N921R, cancelled Feb 16, 2011

Service difficulty reports · 80

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 = 'N921R' AND deregistration_id = 'N921R-2011-02-16'
  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 N921RM81664Skin · cracked"D" PIT DOOR DAMAGED FORWARD UPPER SKIN AT CORNER. APPROX .375 INCH CRACK RADIATED FROM EDGE OF FUSELAGE SKIN IN DOOR RADIUS AND TERMINATED AT FIRST FASTENER.Oct 26, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R63501Skin · dentedFOUND FUSELAGE EXTERIOR STA 78 BTW L17L AND L18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000 0551.Jan 9, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R63504Skin · dentedFOUND FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L SKIN WITH DENT. REPAIRED SKIN OF FUSELAGE EXTERIOR STA 78 BTW L-17L AND L-18L IAW DC8 SRM 53-2-0, TR NR 53-170 CPCP 5000-0551.Jan 9, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R54017Splice · corrodedLWR FUSELAGE EXTERIOR STA 1766 L-33L MANUFACTURING SPLICE WITH CORROSION. REMOVED SPLICE IAW DPS 3.67.27, FABRICATED NEW SPLICE IAW DC8 SRM 53-4-1 AND DPS 3.69.4. PRIMED NEW SPLICE IAW DC8 SRM 51-1-8 AND INSTALLED NEW SPLICE IAW DC8 SRM 51-1-21 CPCP 5000 055Jan 8, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R54815Skin · dentedLT WING XW 68 INBOARD FLAP TRAILING EDGE LOWER SURFACE WITH DENT ( L=3 1/8, A=2 1/2, Y=.0935). CUTOUT DAMAGED AREA AND FABRICATED FILLER, SPLICE AND SKIN IAW DC8 SRM 57-2-5 AND DC8 SRM 57-7-1. TREATED AND PRIMED REPAIR AREA AND PARTS IAW DC8 SRM 51-1-8. INSJan 8, 2007 · N921R · Doug DC863F · Trailing Edge FlapsSDR N921R53410Door Frame · crackedFUSELAGE STA 8 NLG W/W DOOR JAMB RT CORNER SKIN WITH 1" CRACK. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 51-07030-1 REV NEW 01-25-07 PAGE 1 AND 2. ISSUED FAA FORM 8110-3 CPCP 4000 0551.Jan 8, 2007 · N921R · Doug DC863F · Fuselage Main, StructureSDR N921R53309None · noneFUSELAGE STA 8 NLG WW DOOR JAMB LT CORNER SKIN WITH TEMPORARY REPAIR. REPAIRED SKIN IAW FLIGHT VEHICLES CONSULTING INC DWG NR 53-07030-1 REV NEW 01-25-09 PAGE 1/3. ISSUED FAA FORM 8110-3. CPCP 4000 0551Jan 8, 2007 · N921R · Doug DC863F · Standard Practices/StructuresSDR N921R53506Skin · damagedFUSELAGE STA 32 NLG DOOR SKIN HAS 2 NICKS. REPAIRED SKIN OF FUSELAGE STA 32 NLG RT DOOR IAW DC8 SRM 52-2-0 CPCP 4000 0551.Jan 8, 2007 · N921R · Doug DC863F · Landing Gear DoorsSDR N921R53905Skin · corrodedLOWER FUSELAGE EXTERIOR STA 720 L-17L SKIN WITH CORROSION. OPENED SKIN AREA IAW DPS 3-67-27, FOUND CORRODED INNER DOUBLER, REMOVED INNER DOUBLER IAW DPS 3-67-27. FABRICATED NEW INNER DOUBLER IAW DC8 SRM 53-5-3 & DPS 3-69-4. TREATED AND PRIMED AREA AND NEW DJan 8, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R50502Skin · dentedRUDDER ZR 138 LEFT SKIN AFT SECTION WITH DENT. REMOVED LT SKIN SECTION IAW DPS 3.67-27. FABRICATED NEW SKIN IAW DPS 3.69-4. TREATED AND PRIMED AREA AND NEW SKIN IAW DC8 SRM 51-1-8. INSTALLED NEW SKIN IAW DC8 SRM 51-1-21.Jan 6, 2007 · N921R · Doug DC863F · Rudder, Plate/SkinSDR N921R40407Frame Splice · corrodedMAIN CARGO COMPARTMENT STA 520, L-17R FRAME SPLICE WITH CORROSION. REMOVED FRAME SPLICE IAW DPS 3-67-29. FABRICATED NEW FRAME SPLICE IAW DPS 3-69-4, PRIMED SPLICE IAW DC8 SRM 51-1-8. INSTALLED FRAME SPLICE IAW DC8 SRM 51-1-27 CPCP 5730-0551.Jan 5, 2007 · N921R · Doug DC863F · Fuselage Main, FrameSDR N921R28116Stringer Splice · crackedFWD CARGO COMPARTMENT BTW STA 440 AND 460, L31L SPLICE FITTING WITH 3/4" CRACK. REMOVED AND REPLACED SPLICE FITTING OF FWD CARGO COMPARTMENT BTW STA 440 AND STA 460, L31L IAW DC8 SRM 51-1-20 AND SRM 53-4-1 CPCP 557L 0551.Jan 4, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/StringerSDR N921R28211Finger Doubler · corrodedFWD CARGO COMPARTMENT STA. 480, L31R FINGER DOUBLER WITH CORROSION. CLEANED CORROSION IAW DC8 SRM 51-1-8. FOUND TO BE WITHIN LIMITS IAW DC8 SRM 53-2-0. TREATED & PRIMED AREA IAW DC8 SRM 51-1-8 CPCP 557R 0551.Jan 4, 2007 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR N921R72213Longeron · corrodedFOUND FUSELAGE STA 1540 L29L SKIN RIVETS SHEARED AND LONGERON 29L WITH CORROSION. REPAIRED LONGERON 29L AT FS 1540 IAW DC8 SRM 53-2-2 FIGURE 8.Jan 3, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/StringerSDR N921R19512Stringer Splice · crackedFOUND MAIN CARGO COMPARTMENT STA 680, L4R AFT SPLICE FITTING WITH CRACK. REMOVED AND REPLACED FITTING IAW DC8 SRM 51-1-20 AND 53-4-1 CPCP 5730-0553.Jan 3, 2007 · N921R · Doug DC863F · Fuselage Main, Longeron/StringerSDR U2RA3201Skin · corrodedTOP OF LT MAIN LANDING GEAR TOP SURFACE CORRODED APPROXIMATELY 1 X 4 INCHES AT STATION 860, LBL 40 TO LBL 44.May 24, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR U2RA3218Frame · damagedFUSELAGE FRAME DAMAGED AT STATION 1560, L21L.May 23, 2005 · N921R · Doug DC863F · Fuselage Main, FrameSDR U2RA3142Pressure Panel · corrodedFS 980 TO FS 970 TOP SURFACE OF THE RIGHT MAIN LANDING GEAR WELL HAS POPPED RIVETS/BULGING AT ATTACH ANGLE, IDENTIFIED AS LEVEL 2 CORROSION.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR U2RA3147Frame · corrodedSEVERAL SMALL AREAS OF CORROSION IN FWD ACCESSORY COMPARTMENT AT AFT BULKHEAD CIRCUMFERENTIAL FS 80 L32L TO L32R. IDENTIFIED AS LEVEL 2 CORROSION.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, FrameSDR U2RA2962Finger Doubler · corrodedRIVET HEAD POPPED FS 200, RT SIDE OF THE AIRCRAFT BELOW THE AUX STATIC PORT IDENTIFIED AS LEVEL 2 CORROSION.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR U2RA3216Fitting · crackedFITTING CRACKED AFT OF CARGO DOOR AT FS 300 AT CUSP LT SIDE.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Attach FittingsSDR U2RA3399Stringer · crackedRIGHT WING LOWER INNER STRINGER CRACKED AT WING STATION X624.May 10, 2005 · N921R · Doug DC863F · Wing, Longeron/StringerSDR U2RA3140Fitting · crackedLONGERON 24 LT AFT BATHTUB FITTING CRACKED AT FS 1690.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Attach FittingsSDR U2RA3396Skin · crackedR2 DOOR HAS CRACK INDICATION AT UPPER AFT CORNER FS 1660, L11R.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR U2RA2982Skin · corrodedFS 12 IN NOSE WHEEL WELL CEILING SKIN BULGING WITH 3 POPPED RIVETS, IDENTIFIED AS LEVEL 2 CORROSION.May 10, 2005 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR 2039Skin Panel · crackedDURING REPETITIVE INSPECTION OF A/D 2000-20-08 ON LEFT FRONT PAX ENTRANCE DOOR LOWER FORWARD CORNER, VISUALLY DETECTED FUSELAGE SKIN CRACK EXTENDING OUTWARD FROM DOOR RADIUS 1.5 INCH.May 22, 2004 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR 2025Oil Filter · leakingSHUTDOWN NR 2 ENGINE CLIMBING OUT OF ILG AT FL240 AT 1220Z OIL QUANTITY DROPPED TO 1 GALLON, WINDMILLING OIL PRESSURE 20 PSI.May 13, 2004 · N921R · Doug DC863F · Engine Oil QuantitySDR 2006Track · damagedPOST FLIGHT INSPECTION NR 2 THRUST REVERSER AND TRANSLATING RING DAMAGED.LOWER T/R TRACK STOP AND ATTACHING HARDWARE MISSING. DOUGLAS SERVICE BULLETIN 78-100 IDENTIFIES THIS PROBLEM.Apr 23, 2004 · N921R · Doug DC863F · Engine Thrust ReverserSDR 1982Wire · shortedNR 1 ENGINE OIL PRESSURE WARNING LIGHT ILLUMINATED. PERFORMED PRECAUTIONARY SHUTDOWN NR 1 ENGINE AT 2245Z, OIL PRESSURE 45PSI,OIL TEMP 95 DEGREES C, WINDMILLING OIL PRESSURE 32 PSI.Mar 18, 2004 · N921R · Doug DC863F · Engine Oil PressureSDR 1965Crank Assy · fracturedFLIGHT CREW REPORTED WING SLOT LIGHT ON WITH FLAPS EXTENDED. FOUND RIGHT AHND EXTENDED LEADING OOUTBOARD SLOT DOOR INOPERATIVE DUE TO FRACTURED AND BROKEN CRANK ASSEMBLY AT STA.XS476Feb 28, 2004 · N921R · Doug DC863F · Leading Edge Slat Control SystemSDR U2R2004F00001Fastener · mismanufacturedREPAIRED L2 DOOR AT LOWER FORWARD CORNER FS1620 IAW MM.Oct 29, 2003 · N921R · Doug DC863F · FastenersSDR U2R2004F00000Spar Cap · crackedDURING REPETIVE COMPLIANCE WITH AD AND SB, DETECTED 2 CRACKS AT RT WING FRONT SPAR LOWER CAP, REPAIRED IAW SB. REMAINING HOLES STRESS COINED TO CONDITION 1, OPTION 2.Oct 29, 2003 · N921R · Doug DC863F · Wing SparSDR U2RB102903Spar Cap · crackedDURING REPETITIVE COMPLIANCE WITH A/D 2001-06-02 & S/B 57-90 R5 DETECTED 2 EACH CRACK INDICATIONS IN NON ADJACENT ATTACHMENT HOLES OF THE FORWARD LEG OF THE RIGHT WING FRONT SPAR LOWER CAP. REPAIRED 2 EACH CRACKED HOLES IAW DC-8 S/B 57-90 R5 TABLE 4, CONDITIOOct 29, 2003 · N921R · Doug DC863F · Wing SparSDR 20010124SG002Compressor · overservicedON TEST FLIGHT, SMOKE IN COCKPIT. FOUND NR 2 AND NR 3 TURBO COMPRESSORS OVERSERVICED. SERVICED PROPERLY IAW MM 21-10-01. (M)Dec 13, 2000 · N921R · Doug DC863F · Cabin Compressor SystemSDR RRXA99803Control Cable · unsecureLANDING GEAR WOULD NOT RETRACT AFTER TAKEOFF. NO ATTEMPT AT HANDLE LATCH FLIGHT RELEASE. FOUND LANDING GEAR ANTI RETRACTION CABLE NOT SECURE, SECURED SAME LDG GEAR HANDLE AND GEAR OPS NORMAL ON GRD CK.May 20, 1999 · N921R · Doug DC863F · Landing Gear Retraction/Extension SystemSDR RRXA98270Wheel · broke offON LANDING, THE NR 1 MLG WHEEL AND TIRE ASSEMBLY BROKE FROM AXLE. TIRE ASSEMBLY ROLLED INTO PARKED EQUIPMENT. AIRCRACFT WAS TOWED TO RAMP FOR INSPECTION. *S/D* REMOVED AND REPLACED NR 1 MAIN WHEEL AND TIRE ASSEMBLY, REPLACED NR 1 MAIN BRAKE ASSEMBLY, REPLAJul 20, 1998 · N921R · Doug DC863F · Wheel/Ski/FloatSDR RRXA97321Floorbeam · corrosionDURING A MAINTENANCE VISIT, FOUND FLOORBEAM CORRODED BEYOND LIMITATIONS IAW DC-8 SRM AT STA 920.57 LEFT. FABRICATED AND INSTALLED REPAIR ANGLE IAW FAA APPROVED COTNEY ENGINEERING SKETCH D02-R04. TREATED AREA IAW DC-8 SRM 51-1-8.Dec 14, 1997 · N921R · Doug DC863F · Fuselage Main, Floor BeamSDR RRXA97265Pressure Web · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE UNDER FINGER DOUBLER ATTACH TO PRESSURE WEB AT, STA 974 AND BL 65 RIGHT SIDE. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R16 ANSep 12, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA97262Longeron · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE ON LONGERON 31 LEFT AT, STA 163 TO STA 170. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R17 AND DC-8 SRM 51-1-8, 51-1-21 AND 53-2Sep 12, 1997 · N921R · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA97263Beam · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE TO AFT PRESSURE BULKHEAD VERTICAL BEAM AT STA 1754 RIGHT SIDE, LOWER AFT FACE. *S/D* REMOVED CORROSION DAMAGE, FABRICATED AND INSTALLED REPAIR ANGLES IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R18. Sep 11, 1997 · N921R · Doug DC863F · Fuselage Main, StructureSDR RRXA97256Support · corrodedDURING A MAINTENANCE VISIT, FOUND CORROSION DAMAGE PAST LIMITATIONS ON FLOOR SUPPORT AT, STA 1660 AND BL 33 RIGHT. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED (2 EACH) FILLERS AND DOUBLERS IAW FAA DER APPROVED ENGINEERING SKETCH D02-R15 AND DC-8Sep 4, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA97264Longeron · crackedDURING A MAINTENANCE VISIT, FOUND CRACK ON LONGERON 34 RIGHT AT, STA 1270. *S/D* REMOVED LONGERON 34R, FABRICATED AND INSTALLED REPAIR SPLICE IAW FAA DER APPROVED COTNEY ENGINEERING SKETCH D02-R09.Sep 3, 1997 · N921R · Doug DC863F · Fuselage Main, Longeron/StringerSDR RRXA97319Skin · damagedDURING A MAINTENANCE VISIT, FOUND FUSELAGE OUTER SKIN BENT AND DAMAGED BELOW A PIT DOOR BETWEEN STA 296 TO STA 302. REMOVED DAMAGED SKIN SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW FAA APPROVED DER COTNEY ENGINEERING SKETCH D02-R01.Aug 27, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA97252Skin · corrodedDURING C-CHECK INSPECTION, FOUND BULGE IN FUSELAGE SKIN LONGERON 28 LT FS 1655 TO 1660.Aug 27, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA97249Pressure Web · corrodedDURING C-CHECK INSPECTION, FOUND PRESSURE WEB UPPER SURFACE CORRODED FS 923 BL 0.Aug 27, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA97251Angle · corrosionDURING C-CHECK INSPECTION, FOUND LT WING INBD L/E UPPER SCREW ATTACH HOLES CORRODED AT ATA XFS 41 TO 55. *S/D* REMOVED CORROSION AND FOUND LEADING EDGE UPPER SPAR ATTACHMENT ANGLE DAMAGED BEYOND LIMITATIONS IAW DC-8 SRM. REMOVED ATTACHMENT ANGLE, FABRICATEDAug 26, 1997 · N921R · Doug DC863F · Wing Miscellaneous StructureSDR RRXA97250Angle · corrosionDURING C-CHECK INSPECTION, FOUND LT WHEEL WELL UPPER PRESSURE WEB ATTACH ANGLE CORRODED FS 857 BL 41 TO 46 LT. *S/D* REMOVED ATTACHMENT ANGLE, REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR DOUBLER IAW DC-8 SRM 53-2-5 FIGURE 16 SHEET 2. TREATED AREA IAWAug 26, 1997 · N921R · Doug DC863F · Fuselage Miscellaneous StructureSDR RRXA97248Skin · corrodedDURING C-CHECK, INSPECTION FOUND RT FWD WASTE SERVICE DOOR HINGE ATTACH AREA IS CORRODED FS 83 TO 96, LONGERON 27 RT AND 28. *S/D* REMOVED DAMAGED SECTION, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW FAA DER COTNEY ENGINEERING SKETCH D02-R10. TREAug 26, 1997 · N921R · Doug DC863F · Fuselage Main, Plate/SkinSDR RRXA97247Frame · corrodedDURING C-CHECK INSPECTION, FOUND FS 1020 FRAME HAS CORROSION ON UPPER FWD FLANGE ABOVE LONGERON 33 AND 34 LT.Aug 25, 1997 · N921R · Doug DC863F · Fuselage Main, FrameSDR RRXA97246Skin · crackedDURING C-CHECK INSPECTION, FOUND LT WING CENTER OF LEADING EDGE CRACKED AT SCREW HOLE (LOWER SURFACE) STA XFS 520. *S/D* REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER, IAW FAA DER APPROVED ENGINEERING SKETCH D02-R12, AND TREATED ARAug 25, 1997 · N921R · Doug DC863F · Wing, Plate/Skin
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