# Pratt & Whitney JT8D-219 - Type: Engine model (FAA registry) - Registry code: 51694 - Manufacturer (registry): P & W - Model: JT8D-219 - Engine type: Turbo-fan - Power: 21,000 lb thrust - Data sheet: [TCDS E9NE](https://openairdocs.org/tcds/E9NE) (OpenAirDocs) - Holder: Pratt & Whitney - Installed in: 22 registered aircraft - Page: https://openairdocs.org/engine/pratt-whitney-jt8d-219 Model codes come from the FAA registry's reference file. ## ADs that may apply (OpenAirDocs) Matched to this engine model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment. - [AD 2021-22-19](https://openairdocs.org/ad/2021-22-19): Turbine Engine Compressor Section · Pratt & Whitney JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 2021 - [AD 2015-14-05](https://openairdocs.org/ad/2015-14-05): Cracking in the low-pressure turbine (LPT) shaft · Pratt & Whitney Division JT8D-217C and JT8D-219. Effective Aug 25, 2015 - [AD 2011-04-04](https://openairdocs.org/ad/2011-04-04): Critical life-limited parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 22, 2011 - [AD 97-17-04 R1](https://openairdocs.org/ad/97-17-04-R1): Front compressor front hub · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Apr 22, 2010 - [AD 2006-17-07 R1](https://openairdocs.org/ad/2006-17-07-R1): High pressure compressor (HPC) front hubs and HPC disk · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Nov 2, 2006 - [AD 2005-21-01](https://openairdocs.org/ad/2005-21-01): High pressure turbine (HPT) shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 21, 2005 - [AD 2005-17-16](https://openairdocs.org/ad/2005-17-16): Critical life-limited rotating parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Sep 30, 2005 - [AD 2004-26-04](https://openairdocs.org/ad/2004-26-04): HPT containment hardware · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 9, 2005 - [AD 2003-16-05](https://openairdocs.org/ad/2003-16-05): High pressure compressor (HPC) disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 12, 2003 - [AD 2002-21-17](https://openairdocs.org/ad/2002-21-17): Fan duct and fan exit guide vane · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Nov 29, 2002 - [AD 2002-16-08](https://openairdocs.org/ad/2002-16-08): Combustion Chamber Outer Case (CCOC) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 20, 2002 - [AD 99-10-11](https://openairdocs.org/ad/99-10-11): Fan Blades and Shrouds · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jun 14, 1999 - [AD 99-01-08](https://openairdocs.org/ad/99-01-08): Stage 7 through Stage 15 High-Pressure Compressor (HPC) Disks · Pratt & Whitney Division JT3D-1, JT3D-1-MC6, JT3D-1-MC7 and 30 more. Effective Jan 5, 1999 - [AD 98-21-24](https://openairdocs.org/ad/98-21-24): Compressor Disks · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Nov 16, 1998 - [AD 96-15-06](https://openairdocs.org/ad/96-15-06): First Stage Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Sep 3, 1996 - [AD 95-02-16](https://openairdocs.org/ad/95-02-16): Fuel Nozzle and Support Assembly · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 17 more. Effective Feb 21, 1995 - [AD 91-24-14](https://openairdocs.org/ad/91-24-14): Bearing Seal Spacer · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jan 21, 1992 - [AD 88-04-02](https://openairdocs.org/ad/88-04-02): Anti-rotation Pin Failures · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 4, 1988 - [AD 75-05-06](https://openairdocs.org/ad/75-05-06): Fuel Manifold Leakage · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Feb 24, 1977 - [AD 70-26-05](https://openairdocs.org/ad/70-26-05): First Stage Compressor Rotor Blades · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 29, 1970 - [AD 70-25-08](https://openairdocs.org/ad/70-25-08): Seventh Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Dec 15, 1970 - [AD 70-11-03](https://openairdocs.org/ad/70-11-03): Sixth Stage Compressor Discs · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Jun 12, 1970 - [AD 70-02-02](https://openairdocs.org/ad/70-02-02): Sixth Stage Compressor Rotor Disc · Pratt & Whitney Division JT8D-1, JT8D-11, JT8D-15 and 18 more. Effective Apr 15, 1970 Historical (superseded or no longer in force): - [AD 2011-07-02](https://openairdocs.org/ad/2011-07-02) (historical): Turbine Blade · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 28, 2011 - [AD 2006-17-07](https://openairdocs.org/ad/2006-17-07) (historical): Fretting and fluorescent magnetic particle inspections (FMPI) for cracking in the area of the tierod holes on the HPC front hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 18 more. Effective Oct 4, 2006 - [AD 2005-18-02](https://openairdocs.org/ad/2005-18-02) (historical): Engine manufacturer's time limits section (TLS) · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 28, 2006 - [AD 2005-02-03](https://openairdocs.org/ad/2005-02-03) (historical): Turbine (LPT) Blades 3rd and 4th Stage · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Mar 3, 2005 - [AD 2002-23-14](https://openairdocs.org/ad/2002-23-14) (historical): High Pressure Compressor (HPC) Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 31, 2002 - [AD 2002-13-09](https://openairdocs.org/ad/2002-13-09) (historical): Rotating engine parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 30, 2002 - [AD 2000-21-07](https://openairdocs.org/ad/2000-21-07) (historical): Critical Life-Limited Parts · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Apr 23, 2001 - [AD 99-26-06](https://openairdocs.org/ad/99-26-06) (historical): Combustion Chamber Outer Case · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 22, 2000 - [AD 99-27-01](https://openairdocs.org/ad/99-27-01) (historical): Low Pressure Turbine Blades · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Feb 2, 2000 - [AD 99-22-14](https://openairdocs.org/ad/99-22-14) (historical): High Pressure Turbine Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Dec 28, 1999 - [AD 99-12-04](https://openairdocs.org/ad/99-12-04) (historical): Critical Life Limited Part Inspection · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Jul 8, 1999 - [AD 97-19-13](https://openairdocs.org/ad/97-19-13) (historical): High Pressure Turbine (HPT) Shaft · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217A and 2 more. Effective Oct 24, 1997 - [AD 97-17-04](https://openairdocs.org/ad/97-17-04) (historical): Fan Hubs · Pratt & Whitney Division JT8D-209, JT8D-217, JT8D-217C and 1 more. Effective Sep 30, 1997 ## Information bulletins (advisory) (2) - [SAIB NE-16-22](https://openairdocs.org/saib/NE-16-22): Turbine Engine Combustion Section JT8D Series Turbofan Engines. Issued Sep 2, 2016 - [SAIB NE-10-32](https://openairdocs.org/saib/NE-10-32): Turbine Engine Accessory Drive. Issued May 7, 2010 ## Registered aircraft (22) - [N291EA](https://openairdocs.org/aircraft/N291EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53039 - [N292EA](https://openairdocs.org/aircraft/N292EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53208 - [N293EA](https://openairdocs.org/aircraft/N293EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53209 - [N294EA](https://openairdocs.org/aircraft/N294EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53210 - [N295EA](https://openairdocs.org/aircraft/N295EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53211 - [N296EA](https://openairdocs.org/aircraft/N296EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53212 - [N297EA](https://openairdocs.org/aircraft/N297EA): [Corsair Two LLC](https://openairdocs.org/faa-owner/CORSAIR%20TWO%20LLC), [Hillsboro, OR](https://openairdocs.org/faa-place/OR/Hillsboro), built 1991, S/N 53213 - [N637SH](https://openairdocs.org/aircraft/N637SH): [Pacific Aircorp 49741 Inc](https://openairdocs.org/faa-owner/PACIFIC%20AIRCORP%2049741%20INC), [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco), S/N 49568 - [N721MN](https://openairdocs.org/aircraft/N721MN): [Bd Md-87 LLC](https://openairdocs.org/faa-owner/BD%20MD-87%20LLC), [Longwood, FL](https://openairdocs.org/faa-place/FL/Longwood), built 1989, S/N 49767 - [N802WA](https://openairdocs.org/aircraft/N802WA): [Caribbean Sun Airlines Inc DBA](https://openairdocs.org/faa-owner/CARIBBEAN%20SUN%20AIRLINES%20INC%20DBA), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1990, S/N 53052 - [N805ML](https://openairdocs.org/aircraft/N805ML): [Smb Md-87 II LLC](https://openairdocs.org/faa-owner/SMB%20MD-87%20II%20LLC), [Longwood, FL](https://openairdocs.org/faa-place/FL/Longwood), S/N 49777 - [N807WA](https://openairdocs.org/aircraft/N807WA): [Federal Dynamics Corp](https://openairdocs.org/faa-owner/FEDERAL%20DYNAMICS%20CORP), [Henderson, NV](https://openairdocs.org/faa-place/NV/Henderson), built 1993, S/N 53093 - [N808WA](https://openairdocs.org/aircraft/N808WA): [Caribbean Sun Airlines Inc](https://openairdocs.org/faa-owner/CARIBBEAN%20SUN%20AIRLINES%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1990, S/N 53044 - [N831US](https://openairdocs.org/aircraft/N831US): [USA Jet Airlines Inc](https://openairdocs.org/faa-owner/USA%20JET%20AIRLINES%20INC), [Belleville, MI](https://openairdocs.org/faa-place/MI/Belleville), built 1989, S/N 49791 - [N832US](https://openairdocs.org/aircraft/N832US): [USA Jet Airlines Inc](https://openairdocs.org/faa-owner/USA%20JET%20AIRLINES%20INC), [Belleville, MI](https://openairdocs.org/faa-place/MI/Belleville), built 1991, S/N 53259 - [N83GF](https://openairdocs.org/aircraft/N83GF): [Wilmington Trust Co Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20CO%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1991, S/N 49950 - [N883GA](https://openairdocs.org/aircraft/N883GA): [Falcon Commercial Aviation LLC](https://openairdocs.org/faa-owner/FALCON%20COMMERCIAL%20AVIATION%20LLC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1988, S/N 49710 - [N887GA](https://openairdocs.org/aircraft/N887GA): [Rising Sun Aviation LLC](https://openairdocs.org/faa-owner/RISING%20SUN%20AVIATION%20LLC), [Irving, TX](https://openairdocs.org/faa-place/TX/Irving), built 1990, S/N 49932 - [N963CE](https://openairdocs.org/aircraft/N963CE): [Arctic One LLC](https://openairdocs.org/faa-owner/ARCTIC%20ONE%20LLC), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1994, S/N 53450 - [N967CE](https://openairdocs.org/aircraft/N967CE): [Arctic One LLC](https://openairdocs.org/faa-owner/ARCTIC%20ONE%20LLC), [Fairbanks, AK](https://openairdocs.org/faa-place/AK/Fairbanks), built 1996, S/N 49855 - [N982CA](https://openairdocs.org/aircraft/N982CA): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1986, S/N 49415 - [N986AK](https://openairdocs.org/aircraft/N986AK): [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 1989, S/N 49412 ## NTSB investigations (10) 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 DCA25WA176](https://openairdocs.org/ntsb/DCA25WA176), Mar 31, 2025: Mcdonnell Douglas MD 83 (N802WA), Havana, Cuba, incident, no damage - [NTSB DCA24WA282](https://openairdocs.org/ntsb/DCA24WA282), Jun 2, 2024: Mcdonnell Douglas MD 83 (N802WA), Santa Clara, Cuba, incident, minor damage - [NTSB ENG24LA012](https://openairdocs.org/ntsb/ENG24LA012), Mar 1, 2024: Mcdonnell Douglas DC-9-87 (N296EA), Missoula, MT, incident, minor damage. Probable cause: The use of a new long term fire retardant with a chemical composition incompatible with the retardant previously in use for the integration-operational field evaluation without adequate testing and… - [NTSB DCA18WA247](https://openairdocs.org/ntsb/DCA18WA247), Jul 11, 2018: Douglas DC9 (N802WA), Chichen Itza, Mexico, incident, no damage - [NTSB DCA18FA144](https://openairdocs.org/ntsb/DCA18FA144), Apr 20, 2018: Mcdonnell Douglas DC 9 83(MD-83) (N807WA), Alexandria, LA, substantial damage. Probable cause: the failure of the right main landing gear under normal loads due to fatigue cracking in an area subject to an FAA Airworthiness Directive that was not adequately inspected. - [NTSB ENG17IA017](https://openairdocs.org/ntsb/ENG17IA017), Mar 19, 2017: Douglas DC 9 83 (N881GA), Dayton, OH, incident, no damage. Probable cause: The probable cause of the No. 2 (right) engine fire was an uncontained generator failure. Deformed rotating generator components and/or metal fragments radially released by the generator severed the… - [NTSB DCA17FA076](https://openairdocs.org/ntsb/DCA17FA076), Mar 8, 2017: Mcdonnell Douglas MD80 (N786TW), Ypsilanti, MI, substantial damage. Probable cause: the jammed condition of the airplane's right elevator, which resulted from exposure to localized, dynamic wind while the airplane was parked and rendered the airplane unable to rotate during takeoff.… - [NTSB OPS17IA003](https://openairdocs.org/ntsb/OPS17IA003), Oct 21, 2016: Douglas DC 9 83 (N425NV), Westfield, MA, incident, no damage. Probable cause: The air traffic controller issuing the aircraft a clearance to land while there was a vehicle authorized to be on the same runway. Contributing to the incident was the air traffic controller's… - [NTSB OPS11IA686](https://openairdocs.org/ntsb/OPS11IA686), Jun 27, 2011: Mcdonnell Douglas DC-9-83(MD-83) (N416NV), Apache Junction, AZ, incident, no damage. Probable cause: The failure of the pilots of both airplanes to see and avoid each other and to maneuver as advised by the air traffic controller in time to prevent the conflict that resulted in the reported near… - [NTSB SEA94IA103](https://openairdocs.org/ntsb/SEA94IA103), Apr 18, 1994: Mcdonnell Douglas MD-83 (N931AS), Seattle, WA, incident, minor damage. Probable cause: THE FATIGUE FRACTURE OF A MAIN GEAR WHEEL HUB. ## FAA accident and incident reports (35) 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 20220311012649I](https://openairdocs.org/incident/20220311012649I), Mar 11, 2022: Mcdonnell Douglas Aircraft Co MD-88 (N832US), Iag, NY, No damage. On March 11, 2022 at 5:42 local 2242Z, an incident involving[privacy data omitted]Niagara Falls International Airport, Niagara Falls NY (Iag) to willow run… - [Incident 20180730018389I](https://openairdocs.org/incident/20180730018389I), Jul 30, 2018: Mcdonnell Douglas DC-9-87 (N291EA), Hayden Lake, ID, No damage. On takeoff, all things were normal up through takeoff power being applied and normal acceleration. At approximately V1 there was a sound from the back of the… - [Accident 20180420022279A](https://openairdocs.org/incident/20180420022279A), Apr 20, 2018: Mcdonnel Duglas DC-9-83 (N807WA), Alexandria, LA, Substantial damage. On April 20, 2018, at about 1935UTC (1435 CST), a caribbean sun airlines, MD83 (DC-9-83), N807WA, dba world atlantic airlines, right main landing gear… - [Incident 20180420014849I](https://openairdocs.org/incident/20180420014849I), Apr 20, 2018: Mcdonnell Douglas Aircraft Co MD-88 (N412NV), Savannah, GA, Minor damage. Pf=CA, pm=fo. Auto pilot was disconnected at approximately 1000'. Winds were calm. The captain was only making minor corrections with the ailerons. As he moved… - [Incident 20180408024949I](https://openairdocs.org/incident/20180408024949I), Apr 8, 2018: Mcdonnell Douglas DC-9-83(MD-83) (N429NV), Sioux Falls, SD, Minor damage. On Sunday, April 8, 2018, at 1024 local, allegiant air flight: aay 456, N429NV, a Mcdonnell Douglas DC-9-83, from mccarran international airport (las vegas,… - [Incident 20170330005159I](https://openairdocs.org/incident/20170330005159I), Mar 30, 2017: Douglas DC-9-83 (N883GA), Mesa, AZ, No damage. During climb the LH engine was not Producing full power. Between low Teens up to 10000 our climb rate was About 500FPM. Initial engine numbers On climb LH 1.98… - [Incident 20170319012909I](https://openairdocs.org/incident/20170319012909I), Mar 19, 2017: Douglas DC-9-83 (N881GA), Vandalia, OH, No damage. Rt engine failure followed by engine fire @ 14000' 280KTS. Fire would not extinguish. Used both fire bottles. Removed and replaced right engine and failed… - [Accident 20170308005569A](https://openairdocs.org/incident/20170308005569A), Mar 8, 2017: Mcdonnell Douglas DC-9-83(MD-83) (N786TW), Yipsilanti, MI, Substantial damage. Flight crew began take-off from runway 23 left. Captain rejected take-off above V1 because the aircraft would not pitch up to rotation atitude upon application… - [Incident 20161201018889I](https://openairdocs.org/incident/20161201018889I), Dec 1, 2016: Mcdonnell Douglas DC-9-83(MD-83) (N406NV), St Pete Clearwa, FL, No damage. Aircraft was being towed without ATC clearance. Tug driver qualifications were revoked until retraining could be accomplished. Airports division is also… - [Incident 20160201003549I](https://openairdocs.org/incident/20160201003549I), Feb 1, 2016: Douglas DC-9-83 (N881GA), Grand Island, NE, No damage. Approximately five minutes after reaching FL 360, cabin altitude master warning illuminated. Emergency descent. Cabin lost pressurization. Oxygen masks… - [Incident 20160103019099I](https://openairdocs.org/incident/20160103019099I), Jan 3, 2016: Mcdonnell Douglas DC-9-83(MD-83) (N875GA), Grand Junction, CO, No damage. At 33000 cruise we felt the aircrft shudder and heard a bang. The right engine spooled down EGT went to 800C run qrh 72.3 and secured right engine landed in… - [Incident 20151231023219I](https://openairdocs.org/incident/20151231023219I), Dec 31, 2015: Douglas DC-9-83 (N405NV), Chattanooga, TN, No damage. Flt level 320 low vibration of aircraft followed by N1 roll back of r engine and EGT rise to 800 c ran qrh 72.3 and secured engine. - [Incident 20150913019719I](https://openairdocs.org/incident/20150913019719I), Sep 13, 2015: Mcdonnell Douglas DC-9-87 (N291EA), Fresno, CA, No damage. Aircraft departed fat RWY29R on a public use fire mission for the united states forest service (usfs). After departure, the pilot reported that he had lost… - [Incident 20150817013669I](https://openairdocs.org/incident/20150817013669I), Aug 17, 2015: Mcdonnell Douglas DC-9-83(MD-83) (N407NV), Las Vegas, NV, No damage. Flight AAY436, aircraft N407NV an MD-83 was on takeoff roll, at approximately 120 KTS the nose started to come up, crew pushed yoke full forward and nose still… - [Incident 20140519008239I](https://openairdocs.org/incident/20140519008239I), May 19, 2014: Mcdonnell Douglas DC-9-83(MD-83) (N415NV), Mesa, AZ, No damage. During the final walk thru after the departure announcement [privacy data omitted] was walking to the aft of the aircraft and thought she could smell smoke… - [Incident 20130916025169I](https://openairdocs.org/incident/20130916025169I), Sep 16, 2013: Mcdonnell Douglas DC-9-83(MD-83) (N415NV), Las Vegas, NV, Minor damage. Allegiant air LLC flight 436 operating from Las Vegas, Nevada to peoria, Illinois evacuated passengers on ramp in front of the airport fire department.… - [Incident 20121228028819I](https://openairdocs.org/incident/20121228028819I), Dec 28, 2012: Mcdonnell Douglas DC-9-82(MD-82) (N886GA), Fort Wayne, IN, No damage. At approx 1515EST local, gl-roc informed this office that at 1805Z, allegiant flt 959 enroute from ksbn to kpgd with 154 persons on board, had declared an… - [Incident 20120715011999I](https://openairdocs.org/incident/20120715011999I), Jul 15, 2012: Mcdonnell Douglas DC-9-83(MD-83) (N416NV), Des Moines, IA, Minor damage. N416NV, a MD-83 was departing from Des Moines International Airport runway 23 as allegiant air (WX0A) flight 497 at or around 20:05 local time with 150… - [Incident 20120603010789I](https://openairdocs.org/incident/20120603010789I), Jun 3, 2012: Mcdonnell Douglas DC-9-83 (MD-83) (N424NV), Grand Island, NE, Minor damage. On June 3, 2012, at approximately 1231 CDT, the RH MLG on allegiant air, LLC, Mcdonnell Douglas MD-83, N424NV, became stuck in the mud as the PIC attempted to… - [Incident 20110125001809I](https://openairdocs.org/incident/20110125001809I), Jan 25, 2011: Mcdonnell D MD 83 (N802WA), Latham, NY, No damage. On January 25, 2001, the flight crew of aircraft departed westover air-reserve base (kcef) en-route to bradford regional airport (kbfd) in bradford,… - [Incident 20100910045339I](https://openairdocs.org/incident/20100910045339I), Sep 10, 2010: Mcdonnell D DC-9-82(MD- (N887GA), Lake Charles, LA, Minor damage. Aircraft departing Lake Charles Regional on rwy.15. Aircraft left main gear struck threshold lights at end of runway. Tire tracks in dirt indicate aircraft… - [Incident 20100725040959I](https://openairdocs.org/incident/20100725040959I), Jul 25, 2010: Mcdonnell D DC-9-83(MD- (N880GA), Flagstaff, AZ, Minor damage. WX0A flight 625 declared an emergency becasue of a fre indication in the #2 engine and diverted to Flagstaff, Arizona. Passengers were evacuated via slides… - [Incident 20100430032929I](https://openairdocs.org/incident/20100430032929I), Apr 30, 2010: Mcdonnell D MD-88 (N414NV), Las Vegas, NV, Minor damage. Allegiant flight # 506, MD-88, N414NV, enroute to Las Vegas, blew a tire while departing fresno, CA. - [Incident 20091118051319I](https://openairdocs.org/incident/20091118051319I), Nov 18, 2009: Mcdonnell D DC-9-87 (N952MA), Wichita, KS, Minor damage. On November 18, 2009 flight 5813 departed runway 19R and at approximately 2000 feet AGL the flight crew heard a loud bang and the aircraft momentarily "lurched… - [Incident 20090104000099I](https://openairdocs.org/incident/20090104000099I), Jan 4, 2009: Doug DC983 (N875GA), Lincoln, NE, No damage. N875GA, DC-9-83, being operated by allegiant airlines as flight 443, enroute des moines, IA to las vegas, NV, reported to air traffic control that they had a… - [Incident 20080727842109I](https://openairdocs.org/incident/20080727842109I), Jul 27, 2008: Doug DC987 (N952MA), Reno, NV, Minor damage. (-23) Carrier ground crew personnel were in the break room upon aircraft arrival at gate C-11. A fuel truck that was fueling an aircraft at gate C-9 extended… - [Incident 20071210827779I](https://openairdocs.org/incident/20071210827779I), Dec 10, 2007: Doug DC983 (N883GA), Idaho Falls, ID, No damage. (-23) On Monday December 10, 2007, at 1937Z (1237 mountain time) an allegiant airlines (designator WX0A) Douglas DC-9-83, N883GA, s/n 49710 reported that while… - [Incident 20060704018609I](https://openairdocs.org/incident/20060704018609I), Jul 4, 2006: Doug DC983 (N591AA), Fresno, CA. (-23) During the takeoff phase at lift-off, the right engine (#2) experienced severe compressor stalls that required immediate shutdown of the engine. This… - [Incident 20020521013129I](https://openairdocs.org/incident/20020521013129I), May 21, 2002: Doug MD83 (N591AA), Wichita, KS. (-23) American airlines flt #1061 enroute ord-phx lost oil quantity on #2 engine, with oil temp rise. Shut down #2 engine and diverted into ict. Aircraft… - [Incident 20010928028069I](https://openairdocs.org/incident/20010928028069I), Sep 28, 2001: Doug DC982 (N448AA), Rochester, NY. (-23) On September 28, 2001, about 1030 EST, a Douglas DC-9-82, N448AA, flight 1271, operated by American airlines inc, during powerback on the ramp, ran the… - [Incident 19970306004429I](https://openairdocs.org/incident/19970306004429I), Mar 6, 1997: Doug DC983 (N591AA), Rochester, NY, Minor damage. Narrative: on March 6, 1997, an American airlines DC-9-83, N591AA, was taxiing to runway 22 at Rochester/monroe county airport (roc) for take-off. The pilot… - [Incident 19960311006669I](https://openairdocs.org/incident/19960311006669I), Mar 11, 1996: Doug DC982 (N931AS), Oakland, CA, Minor damage. Bird strike on takeoff LH main gear severed hydraulic lines landed pdx ok. Bent gear door rod. - [Incident 19940417029239I](https://openairdocs.org/incident/19940417029239I), Apr 17, 1994: Doug DC982 (N931AS), Seattle, WA, Minor damage. After taxi into gate area tower advised smoke from landing gear. Evacuated wheel hub fractured. Replaced. - [Incident 19930821034109I](https://openairdocs.org/incident/19930821034109I), Aug 21, 1993: Doug DC982 (N931AS), Portland, OR, Minor damage. Hydraulic failure after takeoff. Returned. Right gear door dragged on runway. Slat hydraulic line loose. - [Incident 19900909053709I](https://openairdocs.org/incident/19900909053709I), Sep 9, 1990: Doug DC982 (N448AA), Elko, NV. Erratic passenger demanded to speak to the captain. Due to likelyhood of a bomb threat made a precautionary landing ## Service difficulty reports (1,944, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR FXGA07292025001](https://openairdocs.org/sdr/FXGA07292025001), Jul 29, 2025: DUCT CLAMP. LEAKING. TAIL COMPARTMENT TEMP HIGH ILLUMINATED, FOUND #2 ENGINE BLEED AIR LEAK IN TAIL SECTION, REPLACED CLAMP IAW MD-80 AMM 20-10-11. GROUND RUN-UP OPERATIONAL CHECK G - [SDR FXGA07292025002](https://openairdocs.org/sdr/FXGA07292025002), Jul 29, 2025: OVERHEAT SENSOR. ACTIVATED. TAIL COMPARTMENT TEMP HIGH ILLUMINATED, REPLACED R/H TAIL COMPARTMENT TEMP SENSOR IAW MD-80 AMM 36-20-02. OPERATIONAL CHECK GOOD - [SDR FXGA07302025001](https://openairdocs.org/sdr/FXGA07302025001), Jul 29, 2025: DUCT. CRACKED. TAIL COMPARTMENT TEMP HIGH LIGHT ILLUMINATED DURING CLIMB. FOUND RT BLEED AIR SOURCE DUCT WELD BROKEN. REMOVED AND REPLACED 13THSTAGE BLEED AIR SOURCE DUCTING B - [SDR 2WAA20250401086](https://openairdocs.org/sdr/2WAA20250401086), Mar 31, 2025: ENGINE. FAILED. LH ENGINE FAILURE AFTER TAKEOFF - [SDR 2024F00168](https://openairdocs.org/sdr/2024F00168), Jul 10, 2024: ENGINE. FAILED. SHORTLY AFTER TAKE OFF RIGHT ENGINE FAILED - [SDR FXGA20240426001](https://openairdocs.org/sdr/FXGA20240426001), Apr 25, 2024: UNLOCK CYLINDER. LEAKING. NOSE LANDING GEAR FAILED TO EXTEND WITH NORMAL MEANS, CYCLED GEAR AND NOSE GEAR EXTENDED NORMALLY. LANDED WITH NO FURTHER INCEDENT - [SDR FXGA20240417001](https://openairdocs.org/sdr/FXGA20240417001), Apr 16, 2024: HINGE. WORN. BIG VIBRATION FELT AFTER TAKEOFF IN AIRCRAFT AND YOKE. NOSE GEAR FORWARD DOORS CLOSING LINKAGE FOUND TO BE WORN - [SDR 2023F00301](https://openairdocs.org/sdr/2023F00301), Sep 19, 2023: FUEL CONTROL. SHEARED. #2 ENGINE THROTTLE WOULD NOT RESPOND TO MOVEMENT. ALL ENGINE INDICATIONS NORMAL AT CRUISE. RETURN TO KLRD RAN QRH FOR ENGINE FAILURE SHUTDOWN #2 ENGINE. INFORME - [SDR FXGA2021102001](https://openairdocs.org/sdr/FXGA2021102001), Nov 2, 2021: NONE. NONE. LEFT PAC SUPPLY PRESSURE DROPPED TO ZERO FOLLOWED BY LOSS OF PRESSURIZATION WHILE IN CRUISE TO ANC. FOUND LOOSE CLAMP AND DUCTING FROM ACM OUTPUT. - [SDR FXGA20210721001](https://openairdocs.org/sdr/FXGA20210721001), Jul 16, 2021: PUMP. FAULTED. CENTER FUEL PRESSURE LOW LIGHT ILLUMINATED/CENTER TANK FAILS TO FEED IN FLIGHT. RAN QRH PROCEDURE.(FOUND AFT CENTER FUEL TANK BOOST PUMP CIRCUIT BREAKER OPEN) - [SDR FXGA20210706](https://openairdocs.org/sdr/FXGA20210706), Jul 2, 2021: LINER. DELAMINATED. ON DEPARTURE #1 ENGINE COMMPRESSOR STALLS, REDUCED POWER AND RETURNED TO KLRD, UPON VISUAL INSPECTION TURBINE LINER WAS DELAMINATED FROM ENGINE TURBINE CASE. - [SDR FXGA202105270006](https://openairdocs.org/sdr/FXGA202105270006), May 25, 2021: GENERATOR. INOPERATIVE. LEFT GENERATOR OFF LIGHT ILLUMINATED IN FLIGHT. WHEN L GEN WAS RESET PER THE QRH THE AC CROSSTIE LOCKOUT LIGHT AND DC BUS OFF LIGHTS ALSO ILLUMINATED - [SDR FXGA20210328](https://openairdocs.org/sdr/FXGA20210328), Mar 26, 2021: FIRE DETECTOR. FALSE ACTIVATION. CARGO FIRE MASTER WARNING ILLUMINATED WITH LOWER AFT COMPARTMENT FIRE INDICATION. NO FIRE DETECTED AFTER LANDING. - [SDR FXGA20201026](https://openairdocs.org/sdr/FXGA20201026), Oct 26, 2020: CONTROL CABLE. BINDING. GEAR HANDLE STUCK IN UP POSITION, UNABLE TO LOWER THE GEAR IN BET ON FINAL APPROACH RWY 19. RETURN TO ANC, UNABLE TO LOWER THE FLAPS IN LANDING IN ANC, UNTIL 5 - [SDR 2020F00378](https://openairdocs.org/sdr/2020F00378), Aug 19, 2020: SLIDE. LOW PRESSURE. ON 8/19/20 DURING THE SERVICE CHECK ON N804WA, IT WAS DISCOVERED THAT THE L2 ESCAPE SLIDE {SN 1205} HAD LOW PRESSURE. - [SDR DALA2020030501639](https://openairdocs.org/sdr/DALA2020030501639), Mar 4, 2020: START VALVE. MALFUNCTIONED. R START VALVE OPEN ANNUNCIATED IN FLIGHT. SDR REPORTED DUE TO EMERGENCY DECLARED ACCORDING TO MCC EVENT NOTIFICATION. RT VALVE ANNUN ON EOAP ON ARRIVAL. R/R RT - [SDR DALA2020020700952](https://openairdocs.org/sdr/DALA2020020700952), Feb 6, 2020: DUCT. BLOWN. SHIP 965 -ATB- DUE TO NBR 1 ENGINE FIRE INDICATION. CREW REPORTED FIRE INDICATION PULLED THROTTLE BACK AND FIRE INDICATION EXTINGUISHED. CORRECTIVE ACTION: MAIN - [SDR DALA2020012600597](https://openairdocs.org/sdr/DALA2020012600597), Jan 25, 2020: ANGLE. CRACKED. 2EA CLIPS ARE CRACKED INSIDE #2 ENG NOSE COWL. REPLACED THE #2 NOSE COWL PER MD88 AMM 71-10-01 OFF PT # 5930645-509 S# DL 56 ON PT #5930654-509 S# 49416 FTN 91V - [SDR 2020FA0000204](https://openairdocs.org/sdr/2020FA0000204), Jan 8, 2020: FRAME. CRACKED. DURING 72-MONTH INSPECTION, CRACKING WAS DISCOVERED AT FRAME STA 1209. THE UPPER FRAME CAP IS CRACKED IN TWO LOCATIONS COMMON TO LONGERON 2L AND 2R. THE FRAME D - [SDR DALA2019112206845](https://openairdocs.org/sdr/DALA2019112206845), Nov 20, 2019: TIRE. FAILED. SDR REPORTED DUE TO NO 3 AND NO 4 TIRE COMING APART (ODI # 2019-00655) CAUSING COMPRESSOR DAMAGE TO NUMBER 2 ENGINE. THE TIRES WILL BE REPORTED ON A SEPARATE LO - [SDR DALA2019110406366](https://openairdocs.org/sdr/DALA2019110406366), Nov 3, 2019: ENGINE. OVERTEMP. SHIP 969 - IFSD & ATB - DUE TO LEFT ENGINE HIGH OIL TEMPERATURE. FLT CREW REPORTED AT 2000 FT THAT OIL TEMP WAS AT 165DEG AND WHEN POWER WAS ADDED, OIL TEMP WEN - [SDR DALA2019100405680](https://openairdocs.org/sdr/DALA2019100405680), Oct 4, 2019: ENGINE. FAILED. DURING TAKE OFF ROLL, AFTER 80 KNOTS, AIRCRAFT FELT A JOLT ON RIGHT SIDE AND A POPPING NOISE. THE RIGHT ENGINE EGT ROSE QUICKLY TOWARD 900 DEGREES. TAKE OFF WAS - [SDR DALA2019082905056](https://openairdocs.org/sdr/DALA2019082905056), Aug 28, 2019: ENGINE. FAILED. ATB - DUE TO RIGHT ENGINE ISSUES. FLT CREW REPORTED DURING CLIMB RIGHT OIL PRESSURE WENT TO 57 PSI AND FELT VIBRATION. FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN - [SDR DALA2019082304925](https://openairdocs.org/sdr/DALA2019082304925), Aug 22, 2019: VALVE. FAILED. DIVERTED DUE TO RIGHT ENGINE HIGH OIL TEMPERATURE. AFTER TAKEOFF OIL TEMP STEADILY CLIMBED TO 135DEG. FLT CREW SHUT DOWN ENGINE PER QRH. MAX OIL TEMP REACHED WA - [SDR DALA2019081904845](https://openairdocs.org/sdr/DALA2019081904845), Aug 19, 2019: GAUGE. FAILED. CREW LOST THE LT GENERATOR WHILE THE RT GENERATOR WAS ALREADY ON MEL. REPLACED LT ENG. GENERATOR, CSD, AND OIL COOLER. FLUSHED OIL LINES AND SERVICED CSD. FOUND - [SDR 2WAA20190820014](https://openairdocs.org/sdr/2WAA20190820014), Aug 14, 2019: ENGINE. FAILED. 1. RIGHT ENGINE FAILURE DURING CRUISE, FOLLOWED QRH PROCEDURES AND DIVERTED TO BRO, DECLAIRED EMERGENCY UNEVENTFUL LANDING. 2. DURING WALK-AROUND, DISCOVERED PA - [SDR DALA2019081104694](https://openairdocs.org/sdr/DALA2019081104694), Aug 11, 2019: ENGINE. FAILED. LEFT ENG FAILURE 2-4 SEC AFTER LIFT OFF ENGINE INDICATIONS SHOWED 0 PER N2 AND 0 PER NE EGT APROX 628 SHUT DOWN ENGINE IAW CHECKLIST. REPLACE NR 1 ENGINE ON SPC - [SDR AALA201908129019](https://openairdocs.org/sdr/AALA201908129019), Aug 7, 2019: PUMP. ERRATIC. AIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT ENGINE WANDERS AT CRUSE EPR 1.92 - 1.94 N1 92-94 N2 93-95 EGT FLEXS 5 534-539 (STABLE AT IDLE) (NO DIFFERENCE IF A/T I - [SDR AALA2019081209010](https://openairdocs.org/sdr/AALA2019081209010), Aug 7, 2019: FCU. ERRATIC. AIRCRAFT WAS GROUNDED: PILOT REPORTS LEFT ENGINE WONDERS AT CRUSE EPR 1.92 - 1.94 N1 92-94 N2 93-95 EGT FLEXS 5 534-539 (STABLE AT IDLE) (NO DIFFERENCE IF A/T I - [SDR DALA2019080604590](https://openairdocs.org/sdr/DALA2019080604590), Aug 5, 2019: TURBINE. DAMAGED. RETURNED TO DEPARTURE FOR ENGINE FAILURE. CREW REPORTED AT 3800' HEARD A COMPRESSOR STALL AND RIGHT ENGINE PARAMETERS ROLLED BACK AND EGT CLIMBED. FOLLOWED THE - [SDR DALA2019072604451](https://openairdocs.org/sdr/DALA2019072604451), Jul 17, 2019: ENGINE. FAULTY. SHIP 0956 (DIV) DIVERTED TO COS DUE TO A DUAL EGT AND N1 EXCEEDANCE DURING WINDSHEAR GO-AROUND. AIRCRAFT ENCOUNTERED MICRO-BURST AND WAS DIRECTED TO DIVERT TO C - [SDR DALA2019071104154](https://openairdocs.org/sdr/DALA2019071104154), Jul 10, 2019: ENGINE. MALFUNCTIONED. LEFT ENGINE FAILURE FL 310 CRUISE FLIGHT. DULL THUMP FOLLOWED BY MODERATE AIRFRAME VIBRATION. SHUT ENGINE DOWN. PERFORMING SEVERE ENGINE DAMAGE QRH CHECKLIST. I - [SDR DALA2019062403763](https://openairdocs.org/sdr/DALA2019062403763), Jun 23, 2019: ENGINE. SURGES. ON ARRIVAL AT 10K, STARTED A DESCENT TO 5K. PLANE STARTED TO GET SLOW, WENT TO V.S. TRP WAS IN CR. THROTTLE BURST CAUSED N1 EXCEEDENCE ON BOTH ENGINES. 104.5 FO - [SDR AALA201906199006](https://openairdocs.org/sdr/AALA201906199006), Jun 18, 2019: INDICATOR. FAULTY. AIRCRAFT WAS GROUNDED: RIGHT ENGINE OIL PRESSURE INDICATION FLASHED ON TAKEOFF AND INITIAL CLIMB. MAXIMUM PRESSURE OBSERVED WAS 56PSI. RIGHT OIL PRESSURE INDICA - [SDR AALA2019061329007](https://openairdocs.org/sdr/AALA2019061329007), Jun 10, 2019: GROUND WIRE. LOOSE. AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT ENGINE IDLE HIGH IN FLIGHT AND ON GROUND. GRD 1.08 EPR 37 N1 66 N2 FLT 1.14 EPR 57 N1 77 N2. MAINTENANCE SECURED GROU - [SDR DALA2019061323545](https://openairdocs.org/sdr/DALA2019061323545), Jun 8, 2019: COMPRESSOR. STALLED. IFSD & ATB - THE CREW RETURNED THE AIRCRAFT BACK TO DEPARTURE FOLLOWING THE FAILURE OF THE #1 ENGINE. THE LEFT ENGINE EXPERIENCED A COMPRESSOR STALL ON TAKEOFF, - [SDR DALA2019060323357](https://openairdocs.org/sdr/DALA2019060323357), Jun 1, 2019: GENERATOR. DISCONNECTED. AT 12,000 MSL, AUTO THROTTLES/AUTOPILOT DISCONNECTED L AC BUSS OFF, AND AC CROSS TIE LOCKOUT, L GEN OFF STALL IND FAIL, ON OAP, RAN QRH FOR LAC BUS OFF & AC CRO - [SDR DALA2019050302784](https://openairdocs.org/sdr/DALA2019050302784), May 3, 2019: ENGINE. MALFUNCTIONED. CLB PWR @ APPROX 6500 CLIMBING RT OIL QUANTITY WENT TO ZERO FOLLOWED BY RT OIL LOW MESSAGE. FOLLOWED QRH AND SHUT DOWN PER CHECKLIST. NO ABNORMAL APPROCH AND LA - [SDR AALA201904309027](https://openairdocs.org/sdr/AALA201904309027), Apr 27, 2019: FUEL CONTROL. UNRELIABLE. AIRCRAFT WAS GROUNDED: PILOT REPORTS PUSHED UP POWER FOR T/O, #2 RT ENGINE HAS NO EPR MOVEMENT, NO N1 MOVEMENT, VERY LITTLE N2, EGT 470 AND INCREASED W/ PUSH UP - [SDR DALA2019042982690](https://openairdocs.org/sdr/DALA2019042982690), Apr 26, 2019: ENGINE. FAILED. ON SHORT FINAL HEARD A LOUD BANG FOLLOWED BY NOTICEABLE YAW MOMENT TO THE LEFT. LEFT ENGINE INSTRUMENTS ROLLED BACK TO 1.02 EPR 20 PERCENT N1 EGT 525, N2 48 PER - [SDR DALA2019042002531](https://openairdocs.org/sdr/DALA2019042002531), Apr 19, 2019: STIFFENER. CRACKED. NOSE COWL CRACKED. INTERNAL FWD BULKHEAD STIFFENER AT 07:00 UPPER AND LOWER FAST. HOLES (2 AREAS)MARKED. INTERNAL FWD BULKHEAD STIFFENER AT 6:30 LOWER FAST. EXT - [SDR DALA2019040802291](https://openairdocs.org/sdr/DALA2019040802291), Apr 8, 2019: FUEL CONTROL. MALFUNCTIONED. AFTER TAKEOFF AND DURING CLIMB- B/W 8-10K L INLET FUEL PRESS. LO ILLUMINATED ON EOAP. RAN QRH- 12.22- ONCE ALL PUMPS WERE ON, ONLY 150LB. OF FUEL IN CENTER AT T - [SDR AALA201904031007](https://openairdocs.org/sdr/AALA201904031007), Apr 1, 2019: FCU. UNRELIABLE. AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT ENGINE ROLLED BACK TO IDLE WHILE SLOWING TO .74 MACH AT FL360.ENGINE HEAT WAS TURNED ON ALONG WITH RH FUEL HEAT.(-4) - [SDR AALA201904039014](https://openairdocs.org/sdr/AALA201904039014), Apr 1, 2019: PUMP. UNRELIABLE. AIRCRAFT WAS GROUNDED: PILOT REPORTS RIGHT ENGINE ROLLED BACK TO IDLE WHILE SLOWING TO .74 MACH AT FL360.ENGINE HEAT WAS TURNED ON ALONG WITH RH FUEL HEAT.(-4) - [SDR DALA2019031001552](https://openairdocs.org/sdr/DALA2019031001552), Mar 9, 2019: ENGINE. DAMAGED. PASSING 1100' IN CLIMB POWER, HEARD LOUD BANG FROM RIGHT ENGINE. RIGHT ENGINE ROLLED BACK AND STOPPED PRODUCING USEABLE THRUST. N1 APPROX 30 %. OIL PRESSURE 43 - [SDR DALA2019030201363](https://openairdocs.org/sdr/DALA2019030201363), Mar 1, 2019: ENGINE. MALFUNCTIONED. ON CLIMB OUT BETWEEN 14,500 AND 15,000 FEET WE HEARD A LOUD BANG ACCOMPANIED WITH AN AIRCRAFT SHUTTER AND NOTED LEFT ENGINE NO EPR, NO N1, EGT APPROX. 775, DID - [SDR DALA2019021871017](https://openairdocs.org/sdr/DALA2019021871017), Feb 16, 2019: DUCT. BLOWN. RIGHT ENGINE FIRE LIGHT BELLS PASSING APPROX. 800 FT ON TAKEOFF. NO ENGINE INDICATIONS OF FIRE OR DAMAGE. FIRE LIGHT WENT OUT BEFORE BLOWING FIRE BOTTLE OR SHUT - [SDR DALA2019021500962](https://openairdocs.org/sdr/DALA2019021500962), Feb 14, 2019: COOLER. LEAKING. DURING PAX BOARDING APU STARTED AND A/C PACKS TURNED ON . AFTER APPROX. 5 MINUTES WE SMELLED JET EXHAUST/ JET A FUMES IN CABIN. SHUT DOWN APU AND SMELL/ FUMES D - [SDR DALA2019021200940](https://openairdocs.org/sdr/DALA2019021200940), Feb 11, 2019: COMPRESSOR. STALLED. IFSD & ATB - DUE TO THE LOSS OF THE NR 1 ENGINE. AT APPROX 600FT AGL, FLT CREW REPORTED LEFT ENGINE COMPRESSOR STALL AND ENGINE ROLL BACK. CREW FOLLOWED QRH AND - [SDR AALA201901289014](https://openairdocs.org/sdr/AALA201901289014), Jan 26, 2019: BLEED VALVE. FAULTY. DESCENDING THROUGH FL 190, THE FORWARD PORTION OF AIRCRAFT EXPERIENCED A MODERATE BURNING RUBBER ODOR. DISSAPATED QUICKLY. ALL ELECTRICAL AND AIR CONDITION SYST All 1,944: https://openairdocs.org/engine/pratt-whitney-jt8d-219/reports.md ## STCs that may be installed (OpenAirDocs) (11) Approved for this engine 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 SE482CH](https://openairdocs.org/stc/SE482CH): Installation of Tube Processing Corporation (TPC) JT8D-200 Anti-Ice tube assemblies Part Numbers 2026-TP, 2027-TP, 2028-TP and 2029-TP and support brackets Part Number 2060-TP, 2061-TP, 2062-TP and 2063-TP. United Technologies Corporation, Pratt & Whitney Division - [STC SE01944LA](https://openairdocs.org/stc/SE01944LA): Installation of a JET Engineering, Ltd. Turbine Exhaust Cone Mixer (TECM). Jet Engineering LTD - [STC SE02128AT](https://openairdocs.org/stc/SE02128AT): Installation of a replacement ring manufactured by Praxair as part of the Praxair Second Stage Turbine inner air seal ring assembly. PAS Technologies Inc - [STC SE00429AT](https://openairdocs.org/stc/SE00429AT): Incorporate an alternate gear box stud installation. Jet Avion Corporation - [STC SE2117SO](https://openairdocs.org/stc/SE2117SO): Installation of an oil tank safety cap adapter which prevents loss of oil in the event of loss or damage to the oil filler cap. Jet Avion Corporation - [STC SE01650SE](https://openairdocs.org/stc/SE01650SE): Installation of Aviation Fleet Solutions MD-80 heavy weight noise abatement system. Aviation FLeet Solutions LLC - [STC SE2930SO](https://openairdocs.org/stc/SE2930SO): Installation of an alternate gearbox cover seal utilizing an aluminum retainer .040-inch thick with a molded-in-place elastomeric seal contoured to fit the main housing/cover flange interface. Parker O-Seal Division - [STC SE1683GL](https://openairdocs.org/stc/SE1683GL): Installation of Rexnord O-Ring face seal P/N's 1-1337-701, 1-1633-701, 1-1738-701, and/or1-2233-701. Rexnord, Inc - [STC SE86WE](https://openairdocs.org/stc/SE86WE): Replace the airoils on P&WA P/Ns 495051, 478351, 583751, 653851, 653951, 572451, 583351, 653751, 653151, 676951, 728951, 709951, 710751, 627751, 737271, 578551, 738271, 747171, 792871, 786471, 583751, 777971, 780591, 782571, 793181, 799771, 794481, 794491 , 798781, and 799191. Chromizing Company - [STC SE557NE](https://openairdocs.org/stc/SE557NE): Installation of oil tank shuttle valve. Stockbridge William D - [STC SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division ## PMA parts (OpenAirDocs) (over 1,000, first 50) Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this engine model on its data sheet, so check the FAA record before relying on it. Newest first. - [E800005](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID186250455020260305201703.0001): Bushing – Sleeve, .562 x .7523 x .290. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 800005 · Oct 28, 2024 - [570566](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148867501520260305211425.0001): Bushing – Diffuser Case, Assy of. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 570566 · Oct 28, 2024 - [E823652](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID102138852020260305201703.0001): Vane Cluster – Low Pressure Turbine, 2 Stage. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 823652 · Oct 28, 2024 - [823078-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID101644115520260305170151.0001): Housing Assy – Gearbox, Rear. Extex Engineered Products Inc. · PMA PQ2203NM · Replaces 823078-01 · Oct 28, 2024 - [VL1268PW95](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID137365938620240320173441.0001): Washer. Proponent Inc. · PMA PQ1383NM · Replaces 761768 · Mar 11, 2024 - [AA134S-1KT](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID184879292020230503123547.0001): Igniter Plug. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces AA134S-1 · Apr 27, 2023 - [RD1010](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119262724320230824100842.0001): Ring, Cut. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces 709237 · Apr 18, 2023 - [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192781976020231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023 - [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID179125890820240306163131.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023 - [1058V0100](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID177996651520231218190434.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 793304 Rev. B (10-18-82) · Apr 7, 2023 - [1058V0400-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID116398550720240306163132.0001): Start Bleed Control Valve. Goodrich Corporation · PMA PQ1352NM · Replaces 804848 Original 6/19/89 · Apr 7, 2023 - [1058V0400](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID198502891520230914183258.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 802211 Rev. ORIGINAL (6-21-85) · Mar 29, 2023 - [1058V0400-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID125479340120230914183259.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 806146 Rev. Original (7-1-88) · Mar 29, 2023 - [1058V0100-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID119161084320230914183256.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 804849 Rev. ORIGINAL (6-19-87) · Mar 29, 2023 - [1058V0600](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID115763985220230914183300.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 814099 Rev. Original (4-29-93) · Mar 29, 2023 - [1058V0700](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108551373220230914183257.0001): Start Bleed Control Valve. Honeywell International Inc. · PMA PQ1222NM · Replaces 803533 Rev. Original (2/25/87) · Mar 29, 2023 - [819771WD](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127249453620260805175346.0001): Bearing, Ball. Wencor LLC (formerly Dixie Aerospace LLC) · PMA PQ1630CE · Replaces 819771 · Jul 21, 2022 - [ST2273JP-07](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176398738120230330123014.0001): Pin. Jet Parts Engineering Inc · PMA PQ1739CE · Replaces ST2273-07 · Jul 6, 2021 - [DEC01- 039-501](https://drs.faa.gov/browse/excelExternalWindow/5A5B9C31B2BCC0F586258629005AC1D4.0001): Lever - Pressure Ratio Bleed Control. Turbine Kinetics Inc, A HEICO Aerospace Company · PMA PQ0816NE · Replaces 393909 · Nov 16, 2020 - [758308P10WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID903782019520210611172529.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P10W · Oct 15, 2020 - [758308WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID883733558820210611172526.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308 · Oct 15, 2020 - [758308P15WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID853154829220210611172530.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P15W · Oct 15, 2020 - [739585WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID766647496220210611172340.0001): Seal Face # 4 ½ Bearing. Wencor LLC · PMA PQ1370NM · Replaces 728982 · Oct 15, 2020 - [758308P20WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID740415996320210611172532.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P20W · Oct 15, 2020 - [758308P5WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID692977346202106111725280.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P5W · Oct 15, 2020 - [740259WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID435910374620210611172341.0001): Rivet-Tubular. Wencor LLC · PMA PQ1370NM · Replaces 740259 · Oct 15, 2020 - [738615WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID408467792120210611172335.0001): Seal-Face #6 Bearing. Wencor LLC · PMA PQ1370NM · Replaces 716299 · Oct 15, 2020 - [760016WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID248028746020210611172546.0001): Bolt-Externally Relieved Body, DH. Wencor LLC · PMA PQ1370NM · Replaces 760016 · Oct 15, 2020 - [758308P25WWE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID202417483920210611172533.0001): Seal-Ring. Wencor LLC · PMA PQ1370NM · Replaces 758308P25W · Oct 15, 2020 - [RD3003](https://drs.faa.gov/browse/excelExternalWindow/ECBA00B8EECE3F71862585D600471174.0001): Spacer, Sleeve. Jet Avion Corporation A HEICO Aerospace Company · PMA PQ1015CE · Replaces Pratt & Whitney P/N 781982 · Jul 8, 2020 - [F50030-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195391980820240703183033.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 744238 · Apr 1, 2020 - [H22-5PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID195032076420240703182915.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 395037 · Apr 1, 2020 - [K1000X4PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190779431820240703183043.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 753965 · Apr 1, 2020 - [F53816-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180597416120240703183054.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces ST1572-04 · Apr 1, 2020 - [K29109-4-2](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171669181720240703182950.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 638671 · Apr 1, 2020 - [F29964-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID171652783720240703182948.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 637285 · Apr 1, 2020 - [K39085-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170214002920240703183011.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 650410 · Apr 1, 2020 - [K2000-4CW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID168219310320240703183042.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 751942 · Apr 1, 2020 - [H29220-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID167914324120240703182958.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 639299 · Apr 1, 2020 - [F29724-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165439618320240703182932.0001): Nut, plain, bbl. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 594405 · Apr 1, 2020 - [CN29116-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID162022931620240703182945.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 627798 · Apr 1, 2020 - [H29220-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID160362046020240703183000.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 639335 · Apr 1, 2020 - [MF49663-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID158888513120240703183015.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 677828 · Apr 1, 2020 - [H29908-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147545014320240703182947.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 627799 · Apr 1, 2020 - [F29724-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147155505220240703183018.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 696690 · Apr 1, 2020 - [MK2000-3PW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147150668320240703183028.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 715018 · Apr 1, 2020 - [K29109-4-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145462505320240703182954.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 638674 · Apr 1, 2020 - [MF39839-4](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143884569520240703183032.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 743080 · Apr 1, 2020 - [F5000-4CWPW](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143552543320240703183039.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces 751929 · Apr 1, 2020 - [H49513-3](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142433141520240703183102.0001): Nut, S-L. Arconic Global Fasteners & Rings, Inc., dba Arconic Fastening Systems · PMA PQ1351NM · Replaces ST2119-09 · Apr 1, 2020 All of them: https://openairdocs.org/engine/pratt-whitney-jt8d-219/pma.md --- 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.