. LEAKING. DURING SCHEDULED MX A FUEL LEAK WAS FOUND ON THE LT WING LE ON A PREVIOUS REPAIR FROM APPROX WS 239 TO WS 249.75. MX REPAIRED THE LT WING LE PREVIOUS REPAIR IAW
- [SDR GLBA200903212](https://openairdocs.org/sdr/GLBA200903212), Mar 21, 2009: ACTUATOR. WORN. PILOTS REPORTED THAT DURING GEAR EXTENSION THE LEFT MAIN GEAR WAS FLICKERING ON AND OFF AND REC IN TRANSIT LIGHTS WERE ILLUMINATED. THEY RECYCYLED THE LANDING G
- [SDR BSAASDR0725](https://openairdocs.org/sdr/BSAASDR0725), Oct 5, 2007: SKIN. TORN. RIGHT FLAP HUMP MISSING LARGE SECTION OF SHEET METAL. FLAP WAS REMOVED AND REPLACED.
- [SDR BSAASDR0607](https://openairdocs.org/sdr/BSAASDR0607), Feb 27, 2006: SPAR CAP. DAMAGED. PITTING CORROSION WAS FOUND ON THE RIGHT WING ON THE LOWER WING SPAR CAP IN THE THIRD ELEMENT SPAR STRAP JUST AFT OF THE WING DRAIN LOCATED JUST OUTBOARD OF THE
- [SDR 67971](https://openairdocs.org/sdr/67971), Dec 26, 2004: ANNUNCIATOR. FAILED. TAIL DE-ICE ANNUNCIATOR FAILED IN FLIGHT DURING ICING CONDITIONS, AIRCRAFT LANDED WITH NO FURTHER INCIDENT. REMOVED AND REPLACED TAIL DE-ICE SENSOR AND SERVICED
- [SDR 63594](https://openairdocs.org/sdr/63594), Aug 2, 2004: FIRE DETECTOR. MALFUNCTIONED. ON TAKEOFF ROLL OUT, FLIGHT CREW OBSERVED LT ENGINE FIRE BOTTLE DISCHARGED ANNUN. ILLUMINATED. CREW ABORTED TAKE OFF AND RETURNED TO THE GATE WITH NO FURTHER IN
- [SDR 58784](https://openairdocs.org/sdr/58784), Feb 12, 2004: PRESSURE SWITCH. INOPERATIVE. AFTER DEPARTING FROM MSS. CREW CLIMBED THROUGH INCING CONDITIONS AND FOUND TAIL DE-ICE TO BE INOP. IN BOTH MODES. THEY DIVERTED TO DUJ. UNDER A DISPATCH DECLARE
- [SDR 58604](https://openairdocs.org/sdr/58604), Feb 5, 2004: ANNUNCIATOR. FALSE INDICATION. WHILE ON FLIGHT, PASSENGER DOOR ANNUNCIATOR ILLUMINATED IN FLIGHT. THE CAPTAIN FOLLOWED PROCEDURES TO LAND AT AN ALTERNATE FIELD TRI. CREW INSPECTED DOOR AND FO
- [SDR 54574](https://openairdocs.org/sdr/54574), Sep 20, 2003: SWITCH. OUT OF ADJUST. MASTER WARNING ILLUM WITH A CABIN DOOR ANNUNCIATOR. TAKEOFF WAS ABORTER AFT RETURNED TO GATE. ADJUSTED CABIN DOOR ANNUNCIATOR LIGHT SWITCH.
- [SDR AMWA33](https://openairdocs.org/sdr/AMWA33), Sep 7, 2003: RIB. CRACKED. RIB CRACKED AT CSS 69.184 AT STRG P/N 101-640000-46 RT AND STRG P/N 101-640000-45 LT SIDE (2EA CRACK AT THIS RIB).
- [SDR AMWA32](https://openairdocs.org/sdr/AMWA32), Sep 7, 2003: RIB. CRACKED. RIB AT CS 54.026 CRACKED AT STRG. P/N 101-640000-46 STRG P/N 101-640000-47 ON RT SIDE AND STRG P/N 101-640000-39 LT SIDE (3EA CRACKS ON THIS RIB).
- [SDR AMWA31](https://openairdocs.org/sdr/AMWA31), Sep 7, 2003: RIB. CRACKED. RIB AT CSS 39.289 CRACKED AT STRG P/N 101-640000-39, 1EA CRACK AT THIS RIB.
- [SDR AMWA8](https://openairdocs.org/sdr/AMWA8), Feb 12, 2003: SPAR CAP. CHAFED. UPON A DETAILED INSPECTION MAINTENANCE FOUND THE ELECTRIC LINE CHAFING ON RIGHT FORWARD WING SPAR IN THE WHEEL WELL. BLENDED LOWER WING SPAR CAP IN ACCORDANCE W
- [SDR 97ZZZM968](https://openairdocs.org/sdr/97ZZZM968), Aug 9, 1997: TURBINE. FAILED. IN MCI, THE RIGHT ENGINE HAD A CONTAINED ENGINE FAILURE DURING START. REMOVED AND REPLACED RIGHT ENGINE GAS GENERATOR AND POWER SECTION. TEAR DOWN INSP REVEALED
- [SDR 97ZZZX4237](https://openairdocs.org/sdr/97ZZZX4237), Jun 28, 1997: DOVETAIL BLKHD. CRACKED. DURING BEECH TEMP. REV 5-6 FLAP INSPECTION, THE LEFT INBOARD FLAP DOVETAIL BULKHEAD WAS FOUND WITH A CRACK. STOP DRILLED AND INSTALLED DOUBLER IAW AMWA T.O. 190
- [SDR 97ZZZM977](https://openairdocs.org/sdr/97ZZZM977), Jun 28, 1997: BRACKET. WORN. AT ICT OVERNIGHT MAINTENANCE INSPECTION PER BEECH TEMP REV 5-6, FOUND LHOB FLAP. INBOARD ATTACH BRACKET WORN. REMOVED AND REPLACED ATTACH BRACKET IAW SRM 57-00 
- [SDR 96ZZZM1243](https://openairdocs.org/sdr/96ZZZM1243), Jul 17, 1996: P3 LINE. LOOSE. FLT 5627 - AFTER TAKEOFF RIGHT ENGINE ROLLED BACK TORQUE AND THEN STABILIZED AT ABOUT 1000 FT/LBS OF TORQUE, AIRCRAFT. RETURNED TO FIELD AT MCI. MAINTENANCE TIG
- [SDR 96ZZZX1754](https://openairdocs.org/sdr/96ZZZX1754), Feb 18, 1996: BLADE. SPLIT. DURING ROUTINE MAINTENANCE, THE TRAILING EDGE WAS FOUND SPLIT APROXIMATELY 1.5 INCHES. REPAIRED IAW HARTZELL MM AND FORM 8110-3.
- [SDR 96ZZZX1753](https://openairdocs.org/sdr/96ZZZX1753), Feb 10, 1996: BLADE. SPLIT. DURING ROUTINE MAINTENANCE, PROPELLER BLADE, SN 1655, WAS FOUND TO HAVE A 4 INCH SPLIT ON TRAILING EDGE. REPAIRED IAW HARTZELL MM AND FORM 8110-3 FROM HARTZELL.

## FAA accident and incident reports (5)

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 20040212001569I](https://openairdocs.org/incident/20040212001569I), Feb 12, 2004: Beech 1900D (N182YV), Du Bois, PA. (-23) On February 12, 2004, flight 5104 aircraft N182YV while enroute from mss to art diverted to duj because the tail de-ice was inop. Air midwest dispatch…
- [Incident 20010928028719I](https://openairdocs.org/incident/20010928028719I), Sep 28, 2001: Beech 1900D (N182YV), Nashville, TN. (-23) N182YV 09/28/01 flight 693 lit/bna - on approach into bna crew selected gear down. The landing gear did not extend. The landing gear power pack failed to…
- [Incident 20000607021119I](https://openairdocs.org/incident/20000607021119I), Jun 7, 2000: Beech 1900D (N182YV), Pittsburgh, PA. (-23) On approach to venango regional airport (fkl) franklin, PA, (an uncontrolled airport) the pilot selected gear down and the right main gear down lock…
- [Incident 19970213005389I](https://openairdocs.org/incident/19970213005389I), Feb 13, 1997: Beech 1900D (N182YV), Kansas City, MO. Narrative: air midwest inc., flight AMW649, aircraft N182YV departed mci at 08:20 CST on 02/13/97 enroute to cid. During climb-out the #2 engine propeller…
- [Incident 19960716022949I](https://openairdocs.org/incident/19960716022949I), Jul 16, 1996: Beech 1900D (N182YV), Kansas City, MO. Narrative: after initial climb-out the aircraft number 2 engine experienced a reduction in torque. The crew immediately returned the aircraft to mci, where…

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