# GE CF6-80C2B2 - Type: Engine model (FAA registry) - Registry code: 30102 - Manufacturer (registry): GE - Model: CF6-80C2B2 - Engine type: Turbo-fan - Power: 51,950 lb thrust - Data sheet: [TCDS E13NE](https://openairdocs.org/tcds/E13NE) (OpenAirDocs) - Holder: General Electric Company GE Aerospace - Installed in: 2 registered aircraft - Page: https://openairdocs.org/engine/ge-cf6-80c2b2 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 2021-26-22](https://openairdocs.org/ad/2021-26-22): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 14, 2022 - [AD 2021-14-11](https://openairdocs.org/ad/2021-14-11): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 25 more. Effective Aug 27, 2021 - [AD 2021-03-02](https://openairdocs.org/ad/2021-03-02): Fuel Control/Turbine Engines · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Mar 31, 2021 - [AD 2016-08-10](https://openairdocs.org/ad/2016-08-10): Accessory heat shield · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Jun 1, 2016 - [AD 2014-21-01](https://openairdocs.org/ad/2014-21-01): Fuel manifold · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Nov 28, 2014 - [AD 2013-08-20](https://openairdocs.org/ad/2013-08-20): Fuel tube · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 14 more. Effective May 31, 2013 - [AD 2012-03-12](https://openairdocs.org/ad/2012-03-12): No. 3 bearing packing · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Apr 5, 2012 - [AD 2009-21-07](https://openairdocs.org/ad/2009-21-07): Thrust and thrust control · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 21 more. Effective Dec 1, 2009 - [AD 2009-07-03](https://openairdocs.org/ad/2009-07-03): Eddy current inspection (ECI) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Apr 30, 2009 - [AD 2009-04-10](https://openairdocs.org/ad/2009-04-10): Critical life-limited parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 30 more. Effective Mar 30, 2009 - [AD 2008-21-11](https://openairdocs.org/ad/2008-21-11): Low-pressure turbine (LPT) cases · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Nov 28, 2008 - [AD 2007-11-20](https://openairdocs.org/ad/2007-11-20): Fuel shroud retaining rings · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 22 more. Effective Jul 10, 2007 - [AD 2007-05-14](https://openairdocs.org/ad/2007-05-14): Cast titanium weld- repaired forward engine mount platforms · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 9, 2007 - [AD 2006-16-06](https://openairdocs.org/ad/2006-16-06): Certain stage 1 high- pressure turbine (HPT) rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Sep 5, 2006 - [AD 2005-17-05](https://openairdocs.org/ad/2005-17-05): High pressure compressor rotor (HPCR) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 25 more. Effective Sep 27, 2005 - [AD 2004-22-07](https://openairdocs.org/ad/2004-22-07): Stage 2 nozzle guide vanes (HPT S2 NGVs) · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 1, 2004 - [AD 2003-02-07](https://openairdocs.org/ad/2003-02-07): Low pressure turbine (LPT) shrouds · General Electric CF6-50A, CF6-50C, CF6-50C1 and 30 more. Effective Mar 3, 2003 - [AD 2002-25-08](https://openairdocs.org/ad/2002-25-08): High pressure compressor rotor · General Electric CF6-45A, CF6-45A2, CF6-50A and 40 more. Effective Jan 23, 2003 - [AD 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 2002 - [AD 2000-03-04](https://openairdocs.org/ad/2000-03-04): General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Apr 10, 2000 - [AD 99-01-01](https://openairdocs.org/ad/99-01-01): Accessory Gearbox (AGB) idler adapters · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jan 21, 1999 - [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 97-22-14](https://openairdocs.org/ad/97-22-14): (HPCR) 3-9 Spool · General Electric CF6-50A, CF6-50C, CF6-50C1 and 29 more. Effective Nov 17, 1997 - [AD 96-16-07](https://openairdocs.org/ad/96-16-07): Rear Right Hand Mount Link · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective Aug 28, 1996 - [AD 95-10-11](https://openairdocs.org/ad/95-10-11): Fan Reversers · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 17 more. Effective May 31, 1995 - [AD 94-20-06](https://openairdocs.org/ad/94-20-06): Oil System · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Dec 27, 1994 - [AD 94-06-03](https://openairdocs.org/ad/94-06-03): High Pressure Turbine Disk · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 16 more. Effective Apr 29, 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 91-15-25](https://openairdocs.org/ad/91-15-25): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Sep 6, 1991 - [AD 91-11-05](https://openairdocs.org/ad/91-11-05): High Pressure Compressor Rotor · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 16 more. Effective Jul 5, 1991 Historical (superseded or no longer in force): - [AD 2020-20-13](https://openairdocs.org/ad/2020-20-13) (historical): Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Nov 12, 2020 - [AD 2018-15-04](https://openairdocs.org/ad/2018-15-04) (historical): Turbine/Turboprop Engine--Turbine Section · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Oct 2, 2018 - [AD 2009-05-02](https://openairdocs.org/ad/2009-05-02) (historical): Drainless fuel manifold assemblies · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 26 more. Effective Mar 31, 2009 - [AD 2004-04-07](https://openairdocs.org/ad/2004-04-07) (historical): Stage 1 HPT rotor disks · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 21 more. Effective Mar 12, 2004 - [AD 2002-07-12](https://openairdocs.org/ad/2002-07-12) (historical): Life Limits Section of Continued Airworthiness (ICA) - Selected Critical Life-limited Parts · General Electric CF6-80A, CF6-80A1, CF6-80A2 and 27 more. Effective May 15, 2002 - [AD 2001-10-07](https://openairdocs.org/ad/2001-10-07) (historical): High Pressure Turbine Rotor Disks · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 19 more. Effective Jun 18, 2001 - [AD 2000-16-12](https://openairdocs.org/ad/2000-16-12) (historical): High Pressure Compressor Rotor Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Sep 5, 2000 - [AD 99-24-15](https://openairdocs.org/ad/99-24-15) (historical): High Pressure Compressor Rotor (HPCR) Stage 3-9 Spools · General Electric CF6-45A, CF6-45A2, CF6-50A and 39 more. Effective Jan 28, 2000 - [AD 99-08-13](https://openairdocs.org/ad/99-08-13) (historical): General Electric CF6-80A, CF6-80A1, CF6-80A2 and 26 more. Effective May 13, 1999 - [AD 91-20-02](https://openairdocs.org/ad/91-20-02) (historical): Fuel Manifolds · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 12 more. Effective Nov 25, 1991 - [AD 90-26-01](https://openairdocs.org/ad/90-26-01) (historical): Fuel Manifold Systems · General Electric CF6-80C2A1, CF6-80C2A2, CF6-80C2A3 and 11 more. Effective Dec 20, 1990 ## Information bulletins (advisory) (5) - [SAIB 2023-15](https://openairdocs.org/saib/2023-15): Falsified Forms from AOG Technics. Issued Dec 19, 2023 - [SAIB NE-11-27](https://openairdocs.org/saib/NE-11-27): Fuel Injector Nozzle - CF6-80 Improperly Welded Fuel Nozzles. Issued Apr 5, 2011 - [SAIB NE-10-37](https://openairdocs.org/saib/NE-10-37): Engine Fuel and Control: FADEC Fuel Metering Valve Resolver Feedback Faults. Issued Jul 12, 2010 - [SAIB NE-08-44](https://openairdocs.org/saib/NE-08-44): Engine Thrust Reverser Transcowl Clevis Pin. Issued Sep 3, 2008 - [SAIB NE-07-01](https://openairdocs.org/saib/NE-07-01): Dual engine flameouts on twin engine airplanes. Issued Oct 12, 2006 ## Registered aircraft (2) - [N1373A](https://openairdocs.org/aircraft/N1373A): [Msn 27205 LLC](https://openairdocs.org/faa-owner/MSN%2027205%20LLC), [Purchase, NY](https://openairdocs.org/faa-place/NY/Purchase), built 1994, S/N 27205 - [N999YV](https://openairdocs.org/aircraft/N999YV): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1987, S/N 23801 ## NTSB investigations None matched to aircraft with this engine model. ## 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 20180119006699I](https://openairdocs.org/incident/20180119006699I), Jan 19, 2018: Boeing 767-241 (N881YV), Miami, FL, Minor damage. After landing and during roll out, the crew experienced a vibration. The aircraft entered the taxiway and stopped due to the vibration. The crew was advised by… ## Service difficulty reports (156, newest 50) As reported by operators and repair stations, by the model named in the report. - [SDR UIEA2025022500162](https://openairdocs.org/sdr/UIEA2025022500162), Mar 15, 2025: CASE. CORRODED. ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WITH CORROSION.(

ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WAS - [SDR UIEA2025030194202](https://openairdocs.org/sdr/UIEA2025030194202), Mar 15, 2025: CASE. CORRODED. ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE WITH SEVERAL POINTS OF CORROSION (2EA).(

ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLAN - [SDR UIEA2025030600215](https://openairdocs.org/sdr/UIEA2025030600215), Mar 15, 2025: BOLT. CORRODED. ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11 WITH CORROSION.(

ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11, CORROSION WAS EVALUA - [SDR UIEA2025031200278](https://openairdocs.org/sdr/UIEA2025031200278), Mar 15, 2025: CASE. CORRODED. ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(

ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS RE - [SDR UIEA2025031200279](https://openairdocs.org/sdr/UIEA2025031200279), Mar 15, 2025: CASE. CORRODED. ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(

ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 - [SDR 21GA202412223021](https://openairdocs.org/sdr/21GA202412223021), Dec 22, 2024: ENGINE. SURGES. RIGHT ENGINE SURGING. IT STOPPED WHEN THROTTLES REDUCED. THERE WERE NO EXCEEDENCES. ENGINE OPERATON BECAME NORMAL AGAIN. PERFORMED BORESCOPE INSPECTION. NO DEFE - [SDR UIEA2024092000910](https://openairdocs.org/sdr/UIEA2024092000910), Sep 20, 2024: ENGINE. NO DISCREPANCY. BIRD STRIKE ON #1 ENG(

PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-18 & PERFORMED BIRD STRIKE CLEANING IAW AMM 12-25-04. NO DEFECTS AT THIS TIME.

) - [SDR 21GA20211119001](https://openairdocs.org/sdr/21GA20211119001), Nov 19, 2021: COOLING DUCT. RUPTURED. LEFT ENGINE FIRE MASTER WARNING MESSAGE AT FLIGHT LEVEL 260. SHUTDOWN LEFT ENGINE AND RETURNED TO AIRPORT. FOUND LEFT ENGINE LOW PRESSURE TURBINE CASE COOLING D - [SDR UIEA2021102702292](https://openairdocs.org/sdr/UIEA2021102702292), Oct 26, 2021: PRESSURE SWITCH. NONE. RT ENGINE LOW OIL PRESSURE INDICATION INOP (LOW ENG OIL PRESS INDICATION SYSTEM (-200/-300), ALL EXCEPT JT9D WITHOUT SB767-78-8 INSTALLED, AND CF6-80A/A2 WITHOU - [SDR UIEA2021052301165](https://openairdocs.org/sdr/UIEA2021052301165), May 23, 2021: BLADES. DENTED. FOUND LEADING EDGE FAN BLADES ON #1 ENGINE BLADES 4, 6, 7, 13, 15, 16, 29, 34, & 36 TO HAVE MINOR DENTS.(

INSPECTED FAN BLADES IAW B767 AMM 72-31-02. ALL - [SDR UIEA2021040600842](https://openairdocs.org/sdr/UIEA2021040600842), Apr 6, 2021: SWITCH. FAULTED. R ENGINE OIL PRESS LIGHT INOP(

TRANSFERRED TO MDDR # 144739 PER MEL 79-33-01-01 CAT C DUE 12 APR 21.

LOG PAGE 1145808: R&R KORREY SWITCH ASSEMBLY IA - [SDR UIEA2021040900867](https://openairdocs.org/sdr/UIEA2021040900867), Apr 6, 2021: DUCT. DAMAGED. UPON INSPECTION OF #1 ENGINE FOUND A HOLE IN THE L/H SIDE LOW TURBINE COOLING DUCT.(

REMOVED AND REPLACED THE DUCT IAW GE CF6-80C2 ESM 72-00-04. PERFORMED IDL - [SDR UIEA2021040700843](https://openairdocs.org/sdr/UIEA2021040700843), Apr 4, 2021: DUCT. DAMAGED. ON DESCENT L N2 VIB FLUCTUATED BETWEEN 2.7-5.0 FL 180-N1 APPROX 45%-IDLE 270KTS. NORMAL ENGINE INDICATIONS OTHERWISE(

T/S IAW 767 FIM TASK 71-05 FAULT TREE 85 - [SDR UIEA2021032200683](https://openairdocs.org/sdr/UIEA2021032200683), Mar 21, 2021: ECU. FAULTED. L ENG CONTROL EICAS CAUTION & STATUS MSG AFTER ENGINE START(

PERFORMED PIMU BITE PER FIM 71-01-00/101, TEST OK. CLEARED EICAS MESSAGE. PERFORMED TWO ENG ( - [SDR UIEA2021031000516](https://openairdocs.org/sdr/UIEA2021031000516), Mar 10, 2021: ANTI-ICE VALVE. MALFUNCTIONED. RIGHT ENGINE ANTI ICE VALVE LIGHT ILLUMINATED.(

TRANSFERRED TO MEL 30-21-01-04-02 CAT C MDDR 143629. DUE 20MAR21 MT PROCEDURES COMPLIED.

TPA MX, 13MAR, - [SDR UIEA2021011400052](https://openairdocs.org/sdr/UIEA2021011400052), Jan 14, 2021: BULB. INOPERATIVE. RT ENGINE LOW OIL PRESS LIGHT INOPERABLE EICAS INDICATION NORMAL. LOW ENGINE OIL PRESS INDICATION SYSTEM (-200/-300), ALL EXCEPT JT9D WITHOUT SB767-78-8 INSTALL - [SDR UIEA2020120402530](https://openairdocs.org/sdr/UIEA2020120402530), Dec 3, 2020: GUIDE VANE. DAMAGED. ON WALK AROUND FOUND BACKSIDE OF STARTER VANE 9 O`CLOCK POSITION ON LT ENGINE CRACKING AND COMING OFF. REMOVED EXCESS MATERIAL FROM STARTER GUIDE VANE, IAW AMM - [SDR UIEA2020102002278](https://openairdocs.org/sdr/UIEA2020102002278), Oct 19, 2020: BOLT. BROKEN. ITEM 7: TWO BOLTS BROKEN ON FAN MODULE T/R SUPPORT RING 3 O'CLOCK POSITION NR 1 ENGINE P/N MS9567-10. ITEM 8: LT ENGINE COOLING AIR SUPPLY DUCT HAS A BROKEN BRA - [SDR UIEA2020081101738](https://openairdocs.org/sdr/UIEA2020081101738), Aug 9, 2020: WARNING MESSAGE. ILLUMINATED. BETWEEN 8000 + 10000 MSL LEFT ENGINE FAN VIBE INDICATED 4.2. PERFORMED T/S IAW FIM 71-05 FAULT 852 DETAILED INSPECTION #1 ENG INLET AND EXHAUST, NO DAMAGE NOTED - [SDR UIEA2020080501711](https://openairdocs.org/sdr/UIEA2020080501711), Aug 5, 2020: SWITCH. MALFUNCTIONED. AFTER ENGINE START, IDLE DISAGREE EICAS MESSAGE. REMOVE AND REPLACE #2 ENG LH TR LOGIC SWITCH IAW 78-36-01-004-001; 78-36-01-404-008. OPS CHECK SATISFACTOR - [SDR UIEA2020042900918](https://openairdocs.org/sdr/UIEA2020042900918), Apr 29, 2020: ACCELEROMETER. FAULTY. HIGH N2 VIBRATION READINGS NOTED ON ENG 1.(

RAN ENG AND FOUND INDICATION INTERMITTENT. PLACED INDICATION ON MEL 77-31-01-01, MDDR 127716, CAT 'C'. 

REMOVED LEFT ENGINE FUEL FILTER AND INSTALLED NEW FUEL FILTER IAW B7 - [SDR UIEA2020040700705](https://openairdocs.org/sdr/UIEA2020040700705), Apr 5, 2020: MANIFOLD. CRACKED. #1 ENGINE AFT LPT COOLING AIR MANIFOLD CRACKED AT 5 O'CLOCK POSITION, REFERENCE DMI 126347 #1 ENG TCC INOP PER COMPANY REQUEST.(

REMOVED AND REPLACED #5 POSIT - [SDR UIEA2020030200355](https://openairdocs.org/sdr/UIEA2020030200355), Feb 28, 2020: IGNITER. OUT OF ADJUST. #2 ENGINE #1 IGNITER INOP(

TRANSFERRED TO DMI 125163 IAW MEL 74-00-01B, CAT 'C'.

LP 1166888: PERF - [SDR UIEA2019111545909](https://openairdocs.org/sdr/UIEA2019111545909), Nov 14, 2019: WARNING MESSAGE. FALSE ACTIVATION. R ENGINE ANTI ICE EICAS MESSAGE MOMENTARILY DISPLAYED AFTER R ENGINE START - R ENG VALVE LIGHT AS WELL.(

RAN ENGINES IAW AMM 71-00-00 AND OPS CHECK R ENGINE A - [SDR 21GA20191107003](https://openairdocs.org/sdr/21GA20191107003), Nov 5, 2019: SKIN. CRACKED. RH R1 DOOR CUTOUT AFT LOWER CORNER SKIN CRACKED 4” LONG AT STATION 347 BETWEEN STRINGERS 19 & 20 R. - [SDR 21GA20191107004](https://openairdocs.org/sdr/21GA20191107004), Nov 5, 2019: STRUCTURE. CORRODED. RH UPPER CENTER TANK SKIN HAS CORROSION AT RBL 71 OF REAR SPAR. - [SDR UIEA2019101305708](https://openairdocs.org/sdr/UIEA2019101305708), Oct 13, 2019: RELAY. FAILED. RIGHT ENGINE PARAMETERS DURING IDLE TAXI; N2 64.8%- 73.6%, N1 25.8- 34.5, EGT 310-380 DEG, FF 1.3- 2.0. NO FLUCTUATIONS NOTED DURING CRUISE. REMOVED & REPLACED - [SDR UIEA2019100325625](https://openairdocs.org/sdr/UIEA2019100325625), Oct 1, 2019: UNKNOWN. VIBRATION. DURING CLIMB OUT, LT ENG FAN VIBRATION WAS BETWEEN 4.6 AND 5.0 WITH NO APPRECIABLE VIBRATION FELT IN CONTROLS OR COCKPIT. DURING CRUISE, FAN VIBRATION WAS 1.6. - [SDR UIEA2019093005606](https://openairdocs.org/sdr/UIEA2019093005606), Sep 28, 2019: SENSOR. MALFUNCTIONED. IN FLIGHT AND ON THE GROUND, "IDLE DISAGREE" INTERMITTENTLY SHOWED ON EICAS. RT ENGINE CYCLES BETWEEN LOW AND HI IDLE SPEED, EVERY 15 SEC.(

TRANSFERRED TO MDD - [SDR UIEA2019082215251](https://openairdocs.org/sdr/UIEA2019082215251), Aug 21, 2019: UNKNOWN. VIBRATION. DURING TAKEOFF AND CLIMB, L ENG FAN VIBRATION REACHED 4.4 UNITS. PERFORMED FIM 71-05 FT 856. GVI OF LEFT ENGINE IS GOOD, VIB IS TRANSIENT. AIRCRAFT OK FOR SERVI - [SDR UIEA2019051304188](https://openairdocs.org/sdr/UIEA2019051304188), May 11, 2019: IGNITER. WORN. NR 1 ENGINE (2 EA) IGNITER PLUGS ARE WORN(

REMOVED AND REPLACED (2 EA) NR 1 ENGINE IGNITER PLUGS IAW AMM 74-21-02

) - [SDR UIEA2019051304187](https://openairdocs.org/sdr/UIEA2019051304187), May 11, 2019: IGNITER. WORN. NR 2 ENGINE (2 EA) IGNITOR PLUGS ARE WORN(

REPLACED NR 2 ENGINE IGNITOR PLUGS (2 EA) IAW 74-21-02

) - [SDR UIEA2019040413756](https://openairdocs.org/sdr/UIEA2019040413756), Apr 2, 2019: SWITCH. MALFUNCTIONED. RT AUX PITOT KORRY SWITCH WILL NOT STAY IN PLACE.(

TRANSFERRED TO MDDR 109578, VERIFIED EICAS MESSAGE IAW DDG 30-31-02.

REMOVED AND REPLACED THE KORRY S - [SDR UIEA2018040400579](https://openairdocs.org/sdr/UIEA2018040400579), Apr 4, 2018: O-RING. FAILED. NR 1 ENGINE FUEL PRESSURE SWITCH HAS BLOWN O-RING. REMOVED AND REPLACED THE O-RING IAW AMM 73-34-01. - [SDR UIEA2018031200366](https://openairdocs.org/sdr/UIEA2018031200366), Mar 9, 2018: MODULE. MALFUNCTIONED. RIGHT SPAR VALVE INOPERATIVE. REPLACED THE ENGINE FUEL CONTROL MODULE IAW AMM 76-11-09 AND 28-22-1 .OPS AND ENGINE RUNS OK. - [SDR UIEA2017102502097](https://openairdocs.org/sdr/UIEA2017102502097), Oct 26, 2017: BARREL NUT. WORN. NR 2 PYLON AFT ENGINE MOUNT BARREL NUTS WORN. NEW BARREL NUTS INSTALLED. - [SDR UIEA2017102502095](https://openairdocs.org/sdr/UIEA2017102502095), Oct 26, 2017: CIRCUIT CARD. FAILED. EEC DISCRETE CARD M644 INTERNAL RELAY K13 FAILED TO OPERATE. THE CARD WAS REPLACED. - [SDR UIEA2017102502094](https://openairdocs.org/sdr/UIEA2017102502094), Oct 26, 2017: COWLING. DELAMINATED. NR 2 ENGINE, NR 2 RT FAN COWL FOUND DELAMINATED AT THE 2 O'CLOCK POSITION. THE FAN COWL WAS REPLACED. - [SDR 21GA201702110001](https://openairdocs.org/sdr/21GA201702110001), Feb 9, 2017: ENGINE. FLUCTUATES. DURING CRUISE AT FLT LEVEL 390 LEFT ENGINE FLUCTUATED ERRATICALLY 400 DEGREES, OTHER PARAMETERS NORMAL - [SDR 2D7A201612300001](https://openairdocs.org/sdr/2D7A201612300001), Dec 30, 2016: BATTERY PACK. DISCHARGED. DURING MAINTENANCE CHECK, THE EXIT SIGNS WOULD NOT ILLUMINATE. FOUND THE BATTERY PACK DISCHARGED. - [SDR 2DYA20150602007](https://openairdocs.org/sdr/2DYA20150602007), May 6, 2015: TURBINE BLADES. DAMAGED. CLIMBING THROUGH 4000' CREW HAD HIGH ENG VIBRATION WITH EGT GOING INTO YELLOW ARC ON LT ENG. ENG PULLED BACK TO IDLE THRUST & STILL HAD VIBRATION. ENG SHUTDOWN - [SDR USAA2014122400005](https://openairdocs.org/sdr/USAA2014122400005), Dec 22, 2014: PUMP. LEAKING. ENROUTE, RT ENGINE OIL PRESSURE DROPPED TO 13 PSI, WITH OIL QTY LOSS. SHUTDOWN THE RT ENGINE. LANDED WITHOUT FURTHER INCIDENT. REPLACED THE NR 2 ENGINE LUBE PUM - [SDR USAA2014060900001](https://openairdocs.org/sdr/USAA2014060900001), Jun 8, 2014: THRUST REVERSER. DAMAGED. CLT FLT 749 MAD TO CLT. RT ENG OTBD THRUST REVERSER DAMAGED. R & R NR 2 ENG OTBD THRUST REVERSER. VENDOR SHOP FINDINGS, REPLACED THE DAMAGED SKINS OF THE CORE C - [SDR USAA2014032700002](https://openairdocs.org/sdr/USAA2014032700002), Mar 26, 2014: LINE. CHAFED. SJU FLT 803 EN-ROUTE GRU TO CLT. RT ENG OIL QTY DROPPED TO 0, NO OTHER INDICATIONS, OIL PRESS NORMAL. THE POWER WAS REDUCED IN THE RT ENG, BUT THE ENG WAS NOT S - [SDR USAA2013112900012](https://openairdocs.org/sdr/USAA2013112900012), Nov 27, 2013: PIN. BENT. LEFT ENG FUEL FILTER FAULT EICAS MSG DURING CRUISE FLIGHT. THE FLIGHT DIVERTED TO THE NEAREST SUITABLE AIRPORT & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOU - [SDR USAA2013112900011](https://openairdocs.org/sdr/USAA2013112900011), Nov 26, 2013: PRESSURE SWITCH. FAULTY. DUB FLT 750 EN ROUTE PHL TO BRU. EICAS MESSAGE LT ENG FUEL FILT DISPLAYED DURING CRUISE FLIGHT. A DIVERSION TO THE NEAREST SUITABLE AIRPORT WAS REQUIRED BY THE - [SDR USAA2013102900016](https://openairdocs.org/sdr/USAA2013102900016), Oct 25, 2013: PRESSURE SWITCH. FAULTY. ENROUTE, CREW RECEIVED EICAS MESSAGE "LT ENG FUEL FILTER" DURING FLIGHT. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R LT ENGINE FU - [SDR USAA2013031900002](https://openairdocs.org/sdr/USAA2013031900002), Mar 16, 2013: CHECK VALVE. FAILED. FLT 1628 ENROUTE, NR 2 ENGINE FLAMED OUT DURING REVERSE SELECTION ON LANDING. THE FLIGHT TAXIED TO THE GATE WITHOUT FURTHER INCIDENT. MX REPLACED THE NR 2 ENGIN - [SDR USAA2012111600012](https://openairdocs.org/sdr/USAA2012111600012), Nov 13, 2012: PUMP. FAILED. THE RIGHT ENGINE FLAMED OUT ON DESCENT INTO CLT. R ENG SPEED CARD (EICAS). AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. REPLACED TH All 156: https://openairdocs.org/engine/ge-cf6-80c2b2/reports.md ## STCs that may be installed (OpenAirDocs) (6) 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 SE01543CH](https://openairdocs.org/stc/SE01543CH): Replace Hamilton Sundstrand P/N 778839-13, 778839-14, 778839-19, 778839-20, 778839-37, 778839-38, 816682-1, 840618-2, 880724 carbon bushings with Cook Airtomic P/N AIR22947 Slotted Entry Busing in the High Pressure Shutoff Valve. Cook Airtomic - [STC SE01478CH](https://openairdocs.org/stc/SE01478CH): Installation of Cook Airtomic alignment joint p/n AIR 22912. Cook Airtomic - [STC SE00969CH](https://openairdocs.org/stc/SE00969CH): Install AeroControlex P/N 2605290-001 variable stator feedback control cable. AeroControlex Group TransDigm Inc - [STC SE01471AT](https://openairdocs.org/stc/SE01471AT): Replace right and left side Rohr, Inc. fire detection harness on GE CF6-80C2 engine. Unison Industries. Lists CF6-80C2 Series - [STC SE00463LA](https://openairdocs.org/stc/SE00463LA): Install fireproof blankets on the engine fan reverser intermediate fireseal, in lieu of fireproof intumescent coating. This STC is jointly by owned by Hi Temp Insulation and MRA Systems acting through Middle River Aircraft Systems, 103 Chesapeake Park Plaza, Baltimore, MD 21220. Hi Temp Insulation Inc - [STC SA2227SO](https://openairdocs.org/stc/SA2227SO): Installation of wiring and associated components for utilization of the Rolls Royce, Inc., ARINC, interface/readers UT1317 or UT1317/1, for the purpose of acquisition, recording, and analysis in real time of engine/aircraft/ systems. (767 SERIES POWERED BY RR RB-11-524 SERIES. Rolls Royce, Inc. Lists CF6-80 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.