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"

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SDR GLBA201105131Unknown · odorTHE PILOT REPORTED THAT DURING DESCENT THEY SMELLED FUEL. MX CLEANED THE EPA CANNISTER AND CHECKED FUEL VALUES ON BOTH ENGINES, PERFORMED FCD 1900-08-30-01 STEPS 3&4, NO FURTHER DEFECTS NOTED.May 13, 2011 · N201GL · Beech 1900D · Air Distribution SystemSDR GUUA93853051211ASkin · crackedDURING SCHEDULED ROUTINE MX LOWER FUSELAGE BELLY SKIN HAS A SMALL CRACK AND SIGNS OF CORROSION BETWEEN FS 456.00 AND 482.75 AT STRINGER 14R. REMOVED DAMAGED AREA AND INSTALLED SKIN FILLER REPAIR AND EXTERNAL DOUBLER REPAIR.May 12, 2011 · N81538 · Beech 1900D · Fuselage Main, Plate/SkinSDR GUUA94232051111AUplock Switch · dirtyPILOT REPORTED WHEN LANDING GEAR SELECTED UP THE RED GEAR UNSAFE LIGHTS REMAIN ILLUMINATED. RAN QRH SELECTED GEAR DOWN AND GOT 3 GREEN LIGHTS EXECUTED A NORMAL LANDING. CLEANED NLG UPLOCK SWITCH, OPS CHECKS GOOD.May 11, 2011 · N47542 · Beech 1900D · Landing Gear Position and WarningSDR 2011FA0000297Fuel Sys · contaminatedFLIGHT CREW REPORTED RT FUEL INDICATOR BOUNCES 700-800 LBS IN FLIGHT. NORMAL TROUBLESHOOTING SHOWED SYS NORMAL. REMOVED CONNECTOR PLUGS TO FUEL CONTROL RELAY PANEL, UNDER CTR FLOOR, AND FOUND WATER IN ALL PLUGS. NO INDICATION OF WATER POOLING IN FLOOR AND ALL May 9, 2011 · N842E · Beech 1900D · Aircraft Fuel Distribution SystemSDR CA110516013Control System · out of rigPOWER ROLL BACK/IFSD DURING CLIMB, THE LT ENGINE NG ROLLED BACK TO 73 PERCENT WITH ASSOCIATED DECREASE IN FUEL FLOW. POWER LEVER ADVANCE HAD NO EFFECT AND THE ENGINE WAS SHUTDOWN AS A PRECAUTIONARY MEASURE. THE ACFT RETURNED TO THE POINT OF DEPARTURE WHERE ANMay 8, 2011 · Beech 1900D · Fuel Controlling SystemSDR GUUA95661050511AGovernor · failedNR 1 ENGINE PROP RPM HAD UNCOMMANDED DROP TO 1000 RPM IN FLIGHT SUSPECT PRIMARY GOVERNOR FAILURE. SHUTDOWN AND SECURED THE NR 1 ENGINE. LANDED WITHOUT INCIDENT. REPLACED NR 1 ENGINE PROPELLER PRIMARY GOVERNOR. OPS CHECK GOOD.May 5, 2011 · N81556 · Beech 1900D · Propeller GovernorSDR GLBA20110503FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND A CRACK IN CARGO DOOR FUSELAGE FWD FRAME AT F.S. 456, AT THE UPPER IB NUTPLATE AREA AT THE LONG GAS STRUT MOUNT, 1" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIMay 3, 2011 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GUUA95752050311AHandle · lack of lubeDURING SCHEDULED ROUTINE INSP DISCOVERED RT FWD EXIT OUTER HANDLE STIFF TO OPERATE. LUBED RT FWD EMERGENCY EXIT OUTER HANDLE.May 3, 2011 · N87557 · Beech 1900D · Emergency ExitsSDR GUUA95553050311BAngle · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSP DISCOVERED RT CLOSING ANGLE CRACKED 2.1 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous StructureSDR GUUA95553050311AAngle · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSP, DISCOVERED LT CLOSING ANGLE CRACKED 2.0 INCHES AT FS 288.0. STOP DRILLED CRACK AND INSTALLED 13.5 INCH REPAIR ANGLE.May 3, 2011 · N87555 · Beech 1900D · Fuselage Miscellaneous StructureSDR V0DR2011011Jam-Nut · bindingDURING INSP OF A AIRSTAIR DOOR STRUT THE TECH R & R (1) END CAP JAM NUT WITH A NEW 1 FROM STOCK. DURING ASSY THE TECH NOTED THAT THE END CAP JAM NUT WOULD NOT THREAD ONTO THE TUBE ASSY FREELY WITHOUT EXCESSIVE FORCE. DURING TROUBLE SHOOTING THE JAM NUT WAS RMay 3, 2011 · Beech 1900D · Passenger/Crew DoorsSDR V0DR2011010Slip Ring · deterioratedDURING SCHEDULED MX, A MECHANIC NOTED THAT DURING CLEANING OF THE PROP DEICE SLIP RING THAT THE DIELECTRIC FILLER IN BETWEEN COPPER RINGS APPEARED TO BE DETERIORATING. THE PROPELLER WAS REMOVED FROM SERVICE. THE PROP DEICE SLIP RING WAS R & R AND THE PROP REMay 3, 2011 · N245GL · Beech 1900D · Propeller Deice Boot SectionSDR GLBA20110502GKeel · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RH NACELLE OB KEEL CRACKED AT GRAVEL FENDER WEB AND THINNED ABOVE CRACK AT UPPER 2 RIVETS. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, KeelSDR GLBA20110502JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS, FRAME AT F.S. 273.25 AND STRINGER 10L AND IN T-FRAME AT SAME LOCATION, .7" AND .9" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IMay 2, 2011 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GLBA20110502FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND TWO CRACKS ON LT SIDE OF FUSELAGE UPWARD ALONG F.S. 273.25 AND STRINGER 10L, LENGTHWISE ALONG W.L. 93, 2.2" HIGH AND 4.2 WIDE IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMEDMay 2, 2011 · N211GL · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA201120110502HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED AT STRINGER CUTOUT, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53May 2, 2011 · N211GL · Beech 1900D · Fuselage Main, FrameSDR GUUA94057050211CStringer · corrodedDURING SCHEDULED X-RAY INSP DISCOVERED RT WING FWD LOWER BONDED J STRINGER HAS CORROSION BETWEEN WS 114.25 AND 124.25 . REMOVED CORROSION AND INSTALLED REPAIR STRAP.May 2, 2011 · N16540 · Beech 1900D · Wing, Longeron/StringerSDR GUUA94057050211DSpar · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED RIGHT WING LOWER MAIN SPAR AREA OF CORROSION BETWEEN WS 124.25 TO WS 135.86. BLENDED OUT CORROSION AND INSTALLED REPAIR STRAP.May 2, 2011 · N16540 · Beech 1900D · Wing SparSDR GUUA94057050211BSkin · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING FORWARD OF MAIN SPAR AREA OF CORROSION AT WS 124.25. REMOVED CORROSION FABRICATED AND INSTALLED EXTERNAL STRAP REPAIR.May 2, 2011 · N16540 · Beech 1900D · Wing, Plate/SkinSDR GUUA94057050211AStringer · corrodedDURING SCHEDULED X-RAY INSPECTION DISCOVERED LEFT WING LOWER BONDED SKIN FORWARD J STRINGER CORRODED TWO SPOTS BETWEEN WS 114.25 AND 124.25. REMOVED CORROSION FABRICATED AND INSTALLED INTERNAL STRAP REPAIR.May 2, 2011 · N16540 · Beech 1900D · Wing, Longeron/StringerSDR GUUA93632042811ARelay · shortedWHEN LANDING GEAR WAS SELECTED DOWN NO DOWN ANNUNCIATORS ILLUMINATED. RAN QRH AND EXTENDED LANDING GEAR MANUALLY. ALL GREEN ANNUNCIATORS ILLUMINATED EXCUTED SAFE LANDING. R & R LANDING GEAR RELAY.Apr 28, 2011 · N81536 · Beech 1900D · Landing Gear Retraction/Extension SystemSDR GLBA20110428FStructure · damagedMAJOR REPAIR - MX REPORT THAT DURING REFUELING, THE FUEL TRUCK STRUCK THE RT STABILON, THE RT STABILON WAS REPLACED ON 192GL. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-55-007. MATERIALS UTILIZED ARE INCLUDED IN THApr 27, 2011 · N192GL · Beech 1900D · Empennage StructureSDR GLBA20110420JFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE CARGO DOOR FUSELAGE FRAME AT FS 500 AND STRINGERS 4L & 5L CRACKED AT THE STRUT MOUNT UPPER IB NUTPLATE AREA, .65" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REApr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110420HFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT FS 456 AND STRINGER 3L & 4L AT THE GAS STRUCT MOUNT UPPER IB NUTPLATE AREA, .25" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMEDApr 19, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110420FSpar · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A CRACK RADIATING FROM THE DEICE TUBING HOLE IN THE HORIZONTAL STAB MAIN SPAR CENTER WEB, .3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IApr 19, 2011 · N182YV · Beech 1900D · Horizontal Stabilizer, Spar/RibSDR GLBA20110420GDoor Frame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE UPPER GARGO DOOR FUSELAGE FRAME AT FS 460 AND STRINGER 3L CRACKED 1.3" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53Apr 19, 2011 · N261GL · Beech 1900D · Fuselage Main, StructureSDR GLBA20110418FFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 9AR CRACKED .15" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-023. MATERApr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GLBA20110418GFrame · crackedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND THE RH FUSELAGE FRAME AT F.S. 456 AND STRINGER 10R CRACKED .2" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS I.A.W. EO 11-1900-53-025. MATERIApr 18, 2011 · N182YV · Beech 1900D · Fuselage Main, FrameSDR GUUA94053041711BDoor Frame · crackedDURING SCHEDULED ROUTINE STRUCTURAL INSPECTION DISCOVERED AIRSTAIR DOOR FRAME CRACKED AT UPPER AND LOWER COUNTER BALANCE MOUNTS APPROXIMATELY FS 150.6 AND WL 105. REMOVED DAMAGED SECTION OF ANGLE AND INSTALLED NEW SECTION.Apr 17, 2011 · N16540 · Beech 1900D · Fuselage Main, StructureSDR GUUA94053041711ASkin · corrodedDURING SCHEDULED ROUTINE STRUCTURAL INSP CORROSION FOUND BETWEEN FS 378.25 AND FS 393.25 BETWEEN STRINGERS 9AL AND 10L. REMOVED DAMAGED SKIN AND INSTALLED EXTERNAL REPAIR DOUBLER.Apr 17, 2011 · N16540 · Beech 1900D · Fuselage Main, Plate/SkinSDR GLBA20110416AHose · leakingPILOT REPORTED THAT THE LANDING GEAR WOULD NOT COME UP. THE GEAR INTRANSIT LIGHTS REMAINED ILLUMINATED, NONE OF THE 3 GREEN LIGHTS WOULD ILLUMINATE AFTER THE GEAR HANDLE WAS DOWN, MANUALLY EXTENDED GEAR TO GET 3 GREENS, TRANSIT LIGHTS EXT. MAINTENANCE FOUND A Apr 16, 2011 · N192GL · Beech 1900D · Hydraulic System, MainSDR GUUA94557041611ASpar · corrodedDURING SCHEDULED ROUTINE X-RAY INSPECTION DISCOVERED CORROSION ON LEFT WING FORWARD SPAR AFT FLANGE WS 128.50. REMOVED CORROSION FROM FORWARD SPAR AFT FLANGE AND INSTALLED REINFORCEMENT DOUBLER STRAP.Apr 16, 2011 · N53545 · Beech 1900D · Wing SparSDR CA110427007Blades · fractured(CAN) ABORTED T/O. SECOND STAGE POWER TURBINE BLADES WERE FOUND FRACTURED. THE ENGINE IS BEING REPLACED.Apr 14, 2011 · Beech 1900D · Turbine SectionSDR CA110415001Skin · delaminated(CAN) LT UPPER FWD NACELLE COVER PANEL STARTED DELAMINATING AND TEARING BACK WHILE IN FLIGHT. PASSENGERS NOTIFIED THE FLIGHT CREW AND THE ACFT LANDED WITHOUT INCIDENT. ANOTHER PANEL WAS INSTALLED AND ACFT RETURNED TO SERVICE.Apr 14, 2011 · Beech 1900D · Nacelle/Pylon, Plate/SkinSDR GLBA201104141Unknown · odorPASSENGERS REPORTED A STRONG FUELD SMELL IN THE BACK OF THE AIRCRAFT. MAINTENANCE RAN BOTH ENGINES AND INSPECTED FOR FUEL LEAKS AND ODORS INSIDE IN THE AIRCRAFT, COULD NOT DUPLICATE ANY ODORS OR LEAKS, OK FOR SERVICE.Apr 14, 2011 · N178YV · Beech 1900D · Air Distribution SystemSDR GLBA201104153Bulb · inoperativePILOT REPORTED THAT DURING THERE POST FLIGHT INSP THEY FOUND BOTH INSTRUMENT EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE ARE OUT. MAINTENANCE INSPECTED THE SYSTEM AND REPLACED THE EMERGENCY LIGHTS BULBS, IAW BMM 33-10-04 PARAGRAPH 1, OPS CHECKED GOOD.Apr 14, 2011 · N169GL · Beech 1900D · Emergency LightingSDR V0DR2011009Rod End · mismanufacturedTHE TECH DURING ASSY OF A AIRSTAIR DOOR STRUT NOTED THAT A TIE ROD WOULD NOT THREAD ON TO THE SHAFT. FURTHER TROUBLESHOOTING REVEALED THE NEW TIE ROD WAS A LT THREAD INSTEAD OF A RT THREAD. THE REST OF THE STOCK WAS INSPECTED AND A TOTAL OF (3) WERE FOUND TOApr 14, 2011 · Beech 1900D · Passenger/Crew DoorsSDR V0DR20011008Strut · bindingA TECH REPORTED THAT DURING THE DRY FITTING OF PARTS (PRECHECK FOR BINDING) FOR A AIRSTAIR DOOR STRUT THAT A NEW SHAFT WOULD NOT MOVE FREELY WITHIN THE TUBE. AFTER TROUBLESHOOTING, IT WAS NOTED THAT ONE AREA OF THE SHAFT WAS SLIGHTLY LARGER. A NEW SHAFT WAS Apr 14, 2011 · Beech 1900D · Passenger/Crew DoorsSDR GUUA94753041311ADoor Frame · crackedDURING SCHEDULED ROUTINE MAINTENANCE DISCOVERED AFT CARGO DOOR FRAME CRACKED APPROXIMATELY 90% OF WIDTH AND 3.5 INCHES LENGTH AT APPROXIMATELY FS 509.50 STRINGER 10L. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED NEW SECTION OF FRAME.Apr 13, 2011 · N69547 · Beech 1900D · Fuselage Main, StructureSDR GLBA200904152Computer · malfunctionedUNSCHEDULED RUDDER BOOST ACTIVATION IN FLIGHT. RESOLVED WITH EMERGENCY CHECKLIST. YAW DAMPER WORKS CORRECTLY. MX R & R THE NR1 YAW DAMP/ RB COMPUTER, OPS CK GOOD IAW MM 27-26-00.Apr 13, 2011 · N122UX · Beech 1900D · Rudder Control SystemSDR GLBA20110413FSkin · delaminatedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSP MX FOUND EROSION DAMAGE TO THE TOP OF L/E TIP OF THE RT WINGLET, DELAMENATION ON THE INBD SIDE. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-57-003. MATERIALS UTILIZEDApr 13, 2011 · N257GL · Beech 1900D · Wing, Plate/SkinSDR GUUA94732041211AWire · chafedFLIGHT: 9294 ON DESCENT GEAR WARNING HORN COULD NOT BE SILENCED. REPLACED PCB A119 AND REPLACED FOUR INCH SECTION OF CHAFED WIRE G35A22 OPERATIONAL CHECK GOOD.Apr 12, 2011 · N69547 · Beech 1900D · Landing Gear System WiringSDR GUUA94252041111ALatch · out of adjustPILOT REPORTED AIRSTAIR DOOR CAM LOCKS, DOOR DIFFICULT TO LOCK AND UNLOCK FROM OUTSIDE. ADJUSTED AIRSTAIR DOOR UPPER FWD CAM LATCH, OPS CHECK GOOD.Apr 11, 2011 · N47542 · Beech 1900D · Passenger/Crew DoorsSDR GUUA93532041011ABrake · intermittentPILOT REPORTED WHILE TAXING WITH ANTI SKID ON BRAKING IS INTERMITTENT PEDALS GET STIFF AND NO BRAKING IS APPLIED, WITH ANTI SKID OFF BREAKING IS NORMAL. C-CHECKED ANTISKID ACCUMULATOR PRESSURE AND SERVICED HYD RESERVOIR OPS CHECK GOOD.Apr 10, 2011 · N81535 · Beech 1900D · Landing Gear Brake SystemSDR GLBA20110410FSkin · dentedMAJOR REPAIR - DURING A SCHEDULED ROUNTINE INSPECTION MAINTENANCE FOUND A DENT AT FS 316 AND WL 159, APPROX 2.25" * 2.25", JUST LESS THAN .25" DEEP. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-021. MATEApr 9, 2011 · N153GL · Beech 1900D · Fuselage Main, Plate/SkinSDR V0DR2011007Bearing · seizedDURING SCHEDULED BRUSH, CHANGE THE REPAIR THE TECH NOTED NOISE FROM THE BEARINGS. INSP REVEALED THE ARMATURE, 1 OF THE (COMMUTATOR END) BEARINGS HAD FAILED. A VISUAL INSP OF THE BEARING REVEALED THE GREASE HAD SEEPED PAST THE SEALED AREA AND THE BEARING WOULApr 8, 2011 · N170GL · Beech 1900D · Air Distribution FanSDR V0DR2011006Keyway · mismanufacturedKEYWAY LINERS WHERE BEING R & R DURING MX ON 5006028-5 MAIN WHEEL ASSY. THE TECH, AFTER COMPLETING OTHER MX WAS IN THE PROCESS OF INSTALLING NEW KEYWAY LINERS. THE TECH NOTICED THAT 1 OF THE KEYWAY LINERS WAS LOOSE WHEN PUT INTO POSITION ONTO THE WHEEL HALF Apr 8, 2011 · Beech 1900D · Wheel/Ski/FloatSDR GUUA95632040711ADownlock Switch · shortedON APPROACH, WHEN GEAR EXTENDED, LANDING GEAR INDICATOR CIRCUIT BREAKER TRIPPED AND LANDING GEAR HANDLE LIGHT UNABLE TO TEST, WHEN CIRCUIT BREAKER RESET 3 GREEN LOCK INDICATION AND THEN CIRCUIT BREAKER TRIPPED AGAIN. REPLACED AND ADJUSTED NLG DOWNLOCK SWITCH Apr 7, 2011 · N81556 · Beech 1900D · Landing Gear Position and WarningSDR GUUA92732040711ABrake Assy · malfunctionedAFTER LANDING THE BRAKES WERE INEFFECTIVE, TURNED OFF ANTISKID AND BRAKES WORKED, ANTI SKID FAIL NEVER ILLUMINATED. DRAINED AND SERVICED BRAKE SYS, OPS CHECK GOOD.Apr 7, 2011 · N46AR · Beech 1900D · Landing Gear Brake SystemSDR GLBA20110405FSkin · crackedMAJOR REPAIR - DURING A SCHEDULED ROUTINE INSPECTION MAINTENANCE FOUND THE RT AILERON IB LEADING EDGE SKIN BENT IN 3.5" ON BOTTOM SIDE, CLOSURE RIB DAMAGED, OB LWR LEADING EDGE SKIN CRACKED .625" AND BENT 1.5" FROM LEADING EDGE TO 2.5" BACK. MAINTENANCE REPAIRApr 5, 2011 · N192GL · Beech 1900D · Ailerons
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