# Service difficulty reports: GE CF6-50C2

A list on [GE CF6-50C2](https://openairdocs.org/engine/ge-cf6-50c2.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 15 · 719 reports

- [SDR FDEA202211292851](https://openairdocs.org/sdr/FDEA202211292851.md): Engine · fire · Nov 29, 2022 · N306FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > DURING ENGINE 1 START SEQUENCE, ENGINE TOOK LONGER THAN NORMAL TO START. IGNITER USED WAS B, SWITCHED TO A DURING START. ENGINE APPEARED TO START NORMALLY, BUT GROUND CREW ANNOUNCED OVER HEADSET THAT THE AIRPLANE WAS ON FIRE AND TO EVACUATE THE AIRPLANE
- [SDR FDEA202105041096](https://openairdocs.org/sdr/FDEA202105041096.md): O-Ring · failed · May 4, 2021 · N308FE · Doug MD1030F · Engine Oil Pressure
  > ON CLIMB OUT, #2 ENGINE OIL QUANTITY WENT TO 1 QT. SUBSEQUENTLY OIL PRESSURE BEGAN TO DROP BELOW THE GREEN BAND. FOLLOWED QRH TO SHUT DOWN #2 ENGINE AND LAND AT NEAREST SUITABLE FIELD. FOUND MAIN GEAR BOX OIL LINE CHIP DETECTOR O-RING TORN. R&R'D MAIN
- [SDR FDEA202103160657](https://openairdocs.org/sdr/FDEA202103160657.md): Engine · failed · Mar 16, 2021 · N321FE · Doug MD1030F · Turbine Engine Reduction Gear
  > APPROXIMENTELY 30 MINUTES IN TO FLIGHT (FL350) CREW HEARD A VERY LOUD BANG WITH SIGNIFICANT AIRCRAFT YAW. OBSERVED ENGINE NO 1 N1 ROLL BACK WITH CONFIRM ENG OUT ON FMS. DETERMINED N1 ON ENG 1 HAD SEIZED AND EXECUDED PHASE 1. COMPLIED AND COMPLETED ENGING 1
- [SDR FDEA202101210162](https://openairdocs.org/sdr/FDEA202101210162.md): Engine · power loss · Jan 21, 2021 · N313FE · Doug MD1030F · Fuel Controlling System
  > ON TAKE OFF ROLL NR 1 ENGINE WAS SLOW TO COME TO TAKEOFF POWER. DURING FLIGHT WITH THROTTLES ALIGNED, NR 1 ENGINE N1 WAS 10% BEHIND THE OTHER ENGINES. ON GROUND AFTER LANDING ENGINE NR 1 WAS 900 LBS FUEL FLOW WHILE ENGINES NR 2 & NR 3 WERE 1300-1500 FUEL FL
- [SDR FDEA202007302007](https://openairdocs.org/sdr/FDEA202007302007.md): Door Frame · corroded · Jul 30, 2020 · N304FE · Doug MD1030F · Cargo/Baggage Doors
  > FWD CARGO DOOR NR 1 LATCH SPOOL DOOR JAMB HOLES ARE CORROSION REPAIRED PER EA. 8-5350-T0356071.
- [SDR FDEA2020061641236](https://openairdocs.org/sdr/FDEA2020061641236.md): Wire Harness · defective · Jun 14, 2020 · N306FE · Doug MD1030F · Engine Indicating System Wiring
  > ON DESCENT NR 2 ENGINE EGT EXCEEDANCE 1007*C, PRECAUTIONARY SHUT DOWN. NO OTHER EXCEEDANCES, EGT GAUGE "X'D" OUT SEVERAL TIMES. WHEN TROUBLESHOOTING EGT HARNESS PER AMM 77-21-01-2, FOUND UPPER HARNESS LEAD HAD NORMAL, THEN HIGH THEN OPEN RESISTANCE WHEN SHAK
- [SDR FDEA201906111271](https://openairdocs.org/sdr/FDEA201906111271.md): Engine · fluctuates · Jun 11, 2019 · N316FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > CLIMBOUT OUT OFF FL230"ENG 3 EXCEEDANCE"LVL ALERT DISPLAYED.EGT OBSERVERED AT 964 WITH PWR EQUAL OTHER PARAMETERS EQUAL.DURING CRUISE HAD #3 ENG PULLED BACK 10-15% N1 TO KEEP BELOW YELLOW ARC.NOTICED SLOW FLUCTUATIONS FROM 590 EGT TO 800 DURING LVL FLT.
- [SDR 2019F00027](https://openairdocs.org/sdr/2019F00027.md): Slide Raft · defective · May 21, 2018 · Doug DC1030F · Escape Slide
  > AIRCRAFT DECLARED AN IFE FOR SMOKE IN THE COCKPIT. UPON LANDING CREW DEPLOYED THE LEFT FORWARD DOOR (DOOR 1L) SLIDE/RAFT BUT IT FAILED TO FULLY INFLATE. FLIGHT CREW WENT TO DEPLOY THE SLIDE/RAFT LOCATED IN THE NUMBER 1 RIGHT DOOR (DOOR 1R) THE SLIDE/RAFT FEL
- [SDR FDEA201512304103](https://openairdocs.org/sdr/FDEA201512304103.md): Engine · malfunctioned · Dec 30, 2015 · N304FE · Doug MD1030F · Engine Oil Indicating System
  > 1:30 INTO A 3:30 FLIGHT, NR 1 OIL QTY READ 0. IAW QRH MONITORED TEMP & PRESS FOR THE NEXT 15 MINS, TEMP REMAINED NORMAL, BUT PRESS DROPPED TO 21 WITH AMBER BOX. IAW QRH SHUT THE ENG DOWN USING ENG SHUT DOWN INFLIGHT. COORDINATED & DIVERTED UNEVENTFULLY. R &
- [SDR FDEA201511283809](https://openairdocs.org/sdr/FDEA201511283809.md): Sensor · failed · Nov 28, 2015 · N306FE · Doug MD1030F · Power Indicating System
  > REJECTED TAKEOFF FOR ENG FAIL LIGHT AT 90 KTS. FOLLOWING REJECT, ALL ENG INDICATIONS APPEARED NORMAL. NO INDICATION OF WHICH ENG CAUSED THE ENG FAIL LIGHT. R & R NR 2 ENG FAN SENSOR POSITION 2 IAW AMM 71-11-01-2. OPERATIONS CHECKED GOOD. ACFT OK FOR SERVIC
- [SDR CA151123011](https://openairdocs.org/sdr/CA151123011.md): Circuit Breaker · faulty · Nov 22, 2015 · Doug DC1030F · AC Power Distribution System
  > (CAN) IN FLIGHT, THE AIRCRAFT EXPERIENCED A LT EMERGENCY AC BUSS ELECTRICAL FAILURE. THE FLIGHT CREW ACCOMPLISHED THE APPROPRIATE CHECKLIST PROCEDURES AND DECLARED AN EMERGENCY, DIVERTED AND LANDED UNEVENTFULLY. THE MAINTENANCE INSPECTION FOUND A REMOTE CONTRO
- [SDR FDEA201510113165](https://openairdocs.org/sdr/FDEA201510113165.md): Via · malfunctioned · Oct 11, 2015 · N313FE · Doug MD1030F · Engine Indicating System
  > DURING TAKEOFF ROLL, ENGINE FAIL LIGHT AT APPROX 95 KTS. ALL ENGINE PARAMETERS APPEARED NORMAL. SWAPPED THE NR 1 VIA WITH THE NR 3 VIA IAW AMM 31-43-01-4. VIA OP CHECKED NORMAL IAW 31-43-01-5.
- [SDR FDEA201510113166](https://openairdocs.org/sdr/FDEA201510113166.md): Autothrottle Sys · malfunctioned · Oct 11, 2015 · N313FE · Doug MD1030F · Autopilot System
  > REJECTED TAKEOFF AT 80 KTS. ONCE TAKEOFF POWER WAS SET, APPROACHING 80 KTS. THE AUTO THROTTLES PULLED BACK, NR 3 THROTTLE APPROX TWO KNOB WIDTHS. ENG FAIL LIGHT ILLUMINATED. PER CONVERSATION WITH FLIGHT CREW, ALL OTHER ENG INDICATIONS WERE NORMAL, BEFORE &
- [SDR FDEA201509232919](https://openairdocs.org/sdr/FDEA201509232919.md): Oil System · leaking · Sep 23, 2015 · N321FE · Doug MD1030F · Turbine Engine Oil System
  > ON CLIMB OUT, PASSING FL 180, OIL QTY RAPIDLY DECREASED TO 0. OIL PRESSURE DROPPED TO BELOW 12 PSI. OIL TEMP INCREASED TO 147 DEGREES & CLIMBING, IAW QRH ENGINE SHUTDOWN. INSTALLED NR 2 ENGINE IAW WC 71T1710. OPS & LEAK CHECKED NORMAL. OK FOR SERVICE.
- [SDR FDEA201507252391](https://openairdocs.org/sdr/FDEA201507252391.md): Structure · cracked · Jul 25, 2015 · N321FE · Doug MD1030F · Engine Cowling System
  > CRACK FOUND ON CORE COWL NEXT TO PREVIOUS WELD REPAIR. WELD IAW 70-41-00.
- [SDR FDEA201505081434](https://openairdocs.org/sdr/FDEA201505081434.md): Longeron · cracked · May 8, 2015 · N311FE · Doug MD1030F · Engine Cowling System
  > NUMBER 1 ENG CORE COWL LONGERON CRACKED AFT OF CTR HINGE BRACKET. #1 ENGINE CORE COWL REPLACED.
- [SDR FDEA201502210565](https://openairdocs.org/sdr/FDEA201502210565.md): Manifold · ruptured · Feb 21, 2015 · N303FE · Doug MD1030F · Engine Fuel Distribution
  > AT APPROX 1000 FEET ON STABLE FLAPS 35 DEGREES APPROACH, THE NR 3 ENG FLAMED OUT. IAW CREW, N2 INDICATION ROLLED BACK & AFTER TOUCHED DOWN, NR 3 ENGINE WAS SHUTDOWN. LT FUEL MANIFOLD FOUND RUPTURED, R & R.
- [SDR CA150303009](https://openairdocs.org/sdr/CA150303009.md): Thrust Reverser · damaged · Feb 17, 2015 · Doug DC1030F · Engine Thrust Reverser
  > (CAN) AFTER LANDING, THE FLIGHT CREW NOTICED THE NR 2 ENGINE THRUST REVERSER PRESSURE AND UNLOCK LIGHT REMAINED ILLUMINATED AFTER BEING SELECTED TO CLOSE. UPON INSPECTION, MAINTENANCE DETERMINED THE RT THRUST REVERSER ASSY WAS DAMAGED AND STUCK IN THE DEPLOYE
- [SDR CA150212009](https://openairdocs.org/sdr/CA150212009.md): Dimmer · failed · Feb 11, 2015 · Doug DC1030F · Instrument Panel
  > (CAN) IN FLIGHT, THE FLIGHT CREW NOTICED SMOKE EMITTING FROM THE COCKPIT OVERHEAD PANEL. THE ELECTRICAL SMOKE PROCEDURE CHECKLIST WAS CARRIED OUT AND THE SMOKE CEASED. THE CREW COMPLETED A FUEL DUMP BEFORE RETURNING TO BASE FOR AN UNEVENTFUL LANDING. MAINTENAN
- [SDR FDEA201501080096](https://openairdocs.org/sdr/FDEA201501080096.md): Blade · damaged · Jan 8, 2015 · N307FE · Doug MD1030F · Turbine Engine Compressor Section
  > DURING BIRD STRIKE INSPECTION, FOUND FOUR FAN BLADES DAMAGED NR 3 ENG. REFERENCE WRI 05-50/1662 FOR PARTS IAW BIRD STRIKE CHECK IAW AMM 05-62-00-6 & AMM 72-00-00-6-1 K. INSPECTED NR 3 ENG CORE INLET FOR EVIDENCE OF FOD INGESTION. NO DEBRIS OR FOD NOTED AT C
- [SDR CA141208005](https://openairdocs.org/sdr/CA141208005.md): Switch · intermittent · Dec 5, 2014 · Doug DC1030F · Engine Oil Indicating System
  > (CAN) AT TOP OF CLIMB, THE NR 2 ENGINE OIL STRAINER CLOGGED LIGHT ILLUMINATED. CREW COMPLETED THE INFLIGHT SHUT DOWN PROCEDURE. AFTER LANDING SAFELY, THE OIL STRAINER FILTER WAS REMOVED/INSPECTED AND WAS FOUND CLEAN AND WITHOUT ANY CONTAMINATION. OIL STRAINER
- [SDR FDEA201411023449](https://openairdocs.org/sdr/FDEA201411023449.md): Wire Harness · unknown · Nov 2, 2014 · N302FE · Doug MD1030F · Engine Indicating System Wiring
  > DURING DESCENT, RECEIVED NR 3 ENGINE EXCEEDANCE CAUSED EGT HIGH. EGT TEMP FLUCTUATED BETWEEN 1000 & 1087 DEGREES, SHUTDOWN ENGINE. ALL OTHER ENGINE INDICATIONS NORMAL. REMOVED AND REPLACED RT UPPER AND RT LOWER THERMOCOUPLE HARNESSES. REMOVED AND REPLAC
- [SDR FDEA201408292355](https://openairdocs.org/sdr/FDEA201408292355.md): Engine · damaged · Aug 29, 2014 · N312FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > NUMBER 1 ENG OIL QTY LOSS DOWN TO ZERO, PRESS DECREASE FOLLOWED SHORTLY THEREAFTER. SHUTDOWN ENG & DIVERTED. APPROX 35 PSI WHEN ENG SHUTDOWN DECISION WAS MADE. DUE TO DEBRIS FOUND IN THE TGB SCAVENGE SCREEN, REPLACED NR 1 ENGINE ASSY PER WORK CARDS 71T0101
- [SDR FDEA201405311239](https://openairdocs.org/sdr/FDEA201405311239.md): Hose · leaking · May 31, 2014 · N302FE · Doug MD1030F · Engine Thrust Reverser
  > DURING CLIMB OUT, SUFFERED NR 3 THRUST REVERSER PRESSURE FAULT. PERFORMED QRH & RETURNED TO DEPARTURE. REPLACED PNU FLEX LINE. FOUND CONNECTOR TO RT THRUST REVERSER LOCK LOOSE. TIGHTEND CONNECTOR. NO FAULTS IN AIU-1, -2 OR -3. OPS CHECKED NR 3 THRUST REVE
- [SDR FDEA201405070960](https://openairdocs.org/sdr/FDEA201405070960.md): Engine · overtemp · May 7, 2014 · N308FE · Doug MD1030F · Engine (Turbine/Turboprop)
  > PASSING 1200 FT, NR 3 ENGINE EGT WENT TO 969 C, PULLED THROTTLE BACK, TEMP STABILIZED, BUT WITHIN MINUTES STARTED FLUCTUATING INTO THE AMBER TOWARDS RED. PULLED THROTTLE TO IDLE & LT RED WITH THROTTLE AT IDLE. NR 3 ENGINE EGT EXCEEDANCE. ACCOMPLISH A BOROSC
- [SDR CA140321017](https://openairdocs.org/sdr/CA140321017.md): Line · split · Mar 17, 2014 · Doug DC1030F · Turbine Engine Oil System
  > (CAN) THE NR 3 ENGINE WAS SHUTDOWN IN FLIGHT DUE TO LOW OIL PRESSURE CAUSED BY OIL DEPLETION. THE FLIGHT CONTINUED TO THE NEAREST SUITABLE AIRPORT WHERE MAINTENANCE DISCOVERED A RETURN OIL SCAVENGE LINE SPLIT AND LEAKING. FURTHER INVESTIGATION IDENTIFIED VIBR
- [SDR FDEA201403050452](https://openairdocs.org/sdr/FDEA201403050452.md): Switch · failed · Mar 5, 2014 · N455FE · Airbus A310222 · Engine Thrust Reverser
  > ACCELERATING ABOVE 10,000 & 250 KTS, NR 1 ENGINE THRUST REVERSER UNLOCK ILLUMINATED STEADY. ALL OTHER INDICATIONS NORMAL. TROUBLESHOT IAW TSM 78-31-00, FOUND THE RT MASTER ACTUATOR SECONDARY LOCK SWITCH INOPERATIVE. REMOVED AND REPLACED THE NR 1 ENGINE RT
- [SDR CA131218026](https://openairdocs.org/sdr/CA131218026.md): Control Handle · sticking · Dec 13, 2013 · Doug DC1030F · Landing Gear Selector
  > (CAN) ON APPROACH, AFTER EXTENDING THE GEAR THE FLT DECK INDICATION FOR THE GEAR, GREEN, FAILED TO ILLUMINATE ON BOTH THE FRONT AND REAR PANELS, ONLY THE RED UNSAFE LIGHTS ILLUMINATED. THE CREW CYCLED THE GEAR WITH THE SAME RESULT, SO THEY COMPLETED A MISSED
- [SDR CA130704005](https://openairdocs.org/sdr/CA130704005.md): Windshield · cracked · Jul 3, 2013 · Doug DC1030 · Flight Compartment Windows
  > (CAN) IN FLIGHT, THE L1 WINDOW BEGAN ARCING AND THE OUTER PANE, CRAZED, CRACKED INTO MULTIPLE PIECES. THE CREW TURNED OFF THE ANTI-ICE AND THE ACFT CONTINUED TO DESTINATION. THE L1 WINDOW AND ANTI-ICE CONTROLLER WERE REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR FDEA201305100965](https://openairdocs.org/sdr/FDEA201305100965.md): Wire Harness · damaged · May 10, 2013 · N318FE · Doug MD1030F · Turbine Engine System Wiring
  > DURING CLIMBOUT WITH AIRFRAME & ENGINE ANTI ICE ON, RECEIVED LEVEL 3 BLEED AIR 1 TEMP HIGH ALERT. PROCEEDED WITH QRH PROCEDURE. SHUTOFF BLEED AIR 1 AND TEMP DECREASED. ALERT WENT OUT. PEAK TEMP NOTED 295 DEG C. CLAMP ON LOW PRESSURE CHECK VALVE FAILED ALLOW
- [SDR FDEA201305040906](https://openairdocs.org/sdr/FDEA201305040906.md): Bulb · malfunctioned · May 4, 2013 · N312FE · Doug MD1030F · Engine Oil Temperature
  > NR 1 ENGINE OIL TEMP WENT INTO RED ON DEPARTURE THEN YELLOW X. RETURNED TO DEPARTURE. R & R NR 1 ENG OIL TEMP BULB.
- [SDR CA130405007](https://openairdocs.org/sdr/CA130405007.md): Wheel Half · cracked · Apr 3, 2013 · Doug DC1030F · Wheel/Ski/Float
  > (CAN) 0.700" LONG CRACK FOUND ON OTBD WHEEL HALF DURING ROUTINE O/H PROCEDURES. METHOD USED TO DETECT CRACK WAS HFEC. CRACK ORIGINATES ON MATING SURFACE, BETWEEN SPOKE AND BOLT HOLE.
- [SDR FDEA201302110318](https://openairdocs.org/sdr/FDEA201302110318.md): Pressure Switch · failed · Feb 11, 2013 · N313FE · Doug MD1030F · Engine Fuel Distribution
  > NR 1 ENGINE "FUEL FILTER BYPASS" WARNING DURING CRUISE FLT, R & R NR 1 ENGINE DIFFERENTAL PRESSURE SWITCH AND MAIN ENGINE FUEL FILTER IAW 73-34-01-2. LEAK CHECKED GOOD. FILTER LIGHT STILL COMES ON WHEN FUEL LEVER ENGAGED. TROUBLESHOT IAW FIM CODE 73-31
- [SDR FDEA201210253749](https://openairdocs.org/sdr/FDEA201210253749.md): Wire Harness · chafed · Oct 25, 2012 · N312FE · Doug MD1030F · Engine Indicating System Wiring
  > WITH T/O POWER SET, GOT AT APPROX 100 KIAS, A LEVEL 1 ALERT ENG 1 EXCEEDENCE AND NR 1 EGT HIGH (984) REJECTED TAKEOFF AND RAN QRH. DURING TAXI IN AT IDLE (N1 25.1 EGT 567 N2 66.7 1560 FF). R & R ALL 4 EGT HARNESSES AND LEADS, OPS CKD OK AND HAS FLOWN 2 CY
- [SDR FDEA201209263446](https://openairdocs.org/sdr/FDEA201209263446.md): Connector · failed · Sep 26, 2012 · N313FE · Doug MD1030F · Engine Indicating System Wiring
  > ON TAKEOFF ROLL AS POWER SET, NR 2 ENG N1 SURGED, MADE SLIGHT NR 2 THROTTLE REDUCTION AND ADJUSTED, AT THAT TIME ENGINE NR 2 N1 OVERSHOT RED LINE BY A LARGE MARGINE, REJECTED AT 75 KNOTS NO ENGINE POWER SURGED NOTICED. REMOVED & REPLACED CONNECTOR P1-800
- [SDR FDEA201208273182](https://openairdocs.org/sdr/FDEA201208273182.md): Battery · inoperative · Aug 27, 2012 · N307FE · Doug MD1030F · Emergency Lighting
  > DOOR SLIDE PRESSURE LIGHT TEST INOPERATIVE. SECURED BASE OF LIGHT SOCKET AND REPLACED BATTERIES. OPS CHECK NORMAL. MM 25-61-03-5 & SMP. FINAL CLOSED.
- [SDR FDEA201208082936](https://openairdocs.org/sdr/FDEA201208082936.md): Panel · worn · Aug 8, 2012 · N303FE · Doug MD1030F · Nacelle/Pylon, Plate/Skin
  > NR 2 PYLON CUT-OUT FOR PANEL 457CL EDGE IN CONTACT WITH LATCHES ARE WORN OUT. REPAIRED NR 2 PYLON LT ACCESS DOOR LANDING OF 457CL IAW EA 8-5450-162534, REPAIR CLASSIFED AS MAJOR.
- [SDR FDEA201208042839](https://openairdocs.org/sdr/FDEA201208042839.md): Seat Track · worn · Aug 4, 2012 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO SEAT TRACK RBL 28, FS 1471 HAS 2 WORN LOBES. REPAIRED SEAT TRACK AT BS 1411 -1531, RBL 28 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.
- [SDR FDEA201208042840](https://openairdocs.org/sdr/FDEA201208042840.md): Seat Track · worn · Aug 4, 2012 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO SEAT TRACK RBL48, BS 1591 - 1599 HAS 3 WORN LOBES. REPAIRED SEAT TRACK AT BS 1561 -1611, RBL 48 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.
- [SDR FDEA201208022819](https://openairdocs.org/sdr/FDEA201208022819.md): Cargo Track · worn · Aug 2, 2012 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO TRACK 48L, FS 1510 TO 1491 HAS THREE WORN LOBES. REPAIRED IAW SRM 53-70-00 FIG.1. MAJOR REPAIR.
- [SDR FDEA201208022821](https://openairdocs.org/sdr/FDEA201208022821.md): Cargo Track · worn · Aug 2, 2012 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO TRACK 48L, FS 1381 TO 1391 HAS NINE WORN LOBES. BLENDED DAMAGED AREA MAT.=.225, MAT. LOSS=.003" MAT. REMAINING= 0.222 FOUND TO BE IN LIMITS & LOBES WERE OUT OF LIMITS WITH REMAINING OF.240" IAW SRM 53-70-00 FIG 5, SHEET 1. REMOVED SEAT TRACK FR
- [SDR FDEA201208022822](https://openairdocs.org/sdr/FDEA201208022822.md): Cargo Track · worn · Aug 2, 2012 · N303FE · Doug MD1030F · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CARGO TRACK, FS 1381 HAS ONE WORN LOBE. BLENDED LOBE, OUT OF LIMITS IAW SRM 53-70-00 FIG 5, SH 1, FABRICATED SEAT TRACK AND REPAIRED AT STA 1351-1381, RBL 75 IAW SRM 53-70-00, FIG 1. MAJOR REPAIR.
- [SDR FDEA201207272722](https://openairdocs.org/sdr/FDEA201207272722.md): Skin · damaged · Jul 27, 2012 · N303FE · Doug MD1030F · Trailing Edge Flaps
  > RT WING INBD FLAP HAS PUNCTURE ON T/E 3' OTBD OF SPRING CARTRIDGE. REMOVED DAMAGE IAW SRM 57-10-00, FIG 85. FABRICATED DOUBLER LOCATED AND DRILLED FASTENER HOLES IAW SRM 51-31-01. INSTALLED DOUBLER IAW SRM 51-31-01. TREATED AND PRIMED IAW SRM 57-21-01. PA
- [SDR FDEA201207262686](https://openairdocs.org/sdr/FDEA201207262686.md): Bolt · corroded · Jul 26, 2012 · N304FE · Doug MD1030F · Main Landing Gear
  > LT MAIN LANDING GEAR TRUCK BEAM PIVOT BOLT PITTED, AND HAS CHROME PLATING THAT IS FLAKING. R & R PIVOT BOLT REF SEQ 741 MAIN GEAR SHOCK STRUT.
- [SDR FDEA201207262820](https://openairdocs.org/sdr/FDEA201207262820.md): Skin · misrepaired · Jul 26, 2012 · N303FE · Doug MD1030F · Fuselage Main, Plate/Skin
  > SKIN AT BS 1920 L44L MISREPAIRED. REPAIRED IAW CURRENT SRM 53-20-00 FIG. 6 VOL. I. MAJOR REPAIR
- [SDR FDEA201207242664](https://openairdocs.org/sdr/FDEA201207242664.md): Contactor · damaged · Jul 24, 2012 · N302FE · Doug MD1030F · Instrument System Wiring
  > EMERGENCY PWR OFF, LIGHT INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 24-08-03-01 CATEGORY: C EXPIRATION: 01AUG12 "MEL 24-08-03-01: EMER PWR OFF LIGHT - INOP." FOUND THAT THE CENTER CONTACT BEHIND THE EMER PWR OFF LIGHT ASSY HAS NO SPRING PRESSURE. NEED TO
- [SDR FDEA201207082518](https://openairdocs.org/sdr/FDEA201207082518.md): O-Ring · failed · Jul 8, 2012 · N303FE · Doug MD1030F · Hydraulic System, Main
  > HYD 1 FAILED. FOUND O-RING BLOWN ON 3-1 RMP NR 1 SYS S/O VALVE. R & R O-RING REF MM 29-22-02-2. LEAK CHECKED GOOD. SERVICED NR 1 SYSTEM TO 6.5 GAL. CYCLED ALL FLT CONTROLS NUMEROUS TIMES. SYS QTY NEVER BELOW 1.3 GALS. ACFT OK FOR SERVICE.
- [SDR FDEA201206262355](https://openairdocs.org/sdr/FDEA201206262355.md): Lead · malfunctioned · Jun 26, 2012 · N317FE · Doug MD1030F · Engine Indicating System Wiring
  > DURING CLIMBOUT ON A REDUCED POWER TAKEOFF, PASSING ABOUT 1500-2000 FT. RECEIVED A NR 1 ENGINE EXCEEDENCE WITH TEMP REACHING ABOUT 970. A MINUTE OR SO LATER RECEIVED A SIMILAR INDICATION WITH DIAL INDICATING A HIGHER TEMP, EVENTUALLY WITH A PEAK AT 1070C AN
- [SDR CA120523001](https://openairdocs.org/sdr/CA120523001.md): Cable · broken · May 19, 2012 · Doug DC1030 · Stabilizer Control System
  > (CAN) IN CRUISE CREW NOTICED THAT THE LT SIDE OF THE HORIZONTAL STABILIZER MECHANICAL CONTROL LEVERS, LT SIDE OF THE SUITCASE HANDLES. RAPIDLY MOVED TO THE NOSE DOWN POSITION. THE CREW RETURNED TO THE NEAREST SUITABLE AIRPORT. MAINTENANCE FOUND THE LT HORIZ
- [SDR CA120504010](https://openairdocs.org/sdr/CA120504010.md): Valve · malfunctioned · Apr 30, 2012 · Doug DC1030 · Engine Thrust Reverser
  > (CAN) IN CRUISE, ENGINE NR 2 REVERSER PRESSURE LIGHT ILLUMINATED IAW AOM PROCEDURE, CREW PERFORMED A PRECAUTIONARY SHUTDOWN AND RETURNED TO DEPARTING STATION. MAINTENANCE REPLACED THE OVER PRESSURE INLET SHUTOFF VALVE AND THE ACFT WAS RETURNED TO SERVICE.

Next page: https://openairdocs.org/engine/ge-cf6-50c2/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 = 'CF650C2'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-cf6-50c2/reports

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