N959R, cancelled Apr 24, 2002

Service difficulty reports · 16

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 = 'N959R' AND deregistration_id = 'N959R-2002-04-24'
  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 20010403CW001Wire · brokenAFTER TAKEOFF, PILOT NOTICED ODD SMELL, FOLLOWED BY SMOKE. HE DECLARED AN EMERGENCY AND RETURNED TO AIRPORT WITHOUT INCIDENT. TROUBLE SHOT SYSTEM, FOUND OLD DEAD END GALLEY WIRE LAYING ON RES R4-35. REMOVED OLD WIRE. CHECKED WIRING TO SWITCHES 51-403, 51-3Jan 10, 2001 · N959R · Doug DC863F · Light System WiringSDR RRXA97282Linkage · lack of lubeLOUD BANGING NOISE FROM NOSE OF AIRCRAFT AFTER ROTATION. RT NOSE GEAR DOOR FOUND OPEN. LUBRICATED DOOR LOCK LINKAGE, OPERATED DOOR SEVERAL TIMES AND OPS OK.Sep 27, 1997 · N959R · Doug DC863F · Landing Gear Door Retract SectionSDR RRXA96176Panels · crackedFERRY FLIGHT, DUE TO HORIZONAL STABILIZER DAMAGE. FOUND 2 EACH HORIZONAL STABILIZER LOWER PANELS DAMAGED AT STA XE160 AND XE171. CUT OUT DAMAGED PANEL AND STRINGER, FABRICATED NEW PANEL SECTIONS AND SPLICED IN IAW DOUGLAS DWG SRO8550001-7041.Dec 24, 1996 · N959R · Doug DC863F · Horizontal Stabilizer, Plate/SkinSDR RRXA96030Plating · crackedKMCN - DURING C-CHECK, FOUND LEADING EDGE SKIN CRACK THROUGH HI-LOCK LOWER RIGHT AT XFS 210 BELOW INBOARD END OF ACCESS 583C. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R03. (M)Apr 14, 1996 · N959R · Doug DC863F · Wing, Plate/SkinSDR RRXA96028Plating · crackedKMCN - DURING C-CHECK, FOUND SKIN CRACKED THROUGH RIVET INBOARD SLOT L/E UPPER, OUTBOARD FORWARD RIGHT WING. FABRICATED DOUBLER FROM 7075T6 AL AND INSTALLED IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R02 AND IAW DC-8 SRM 51-1-21, 51-1-20C. (M)Apr 14, 1996 · N959R · Doug DC863F · Trailing Edge FlapsSDR RRXA96027Web · crackedKMCN - DURING C-CHECK, FOUND CORROSION BULGE AND LONGITUDINAL STIFFENER CRACKED TOP RIGHT WHEEL WELL AT Y=902, X-25 AND Z=10. REMOVED CORROSION AND 6 INCH SECTION OF STIFFENER (CUT OUT 5.250 INCH BY 6.75 INCH). REMOVED SECTION OF PRESS WEB. FABRICATED AND IApr 14, 1996 · N959R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA96038Frame · misdrilledKMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=300 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R05 AND IAW DC-8 SRM 51-1-20D. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96037Frame · misdrilledKMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=660 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R05 AND IAW DC-8 SRM 53-2-0. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96036Frame · misdrilledKMCN - DURING C-CHECK, FOUND HOLE DRILLED THROUGH FRAME AT Y=1040 ABOVE LONGERON 21 LEFT. FABRICATED INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R-5 AND IAW DC-8 SRM 51-1-20D. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96035Frame · misdrilledKMCN - DURING C-CHECK, FOUND HOLES DRILLED IN MAIN FRAME AT Y=940 ABOVE LONGERON 21 LEFT SIDE. FABRICATED, INSTALLED REPAIR IAW APPROVED COTNEY ENGINEERING SKETCH A46-R06 AND IAW DC8 SRM 51-1-20D. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96026Pressure Web · corrodedKMCN - DURING C-CHECK, FOUND CORROSION ON UPPER WHEEL WELL WEB AT Y=879.375, FROM X=57 TO X=66 AND Z=10. CORROSION REMOVED, REQUIRED CUTTING PRESSURE WEB CUSP ANGLE AND HAT CHANNEL. REMOVED DAMAGE AREAS OF PRESS WEB, FABRICATED AND INSTALLED REPAIRS TO WEB CApr 12, 1996 · N959R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA96022Frame · misdrilledZIAD - DURING C-CHECK, FOUND HOLE DRILLED IN FRAME AT Y=759 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R07 AND IAW DC-8 SRM 53-2-0, 53-7-3. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96021Frame · misdrilledKMCN - DURING C-CHECK, FOUND HOLES DRILLED IN FRAME AT Y=879 ABOVE LONGERON 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW DER APPROVED COTNEY ENGINEERING SKETCH A46-R06 AND DC-8 SRM 51-1-20D. (M)Apr 12, 1996 · N959R · Doug DC863F · Fuselage Main, FrameSDR RRXA96029Fitting · crackedKMCN - DURING C-CHECK, FOUND LEFT MLG SUPPORT FITTING CRACKED. CONFIRMED WITH DYE CHECK AND EDDY CURRENT. REMOVED REPLACED LEFT MLG SUPPORT FITTING IAW DC-8 SRM 51-3-0 AND DACO MLG FITTING REPLACEMENT GUIDE. (M)Apr 11, 1996 · N959R · Doug DC863F · Wing, Landing Gear Attach FittingsSDR 95ZZZM658Door · out of adjustFLT MAC 111 - OMFJ-LICZ - AIRCRAFT EXPERIENCED RAPID DE-PRESSURIZATION AT FL 390. CABIN ALTITUDE STABILIZED AT 13,500 FEET. MAX CABIN DIFFERENTIAL AT 6.6 PSI. PERFORMED CHECKLIST IAW QRH. MAINTENANCE FOUND THE FORWARD AIR CONDITIONING ACCESS DOOR OUT OF ADOct 23, 1995 · N959R · Doug DC863F · Air Conditioning DoorsSDR 95ZZZX3972Jamb · crackedMAIN CARGO DOOR LOWER AFT DOOR, THRESHOLD HAS A CRACK. REPAIRED CRACKED CORNER FILLET AT MAIN CARGO DOOR JAMB, AFT LOWER CORNER IAW TIMCO REO DC08-53-1565.Jun 14, 1995 · N959R · Doug DC863F · Fuselage Miscellaneous Structure
Back to N959R, cancelled Apr 24, 2002