# Emry E-90 - Type: Aircraft model (FAA registry) - Registry code: 05611QB - Manufacturer (registry): EMRY - Model: E-90 - Aircraft type: Balloon - Category: Balloon - Engines: None - Seats: 1 - Weight class: Up to 12,499 lb - Certification: Not type certificated - Registered aircraft: 1 - Page: https://openairdocs.org/model/emry-e-90 Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker. ## ADs that may apply (OpenAirDocs) Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. None matched. ## Registered aircraft (1) - [N9187Y](https://openairdocs.org/aircraft/N9187Y): [Emry Gordon](https://openairdocs.org/faa-owner/EMRY%20GORDON), [Norfolk, NE](https://openairdocs.org/faa-place/NE/Norfolk), built 2001, S/N 51378 ## STCs approved for it (309, first 50) - [STC SA00061LA](https://openairdocs.org/stc/SA00061LA): Installation of JPI digital tachometer.. J P Instruments - [STC SA00068SE](https://openairdocs.org/stc/SA00068SE): Installation of fuel flow/pressure instruments. (W/TSIO-360-MB1). Electronics International Inc. - [STC SA00069LA](https://openairdocs.org/stc/SA00069LA): Installation of passenger communication system.. AlliedSignal Avionics - [STC SA00112AT](https://openairdocs.org/stc/SA00112AT): Installation of a Marathon KSP 400 battery.. Aviall Services, Inc. - [STC SA00149BO](https://openairdocs.org/stc/SA00149BO): Installation of Aircraft Components, Inc. Volt and Vac Alert System, P/N 2044-1. Aircraft Components Inc - [STC SA00161BO (3 OF 3](https://openairdocs.org/stc/SA00161BO%20(3%20OF%203): Installation of Avidyne Corporation FlightMax 700-00007-( ) EX500 Multi-Function Display.. Avidyne Corporation - [STC SA00227NY](https://openairdocs.org/stc/SA00227NY): Installation of Sky Harbour Aircraft Refinishing Ltd. Ice Damage Prevention Plates.. Sky Harbour Aircraft Refinishing - [STC SA00237WI](https://openairdocs.org/stc/SA00237WI): Installation of a Bendix/King EFIS-4 0electronic flight instrument system. Elliott Aviation Technical Products - [STC SA00243BO (4 OF 5)](https://openairdocs.org/stc/SA00243BO%20(4%20OF%205)): Installation of Centurion Consulting, Inc. GPS Steering Assist Module (SAM) with roll steering (p/n 0025-5100), or without roll steering (p/n 0025-5200).. Icarus Avionics, LLC - [STC SA00257AT](https://openairdocs.org/stc/SA00257AT): Installation of a Concorde RG-380E sealed lead acid battery.. Textron Aviation Inc - [STC SA00269BO](https://openairdocs.org/stc/SA00269BO): Installation of Avidyne Corporation TWX 670 Tactical Weather Detection System P/N 850-00026-000-( ) consisting of Avidyne Processor P/N 700-00033-000-( ), Sensor Systems Inc. Antenna P/N S72-1715-1 with doubler plate P/N S72-171530-1, and Avidyne Mounting Tray P/N 700-00034-000.. Avidyne Corporation - [STC SA00273WI](https://openairdocs.org/stc/SA00273WI): Installation of Stretcher, Patient Loading, and Support system.. Lifeport Inc - [STC SA00281BO](https://openairdocs.org/stc/SA00281BO): Installation of Avidyne Corporation MLX770 MultiLink Broadcast Transceiver P/N 700-00163-( ), Sensor Systems Inc. Antenna P/N S67-1575-109, or equivalent, and optional Avidyne Mounting Tray P/N 700-00165-000. Avidyne Corporation - [STC SA00290BO](https://openairdocs.org/stc/SA00290BO): Installation of Avidyne Corporation Part Number 700-00167-XXX Multi-Function Display and Mounting Tray Assembly Part Number 700-00168-XXX. Avidyne Corporation - [STC SA00343BO](https://openairdocs.org/stc/SA00343BO): Installation of a single configuration or a dual configuration Avidyne Corporation Integrated Flight Display, Model IFD540 loaded with Release 10.0 software (or later FAA approved release). Avidyne Corporation - [STC SA00344BO PAGE 1](https://openairdocs.org/stc/SA00344BO%20PAGE%201): Installation of Parmetheus Plus LED PAR36 and PAR46 taxi and landing lights.. Whelen Aerospace Technologies - [STC SA00352BO PAGE 1](https://openairdocs.org/stc/SA00352BO%20PAGE%201): Installation of an Avidyne Corporation Mode A/C/S Transponder with ADS-B Out capability, Model AXP340 loaded with Version 3.13 software (or later FAA approved version),. Avidyne Corporation - [STC SA00367SE](https://openairdocs.org/stc/SA00367SE): Installation of a Nose Baggage Compartment on Beech KingAir Models.. Sierra Nevada Corporation/Integrated Mission Systems - [STC SA00415WI](https://openairdocs.org/stc/SA00415WI): Installation of a baggage door.. Avcon Industries Inc - [STC SA00443WI-D](https://openairdocs.org/stc/SA00443WI-D): Installation of Bendix/King IU 2023B Graphics Unit, optional CC 2024D Checklist Controller and Flitefone 800 Accessories.. Honeywell International Inc - [STC SA00453WI](https://openairdocs.org/stc/SA00453WI): Installation of a Lateral Tracking Seat Base.. Aviation Fabricators Inc - [STC SA00482DE](https://openairdocs.org/stc/SA00482DE): Installation of an Aircraft Noise Control (ANC) System.. Quiet Flight LLC - [STC SA00575WI](https://openairdocs.org/stc/SA00575WI): Installation of Phoenix Aerospace, Inc. (PAI) Solid State DC Voltage Regulator, Model VR-1010-24-2A.. Phoenix Aerospace, Inc - [STC SA00622WI](https://openairdocs.org/stc/SA00622WI): Shoulder harness anchor installation. Aviation Fabricators Inc - [STC SA00635WI](https://openairdocs.org/stc/SA00635WI): Jump seat installation.. Aviation Fabricators Inc - [STC SA00660AT-D](https://openairdocs.org/stc/SA00660AT-D): Installation of an Aircraft Security System. Textron Aviation Inc - [STC SA00674WI-D](https://openairdocs.org/stc/SA00674WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II system installation.. Rockwell Collins Inc - [STC SA00686SE](https://openairdocs.org/stc/SA00686SE): Installation of American Aviation, Inc., engine exhaust stacks.. American Aviation Inc - [STC SA00692SE](https://openairdocs.org/stc/SA00692SE): Replacement of certain BF Goodrich pneumatic deicer boots. SMR Technologies - [STC SA00706SE](https://openairdocs.org/stc/SA00706SE): Installation of fuselage mounted emergency medical stowage box with or without oxygen and systems outlets.. Lifeport Inc - [STC SA00737WI](https://openairdocs.org/stc/SA00737WI): Landing gear position switch and squat switch modification.. Supplemental Technologies Corporation - [STC SA00741WI](https://openairdocs.org/stc/SA00741WI): Installation of the Concorde RG-380E/K series VRSLA batteries in airplanes listed on the attached FAA approved Model List (AML). Aero-Mach Wilco LLC - [STC SA00749AT](https://openairdocs.org/stc/SA00749AT): Modification of flush type fuel caps for installation of a locking cylinder and keeper. (1964 and subsequent). Aero Trim, Inc - [STC SA00765DE](https://openairdocs.org/stc/SA00765DE): Installation of Automatic Dependent Surveillance Broadcast (ADS-B) Out functionality using the BendixKing KT74 Transponder and qualified position sensor. Peregrine - [STC SA00780SE](https://openairdocs.org/stc/SA00780SE): Installation of the True Lock Safety Retention Axle Lock Nut System. True Lock LLC - [STC SA00782WI-D](https://openairdocs.org/stc/SA00782WI-D): Modification of Collins VHF-22A/VHF-22B VHF COMM Receiver Transmitter with CTL-22 Control Pro Line II System Installation to a Collins VHF-22C/VHF-22D VHF COMM Receiver Transmitter with CTL-22C Control 8.33 kHz Pro Line II System Installation.. Textron Aviation Inc - [STC SA00823CH](https://openairdocs.org/stc/SA00823CH): Installation of various de-icer wire harnesses.. SMR Technologies - [STC SA00829SE](https://openairdocs.org/stc/SA00829SE): Installation of Merlyn Products landing gear assembly kit 23-1-LW30 in accordance with Merlyn Products Installation Instructions Report 23-1-LW30, Revision A, dated June 7, 2000.. Merlyn Products Inc. - [STC SA00841CH](https://openairdocs.org/stc/SA00841CH): Installation of four place side facing divan.. Daedalus, Inc - [STC SA00872SE](https://openairdocs.org/stc/SA00872SE): Installation of modified ram air engine induction system (Option I or Option II).. American Aviation Inc - [STC SA00889DE](https://openairdocs.org/stc/SA00889DE): Installation of Teledyne Battery Products P/N 7638-44 Lead-Acid Battery. Teledyne Battery Products - [STC SA00948CH](https://openairdocs.org/stc/SA00948CH): Installation of various de-icer wire harnesses. (E90 modified by STC SA3593NM, F90 modified by STC SA4131NM, B200 modified by STC SA2698NM-S, DHC-6 Series modified by STC SA3532NM). SMR Technologies Inc - [STC SA01004AT](https://openairdocs.org/stc/SA01004AT): Installation of right hand side nacelle fuel cell assembly.. FFC Manufacturing - [STC SA01046CH](https://openairdocs.org/stc/SA01046CH): Installation of SMR Technologies engine inlet anti-icer models.. SMR Technologies Inc - [STC SA01071CH](https://openairdocs.org/stc/SA01071CH): Installation of AlliedSignal MK VII Enhanced Ground Proximity Warning System (EGPWS).. Elliott Aviation Technical Products - [STC SA01085LA](https://openairdocs.org/stc/SA01085LA): Installation of the VNS 1000 Voice Navigation System.. VNS Incorporated - [STC SA01110CH](https://openairdocs.org/stc/SA01110CH): Installation of wing fuel tank quick valve drains.. Storehouse LLC - [STC SA01114CH](https://openairdocs.org/stc/SA01114CH): Installation of P2 Incorporated 6600 Audio Advisory system. P2 Incorporated - [STC SA01126WI](https://openairdocs.org/stc/SA01126WI): Replacement of wing tie down ring assembly on Classic Beechcraft model airplanes with one piece machined part number APMA35-115632. DER Associates Ltd. - [STC SA01141WI-D](https://openairdocs.org/stc/SA01141WI-D): Modification of a single or dual Collins TDR-94 or TDR-94D Mode S Transponder System installation with CTL-92 control head to a Flight ID capable Collins TDR-94 or TDR-94 Mode S Transponder System installation with CTL-92E control head.. Rockwell Collins Inc All 309: https://openairdocs.org/model/emry-e-90/stcs.md ## NTSB investigations None matched to aircraft with this model. ## FAA accident and incident reports None matched to aircraft with this model. ## Service difficulty reports (139, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR 2024FA0000739](https://openairdocs.org/sdr/2024FA0000739), Sep 26, 2024: GPS. DEFECTIVE. WHILE ENROUTE TO KLVS FROM KGUY, THE GARMIN GNS530W SCREEN SHUT OFF. WHILE TROUBLESHOOTING, A STRONG ELECTRICAL SMELL FILLED THE CABIN. THE AIRCRAFT DIVERTED TO - [SDR T4OR2022071400002](https://openairdocs.org/sdr/T4OR2022071400002), Jul 14, 2022: BRAKE ASSY. BROKEN. DURING LANDING ROLL-OUT BRAKING, THE LEFT BRAKE PEDAL WENT MOST OF ITS TRAVEL WITH LITTLE BRAKING EFFECT. IT WAS DISCOVERED THE LEFT BRAKE TORQUE PLATE WAS CRAC - [SDR 9LMR032222N600AC](https://openairdocs.org/sdr/9LMR032222N600AC), Mar 22, 2022: TEST SWITCH. CREW ERROR. LANDING GEAR INDICATOR GREEN LIGHT PRESS-TO-TEST, REMOVED, INSPECTED AND RE-INSTALLED . NO DISCREPANCIES NOTED AT THIS TIME. LANDING GEAR RETRACTION SYSTEM INSP - [SDR HAEA20190614001](https://openairdocs.org/sdr/HAEA20190614001), Jun 12, 2019: AXLE. MISSING. ON DEPARTURE FROM KGVT THE CREW HEARD A NOISE FROM THE RH WING AREA, NOT SURE WHAT IT WAS THEY LEFT THE GEAR DOWN AND LOCKED AND PERFORMED A FLY BY THE TOWER AN - [SDR 2019F00061](https://openairdocs.org/sdr/2019F00061), Aug 13, 2018: BOOT. DETACHED. 08-11-2018 THE AIRCRAFT HAD A PROPELLER DE-ICE BOOT REPLACED THAT HAD FALLEN OFF. 08-12-2018 ON A FLIGHT, THE BOOT DETACHED FROM THE PROPELLER AND WAS REPAIRED. - [SDR 2018FA0000290](https://openairdocs.org/sdr/2018FA0000290), Mar 29, 2018: BOLT. LOOSE. DURING FLIGHT FROM KVNY TO KJAC THE CAPTAIN NOTICED FUEL LEAKING FROM THE FILL CAP AREA OF THE LEFT HAND NACELLE FUEL TANK. THE AIRCRAFT WAS DIVERTED TO KLAS FO - [SDR 2018FA0000081](https://openairdocs.org/sdr/2018FA0000081), Mar 7, 2018: SKIN. CHAFED. ON REMOVAL OF THE HORIZONTAL STABILIZERS FROM THE FUSELAGE, SIGNIFICANT FUSELAGE SKIN CHAFFING WAS FOUND ON BOTH SIDES OF THE AIRCRAFT FROM THE RUBBER SEAL THAT - [SDR 2018FA0000057](https://openairdocs.org/sdr/2018FA0000057), Feb 14, 2018: CLAMP. BROKEN. FOUND BOTH OXYGEN BOTTLE HOLD-DOWN CLAMP BASES BROKEN IN TWO. - [SDR CA180117004](https://openairdocs.org/sdr/CA180117004), Jan 16, 2018: BRACKET. CRACKED. (CAN) DURING ROUTINE MAINTENANCE DISCOVERED FLAP TRACK BRACKET CRACKED AT REAR OF SLOT. (TC NR 20180117004). - [SDR 2016F00123](https://openairdocs.org/sdr/2016F00123), May 7, 2016: WIRE. CHAFED. EXPERIENCED A MASTER WARNING & FIRE INDICATION ON THE NR 2 ENG, SHORTLY AFTER GETTING INTO SOME HEAVY PRECIPITATION. THE PILOT RESET THE MASTER WARNING, BOTH TH - [SDR NBFA201508030001](https://openairdocs.org/sdr/NBFA201508030001), Aug 1, 2015: UNKNOWN. SMOKE. DURING CRUISE, THE CREW SMELLED AND SAW LIGHT SMOKE COMING FROM BEHIND THE GLARE SHIELD. USING CREW PROCEDURES, UNNECESSARY ELECTRICAL SYSTEM WERE SHUTDOWN. SOU - [SDR HAEA2015040500231](https://openairdocs.org/sdr/HAEA2015040500231), Jun 2, 2015: RUDDER MAST. DAMAGED. DURING PHASE 1 ACFT INSPECTION, DISCOVERED THE RUDDER TO BELL CRANK RT ATTACH BOLT MISSING. FURTHER INVESTIGATION REVEALED THE BOLT HAD FAILED. AN INSPECTION OF - [SDR CA130524003](https://openairdocs.org/sdr/CA130524003), May 23, 2013: GYRO. FAILED. (CAN) AFTER REPLACEMENT OF DISPLACEMENT GYRO, FLIGHT CREW NOTIFIED MAINTENANCE THAT THE ATTITUDE INDICATOR INFORMATION WAS BACKWARDS. MAINTENANCE FOUND THE FORW - [SDR GNL2013F00000](https://openairdocs.org/sdr/GNL2013F00000), Apr 2, 2013: ATTACH FITTING. CRACKED. LEFT LOWER FORWARD WING ATTACH FITTING CRACKED. CRACK WAS FOUND DURING SIRM WING ATTACH FITTING INSPECTION. EDDY CURRENT WAS THE INSPECTION METHOD. MFG SUPPORT - [SDR 2013FA0000150](https://openairdocs.org/sdr/2013FA0000150), Mar 6, 2013: G SWITCH. MISINSTALLED. WHILE PERFORMING THE ANNUAL ELT INSPECTION, THE ELT WOULD NOT SIGNAL DURING THE "SHAKE" TEST. THE COVER WAS REMOVED FOR A VISUAL INSPECTION. THE G-SWITCH WAS IN - [SDR CA121004006](https://openairdocs.org/sdr/CA121004006), Oct 4, 2012: SUPPORT BRACKET. CRACKED. (CAN) DURING SCHEDULED INSPECTION, THE BEARING INSIDE THE LANDING GEAR TORQUE TUBE SUPPORT BRACKET HAD MOVED OUT OF PLACE. FURTHER INVESTIGATION REVEALED A CRAC - [SDR CA120719002](https://openairdocs.org/sdr/CA120719002), Jul 17, 2012: GASKET. SPLIT. (CAN) NACELLE GASKETS SPLIT AT BOLT HOLES AND CAUSED FUEL LEAK. GASKETS REPLACED IAW SB 28-4059. - [SDR CA110802009](https://openairdocs.org/sdr/CA110802009), Aug 2, 2011: RIB. CRACKED. DURING INSP, FRETTING (SMOKING) WAS FOUND TO BE COMING FROM BETWEEN THE ELEVATOR TORQUE TUBE AND THE INBD RIB THAT THE TUBE ATTACHES TO. AFTER DISASSEMBLY, CRAC - [SDR GNL2011F00001](https://openairdocs.org/sdr/GNL2011F00001), Jul 26, 2011: RESISTOR. SHORTED. ACFT IN CRUISE FLIGHT. ELECTRIC SMOKE FILLED THE CABIN AND COCKPIT. NON-ESSENTIAL EQUIPMENT WAS TURNED OFF AND THE SMOKE CLEARED. THERE WERE NO TRIPPED CIRCUIT - [SDR GNL2011F00000](https://openairdocs.org/sdr/GNL2011F00000), Dec 27, 2010: CONTROLLER. INTERMITTENT. ACFT CLIMBING THROUGH 12,000 FT, CREW NOTICED A HAZE IN THE CABIN FOLLOWING INCREASE IN CABIN TEMP. A DESCENT TO 11,000 FT WAS MADE. ATTEMPTS WERE MADE TO STOP - [SDR YUUR101220105690](https://openairdocs.org/sdr/YUUR101220105690), Dec 7, 2010: CONNECTOR. SEPARATED. (YUUR) DURING PRE-INSP GROUND RUNS THE PROPELLER DE-ICE AMPERAGE WAS NOTED LOW. INSP REVEALED THE BLADE DE-ICE BOOT LEAD IS A 2 PIECE ASSY WITH A MOLEX TYPE CON - [SDR DGCA10851](https://openairdocs.org/sdr/DGCA10851), Dec 3, 2010: WINDSHIELD. CRACKED. CO-PILOTS WINDSHIELD CRACKED. - [SDR 2010FA0001089](https://openairdocs.org/sdr/2010FA0001089), Oct 6, 2010: FIRE WARNING. FALSE ACTIVATION. FIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVEDENCE OF ACTUAL FIRE. CHECK LIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED. INSPECTED AND TROUBLESHOT - [SDR 2010FA0001085](https://openairdocs.org/sdr/2010FA0001085), Oct 6, 2010: FIRE WARNING. FALSE ACTIVATION. FIRE WARNING ON RT ENGINE WITH NO SUPPORTING EVIDENCE OF ACTUAL FIRE. CHECKLIST COMPLIED WITH AND PRECAUTIONARY LANDING ACCOMPLISHED. - [SDR CA100922002](https://openairdocs.org/sdr/CA100922002), Sep 17, 2010: CONTROL CABLE. DAMAGED. ELEVATOR TRIM CABLE WAS FOUND UNSPOOLED OFF BOTH FWD AND AFT TRIM DRUMS. - [SDR CA100531006](https://openairdocs.org/sdr/CA100531006), May 21, 2010: BLOWER MOTOR. OVERHEATED. CABIN VENTILATION BLOWER MOTOR OVERHEATED AND CREATED SMOKE IN THE COCKPIT. PILOT WAS FORCED TO DO AN EMERGENCY LANDING. UPON INVESTIGATION THE BLOWER MOTOR CIR - [SDR VIB4 1536](https://openairdocs.org/sdr/VIB4%201536), Apr 22, 2010: CIRCUIT BREAKER. INTERMITTENT. (VIB4) DURING TAKEOFF THE ACFT ATTEMPTED A NORMAL GEAR RETRACTION. THE LANDING GEAR STARTED A NORMAL RETRACTION WHEN IT STOPPED EARLY IN THE RETRACTION CYCLE. W - [SDR CA100218013](https://openairdocs.org/sdr/CA100218013), Feb 10, 2010: SKIN. CRACKED. (CAN) FUSELAGE PRESSURE SKINS P/N 50-420011-1051 AND 1052 CRACKED AND WORN BY CHAFING ACTION BETWEEN THEM AND FILLETS PN 50-420023-31 AND 32 DUE TO NORMAL WING - [SDR CA100218012](https://openairdocs.org/sdr/CA100218012), Feb 10, 2010: SKIN. CRACKED. (CAN) FUSELAGE PRESSURE SKINS PN 50-120156-81 AND 82 CRACKED AT LOWER SPAR CAP PENETRATIONS. (TC 20100218012) - [SDR DGCA09331](https://openairdocs.org/sdr/DGCA09331), Nov 2, 2009: FUEL CONTROL. HUNG UP. ON LANDING THE ENG POWER HUNG AT APP 800 LBS OF TORQUE. FOUND FUEL CONTROL UNIT FAULTY. - [SDR CA091020001](https://openairdocs.org/sdr/CA091020001), Oct 20, 2009: SPLICE. MISSING. (CAN) DURING INSP OF FUSELAGE BELLY SKINS JUST AFT OF FWD WING SPAR, AN UNUSUAL SKIN BUTT SPLICE WAS FOUND. SPLICE HAS ONLY A SINGLE ROW OF RIVETS IN A PRESSURI - [SDR CA090617003](https://openairdocs.org/sdr/CA090617003), Jun 16, 2009: HINGE. CRACKED. (CAN) LT HORIZ STAB CTR HINGE LWR OTBD CORNER CRACKED. INITIALLY APPEARED TO BE CRACK IN THE PAINT UNTIL CLOSER EXAMINATION. - [SDR 2009F00036](https://openairdocs.org/sdr/2009F00036), May 27, 2009: BOLT. CRACKED. POSSIBLE CRACK IN AFT WING BOLTS UPPER (POSSIBLY WAS CAD PLATING ON BOLTS) SHOWING IN THREADS OF BOLTS. - [SDR T4OR 4995 70](https://openairdocs.org/sdr/T4OR%204995%2070), Apr 23, 2009: ROLLER. WORN. RT OTBD FLAP ATTACH POINT BRACKETS (RIBS) ARE WORN WHERE AFT FLAP TRACK ROLLERS ARE ATTACHED. BRACKETS ARE WORN APPROXIMATELY .015 INCH TO .020 INCH DEEP IN THE - [SDR VQMAF010510](https://openairdocs.org/sdr/VQMAF010510), Mar 13, 2009: CIRCUIT BOARD. BURNED OUT. A CABIN ALTITUDE WARNING PRESSURE SWITCH TEST WAS PERFORMED BY METHOD 2, AS REFERENCED IN MM 21-30-00, PAGE 214, ITEMS A-F. DETERMINED THAT THE TEST FAILED ITEM - [SDR CIEA200800009](https://openairdocs.org/sdr/CIEA200800009), Dec 16, 2008: WINDSHIELD. CRACKED. DURING CRUISE AT FL240 APPROX 80 TO 90 MILES FROM KCPR, THE RT SIDE FRONT WINDSHIELD CRACKED. AT THE TIME, THE TEMPERATURE OUTSIDE WAS -38 DEGREES CELSIUS AND T - [SDR 2008FA0000670](https://openairdocs.org/sdr/2008FA0000670), Oct 10, 2008: FUEL LINE. CRACKED. WHILE PERFORMING ENGINE RUNS FOR RIGHT ENGINE FLOW PACK CHANGE FOUND FUEL LEAK FROM FUEL LINE FROM FCU TO TOP OF START CONTROL UNIT. FITTING CRACKED ABOVE SCU. - [SDR 2008FA0000321](https://openairdocs.org/sdr/2008FA0000321), Apr 25, 2008: SPAR CAP. CRACKED. THE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, (4TH RIVET FROM END OF SPAR CAP)IN THE REAR ROW OF RIVETS, & EXTENDS TO T - [SDR 2008FA0000326](https://openairdocs.org/sdr/2008FA0000326), Apr 25, 2008: SPAR CAP. CRACKED. THE CRACK EMANATES FROM THE 5TH RIVET OUTBOARD OF THE LOWER FORWARD WING BOLT FITTING, 4TH RIVET FROM END OF SPAR CAP, IN THE FRONT ROW OF RIVETS, AND EXTENDS T - [SDR R025878](https://openairdocs.org/sdr/R025878), Apr 9, 2008: CLAMP. CRACKED. 838-67 CLAMP ASSY SN EF3099. CRACK FOUND INTERSECTING THE THREADED LINK SCREW HOLE. - [SDR CA080423013](https://openairdocs.org/sdr/CA080423013), Mar 28, 2008: FUEL CONTROL. MALFUNCTIONED. (CAN) DURING APPROACH, UPON RETARDING THE POWER LEVER TO IDLE, THE ENGINE ACCELERATED TO 90 PERCENT NG WITH AN ASSOCIATED TEMPERATURE OF 800 DEGREES. THE PILOT - [SDR 2008FA0000082](https://openairdocs.org/sdr/2008FA0000082), Feb 18, 2008: CAPACITOR. BURNED. AT CRUISE FL 150, CREW NOTICED SMOKE AND ELECTRICAL ODOR COMING FROM SIDEWALL UNDERNEATH EMERGENCY EXIT. PIC DECLARED EMERGENCY AND LANDED AC WITHOUT FURTHER IN - [SDR O7Z2008F00000](https://openairdocs.org/sdr/O7Z2008F00000), Jan 28, 2008: SPAR CAP. CRACKED. FWD OB LOWER WING SPAR CAPS ARE CRACKED. LT AND RT ASSY CRACKS RADIATE FROM THE (4) HUCK RIVET FWD THROUGH WING ATTACH HINGE. THE AIRCRAFT WAS INSPECTED 15 MONT - [SDR LW29212112007](https://openairdocs.org/sdr/LW29212112007), Dec 11, 2007: UNKNOWN. ODOR. DEPARTED, UPON REACHING 7500 FEET SMELLED BURNING OIL FUMES IN CABIN. CLOSED BLEED AIR'S, TURNED OFF ENVIRONMENTAL SYSTEMS AND DUMPED CABIN. SAFELY RETURNED TO - [SDR 2007FA0000853](https://openairdocs.org/sdr/2007FA0000853), Sep 20, 2007: FLANGE. CRACKED. (2) NEW ENGINES WERE INSTALLED IAW MFG MODIFICATIONS, WITH 938.0 HRS SINCE NEW. AIRCRAFT WAS IN FOR A PHASE INSPECTION AND FOUND 3 OUT OF L1 EXHAUST FLANGES ON - [SDR 2007FA0000752](https://openairdocs.org/sdr/2007FA0000752), Jul 25, 2007: ENGINE. FAILED. AIRCRAFT IN CRUISE AT 22,000 WITH ALL ENGINE INDICATIONS NORMAL. A LOUD NOISE FOLLOWED BY POWER LOSS AND REDLINE ITT ON THE LT ENGINE. THE CT BLADES, ITT PROBES - [SDR CIEA200700003](https://openairdocs.org/sdr/CIEA200700003), Apr 6, 2007: COWLING. BENT. DURING TAKEOFF ROLL OF THE AC, AT THE POINT OF LIFTOFF, THE PILOT NOTICED THE LT ENGINE UPPER AFT COWLING HAD COME OPEN. THE TAKEOFF WAS ABORTED AND THE AC CAME - [SDR LE72008F00000](https://openairdocs.org/sdr/LE72008F00000), Jan 16, 2007: RELAY. FAILED. LANDING GEAR FAILED TO EXTEND, GEAR LOWERED MANUALLY. (K) - [SDR CA060822006](https://openairdocs.org/sdr/CA060822006), Aug 22, 2006: FRAME. CRACKED. (CAN) LT SIDE OF FUSELAGE, DISCOVERED 4 LOOSE RIVETS AT FS 176.5. MAINTENANCE DEPT REMOVED INTERIOR TO INVESTIGATE DEFECT. IT WAS DISCOVERED THAT FRAME MEMBER P - [SDR 2006FA0000090](https://openairdocs.org/sdr/2006FA0000090), Jan 6, 2006: PLATE. CRACKED. DURING A PHASE I AND II INSPECTION A CRACK WAS FOUND IN THIS PART ATTACHED TO THE RT GEAR ASSY. THE CRACK IS ON THE TORQUE PLATE UPPER FORWARD BRAKE CYLINDER PI All 139: https://openairdocs.org/model/emry-e-90/reports.md ## The same model under other registry codes Amateur-built copies and renamed makers get their own codes. - [Beech E-90](https://openairdocs.org/model/beech-e-90): 145 registered aircraft, registry code 1152914 - [Raytheon E90](https://openairdocs.org/model/raytheon-e90): 1 registered aircraft, registry code 7150051 --- 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.