# Service difficulty reports: GE CF6-80C2B2

A list on [GE CF6-80C2B2](https://openairdocs.org/engine/ge-cf6-80c2b2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 4 · 156 reports

- [SDR UIEA2025022500162](https://openairdocs.org/sdr/UIEA2025022500162.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WITH CORROSION.(<P>ENG 2, FAN CASE AREA AT 6 O´CLOCK POSITION, AROUND THE ANCHORED NUT WAS REMOVED, CORROSION LEVEL 1 WAS REWORKED, INSPECTED, EVALUATED AND ALLOWABLE LIMITS FOUND IAW AMM 72
- [SDR UIEA2025030194202](https://openairdocs.org/sdr/UIEA2025030194202.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE WITH SEVERAL POINTS OF CORROSION (2EA).(<P>ENG 1, FWD FAN CASE, AT 6 O'CLOCK APPROX, FWD MATING FLANGE CORROSION LEVEL 1 WERE REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW
- [SDR UIEA2025030600215](https://openairdocs.org/sdr/UIEA2025030600215.md): Bolt · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11 WITH CORROSION.(<P>ENG 2, FAN CASE, OGVS BOLTS AREA, 113 BOLTS, BETWEEN 7 - 11, CORROSION WAS EVALUATED, REMOVED, AND PERFORMED DVI, FOUND TO BE WITHIN ALLOWABLE DAMAGE LIMITS IAW. AMM 72-33-00-206-00
- [SDR UIEA2025031200278](https://openairdocs.org/sdr/UIEA2025031200278.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, WITH SEVERAL POINTS OF CORROSION (3EA).(<P>ENG 1, AFT FAN CASE, AT 5 TO 6 O'CLOCK APROX, CORROSIONS LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS. NO FURTHER DEFECTS NOTED.</P>)
- [SDR UIEA2025031200279](https://openairdocs.org/sdr/UIEA2025031200279.md): Case · corroded · Mar 15, 2025 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE WITH CORROSION L=2.100" W=1"(<P>ENG 2, FAN CASE, AT 6' O CLOCK, UNDER STRUT AREA, BASE, CORROSION LEVEL 1 WAS REWORKED, EVALUATED, INSPECTED AND FOUND TO BE WITHIN ALLOWABLE LIMITS IAW AMM 72-33-00-206-001
- [SDR 21GA202412223021](https://openairdocs.org/sdr/21GA202412223021.md): Engine · surges · Dec 22, 2024 · N881YV · Boeing 767241 · Engine (Turbine/Turboprop)
  > RIGHT ENGINE SURGING. IT STOPPED WHEN THROTTLES REDUCED. THERE WERE NO EXCEEDENCES. ENGINE OPERATON BECAME NORMAL AGAIN. PERFORMED BORESCOPE INSPECTION. NO DEFECTS NOTED.
- [SDR UIEA2024092000910](https://openairdocs.org/sdr/UIEA2024092000910.md): Engine · no discrepancy · Sep 20, 2024 · N1373A · Boeing 76731K · Engine (Turbine/Turboprop)
  > BIRD STRIKE ON #1 ENG(<P>PERFORMED CONDITIONAL INSPECTION IAW AMM 05-51-18 & PERFORMED BIRD STRIKE CLEANING IAW AMM 12-25-04. NO DEFECTS AT THIS TIME.</P>)
- [SDR 21GA20211119001](https://openairdocs.org/sdr/21GA20211119001.md): Cooling Duct · ruptured · Nov 19, 2021 · N881YV · Boeing 767241 · Pneumatic Distribution System
  > 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 DUCT RUPTURED. REPLACED DUCT.
- [SDR UIEA2021102702292](https://openairdocs.org/sdr/UIEA2021102702292.md): Pressure Switch · none · Oct 26, 2021 · N1373A · Boeing 76731K · Engine Oil Temperature
  > 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 WITHOUT SB767-78-8 INSTALLED)(<P>TRANSFERRED TO MDDR 155755 IAW MEL 79-33-01-01, CAT C, DUE DME 05NOV21. P
- [SDR UIEA2021052301165](https://openairdocs.org/sdr/UIEA2021052301165.md): Blades · dented · May 23, 2021 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > FOUND LEADING EDGE FAN BLADES ON #1 ENGINE BLADES 4, 6, 7, 13, 15, 16, 29, 34, & 36 TO HAVE MINOR DENTS.(<P>INSPECTED FAN BLADES IAW B767 AMM 72-31-02. ALL BLADES FOUND TO BE WITHIN AMM LIMITS FOR SERVICE. NO OTHER ACTION NECESSARY. TRANSFERRED TO NON-MEL # 14
- [SDR UIEA2021040600842](https://openairdocs.org/sdr/UIEA2021040600842.md): Switch · faulted · Apr 6, 2021 · N1373A · Boeing 76731K · Engine Oil Pressure
  > R ENGINE OIL PRESS LIGHT INOP(<P>TRANSFERRED TO MDDR # 144739 PER MEL 79-33-01-01 CAT C DUE 12 APR 21.</P><P>LOG PAGE 1145808: R&R KORREY SWITCH ASSEMBLY IAW SWPM 20-83-11, OPS CHECK GOOD. THIS CLOSES MDDR 144739.</P><P><BR /></P>)
- [SDR UIEA2021040900867](https://openairdocs.org/sdr/UIEA2021040900867.md): Duct · damaged · Apr 6, 2021 · N1373A · Boeing 76731K · Turbine Engine Compressor Section
  > UPON INSPECTION OF #1 ENGINE FOUND A HOLE IN THE L/H SIDE LOW TURBINE COOLING DUCT.(<P>REMOVED AND REPLACED THE DUCT IAW GE CF6-80C2 ESM 72-00-04. PERFORMED IDLE LEAK CHECK IAW AMM 71-00-00-795-034-H03, TEST #3. LEAK AND OPS CHECK GOOD. ALL PARAMETERS NORMAL.
- [SDR UIEA2021040700843](https://openairdocs.org/sdr/UIEA2021040700843.md): Duct · damaged · Apr 4, 2021 · N1373A · Boeing 76731K · Turbine Section
  > ON DESCENT L N2 VIB FLUCTUATED BETWEEN 2.7-5.0 FL 180-N1 APPROX 45%-IDLE 270KTS. NORMAL ENGINE INDICATIONS OTHERWISE(<P>T/S IAW 767 FIM TASK 71-05 FAULT TREE 858. FOUND LPT DUCT DAMAGE. </P><P>REF LP 1145806. REMOVED AND REPLACED THE DUCT IAW CF6-80C2 ESM 72-0
- [SDR UIEA2021032200683](https://openairdocs.org/sdr/UIEA2021032200683.md): Ecu · faulted · Mar 21, 2021 · N1373A · Boeing 76731K · Fuel Controlling System
  > L ENG CONTROL EICAS CAUTION & STATUS MSG AFTER ENGINE START(<P>PERFORMED PIMU BITE PER FIM 71-01-00/101, TEST OK. CLEARED EICAS MESSAGE. PERFORMED TWO ENG (L) RUNS PER AMM 71-00-00, CHECK OK. </P><P>LOG PAGE 1457801: REMOVED AND REPLACED LEFT ENG ELECTRONIC CO
- [SDR UIEA2021031000516](https://openairdocs.org/sdr/UIEA2021031000516.md): Anti-Ice Valve · malfunctioned · Mar 10, 2021 · N1373A · Boeing 76731K · Engine Anti-Icing System
  > RIGHT ENGINE ANTI ICE VALVE LIGHT ILLUMINATED.(<P>TRANSFERRED TO MEL 30-21-01-04-02 CAT C MDDR 143629. DUE 20MAR21 MT PROCEDURES COMPLIED.</P><P>TPA MX, 13MAR, LP 1457787 ITEM M3: REMOVED AND REPLACED R/H ENG #2 THERMAL COWL ENG INLET ANTI-ICE VALVE AS PER AMM
- [SDR UIEA2021011400052](https://openairdocs.org/sdr/UIEA2021011400052.md): Bulb · inoperative · Jan 14, 2021 · N1373A · Boeing 76731K · Central Warning
  > 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 INSTALLED, AND CF6-80A/A2 WITHOUT SB767-78-8 INSTALLED. TRANSFERRED TO MDDR 140889, IAW DDG 79-33-01-01 C
- [SDR UIEA2020120402530](https://openairdocs.org/sdr/UIEA2020120402530.md): Guide Vane · damaged · Dec 3, 2020 · N1373A · Boeing 76731K · Turbine Engine Compressor Section
  > 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 72-33-00. OPERATIONS CHECK GOOD.
- [SDR UIEA2020102002278](https://openairdocs.org/sdr/UIEA2020102002278.md): Bolt · broken · Oct 19, 2020 · N1373A · Boeing 76731K · Turbine Engine Compressor Section
  > 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 BRACKET P/N 1470M39G08. ITEM 9: LT ENGINE COOLING AIR SUPPLY TUBE RUPTURED P/N 1678M86G07. ITEM 11:
- [SDR UIEA2020081101738](https://openairdocs.org/sdr/UIEA2020081101738.md): Warning Message · illuminated · Aug 9, 2020 · N1373A · Boeing 76731K · Engine Vibration Analyzer
  > 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. ENGINE NORMAL CONDITION AND ENGINE METAL DETECTORS OK.
- [SDR UIEA2020080501711](https://openairdocs.org/sdr/UIEA2020080501711.md): Switch · malfunctioned · Aug 5, 2020 · N1373A · Boeing 76731K · Fuel Controlling System
  > 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 SATISFACTORY PER 71-00-862-053-H03 AND 71-00-00-862-020-H03 AND GROUND/APPROACH IDLE VERIFIED PER TRIM TABLE 71-01
- [SDR UIEA2020042900918](https://openairdocs.org/sdr/UIEA2020042900918.md): Accelerometer · faulty · Apr 29, 2020 · N1373A · Boeing 76731K · Engine Vibration Analyzer
  > HIGH N2 VIBRATION READINGS NOTED ON ENG 1.(<P>RAN ENG AND FOUND INDICATION INTERMITTENT. PLACED INDICATION ON MEL 77-31-01-01, MDDR 127716, CAT 'C'. </P><P>LP <SPAN>1131038: </SPAN><SPAN>REMOVED AND REPLACED #1 ENGINE COMPRESSOR REAR FRAME ACCELEROMETER ASSY I
- [SDR UIEA2020042700844](https://openairdocs.org/sdr/UIEA2020042700844.md): Fuel Filter · faulted · Apr 26, 2020 · N1373A · Boeing 76731K · Engine Fuel Distribution
  > LEFT ENGINE FUEL FILTER STATUS MESSAGE. EICAS MESSAGE CAME ON DURING CLIMB OUT FROM PDX.(<P>REMOVED LEFT ENGINE FUEL FILTER AND INSTALLED NEW FUEL FILTER IAW B767 73-11-02. LEAK CHECK GOOD, CLEARED EICAS MESSAGE.</P>)
- [SDR UIEA2020040700705](https://openairdocs.org/sdr/UIEA2020040700705.md): Manifold · cracked · Apr 5, 2020 · N1373A · Boeing 76731K · Engine Cooling System
  > #1 ENGINE AFT LPT COOLING AIR MANIFOLD CRACKED AT 5 O'CLOCK POSITION, REFERENCE DMI 126347 #1 ENG TCC INOP PER COMPANY REQUEST.(<P>REMOVED AND REPLACED #5 POSITION LPT COOLING AIR MANIFOLD IAW AMM 75-24-03. OPS CHK GOOD.</P>)
- [SDR UIEA2020030200355](https://openairdocs.org/sdr/UIEA2020030200355.md): Igniter · out of adjust · Feb 28, 2020 · N1373A · Boeing 76731K · Spark Plug/Igniter
  > #2 ENGINE #1 IGNITER INOP(<P><SPAN>TRANSFERRED TO DMI 125163 IAW MEL 74-00-01B, CAT 'C'.</SPAN></P><P><SPAN>LP </SPAN><SPAN>1166888: </SPAN><SPAN>PERFORMED IMMERSION DEPTH CHECK OF THE #2 ENGINE #1 IGNITER IAW B767 AMM 74-21-02. ADDED 3 SPACER GASKETS TO THE 2
- [SDR UIEA2019111545909](https://openairdocs.org/sdr/UIEA2019111545909.md): Warning Message · false activation · Nov 14, 2019 · N1373A · Boeing 76731K · Engine Anti-Icing System
  > R ENGINE ANTI ICE EICAS MESSAGE MOMENTARILY DISPLAYED AFTER R ENGINE START - R ENG VALVE LIGHT AS WELL.(<P>RAN ENGINES IAW AMM 71-00-00 AND OPS CHECK R ENGINE ANTI ICE VALVE IAW AMM 30-21-00. VALVE OPERATED NORMAL AT THIS TIME.</P>)
- [SDR 21GA20191107003](https://openairdocs.org/sdr/21GA20191107003.md): Skin · cracked · Nov 5, 2019 · N999YV · Boeing 767241 · Fuselage Main, Plate/Skin
  > 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.md): Structure · corroded · Nov 5, 2019 · N999YV · Boeing 767241 · Fuel Storage
  > RH UPPER CENTER TANK SKIN HAS CORROSION AT RBL 71 OF REAR SPAR.
- [SDR UIEA2019101305708](https://openairdocs.org/sdr/UIEA2019101305708.md): Relay · failed · Oct 13, 2019 · N1373A · Boeing 76731K · Fuel Control/Turbine Engines
  > 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 K433 RT IDLE SOLENOID RELAY IAW AMM 20-11-00 AND WDM 73-21-19. PERFORMED ENGINE IDLE RUN IAW B767 AM
- [SDR UIEA2019100325625](https://openairdocs.org/sdr/UIEA2019100325625.md): Unknown · vibration · Oct 1, 2019 · N1373A · Boeing 76731K · Engine (Turbine/Turboprop)
  > 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. PERFORMED FIM 71-03 FT 852, STEP 4, NOTE 1, SURVEY L ENG IAW AMM 72-31-02. NO DAMAGE OR SHINGLING
- [SDR UIEA2019093005606](https://openairdocs.org/sdr/UIEA2019093005606.md): Sensor · malfunctioned · Sep 28, 2019 · N1373A · Boeing 76731K · Fuel Control/Turbine Engines
  > IN FLIGHT AND ON THE GROUND, "IDLE DISAGREE" INTERMITTENTLY SHOWED ON EICAS. RT ENGINE CYCLES BETWEEN LOW AND HI IDLE SPEED, EVERY 15 SEC.(<P>TRANSFERRED TO MDDR #118414 AS PER MEL 73-21-01-03, CAT 'C', DUE: 09OCT19. T/S TO EEC USING FIM 71-05, SHEET 11. </P>
- [SDR UIEA2019082215251](https://openairdocs.org/sdr/UIEA2019082215251.md): Unknown · vibration · Aug 21, 2019 · N1373A · Boeing 76731K · Engine (Turbine/Turboprop)
  > 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 SERVICE AT THIS TIME. </P>)
- [SDR UIEA2019051304188](https://openairdocs.org/sdr/UIEA2019051304188.md): Igniter · worn · May 11, 2019 · N1373A · Boeing 76731K · Spark Plug/Igniter
  > NR 1 ENGINE (2 EA) IGNITER PLUGS ARE WORN(<P>REMOVED AND REPLACED (2 EA) NR 1 ENGINE IGNITER PLUGS IAW AMM 74-21-02</P>)
- [SDR UIEA2019051304187](https://openairdocs.org/sdr/UIEA2019051304187.md): Igniter · worn · May 11, 2019 · N1373A · Boeing 76731K · Spark Plug/Igniter
  > NR 2 ENGINE (2 EA) IGNITOR PLUGS ARE WORN(<P>REPLACED NR 2 ENGINE IGNITOR PLUGS (2 EA) IAW 74-21-02</P>)
- [SDR UIEA2019040413756](https://openairdocs.org/sdr/UIEA2019040413756.md): Switch · malfunctioned · Apr 2, 2019 · N1373A · Boeing 76731K · Engine Fuel and Control
  > RT AUX PITOT KORRY SWITCH WILL NOT STAY IN PLACE.(<P>TRANSFERRED TO MDDR 109578, VERIFIED EICAS MESSAGE IAW DDG 30-31-02.</P><P>REMOVED AND REPLACED THE KORRY SWITCH ASSY IAW B767 AMM 33-13-00. OPS CHECK GOOD AT THIS TIME. THIS CLEARS MDDR 109578.<BR DATA-MCE-
- [SDR UIEA2018040400579](https://openairdocs.org/sdr/UIEA2018040400579.md): O-Ring · failed · Apr 4, 2018 · N1373A · Boeing 76731K · Fuel Controlling System
  > 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.md): Module · malfunctioned · Mar 9, 2018 · N1373A · Boeing 76731K · Fuel Control/Turbine Engines
  > 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.md): Barrel Nut · worn · Oct 26, 2017 · N1373A · Boeing 76731K · Engine Mount Section
  > NR 2 PYLON AFT ENGINE MOUNT BARREL NUTS WORN. NEW BARREL NUTS INSTALLED.
- [SDR UIEA2017102502095](https://openairdocs.org/sdr/UIEA2017102502095.md): Circuit Card · failed · Oct 26, 2017 · N1373A · Boeing 76731K · Fuel Controlling System
  > EEC DISCRETE CARD M644 INTERNAL RELAY K13 FAILED TO OPERATE. THE CARD WAS REPLACED.
- [SDR UIEA2017102502094](https://openairdocs.org/sdr/UIEA2017102502094.md): Cowling · delaminated · Oct 26, 2017 · N1373A · Boeing 76731K · Turbine Engine Air Inlet Section
  > 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.md): Engine · fluctuates · Feb 9, 2017 · N999YV · Boeing 767241 · Engine (Turbine/Turboprop)
  > DURING CRUISE AT FLT LEVEL 390 LEFT ENGINE FLUCTUATED ERRATICALLY 400 DEGREES, OTHER PARAMETERS NORMAL
- [SDR 2D7A201612300001](https://openairdocs.org/sdr/2D7A201612300001.md): Battery Pack · discharged · Dec 30, 2016 · N999YV · Boeing 767241 · Emergency Lighting
  > DURING MAINTENANCE CHECK, THE EXIT SIGNS WOULD NOT ILLUMINATE. FOUND THE BATTERY PACK DISCHARGED.
- [SDR 2DYA20150602007](https://openairdocs.org/sdr/2DYA20150602007.md): Turbine Blades · damaged · May 6, 2015 · N881YV · Boeing 767241 · Turbine Section
  > 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 & RETURNED. VISUAL DAMAGE TO TURBINE BLADES. UPON INSPECTION, BORESCOPE, IT WAS DETERMINED THAT
- [SDR USAA2014122400005](https://openairdocs.org/sdr/USAA2014122400005.md): Pump · leaking · Dec 22, 2014 · N256AY · Boeing 7672B7 · Turbine Engine Oil System
  > 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 PUMP DUE TO DAMAGED THREADS ON THE TGB INLET SCREEN. REPLACED THE SCAVENGE OIL FILTER. CHECKED TH
- [SDR USAA2014060900001](https://openairdocs.org/sdr/USAA2014060900001.md): Thrust Reverser · damaged · Jun 8, 2014 · N255AY · Boeing 7672B7 · Engine Thrust Reverser
  > 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 COWL.
- [SDR USAA2014032700002](https://openairdocs.org/sdr/USAA2014032700002.md): Line · chafed · Mar 26, 2014 · N248AY · Boeing 767201 · Engine Oil Distribution (Airframe Furnished)
  > 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 SHUT DOWN. THE DECISION WAS MADE TO DIVERT TO SJU, THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. MX F
- [SDR USAA2013112900012](https://openairdocs.org/sdr/USAA2013112900012.md): Pin · bent · Nov 27, 2013 · N251AY · Boeing 7672B7 · Engine Fuel System Wiring
  > LEFT ENG FUEL FILTER FAULT EICAS MSG DURING CRUISE FLIGHT. THE FLIGHT DIVERTED TO THE NEAREST SUITABLE AIRPORT & THE FLIGHT LANDED WITHOUT FURTHER INCIDENT. FOUND BENT PIN AT CONNECTOR D4202P PIN 1. REPLACED PIN & CONNECTOR D4202P.
- [SDR USAA2013112900011](https://openairdocs.org/sdr/USAA2013112900011.md): Pressure Switch · faulty · Nov 26, 2013 · N251AY · Boeing 7672B7 · Fuel Pressure Sensor
  > 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 QRH. THE FLIGHT DIVERTED TO DUB & LANDED WITHOUT FURTHER INCIDENT. REPLACED THE FUEL FILTER ELE
- [SDR USAA2013102900016](https://openairdocs.org/sdr/USAA2013102900016.md): Pressure Switch · faulty · Oct 25, 2013 · N251AY · Boeing 7672B7ER · Fuel Pressure Sensor
  > ENROUTE, CREW RECEIVED EICAS MESSAGE "LT ENG FUEL FILTER" DURING FLIGHT. THE FLIGHT DIVERTED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE R & R LT ENGINE FUEL FILTER DIFFERENTIAL PRESSURE SWITCH & LT ENGINE MAIN FUEL FILTER ELEMENT.
- [SDR USAA2013031900002](https://openairdocs.org/sdr/USAA2013031900002.md): Check Valve · failed · Mar 16, 2013 · N256AY · Boeing 7672B7ER · Engine (Turbine/Turboprop)
  > 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 ENGINE MEC AND FUEL PUMP, PERFORMED THE NR 2 ENGINE VSV ADJUSTMENT, AND CLEARED THE CDP AND CBP WATER
- [SDR USAA2012111600012](https://openairdocs.org/sdr/USAA2012111600012.md): Pump · failed · Nov 13, 2012 · N256AY · Boeing 7672B7ER · Engine Fuel Pump
  > 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 THE RT ENGINE MAIN ENGINE CONTROL, FUEL PUMP, CIT SENSOR, T2 SENSOR, AND N1 SENSOR. MAIN ENGINE CON

Next page: https://openairdocs.org/engine/ge-cf6-80c2b2/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
WHERE engine_model_key = 'CF680C2B2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-80c2b2/reports

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