Beech 1900D

Service difficulty reports · 7,152

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duckdb -csv -c "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 = '1900D'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR GLBA2014100800449Bulkhead · buckledDURING A SCHEDULED INSPECTION FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO STRINGER 11L. PREVIOUS REPAIR DOUBLER BETWEEN STRINGER 11L & 13L BUCKLED. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-Oct 8, 2014 · N231YV · Beech 1900D · Fuselage Main, BulkheadSDR 29GA2014101300001Governor · malfunctionedON SHORT FINAL NR 2 ENGINE AUTOFEATHERED MULTIPLE TIMES, AND CAME BACK TO NORMAL OPERATING. REPLACED OVERSPEED GOVERNOR OPS AND LEAK CHECK GOOD.Oct 8, 2014 · N81535 · Beech 1900D · Propeller GovernorSDR GLBA2014100700448Frame · crackedDURING A SCHEDULED INSPECTION FOUND 2 CRACKS IN THE FUSELAGE FRAME AT FS 183.25 AT 2 LOCATIONS. 1ST AT INBD CORNER AREA AT ENVIRONMENTAL DUCT CUT OUT, ONE CRACK IS FROM CUT OUT ALL THE WAY THROUGH THE BEND RADIUS TO THE EDGE FRAME. SECOND IS FROM FASTENER INOct 7, 2014 · N231YV · Beech 1900D · Fuselage Main, FrameSDR 29GA2014100600001Pressure Switch · intermittentDURING SHORT FINAL, NR 2 PROPELLER AUTOFEATHERED. REPLACED LT HIGH PRESSURE AUTOFEATHER SWITCH. OPS CHECKED GOOD.Oct 6, 2014 · N81535 · Beech 1900D · Propeller GovernorSDR CA141014004Rib · corroded(CAN) CORROSION FOUND ON LOWER RIB FLANGE JUST FORWARD OF SPAR @ LWS 124.25. RECTIFICATION: REPAIR CARRIED OUT IAW CAS ENGINEERING A-RA14-031/D ISSUE NO. 1 APPROVED SEPT 25/14 (EA#B1900-57-001). CORROSION DAMAGE REMOVED FROM RIB FLANGE (0.270Ï¿½ X 2.4Ï¿½). REOct 5, 2014 · Beech 1900D · Wing, Rib/BulkheadSDR CA141007005Grounding Strap · damaged(CAN) REQUESTED AN IMMEDIATE DESCENT AND WAS CLEARED TO 3000` FROM 17000`. PILOT REPORTED THAT THE ACFT WAS HAVING AN ELECTRICAL ISSUE WITH RADIOS AND THERE WAS A FAINT ODOR OF SMOKE IN COCKPIT. PILOT DID NOT DECLARE AN EMERGENCY AND INDICATED THAT THE PROBLOct 5, 2014 · Beech 1900D · Communications System WiringSDR CA141014008Skin · corroded(CAN) FINDING: BELLY SKIN CORROSION AT STA 258 BETWEEN STRINGERS 15L AND 16L. REPAIRED IAW SRM 51-70-06 METHOD A. DAMAGED SKIN REMOVED. INNER DOUBLER MADEWITH SKIN FILLER. ALL WET ASSEMBLY WITH PR1422 USING ALL MS20470AD4 SOLID RIVETS. ALL AFFECTED AREAS PREPSep 29, 2014 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA2014100100001Switch · out of adjustRIGHT ENGINE AUTOFEATHERED ON SHORT FINAL WITH THE POWER AT IDLE. ADJUSTED PEDESTAL ARMING SWITCHES.Sep 29, 2014 · N81535 · Beech 1900D · Propeller Feathering/ReversingSDR GLBA2014092600446Skin · damagedDURING A SCHEDULED INSPECTION FOUND A LIGHTNING STRIKE ON THE OTBD TE LT ELEVATOR JUST OTBD OF THE MOST OTBD STATIC WICK. SKIN HAS .5 INCH X .25 INCH DAMAGE STARTING INBD OF THE FIBERGLASS END CAP & TRAVELING OUTWARD UNDER THE END CAP, DAMAGING THE END CAP. Sep 26, 2014 · N231YV · Beech 1900D · Elevator, Plate/SkinSDR 29GA2014092400001Pressure Switch · intermittentRIGHT ENGINE WENT INTO AUTOFEATHER FOUR TIMES ON SHORT FINAL, 200 FEET AGL. REPLACED RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH, OPS AND LEAK CHECKED GOOD.Sep 24, 2014 · N81535 · Beech 1900D · Propeller Feathering/ReversingSDR 29GA2014092500001Pressure Switch · intermittentRT ENGINE WENT INTO AUTOFEATHER FOUR TIMES ON SHORT FINAL, 200 FEET AGL. REPLACED RT ENGINE AUTOFEATHER LOW PRESSURE SWITCH OPS AND LEAK CHECKED GOOD.Sep 24, 2014 · N81535 · Beech 1900D · Propeller Controlling SystemSDR GLBA2014092200444Skin · dentedMAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND DENT IN THE VERT STAB LE, DENT AREA BEGINS AT CSS 54.026, JUST ABOVE RIB UPWARD TO CSS 66.00, DEPTH APPROX .5 INCHES TO .75 INCHES, ALLOWING FOR ORIGINAL CONTOUR AT LE. REPAIRED THE AFFECTED AREA & Sep 22, 2014 · N165YV · Beech 1900D · Vertical Stabilizer, Plate/SkinSDR GLBA2014092200445Structure · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FWD VERT STAB HAT SECTION AT FWD FLANGE BEND RADIUS, .20% CHORD & VSS 90.0, 1 INCH IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-55-009. MATERIASep 22, 2014 · N165YV · Beech 1900D · Vertical Stabilizer Miscellaneous StructureSDR GLBA2014091900443Skin · corrodedDURING A SCHEDULED INSPECTION FOUND SKIN CORROSION & BULGING, 6 INCH AREA, RUNNING LATERALLY ALONG FORMER RING UNDER CARGO BAY AREA AT APPROX FS 497.00 & APPROX WL 76.00 RUNNING APPROX RBL 9.00 TO RBL 15.00. THE CORROSION & BULGING SKIN HAS CAUSED A .5 INCH Sep 18, 2014 · N255GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014091900442Rib · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT WING INBD RIB AT JUNCTION WITH WING SPAR FS 288, RIB ANGLE DOUBLER CRACKED 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-190Sep 18, 2014 · N165YV · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014091900440Frame · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE FUSELAGE FRAME CHANNEL AT FS 177.35 & STRINGER 13L IN THE FRAME FLANGE BEND RADIUS, .7 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 1Sep 17, 2014 · N165YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2014091900441Frame · crackedMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND A CRACK IN THE RT FUSELAGE FRAME AT FS 177.35 & STRINGER 9AR RADIATING UPWARD FROM STRINGER 9AR CUT OUT, .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IASep 17, 2014 · N165YV · Beech 1900D · Fuselage Main, FrameSDR GLBA2014091900439Stringer · bentMAJOR REPAIR - DURING A SCHEDULED INSPECTION MAINTENANCE FOUND STRINGER 11L BENT APPROX 2 INCHES IN LENGTH BETWEEN FS 513.50 & FS 523.50. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-034. MATERIALS UTILIZED ARE INCLUDSep 17, 2014 · N201GL · Beech 1900D · Fuselage Main, Longeron/StringerSDR GLBA2014091600438Skin · crackedDURING A SCHEDULED INSPECTION FOUND A 7/8 INCH LONGITUDINAL CRACK ON THE UPPER FUSELAGE AT APPROX FUSELAGE STATION 214.25 ON FUSELAGE SKIN 27 APPROX 2 INCHES RIGHT OF UPPER CTR LINE & APPROX 2 INCHES LEFT OF COMM 1 ANTENNA IN LINE WITH THE LE OF THE ANTENNA BASep 16, 2014 · N245GL · Beech 1900D · Fuselage Main, Plate/SkinSDR CA140918007Cable · frayed(CAN) DURING 200 HOUR DOOR CABLE PULLEY INSPECTION, THE UPPER AFT. DOOR CABLE WAS FOUND FRAYED. CABLE P/N: 129-215059-13 WAS REPLACED WITH A SERVICEABLE CABLE. IT SHOULD BE NOTED THAT THIS IS A REOCCURING INSPECTION WITH INTERVIALS OF 200 HRS. FURTHER THE CABLSep 11, 2014 · Beech 1900D · Passenger/Crew DoorsSDR GLBA2014091100437Skin · damagedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND A LIGHTNING STRIKE ON THE OTBD RT ELEVATOR TE JUST OTBD OF THE OTBD MOST STATIC WICK CAUSING DAMAGE TO THE FIBERGLASS TIP, THE ADJACENT SHEET METAL & AN EXISTING PATCH. THERE ARE .060 INCH DIAMETER & .225 INCH DSep 11, 2014 · N154GL · Beech 1900D · Elevator, Plate/SkinSDR 29GA2014091100001Landing Gear · malfunctionedNOSE GEAR WOULD NOT RETRACT AFTER TAKEOFF. PERFORMED LANDING GEAR OPS CHECKS, COULD NOT DUPLICATE.Sep 10, 2014 · N87557 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR V0DR20140908002Wheel · crackedRECEIVED VENT BLOWER IN FOR OVERHAUL. THE TECHNICIAN WAS REASSEMBLING THE VENT BLOWER, AFTER GETTING THE BLOWER ASSEMBLY TOGETHER HE PREPARED THE VENT BLOWER TO RUN IN THE BRUSHES. NOTED THAT WITH POWER APPLIED TO THE VENT BLOWER A NOISE, FAINT, WAS HEARD UPSep 8, 2014 · N165YV · Beech 1900D · Air Distribution FanSDR V0DR20140908001O-Ring · deterioratedCUSTOMER REPORTED POSSIBLE OIL COMING FROM PROPELLER HUB & BLADE SOCKETS. RECEIVED PROPELLER ASSEMBLY IN, PRIOR TO DISASSEMBLY TECHNICIANS APPLIED PRESS FOR TROUBLESHOOTING PURPOSES, BUT NO DROP IN AIR PRESS WAS NOTED. THE TECHNICIANS PROCEEDED TO DISASSEMBLSep 8, 2014 · N165YV · Beech 1900D · Propeller Hub SectionSDR ERAA20140054Unknown · smokePAX REPORTED COLD AIR COMING FROM VENTS. AFTER LANDING 2 PAXS SITTING BEHIND THE EXIT ROWS REPORTED SMOKE COMING FROM THE LOWER VENTS. PAX DID NOT REPORT SMOKE TILL AFTER DEPLANED. GND RUN BOTH ENGS, BLEED AIR & CABIN TEMP CONTROL. OPERATIONS CHECKED GOOD,Sep 6, 2014 · N971EA · Beech 1900D · Air Distribution SystemSDR GLBA2014090200436Skin · crackedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION IN AN AREA OF 4.5 INCHES BY 3.5 INCHES CAUSING A CRACK & BUILDING SKIN & A SHEARED RIVET BEHIND THE LT VORTEX GENERATOR & IN FRONT OF THE FORMER RING CENTERED AT FS 243.25 & WL 85.40. REPAIRED IAW EO 1Sep 2, 2014 · N240GL · Beech 1900D · Wing, Plate/SkinSDR CA140908016Inverter · failed(CAN) ACFT DEPARTED AND A FEW MINUTES INTO THE FLIGHT REQUESTED TO RETURN TO THE AIRPORT DUE TO AN AC BUS FAILURE, RESULTING IN SOME INSTRUMENT FAILURES. NO EMERGENCY OR ASSISTANCE REQUIRED AND THE ACFT LANDED WITHOUT INCIDENT. AFTER THE ACFT LANDED MAINTENAAug 30, 2014 · Beech 1900D · AC InverterSDR GLBA2014082900435Skin · damagedDURING A SCHEDULED INSPECTION MAINTENANCE, FOUND WING SKIN BENT UPWARDS ON TRAILING EDGE BETWEEN WS 114.25 & 124.25. REPAIRED IAW EO 14-1900-57-006.Aug 29, 2014 · N231YV · Beech 1900D · Wing, Plate/SkinSDR GLBA2014082900434Frame · corrodedDURING A SCHEDULED INSPECTION MAINTENANCE FOUND CORROSION ON THE FUSELAGE FRAME AT FS 198.25 BETWEEN STRINGERS 15L & 14L, UPPER SURFACE, AREA CORRODED 2.25 INCHES BY .75 INCHES. DEEPEST PITTED AREA IS APPROX .03 INCHES ALONG LE, DEEP PITTED SPOT TOWARD STRINGAug 29, 2014 · N202UX · Beech 1900D · Fuselage Main, FrameSDR GLBA2014082500432Rib · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE RT WING INBD RIB AT BL 29 & WING SPAR, RIB FLANGE CRACKED AT JUNCTION WITH WING SPAR, APPROX 1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-57-005. MAAug 25, 2014 · N202UX · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014082600433Repair · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE LT HEAVY CLOSING ANGLE REPAIR AT FS 288.00, IN THE BEND RADIUS OF THE REPAIR ANGLE, .65 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-030. MATERIALSAug 25, 2014 · N202UX · Beech 1900D · Fuselage Miscellaneous StructureSDR GLBA2014082500431Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FLANGE RADIUS ON THE FRAME AT FS 451 & STRINGER 10R .5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-029. MATERIALS UTILIZED ARE INCLUDED IN THE ENGAug 25, 2014 · N202UX · Beech 1900D · Fuselage Main, FrameSDR CA140908015Acm · failed(CAN) ON START UP THE CREW NOTICED SMOKE IN THE COCKPIT & CABIN. AFTER SOME TROUBLESHOOTING THE CREW SELECTED THE LT & RT ENVIRO SWITCHES TO THE OFF POSITION & THE SMOKE DISSIPATED. THE ACFT WAS INSPECTED & DISPATCHED UNDER THE COMPANY`S MEL PROTOCOL REQUIREAug 15, 2014 · Beech 1900D · Cabin Cooling SystemSDR CA140819003Acm · smoke(CAN) THE CREW OF THE B1900D ON TAKE-OFF ROLL REJECTED THE TAKE-OFF DUE TO SMOKE IN THE COCKPIT & CABIN. THE CREW WAS ABLE TO TAXI BACK TO THE GATE AND DEPLANE WITHOUT FURTHER INCIDENT. AFTER THE PASSENGERS WERE DISEMBARKED THE AIRCRAFT WAS ASSESSED BY ESSENTAug 15, 2014 · Beech 1900D · Cabin Cooling SystemSDR GLBA2014081800429Engine · failedPILOT 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 & DIVERTED. REMOVED AND REPLACED THE ENGINE R & R RT ENG ASSEMBLY IAW TC 1900-7100.00 REV 8. OPAug 15, 2014 · N184UX · Beech 1900D · Engine (Turbine/Turboprop)SDR CA140815003Actuator · malfunctioned(CAN) DURING A LEFT HAND END CAP INSPECTION PER MANUFACTURER`S INSTRUCTIONS IAW MM CHAPTERS 05-10-00-201 SECTION J & 32-30-10-201 SECTION D (ENCOMPASSING AD2009-23-01 & SB3870) IT WAS DISCOVERED THAT THE END CAP ON THE ACTUATOR, MAIN GEAR EXHIBITED A REPEATABLAug 14, 2014 · Beech 1900D · Landing Gear ActuatorSDR 29GA2014082600002Skin · crackedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED LT BELLY SKIN CRACKED 0.25 INCHES NEAR WING ROOT, BS 258, STRINGER 15L. REMOVED CRACK AND INSTALL EXTERNAL DOUBLER.Aug 14, 2014 · N87557 · Beech 1900D · Fuselage Main, Plate/SkinSDR 29GA2014082500001Skin · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED LT FORWARD CENTER UNDERBELLY WING ROOT CRACKED 1 INCH BS 258, STRINGER 15L. REPAIRED FUSELAGE SKIN. REMOVED CRACK AND INSTALL EXTERNAL DOUBLER.Aug 14, 2014 · N81535 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014081400428Skin · damagedDURING A SCHEDULED INSPECTION FOUND A .05 INCH HOLE IN THE BELLY SKIN NEAR THE ADF ANTENNA AT APPROX FS 219. REPAIRED THE AFFECTED AREA & PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-028. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.Aug 13, 2014 · N220GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA2014081200427Turnbuckle · out of adjustRIGHT FWD EMER EXIT HANDLE STICKING OUT. ADJUSTED THE DOOR LATCH TURNBUCKLE IAW MM 52-20-00. OPERATIONS CHECKED GOOD.Aug 11, 2014 · N240GL · Beech 1900D · Emergency ExitsSDR CA140814001Control System · malfunctioned(CAN) A BEECH 1900D ON APPROACH WAS STRUCK BY LIGHTENING. THE AIRCRAFT LANDED WITHOUT INCIDENT. UPON INSPECTION BY THE FLIGHT CREW IT WAS REPORTED TO MAINTENANCE THERE WAS EVIDENCE OF DISCHARGE THROUGH THE LT ELEVATOR, LT STRAKE AND RIVETS ON THE FUSELAGE. MAIAug 8, 2014 · Beech 1900D · Elevator Control SystemSDR CA140808006Blower · burned(CAN) SMOKE WAS NOTICED IN THE CABIN. CREW DECLARED AND EMERGENCY AND RETURNED TO THE AIRPORT. FWD CABIN VENT BLOWER WAS FOUND BURNED ON THE LOW SPEED MODE CIRCUITRY. VENT BLOWER WAS REPLACED AND SYSTEM TESTED SERVICEABLE.Aug 7, 2014 · Beech 1900D · Air Distribution FanSDR 29GA2014081600002Spar Cap · crackedDURING SCHEDULED MAINTENANCE, DISCOVERED VERTICAL STABILIZER FORWARD LT SPAR CAP ANGLE CRACKED. REMOVED CRACKED SPAR CAP ANGLES AND INSTALLED NEW REPAIR SPAR CAP ANGLES WITH SPLICE ANGLES.Aug 6, 2014 · N81535 · Beech 1900D · Vertical Stabilizer, Spar/RibSDR GLBA2014080500426Rib · crackedDURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE RT INBD RIB LOWER CAP ON THE JOGGLE JUST FWD OF THE WING SPAR, 0.625 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-57-004. MAJOR REPAIR.Aug 5, 2014 · N192GL · Beech 1900D · Wing, Rib/BulkheadSDR GLBA2014073100425Frame · crackedDURING A SCHEDULED INSPECTION FOUND A CRACK IN THE FUSELAGE FRAME AT BS 183.25, BETWEEN STRINGERS 2 & 3R. CRACK RADIATES DOWNWARD FROM FASTENER, .2 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-027. MAJOR REPAIR .Jul 31, 2014 · N192GL · Beech 1900D · Fuselage Main, FrameSDR CA140729001Diode · arced(CAN) PILOT`S EADI INTERMITTENT, TROUBLESHOOTING CARRIED OUT BY MAINTENANCE WHICH DETERMINED DIODE CR41 IN NOSE JUNCTION BOX BURNED AND ARCHING. DIODE REPLACED, SYSTEM CHECKED SERVICEABLE. REF WIRING INTERFACE-JUNCTION BOX DWG 129-340016 SHEET 5.Jul 25, 2014 · Beech 1900D · Navigation System WiringSDR CA140728022Shaft · cracked(CAN) DURING AN A, B, C STRUCTURAL INSPECTION CHECK MAINTENANCE NOTICED THAT THE LT INBD FLAP ACTUATOR SHAFT ASSY PN 101-380000-1 WAS PULLED AWAY FROM THE "B" NUT SECURING IT TO THE FLAP GEARBOX. THE SHAFT ASSLY WAS R & R WITH A NEW UNIT. THE SYS WAS FUNCTIOJul 25, 2014 · Beech 1900D · Trailing Edge Flap Control SystemSDR CA140728020Wire · damaged(CAN) DURING AN A,B,C STRUCTURAL INSPECTION CHECK MAINTENANCE NOTICED A SINGLE WIRE FROM AN ADJACENT WIRE BUNDLE WAS WRAPPED AROUND THE REVERSE LINKAGE FOR THE PROPELLER CONTROL. THE WIRE WAS FURTHER INSPECTED AND FOUND CHAFED. THE WIRE WAS REPAIRED AND RE-SECJul 25, 2014 · Beech 1900D · Engine Control System WiringSDR CA140804006Engine · surges(CAN) WHILE IN CRUISE THE RT ENGINE WAS SURGING WITH TQ AND NP FLUCTUATING AND ACFT YAW. ITT STARTED TO RISE AND CREW SECURED THE ENGINE WHEN ITT REACHED 850 DEGREES. CUSTOMER REPORTED A CT DISK AND STATOR REPLACED 50 HOURS PRIOR THIS EVENT AND THAT GRINDING Jul 24, 2014 · Beech 1900D · Engine (Turbine/Turboprop)SDR 29GA2014081600003Spar · crackedDURING SCHEDULED ROUTINE MAINTENANCE, DISCOVERED HORIZONTAL STABILIZER FWD MAIN SPAR WEB CRACKED AREA OF DE-ICE TUBING HOLE. INSTALLED SPLICE REPAIR AND INSTALLED REPAIR ANGLES.Jul 24, 2014 · N87557 · Beech 1900D · Horizontal Stabilizer, Spar/Rib
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