# Service difficulty reports: N964R, cancelled Dec 17, 2002 A list on [N964R, cancelled Dec 17, 2002](https://openairdocs.org/deregistered/N964R-2002-12-17.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 2 · 82 reports - [SDR RRXA99190](https://openairdocs.org/sdr/RRXA99190.md): Compressor · stalled · Mar 29, 1999 · N964R · Doug DC863 · Turbine Engine Compressor Section > AT 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 RRXA99600](https://openairdocs.org/sdr/RRXA99600.md): Skin · corroded · Feb 1, 1999 · N964R · Doug DC863 · Wing, Plate/Skin > DURING 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 R - [SDR RRXA99998](https://openairdocs.org/sdr/RRXA99998.md): Skin · damaged · Dec 15, 1998 · N964R · Doug DC863 · Cargo/Baggage Doors > DURING 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 APPR - [SDR RRXA99981](https://openairdocs.org/sdr/RRXA99981.md): Flange · damaged · Dec 11, 1998 · N964R · Doug DC863 · Wing Miscellaneous Structure > DURING 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 APPROVE - [SDR RRXA99977](https://openairdocs.org/sdr/RRXA99977.md): Frame · misdrilled · Dec 10, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98592](https://openairdocs.org/sdr/RRXA98592.md): Floorbeam · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Floor Beam > DURING 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 RRXA98591](https://openairdocs.org/sdr/RRXA98591.md): Web · corroded · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Miscellaneous Structure > DURING 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 RRXA98590](https://openairdocs.org/sdr/RRXA98590.md): Frame · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98589](https://openairdocs.org/sdr/RRXA98589.md): Pan · cracked · Nov 19, 1998 · N964R · Doug DC863 · Passenger/Crew Doors > DURING 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 RRXA98588](https://openairdocs.org/sdr/RRXA98588.md): Frame · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98587](https://openairdocs.org/sdr/RRXA98587.md): Longeron · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Longeron/Stringer > DURING 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 ENGINEER - [SDR RRXA98586](https://openairdocs.org/sdr/RRXA98586.md): Skin · gouged · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Plate/Skin > DURING 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 RRXA98585](https://openairdocs.org/sdr/RRXA98585.md): Frame · corroded · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98584](https://openairdocs.org/sdr/RRXA98584.md): Skin · dented · Nov 19, 1998 · N964R · Doug DC863 · Elevator, Plate/Skin > DURING 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 RRXA98583](https://openairdocs.org/sdr/RRXA98583.md): Frame · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 D - [SDR RRXA98582](https://openairdocs.org/sdr/RRXA98582.md): Rib · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Wing, Rib/Bulkhead > DURING 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 RRXA98581](https://openairdocs.org/sdr/RRXA98581.md): Longeron · corrosion · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Longeron/Stringer > DURING 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 RRXA98580](https://openairdocs.org/sdr/RRXA98580.md): Web · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Miscellaneous Structure > DURING 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 RRXA98579](https://openairdocs.org/sdr/RRXA98579.md): Frame · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98578](https://openairdocs.org/sdr/RRXA98578.md): Skin · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Cargo/Baggage Doors > DURING 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 RRXA98577](https://openairdocs.org/sdr/RRXA98577.md): Frame · misdrilled · Nov 19, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98576](https://openairdocs.org/sdr/RRXA98576.md): Spar · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Wing Spar > DURING 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 RRXA98575](https://openairdocs.org/sdr/RRXA98575.md): Frame · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98574](https://openairdocs.org/sdr/RRXA98574.md): Frame · cracked · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98573](https://openairdocs.org/sdr/RRXA98573.md): Frame · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98572](https://openairdocs.org/sdr/RRXA98572.md): Frame · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98571](https://openairdocs.org/sdr/RRXA98571.md): Floorbeam · damaged · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Floor Beam > DURING 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 RRXA98570](https://openairdocs.org/sdr/RRXA98570.md): Frame · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98569](https://openairdocs.org/sdr/RRXA98569.md): Longeron · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Longeron/Stringer > DURING 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 RRXA98568](https://openairdocs.org/sdr/RRXA98568.md): Splice · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Wing Miscellaneous Structure > DURING 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 RRXA98567](https://openairdocs.org/sdr/RRXA98567.md): Frame · misdrilled · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 RRXA98566](https://openairdocs.org/sdr/RRXA98566.md): Skin · cracked · Nov 18, 1998 · N964R · Doug DC863 · Fuselage Main, Plate/Skin > DURING 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 RRXA98565](https://openairdocs.org/sdr/RRXA98565.md): Angle · chafed · Nov 18, 1998 · N964R · Doug DC863 · Wing Miscellaneous Structure > DURING 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 RRXA98564](https://openairdocs.org/sdr/RRXA98564.md): Frame · cracked · Nov 17, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 R - [SDR RRXA99994](https://openairdocs.org/sdr/RRXA99994.md): Frame · misdrilled · Nov 12, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 INSTAL - [SDR RRXA99974](https://openairdocs.org/sdr/RRXA99974.md): Skin · misrepaired · Nov 11, 1998 · N964R · Doug DC863 · Wing, Plate/Skin > DURING 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 TI - [SDR RRXA99971](https://openairdocs.org/sdr/RRXA99971.md): Bushing · mismanufactured · Nov 10, 1998 · N964R · Doug DC863 · Landing Gear Retraction/Extension System > DURING 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 B - [SDR RRXA99970](https://openairdocs.org/sdr/RRXA99970.md): Rail · mismanufactured · Nov 9, 1998 · N964R · Doug DC863 · Engine Thrust Reverser > DURING 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 N - [SDR RRXA99989](https://openairdocs.org/sdr/RRXA99989.md): Frame · misdrilled · Nov 6, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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 APPRO - [SDR RRXA99972](https://openairdocs.org/sdr/RRXA99972.md): Strut · corroded · Nov 3, 1998 · N964R · Doug DC863 · Main Landing Gear Strut/Axle/Truck > DURING 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 ENGI - [SDR RRXA99986](https://openairdocs.org/sdr/RRXA99986.md): Bulkhead · corroded · Oct 30, 1998 · N964R · Doug DC863 · Fuselage Main, Bulkhead > DURING 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 TIMCO - [SDR RRXA99975](https://openairdocs.org/sdr/RRXA99975.md): Bushing · gouged · Oct 30, 1998 · N964R · Doug DC863 · Landing Gear Retraction/Extension System > DURING 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 SKE - [SDR RRXA99973](https://openairdocs.org/sdr/RRXA99973.md): Floorbeam · misdrilled · Oct 29, 1998 · N964R · Doug DC863 · Fuselage Main, Floor Beam > DURING 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 A - [SDR RRXA99987](https://openairdocs.org/sdr/RRXA99987.md): Fitting · misdrilled · Oct 28, 1998 · N964R · Doug DC863 · Fuselage Miscellaneous Structure > DURING 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 AP - [SDR RRXA99980](https://openairdocs.org/sdr/RRXA99980.md): Hinge · damaged · Oct 23, 1998 · N964R · Doug DC863 · Ailerons > DURING 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 EN - [SDR RRXA99985](https://openairdocs.org/sdr/RRXA99985.md): Bulkhead · misdrilled · Oct 22, 1998 · N964R · Doug DC863 · Fuselage Main, Bulkhead > DURING 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 ENGINEERI - [SDR RRXA99978](https://openairdocs.org/sdr/RRXA99978.md): Web · cut · Oct 22, 1998 · N964R · Doug DC863 · Fuselage Main, Structure > DURING 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 REP - [SDR RRXA99982](https://openairdocs.org/sdr/RRXA99982.md): Frame · misdrilled · Oct 21, 1998 · N964R · Doug DC863 · Fuselage Main, Frame > DURING 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. F - [SDR 98ZZZX4166](https://openairdocs.org/sdr/98ZZZX4166.md): Beam · cracked · Oct 21, 1998 · N964R · Doug DC863 · Fuselage Miscellaneous Structure > AT 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 OPE - [SDR 98ZZZX4165](https://openairdocs.org/sdr/98ZZZX4165.md): Beam · cracked · Oct 21, 1998 · N964R · Doug DC863 · Fuselage Miscellaneous Structure > AT 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 Next page: https://openairdocs.org/deregistered/N964R-2002-12-17/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 = 'N964R' AND deregistration_id = 'N964R-2002-12-17' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N964R-2002-12-17/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.