# GE CF34-8C1

- Type: Engine model (FAA registry)
- Registry code: 30049
- Manufacturer (registry): GE
- Model: CF34-8C1
- Engine type: Turbo-fan
- Power: 13,790 lb thrust
- Data sheet: [TCDS E00063EN](https://openairdocs.org/tcds/E00063EN) (OpenAirDocs)
- Holder: General Electric Company GE Aerospace
- Installed in: 1 registered aircraft
- Page: https://openairdocs.org/engine/ge-cf34-8c1

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 2021-23-51](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 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 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 2005-07-06](https://openairdocs.org/ad/2005-07-06): Master variable geometry (VG) actuators · General Electric CF34-8C1 and CF34-8C5. Effective Apr 15, 2005
- [AD 2003-09-14](https://openairdocs.org/ad/2003-09-14): Combustion chamber assemblies · General Electric CF34-8C1. Effective Jun 12, 2003
- [AD 2002-23-02](https://openairdocs.org/ad/2002-23-02): Airworthiness Limitations Section (ALS) - Critical Life-Limited Parts · General Electric CF34-8C1. Effective Dec 26, 2002

Historical (superseded or no longer in force):

- [AD 2019-22-05](https://openairdocs.org/ad/2019-22-05) (historical): Compressor bleed governor · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 3 more. Effective Dec 23, 2019
- [AD 2017-23-06](https://openairdocs.org/ad/2017-23-06) (historical): Compressor bleed governor · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 1 more. Effective Nov 30, 2017
- [AD 2003-26-05](https://openairdocs.org/ad/2003-26-05) (historical): Master Variable Geometry (VG) Actuators · General Electric CF34-8C1, CF34-8C5, CF34-8C5A1 and 3 more. Effective Jan 20, 2004

## Registered aircraft (1)

- [N804X](https://openairdocs.org/aircraft/N804X): [Northrop Grumman Systems Corp](https://openairdocs.org/faa-owner/NORTHROP%20GRUMMAN%20SYSTEMS%20CORP), [El Segundo, CA](https://openairdocs.org/faa-place/CA/El%20Segundo), built 1999, S/N 10002

## 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 (1,415, newest 50)

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

- [SDR N6WA2026082104](https://openairdocs.org/sdr/N6WA2026082104), Aug 19, 2026: SENSOR. FAULTED. LEFT ENG HIGH OIL TEMP 164C IN FLIGHT. VARIABLE WITH THROTTLE. AFTER SHUT DOWN RIGHT ENGINE 81C AND LEFT 145C. (RETURN FROM FLIGHT). REMOVED AND INSTALLED LEFT 
- [SDR N6WA2026073001](https://openairdocs.org/sdr/N6WA2026073001), Jul 30, 2026: ENGINE. DEGRADED. LEFT ENG DEGRADED CAUTION, ITT SPIKED, THRUST REDUCED ON LEFT ENGINE. REMOVED AND REPLACED LT ENG IAW AMM 71-00-00 ALL LEAK & OPS CHKD GOOD.
- [SDR N6WA2026070206](https://openairdocs.org/sdr/N6WA2026070206), Jun 30, 2026: WARNING MESSAGE. ILLUMINATED. L FADEC CAU MSG IN FLIGHT. REMOVED AND REPLACED LT FADEC IAW AMM 73-21-01, PERFORMED OPS CHECK GOOD, NO DEFECTS AT THIS TIME.
- [SDR N6WA2026041603](https://openairdocs.org/sdr/N6WA2026041603), Apr 14, 2026: ENGINE. INDICATION. HIGH ITT ON LEFT ENG @ 89.9 N1. (PEAK TEMP 968 C). PERFORMED COMP WASH OF LEFT ENGINE IAW SP-44. REQUIRES POWER RUN TO COMPLETE. SEE LOG PAGE 635974 ITEM 2.
- [SDR VNAA2026021412201](https://openairdocs.org/sdr/VNAA2026021412201), Feb 12, 2026: PIN. DAMAGED. LEFT ENG VIBRATION, 1.8 AT 87 N1, FL 330. RAN QRH VIBRATION INCREASED 2.1 DIVERTED TO ATL. REMOVED AND REPLACED THE FAN BLADE PINS IAW AMM 72-21-02-400-801-A01-
- [SDR REXA2025123001057](https://openairdocs.org/sdr/REXA2025123001057), Dec 22, 2025: FADEC. FAULTED. LOST RT ENGINE CLIMBING THRU 7,000FT HEARD A BANG AND LOST RT ENG GAUGES. INSPECTED INLET AND AFT CORE COWL IAW MOD NO DEFECTS OR DAMAGE NOTED AT THIS TIME IAW 
- [SDR VNAA2025121811101](https://openairdocs.org/sdr/VNAA2025121811101), Dec 17, 2025: SHUTOFF VALVE. FAULTED. L ENG BLEED MSG IN FLIGHT ALSO THIS CAUSE A L COWL A/I MSG. / REMOVED AND REPLACED LH ENG HPSOV IAW AMM 36-12-05-000/400-801-A01. PERFORMED LH ENG HPSOV LEAK AN
- [SDR SWIA2025121800017](https://openairdocs.org/sdr/SWIA2025121800017), Dec 17, 2025: WARNING MESSAGE. ILLUMINATED. RIGHT ENGINE OIL PRESSURE WARNING MESSAGE IN FLIGHT. LEAD TO LOSS OF ENGINE INFLIGHT HAD TO RETURN TO TUS SINGLE ENGINE LANDING. (FLIGHT 6088) OPEN.
- [SDR VNAA2025120811101](https://openairdocs.org/sdr/VNAA2025120811101), Dec 6, 2025: WARNING MESSAGE. FALSE ACTIVATION. ANTI-ICE DUCT WARNING MSG. COMPLIED WITH QRH SUCCESSFULLY. INTERROGATED THE MDC PER AMM 45-45-00-970-804 FOR MAINTENANCE FAULT HISTORY AND FOUND B1-039268 & B1-
- [SDR REXA2025092300871](https://openairdocs.org/sdr/REXA2025092300871), Sep 18, 2025: FADEC. INOPERATIVE. AT FL 310 AND WE WERE TOLD TO DESCEND DOWN TO 11,00. WE HAD A R ENGINE FLAME OUT AND LOST OUT R ENGINE, R FADEC FAULT AND L FADEC FAULT STATUS MESSAGE CAME ON. 
- [SDR VNAA20250127004](https://openairdocs.org/sdr/VNAA20250127004), Dec 4, 2024: BRACKET. CRACKED. AIR WATER SPRAYER SYSTEM BRACKET RAM AIR WATER SPRAYER SYSTEM BRACKET WAS REPAIRED PER EA 23-C7-21-0435 REV.IR SECTION III - PERMANENT REPAIR AND PER PER REO 67
- [SDR SWIA2024120301319](https://openairdocs.org/sdr/SWIA2024120301319), Dec 2, 2024: ENGINE. VIBRATION. AFTER TAKEEOFF ENGINE 1 VIBRATION WAS AT 3.9 COMPLIED WITH QRHDECENDED AS REQUIRED. WHEN REACHED 12K FEET IDLE POWER, VIBES RETURN TO THE NORMAL RANGE. DECLARED
- [SDR SWIA2024112700019](https://openairdocs.org/sdr/SWIA2024112700019), Nov 19, 2024: VALVE. SMOKE. SOON AFTER TAKEOFF BOTH FLIGHT ATTENDANTS REPORTED SMELLING SMOKE AND A HAZE IN THE CABIN. NO MESSAGED APPEARED ON EICAS. JUST PRIOR TO LANDING BACK IN ICT THE 
- [SDR SWIA2024052000328](https://openairdocs.org/sdr/SWIA2024052000328), Mar 28, 2024: BRACKET. CRACKED. RH ENG NACELLE TRAN COWL OB LOWER A BRACKET CRACKED (C-CHECK RO 5/20/2024) REMOVED AND REPLACE NEW STANDOFF P/N CN624-2082-29 AT RH NACELLE TRAN COWL OB LOWER I
- [SDR VNAA202301051111](https://openairdocs.org/sdr/VNAA202301051111), Dec 27, 2022: BLEED VALVE. FAULTED. LEFT ENGINE SURGE CLOSED CAUTION MSG IN FLIGHT. REMOVED AND REPLACED OPERABILITY BLEED VALVE IAW CRJ700 AMM 75-31-01-000/400-801-A01.
- [SDR VNAA202208181111](https://openairdocs.org/sdr/VNAA202208181111), Aug 16, 2022: NONE. NONE. ABNORMAL RH ENG VIBE UP TO 2.6 BAD VIBE RESONATING THRU AIRFRAME AND RATTLING SEATS, WAS ABLE TO REDUCE VIBE TO NORMAL ONLY AT IDLE. NO ABNORMAL N1, ITT OR OIL 
- [SDR SWIA202265898](https://openairdocs.org/sdr/SWIA202265898), Apr 26, 2022: NONE. CRACKED. LH LOWER TRANSCOWL O/B STAND-OFF APPEARS CRACKED. (C-CHECK RO 6/6/2022) REPLACED LH LOWER TRASNCOWL OB STAND OFF REF CRJ700 SRM 51-42-14-001-001-A01 AND DWG CN6
- [SDR SWIA202265899](https://openairdocs.org/sdr/SWIA202265899), Apr 26, 2022: NONE. DEPARTED. RH UPPER TRANSCOWL Z ANGLE 1 MISSING FASTENER HEAD AND APPEARS DISBONDED. (C-CHECK RO 6/6/2022) COMPLIED WITH ALL STEPS 1 THRU 25 OF MHIRJ REO 670-54-21-1536 RE
- [SDR SWIA202265163](https://openairdocs.org/sdr/SWIA202265163), Mar 25, 2022: NONE. CRACKED. DURING A4 INSPECTION OF THE LH ENGINE INLET, FOUND 2 DENTS WITH CRACKS AT THE 3 AND 5 O' CLOCK POSITIONS, BOTH ARE OUT OF LIMITS. (FILED - CLOSED) REMOVED AND R
- [SDR SWIA202264950](https://openairdocs.org/sdr/SWIA202264950), Feb 7, 2022: NONE. CRACKED. REPLACEMENT TRANSCOWL ASSY PN: KCN624-2003-4 FOR JOB 710194111 OP338 RECEIVED WITH A CRACKED A-BRACKET (STAND-OFF ANGLE PN: CN624-2082-201) ON INBOARD SIDE THAT
- [SDR VNAA202202071111](https://openairdocs.org/sdr/VNAA202202071111), Feb 3, 2022: CABLE. FAULT MESSAGE. EMERGENCY DUE TO AN ENGINE WARNING LIGHT FOLLOWED BY A KNOCKING NOISE IN THE ENGINE. AIRCRAFT REQUESTED TO RETURN TO CLT AND LANDED WITHOUT INCIDENT. RTF - L FA
- [SDR SWIA202264942](https://openairdocs.org/sdr/SWIA202264942), Feb 3, 2022: NONE. CRACKED. LH UPPER TRANSCOWL IB STAND-OFF CRACKED. (C-CHECK RO 3/11/2022) ON L/H UPPER TRANSCOWL, ORDERED & RECEIVED NEW STAND- OFF ANGLE P/N CN624-2082-201. REMOVED CRAC
- [SDR SWIA202264943](https://openairdocs.org/sdr/SWIA202264943), Feb 3, 2022: NONE. CRACKED. RH LOWER TRANSCOWL Z ANGLE MISSING FASTENERS & DISBONDED FROM INNER PERFORATE. (C-CHECK RO 3/11/2022) PERMENANTLY REPAIRED R/H LWR TRANSCOWL INNER SKIN CRACK RE
- [SDR SWIA202264945](https://openairdocs.org/sdr/SWIA202264945), Feb 3, 2022: NONE. WORN. RH LOWER TRANSCOWL BEARING PADS, FWD PAD IS WORN, AFT PAD IS MISSING (C-CHECK RO 3/11/2022) REMOVED AND INSTALLED NEW BEARING PAD INTO R/H LOWER TRANSCOWL (PN C
- [SDR SWIA202264725](https://openairdocs.org/sdr/SWIA202264725), Jan 29, 2022: NONE. CHAFED. ON R/H UPPER TRANSCOWL, INNER COAMING HAS CHAFE DAMAGE AT FWD EDGE. (C CHECK RO 02/25/2022) ON R/H UPPER TRANSCOWL, REPAIRED CHAFE DAMAGE ON INNER COAMING AT FW
- [SDR SWIA202264646](https://openairdocs.org/sdr/SWIA202264646), Jan 24, 2022: NONE. CHAFED. RH LOWER TRANSCOWL LATCH DOOR COAMING CHAFED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED RH LOWER TRANSCOWL LATCH DOOR COAMING P/N CN624-2060-207. REF. AND CO
- [SDR SWIA202264719](https://openairdocs.org/sdr/SWIA202264719), Jan 19, 2022: NONE. CRACKED. LH LOWER TRANSCOWL OUTER SKIN CRACKED FROM FWD LATCH CUTOUT AFT TOWARDS THE LATCH DOOR CUTOUT. (C CHECK RO 02/25/2022) L/H LOWER TRANSCOWL OUTER SKIN CRACK @ FW
- [SDR SWIA202264720](https://openairdocs.org/sdr/SWIA202264720), Jan 19, 2022: NONE. MISSING. RH UPPER TRANSCOWL Z ANGLE MISSING FASTENERS & DISBONDED FROM INNER PERFORATE. (C CHECK RO 02/25/2022) REPAIRED R/H UPPER TRANSCOWL Z ANGLE REF MHIRJ REO 670-54
- [SDR SWIA202264721](https://openairdocs.org/sdr/SWIA202264721), Jan 19, 2022: NONE. MISSING. RH LOWER TRANSCOWL I/B STANDOFF MISSING MATERIAL. (C CHECK RO 02/25/2022) REMOVED AND REPLACED RH LOWER TRANSCOWL INBD STANDOFF P/N CN624-2082-201. REF. REO 670
- [SDR SWIA202264638](https://openairdocs.org/sdr/SWIA202264638), Jan 4, 2022: NONE. DAMAGED. RH LOWER TRANSCOWL Z ANGLE MISSING FASTENERS & APPEARS DISBONDED FROM INNER PERFORATE. (C CHECK RO 02/22/2022) REMOVED AND INSTALLED RH LOWER TRANSCOWL Z-ANGLE 
- [SDR SWIA202264639](https://openairdocs.org/sdr/SWIA202264639), Jan 4, 2022: NONE. CRACKED. RH LOWER TRANSCOWL OB STANDOFF CRACKED. (C CHECK RO 02/22/2022) REMOVED AND REPLACED CRACKED STAND OFF P/N CN624-2082-201 ON OUTBD SIDE OF RH LOWER TRANSCOWL. R
- [SDR SWIA202164509](https://openairdocs.org/sdr/SWIA202164509), Dec 24, 2021: NONE. DAMAGED. REMOVE AND REPLACE LATCH DOOR COAMING ON R/H LWR TRANSCOWL (C CHECK RO 2/17/2022) REMOVED DAMAGED LATCH DOOR COAMING & INSTALLED NEW LATCH DOOR COAMING P/N CN62
- [SDR SWIA202164147](https://openairdocs.org/sdr/SWIA202164147), Dec 15, 2021: NONE. CRACKED. LH UPPER TRANSCOWL CRACKED ON INNER SKIN UNDER Z-STIFFENERS FOR LATCH DOOR COAMING (C CHECK RO 02-03-22) PERFORMED REO REPAIR ON LH UPPER TRANSCOWL Z-STIFFENER 
- [SDR SWIA202164146](https://openairdocs.org/sdr/SWIA202164146), Dec 13, 2021: NONE. CHAFED. LH UPPER TRANSCOWL LATCH DOOR COAMING CHAFED AT LATCH DOOR MATING SURFACES NEAR ALIGNMENT PIN OPINING AND ON LEADING EDGE IB SIDE (C CHECK RO 02-03-22) REMOVED 
- [SDR SWIA202164495](https://openairdocs.org/sdr/SWIA202164495), Dec 13, 2021: NONE. CHAFED. LH UPPER TRANSCOWL EXTERNAL SKIN CHAFED AT AFT SIDE OF LATCH DOOR OPINING (C CHECK RO 2/17/2022) REPAIRED CHAFED EXTERNAL SKIN ON AFT SIDE OF LATCH DOOR OPENING
- [SDR SWIA202164496](https://openairdocs.org/sdr/SWIA202164496), Dec 13, 2021: NONE. DAMAGED. RH LOWER TRANSCOWL FWD "Z" STIFFENER HAS SEVERAL SHEARED FASTENERS (C CHECK RO 2/17/2022) REPAIRED R/H LWR TRANSCOWL Z STIFFNER AND INNER SKIN REF MHIRJ REO 670
- [SDR SWIA202164497](https://openairdocs.org/sdr/SWIA202164497), Dec 13, 2021: NONE. DAMAGED. LH UPPER TRANSCOWL HAS 1EA LOSE FASTENER ON Z STIFFENER FOR LATCH DOOR DOMAINING (C CHECK RO 2/17/2022) L/H UPPER TRANSCOWL HAS BEEN REPAIRED REF REO# 670-54-21
- [SDR SWIA202163912](https://openairdocs.org/sdr/SWIA202163912), Dec 8, 2021: NONE. ELONGATED. LH UPPER TRANSCOWL LATCH DOOR SPIGOT HOLE APPEARS ELONGATED. (C CHECK RO 1/18/2022) ELONGATED SPIGOT HOLE ON L/H UPPER TRANSCOWL HAS BEEN REPAIRED REF REO# 670-
- [SDR SWIA202163913](https://openairdocs.org/sdr/SWIA202163913), Dec 8, 2021: NONE. ELONGATED. RH LOWER TRANSCOWL LATCH DOOR SPIGOT HOLE APPEARS ELONGATED. (C CHECK RO 1/18/2022) R/H LOWER TRANSCOWL HAS BEEN REPAIRED REF REO# 670-54-21-1207, REV A, DATED 
- [SDR SWIA202164145](https://openairdocs.org/sdr/SWIA202164145), Dec 8, 2021: NONE. CRACKED. LH LOWER TRANSCOWL FWD LATCH COAMING APPEARS CRACKED FROM FWD LATCH CUTOUT FORWARD TO THE LEADING EDGE. (C CHECK RO 02-03-22) PERFORMED LH LOWER TRANSCOWL FWD L
- [SDR SWIA202164654](https://openairdocs.org/sdr/SWIA202164654), Dec 7, 2021: NONE. GOUGED. * RH ENGINE TRANSCOWL LATCH DOOR ASSY AFT HINGE IS GOUGED (MARKED) (C CHECK RO 02/22/2022) REMOVED AND REPLACED AFT TRANSCOWL LATCH DOOR HINGE IAW CRJ-700-SRM T
- [SDR SWIA202164677](https://openairdocs.org/sdr/SWIA202164677), Dec 7, 2021: NONE. MISINSTALLED. *LEFT ENGINE NACELLE NYLON INSERT IS NOT INSTALLED AT HINGE LINE (C CHECK RO 02/22/2022) REMOVED AND REPLACED WITH NEW LH LOWER INBOARD HINGE BEAM TRANSCOWL SLI
- [SDR SWIA202164461](https://openairdocs.org/sdr/SWIA202164461), Dec 4, 2021: NONE. CRACKED. RH LOWER TRANSCOWL OB STAND-OFF ANGLE (A-BRACKET) CRACKED (C CHECK RO 2/17/2022) REMOVED AND REPLACED RH LWR TRANSCOWL OB STAND OFF A-BRACKET IAW CRJ700 SRM 51-
- [SDR SWIA202163849](https://openairdocs.org/sdr/SWIA202163849), Dec 2, 2021: NONE. WORN. LH UPPER TRANSCOWL LATCH DOOR CHANNELS WORN ( PN CN624-2048-201 AND PN CN624-2049-201) (C CHECK RO 1/16/2022) REMOVED AND INSTALLED NEW CHANNEL P/N CN624-2048-2
- [SDR SWIA202164530](https://openairdocs.org/sdr/SWIA202164530), Dec 2, 2021: NONE. BROKEN. * LH ENGINE LOWER COWL OB NYLON TRACK INSERT HAS END BROKEN OFF (FLAGGED). (C CHECK RO 2/17/2022) REMOVED AND INSTALLED NEW LH ENGINE LOWER OTBD COWL NYLON TRAC
- [SDR SWIA202163229](https://openairdocs.org/sdr/SWIA202163229), Dec 1, 2021: NONE. DAMAGED. R/H ENGINE UPPER TRANSCOWL LATCH (AFT) WORN AT ATTACHMENT PIN. LATCH REMOVED. (C CHECK RO 12-19-21) REMOVED R/H LOWER AFT TRANSCOWL LATCH IN ACCORDANCE TO CRJ70
- [SDR SWIA202163244](https://openairdocs.org/sdr/SWIA202163244), Nov 11, 2021: NONE. WORN. *RH UPPER TRANSCOWL HAS WEAR ON COAMING. AREAS MARKED (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM THE RH UPPER TRANSCOWL, REF CRJ700 SRM 51-42-13-001-001 
- [SDR SWIA202163239](https://openairdocs.org/sdr/SWIA202163239), Nov 10, 2021: NONE. WORN. *LH LOWER TRANSCOWL HAS WEAR ON OTBD LEADING EDGE INNER SKIN (C-CHECK RO 12/26/2021) COMPLIED WITH REO 670-54-21-1485 REV -- DATED 2021-11-30 REPAIR TO LH LOWER
- [SDR SWIA202163240](https://openairdocs.org/sdr/SWIA202163240), Nov 10, 2021: NONE. WORN. *LH LOWER TRANSCOWL HAS WEAR ON COAMING LEADING EDGE (C-CHECK RO 12/26/2021) REMOVED WORN COAMING FROM LH LOWER TRANSCOWL. REF CRJ700 SRM 51-42-13-001-001 A01. 
- [SDR SWIA202163193](https://openairdocs.org/sdr/SWIA202163193), Nov 9, 2021: NONE. LOOSE. LH UPPER TRANSCOWL Z ANGLE RIVETS LOOSE IN INNER PERFORATE. (C CHECK RO 12-19-21) ACCOMPLISHED REPAIR TO INNER PERFORATED SKIN OF LH UPPER TRANSCOWL AND REPLACE

All 1,415: https://openairdocs.org/engine/ge-cf34-8c1/reports.md

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