N638NN

Service difficulty reports · 73

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

Query with SQL
duckdb -csv -c "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 = 'N638NN' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR WRXR20250402001Frame · gougedGOUGE FOUND ON FRAME. FS 333 LH STRINGER 1. REMOVED DAMAGE AT FS 333 STR 1LH IAW CRJ 900 SRM 51-12-00-001-001-A01. C/W EA NO: 53-2025-0440 REV -- DATE 2025-04-02Apr 2, 2025 · N638NN · Cndair CL6002D24 · Fuselage Main, FrameSDR WRXR20250401001Frame · corrodedCORROSION FOUND ON FRAME WEB 310 BETWEEN STGR 26LH-27. ENSURED BLEND-OUTS WERE PERFORMED TO A SMOOTH CONTOUR IN ACCORDANCE WITH SRM 51-21-06 USING 20:1 TRANSITION RATIO.Apr 1, 2025 · N638NN · Cndair CL6002D24 · Fuselage Main, FrameSDR WRXR20250331002Mount · corrodedGALLEY #3 HAS CORRODED MOUNT (PN:CDSP2019-7C650). REMOVED AND REPLACED GALLEY #3 MOUNT IAW CRJ 900 VCMM 25-33-30.Mar 31, 2025 · N638NN · Cndair CL6002D24 · Fuselage, Equipment Attach FittingsSDR WRXR20250331001Angle · bentFS280.00 BULKHEAD UPPER L BRACKET BENT 3 INCHES LEFT OF DOOR. HAND DRESSED, DEPTH RECORDED IS 0.006” IAW REO 670-51-00-085 REV. -A 2017-08-23.Mar 31, 2025 · N638NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WRXR20250327001Skin · gougedGOUGES FOUND IN METAL NUTPLATE BRACKET AND STRUCTURE AT MID CARGO DOOR SURROUND AT F.S. 661.00+5.00 AND 661.00+8.00. REMOVED GOUGE FROM STRUCTURE AT MID CARGO DOOR SURROUND FS 661.00+8.00. NDT EVALUATE BLENDED AREA ON STRUCTURE AT MID CARGO DOOR SURROUND AT Mar 27, 2025 · N638NN · Cndair CL6002D24 · Fuselage Main, Plate/SkinSDR WRXR20250326001Vane · dented2 GOUGES ON LEFT HAND INBOARD FLAP VANE AT WS80 AND WS90. BLENDED GOUGES, GRIDDED, AND REQUESTED NDT FOR REMAINING THICKNESS MEASUREMENTS IAW CRJ 900 SRM 57-52-01-101-001-A01. COMPLIED WITH REO 690-57-52-513 REV--.Mar 26, 2025 · N638NN · Cndair CL6002D24 · Trailing Edge FlapsSDR WRXR20250325003Skin · dentedSMALL DENT DISCOVERED ON UNDERSIDE OF LEFT WING INBOARD GROUND SPOILER, PENETRATING SURFACE COATING. DENT DIMENSIONS 0.4" LONG X 0.4" WIDE X .023" DEEP.Mar 25, 2025 · N638NN · Cndair CL6002D24 · SpoilersSDR WRXR20250325002Strap · corrodedCORROSION FOUND ON SUBSTRUCTURE AT FS 847.00 ALONG RH BOTTOM SIDE. REMOVED CORROSION ON STRAP P/N SH670-39347-8 LOCATED ON SUBSTRUCTURE BETWEEN FS 847.00 - FS 847.00+32.00 RBL36 IAW CRJ 900 SRM 51-21-06-001-001-A01. BLEND ON STRAP P/N SH670-39347-8 IS OUT OF LMar 25, 2025 · N638NN · Cndair CL6002D24 · Fuselage Miscellaneous StructureSDR WRXR20250325001Strap · corrodedSTRAP THAT JOINS PANEL 194AB TO 195AB PANEL HAS MULTIPLE SPOTS OF CORROSION AT RH BL22.50 TO LH BL 22.50.00. FS 761.85. FABRICATED, LOCATED AND DRILLED STRAP IAW CRJ 900 SRM 51-24-21-001-001-A01. INSTALLED NUT PLATES 20EA. IAW CRJ 900 SRM 51-45-00-001-001-A01.Mar 25, 2025 · N638NN · Cndair CL6002D24 · Aerodynamic FairingsSDR WRXR20250324001Angle · corrodedCORROSION ABOVE PANEL 691JB, ON WING, AT RH WS222.46 - WS260.04. REMOVED CORROSION TO AREA ABOVE PANEL 691JB AT RH WS222.46 - WS260.04 AND CREATED GRID FOR NDT TO DETERMINE MATERIAL THICKNESS IAW CRJ 900 SRM 51-21-06-001-001-A01. ALODINED, PRIMED, AND PAINTED,Mar 24, 2025 · N638NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR WRXR20250321001Floorbeam · crackedFOUND A CRACK 0.60 LONG ON RH FLOOR BEAM P/N CC670-33202 LOCATED AT RBL12 AT APPROXIMATELY FS221.73. FABRICATED A -1 ANGLE, COMPLIED WITH REO 690-53-11-1947 REV --.Mar 21, 2025 · N638NN · Cndair CL6002D24 · Fuselage Main, Floor BeamSDR WRXR20250320001Support Bracket · gougedDURING MAINTENANCE GOUGES WERE FOUND ON THE SUPPORT BRACKET FOR THE FORWARD UNDER WING FAIRING 193AB. BLENDED THE DAMAGED AREA TO A SMOOTH CONTOUR WITH A 20 TO 1 TAPER RATIO IAW CRJ900 SRM 51-12-00-001-001-A01. HIGH FREQUENCY EDDY CURRENT INSPECTION PER NDTM 5Mar 20, 2025 · N638NN · Cndair CL6002D24 · Wing, Attach FittingsSDR WRXR20250318003Vane · gougedRH INB FLAP VANE ACCESS PANEL 684ET IS SHOWING SIGNS OF CHAFING. PERFORMED BLENDING ON PANEL 684ET IAW CRJ 900 SRM 51-12-00-001-001-A01. R&R BLENDED RIVETS IAW CRJ 900 SRM 51-42-06-001-001-A01. RESTORED FINISH IAW CRJ 900 SRM 51-21-11-001-001-A01, 51-25-06-00Mar 18, 2025 · N638NN · Cndair CL6002D24 · Trailing Edge FlapsSDR WRXR20250318002Access Panel · gougedDURING MAINTENANCE CHAFING WAS FOUND ON INBOARD FLAP ACCESS PANEL 584EB. THE CHAFING WAS BLENDED AND NDT PERFORMED. NDT MEASURED REMAINING THICKNESS AND INDICATED NO CRACKS.Mar 18, 2025 · N638NN · Cndair CL6002D24 · Wing, Plate/SkinSDR WRXR20250318001Skin Panel · gougedDURING MAINTENANCE, CHAFING DAMAGE WAS FOUND ON LH INBD FLAP PANEL 584ET P/N CC670-14027-3. PERFORMED BLENDING ON PANEL 584ET. PROVIDED 2IN. X 3IN. GRID FOR NDT.Mar 18, 2025 · N638NN · Cndair CL6002D24 · Trailing Edge FlapsSDR WRXR20250317001Channel · bentDURING MAINTENANCE A DENT/ BEND WAS FOUND ON THE UPPER CHANNEL ABOVE THE AFT CARGO DOOR. HAND DRESSED TO REFORM THE PART BACK TO THE ORIGINAL CONTOUR. REFINISHED AND COMPLIED ALL STEPS WITH EA NO. 53-2025-0266 REV. - - 2025-03-01.Mar 17, 2025 · N638NN · Cndair CL6002D24 · Cargo/Baggage DoorsSDR WRXR20250314003Fairing · corrodedON 193AB PANEL, AT BL0.00, WL68.00, FS732.00, FOUND MULTIPLE SPOTS OF CORROSION ON LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4). REMOVED AND REPLACED LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4) IAW CRJ. 900 SRM 51-42-13-001-001-A01.Mar 14, 2025 · N638NN · Cndair CL6002D24 · Aerodynamic FairingsSDR WRXR20250314002Fairing · corrodedON 193AB PANEL, AT BL0.00, WL68.00, FS732.00, FOUND MULTIPLE SPOTS OF CORROSION ON LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4). REMOVED AND REPLACED LH AND RH STRAPS (P/NS CC670-39052-3 AND CC670-39052-4) IAW CRJ. 900 SRM 51-42-13-001-001-A01.Mar 14, 2025 · N638NN · Cndair CL6002D24 · Aerodynamic FairingsSDR WRXR20250314001Strap · corrodedCORROSION UNDER PANEL 621AB IN FORWARD INBOARD AND FORWARD OUTBOARD CORNERS AROUND FASTENER HOLES. WS49 AND WS28. REMOVED CORROSION AT R/H WS28 AND WS49 ON AREA OF WING UNDER PANEL 621AB IN FORWARD INBOARD AND FORWARD OUTBOARD CORNERS AROUND FASTENER HOLES ANDMar 14, 2025 · N638NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR WRXR20250313003Seat Track · gougedDAMAGE TO LEFT SIDE SEAT RAIL AT APPROX. STA 977. REMOVED AND REPLACED SEAT RAIL IAW REO 670-53-00-589 TORQUED IAW AMM TASK 20-21-00-910-801-A01.Mar 13, 2025 · N638NN · Cndair CL6002D24 · Fuselage, Seat/Cargo Attach FittingsSDR WRXR20250313002Strap · corrodedCORROSION FOUND AT WS29.00 ON STRUCTURE SIDE WHERE PANEL 521AT MEETS STRUCTURE. REMOVED CORROSION AT L/H WS 29.00 WHERE ACCESS PANEL 521AT ATTACHES TO THE WING IAW CRJ 900 SRM 51-21-06-001-001-A01. BLENDED CORROSION DAMAGE ON L/H WING UPPER FIXED LEADING EDGE Mar 13, 2025 · N638NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR WRXR20250313001Strap · corrodedCORROSION FOUND AT WS29.00 ON STRUCTURE SIDE WHERE PANEL 521AT MEETS STRUCTURE. REMOVED CORROSION AT L/H WS 29.00 WHERE ACCESS PANEL 521AT ATTACHES TO THE WING IAW CRJ 900 SRM 51-21-06-001-001-A01. BLENDED CORROSION DAMAGE ON L/H WING UPPER FIXED LEADING EDGE Mar 13, 2025 · N638NN · Cndair CL6002D24 · Wing Miscellaneous StructureSDR WRXR20250310001Mount Bracket · corrodedFOUND CORRODED FLOOR FOOT MOUNT UPON REMOVAL OF GALLEY #1 AT FS 310.00 RH BL22.50. (LH AFT FLOOR FOOT). REMOVED AND REPLACED CORRODED FLOOR FOOT MOUNT (PN CDSP2019-7C-620) ON GALLEY #1 LOCATION AFT LH.Mar 10, 2025 · N638NN · Cndair CL6002D24 · Fuselage, Equipment Attach Fittings
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