# Service difficulty reports: GE CT7-2A

A list on [GE CT7-2A](https://openairdocs.org/engine/ge-ct7-2a.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 2 · 83 reports

- [SDR 9EKA20200409001](https://openairdocs.org/sdr/9EKA20200409001.md): Tube · broken · Apr 9, 2020 · N787SR · Bell 214ST · Engine (Turbine/Turboprop)
  > WHILE CONDUCTING AN APPROACH ENGINE NO.1 POWER ROLLED BACK. OBSERVATIONS AND ACTIONS WERE: 1. SOUND OF ENGINE SPOOL DOWN 2. ENG.1 OUT LIGHT, FOLLOWED BY MASTER CAUTION LIGHT. 3. TQ SPLIT SHOWING ENG.1 DECREASING TOWARDS ZERO. 4. CONFIRMED ENG.1 GAUGES
- [SDR 9EKA20160512006](https://openairdocs.org/sdr/9EKA20160512006.md): Ecu · faulty · May 12, 2016 · N390AL · Bell 214ST · Fuel Control/Turbine Engines
  > ENGINE 1 INDICATED EXCESSIVE TORQUE SPLIT WITH YAW MOTION OF THE ACFT. ENG 1 THROTTLE WAS MANUALLY BROUGHT DOWN TO 10% BELOW NR 2 & SAFELY RETURNED TO BASE.
- [SDR 9EKA20160420005](https://openairdocs.org/sdr/9EKA20160420005.md): Beam · cracked · Apr 20, 2016 · N825H · Bell 214* · Fuselage Main, Structure
  > DURING INSPECTION OF AIRFRAME FOR SUSPECTED CAUSE FOR TWO REV VIBRATIONS, FOUND A 4.9 INCH X1.25 INCH CRACK IN THE LT BAGGAGE COMPARTMENT & ENG DECK AT FS STATION 278 - 280. FUSELAGE LT UPPER BEAM CAP IS CRACKED IN LT BAGGAGE COMPARTMENT & UNDER ENG DECK.
- [SDR 9EKA20160224002](https://openairdocs.org/sdr/9EKA20160224002.md): Blade · cracked · Feb 24, 2016 · N511EV · Bell 214ST · Main Rotor Blades
  > MAIN ROTOR BLADE HAS A 2 INCH CRACK IN THE CHORD DIRECTION OF THE TIP SHOE, CAUSED FROM EROSION, AS A RESULT FROM UNIMPROVED LANDING ZONES.
- [SDR 9EKA20160219001](https://openairdocs.org/sdr/9EKA20160219001.md): Stud · sheared · Feb 19, 2016 · N214EB · Bell 214ST · Main Rotor Mast/Swashplate
  > TWO MAIN ROTOR TRANSMISSION MAST STUDS FOUND SHEARED OFF DURING 25 HOUR INSPECTION.
- [SDR 9EKA20151201026](https://openairdocs.org/sdr/9EKA20151201026.md): Chip Detector · activated · Dec 1, 2015 · N214EB · Bell 214ST · Tail Rotor Drive Indicating System
  > PILOT REPORTED MOMENTARY TAIL ROTOR GEAR BOX CHIP LIGHT ON MASTER CAUTION PANEL.
- [SDR 9EKA20150916024](https://openairdocs.org/sdr/9EKA20150916024.md): Engine · failed · Sep 16, 2015 · N214EB · Bell 214ST · Engine (Turbine/Turboprop)
  > DURING CRUISE FLIGHT IN A SHALLOW RIGHT HAND TURN, NR 2 ENG EXPERIENCED HIGH SIDE FAILURE IMMEDIATELY, FOLLOWED BY UNCOMMANDED SHUTDOWN. ACFT RECOVERED 26 MILES BACK TO BASE IN SINGLE ENG CONFIGURATION.
- [SDR 9EKA2015FA0000414](https://openairdocs.org/sdr/9EKA2015FA0000414.md): Chip Detector · damaged · Aug 28, 2015 · N511EV · Bell 214ST · Turbine Engine Oil System
  > ON RETURN TO BASE, NR 2 ENGINE CHIP DETECTOR CAUTION LIGHT ILLUMINATED AND STAYED ON, EMERGENCY PROCEDURES IAW THE RFM WERE C/W BY THE PIC, CONDUCTED TROUBLESHOOTING AND FOUND ELECTRICAL CHIP DETECTOR HOUSING DAMAGED CAUSING FALSE CAUTION LIGHT, REPLACED WITH
- [SDR 9EKA02162015003](https://openairdocs.org/sdr/9EKA02162015003.md): Turbine · cracked · Feb 13, 2015 · N512EV · Bell 214ST · Turbine Engine Compressor Section
  > DURING 25 HR SCHEDULED INSPECTION, CRACK WAS FOUND IN EXHAUST AREA OF NR 1 POWER TURBINE. MM WAS REFERENCED & NO CRACKS ARE ALLOWED, AWAITING PT CHANGE.
- [SDR 9EKA02162015002](https://openairdocs.org/sdr/9EKA02162015002.md): Hose · chafed · Jan 30, 2015 · N511EV · Bell 214ST · Main Rotor Gearbox
  > WHILE IN STEADY STATE CRUISE FLIGHT AT 70% TQ, MAIN TRANSMISSION OIL CAUTION LIGHT ILLUMINATED & THE OIL PRESS GAUGE FOR THE TRANSMISSION WAS OBSERVED DECREASING RAPIDLY. PRECAUTIONARY EMER LANDING WAS MADE IN LESS THAN 1 MIN & THE ACFT SAFELY TOUCHED DOWN.
- [SDR 9EKA02162015001](https://openairdocs.org/sdr/9EKA02162015001.md): Skin · debonded · Dec 25, 2014 · N214EB · Bell 214ST · Rotorcraft Tail Boom
  > TAIL BOOM, EMPENNAGE METALLIC SKIN, HONEYCOMB STRUCTURE ON RT SIDE JUST AFT OF THE FWD VOR ANTENNA MOUNT WL 74, BS 294 HAS DISBONDED. INSPECTION WAS PERFORMED IAW BHT ALL SRM 2-13. TAIL BOOM IS BEING REPLACED WITH REPAIRED SERVICE TAIL BOOM. DAMAGED TAIL BO
- [SDR 2013FA0000625](https://openairdocs.org/sdr/2013FA0000625.md): Case · cracked · Nov 1, 2013 · N825H · Bell 214ST · Main Rotor Gearbox
  > DURING INVESTIGATION OF AN OIL LEAK, A CRACK WAS FOUND IN THE MAIN TRANSMISSION UPPER LEFT HAND RING GEAR CASE.
- [SDR 9EKA2013082300003](https://openairdocs.org/sdr/9EKA2013082300003.md): Tab · missing · Aug 23, 2013 · N214EB · Bell 214ST · Main Rotor Blades
  > WHILE CONDUCTING A "POST FLIGHT" INSPECTION, MECHANICS NOTICED THAT ONE OF THE MAIN ROTOR BLADES WAS MISSING A TRIM TAB.
- [SDR 9EKA2013082200002](https://openairdocs.org/sdr/9EKA2013082200002.md): Fitting · cracked · Aug 21, 2013 · N390AL · Bell 214ST · Rotorcraft Tail Boom
  > CRACK ON THE VERTICAL SPAR OF THE TAIL IT IS LOCATED IN THE COLD WORK AREA JUST ABOVE THE OUTPUT QUILL OF THE 42 DEG GEARBOX. LOCATED ON THE LEFT SIDE AT BS 569.689, WL 95 ON FIN STATION 32. CRACK IS.040 DEEP AND 1.1 INCHES LONG.
- [SDR LCFA20130429001](https://openairdocs.org/sdr/LCFA20130429001.md): Tail Boom · cracked · Apr 29, 2013 · N822H · Bell 214ST · Rotorcraft Tail Boom
  > LEFT SIDE OF THE TAIL BOOM CRACKED IMMEDIATELY FORWARD AND BELOW THE FORWARD MOUNT OF THE LEFT VOR ANTENNA. LENGTH OF CRACK IS APPROXIMATELY 20/64" LONG AND EXTENDS FROM THE ANTENNA BASE TOWARD A RIVET NEAR THE AFT EDGE OF A SPLICE BETWEEN THE MAIN TAIL BOOM
- [SDR LCFA2012F00259](https://openairdocs.org/sdr/LCFA2012F00259.md): Bearing Support · broken · Nov 16, 2012 · N787SR · Bell 214ST · Standard Practices/Structures
  > ROD END BEARING, FOUND BROKEN AFTER COMPLETION OF FLIGHT, ON POST INSPECTION.
- [SDR LCFA2012F00073](https://openairdocs.org/sdr/LCFA2012F00073.md): Attach Fitting · cracked · Apr 11, 2012 · N214EB · Bell 214ST · Rotorcraft Tail Boom
  > WHILE PERFORMING AN URELATED MX WALK-AROUND INSPECTION, NOTED A CRACK ON THE UPPER LT MAIN FUSELAGE TO TAILBOOM ATTACHMENT FITTING. THIS IS A KNOWN ISSUE.
- [SDR 3S8R201108230001](https://openairdocs.org/sdr/3S8R201108230001.md): Frame · cracked · Aug 23, 2011 · N28014 · Bell 214ST · Fuselage Main, Frame
  > MAIN GEAR BOX FRAME HAS A CRACK ON THE LT SIDE RADIUS, STA 227.10, WL 65.00.
- [SDR P4YA2011050900001](https://openairdocs.org/sdr/P4YA2011050900001.md): Drive Shaft · cracked · May 9, 2011 · N5748M · Bell 214ST · Tail Rotor Drive Shaft
  > DURING A 25HR CHECK, THE NR 6 TAIL ROTOR DRIVESHAFT MOUNTING FLANGE WAS DISCOVERED CRACKED ON THE OUTPUT SIDE OF THE IGB COUPLING. THE CRACKS ARE AROUND THE BOLT HOLES. THE TRDS IS ON-CONDITION.
- [SDR P4Y2008F00000](https://openairdocs.org/sdr/P4Y2008F00000.md): Skin · cracked · Jun 7, 2008 · N5748M · Bell 214ST · Fuselage Main, Plate/Skin
  > STRUCTURAL DAMAGE TO AC LT SIDE TRANSMISSION AREA CAUSED BY CONTACT WITH FORKLIFT BASE DURING CARGO LOADING OPERATIONS. (K)
- [SDR HEEA113269](https://openairdocs.org/sdr/HEEA113269.md): Hose · ruptured · Dec 17, 2006 · N8045T · Bell 214ST · Hydraulic System, Main
  > NR 1 HYDRAULIC PUMP CAPTION ILLUMINATED WITH PRESSURE AT ZERO, PRESSURE FLUCTUATED A COUPLE OF TIMES ACCOMPANIED WITH A LOUD NOISE. MAINTENANCE FOUND NR 1 SYSTEM PRESSURE HOSE TO THE CYCLIC SERVO RUPTURED.
- [SDR HEEA111397](https://openairdocs.org/sdr/HEEA111397.md): Oil Cooler · contaminated · Oct 6, 2006 · N5748M · Bell 214ST · Hydraulic System, Main
  > OIL COOLER CAUTION LIGHT ILLUMINATED IN FLIGHT WITH ASSOCIATED UTILITY HYD CAUTION LIGHT FLICKERING. APPROPRIATE EMERGENCY PROCEDURE PERFORMED. MAINTENANCE CLEANED GRASS BUILDUP FROM OIL COOLER CORE.
- [SDR HEEA111385](https://openairdocs.org/sdr/HEEA111385.md): Seal · leaking · Oct 4, 2006 · N192PH · Skrsky S92A · Turbine Engine Oil System
  > OIL PRESSURE WAS NORMAL AFTER TAKEOFF, ABOUT 35 MIN IN CRUISE FLIGHT, NR 2 ENGINE OIL PRESSURE HAD DROPPED TO 55 PSI, THEN ON ARRIVAL, NR 2 ENGINE OIL PRESSURE WAS BETWEEN 47 AND 50 PSI. REPLACED G AXIS SEAL.
- [SDR HEEA111000](https://openairdocs.org/sdr/HEEA111000.md): Pump · failed · Aug 31, 2006 · N59806 · Bell 214ST · Aircraft Fuel Distribution System
  > NR 2 FUEL TRANSFER PUMP FAILED, CONTINUED WITH NO FURTHER PROBLEMS. MAINTENANCE REPLACED THE NR 2 TRANSFER PUMP.
- [SDR ALG2006F00036](https://openairdocs.org/sdr/ALG2006F00036.md): Wire · shorted · Apr 17, 2006 · N391AL · Bell 214ST · Auto Flight System Wiring
  > IN FLIGHT, BOTH ELEVATORS FAILED, AARS ROLL FAILED, SCAS PITCH FAILED, AND FBW ELEVATORS WENT FULL UP. THE AIRCRAFT ROLLED LT AND PITCHED UP. WITH FULL FWD AND FULL RT CYCLIC, PILOTS DID NOT REGAIN CYCLIC CONTROL UNTIL THE AIRSPEED HAD DROPPED BELOW 100 KTS.
- [SDR ALG2006F00035](https://openairdocs.org/sdr/ALG2006F00035.md): Current Limiter · inoperative · Mar 31, 2006 · N392AL · Bell 214ST · DC Regulator
  > IN FLIGHT, EN ROUTE, THE FOLLOWING INDICATION WENT TO (0). NR 1 NG, NR 1 ENG PRESS, TEMP, C-BOX PRESS, NR 1 HYD PRESS, NR 2 HYD TEMP. NO CAUTION LIGHTS ILLUMINATED. AC DIVERTED, MAINTENANCE REMOVED AND REPLACED NR 1 CURRENT LIMITER, (PN 209-375-096-103). (
- [SDR HEEA108122](https://openairdocs.org/sdr/HEEA108122.md): Swashplate · out of adjust · Feb 16, 2006 · N3897N · Bell 214ST · Main Rotor Mast/Swashplate
  > 3 MINUTES AFTER TAKEOFF, A LOW RUMBLE WAS HEARD FOLLOWED BY A VERTICAL VIBRATION. AIRCRAFT WAS FLOWN AND SHUT DOWN WAS ACCOMPLISHED. UPON INSPECTION THE AIRCRAFT GREASE WAS FOUND SPLATTERED OVER THE UPPER TRANSMISSION COWLING. MAINTENANCE FOUND THE SWASHPL
- [SDR HEEA107966](https://openairdocs.org/sdr/HEEA107966.md): Window · missing · Feb 7, 2006 · N59806 · Bell 214ST · Flight Compartment Windows
  > DURING TAKEOFF CREW HEARD POPPING NOISE AND NOTICED PILOT'S SKYLIGHT MISSING, APPARENTLY CAME OFF DURING TAKEOFF.
- [SDR HEEA107922](https://openairdocs.org/sdr/HEEA107922.md): Packing · cut · Jan 17, 2006 · N8045T · Bell 214ST · Engine Oil Pressure
  > DURING CRUISE FLIGHT NR 2 ENGINE OIL PRESSURE DECREASED TO APPROXIMATELY 15 PSI OVER ABOUT 60 SECONDS. ENGINE OIL PRESSURE EMERGENCY PROCEDURE WAS PERFORMED. AIRCRAFT DIVERTED FOR OEI LANDING. MAINTENANCE FOUND A CUT PACKING ON THE ENGINE CHIP PLUG ALLOWIN
- [SDR HEEA107418](https://openairdocs.org/sdr/HEEA107418.md): Pump · popped · Dec 14, 2005 · N3897N · Bell 214ST · Fuel Transfer Valve
  > DURING CRUISE FLIGHT, THE NR 2 TRANSFER LIGHT ILLUMINATED AND CIRCUIT BREAKER POPPED. FOLLOWED EMERGENCY PROCEDURE AND LANDED. MAINTENANCE REPLACED NR 2 TRANSFER PUMP.
- [SDR ALG2005F00121](https://openairdocs.org/sdr/ALG2005F00121.md): Filter · failed · Dec 6, 2005 · N391AL · Bell 214ST · Aircraft Fuel Filter/Strainer
  > ON TAKEOFF, NR 2 ENGINE FUEL FILTER LIGHT CAME ON, AND THE PILOT LANDED THE AC. THE MECHANIC REMOVED AND REPLACED NR 2 ENGINE FUEL FILTER ELEMENT, GROUND RUN AND LEAK CHECKED IAW MM, AC WAS RETURNED TO SERVICE. (K)
- [SDR HEEA107317](https://openairdocs.org/sdr/HEEA107317.md): Wire · chafed · Dec 1, 2005 · N59806 · Bell 214ST · Auto Flight System Wiring
  > SCAS FAILED IN FLIGHT. ATTEMPTED TO RESET IT BUT IT BLEW THE CIRCUIT BREAKER. SECURED OFF AND CONTINUED TO BASE WITHOUT INCIDENT. MAINTENANCE REPAIRED CHAFED WIRE WHICH RUNS BETWEEN THE SCAS AMP AND THE YAW ACTUATOR.
- [SDR ALG2005F00056](https://openairdocs.org/sdr/ALG2005F00056.md): Line · leaking · Jul 30, 2005 · N390AL · Bell 214ST · Hydraulic System, Main
  > ENROUTE, A HOWLING NOISE STARTED AND BECAME LOUDER, THE PILOT NOTICED NR 1 HYD PRESSURE FLUCTUATED BETWEEN 200-300 PSI. THE PILOT TURNED OFF NR 1 HYD NOISE WENT AWAY. UPON LANDING THE MECHANIC FOUND NR 1 PRESSURE LINE TO THE COLLECTIVE SERVO IS LEAKING. HE
- [SDR HEEA107351](https://openairdocs.org/sdr/HEEA107351.md): Engine · malfunctioned · Jul 22, 2005 · N3897N · Bell 214ST · Engine (Turbine/Turboprop)
  > IN CRUISE, NR 1 ENGINE NR AND NG AND MGT WENT HIGH, TORQUE AND NP SHOWED ZERO, REDUCED NR 1 THROTTLE AND PERFORMED CHECKLIST AND SHUT ENGINE DOWN. ROTOR RPM WENT TO 107 FOR 10 SECONDS. INSPECTED ENGINE AND REPLACED YELLOW ENGINE HARNESS AND ECU.
- [SDR CA050309001](https://openairdocs.org/sdr/CA050309001.md): Tube · chafed · Mar 1, 2005 · Bell 214ST · Hydraulic System, Main
  > (CAN) DURING ROUTINE MAINTENANCE, THE SUBJECT TUBE WAS FOUND WITH A (0.375 INCH X 0.187 INCH) HOLE THAT ORIGINATED FROM CHAFING WITH A HYDRAULIC OIL LINE. THE HOLE WAS LOCATED APPROXIMATELY IN THE CENTER OF THE TUBE. THE TOTAL CHAFING DAMAGE IN THIS AREA, CO
- [SDR ALG2004F00059](https://openairdocs.org/sdr/ALG2004F00059.md): Warning Light · activated · Oct 11, 2004 · N392AL · Bell 214ST · Main Rotor Mast/Swashplate
  > FIVE MINUTES AFTER TAKEOFF, AC815 TRANSMISSION CHIP LIGHT ILLUMINATED, PILOT RETURNED TO RIG. MECHANIC REMOVED, CLEANED, AND INSPECTED ALL TRANSMISSION CHIP PLUGS, NO CONTAMINANTS NOTED. CONNECTOR PLUGS WERE EXAMINED AND FOUND SERVICEABLE. AC WAS RETURNED T
- [SDR HEEA096018](https://openairdocs.org/sdr/HEEA096018.md): Bleed Valve · malfunctioned · Jun 22, 2004 · N59806 · Bell 214ST · Compressor Bleed Valve
  > WHILE HOVERING FOR TAKEOFF,NR 2 MGT STARTING RISING. MGT SPIKED AT 933 DEGREES THREE TIMES, THEN STAYED AT 933 DEGREES. AIRCRAFT WAS SENT DOWN AND MGT RETURNED TO NORMAL FLAT PITCH.
- [SDR HEEA092089](https://openairdocs.org/sdr/HEEA092089.md): Ecu · malfunctioned · Jan 10, 2004 · N59806 · Bell 214ST · Fuel Control/Turbine Engines
  > SHORTLY AFTER TAKE OFF NR 1 ENGINE TORQUE FLUCTUATED. MAINTENANCE FOUND ECU DEFECTIVE.
- [SDR HEEA092091](https://openairdocs.org/sdr/HEEA092091.md): Ecu · malfunctioned · Jan 9, 2004 · N59806 · Bell 214ST · Fuel Control/Turbine Engines
  > AFTER TAKEOFF TORQUE GUAGES FLUCTUATED. RETURNED TO BASE.
- [SDR HEEA089035](https://openairdocs.org/sdr/HEEA089035.md): Engine · malfunctioned · Aug 27, 2003 · N59806 · Bell 214ST · Engine (Turbine/Turboprop)
  > ENROUTE FROM GB-426, AIRCRAFT LOST POWER ON NR 2 ENGINE. CONTINUED TO MCY AND PERFORMED SINGLE ENGINE LANDING.
- [SDR ALGA087781](https://openairdocs.org/sdr/ALGA087781.md): Starter · malfunctioned · Jun 26, 2003 · N391AL · Bell 214ST · Engine Starter
  > WILL NOT ENGAGE EVERYTIME. REQUEST WARRANTY REPAIR. RO 33256 DMR 719713
- [SDR ALGA087782](https://openairdocs.org/sdr/ALGA087782.md): Starter · failed · Jun 26, 2003 · N391AL · Bell 214ST · Engine Starter
  > STARTER WILL NOT ENGAGE. REQUEST WARRANTY REPAIR. DMR 719714 RO33252
- [SDR MALA030287](https://openairdocs.org/sdr/MALA030287.md): Pressure Switch · failed · May 29, 2003 · N106XJ · Saab SF340A · Fuel Controlling System
  > DURING CLIMBOUT ON FLIGHT 3183, RT MAIN PUMP LIGHT ILLUMINATED AFTER TAKEOFF. AIR RETURN TO MSP. MAINTENANCE REPLACED MAIN FUEL PRESSURE SWITCH P/N 8346-001, OPS AND LEAK CHECK GOOD.
- [SDR HEEA086685](https://openairdocs.org/sdr/HEEA086685.md): Exciter · malfunctioned · May 22, 2003 · N3897N · Bell 214ST · Exciter
  > EXCITER PRODUCES SLOW LIGHT OFF. REPLACED.
- [SDR HEEA086686](https://openairdocs.org/sdr/HEEA086686.md): Pressure Switch · malfunctioned · May 22, 2003 · N59806 · Bell 214ST · Engine Oil Cooler
  > NR 2 ENGINE BLOWER LIGHT CAME ON AFTER ENGINE START. REPLACED.
- [SDR HEEA086590](https://openairdocs.org/sdr/HEEA086590.md): Seal · leaking · May 12, 2003 · N59806 · Bell 214ST · Turbine Engine Oil System
  > FIFTY TWO MINUTES AFTER TAKEOFF, NR 2 ENGINE OIL LIGHT ILLUMINATED WITH COINCIDING PRESSURE DROP OF NR 2 ENGINE OIL PRESSURE GAUGE. PRESSURE WENT TO ZERO WHILE NR 2 ENGINE WAS SHUT DOWN IN FLIGHT.
- [SDR HEEA084413](https://openairdocs.org/sdr/HEEA084413.md): Igniter · failed · Feb 12, 2003 · N8045T · Bell 214ST · Spark Plug/Igniter
  > ENGINE HARD TO START. REPLACED IGNITERS.
- [SDR ALG2003F00029](https://openairdocs.org/sdr/ALG2003F00029.md): Cartridge · inoperative · Dec 3, 2002 · N309AL · Bell 214ST · Fuel Boost Pump
  > DURING CRUISE FLIGHT, NR 1 FUEL TRANSFER PUMP CAUTION LIGHT ILLUIMINATED, AIRCRAFT LANDING WAS UNEVENTFUL, MAINTENANCE WAS NOTIFIED. THE MECHANIC FOUND NR 1 FUEL PUMP TRANSFER PUMP INOPERATIVE, HE REMOVED AND REPLACED THE PUMP AND AIRCRAFT RETURNED TO SERVIC
- [SDR HEEA080441](https://openairdocs.org/sdr/HEEA080441.md): Bleed Valve · malfunctioned · Jul 9, 2002 · N3897N · Bell 214ST · Compressor Bleed Valve
  > NR 1 ENGINE HAS LOW POWER DUE TO MALFUNCTIONING BLEED VALVE. TO BE SENT TO VENDOR FOR REPAIR.
- [SDR HEEA080115](https://openairdocs.org/sdr/HEEA080115.md): Igniter · worn · Jun 25, 2002 · N59806 · Bell 214ST · Spark Plug/Igniter
  > IGNITER WORN. TO BE SENT TO VENDOR FOR CREDIT.

Next page: https://openairdocs.org/engine/ge-ct7-2a/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 = 'CT72A'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/ge-ct7-2a/reports

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