# Service difficulty reports: Embraer EMB-110P1

A list on [Embraer EMB-110P1](https://openairdocs.org/model/embraer-emb-110p1.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 176 reports

- [SDR AXSA202205120002](https://openairdocs.org/sdr/AXSA202205120002.md): Smoke Detector · false activation · May 12, 2022 · N119WA · Emb EMB110P1 · Fire Detection
  > THE PILOT OBSERVED A CARGO COMPARTMENT SMOKE WARNING LIGHT IN THE COCKPIT SHORTLY AFTER TAKEOFF FROM PBG EN ROUTE TO BUF. THE PILOT RETURNED TO PBG AND LANDED WITHOUT INCIDENT. AN EMERGENCY WAS NOT DECLARED. THE PILOT REPORTED AFTER LANDING THAT THERE DID NOT
- [SDR 2022F00200](https://openairdocs.org/sdr/2022F00200.md): Lamp · broken · Apr 7, 2022 · N117WA · Emb EMB110P1 · Flight Compartment Lighting
  > THE PILOT REPORTED A VISIBLE PUFF OF SMOKE FROM THE OVERHEAD PANEL AREA TO MAINTENANCE. MAINTENANCE FOUND TWO WHEAT BULBS BROKEN AND POSSIBLY SHORTED TOGETHER IN DE-ICE PANEL BACK LIGHTING. NO OTHER ELECTRICAL ISSUES WERE FOUND. ALL SYSTEMS WERE FUNCTIONAL.
- [SDR AXSA202204270001](https://openairdocs.org/sdr/AXSA202204270001.md): Lamp · broken · Apr 6, 2022 · N117WA · Emb EMB110P1 · Flight Compartment Lighting
  > AFTER LANDING, THE PILOT REPORTED A VISIBLE PUFF OF SMOKE FROM THE OVERHEAD PANEL AREA TO MAINTENANCE. MAINTENANCE FOUND TWO WHEAT BULBS BROKEN AND POSSIBLY SHORTED TOGETHER IN THE DE-ICE PANEL BACK LIGHTING. NO OTHER ISSUES WERE FOUND. ALL SYSTEMS WERE FUNCTI
- [SDR AXSA2020061200001](https://openairdocs.org/sdr/AXSA2020061200001.md): Control Unit · defective · Jun 11, 2020 · N119WA · Emb EMB110P1 · AC Regulator
  > LOST BOTH GENERATORS IN FLIGHT
- [SDR AXSA2019061400019](https://openairdocs.org/sdr/AXSA2019061400019.md): Blades · cracked · Jun 14, 2019 · N116WA · Emb EMB110P1 · Turbine Section
  > DURING A HOT SECTION 3 CT BLADES WERE FOUND TO BE CRACKED AT THE FIR TREE.
- [SDR AXSA2018082700001](https://openairdocs.org/sdr/AXSA2018082700001.md): Engine · unknown · Aug 25, 2018 · N118WA · Emb EMB110P1 · Engine (Turbine/Turboprop)
  > DURING CLIMB OUT, LEAVING 3500 FEET, A MUFFLED BANG WAS HEARD, FOLLOWED BY A YAW. THE ENGINE FAILURE DRILL WAS CARRIED OUT FOLLOWED BY THE CHECKLIST AFTER AN EMERGENCY WAS DECLARED. AN UNEVENTFUL LANDING WAS CARRIED OUT, AN ASSESSMENT OF NO FIRE WAS MADE B
- [SDR AXSA2017121100001](https://openairdocs.org/sdr/AXSA2017121100001.md): Accumulator · empty · Dec 8, 2017 · N113WA · Emb EMB110P1 · Landing Gear Retraction/Extension System
  > LANDING GEAR NOSE WHEEL WILL NOT COME UP DURING FLIGHT AND DURING LANDING NOSE WHEEL WAS NOT CENTER.
- [SDR AXSA2016040700001](https://openairdocs.org/sdr/AXSA2016040700001.md): Connector · dirty · Apr 6, 2016 · N118WA · Emb EMB110P1 · Ice/Rain Protection System Wiring
  > WHILE ENROUTE, APPROXIMATELY 15 MINUTES AFTER T/O THE ENGINE AIR INLET DEICE SYS ON ACFT 118WA FAILED. PILOT DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE.
- [SDR AXSA020160129001](https://openairdocs.org/sdr/AXSA020160129001.md): Rod End · worn · Jan 28, 2016 · N117WA · Emb EMB110P1 · Landing Gear Door Retract Section
  > EVENING FLIGHT WIG 1361, DURING CLIMB THE GEAR IN TRANSIT LIGHT WOULD NOT EXTINGUISH. ACFT RETURNED SAFELY. INITIAL INVESTIGATION SHOWS WEAK SPRING IN DOOR ROD END.
- [SDR AXSA20150107001](https://openairdocs.org/sdr/AXSA20150107001.md): Link · detached · Jan 6, 2016 · N830AC · Emb EMB110P1 · Landing Gear Door Retract Section
  > MORNING FLIGHT 1050, DEPARTED AT 0735 LOCAL TIME, BUT PERFORMED AN AIR RETURN TO ITS STARTING POINT AT 0752 DUE TO A GEAR NOT RETRACTED INDICATION. MX TECHNICIAN DETERMINED THAT A QUICK RELEASE DOOR LINK HAD COME OFF, ALLOWING THE LT MLG TO CONTACT ITS BELL C
- [SDR AXSA2015112590038](https://openairdocs.org/sdr/AXSA2015112590038.md): Turbine Wheel · disintegrated · Nov 24, 2015 · N117WA · Emb EMB110P1 · Turbine Section
  > THE PILOT REPORTED THAT IN CRUISE, APPROX 20 MINUTES AFTER TAKEOFF, THE RT ENG SURGED MORE THAN ONCE & HE ELECTED TO SHUT IT DOWN. HE THEN DECLARED AN EMER & DIVERTED, MAKING A SUCCESSFUL LANDING. A VISUAL INSPECTION WITH BORESCOPE BY MX PERSONNEL REVEALED M
- [SDR AXSA20150910001](https://openairdocs.org/sdr/AXSA20150910001.md): Turbine Blades · loose · Sep 10, 2015 · N116WA · Emb EMB110P1 · Turbine Section
  > ON THE PILOTS PREFLIGHT, NOTICED A NOISE WHEN SPINNING THE RT PROP. THE ENG WAS INSPECTED, INSPECTION REVEALED THE POWER TURBINE BLADES WERE COMING LOOSE FROM THE POWER TURBINE DISK. THE ACFT WAS GNDED. A MORE IN-DEPTH INSPECTION WILL BE PERFORMED AT A LATE
- [SDR AXSA20150722001](https://openairdocs.org/sdr/AXSA20150722001.md): Transponder · smoke · Jun 30, 2015 · N119WA · Emb EMB110P1 · ATC Transponder System
  > PILOT REPORTED SMOKE COMING FROM BEHIND TRANSPONDER.
- [SDR CA131021008](https://openairdocs.org/sdr/CA131021008.md): Engine · malfunctioned · Oct 10, 2013 · Emb EMB110P1 · Engine (Turbine/Turboprop)
  > (CAN) ON LANDING, THE ACFT EXITED THE RUNWAY. DURING THE ON GROUND INVESTIGATION, THE ENGINEER AND THE PILOT ON SITE TRIED TO START THE ACFT ENGINES AND THE LT ENGINE ACCELERATED UNCONTROLLABLY CAUSING THE ITT TO FLASH AMBER AND THE TORQUE TO FLASH RED MOMENT
- [SDR AXSA20121227006](https://openairdocs.org/sdr/AXSA20121227006.md): Downlock Switch · obstructed · Dec 27, 2012 · N116WA · Emb EMB110P1 · Landing Gear Position and Warning
  > WHILE ON APPROACH INTO BTV, PILOT SELECTED GEAR DOWN AND NOTICED THAT THE INTRANSIT LIGHT REMAINED ON AND THE NOSE WHEEL LIGHT STAYED OFF. PILOT RECYCLED GEAR SEVERAL TIMES WITH NO CHANGE. PILOT PERFORMED EMERGENCY GEAR EXTENSION CHECKLIST AND PUMPED GEAR DO
- [SDR AXSA20120313002](https://openairdocs.org/sdr/AXSA20120313002.md): Fitting · cracked · Mar 13, 2012 · N115WA · Emb EMB110P1 · Hydraulic System, Main
  > CAE - ON GEAR EXTENSION GOT A HYDRAULIC FLUID LIGHT. TURNED MANUAL GEAR EXTENSION TO EMERGENCY. SHORTLY THEREAFTER GOT HYDRAULIC WARNING LIGHT. MANUALLY PUMPED GEAR AND VERIFIED THREE GREEN. ON EXIT FROM RUNWAY BRAKES WERE MARGINAL AND TUG WAS CALLED. MAI
- [SDR CA100831011](https://openairdocs.org/sdr/CA100831011.md): Brake Pads · missing · Aug 29, 2010 · Emb EMB110P1 · Landing Gear Brake System
  > DURING DAILY INSP, THE LT BRAKE UNIT WAS NOTICED TO HAVE THE AFT INBD BRAKE PAD MISSING.
- [SDR CA090305013](https://openairdocs.org/sdr/CA090305013.md): Duct · cracked · Mar 3, 2009 · Emb EMB110P1 · Turbine Engine Oil System
  > (CAN) DURING A DAILY INSP AN AME FOUND THE ENGINE OIL TO BE DIRTY AND IT HAD A YELLOWISH COLOR. FURTHER INSP OF THE ENGINE REVEALED A CRACKED INNER EXHAUST OUTLET DUCT. THE ENGINE WAS REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR CA080902005](https://openairdocs.org/sdr/CA080902005.md): Housing · broken · Aug 31, 2008 · Emb EMB110P1 · Main Landing Gear Strut/Axle/Truck
  > (CAN) WHEN LANDING AT THE AIRPORT ON A TRAINING FLIGHT THE NLG PARTIALLY RETRACTED TOWARDS THE REAR OF THE ACFT. THE ACFT PITCHED RT AND FULL LT BRAKE WAS USED TO KEEP THE ACFT ON THE RUNWAY. THE ACFT MOMENTARILY LT THE RT SIDE OF THE RUNWAY AND STRUCK A RUNWA
- [SDR CA080213009](https://openairdocs.org/sdr/CA080213009.md): Worm Drive · stripped · Nov 1, 2007 · Emb EMB110P1 · Trailing Edge Flap Actuator
  > (CAN) AFTER LANDING, THE WING FLAPS OF AN AC COULD NOT BE RETRACTED. THE ASYMMETRY WARNING SYSTEM HAD BEEN TRIPPED. THE LT AND RT FLAP ACTUATORS WERE REPLACED WITH OVERHAULED UNITS AND THE AC WAS DISPATCHED. UPON DISASSEMBLY OF THE ACTUATOR AT THE OVERHAUL SHO
- [SDR 2007FA0000917](https://openairdocs.org/sdr/2007FA0000917.md): Rod · broken · Aug 20, 2007 · N621KC · Emb EMB110P1 · Fuel Control/Reciprocating Engines
  > DURING A 150 HR INSPECTION THE LOWER FUEL CONTROL ROD WAS FOUND BROKEN ON THREADED SHAFT WHERE IT SCREWS INTO COUPLING. IT LOOKS LIKE IT MAY HAVE BEEN BENT AND A MORE DETAILED INSPECTION OF THIS COMPONENT SHOULD OCCUR. (K)
- [SDR CA070103009](https://openairdocs.org/sdr/CA070103009.md): Turbine Blades · fractured · Dec 10, 2006 · Emb EMB110P1 · Turbine Section
  > (CAN) DURING CRUISE ENGINE POWER REDUCED UNCOMMANDED, ACCOMPANIED BY A LOUD NOISE AND FLAMES EXITING THE EXHAUST. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER TURBINE BLADES AND A SEIZED REDUCTION GEARBOX. MFG WILL MONITOR INVESTIGATION OF THE EVENT AND AD
- [SDR CA061212005](https://openairdocs.org/sdr/CA061212005.md): Pump · failed · Dec 10, 2006 · Emb EMB110P1 · Hydraulic Pump (Electric/Engine), Main
  > (CAN) (5) MINUTES AFTER AN ENGINE FAILURE OF THE RT ENGINE (SDR 20061212001) THE HYDRAULIC LIGHT CAME ON EVEN THOUGH THE LT ENGINE WAS OPERATING NORMALLY. THE CREW ATTEMPTED TO EXTEND THE LANDING GEAR NORMALLY BUT IT WOULD NOT LOCK. THE GEAR WAS THEN SUCCESSFU
- [SDR CA061212001](https://openairdocs.org/sdr/CA061212001.md): Engine · failed · Dec 10, 2006 · Emb EMB110P1 · Engine (Turbine/Turboprop)
  > (CAN) SHORTLY AFTER COMPLETING THE DESCENT CHECKS FOR A LANDING (WITH ENGINES OPERATING NORMALLY, ENGINE INSTRUMENTS IN THE GREEN, THE CREW HEARD A LOUD NOISE FOLLOWED BY A SUDDEN LOSS OF POWER ON THE RT ENGINE. IMMEDIATELY FOLLOWING THE SUDDEN LOSS OF POWER T
- [SDR CA060810006](https://openairdocs.org/sdr/CA060810006.md): Support · cracked · Jul 26, 2006 · Emb EMB110P1 · Elevator, Tab Structure
  > (CAN) WHILE DOING AN INSPECTION OF THE LTO ELEVATOR AND ITS ASSOCIATED PARTS A CRACK WAS FOUND IN THE ELEVATOR BALANCE WEIGHT SUPPORT. THE CRACK MEASURED 2.3750 OF AN INCH IN LENGTH AND STARTED APPROXIMATELY 2 INCHES BELOW THE LOWER THROUGH-TUBE FOR THE BALA
- [SDR CA060720002](https://openairdocs.org/sdr/CA060720002.md): Channel · cracked · Jul 20, 2006 · Emb EMB110P1 · Nacelle/Pylon, Frame/Spar/Rib
  > (CAN) WHILE CARRYING OUT MAINTENANCE IN THE RT LANDING GEAR AREA, A CRACK WAS FOUND IN THE IB LOWER NACELLE CHANNEL. THIS NACELLE CHANNEL IS THE ATTACH POINT FOR THE INBOARD GEAR DOOR HINGE. THE CRACK WAS LOCATED IN AFT PORTION OF THE HINGE ATTACH AREA MEASUR
- [SDR CA060720001](https://openairdocs.org/sdr/CA060720001.md): Attach Bracket · cracked · Jun 21, 2006 · Emb EMB110P1 · Elevator Miscellaneous Structure
  > (CAN) DURING ROUTINE MAINTENANCE 2 CRACKS WERE DISCOVERED ON THE RT OB ELEVATOR HINGE ATTACH BRACKET. THE CRACKS WERE LOCATED ON THE LOWER FORWARD PORTION OF THE BRACKET IN THE MOST FORWARD PORTION OF A 90 DEGREE BEND AND WERE APPROX.7500 OF AN INCH IN LENGTH
- [SDR CA060607004](https://openairdocs.org/sdr/CA060607004.md): Blower · burned out · Jun 6, 2006 · Emb EMB110P1 · Cabin Cooling System
  > (CAN) SHORTLY AFTER START UP, THE GROUND VENTILATION FAN WAS TURNED ON AND SMOKE STARTED TO ENTER THE AIRCRAFT CABIN. MAINTENANCE FOUND THE GROUND VENT BLOWER TO BE AT FAULT. THE GROUND VENT BLOWER WAS REMOVED AND DEFERRED. THE AIRCRAFT WAS THEN RETURNED TO SE
- [SDR CA060411001](https://openairdocs.org/sdr/CA060411001.md): Propeller · malfunctioned · Apr 4, 2006 · Emb EMB110P1 · Propeller Governor
  > ON THE TAKEOFF ROLL, THE RT PROPELLER RPM WOULD ONLY GO TO 83% AND NOT BEYOND. THE AIRCRAFT RETURNED TO THE HANGAR WHERE MAINTENANCE FOUND THE RT PROPELLER TO BE AT FAULT. THE PROPELLER WAS REPLACED AND THE AIRCRAFT WAS RETURNED TO SERVICE. THE PROPELLER HA
- [SDR CA060328002](https://openairdocs.org/sdr/CA060328002.md): Channel · cracked · Mar 26, 2006 · Emb EMB110P1 · Horizontal Stabilizer Miscellaneous Structure
  > (CAN) DURING COMPLETION OF A 6C INSP, MAINT FOUND A CRACK IN THE FWD LT HORIZONTAL STABILIZER MACHINED CHANNEL. THIS PARTICULAR INSP WAS COMPLETED DUE TO AD 83-03-03R6 REQUESTING AN INITIAL INSP AND MODIFICATION OF ATTACHMENT AREA. INITIAL REQUIREMENTS WERE PR
- [SDR CA060214005](https://openairdocs.org/sdr/CA060214005.md): Blower · burned · Feb 13, 2006 · Emb EMB110P1 · Air Distribution Fan
  > (CAN) DURING CRUISE FLIGHT, WITH NO PASSENGERS ON BOARD, THE CREW NOTICED AN ELECTRICAL BURNING SMELL IN THE AIRCRAFT AND SMOKE IN THE CABIN. THE AIRCRAFT WAS DIVERTED TO THE NEAREST SUITABLE AIRPORT AND LANDED. UPON INVESTIGATION MAINTENANCE PERSONNEL DISCOVE
- [SDR AU510001504](https://openairdocs.org/sdr/AU510001504.md): Door · missing · Dec 12, 2005 · Emb EMB110P1 · Landing Gear Doors
  > RT MAIN LANDING GEAR INBOARD DOOR MISSING. HINGES AND DOOR OPERATING RODS BROKEN.
- [SDR CA051129016](https://openairdocs.org/sdr/CA051129016.md): Drive Shaft · fractured · Nov 5, 2005 · Emb EMB110P1 · Engine Fuel Pump
  > DURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION AND WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL PUMP DRIVE SHAFT.
- [SDR CA051104001](https://openairdocs.org/sdr/CA051104001.md): Spline · damaged · Oct 5, 2005 · Emb EMB110P1 · Engine Fuel Pump
  > (CAN) DURING CRUISE THE ENGINE WAS REPORTED TO HAVE LOST POWER AND THE CREW SHUTDOWN THE ENGINE IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A DAMAGED FUEL PUMP DRIVE SPLINE.
- [SDR CA051011006](https://openairdocs.org/sdr/CA051011006.md): Drive Assy · sheared · Oct 5, 2005 · Emb EMB110P1 · Engine Fuel Pump
  > IN CRUISE FLT AT 7000 FEET, NR 1 ENGINE LOST POWER. FLT CREW SECURED NR 1 ENGINE IAW APPLICABLE FLT MANUAL PROCEDURES AND LANDED A/C AT NEAREST AIRPORT. UPON INVESTIGATION, MX FOUND THAT CAUSE OF ENG FAILURE WAS DUE TO ENG DRIVEN FUEL PUMP. WHEN FUEL PUMP W
- [SDR CA050823001](https://openairdocs.org/sdr/CA050823001.md): Support · cracked · Aug 22, 2005 · Emb EMB110P1 · Trailing Edge Flaps
  > (CAN) DURING A ROUTINE INSPECTION, MAINTENANCE FOUND A CRACK IN THE RT FLAP ASYMMETRY TELEFLEX CABLE SUPPORT. THIS SUPPORT IS LOCATED ON THE RT FLAP IB SUPPORT AND IS ATTACHING POINT FOR ASYMMETRY DETECTOR TELEFLEX ROD END. FURTHER INVESTIGATION, A SECOND CRAC
- [SDR CA050615005](https://openairdocs.org/sdr/CA050615005.md): Angle · cracked · Jun 12, 2005 · Emb EMB110P1 · Elevator Tab, Attach Fittings
  > (CAN) DURING A ROUTINE MAINTENANCE INSPECTION 2 SMALL CRACKS WERE FOUND IN THE LT ELEVATOR TRIM TAB ACTUATOR SUPPORT BRACKET ATTACH POINT AREA. THE CRACKS WERE FOUND IN THE AREA AROUND THE 2 LOWER SUPPORT BRACKET BOLT HOLES. UPON FURTHER INVESTIGATION BOTH THE
- [SDR CA050420003](https://openairdocs.org/sdr/CA050420003.md): Hinge Bracket · cracked · Apr 18, 2005 · Emb EMB110P1 · Rudder Structure
  > (CAN) DURING A ROUTINE MAINTENANCE INSPECTION, A CRACK WAS FOUND ON THE RUDDER UPPER HINGE BRACKET. THIS BRACKET IS ATTACHED TO THE RUDDER FRONT SPAR AND ATTACHED TO THIS ARE TWO FLANGES FOR THE RUDDER UPPER HINGE BOLT. THE CRACK ON THE BRACKET EXTENDS FROM
- [SDR CA050418013](https://openairdocs.org/sdr/CA050418013.md): Angle · cracked · Apr 15, 2005 · Emb EMB110P1 · Elevator Miscellaneous Structure
  > INSP REVEALED CRACK ON LT ELEVATOR TRIM TAB ACTUATOR SUPPORT BRACKET ATTACH POINT REINFORCING ANGLE. CRACK FOUND AT UPPER LT SUPPORT BRACKET BOLT HOLE AND PROPAGATED TO RIVETS DIRECTLY ADJACENT TO HOLE ON BOTH LT AND RT SIDES. UPON FURTHER INVESTIGATION SM
- [SDR 2005FA0000360](https://openairdocs.org/sdr/2005FA0000360.md): Heater · leaking · Feb 24, 2005 · N83BA · Emb EMB110P1 · Fuel Heater
  > PILOT OBSERVED FLUCTUATING OIL PSI (100-70PSI) BROUGHT POWER BACK TO 200 LBS. TQ AND OIL PSI DROPPED TO 50 PSI. PILOT FEATHERED AND SHUTDOWN EFFECTED ENGINE. AFTER MECH INVESTIGATED THE PROBLEM, FOUND THAT FUEL HAD MIXED WITH THE OIL SUPPLY AND DILUTED IT TO
- [SDR CA050221008](https://openairdocs.org/sdr/CA050221008.md): Governor · malfunctioned · Feb 2, 2005 · Emb EMB110P1 · Propeller Governor
  > (CAN) DURING FLIGHT, THE PROPELLER SPEED DECREASED TO 80 PERCENT UNCOMMANDED. THE CREW COULD NOT MODULATE THE PROPELLER SPEED AND SHUT THE ENGINE DOWN IN FLIGHT. THE PROPELLER GOVERNOR WAS SUBSEQUENTLY REPLACED.
- [SDR CA050207002](https://openairdocs.org/sdr/CA050207002.md): Governor · uncontrollable · Feb 2, 2005 · Emb EMB110P1 · Propeller Governor
  > (CAN) THE AIRCRAFT WAS IN ENROUTE, WHEN THE RT ENGINE PROPELLER RPM DROPPED, UNCOMMANDED, TO 80 PERCENT. THE PROPELLER RPM COULD NOT BE CONTROLLED, NOR COULD THE PROPELLER BE FEATHERED, AND THE RT ENGINE WAS SHUTDOWN AS A PRECAUTION. THE AIRCRAFT RETURNED TO
- [SDR CA041215001](https://openairdocs.org/sdr/CA041215001.md): Exhaust Duct · cracked · Dec 14, 2004 · Emb EMB110P1 · Engine Collector/Tailpipe/Nozzle
  > (CAN) DURING ROUTINE MAINTENANCE 2 CRACKS WERE FOUND ON THE STARBOARD ENGINE EXHAUSTDUCT. THE CRACKS WERE LOCATED APPROXIMATELY 1.250 INCHES AFT OF THE REDUCTION GEARBOX MOUNTING FLANGE BETWEEN THE 10 AND 11:30 CLOCK POSITIONS. THE ORIGIN APPEARED TO BE FROM T
- [SDR BQT2004F00000](https://openairdocs.org/sdr/BQT2004F00000.md): Display · failed · Sep 10, 2004 · N49BA · Emb EMB110P1 · Weather Radar System
  > FLIGHT WITH CARGO ON BOARD, PILOT SAID RADAR SCREEN WENT BLANK. SHORTLY AFTER HE SAID THE COCKPIT STARTED TO FILL UP WITH SMOKE. RADIOED TOWER AND DIVERTED FROM INTENDED DESTINATION TO CLOSEST AIRPORT. LANDED WITHOUT INCIDENT WITH THE LOCAL FIRE DEPT STANDI
- [SDR CA040827006](https://openairdocs.org/sdr/CA040827006.md): Bolt · loose · Jul 9, 2004 · Emb EMB110P1 · Trailing Edge Flaps
  > (CAN) ON A WALK AROUND INSPECTION ONE OF FOUR BOLTS FOR THE OB LT FLAP DEFECTER WAS FOUND TO HAVE BACKED OFF.
- [SDR CA040708007](https://openairdocs.org/sdr/CA040708007.md): Engine · failed · Jul 6, 2004 · Emb EMB110P1 · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT, THE CREW OBSERVED THE LT ENGINE T5 TEMPERATURE STARTING TOFLUCTUATE FOLLOWED BY A COMPLETE LOSS OF T5 TEMPERATURE INDICATION. ONCE ON THE GROUND, DURING A TROUBLESHOOTING MAINTENANCE RUN, IT WAS ALSO OBSERVED THAT THE ENGINE WAS MAKING A
- [SDR CA031016001](https://openairdocs.org/sdr/CA031016001.md): Line · ruptured · Oct 15, 2003 · Emb EMB110P1 · Engine Fuel Distribution
  > (CAN) WHILE CARRYING OUT MAINTENANCE IN THE ACCESSORY SECTION AREA OF THE LT ENGINE (PT6A-34) A STRONG FUEL SMELL WAS NOTICED BY MAINTENANCE. A FURTHER INVESTIGATION REVEALED THAT WITH THE AIRFRAME FUEL BOOST PUMPS SELECTED ON THAT THERE WAS FUEL SPRAYING FRO
- [SDR CA030318014](https://openairdocs.org/sdr/CA030318014.md): Actuator · failed · Mar 6, 2003 · Emb EMB110P1 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) SHIMMY WHEN TAXIING & NECESSARY TO CENTRE THE NOSE GEAR MANUALLY IN ORDER TO GET THE GEARS TO RETRACT ON TAKEOFF. AFTER INVESTIGATION IN COLLABORATION WITH THE O/H FACILITY (THE GEAR WAS FRESHLY O/H), WE FOUND THAT IN THE NOSE STEERING RACK ACTUATOR, B
- [SDR CA030120007](https://openairdocs.org/sdr/CA030120007.md): Starter Gen · failed · Jan 17, 2003 · Emb EMB110P1 · Starter-Generator
  > (CAN) DURING A ROUTINE MAINTENANCE INSPECTION IN THE AREA AT THE REAR OF THE RT ENGINE COMPARTMENT IT WAS NOTICED THAT THERE WAS AN ABUNDANCE OF METALLIC DUST IN THE AREA SURROUNDING THE REAR OF THE STARTER GENERATOR. A THOROUGH INVESTIGATION REVEALED THE DUST
- [SDR CA030318012](https://openairdocs.org/sdr/CA030318012.md): Strut · broken · Nov 20, 2002 · Emb EMB110P1 · Nose/Tail Landing Gear Strut/Axle
  > (CAN) SHIMMY FROM NOSE GEAR WHEN TAXIING. AFTER DISASSEMBLING THE NLG OLEO STRUT ASSEMBLY, IT HAD BEEN FOUND BROKEN. (THE THREADED SECTION AT THE TOP WHERE NUT P/N 15134 SCREW ON.)CORRECTION: REPLACING NOSE GEAR ASSEMBLY FIXED THE PROBLEM. NO CAUSE HAVE BEEN

Next page: https://openairdocs.org/model/embraer-emb-110p1/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 = 'EMB110P1'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/embraer-emb-110p1/reports

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