# Pratt & Whitney JT8D-5 - Type: Engine model (FAA registry) - Registry code: 52046 - Manufacturer (registry): P & W - Model: JT8D-5 - Engine type: Turbo-jet - Power: 12,250 lb thrust - Data sheet: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Holder: Pratt & Whitney - Installed in: 0 registered aircraft - Page: https://openairdocs.org/engine/pratt-whitney-jt8d-5 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 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 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 80-15-51](https://openairdocs.org/ad/80-15-51): Engine Rear Compressor Front Hubs · Pratt & Whitney Division JT8D-209, JT8D-1, JT8D-11 and 11 more. Effective Aug 21, 1980 - [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 ## Registered aircraft None registered with this engine model now. ## NTSB investigations (22) 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 DFW07LA155](https://openairdocs.org/ntsb/DFW07LA155), Jul 10, 2007: Boeing 737-232 (N332DL), Tunica, MS, no damage, 1 fatal. Probable cause: Gorund service personal's removal of the portable stairway prior to the main cabin door being secured. Factors were the high winds and heavy rain. - [NTSB NYC07LA121](https://openairdocs.org/ntsb/NYC07LA121), May 18, 2007: Douglas DC-9-31 (N1799U), Syracuse, NY, substantial damage. Probable cause: The senior ground agent's failure to follow written procedures and directives. - [NTSB CHI02FA289](https://openairdocs.org/ntsb/CHI02FA289), Sep 22, 2002: McDonnell Douglas DC-9-32 (N941N), Minneapolis, MN, substantial damage. Probable cause: The fatigue failure of the main landing gear strut due to inclusions in the material, residual stresses, and dissolved hydrogen content. - [NTSB CHI01IA046](https://openairdocs.org/ntsb/CHI01IA046), Dec 14, 2000: McDonnell Douglas DC-9-31 (N9342), Chicago, IL, incident, minor damage. Probable cause: Failure of the captain to maintain clearance from the other airplane that was stopped. Factors relating to this accident were the snow-covered taxiways and the ground controller disregarding the… - [NTSB MIA99FA005](https://openairdocs.org/ntsb/MIA99FA005), Oct 7, 1998: Boeing 727-224 (N66734), Miami, FL, substantial damage. Probable cause: The catastrophic failure of the 8th stage high pressure compressor disk from cadmium embrittlement as a result of improper adherence to the prescribed plating procedures and requirements by the… - [NTSB SEA97FA202](https://openairdocs.org/ntsb/SEA97FA202), Sep 2, 1997: McDonnell Douglas DC-9-82 (MD-82) (N951AS), Seattle, WA, substantial damage. Probable cause: fatigue failure of the nose landing gear upper lock link, due in part to reduced strength after the manufacturing process was changed from forged to machined plate stock; and inadequate… - [NTSB FTW96RA039](https://openairdocs.org/ntsb/FTW96RA039), Nov 7, 1995: Boeing B727-224 (N79750), Panama City, Panama, incident - [NTSB NYC91IA165](https://openairdocs.org/ntsb/NYC91IA165), Jul 2, 1991: Boeing 727-254 (N913TS), Buffalo, NY, incident, no damage. Probable cause: CHAFFING FIRE DETECTOR LOOP ON THE NUMBER ONE ENGINE. - [NTSB CHI91IA078](https://openairdocs.org/ntsb/CHI91IA078), Jan 21, 1991: Boeing 727-251 (N295US), St. Paul, MN, incident, minor damage. Probable cause: THE PARTIAL FAILURE OF THE AIRPLANE'S AUXILIARY POWER UNIT, AND THE INADEQUATE COMPONENT PRODUCED BY THE MANUFACTURER. - [NTSB MIA90IA039](https://openairdocs.org/ntsb/MIA90IA039), Dec 15, 1989: Boeing 727 (N64339), Ormond Beach, FL, incident, no damage. Probable cause: FAILURE OF THE PILOT IN COMMAND IN THE BEECH 300 TO COMPLY WITH AN ATC CLEARANCE IN A TIMELY MANNER, WHILE DIVERTING HIS ATTENTION, AND FAILURE OF THE ATC CONTROLLER TO ASSURE THAT IFR SEPARATION WAS… - [NTSB BFO88IA012](https://openairdocs.org/ntsb/BFO88IA012), Dec 5, 1987: Mcdonnell Douglas DC-9-32 (N924L), Baltimore, MD, incident, no damage - [NTSB DCA86RA023](https://openairdocs.org/ntsb/DCA86RA023), Apr 2, 1986: Boeing 727-231 (N54340), Athens, Greece, 4 fatal - [NTSB DCA86AA018](https://openairdocs.org/ntsb/DCA86AA018), Feb 21, 1986: McDonnell Douglas DC-9-31 (N961VJ), Erie, PA, substantial damage - [NTSB LAX84AA132](https://openairdocs.org/ntsb/LAX84AA132), Dec 28, 1983: Boeing 727-224 (N79750), New York, NY, substantial damage - [NTSB CHI83IA063](https://openairdocs.org/ntsb/CHI83IA063), Dec 19, 1982: Douglas DC9-30 (N9344), Pellston, MI, incident, no damage - [NTSB FTW82DA139](https://openairdocs.org/ntsb/FTW82DA139), Apr 19, 1982: Boeing 727-200 (N32717), Austin, TX, substantial damage - [NTSB MKC81FA051](https://openairdocs.org/ntsb/MKC81FA051), Aug 13, 1981: Douglas DC-9 (N924L), St.Louis, MO, substantial damage - [NTSB FTW81DA092](https://openairdocs.org/ntsb/FTW81DA092), May 18, 1981: Douglas DC-9 (N1295L), New Orleans, LA, no damage - [NTSB CHI79FA047](https://openairdocs.org/ntsb/CHI79FA047), Apr 21, 1979: Douglas DC-9 (N941N), Mosinee, WI, substantial damage - [NTSB MIA75IM042](https://openairdocs.org/ntsb/MIA75IM042), Jan 8, 1975: Boeing 727 (N7642U), Birmingham, AL, incident, minor damage - [NTSB CHI74AC040](https://openairdocs.org/ntsb/CHI74AC040-187705), Dec 9, 1973: Boeing 727 (N259US), Madison, WI, substantial damage - [NTSB IAD71II039](https://openairdocs.org/ntsb/IAD71II039), Feb 15, 1971: Boeing 727 (N7644U), Dulles Int Apt, DC, incident, no damage ## FAA accident and incident reports (161, 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. - [Accident 20070710017209A](https://openairdocs.org/incident/20070710017209A), Jul 10, 2007: Boeing 737232 (N332DL), Tunica, MS, No damage, 1 fatal. (-23) Prior to departure flight mechanic (assisting the flight attendant) fell out of aircraft doorway while closing door. - [Accident 20070518014589A](https://openairdocs.org/incident/20070518014589A), May 18, 2007: Doug DC931 (N1799U), Buffalo, NY, Substantial damage. (-23) On may 18, 2007, at 1320 EST, a northwest airlines, DC-9-31, flight 1411, N1799U experienced a cabin pressurization problem during climb after departing… - [Incident 20060707021639I](https://openairdocs.org/incident/20060707021639I), Jul 7, 2006: Doug DC931 (N1799U), Rochester, NY. (-23) The nwaa maintenance log book page #3705980 stated the following entry from company maintenance. Discrepancy: station employee reports smoke in cabin at… - [Incident 20050713014589I](https://openairdocs.org/incident/20050713014589I), Jul 13, 2005: Boeing 737232 (N332DL), Kansas City, MO. (-23) On July 13, 2005 delta airlines flight 455 a B737-200 returned to mci due to an unknown vibration in the cockpit. No emergency was declared. Maintenance… - [Incident 20050502006569I](https://openairdocs.org/incident/20050502006569I), May 2, 2005: Boeing 727222 (N7644U), Lincoln, NE. (-23) Ctt flight 109 enroute from den to mke experienced a smoke detector light illuminate during flight. Reset system, light re-illuminated. Cat's (central… - [Incident 20031105028309I](https://openairdocs.org/incident/20031105028309I), Nov 5, 2003: Boeing 727222 (N7644U), St Louis, MO. (-23) Ryan flight 128 declared emergency due to loss of oil pressure on #3 engine. Aircraft diverted to stl and landed without incident. Maintenance found oil… - [Incident 20030901032569I](https://openairdocs.org/incident/20030901032569I), Sep 1, 2003: Doug DC932 (N9346), Syracuse, NY. (-23) On 09/01/2003 at approximately 07:56 EST, a DC-93-32, registration number N9346, operated by nwaa experienced compressor stalls on the #2 engine while at… - [Accident 20020922037939A](https://openairdocs.org/incident/20020922037939A), Sep 22, 2002: Doug DC932 (N941N), Minneapolis, MN, Substantial damage. (-23) On taxi for departure, the right main landing gear collapsed. The upper strut housing cracked which allowed the inner strut to become free. The… - [Incident 20020715028039I](https://openairdocs.org/incident/20020715028039I), Jul 15, 2002: Doug DC932 (N941N), Omaha, NE. (-23) N941N, DC9-32, being operated by northwest airlines as flight 1526 departed Omaha, NE, enroute to minneapolis, MN. During climb the crew reported smoke… - [Incident 20020228036479I](https://openairdocs.org/incident/20020228036479I), Feb 28, 2002: Boeing 727251 (N252US), Fort Wayne, IN. (-23) See attached SDR: flight 715 from elp to fwa; on descent the aircraft had outboard split flap indication. The crew used the alternate flap system to… - [Incident 20010716020979I](https://openairdocs.org/incident/20010716020979I), Jul 16, 2001: Doug DC932 (N824AT), Moline, IL. (-23) During descent into mli the aircraft experienced a forward cargo fire detection. Crew initiated emergency procedures and discharged #1 fire bottle. Crew… - [Incident 20010404009319I](https://openairdocs.org/incident/20010404009319I), Apr 4, 2001: Boeing 727251 (N266US), Miami, FL, Minor damage. (-23)On April 4, 2001, falcon flight #010, departing from Miami International Airport, with a final destination of tallahassee, Florida experienced a tail… - [Incident 20010221005299I](https://openairdocs.org/incident/20010221005299I), Feb 21, 2001: Boeing 727251 (N252US), Minneapolis, MN, Minor damage. (-23) As a/c was being marshalled to parking, left wing tip struck hangar wall causing minor damage to strobe light lens, and assembly, as well as surrounding… - [Incident 20001119030609I](https://openairdocs.org/incident/20001119030609I), Nov 19, 2000: Doug DC931 (N9343), Grand Rapids, MI, Minor damage. (-23) On 11/19/00, at approx. 1148 pm EST, during the landing roll on the snow covered runway, 1" loose snow, nwaa flight #1107, a DC-9-31, right-hand main… - [Incident 20000627032909I](https://openairdocs.org/incident/20000627032909I), Jun 27, 2000: Boeing 727222 (N7643U), Columbia, SC, Minor damage. (-23)The pilot in command stated that during landing he was slightly out of alignment with the runway, he made a right hand correction and landed normal. Post… - [Incident 20000529017059I](https://openairdocs.org/incident/20000529017059I), May 29, 2000: Doug DC931 (N9343), Kansas City, MO. (-23)On may 30, 2000, at approximately 0616 CDT, northwest airlines flight 1030, a Douglas DC-9-30, N9343, attempted take off at Kansas City, MO, (mci). Take… - [Incident 19991229038449I](https://openairdocs.org/incident/19991229038449I), Dec 29, 1999: Doug DC931 (N964N), Traverse City, MI. After landing runway 28 tvc, flight #1539 slid off the departure end of runway. The crew of 4 and 100 passengers were not injuried and the aircraft was not… - [Incident 19990812042599I](https://openairdocs.org/incident/19990812042599I), Aug 12, 1999: Doug DC982 (N936AS), Newark, NJ. (-23)An air carrier aircraft departed the gate and then returned due to mechanical problems. All passengers deplaned from the aircraft during a plane change.… - [Incident 19990712025679I](https://openairdocs.org/incident/19990712025679I), Jul 12, 1999: Boeing 727227 (N772AT), Indianapolis, IN. During climb out the lower aft body overheat light on, then standby hydraulic system "on" light and "overheat" light came on. Returned to Indianapolis. - [Incident 19990628025669I](https://openairdocs.org/incident/19990628025669I), Jun 28, 1999: Boeing 727227 (N772AT), Indianapolis, IN. Climbing through flight level 18.0 the number one engine oil pressure dropped to 35 PSI, oil temperature increased to 120*. Throttle retarded, oil pressure… - [Accident 19981007035229A](https://openairdocs.org/incident/19981007035229A), Oct 7, 1998: Boeing 727224 (N66734), Miami, FL, Substantial damage. On October 7, 1998, about 0710 eastern daylight time, a Boeing 727-224, N66734, operated by Continental airlines, inc. as flight 1521, title 14 CFR part 121… - [Incident 19980324007959I](https://openairdocs.org/incident/19980324007959I), Mar 24, 1998: Boeing 737247 (N309VA), Greensboro, NC, Minor damage. Narrative: pilot statement: "on climb out of iad at about 17,000 feet, we felt a violent bump. We asked the center about any aircraft in the area, they had… - [Incident 19980316036529I](https://openairdocs.org/incident/19980316036529I), Mar 16, 1998: Boeing 727251 (N267US), Miami, FL. (-5) On flight from montego bay, jamaica, to newark, new jersey, N267US, a Boeing 727, lost cabin pressure. The crew declared an emergency, descended to a… - [Accident 19970901047979A](https://openairdocs.org/incident/19970901047979A), Sep 1, 1997: Doug DC982 (N951AS), Seattle, WA, Substantial damage. (-16) On sept. 1, 1997, upon landing gear extention for landing at Seattle airport, the crew of Alaska airlines flight 255 reported an unsafe gear indication… - [Incident 19961002042109I](https://openairdocs.org/incident/19961002042109I), Oct 2, 1996: Boeing 727227 (N773AT), Indianapolis, IN. Smoke in cockpit boiler VORTAC. Diverted ind. Right heater exchange panel delaminated. Ducts seals broken. - [Incident 19960411013851I](https://openairdocs.org/incident/19960411013851I), Apr 11, 1996: Boeing 727227 (N773AT), Chicago, IL, Minor damage. Narrative: on April 11, 1996, at about 11:00 p.m. at Chicago's Midway airport, an American trans air, B-727, N773AT was push back from gate C-5 for a… - [Incident 19960305006649I](https://openairdocs.org/incident/19960305006649I), Mar 5, 1996: Boeing 727225 (N918TS), New York, NY, Minor damage. Narrative: on March 5, 1996, us air shuttle, aircraft N918TS, flight 6051, from boston. While five miles out on approach to runway 22 at lga a seven foot… - [Incident 19960222004729I](https://openairdocs.org/incident/19960222004729I), Feb 22, 1996: Boeing 72725C (N932UP), Syracuse, NY, Minor damage. Narrative: on 2/22/96 at 05:45, a Boeing 727, N932UP, registered to united parcel service 1400 hurstbourne pkwy, louisville, KY, had a right wing tip strike… - [Incident 19960124019679I](https://openairdocs.org/incident/19960124019679I), Jan 24, 1996: Doug DC931 (N9341), Cleveland, OH. Narrative: NWA604 was inbound to Cleveland Hopkins from the northwest NWA604 was given a clearance to 7000'. Which they acknowledged. A commuter bta 3110… - [Incident 19960116002299I](https://openairdocs.org/incident/19960116002299I), Jan 16, 1996: Boeing 727231 (N64320), San Antonio, TX. Narrative: trans world airlines, flight 199, a Boeing 727-231, inbound stl-sat, experienced a door indication of the aft air stair door, which is not in the… - [Incident 19951107036249I](https://openairdocs.org/incident/19951107036249I), Nov 7, 1995: Boeing 727224 (N79750), Panama City, PN, Substantial damage. Plane sitting on ramp, 1,200 lbs of matches caught fire, burned through caro compartment lining. - [Incident 19950313006819I](https://openairdocs.org/incident/19950313006819I), Mar 13, 1995: Boeing 737232 (N332DL), Nashville, TN. Narrative: on 3/13/95, delta 1580 at B-737 (N332DL) was enroute from omaha, NE (oma) to atlanta, ga (atl) at FL 33000. Approximately 80 NM northwest of bna the… - [Incident 19940713026369I](https://openairdocs.org/incident/19940713026369I), Jul 13, 1994: Boeing 727 (N778AT), Ft Lauderdale, FL, Minor damage. On climbout slats failed retract. Lost a hydraulic pressure. Found slat actuator separated. 6 of 8 acuators missing - [Incident 19940226009459I](https://openairdocs.org/incident/19940226009459I), Feb 26, 1994: Boeing 737200 (N260US), Norfolk, VA, Minor damage. Blew right main landing gear tire on rollout. Brakes caught on fire. Emergency evacuation ordered. - [Incident 19931216049529I](https://openairdocs.org/incident/19931216049529I), Dec 16, 1993: Boeing 727225 (N917TS), New York, NY, Minor damage. Leading edge flaps malfunctioned on approach. Landed safely. Section of flap missing. Piece found in courtyard. - [Incident 19931010043539I](https://openairdocs.org/incident/19931010043539I), Oct 10, 1993: Boeing 727225 (N917TS), Washington, DC. NR1 engine oil temperature rise. Engine shut down. Landed at destination. Fuel oil heater valve stuck open. - [Incident 19930930043779I](https://openairdocs.org/incident/19930930043779I), Sep 30, 1993: Boeing 737200 (N11244), Cleveland, OH. Amber over heat light on during climbout. Shut engine down. Returned. Landed safely. Found no abnormalities. - [Incident 19921117051369I](https://openairdocs.org/incident/19921117051369I), Nov 17, 1992: Boeing 727251 (N266US), Portland, OR. Pilot returned to airport after NR1 engine start valve light illuminated. Replaced starter control valve. - [Incident 19920909040419I](https://openairdocs.org/incident/19920909040419I), Sep 9, 1992: Doug DC931 (N964N), Chicago, IL. Cabin decompression on descent. Oxygen masks were deployed. Found a faulty outflow vlave. - [Incident 19920611023229I](https://openairdocs.org/incident/19920611023229I), Jun 11, 1992: Boeing 727222 (N7639U), Des Moines, IA. Flaps froze on takeoff. Diverted. Landed safely. Right outboard flap jackscrew jammed in fairing. - [Incident 19920421018669I](https://openairdocs.org/incident/19920421018669I), Apr 21, 1992: Boeing 727224 (N66734), Newark, NJ, Minor damage. Pilot advised passenger had observed portion of right wing break off. Returned. Inboard flap had separated. - [Incident 19920410012099I](https://openairdocs.org/incident/19920410012099I), Apr 10, 1992: Boeing 727180C (N920UP), Louisville, KY, Minor damage. Aircraft sustained a bird strike on descent. Landed safely. - [Incident 19920322011279I](https://openairdocs.org/incident/19920322011279I), Mar 22, 1992: Doug DC932 (N941N), Detroit, MI, Minor damage. 2 Compressor stalls on takeoff. Aborted. Returned to gate. Engine checked normal. Suspect water and slush ingestion - [Incident 19920302007289I](https://openairdocs.org/incident/19920302007289I), Mar 2, 1992: Boeing 727222 (N7631U), Indianapolis, IN. Smoke in cabin. Diverted to Indianapolis. Found cause of smoke to be a failed gasper motor. - [Incident 19920229008199I](https://openairdocs.org/incident/19920229008199I), Feb 29, 1992: Boeing 727251 (N295US), Kansas City, MO. Lost hydraulic pressure on a system on climb. Returned. Flow regulator and filters were replaced. - [Incident 19920226006859I](https://openairdocs.org/incident/19920226006859I), Feb 26, 1992: Doug DC932 (N9346), Detroit, MI. Exhaust odor in cabin from smoking APU at start of push back. Shut APU down. Evacuated. No evidence of fire. - [Incident 19920220011409I](https://openairdocs.org/incident/19920220011409I), Feb 20, 1992: Boeing 727251 (N255US), Fort Myers, FL, Minor damage. Rear galley fire en route. Shut off power. Used halon bottle. Flight attendant burned finger tips. Continued flight. - [Incident 19911105060129I](https://openairdocs.org/incident/19911105060129I), Nov 5, 1991: Boeing 727277 (N546DA), Oceanside, CA. Advised of unidentified aircraft. Later climbed in response to TCAS alert. Passed safely. - [Incident 19910809046899I](https://openairdocs.org/incident/19910809046899I), Aug 9, 1991: Boeing 737232 (N332DL), Salt Lake City, UT. Unsafe gear indication on final. Cabin filled with smoke while taxiing. Found gear accessory unit had failed. - [Incident 19910807036379I](https://openairdocs.org/incident/19910807036379I), Aug 7, 1991: Boeing 727222 (N7643U), Des Moines, IA, Minor damage. Inboard tires locked on landing due to failure of anti skid system. All 161: https://openairdocs.org/engine/pratt-whitney-jt8d-5/incidents.md ## Service difficulty reports (38) As reported by operators and repair stations, by the model named in the report. - [SDR FOTR2101904400](https://openairdocs.org/sdr/FOTR2101904400), Feb 21, 2011: SKIN. DEBONDED. LT WING T/E NR 6 SPOILER UPPER SKIN IS DISBONDED. REMOVED DAMAGE APPROX 13" X 5.5" AND CLEANED AND PREPPED AREA IAW SRM 51-40-20, PG 12-14 PARA 7.FABRICATED REP - [SDR FOTR2101904217](https://openairdocs.org/sdr/FOTR2101904217), Feb 21, 2011: FRAME. GOUGED. FRAME AT STA 640 STR 6R IS GOUGED AND DENTED. REMOVED DAMAGED AREA OF FRAME 1.5" X 1.5" IAW SRM 51-10-1. FABRICATED CHANNEL 2 EA 12" X 3" FROM 7075-0 .063 PO 90 - [SDR FOTR2101904218](https://openairdocs.org/sdr/FOTR2101904218), Feb 21, 2011: FRAME. GOUGED. FRAME AT STA 660 BETWEEN STR 6R AND STR 7R IS GOUGED. REMOVED DAMAGED AREA OF FRAME IAW SRM 51-10-1, DIM 1.5" X 1.5". FABRICATED 2 EA CHANNELS 12" X 3" FROM 707 - [SDR FOTR2101903974](https://openairdocs.org/sdr/FOTR2101903974), Feb 21, 2011: COVER. CRACKED. LT WING L/E NR 2 SLAT TRACK COVER CRACKED. (OTBD TRACK) STOP DRILLED CRACK ON NR 2 SLAT IAW SRM 51-10-1. FABRICATED REPAIR DOUBLER FROM 7075T6 .080" PO 9007282 - [SDR FOTR2101904392](https://openairdocs.org/sdr/FOTR2101904392), Feb 21, 2011: FRAME. DENTED. AFT CARGO COMPARTMENT, FRAME DENTED BETWEEN STRINGER 25L-26L BS 1090 CUTOUT DAMAGED AREA 1" X 1.25" IAW SRM 51-40-3, FIG 1. FABRICATED REPAIR FRAME FROM 7075-0 - [SDR FOTR2101903914](https://openairdocs.org/sdr/FOTR2101903914), Feb 21, 2011: SKIN. BENT. PREVIOUS REPAIR ON RT WING INBD FLAP, INBD END BENT, WBL 70. REMOVED PREVIOUS REPAIR IAW SRM 51-30-2. FABRICATED REPAIR PART FROM 2024T3 .063 DIM 2.5" X 2" PO 9 - [SDR C8GA2010000073](https://openairdocs.org/sdr/C8GA2010000073), Nov 10, 2010: INDICATOR. MALFUNCTIONED. ON TAKEOFF ROLL, THE NR1 EPR INDICATION PEGGED. THE TAKEOFF WAS ABORTED AND THE ACFT RETURNED TO THE BLOCKS. HIGH ENERGY INSP WAS PERFORMED. R & R THE NR1 EPR I - [SDR DALA1013589936](https://openairdocs.org/sdr/DALA1013589936), Jun 17, 2010: SKIN. CRACKED. DURING LINE CHECK FOUND CRACK IN FORWARD ENTRY DOOR INNER SKIN AT FASTENER HOLE. R & R LOWER AFT DOOR INNER SKIN IAW SRM. - [SDR KNNA200700041](https://openairdocs.org/sdr/KNNA200700041), Sep 2, 2007: HOSE. LEAKING. WHILE EN ROUTE TO ATLANTA HARTSFIELD AIRPORT (KATL) FROM TUNICA, MISSISSIPPI (KUTA) AS SKY KING FLT (SGB332) THE CREW NOTICED A SLOW LOSS OF SYSTEM “A” HYDRAULI - [SDR 2006FA0000657](https://openairdocs.org/sdr/2006FA0000657), Jul 20, 2006: SUPPORT. CRACKED. DURING C-CHECK ROUTINE INSPECTION A 1 INCH CRACK (APPROX) WAS FOUND IN LT OB AILERON LOCKOUT MECHANISM SUPPORT ASSY CASTING IN THE RADIUS AREA OF THE AILERON CR - [SDR C7WA200600004](https://openairdocs.org/sdr/C7WA200600004), Feb 24, 2006: REGULATOR. INTERMITTENT. NR 1 GENERATOR EXPERIENCED AN UNDER VOLTAGE CAUSING A VERTICAL TRIP. NR3 GENERATOR ALREADY ON DMI. REMOVED AND REPLACED NR1 POSITION VOLTAGE REGULATOR SYSTEM OP - [SDR C7WA200600006](https://openairdocs.org/sdr/C7WA200600006), Feb 24, 2006: SMOKE WARNING. ACTIVATED. CARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. RAN PROCEEDURE AND DIVERTED. COULD NOT DUPLICATE. TESTED SYSTEM IAW MM. (K) - [SDR C7WA200600001](https://openairdocs.org/sdr/C7WA200600001), Feb 13, 2006: SEAL. LEAKING. ENGINE NR 1 LOSS OIL DURING FLIGHT. INSTALLED NEW OIL LINE DONUT SEALS ON GEARBOX OIL LINES. NO LEAKS NOTED DURING ENGINE RUNS IAW MM. (K) - [SDR C7WA200500126](https://openairdocs.org/sdr/C7WA200500126), Dec 30, 2005: SEQUENCE VALVE. INTERMITTENT. DURING APPROACH, RT MLG AND NOSE GEAR INDICATION SHOWED UNSAFE. ON SECOND ATTEMPT GEARS CAME DOWN NORMALLY. ON GEAR OPERATIONAL CHECK RT MLG FAILED TO EXTEND, N - [SDR 2006FA0000645](https://openairdocs.org/sdr/2006FA0000645), Nov 8, 2005: CONTROL VALVE. FAILED. NR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WA - [SDR 2006FA0000070](https://openairdocs.org/sdr/2006FA0000070), Sep 22, 2005: CHAIN. DETACHED. DURING C-CHECK, INSPECTION OF FWD DOOR EMERGENCY ESCAPE SLIDE BUSTLE LATCH CHAIN WAS FOUND DETACHED FROM THE SPLIT RING. THE SPLIT RING HAD BECOME ELONGATED AND - [SDR C7WA200500108](https://openairdocs.org/sdr/C7WA200500108), Jul 5, 2005: BRAKE. SEIZED. AIR RETURN, ON CLIMBOUT AT 14,000 FT WHEEL WELL FIRE LIGHT ILLUMINATED. RAN CHECK LIST FIRE LIGHT WENT OUT. FOUND NR 2 BRAKE ASSEMBLY. SEIZED. REMOVED AND REPLA - [SDR GAIA0521OP](https://openairdocs.org/sdr/GAIA0521OP), Jun 23, 2005: COALESCER BAG. DIRTY. DURING CLIMB OUT, FUEL ODOR, LANDING WAS MADE WITHOUT INCIDENT. CHECKED AFT SPAR ENGINE FUEL FEED LINE SHROUDS, NO LEAKS NOTED. REMOVED AND REPLACED BOTH WATER - [SDR C7WA200500094](https://openairdocs.org/sdr/C7WA200500094), Apr 11, 2005: SWITCH. OUT OF ADJUST. CARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. ADJUSTED MAIN CARGO DOOR VENT LIGHT SWITCH IAW MM. OPS CHECK GOOD. (K) - [SDR C7WA200500098](https://openairdocs.org/sdr/C7WA200500098), Apr 11, 2005: PUMP. INOPERATIVE. AIR RETURN: NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS FAILED. REMOVED AND REPLACED NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS. REMOVED AND REPLACED (B) SYSTEM CASE - [SDR C7WA200500095](https://openairdocs.org/sdr/C7WA200500095), Apr 11, 2005: WARNING SYSTEM. MALFUNCTIONED. APU FIRE BELL SOUNDS OFF AND CANNOT BE SILENCED. NO WARNING LIGHTS OR OTHER INDICATIONS THAT A PROBLEM EXISTS. REMOVED, CLEANED AND REINSTALLED APU FIRE DETECTO - [SDR C7WA200300075](https://openairdocs.org/sdr/C7WA200300075), Jan 12, 2005: WIRE. SHORTED. IN FLIGHT SHUTDOWN NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN ALT AT 12,000 FEET, PERFORMED ABNORMAL CHECKLIST AS REQUIRED. FOUND WIRES SHORTED IN CONNEC - [SDR COOSDR040041](https://openairdocs.org/sdr/COOSDR040041), Sep 24, 2004: FITTING. CRACKED. FUSELAGE NOSE LANDING GEAR WHEEL WELL RT SIDE AT Y STA 69.55-X 24 INCH -Z16 INCH FITTING (PN 49568801) WITH CRACK. (K) - [SDR UPS04242437](https://openairdocs.org/sdr/UPS04242437), May 14, 2004: MOUNT. CORRODED. INSPECTION TYPE:C NR 1 ENG FWD MOUNT HOLES HAVE PITTING CORROSION IN BOTH IB HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592. - [SDR UPS04242438](https://openairdocs.org/sdr/UPS04242438), May 14, 2004: MOUNT. CORRODED. INSPECTION TYPE: C ENGINE NR 3 FWD MOUNT HOLE HAVE PITTING CORROSION IN BOTH I/B HOLES. HOLES REPAIRED IAW UPS EO B727-5440-11592. - [SDR UPS04242434](https://openairdocs.org/sdr/UPS04242434), May 12, 2004: LAP JOINT. CORRODED. INSPECTION TYPE:C MATERIAL LOSS (LAP JOINT CORROSION) AT S-6L BS 685. REPAIRED IAW UPS EO B727-5330-0509 APPX C, AND SRM 53-3 0-1, FIG 5. - [SDR UPS04242439](https://openairdocs.org/sdr/UPS04242439), May 11, 2004: SKIN. CRACKED. INSPECTION TYPE: C CRACK IN SKIN AT FWD CARGO DOOR CUTOUT AT FWD LWR CORNER. REPAIRED IAW AAAE EO 2004-050-001. REFERENCE UPS EO B72 7-5330-20497-A. - [SDR UPS04242436](https://openairdocs.org/sdr/UPS04242436), May 8, 2004: SKIN. DENTED. INSPECTION TYPE:C 2 DENTS IN SKIN AT BS 1245, STR 19R . REPAIRED IAW SRM 53-30-3, FIG 13A. - [SDR RYN76394A](https://openairdocs.org/sdr/RYN76394A), Oct 19, 2003: SKIN. CORRODED. DURING A SCHEDULED INSPECTION FOUND FUSELAGE SKIN AT STA 303 STR 17-18R, UNDER FORWARD LAV SERVICE PANEL, HAS EXFOILIATED CORROSION. - [SDR RYN2004F00023](https://openairdocs.org/sdr/RYN2004F00023), Sep 3, 2003: SMOKE DETECTOR. FALSE ACTIVATION. AC DEPARTED, ENROUTE, MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. AC DIVERTED WITHOUT INCIDENT. INSPECTED AC FOR EVIDENCE OF BURNED WIRES AND FLUID - [SDR RYN2004F00024](https://openairdocs.org/sdr/RYN2004F00024), Sep 3, 2003: FLAP. MALADJUSTMENT. AFTER TAKEOFF, ACCELRATED TO 300 KNOTS. CREW EXPERIENCED MODERATE VIBRATION. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. ADJUSTED LT AND RT AFT FLAPS. REMOVED AND R - [SDR RYN2004F00021](https://openairdocs.org/sdr/RYN2004F00021), Jul 12, 2003: ACTUATOR. LEAKING. AFTER TAKEOFF, DURING ASCENT TO FLIGHT LEVEL 24.0 NR 7 FLAP LED AND YELLOW LIGHTS STAYED ILLUMINATED DURING FLAP RETRACTION. IMPLEMENTED PROCEDURES IAW MM FOR T - [SDR RYN2003F00000](https://openairdocs.org/sdr/RYN2003F00000), Jan 23, 2003: ACTUATOR. DEFECTIVE. DURING CLIMBOUT, NR 7 LEADING EDGE SLAT WOULD NOT RETRACT. EMERGENCY FLAP PROCEDURES FOLLOWED. AIRCRAFT RETURNED AND LANDED WITHOUT INCIDENT. - [SDR RYN2003F00005](https://openairdocs.org/sdr/RYN2003F00005), Jan 9, 2003: FITTING. CRACKED. DURING B CHECK, LT AND RT MAIN GEAR BEAM FITTING SAFETY BOLT LUGS FOUND CRACKED. - [SDR RYN76393A](https://openairdocs.org/sdr/RYN76393A), Oct 19, 2002: SUPPORT BEAM. CRACKED. DURING SERVICE CHECK, FOUND CRACK ON LT MAIN LANDING GEAR SUPPORT BEAM, OB ATTACH LUGS AT UPPER LOCK BOLT LUG. - [SDR RYN76392A](https://openairdocs.org/sdr/RYN76392A), Oct 19, 2002: INTERCOSTAL. CRACKED. DURING A SCHEDULED INSPECTION, FOUND RT AFT FUSELAGE TAIL HAS 1 INTERCOASTAL WITH A CRACK RUNNING FROM THE UPPER AFT CORNER APPROXIMATELY 1.125 INCH IN LENGTH. - [SDR RYN76391A](https://openairdocs.org/sdr/RYN76391A), Oct 19, 2002: SKIN. CRACKED. DURING A SCHEDULED INSPECTION, FOUND BULGE IN SKIN AND APPROXIMATELY 2.5 INCH HORIZONTAL CRACK AT STA 1020, STRINGER 26R. - [SDR 96ZZZX233](https://openairdocs.org/sdr/96ZZZX233), Dec 10, 1995: HEAT VALVE. FAILED. STL - FLT 192 - DURING CLIMB, NR 1 ENGINE FUEL HEAT VALVE INTRANSIT LIGHT STAYED ON WITH SWITCH IN THE OFF POSITION. SHUT DOWN NR 1 ENGINE AND RETURNED FROM FLI ## STCs that may be installed (OpenAirDocs) (13) 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 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. Lists JT8D Series - [STC SE497NE](https://openairdocs.org/stc/SE497NE): Installation of oil tank filler neck check valve assembly. Aviation Components Support - [STC SE3916NM](https://openairdocs.org/stc/SE3916NM): Installation of CADC bleed valve supports brackets, P/N B10002 or RB10003, as a replacement part for P&W P/N 578273. Aeroparts Mfg & Repair. Lists JT8D Series - [STC SE79WE](https://openairdocs.org/stc/SE79WE): Installation of CADC bleed valve support brackets, P/N B10001 or RB10006, as a replacement part for P&W P/N 493317 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Aeroparts Mfg & Repair. Lists JT8D Series - [STC SE00049AT-D](https://openairdocs.org/stc/SE00049AT-D): Installation of Intermediate Compressor Case (JT8D SERIES). Aero Component Technologies. Lists JT8D Series - [STC SE557NE](https://openairdocs.org/stc/SE557NE): Installation of oil tank shuttle valve. Stockbridge William D - [STC SE2666SO](https://openairdocs.org/stc/SE2666SO): Modification of the anti-ice mount bracket. Cook Airtomic - [STC SE593NE](https://openairdocs.org/stc/SE593NE): Installation of a Select Controls Inc. Engine Oil Shuttle Valve, P/N 2057-1-001. (See Eligibility List). Basken Valve Corporation. Lists JT8D Series - [STC SE1930SO](https://openairdocs.org/stc/SE1930SO): Installation of power control shaft bushing. Cook Airtomic Division. Lists JT8D Series - [STC SE83WE](https://openairdocs.org/stc/SE83WE): Installation of heat shield assembly P/N 408-007 as a replacement part for P&W P/N499941 or 749609 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series - [STC SE84WE](https://openairdocs.org/stc/SE84WE): Installation of heat shield assembly 408-008 as a replacement part for P&W No. 586918 used on JT8D-1, -5, -7, -9, -9A, -15 and -17 engines. Hughes Helicopter. Lists JT8D Series - [STC SE67WE](https://openairdocs.org/stc/SE67WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series - [STC SA2627WE](https://openairdocs.org/stc/SA2627WE): Installation of fuel control rod end bearings. Triumph Corporation. Lists JT8D Series --- 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.