# Raytheon 1900

- Type: Aircraft model (FAA registry)
- Registry code: 7150020
- Manufacturer (registry): RAYTHEON AIRCRAFT COMPANY
- Model: 1900
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 19
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A24CE](https://openairdocs.org/tcds/A24CE) (OpenAirDocs)
- Holder: Textron Aviation Inc.
- Registered aircraft: 0
- Page: https://openairdocs.org/model/raytheon-1900

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2014-02-03](https://openairdocs.org/ad/2014-02-03): Flight Controls · Textron 1900, 1900C and 1900D. Effective Mar 7, 2014
- [AD 2013-24-03](https://openairdocs.org/ad/2013-24-03): Stabilizers · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 13, 2014
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2009-23-03](https://openairdocs.org/ad/2009-23-03): Flanges · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 14, 2009
- [AD 2009-23-01](https://openairdocs.org/ad/2009-23-01): Main Landing Gear · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 8, 2009
- [AD 2006-18-51](https://openairdocs.org/ad/2006-18-51): Left and right wing rear spar lower caps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 8, 2006
- [AD 2005-18-21](https://openairdocs.org/ad/2005-18-21): Elevator hinge support attachments · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Sep 13, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2004-23-02](https://openairdocs.org/ad/2004-23-02): Nose Landing Gear (NLG) Fork · Textron 100, 1900, 1900C and 50 more. Effective Dec 23, 2004
- [AD 2004-17-02](https://openairdocs.org/ad/2004-17-02): Cross shaft attach bolt · Textron 100, 1900, 1900C and 52 more. Effective Oct 4, 2004
- [AD 2004-09-07](https://openairdocs.org/ad/2004-09-07): Canted Bulkhead Located at Fuselage Station (FS) 588.10 · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jun 14, 2004
- [AD 2004-01-13](https://openairdocs.org/ad/2004-01-13): Vent blower assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 19, 2004
- [AD 2003-20-10](https://openairdocs.org/ad/2003-20-10): Elevator Trim System Maintenance Procedures · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 15, 2003
- [AD 2003-03-18](https://openairdocs.org/ad/2003-03-18): Elevator Control System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 2003
- [AD 2002-23-11](https://openairdocs.org/ad/2002-23-11): Elevator Balance Weight Attachment Screws · Textron 1900, 1900C, 1900C (C-12J) and 30 more. Effective Jan 10, 2003
- [AD 2001-22-16](https://openairdocs.org/ad/2001-22-16): Engine Truss Assembly · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 17, 2001
- [AD 2001-18-07](https://openairdocs.org/ad/2001-18-07): Flap Flexible Shaft Assemblies · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 12, 2001
- [AD 2000-20-07](https://openairdocs.org/ad/2000-20-07): Cockpit Voice Recorder (CVR) System · Textron 1900, 1900C and 1900D. Effective Nov 22, 2000
- [AD 97-15-13 R2](https://openairdocs.org/ad/97-15-13-R2): Airstair Door Handle and Latch Housing · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective May 28, 1999
- [AD 99-04-08](https://openairdocs.org/ad/99-04-08): Main Landing Gear Hydraulic Actuators · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Mar 26, 1999
- [AD 99-01-03](https://openairdocs.org/ad/99-01-03): Flaps · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 8, 1999
- [AD 98-26-16](https://openairdocs.org/ad/98-26-16): Emergency Exit Doors · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Feb 5, 1999
- [AD 98-21-20](https://openairdocs.org/ad/98-21-20): Exterior Marking Placards · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Nov 20, 1998
- [AD 97-26-15](https://openairdocs.org/ad/97-26-15): Main Landing Gear Actuator · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 25, 1998
- [AD 97-25-03](https://openairdocs.org/ad/97-25-03): AFM - Limitations - Power Levers · Textron 100, 1900, 1900C and 44 more. Effective Jan 21, 1998
- [AD 97-06-06](https://openairdocs.org/ad/97-06-06): Pilot and Copilot Chairs Locking Pins · Textron 100, 1900, 1900C and 43 more. Effective May 9, 1997
- [AD 95-26-15 R1](https://openairdocs.org/ad/95-26-15-R1): Traffic Alert and Collision Avoidance Systems · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 159 more. Effective Dec 26, 1996
- [AD 96-09-13](https://openairdocs.org/ad/96-09-13): AFM - Icing · Textron 1900, 1900C, 1900D and 7 more. Effective Jun 11, 1996
- [AD 95-14-02](https://openairdocs.org/ad/95-14-02): Instrument Air System · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Aug 31, 1995
- [AD 94-20-05](https://openairdocs.org/ad/94-20-05): Hot Battery Bus · Textron 1900, 1900C, 1900C (C-12J) and 1 more. Effective Oct 14, 1994
- [AD 90-06-13](https://openairdocs.org/ad/90-06-13): Vertical Gyro · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 14 more. Effective Mar 30, 1990
- [AD 85-21-07 R1](https://openairdocs.org/ad/85-21-07-R1): POH/AFM Addendum · Textron 1900, 1900C and 1900C (C-12J). Effective Jul 10, 1987
- [AD 87-04-24](https://openairdocs.org/ad/87-04-24): Elevator Trim Cable System · Textron 1900, 1900C, 200 and 28 more. Effective Apr 14, 1987
- [AD 87-05-02](https://openairdocs.org/ad/87-05-02): POH/AFM Changes · Textron 1900, 1900C and 1900C (C-12J). Effective Mar 23, 1987

Historical (superseded or no longer in force):

- [AD 2011-27-51](https://openairdocs.org/ad/2011-27-51) (historical): Flight Controls · Hawker Beechcraft 1900, 1900C, 1900C (C-12J) and 1 more. Effective Jan 18, 2012
- [AD 97-22-16](https://openairdocs.org/ad/97-22-16) (historical): Vent Blower Assembly Bearing · Raytheon 1900, 1900C, 1900C (C-12J) and 1 more. Effective Dec 5, 1997
- [AD 97-15-13 R1](https://openairdocs.org/ad/97-15-13-R1) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 22, 1997
- [AD 97-15-13](https://openairdocs.org/ad/97-15-13) (historical): Airstair Door Handle And Latch Housing · Raytheon 1900, 1900C and 1900D. Effective Sep 5, 1997
- [AD 97-14-16](https://openairdocs.org/ad/97-14-16) (historical): Outboard Flap Attachment Brackets And Aft Roller Bearings · Raytheon 1900, 1900C and 1900D. Effective Aug 4, 1997
- [AD 97-04-02](https://openairdocs.org/ad/97-04-02) (historical): Exterior Marking Placards For Airstair And Cargo Doors · Raytheon 1900, 1900C and 1900D. Effective Mar 10, 1997
- [AD 95-02-18](https://openairdocs.org/ad/95-02-18) (historical): Engine Truss Assembly · Raytheon 1900, 1900C and 1900D. Effective Mar 25, 1995
- [AD 87-22-01 R1](https://openairdocs.org/ad/87-22-01-R1) (historical): Nose Landing Gear Fork · Raytheon 100 Model or Series (all), 1900, 1900C and 50 more. Effective Sep 30, 1989

## Information bulletins (advisory) (6)

- [SAIB CE-15-15](https://openairdocs.org/saib/CE-15-15): Empennage  Horizontal & Vertical Stabilizer Structure. Issued Apr 20, 2015
- [SAIB CE-12-36](https://openairdocs.org/saib/CE-12-36): Flight Controls: Aileron. Issued Jun 19, 2012
- [SAIB CE-05-83](https://openairdocs.org/saib/CE-05-83): . Issued Aug 26, 2005
- [SAIB CE-02-19](https://openairdocs.org/saib/CE-02-19): . Issued Mar 11, 2002
- [SAIB CE-00-24](https://openairdocs.org/saib/CE-00-24): . Issued Jul 11, 2000
- [SAIB CE-00-15](https://openairdocs.org/saib/CE-00-15): . Issued Jan 21, 2000

## Registered aircraft

None registered with this model now.

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (87, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR JIKA2024052901](https://openairdocs.org/sdr/JIKA2024052901), May 24, 2024: HYDRAULIC LINE. CHAFED. DURING LANDING, THE FLIGHT CREW ATTEMPTED TO LOWER THE GEAR NORMALLY. IT WAS OBSERVED THAT THERE WAS A LOW HYDRAULIC LIGHT FLICKER INDICATING A LOSS OF PRESSURE
- [SDR JIKA2024021601](https://openairdocs.org/sdr/JIKA2024021601), Feb 13, 2024: WIRE HARNESS. SHORTED. WHEN THE FLIGHT CREW PLACED THE LANDING GEAR HANDLE IN THE DOWN POSITION THE CIRCUIT BREAKER POPPED AND CAUSED THE LANDING GEAR INDICATION LIGHTS TO COMPLETELY 
- [SDR JIKA2019101701](https://openairdocs.org/sdr/JIKA2019101701), Oct 15, 2019: PACKING. LEAKING. APPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKL
- [SDR JIKA2018100201](https://openairdocs.org/sdr/JIKA2018100201), Oct 2, 2018: UNKNOWN. SMOKE. THE PILOT REPORTED THAT WHILE INFLIGHT THERE WAS SMOKE OR VAPOR COMING FROM UNDERNEATH THE PILOT AND CO-PILOTS SEATS, WHERE THE FLOOR VENTS ARE LOCATED. THE ENV
- [SDR JIKA2018100192701](https://openairdocs.org/sdr/JIKA2018100192701), Oct 1, 2018: CIRCUIT BREAKER. DEFECTIVE. DISCREPANCY: THE PILOT REPORTED ON APPROACH INTO KBUR, THE CREW SELECTED THE GEAR LEVER TO DOWN. THE THREE GREEN GEAR INDICATORS DID NOT ILLUMINATE. THE CREW EL
- [SDR JIKA2018060453002](https://openairdocs.org/sdr/JIKA2018060453002), May 30, 2018: FILTER. CONTAMINATED. THE PILOT REPORTED DURING TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAIL INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP FA
- [SDR JIKA201806043001](https://openairdocs.org/sdr/JIKA201806043001), May 30, 2018: FILTER. CONTAMINATED. THE PILOT REPORTED AFTER TAKEOFF, THAT THE RIGHT LOW PRESSURE FUEL PUMP FAILED INDICATION ILLUMINATED. THE PILOT ACTIVATED THE RIGHT BOOST PUMP. THE FUEL PUMP F
- [SDR JIKA2018032301](https://openairdocs.org/sdr/JIKA2018032301), Mar 23, 2018: UNKNOWN. SMOKE. THE PILOT REPORTED DURING APPROACH, THERE WAS AN UNUSUAL ODOR FOLLOWED BY LIGHT SMOKE IN THE COCKPIT. THE PILOT FOLLOWED PROCEDURES AND TURNED THE BLEED SYSTEM 
- [SDR JIKA2016052301](https://openairdocs.org/sdr/JIKA2016052301), May 23, 2016: FUEL CELL. LEAKING. EN-ROUTE THE PILOT REPORTED A STRONG FUEL ODOR FROM THE CABIN AREA. DEPRESSURIZED THE CABIN, USED OXYGEN & OPENED THE FRESH AIR VENTS, LANDED WITHOUT INCIDENT. 
- [SDR JIKA201512081501](https://openairdocs.org/sdr/JIKA201512081501), Dec 3, 2015: FUEL CONTROL. LOW PRESSURE. EN-ROUTE, THE PILOT REPORTED THAT THE RT ENG TORQUE STARTED TO DROP OFF. THE PILOT WAS ABLE TO MATCH TOQUE BY ADVANCING THE RT POWER LEVER. DURING APPROACH, THE
- [SDR CA141103001](https://openairdocs.org/sdr/CA141103001), Oct 22, 2014: ENGINE. POWER LOSS. (CAN) DURING THE CRUISE THE CAPTAIN NOTICED THE NR 1 ENGINE SHOWING 93% N1 MAX AND SHORTLY AFTER NOTICING THIS, THE LH GENERATOR FAILED. THE CREW THEN ATTEMPTED
- [SDR GLBA2013021500177](https://openairdocs.org/sdr/GLBA2013021500177), Feb 14, 2013: BULB. INOPERATIVE. PILOT REPORTED THAT THE EMERGENCY LIGHTS ON THE F/O'S SIDE DO NOT ILLUMINATE AND ARE ALSO INOPERATIVE IN INDIRECT LIGHT MODE. MX REPLACED THE BULBS AND SECURED 
- [SDR HSYA20110307001](https://openairdocs.org/sdr/HSYA20110307001), Mar 7, 2011: TORQUE LINK. DAMAGED. RT MLG TORQUE LINK DISCONNECTED AT START OF ACFT TAXING FROM BLOCKS. UPON INSP, MX DISCOVERED INCORRECT WASHER INSTALLATION AT UPPER AND LOWER TORQUE LINK ATTAC
- [SDR GUUA94055030609D](https://openairdocs.org/sdr/GUUA94055030609D), Mar 6, 2009: SPAR CAP. CORRODED. DURING SCHEDULED ROUTINE INSP, DISCOVERED RT HORIZONTAL STABILIZER UPPER REAR SPAR CAP HAS EXFOLIATION. REPLACED RIGHT HORIZONTAL STABILIZER UPPER REAR SPAR CAP
- [SDR GUUA94055030609C](https://openairdocs.org/sdr/GUUA94055030609C), Mar 6, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR OTBD HINGE BRACKET HAS SURFACE CORROSION. REPLACED RT ELEVATOR OUTBOARD HINGE BRACKET.
- [SDR GUUA94055030609B](https://openairdocs.org/sdr/GUUA94055030609B), Mar 6, 2009: HINGE BRACKET. CORRODED. DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA93352011609A](https://openairdocs.org/sdr/GUUA93352011609A), Jan 16, 2009: DOOR. STIFF. DURING SCHEDULED ROUTINE MX, DISCOVERED RT FWD EMERGENCY EXIT HARD TO OPEN. LUBRICATED RT FWD EMERGENCY EXIT DOOR OUTSIDE HANDLE. OPS CHECK OK.
- [SDR TAS07003](https://openairdocs.org/sdr/TAS07003), Nov 16, 2007: CAP. CRACKED. MLG ACTUATOR WAS RECEIVED DUE TO INDICATIONS FOUND IN THE END CAP DURING ULTRASONIC TESTING. ACTUATOR WENT THROUGH A PRELIMINARY INSPECTION AND A COMPLETE FUNCT
- [SDR TIM2005F00003](https://openairdocs.org/sdr/TIM2005F00003), Apr 4, 2005: SKIN. CORRODED. CORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB P
- [SDR TIM2005F00002](https://openairdocs.org/sdr/TIM2005F00002), Apr 4, 2005: SKIN. CORRODED. CORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K)
- [SDR HSY2005F00001](https://openairdocs.org/sdr/HSY2005F00001), Jan 14, 2005: SENSOR. DEFECTIVE. (MRR NR 01-011405) LOSS OF NR 1 ENGINE OIL PRESSURE. LOOSE AND LEAKING OIL TEMPERATURE SENSOR. LOOSE BUT IN SERVICEABLE CONDITION. REMOVED TEMPERATURE SENSOR, I
- [SDR TIM2004F00000](https://openairdocs.org/sdr/TIM2004F00000), Sep 30, 2004: TUBE. PIN HOLE. WHILE DOING A ROUTINE INSPECTION, IT WAS NOTICED HYDRAULIC FLUID ON THE LOWER PORTION OF THE LT IB WING. AFTER CLEANING THE AREA AND PERFORMING A RETRACTION TES
- [SDR GLBA2003072](https://openairdocs.org/sdr/GLBA2003072), Jun 2, 2003: PRESSURE SWITCH. MALFUNCTIONED. RIGHT EVIR ILLUM, ON T/O ROLL. CHECKED THE PRESSURE SOLENOID FOR OPERATION AND LEAKAGE AND RIGHT PROP PRESSURE SWITCH FOR PROPER OPERATION, BOTH GOOD. CHECKED R
- [SDR GLBA2003070](https://openairdocs.org/sdr/GLBA2003070), Jun 1, 2003: FILTER. DIRTY. AIRCRAFT WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER FILTER, OPS CHECK GOOD.
- [SDR GLBA2003071](https://openairdocs.org/sdr/GLBA2003071), May 30, 2003: SWITCH. OUT OF ADJUST. AIRCRAFT RETURNS, FLAPS WILL NOT RETRACT. ADJUSTED FLAP SAFETY SWITCH, OPS CK GOOD.
- [SDR TIM2002F00010](https://openairdocs.org/sdr/TIM2002F00010), Feb 15, 2002: ANGLE. BROKEN. ANGLE LOCATED ABOVE THE ICE DOOR HINGE. THIS ANGLE HOLDS THE LOWER FIRE SEAL BULK HEAD WHEN THIS ANGLE CRACKS, IT ALLOWS THE OUTSIDE COWL RIVETS TO WORK LOOSE, 
- [SDR AUS20020164](https://openairdocs.org/sdr/AUS20020164), Jan 31, 2002: LIGHT. FAILED. (AUS) RH MAIN LANDING GEAR POSITION LIGHT FAILED.
- [SDR TIM2002F00009](https://openairdocs.org/sdr/TIM2002F00009), Jan 16, 2002: BOLT. CORRODED. BOLT PN 908200115, CONNECTING NOSE GEAR DRAG BRACE TO NOSE STRUT, AND BOLT PN 908200111 CONNECTING THE TWO DRAG BRACE HALVES WAS FOUND WITH PITTING TYPE CORROSI
- [SDR OYG2002F00000](https://openairdocs.org/sdr/OYG2002F00000), Dec 5, 2001: COWLING. CRACKED. SEVERAL CRACKS WERE FOUND ON THE INSIDE OF THE AIR INLET COWL (HOT LIP) THESE CRACKS RUN HORIZONTALLY AND VERTICALLY ALONG THE WELD THE POSSIBLE CAUSE MIGHT BE 
- [SDR TIM2002F00004](https://openairdocs.org/sdr/TIM2002F00004), Dec 4, 2001: CABLE. BROKEN. AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.
- [SDR 2003F00020](https://openairdocs.org/sdr/2003F00020), Nov 27, 2001: ANGLE. CRACKED. GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. REPLACED THE LEFT ENGINE COWLING REINFORCEMENT ANGLE, THE ENGINE TRUSS BRACKET RECEPTACLE, AND 
- [SDR 2003F00019](https://openairdocs.org/sdr/2003F00019), Nov 27, 2001: BRACKET. CRACKED. GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. STRUCTURAL REPAIRS ARE IN PROGRESS. (M)
- [SDR TIM2001F00011](https://openairdocs.org/sdr/TIM2001F00011), Oct 16, 2001: WIRE. BROKEN. THE ICE VANE CONTROL WIRE NUMBER 20A20 BROKE AT THE TERMINAL END UNDER THE PANEL AT INST ZONE 245 CAUSING A SHORT WHICH CAUSED SMOKE IN THE COCKPIT.
- [SDR TIM2001F00009](https://openairdocs.org/sdr/TIM2001F00009), Oct 15, 2001: BULKHEAD. CRACKED. THE LEFT COWLING BULKHEAD AT STATION 238.18 THAT THE LOWER FRONT ENGINE COWLING ATTACHES TO WAS BROKEN OUT ON THE RIGHT LOWER SIDE. THE LOCATION IS WHERE ONE OF
- [SDR 2001F00623](https://openairdocs.org/sdr/2001F00623), Oct 4, 2001: SHAFT. DEFECTIVE. INSPECTION OF FLAP CABLES AS OUTLINED IN BEECH S/B 27-3397 PER AD 2001-18-07 REVEALED THE RIGHT OUTBOARD FLAP CABLE DEFECTIVE. THE INNER SHAFT RETAINER WAS NOT 
- [SDR TIM2001F00006](https://openairdocs.org/sdr/TIM2001F00006), May 22, 2001: B-NUT. LOOSE. OIL LINE TO THE TORQUE MANIFOLD, B-NUT CAME LOOSE, OIL PRESSURE FLUCTUATED AND ENGINE SHUT DOWN. AIRCRAFT LANDED. ENGINE WAS INSPECTED AS PER MM, LOW OIL PRESSU
- [SDR GUU2001F00008](https://openairdocs.org/sdr/GUU2001F00008), Apr 25, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGH
- [SDR GUU2001F00007](https://openairdocs.org/sdr/GUU2001F00007), Apr 25, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS ON INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT 
- [SDR 2001F00089](https://openairdocs.org/sdr/2001F00089), Apr 24, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT E
- [SDR 2001F00088](https://openairdocs.org/sdr/2001F00088), Apr 24, 2001: HINGE BRACKET. CORRODED. DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIG
- [SDR ME42001F00000](https://openairdocs.org/sdr/ME42001F00000), Mar 26, 2001: SPRING. BROKEN. HARTZELL PROPELLER MODEL NUMBER HC-B4MP-3A/M10877K WITH SERIAL NUMBER FW778 WAS RECEIVED FOR HUB REPLACEMENT IAW AD NOTE 96-18-14. DURING THE DISASSEMBLY, THE S
- [SDR 20000925SH017](https://openairdocs.org/sdr/20000925SH017), Sep 5, 2000: TRUSS. CRACKED. GJT - RIGHT ENGINE TRUSS MOUNT CRACKED NEAR WELD AT UPPER OUTBOARD ATTACH POINT. AREA ''A''. CRACKED AT TYPICAL LOCATION AS IDENTIFIED IN AD 95-02-18, BEECH SB 
- [SDR 20000725AP006](https://openairdocs.org/sdr/20000725AP006), Apr 26, 2000: BRACKET. CORRODED. DURING ROUTINE MAINTENANCE, RIGHT MIDDLE ELEVATOR ATTACH BRACKET HINGE CORRODED. REMOVED AND REPLACED MIDDLE ELEVATOR HINGE ATTACH BRACKET. (M)
- [SDR MASA00018](https://openairdocs.org/sdr/MASA00018), Feb 10, 2000: BULB. UNSERVICEABLE. FLT 6202 - FLG-PHX - DURING STANDARD PRE-FLIGHT CHECK, THE CREW NOTED THE INSTRUMENT EMERGENCY LIGHT ON THE CAPTAINS SIDE WAS INOPERATIVE. THIS ITEM WAS DEFERRE
- [SDR 20000725AP004](https://openairdocs.org/sdr/20000725AP004), Jul 1, 1999: TRUSS. CRACKED. C-2 INSPECTION, RIGHT ENGINE TRUSS HAS A CRACK AT INBOARD COWLING ATTACH BRACKET. REMOVED AND REPLACED RIGHT ENGINE TRUSS. (M)
- [SDR 98ZZZM612](https://openairdocs.org/sdr/98ZZZM612), Jul 26, 1998: SWITCH. OUT OF ADJUST. FLT 9472 - TLH-TPA - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS IN APPROACH POSITION. ADJUSTED APPROACH LIMITS SWITCH. OPERATIONAL CHECKS SATISFACTORY. (M)
- [SDR 98ZZZM613](https://openairdocs.org/sdr/98ZZZM613), Jul 25, 1998: LEVER. OUT OF ADJUST. FLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LEVER GUARD. OPERATIONAL CHECKS SATISFACTOR
- [SDR 98ZZZX2865](https://openairdocs.org/sdr/98ZZZX2865), Jul 16, 1998: ACM. MALFUNCTIONED. RSW/MIA - FLT 9283 - ON TAKEOFF, SMOKEY SMELL WHEN ACM IS SELECTED. SMELL DISSIPATED AFTER 30 SECONDS. RAN AIRCRAFT ENGINES WITH ACM RUNNING. COULD NOT DUPLICAT
- [SDR 98ZZZX2261](https://openairdocs.org/sdr/98ZZZX2261), Jun 4, 1998: BEARING. FAILED. TACHOMETER/GENERATOR WAS OVERHAULED 55.9 HOURS AGO. UNIT STOPPED WORKING. ON REMOVAL, FOUND DRIVE SHAFT SNAPPED IN TWO. ON DI SASSEMBLY, FOUND BOTH BEARINGS HAD
- [SDR 98ZZZX2410](https://openairdocs.org/sdr/98ZZZX2410), Jun 3, 1998: LINE. CRACKED. EYW/MIA - FLT 5300 - LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED RIGHT HAND 'UP' HYDRAULIC LINE. (X)

All 87: https://openairdocs.org/model/raytheon-1900/reports.md

## STCs that may be installed (OpenAirDocs) (113, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA01800SE](https://openairdocs.org/stc/SA01800SE): Fabrication and installation of new or replacement of existing instrument panel lights dimmer control. TCW Technologies, LLC
- [STC SA01861SE](https://openairdocs.org/stc/SA01861SE): Fabrication and installation of Landing Light Controller. TCW Technologies, LLC
- [STC SA04837NY](https://openairdocs.org/stc/SA04837NY): Installation of AeroLED's Holdings, LLC., position lights, navigation lights, strobe lights and beacon lights. AeroLED's Holdings, LLC
- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA12345IB](https://openairdocs.org/stc/SA12345IB): Replacement of the Halon Type 1211 portable fire extinguisher with the Halotron BrX portable fire extinguisher. Cessna Duesseldorf Citation Service Center GmbH
- [STC SA02355AK](https://openairdocs.org/stc/SA02355AK): Installation of cargo barrier net; Tednologies Inc.(TI) P/N 150A-28-000. Tednologies Inc
- [STC SA11158SC](https://openairdocs.org/stc/SA11158SC): Demonstration of aircraft tolerance to potential electromagnetic interference from certain Transmitting Potable Electronic Devices (T-PEDS). Liberty Partners Inc
- [STC SA09887AC](https://openairdocs.org/stc/SA09887AC): Installation of an Avionica MK-III mini Quick Access Recorder (QAR) and optional 4G or LTE Avionica Cellular Module (avCM. Aircraft Systems and Manufacturing Inc
- [STC ST02754NY](https://openairdocs.org/stc/ST02754NY): Replacement of JET PS835C or PS835D Battery packs with Securaplane XL244-D Battery Packs. Securaplane Technologies Inc
- [STC SA02386AK](https://openairdocs.org/stc/SA02386AK): Replacement of existing landing and/or taxi light reflector and bulbs with Light Emitting Diode (LED) lighting systems. AeroLED's Holding LLC
- [STC SA00322BO](https://openairdocs.org/stc/SA00322BO): Installation of a Supplemental Exterior Lighting System. ATI Engineering Services LLC
- [STC SA04051CH](https://openairdocs.org/stc/SA04051CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC SA01050WI](https://openairdocs.org/stc/SA01050WI): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA00128IB](https://openairdocs.org/stc/SA00128IB): Antenna Installation and Bulkhead Feedthrough. Avmax Aviation Services Inc
- [STC SA00120IB](https://openairdocs.org/stc/SA00120IB): Installation of the Universal Kapture Cockpit Voice Recorder (CVR) with Recorder Independent Power Supply (RIPS). Avmax Aviation Services Inc
- [STC SA02010WI](https://openairdocs.org/stc/SA02010WI): Installation of the Mid-Continent Instruments & Avionics MD23 FLEX Custom Function Display (CFD). Mid-Continent Instruments and Avionics
- [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC
- [STC SA02444AK](https://openairdocs.org/stc/SA02444AK): Approval of the L-3 Communications NGT 9000/9000R ADS-B system installed. ADS-B Technologies LLC
- [STC SA04634NY](https://openairdocs.org/stc/SA04634NY): Modification of the Brake Master Cylinder. Marsh Brothers Aviation Inc
- [STC SA04459NY](https://openairdocs.org/stc/SA04459NY): Installation of MT-Propeller Entwicklung GmbH model MTV-27-1-( )-C-F-R(P)/CFR260-65( ) 5-blade, constant speed, full feathering, reversible propellers and spinners. MT- Propeller Entwicklung GmbH
- [STC SA10236SC](https://openairdocs.org/stc/SA10236SC): Installation of a GDC 31 Roll Steering Converter. DAC International Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA02268CH](https://openairdocs.org/stc/SA02268CH): Installation of Airwolf Filter Corp. Air Oil Separator. Airwolf Filter Corporation
- [STC SA01452CH](https://openairdocs.org/stc/SA01452CH): Installation of an air ambulance conversion kit. Med-Pac Inc
- [STC SA00889DE](https://openairdocs.org/stc/SA00889DE): Installation of Teledyne Battery Products P/N 7638-44 Lead-Acid Battery. Teledyne Battery Products
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights. Whelen Aerospace Technologies
- [STC SA01923WI](https://openairdocs.org/stc/SA01923WI): Installation of an Auxiliary Aural Alert System. Hawker Pacific Pty Ltd
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA02013CH](https://openairdocs.org/stc/SA02013CH): Installation of Avidyne Corporation Traffic Advisory System (TAS). Avidyne Corporation
- [STC SA2366CE](https://openairdocs.org/stc/SA2366CE): Installation of cabinetry on the airplane seat tracks. Textron Aviation Inc
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA03902NY](https://openairdocs.org/stc/SA03902NY): Installation of the Hyperion/Orion LED wing tip and tail light assemblies. KAD Aerospace Corp
- [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation
- [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation
- [STC SA1129GL](https://openairdocs.org/stc/SA1129GL): Install Aero Medical Products Mfg. air ambulance stretcher p/n 125 using Installation Kit p/n 805. Paul/ Lanna Egan LLC
- [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC
- [STC SA01969SE](https://openairdocs.org/stc/SA01969SE): Installation of a Mid-Continent MD302 Standby Attitude Module. Mid-Continent Instruments and Avionics
- [STC SA01229SE PAGE 2](https://openairdocs.org/stc/SA01229SE%20PAGE%202): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA3783NM](https://openairdocs.org/stc/SA3783NM): Installation of upper wing reinforcing kit. Dynamic Aviation Group Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA03153NY](https://openairdocs.org/stc/SA03153NY): Installation of structural provisions for a Latitude Iridium/GPS antenna. Latitude Technologies Corporation
- [STC SA02149AK](https://openairdocs.org/stc/SA02149AK): Installation of GX50/60 GPS Navigator, Capstone configured MX20 Multi-Function Display and UAT transceiver. Garmin International Inc
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA5227NM](https://openairdocs.org/stc/SA5227NM): Reduce number of passenger seats installed from 19 to 9. Corporate Air
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc

All 113: https://openairdocs.org/model/raytheon-1900/stcs.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Beech 1900](https://openairdocs.org/model/beech-1900): 7 registered aircraft, registry code 1154160

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