# Lockheed 382E - Type: Aircraft model (FAA registry) - Registry code: 526413U - Manufacturer (registry): LOCKHEED - Model: 382E - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-prop - Seats: 3 - Weight class: 20,000 lb and over - Cruise speed: 262 mph - Certification: Type certificated - Data sheet: [TCDS A1SO](https://openairdocs.org/tcds/A1SO) (OpenAirDocs) - Holder: Lockheed Martin Corporation - Registered aircraft: 0 - Page: https://openairdocs.org/model/lockheed-382e 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 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2024-01-02](https://openairdocs.org/ad/2024-01-02): Fuselage · Lockheed 382, 382B, 382E and 9 more. Effective Jan 24, 2024 - [AD 2023-22-06](https://openairdocs.org/ad/2023-22-06): Powerplant · Lockheed Martin 382, 382B, 382E and 8 more. Effective Nov 21, 2023 - [AD 2023-11-10](https://openairdocs.org/ad/2023-11-10): Fuselage · Lockheed Martin 382, 382B, 382E and 9 more. Effective Jul 11, 2023 - [AD 2023-09-13](https://openairdocs.org/ad/2023-09-13): Wings · Lockheed Martin 382, 382B, 382E and 7 more. Effective May 31, 2023 - [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 2021-09-15](https://openairdocs.org/ad/2021-09-15): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Jun 1, 2021 - [AD 2019-25-20](https://openairdocs.org/ad/2019-25-20): Flight controls · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Feb 28, 2020 - [AD 2015-22-11](https://openairdocs.org/ad/2015-22-11): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 28, 2015 - [AD 2015-18-02](https://openairdocs.org/ad/2015-18-02): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 2015 - [AD 2015-06-08](https://openairdocs.org/ad/2015-06-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 2015 - [AD 2015-05-08](https://openairdocs.org/ad/2015-05-08): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 24, 2015 - [AD 2014-17-02](https://openairdocs.org/ad/2014-17-02): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Sep 9, 2014 - [AD 2012-06-09](https://openairdocs.org/ad/2012-06-09): Standard practices/structures · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 15, 2012 - [AD 2011-15-02](https://openairdocs.org/ad/2011-15-02): Fuel · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 19, 2011 - [AD 2009-11-03](https://openairdocs.org/ad/2009-11-03): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 4, 2009 - [AD 2008-14-10](https://openairdocs.org/ad/2008-14-10): Upper engine mount bolts · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jul 22, 2008 - [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001 - [AD 99-25-04](https://openairdocs.org/ad/99-25-04): Floor to Ring Fittings · Lockheed Martin 382, 382B, 382E and 3 more. Effective Jan 7, 2000 - [AD 97-21-13](https://openairdocs.org/ad/97-21-13): AFM - Power Levers · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1997 - [AD 97-05-07](https://openairdocs.org/ad/97-05-07): AFM Supplement 382-16 · Lockheed Martin 382, 382E and 382G. Effective Apr 4, 1997 - [AD 97-04-15](https://openairdocs.org/ad/97-04-15): Fire Extinguisher Bottle Cartridges · Bombardier DHC-8-101, DHC-8-102, DHC-8-103 and 24 more. Effective Mar 7, 1997 - [AD 96-24-14](https://openairdocs.org/ad/96-24-14): Main Landing Gear Brakes Inspection · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 27, 1997 - [AD 95-07-03](https://openairdocs.org/ad/95-07-03): Auxiliary Power Units · Allliedsignal Aerospace Auxiliary Power Units, 707-100 Long Body, 707-100B Long Body and 46 more. Effective May 3, 1995 - [AD 94-26-15](https://openairdocs.org/ad/94-26-15): Outer Wing Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 3, 1995 - [AD 92-10-14](https://openairdocs.org/ad/92-10-14): AFM Changes - Cabin Pressure · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 29, 1992 - [AD 89-16-09](https://openairdocs.org/ad/89-16-09): Nose Landing Gear Strut Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 7, 1989 - [AD 88-09-03](https://openairdocs.org/ad/88-09-03): Control Column Base · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 7, 1988 - [AD 88-10-06](https://openairdocs.org/ad/88-10-06): Wing Panel Risers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988 - [AD 88-10-05](https://openairdocs.org/ad/88-10-05): Wing Panel Doublers · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 25, 1988 - [AD 87-18-04](https://openairdocs.org/ad/87-18-04): Circuit Breaker Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Sep 17, 1987 - [AD 85-23-03](https://openairdocs.org/ad/85-23-03): Fire Estinguisher Squib Insp. · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 24, 1985 - [AD 81-12-02](https://openairdocs.org/ad/81-12-02): Longerons · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 5, 1981 - [AD 79-05-05](https://openairdocs.org/ad/79-05-05): Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jan 2, 1980 - [AD 79-25-06](https://openairdocs.org/ad/79-25-06): Window Latch Catches · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 19, 1979 - [AD 79-18-12](https://openairdocs.org/ad/79-18-12): Auxiliary Power Units · Airbus BAC 1-11 200 Series, BAC 1-11 400 Series, Manufacturing Company Auxiliary Power Units and 46 more. Effective Oct 8, 1979 - [AD 79-03-04](https://openairdocs.org/ad/79-03-04): Ballscrew Assembly in MLG · Lockheed Martin 382, 382B, 382E and 2 more. Effective Feb 5, 1979 - [AD 74-12-06](https://openairdocs.org/ad/74-12-06): Outer Wing Beam Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Dec 8, 1978 - [AD 75-17-04](https://openairdocs.org/ad/75-17-04): Main Frames · Lockheed Martin 382, 382B, 382E and 2 more. Effective Apr 21, 1978 - [AD 75-19-02](https://openairdocs.org/ad/75-19-02): Wing Beam Caps · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978 - [AD 75-18-04](https://openairdocs.org/ad/75-18-04): Outer Wing Lower Panels · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978 - [AD 75-18-03](https://openairdocs.org/ad/75-18-03): Outer Wing Spar Cap · Lockheed Martin 382, 382B, 382E and 2 more. Effective Mar 20, 1978 - [AD 76-09-11](https://openairdocs.org/ad/76-09-11): Crank Arm or Servo Valve Assembly · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 14, 1976 - [AD 75-17-35](https://openairdocs.org/ad/75-17-35): Propeller Torque Check · Lockheed Martin 382, 382B, 382E and 2 more. Effective Aug 13, 1975 - [AD 74-24-08](https://openairdocs.org/ad/74-24-08): Engine Throttle Cables · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 27, 1974 - [AD 74-24-04](https://openairdocs.org/ad/74-24-04): Lower Center Wing · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 20, 1974 Historical (superseded or no longer in force): - [AD 2019-18-09](https://openairdocs.org/ad/2019-18-09) (historical): Wings · Coulson EC-130Q, C-130A, C-130A and 11 more. Effective Oct 11, 2019 - [AD 2013-18-09](https://openairdocs.org/ad/2013-18-09) (historical): Communications · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 137 more. Effective Oct 3, 2013 - [AD 2011-09-04](https://openairdocs.org/ad/2011-09-04) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jun 22, 2011 - [AD 2011-09-03](https://openairdocs.org/ad/2011-09-03) (historical): Wings · Lockheed Martin 382, 382B, 382E and 2 more. Effective May 26, 2011 - [AD 2008-20-01](https://openairdocs.org/ad/2008-20-01) (historical): Fuel tank systems · Lockheed Martin 382, 382B, 382E and 2 more. Effective Nov 3, 2008 - [AD 74-08-09 R2](https://openairdocs.org/ad/74-08-09-R2) (historical): Waste Receptacles · Aero Spacelines 377, 377MG, 377SGT and 268 more. Effective Jul 29, 1996 - [AD 96-12-20](https://openairdocs.org/ad/96-12-20) (historical): Upper Truss Mounts · Lockheed Martin 382, 382B, 382E and 2 more. Effective Jul 15, 1996 ## Information bulletins (advisory) (1) - [SAIB NM-09-03](https://openairdocs.org/saib/NM-09-03): Engine Fuel and Control - Implementing Fuel Tank System Airworthiness Limitations. Issued Dec 11, 2008 ## Registered aircraft None registered with this model now. ## NTSB investigations (1) 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 NYC71AN047](https://openairdocs.org/ntsb/NYC71AN047), Oct 10, 1970: Lockheed Ga 382B (N9248R), Wrightstown, NJ, destroyed, 3 fatal ## FAA accident and incident reports (1) 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 19901007051569I](https://openairdocs.org/incident/19901007051569I), Oct 7, 1990: Lkheed 382E (N923SJ), Barnesville, OH. Hazardous material created fumes in cabin. Emergency landing. No evidence of leakage or spillage. ## Service difficulty reports (57, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR SRAA98A0202](https://openairdocs.org/sdr/SRAA98A0202), Feb 3, 1998: PROPELLER. LEAKING. DURING CLIMB-OUT FROM MHZ FLIGHT 507, NR 1 ENGINE RPM WENT TO 104 PERCENT NO CHANGE IN MECHANICAL GOVERNING, NR 1 PROP PITCH LOCKED, FEATHERED NR 1 PROP AND FOU - [SDR SRAA971214](https://openairdocs.org/sdr/SRAA971214), Dec 17, 1997: SHUTOFF VALVE. MALFUNCTIONED. TEN MINUTES INTO FLIGHT FROM RSW, FLIGHT 356, CARGO COMPARTMENT AIR CONDITIONER OVERHEAT LIGHT CAME ON. SHUT SYSTEM OFF AND ISOLATED SYSTEM. OVERHEAT LIGHT WENT - [SDR SRAA971204](https://openairdocs.org/sdr/SRAA971204), Dec 3, 1997: FITTING. BROKEN. AFTER LOADING CARGO, UPON CLOSING CARGO DOOR, FOUND CARGO RAMP LOCKS WOULD NOT ENGAGE, CARGO RAMP LOCK ACTUATOR SUPPORT FITTING FRACTURED. REPLACED FITTING AND - [SDR SRAA971111](https://openairdocs.org/sdr/SRAA971111), Nov 30, 1997: VOLTAGE REG. MALFUNCTIONED. ON TAKEOFF ROLL, AFTER ENGINES WERE UP TO SPEED FOR TAKEOFF, ESSENTIAL AC BUSS WENT OFF LINE A , B, C PHASE C/B'S ON ESSENTIAL AC POPPED. REJECTED TAKEOFF AND R - [SDR SRAA971109](https://openairdocs.org/sdr/SRAA971109), Nov 25, 1997: VALVE HOUSING. DEFECTIVE. ON TAKEOFF ROLL, NR 1 ENGINE TORQUE READING CLIMBED RAPIDLY THEN DROPPED TO 7,000 LBS, RPM DROPPED TO 97 PERCENT. ABORTED TAKEOFF WITHOUT INCIDENT. FOUND NR 1 P - [SDR SRAA971001](https://openairdocs.org/sdr/SRAA971001), Oct 1, 1997: ENGINE. BIRD STRIKE. ON TAKEOFF FOR FLIGHT 514 FROM IST, NR 1 RPM ROLLED BACK DUE TO BIRD STRIKE, SHUT DOWN NR 1 ENGINE IAW AOM AND CONTINUED FLIGHT TO LTAG. POST FLIGHT INSPECTION - [SDR SRAA970917](https://openairdocs.org/sdr/SRAA970917), Sep 29, 1997: FILTER. CRACKED. DURING FLIGHT, NR 1 ENGINE OIL QUANTITY FROM 10 GAL TO 4 GAL, PRECAUTIONARY SHUT DOWN NR 1 ENGINE AND ACCOMPLISHED AIR TURNBACK TO MHZ WITHOUT INCIDENT. INSPECT - [SDR SRAA970912](https://openairdocs.org/sdr/SRAA970912), Sep 24, 1997: CLAMP. LOOSE. WHILE TAXIING, NR 1 NACELLE OVERHEAT WARNING LIGHT CAME ON, AIRCRAFT BLOCKED IN WITHOUT INCIDENT. INSPECTED NR 1 ENGINE AND FOUND CLAMP ON F-STACK BLEED AIR DUC - [SDR SRAA970911](https://openairdocs.org/sdr/SRAA970911), Sep 23, 1997: CONTROL VALVE. LEAKING. AFTER ARRIVAL WHILE SETTING PARKING BRAKE CREW HEARD A CLICK AND NOTICED CLOUD AND HYDRAULIC ODOR COMING FROM THROTTLE QUANRANT. INSPECTED AIRCRAFT AND FOUND HY - [SDR SRAA970910](https://openairdocs.org/sdr/SRAA970910), Sep 18, 1997: FLOW CONTL VLV. INOPERATIVE. DURING FLIGHT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON. TURN OFF SYSTEM AND LIGHT WENT OUT SHORTLY AFTER. INSPECTED AIRCRAFT AND FOUND CARGO COMPARTMENT FLOW C - [SDR SRAA970816](https://openairdocs.org/sdr/SRAA970816), Aug 27, 1997: CLAMP. LOOSE. DURING CRUISE FOR FLIGHT 746 FROM AMS, AT FL 20.0 A LOUD BANG WAS HEARD FOLLOWED BY 2000 FPM CABIN RATE OF CLIMB, INITIATED EMERGENCY DESCENT TO A SAFE ALTITUDE - [SDR SRAA970807](https://openairdocs.org/sdr/SRAA970807), Aug 13, 1997: GEAR BOX. DECOUPLED. DURING FLIGHT AT FL260 FROM AAB, NR 1 ENGINE HAD LOSS OF TORQUE, TIT INDICATION WENT TO 540 DEG WITH F/F TO 440 LBS AND GENERATOR OUT LIGHT CAME ON. SHUT DOWN N - [SDR SRAA970806](https://openairdocs.org/sdr/SRAA970806), Aug 12, 1997: TRU. INOPERATIVE. AFTER TAKEOFF FROM NBO, NR 2 TRANSFORMER RECTIFIER WENT INOP. DUMPED 8200 LBS OF FUEL AND ACCOMPLISHED AIR TURN BACK TO NBO, AIRCRAFT LANDED WITHOUT INCIDENT. I - [SDR SRAA970709](https://openairdocs.org/sdr/SRAA970709), Jul 7, 1997: CLAMP. LOOSE. ON DESCENT, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON, AIRCRAFT LANDED WITHOUT INCIDENT. FOUND TOP CLAMP TO FLOW CONTROL AND SHUT OFF VALVE LOOSE, RETORQUED CLAM - [SDR SRAA970613](https://openairdocs.org/sdr/SRAA970613), Jun 24, 1997: CONNECTOR. CORROSION. ON ENGINE START AT AAB, SMOKE DETECTOR AND HORN WENT OFF. INSPECTED CARGO COMPARTMENT FOUND NO SIGN OF SMOKE, PULLED CIRCUIT BREAKER TO CUT OFF HORN. FOUND CANN - [SDR SRAA970606](https://openairdocs.org/sdr/SRAA970606), Jun 9, 1997: SPRING. DISCONNECTED. ON TAKEOFF ROLL, DOOR WARNING LIGHT ILLUMINATED ON TAKEOFF. ABORTED TAKEOFF AND AIRCRAFT RETURNED TO BLOCK. INSPECTED CARGO DOOR AND FOUND SPRING ON CARGO DOOR - [SDR SRAA970604](https://openairdocs.org/sdr/SRAA970604), Jun 7, 1997: WARNING LIGHT. ILLUMINATED. ON TAKEOFF ROLL AT 100 KNOTS, DOOR WARNING LIGHT CAME ON. ABORTED TAKEOFF WITHOUT INCIDENT. ITEM IS BEING INVESTIGATED. - [SDR SRAA970517](https://openairdocs.org/sdr/SRAA970517), May 30, 1997: CLAMP. LOOSE. ON TAXI OUT, CARGO COMPARTMENT OVERHEAT LIGHT ILLUMINATED. SHUT OFF AIR CONDITIONING PACK AND RETURNED TO BLOCK. FOUND LOOSE CLAMP ON HEAT EXCHANGER. RESEALED A - [SDR SRAA970418](https://openairdocs.org/sdr/SRAA970418), Apr 26, 1997: GASKETS. LEAKING. CARGO COMPARTMENT AIR CONDITIONING OVERHEAT LIGHT ILLUMINATED ON APPROACH. LANDED WITHOUT INCIDENT. REPLACED LEAKING GASKETS AT C/C FLOW CONTROL AND S/O VALVE A - [SDR SRAA970414](https://openairdocs.org/sdr/SRAA970414), Apr 20, 1997: WINDOW FRAME. CRACKED. ON POST FLIGHT INSPECTION, FOUND CAPTAIN'S SWING WINDOW FRAME HAD TWO CRACKS APPROX 1 INCH GOING UPWARD AND AFT ON TOP CORNER. ITEM IS CURRENTLY UNDER REPAIR. - [SDR SRAA970413](https://openairdocs.org/sdr/SRAA970413), Apr 20, 1997: SWITCHES. OUT OF ADJUST. ON CLIMBOUT, CARGO RAMP OPEN LIGHT CAME ON, DEPRESSURIZED AND CHECKED RAMP, NO ABNORMAL CONDITION FOUND. AIRCRAFT CONTINUED TO DESTINATION. FOUND LT AND RT RAMP - [SDR SRAA970308](https://openairdocs.org/sdr/SRAA970308), Mar 26, 1997: CONTROL CABLE. OUT OF POSITION. DURING FLIGHT 940 FROM EHAM TO LGWL, FOUND ELEVATOR STICKS AFTER 3 IN OF AFT TRAVEL. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. FOUND ALCLAD - [SDR SRAA970204](https://openairdocs.org/sdr/SRAA970204), Feb 6, 1997: DOWNLOCK SWITCH. MALFUNCTIONED. DURING GEAR EXTENSION FOR LANDING INTO AMS FLIGHT 940, NOSE LANDING GEAR INDICATION LIGHT IN GEAR HANDLE WOULD NOT ILLUMINATE. VERIFIED GEAR DOWN AND LOCKED, AI - [SDR SRAA970201](https://openairdocs.org/sdr/SRAA970201), Feb 4, 1997: DUCT. CRACKED. ON CLIMB-OUT FROM MIA FLIGHT 1203, CARGO COMPARTMENT OVERHEAT LIGHT CAME ON, ACCOMPLISHED AIR TURN BACK TO MIA. REMOVED AND REPLACED CARGO COMPARTMENT COOLING T - [SDR SRAA970113](https://openairdocs.org/sdr/SRAA970113), Jan 15, 1997: B-NUT. LOOSE. ONE HOUR INTO FLIGHT LOST BOOSTER HYDRAULIC SYSTEM. RETURN TO KOAK AND AIRCRAFT LANDED WITHOUT INCIDENT. FOUND HYDRAULIC LINE B-NUT IN AUXILIARY CAVITY LOOSE. R - [SDR SRAA970105](https://openairdocs.org/sdr/SRAA970105), Jan 9, 1997: DOOR. BROKEN. DURING TAKEOFF ROLLOUT AT APPROX 50 KIAS, CREW HEARD A LOUD NOISE THAT CAME FROM REAR OF AIRCRAFT. LOAD HAD BROKEN LOOSE, REJECTED TAKEOFF AND AIRCRAFT RETURNED - [SDR SRAA961215](https://openairdocs.org/sdr/SRAA961215), Dec 28, 1996: LIGHT. MISINSTALLED. DURING FLIGHT, FOUND THE EMERGENCY EXIT LIGHT WOULD NOT FUNCTION PROPERLY IN THE ARMED OR ON POSITIONS. FOUND LIGHT ASSEMBLY MOUNTED BACKWARDS. REMOVED LIGHT, C - [SDR SRAA961213](https://openairdocs.org/sdr/SRAA961213), Dec 24, 1996: VALVE HOUSING. DEFECTIVE. DURING FLIGHT, NR 4 ENGINE WENT TO 103 PERCENT RPM, AT THE SAME TIME ENGINE TORQUE, TIT AND FUEL FLOW READINGS WERE DECREASING. SHUT DOWN NR 4 ENGINE AND LANDED - [SDR SRAA961211](https://openairdocs.org/sdr/SRAA961211), Dec 19, 1996: VALVE HOUSING. FAILED. ON CLIMBOUT, AT FL 175 NR 2 PROP RPM WENT TO 105 PERCENT. SHUT DOWN NR 2 ENGINE AND CONTINUED TO DESTINATION. AIRCRAFT LANDED AT TOL WITHOUT INCIDENT. REPLACED - [SDR SRAA961208](https://openairdocs.org/sdr/SRAA961208), Dec 16, 1996: DIR GYRO. FAILED. AFTER TAKEOFF, FOUND NR 1 COMPASS WOULD NOT TURN. DUMPED FUEL AND ACCOMPLISHED AIR TURNBACK TO CHS. FOUND NR 1 DIRECTIONAL GYRO FAULTY. REMOVED AND REPLACED NR - [SDR SRAA961114](https://openairdocs.org/sdr/SRAA961114), Nov 21, 1996: AIR SPEED IND. INOPERATIVE. ON TAKEOFF ROLL, F/O'S AIRSPEED INDICATOR STUCK AT 50 KIAS WITH CAPTAIN'S INDICATOR READING 70 KIAS. ABORTED TAKEOFF WITHOUT INCIDENT. PERFORMED PITOT STATIC CH - [SDR SRAA961110](https://openairdocs.org/sdr/SRAA961110), Nov 13, 1996: DOME SEAL. LEAKING. ON CLIMB-OUT FLIGHT 1203 FROM CHS, NR 1 AND NR 3 PROPELLER LOW OIL LIGHTS CAME ON. ACCOMPLISHED AIR TURN BACK TO CHS. FOUND NR 1 PROPELLER LEAKING FLUID OUT OF - [SDR SRAA961108](https://openairdocs.org/sdr/SRAA961108), Nov 7, 1996: GASKET. UNSEATED. DURING FLIGHT 1005, FOUND RIGHT FORWARD WHEELWELL EXTREMELY HOT WHEN CARGO COMPARTMENT OVERHEAT WARNING LIGHT CAME ON. AIRCRAFT WILL NOT PRESSURIZE PROPERLY, ON - [SDR SRAA961016](https://openairdocs.org/sdr/SRAA961016), Oct 31, 1996: HYD FITTING. LEAKING. DURING FLIGHT, UTILITY HYDRAULIC PRESSURE DUMPED, MANUALLY LOWERED GEAR AND LANDED WITHOUT INCIDENT. FOUND NORMAL BRAKE LINE UNDER FLIGHT DECK LEAKING. REPLACED - [SDR SRAA960904](https://openairdocs.org/sdr/SRAA960904), Sep 7, 1996: ENGINE. MALFUNCTIONED. ON TAKEOFF ROLL, NR 3 ENGINE WAS FOUND SLOW TO RESPOND TO THROTTLE MOVEMENT, AT APPROXIMATELY 40 KTS TAKEOFF WAS REJECTED, NO EXCESSIVE BRAKING FORCE USED. PERF - [SDR SRAA960905](https://openairdocs.org/sdr/SRAA960905), Sep 3, 1996: OVERHEAT WARNING. ACTIVATED. WHILE PULLING OFF OF RUNWAY, NR 2 ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. SHUTDOWN NR 2 ENGINE WHILE TAXING. - [SDR SRAA960801](https://openairdocs.org/sdr/SRAA960801), Aug 4, 1996: B-NUT. LOOSE. AFTER TAXIING OUT FOR FLIGHT 1206 FROM HOW, NR 2 ENGINE NACELLE OVERHEAT WARNING LIGHT CAME ON. SHUT DOWN ENGINE AND RETURNED TO BLOCK. FOUND LOOSE 'B' NUT ON N - [SDR SRAA960709](https://openairdocs.org/sdr/SRAA960709), Jul 30, 1996: ENGINE. RPM FLUX. ON TAKEOFF ROLL FOR FLIGHT 1205 OUT OF COF, NR 4 ENGINE HAD 2 PERCENT RPM FLUX WITH ALL OTHER PARAMETERS FLUXING ALSO, REJECTED TAKEOFF WITHOUT FURTHER INCIDENT - [SDR SRAA69607](https://openairdocs.org/sdr/SRAA69607), Jun 20, 1996: ADI. FAILED. DURING FLIGHT 9001 OUT OF YIP, CO-PILOTS GYRO FLAG CAME IN VIEW, ACCOMPLISHED AIR TURN BACK TO YIP WITHOUT INCIDENT. FOUND CO-PILOTS ADI FAILED, REMOVED AND REP - [SDR SRAA59603](https://openairdocs.org/sdr/SRAA59603), May 12, 1996: ENGINE. DAMAGED. FLT NR 1 AD08 REPORTED, NR 1 ENGINE BLEED AIR CAUSED AIR CONDITIONING TO EMIT FUMES, CLOSED NR 1 BLEED VALVE TO ELIMINATE FUMES. ON LANDING, CARGO COMPARTMENT F - [SDR SRAA59601](https://openairdocs.org/sdr/SRAA59601), May 5, 1996: COALESCER. DIRTY. ON DESCENT INTO MHZ CARGO AND FLIGHT DECK FILLED UP WITH SMOKE COMING FROM CARGO COMPARTMENT AIR CONDITIONER, ACCOMPLISHED LANDING WITHOUT INCIDENT. FOUND WATER - [SDR SRAA49605](https://openairdocs.org/sdr/SRAA49605), Apr 25, 1996: BLEED VALVE. DIRTY. FLIGHT 3904 - REPORTED NR 2 ENGINE FLAME OUT EN ROUTE MOMBASA, SECURED ENGINE PER AOM, PROCEEDED TO DESTINATION AND LANDED WITHOUT INCIDENT. MX CLEANED DIRTY 5T - [SDR SRAA39603](https://openairdocs.org/sdr/SRAA39603), Mar 28, 1996: DUCT. BLOWN. DURING DESCENT FOR FLT ADH3 INTO EZE, NR 2 ENGINE NACELLE OVERHEAT LIGHT ILLUMINATED AT 6,000 FEET ALTITUDE, FEATHERED NR 2 PROPELLER AND SHUT DOWN NR 2 ENGINE, - [SDR 96ZZZM615](https://openairdocs.org/sdr/96ZZZM615), Mar 5, 1996: VALVE HOUSING. DEFECTIVE. DURING FLIGHT AD08 NR 2 ENGINE RPM DECAYED TO 97 PERCENT, PRECAUTIONARY SHUTDOWN NR 2 ENGINE AND LANDED SAFELY AT AAB. FOUND NR 2 VALVE HOUSING MALFUNCTIONED, R - [SDR SRAA29602](https://openairdocs.org/sdr/SRAA29602), Feb 2, 1996: VENT TUBE. CRACKED. FLT UPA3060 - ON CLIMB-OUT FROM LTN, NR 3 ENGINE NACELLE OVEHEAT LIGHT ILLUMINATED, SHUT DOWN NR 3 ENGINE AND ACCOMPLISHED AIR TURN BACK TO LTN. FOUND COMPRESSO - [SDR SRAA19602](https://openairdocs.org/sdr/SRAA19602), Jan 19, 1996: RETRACT MECH. LACK OF LUBE. CYWG - FLT 1002 - OUT OF CYWG ON LANDING GEAR RETRACTION (OAT MINUS 35 DEGREES CELSIUS), RT MLG INDICATED FULL DOWN. ON DESCENT TO LAX, RT MLG INDICATED UP - (O - [SDR SRAA960103](https://openairdocs.org/sdr/SRAA960103), Jan 6, 1996: SKIN. PUNCTURED. DURING ROUTINE MAINTENANCE, FOUND 2 HOLES PUNCTURED THROUGH CARGO DOOR SKIN AT APPROX FS STA 920. HOLES MEASURED APPROX 2 WIDE, ACCOMPLISHED REPAIR IAW LOCKHEED - [SDR SRAA960102](https://openairdocs.org/sdr/SRAA960102), Jan 6, 1996: VERT BEAM WEB. CRACKED. DURING ROUTINE INSPECTION, FOUND LEFT FORWARD MLG WHEEL WELL HAS 2 CRACKS ON VERTICAL BEAM WEB, APPROX WL 175. ONE CRACK IS APPROX 2 INCHES AND THE OTHER APPROX - [SDR SRAA129503](https://openairdocs.org/sdr/SRAA129503), Dec 14, 1995: VALVE HOUSING. DAMAGED. FLT NR 9006 - SNN-YQX - NR 1 ENGINE RPM SLOWLY DECAYED TO 98 PERCENT WHILE SLAVING TO NR 2 ENGINE AS MASTER. WITH NO MASTER SELECTED, NR 1 PROP GOES TO 96.7 PER - [SDR SRAA129502](https://openairdocs.org/sdr/SRAA129502), Dec 8, 1995: VALVE HOUSING. INOPERATIVE. DURING FLIGHT MAD08 TO MHZ, NR 3 ENGINE RPM DECAYED TO 97 PERCENT AND TORQUE WAS 5,000-10,000 INCHES/POUNDS AT FLIGHT IDLE (DEPENDING ON ALTITUDE), SHUT DOWN EN All 57: https://openairdocs.org/model/lockheed-382e/reports.md ## STCs that may be installed (OpenAirDocs) (33) 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 SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc - [STC ST02495LA](https://openairdocs.org/stc/ST02495LA): Installation of a multipurpose hatch system. R4 Integration Inc - [STC SA3934NM](https://openairdocs.org/stc/SA3934NM): Fabrication of Biegert Airborne dispersant delivery system (ADDS). Oil Spill Response (Americas) Limited - [STC SA733CE](https://openairdocs.org/stc/SA733CE): Installation of cargo pallets. Telair US LLC - [STC ST01635WI-D](https://openairdocs.org/stc/ST01635WI-D): Modification of Rockwell Collins, Inc. VHF-4000 and VHF-4000E installations. Rockwell Collins Inc - [STC SA3132NM](https://openairdocs.org/stc/SA3132NM): Installation of a de-icing system on the Hamilton Standard P/N 554654 propeller spinner. ROBERT W. MURRAY - [STC SA3407NM](https://openairdocs.org/stc/SA3407NM): Installation of a de-icing system on the Hamilton Standard P/N 560501 propeller spinner afterbody. ROBERT W. MURRAY - [STC ST00435CH-D](https://openairdocs.org/stc/ST00435CH-D): Installation of a Collins TCAS-94 Traffic Alert and Collision Avoidance System (TCAS-II) system. Duncan Aviation Inc - [STC ST434CH-D](https://openairdocs.org/stc/ST434CH-D): Installation of Dual Trimble TNL8100 GPS Navigation Systems. Duncan Aviation Inc - [STC SA1625WE](https://openairdocs.org/stc/SA1625WE): Pallet assembly provisions. Lockheed Martin Aeronautics Company - [STC ST00224AT](https://openairdocs.org/stc/ST00224AT): Installation of an Expanded Parameters Digital Flight Data Recorder. ASB Avionics - [STC SA02365CH](https://openairdocs.org/stc/SA02365CH): Installation of NASI Supplemental Air-Conditioning System. National Aircraft Service Inc - [STC ST01307WI-D](https://openairdocs.org/stc/ST01307WI-D): Modification of a Collins TVI-920/TVI-920D Vertical Speed/TCAS Indicator installation. Rockwell Collins Inc - [STC SA3171WE](https://openairdocs.org/stc/SA3171WE): The auxiliary power unit Model GTC 85-71 located in the forward end of the left hand main landing gear wheel well fairing has been replaced by an AiResearch Gas turbine compressor Model GTCP85-98CK(A). Kellstrom Defense Aerospace Inc - [STC SA1371GL](https://openairdocs.org/stc/SA1371GL): Installation of Norton Radome Kit No. 4853CX. Saint-Gobain Performance Plastics Corp - [STC SA3144WE](https://openairdocs.org/stc/SA3144WE): Installation of Collins FPC-75 ground proximity warning system. Rockwell Collins Inc - [STC ST09345SC](https://openairdocs.org/stc/ST09345SC): Installation of a dual independent UNS-1Msp navigation management system. New Systems - [STC ST555CH](https://openairdocs.org/stc/ST555CH): Approve operation at runway gradients up to 8 %. Southern Air Transport - [STC ST435CH-D](https://openairdocs.org/stc/ST435CH-D): Installation of a Collins TCAS-94 traffic alert and collision avoidance system (TCAS-II) system. Duncan Aviation - [STC SA384SO](https://openairdocs.org/stc/SA384SO): Installation of C-5A engine/EBU transportation dolly. Lockheed Martin Aeronautics Company - [STC ST374SO](https://openairdocs.org/stc/ST374SO): Palletized cargo loading system per Lockheed Industrial Products top assy. dwg. 256-000. Lockheed Martin Aeronautics Company - [STC ST400SO](https://openairdocs.org/stc/ST400SO): Installation of palletized cargo loading and restraint system. Lockheed Martin Aeronautics Company - [STC ST401SO](https://openairdocs.org/stc/ST401SO): Installation of palletized cargo loading and restraint. Lockheed Martin Aeronautics Company - [STC ST407SO](https://openairdocs.org/stc/ST407SO): Installation of palletized cargo loading and restraint system. Lockheed Martin Aeronautics Company - [STC ST439SO](https://openairdocs.org/stc/ST439SO): Installation of palletized carrgo loading and restraint system. Lockheed Martin Aeronautics Company - [STC ST531SO](https://openairdocs.org/stc/ST531SO): Increase in maximum landing weight from 130,000 pounds to 135,000 pounds. (382B s/n 4209, 4234, 4248) (382E s/n 4222, 4300). Lockheed Martin Aeronautics Company - [STC SA2461WE](https://openairdocs.org/stc/SA2461WE): Modify tye design by installation of Sorm bulk liquid cargo tank assembly SI-3100. Sorm Industries - [STC ST521SO](https://openairdocs.org/stc/ST521SO): Increase in maximum landing weight to 135,000 pounds and maximum zero fuel weight to 128,790 pounds with pylon tanks on and 127,000 pounds with pylon tanks off. Lockheed Martin Aeronautics Company - [STC SA569AL](https://openairdocs.org/stc/SA569AL): Installation Collins FPC-75 ground proximity warning system. Alaska Intl Air, Inc - [STC ST527SO](https://openairdocs.org/stc/ST527SO): Installation of inplane cargo system. Southern Air Transport, Inc - [STC SA448AL](https://openairdocs.org/stc/SA448AL): Modification of Lockheed Air Service Model 109C/R Flight Recorder. Alaska International Air - [STC SA2418WE](https://openairdocs.org/stc/SA2418WE): Installation of cargo loading system. Saturn Airways, Inc - [STC SA1156SO](https://openairdocs.org/stc/SA1156SO): Installation of dual Litton, LTN-211, Omega navigation system(ONS). Southern Air Transport Inc --- 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.