N964R, cancelled Dec 17, 2002
Service difficulty reports · 82
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 = 'N964R' AND deregistration_id = 'N964R-2002-12-17' 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.
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 = 'N964R' AND deregistration_id = 'N964R-2002-12-17' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR RRXA99190Compressor · stalledAT ROTATION EXPERIENCED COMPRESSOR STALLS NR 4 ENG. RETARTED ENGINE, 30 SECONDS LATER ENGINE FAILED. NO FIRE, PERFORMED EMERGENCY FIRE AND DAMAGE SHUT DOWN. REMOVED AND REPLACED NR 4 ENG IAW EWA MEL 77. OPS CKS LEAK, CKS GOOD.SDR RRXA99600Skin · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO THE LEFT WING, LEADING EDGE, SKIN SCREW HOLES AT XFS 708 TO XFS 710, 2 INCHES BELOW TOP. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED RSDR RRXA99998Skin · damagedDURING A MAINTENANCE VISIT, FOUND DRILL DAMAGE, INNER SKIN OF MAIN CARGO DOOR, NUMEROUS AREAS. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPLACEMENT INNER SKIN PANEL AND WEB IAW FAA APPRSDR RRXA99981Flange · damagedDURING A MAINTENANCE VISIT, FOUND OVERSIZED HOLES IN AFT UPPER SPAR FLANGE ON RIGHT WING BETWEEN XRS= 436.500 AND XRS = 456.563. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. OVERSIZED HOLES APPROVED IAW FAA APPROVESDR RRXA99977Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND FRAMES AT STA= 1200 AND STA= 1220 INNER FLANGE HAD MISDRILLED HOLES BETWEEN LONGERONS 18 RIGHT AND LONGERON 20 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. INSTALLED FREEZE SDR RRXA98592Floorbeam · misdrilledDURING MAINTENANCE VISIT, FOUND FLOORBEAM AT FS 1700 WITH MISDRILLED HOLES IN UPPER HORIZONTAL FLANGE. REMOVED DAMAGED SECTION, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND FILLERS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH SDR RRXA98591Web · corrodedDURING MAINTENANCE VISIT, FOUND FORWARD PRESSURE WEB WITH CORROSION BETWEEN STA 9 AND 12. REMOVED DAMAGED AREA, TREATED IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05707.SDR RRXA98590Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAMS FS 1200 AND 1220 WITH MISDRILLED HOLES. REMOVED DAMAGED AREAS, TREATED AREAS IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05696.SDR RRXA98589Pan · crackedDURING MAINTENANCE VISIT, FOUND LEFT FORWARD ENTRY DOOR PAN CRACKED AT LOWER FORWARD CORNER. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05648, AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98588Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME FS 940 WITH MISDRILLED HOLES AT VERIOUS LOCATIONS. REMOVED DAMAGED AREAS, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APPROVED TIMCO SKETCH REO-05618.SDR RRXA98587Longeron · misdrilledDURING MAINTENANCE VISIT, FOUND LONGERONS AT FS 160 AND 180 WITH MISDRILLED HOLES IN LONGERONS 25, 26, 27 AND 28 LEFT. REMOVED DAMAGED AREA, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLES AND STRAPS IAW FAA DER APPROVED TIMCO ENGINEERSDR RRXA98586Skin · gougedDURING MAINTENANCE VISIT, FOUND SKIN GOUGED AT FS 1395 AT LONGERON 27 RIGHT. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05604, AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98585Frame · corrodedDURING MAINTENANCE VISIT, FOUND FRAME FS 380 WITH CORROSION IN FASTENER HOLE AT LONGERON 34 LEFT. REMOVED CORROSION, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR BUSHING AND STRAP IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05598.SDR RRXA98584Skin · dentedDURING MAINTENANCE VISIT, FOUND LT ELEVATOR UPPER SKIN AT STA XE=200 DENTED BEYOND LIMITS. REMOVED DAMAGES AREA, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05594, AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98583Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 520 WITH MISDRILLED HOLES BETWEEN LONGERONS 6 AND 9 RIGHT AND AT LONGERON 20 LEFT. FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND SHIMS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05591, AREA TREATED IAW DSDR RRXA98582Rib · misdrilledDURING MAINTENANCE VISIT, FOUND LT WING LEADING EDGE RIB WITH MISDRILLED HOLE AT WS XFS 540. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05589, AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98581Longeron · corrosionDURING MAINTENANCE VISIT, FOUND LONGERON 8 LEFT WITH CORROSION AT FS 1734. REMOVED DAMAGED AREA, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR ANGLE AND STRAPS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05583.SDR RRXA98580Web · misdrilledDURING MAINTENANCE VISIT, FOUND WEB AT FS 1180 AND FS 1220 BETWEEN LONGERONS 19 AND 21 RIGHT WITH MISDRILLED HOLES. FABRICATED AND INSTALLED DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05582, AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98579Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 260 WITH MISDRILLED HOLES BETWEEN LONGERONS 35 LEFT AND 35 RIGHT. REMOVED DAMAGED AREAS AS REQUIRED, FABRICATED AND INSTALLED REPAIR ANGLES, STRAPS AND SHIMS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05580, SDR RRXA98578Skin · misdrilledDURING MAINTENANCE VISIT, FOUND UPPER DECK MAIN CARGO DOOR LOWER INNER SKIN WITH MISDRILLED HOLES AT FS 211.97. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05572, AREAS TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98577Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 834 WITH MISDRILLED HOLES AT VARIOUS LOCATIONS. FABRICATED AND INSTALLED REPAIRS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05568, AREAS TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98576Spar · misdrilledDURING MAINTENANCE VISIT, FOUND LT WING LOWER FRONT SPAR FORWARD FLANGE WITH MISDRILLED HOLES BETWEEN WS XFS 417 AND XFS 424. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05566 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA98575Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 920 WITH MISDRILLED HOLES AT VERIOUS LOCATIONS. FABRICATED AND INSTALLED REPAIRS IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05555 AND TREATED AREAS IAW DC-8 SRM 51-1-8.SDR RRXA98574Frame · crackedDURING MAINTENANCE VISIT, FOUND FRAME AT FS 965 AT MLG DOOR JAMB CRACKED FROM FASTENER HOLE TO EDGE OF PART. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05553 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA98573Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 700 WITH MISDRILLED HOLE BETWEEN LONGERONS 5 AND 6 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05550 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98572Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 717 WITH MISDRILLED HOLE BETWEEN LONGERONS 20 AND 21 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05546 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98571Floorbeam · damagedDURING MAINTENANCE VISIT, FOUND FLOORBEAM UPPER FLANGE AT FS 960 WITH DRILL NICK AT 5.75 INCHES INBOARD OF LT CUSP. BLENDED AND REPAIRED IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05539 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA98570Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 1140 WITH MISDRILLED HOLES BETWEEN LONGERONS 31 AND 33 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05530 AND TREATED AREA IAW DC-8 SRM 51-1-8.SDR RRXA98569Longeron · misdrilledDURING MAINTENANCE VISIT, FOUND LONGERON 25 RIGHT AT FS 280 WITH MISDRILLED HOLES. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05520 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98568Splice · misdrilledDURING MAINTENANCE VISIT, FOUND SPLICE WITH DRILL DAMAGE ON LT WING L/E AT STA XW 257. REMOVED DAMAGED SPLICE, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05507 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98567Frame · misdrilledDURING MAINTENANCE VISIT, FOUND FRAME AT FS 1120 WITH MISDRILLED HOLES BETWEEN LONGERONS 30 AND 33 LEFT. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05506 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98566Skin · crackedDURING MAINTENANCE VISIT, FOUND INTERNAL SKIN CRACKED AT FS 940 ABOVE LONGERON 24R. FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05492 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98565Angle · chafedDURING MAINTENANCE VISIT FOUND ANGLE CHAFED EXCEEDING ALLOWABLE LIMITS ON LEFT WING INBOARD T/E STRUCTURE AT WING STA XWS-12. REPLACED ANGLE IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH REO-05479 AND AREA TREATED IAW DC-8 SRM 51-1-8.SDR RRXA98564Frame · crackedDURING MAINTENANCE VISIT, FOUND FRAME FS 70 CAP CRACKED AT LONGERON 20 RIGHT AND DRILL DAMAGE AT LONGERON 13 TO 15 RIGHT. REMOVED DAMAGED AREAS, TREATED AREA IAW DC-8 SRM 51-1-8, FABRICATED AND INSTALLED REPAIR IAW FAA DER APPROVED TIMCO ENGINEERING SKETCH RSDR RRXA99994Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND MISDRILLED HOLES, FRAME UPPER FUSELAGE, AT STA= 940, LONGERON 7 LEFT, COMMON TO INBOARD FLANGE IN THE CABIN AREA. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALSDR RRXA99974Skin · misrepairedDURING A MAINTENANCE VISIT, FOUND CORROSION, NUMEROUS BLENDOUTS, RIGHT WING LOWER SKIN BEAVER TAIL DOUBLER. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED TISDR RRXA99971Bushing · mismanufacturedDURING A MAINTENANCE VISIT, FOUND BUSHING, LT MLG RETRACT PIN BOSS HOLD, BRUSH CAD PLATED IN PLACE OF DIP CAD PLATED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. ACCEPTABLE CAD PLATE BUSHING IAW FAA APPROVED TIMCO DER ENGINEERING SKETCH REO NR 057772 PROVIDED BY BSDR RRXA99970Rail · mismanufacturedDURING A MAINTENANCE VISIT, FOUND COUNTERBORES WERE MACHINED OVERSIZE, NR 1 THRUST REVERSER RAIL, UPPER TRACK, (P/N 5753399-1). DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED RAIL AND INSTALLED IAW DAC DWG NSDR RRXA99989Frame · misdrilledDURING A MAINTENANCE VISIT, FOUND 3 EACH DRILLED HOLES CLOSE TO RADIUS ON FRAME AT STA= 280 AT LONGERON 25 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER IAW FAA APPROSDR RRXA99972Strut · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, LANDING GEAR WHEEL, RETRACT PIN BOSS, SHOCK STRUT, LT MLG. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 5-1-1-8. FABRICATED AND INSTALLED BUSHING IAW FAA APPROVED TIMCO DER ENGISDR RRXA99986Bulkhead · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION, FUSELAGE, AFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIRED DOUBLER TO BULKHEAD WEB IAW FAA APPROVED TIMCOSDR RRXA99975Bushing · gougedDURING A MAINTENANCE VISIT, FOUND GOUGED AND PITTING, BUSHING-FLANGED, PIVOT AXIS, MAIN LANDING GEAR. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. BLENDOUT LIMITS APPROVED IAW FAA APPROVED TIMCO DER ENGINEERING SKESDR RRXA99973Floorbeam · misdrilledDURING A MAINTENANCE VISIT, FOUND FLOORBEAM, AT STA= 1700, UPPER HORIZ FLANGES HAS MISDRILLED HOLES ENTIRE LENGTH OF FLOORBEAM. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED REPAIR AND INSTALLED IAW FAA ASDR RRXA99987Fitting · misdrilledDURING A MAINTENANCE VISIT, FOUND (1) DISCREPANT HOLE (3/16) DIA LOCATED ON EDGE OF FITTING 6 ABOVE RT CUSP AT STA= 798. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APSDR RRXA99980Hinge · damagedDURING A MAINTENANCE VISIT, FOUND HINGE FITTING, LEFT OUTBD AILERON, 2014-T6 FORG REQUIRED TO BE REPLACED. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED FITTING IAW FAA APPROVED TIMCO DER ENSDR RRXA99985Bulkhead · misdrilledDURING A MAINTENANCE VISIT, FOUND TRIPLE DRILLED RTAFT PRESS BULKHEAD, AT STA= 1766. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. REPAIRED MISDRILLED HOLES BY RIVET INSTALLATION IAW FAA APPROVED TIMCO DER ENGINEERISDR RRXA99978Web · cutDURING A MAINTENANCE VISIT, FOUND FWD CARGO CROSS SLID WEB CUT TO FACILITATE OTHER MAINTENANCE AT STA= 295 AND STA= 325 AT LONGERON33 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FABRICATED AND INSTALLED REPSDR RRXA99982Frame · misdrilledDURING A MAINTENANCE VISIT FOUND DOUBLE DRILLED HOLE ON FRAME, AT STA= 717 BETWEEN LONGERONS 20 LEFT AND LONGERON 21 LEFT AND LONGERONS 20 RIGHT AND LONGERON 21 RIGHT. DAMAGE EXCEEDED LIMITS IAW DC-8 SRM. REMOVED DAMAGED, TREATED AREA IAW DC-8 SRM 51-1-8. FSDR 98ZZZX4166Beam · crackedAT D-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROX 1 INCH EACH SIDE OF THE ACFT CENTERLINE. THE CRACKS APPEAR TO OCCUR UNDER NORMAL OPESDR 98ZZZX4165Beam · crackedAT D-CHECK, CRACKS WERE FOUND IN THE J-BEAM WHICH IS ATTACHED TO THE AFT FACE OF THE AFT PRESSURE BULKHEAD. THE CRACKS ORIGINATE IN THE RADII ADJACENT TO ATTACH BOLTS APPROXIMATELY 1 INCH EACH SIDE OF THE AIRCRAFT CENTERLINE. THE CRACKS APPEAR TO OCCUR UNDER
Back to N964R, cancelled Dec 17, 2002