# Service difficulty reports: Beech 1900

A list on [Beech 1900](https://openairdocs.org/model/beech-1900.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 87 reports

- [SDR JIKA2024052901](https://openairdocs.org/sdr/JIKA2024052901.md): Hydraulic Line · chafed · May 24, 2024 · N330AF · Beech 1900 · Hydraulic System, Main
  > 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. THE FLIGHT CREW THEN EXTENDED THE LANDING GEAR THROUGH MANUAL EXTENSION AND LANDED THE AIRCRAFT SA
- [SDR JIKA2024021601](https://openairdocs.org/sdr/JIKA2024021601.md): Wire Harness · shorted · Feb 13, 2024 · N3052K · Beech 1900 · Landing Gear System Wiring
  > 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 EXTINGUISH. THE PILOT RESET THE CIRCUIT BREAKER AND CYCLED THE LANDING GEAR HANDLE ONCE MORE, BUT TH
- [SDR JIKA2019101701](https://openairdocs.org/sdr/JIKA2019101701.md): Packing · leaking · Oct 15, 2019 · N718AF · Beech 1900 · Turbine Engine Oil System
  > APPROXIMATELY 1HR INTO FLIGHT, RIGHT ENGINE OIL PRESSURE DROPPED TO 40PSI ACCOMPANIED WITH LOW OIL PRESSURE WARNING ANNUNCIATOR LIGHT. CREW COMPLIED WITH CHECKLIST ACTION TO SECURE THE RIGHT ENGINE. THE FLIGHT WAS CONTINUED TO DESTINATION WITH SINGLE ENGINE A
- [SDR JIKA2018100201](https://openairdocs.org/sdr/JIKA2018100201.md): Unknown · smoke · Oct 2, 2018 · N3052K · Beech 1900 · Air Distribution System
  > 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 ENVIRONMENTAL BLEED AIR HAD BEEN TURNED ON AND THERE WAS NO SMELL ASSOCIATED WITH THE SMOKE OR VAPOR OB
- [SDR JIKA2018100192701](https://openairdocs.org/sdr/JIKA2018100192701.md): Circuit Breaker · defective · Oct 1, 2018 · N112Y · Beech 1900 · Landing Gear Retraction/Extension System
  > 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 ELECTED TO MANUALLY EXTEND THE GEAR AND THE THREE GREEN GEAR INDICATORS ILLUMINATED. THE AIRCRAFT LAND
- [SDR JIKA2018060453002](https://openairdocs.org/sdr/JIKA2018060453002.md): Filter · contaminated · May 30, 2018 · N330AF · Beech 1900 · Aircraft Fuel Distribution System
  > 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 FAIL INDICATION EXTINGUISHED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINTENANC
- [SDR JIKA201806043001](https://openairdocs.org/sdr/JIKA201806043001.md): Filter · contaminated · May 30, 2018 · N330AF · Beech 1900 · Aircraft Fuel Distribution System
  > 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 FAILED INDICATION EXTINGUISHED. THE PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINTEN
- [SDR JIKA2018032301](https://openairdocs.org/sdr/JIKA2018032301.md): Unknown · smoke · Mar 23, 2018 · N330AF · Beech 1900 · Air Distribution System
  > 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 TO THE OFF POSITION AND REPORTED THE SMOKE DISSIPATED. LANDED WITHOUT INCIDENT. NO EMERGENCY WAS D
- [SDR JIKA2016052301](https://openairdocs.org/sdr/JIKA2016052301.md): Fuel Cell · leaking · May 23, 2016 · N330AF · Beech 1900 · Fuel Storage
  > 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. INSPECTED THE ACFT, THE INSPECTION INCLUDED REMOVING THE CABIN FLOORBOARDS & INSPECTING FOR ANY SI
- [SDR JIKA201512081501](https://openairdocs.org/sdr/JIKA201512081501.md): Fuel Control · low pressure · Dec 3, 2015 · N3052K · Beech 1900 · Fuel Control/Turbine Engines
  > 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 RT ENG BEGAN TO SURGE. THE PILOT PERFORMED A PRECAUTIONARY IN FLIGHT SHUTDOWN OF THE RT ENG. DE
- [SDR CA141103001](https://openairdocs.org/sdr/CA141103001.md): Engine · power loss · Oct 22, 2014 · Beech 1900 · Engine (Turbine/Turboprop)
  > (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 TO RESET THE GENERATOR BUT THE GENERATOR DID NOT COME BACK ONLINE. THE LH ENGINE OIL LOW ANNUNCIATO
- [SDR GLBA2013021500177](https://openairdocs.org/sdr/GLBA2013021500177.md): Bulb · inoperative · Feb 14, 2013 · N153GL · Beech 1900 · Emergency Lighting
  > 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 WIRING, OPS CHECKED GOOD.
- [SDR HSYA20110307001](https://openairdocs.org/sdr/HSYA20110307001.md): Torque Link · damaged · Mar 7, 2011 · N122G · Beech 1900 · Landing Gear Retraction/Extension System
  > 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 ATTACH POINT.
- [SDR GUUA94055030609D](https://openairdocs.org/sdr/GUUA94055030609D.md): Spar Cap · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Horizontal Stabilizer, Spar/Rib
  > 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.md): Hinge Bracket · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Elevator Miscellaneous Structure
  > 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.md): Hinge Bracket · corroded · Mar 6, 2009 · N16540 · Beech 1900 · Elevator Miscellaneous Structure
  > DURING SCHEDULED ROUTINE INSP DISCOVERED RT ELEVATOR CTR HINGE BRACKET EXFOLIATED. REPLACED RT ELEVATOR CENTER HINGE BRACKET.
- [SDR GUUA93352011609A](https://openairdocs.org/sdr/GUUA93352011609A.md): Door · stiff · Jan 16, 2009 · N81533 · Beech 1900 · Emergency Exits
  > 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.md): Cap · cracked · Nov 16, 2007 · Beech 1900 · Landing Gear Actuator
  > MLG ACTUATOR WAS RECEIVED DUE TO INDICATIONS FOUND IN THE END CAP DURING ULTRASONIC TESTING. ACTUATOR WENT THROUGH A PRELIMINARY INSPECTION AND A COMPLETE FUNCTIONAL TEST WITH NO EXTERNAL EVIDENCE OF LEAKING OR CRACKING. AFTER DISASSEMBLY, A CRACK IN THE INT
- [SDR TIM2005F00003](https://openairdocs.org/sdr/TIM2005F00003.md): Skin · corroded · Apr 4, 2005 · N127BA · Beech 1900 · Elevator, Plate/Skin
  > 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 PUSH ROD, RT ELEVATOR TRIM TAB HORN. (K)
- [SDR TIM2005F00002](https://openairdocs.org/sdr/TIM2005F00002.md): Skin · corroded · Apr 4, 2005 · N127BA · Beech 1900 · Fuselage Main, Plate/Skin
  > CORROSION FOUND ON SKIN FS243-FS273 AND STRINGERS 14L-15R. (K)
- [SDR HSY2005F00001](https://openairdocs.org/sdr/HSY2005F00001.md): Sensor · defective · Jan 14, 2005 · N7254R · Beech 1900 · Engine Oil Temperature
  > (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, INSPECTED, AND REINSTALLED. RAN ENGINE AND FOUND NO FURTHER DEFECTS. (NM05200502782) (K)
- [SDR TIM2004F00000](https://openairdocs.org/sdr/TIM2004F00000.md): Tube · pin hole · Sep 30, 2004 · N192GA · Beech 1900 · Hydraulic System, Main
  > 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 TEST, IT WAS DETERMINED THAT THE RETRACTION TUBE HAD A PIN HOLE IN IT. COULD NOT GUESS ON THE PROBABL
- [SDR GLBA2003072](https://openairdocs.org/sdr/GLBA2003072.md): Pressure Switch · malfunctioned · Jun 2, 2003 · N245UE · Beech 1900 · Cabin Cooling System
  > 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 RIGHT ENVIR TEMP AND PRESSURE, OPS CHECK GOOD.
- [SDR GLBA2003070](https://openairdocs.org/sdr/GLBA2003070.md): Filter · dirty · Jun 1, 2003 · N247UE · Beech 1900 · Cabin Pressure Control System
  > AIRCRAFT WILL NOT PRESSURIZE. CLEANED PRESSURE CONTROLLER FILTER, OPS CHECK GOOD.
- [SDR GLBA2003071](https://openairdocs.org/sdr/GLBA2003071.md): Switch · out of adjust · May 30, 2003 · N118UE · Beech 1900 · Trailing Edge Flap Control System
  > AIRCRAFT RETURNS, FLAPS WILL NOT RETRACT. ADJUSTED FLAP SAFETY SWITCH, OPS CK GOOD.
- [SDR TIM2002F00010](https://openairdocs.org/sdr/TIM2002F00010.md): Angle · broken · Feb 15, 2002 · N172GA · Beech 1900 · Nacelle/Pylon, Main Frame
  > 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, AND THIS CAUSES THE COWL SIDE SKIN TO CRACK.
- [SDR AUS20020164](https://openairdocs.org/sdr/AUS20020164.md): Light · failed · Jan 31, 2002 · Beech 1900 · Landing Gear Position and Warning
  > (AUS) RH MAIN LANDING GEAR POSITION LIGHT FAILED.
- [SDR TIM2002F00009](https://openairdocs.org/sdr/TIM2002F00009.md): Bolt · corroded · Jan 16, 2002 · N172GA · Beech 1900 · Nose/Tail Landing Gear Strut/Axle
  > 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 CORROSION.
- [SDR OYG2002F00000](https://openairdocs.org/sdr/OYG2002F00000.md): Cowling · cracked · Dec 5, 2001 · N199GA · Beech 1900 · Engine Cowling System
  > 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 THE HARMONICS OF THE VIBRATIONS FROM THE ENGINE AND PROPELLER. POSSIBLY GOING TO A THICKER GAUGE OF
- [SDR TIM2002F00004](https://openairdocs.org/sdr/TIM2002F00004.md): Cable · broken · Dec 4, 2001 · N172GA · Beech 1900 · Entrance Stairs
  > AIRSTAIR DOOR CABLE BROKE, ALLOWING ONE SIDE OF THE DOOR TO REMAIN UNLOCKED.
- [SDR 2003F00020](https://openairdocs.org/sdr/2003F00020.md): Angle · cracked · Nov 27, 2001 · N715GL · Beech 1900 · Nacelle/Pylon Miscellaneous Structure
  > GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. REPLACED THE LEFT ENGINE COWLING REINFORCEMENT ANGLE, THE ENGINE TRUSS BRACKET RECEPTACLE, AND THE UPPER AFT ANGLES. THE REPAIRS WERE COMPLETED 12-03-01 TAT 21, 140.9. (M)
- [SDR 2003F00019](https://openairdocs.org/sdr/2003F00019.md): Bracket · cracked · Nov 27, 2001 · N715GL · Beech 1900 · Nacelle/Pylon Miscellaneous Structure
  > GJT - LEFT ENGINE NACELLE LOWER AFT BULKHEAD HAS SEVERAL CRACKS. STRUCTURAL REPAIRS ARE IN PROGRESS. (M)
- [SDR TIM2001F00011](https://openairdocs.org/sdr/TIM2001F00011.md): Wire · broken · Oct 16, 2001 · N172GA · Beech 1900 · Ice/Rain Protection System Wiring
  > 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.md): Bulkhead · cracked · Oct 15, 2001 · Beech 1900 · Engine Cowling System
  > 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 THE FOUR BOLTS SECURE THE COWL TO THE BULKHEAD. PICTURES INCLUDED.
- [SDR 2001F00623](https://openairdocs.org/sdr/2001F00623.md): Shaft · defective · Oct 4, 2001 · N172GA · Beech 1900 · Trailing Edge Flap Control System
  > 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 ATTACHED TO THE FERRULE AS REQUIRED. (M)
- [SDR TIM2001F00006](https://openairdocs.org/sdr/TIM2001F00006.md): B-Nut · loose · May 22, 2001 · N172GA · Beech 1900 · Engine Oil Distribution (Airframe Furnished)
  > 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 PRESSURE PROCEDURE. NO DAMAGE FOUND - OIL SERVICED AND ENGINE TEST RUN PER P/W CHECK.
- [SDR GUU2001F00008](https://openairdocs.org/sdr/GUU2001F00008.md): Hinge Bracket · corroded · Apr 25, 2001 · N194GA · Beech 1900 · Elevator Structure
  > DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)
- [SDR GUU2001F00007](https://openairdocs.org/sdr/GUU2001F00007.md): Hinge Bracket · corroded · Apr 25, 2001 · N194GA · Beech 1900 · Elevator Structure
  > DURING SCHEDULED MAINTENANCE, RIGHT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS ON INTERGRANULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR CENTER HINGE BRACKET. (M)
- [SDR 2001F00089](https://openairdocs.org/sdr/2001F00089.md): Hinge Bracket · corroded · Apr 24, 2001 · N199GA · Beech 1900 · Horizontal Stabilizer Structure
  > DURING SCHEDULED MAINTENANCE, LEFT CENTER ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED LEFT ELEVATOR CENTER HINGE BRACKET. (M)
- [SDR 2001F00088](https://openairdocs.org/sdr/2001F00088.md): Hinge Bracket · corroded · Apr 24, 2001 · N199GA · Beech 1900 · Horizontal Stabilizer Structure
  > DURING SCHEDULED MAINTENANCE, RIGHT OUTBOARD ELEVATOR HINGE BRACKET MOUNTED ON THE STABILIZER SHOWED SIGNS OF INTERGRANNULAR CORROSION. REMOVED AND REPLACED RIGHT ELEVATOR OUTBOARD HINGE BRACKET. (M)
- [SDR ME42001F00000](https://openairdocs.org/sdr/ME42001F00000.md): Spring · broken · Mar 26, 2001 · N125BA · Beech 1900 · Propeller Assembly
  > 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 SPRING, PN A3496, IN THE SPRING KIT ASSEMBLY WAS NOTED BROKEN. TALKING WITH THE FLIGHT CREW, THEY S
- [SDR 20000925SH017](https://openairdocs.org/sdr/20000925SH017.md): Truss · cracked · Sep 5, 2000 · N7254R · Beech 1900 · Engine Mount Section
  > 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 NR 2255 R6. REMOVED AND REPLACED THE TRUSS ASSEMBLY. THE REPETATIVE INSPECTIONS REQUIRED BY A
- [SDR 20000725AP006](https://openairdocs.org/sdr/20000725AP006.md): Bracket · corroded · Apr 26, 2000 · N189GA · Beech 1900 · Elevator Structure
  > 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.md): Bulb · unserviceable · Feb 10, 2000 · N93ZV · Beech 1900 · Emergency Lighting
  > 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 DEFERRED PER MEL 3302 AND THE AIRCRAFT DEPARTED TO PHX. (M)
- [SDR 20000725AP004](https://openairdocs.org/sdr/20000725AP004.md): Truss · cracked · Jul 1, 1999 · N189GA · Beech 1900 · Engine Mount Section
  > 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.md): Switch · out of adjust · Jul 26, 1998 · N188GA · Beech 1900 · Trailing Flap Position Indicating System
  > 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.md): Lever · out of adjust · Jul 25, 1998 · N188GA · Beech 1900 · Trailing Edge Flap Control System
  > FLT 9483 - MIA-MCO - GEAR WARNING HORN SOUNDS WITH GEAR UP AND FLAPS MOVED INTO APPROACH. REPOSITIONED FLAP SELECTOR LEVER GUARD. OPERATIONAL CHECKS SATISFACTORY. (M)
- [SDR 98ZZZX2865](https://openairdocs.org/sdr/98ZZZX2865.md): Acm · malfunctioned · Jul 16, 1998 · N194GA · Beech 1900 · Cabin Cooling System
  > 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 DUPLICATE. (X)
- [SDR 98ZZZX2261](https://openairdocs.org/sdr/98ZZZX2261.md): Bearing · failed · Jun 4, 1998 · Beech 1900 · Engine RPM Indicating System
  > 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 FAILED. THESE BEARINGS HAVE NO IDENTIFYING MARKINGS ON THEM, ONLY ON THE SHIPPING TUBES IS THERE
- [SDR 98ZZZX2410](https://openairdocs.org/sdr/98ZZZX2410.md): Line · cracked · Jun 3, 1998 · N192GA · Beech 1900 · Hydraulic System, Main
  > EYW/MIA - FLT 5300 - LANDING GEAR DOES NOT RETRACT. REMOVED AND REPLACED RIGHT HAND 'UP' HYDRAULIC LINE. (X)

Next page: https://openairdocs.org/model/beech-1900/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE aircraft_model_key = '1900'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/beech-1900/reports

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