# N17541: 1996 Beech 1900D, registration cancelled 2012-10-24

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: October 24, 2012
- Exported to: Canada
- 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-203
- Year built: 1996
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-prop
- Airworthiness: Standard, commuter
- Airworthiness date: March 13, 1996
- Certificate issued: May 9, 2011
- Last registry action: January 10, 2012
- Mode S code: A12EBE
- Owner when cancelled: [Silver Airways Corp](https://openairdocs.org/faa-owner/SILVER%20AIRWAYS%20CORP)
- Location: [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale)
- Owner type: Corporation
- Owner's area on the map: 26.0870° N, 80.1530° W: Placed by OpenAirDocs at the center of ZIP code 33315, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N17541
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=17541
- Page: https://openairdocs.org/deregistered/N17541-2012-10-24

From the FAA registry file of October 29, 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 (73, newest 50)

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

- [SDR 29GA94153071412](https://openairdocs.org/sdr/29GA94153071412), Jul 14, 2012: SKIN. CORRODED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED SEVERE CORROSION AT FS 363.25 STRINGER 16. REMOVED DAMAGED SKIN AREA AND STRINGER 16 DAMAGE AND INSTALLED FUSELA
- [SDR 29GA94153062912](https://openairdocs.org/sdr/29GA94153062912), Jun 29, 2012: SKIN. WRINKLED. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED BELLY SKIN WRINKLE AT BEACON LOCATION.
- [SDR 29GA94132012112A](https://openairdocs.org/sdr/29GA94132012112A), Jan 21, 2012: POWERPACK. LOW. FLIGHT: 4068 FKL/DUJ AFTER LANDING GEAR HANDLE IS MOVED UP GEAR IN TRANSIT LIGHT AND MOTOR DO NOT ACTUATE FOR 2.4 SECONDS AFTER THIS TIME GEAR RETRACTS AND EXTE
- [SDR 29GA94132011912A](https://openairdocs.org/sdr/29GA94132011912A), Jan 19, 2012: UNKNOWN. LOW. FLIGHT: 4070 CLE/CLE AFTER DEPARTING AND PUTTING THE GEAR HANDLE UP NOTHING HAPPENED AFTER 1500 FEET LOOKED AT GEAR AND SAW GEAR RELAY CIRCUIT BREAKER WAS POPPE
- [SDR 29GA2012010494153](https://openairdocs.org/sdr/29GA2012010494153), Jan 4, 2012: SKIN. CORRODED. DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 16-15R APPROXIMATELY. REMOVED DAMAGE
- [SDR 29GA94153010412A](https://openairdocs.org/sdr/29GA94153010412A), Jan 4, 2012: SKIN. CORRODED. DURING SCHEDULED STRUCTURAL INSPECTION DISCOVERED AREA OF CORROSION THROUGH OUTER SKIN AT APPROXIMATELY FS 327.630 STRINGER 12L APPROXIMATELY. REMOVED DAMAGED S
- [SDR 29GA94152122811A](https://openairdocs.org/sdr/29GA94152122811A), Dec 28, 2011: HANDLE. LACK OF LUBE. REPORT: DURING SCHEDULED ROUTINE C-2 INSPECTION DISCOVERED RIGHT FORWARD EMERGENCY EXIT DOOR OUTSIDE HANDLE STIFF (HARD TO OPEN. LUBRICATED RIGHT FORWARD EMERGE
- [SDR 29GA94152112811A](https://openairdocs.org/sdr/29GA94152112811A), Nov 28, 2011: HANDLE. LACK OF LUBE. DURING SCHEDULED ROUTINE C-1 INSPECTION DISCOVERED LEFT EMERGECNY EXIT OUTER HANDLE WILL NOT SPRING OPEN. LUBRICATED LEFT EMERGENCY EXIT OUTER HANDLE. OUTER HAN
- [SDR 29GA94153081511A](https://openairdocs.org/sdr/29GA94153081511A), Aug 15, 2011: SKIN. CRACKED. REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED R
- [SDR 29GA94153081211A](https://openairdocs.org/sdr/29GA94153081211A), Aug 12, 2011: SKIN. CRACKED. REPORT: DURING SCHEDULED ROUTINE INSPECTION DISCOVERED AIRSTAIR DOOR LOWER COUNTER BALANCE BRACKET ATTACH POINT SKIN CRACK. REMOVED DAMAGED AREA AND INSTALLED R
- [SDR 29GA94132071911A](https://openairdocs.org/sdr/29GA94132071911A), Jul 19, 2011: RELAY. SHORTED. FLIGHT 9257 EYW/FLL PILOT REPORTED LANDING GEAR RELAY POPPED WHEN EXTENDING GEAR. REPLACED LANDING GEAR RELAY OPERATIONAL CHECK OK.
- [SDR GUUA94132052311A](https://openairdocs.org/sdr/GUUA94132052311A), May 23, 2011: SWITCH. DEFECTIVE. PILOT REPORTED ON GEAR RETRACTION LANDING GEAR HORN SOUNDED AND STAYED RED UNTIL LANDING GEAR WAS EXTENDED AGAIN. REPLACED LANDING GEAR WARNING HORN SWITCH.
- [SDR GUUA94161022511A](https://openairdocs.org/sdr/GUUA94161022511A), Feb 25, 2011: ANNUNCIATOR. NO INDICATION. PILOT REPORTED WITH N1 AT 95 PERCENT "AFX DISABLE" ANNUNCIATOR WAS ILLUMINATED AND LT AFX WAS NOT ILLUMINATED. RERACKED ANNUNCIATOR FAULT DETECTION PCB AUTOFEAT
- [SDR GUUA94132022411A](https://openairdocs.org/sdr/GUUA94132022411A), Feb 24, 2011: INDICATION SYS. INOPERATIVE. FLIGHT: 9131 TPA/TLH PILOT REPORTED DURING APPROACH NO GEAR SAFE INDICATION AND LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED. RETURNED TO TPA LANDED WITHOUT IN
- [SDR GUUA94171123010A](https://openairdocs.org/sdr/GUUA94171123010A), Dec 30, 2010: BRACKET. CRACKED. DURING MAGNETIC PARTICLE INSP, DISCOVERED ENGINE TRUSS COWL BRACKET WELD AREA CRACKED. PERFORMED WELD REPAIR TO ENGINE TRUSS COWL BRACKET WELD AREA.
- [SDR GUUA94152090910A](https://openairdocs.org/sdr/GUUA94152090910A), Sep 9, 2010: HANDLE. STIFF. DURING SCHEDULED ROUTINE INSP DISCOVERED LT EMERGENCY EXIT HANDLE STIFF TO OPERATE. LUBRICATED LT EMERGENCY EXIT HANDLE.
- [SDR GUUA94155071910C](https://openairdocs.org/sdr/GUUA94155071910C), Jul 19, 2010: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR INBOARD HINGE BRACKET HAS CORROSION. REPLACED RIGHT ELEVATOR INBOARD HINGE BRACKET.
- [SDR GUUA94155071910B](https://openairdocs.org/sdr/GUUA94155071910B), Jul 19, 2010: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA94155071910A](https://openairdocs.org/sdr/GUUA94155071910A), Jul 19, 2010: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSPECTION DISCOVERED RIGHT ELEVATOR CENTER HINGE BRACKET EXFOLIATED. REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA94132060310A](https://openairdocs.org/sdr/GUUA94132060310A), Jun 3, 2010: BULB. INOPERATIVE. DURING APPROACH SELECTED LANDING GEAR DOWN HAD GREEN LIGHT INDICATION ON THE MAIN GEAR BUT NOT ON THE NOSEWHEEL. R & R LANDING GEAR INDICATOR BULBS.
- [SDR GUUA94153050410B](https://openairdocs.org/sdr/GUUA94153050410B), May 4, 2010: SHIM. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED CORROSION FS 363 FWD AND AFT OF ANGLE BETWEEN STRINGERS 15L AND STRINGER 16. REMOVED AREA OF CORROSION AND REPLACED SEC
- [SDR GUUA94153050410A](https://openairdocs.org/sdr/GUUA94153050410A), May 4, 2010: STRINGER. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR CORROSION APPROX FS 258, STRINGER 14L, FWD OF ANGLE AT SPLICE AREA OF STR 14L. REMOVED DAMAGED SECTION OF STRI
- [SDR GUUA94152050410A](https://openairdocs.org/sdr/GUUA94152050410A), May 4, 2010: HANDLE. BINDING. DURING SCHEDULED ROUTINE INSP DISCOVERED SEAT 6A EMERGENCY EXIT INTERIOR HANDLE IS HARD TO OPERATE. LUBRICATED SEAT 6A EMERGENCY EXIT INTERIOR AND EXTERIOR DOOR
- [SDR GUUA94153043010](https://openairdocs.org/sdr/GUUA94153043010), Apr 30, 2010: ANGLE. CRACKED. DURING SCHEDULED ROUTINE INSP, DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STR, 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. REMOVED 2.2
- [SDR GUUA94153043010A](https://openairdocs.org/sdr/GUUA94153043010A), Apr 30, 2010: ANGLE. CRACKED. DURING SCHEDULED ROUTINE INSP DISCOVERED INTERIOR FUSELAGE ANGLE CRACKED AT FS 150 STRINGER 9AL AT AIRSTAIR DOOR TOP AFT ATTACH POINT OF LOWER BRACKET. (OPEN)
- [SDR GUUA94152021810A](https://openairdocs.org/sdr/GUUA94152021810A), Feb 18, 2010: PANEL. OUT OF LIMITS. PILOT REPORTED CABIN DOOR HARD TO OPEN AFTER LANDING. TRIMMED CABIN DOOR INTERIOR PANEL AROUND PUSH BUTTON OPS CHECK GOOD.
- [SDR GUUA94129012410A](https://openairdocs.org/sdr/GUUA94129012410A), Jan 24, 2010: LINE. LEAKING. DURING FLIGHT HYD LOW LIGHT ILLUMINATED UPON LANDING GEAR EXTENSION, FOUND LARGE HYD FLUID PUDDLE UNDER WING. REPLACED HAND PUMP HYD RETURN LINE. LANDING GEAR O
- [SDR GUUA94132011710A](https://openairdocs.org/sdr/GUUA94132011710A), Jan 17, 2010: ACTUATOR. BYPASSING. DURING FLIGHT LANDING GEAR MOTOR RECYCLING IN AIR ABOUT EVERY THREE TO FOUR MINUTES. REPLACED LT MLG ACTUATOR, OPS CHECK GOOD.
- [SDR GUUA94155121409B](https://openairdocs.org/sdr/GUUA94155121409B), Dec 14, 2009: HINGE. CORRODED. DURING SCHEDULED ROUTINE INSP, DISCOVERED RUDDER CTR HINGE HAS CORROSION. REPLACED RUDDER CTR HINGE.
- [SDR GUUA94155121409A](https://openairdocs.org/sdr/GUUA94155121409A), Dec 14, 2009: HINGE. CORRODED. DURING SCHEDULED ROUTINE INSP, DISCOVERED VERTICAL STABILIZER UPPER RUDDER HINGE HAS CORROSION. REPLACED VERTICAL STABILIZER UPPER RUDDER HINGE.
- [SDR GUUA94132112909A](https://openairdocs.org/sdr/GUUA94132112909A), Nov 29, 2009: PRESSURE SWITCH. OUT OF ADJUST. PILOT REPORTED DELAY IN NOSE WHEEL EXTENSION 4 SECONDS AFTER MAINS. REPLACED HYD PRESSURE SWITCH AND ADJUSTED NLG DOWN POSITION SWITCH. LANDING GEAR OPS CHECK N
- [SDR GUUA94157111409A](https://openairdocs.org/sdr/GUUA94157111409A), Nov 14, 2009: ACCESS PANEL. DELAMINATED. DURING SCHEDULED ROUTINE MX DISCOVERED RT WING FUEL ACCESS PANEL 631DB LEAKING FUEL. INSTALLED EXTERNAL RING DOUBLER ON WING SKIN AT FUEL ACCESS PANEL 631DB, NO
- [SDR GUUA94157103109B](https://openairdocs.org/sdr/GUUA94157103109B), Oct 31, 2009: SPAR. CORRODED. DURING SCHEDULED X-RAY INSP OF LT WING COLLECTOR TANK FOUND SEVERAL SPOTS OF CORROSION ON LWR MAIN SPAR. REMOVED CORROSION FABRICATED AND INSTALLED REPAIR STRAP
- [SDR GUUA94157103109A](https://openairdocs.org/sdr/GUUA94157103109A), Oct 31, 2009: STRINGER. CORRODED. DURING SCHEDULED X-RAY INSP DISCOVERED LT WING COLLECTOR TANK LWR SKIN AFT OF MAIN SPAR BONDED STR HAS MINOR SURFACE CORROSION. REMOVED CORROSION AND INSTALLED 
- [SDR GUUA94152081909A](https://openairdocs.org/sdr/GUUA94152081909A), Aug 19, 2009: DOOR. STUCK. DURING SCHEDULED ROUTINE INSP DISCOVERED RT AFT EMERGENCY EXIT WILL NOT COME OUT OF FRAME. (JAMMED) LUBRICATED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.
- [SDR GUUA94155062209A](https://openairdocs.org/sdr/GUUA94155062209A), Jun 22, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE MX DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. C/A: REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA941062209A](https://openairdocs.org/sdr/GUUA941062209A), Jun 22, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSP, DISCOVERED RT ELEVATOR OTBD HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR OTBD HINGE BRACKET.
- [SDR GUUA94132041609A](https://openairdocs.org/sdr/GUUA94132041609A), Apr 16, 2009: SQUAT SWITCH. FAILED. DURING TEST FLIGHT LT MAIN LANDING GEAR DID NOT EXTEND. MANUALLY EXTENDED LANDING GEAR. LT MAIN GEAR ILLUMINATED DOWN AND LOCKED. OBTAINED 3 GREEN DOWN AND LOCK
- [SDR GUUA94132040609A](https://openairdocs.org/sdr/GUUA94132040609A), Apr 6, 2009: WIRE. CHAFED. DURING FLIGHT, DISCOVERED LANDING GEAR CIRCUIT BREAKER POPPED. REPAIRED CHAFED WIRE D6D22 ON TOP LT NACELLE.
- [SDR GUUA94132032909A](https://openairdocs.org/sdr/GUUA94132032909A), Mar 29, 2009: PCB. FAILED. PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPERATIONAL CHECK NORMAL.
- [SDR GUUA94132032908A](https://openairdocs.org/sdr/GUUA94132032908A), Mar 29, 2009: PCB. DAMAGED. PILOT REPORTED NO 3 GREEN GEAR INDICATION LIGHTS. REPLACED PCB A319. LANDING GEAR OPS CHECK, NORMAL.
- [SDR GUUA94132032809A](https://openairdocs.org/sdr/GUUA94132032809A), Mar 28, 2009: CIRCUIT BREAKER. TRIPPED. DURING APPROACH LANDING GEAR INDICATION CIRCUIT BREAKER POPPED AFTER SELECTING GEAR DOWN. RETURNED TO DEPARTURE. LANDED WITHOUT INCIDENT. OPS CHECK FOUND TO BE 
- [SDR GUUA94132022109B](https://openairdocs.org/sdr/GUUA94132022109B), Feb 21, 2009: CIRCUIT BREAKER. UNKNOWN. FLIGHT: 9233 DURING FLIGHT LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED UNABLE TO RESET. RETURNED TO FLL. REPLACED LANDING GEAR INDICATOR CIRCUIT BREAKER. LAND
- [SDR GUUA94132022109A](https://openairdocs.org/sdr/GUUA94132022109A), Feb 21, 2009: WIRE. BROKEN. FLIGHT: 9270 DURING APPROACH LANDING GEAR INDICATOR CIRCUIT BREAKER POPPED AFTER GEAR EXTENSION. FOUND BROKEN BROKEN WIRE ON LEFT LANDING GEAR DOWN LOCK CONNECT
- [SDR GUUA94132022009A](https://openairdocs.org/sdr/GUUA94132022009A), Feb 20, 2009: CIRCUIT BREAKER. TRIPPED. AFTER TAKEOFF, LANDING GEAR CIRCUIT BREAKER POPPED AFTER GEAR RETRACTED, RESET CIRCUIT BREAKER, STAYED IN THE REST OF THE FLIGHT. PERFORMED OPS CHECK OF LANDING
- [SDR GUUA94152120908A](https://openairdocs.org/sdr/GUUA94152120908A), Dec 9, 2008: DOOR. OUT OF RIG. DURING SCHEDULED ROUTINE MX DISCOVERED RT AFT EMERGENCY EXIT HARD TO OPEN. RERIGGED RT AFT EMERGENCY EXIT. OPS CHECK GOOD.
- [SDR GUUA94157120908A](https://openairdocs.org/sdr/GUUA94157120908A), Dec 9, 2008: SKIN. CORRODED. DURING SCHEDULED ROUTINE MX DISCOVERED RT OTBD WING UPPER SKIN TRAILING EDGE HAD CORROSION AND DEBOND BETWEEN WS 139 THROUGH 158. REMOVED DAMAGED SKIN AND FABRI
- [SDR GUUA11040801](https://openairdocs.org/sdr/GUUA11040801), Nov 4, 2008: WIRE. BROKEN. FLIGHT 5201 MIA/FLL - DURING APPROACH LEFT LANDING GEAR INDICATION LIGHTS DOES NOT SHOW LOCKED. CONTINUED TO FLL. LANDED WITHOUT INCIDENT. REPAIRED BROKEN WIRE 
- [SDR GUUA10260801](https://openairdocs.org/sdr/GUUA10260801), Oct 26, 2008: HANDLE. LACK OF LUBE. DURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LEFT EMERGENCY EXIT DIFFICULT TO OPEN. LUBRICATED LEFT EMERGENCY EXIT HANDLE.
- [SDR GUUA05200801](https://openairdocs.org/sdr/GUUA05200801), May 20, 2008: SQUAT SWITCH. LOOSE. FLIGHT: 9140 AFTER TAKEOFF, LANDING GEAR WILL NOT RETRACT. RETURNED TO DEPARTURE, LANDED WITHOUT INCIDENT RESECURED RT LANDING GEAR SQUAT SWITCH. LANDING GEAR E

All 73: https://openairdocs.org/deregistered/N17541-2012-10-24/reports.md

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