# Service difficulty reports: N540EG

A list on [N540EG](https://openairdocs.org/aircraft/N540EG.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 3 · 111 reports

- [SDR VNAA2026081222501](https://openairdocs.org/sdr/VNAA2026081222501.md): Selector Valve · faulted · Aug 10, 2026 · N540EG · Cndair CL6002C10 · Landing Gear Retraction/Extension System
  > GO AROUND GEAR NOT COMING DOWN. MANUAL. REMOVED AND REPLACED LANDING GEAR SELECTOR VALVE IAW AMM 32-32-10-000/400-801-A01. PERFORMED OPS TEST OF LANDING GEAR EXTENSION RETRACTION SYSTEM IAW AMM 32-30-00-710-801-A01 AND OPS TEST OF LANDING GEAR ALTERNATE EXTE
- [SDR VNAA2026020211601](https://openairdocs.org/sdr/VNAA2026020211601.md): Steering Sys · malfunctioned · Feb 1, 2026 · N540EG · Cndair CL6002C10 · Landing Gear Steering System
  > STEERING INOP CAUTION MSG DURING FLIGHT / PERFORMED BITE TEST OF THE STEERING SYSTEM IAW AMM 32-50-00-740-801-A01. OPS CHECK GOOD NO FURTHER DEFECTS NOTED AT THIS TIME.
- [SDR WRXR20250127001](https://openairdocs.org/sdr/WRXR20250127001.md): Floor Support · corroded · Jan 27, 2025 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH FLOOR SILL PN:SH670-32172-11 @ FS. 280-319 HAS MULTIPLE AREAS OF CORROSION. REMOVED AND REPLACED RH FLOOR SILL PN:SH670-32172-11 FWD. OF THE GALLEY SERVICE DOOR @ FS280-FS319.
- [SDR WRXR20250122001](https://openairdocs.org/sdr/WRXR20250122001.md): Skin · gouged · Jan 22, 2025 · N540EG · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WS128.00 FLAP SKIN HAS GOUGING DUE TO AFT FAIRING 586BB SEAL. COMPLIED WITH REO 670-57-52-590 REV: -- DATED: 2025-01-07 NO DEVIATION FROM THE REO - FABRICATED 1 (EA) EXTERNAL STRAP AND 2 (EA) INTERNAL STRAPS FROM 2024 T3 AL ALLOY ALCAD.063". FABRICATED 1 (
- [SDR WRXR20250117001](https://openairdocs.org/sdr/WRXR20250117001.md): Hinge · gouged · Jan 17, 2025 · N540EG · Cndair CL6002C10 · Trailing Edge Flaps
  > GOUGE ON RH HINGE ARM FITTING PN.CC670-14131-4 AT I/B FLAP WS54.55. MEASURES.250 X.025. ROTO-PEEN REWORKED AREA IAW CRJ 700 SRM 51-24-11. ALODINED AND PRIMED RH HINGE ARM FITTING PN.CC670-14131-4 AT I/B FLAP WS54.55. IAW CRJ700 SRM 51-21-001-001-A01 AND CRJ
- [SDR WRXR202501161111](https://openairdocs.org/sdr/WRXR202501161111.md): Frame · corroded · Jan 16, 2025 · N540EG · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS879 IS CORRODED BETWEEN STRINGERS 26L AND 26R C/T KEEL BEAM ATTACHMENT FITTINGS. FOUND UPON CLEANING OF BLUE WATER SPILL. EVALUATED AREA, FRAME STATION 879, BETWEEN STR 26L-26R ORIGINAL MATERIAL.063" MATERIAL REMAINING.046" MATERIAL LOSS.017" ALLOWA
- [SDR WRXR20250113004](https://openairdocs.org/sdr/WRXR20250113004.md): Fairing · eroded · Jan 13, 2025 · N540EG · Cndair CL6002C10 · Vertical Stabilizer
  > DURING MAINTENANCE PANEL 326AL WAS FOUND WITH DAMAGE TO THE COPPER MESH ON THE EXTERNAL SURFACE. SANDED DAMAGED AREA TO REMOVE BONDED MESH. CLEANED AREA TO REMOVE ANY DUST. CUT PLIES TO FIT AREA.
- [SDR WRXR20250113003](https://openairdocs.org/sdr/WRXR20250113003.md): Fairing · worn · Jan 13, 2025 · N540EG · Cndair CL6002C10 · Vertical Stabilizer Miscellaneous Structure
  > PANEL 326AR HAS COMPOSITE DAMAGE TO 10 HOLES THAT WILL REQUIRE REPAIR. CLEANED THE DAMAGED AREA USING ALCOHOL AND A LINT FREE CLOTH WIPING DRY PRIOR TO EVAPORATION. CUT PLIES OF CU040CX36 COPPER WIRE MESH TO FIT THE REPAIR AREA. TRIMMED TO FIT.
- [SDR WRXR20250113002](https://openairdocs.org/sdr/WRXR20250113002.md): Skin · chafed · Jan 13, 2025 · N540EG · Cndair CL6002C10 · Trailing Edge Flaps
  > RH WS54.55 AFT HINGE WAS CHAFFING ON FLAP LOWER SKIN COMMON TO FAIRING SEAL. BLENDED CHAFE DAMAGE TO RH INBD FLAP LOWER SKIN, (DWG: CC670-14061, AL ALY ALCD 2024-T3, 0.063” NOMINAL STOCK THICKNESS, 0.052” ± 0.003” & 0.040” ± 0.003” CHEM. MILL POCKET THICKNESS
- [SDR WRXR202500113001](https://openairdocs.org/sdr/WRXR202500113001.md): Mount · cracked · Jan 13, 2025 · N540EG · Cndair CL6002C10 · Fuselage Main, Structure
  > HAIRLINE CRACK MEASURING.55'' WAS FOUND IN THE RADIUS OF THE STRUCTURE FOR THE SPR. FABRICATED REPAIR ANGLE -1 MAKE FROM ALUM ALLOY 2024 T3.050 LOT# 44682B7/1.16. LOCATED AND DRILLED NEW FABRICATED ANGLE -1 IAW REO 670-28-25-013 REV. --. INSTALLED NEW ANGLE:
- [SDR WRXR20250107002](https://openairdocs.org/sdr/WRXR20250107002.md): Skin Panel · gouged · Jan 7, 2025 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > GOUGE DAMAGE TO RH FIXED LEADING EDGE SKIN BETWEEN S.STA 210.69 AND SLAT TRACK 2-1. TRIMMED FOR PROPER FITMENT AND REMOVED ALL SHARP EDGES ON NEW LEADING EDGE SKIN PANEL 622BR PN:CC670-12301-6. LOCATED, DRILLED, COUNTERSUNK, AND DEBURRED ALL FASTENER HOLE LOCA
- [SDR WRXR20250107001](https://openairdocs.org/sdr/WRXR20250107001.md): Skin · gouged · Jan 7, 2025 · N540EG · Cndair CL6002C10 · Wing Miscellaneous Structure
  > AFTER REMOVAL OF RH FLAP FAIRING 692AB FOUND GOUGING ON WING ON FWD SIDE OF PANEL TO WING MATING SURFACE DUE TO CERAM-KOTE ON SEAL. REMOVED DAMAGE BLEND PER ENGINEERING. ROTO-PEENED REWORKED AREA. COMPLIED WITH REO 670-57-21-1019 REV --.
- [SDR WRXR20250106003](https://openairdocs.org/sdr/WRXR20250106003.md): Angle · corroded · Jan 6, 2025 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON GALLEY SERVICE DOOR LOWER SILL STRUCTURE, FROM FS 319.00 TO FS 349.00 (STGR 17L), UNDER DOOR LATCH FITTINGS. REMOVED GALLEY SERVICE DOOR LOWER SILL STRUCTURE PN:SH670-31996-3 IAW CRJ700 SRM 51-42-06-001-001-A01 AND 51-42-21-001-001-A01 INSTA
- [SDR WRXR20250106002](https://openairdocs.org/sdr/WRXR20250106002.md): Skin · chafed · Jan 6, 2025 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > LH WS220 LOWER WING SKIN HAS CHAFFING COMMON TO THE 595AB FAIRING SEAL. BLENDED LH WS220 LOWER WING SKIN COMMON TO THE 595AB FAIRING SEAL. SHOT PEENED REWORKED AREA.
- [SDR WRXR20250106001](https://openairdocs.org/sdr/WRXR20250106001.md): Striker · corroded · Jan 6, 2025 · N540EG · Cndair CL6002C10 · Fuselage Main, Structure
  > CORROSION FOUND ON FITTING SEAL STRIKER P/N SH670-31412-7 AT RH, STGR 18 FS319 TO FS 349, REPLACEMENT REQUIRED NO ALLOWABLE DAMAGES IN THIS AREA. REMOVED CORRODED SH670-31412-7 SEAL STRIKER AT RH, STGR 18 FS319 TO FS 349. INSTALLED NEW SEAL STRIKER P/N SH670-3
- [SDR WRXR20250102001](https://openairdocs.org/sdr/WRXR20250102001.md): Skin Panel · gouged · Jan 2, 2025 · N540EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > FOUND TWO GOUGES AND TWO FASTENERS WITH CORROSION UNDER PANELS 196DR AND 195DL APPROX. F.S 969, L/H STRG. 27. LOWER SKIN PANEL PN:SH670-37060. PERFORMED REPAIR AT FS 969 STRINGER 27L C/T LOWER SKIN PANEL PN: SH670-37060 IAW REO 670-53-00-757 REV. A(P3)
- [SDR WRXR20241224007](https://openairdocs.org/sdr/WRXR20241224007.md): Protector · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON MID FWD, PROTECTOR, WEB FLOOR PART # SH670-32040-1 COMMON TO SERVICE DOOR SILL. REMOVED FWD, PROTECTOR, WEB FLOOR PART # SH670-32040-1 IAW CRJ 700 SRM 51-42-06-001-001-A01 INSTALLED NEW PROTECTOR WEB FLOOR PN SH670-32040-1 IAW CRJ 700 SRM 51
- [SDR WRXR20241224006](https://openairdocs.org/sdr/WRXR20241224006.md): Protector · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FWD, PROTECTOR, WEB FLOOR PART # SH670-32040-1 COMMON TO SERVICE DOOR SILL. REMOVED FWD, PROTECTOR, WEB FLOOR PART # SH670-32040-1 COMMON TO SERVICE DOOR SILL. IAW CRL700 SRM 51-40-00-001-001-A01. INSTALLED NEW PROTECTOR, WEB FLOOR PART # SH
- [SDR WRXR20241224005](https://openairdocs.org/sdr/WRXR20241224005.md): Closeout Panel · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > WHILE REMOVING MANUAL POCKET ASSY FOR ACCESS TO INSPECTIONS, FOUND MODERATE CORROSION ON COCKPIT FLOOR STRUCTURE CLOSING PANEL WHERE MANUAL POCKET ASSY ATTACHES TO. BLENDED CORROSION IAW CRJ 700 SRM 51-21-06-001-001-A01.
- [SDR WRXR20241224004](https://openairdocs.org/sdr/WRXR20241224004.md): Angle · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON AFT, ANGLE PART # SH670-31982-1 COMMON TO AFT PROTECTOR, WEB FLOOR PART # SH670-32040-2. REMOVED AFT, ANGLE PART # SH670-31982-1 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE PN SH670-31982-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR WRXR20241224003](https://openairdocs.org/sdr/WRXR20241224003.md): Angle · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON MID AFT, ANGLE PART # SH670-31982-1 COMMON TO MID AFT, PROTECTOR, WEB FLOOR PART # SH670-32040-2. REMOVED MID AFT, ANGLE PART # SH670-31982-1 IAW CRJ700 SRM 51-42-06-001-001-A01. INSTALLED NEW ANGLE PN SH670-31982-1 IAW CRJ 700 SRM 51-42-06-
- [SDR WRXR20241224001](https://openairdocs.org/sdr/WRXR20241224001.md): Angle · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON MID FWD, ANGLE PART # SH670-31982-1 COMMON TO FWD PROTECTOR, WEB FLOOR PART # SH670-32040-1. REMOVED CORRODED MID FWD, ANGLE PART # SH670-31982-1 AND INSTALLED NEW ANGLE PN SH670-31982-1 IAW CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR WRXR20241224002](https://openairdocs.org/sdr/WRXR20241224002.md): Angle · corroded · Dec 24, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON FWD, ANGLE PART # SH670-31982-1 COMMON TO FWD PROTECTOR, WEB FLOOR PART # SH670-32040-1. LOCATED AT STRINGER 18 C/T FWD. GALLEY SERVICE DOOR LOWER SILL BETWEEN FS.319-FS349. REMOVED FWD, ANGLE PN:SH670-31982-1 IAW CRJ700 SRM 51-42-06-001-001
- [SDR WRXR20241219002](https://openairdocs.org/sdr/WRXR20241219002.md): Skin · gouged · Dec 19, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge Flaps
  > LH WS54.55 FLAP SKIN GOUGED DUE TO AFT HINGE FAIRING SEAL. REMOVED AND REPLACED 48 (EA) DAMAGED FASTENERS AFTER BLENDING WAS PERFORMED ON L/H WS54.55 LOWER FLAP SKIN IAW REO 670-57-52-585. RESTORED FINISH OF THE REWORKED AREAS ON L/H WS54.55 LOWER FLAP SKIN IA
- [SDR WRXR20241219001](https://openairdocs.org/sdr/WRXR20241219001.md): Channel · corroded · Dec 19, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CHANNEL BETWEEN FS1031- FS1051 BETWEEN STRINGER 27 AND26R HAS CORROSION ON UPPER FACE. PN: MM670-43255-003. REMOVED AND REPLACED CHANNEL PN: MM670-43255-003 FS 1031-1051 STR. 27-26R IAW CRJ700 SRM 51-42-06-001-001-A01, CRJ700 SRM 51-23-00-001-001-A01, & CRJ700
- [SDR WRXR20241218003](https://openairdocs.org/sdr/WRXR20241218003.md): Floorbeam · corroded · Dec 18, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > AFT BAGGAGE BAY FLOOR STRUCTURE @ FS1047.00 AFT OF DOOR STRUCTURE. INTERCOSTAL PN:MM670-35372-005 HAS MODERATE CORROSION. REMOVED MODERATE CORROSION ON INTERCOSTAL C/T AFT BAGGAGE BAY FLOOR STRUCTURE @ FS 1047 IAW CRJ 700 SRM 51-21-06-001-001-A01. GRIDDED AREA
- [SDR WRXR20241218002](https://openairdocs.org/sdr/WRXR20241218002.md): Skin · chafed · Dec 18, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > CUSTOMER REPORTS QTY (3) BLENDED AREAS OF CHAFE DAMAGE TO AFT WING PLANK LOWER SKIN (DWG CC670-10046, AL ALY 7475-T7351, 0.250”,0.270”,0.300” AND 0.350” NOM. THK. +/-0.005” AT BLENDED AREAS) BTW STR10L – AUX SPAR DATUM AND WS48.95-WS68.00. BLENDING OF DAMAGE W
- [SDR WRXR20241218001](https://openairdocs.org/sdr/WRXR20241218001.md): Floor Support · cracked · Dec 18, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RH SUPPORT STRUCTURE FLOOR BEAM @BL12.00 HAS A HAIRLINE CRACK MEASURING.2" IN LENGTH. PN:CC670-33202-30. COMPLIED WITH REO 670-53-11-2059.USING ALODINED IAW CRJ700 SRM 51-21-11 STICK # M-CR EXP. 2/25. PRIMED IAW CRJ 700 SRM 51-25-06 WITH 10P-2NF BATCH # 84740
- [SDR WRXR20241217003](https://openairdocs.org/sdr/WRXR20241217003.md): Skin · dented · Dec 17, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > DURING ROUTINE OPERATIONS AT (CVG), MAINTENANCE NOTED THAT THE RH, AFT STRUCTURE (P/N WA670-30632-3) HAS (1 EA.) LIGHTNING STRIKE. POST BLEND, THE DAMAGE HAS BEEN MEASURED AT 0.0015” DEEP (REO 670-53-84-167). COMPLIED WITH EA 23-C7-53-1115; PERFORM A DETAILED
- [SDR WRXR20241217002](https://openairdocs.org/sdr/WRXR20241217002.md): Stringer · corroded · Dec 17, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > FOUND MODERATE CORROSION ON RH STG 25 BETWEEN F.S. 280.00 AND 333.00. REMOVED AND REPLACED STRINGER 25R PN: SH670-31212-2U. FS 295-333 IAW CRJ 700 SRM 51-42-06-001-001-A01. ALODINE, PRIMED, & PAINTED EXT BARE METAL SURFACE IAW CRJ700 SRM 51-21-16-001-001-A01.
- [SDR WRXR20241217001](https://openairdocs.org/sdr/WRXR20241217001.md): Strap · corroded · Dec 17, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND IN MULTIPLE PLACES AT FS 909 AFT BELLY FAIRING SUPPORT STRAP PN: SH670-39341-3 X2 AND SH670-39338-3. REMOVE SEALANT PAD. REMOVE ALL CORROSION AND EVALUATE OVERALL DAMAGE. REMOVED CORROSION FROM 2EA. STRAPS PER CRJ700 SRM 51-21-06-001-001-A01. F
- [SDR WRXR20241216008](https://openairdocs.org/sdr/WRXR20241216008.md): Door Sill · gouged · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > THERE ARE FIVE GOUGES ON THE UPPER FACE OF THE GALLEY SERVICE DOOR LOWER SILL PN: SH670-31980-17. FROM AFT TO FWD THE MEASUREMENTS ARE 0.200" X 0.350" X 0.013", 0.300" X 0.450" X 0.022", 0.200" X 0.250" X 0.017", 0.200" X 0.200" X 0.018" AND 0.250" X 0.350" X
- [SDR WRXR202412161008](https://openairdocs.org/sdr/WRXR202412161008.md): Strap · corroded · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Aerodynamic Fairings
  > CORROSION FOUND IN MULTIPLE PLACES AT FS 909 AFT BELLY FAIRING SUPPORT STRAP PN: SH670-39341-3 X2 AND SH670-39338-3. REMOVED CORROSION FROM 3EA. STRAPS PER CRJ700 SRM 51-21-06-001-001-A01. FABRICATED STRAP P/N SH670-39338-3 IAW CRJ 700 SRM 51-71-00-001-001-A01
- [SDR WRXR20241216007](https://openairdocs.org/sdr/WRXR20241216007.md): Intercostal · corroded · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE, FWD OF FS 364.00, CORRSION NOTED UNDER BLUE PAINT APPLIED TO BOTH INTERCOSTALS (STGR 27). REMOVED AND REPLACED RH INTERCOSTAL (SH670-32075-4) COMMON TO AVIONICS BAY DOOR FWD OF FS 364.00 @ STGR 27 IAW SRM 51-42-00-001-001.
- [SDR WRXR20241216006](https://openairdocs.org/sdr/WRXR20241216006.md): Door · corroded · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AVIONICS BAY DOOR SURROUND STRUCTURE, FWD OF FS 364.00, CORRSION NOTED UNDER BLUE PAINT APPLIED TO BOTH INTERCOSTALS (STGR 27). REMOVED AND REPLACED LH INTERCOSTAL (SH670-32075-3) COMMON TO AVIONICS BAY DOOR FWD OF FS 364.00 @ STGR 27 IAW SRM 51-42-00-001-001.
- [SDR WRXR20241216005](https://openairdocs.org/sdr/WRXR20241216005.md): Panel · gouged · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > FOUND GOUGING ON WING ON FWD SIDE OF FAIRING PANEL 592AB TO WING MATING SURFACE. BLENDED GOUGES ON LOWER LH WING SKIN AT AREAS C/T PANEL 592AB IAW CRJ700 SRM 51-12-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW CRJ700 SRM 51-24-11. ALODINE AND PRIMED AND PAINTE
- [SDR WRXR20241216004](https://openairdocs.org/sdr/WRXR20241216004.md): Angle · cracked · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Wing Miscellaneous Structure
  > CRACK FOUND ON ANGLE PN: CC670-10338-2 COMMON TO 642AZ PANEL IN RH MLG WHEEL WELL AREA. MEASURES 1.1" LENGTH. FABRICATED NEW ANGLE, MATERIAL USED 7075 T6.063" LOT # 407535/2.9.6 I/A/W CRJ 700 SRM 51-24-16. LOCATED AND DRILLED HOLES IN NEW ANGLE I/A/W CRJ 700
- [SDR WRXR20241216003](https://openairdocs.org/sdr/WRXR20241216003.md): Skin · gouged · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGES ON FAIRING 196AR AND FIXED FAIRING SH670-36302-6. CLEANED AND EVALUATED DAMAGE IAW CRJ700 SRM 53-3-52-32-101-001-A01. SMOOTH AND BLENDED DAMAGED AREA IAW CRJ700 SRM 51-12-00-001-001-A01. REMOVED AND REPLACED 5EA. FASTENERS IAW CRJ700 SRM 51-42-00-001-00
- [SDR WRXR20241216002](https://openairdocs.org/sdr/WRXR20241216002.md): Skin · gouged · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > GOUGES ON FAIRING 195AL AND FIXED FAIRING SH670-36302-5. CLEANED AND EVALUATED PANEL 195AL IAW CRJ700 SRM 53-82-83-101-001-A01. DAMAGE FOUND TO BE MORE THAN THE 4” MAXIMUM LENGTH AND HAS WORN PAST THE COPPER MESH DOWN TO BARE COMPOSITE. SMOOTH AND BLENDED DAMA
- [SDR WRXR20241216001](https://openairdocs.org/sdr/WRXR20241216001.md): Rail · gouged · Dec 16, 2024 · N540EG · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > R/H #1 SIDE SEAT TRACK SPLICE AT FS469 - FS485 FOUND DAMAGE AT 7TH CROSS SECTION FROM THE AFT EOP. DATUM X AND Y GOUGED ON BOTH SIDES. REMOVED AND REPLACED RH #1 SIDE SEAT TRACK DAMAGED SPLICE SECTION WITH A NEW SPLICED SECTION (EXTRUSION: 20276-288-0-0) AT F
- [SDR WRXR202412130001](https://openairdocs.org/sdr/WRXR202412130001.md): Skin · chafed · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > LH FLAP FAIRING 586AB FOUND GOUGING ON WING ON FWD SIDE OF PANEL TO WING MATING SURFACE DUE TO CERAM-KOTE ON SEAL. BLENDED GOUGES ON LOWER LH WING SKIN AT AREAS C/T PANEL 586AB IAW CRJ700 SRM 51-12-00-001-001-A01. ROTO-PEENED REWORKED AREA IAW CRJ700 SRM 51-24
- [SDR WRXR20241213005](https://openairdocs.org/sdr/WRXR20241213005.md): Skin · chafed · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Trailing Edge Flaps
  > RH WS128.00 FLAP SKIN HAS GOUGING DUE TO AFT FAIRING 686BB SEAL. BLENDED GOUGES COMMON TO FAIRING 686BB RH WS128.00 FLAP SKIN IAW CRJ 700 SRM 51-12-00-001-001-A01. PERFORMED REPAIR ON RH WS128.00 FLAP SKIN GOUGING COMMON TO FAIRING 686BB IAW REO 670-57-52-584
- [SDR WRXR20241213004](https://openairdocs.org/sdr/WRXR20241213004.md): Skin · chafed · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > LH WS264 HAS CHAFFING ON WING COMMON TO THE FWD. FARING 597AB SEAL. BLENDED DAMAGE TO A SMOOTH CONTOUR IAW SRM 51-12-00. INSTALLED HI-LITES IAW SRM 51-42-21 AND SRM 51-23-00. EDDY CURRENT INSPECTED IAW NDTM 53-00-000-251. ATT # 11. SHOT PENNED IAW SRM 51-24-11
- [SDR WRXR20241213003](https://openairdocs.org/sdr/WRXR20241213003.md): Fitting · corroded · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Frame
  > AT FS. 319 FRAME SPLICE FITTING HAS CORROSION PITTING. REPLACED SPLICE FITTING PN:SH670-31984-1 FS 319 STR 18R IAW CRJ 700 51-42-21-001-001-A01.
- [SDR WRXR20241213002](https://openairdocs.org/sdr/WRXR20241213002.md): Fitting · corroded · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Structure
  > DURING DETAILED INSPECTION FOR TASK 53-10-305-JIC FOUND MODERATE CORROSION ON THE LH SIDEOF THE JACK FITTING SUPPORT WHERE IT MEETS THE FUSELAGE. REMOVED AND REPLACED JACK PAD SUPPORT FITTINGS CC670-32179-2 AND CC670-32179-3S IAW CRJ 700 SRM 51-42-06-001-001-A
- [SDR WRXR20241213001](https://openairdocs.org/sdr/WRXR20241213001.md): Fitting · corroded · Dec 13, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Structure
  > DURING DETAILED INSPECTION FOR TASK 53-10-305-JIC FOUND MODERATE CORROSION ON THE LH SIDE OF THE JACK FITTING SUPPORT WHERE IT MEETS THE FUSELAGE. REMOVED AND REPLACED JACK PAD SUPPORT FITTINGS CC670-32179-2 AND CC670-32179-3S IAW CRJ 700 SRM 51-42-06-001-001-
- [SDR WRXR20241211002](https://openairdocs.org/sdr/WRXR20241211002.md): Frame · gouged · Dec 11, 2024 · N540EG · Cndair CL6002C10 · Nacelle/Pylon, Frame/Spar/Rib
  > BARE METAL AND NICKS ON TOP SIDE OF PYLON FRAME PN: MM670-37223-001 COMMON TO PYLON LEADING EDGE PANEL 411AT. REMOVED O/B NUTPLATE ON FLANGE, SMOOTH AND BLENDED DAMAGED AREA IAW CRJ700 SRM 51-12-00-001-001-A01. PERFORMED REPAIR ON BARE METAL AND NICKS ON TOP S
- [SDR WRXR20241211001](https://openairdocs.org/sdr/WRXR20241211001.md): Skin · gouged · Dec 11, 2024 · N540EG · Cndair CL6002C10 · Wing, Plate/Skin
  > RH WS264 LOWER WING SKIN HAS CHAFFING COMMON TO 697AB FAIRING SEAL. REMOVED DAMAGE BLEND PER ENGINEERING NOTE 3 IAW CRJ 700 SRM 51-12-00-001-A01. ULTRASONIC INSPECTED BLENDED AREAS FOR REMAINING MATERIAL THICKNESS IN ACCORDANCE WITH MHIRJ NON-DESTRUCTIVE TESTI
- [SDR WRXR20241210001](https://openairdocs.org/sdr/WRXR20241210001.md): Splice · gouged · Dec 10, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Structure
  > GOUGE ON THE FWD SPLICE PLATE OF THE GALLEY DOOR MEASURING 0.100" X 2.400" X 0.015" RIGHT ABOVE THE LOWER SILL ON THE SERVICE DOOR. FABRICATED AND INSTALLED NEW LOWER FWD SPLICE PLATE TO MATCH P/N: SH670-31422-1 FOR GALLEY SERVICE DOOR SURROUND STRUCTURE WITH
- [SDR WRXR20241209003](https://openairdocs.org/sdr/WRXR20241209003.md): Stringer · corroded · Dec 9, 2024 · N540EG · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > STRINGER 24R AT FS 295 TO FS310 IS CORRODED BEYOND THE SRM LIMITS. REMOVED STRINGERS CLIPS 4EA AT FS 295, 310, 319, 333 STGR 24RH AND STRINGER SPLICE AT FS 333 STGR 24RH. REMOVED STR 24R FROM FS 280-333 IAW CRJ700 SRM 51-42-06. INSTALLED STRINGER CLIPS 4EA AT

Next page: https://openairdocs.org/aircraft/N540EG/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 = 'N540EG' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N540EG/reports

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