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1996 Beechcraft 1900D
N201GL · Serial UE-201
Currently Registered as of Oct 6, 2026Manufacturer-certified specifications for this aircraft type — not a claim about this specific airframe's current configuration.
N-Number History
- N201GL — Sep 9, 2026 to present
Full FAA Registration Record
| Serial Number (as registered) | UE-201 |
|---|---|
| Aircraft Unique ID Number | 00615681 |
| FAA Manufacturer / Model Code | 1154162 |
| Aircraft Engine Type | Turboprop |
| Engine Manufacturer / Model | P&W PT6A SER |
| Certification of Aircraft Registration Date | Mar 25, 2023 |
| Airworthiness Certificate Issue Date | Mar 4, 1996 |
| Airworthiness Classification | Standard (Commuter) |
| Registration Status | Currently Registered |
| Aircraft Registration Expiration Date | Mar 31, 2030 |
| Last FAA Update | Oct 6, 2026 |
| Registration Country | US |
| Registration State | UT |
| Weight Class | CLASS 2 |
| TC Data Sheet | — |
| TC Data Holder | — |
| FAA AIDS Report | 20140913016549I |
Accident & Incident History (NTSB)
No NTSB accident or incident record found for this aircraft.
See NTSB history for every Beechcraft 1900D on file → (FAA-registered and foreign/military aircraft, combined)
Service Difficulty Reports (FAA)
Filing a Service Difficulty Report is required by law for repair stations, aircraft manufacturers, and airlines, but is largely voluntary for privately owned, individually operated aircraft. A blank result below reflects who's required to report a defect, not necessarily a clean maintenance history — and conversely, reports on file are rarely the complete picture for an aircraft that's mostly been privately maintained.
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RIB
Dec 9, 2022
CRACKS IN LEFT HAND CENTER WING MAIN RIB, AT LEFT BUTTOCK LINE 29, RADIATING FROM FASTENER HOLES OF U-SHAPED STIFFENER CHANNEL FLANGES AT BS 303 AFT FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.3, WATER LINE 80.5. BS 303 AFT FLANGE RADIATING INBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.5, WATER LINE 81.5. BS 318 FORWARD FLANGE RADIATING BOTH INBOARD AND OUTBOARD FROM FASTENER HOLE AT LEFT BUTTOCK LINE 28.5, WATER LINE 80.5.
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CABLE
May 1, 2017
MAINTENANCE REPORTED THAT THE UPPER FORWARD [AIRSTAIR] DOOR REQUIRES REPLACEMENT. REMOVED AND REPLACED THE UPPER FORWARD DOOR CABLE IAW BEECH 1900D AMM 52-10-02.
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STRINGER
Aug 23, 2016
DURING A SCHEDULED INSPECTION, MAINTENANCE FOUND STRINGER 4R IS CRACKED IN THE RADIUS ON THE FORWARD END. MAJOR REPAIR
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ACM
Mar 27, 2015
PILOT REPORTED THAT THE PRESSURIZATION OPERATIONS CHECKED GOOD DURING RUN-UP, UPON CLIMB PRESSURIZED TO APPROX DIFF OF 3.0 & FAILED TO FURTHER PRESSURIZE. CABIN ALTITUDE HIGH ANNUNCIATOR ILLUMINATED, DEPLOYED OXYGEN MASKS, DECLARED AN EMERGENCY & RETURNED. R & R ACM IAW MM 21-51-01. OPS CHECKED GOOD.
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BULKHEAD
Mar 9, 2015
DURING A SCHEDULED INSPECTION, FOUND THE CANTED BULKHEAD AT FS 588.10 BUCKLED FROM STRINGER 12R TO 12L. REPAIRED THE BULKHEAD IAW EO 15-120-53-001. MAJOR REPAIR.
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SKIN
Jan 12, 2015
DURING A SCHEDULED INSPECTION, FOUND THE UPPER INBD RT WING SKIN TE CHAFED & CORRODED WITH SEVERAL ELONGATED HOLES AT BL 36. CHAFE 8.5 INCHES LONG, 2 INCHES WIDE AT THE WIDEST PART & .020 INCHES DEEP BEFORE CORROSION REMOVAL. FOUND TO BE A MINOR REPAIR IAW GMM 8 4 1 B.
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SKIN
Dec 17, 2014
DURING A SCHEDULED INSPECTION, FOUND THE BELLY SKIN AT BS 220 & STRINGER 15L HAS A .25 INCH HOLE WORN THROUGH THE SKIN. WORN AREA IS FWD & AFT APPROX 25 INCHES IN LENGTH & WIDTH IS APPROX .065 INCHES. REPAIRED IAW EO 14-1900-53-054
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FRAME
Dec 17, 2014
DURING A SCHEDULED INSPECTION, FOUND THREE CRACKS IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.50 BETWEEN STRINGERS 4 - 5L IN THE BEND RADIUS OF THE FRAME, TWO INCHES IN TOTAL LENGTH. REPAIRED IAW EO 14-1900-53-057.
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FRAME
Dec 17, 2014
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR FUSELAGE FRAME AT BS 509.5 & STRINGER 11L, .75 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-057.
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FRAME
Dec 17, 2014
DURING A SCHEDULED INSPECTION FOUND A CRACK IN THE CARGO DOOR UPPER FRAME AT FS 460 & STRINGER 3L, 2.1 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-058.
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SKIN
Dec 17, 2014
DURING A SCHEDULED INSPECTION, FOUND A CRACK IN THE CARGO BAY LT INNER SKIN AT BS 509.5 & STRINGER 11L, .9 INCHES IN LENGTH. REPAIRED IAW EO 14-1900-53-059.
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BULKHEAD
Dec 15, 2014
MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE CANT BULKHEAD FLANGE AT FS 588.10 & BETWEEN STRINGER 8R & 7R, 1.5 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-055.
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FRAME
Dec 15, 2014
MAJOR REPAIR DURING A SCHEDULED INSPECTION MAINTENANCE FOUND CRACK IN THE FUSELAGE FRAME IN THE FLANGE BEND RADIUS AT FS 177.35 BETWEEN STRINGERS 12L & 13L, 1.1 INCHES IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 14-1900-53-056.
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STRINGER
Sep 17, 2014
MAJOR 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 INCLUDED IN THE ENGINEERING ORDER.
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CONNECTOR
Mar 13, 2014
UPON EXTENDING GEAR ON FINAL, RT GEAR R & H ANNUNCIATORS FAILED TO ILLUMINATE. UPON COMPLETION OF CHECKLIST, ALL OTHER INDICATIONS REVEALED GEAR DOWN & LOCKED. INSTRUCTED BY MX TO RECYCLE GEAR, J HOOK WOULD NOT ALLOW GEAR HANDLE TO BE MOVED UP. ATTEMPTED TO EXTEND GEAR MANUALLY, RT GEAR ANNUNCIATORS REMAINED EXTINGUISHED. THE PLANE LANDED SAFELY & WAS TOWED TO GATE WITH GEAR PINS INSTALLED. AN EMERGENCY WAS DECLARED FOR THIS EVENT. INSPECTED & FOUND RT GEAR DOWN LOCK & SQUAT, P1, SWITCH NOT SECURED & LOCKED. TIGHTENED, SECURED & LOCKED P1 CONNECTOR. PERFORMED MLG EXTENSION & RETRACTION 6 TIMES, OPERATIONS CHECKED GOOD.
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CLAMP
Mar 14, 2013
PILOT REPORTED THAT AT ALTITUDE 18500, CABIN ALTITUDE HIGH ANNUCICATOR ILLUMINATED. CABIN ALTITUDE INDICATED 10000 FT AND CABIN INDICATED 800 FT IAW MIN WITH INCREASE IN TRENDS, PASS O2 MASK DEPLOYED, CLIMB DIFFERENTIAL PRESSURE AT 2.8 AT TIME OF CLIMB ALTITUDE HIGH ANNUCICATOR ILLUMINATED. MX SECURED A LOOSE CLAMP ON HEAT EXCHANGER, OPS CHECKED GOOD.
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SPAR
Oct 1, 2012
DURING A SCHEDULED ROUTINE INSP FOUND FOUR CRACKS ON THE HORIZONTAL STAB FWD SPAR WEB AT HSS 00.00, 2" IN LENGTH TOTAL. REPAIRED IAW EO 11-1900-55-046.
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SPAR
Oct 1, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND TWO CRACKS ON THE HORIZONTAL STAB AFT SPAR WEB AT RELIEF HOLE AT HSS 00.0, .5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-045.
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SPAR
Sep 29, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND FOUR CRACKS ON THE VERTICAL STAB RT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT CHORD, CRACKED FROM FIRST RIVET HOLE AND SECOND CRACK IS FROM SECOND RIVET HOLE, AND THIRD CRACK AT THIRD RIVET HOLE, AND FOURTH CRACK AT FOURTH RIVET HOLE, 6.125 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-044.
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SPAR
Sep 29, 2012
DURING A SCHEDULED ROUTINE INSPECTION, FOUND A CRACK ON THE VERTICAL STAB LT FWD SPAR CAP ANGLE AT VSS 84.10 AT 20 PERCENT. 1.5 INCHES IN LENGTH. REPAIRED IAW EO 11-1900-55-043.
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BULB
Dec 4, 2011
EMERGENCY LIGHTS ON THE CAPTAIN'S SIDE INOP. MX RELAMPED CAPT EMERGENCY LIGHT IAW B-1900 33-60-00-801, ALL CHECKED GOOD.
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FCU
Oct 18, 2011
PILOT REPORTED THAT THERE IS A LEAK COMING FROM THE SMALL DRAIN ON THE LT ENGINE. MX REPLACED THE LT HP FUEL PUMP AND FCU, OPS AND LEAK CHECKED GOOD.
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FRAME
Aug 29, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE CARGO BAY BULKHEAD AT FS 531, LT UPPER OTBD CORNER CRACKED .75" IN LENGTH. REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-053. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
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FRAME
Aug 29, 2011
MAJOR REPAIR - DURING A SCHEDULED ROUTINE INSP THE FUSELAGE FRAME AT FS 456 & STRINGER 10R CRACKED, .55" IN LENGTH. MAINTENANCE REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 11-1900-53-052. MATERIALS UTILIZED ARE INCLUDED IN THE ENGINEERING ORDER.
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FUEL CONTROL
Aug 22, 2011
PILOT REPORTED THAT THE RT ENGINE IS LEAKING FUEL FWD OF THE WHEEL WELL, DRIPPING STOPS ATFTER SHUTDOWN. MX REPLACED THE RT FCU IAW TC 1900-7320.00 AND REPLACED HP PUMP IAW MM 73-10-02 SEC 6, REPLACED STARTER GEN, RIG CHECKS, RUN AND LEAK CHECKED GOOD.
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BULB
Aug 10, 2011
PILOT REPORTED THAT THEY DID NOT GET A NOSE GEAR DOWN AND LOCK INDICATION WITH THE GEAR DOWN AND LOCKED. MX REPLACED THE LIGHT BULBS, OK FOR SERVICE.
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BULB
Aug 10, 2011
ON FINAL, DID NOT RECEIVE NOSE GEAR DOWN AND LOCKED INDICATION. MX REPLACED THE LIGHT BULBS, PN: 327 IAW BMM 33-10-05, OPS CKS AND SWING CHECKS GOOD IAW AIM MI 32-01.
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PUMP
Jul 18, 2011
PILOT REPORTED THAT FUEL WAS LEAKING FROM THE NR2 ENGINE GANG DRAIN. MX REPLACED THE NR2 ENGINE DRIVEN FUEL PUMP IAW BMM 73-10-00.
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UNKNOWN
May 13, 2011
THE 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.
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FLOOR SUPPORT
Apr 21, 2010
MAJOR REPAIR - DURING ROUTINE SCHEDULED MX, A CRACK WAS FOUND AT FS 482 APPROX 24" INBD OF DOOR THRESHOLD. CRACK APPROX 1". CRACK IS AFT OF NUTPLATE IN RADIUS OF UPPER ANGLE FOR FLOOR SUPPORT WEB. MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-016. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
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ANGLE
Apr 20, 2010
MAJOR REPAIR - DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND AT FS 456 JUST LT OF STRINGER NR 1 FWD OF THE REINFORCING ANGLE ATTACHED TO THE FUSELAGE SECTION CRACK EXTENDS FROM EDGE OF ANGLE THROUGH FASTENER HOLE APPROX .375". TOTAL LENGTH OF CRACK APPROX 1". MX REPAIRED THE AFFECTED AREA AND PERFORMED ALL REQUIRED RII INSPECTIONS IAW EO 10-1900-53-017. MATERIALS UTILIZED ARE INCLUDED IN THE EO.
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BULB
Mar 23, 2010
THE PILOTS DISCOVERED THAT THE CAPTAINS SIDE INTRUMENT EMERGENCY LIGHT WAS BURN OUT. MAINTENANCE REMOVED AND REPLACED THE BULB AND THE LIGHT OPERATIONALLY CHECKED GOOD I.A.W. 1900D MM 33-10-00.
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TRANSMITTER
Dec 2, 2009
RT ENG WENT INTO AND OUT OF FEATHER ON SHORT FINAL. MX TROUBLESHOT THE SYS AND FOUND THE TORQUE INDICATION BAD. MX REMOVED AND REPLACED THE TORQUE TRANSMITTER IAW MM 77-10-00. OPS CHECK OF THE AUTOFEATHER SYS WAS GOOD IAW MM 61-20-00.
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AUTOFEATHER SYS
Nov 27, 2009
SUSPECTED AUTOFEATHER - UPON APPROACH, THE PILOTS REPORTED THAT THE RT PROPELLER AUTOFEATHERED WITH TORQUE AT APPROX 1000 LBS. MX PERFORMED THE AUTOFEATHER OPERATIONAL CHECK 5 TIMES AND ALL INDICATIONS WERE WELL WITHIN LIMITS. NO DEFECTS NOTINE IN DURING THE AFX OPS TEST REF MM 61-21-00.
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BULB
Sep 29, 2009
PILOTS REPORTED THAT ONE EMERGENCY INSTRUMENT LIGHT WAS FOUND TO BE INOPERATIVE. MAINTENANCE REMOVED BULB 1864 BY PUSHING IN AND TURNING THE A QUARTER UNTIL IT WAS FREE, REMOVED AND REPLACED THE BLUE SLEEVE TO THE NEW BULB AND INSTALLED BY PUSHING IN AND PERFORMING A QUARTER TURN. OPERATIONAL CHECK WAS GOOD.
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INDICATOR
Apr 30, 2009
IN CRUISE AT 2300 NR 1 TORQUE GAUGE WAS FLUCTUATING 200-300FT/LBS. COULD HEAR THE CHANGE IN TORQUE. OCCURRED WITH PROP SYNC ON AND OFF. WHEN TORQUE BELOW 2500FT/LBS IN DESCENT ALL PWR CHANGE DECREASES AN ADDITIONAL 300FT/LBS WITHOUT BEING COMMANDED WITH POWER LEVERS. FLUCTUATIONS NOTED IN CRUISE NOT OBSERVED BELOW 16000. MAINTENANCE REMOVED AND REPLACED THE NR 1 TORQUE INDICATOR I.A.W. BMM 31-10-00. OPERATIONAL CHECKS WERE GOOD. NO DEFECTS NOTED.
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SKIN
Feb 23, 2009
DURING ROUTINE SCHEDULED MX A CHAFE WAS FOUND ON THE BELLYSKIN AT APPROX FS 224.0 BETWEEN STRINGER 15L & 16L. ONE OF THEM WAS 2.9 INCHES IN LENGTH AND THE OTHER WAS 2.4 INCHES IN LENGTH RUNNING PARALLEL TO EACH OTHER. MAINTENANCE REPAIRED THE BELLY SKIN AT FS 224.0 BETWEEN STRINGER 15L & 16L IAW EO 09UE201-07. REPAIR APPROXIMATELY 5.625 X 3.375 OUT OF 2024 T3 .032, MS20470AD4 RIVETS. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
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SKIN
Feb 20, 2009
DURING ROUTINE SCHEDULED MX THE SKIN OF FUSELAGE WAS FOUND CRACKED AROUND TWO RIVETS ONE ON EACH SIDE OF STRINGER ONE AT F.S. 150.60. MAINTENANCE REMOVED CRACKS BY .750” DIAMETER CUT OUTS. FABRICATED FILLERS FOR LT AND RT SIDE. FABRICATED EXTERNAL PATCH.
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STRINGER
Feb 20, 2009
DURING ROUTINE SCHEDULED MX A CRACK WAS FOUND ON FRAME AT FSS 150.60 STRINGER 9R RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.
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FRAME
Feb 20, 2009
DURING ROUTINE SCHEDULED MX CRACK WAS FOUND ON FRAME AT STRINGER 9R FS 163.975 STRINGER RELIEF CUTOUT. MAINTENANCE DETERMINED THIS DID NOT MEET THE CRITERIA OF A MAJOR REPAIR, HOWEVER, MAINTENANCE REPAIRED THE AFFECTED AREA PER BEECH 1900 SRM 51-70-21.
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ANGLE
Feb 20, 2009
DURING ROUTINE SCHEDULED MX THE LT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAJOR REPAIR - MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER IAW EO 09-201-2. REPAIR APPROXIMATELY 13.5". RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
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ANGLE
Feb 20, 2009
DURING ROUTINE SCHEDULED MX, THE RT HEAVY ANGLE WAS FOUND CRACKED AT FS 288.0. MAINTENANCE REPAIRED THE RIGHT HAND HEAVY DOUBLER I.A.W. .EO. 09-201-2. REPAIR APPROXIMATELY 13.5". PART NUMBER 114-430002-7180. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
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FRAME
Feb 20, 2009
DURING ROUTINE SCHEDULED MAINTENANCE FOUND A FRAME CRACKED ON THE FORWARD SIDE OF THE AIRSTAIR DOOR ENTRANCE FRAME AT THE LOWER SNUBBER MOUNT BRACKET UPPER NUTPLATE. MAINTENANCE REPAIRED THE AIRSTAIR DOOR ENTRANCE FRAME IAW EO 09-UE201-05.
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SKIN
Feb 20, 2009
DURING ROUTINE SCHEDULED MAINTENANCE A HOLE IN THE FUSELAGE WAS FOUND AT F.S. 405.5 LEFT OF STRINGER 14L APPROXIMATELY 1.5 INCHES. HOLE SIZE APPROXIMATELY .375 X .125. MAINTENANCE REMOVED DAMAGE, HOLE .875” CIRCLE, INSTALLED COVER PATCH. COVER PATCH ALODINED AND INSTALLED USING AC240 B1/2. PATCH PAINTED TO MATCH AIRCRAFT. RII INSPECTION COMPLIED WITH PER TASKCARD 8.2.1.
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SKIN
Feb 19, 2009
DURING ROUTINE SCHEDULED MX THE SKIN OF THE FUSELAGE IS CORRODED UNDERNEATH FRAME AT FS 203.25 AT STRINGER 15R TOWARDS 16R. LENGTH IS APPROIMATELY 3.5" AND RUNS UNDER FRAME. MX REMOVED DAMAGED SKIN AND INSTALLED INSERTION PATCH AND DOUBLERS. SKIN PATHC 11 X 5.7 .025", 2024 T3 AL ALCLAD. TWO DOUBLERS 6.8 X 3.8 .032", 2024 T3 AL ALCLAD. TWO DOUBLERS 4.7 X 4.5 .O32 , 2024 T3 AL ALCLAD. MS204070AD4 RIVETS.
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RIB
Jul 20, 2007
LT WING RIB OB OF POWER PACK CRACKED AT (L) BRACKET APPROX. 1 INCH BY 1 INCH IN LENGTH ORIGINATING FROM RIVET HEAD. MAINTENANCE REPAIRED THE LT WING RIB OB OF HYDRAULIC POWER PACK ONE INCH CRACK AT W.S. 79.65 IAW SRM 51-70. REPAIR DIMENSION 4 INCH BY 2.7500 INCH. MATERIAL 2024 T-3 .063 INCH.
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SKIN
Aug 31, 2004
PAX DOOR HAS CORROSION AROUND DOOR HANDLE, REPAIRED PER EO 04-14.
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SHUTOFF VALVE
Mar 13, 2004
RT ENVIRO FAIL ANN ILLUMINATED, R&R RT PRSOV PN 114-380059-5 MM OPS AND LEAK CK GOOD
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WARNING LIGHT
Feb 24, 2004
CABIN DOOR ANNUNCIATOR CAME ON,R&R AIRSTAIR DOOR FWD LATCH HANDLE SWITCH PN V3-10108 OPS CK GOOD
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BRUSH BLOCK
Dec 29, 2003
RT PROP DEICE AND PILOT AND COPILOT W/S NOT HEATING, REMOVED AND REPLACED BRUSH BLOCK PN 4E3196-1GLA AND PROP AMP IND PN 114-380049-5.
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WIRE
Aug 27, 2003
CABIN SIDE HEADSET GETS A LOT OF STATIC AND CUTS IN AND OUT, REPAIRED WIRING UNDER ENTRY FLOORBOARD BETWEEN CAPT'S PHONE JACK TO OBSERVE, PHONE JACK. OPS CK GOOD.
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BEARING
Jan 17, 2003
REPLACED PROP DUE OVERHAUL FOUND NR 2 BLADE BEARING HAD FAILED. REMOVED AND REPLACED PROP.
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WINDSHIELD
Jan 11, 2003
FO'S WINDOW CRACKED, R&R FO'S WINDSHIELD
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SHUTOFF VALVE
Feb 17, 2002
LEFT ENGINE TORQUE FLUCTUATION WITH CABIN BLEED FUNCTIONS. REPLACED PRSOV, OPS CHECKED SYSTEM SATISFACTORY.
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ENGINE
Jan 15, 2002
LEFT ENGINE TORQUE FLUX. INSPECTED BLEED VALVE AND BLENDED 1ST STAGE COMPRESSOR BLADES. COULD NOT DUPLICATE. TORQUE FLUX.
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DUCT
Jan 14, 2002
RIGHT BLEED AIR FAIL. INSPECTED AND REPAIRED EVA TUBING, OPS CHECKED SYSTEM SATISFACTORY.
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TRANSMITTER
Jan 10, 2002
LEFT ENGINE TORQUE FLUX, INSPECTED REPLACED TRANSMITTER OPS CHECKED SYSTEM SATISFACTORY
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TRANSMITTER
Sep 1, 2001 (possible match)
LEFT FUEL FLOW FLUX ON T/O. REPLACED FUEL FLOW TRANSMITTER, OPS CHECKED SYSTEM SATISFACTORY.
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BRAKE
Jul 18, 2001 (possible match)
AIR CRAFT VEERED LEFT ON T/O ROLL, INSPECTED DETERMINED LEFT BRAKE LOCKED UP, REPLACED BOTH #1&2 BRAKES OPS CHECKED SATISFACTORY
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WINDSHIELD
Jul 1, 2001 (possible match)
COPILOTS WINDSHIELD CRACKED IN FLIGHT, REPLACE WINDSHIELD
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ENGINE
May 18, 2001 (possible match)
LEFT ENGINE TORQUE FLUX, INSPECTED ALL PARAMETERS WITHIN LIMITS. RETURNED TO SERVICE.
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BRUSH BLOCK
Apr 10, 2001 (possible match)
LEFT PROP DEICE AMPS LOW. CLEANED AND RESHIMMED BRUSH BLOCK, OPS CHECKED SYSTEM GOOD. RETURNED TO SERVICE.
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WINDSHIELD
Nov 29, 2000 (possible match)
BIRD STRIKE ON BOTH LEFT AND RIGHT WINDSHIELDS. BOTH WINDSHIELDS BROKEN. REPLACED LEFT AND RIGHT WINDSHIELDS, P/N 1145043 & 101384025. (M)
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ALTIMETER
Feb 8, 2000 (possible match)
ALTIMETER FLAGGED AT 4,200 FEET AND REMAINED INOPERABLE. VERIFIED ON BENCH. (X)
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BLEED AIR
Apr 12, 1997 (possible match)
BWI - DUAL 'BLEED AIR FAIL' DURING TAKEOFF. MAINTENANCE COULD NOT DUPLICATE. (X)
Reported Incidents (FAA AIDS)
The FAA's Accident/Incident Data System tracks events below the damage/injury threshold that makes something an NTSB-investigated accident — mostly minor incidents that never became a full NTSB case. A report below marked "Accident" may be the same event already shown above under NTSB; that overlap is expected, not a data error.
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Incident
Sep 13, 2014 — LOS ANGELES, CA (possible match)
General Information
- N-Number (as reported)
- 201GL
- Event Time
- 02:20
- Airport
- LOS ANGELES INTL
- Mid Air Collision
- Not A Midair
- Flight Phase
- Ground/Ramp/Ma
Aircraft Information
- Damage
- Minor
- Aircraft (as reported)
- BEECH 1900D
- Flight Conducted Under
- AIR TAXI/COMMUTER
- Engine (as reported)
- P&W PT6A SER
- Operator
- GLBA
- Total Aboard
- 2
- Injuries
- 0 fatal, 0 non-fatal
Event Remarks
WHILE PREPARING FOR DEPARTURE, GREAT LAKES AIRLINE FLIGHT GLA3048, N201GL, BE1900 WAS STRUCK BY DEBRIS CAUSED BY JET BLAST FROM DAL 2332. TWO PILOTS ON BOARD, NO INJURIES. MINOR DAMAGE TO AIRCRAFT FUSELAGE STATION 516 FOUND TO BE WITHIN LIMITS IAW BE-1900 SRM 51-10-01-00. GLBA CMO INVOLVED
FAA AIDS report 20140913016549I
Registration data, N-number history, and manufacturer type specs come from the FAA. Accident/incident history comes from the NTSB, matched by N-number (older records are cross-checked against this aircraft's registration history where possible — see the "possible match" note above for the residual cases we can't fully confirm). Service difficulty reports come from the FAA's own SDR program. Reported incidents come from the FAA's Accident/Incident Data System (AIDS), matched by N-number. None of this is a substitute for reviewing an aircraft's logbooks and maintenance records before purchase.
Search for Safety and Maintenance Records by Year, Make and Model of Aircraft See aggregate NTSB accident/incident history, FAA Service Difficulty Reports and FAA Accident/Incident Data System Reports across every aircraft of a given year, manufacturer, and/or model — not just one airframe.
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FAA's own deregistration data doesn't include a reason code (no "sold," "destroyed," or "scrapped" field), and its Registration Status values (shown in the results below) run almost entirely "Unknown" in practice — not a useful way to narrow this list. NTSB Accident History instead filters by whether that specific airframe has an NTSB accident or incident on record, and whether any of them marked it Destroyed — the closest signal this report can offer for whether an aircraft's exit from the registry followed an accident. FAA AIDS History filters the same way using FAA's own Accident/Incident Data System records instead, matched by that airframe's event type (Incident/Accident) and reported damage.
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Frequently Asked Questions
What's the difference between an NTSB report and an FAA AIDS report?
The NTSB investigates accidents and serious incidents — events that meet a specific federal damage or injury threshold. FAA's Accident/Incident Data System (AIDS) tracks events that fall below that threshold: mostly minor incidents that were reported to the FAA but never rose to the level of a full NTSB investigation. Because both systems can end up recording the same real-world event, a report marked "Accident" under FAA AIDS may be the very same event already shown above under NTSB — that overlap is expected, not a data error.
What does "(possible match)" mean next to a report?
Every NTSB, FAA Service Difficulty, and FAA AIDS record is linked to a specific aircraft by its N-number (and, when available, its manufacturer serial number). A record is marked "confirmed" when our own tracked registration history shows this exact airframe held that N-number on the date of the event. It's marked "(possible match)" when we can't fully verify that — most often because the event happened further back than our registration history reaches. N-numbers get reassigned to a completely different aircraft over the decades, so a "possible match" is our best available inference, not a certainty.
My aircraft shows no FAA Service Difficulty Reports (SDRs) — does that mean it has a clean maintenance history?
Not necessarily. Filing a Service Difficulty Report is required by law for repair stations, aircraft manufacturers, and airlines, but it's largely voluntary for privately owned, individually operated aircraft. A blank SDR result reflects who's required to report a defect, not necessarily a clean maintenance history.
My aircraft shows no NTSB or FAA AIDS records — is that unusual?
No — it's the common case. The large majority of aircraft never appear in either system at all. An empty result under Accident & Incident History (NTSB) or Reported Incidents (FAA AIDS) simply means no event of that kind is on file for this airframe; it isn't a sign that data is missing.
Does a clean record on this page mean the aircraft is safe to buy?
No. This page reflects only what's on file in federal public records — it isn't a substitute for reviewing an aircraft's own logbooks and maintenance records, and ideally having a qualified mechanic perform a pre-purchase inspection, before you buy.
Where does this data come from, and how current is it?
Registration data, N-number history, and manufacturer type specs come from the FAA's own registry. Accident and incident history comes from the NTSB. Service difficulty reports come from the FAA's SDR program. Reported incidents come from the FAA's Accident/Incident Data System (AIDS). All four are public federal records that we import and refresh on an ongoing basis, so newly filed reports appear over time — but there's typically some lag between when the FAA or NTSB publishes a record and when it shows up here.
