# Service difficulty reports: Rotec R2800

A list on [Rotec R2800](https://openairdocs.org/engine/rotec-r2800.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 114 reports

- [SDR FXGA2026FA0000409](https://openairdocs.org/sdr/FXGA2026FA0000409.md): Doubler · corroded · May 19, 2026 · N747CE · Doug DC6A · Wing, Plate/Skin
  > R/H SPAR NEEDS REPAIR DOUBLER AT STA 167 REPLACED DUE TO CORROSION AT MAX LIMIT.
- [SDR FXGA2026FA0000410](https://openairdocs.org/sdr/FXGA2026FA0000410.md): Flange · cracked · May 19, 2026 · N747CE · Doug DC6A · Wing Miscellaneous Structure
  > CRACK INDICATION NR 3 TANK 182C FLANGE, REPAIRED PER EO 2609
- [SDR FXGA2026FA0000411](https://openairdocs.org/sdr/FXGA2026FA0000411.md): Skin · corroded · May 19, 2026 · N747CE · Doug DC6A · Fuselage Main, Plate/Skin
  > CORROSION WAS NOTED ON FUSELAGE PLATING @ L/H OVERWING EMERGENCY EXIT DOOR FRAME, LOWER AFT CORNER. REPAIRED PER EO 2608
- [SDR FXGA20200826001](https://openairdocs.org/sdr/FXGA20200826001.md): Spring · broken · Aug 25, 2020 · N747CE · Doug C118A · Hydraulic System, Main
  > HYDRAULIC BYPASS STUCK IN UP POSITION, UPON INSPECTIN FOUND HYDRAULIC BYPASS RETURN SPRING BROKEN.
- [SDR FXGA201812240001](https://openairdocs.org/sdr/FXGA201812240001.md): Propeller · sheared · Dec 21, 2018 · N451CE · Doug C118A · Propeller Feathering/Reversing
  > EXCESSIVE VIBRATION ON #4 ENGINE NO OTHER INDICATION PRECAUTIONARY SHUTDOWN #4 ENGINE/ TWO BLADES WENT TO FEATHER THIRD BLADE STAYED IN LOW PITCH CONDITION
- [SDR FXGA20171208001](https://openairdocs.org/sdr/FXGA20171208001.md): Carburetor · leaking · Dec 7, 2017 · N451CE · Doug C118A · Fuel Control/Reciprocating Engines
  > COMING OUT OF REVERSE #1 ENGINE STARTED ON FIRE, UNABLE TO RESTART BLEW RIGHT SIDE CO2 BANK
- [SDR FXGA201712050001](https://openairdocs.org/sdr/FXGA201712050001.md): Warning System · activated · Nov 28, 2017 · N151 · Doug DC6A · Landing Gear Position and Warning
  > UNSAFE LEFT MAIN GEAR INDICATION AFTER CYCLING SEVERAL TIMES FINALLY GOT DOWN & LOCKED SAFE INDICATION.
- [SDR 2017FA0000381](https://openairdocs.org/sdr/2017FA0000381.md): Valve · failed · Jul 20, 2017 · N527CL · Reciprocating Engine Cylinder Section
  > APPROXIMATELY 25 HOURS INTO PHASE 1 OF THE EXPERIMENTAL AMATEUR BUILT FLIGHT TEST, WHILE AIRBORNE OVER THE HOME AIRPORT, KLNR, THE EXHAUST VALVE IN THE NR 4 LOWER CYLINDER FAILED, DROPPING THE HEAD OF THE VALVE INTO THE COMBUSTION CHAMBER. THE PILOT SHUT THE
- [SDR 2017F00172](https://openairdocs.org/sdr/2017F00172.md): Line · cracked · Jul 19, 2017 · N9056R · Doug DC6A · Hydraulic System, Main
  > COMPLETE HYDRAULIC SYSTEM FAILURE, EMERGENCY LANDING PROCEDURES FOLLOWED. REPLACED HYDRAULIC PRESSURE LINE NR 2. FOUND CRACK AT B-NUT. REPLACED THE LINE. PREFORMED LEAK CHECK & OPS CHECK OKAY. RELEASED AIRCRAFT FOR CONT SERVICE.
- [SDR FXGA20170411001](https://openairdocs.org/sdr/FXGA20170411001.md): Test Switch · malfunctioned · Apr 10, 2017 · N151 · Doug DC6B · Fire Detection
  > AFT BAG FIRE HANDLE INTERMITTENT ILLUMINATION. (LT/RT CYL ALSO)
- [SDR Q9U201410170001](https://openairdocs.org/sdr/Q9U201410170001.md): Governor · failed · Oct 3, 2014 · N145GT · Cvac C131D · Propeller Governor
  > PROPELLER GOVERNOR WOULD NOT DECREASE BELOW 2500 RPM. AFTER REACHING CRUISE ALTITUDE, CREW WAS UNABLE TO DECREASE THE ENGINE RPM BELOW 2500. SHORTLY THEREAFTER THE RPM BEGAN TO GRADUALLY INCREASE ON ITS OWN. ENGINE WAS FEATHERED TO PREVENT PROPELLER OVERSPE
- [SDR FXGA20120711001](https://openairdocs.org/sdr/FXGA20120711001.md): Fire Warning · illuminated · Jul 2, 2012 · N351CE · Doug C118A · Fire Detection
  > NR 1 ENGINE OBSERVED ZONE 1 FIRE INDICATION DURING TAKEOFF POWER.
- [SDR CA110601010](https://openairdocs.org/sdr/CA110601010.md): Cylinder Head · cracked · May 31, 2011 · Doug DC6B · Reciprocating Engine Cylinder Section
  > NR1 ENGINE RUNNING ROUGH WHEN LEANED OUT NR3 CYL EXHAUST EAR CRACKED. CYLINDER REPLACED.
- [SDR FXGA351A](https://openairdocs.org/sdr/FXGA351A.md): Skin · cracked · Dec 7, 2010 · N351CE · Doug C118A · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN CRACKED AT NR2 VHF COM ANTENNA DOUBLER. REPAIRED IAW EAC EO 1061 AND 8110-3 NR1032, DATED 12/07/2010.
- [SDR FXGAN54514](https://openairdocs.org/sdr/FXGAN54514.md): Lever · worn · May 14, 2010 · N54514 · Curtis C46DAIRLIFT · Landing Gear Selector
  > LANDING GEAR LEVER STUCK IN THE NEUTRAL POSITION. LANDING GEAR EXTENDED USING EMERGENCY PROCEDURES ACFT DIVERTED FOR UNEVENTFUL LANDING.
- [SDR 2010F00099](https://openairdocs.org/sdr/2010F00099.md): Brush Block · worn · Mar 8, 2010 · N351CE · Doug C118A · Propeller/Rotor Anti-Ice/De-Ice System
  > DURING ICING THE NR (4) PROPELLER DEICE INDICATED 50 AMPS, SPARKS VISIBLE IN THE COWLING.
- [SDR I5HA0824013](https://openairdocs.org/sdr/I5HA0824013.md): Wing · dented · Dec 18, 2008 · N150PA · Cvac 240* · Wing, Plate/Skin
  > DURING THE LANDING FLARE, A BIRD STRUCK THE OTBD L/E OF THE LT WING. THE CREW LANDED THE ACFT WITHOUT FURTHER INCIDENT. THE LEADING EDGE WAS REMOVED AND REPLACED AND THE ACFT RETURNED TO SERVICE.
- [SDR I5HA0824006](https://openairdocs.org/sdr/I5HA0824006.md): Engine · damaged · Jul 16, 2008 · N150PA · Cvac T29B · Engine (Reciprocating)
  > JUST AFTER TAKEOFF AT APPROXIMATELY 1700 (L) CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENG. THE CAPTAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED AN EM
- [SDR I5H2008F00001](https://openairdocs.org/sdr/I5H2008F00001.md): Engine · making metal · Jul 16, 2008 · N150PA · Cvac T29B · Engine (Reciprocating)
  > JUST AFTER TAKEOFF, AT APPROXIMATELY 1700, THE CREW OBSERVED A HIGH OIL TEMPERATURE INDICATION ON THE LT ENGINE. THE CAPTAIN REDUCED POWER AND THE OIL TEMPERATURE CAME DOWN BUT THE OIL PRESSURE ALSO CAME DOWN TO AN ABNORMALLY LOW PRESSURE. THE CREW DECLARED A
- [SDR 200600077](https://openairdocs.org/sdr/200600077.md): Hinge · fractured · Sep 19, 2006 · N9701F · Frchld C82ASTWDAVIS · Elevator Control System
  > LT AND RT FURTHEST OB ELEVATOR HINGE BRACKET ON THE STABILIZER WERE BROKEN. IT APPEARS TO BE FROM WIND GUSTS. THE CENTER 3 HINGES WERE UNAFFECTED.
- [SDR EVA2006F00000](https://openairdocs.org/sdr/EVA2006F00000.md): Clamp · out of position · Sep 16, 2006 · N1822M · Curtis C46* · Engine Collector/Tailpipe/Nozzle
  > EXHAUST COLLECTOR CONNECTION MOVED OUT OF POSITION AFTER TAKEOFF, ALLOWING EXHAUST GAS TO ESCAPE AND ILLUMINATE THE ZONE 1 FIRE WARNING. ENGINE WAS SHUTDOWN AND AIRCRAFT RETURNED TO DEPARTURE AIRPORT. AIRCRAFT RECEIVED NO DAMAGE AND REPAIRS WERE ACCOMPLISHED
- [SDR NACA20060005](https://openairdocs.org/sdr/NACA20060005.md): Heater · leaking · Jan 24, 2006 · N6174C · Doug DC6A · Heating System
  > SUSPECT CABIN HEATER EXHAUST FUMES IN COCKPIT.REPLACED CABIN HEATER ASSEMBLY. LEAK AND OP CHECKED GOOD. REF: NAC MM. SEC. VII. PAGE 81 AND 82.
- [SDR I5HA0524006](https://openairdocs.org/sdr/I5HA0524006.md): Engine · leaking · Sep 16, 2005 · N156PA · Cvac 240* · Turbine Engine Oil System
  > DURING CLIMBOUT, THE PILOT OBSERVED A LOSS OF OIL QUANTITY FROM THE LT ENGINE. THE CREW PERFORMED AN EMERGENCY SHUTDOWN OF THE LT ENGINE AND RETURNED TO DEPARTURE. THE CAUSE OF THE OIL LOSS HAS NOT YET BEEN DETERMINED AND THE AIRCRAFT REMAINS AT DEPARTURE.
- [SDR 0509137](https://openairdocs.org/sdr/0509137.md): Exhaust Riser · separated · Sep 6, 2005 · N234P · Lkheed PV1 · Engine Collector/Tailpipe/Nozzle
  > NR 5 EXHAUST RISER HAD SEPARATED FROM ENGINE JUST BELOW THE FLANGE WELD. THE OWNER STATED THIS WAS THE SECOND TIME THIS HAS HAPPENED IN 40 HOURS. REPLACED ALL 3 RISERS AND COLLECTOR.
- [SDR I5HA0524003](https://openairdocs.org/sdr/I5HA0524003.md): Line · loose · May 28, 2005 · N156PA · Cvac 240* · Engine RPM Indicating System
  > WHILE ENROUTE, MAINTENANCE, THE PILOT OBSERVED A LOSS OF TORQUE PRESSURE ON THE LT ENGINE WITH NO SECONDARY INDICATIONS. AS A PRECAUTION, THE PILOT ELECTED TO SHUT-DOWN THE ENGINE AND MADE AN UNEVENTFUL LANDING. DURING INSPECTION OF ENGINE, LOOSE TORQUE TRAN
- [SDR I5HA0524001](https://openairdocs.org/sdr/I5HA0524001.md): Augmentor Tube · fire · Mar 31, 2005 · N156PA · Cvac 240* · Engine Collector/Tailpipe/Nozzle
  > RT ENG FIRE WARNING BELL SOUNDED AND ASSOC FIRE WARNING LIGHT ILLUMINATED DURING TAXI. RT FIRE BOTTLE WAS DISCHARGED AND ENG SHUTDOWN. FIRE WAS EXTINGUISHED WITH NO FURTHER ACTION. EXAMINATION OF RT ENG REVEALED INSIDE OF AUGMENTOR TUBE HAD CAUGHT FIRE. FIR
- [SDR CA050222011](https://openairdocs.org/sdr/CA050222011.md): Bolt · broken · Feb 22, 2005 · Reciprocating Engine Rear Section
  > (CAN) UPON INSPECTION OF THE ENGINE DURING A SCHEDULED B-CHECK, ONE OF THE BOLTS HOLDING THE POWERCASE AND REAR ACCESSORY CASE TOGETHER WAS FOUND MIGRATING OUT OF THE POWERCASE BETWEEN CYLINDER NR4 AND NR5. ENGINE WAS REMOVED FOR REPAIR BY OVERHAUL SHOP.
- [SDR NACA20040047](https://openairdocs.org/sdr/NACA20040047.md): Warning Switch · false activation · Oct 18, 2004 · N7919C · Doug DC6B · Trailing Flap Position Indicating System
  > TAKE-OFF WARNING HORN ON TAKE-OFF ROLL. REMOVED AND REPLACED FLAP POSITION WARNING SWITCH.
- [SDR CA040818003](https://openairdocs.org/sdr/CA040818003.md): Shaft · sheared · Aug 18, 2004 · Reciprocating Engine Front Section
  > (CAN) TWO PINION SHAFTS FOUND SHEARED WHEN REDUCTION GEAR SECTION REMOVED. ALL BROKEN PARTS FOUND AND ENGINE CLEANED FOR REASSEMBLY. GEAR SECTION SENT TO OVERHAUL SHOP FOR REPAIR.
- [SDR NACA20040050](https://openairdocs.org/sdr/NACA20040050.md): Skin · damaged · Jul 24, 2004 · N99330 · Doug DC6A · Fuselage Main, Plate/Skin
  > HOLE IN FUSELAGE AFT OF THE REAR CARGO DOOR AT STA 807.5L TO 822L. REMOVED DAMAGE AND FABRICATED A NEW PATCH FROM 0.80 7075-T6. REF: DOHM FIGURE 12-22.
- [SDR NACA20040051](https://openairdocs.org/sdr/NACA20040051.md): Frame · cracked · Jun 17, 2004 · N99330 · Doug DC6A · Fuselage Main, Frame
  > RT FUSELAGE CIRCUMFERENTIAL AT STA. R460 CRACKED APPROXIMATELY 3 INCHES ABOVE FLOOR LEVEL. REPLACED ANGLE WITH THE SAME TYPE AND MATERIAL.090 7075 T6. FABRICATED AND INSTALLED REPAIR (L) AND STRAP WITH REFERENCE TO DOHM FIG. 11-52 AND FIG. 12-10 SHEET 2.
- [SDR LO62004F00000](https://openairdocs.org/sdr/LO62004F00000.md): Generator · inoperative · May 6, 2004 · N3427 · Cvac 34032 · AC Generation System
  > LEFT AC GENERATOR OPERATION INTERMITTENT AND UNSTEADY IAW VOLTMETER. REPLACED GEN WITH OVERHAULED UNIT.
- [SDR LO62004F00001](https://openairdocs.org/sdr/LO62004F00001.md): Actuator · inoperative · May 6, 2004 · N3427 · Cvac 34032 · Engine Cowl Flaps
  > RT SIDE, COWL FLAP ACTUATOR BECAME INTERMITTENT. FINALLY COWL FLAPS STOPPED PART WAY OPEN. REPLACED ACTUATOR WITH OVERHAULED UNIT.
- [SDR CA040510003](https://openairdocs.org/sdr/CA040510003.md): Control Cable · corroded · May 3, 2004 · Cndair CL2151A10 · Rudder Control System
  > DURING A STRUCTURAL REPAIR TO THE RT REAR WING-TO-FUSELAGE FRAME ANGLE A PANEL AT WS 60.80, ADJACENT TO REAR SPAR, HAD TO BE DRILLED OFF TO FACILITATE THE REPAIR. IT WAS AT THIS TIME CORROSION WAS DISCOVERED ON THE RUDDER/AILERON INTERCONNECT CABLE P/N 215-90
- [SDR I5HA0324002](https://openairdocs.org/sdr/I5HA0324002.md): Cylinder · failed · Oct 24, 2003 · N99380 · Cvac 240* · Reciprocating Engine Cylinder Section
  > EN ROUTE, PILOT NOTICED A DECREASE IN OIL QTY ON RT ENG. CONTINUED TO PIT. ELECTED TO KEEP RT ENG RUNNING. OIL QTY CONTINUED TO DECREASE. PILOT NOTICED MINOR TORQUE FLUCTUATION JUST PRIOR TO TOUCHDOWN. UPON TOUCHDOWN, NOTIFIED THAT THE RT ENG ON FIRE. E-H
- [SDR NACA20030112](https://openairdocs.org/sdr/NACA20030112.md): Fire Warning · false activation · Sep 16, 2003 · N99330 · Doug DC6A · Fire Detection
  > TAIL HEATER FIRE WARNING INTERMITTENTLY CAME ON AFTER HEATER CHECK. GROUND OPS CHECKED ANTI-ICE HEATER SYSTEM PER NAC DC-6 OPS MANUAL CH.14-20 SECT. C, CHECKED GOOD. INSPECTED HEATER FOR VISUAL DISTRESS, NONE NOTED.
- [SDR 2003F00529](https://openairdocs.org/sdr/2003F00529.md): Engine · malfunctioned · Jul 11, 2003 · N156PA · Cvac 240* · Engine (Turbine/Turboprop)
  > WHILE EN ROUTE TO CVG FROM PIT, IN CRUISE CONFIGURATION, THE CREW FELT A SHUDDER IN THE LEFT ENGINE. FIFTEEN MINUTES LATER FELT ANOTHER SHUDDER AND AGAIN ONE MINUTE LATER WITH A LARGE TORQUE SWING AND OIL QUANTITY DROP. THE OIL LOSS WAS FASTER THAN THE CAPAC
- [SDR CA030528015](https://openairdocs.org/sdr/CA030528015.md): Cotter Pin · mismanufactured · May 28, 2003 · Curtis C46FAIRLIFT · Fasteners
  > (CAN) THE COTTER PINS RECIEVED FROM AIRCRAFT PARTS INTERNATIONAL ARE FAULTY AROUND THE HEAD. THE COTTER PINS ARE MANUFACTURED BY WESTERN WIRE. WE RECIEVED THEM IN MARCH 2003. WHEN I CALLED THE SUPPLIER AND EXCHANGED LOT NUMBERS, HE HAD A DIFFERENT LOT NUMBER O
- [SDR BKJ2003F00000](https://openairdocs.org/sdr/BKJ2003F00000.md): Brake Assy · leaking · Jan 11, 2003 · N24DR · Cvac 440 · Landing Gear Brake System
  > DURING LANDING CHECK, UPON ARRIVAL TO AIRPORT. PILOTS NOTICED LOW HYDRAULIC RESEVOIR LEVEL. TOWER WAS NOTIFIED AND A NORMAL LANDING WAS MADE. AS A PRECAUTION, THE AIRCRAFT WAS TOWED TO PARKING. INSPECTION REVEALED A LEAKING BRAKE ASSEMBLY.
- [SDR NAFA2002001](https://openairdocs.org/sdr/NAFA2002001.md): Cylinder · cracked · Dec 5, 2002 · N7780B · Doug DC6 · Reciprocating Engine Cylinder Section
  > NR 3 ENGINE PRECAUTIONARY SHUT DOWN FOR A NR 2 CYLINDER SHORTED SECONDARY. REPLACED NR 2 CYLINDER.
- [SDR Q2A2003F00000](https://openairdocs.org/sdr/Q2A2003F00000.md): Fitting · cracked · Nov 13, 2002 · N77WF · Beech E90 · Wing, Attach Fittings
  > WHILE PERFORMING NDT INSPECTION OF WING ATTACH FITTINGS, LEFT LOWER FORWARD FITTING FOUND CRACK IN RADIUS OF BOLT HOLE. SPAR WAS THEN REPLACED.
- [SDR CA021029007](https://openairdocs.org/sdr/CA021029007.md): Line · cracked · Oct 29, 2002 · Cndair CL2151A10 · Hydraulic System, Main
  > (CAN) DURING A 'B' CHECK INSPECTION, A HYDRAULIC SYSTEM FUNCTION CHECK WAS BEING COMPLETED. A LEAK WAS DETECTED AT THE AUX HYDRAULIC RETURN LINE LOCATED IN THE FORWARD SKI SLOPE OF THE AIRCRAFT. UPON INVESTIGATION A CRACK WAS FOUND WITH A PIECE OF THE LINE MIS
- [SDR NACA20020051](https://openairdocs.org/sdr/NACA20020051.md): Pushrod · bent · Sep 28, 2002 · N1377K · Doug C118A · Reciprocating Engine Cylinder Section
  > NR 4 ENGINE SHUT DOWN AT 1802Z FOR A NR 12 CYLINDER DOUBLE SHORTED SECONDARY AND WON'T LEAN. FOUND EXHAUST AND INTAKE PUSH RODS BENT. REPLACED AND SET VALVES. INSPECTED CYLINDER FOR DAMAGE, CHECKED GOOD. OP CHECK GOOD ON RUNUP.
- [SDR 2002FA0001126](https://openairdocs.org/sdr/2002FA0001126.md): Oil Tank · ruptured · Sep 3, 2002 · N153JR · Cvac 340CVAC · Engine Oil Storage (Airframe Furnished)
  > THE OIL TANK WAS OVERFILLED ON LEFT ENGINE. ON TAKE OFF ROLL, THE PRESSURE FROM THE OVERFILL CAUSED THE TANK TO RUPTURE. OIL THEN BEGAN TO SPRAY ONTO THE EXHAUST SYSTEM. THIS OIL IGNITED AND THE SUBSEQUENT FLAMES DAMAGED THE NACELLE IN THE AREA AFT OF THE O
- [SDR NACA20020040](https://openairdocs.org/sdr/NACA20020040.md): Cylinder · cracked · Aug 31, 2002 · N779TA · Doug DC6 · Reciprocating Engine Cylinder Section
  > FEATHERED THE NR 4 ENGINE IN CRUISE DUE TO BACKFIRED, LOW BMEP. REPLACED THE NR 3 CYLINDER.
- [SDR NACA20020041](https://openairdocs.org/sdr/NACA20020041.md): Ignition Lead · shorted · Aug 31, 2002 · N43872 · Doug DC6 · Ignition Harness (Distribution)
  > PRECAUTIONARY SHUTDOWN THE NR 3 ENGINE DUE TO DOUBLE SHORTED SECONDARY ON THE NR 10 CYLINDER. REPLACED SPARK PLUGS, Y-LEAD, SHORT LEADS, AND COIL.
- [SDR NACA20020039](https://openairdocs.org/sdr/NACA20020039.md): Cylinder · cracked · Aug 28, 2002 · N779TA · Doug DC6 · Reciprocating Engine Cylinder Section
  > NR 4 ENGINE FEATHERED DUE TO BACKFIRING. REMOVED AND REPLACED THE NR 18 CYLINDER.
- [SDR NACA20020038](https://openairdocs.org/sdr/NACA20020038.md): Cylinder · defective · Aug 21, 2002 · N99330 · Doug DC6A · Reciprocating Engine Cylinder Section
  > SHUTDOWN THE NR 3 ENGINE DUE TO DOUBLE SHORTED SECONDARY CYLINDER NR 11 AND DOUBLE SHORTED SECONDARY CYLINDER NR 15. REMOVED AND REPLACED THE NR 11 AND NR 15 CYLINDERS.
- [SDR NACA20020037](https://openairdocs.org/sdr/NACA20020037.md): Cylinder · cracked · Aug 19, 2002 · N779TA · Doug DC6 · Reciprocating Engine Cylinder Section
  > FEATHERED THE NR 3 ENGINE AT 0312Z DUE TO BACKFIRING AND ROUGH RUNNING. REPLACED THE NR 4 CYLINDER.
- [SDR NACA20020035](https://openairdocs.org/sdr/NACA20020035.md): Cylinder · cracked · Aug 7, 2002 · N1377K · Doug C118A · Reciprocating Engine Cylinder Section
  > FEATHERED THE NR 3 ENGINE AT 1841Z DUE TO RUNNING ROUGH AND LOW COMPRESSION INDICATED, NR 6 OR NR 17. REMOVED AND REPLACED THE NR 17 CYLINDER ON THE NR 3 ENGINE.

Next page: https://openairdocs.org/engine/rotec-r2800/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 = 'R2800'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/engine/rotec-r2800/reports

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