# N184UX: 1995 Beech 1900D - Status: Valid registration - Airframe: [Beech 1900D](https://openairdocs.org/model/beech-1900d) (registry code 1154162, 19 seats) - 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) (Textron Aviation Inc.) (OpenAirDocs) - Serial number: UE-184 - Year built: 1995 - Type: Fixed wing multi engine - Engine type: Turbo-prop - Airworthiness: Standard, commuter - Airworthiness date: November 27, 1995 - Certificate issued: March 25, 2023 - Expires: March 31, 2030 - Mode S code: A15160 - Registered owner: [Alpine Aviation Inc](https://openairdocs.org/faa-owner/ALPINE%20AVIATION%20INC) - Location: [Provo, UT](https://openairdocs.org/faa-place/UT/Provo) - Owner type: Corporation - Owner's area on the map: 40.2272° N, 111.6958° W: Placed by OpenAirDocs at the center of ZIP code 84601, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=184UX - Page: https://openairdocs.org/aircraft/N184UX From the FAA registry file of October 21, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Pratt & Whitney PT6A model are included. ## ADs that may apply (OpenAirDocs): 77 in force ### Matched by airframe (Beech 1900D) - [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 2006-16-18 R1](https://openairdocs.org/ad/2006-16-18-R1): Installing a warning placard on the TAWS/RMI · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 100 more. Effective Jul 18, 2008 - [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 2004-17-02](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 2003-09-12](https://openairdocs.org/ad/2003-09-12): Rivets · Textron 1900D. Effective Jun 27, 2003 - [AD 2003-04-26](https://openairdocs.org/ad/2003-04-26): AC Inverter and Inverter Sync Wire Shield · Textron 1900D. Effective Apr 21, 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 2002-14-19](https://openairdocs.org/ad/2002-14-19): Collins Air Data Computers (ADC) · Boeing DC-8-11, DC-8-12, DC-8-21 and 36 more. Effective Aug 23, 2002 - [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 2001-15-17](https://openairdocs.org/ad/2001-15-17): Transponder Control Panels · Bombardier ATR42-200, ATR42-300, ATR42-320 and 30 more. Effective Aug 20, 2001 - [AD 2001-11-03](https://openairdocs.org/ad/2001-11-03): Blower Motor Circuit · Textron 1900D, 58, 58A and 5 more. Effective Jul 20, 2001 - [AD 2001-04-05](https://openairdocs.org/ad/2001-04-05): Global Positioning System · Textron 1900D with STC SA00245WI-D. Effective Apr 9, 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 2000-19-04](https://openairdocs.org/ad/2000-19-04): Wing Fuel Quantity Wiring Harness · Textron 1900C, 1900C (C-12J) and 1900D. Effective Oct 31, 2000 - [AD 99-18-15](https://openairdocs.org/ad/99-18-15): Landing Gear Emergency Hand Pumps · Textron 1900D, B200, B300 and 1 more. Effective Sep 27, 1999 - [AD 99-16-12](https://openairdocs.org/ad/99-16-12): Electric Elevator Trim · Textron 1900D. Effective Sep 27, 1999 - [AD 99-12-07](https://openairdocs.org/ad/99-12-07): Passenger Oxygen Container And Mask Assembly · Textron 1900D. Effective Jul 23, 1999 - [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 99-09-15](https://openairdocs.org/ad/99-09-15): Flight Control Mechanism · Textron 1900D, 58, 58A and 5 more. Effective May 18, 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 98-13-11](https://openairdocs.org/ad/98-13-11): Ground Idle Low Pitch Stop System · Textron 1900D. Effective Aug 3, 1998 - [AD 98-09-12](https://openairdocs.org/ad/98-09-12): Inspect Communication Systems · Textron 1900D. Effective Jun 12, 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 97-17-08](https://openairdocs.org/ad/97-17-08): Propeller Mounting Bolts · Textron 1900D. Effective Sep 24, 1997 - [AD 97-10-14](https://openairdocs.org/ad/97-10-14): Stabilon Attachment Angles · Textron 1900D. Effective Jul 7, 1997 - [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 97-03-01](https://openairdocs.org/ad/97-03-01): Right-Hand Exhaust Stacks · Textron 1900D. Effective Mar 14, 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 96-22-12](https://openairdocs.org/ad/96-22-12): Inspect fuel filter assembly · Textron 1900C, 1900C (C-12J), 1900D and 1 more. Effective Dec 13, 1996 - [AD 96-15-01](https://openairdocs.org/ad/96-15-01): Windshield Heat Control Circuit Breakers · Textron 1900D. Effective Sep 19, 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 95-26-14](https://openairdocs.org/ad/95-26-14): Inspect Cabin Partition Bracket · Textron 1900D. Effective Jan 31, 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 95-02-17](https://openairdocs.org/ad/95-02-17): Elevator Trim Tab Control Cable · Textron 1900D. Effective Apr 17, 1995 ### Matched by engine (Pratt & Whitney PT6A series) - [AD 2024-04-51](https://openairdocs.org/ad/2024-04-51): Turbine Section · Pratt & Whitney Canada PT6A-64, PT6A-66, PT6A-66A and 17 more. Effective Mar 28, 2024 - [AD 2022-08-13](https://openairdocs.org/ad/2022-08-13): Turbine Section · Pratt & Whitney Canada PT6A-34, PT6A-34B, PT6A-34AG and 2 more. Effective May 27, 2022 - [AD 2016-05-13](https://openairdocs.org/ad/2016-05-13): Corrosion and perforation of the two-ply Cu-Be bellows in Woodward FCUs. · Pratt & Whitney Canada PT6A-60AG, PT6A-65AG, PT6A-67AF and 1 more. Effective Apr 22, 2016 - [AD 2014-17-08 R1](https://openairdocs.org/ad/2014-17-08-R1): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Jun 5, 2015 - [AD 2014-11-05](https://openairdocs.org/ad/2014-11-05): Reinforcement liner to the power turbine (PT) containment ring and, for certain PT containment rings, adding scallops · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 18 more. Effective Aug 5, 2014 - [AD 2012-09-10](https://openairdocs.org/ad/2012-09-10): First stage sun gears · Pratt & Whitney Canada PT6A-110, PT6A-112, PT6A-114 and 12 more. Effective May 23, 2012 - [AD 2011-25-12](https://openairdocs.org/ad/2011-25-12): Sun gear · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Dec 28, 2011 - [AD 2011-20-51](https://openairdocs.org/ad/2011-20-51): Gears · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 4 more. Effective Nov 1, 2011 - [AD 2004-25-18](https://openairdocs.org/ad/2004-25-18): Propeller governor assemblies · Pratt & Whitney Canada PT6A-60A and PT6A-65B. Effective Jan 18, 2005 - [AD 2002-23-13](https://openairdocs.org/ad/2002-23-13): Turbine Exhaust Ducts · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 20 more. Effective Dec 31, 2002 - [AD 2001-20-01](https://openairdocs.org/ad/2001-20-01): Compressor Bleed Valve Assembly · Pratt & Whitney Canada PT6A-114A and PT6A-25C. Effective Nov 5, 2001 - [AD 97-04-12](https://openairdocs.org/ad/97-04-12): Compressor Bleed-off Valve · Pratt & Whitney Canada PT6A-11, PT6A-110, PT6A-112 and 52 more. Effective Mar 14, 1997 - [AD 95-13-08](https://openairdocs.org/ad/95-13-08): Compressor Turbine Disk · Pratt & Whitney Canada PT6A-67D. Effective Jul 12, 1995 - [AD 93-23-06](https://openairdocs.org/ad/93-23-06): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50. Effective Jan 26, 1994 - [AD 92-15-11](https://openairdocs.org/ad/92-15-11): Compressor Delivery Air Line (P3) Filter Assembly · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-21 and 7 more. Effective Aug 17, 1992 - [AD 90-12-05](https://openairdocs.org/ad/90-12-05): Engine Overhaul · Pratt & Whitney Canada PT6A-15AG, PT6A-27, PT6A-28 and 3 more. Effective May 30, 1990 - [AD 86-10-05](https://openairdocs.org/ad/86-10-05): First Stage Compressor Hub · Pratt & Whitney Canada PT6A-42. Effective Jun 5, 1986 - [AD 80-08-12](https://openairdocs.org/ad/80-08-12): Fuel Pump Drive Coupling Splines · Pratt & Whitney Canada PT6A-11, PT6A-112, PT6A-135 and 24 more. Effective Apr 18, 1980 - [AD 80-04-02](https://openairdocs.org/ad/80-04-02): Push-Pull Control Terminal · Pratt & Whitney Canada PT6A-20, PT6A-6A, PT6A-6B and 1 more. Effective Feb 8, 1980 - [AD 78-17-07](https://openairdocs.org/ad/78-17-07): Fuel Control Unit · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Aug 31, 1978 - [AD 78-12-04](https://openairdocs.org/ad/78-12-04): No. 2 Bearing Pressure Oil Transfer Tube Assembly · Pratt & Whitney Canada PT6A-38, PT6A-41 and PT6A-45A. Effective Jun 19, 1978 - [AD 75-06-01](https://openairdocs.org/ad/75-06-01): Gearbox Deterioration · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 11 more. Effective Apr 1, 1977 - [AD 75-11-04](https://openairdocs.org/ad/75-11-04): Reduction Gearbox Engine Distress · Pratt & Whitney Canada PT6A-20, PT6A-20A, PT6A-20B and 8 more. Effective May 20, 1975 - [AD 70-16-01](https://openairdocs.org/ad/70-16-01): Turbo Propeller Governors · Pratt & Whitney Canada PT6A-11, PT6A-11AG, PT6A-15AG and 5 more. Effective Aug 4, 1970 - [AD 69-23-06](https://openairdocs.org/ad/69-23-06): Fuel Pumps · Pratt & Whitney Canada PT6A-20, PT6A-27, PT6A-28 and 4 more. Effective Nov 15, 1969 - [AD 68-05-03](https://openairdocs.org/ad/68-05-03): Reverse Mode · Pratt & Whitney Canada PT6A-20 and PT6A-6B. Effective Feb 28, 1968 ### 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 2006-24-11](https://openairdocs.org/ad/2006-24-11) (historical): Forward, vertical, and aft flanges · Hawker Beechcraft 1900C, 1900C (C-12J) and 1900D. Effective Dec 11, 2006 - [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 2014-17-08](https://openairdocs.org/ad/2014-17-08) (historical): Compressor turbine (CT) blades · Pratt & Whitney Canada PT6A-114 and PT6A-114A. Effective Oct 8, 2014 - [AD 88-24-02](https://openairdocs.org/ad/88-24-02) (historical): Airframe Chip Detector Flag System · Pratt & Whitney Canada PT6A-50 All 87: https://openairdocs.org/aircraft/N184UX/ads.md ## Information bulletins (advisory) (10 in force) - [SAIB 2026-02](https://openairdocs.org/saib/2026-02): Elevator Tab Control System. Issued Jan 21, 2026 - [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-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 - [SAIB NE-15-21](https://openairdocs.org/saib/NE-15-21): Fuel Injector Nozzle. Issued Aug 19, 2015 - [SAIB NE-12-04](https://openairdocs.org/saib/NE-12-04): Turbine/ Turboprop Engine: Reduction Gearbox. Issued Nov 1, 2011 - [SAIB NE-10-47](https://openairdocs.org/saib/NE-10-47): Turbine Engine Compressor Section. Issued Aug 30, 2010 - [SAIB NE-06-34](https://openairdocs.org/saib/NE-06-34): . Issued Mar 21, 2006 - [SAIB CE-03-24](https://openairdocs.org/saib/CE-03-24): . Issued Feb 19, 2003 ## NTSB investigations None matched to N184UX. ## FAA accident and incident reports None matched to N184UX. ## Service difficulty reports (81, newest 50) As reported by operators and repair stations. - [SDR TIMA2024071105007](https://openairdocs.org/sdr/TIMA2024071105007), Jul 5, 2024: ENGINE. POWER LOSS. AFTER DESCENDING AND LEVELING OFF LEFT ENGINE TORQUE NOT RISISNG PROPERLY AND INCORRECT ENGINE CONTROL/FEEL, PILOT NOTICED IMPROPER PWOER OUT OF LEFT ENGINE AND - [SDR TIMA20221003011](https://openairdocs.org/sdr/TIMA20221003011), Sep 27, 2022: ENGINE. LOW TORQUE. NORMAL START, NORMAL RUNNUP. ADVANCED POWER ON RWY 28R AND MANIPULATED POWER LEVERS TO MATCH TORQUES. ROTATED AT VR AND NOTICED AN ABNORMAL SPLIT IN THE POSITIO - [SDR GLBA2016082500607](https://openairdocs.org/sdr/GLBA2016082500607), Aug 23, 2016: BRACKET. WORN. PILOT REPORTED THAT THE LEFT PROPELLER SEEMS LIKE IT TRIES TO AUTOFEATHER FURING FINAL. MAINTENANCE R & R THE BETA ARM LEVER IAW BMM 61-20-00 STEP 2 PN:3054890- - [SDR GLBA2016031800575](https://openairdocs.org/sdr/GLBA2016031800575), Mar 18, 2016: SUPPORT. CRACKED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE LT SIDEWALL SEAT TRACK SUPPORT, STRINGER 10L, CRACKED IN THE FLANGE BEND RADIUS, AT FS 327.63, 1" IN LENG - [SDR GLBA2016030200574](https://openairdocs.org/sdr/GLBA2016030200574), Mar 2, 2016: PANEL. CRACKED. MAJOR REPAIR DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE NUTPLATE PANEL FOR THE ACCESS DOOR 632IB, WS 148.2, RT WING LOWER SIDE, 1.4" IN LENGTH. WILL BE - [SDR GLBA2016021700571](https://openairdocs.org/sdr/GLBA2016021700571), Feb 15, 2016: BRACKET. WORN. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE INBD ATTACH BOLT WORN INTO BRACKET ON THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUBMITT - [SDR GLBA2016021500570](https://openairdocs.org/sdr/GLBA2016021500570), Feb 12, 2016: FRAME. CRACKED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND FUSELAGE FRAME FLANGE CRACKED, FROM THE BEND RADIUS TO THE EDGE OF THE FLANGE, FS 150.60 BETWEEN STRINGER 2R - [SDR GLBA2016021500569](https://openairdocs.org/sdr/GLBA2016021500569), Feb 12, 2016: SKIN. DENTED. DURING A SCHEDULED INSPECTION, FOUND A DENT IN THE FUSELAGE SKIN, BETWEEN FS 378.25 & 381.25, BELOW STRINGER 12L. DENT APPROX SIZE 2.7 X 2. MAJOR REPAIR. - [SDR GLBA2016021500568](https://openairdocs.org/sdr/GLBA2016021500568), Feb 12, 2016: SKIN. CRACKED. DURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT FS 225.25, BETWEEN STRINGER 16 & 15R, CRACKED APPROX .2" IN LENGTH, EVIDENCE OF CORROSION FROM STRINGER 1 - [SDR GLBA2016021500567](https://openairdocs.org/sdr/GLBA2016021500567), Feb 12, 2016: BRACKET. WORN. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND THE OTBD ATTACH BOLT WORN INTO THE BRACKET OF THE RT INBD FLAP ACTUATOR. SUPPLEMENTAL INFORMATION WILL BE SUB - [SDR GLBA2016020900566](https://openairdocs.org/sdr/GLBA2016020900566), Feb 8, 2016: SKIN. DAMAGED. MAJOR REPAIR, DURING A SCHEDULED INSPECTION, FOUND AT FS 281.00, BETWEEN STRINGERS 14L & 13L, A 3" LONG, .5" WIDE WARE IMPRESSION FROM THE HYD LINE & A SMALL PI - [SDR GLBA2015082000531](https://openairdocs.org/sdr/GLBA2015082000531), Aug 19, 2015: SNUBBER. DETACHED. SIG EVENT, PILOT NOTED THAT THE CABIN DOOR SNUBBER DETACHED IN FLIGHT. LOCATED THE UPPER BOLT FOR THE AIRSTAIR DOOR SNUBBER ON THE FLOORBOARD. INSPECTED THREADS - [SDR GLBA2015010200489](https://openairdocs.org/sdr/GLBA2015010200489), Jan 1, 2015: MASTER CYLINDER. LEAKING. THE LT BRAKE PEDAL IS MUSHY & IT MUST BE FULLY DEPRESSED TO ACTIVATE THE BRAKES. FOUND EVIDENCE TO SUSPECT THAT THE CAPTAIN'S LT BRAKE MASTER CYLINDER, SN 4112, - [SDR GLBA2014123000487](https://openairdocs.org/sdr/GLBA2014123000487), Dec 29, 2014: LINE. LOOSE. THE CAPTAIN`S LEFT BRAKE PEDAL WENT TO THE FLOOR. FOUND THE BRAKE LINE LOOSE AT CLUSTER FITTING BETWEEN 1 & 2 BRAKE. TIGHTENED BRAKE LINE & BLED BRAKES IAW TC 1 - [SDR GLBA2014081800429](https://openairdocs.org/sdr/GLBA2014081800429), Aug 15, 2014: ENGINE. FAILED. PILOT REPORTED THAT AFTER REACHING CRUISE FLT LEVEL 240, NR 2 ENGINE FAILED WITH A BANG. LOST ALL POWER, PROP AUTO FEATHERED, RAN CHECK LIST, EMERGENCY DECLARED - [SDR GLBA2013081600294](https://openairdocs.org/sdr/GLBA2013081600294), Aug 16, 2013: SKIN. CRACKED. DURING A SCHEDULED INSPECTION FOUND THE RT FUSELAGE BELLY SKIN CRACKED AT JUNCTION WITH WING SPAR AT FS 288, FWD SIDE OF WING SPAR, .9" IN LENGTH. REPAIRED IAW - [SDR GLBA2013080200289](https://openairdocs.org/sdr/GLBA2013080200289), Aug 2, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND A CRACK IN THE COCKPIT RT SIDEWALL FRAME AT FS 107 AT UPPER FASTENER, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-053. - [SDR GLBA2013080200288](https://openairdocs.org/sdr/GLBA2013080200288), Aug 2, 2013: LONGERON. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE COCKPIT RT SIDEWALL LONGERON AT FS 107, .5" IN LENGTH. REPAIRED IAW EO 13-1900-53-054. - [SDR GLBA2013073000287](https://openairdocs.org/sdr/GLBA2013073000287), Jul 29, 2013: STRINGER. DAMAGED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A HOLE IN THE STRINGER ON THE VERTICAL STAB, LT SIDE AT CSS-68 AND 29.75 PERCENT CHORD, HOLE APPROX .5" IN DIAMETER - [SDR GLBA2013073000286](https://openairdocs.org/sdr/GLBA2013073000286), Jul 29, 2013: RIB. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE RT INBD WING INBD RIB AT BL-29 AFT SIDE BY SPAR, .75 INCHE IN LENGTH. REPAIRED IAW EO 13-1900-57-014 - [SDR GLBA2013073000284](https://openairdocs.org/sdr/GLBA2013073000284), Jul 29, 2013: ANGLE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE A/S DOOR ANGLE AT FS 150.60 AT BOTH UPPER SNUBBER MOUNT NUTPLATES, TWO INCHES IN LENGTH. REPAIRED - [SDR GLBA2013073000283](https://openairdocs.org/sdr/GLBA2013073000283), Jul 29, 2013: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND THREE CRACKS IN THE FUSELAGE FRAME AT BS 183.5, BETWEEN S2-3R AND SECOND CRACK FOUND FIVE INCHES OTBD, AND THIRD CR - [SDR GLBA2013072600280](https://openairdocs.org/sdr/GLBA2013072600280), Jul 26, 2013: VALVE. INOPERATIVE. PILOT REPORTED ON GEAR EXTENSION, INTRANSIT LIGHT ILLUMINATED MOMENTARILY, THEN GEAR HANDLE CIRCUIT BREAKER TRIPPED, LOST ALL GEAR INDICATIONS, FOLLOWED CHECKLI - [SDR GLBA2013072900282](https://openairdocs.org/sdr/GLBA2013072900282), Jul 26, 2013: CIRCUIT BREAKER. TRIPPED. PILOT REPORTED THAT THE LANDING GEAR CIRCUIT BREAKER TRIPPED IN FLT, PERFORMED MANUAL EXTENTION. COULD NOT DUPLICATE. - [SDR GLBA2013072900281](https://openairdocs.org/sdr/GLBA2013072900281), Jul 26, 2013: LANDING GEAR. FAILED. PILOT REPORTED THAT DURING AN OPS CHECK, FLIGHT TO TEST THE GEAR, THE GEAR FAILED TO EXTEND, 2 AMP CIRCUIT BREAKER TRIPS AT HANDLE, PUMPED GEAR DOWN MANUALLY. O - [SDR GLBA2013072500280](https://openairdocs.org/sdr/GLBA2013072500280), Jul 24, 2013: RELAY. FAILED. DURING CRUISE, LOWERED LANDING GEAR HANDLE, HEARD NOTHING, INTRANSIT LIGHT WAS ON THEN WENT OUT AFTER 60 SECONDS, NOTICED LANDING GEAR HANDLE CIRCUIT BREAKER TR - [SDR GLBA2013060400256](https://openairdocs.org/sdr/GLBA2013060400256), Jun 4, 2013: GEARBOX. FAILED. DURING CLIMBOUT EXPERIENCED SMOKE IN THE CABIN, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE, FLAPS DID NOT EXTEND, SMOKE DISSAPATED AFTER FIVE MINUTES. R & - [SDR GLBA2013012100159](https://openairdocs.org/sdr/GLBA2013012100159), Jan 18, 2013: BULB. INOPERATIVE. PILOT REPORTED THAT THE CAPT'S SIDE EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED LIGHT BULBS, OPS CHECKED GOOD. - [SDR GLBA2012121000131](https://openairdocs.org/sdr/GLBA2012121000131), Dec 7, 2012: BULB. INOPERATIVE. PILOT REPORTED THAT THE INSTRUMENT EMERGENCY LIGHT IS INOPERATIVE. MX REPLACED THE BULB, OPS CHECKED GOOD. - [SDR GLBA2012092400067](https://openairdocs.org/sdr/GLBA2012092400067), Sep 24, 2012: ANGLE. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION FOUND TWO CRACKS ON THE LT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH, AND - [SDR GLBA2012092400066](https://openairdocs.org/sdr/GLBA2012092400066), Sep 24, 2012: SPAR CAP. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND CRACK ON THE RT FWD SPAR CAP ANGLE ON THE VERTICAL STAB COMING DOWN TO THE FIRST FASTENER, .375" IN LENGTH. REPAIRE - [SDR GLBA2012082400039](https://openairdocs.org/sdr/GLBA2012082400039), Aug 23, 2012: BULB. INOPERATIVE. PILOT REPORTED THAT THE F/O EMERGENCY LIGHT BULB IS INOPERATIVE. MX REPLACED BULB, OPS CHECKED GOOD. - [SDR GLBA2012042701](https://openairdocs.org/sdr/GLBA2012042701), Apr 27, 2012: BULKHEAD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FWD PRESSURE BULKHEAD ALONG THE OTBD ROW OF FASTENERS NEXT TO THE RT NOSE GEAR WEB AT FS 84.00, . - [SDR GLBA2012042605](https://openairdocs.org/sdr/GLBA2012042605), Apr 25, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 150 AND STRINGER 9AL, AT NUTPLATE FOR A/S DOOR STRUT LWR MOUNT, .75" IN LENGTH. REPAIRED - [SDR GLBA2012042604](https://openairdocs.org/sdr/GLBA2012042604), Apr 25, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK IN THE FRAME AT FS 164 AND STRINGER 9AR AT CUTOUT, .35" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED - [SDR GLBA2012042603](https://openairdocs.org/sdr/GLBA2012042603), Apr 25, 2012: FRAME. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS IN THE FUSELAGE FRAME AT FS 509 AND AFT GAS STRUT MOUNT AREA FROM CENTER OF THE UPPER INBD GAS STRUT NUT - [SDR GLBA2012042602](https://openairdocs.org/sdr/GLBA2012042602), Apr 25, 2012: BULKHEAD. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE FWD PRESSURE BULKHEAD ALONG ROW OR FASTENERS NEXT TO THE LT NOSE GEAR WEB, FS 84.00, 7.25" IN LENGTH - [SDR GLBA2012022801](https://openairdocs.org/sdr/GLBA2012022801), Feb 28, 2012: SPAR. CRACKED. DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE HORIZONTAL FWD SPAR WEB JUST INBD OF RT HSS 00.0, APPROX .5" IN LENGTH. REPAIRED THE AFFECTED AREA A - [SDR GLBA20111116G](https://openairdocs.org/sdr/GLBA20111116G), Nov 15, 2011: UPLOCK SWITCH. INOPERATIVE. WITH THE AUTOFEATHER SWITCH OFF, AUTOFEATHER OFF ANNUNCIATOR AND MAST CAUTION ANNUNCIATOR DO NOT ILLUMINATE. MX REPLACED THE LT UPLOCK SWITCH IAW EO 11-1900-32- - [SDR GLBA20111020G](https://openairdocs.org/sdr/GLBA20111020G), Oct 19, 2011: PROPELLER. MALFUNCTIONED. PILOT REPORTED THAT THE LT PROP WON'T MANUALLY FEATHER. MX INSPECTED THE LINKAGE AND RAN ENG, NO DEFECTS NOTED. - [SDR GLBA201110181](https://openairdocs.org/sdr/GLBA201110181), Oct 18, 2011: BULB. BURNED OUT. EMERGENCY LIGHT UNDER GLARESHIELD ON CAPT SIDE INOPERATIVE FOUND DURING PREFLIGHT INSPECTION BY CREW. MX DETERMINED BULB WAS BURNED OUT AND REPLACED THE BULB. - [SDR GLBA20111017J](https://openairdocs.org/sdr/GLBA20111017J), Oct 14, 2011: HANDLE. OUT OF POSITION. PILOT REPORTED THAT THE EMERGENCY HANDLE AT 6C IS PUSHED IN. MX RESEATED THE EMERGENCY DOOR IAW BMM 52-20-01, OK FOR SERVICE. - [SDR GLBA20110929G](https://openairdocs.org/sdr/GLBA20110929G), Sep 28, 2011: LINE. LEAKING. PILOT REPORTED THAT THERE IS A POSSIBLE FUEL LEAK ON THE RT ENGINE NACELLE INSIDE THE WHEEL WELL. MX REPLACED THE FUEL DRAIN LINES, LEAK CHECKED GOOD. - [SDR GLBA20110926F](https://openairdocs.org/sdr/GLBA20110926F), Sep 25, 2011: HANDLE. DAMAGED. PILOT REPORTED THAT THE EMERGENCY EXIT DOOR AT 6C HANDLE SEEMS TO BE DEPRESSED. MX REINSTALLED THE DOOR IAW BMM 52-26-00, SYS OK FOR SERVICE. - [SDR GLBA20110908F](https://openairdocs.org/sdr/GLBA20110908F), Sep 7, 2011: HANDLE. UNSECURE. PILOT REPORTED THAT THE RT SIDE EMERGENCY DOOR HANDLE LOOKS NOT SECURED. MX RESECURED THE EMERGENCY EXIT DOOR REF 52-20-00. - [SDR GLBA20110805F](https://openairdocs.org/sdr/GLBA20110805F), Aug 5, 2011: SKIN. DENTED. DURING A SCHEDULED ROUTINE INSP MX FOUND A DENT IN THE RT WING L/E AT WS 167.24 MEASURING 7" WIDE, 3" HIGH, .5" DEEP. REPAIRED THE AFFECTED AREA AND PERFORMED A - [SDR GLBA20110613G](https://openairdocs.org/sdr/GLBA20110613G), Jun 12, 2011: WIRE. CHAFED. PILOT REPORTED THAT WHEN GEAR WAS SELECT UP, GEAR FAILED TO RETRACT, LANDING GEAR CB TRIPPED, RETURNED TO DEPARTURE. MX RESECURED A LOOSE PCB AND REPAIRED A CHA - [SDR GLBA20101027G](https://openairdocs.org/sdr/GLBA20101027G), Oct 27, 2010: FRAME. CRACKED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND A .5" CRACK IN THE LT HEAVY ANGLE IN THE BEND RADIUS AT FS 303.25. MX REPAIRED THE AFFECTED AREA AND PE - [SDR GLBA20101027F](https://openairdocs.org/sdr/GLBA20101027F), Oct 27, 2010: SKIN. DEBONDED. MAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND THE AIRSTAIR DOOR DEBONDED AT THE HINDGE ATTACH AREA AND OUTER SKIN DEBONDED 3.5" TO 4" INWARD FROM EDG - [SDR GLBA20100329G](https://openairdocs.org/sdr/GLBA20100329G), Mar 28, 2010: CIRCUIT BOARD. DETERIORATED. SUSPECTED AUTOFEATHER - PILOTS REPORTED THAT THE NR 2 ENGINE AUTOFEATHER WAS CYCLING DURING FINAL APPROACH. MX R & R THE HIGH AND LOW PRESSURE SWITCHES IAW BMM All 81: https://openairdocs.org/aircraft/N184UX/reports.md ## Related - Other Beech 1900D aircraft: https://openairdocs.org/model/beech-1900d/aircraft.md - STCs for the Beech 1900D: https://openairdocs.org/model/beech-1900d/stcs.md - The Pratt & Whitney PT6A series engine: https://openairdocs.org/engine/pratt-whitney-pt6a-series.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.