# GE CF6-6K

- Type: Engine model (FAA registry)
- Registry code: 30079
- Manufacturer (registry): GE
- Model: CF6-6K
- Engine type: Turbo-fan
- Power: 39,300 lb thrust
- Data sheet: [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Holder: General Electric Company
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf6-6k

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 2003-10-01](https://openairdocs.org/ad/2003-10-01): High pressure turbine rotor (HPTR) rear shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 17, 2003
- [AD 2002-05-03](https://openairdocs.org/ad/2002-05-03): Life-Limited Rotating Parts · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Apr 12, 2002
- [AD 98-22-06](https://openairdocs.org/ad/98-22-06): Fan Disks · General Electric CF6-45A, CF6-45A2, CF6-50A and 41 more. Effective Nov 23, 1998
- [AD 98-18-10](https://openairdocs.org/ad/98-18-10): Low Pressure Turbine Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 30, 1998
- [AD 94-09-18](https://openairdocs.org/ad/94-09-18): High Pressure Turbine Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective Jun 6, 1994
- [AD 93-14-18](https://openairdocs.org/ad/93-14-18): High pressure turbine (HPT) thermal shields · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Oct 4, 1993
- [AD 91-24-01](https://openairdocs.org/ad/91-24-01): Compressor Rear Frame Casing · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective May 26, 1992
- [AD 91-15-03](https://openairdocs.org/ad/91-15-03): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Aug 5, 1991
- [AD 91-12-09](https://openairdocs.org/ad/91-12-09): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 27, 1991
- [AD 91-01-04](https://openairdocs.org/ad/91-01-04): Fan Disk · General Electric CF6-45A, CF6-45A2, CF6-50A and 19 more. Effective Jan 22, 1991
- [AD 90-19-08](https://openairdocs.org/ad/90-19-08): Low Pressure Turbine Rotor Stage One Disk · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Oct 15, 1990
- [AD 89-20-01 R1](https://openairdocs.org/ad/89-20-01-R1): Fan Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Dec 12, 1989
- [AD 88-12-01](https://openairdocs.org/ad/88-12-01): High Pressure Compressor Rear Shafts · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Jun 6, 1988
- [AD 81-19-08](https://openairdocs.org/ad/81-19-08): Low Pressure Turbine Rotor Stage 2 Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1981
- [AD 80-03-06](https://openairdocs.org/ad/80-03-06): Stage 2 HPT Disks · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Feb 8, 1980

Historical (superseded or no longer in force):

- [AD 99-08-18](https://openairdocs.org/ad/99-08-18) (historical): General Electric CF6-45A, CF6-45A2, CF6-50A and 15 more. Effective May 13, 1999
- [AD 95-18-14](https://openairdocs.org/ad/95-18-14) (historical): High Pressure Compressor Rotor · General Electric CF6-6D, CF6-6D1, CF6-6D1A and 2 more. Effective Sep 21, 1995

## Registered aircraft

None registered with this engine 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 SEA07TA181](https://openairdocs.org/ntsb/SEA07TA181), Jun 26, 2007: McDonnell Douglas DC 10-10 (N450AX), Tehachapi, CA, substantial damage. Probable cause: The captain's failure to maintain clearance from trees.

## 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.

- [Accident 20070625015059A](https://openairdocs.org/incident/20070625015059A), Jun 25, 2007: Doug DC1010 (N450AX), Tehachapi, CA, Substantial damage. (-23) While on a fire suppression flight for the California dept of forestry, a DC-10-10 was in a left turn to final for a drop. While in a left turn the left…

## Service difficulty reports (54, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR FDEA202105271414](https://openairdocs.org/sdr/FDEA202105271414), May 27, 2021: ENGINE. MALFUNCTIONED. AT FL380 ALL ENGINES WERE OPERATING NORMALLY. AS WE BEGAN OUR DESCENT AND THROTTLES CAME BACK TOWARDS IDLE ECS SURGED FOLLOWED BY A LEVEL 2 AIRSYS 2 PRES LO AND
- [SDR FDEA2020042730686](https://openairdocs.org/sdr/FDEA2020042730686), Apr 3, 2020: ENGINE. MALFUNCTIONED. CLIMBING THRU FL340 WITH ENGINES ALL AT CLIMB POWER WE FELT A BUMP LIKE MINOR TURBULENCE. THEN ANOTHER AND ANOTHER. WE SAW ENG 2 N1 FLUCTUATING SO WE SUSPECTED 
- [SDR FDEA2019081291831](https://openairdocs.org/sdr/FDEA2019081291831), Aug 9, 2019: ENGINE. FAILED. APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE
- [SDR FDEA2019122089831](https://openairdocs.org/sdr/FDEA2019122089831), Aug 9, 2019: ENGINE. OVERTEMP. PDIS 360 77-20 6391 09AUG19 MEM OPEN U LOGPAGES:2977480 APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010?, THROTTLE
- [SDR FDEA201803200740](https://openairdocs.org/sdr/FDEA201803200740), Mar 20, 2018: ENGINE. FAILED. ENG FAILURE NR 1 ENG CLIMBING THRU 5K. YAW, LOUD BANG RAPIDLY RISING EGT. ENG EXCEEDANCE 942 DEG. THROTTLE TRIMMED POSITIONED TO IDLE. ENG SHUT DOWN. FIRE BOTTL
- [SDR 2013FA0000705](https://openairdocs.org/sdr/2013FA0000705), Aug 15, 2013: ENGINE. SEIZED. NR 2 ENGINE HAD SUDDEN SEIZURE, NO FIRE INDICATION, PRECEDED BY LOAD BANG, PERFORMED EMERGENCY PROCEDURES.
- [SDR 06FDEA03705](https://openairdocs.org/sdr/06FDEA03705), Oct 19, 2006: DOOR FRAME. MISREPAIRED. MAIN CABIN R3 PASSENGER DOOR JAMB AT STA 1305 LONGERON NR 27 EXISTING REPAIR. INSPECTION OF EXISTING REPAIR CARRIED OUT IAW ED 8-5100-7-5001 P2. FOUND 2 FASTENE
- [SDR 06FDEA03707](https://openairdocs.org/sdr/06FDEA03707), Oct 19, 2006: DOOR FRAME. MISREPAIRED. INTERNAL FUSELAGE CAC AREA AT STA 1156 TO 1158 BETWEEN LONGERONS 31 TO 28 LT SIDE EXISTING REPAIR. PERFORMED INSPECTION IAW EO NR 8-5100-7-5001 P2 CRITERIA FOUN
- [SDR 06FDEA0902](https://openairdocs.org/sdr/06FDEA0902), Mar 2, 2006: SKIN. CRACKED. DISCREPANCY EXISTING DOUBLER FUSELAGE SKIN STA 383 AND 410 Z-30 FOUND EXT DOUBLER REPAIR. REMOVED OLD SKIN INSTALLED NEW SKIN P/N ABA7049-3 IAW DWG ABA7049/ABA7
- [SDR 06FDEA0901](https://openairdocs.org/sdr/06FDEA0901), Mar 2, 2006: SKIN. DENTED. DISCREPANCY EXT FUSELAGE LOWER DEEP DENT ON EXT SKIN AT STA 1970 FROM LONG.38 LT TO LONG 39LT. REFORMED DENT AND NDI INSP. NO CRACK FOUND IAW SRM 53-20-00 FIG 1
- [SDR 06FDEA0894](https://openairdocs.org/sdr/06FDEA0894), Mar 2, 2006: SKIN. DENTED. DISCREPANCY LWR FUSELAGE RT SIDE FOUND MANY DENTS ON SKIN STA 979 LONG 39 TO 42. REMOVED DENT IAW SRM 53-20-00 FIG 13 SHT 14 NOTE (C) VOL 1 PERFORMED INSP IAW S
- [SDR 05FDEA04003](https://openairdocs.org/sdr/05FDEA04003), Nov 29, 2005: SKIN. DAMAGED. LT IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED DURING STRIPPING ACTIVITIES. REMOVED FLAP SECTION IAW SRM 51-31-01. REFORMED RIB IAW DPS 3.69. PERFORMED INSPECT
- [SDR 05FDEA04004](https://openairdocs.org/sdr/05FDEA04004), Nov 29, 2005: SKIN. DAMAGED. DURING STRIPPING ACTIVITIES, RR IB FLAP SKIN UPPER SIDE ACCIDENTALLY DAMAGED CAUSING CRACK 3 INCHES LONG. REMOVED FLAP SECTION IAW SRM 51-31-01. PERFORMED INSPE
- [SDR 05FDEA04005](https://openairdocs.org/sdr/05FDEA04005), Nov 29, 2005: DOUBLER. CORRODED. DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF RT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.
- [SDR 05FDEA04006](https://openairdocs.org/sdr/05FDEA04006), Nov 29, 2005: DOUBLER. CORRODED. DURING PRE-PAINT INSPECTION FOUND CORROSION WITH EXFOLIATION ON BEVER/TAIL OF LT WING AT STA XORS 284. REPAIRED IAW EA 8-5710-93818.
- [SDR 05FDEA03465](https://openairdocs.org/sdr/05FDEA03465), Oct 21, 2005: SKIN. DENTED. LWR FUS RT SIDE ON SKIN: BTW LONG 37 AND LONG 38 FOUND AT STA 1009 NR 1EA DENT (LENGTH 1,063 INCH X DEPTH 0,082 INCH) AND AT STA 1006 FOUND 1EA DENT (DEPTH 0,16
- [SDR 05FDEA03475](https://openairdocs.org/sdr/05FDEA03475), Oct 21, 2005: RIB. CORRODED. LT HORIZ STAB LEADING EDGE OB FOUND CORROSION BETWEEN SKIN AND RIB. REMOVED CORROSION AND REPAIRED WITH NR 2EA DOUBLER IAW SRM 55-13-01 FIG 1 VOL3.
- [SDR 05FDEA02603](https://openairdocs.org/sdr/05FDEA02603), Aug 24, 2005: FRAME. WORN. AIR COND COMPT LT SIDE FOUND WORN FRAME AT STA 588 X=64. TRIMMED WORN AREA AND REPAIR IAW SRM.
- [SDR 05FDEA02604](https://openairdocs.org/sdr/05FDEA02604), Aug 24, 2005: SKIN. DENTED. LT WING LOWER SURFACE ON IB AILERON: FOUND NR 1 DENT ( LENGTH 0.87 INCH ; DEPTH 0.094 INCH) AND FOUND NR 1 DENT (LENGTH 0.63 INCH ; DEPTH 0.027 INCH) AT STA XW 
- [SDR 05FDEA02605](https://openairdocs.org/sdr/05FDEA02605), Aug 24, 2005: RIB. CRACKED. RT WING L/E AT XORS 526 FOUND RIB CRACKED. ACCOMPLISHED WING OB EDGE FORMER REPAIR IAW SRM.
- [SDR 05FDEA02606](https://openairdocs.org/sdr/05FDEA02606), Aug 24, 2005: SKIN. CRACKED. RT WING FIXED L/E AT SLAT TRACK NR 7 FOUND NR 1 CRACK 1 INCH LONG ON SKIN AT XORS 372. CUT DAMAGED AREA AND REPAIRED WITH DOUBLER IAW SRM.
- [SDR 05FDEA02607](https://openairdocs.org/sdr/05FDEA02607), Aug 24, 2005: STRUCTURE. DAMAGED. MAIN CABIN INTERNAL FUSELAGE FOUND NR 2 HOLES DIAM. 0.25 INCH TOO CLOSE AT STA 1561, LONGERON 8 LT SIDE. CUT OUT DAMAGED AREA AND REPAIRED IAW SRM.
- [SDR 05FDEA02608](https://openairdocs.org/sdr/05FDEA02608), Aug 24, 2005: FASTENER. WRONG PART. AIR COND COMPT LT SIDE FOUND EXISTING REPAIR WITH WRONG FASTENERS (CHERRY AND BOLT) ON NLG BLKHD. REMOVED EXISTING REPAIR, TRIMMED OUT DAMAGED AREA AND REPAIRED
- [SDR 05FDEA02609](https://openairdocs.org/sdr/05FDEA02609), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT STA XORS 936 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER, FILLER AND DOUBLER REPAIR IAW SRM.
- [SDR 05FDEA02614](https://openairdocs.org/sdr/05FDEA02614), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT STA 750 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02615](https://openairdocs.org/sdr/05FDEA02615), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT STA XORS702 FOUND NR 1 RIB CRACKED. ACCOMPLISH FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02616](https://openairdocs.org/sdr/05FDEA02616), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 696 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND REPAIR ANGLE.
- [SDR 05FDEA02617](https://openairdocs.org/sdr/05FDEA02617), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 733 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02618](https://openairdocs.org/sdr/05FDEA02618), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 742 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02619](https://openairdocs.org/sdr/05FDEA02619), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 831 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02620](https://openairdocs.org/sdr/05FDEA02620), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 598 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02621](https://openairdocs.org/sdr/05FDEA02621), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 615 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02622](https://openairdocs.org/sdr/05FDEA02622), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 490 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02623](https://openairdocs.org/sdr/05FDEA02623), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 485 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02624](https://openairdocs.org/sdr/05FDEA02624), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 454 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM.
- [SDR 05FDEA02625](https://openairdocs.org/sdr/05FDEA02625), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 402 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02626](https://openairdocs.org/sdr/05FDEA02626), Aug 24, 2005: RIB. CRACKED. RT WING FIXED LEADING EDGE AT XORS 352 FOUND NR 1 RIB CRACKED. ACCOMPLISHED FORMER REPAIR IAW SRM AND INSTALLED ANGLE REPAIR.
- [SDR 05FDEA02447](https://openairdocs.org/sdr/05FDEA02447), Aug 12, 2005: SKIN. UNKNOWN. FOUND REPAIR AT STA 1159 - 1139 LONGERON 41-48 RT. REPAIRED IAW FEDEX 8-5330-84091A.
- [SDR 05FDEA02449](https://openairdocs.org/sdr/05FDEA02449), Aug 12, 2005: STRUCTURE. CORRODED. CTR WING LWR BARREL STA 1216 LONGERON 48 REWORK OF CORROSION 40 PERCENT. MATERIAL LOSS TO STANDING LEG. CUT OUT CORRODED SECTION OF LONGERON IAW SRM 53-00-01 FI
- [SDR 05FDEA01680](https://openairdocs.org/sdr/05FDEA01680), Jun 24, 2005: ENGINE. MALFUNCTIONED. NR 1 ENGINE REMAINED AT FLIGHT IDLE DURING DESCENT AND WOULD NOT FOLLOW THROTTLE. N1 AND N2 SLOWLY STARTED DECAYING UNTIL GEN, AIR, HYDRAULIC ALERTS STARTED COM
- [SDR 05FDEA00287](https://openairdocs.org/sdr/05FDEA00287), Feb 14, 2005: ENGINE. VIBRATION. AT FL 340 EXPERIENCED NR 1 ENGINE VIBRATION, N1 ROLLED BACK TO 34%, N2 62% FF 690 LBS. EXECUTED ENG FIRE SEVERE DAMAGE CHECKLIST, FUEL DUMP ABOUT 3000 LBS, DECL
- [SDR HALA0100292](https://openairdocs.org/sdr/HALA0100292), Dec 11, 2001: FCU. MALFUNCTIONED. FLT 481 - PPT - NR 3 ENGINE FLAMED OUT ON APPROACH. ENGINE HAD BEEN AT IDLE POWER 5 MINUTES. REMOVED AND REPLACED FUEL CONTROL. OPS AND LEAK CHECK GOOD. (M)
- [SDR HALA0100204](https://openairdocs.org/sdr/HALA0100204), Aug 8, 2001: MEC. FAILED. FLT 938 - INBOUND TO ANC, HAD NR 2 ENGINE QUIT AT 15,000 FT, ATTEMPTED RESTART, NO SUCCESS. DECLARED EMERGENCY. REMOVED AND REPLACED MEC AND FUEL PUMP. TRIM RUN
- [SDR CNMA200100029](https://openairdocs.org/sdr/CNMA200100029), Aug 6, 2001: BEARING. FAILED. DURING CLIMBOUT #3 ENGINE OIL STRAINER CLOGGED LIGHT CAME ON AND THROTTLE WAS REDUCED AND LIGHT WENT OUT. SHORTLY THERE AFTER OIL QTY DROPPED TO "0" AND ENGINE 
- [SDR CNMA200100025](https://openairdocs.org/sdr/CNMA200100025), Jun 6, 2001: LEVER. STUCK. AT FLIGHT LEVEL 360 NR 2 ENG THROTTLE BECAME JAMMED AT A POWER SETTING OF 94 PERCENT N1. REPEATED ATTEMPTS WERE MADE TO FREE THROTTLE LEVER, NONE SUCCESSFUL. AF
- [SDR CNMA200100012](https://openairdocs.org/sdr/CNMA200100012), Apr 14, 2001: FILTER. CLOGGED. NR 2 ENGINE OIL STRAINER CLOG LIGHT ILLUMINATED IN FLIGHT. PERFORMED OIL STRAINER CLOG LIGHT ABNORMAL CHECKLIST. CLOG LIGHT REMAINED ILLUMINATED. ENGINE WAS SHU
- [SDR AALA20001213](https://openairdocs.org/sdr/AALA20001213), Jul 22, 2000: ENGINE. FAILED. SFO - FLT 39 - DURING TAKEOFF, IN EXCESS OF 100 KNOTS, THE NR 2 ENGINE FAIL LIGHT ILLUMINATED, REJECTED TAKEOFF, ENGINE NR 2 FLAMED OUT AFTER CLEARING THE RUNWA
- [SDR 00FDEA00124](https://openairdocs.org/sdr/00FDEA00124), Mar 1, 2000: ENGINE. MALFUNCTIONED. ON ROTATION AIRCREW HEARD LOUD NOISE, SEEMING TO ORIGINATE FROM LEFT SIDE OF A/C. NR 1 EGT AMBER O/H LIGHT ILLUM ON LANDING (AFT LAND). MEM TOWER SAW 2-3 ORANGE
- [SDR AALA990882](https://openairdocs.org/sdr/AALA990882), Jun 16, 1999: FUEL CONTROL. DEFECTIVE. LAX - FLT 162 - DURING APPROACH LAX AT APPROX 1,006 FEET, THE NR 1 ENGINE FLAMED OUT. FUEL PRESSURE WAS ZERO. FUEL PUMPS WERE ON, HAD 5200 LBS OF FUEL IN NR 1 T
- [SDR HALA9900079](https://openairdocs.org/sdr/HALA9900079), Mar 19, 1999: ENGINE. FAILED. GEN 3 OFF AND GEN FAIL LIGHTS BOTH ILLUMINATED AND NR 3 AC LOAD INDICATED ZERO. NR 3 CSD OIL PRESS LOW LIGHT ILLUMINATED CSD OIL OUTLET TEMP NORMAL AND RISE TEM

All 54: https://openairdocs.org/engine/ge-cf6-6k/reports.md

## STCs that may be installed (OpenAirDocs) (2)

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 SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc
- [STC SE00461LA](https://openairdocs.org/stc/SE00461LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. Hi Temp Insulation Inc

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