# Lockheed 1329 - Type: Aircraft model (FAA registry) - Registry code: 5263102 - Manufacturer (registry): LOCKHEED - Model: 1329 - Aircraft type: Fixed wing multi engine - Category: Airplane - Engines: 4 · Turbo-jet - Seats: 8 - Weight class: 20,000 lb and over - Cruise speed: 371 mph - Certification: Type certificated - Registered aircraft: 0 - Page: https://openairdocs.org/model/lockheed-1329 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. None matched. ## Registered aircraft None registered with this model now. ## NTSB investigations (4) 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 MIA90FA049](https://openairdocs.org/ntsb/MIA90FA049), Jan 6, 1990: Lockheed L1329 (N96GS), Miami, FL, destroyed, 1 fatal. Probable cause: THE PILOT'S IMPROPER DECISION TO REJECT THE TAKEOFF AFTER THE AIRPLANE HAD PASSED V1 SPEED AND LIFTED OFF THE RUNWAY. A FACTOR WAS A MALFUNCTIONING #2 ENGINE ELECTRONIC ENGINE CONTTROL WHICH CAUSED… - [NTSB FTW80DA095](https://openairdocs.org/ntsb/FTW80DA095), Jul 23, 1980: Lockheed 1329 (N22RB), Beaumont, TX, substantial damage - [NTSB CHI76AC055](https://openairdocs.org/ntsb/CHI76AC055), Mar 25, 1976: Lockheed Ga 1329 (N1EM), Chicago, IL, destroyed, 4 fatal - [NTSB NYC73AN090](https://openairdocs.org/ntsb/NYC73AN090), Dec 27, 1972: Lockheed L1329 (N400M), Saranac Lake, NY, destroyed, 3 fatal ## FAA accident and incident reports (5) 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 19900106000109A](https://openairdocs.org/incident/19900106000109A), Jan 6, 1990: Lkheed 1329 (N96GS), Miami, FL, Destroyed, 1 fatal. NR3 engine overheat light lit on 3 engine takeoff. Aborted ran off end crashed burned. Could have continued takeoff - [Incident 19850803046279I](https://openairdocs.org/incident/19850803046279I), Aug 3, 1985: Lkheed 1329 (N530G), Houston, TX, Minor damage. During taxi to hangar after landing after training flight a bump was felt. Fire on nr 4 tire and 2 others flat. - [Accident 19800723034749A](https://openairdocs.org/incident/19800723034749A), Jul 23, 1980: Lkheed 1329/ (N22RB), Beaumont, TX, Substantial damage. Failed to check gear down. Landed with gear up. - [Incident 19780123004309I](https://openairdocs.org/incident/19780123004309I), Jan 23, 1978: Lkheed 1329/ (N530G), Houston, TX. Thrust reverser deployed during descent when throttles were pulled back. Shut down engine. - [Accident 19760325022109A](https://openairdocs.org/incident/19760325022109A), Mar 25, 1976: Lkheed 132923E (N1EM), Chicago, IL, Destroyed, 2 fatal. PIC flew dash 8 jetstar never flew dash 6 which has 1200 lb less thrust than dash 8. ## Service difficulty reports (13) As reported by operators and repair stations, by the model named in the report. - [SDR 2007FA0000232](https://openairdocs.org/sdr/2007FA0000232), Mar 5, 2007: BATTERY. FAILED. THESE 2 EA PN RG-380E/44 MAIN SHIP BATTERIES WERE INSTALLED ON 10/30/2006. THESE BATTERIES WERE REPLACEMENTS FOR 2 EA BATTERIES THAT HAD BEEN IN SATISFACTORY SE - [SDR 2002FA0001323](https://openairdocs.org/sdr/2002FA0001323), Nov 14, 2002: ANTI-ICE VALVE. INOPERATIVE. ANTI-ICE VALVE RECEIVED FROM OVERHAUL AGENCY WITH A FRESH OVERHAUL, SOLENOID VALVE WAS CLOCKED 90 DEGREE FROM WHERE THE PRODUCTION PRINT SHOWED WHERE IT SHOULD - [SDR 2002FA0001322](https://openairdocs.org/sdr/2002FA0001322), Nov 14, 2002: ANTI-ICE VALVE. INOPERATIVE. ANTI-ICE VALVE RECEIVED FROM OVERHAUL AGENCY WITH A FRESH OVERHAUL, SOLENOID VALVE WAS CLOCKED 90 DEGREE FROM WHERE THE PRODUCTION PRINT SHOWED WHERE IT SHOULD - [SDR QQG2002F00000](https://openairdocs.org/sdr/QQG2002F00000), May 23, 2002: VALVE. INOPERATIVE. ANTI-ICE VALVE FAILED AFTER 62.9 HOURS, AFTER OVERHAUL. VALVE STUCK IN THE CLOSED POSITION. SINCE THERE WAS NO REPLACEMENT VALVES AVAILABLE, AND ATTEMPT WAS MAD - [SDR 20000601SH025](https://openairdocs.org/sdr/20000601SH025), May 22, 2000: DOUBLER. CRACKED. UPON DISCOVERY OF CRACKS IN SN 5078, INSPECTED BOTH SPAR CAPS ON SN 5062 AND DISCOVERED A CRACK ON THE LEFT SIDE SPAR CAP DOUBLER (JE15-15L). THE CRACK IS ADJAC - [SDR 20000601SH024](https://openairdocs.org/sdr/20000601SH024), May 22, 2000: DOUBLER. CRACKED. WHILE DISASSEMBLING THE TAIL FOR PERMANENT STORAGE, A CRACK WAS DISCOVERED ON THE LEFT AND RIGHT SPAR CAP DOUBLERS (JE15-15L AND JE15-15R) ON THE LOWER SIDE OF - [SDR 20000530SH004](https://openairdocs.org/sdr/20000530SH004), May 12, 2000: SPAR CAP. CRACKED. DURING ROUTINE INSPECTION OF THE JE24 PIVOT FITTING, IT WAS RECOMMENDED BY THIS REPAIR STATION TO INSPECT THE LOWER VERTICAL STABILIZER FRONT SPAR CAP DOUBLERS - [SDR CA000209009](https://openairdocs.org/sdr/CA000209009), Jan 28, 2000: FITTING. CRACKED. (CAN) PART CRACKED BEYOND LIMITS. - [SDR CA000209008](https://openairdocs.org/sdr/CA000209008), Jan 28, 2000: FITTING. CRACKED. (CAN) DURING SCHELDULED NDT RT UPPER FWD ATTACH LUG FOUND CRACKED. - [SDR 97ZZZX1208](https://openairdocs.org/sdr/97ZZZX1208), Feb 14, 1997: PUMP. FAILED. FUEL PUMP WAS OVERHAULED BY CRS NR ZK3R027M ON 10-5-93. OVERHAUL REQUIREMENT IS 2000 HOURS. TIME SINCE OVERHAUL ON PART WAS 466 HOURS. PUMP WOULD NOT MAINTAIN P - [SDR 96ZZZX3455](https://openairdocs.org/sdr/96ZZZX3455), Jun 10, 1996: CIRCUIT BOARD. FAILED. THE CIRCUIT BOARD MAINTENANCE RELEASE TAG WAS IDENTIFIED WITH PN 42-15919NL, SN 351, ACTUAL UNIT WAS IDENTIFIED WITH PN 42-15919NL, SN 341. AFTER CIRCUIT BOARD - [SDR 95ZZZX4177](https://openairdocs.org/sdr/95ZZZX4177), Jun 8, 1995: TEMP CONTL COMP. INOPERATIVE. FOLLOW-UP OF SDR RELATING TO PRESSURIZATION PROBLEM, DIFFICULTY TRACED TO TEMP CONTROL BOX LOCATED IN AFT EQUIPMENT AREA. CONTROLLER REPLACED. OPERATIONAL CHECK - [SDR 95ZZZX1254](https://openairdocs.org/sdr/95ZZZX1254), Mar 1, 1995: LATCH. NOT LATCHED. TOP 2 LATCHES WERE NOT LATCHED PERFECTLY ALLOWING PRESSURE SEAL TO BLOW OUT AT THE TOP BETWEEN THE LATCHES. SUBMITTER SUGGESTION IS TO LATCH THE 2 TOP LATCHES F --- 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.