# Service difficulty reports: N761ND

A list on [N761ND](https://openairdocs.org/aircraft/N761ND.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 5 · 214 reports

- [SDR SWIA2025080800004](https://openairdocs.org/sdr/SWIA2025080800004.md): Winglet · ground damage · Aug 4, 2025 · N761ND · Cndair CL6002C10 · Wing Main, Frame Structure
  > IMPACT DAMAGE TO LT WINGLET. WINGLET LEADING EDGE TRANSITION FAIRING DWG: CC670-15356, HAS BEEN PUNCTURED & DEFORMED, WING TIP LENS CLOSING SPAR DWG CC670-15156, MACHINED FLANGE, HAS BEEN DEFORMED. REF EAML 1671206. FLIGHT 6325. TRANSITION FAIRING R & R
- [SDR SWIA202507280005](https://openairdocs.org/sdr/SWIA202507280005.md): Warning Message · false activation · Jul 25, 2025 · N761ND · Cndair CL6002C10 · Central Warning
  > ANTI ICE DUCT WARNING MESSAGE IN CRUISE. RAN QRH MESSAGE CLEARED 1-2 MINS AFTER SELECTING WING ANTI ICE OFF. SYNOPTIC PAGE SHOWED THE RIGHT WING ANTI ICE DUCT RED. (FLIGHT 4989 - FILED CLOSED)PERFORMED OPERATIONAL CHECK OF WING A/I SYSTEM PER AMM 30-12-00 OP
- [SDR SWIA20240813706](https://openairdocs.org/sdr/SWIA20240813706.md): Fitting · corroded · Jul 6, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION ON NOSE JACK-FITTING RH ANGLE ON FWD SIDE OF FS280. (C-CHECK RO 8/11/2024) BLENDED CORROSION TO A SMOOTH CONTOUR REF CRJ 700 SRM 51-21-06-001-001-A01. FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED NEW ANGLE P/N CC670-32154-2 REF CRJ 700 SRM
- [SDR SWIA20240813615](https://openairdocs.org/sdr/SWIA20240813615.md): Skin · bent · Jun 15, 2024 · N761ND · Cndair CL6002C10 · Ailerons
  > DURING MOVEMENT OF RIGHT HAND AILERON, COTTER KEY HEAD CONTACTED AILERON LEADING EDGE CAUSING UPPER LEADING EDGE OF AILERON TO BEND AT HINGES # 2 AND # 3 (C-CHECK RO 8/11/2024) REMOVED UPPER AILERON SKIN REF CRJ700 SRM 51-42-21-001-001-A01 AND INSTALLED
- [SDR SWIA20240813610](https://openairdocs.org/sdr/SWIA20240813610.md): Frame · corroded · Jun 10, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > PLATE AFT OF FS.280 FRAME UNDERFLOOR APPROX. STRG 25L-STRG 25R HAS CORROSION (MARKED) (C-CHECK RO 8/11/2024) REPAIRED PLATE AFT OF FS.280 FRAME UNDERFLOOR APPROX. STRG 25L-STRG 25R REF MHIRJ REO 670-53-11-1982 REV -- DATED 2024-07-09. COMPLIED WITH ALL
- [SDR SWIA20240813606](https://openairdocs.org/sdr/SWIA20240813606.md): Support Beam · chafed · Jun 6, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Structure
  > SUPPORT BEAM FOR AFT BAGGAGE DOOR TRACK HAS CHAFING FROM BAGGAGE DOOR CABLES. (C-CHECK RO 8/11/2024) EVALUATED 2AE CHAFINGS ON SUPPORT BEAM (P/N: MM670-35502-010) FOR AFT BAGGAGE DOOR TRACK WITH LOCATIONS AT FS1000 AND FS1047 OUT OF LIMITS. COMPLIED WIT
- [SDR SWIA20240813602](https://openairdocs.org/sdr/SWIA20240813602.md): Spar · corroded · Jun 2, 2024 · N761ND · Cndair CL6002C10 · Wing Spar
  > CENTER WING REAR SPAR R/H FWD ANGLE FOR THE TIRE BURST PANEL HAS CORROSION. (C-CHECK RO 8/11/2024) EVALUATED RH FWD ANGLE FOR TIRE BURST PANEL OUT OF LIMITS. ORDERED NEW PART, DRILLED AND LOCATED NEW PART. INSTALLED AND PERFORMED LEAK TEST OF AREA.
- [SDR SWIA202408130680](https://openairdocs.org/sdr/SWIA202408130680.md): Door Sill · gouged · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY SILL BETWEEN FS533.00 AND FS581.00 STGR26L CORRODED AND GOUGED IN MULTIPLE AREAS AS MARKED (C-CHECK RO 8/11/2024) REPAIRED CORROSION/GOUGE DAMAGE TO THE FWD BAGGAGE BAY DOOR SURROUND INNER CLOSING SKIN BETWEEN FS533.00-FS581.00 AND S
- [SDR SWIA202408130679](https://openairdocs.org/sdr/SWIA202408130679.md): Tee Angle · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON LBL9 BETWEEN APPROXIMATELY F697.00 AND FS841.00 AS MARKED (C-CHECK RO 8/11/2024) BLENDED CORROSION FROM MULTIPLE LOCATIONS ON LBL9 T-CAP FLOOR STRUCTURE BETWEEN FS697 AND FS841. REPAIRED T-CAP REF
- [SDR SWIA202408130678](https://openairdocs.org/sdr/SWIA202408130678.md): Intercostal · chafed · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > INTECOSTAL IS CHAFED STGR9R BETWEEN FS1144.00 & FS1162.00. (FLAGGED) (C-CHECK RO 8/11/2024) BLENDED OUT CHAFE ON INTERCOSTAL LOCATED ON STGR9R BETWEEN FS1144.00 & FS1162.00. REF CRJ 700 SRM 51-12-00-001-001-A01REMOVED DAMAGED INTERCOSTAL BETWEEN FS 1144
- [SDR SWIA202408130677](https://openairdocs.org/sdr/SWIA202408130677.md): Tee Angle · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.00 AS MARKED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM CENTER FUSELAGE T CAP CORRODED ON RBL9 BETWEEN APPROXIMATELY FS685.00 AND FS697.0. PERFORMED ALL STEPS OF REO 670-
- [SDR SWIA202408130676](https://openairdocs.org/sdr/SWIA202408130676.md): Cap · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON RBL9 BETWEEN APPROXIMATELY F697.00 AND FS841.00 AS MARKED (C-CHECK RO 8/11/2024) CUT OUT DAMAGED AREAS AND PERFROMED PERMANENT REPAIRS TO FS697.00 - FS841.00 RBL 9 BEAM T-CAP AS PER REO 670-53-41-67
- [SDR SWIA202408130675](https://openairdocs.org/sdr/SWIA202408130675.md): Tie Down · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Structure
  > FORWARD CARGO BAY TIE DOWN PAD AT FS581.00 BETWEEN STGR27 AND STGR26L CORRODED AS MARKED (C-CHECK RO 8/11/2024) REMOVED FROM FORWARD CARGO BAY TIE DOWN PAD AT FS581.00 BETWEEN STGR27 AND STGR26L AND INSTALLED NEW BRACKET PN SH670-33389-2 AT FORWARD CAR
- [SDR SWIA202408130674](https://openairdocs.org/sdr/SWIA202408130674.md): Tee Angle · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Structure
  > CENTER FUSELAGE T CAP CORRODEDIN MULTIPLE LOCATIONS ON LBL9 BETWEEN APPROXIMATELY F841.00 AND FS853.00 AS MARKED (C-CHECK RO 8/11/2024) PERFORMED REPAIR PER REO 670-53-41-677 REV -- DATED 2024-07-08 CENTER FUSELAGE T CAP ON LBL9 BETWEEN APPROXIMATELY F
- [SDR SWIA202408130673](https://openairdocs.org/sdr/SWIA202408130673.md): Tie Down · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FORWARD BAGGAGE BAY CARGO TIEDOWN PAD AT FS581.00 BETWEEN STGR23L AND STGR22L CORRODED AS MARKE (C-CHECK RO 8/11/2024) REMOVED FROM FORWARD BAGGAGE BAY CARGO TIEDOWN PAD ( BRACKET) AT FS581.00 BETWEEN STGR23L AND STGR22L REF. CRJ-700 SRM 51-42-21-001-0
- [SDR SWIA20240813601](https://openairdocs.org/sdr/SWIA20240813601.md): Plate · corroded · Jun 1, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L CORRODED (C-CHECK RO 8/11/2024) REMOVED CORROSION FROM FORWARD BAGGAGE BAY JOINT PLATE AT APPROXIMATELY FS581.00 BETWEEN STGR25L AND STGR26L REF. CRJ-700 SRM 51-21-06-
- [SDR SWIA202408130688](https://openairdocs.org/sdr/SWIA202408130688.md): Frame · corroded · May 31, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION AT FS597.00 BETWEEN STGR18L AND STGR19L AS MARKED (C-CHECK RO 8/11/2024) REMOVED CORROSION AT FS597.00 BETWEEN STGR18L AND STGR19L PER CRJ700 SRM 51-21-06-001-001-A01 FOUND OUT OF LIMITS. REMOVED AND INSTALLED A NEW STUB FRAME P/N SH670-33178-
- [SDR SWIA202408130687](https://openairdocs.org/sdr/SWIA202408130687.md): Frame · corroded · May 31, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION AT FS597.00 STGR19R AFT FACE AS MARKED (C-CHECK RO 8/11/2024) PERFORMED REPAIR TO FS597.00 STGR19R AFT FACE BY COMPLYING WILL ALL STEPS OF REO 670-53-31-894 REV -- DATE 2024-06-21. SEE CONTINUATION FOR WORK PERFORMED. COMPLIED WITH TASK CARD 5
- [SDR SWIA20240813531](https://openairdocs.org/sdr/SWIA20240813531.md): Stringer · corroded · May 31, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STGR19R BETWEEN FS364.00 AND FS379.00 AS MARKED (C-CHECK RO 8/11/2024) BLENDED OUT CORROSION ON STGR19R BETWEEN FS364.00 AND FS379.00 REF CRJ-700 SRM 51-21-06-001-001-A01 COMPLIED WITH REO 670-53-21-2423 REV -B DATED 2024-07-27 REPAIR. COMP
- [SDR SWIA202408130682](https://openairdocs.org/sdr/SWIA202408130682.md): Stringer · corroded · May 30, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > CORROSION BETWEEN FS319.70 AND FS333.00 STGR20L AS MARKED (C-CHECK RO 8/11/2024) REMOVED AND INSTALLED NEW REPLACEMENT STGR 20L PER CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01,DWG:SH670-31810 REV Y. COMPLIED WITH 51-900-1002-S
- [SDR SWIA202408130681](https://openairdocs.org/sdr/SWIA202408130681.md): Frame · corroded · May 30, 2024 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION AT FS265.00 AS MARKED BETWEEN STGR26L AND STGR26R (C-CHECK RO 8/11/2024) REMOVED CORROSION AT FS.265 FRAME ATTACH FLANGE BETWEEN STRG 26L AND 26R REF CRJ 700 SRM 51-42-06-001-001-A01 FOUND TO BE OUT OF LIMITS. REMOVED AND INSTALLED A NEW REPLA
- [SDR SWIA20240813530](https://openairdocs.org/sdr/SWIA20240813530.md): Floor Support · corroded · May 30, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT BRACKET MOUNTED ON THE FS319.00 FRAME HAS INTERGRANULAR CORROSION. (MARKED) (C-CHECK RO 8/11/2024) INSTALLED NEW FLOOR SUPPORT BRACKET (FITTING) MOUNTED ON THE FS319.00 FRAME REF CRJ-700 SRM 51-42-21-001-001-A01 AND DWG#SH670-31950 REV-Y.C
- [SDR SWIA202408130666](https://openairdocs.org/sdr/SWIA202408130666.md): Slat Track · corroded · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > RH #2 LEADING EDGE SLAT TRACK 2-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED RIGHT WING SLAT TRACK 2-2 (P/N: CC670-12051-9; S/N: M480) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 2-2 (P/N: CC670-12051-9; S/N: M1830) PER CRJ700 AMM 27-81-41
- [SDR SWIA202408130665](https://openairdocs.org/sdr/SWIA202408130665.md): Slat Track · corroded · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > RH #1 LEADING EDGE SLAT TRACK 1-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED RIGHT WING SLAT TRACK 1-2 (P/N: CC670-12021-9; S/N: M495) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 1-2 (P/N: CC670-12021-9; S/N: M1945) PER CRJ700 AMM 27-81-41
- [SDR SWIA202408130664](https://openairdocs.org/sdr/SWIA202408130664.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #3 LEADING EDGE SLAT TRACK 3-3 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED LH WING DRIVEN SLAT TRACK 3-3 (P/N: CC670-12090-5 S/N: M410) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 3-3 (P/N: CC670-12090-5, S/N M617) PER CRJ700 AMM 27-81-41-400-803-A01. GA
- [SDR SWIA202408130663](https://openairdocs.org/sdr/SWIA202408130663.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #3 LEADING EDGE SLAT TRACK 3-1 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED SLAT TRACK 3-1 ( SN: M481) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 3-1 (SN: M1035) REF CRJ700 AMM 27-81-41-400-801-A01. COMPLIED WITH SKYWEST TASK CARDS 27-900-1009-SKY. GAPS
- [SDR SWIA202408130662](https://openairdocs.org/sdr/SWIA202408130662.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #2 LEADING EDGE SLAT TRACK 2-3 IS GROOVED. (C-CHECK RO 8/11/2024) REMOVED LH WING SLAT TRACK 2-3 AND INSTALLED NEW/SERVICEABLE SLAT TRACK 2-3 PER CRJ700 AMM 27-81-41-400-801-A01. OPS TEST GOOD AT THIS TIMETOOL USED: TORQUE WRENCH ID:TUC6231 CAL DATE
- [SDR SWIA202408130672](https://openairdocs.org/sdr/SWIA202408130672.md): Slat Track · corroded · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #2 LEADING EDGE SLAT TRACK 2-2 IS GROOVED, PITTED/CORRODED IN TWO AREAS. (C-CHECK RO 8/11/2024) LH #2 LEADING EDGE SLAT TRACK 2-2 REMOVED IAW CRJ700 AMM 27-81-41-000-802-A01 AND REPLACED AND INSTALLED WITH NEW SLAT TRACK IAW CRJ700 AMM 27-81-41-400-8
- [SDR SWIA202408130671](https://openairdocs.org/sdr/SWIA202408130671.md): Slat Track · corroded · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #1 LEADING EDGE SLAT TRACK 1-2 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REMOVED LH WING NON DRIVEN SLAT TRACK 1-2 (PN: CC670-12021-9, S/N M496) AND INSTALLED NEW/SERVICEABLE SLAT TRACK 1-2 (PN: CC670-12021-9, S/N M1926) PER CRJ700 AMM TASK
- [SDR SWIA202408130670](https://openairdocs.org/sdr/SWIA202408130670.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > RH #1 LEADING EDGE SLAT TRACK 1-1 IS GROOVED. (C-CHECK RO 8/11/2024) REPAIRED RH #1 LEADING EDGE SLAT TRACK 1-1 REF REO 670-57-42-1581 REV --, DATED 2024-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME.COMPL
- [SDR SWIA202408130669](https://openairdocs.org/sdr/SWIA202408130669.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > RH #3 LEADING EDGE SLAT TRACK 3-1 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) REPAIRED RH #3 LEADING EDGE SLAT TRACK 3-1 PER REO 670-57-42-1585 REV --, DATE 2023-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT TH
- [SDR SWIA202408130668](https://openairdocs.org/sdr/SWIA202408130668.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #1 LEADING EDGE SLAT TRACK 1-3 IS GROOVED. (C-CHECK RO 8/11/2024) BLENDED OUT 2EA GROOVES ON LH SLAT TRACK 1-3 REF CRJ 700 SRM 51-12-00-001-001-A01 REPAIRED THE LH #1 LEADING EDGE SLAT TRACK 1-3 REF REO 670-57-42-1588 REV --, DATED 2024-06-24. COMPLI
- [SDR SWIA202408130667](https://openairdocs.org/sdr/SWIA202408130667.md): Slat Track · corroded · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > RH #1 LEADING EDGE SLAT TRACK 1-3 IS GROOVED, PITTED/CORRODED. (C-CHECK RO 8/11/2024) COMPLIED WITH REO 670-57-42-1583 REV-- DATED 2024-06-21 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIME.COMPLIED WITH 51-900-1002-
- [SDR SWIA20240813525](https://openairdocs.org/sdr/SWIA20240813525.md): Slat Track · grooved · May 25, 2024 · N761ND · Cndair CL6002C10 · Leading Edge Devices
  > LH #1 LEADING EDGE SLAT TRACK 1-1 IS GROOVED. (C-CHECK RO 8/11/2024) REPAIRED LH #1 LEADING EDGE SLAT TRACK 1-1, COMPLIED WITH REO 670-57-42-1586 REV: -- DATE 2024-06-24 - RIGGING CHECK GOOD PER CRJ700 AMM 27-81-00-820-801-A02. OPS TEST GOOD AT THIS TIM
- [SDR SWIA202408130686](https://openairdocs.org/sdr/SWIA202408130686.md): Stand Off · cracked · May 20, 2024 · N761ND · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/11/2024) REPLACED I/B STAND-OFF ANGLE P/N CN624-2082-201 ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-971, REV. B, 2023-11-28. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY.
- [SDR SWIA202408130685](https://openairdocs.org/sdr/SWIA202408130685.md): Bracket · cracked · May 20, 2024 · N761ND · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL HAS A CRACK @ THE END OF THE OMEGA SEAL ABOVE THE "A" BRACKET REPAIRED I/B EDGE OF SCOOP ON L/H LOWER TRANSCOWL, REF. REO 670-54-21-1650, REV. --, 2024-06-19. COMPLIED WITH M-337 AND SKY CARD 51-900-1002-SKY
- [SDR SWI2024F00684](https://openairdocs.org/sdr/SWI2024F00684.md): Coaming · chafed · May 20, 2024 · N761ND · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL INNER COAMING IS CHAFED @ FWD LATCH (C-CHECK RO 8/11/2024) REPAIRED L/H LOWER TRANSCOWL INNER COAMING AT FWD. LATCH, REF. REO 670-54-21-1652, REV. --, 2024-07-04. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CARD 51-900-1002-SKY.
- [SDR SWIA202408130683](https://openairdocs.org/sdr/SWIA202408130683.md): Stand Off · cracked · May 20, 2024 · N761ND · Cndair CL6002C10 · Nacelle/Pylon Miscellaneous Structure
  > L/H UPPER TRANSCOWL INBD "A" BRACKET STANDOFF IS CRACKED (C-CHECK RO 8/11/2024) INSTALLED 1 EA. NEW STANDOFF P/N CN624-2130-201 ON L/H UPPER TRANS COWL, REF. REO 670-54-21-971, REV. B, 2023-11-28, AND CRJ700 SRM 51-40-11-001-001-A01. COMPLIED WITH STEP
- [SDR SWIA20240813520](https://openairdocs.org/sdr/SWIA20240813520.md): Rivet · sheared · May 20, 2024 · N761ND · Cndair CL6002C10 · Engine Thrust Reverser
  > L/H LWR TRANSCOWL HAS Z STIFFENER RIVETS SHEARED (C-CHECK RO 8/11/2024) REPAIRED L/H LOWER TRANSCOWL INNER SKIN COMMON TO ZED STIFFENER AT SHEARED FASTENER HOLES, REF. REO 670-54-21-1652, REV. --, 2024-07-04. COMPLIED WITH MAJOR REPAIR M-337 AND SKY CAR
- [SDR SWIA20240813514](https://openairdocs.org/sdr/SWIA20240813514.md): Angle · cracked · May 14, 2024 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RIGHT TORQUE BOX BL9R FS280.00 OUTBOARD ANGLE OUTBOARD SIDE OF THE TORQUE BOX AT FS280.00 IS CRACKED. (C-CHECK RO 8/11/2024) REMOVED DAMAGED OUTBD ANGLE AT FS280-00 RBL-9 OUT BOARD OF TORQUE BOX. REF CRJ-700 SRM 51-42-21-001-001-A01. INSTALLED 1 EA NEW
- [SDR SWIA20240813513](https://openairdocs.org/sdr/SWIA20240813513.md): Hinge · corroded · May 13, 2024 · N761ND · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP THE INBD HINGE BOX HAS SIGNS OF CORROSION AT HINGE POINT (MARKED) (C-CHECK RO 8/11/2024) PERFORMED REPAIR OF L/H I/B FLAP HINGE BOX CORROSION AT HINGE POINT BY COMPLYING WITH ALL STEPS OF REO 670-57-54-062 REV -- DATE 2024-06-24 COMPLIED WI
- [SDR SWIA20240813511](https://openairdocs.org/sdr/SWIA20240813511.md): Skin · dented · May 11, 2024 · N761ND · Cndair CL6002C10 · Trailing Edge Flaps
  > RIGHT INBOARD FLAP LOWERE SKIN INBOARD OF THE INBOARD FLAP HINGE ARM HAS FOUR DENTS. (MARKED) (C-CHECK RO 8/11/2024) REPAIRED R/H I/B FLAP LOWER SKIN REF CRJ 700 SRM 57-52-01-201-005-A01, FIG. 57-52-01-995-803. SEE CONTINUATION SHEET FOR DETAILS. COMPL
- [SDR SWIA20240813509](https://openairdocs.org/sdr/SWIA20240813509.md): Handle · misaligned · May 9, 2024 · N761ND · Cndair CL6002C10 · Electrical/Electronic Compartment Doors
  > MAIN AVIONICS COMPARTMENT DOOR HANDLE MISALIGNED / STICKS (C-CHECK RO 8/11/2024) INSTALLED NEW MAIN AVIONICS COMPARTMENT DOOR HANDLE HOUSING PER CRJ700 SRM 51-42-21-001-001-A01 AND DWG NO. CC670-38651 REV E. INSTALLED MAIN AVIONICS COMPARTMENT DOOR HAND
- [SDR SWIA2021080560054](https://openairdocs.org/sdr/SWIA2021080560054.md): Striker · gouged · Aug 2, 2021 · N761ND · Cndair CL6002C10 · Fuselage Main, Structure
  > FWD CARGO DOOR SURROUND, FWD SEAL STRIKER AT F.S 535.64 GOUGED BEYOND REPAIR / REF SRM 53-31-23-991-801 ITEM # 102B PN SH670-31426-8 (FILED CLOSED) DRILLED OFF FWD CARGO DOOR SURROUND FWD SEAL STRIKER AT F.S 535.64 IAW SRM 51-42-06, / [PN SH670-31426-8
- [SDR SWIA2019061145970](https://openairdocs.org/sdr/SWIA2019061145970.md): Shaft · out of adjust · Jun 10, 2019 · N761ND · Cndair CL6002C10 · Passenger/Crew Doors
  > RECEIVED A PASSENGER DOOR WARNING MESSAGE IN FLIGHT AFTER HEARING A LOUD NOISE DURING OUR INITIAL CLIMB. ALSO A PROX SYSTEM 1 FAULT STATUS MESSAGE. NO PRESSURIZATION PROBLEMS NOTED. RAN QRH DIVERTED. (FLT#2953) CLOSED FOUND INNER PAX DOOR HANDLE LOWER SHAFT AS
- [SDR SWIA201906045939](https://openairdocs.org/sdr/SWIA201906045939.md): Skin · chafed · May 20, 2019 · N761ND · Cndair CL6002C10 · Ailerons
  > LH AILERON LOWER LEADING EDGE CHAFE. (C-CHECK) RO: 06/01/2019 REMOVED AND REPLACED 2EA L/H AILERON LWR LEADING EDGE PANELS IAW SRM.
- [SDR SWIA201906045938](https://openairdocs.org/sdr/SWIA201906045938.md): Intercostal · corroded · May 9, 2019 · N761ND · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 IS CORRODED. (C-CHECK) RO: 06/01/2019 REPLACED PAX DOOR INTERCOSTAL DD4 P/N 601R318081-1 WITH NEW IAW SRM.
- [SDR SWIA201906045937](https://openairdocs.org/sdr/SWIA201906045937.md): Skin · chafed · May 8, 2019 · N761ND · Cndair CL6002C10 · Ailerons
  > RIGHT AILERON HAS CHAFE MARKS ON TOP LEADING EDGE. (C-CHECK) RO: 06/01/2019 INSTALLED NEW R/H AILERON UPPER LEADING EDGE SKIN IAW SRM.
- [SDR SWIA2019060445934](https://openairdocs.org/sdr/SWIA2019060445934.md): Frame · corroded · May 7, 2019 · N761ND · Cndair CL6002C10 · Fuselage Main, Frame
  > FS 364 FRAME HAS CORROSION AT STR 26R. REMOVED DAMAGE FRAME SECTOR AND INSTALLED A NEW FRAME SECTOR TO FS364 STGR 26R IAW SRM, LEAK CHECK GOOD.
- [SDR SWIA201906045936](https://openairdocs.org/sdr/SWIA201906045936.md): Angle · corroded · May 6, 2019 · N761ND · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT BAGGAGE BAY DOOR SILL CORROSION, LOCATED IN THE CENTER. REMOVED AND INSTALLED NEW AFT BAG BAY DOOR LOWER SILL ANGLE IAW SRM.

Next page: https://openairdocs.org/aircraft/N761ND/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 = 'N761ND' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N761ND/reports

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