# Service difficulty reports: N716EV

A list on [N716EV](https://openairdocs.org/aircraft/N716EV.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 6 · 296 reports

- [SDR SWIA2024112501283](https://openairdocs.org/sdr/SWIA2024112501283.md): Windshield · cracked · Nov 24, 2024 · N716EV · Cndair CL6002C10 · Flight Compartment Windows
  > RIGHT SIDE WINDSHIELD SHATTERED IN FLIGHT. (FLIGHT 4943 - FILED CLOSED) PLEASE REFERENCE AML 1479220PILOT MISTAKENLY CONFUSED THE RH WINDOW FOR THE RH WINDSHIELD. RH WINDSHIELD IS FINE AND NOT SHATTERED. NO FURTHER DEFECTS NOTED. A/C OK FOR SVC.
- [SDR SWIA2024080700005](https://openairdocs.org/sdr/SWIA2024080700005.md): Windshield · cracked · Aug 5, 2024 · N716EV · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN SIDE WINDSHIELD CRACKED INFLIGHT (FLIGHT 4914 - FILED CLOSED) COMPLIED WITH TASK CARD 56-220-1000-SKY REMOVAL AND REPLACEMENT OF PILOT WINDSHIELD (LH), OPS CHECK GOOD A THIS TIME NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR SWIA2024080600005](https://openairdocs.org/sdr/SWIA2024080600005.md): Windshield · cracked · Aug 5, 2024 · N716EV · Cndair CL6002C10 · Flight Compartment Windows
  > CAPTAIN SIDE WINDSHIELD CRACKED INFLIGHT (FLIGHT 4914 - FILED OPENTHIS IS CURRENTLY A WORK IN PROGRESS
- [SDR SWIA2024080500603](https://openairdocs.org/sdr/SWIA2024080500603.md): Floorbeam · corroded · Jun 3, 2024 · N716EV · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOORBOARD SILL AS FS569.00 RBL9 HAS SIGNS OF CORROSION AT FASTENER HOLE (C-CHECK RO 7/24/2024) PERFORMED REPAIR ON DAMAGED AREA AT FLOOR BEAM BETWEEN FS569.00 RBL9 IAW REO 670-53-31-889 REV--(P1) DATE: 2024-06-12, 670-53-31-889 REV--(P2) DATE: 2024-06-
- [SDR SWIA2024080500601](https://openairdocs.org/sdr/SWIA2024080500601.md): Support Fitting · chafed · Jun 1, 2024 · N716EV · Cndair CL6002C10 · Aileron Tabs
  > LH OTBD FLAP INBD AFT SUPPORT FITTINIG HAS CHAFFE DAMAGE ON BOTH INBD LUGS WS178.00 (C-CHECK RO 7/24/2024) REMOVED CHAFFE DAMAGE ON L/H O/B FLAP I/B AFT SUPPORT FITTING IAW CRJ 700 SRM 51-11-00 CRJ 700 SRM 51-12-00 CRJ 700 SRM 51-24-11 CRJ 700 SRM 5
- [SDR SWIA202408050024](https://openairdocs.org/sdr/SWIA202408050024.md): Exhaust Cone · cracked · May 24, 2024 · N716EV · Cndair CL6002C10 · Engine Collector/Tailpipe/Nozzle
  > CRACK IN CORNER OF RH AFT CORE COWL EXHAUST NOZZLE ABOUT 1 INCH IN LENGTH (C-CHECK RO 7/24/2024) REPAIRED DAMAGE ON CORNER OF RH AFT CORE COWL EXHAUST NOZZLE IAW CRJ700 SRM 54-13-00, AND REO 670-54-13-1054 REV-- DATE 2024-07-04. AND IAW REO 670-54-13-1
- [SDR SWIA2024080500607](https://openairdocs.org/sdr/SWIA2024080500607.md): Repair · gouged · May 22, 2024 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGE ON EXISTING REPAIR DOUBLER AT FS977 AT STR27 (C-CHECK RO 7/24/2024) REMOVED AND REPLACED EXISTING REPAIR DOUBLER AT FS 977 AT STR27 IAW REO 670-53-00-290 REV-F DATE 2019-04-26 AND SRM 51-23-03. LEAK CHECK GOOD.
- [SDR SWIA2024080500022](https://openairdocs.org/sdr/SWIA2024080500022.md): Web · cracked · May 22, 2024 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR WEB CRACKED IN RH FWD EQUIPMENT COMPARTMENT AT FS200.0 STR11 RH (C-CHECK RO 7/24/2024) REPAIRED DAMAGE AT RH FLOOR WEB FWD EQUIPMENT COMPARTMENT AT FS 200 STR 11 RH IAW CRJ700 AMM 20-70-00, AMM 20-21-00 SRM51-26-01, SRM 51-41-02, SRM 51-42-06,
- [SDR SWIA2024080500018](https://openairdocs.org/sdr/SWIA2024080500018.md): Skin · gouged · May 18, 2024 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > MULTIPLE GOUGES IN THE EXTERNAL FUSELAGE SKIN AT FS1031.0 AND STR22RH JUST AFT OF THE EXTERNAL GROUND AIR SOURCE PANEL GOUGES ARE LOCATED IN ORANGE FLAGGED BOXED AREA (C-CHECK RO 7/24/2024) REPAIRED DAMAGE ON EXTERNAL SKIN AT FS1031.0 AND STR22RH JUST
- [SDR SWIA2023121400002](https://openairdocs.org/sdr/SWIA2023121400002.md): Unknown · damaged · Dec 12, 2023 · N716EV · Cndair CL6002C10 · Flight Compartment Windows
  > REFERENCE CP27547979 FOR DAMAGED FO'S WINDSHIELD, REMOVE FO'S WINDSHIELD. (FILED CLOSED)REMOVED THE FIRST OFFICER'S WINDSHIELD IAW CRJ 700 AMM 56-11-01. REFERENCE ML 27547979 FOR INSTALLATION OF THE FIRST OFFICER'S WINDSHIELD AND PARTS INFORMATION.
- [SDR SWIA2023050900007](https://openairdocs.org/sdr/SWIA2023050900007.md): Unknown · missing · May 7, 2023 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > THE O/B SEAT TRACK AT SEAT 15A IS MISSING. (FILED CLOSED)INSTALLED THE MISSING O/B SEAT TRACK AT SEAT 15A IN REF TO AMM 25-21-02.
- [SDR SWIA202163090](https://openairdocs.org/sdr/SWIA202163090.md): None · popped · Dec 11, 2021 · N716EV · Cndair CL6002C10 · Doors
  > AFT CARGO DOOR CAUTION (FLIGHT 3189 - FILED CLOSED) UPON A/C ARRIVAL, FOUND AFT CARGO DOOR HANDLE POPPED OUT. PERFORMED GVI OF AFT CARGO DOOR AND FOUND NO DEFECTS NOTED AT THIS TIME. PERFORMED OPS CHECK OF AFT CARGO DOOR LATCHING AND INDICATION SEVERAL TI
- [SDR SWIA202055994](https://openairdocs.org/sdr/SWIA202055994.md): Doubler · damaged · Dec 29, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FORWARD VALVE RETAINER DOUBLER P/N KBA670-31630-9SB AT FS280.00 BETWEEN STGR27 AND STGR26R HAS MISLOCATED VALVE HOLE (C-CHECK) RO 2/5/2021 REPAIRED FUSELAGE SKIN BETWEEN FS280.0 - FS333.0 AND STR 26L - STR 26R. REF REO 670-53-21-1914 REV. -- DATED 2021-01-
- [SDR SWIA202055993](https://openairdocs.org/sdr/SWIA202055993.md): Stringer Splice · corroded · Dec 23, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR SPLICE AT STGR 19R F.S. 477.0 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED WITH NEW FROM STOCK STRINGER SPLICE AT 19R AND FS477 PN: SH670-33264-1 REF CRJ700 SRM 51-42-06-001-001-A01, AND DWG SH670-33264 REV NC. COMPLIED WITH SKYWEST TASK CA
- [SDR SWIA202055992](https://openairdocs.org/sdr/SWIA202055992.md): Doubler · damaged · Dec 22, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > (4EA) DOUBLERS HAVE MISLOCATED HOLES (C-CHECK) RO 2/5/2021 FABRICATED 4EA. NEW REPAIR FILLERS REF. MHIRJ REO 670-53-21-1914 REV --(P1) DATED 2020-12-15. LOCATED AND DRILLED DOUBLERS AND INSTALLED REF. MHIRJ REO 670-53-21-1914 REV --(P1) DATED 2020-12-15. R
- [SDR SWIA202055991](https://openairdocs.org/sdr/SWIA202055991.md): Cleat · corroded · Dec 20, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > PAX DOOR CLEAT AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963 IS CORRODED (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR CLEAT AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963. REF: CRJ-700 S.R.M. 51-42-06-001-001-A01. / COMPLIED WITH SKY CARD 51-900-
- [SDR SWIA202055990](https://openairdocs.org/sdr/SWIA202055990.md): Bracket · corroded · Dec 20, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BRACKET AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963 IS CORRODED (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR BRACKET AT DOOR DATUM 5 TRACE BETWEEN FS347.250 AND FS338.963REF:CRJ-700 S.R.M. 51-42-06-001-001-A01 & DWG 601R31702 REV N. PRESSURE
- [SDR SWIA202055989](https://openairdocs.org/sdr/SWIA202055989.md): Intercostal · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DD3 BETWEEN FS 311.75 AND FS 320.16 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR INTERCOSTAL AT DD3 BETWEEN FS 311.75 AND FS 320.16. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTIN
- [SDR SWIA202055988](https://openairdocs.org/sdr/SWIA202055988.md): Cleat · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLEAT AT FS 311.75 AND DD4 IS CORRODED (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 311.75 AND DD4. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWEST TAS
- [SDR SWIA202055987](https://openairdocs.org/sdr/SWIA202055987.md): Cleat · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLEAT AT FS 320.16 AND DD4 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 320.16 AND DD4. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. / COMPLIED WITH SKY CARD
- [SDR SWIA202055986](https://openairdocs.org/sdr/SWIA202055986.md): Cleat · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR CLEAT AT FS 320.16 AND DD6 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR CLEAT AT FS 320.16 AND DD6. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. / COMPLIED WITH SKY CARD
- [SDR SWIA202055985](https://openairdocs.org/sdr/SWIA202055985.md): Bracket · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BRACKET AT FS 311.75 AND DD6 IS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED PAX DOOR BRACKET AT FS 311.75 AND DD6. REF CRJ-700 SRM 51-42-06-001-001-A01, DWG 601R31702 REV N. SEE ATTACHED CONTINUATION CARD FOR DETAILS. COMPLIED WITH SKYWES
- [SDR SWIA202055984](https://openairdocs.org/sdr/SWIA202055984.md): Intercostal · corroded · Dec 19, 2020 · N716EV · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL AT DOOR DATUM 5 TRACE BETWEEN FS 338.96 AND FS 347.25 HAS CORROSION. (C-CHECK) RO 2/5/2021 EVALUATED PAX DOOR INTERCOSTAL AT DATUM 5 RACE BETWEEN FS338.96 AND FS347.25 OUT OF LIMITS. REMOVED AND REPLACED NEW PAX DOOR INTERCOSTAL AT DOO
- [SDR SWIA202055983](https://openairdocs.org/sdr/SWIA202055983.md): Stiffener · damaged · Dec 18, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > LH LWR TRANSCOWL ZED STIFFNER IS HEAVILY CHAFFED AND GOUGED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED LH LWR ZED STIFFNER, REF CRJ 700 SRM 51-40-11-001-001-A01, BOMBARDIER/SHORTS DWG CN624-2038 REV A AND BOMBARDIER REO 670-54-21-1207 REV A DATED 2015-08-
- [SDR SWIA202055982](https://openairdocs.org/sdr/SWIA202055982.md): Door Frame · corroded · Dec 15, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Structure
  > PAX DOOR FWD FORMER FRAME, UNDER PANEL 832FL, IS CORRODED. (C-CHECK) RO 2/5/2021 REPLACED PAX DOOR FWD FORMER FRAME. REF: CRJ 700 SRM 51-42-06-001-001 (A01), 51-42-21-001-001 (A01), AND DWG 601 R31702 REV. N. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA202055981](https://openairdocs.org/sdr/SWIA202055981.md): Skin · cracked · Dec 12, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > LH UPPER TRANSCOWL HAS 1EA CRACKED OUT HOLE UNDER "Z" ANGLE ON INNER SKIN (MARKED). (C-CHECK) RO 2/5/2021 REPAIRED CRAKED OUT HOLE ON INNER SKIN OF LH UPPER TRANSCOWL PER MHIRJ REO 670-54-21-1413 REV -- DATED 2020-12-16, REF CRJ 700 SRM 51-42-13-001-001-A0
- [SDR SWIA202056004](https://openairdocs.org/sdr/SWIA202056004.md): Hinge Fitting · corroded · Dec 11, 2020 · N716EV · Cndair CL6002C10 · Elevator Structure
  > UPON REMOVAL ON JOB 71008485 OP 76 CAMP 21903312, FOUND R/H ELEVATOR L/E HINGE FITTING #3, P/N AV670-24136-001, TO HAVE PITTING CORROSION IN THE BEARING BORE. REPLACE HINGE FITTING ASSY. (C-CHECK) RO 2/5/2021 ELEVATOR ASSY REPLACED, NEW ELEVATOR ASSY HAS
- [SDR SWIA202055980](https://openairdocs.org/sdr/SWIA202055980.md): Coaming · chafed · Dec 11, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > RH ENGINE LWR TRANSCOWLING COAMING HAS EXCESSIVE CHAFFING AT VARIOUS LOCATIONS. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED TRANSCOWL LATCH COAMING P/N CN624-2060-205 AT RH ENGINE LWR TRANSCOWL. REF BOMBARDIER REO 670-54-21-1207 REV A, DATED 2015-0
- [SDR SWIA202055979](https://openairdocs.org/sdr/SWIA202055979.md): Stiffener · gouged · Dec 10, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L/H ENGINE UPPER TRANS COWL, UPON REMOVAL OF Z STIFFNER GOUGE MARKS ON 2 PLACES (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL Z STIFFENER COMMON TO THE COAMING LATCH DOOR PN-CN624-2038-901. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-
- [SDR SWIA202055978](https://openairdocs.org/sdr/SWIA202055978.md): Bearing · chafed · Dec 10, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L/H ENGINE UPPER TRANS COWL PAD BEARING EXCESSIVE CHAFFING. (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL PAD BEARING PN-CN624-2130-201. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A 2015-08-27 / COMPLIED WITH 51-900-1002
- [SDR SWIA202055977](https://openairdocs.org/sdr/SWIA202055977.md): Intercostal · corroded · Dec 10, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AT F.S. 333.00 STGR 21L, POSSIBLE CORROSION ON THE INTERCOSTAL. (C-CHECK) RO 2/5/2021 REPLACED 21L INTERCOSTAL AT FS333.00 WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 DWG SH670-31810 REV Y. COMPLIED WITH 51-900-1002-SKY. PRESSURE CHECK GOOD.
- [SDR SWIA202055976](https://openairdocs.org/sdr/SWIA202055976.md): Stiffener · missing · Dec 5, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L/H ENGINE UPPER TRANS COWL Z STIFFNER COMMON TO THE COAMING LATCH DOOR HAS 2EA MISSING FASTENER (C-CHECK) RO 2/5/2021 INSTALLED NEW L/H ENGINE UPPER TRANS COWL Z STIFFENER COMMON TO THE COAMING LATCH DOOR PN-CN624-2038-901. REF CRJ-700 SRM 51-42-13-001-00
- [SDR SWIA202055975](https://openairdocs.org/sdr/SWIA202055975.md): Doubler · chafed · Dec 5, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > L/H ENGINE UPPER TRANS COWL DOUBLER HAS HEAVY CHAFFE (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW L/H ENGINE UPPER TRANS COWL DOUBLER PN-CN624-2003-997. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A, DATED 2015-08-27. / COMPLIED WITH 5
- [SDR SWIA202055974](https://openairdocs.org/sdr/SWIA202055974.md): Coaming · chafed · Dec 5, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > L/H ENGINE UPPER TRANS COWL LATCH COAMING HAS HEAVY CHAFFE AROUND HOLE LOCKING AREA (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW L/H ENGINE UPPER TRANS COWL LATCH COAMING PN-CN624-2061-905. REF CRJ-700 SRM 51-42-13-001-001-A01, REO 670-54-21-1207 REV A
- [SDR SWIA202056003](https://openairdocs.org/sdr/SWIA202056003.md): Pcu · corroded · Dec 3, 2020 · N716EV · Cndair CL6002C10 · Aileron Control System
  > R/H AILERON INBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB 7118484, OP4, MX TRANS #21851631 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED R/H AILERON INBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. COMPLI
- [SDR SWIA202056002](https://openairdocs.org/sdr/SWIA202056002.md): Control Unit · corroded · Dec 3, 2020 · N716EV · Cndair CL6002C10 · Aileron Control System
  > L/H AILERON INBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB# 71008484, OPERATION 5, MX TRANS #21851614 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED L/H AILERON INBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GO
- [SDR SWIA202055996](https://openairdocs.org/sdr/SWIA202055996.md): Pcu · corroded · Dec 3, 2020 · N716EV · Cndair CL6002C10 · Aileron Control System
  > R/H AILERON OUTBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB 71008484, OP 4, MX TRANS #21851631 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED R/H AILERON OUTBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST GOOD. CO
- [SDR SWIA202055995](https://openairdocs.org/sdr/SWIA202055995.md): Pcu · corroded · Dec 3, 2020 · N716EV · Cndair CL6002C10 · Aileron Control System
  > L/H AILERON OUTBOARD PCU REQUIRES REPLACEMENT DUE TO CORROSION. SEE JOB# 71008484, OPERATION 5, MX TRANS # 21851614 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED L/H AILERON OUTBOARD PCU IAW CRJ-700 AMM 27-14-01-000-801-A01 AND 27-14-01-400-801-A01. OPS TEST
- [SDR SWIA202056001](https://openairdocs.org/sdr/SWIA202056001.md): Fitting · corroded · Dec 2, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD BAGGAGE BAY DOOR SURROUND STRUCTURE, FWD AND AFT LOWER GUIDE FITTINGS HAVE MOUNTING HARDWARE APPEARS CORRODED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED FWD BAGGAGE BAY SURROUND STRUCTURE FWD AND AFT LOWER GUIDE FITTING MOUNTING HARDWARE REF CRJ 7
- [SDR SWIA202055973](https://openairdocs.org/sdr/SWIA202055973.md): Landing · cracked · Nov 30, 2020 · N716EV · Cndair CL6002C10 · Nacelle/Pylon, Main Frame
  > *LEFT ENG LOWER TRANS COWL LATCH DOOR LANDING CRACKED. (MARKED) (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW LATCH COAMING REF BOMBARDIER REO 670-54-21-1207 REV A, DATED 2015-08-27. / COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202055972](https://openairdocs.org/sdr/SWIA202055972.md): Stringer · corroded · Nov 28, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STGR 25R CORRODED AT F.S. 295 TO F.S. 310.00 (MARKED). (C-CHECK) RO 2/5/2021 REPLACED STGR 25R FROM FS280-FS333 WITH NEW REF CRJ-700 SRM 51-42-06-001-001-A01 51-42-21-001-001-A01 AND DWG SH670-31630 REV K. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA202056000](https://openairdocs.org/sdr/SWIA202056000.md): Seat Track · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > *CORROSION ON RH SIE SEAT RAIL BETWEEN FS 565.00 - 661.00. AREAS MARKED. (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED SEAT RAIL R/H BETWEEN FS 565.00 - FS 661.00 REF CRJ700 AMM 53-00-49-000-801-A17 AND 53-00-49-400-801-A17
- [SDR SWIA202055999](https://openairdocs.org/sdr/SWIA202055999.md): Plate · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON FWD CARGO FLOOR MOUNT PLATE AT FS 581.00, OVER STGR 27 (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-4 REF DWG SH670-33376 REV A AND CRJ-700 SRM TASK 51-42-06-001-001-A01 (SOLID RIVETS).
- [SDR SWIA202055998](https://openairdocs.org/sdr/SWIA202055998.md): Plate · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > *CORROSION ON FWD CARGO FLOOR MOUNT PLATE ON STGR 25L, FS 533.00 (C-CHECK) RO 2/5/2021 REMOVED AND INSTALLED NEW FWD CARGO FLOOR MOUNT PLATE SH670-33376-3 REF DWG SH670-33376 REV A AND CRJ-700 SRM TASK 51-42-06-001-001-A01 (SOLID RIVETS).
- [SDR SWIA202055971](https://openairdocs.org/sdr/SWIA202055971.md): Doubler · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Structure
  > *CORROSION ON DRAIN MAST INTERNAL PLATE/DOUBLER BETWEEN FS 1031.00 €“ 1047.00, RH OF STGR 27 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED AFT DRAIN MAST INTERNAL DOUBLER BETWEEN FS1031.00-1047.00 WITH NEW INTERNAL DOUBLER PN MM670-43255-001 IAW CRJ
- [SDR SWIA202055970](https://openairdocs.org/sdr/SWIA202055970.md): Bracket · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 23L €“ 22L, FS 581.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACE BRACKET AT FWD CARGO STGR 23L €“ 22L, FS 581.00 REF CRJ700 SRM 51-42-21-001-001-A01, CRJ700 SRM / 51-42-06-001-001-A01, DWG SH670-
- [SDR SWIA202055969](https://openairdocs.org/sdr/SWIA202055969.md): Bracket · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 27 -26L, FS 581.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED DAMAGED BRACKET AT FWD CARGO FS 581 STR 27-26L REF CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-42-21-001-001-A01 AND DRW SH670-3338
- [SDR SWIA202055968](https://openairdocs.org/sdr/SWIA202055968.md): Bracket · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON FWD CARGO FLOOR MACHINED BRACKET BETWEEN STGR 25R €“ 24R, FS 549.00 - 565.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED BRACKET AT STGR 25R €“ 24R, FS 549.00 - 565.00 FWD CARGO PN SH670-33852-1 REF CRJ700 / SRM 51-42-21-001-001-A01, CRJ700
- [SDR SWIA202055967](https://openairdocs.org/sdr/SWIA202055967.md): Bracket · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON FWD CARGO FLOOR MACHINED BRACKET AT FS 533.00 BETWEEN STGR 23L €“ 22L (C-CHECK) RO 2/5/2021 REPLACED FWD CARGO FLOOR MACHINED BRACKET AT FS533 BETWEEN STGR23L-STGR22L WITH NEW. REF CRJ-700 SRM 51-42-06-001-001-A01 AND CRJ-700 SRM 51-42-21-00
- [SDR SWIA202055966](https://openairdocs.org/sdr/SWIA202055966.md): Stringer · corroded · Nov 27, 2020 · N716EV · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > *CORROSION ON STGR 25L BETWEEN FS 485.00 €“ 501.00 (C-CHECK) RO 2/5/2021 REMOVED AND REPLACED STGR 25L F.S. 485.00-501.00, REF CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01 AND BOMBARDIER DWG SH670-33200 REV G, LEAK CHECK GOOD. / COMP

Next page: https://openairdocs.org/aircraft/N716EV/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 n_number = 'N716EV' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N716EV/reports

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