# GE CJ610-6 - Type: Engine model (FAA registry) - Registry code: 30122 - Manufacturer (registry): GE - Model: CJ610-6 - Engine type: Turbo-jet - Power: 2,950 lb thrust - Data sheet: [TCDS 1E16](https://openairdocs.org/tcds/1E16) (OpenAirDocs) - Holder: General Electric Company - Installed in: 6 registered aircraft - Page: https://openairdocs.org/engine/ge-cj610-6 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 2010-09-08](https://openairdocs.org/ad/2010-09-08): AFT Technologies combustion liners · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective May 28, 2010 - [AD 2001-10-12](https://openairdocs.org/ad/2001-10-12): Unapproved Parts · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jun 7, 2001 - [AD 98-23-06](https://openairdocs.org/ad/98-23-06): Combustion Liner Assemblies · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Nov 20, 1998 - [AD 97-25-08](https://openairdocs.org/ad/97-25-08): General Electric CF700-2C, CF700-2D, CF700-2D-2 and 7 more. Effective Jan 2, 1998 - [AD 78-07-06](https://openairdocs.org/ad/78-07-06): Compressor Disks · General Electric CF700-2C, CF700-2D, CF700-2D-2 and 2 more - [AD 73-23-05](https://openairdocs.org/ad/73-23-05): First Stage Turbine Discs · General Electric CF700-2C, CJ610-1, CJ610-4 and 2 more ## Information bulletins (advisory) (2) - [SAIB NE-08-49R1](https://openairdocs.org/saib/NE-08-49R1): Turbine Engine Combustion Section. Issued Sep 17, 2008 - [SAIB NE-08-49](https://openairdocs.org/saib/NE-08-49) (historical): Turbine Engine Combustion Section. Issued Sep 9, 2008 ## Registered aircraft (6) - [N262MF](https://openairdocs.org/aircraft/N262MF): [Tsi Holdco Inc](https://openairdocs.org/faa-owner/TSI%20HOLDCO%20INC), [Virginia Beach, VA](https://openairdocs.org/faa-place/VA/Virginia%20Beach), built 2011, S/N 501243 - [N400MS](https://openairdocs.org/aircraft/N400MS): [Mil Oh LLC](https://openairdocs.org/faa-owner/MIL%20OH%20LLC), [Camden, DE](https://openairdocs.org/faa-place/DE/Camden), built 1972, S/N 246 - [N496WM](https://openairdocs.org/aircraft/N496WM): [Supertweet LLC](https://openairdocs.org/faa-owner/SUPERTWEET%20LLC), [Lincoln, NE](https://openairdocs.org/faa-place/NE/Lincoln), built 1972, S/N 71-826 - [N555LJ](https://openairdocs.org/aircraft/N555LJ): [Beck Angelique Verschuur](https://openairdocs.org/faa-owner/BECK%20ANGELIQUE%20VERSCHUUR), [Ione, CA](https://openairdocs.org/faa-place/CA/Ione), S/N 195 - [N610FM](https://openairdocs.org/aircraft/N610FM): [Swift Air International Inc](https://openairdocs.org/faa-owner/SWIFT%20AIR%20INTERNATIONAL%20INC), [San Pedro, CA](https://openairdocs.org/faa-place/CA/San%20Pedro), S/N FM30 - [N890MJ](https://openairdocs.org/aircraft/N890MJ): [Jensen Mark A](https://openairdocs.org/faa-owner/JENSEN%20MARK%20A), [Dallas, TX](https://openairdocs.org/faa-place/TX/Dallas), built 1977, S/N 229 ## NTSB investigations None matched to aircraft with this engine model. ## FAA accident and incident reports None matched to aircraft with this engine model. ## Service difficulty reports (131, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR KC8A20121116001](https://openairdocs.org/sdr/KC8A20121116001), Nov 16, 2012: ENGINE. FLAMED OUT. DURING CLIMBOUT FROM KOSC EN ROUTE TO KJFK THROUGH FLIGHT LEVEL 390, THE RIGHT ENGINE FLAMED OUT. ATC WAS CONTACTED, A LOWER ALTITUDE AND RETURNED TO KYIP WAS R - [SDR 2011F00033](https://openairdocs.org/sdr/2011F00033), Feb 10, 2011: FILTER. CONTAMINATED. CABIN WAS PRESSURIZING BUT PILOT REPORTED ERRATIC CABIN RATE OF CLIMB AND ELECTED TO RETURN TO BASE. MX CHECKED TAILCONE FOR PRESSURE LEAKS NONE FOUND. MX CHECK - [SDR KC8AN76CK](https://openairdocs.org/sdr/KC8AN76CK), Jun 19, 2009: ENGINE. FLAMED OUT. LT ENGINE FLAMED OUT AT 40,000FT, DURING CRUISE IN TURBULENT AIR. PILOT DESCENDED TO A LOWER ALTITUDE AND PERFORMED A SUCCESSFUL RELIGHT OF THE ENGINE. NO ABNOR - [SDR HAEA200800205A](https://openairdocs.org/sdr/HAEA200800205A), Nov 10, 2008: PUMP. FAILED. ENGINE RPM ROLLED BACK FL430 PLUS 30 MINUTES. AIRCRAFT DESCENDED TO FL 150 AND DIVERTED TO GSP. MAINTENANCE DISCOVERED ENGINE DRIVEN FUEL PUMP FAILED. REPLACED - [SDR G41A2007003](https://openairdocs.org/sdr/G41A2007003), Oct 9, 2007: ENGINE. FLAMED OUT. LEARJET N26AT WAS ON THE WAY FROM ELP TO LAX AT FL 410, THE CREW WAS EXPERIENCING SEVERE WEATHER AND REQUESTED TO GO TO FL 450. DURING THE CLIMB THEY HIT TURBUL - [SDR N76CK80606](https://openairdocs.org/sdr/N76CK80606), Aug 6, 2006: ENGINE. FOD. CREW REPORTED RT FIRE WARNING LIGHT FLICKERING WHEN POWER LEVER WAS PULLED BACK TO THE IDLE POSITION. NO SECONDARY INDICATIONS NOTED. FOUND EXHAUST CASE LEAKING - [SDR KC8A0608001](https://openairdocs.org/sdr/KC8A0608001), Aug 3, 2006: GASKET. BLOWN. PILOT REPORTED RT ENGINE FIRE WARNING LIGHT FLICKERING ON DESCENT WITH POWER LEVER REDUCED TO IDLE SPEED. FOUND EXHAUST CASE, CENTER BODY, UPPER RIGHT STRUT SUP - [SDR HAEA200600191](https://openairdocs.org/sdr/HAEA200600191), Jun 27, 2006: ENGINE. POWER LOSS. AIRCRAFT ENCOUNTERED TURBULENCE AT FL430 AND RT ENGINE LOST POWER. AIRCRAFT DESCENDED AND ENGINE REGAINED POWER AT FL250. MAINTENANCE PERFORMED POST OPERATION I - [SDR 4262006N236CA](https://openairdocs.org/sdr/4262006N236CA), Apr 26, 2006: COMPRESSOR WHEEL. FOD. AT 285 KNOTS AT FL270 THE LT ENGINE WENT DOWN TO 20 PERCENT N1. THE AIRCRAFT DIVERTED AND LANDED UNEVENTFUL. MAINTENANCE FOUND FOD ON THE 1ST STAGE OF THE COMPR - [SDR CED2006F00000](https://openairdocs.org/sdr/CED2006F00000), Nov 1, 2005: RUDDER PEDAL. STIFF. THE FLIGHT CREW ABORTED TAKEOFF ROLL. THE FLIGHT CREW NOTICED ON TAKEOFF ROLL THAT THE RUDDER PEDALS FELT STIFF AND HAD VERY LITTLE MOVEMENT. MAINTENANCE INSPEC - [SDR CED2006F00021](https://openairdocs.org/sdr/CED2006F00021), Oct 4, 2005: ENGINE. SHUTDOWN. THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED WITHOUT INCEDENT. MAINTENANCE HAS NOT YET INSPECTED THE AIRCRAFT TO DETE - [SDR CED2006F00020](https://openairdocs.org/sdr/CED2006F00020), Oct 3, 2005: INDICATOR. DEFECTIVE. THE AIRCRAFT ABORTED TAKEOFF ROLL, THE NR 2 ENGINE WAS NOT MAKING TAKEOFF EPR. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND A DEFECTIVE EPR GAUGE. MAINTENANCE R - [SDR CED2006F00005](https://openairdocs.org/sdr/CED2006F00005), Sep 1, 2005: ALTIMETER. FAILED. ON DEPARTURE, THE CAPTAIN`S ALTIMETER FAILED. REMOVED AND REPLACED ALTIMETER. SYSTEM OPS CHECK GOOD. (K) - [SDR CED2006F00010](https://openairdocs.org/sdr/CED2006F00010), Aug 21, 2005: ENGINE. MALFUNCTIONED. HAD TO ABORT THE TAKEOFF WHILE ATTEMPTING TO DEPART. THE REASON FOR THE ABORT WAS THAT THE NR 2 ENGINE WOULD NOT PRODUCE TAKEOFF FOR THE CONDITIONS. MAINTENANCE - [SDR CED2006F00018](https://openairdocs.org/sdr/CED2006F00018), Aug 21, 2005: INSULATOR. DIRTY. WHILE DESCENDING THROUGH FL 220 FOR APPROACH INTO AIRPORT, THE NR2 FIRE LIGHT CAME ON MOMENTARILY. IMMEDIATELY REDUCED THE RT THRUST LEVER TO IDLE. MAINTENANCE - [SDR CED2006F00023](https://openairdocs.org/sdr/CED2006F00023), Jul 21, 2005: ENGINE. MALFUNCTIONED. ON TAKEOFF ROLL, THE NR 2 ENGINE WOULD NEVER PRODUCE TAKEOFF . THE CREW ABORTED TAKEOFF ROLL AND EXITED THE RUNWAY. MAINTENANCE INSPECTED THE AIRCRAFT AND FOUND - [SDR 7032005N213CA](https://openairdocs.org/sdr/7032005N213CA), Jul 3, 2005: HOSE. KINKED. ENROUTE, UPON THE AIRCRAFT REACHING ITS ASSIGNED LEVEL OF FL 430 POWER WAS REDUCED FOR CRUISE AND THE NR 2 ENGINE QUIT. AIRCRAFT DESCENDED TO FL 250 AND THE ENG - [SDR 6252004N8005Y](https://openairdocs.org/sdr/6252004N8005Y), Jun 25, 2005: CABIN PRESSURE. MALFUNCTIONED. WHILE ENROUTE, AT FLIGHT LEVEL 410 THE CABIN ALTITUDE EXCEEDED 10000 FT, THE FLIGHT CREW FOLLOWED THE CHECKLIST PROCEDURES AND DIVERTED AND LANDED WITHOUT FURTH - [SDR 6242004N238CA](https://openairdocs.org/sdr/6242004N238CA), Jun 24, 2005: FIRE LOOP. OUT OF POSITION. ON DECENT, THE FLIGHT CREW RECEIVED INDICATION OF FIRE IN THE NR1 ENGINE. THE FLIGHT CREW PERFORMED THE CHECKLIST AND COULD NOT CANCEL THE FIRE LIGHT. THE FLIGH - [SDR 2006FA0000120](https://openairdocs.org/sdr/2006FA0000120), Jun 17, 2005: STATIC LINE. LOOSE. WHILE ENROUTE, CABIN ALTITUDE EXCEEDED 10,000 FT. THE FLIGHT CREW FOLLOWED EMERGENCY PROCEDURES BUT WAS UNABLE TO RETURN THE CABIN PRESSURIZATION WITHIN NORMAL - [SDR CED2006F00007](https://openairdocs.org/sdr/CED2006F00007), Jun 14, 2005: TIRE. DESTROYED. ON TAKEOFF ROLL THE AIRCRAFT BLEW THE LT MAIN GEAR TIRES IN ELP. (K) - [SDR CED2006F00019](https://openairdocs.org/sdr/CED2006F00019), May 28, 2005: FIRE DETECTOR. FALSE ACTIVATION. WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIGH - [SDR CED2006F00014](https://openairdocs.org/sdr/CED2006F00014), May 19, 2005: ELEMENT. FALSE INDICATION. AFTER TAKEOFF AT FLIGHT LEVEL 220, THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STANDARD EMERGENCY PROCEDURES AND RETU - [SDR CED2006F00008](https://openairdocs.org/sdr/CED2006F00008), May 17, 2005: CASE. CRACKED. WHILE ENROUTE, AT FLIGHT LEVEL 390, FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT - [SDR CED2006F00017](https://openairdocs.org/sdr/CED2006F00017), May 6, 2005: PLATE. MALFUNCTIONED. ON DESCENT, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (K) - [SDR 2004F00421](https://openairdocs.org/sdr/2004F00421), Oct 4, 2004: ENGINE. SHUTDOWN. AT FL370, THE NR 2 ENGINE SHUTDOWN. THE FLIGHT CREW FOLLOWED THE EMERGENCY CHECKLIST AND DIVERTED TO LIT WITHOUT INCIDENT. MAINTENANCE HAS NOT YET INSPECTED THE - [SDR 2004F00338](https://openairdocs.org/sdr/2004F00338), Sep 1, 2004: CONTROL CABLE. BROKEN. THROTTLE CABLE BROKEN 12 INCHES FROM END OF CABLE. BROKEN AT AFT END OF FORWARD CABLE WHERE FORWARD CABLE ATTACHES TO AFT CABLE. (SO13200405891) - [SDR HAEA200400165](https://openairdocs.org/sdr/HAEA200400165), Aug 18, 2004: LANDING GEAR. LACK OF LUBE. LANDING GEAR WOULD NOT RETRACT AFTER TAKE OFF. AIRCRAFT RETURNED TO BASE. MAINTENANCE LUBED LANDING GEAR AND PERFORMED GEAR SWING. CYCLED GEAR AT LEAST 20 TIMES - [SDR CED2004F00004](https://openairdocs.org/sdr/CED2004F00004), May 28, 2004: FIRE WARNING. FALSE ACTIVATION. WHILE ENROUTE, THE CREW EXPERIENCED INDICATION OF FIRE ON THE NR 2 ENGINE. THE CREW THEN FOLLOWED THE EMERGENCY CHECK LIST AND COULD NOT EXTINGUISH THE FIRE LIG - [SDR 00141](https://openairdocs.org/sdr/00141), May 24, 2004: ENGINE. FLAMED OUT. AIRCRAFT ENCOUNTERED TURBULENCE AT FL390K. LT ENGINE FLAMED OUT. ENGINE RELIGHT NORMAL. - [SDR CED2004F00003](https://openairdocs.org/sdr/CED2004F00003), May 21, 2004: FUEL SYS. LEAKING. ON TAKEOFF ROLL AND INITIAL CLIMB OUT, FUEL WAS OBSERVED LEAKING FROM THE LEFT WING TIP. ATC INFORMED THE CREW OF THE LEAK AND INSTRUCTED THEM TO COME AROUND AN - [SDR CED2004F00002](https://openairdocs.org/sdr/CED2004F00002), May 19, 2004: FIRE DETECTOR. MALFUNCTIONED. AFTER TAKEOFF AT FLIGHT LEVEL 220 THE CREW OBSERVED A FIRE INDICATION LIGHT ON THE NR 1 ENGINE. THE FLIGHT CREW FOLLOWED STARNDARD EMERGENCY PROCEDURES AND RETU - [SDR CED2004F00001](https://openairdocs.org/sdr/CED2004F00001), May 17, 2004: CASE. CRACKED. WHILE ENROUTE, AT FLIGHT LEVEL 390 FLIGHT CREW OBSERVED A FIRE INDICATION ON THE NR 2 ENGINE. THE FLIGHT CREW WAS ABLE TO EXTINGUISH THE FIRE INDICATION LIGHT U - [SDR 00140](https://openairdocs.org/sdr/00140), May 14, 2004: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMED OUT AT FL430 IN SEVERE TURBULANCE ON TRIP FROM HKS TO LRD. ENGINE RELET NORMALLY AT FL 250. CONTINUED TRIP TO LRD. MAINTENANCE P - [SDR 2004F00424](https://openairdocs.org/sdr/2004F00424), May 6, 2004: ENGINE. STALLED. ON DESCENT INTO MEMPHIS, TN, THE NR 1 ENGINE STALLED. THE FLIGHT CREW LEFT THE ENGINE RUNNING AT IDLE AND LANDED WITHOUT INCIDENT. (M) - [SDR 00133](https://openairdocs.org/sdr/00133), Mar 20, 2004: ENGINE. FLAMED OUT. PILOT REPORTED, LT ENGINE FLAMED OUT CLIMBING THRU FL38.5, ENGINE RELET AT FL25. CONTINUED FLIGHT WITH NO FURTHER PROBLEM, PILOT INSPECTED ENGINE AT DESTINATION - [SDR 00132](https://openairdocs.org/sdr/00132), Mar 19, 2004: ENGINE. FLAMED OUT. PILOT REPORTED RT ENGINE FLAMMED OUT CLIMBING THROUGH FL 39.5 AIRCRAFT DIVERTED TO GRI. MAINTENANCE DISPATCHED FROM ADS, FOUND NO FOD DAMAGE OR LEAKS, RESTRICTE - [SDR 00131](https://openairdocs.org/sdr/00131), Feb 10, 2004: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL 370. WILL UPDATE THIS SDR AFTER MAINTENANCE. LT ENGINE REMOVED FOR HSI INSPECTION NO ABNORMAL WEAR REPORTED - [SDR CED2004F00000](https://openairdocs.org/sdr/CED2004F00000), Jan 8, 2004: TIRE. SEPARATED. ON CLIMB OUT, THE NOSE GEAR UNSAFE LIGHT ILLUMINATED. THE CREW CYCLED THE GEAR NUMEROUS TIMES WITH NO CHANGE IN THE UNSAFE INDICATION, THEY THEN RETURNED WITHOU - [SDR 2004F00223](https://openairdocs.org/sdr/2004F00223), Jan 8, 2004: NOZZLE. DAMAGED. BRO - ON CLIMB-OUT, THE NR 1 ENGINE FLAMED OUT AT 39,600 FEET. THE AIRCRAFT DESCENDED TO FLIGHT LEVEL 25,000 FEET AND RESTARTED THE ENGINE. THE AIRCRAFT THEN DI - [SDR 2004FA0000020](https://openairdocs.org/sdr/2004FA0000020), Jan 6, 2004: PUMP. LEAKING. INSTALLED OVERHAULED FUEL PUMP FROM MFG ON 4NOV03. DURING AIRCRAFT INSPECTION 22DEC04 HAD FUEL SEEP FROM WIRES ON PUMP. - [SDR CED2003F00000](https://openairdocs.org/sdr/CED2003F00000), Nov 15, 2003: FILTER. INOPERATIVE. ON NOV 20, 2003, THE AIRCRAFT EXPERIENCED LOW FUEL PRESSURE WARNING LIGHTS. UPON INVESTIGATION OF THE DISCREPANCY WE CHANGED THE FUEL FILTERS BECAUSE THE FELT S - [SDR 00117](https://openairdocs.org/sdr/00117), Oct 8, 2003: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMED OUT WHILE CLIMBING TO FL410 IN CONTINOUS LIGHT TO MODERATE TURBULANCE, NO EMERGENCY WAS DECLARED, RELIGHT NORMAL AT FL250, CLIMB - [SDR 00107](https://openairdocs.org/sdr/00107), Aug 27, 2003: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMED OUT CLIMBING FROM FL400 TO FL410 NORMAL RESTART PERFORMED AND RETURN TO FL410 FOR REMAINDER OF FLIGHT WITH NO FURTHER PROBLEM, E - [SDR 2003FA0001156](https://openairdocs.org/sdr/2003FA0001156), Jul 11, 2003: STARTER. VIBRATION. WHILE IN CRUISE FLIGHT AT 370, THE FLIGHT CREW HEARD TWO FLUTTERING VIBRATION SOUNDS. THE VIBRATION NOISES BECAME LOUDER AND LOUDER. ADJUSTING THE THROTTLE ISOL - [SDR 00100](https://openairdocs.org/sdr/00100), Jun 25, 2003: UPLOCK SWITCH. INOPERATIVE. PILOT REPORTED GEAR WOULD NOT RETRACT AFTER DEPARTING YIP, CREW RETURNED TO YIP WITH GEAR DOWN AND LOCKED INDICATION. MAINTENANCE CLEANED LUBED AND ADJUSTED ALL - [SDR 00098](https://openairdocs.org/sdr/00098), Jun 11, 2003: ENGINE. FLAMED OUT. PILOT REPORTED RT ENGINE FLAMED-OUT CLIMBING THRU FL410 FOR FL430. DESCENDED AND RELIGHT NORMAL, CLIMB BACK TO FL410 FOR REMAINDER OF LEG. UPDATE AFTER MAINTENA - [SDR 00096](https://openairdocs.org/sdr/00096), Jun 2, 2003: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAMED-OUT WHILE CLIMBING FROM FL42.5 FOR FL430, DESCEND AND RELIGHT. WILL UPDATE AFTER MAINTENANCE. MAINTENANCE PERFORMED ENGINE INSPE - [SDR 00095](https://openairdocs.org/sdr/00095), Jun 1, 2003: ENGINE. FLAMED OUT. PILOT REPORTED WHILE CLIMBING FROM 410 TO 430 THE LT ENGINE FLAMED-OUT. DESCEND TO RELIGHT ALTITUDE, RELIGHT AND CLIMB BACK TO 410 FOR THE REST OF FLIGHT. WILL - [SDR 00094](https://openairdocs.org/sdr/00094), May 30, 2003: ENGINE. FLAMED OUT. PILOT REPORTED LT ENGINE FLAME-OUT WHILE CLIMBING THRU 41,300 FT. DESCEND AND RELIGHT PERFORMED. UPDATE AFTER MAINTENANCE. All 131: https://openairdocs.org/engine/ge-cj610-6/reports.md ## STCs that may be installed (OpenAirDocs) (5) 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 SE976SO](https://openairdocs.org/stc/SE976SO): Installation of an oil tank sight gauge on a G.E. oil tank, P/N6003T09P04. JSF Aviation Services Inc. Lists CJ610 Series - [STC SE8674SW](https://openairdocs.org/stc/SE8674SW): Modification of the following engine oil tanks by adding a sight glass: 6002T03P01, 6002T03P03, 6003T09P01, 6003T09P02, 6003T09P03, 6003T09P04, 6003T89P01, 6003T89P02, 6003T03P02, 6002T03P04. Bizjet International Sales & Support Inc - [STC SE1057SO](https://openairdocs.org/stc/SE1057SO): Installation of capacitance type probe with oil quantity indicating system in oil tank. Aircraft Equipment Certification Corporation. Lists CJ610 Series - [STC SE949SO](https://openairdocs.org/stc/SE949SO): Installation of an oil level sight gauge. Aircraft Equipment Certification Corporation - [STC SE6CE](https://openairdocs.org/stc/SE6CE): Installation of slotted disc magnetic pickup on overspeed fuel control. Woodward Governor Co --- 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.