# Embraer EMB-110P1

- Type: Aircraft model (FAA registry)
- Registry code: 3260122
- Manufacturer (registry): EMBRAER
- Model: EMB-110P1
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-prop
- Seats: 20
- Weight class: 12,500 to 19,999 lb
- Certification: Type certificated
- Data sheet: [TCDS A21SO](https://openairdocs.org/tcds/A21SO) (OpenAirDocs)
- Holder: Embraer S.A.
- Registered aircraft: 13
- Page: https://openairdocs.org/model/embraer-emb-110p1

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.

- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2014-20-05](https://openairdocs.org/ad/2014-20-05): Flight Controls · Embraer EMB-110P1 and EMB-110P2. Effective Oct 27, 2014
- [AD 2008-23-12](https://openairdocs.org/ad/2008-23-12): Wings-to-fuselage attachments · Embraer EMB-110P1 and EMB-110P2. Effective Dec 22, 2008
- [AD 2005-19-02](https://openairdocs.org/ad/2005-19-02): Nose landing gear (NLG) · Embraer EMB-110P1 and EMB-110P2. Effective Oct 19, 2005
- [AD 2005-18-20](https://openairdocs.org/ad/2005-18-20): "FASTprop" propeller de-icers · Hartzell PHC-C3YF-1RF/F8468A(B,K)-8R constant speed propeller (STC SA00718LA or 17 others). Effective Oct 14, 2005
- [AD 2005-01-19](https://openairdocs.org/ad/2005-01-19): Mode S transponders · GARMIN International GTX 330D, GTX 330, GTX 33D and 830 more. Effective Feb 23, 2005
- [AD 2000-02-27](https://openairdocs.org/ad/2000-02-27): Airframe Pneumatic Deicing Boots · Embraer EMB-110P1 and EMB-110P2. Effective Mar 24, 2000
- [AD 98-01-10](https://openairdocs.org/ad/98-01-10): MLG Wheel Axle/ Piston Tube Assembly · Embraer EMB-110P1 and EMB-110P2. Effective Feb 9, 1998
- [AD 97-26-13](https://openairdocs.org/ad/97-26-13): AFM - Limitation Section - Power Levers · Embraer EMB-110P1 and EMB-110P2. Effective Jan 28, 1998
- [AD 97-01-12](https://openairdocs.org/ad/97-01-12): Ground Proximity Warning System · Airtell International Ground Proximity Warning System, Mystere-Falcon 200, EMB-110P1 and 20 more. Effective Feb 25, 1997
- [AD 96-09-12](https://openairdocs.org/ad/96-09-12): AFM - Icing · Embraer EMB-110P1 and EMB-110P2. Effective Jun 11, 1996
- [AD 92-17-02](https://openairdocs.org/ad/92-17-02): Rudder Trim Tab Actuating System · Embraer EMB-110P1 and EMB-110P2. Effective Sep 11, 1992
- [AD 91-25-11](https://openairdocs.org/ad/91-25-11): Rudder Trim Tab System · Embraer EMB-110P1 and EMB-110P2. Effective Feb 10, 1992
- [AD 91-25-09](https://openairdocs.org/ad/91-25-09): Elevator Trim Tab Actuator Support · Embraer EMB-110P1 and EMB-110P2. Effective Dec 23, 1991
- [AD 90-12-01](https://openairdocs.org/ad/90-12-01): Elevator Balance Weight Arms · Embraer EMB-110P1 and EMB-110P2. Effective Oct 15, 1990
- [AD 89-20-11](https://openairdocs.org/ad/89-20-11): AFM Change - Emergency Exit · Embraer EMB-110P1 and EMB-110P2. Effective Oct 24, 1989
- [AD 88-25-10](https://openairdocs.org/ad/88-25-10): Flap Control Switch · Embraer EMB-110P1 and EMB-110P2. Effective Jan 5, 1989
- [AD 87-13-08](https://openairdocs.org/ad/87-13-08): Airplane Flight Manual/Pilot's Operating Handbook Changes · Embraer EMB-110P1 and EMB-110P2. Effective Aug 6, 1987
- [AD 87-01-05](https://openairdocs.org/ad/87-01-05): Bearings - Flight Control Systems · Embraer EMB-110P1 and EMB-110P2. Effective Jan 22, 1987
- [AD 85-17-04](https://openairdocs.org/ad/85-17-04): Elevator Control Rod Tube · Embraer EMB-110P1 and EMB-110P2. Effective Aug 30, 1985
- [AD 85-01-51](https://openairdocs.org/ad/85-01-51): Empennage Assembly · Embraer EMB-110P1 and EMB-110P2. Effective Feb 26, 1985
- [AD 84-24-53 R1](https://openairdocs.org/ad/84-24-53-R1): Empennage Assembly · Embraer EMB-110P1 and EMB-110P2. Effective Jan 17, 1985
- [AD 82-05-01 R2](https://openairdocs.org/ad/82-05-01-R2): Wing Flap Actuators · Embraer EMB-110P1 and EMB-110P2. Effective Oct 26, 1983
- [AD 83-15-10](https://openairdocs.org/ad/83-15-10): Control Surface Balance · Embraer EMB-110P1 and EMB-110P2. Effective Aug 9, 1983
- [AD 83-14-09](https://openairdocs.org/ad/83-14-09): Rivet Attachments · Embraer EMB-110P1 and EMB-110P2. Effective Jul 27, 1983
- [AD 83-04-03 R1](https://openairdocs.org/ad/83-04-03-R1): Control Wheel Failure · Embraer EMB-110P1 and EMB-110P2. Effective Apr 25, 1983
- [AD 79-04-03 R2](https://openairdocs.org/ad/79-04-03-R2): Landing Gear · Embraer EMB-110P1 and EMB-110P2. Effective Feb 7, 1983
- [AD 82-27-09](https://openairdocs.org/ad/82-27-09): Primary Flight Control Cables · Embraer EMB-110P1 and EMB-110P2. Effective Jan 10, 1983
- [AD 82-20-02](https://openairdocs.org/ad/82-20-02): Icing Conditions · Embraer EMB-110P1 and EMB-110P2. Effective Sep 30, 1982
- [AD 82-18-01](https://openairdocs.org/ad/82-18-01): Water In Fuel Tank · Embraer EMB-110P1 and EMB-110P2. Effective Sep 27, 1982
- [AD 81-14-01](https://openairdocs.org/ad/81-14-01): Rudder Upper Hinge Support · Embraer EMB-110P1 and EMB-110P2. Effective Jul 1, 1981
- [AD 79-10-11](https://openairdocs.org/ad/79-10-11): Flight Control Rods · Embraer EMB-110P1 and EMB-110P2. Effective Dec 19, 1979
- [AD 79-24-05](https://openairdocs.org/ad/79-24-05): Wing Flap Supports · Embraer EMB-110P1 and EMB-110P2. Effective Nov 21, 1979

## Registered aircraft (13)

- [N113WA](https://openairdocs.org/aircraft/N113WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1979, S/N 110 205
- [N115WA](https://openairdocs.org/aircraft/N115WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1964, S/N 110451
- [N116WA](https://openairdocs.org/aircraft/N116WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1982, S/N 110.399
- [N117WA](https://openairdocs.org/aircraft/N117WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1982, S/N 110.388
- [N118WA](https://openairdocs.org/aircraft/N118WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1980, S/N 110.250
- [N120WA](https://openairdocs.org/aircraft/N120WA): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), built 1982, S/N 110.404
- [N316AF](https://openairdocs.org/aircraft/N316AF): [Agape Flights Inc](https://openairdocs.org/faa-owner/AGAPE%20FLIGHTS%20INC), [Venice, FL](https://openairdocs.org/faa-place/FL/Venice), built 1980, S/N 110.271
- [N34A](https://openairdocs.org/aircraft/N34A): [Royal Air Freight Inc](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FREIGHT%20INC), [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford), built 1981, S/N 110.350
- [N49RA](https://openairdocs.org/aircraft/N49RA): [Royal Air Freight Inc](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FREIGHT%20INC), [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford), built 1983, S/N 110.424
- [N621KC](https://openairdocs.org/aircraft/N621KC): [Hkb Aviation LLC](https://openairdocs.org/faa-owner/HKB%20AVIATION%20LLC), [San Antonio, TX](https://openairdocs.org/faa-place/TX/San%20Antonio), S/N 110.335
- [N64DA](https://openairdocs.org/aircraft/N64DA): [Royal Air Freight Inc](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FREIGHT%20INC), [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford), S/N 110.385
- [N72RA](https://openairdocs.org/aircraft/N72RA): [Royal Air Freight Inc](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FREIGHT%20INC), [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford), built 1981, S/N 110.377
- [N73RA](https://openairdocs.org/aircraft/N73RA): [Royal Air Freight Inc](https://openairdocs.org/faa-owner/ROYAL%20AIR%20FREIGHT%20INC), [Waterford, MI](https://openairdocs.org/faa-place/MI/Waterford), built 1982, S/N 110413

## NTSB investigations (20)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA26WA113](https://openairdocs.org/ntsb/DCA26WA113), Feb 5, 2026: Embraer EMB-110P1 (N316AF), Les Cayes, Haiti, destroyed, 2 fatal
- [NTSB ERA14IA249](https://openairdocs.org/ntsb/ERA14IA249), May 21, 2014: Embraer EMB-110P1 (N116WA), Warren, VT, incident, minor damage. Probable cause: The pilot's inadequate preflight inspection, which resulted in a total loss of engine power due to fuel exhaustion.
- [NTSB NYC06MA192](https://openairdocs.org/ntsb/NYC06MA192), Aug 4, 2006: Embraer 110P1 (N59BA), Pownal, VT, destroyed, 1 fatal. Probable cause: The pilot's misinterpretation of the airplane's position relative to the final approach fix, which resulted in the displacement of the descent profile by 6 nautical miles and the subsequent…
- [NTSB ATL06LA022](https://openairdocs.org/ntsb/ATL06LA022), Dec 10, 2005: Embraer EMB-110P1 (N790RA), Orangeburg, SC, substantial damage. Probable cause: The pilot's inadequate preflight inspection and her failure to refuel the airplane which resulted in total loss of engine power due to fuel exhaustion, and subsequent in-flight collision with trees.
- [NTSB NYC06FA027](https://openairdocs.org/ntsb/NYC06FA027), Nov 8, 2005: Embraer 110P1 (N7801Q), Manchester, NH, destroyed. Probable cause: The pilot’s misapplication of flight controls following an engine failure. Contributing to the accident was the failure of the sun gear, which resulted in the loss of engine power. Contributing to…
- [NTSB NYC05FA042](https://openairdocs.org/ntsb/NYC05FA042), Jan 14, 2005: Embraer EMB-110P1 (N49BA), Swanzey, NH, destroyed, 1 fatal. Probable cause: The pilot's improper decision to attempt a single-engine missed approach with the airplane in a slow airspeed, full flap configuration, which resulted in a minimum control speed (Vmc) roll.…
- [NTSB MIA91IA117](https://openairdocs.org/ntsb/MIA91IA117), Apr 5, 1991: Embraer EMB-110P1 (N102TN), Ochopee, FL, incident, minor damage. Probable cause: FAILURE OF THE STUDENT TO USE THE CHECKLIST, INADEQUATE SUPERVISION BY THE PIC/CFI, AND INADEQUATE SUPERVISION BY THE FAA PRINCIPLE OPERATIONS INSPECTOR.
- [NTSB ATL89FA142](https://openairdocs.org/ntsb/ATL89FA142), May 6, 1989: Embraer EMB-110-P1 (N95PB), Mt. Pleasant, TN, destroyed, 1 fatal. Probable cause: PILOT ATTEMPTED TO MAKE A VFR LANDING IN INSTRUMENT CONDITIONS THAT WERE BELOW MINIMUMS FOR THE PUBLISHED INSTRUMENT APPROACH AND COLLIDED WITH TREES AND THE GROUND AFTER ALLOWING THE AIRPLANE TO…
- [NTSB FTW88IA129](https://openairdocs.org/ntsb/FTW88IA129), Jul 9, 1988: Embraer EMB-110P1 (N91DA), Abilene, TX, incident, minor damage
- [NTSB DCA88MA059](https://openairdocs.org/ntsb/DCA88MA059), May 24, 1988: Embraer EMB-110P (N65DA), Lawton, OK, destroyed. Probable cause: NONE SUBMITTED
- [NTSB FTW88IA090](https://openairdocs.org/ntsb/FTW88IA090), Apr 13, 1988: Embraer EMB-110P1 (N905FB), Wichita Falls, TX, incident, minor damage
- [NTSB DCA86AA021](https://openairdocs.org/ntsb/DCA86AA021), Mar 14, 1986: Embraer EMB-110P1 (N1356P), Alpena, MI, destroyed, 3 fatal
- [NTSB CHI86IA037](https://openairdocs.org/ntsb/CHI86IA037), Dec 2, 1985: Embraer EMB-110P1 (N90427), Detroit, MI, incident, minor damage
- [NTSB ANC85LA020](https://openairdocs.org/ntsb/ANC85LA020), Nov 20, 1984: Embraer EMB-110 (N39174), Fairbanks, AK, substantial damage
- [NTSB MIA84IA160](https://openairdocs.org/ntsb/MIA84IA160), May 4, 1984: Embraer EMB-110P1 (N132EM), Miami, FL, incident, minor damage
- [NTSB ANC84MA037](https://openairdocs.org/ntsb/ANC84MA037), Feb 22, 1984: Embraer EM-110P1 (N103VA), Cordova, AK, substantial damage
- [NTSB CHI83IA103](https://openairdocs.org/ntsb/CHI83IA103), Feb 4, 1983: Embraer EMB-110 (N1356P), Milwaukee, WI, incident, minor damage
- [NTSB SEA82IA029](https://openairdocs.org/ntsb/SEA82IA029), Feb 18, 1982: Embraer EMB-11OP1 (N101RA), Boise, ID, incident, minor damage
- [NTSB ATL82IA034](https://openairdocs.org/ntsb/ATL82IA034), Jan 12, 1982: Embraer EMB-110P1 (N615KC), Clarksburg, WV, incident, minor damage
- [NTSB FTW81IA058](https://openairdocs.org/ntsb/FTW81IA058), Mar 25, 1981: Embraer 110P1 (N691RA), Lafayette, LA, incident, minor damage

## FAA accident and incident reports (105, newest 50)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20181116017259I](https://openairdocs.org/incident/20181116017259I), Nov 16, 2018: Embraer EMB-110P1 (N117WA), Plattsburgh, NY, Minor damage. Upon touchdown, aircraft veered to the right, departed the runway, and came to a rest in the grassy area just east of the runway, due to apparent frozen brake…
- [Incident 20180825018529I](https://openairdocs.org/incident/20180825018529I), Aug 25, 2018: Embraer EMB-110P1 (N118WA), Syracuse, NY, No damage. On 08/25/2018, wiggins airways EMB-110, N118WA was departing from syr on flight number 1346 to kptd. As the aircraft was leaving 3500?, the pilot stated they…
- [Incident 20151124018879I](https://openairdocs.org/incident/20151124018879I), Nov 24, 2015: Embraer EMB-110P1 (N117WA), Portland, ME, Minor damage. On 11/24/2015, EMB-110, N117WA on axsa flight # 1032 was in cruise at 5000 feet after departing mht to lew. The pilot felt and heard a strong surge from the…
- [Incident 20140521007849I](https://openairdocs.org/incident/20140521007849I), May 21, 2014: Embraer EMB-110P1 (N116WA), Warren, VT, Minor damage. On 5/21/2014, N116WA, an EMB-110-P1 operated by wiggins airways (axsa) was on a 135 cargo flight (#1042), from mht to btv with a load of ups cargo. [privacy…
- [Accident 20060804030739A](https://openairdocs.org/incident/20060804030739A), Aug 4, 2006: Emb EMB110P1 (N59BA), Pownal, VT, Destroyed, 1 fatal. (-23) On August 4, 2006, an Embraer model 110-P1, N59BA, serial number 110-396, registered to business air incorporated, doing business as (dba) air now,…
- [Accident 20051209029879A](https://openairdocs.org/incident/20051209029879A), Dec 9, 2005: Emb EMB110P1 (N790RA), Orangeburg, SC, Destroyed. (-23) On 12/10/05 aircraft was enroute from sav to cae when pilot declared minimum fuel and was diverted to ogb. Both left and right engines quit producing…
- [Accident 20051108030719A](https://openairdocs.org/incident/20051108030719A), Nov 8, 2005: Emb EMB110P1 (N7801Q), Manchester, NH, Destroyed. (-23) On November 8, 2005, at 0720, an Embraer Emb-110-P1 (commonly known as a bandeirante), registration N7801Q, registered to business air inc., operating as…
- [Accident 20050113000719A](https://openairdocs.org/incident/20050113000719A), Jan 13, 2005: Emb EMB110P1 (N49BA), Keene, NH, Destroyed, 1 fatal. (-23) The aircraft crashed during an ILS to runway 02 at the Keene/Dillant-Hopkins Airport (een). The aircraft was in IMC conditions during the approach. The…
- [Incident 20041214034119I](https://openairdocs.org/incident/20041214034119I), Dec 14, 2004: Emb EMB110P1 (N97BA), Louisville, KY. (-23) The aircraft departed kduj at 0432 gmt on an IFR 135 scheduled cargo flight to ksdf. While working sdf approach control, the pilot failed to comply with…
- [Incident 20040129002389I](https://openairdocs.org/incident/20040129002389I), Jan 29, 2004: Emb EMB110P1 (N34A), Pontiac, MI, Minor damage. (-23) The aircraft was dispatched from ptk at around 17:00 on 1/29/2004 to go to det and pick up a load of freight. The aircraft had been parked outside for…
- [Incident 19980326017209I](https://openairdocs.org/incident/19980326017209I), Mar 26, 1998: Emb EMB110P1 (N73RA), Buffalo, NY. Left main gear torque link key failed allowing wheel assy to rotate damaging tire.
- [Incident 19951212043939I](https://openairdocs.org/incident/19951212043939I), Dec 12, 1995: Emb EMB110P1 (N790RA), San Antonio, TX, Minor damage. Narrative: on December 12, 1995 bandeirante aircraft N790RA, model Emb-110, owned and operated by business air inc., departed corpus christi international at…
- [Incident 19920608022289I](https://openairdocs.org/incident/19920608022289I), Jun 8, 1992: Emb EMB110P1 (N91DA), Dallas-Ft Worth, TX. Experienced gear intransit light on. Hydraulic pressure fluctuating. Right main gear uplock switch out of adjustment
- [Incident 19910430021269I](https://openairdocs.org/incident/19910430021269I), Apr 30, 1991: Emb EMB110P1 (N91DA), Dallas-Ft Worth, TX. Slow right engine propeller speed on takeoff. Aborted. Adjusted propeller governor linkage.
- [Incident 19910405009039I](https://openairdocs.org/incident/19910405009039I), Apr 5, 1991: Emb EMB110P1 (N102TN), Miami, FL, Minor damage. Pilot stated on landing rollout the gear handle came up and gear retracted. FAA observer onboard.
- [Incident 19901010054839I](https://openairdocs.org/incident/19901010054839I), Oct 10, 1990: Emb EMB110P1 (N404AS), Dallas-Ft Worth, TX, Minor damage. Vibration on rollout. Pilot thought it was a flat tire. Left wheel assembly was found on runway.
- [Incident 19900530043829I](https://openairdocs.org/incident/19900530043829I), May 30, 1990: Emb EMB110P1 (N905FB), Dallas-Ft Worth, TX. Low hydraulic warning on approach. Used emergency system. Hydraulic t fitting cracked and leaking oil.
- [Incident 19900313013359I](https://openairdocs.org/incident/19900313013359I), Mar 13, 1990: Emb EMB110P1 (N84940), White Plains, NY. In deteriorating weather pilot advised ATC of low fuel. Requested alternate airport. Landed without incident.
- [Incident 19891114059399I](https://openairdocs.org/incident/19891114059399I), Nov 14, 1989: Emb EMB110P1 (N110SX), Pittsburgh, PA. Prop RPM surge after departure. Returned and landed without incident. Shut engine down while taxiing.
- [Incident 19890802057149I](https://openairdocs.org/incident/19890802057149I), Aug 2, 1989: Emb EMB110P1 (N61CZ), Marathon, FL, Minor damage. Propeller struck a runway light while turning onto taxiway. Stated light and taxiway line not visible at this point
- [Incident 19890531064909I](https://openairdocs.org/incident/19890531064909I), May 31, 1989: Emb EMB110P1 (N101WJ), Chicago, IL, Minor damage. Unable to retract gear on climb. Returned. Gear collapsed on rollout. Nose steering out of rig. Had misdrilled hole
- [Incident 19890509041129I](https://openairdocs.org/incident/19890509041129I), May 9, 1989: Emb EMB110P1 (N850AC), Burbank, CA. Right engine fire warning after climbout. Shut down and returned. Replaced all fire warning wires and probes.
- [Incident 19890508038799I](https://openairdocs.org/incident/19890508038799I), May 8, 1989: Emb EMB110P1 (N850AC), Burbank, CA. Right engine fire warning light. Engine shut down and diverted to Burbank. Found a broken fire warning probe light.
- [Accident 19890506010899A](https://openairdocs.org/incident/19890506010899A), May 6, 1989: Emb EMB110P1 (N95PB), Columbia/Mt Ple, TN, Destroyed, 1 fatal. Tried circling VFR after sdf approach at night with patchy ground fog. Saw airport but fog obscured it on approach.
- [Incident 19890111006189I](https://openairdocs.org/incident/19890111006189I), Jan 11, 1989: Emb EMB110P1 (N622KC), Fresno, CA. Right hand forward emergency door came open. Returned and landed safely.
- [Incident 19881104060949I](https://openairdocs.org/incident/19881104060949I), Nov 4, 1988: Emb EMB110P1 (N102TN), Omaha, NE. Gear not locked after takeoff. Gear against closed door. Returned. Door was loose at ball and socket connector.
- [Incident 19881024064949I](https://openairdocs.org/incident/19881024064949I), Oct 24, 1988: Emb EMB110P1 (N404AS), Dallas-Ft Worth, TX, Minor damage. Fumes in cabin while taxiing for takeoff,evacuated on taxiway. Found center console panel light rheostat faulty.
- [Incident 19881011055639I](https://openairdocs.org/incident/19881011055639I), Oct 11, 1988: Emb EMB110P1 (N104EB), Dallas-Ft Worth, TX. Left wing and propeller struck birds on climbout. No damage sustained.
- [Incident 19880914065019I](https://openairdocs.org/incident/19880914065019I), Sep 14, 1988: Emb EMB110P1 (N78CZ), Orlando, FL, Minor damage. Wake turbulence on final. Loud noise during recovery. Normal landing. Damaged gear door and hinge and lost rod.
- [Incident 19880901056759I](https://openairdocs.org/incident/19880901056759I), Sep 1, 1988: Emb EMB110P1 (N102TN), Omaha, NE. Right gear did not show locked after retracted. Returned and extended gear normally. Latch adjusted.
- [Incident 19880818052619I](https://openairdocs.org/incident/19880818052619I), Aug 18, 1988: Emb EMB110P1 (N622KC), Monterey, CA. Emergency landing due to smoke in cockpit. Evacuated passengers on runway. Found ground cooling fan arcing.
- [Incident 19880709027339I](https://openairdocs.org/incident/19880709027339I), Jul 9, 1988: Emb EMB110P1 (N91DA), Abilene, TX, Minor damage. Ballooned on landing with gear down then gear collapsed on second touchdown. No defects found. Possible pilot error
- [Accident 19880523069719A](https://openairdocs.org/incident/19880523069719A), May 23, 1988: Emb EMB110P1 (N65DA), Lawton, OK, Substantial damage. Lost left engine on liftoff. PIC failed to use proper engine out procedures below VMC. Crashed. Compressor failure.
- [Incident 19880413071019I](https://openairdocs.org/incident/19880413071019I), Apr 13, 1988: Emb EMB110P1 (N905FB), Wichita Falls, TX, Minor damage. Right engine cowling came off on climbout. Damaged control and broke cabin window. Worn elongated fastener holes.
- [Incident 19880123013799I](https://openairdocs.org/incident/19880123013799I), Jan 23, 1988: Emb EMB110P1 (N132EM), Arcata - Eureka, CA, Minor damage. Engine maintained power after power lever reduced to idle. Heavy braking blew tire. Replaced right fuel control unit
- [Incident 19880119011569I](https://openairdocs.org/incident/19880119011569I), Jan 19, 1988: Emb EMB110P1 (N62DA), Dallas-Ft Worth, TX, Minor damage. Made a hard landing and both main tires blew out on landing.
- [Incident 19871117074579I](https://openairdocs.org/incident/19871117074579I), Nov 17, 1987: Emb EMB110P1 (N134EM), Indianapolis, IN. Pilot declared minimum fuel on approach to Indianapolis. Landed without incident.
- [Incident 19871110071059I](https://openairdocs.org/incident/19871110071059I), Nov 10, 1987: Emb EMB110P1 (N110SX), Pittsburgh, PA, Minor damage. Aircraft lined up improperly for takeoff. Struck a runway edge light and flattened the nose tire. Departed runway.
- [Incident 19871026072489I](https://openairdocs.org/incident/19871026072489I), Oct 26, 1987: Emb EMB110P1 (N731A), Bakersfield, CA. A precuationary landing made due to low hydraulic quantity. A hydraulic ground test o ring was found to be leaking.
- [Incident 19870914068269I](https://openairdocs.org/incident/19870914068269I), Sep 14, 1987: Emb EMB110P1 (N91PB), Albany, NY, Minor damage. The wingtip struck a parked dot aircraft, N4, during taxi. Pilot reported the aircraft veered left.
- [Incident 19870903054979I](https://openairdocs.org/incident/19870903054979I), Sep 3, 1987: Emb EMB110P1 (N134EM), Indianapolis, IN. Fumes in cockpit during climbout. Returned to airport. Found oil in air machine ducting caused fumes.
- [Incident 19870803051259I](https://openairdocs.org/incident/19870803051259I), Aug 3, 1987: Emb EMB110P1 (N101RA), Fresno, CA, Minor damage. Takeoff aborted due to caution indication. Nose steering ineffective. Faulty circuit breaker on gear control.
- [Incident 19870406022519I](https://openairdocs.org/incident/19870406022519I), Apr 6, 1987: Emb EMB110P1 (N115MQ), Battle Creek, MI, Minor damage. The left main wheel became loose on landing. The safety was missing on the wheel attach nut.
- [Incident 19870301031759I](https://openairdocs.org/incident/19870301031759I), Mar 1, 1987: Emb EMB110P1 (N92PB), Hyannis, MA, Minor damage. Hard landing after encountering wind shear caused gear and wing damage.
- [Incident 19861223085279I](https://openairdocs.org/incident/19861223085279I), Dec 23, 1986: Emb EMB110P1 (N97PB), Hyannis, MA. The aircraft safely returned to the airport due to smoke in the cabin. Glycol had been spilled in engine bleed air.
- [Incident 19860728051019I](https://openairdocs.org/incident/19860728051019I), Jul 28, 1986: Emb EMB110P1 (N91DA), Memphis, TN. Engine shut down at cruise after a loud noise from engine with maximum T5 temperature. Engine replaced.
- [Incident 19860624034049I](https://openairdocs.org/incident/19860624034049I), Jun 24, 1986: Emb EMB110P1 (N59PB), Allentown, PA. Returned after gear intransit light remained on.
- [Incident 19860611029089I](https://openairdocs.org/incident/19860611029089I), Jun 11, 1986: Emb EMB110P1 (N101WJ), Houston, TX. Right engine flamed out. Restarted after switching fuel tanks. Landed due to fuel imbalance. Dripless stick replaced.
- [Incident 19860425023839I](https://openairdocs.org/incident/19860425023839I), Apr 25, 1986: Emb EMB110P1 (N115MQ), Detroit, MI. ATC clearance to land on runway 21L. Noted aircraft on final for 21C and ATC clearance for landing 21C issued.
- [Incident 19860418049919I](https://openairdocs.org/incident/19860418049919I), Apr 18, 1986: Emb EMB110P1 (N202EB), Memphis, TN. Smoke from instrument panel after turning cockpit lights on. Short in lighting circuit board.

All 105: https://openairdocs.org/model/embraer-emb-110p1/incidents.md

## Service difficulty reports (176, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR AXSA202205120002](https://openairdocs.org/sdr/AXSA202205120002), May 12, 2022: SMOKE DETECTOR. FALSE ACTIVATION. 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 W
- [SDR 2022F00200](https://openairdocs.org/sdr/2022F00200), Apr 7, 2022: LAMP. BROKEN. 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 I
- [SDR AXSA202204270001](https://openairdocs.org/sdr/AXSA202204270001), Apr 6, 2022: LAMP. BROKEN. 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 SHO
- [SDR AXSA2020061200001](https://openairdocs.org/sdr/AXSA2020061200001), Jun 11, 2020: CONTROL UNIT. DEFECTIVE. LOST BOTH GENERATORS IN FLIGHT
- [SDR AXSA2019061400019](https://openairdocs.org/sdr/AXSA2019061400019), Jun 14, 2019: BLADES. CRACKED. DURING A HOT SECTION 3 CT BLADES WERE FOUND TO BE CRACKED AT THE FIR TREE.
- [SDR AXSA2018082700001](https://openairdocs.org/sdr/AXSA2018082700001), Aug 25, 2018: ENGINE. UNKNOWN. 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 EM
- [SDR AXSA2017121100001](https://openairdocs.org/sdr/AXSA2017121100001), Dec 8, 2017: ACCUMULATOR. EMPTY. 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), Apr 6, 2016: CONNECTOR. DIRTY. 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), Jan 28, 2016: ROD END. WORN. 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 
- [SDR AXSA20150107001](https://openairdocs.org/sdr/AXSA20150107001), Jan 6, 2016: LINK. DETACHED. 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 TECHNICIA
- [SDR AXSA2015112590038](https://openairdocs.org/sdr/AXSA2015112590038), Nov 24, 2015: TURBINE WHEEL. DISINTEGRATED. 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 & DI
- [SDR AXSA20150910001](https://openairdocs.org/sdr/AXSA20150910001), Sep 10, 2015: TURBINE BLADES. LOOSE. 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 T
- [SDR AXSA20150722001](https://openairdocs.org/sdr/AXSA20150722001), Jun 30, 2015: TRANSPONDER. SMOKE. PILOT REPORTED SMOKE COMING FROM BEHIND TRANSPONDER.
- [SDR CA131021008](https://openairdocs.org/sdr/CA131021008), Oct 10, 2013: ENGINE. MALFUNCTIONED. (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 
- [SDR AXSA20121227006](https://openairdocs.org/sdr/AXSA20121227006), Dec 27, 2012: DOWNLOCK SWITCH. OBSTRUCTED. 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 S
- [SDR AXSA20120313002](https://openairdocs.org/sdr/AXSA20120313002), Mar 13, 2012: FITTING. CRACKED. CAE - ON GEAR EXTENSION GOT A HYDRAULIC FLUID LIGHT. TURNED MANUAL GEAR EXTENSION TO EMERGENCY. SHORTLY THEREAFTER GOT HYDRAULIC WARNING LIGHT. MANUALLY PUMPED 
- [SDR CA100831011](https://openairdocs.org/sdr/CA100831011), Aug 29, 2010: BRAKE PADS. MISSING. DURING DAILY INSP, THE LT BRAKE UNIT WAS NOTICED TO HAVE THE AFT INBD BRAKE PAD MISSING.
- [SDR CA090305013](https://openairdocs.org/sdr/CA090305013), Mar 3, 2009: DUCT. CRACKED. (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 OUTL
- [SDR CA080902005](https://openairdocs.org/sdr/CA080902005), Aug 31, 2008: HOUSING. BROKEN. (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 
- [SDR CA080213009](https://openairdocs.org/sdr/CA080213009), Nov 1, 2007: WORM DRIVE. STRIPPED. (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 W
- [SDR 2007FA0000917](https://openairdocs.org/sdr/2007FA0000917), Aug 20, 2007: ROD. BROKEN. 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 
- [SDR CA070103009](https://openairdocs.org/sdr/CA070103009), Dec 10, 2006: TURBINE BLADES. FRACTURED. (CAN) DURING CRUISE ENGINE POWER REDUCED UNCOMMANDED, ACCOMPANIED BY A LOUD NOISE AND FLAMES EXITING THE EXHAUST. SUBSEQUENT INSPECTION REVEALED FRACTURED POWER
- [SDR CA061212005](https://openairdocs.org/sdr/CA061212005), Dec 10, 2006: PUMP. FAILED. (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 C
- [SDR CA061212001](https://openairdocs.org/sdr/CA061212001), Dec 10, 2006: ENGINE. FAILED. (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 F
- [SDR CA060810006](https://openairdocs.org/sdr/CA060810006), Jul 26, 2006: SUPPORT. CRACKED. (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
- [SDR CA060720002](https://openairdocs.org/sdr/CA060720002), Jul 20, 2006: CHANNEL. CRACKED. (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 FO
- [SDR CA060720001](https://openairdocs.org/sdr/CA060720001), Jun 21, 2006: ATTACH BRACKET. CRACKED. (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 TH
- [SDR CA060607004](https://openairdocs.org/sdr/CA060607004), Jun 6, 2006: BLOWER. BURNED OUT. (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 T
- [SDR CA060411001](https://openairdocs.org/sdr/CA060411001), Apr 4, 2006: PROPELLER. MALFUNCTIONED. 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 B
- [SDR CA060328002](https://openairdocs.org/sdr/CA060328002), Mar 26, 2006: CHANNEL. CRACKED. (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-
- [SDR CA060214005](https://openairdocs.org/sdr/CA060214005), Feb 13, 2006: BLOWER. BURNED. (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 D
- [SDR AU510001504](https://openairdocs.org/sdr/AU510001504), Dec 12, 2005: DOOR. MISSING. RT MAIN LANDING GEAR INBOARD DOOR MISSING. HINGES AND DOOR OPERATING RODS BROKEN.
- [SDR CA051129016](https://openairdocs.org/sdr/CA051129016), Nov 5, 2005: DRIVE SHAFT. FRACTURED. DURING CRUISE, THE ENGINE EXPERIENCED AN UNCOMMANDED POWER REDUCTION AND WAS SHUT DOWN IN FLIGHT. SUBSEQUENT INSPECTION REVEALED A FRACTURED FUEL PUMP DRIVE SHA
- [SDR CA051104001](https://openairdocs.org/sdr/CA051104001), Oct 5, 2005: SPLINE. DAMAGED. (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 DR
- [SDR CA051011006](https://openairdocs.org/sdr/CA051011006), Oct 5, 2005: DRIVE ASSY. SHEARED. 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 IN
- [SDR CA050823001](https://openairdocs.org/sdr/CA050823001), Aug 22, 2005: SUPPORT. CRACKED. (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 
- [SDR CA050615005](https://openairdocs.org/sdr/CA050615005), Jun 12, 2005: ANGLE. CRACKED. (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 
- [SDR CA050420003](https://openairdocs.org/sdr/CA050420003), Apr 18, 2005: HINGE BRACKET. CRACKED. (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 ATTACH
- [SDR CA050418013](https://openairdocs.org/sdr/CA050418013), Apr 15, 2005: ANGLE. CRACKED. 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 PROPA
- [SDR 2005FA0000360](https://openairdocs.org/sdr/2005FA0000360), Feb 24, 2005: HEATER. LEAKING. 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. AF
- [SDR CA050221008](https://openairdocs.org/sdr/CA050221008), Feb 2, 2005: GOVERNOR. MALFUNCTIONED. (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
- [SDR CA050207002](https://openairdocs.org/sdr/CA050207002), Feb 2, 2005: GOVERNOR. UNCONTROLLABLE. (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 TH
- [SDR CA041215001](https://openairdocs.org/sdr/CA041215001), Dec 14, 2004: EXHAUST DUCT. CRACKED. (CAN) DURING ROUTINE MAINTENANCE 2 CRACKS WERE FOUND ON THE STARBOARD ENGINE EXHAUSTDUCT. THE CRACKS WERE LOCATED APPROXIMATELY 1.250 INCHES AFT OF THE REDUCTIO
- [SDR BQT2004F00000](https://openairdocs.org/sdr/BQT2004F00000), Sep 10, 2004: DISPLAY. FAILED. 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
- [SDR CA040827006](https://openairdocs.org/sdr/CA040827006), Jul 9, 2004: BOLT. LOOSE. (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), Jul 6, 2004: ENGINE. FAILED. 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 
- [SDR CA031016001](https://openairdocs.org/sdr/CA031016001), Oct 15, 2003: LINE. RUPTURED. (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 INVESTIG
- [SDR CA030318014](https://openairdocs.org/sdr/CA030318014), Mar 6, 2003: ACTUATOR. FAILED. (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 WIT
- [SDR CA030120007](https://openairdocs.org/sdr/CA030120007), Jan 17, 2003: STARTER GEN. FAILED. (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 I
- [SDR CA030318012](https://openairdocs.org/sdr/CA030318012), Nov 20, 2002: STRUT. BROKEN. (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 

All 176: https://openairdocs.org/model/embraer-emb-110p1/reports.md

## STCs that may be installed (OpenAirDocs) (76, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC SA02019SE-D](https://openairdocs.org/stc/SA02019SE-D): Installation of Garmin Model GTN 625/635/650; 725/750 Navigation System. Garmin International Inc
- [STC SA00039BO](https://openairdocs.org/stc/SA00039BO): Incorporation of cockpit panel modifications to support single pilot operations without an autopilot. Ameriflight LLC
- [STC SA00132BO](https://openairdocs.org/stc/SA00132BO): Removal of right side windshield heating element. Ameriflight LLC
- [STC SA00405BO](https://openairdocs.org/stc/SA00405BO): De-modification of SFAR 41A compliance. Ameriflight LLC
- [STC SA00517NY](https://openairdocs.org/stc/SA00517NY): Modification of air conditioning system. Ameriflight LLC
- [STC SA01184AT](https://openairdocs.org/stc/SA01184AT): Remove passenger windows and overwing exits and replace with plugs. Modify airstair steps. Ameriflight LLC
- [STC SA02658SE](https://openairdocs.org/stc/SA02658SE): Installation of Garmin GI 275 Multi-Function Display System. Garmin International Inc
- [STC SA814GL](https://openairdocs.org/stc/SA814GL): Installation of nose wheel. Kaman Corporation Aircraft Wheel and Brake LLC
- [STC SA02075SE](https://openairdocs.org/stc/SA02075SE): Installation of a Mid-Continent MD835( ) Lithium Ion Battery. Mid-Continent Instrument Co. Inc
- [STC SA04514NY](https://openairdocs.org/stc/SA04514NY): Single/Dual Transponder System ADS-B Upgrade. Scandinavian Avionics Design ApS
- [STC SA01714WI](https://openairdocs.org/stc/SA01714WI): Installation of a Garmin transponders: (a) GTX 330/330D/33/33D with ADS-B Out functionality; (b) GTX 335/335R/345/345R with ADS-B Out and In functionality; or (c) GTX 335R/345R with ADS-B Out functionality in select airplanes installed with G950/G1000 systems. Garmin International Inc
- [STC SA04330NY](https://openairdocs.org/stc/SA04330NY): Installation of Pitot Heat Failure Warning System. Kenn Borek Air Limited
- [STC SA04165NY](https://openairdocs.org/stc/SA04165NY): Installation of Latitude Technologies Skynode S200 Satcom system must be performed. Latitude Technologies Corporation
- [STC SA01933LA-D](https://openairdocs.org/stc/SA01933LA-D): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA03973NY](https://openairdocs.org/stc/SA03973NY): Replacement of existing TCAS 7.0 by TCAS 7.1. Scandinavian Avionics Design ApS
- [STC SA00382BO](https://openairdocs.org/stc/SA00382BO): Installation of Globalstar Antenna and Cradle provisions to support a Globalstar GPS-1700 in non-composite airplanes. 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 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 SA01229SE PAGE 1](https://openairdocs.org/stc/SA01229SE%20PAGE%201): Installation of GNS 480 (CNX80) GPS WAAS Navigator with integrated VHF Navigation and Communication radios. Garmin International Inc
- [STC SA01933LA-D PAGE 1](https://openairdocs.org/stc/SA01933LA-D%20PAGE%201): Installation of Garmin Model 400W / 500W Series GPS-WAAS Navigation System. Garmin International Inc
- [STC SA02121SE](https://openairdocs.org/stc/SA02121SE): Installation of Garmin GTS 825 (TAS) or GTS 855 (TCAS I) Traffic System. Garmin International Inc
- [STC SA1330GL](https://openairdocs.org/stc/SA1330GL): Revert to Normal Category (14 CFR 23) aircraft vice SFAR 41A by modifying the aircraft. American Eagle Airlines, Inc
- [STC SA01692SE](https://openairdocs.org/stc/SA01692SE): Installation of a Garmin GMX 200 Multi-Function Display. Garmin International Inc
- [STC SA03148NY](https://openairdocs.org/stc/SA03148NY): The installation of the Latitude Technologies Corporation S100 Tracking System. Latitude Technologies Corporation
- [STC SA01487SE-D](https://openairdocs.org/stc/SA01487SE-D): Installation of a GDL 69 or GDL 69A XM Satellite Receiver. Garmin International Inc
- [STC SA00243BO](https://openairdocs.org/stc/SA00243BO): 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 SA178NE](https://openairdocs.org/stc/SA178NE): Remove existing starter-generator and install Aircraft Parts starter generator. Skurka Aerospace Inc
- [STC ST02540AT-D](https://openairdocs.org/stc/ST02540AT-D): Installation of replacement fuel tank sealant system. FFC Manufacturing
- [STC SA01473SE](https://openairdocs.org/stc/SA01473SE): Installation of a GTX 32 (mode C), GTX 33 (mode S), or GTX 33D (mode S with diversity) Remote Transponde. Garmin AT Inc
- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc
- [STC SA01695SE](https://openairdocs.org/stc/SA01695SE): Installation of an antenna. Garmin AT Inc
- [STC SP00400SE](https://openairdocs.org/stc/SP00400SE): Installation of various propeller electrical de-icer models. SMR Technologies
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies
- [STC SA01046CH](https://openairdocs.org/stc/SA01046CH): Installation of SMR Technologies engine inlet anti-icer models. SMR Technologies Inc
- [STC SA01487SE](https://openairdocs.org/stc/SA01487SE): Installation of a GDL 69 or GDL 69A XM Satellite Receiver in accordance with Garmin Supplemental Type Certificate Master Data List, P/N 005-C0217-00, Revision A, dated December 20, 2004, or later FAA approved revision. Garmin AT Inc
- [STC SA4381NM](https://openairdocs.org/stc/SA4381NM): Installation of Cockpit Sun Visor. Rosen Sunvisor Systems LLC. Lists EMB-110 Series
- [STC SA02154AK](https://openairdocs.org/stc/SA02154AK): Installation of the UPS Aviation Technologies Inc. Apollo MX20 multi-function display, P/N 430-0270-500. Garmin AT Inc
- [STC SA02217AK](https://openairdocs.org/stc/SA02217AK): Installation of Garmin AT Model GDL90 UAT Data Link System, in accordance with Garmin AT, Inc., GDL 90 UAT Master Data List, P/N 560-0278-01, Revision A, dated November 12, 2004, or later FAA approved revision. Garmin AT Inc
- [STC SA4962NM](https://openairdocs.org/stc/SA4962NM): Installation of a NSA sunvisor system for the pilot and copilot. Rosen Sunvisor Systems LLC
- [STC SA00823CH](https://openairdocs.org/stc/SA00823CH): Installation of various de-icer wire harnesses. SMR Technologies
- [STC SA00694SE](https://openairdocs.org/stc/SA00694SE): Replacement of certain BF Goodrich pneumatic deicer boots. SMR Technologies
- [STC SA812NE](https://openairdocs.org/stc/SA812NE): Installation of BF Goodrich Model 6975-1 De-Icer kit or BF Goodrich Model 6975-10 De-Icer kit. BF Goodrich Aerospace
- [STC SA5576SW](https://openairdocs.org/stc/SA5576SW): Installation of tail floodlight system. DeVore Aviation Corporation of America, a New Mexico Corporation
- [STC SA00883AT-D](https://openairdocs.org/stc/SA00883AT-D): Installation and operation of an AlliedSignal TCAS CAS 66A System installed. Air Sunshine, Inc
- [STC ST01558AT](https://openairdocs.org/stc/ST01558AT): Installation of an AlliedSignal MK-VI Ground Proximity Warning System (GPWS). Air Sunshine, Inc. Lists EMB-110 Series
- [STC SA00231DE](https://openairdocs.org/stc/SA00231DE): Reconfigure aircraft to a maximum seating of Nine (9) passengers. Leading Edge Aviation Svcs
- [STC SA1167SO](https://openairdocs.org/stc/SA1167SO): Replace existing nickel-cadmium batteries with Teledyne Gill BB638/T series lead-acid battery. Teledyne Battery Products
- [STC SA00884AT-D](https://openairdocs.org/stc/SA00884AT-D): Installation and operation of an AlliedSignal TCAS CAS 66A System. East Coast Avionics, Inc
- [STC SA02020AK](https://openairdocs.org/stc/SA02020AK): Installation of ground proximity warning system. Centaurus Systems, Inc
- [STC SA00634AT](https://openairdocs.org/stc/SA00634AT): Installation of Dayton-Granger dischargers. Dayton-Granger, Inc

All 76: https://openairdocs.org/model/embraer-emb-110p1/stcs.md

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