# GE CF34-8E5A1

- Type: Engine model (FAA registry)
- Registry code: 30062
- Manufacturer (registry): GE
- Model: CF34-8E5A1
- Engine type: Turbo-fan
- Power: 14,510 lb thrust
- Data sheet: [TCDS E00063EN](https://openairdocs.org/tcds/E00063EN) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 0 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf34-8e5a1

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 2026-21-11](https://openairdocs.org/ad/2026-21-11): Turbine Engine Compressor Section · General Electric Company GE Aerospace CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 27, 2026
- [AD 2025-12-08](https://openairdocs.org/ad/2025-12-08): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jul 23, 2025
- [AD 2023-02-05](https://openairdocs.org/ad/2023-02-05): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 9 more. Effective Mar 14, 2023
- [AD 2022-21-06](https://openairdocs.org/ad/2022-21-06): Turbine Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Nov 15, 2022
- [AD 2022-09-14](https://openairdocs.org/ad/2022-09-14): Compressor Bleed Valve · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Jun 24, 2022
- [AD 2022-08-06](https://openairdocs.org/ad/2022-08-06): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Apr 29, 2022
- [AD 2021-26-19](https://openairdocs.org/ad/2021-26-19): Turbine Section · General Electric CF34-8C5, CF34-8C5B1, CF34-8E2 and 6 more. Effective Jan 25, 2022
- [AD 2021-23-51](https://openairdocs.org/ad/2021-23-51): Turbine Engine Compression Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Dec 29, 2021
- [AD 2021-18-13](https://openairdocs.org/ad/2021-18-13): Turbine Engine Combustion Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 22, 2021
- [AD 2018-17-14](https://openairdocs.org/ad/2018-17-14): Thrust Reverser · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 7, 2018
- [AD 2017-20-09](https://openairdocs.org/ad/2017-20-09): Turbine Engine Bypass Section · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Nov 13, 2017
- [AD 2017-17-18](https://openairdocs.org/ad/2017-17-18): Turbine Engine Compressor Section · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective Oct 6, 2017
- [AD 2013-06-06](https://openairdocs.org/ad/2013-06-06): Operability bleed valves (OBV) · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 10 more. Effective May 8, 2013
- [AD 2009-24-06](https://openairdocs.org/ad/2009-24-06): Full authority digital electronic controls · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Dec 28, 2009
- [AD 2008-05-01](https://openairdocs.org/ad/2008-05-01): Fuel metering units (FMU) · General Electric CF34-10E2A1, CF34-10E5, CF34-10E5A1 and 8 more. Effective Apr 3, 2008
- [AD 2005-07-09](https://openairdocs.org/ad/2005-07-09): Master variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Apr 20, 2005

Historical (superseded or no longer in force):

- [AD 2008-16-01](https://openairdocs.org/ad/2008-16-01) (historical): Full authority digital engine controls (FADECs) · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Aug 15, 2008
- [AD 2004-04-04](https://openairdocs.org/ad/2004-04-04) (historical): Master Variable geometry (VG) actuators · General Electric CF34-8E2, CF34-8E2A1, CF34-8E5 and 4 more. Effective Mar 9, 2004

## Registered aircraft

None registered with this engine model now.

## NTSB investigations

None matched to aircraft with this engine model.

## FAA accident and incident reports

None matched to aircraft with this engine model.

## Service difficulty reports (194, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR CA190809017](https://openairdocs.org/sdr/CA190809017), Jun 11, 2019: BUSHING. WORN. (CAN) FLIGHT CREW ADVISED MTCE THE THE #1 ENGINE WAS PERSISTENTLY APPROACHING (BUT NOT EXCEEDING) ITT LIMITS DURING STARTS. MOC REQUESTED AN INSPECTION OF THE V
- [SDR CA190604019](https://openairdocs.org/sdr/CA190604019), May 30, 2019: PCU. CORRODED. (CAN) SPOILER FAULT EICAS MESSAGE AFTER TOUCH DOWN ,FLIGHT CONTROL NO DISPATCH MESSAGE FOLLOWED SHORTLY AFTER . AIRCRAFT OUT OF SERVICE, AOG. WAS TOWED TO HANGA
- [SDR CA190502003](https://openairdocs.org/sdr/CA190502003), Apr 22, 2019: ROD. BROKEN. (CAN) DURING SERVICE CHECK, LEFT WING INB FLAP WAS FOUND LOWER THAN OTHER FLAP. INB AFT FLAP OUTB ROD WAS FOUND SHORTER THAN THE INB ROD. ROD WAS FOUND BROKEN I
- [SDR CA190304017](https://openairdocs.org/sdr/CA190304017), Mar 1, 2019: DUCT. FAILED. (CAN) #1 ENGINE PRE-COOLER INLET DUCT ASSY PART NUMBER 171-03352-405 FOUND CRACKED AND BLOWN OUT DURING A SCHEDULED INSPECTION. COMPOSITE PANEL FOUND BRITTLE DU
- [SDR CA160215001](https://openairdocs.org/sdr/CA160215001), Feb 14, 2016: BRACKET. OUT OF ALIGNMENT. (CAN) DURING CLIMB OUT THE "DOOR UNLOCKED" LIGHT ILLUMINATED AT 1500 AGL. RETURN TO BASE AND UNEVENTFUL LANDING COMPLETED. DOOR UNLOCK ANNUNCIATION EXTINGUISHED
- [SDR CA160205010](https://openairdocs.org/sdr/CA160205010), Feb 3, 2016: LINE. LEAKING. (CAN) AFTER ENGINE SHUTDOWN CREW REPORTED THAT NR 2 ENGINE OIL QUANTITY READS 4.1. THE CREW CARRIED OUT A WALK AROUND FOUND A PUDDLE OF OIL UNDER NR 2 ENGINE. M
- [SDR CA151203005](https://openairdocs.org/sdr/CA151203005), Nov 28, 2015: WIRE HARNESS. DAMAGED. (CAN) ON CLIMB OUT AT APPROXIMATELY 15000 FEET THE ENGINE NR 1 FIRE EICAS MESSAGE CAME ON ALONG WITH THE ALARM. #1 ENGINE SET TO IDLE AND MAYDAY DECLARED. CHECK
- [SDR CA150731006](https://openairdocs.org/sdr/CA150731006), Jul 31, 2015: BRAKE. FAILED. (CAN) DISPATCH REPORTED A FLIGHT INCIDENT THAT ON LANDING THE RT OUTBOARD BRAKE SHATTERED. ON TAXI IN TO GATE THE RT INBOARD BRAKE OVERHEATED. MAINTENANCE FOUND
- [SDR CA150703007](https://openairdocs.org/sdr/CA150703007), Jul 2, 2015: WIRE. SHORTED. (CAN) PILOT REPORTED THAT FUEL 2 LOW LEVEL - EICAS WARNING MESSAGE CAME ON. MEL 28-44-00 APPLIED ALLOWED THE AIRCRAFT TO RETURN TO SERVICE PROVIDED THAT ASSOCIA
- [SDR CA150616008](https://openairdocs.org/sdr/CA150616008), Jun 11, 2015: INSULATION. UNSECURE. (CAN) AFTER B CHECK, DURING A FLIGHT, THERE WAS A PRESS AUTO FAULT MSG. THIS WAS RESET IAW THE FAULT ISOLATION MANUAL. DURING A FLIGHT THERE WAS ANOTHER PRESS A
- [SDR CA150312004](https://openairdocs.org/sdr/CA150312004), Mar 10, 2015: STOP. CRACKED. (CAN) WHILE DOING SCHEDULED INSPECTION TASKS ON "B" CHECK, A CRACK WAS FOUND IN THE RT AILERON UPPER TORQUE TUBE BEARING STOP. REPLACED WITH A NEW ONE.
- [SDR CA150209008](https://openairdocs.org/sdr/CA150209008), Jan 22, 2015: WIRE HARNESS. FAILED. (CAN) THE LANDING GEAR WOULD NOT RETRACT. CREW USED THE DOWNLOCK RELEASE BUTTON TO RETRACT THE GEAR AND THEN RETURNED FOR MAINTENANCE TO TROUBLESHOOT. THE FAULT
- [SDR CA150207002](https://openairdocs.org/sdr/CA150207002), Jan 11, 2015: BEARING. DAMAGED. (CAN) CREW REPORTED AILERONS STIFF. UPON FURTHER INSPECTION, MAINTENANCE FOUND UPPER BEARING REF IPC 27-11-07-06 ON LH FUSELAGE SECTOR TORQUE TUBE BEARING ASSY 
- [SDR CA141007006](https://openairdocs.org/sdr/CA141007006), Sep 29, 2014: RELAY. BURNED. (CAN) 1 COFFEMAKER IN THE FWD GALLEY HAD ELECTRICAL FLASHES AND ARCING EMANATING FOR THE RELAY AT THE BACK OF THE UNIT. A CLOUD OF BLACK SMOKE AND A BIG BLUE/YE
- [SDR CA140916004](https://openairdocs.org/sdr/CA140916004), Sep 11, 2014: CONNECTOR. BROKEN. (CAN) THIS AIRCRAFT HAS HAD NUMEROUS REPORTS OF WING ANTI-ICE LEAK FROM THE LTSLAT 2 SENSOR CAUSING MANY OPERATIONAL INTERRUPTIONS AND DELAYS. ALL THE RECOMMEND
- [SDR CA140710004](https://openairdocs.org/sdr/CA140710004), Jul 1, 2014: LINE. CHAFED. (CAN) FLIGHT CREW REPORTED NR 1 HYDRAULIC SYSTEM FLUID QUANTITY DEPLETING IN FLIGHT. AN EMERGENCY WAS DECLARED AND AIRCRAFT HAD AN UNEVENTFULL LANDING. POST LAN
- [SDR CA140508002](https://openairdocs.org/sdr/CA140508002), May 3, 2014: SENSOR. FAILED. (CAN) A "SLAT FAIL" EICAS MESSAGE ON THE GROUND. ON THE 3RD A LT WING OTBD SLAT SKEW SENSOR WAS REPLACED. ALSO, RIGGING CHECKS WERE CARRIED OUT AND FAULT CLEARE
- [SDR CA140421006](https://openairdocs.org/sdr/CA140421006), Apr 16, 2014: PUMP. DAMAGED. (CAN) FUEL 2 LO LEVEL WARNING EICAS MESSAGE WITTH LOTS OF FUEL IN TANK. EJECTOR ENGINE FEED PUMP REMOVED TO INSPECT FOR DEFECTS. CLAMP FLANGE ON FORWARD SIDE FO
- [SDR CA140423001](https://openairdocs.org/sdr/CA140423001), Apr 16, 2014: WIRE HARNESS. CHAFED. (CAN) A "LANDING GEAR NO DISPATCH" MESSAGE WAS DISPLAYED. IT HAD OCCURRED EARLIER THAT DAY BUT WAS RESETTABLE IAW THE FIM 32-00-00-810-801-A. ANOTHER RESET WAS 
- [SDR CA140421003](https://openairdocs.org/sdr/CA140421003), Apr 14, 2014: DUCT. CRACKED. (CAN) AFTER T/O BLEED 2 OVERPRESS AMBER EICAS ALERT. CHECKLIST PROCEDURE CARRIED OUT WITH NO RELIEF. EMERGENCY DECLARED AND ACFT RETURNED TO DEPARTURE IAW CHECK
- [SDR CA140421005](https://openairdocs.org/sdr/CA140421005), Apr 12, 2014: DUCT. CRACKED. (CAN) RT ENGINE T-DUCT FOUND CRACKED, PN 170-14806-401, MECHANIC ON RAMP NOTED SOUND OF BLEED AIR LEAK DURING REGULAR SCHEDULED ENGINE OIL SERVICE CHECK. RT ENG
- [SDR CA140331008](https://openairdocs.org/sdr/CA140331008), Mar 18, 2014: SENSOR. FAILED. (CAN) DURING CRUISE A "SLAT FAIL" FAILURE WARNING OCCURRED. BECAUSE OF THE ABNORMAL LANDING CONFIGURATION, SLATS UP, AN EMERGENCY WAS DECLARED. AIRCRAFT LANDED 
- [SDR CA140227002](https://openairdocs.org/sdr/CA140227002), Feb 24, 2014: ATTACH FITTING. BROKEN. (CAN) RUDDER LOWER ATTACHMENT FITTING BROKEN, DISCOVERED DURING ROUTINE INSPECTION. CAUSE OF DAMAGE UNKNOWN AT THIS TIME.
- [SDR CA140225009](https://openairdocs.org/sdr/CA140225009), Feb 21, 2014: SENSOR. FAILED. (CAN) AFTER TAKEOFF THE LANDING GEAR LEVER WOULD NOT GO UP. RETURNED FOR LANDING. CONTRACT MAINTENANCE DISCOVERED A FAULTY NLG WOW SENSOR. THIS WAS REPLACED AND
- [SDR CA140128011](https://openairdocs.org/sdr/CA140128011), Jan 24, 2014: SENSOR. FAILED. (CAN) AFTER T/O DEPARTING, THE LANDING GEAR COULD NOT BE SELECTED UP. CREW PERFORMED THE CHECKLIST AND RETURNED. MOC WAS CONTACTED AND A SPECIAL FERRY PERMIT WA
- [SDR CA140121002](https://openairdocs.org/sdr/CA140121002), Jan 15, 2014: LANDING GEAR. LACK OF LUBE. (CAN) AFTER T/O THE LT MLG WOULD NOT RETRACT. THE ACFT RETURNED. MAINTENANCE FOUND THE MID PIVOT POINT OF THE SIDE BRACE STIFF AND NEEDING LUBRICATION. AFTER LU
- [SDR CA131231001](https://openairdocs.org/sdr/CA131231001), Dec 26, 2013: LANDING GEAR. FROZEN. (CAN) INSTANCES OF LANDING GEAR DISAGREE LIGHTS AFTER TAKEOFF ON 17TH, 25TH AND 26TH OF DECEMBER 2013. ON THE 17TH A LOT OF ICING ACCUMULATION WAS FOUND, CLEANE
- [SDR CA131001005](https://openairdocs.org/sdr/CA131001005), Sep 20, 2013: WIRE. CHAFED. (CAN) SMOKE ODOR IN CABIN IN INITIAL CRUISE. ACFT DIVERTED FOR INVESTIGATION. POWER CONTROL BOARD FOUND BURNED. AFFECTED SEAT AND OTHERS, AS A PRECAUTION, PUT O
- [SDR CA130805018](https://openairdocs.org/sdr/CA130805018), Aug 3, 2013: MODULE. FAILED. (CAN) MAYDAY DECLARED FOR A MAU 1 FAULT. MAYDAY DECLARED. MAU 1 POWER, MOD 1 REPLACED IAW AMM 31-41-02 PB401. MAU 1 NIC-PROCESSOR 1 REPLACED IAW AMM 31-41-04, P
- [SDR CA131125014](https://openairdocs.org/sdr/CA131125014), Jul 14, 2013: TORQUE TUBE. CHAFED. (CAN) RUDDER PEDAL TORQUE TUBE GOUGED FROM PANEL COVER. TORQUE TUBE REPLACED, COVER PANELS REWORKED OR VERIFIED CLEARANCE.
- [SDR CA130625005](https://openairdocs.org/sdr/CA130625005), Jun 24, 2013: PANEL. OUT OF POSITION. (CAN) DURING PRIMARY INSPECTION, IT WAS NOTED THAT PANEL 221 EZ WAS CHAFING AGAINST THE PILOTS RT RUDDER PEDAL TORQUE TUBE.
- [SDR CA130524007](https://openairdocs.org/sdr/CA130524007), May 14, 2013: MODULE. OVERHEATED. (CAN) ON ARRIVAL , APU WAS IN OPERATION WHEN CREW SELECTED APU GENERATOR AND BLEED THERE WAS A BURNING ELECTRICAL SMELL, GPU WAS HOOKED UP BUT FAILED SHORTLY TH
- [SDR CA130411001](https://openairdocs.org/sdr/CA130411001), Apr 10, 2013: SHROUD. CORRODED. (CAN) AFTER FINDING CORROSION ON 2 OTHER AIRCRAFT. THE FUEL SHROUDS AND FUEL LINES WERE REMOVED FORM THIS ACFT, CURRENTLY BEING PARTED OUT, TO SERVICE THE FIRST
- [SDR CA130409002](https://openairdocs.org/sdr/CA130409002), Apr 6, 2013: FLAP SYSTEM. FAILED. (CAN) ON APPROACH THE CREW REPORTED THE FLAPS HAD FAILED. AN EMERGENCY WAS DECLARED AND THE FLIGHT LANDED WITHOUT FURTHER COMPLICATIONS. BY CMC FAULT CODE - 275
- [SDR CA130318018](https://openairdocs.org/sdr/CA130318018), Mar 16, 2013: ACTUATOR. LEAKING. (CAN) OVERWEIGHT LANDING DUE TO AIRBORNE RETURN ACCOUNT OF STRONG IRRITATING DIRTY SOCK ODOR EMANATING THROUGHOUT CABIN/FLIGHT DECK. SEQUENCED PACKS, UNABLE TO 
- [SDR CA130204001](https://openairdocs.org/sdr/CA130204001), Feb 1, 2013: DUCT. PUNCTURED. (CAN) UNABLE TO PRESSURIZE AIRCRAFT. RETURNING TO DEPARTURE. NO EMERGENCY DECLARED BY CREW. CABIN ALT HI EICAS WARNING MESSAGE ON WHILE CLIMBING THROUGH FL250, 
- [SDR CA130129005](https://openairdocs.org/sdr/CA130129005), Jan 29, 2013: GASKET. LEAKING. (CAN) WHEN FLIGHT WAS ENROUTE, ACFT EXPERIENCED A NR 1 BLEED FAILURE FOLLOWED BY NR 1 BLEED LEAK MESSAGE. WITH THUNDERSHOWERS FORECAST, THE CREW ELECTED TO RETU
- [SDR CA130114009](https://openairdocs.org/sdr/CA130114009), Jan 8, 2013: FILTER. FAILED. (CAN) THE FLIGHT CREW ENCOUNTERED FUMES IN THE COCKPIT AFTER TAKEOFF. THERE WAS ALSO A POSSIBLE HAZE ASSOCIATED. THERE WERE SIMILAR FUMES REPORTED IN THE FWD & 
- [SDR CA121217004](https://openairdocs.org/sdr/CA121217004), Dec 15, 2012: CONTROL VALVE. FAILED. (CAN) ENCOUNTERED HOT BRAKES AT THE THRESHOLD OF R23 WARNING AMBER, REQUESTED TO BE TOWED TO GATE. REPLACED INBD MAIN BRAKE CONTROL VALVE IAW AMM 32-41-09 PB 40
- [SDR CA121211015](https://openairdocs.org/sdr/CA121211015), Nov 28, 2012: FITTING. COLLAPSED. (CAN) BOTH LT AND RT PYLON TORQUE MOTOR CONTROLLER FITTING AIR FILTERS HAVE COLLAPSED. ACFT WAS DUE FOR N1 VISIT, AND TASK CARD 37-36-11-06-001AC-01 CALLED FOR 
- [SDR CA121128001](https://openairdocs.org/sdr/CA121128001), Nov 25, 2012: ENGINE. POWER LOSS. (CAN) ENGINE SHUTDOWN AFTER T/O, RETURNED TO DEPARTURE. NR 2 ENGINE SUFFERED AN IFSD SHORTLY AFTER TAKEOFF. AT THE TIME, THE THROTTLES WERE AT HIGH POWER SETTIN
- [SDR CA121009006](https://openairdocs.org/sdr/CA121009006), Oct 8, 2012: FLAP SYSTEM. FAILED. (CAN) ON, SHORT FINAL, THE FLIGHT CREW RECEIVED A FLAP DISAGREE MESSAGE. A GO-AROUND WAS INITIATED. DURING THE SECOND APPROACH, NO MESSAGES WERE RECEIVED AND TH
- [SDR CA121009005](https://openairdocs.org/sdr/CA121009005), Oct 7, 2012: TRANSPONDER. FAILED. (CAN) AFTER TAKEOFF THE CREW WAS ADVISED BY ATC THEY WERE NOT RECEIVING TRANSPONDER INFO FROM THE FLIGHT. THE FLIGHT RETURNED AND LANDED NORMALLY. THE CREW DID 
- [SDR CA121009002](https://openairdocs.org/sdr/CA121009002), Oct 6, 2012: DUCT. CRACKED. (CAN) FOUND DURING SCHEDULED MAINTENANCE, T-DUCT BELOW PRE-COOLER ON RT PYLON SIDE IS CRACKED. IPC ATTACHED, PN 170-14806-401.
- [SDR CA120921003](https://openairdocs.org/sdr/CA120921003), Sep 20, 2012: SHUTOFF VALVE. FAILED. (CAN) ON DEPARTURE PASSING 14,000 FT THE SERVICE DIRECTOR REPORTED AN ODOR RESEMBLING DIRTY SOCKS THROUGHOUT THE CABIN. THE FLIGHT CREW SWITCHED OFF THE NR 1 PA
- [SDR CA120914006](https://openairdocs.org/sdr/CA120914006), Sep 13, 2012: INDICATOR. MALFUNCTIONED. (CAN) DEPARTING ON THE TAKE OF ROLL, THE FLIGHT EXPERIENCED AN EGT EXCEEDENCE ON THE NR 1 ENGINE AT 110 KNOTS FOLLOWED BY A REJECTED TAKEOFF AT 120 KNOTS. THE A
- [SDR CA120911004](https://openairdocs.org/sdr/CA120911004), Sep 8, 2012: FLAP SYSTEM. FAILED. (CAN) DURING THE APPROACH, IN SHORT FINAL WHEN SELECTING FULL FLAPS FROM FLAPS 3 CONFIGURATION THE CREW RECEIVED A FLAPS FAIL INDICATION. THEY EXECUTED A GO- AR
- [SDR CA120904009](https://openairdocs.org/sdr/CA120904009), Aug 30, 2012: SENSOR. FAILED. (CAN) ON DEPARTURE, ACFT YAWED TO THE LT, NUMBER 1 SIDE, CREW ELECTED TO LEAVE GEAR DOWN AS THEY THOUGHT POSSIBLE BLOWN TIRE. ATC HAD THEM CLIMB TO 7000FT, AT T
- [SDR CA120828007](https://openairdocs.org/sdr/CA120828007), Aug 27, 2012: CIRCUIT CARD. FAILED. (CAN) AIRCRAFT WAS OSCILLATING WHILE THE AUTOPILOT WAS ENGAGED AT APPROXIMATELY 10000 FT, AUTOPILOT WAS DISENGAGED, THE OSCILLATING WENT AWAY FLT RETURNED. THE 
- [SDR CA120828008](https://openairdocs.org/sdr/CA120828008), Aug 26, 2012: OIL SYSTEM. LOW PRESSURE. (CAN) ENGINE 2 LOW OIL PRESSURE, ENGINE 2 SHUTDOWN, DIVERTED, EMERGENCY DECLARED.

All 194: https://openairdocs.org/engine/ge-cf34-8e5a1/reports.md

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