N650TW

Service difficulty reports not matched to an aircraft · 55

They name N650TW, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. 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 = 'N650TW' AND registry_match IS NULL
  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 TWAA0104608Skin · delaminatedDURING CHECK-C THE RT WING OTBD T/E FLAP OTBD END, 48 INCHES FROM THE OTBD END AND 7.5 IN FROM THE T/E HAD A 5 IN BY 3.75 IN DELAMINATION. INSTALLED REPAIR 9 IN BY 21 IN WET LAYUP USING SRM 51-70-17 AS GUIDE. PRIMED AND PAINTED PER MM 51-22-02.Mar 12, 2001 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0104504Skin · delaminatedDURING CHECK-C MAINT ON THE RT WING THE NUMBER 8 L/E SLAT, 61 IN FROM OTBD END AND 7 IN FROM THE WEDGE T/E, HAD 3.5 BY 5.75 INCH DELAMINATION. INSTALLED 8 IN BY 8 IN METAL TO METAL HOT BOND REPAIR PER SRM 51-70-09.Mar 9, 2001 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA0019902Coffeemaker · faultyCOFFEE MAKER NUMBER 6 WAS EMITTING A BURNED WIRE SMELL. CREW TURNED OFF THE COFFEE MAKER. MAINTENANCE REPLACED IT. CHECK-C 9-10-00 MCI.Dec 22, 2000 · N650TW · Boeing 767205 · Buffet/GalleysSDR TWAA0018702Stringer · damagedSTRINGER 33R WAS FOUND DAMAGED UNDER DENTS AT STA 414 AND STA 470. REPLACED BOTH STRINGER SECTIONS AT 414 AND 470 STATIONS, PER SRM 53-00-03, FIG 202. CHECK-C 9-10-00 MCI.Nov 25, 2000 · N650TW · Boeing 767205 · Fuselage Main, Longeron/StringerSDR TWAA0017701Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM CAP AT STA 1351, BETWEEN STRINGER 33L AND 39L. REPLACED FLOORBEAM CAP AT STA 1351 PER SRM 51-10-02.Nov 2, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017607Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON FLOORBEAM STA 1285, FROM STRINGER 34R TO 39R. REPLACED FLOORBEAM PER SRM 51-40-02 AND SPM 6-70-01.Oct 30, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017606Flap Track · crackedTHE LT WING T.E. NUMBER 3 FLAP TRACK AFT FAIRING HAD A ONE INCH CRACK INBD FWD EDGE, AND HAD A ROUGH EDGE. REPAIRED CRACK AND ROUGH EDGE PER SRM 51-70-03, PAGE 37 FIG 5. TAPER SANDED LAY UP.Oct 27, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0017605Floorbeam · corrodedDURING OP 16 MAINT CHECK, THE CABIN FLOORBEAM TOP HAD CORROSION AT RBL 35 AND RBL 80 IN, STA 303. REMOVED CORRODED SECTION BETWEEN LBL 35 AND RBL 80, STA 303, PER SRM 53-00-51, PAGE 201, 205. REPLACED 40 INCHES OF BEAM CAP.Oct 23, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017516Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOORBEAM AT STA 325, RBL 64 INCHES. REMOVED CORRODED FLOORBEAM AND INSTALLED NEW SECTION OF T CAP AT STA 325, RBL 24 IN TO RBL 80 IN PER SRM 53-00-51, PAGE 201 TO 205.Oct 23, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017515Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON CABIN FLOORBEAM AT STA 287, LBL 36 IN TO RBL 80 IN. REMOVED CORRODED FLOORBEAM AND REPLACED FLOORBEAM T CAP AT STA 287, LBL 36 IN TO RBL 80 PER SRM 53-00-51, PAGE 201 TO 205.Oct 23, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017514Floorbeam · corrodedDURING OP 16 MAINT CHECK, FOUND CORROSION ON AFT CARGO FLOORBEAM CAP AT STA 1395, STRINGER 33L. REMOVED CORRODED FLOORBEAM CAP AND INSTALLED NEW SECTION FROM LBL 34 IN TO 46 IN AT STA 1395, PER SRM 53-60-51, AND SRM 51-40-02.Oct 18, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017513Floorbeam · corrodedDURING OP 16 MAINT CHECK THE FWD CARGO COMPT CARGO FLOORBEAM CAP HAD CORROSION AT STA 368, RBL 36 IN, AT NUT PLATE HOLE. REMOVED BEAM CAP FROM RBL 15 TO RBL 45 AND SPLICED IN NEW PER SRM 53-00-07, FIG 204. REMOVED BAR BEAR WEB CAP FROM RBL 35 TO RBL 45 STA 3Oct 17, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0017512Support Bracket · corrodedDURING OP 16 MAINT CHECK, LT AFT SERVICE DOOR THRESHOLD SUPPORT HAD CORROSION FROM STA 1480 TO 1548, STRINGER 20L. REMOVED AND REPLACED INBOARD FLOOR SUPPORT T SECTION PER SRM 51-10-02, PAGE 12 AND 14.Oct 17, 2000 · N650TW · Boeing 767205 · Fuselage Miscellaneous StructureSDR TWAA0017511Floorbeam · corrodedDURING OP 16 MAINT CHECK AT STA 1307 BETWEEN STRINGER 39R AND 38R, FOOT ON FLOORBEAM HAD CORROSION. REPLACED CORRODED FORMER FOOT WITH STOCK MATERIAL. PROTECTIVE TREATED NEW FORMER FOOT PER SRM 51-20-01 TABLE 1 SHEET 1 PAGE 1. SEALED PARTS FOR INSTALLATION Oct 13, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0015309Floorbeam · corrodedDURING OP 16 MAINT CHECK, AT STA 1109, TOP OF FLOORBEAM HAD CORROSION FROM STRINGER 33R TO 33L, TOP AND BOTTOM SIDES. REMOVED CORRODED BEAM CAP AND MADE NEW CAP PER BOEING PRINT AND DRAWING 146T1201. REPLACED PART PER SPM 6-70-01.Sep 30, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0015308Rib · crackedDURING OP 16 MAINT CHECK, THE RIGHT I/B ELEVATOR, FWD OF FRONT SPAR, FOURTH RIB FROM THE I/B END WAS CRACKED. REPAIRED DAMAGED AREA WITH GRAPHITE BOND REPAIR PER SRM 55-20 AND 51-70.Sep 27, 2000 · N650TW · Boeing 767205 · Elevator, Spar/RibSDR TWAA0015307Skin · delaminatedDURING OP 16 MAINT CHECK, THE RIGHT I/B ELEVATOR HAD SMALL DELAMINATION AREA OF PREVIOUS REPAIR, 5.5 INCHES FWD OF L/E AND 51 INCHES O/B OF I/B END. REMOVED OLD REPAIR AND REPAIRED DAMAGED AREA PER SRM 55-20 AND 51-70.Sep 27, 2000 · N650TW · Boeing 767205 · Elevator, Plate/SkinSDR TWAA0015306Skin · crackedDURING OP 16 MAINT CHECK, ON THE RIGHT I/B ELEVATOR A SMALL CRACK WAS FOUND IN THE ELEVATOR UPPER SKIN 35 IN FWD OF T/E AND 14 INCHES O/B OF THE I/B END, AND A SECOND SMALL CRACK IN THE UPPER SKIN 34 INCHES FWD OF THE T/E AND 12.5 INCHES O/B OF THE I/B END. ISep 27, 2000 · N650TW · Boeing 767205 · Elevator, Plate/SkinSDR TWAA0015305Floorbeam · corrodedDURING OP 16 MAINT CHECK AT STA 1087, TOP OF FLOORBEAM HAD CORROSION FROM 33R TO 33L, ON TOP AND BOTTOM OF TOP. REMOVED DAMAGED T-CAP AND MADE NEW PER DRAWING 146T1201 AND SRM 53-00-07 PAGE 216 TO 219.Sep 26, 2000 · N650TW · Boeing 767205 · Fuselage Main, Floor BeamSDR TWAA0015004Skin · damagedDURING OP 16 MAINT CHECK ON THE LT WING, TOP T/E 24 INCHES FROM O/B END OF O/B AILERON HAD BURNED/DAMAGED SPOT. REWORKED PER SRM 57-60-02, FIG 201, SHEET 2, AND SRM 51-70-03, FIG 1.Sep 22, 2000 · N650TW · Boeing 767205 · AileronsSDR TWAA0010002Light · contaminatedTHE EGRESS LIGHTS WERE INOPERATIVE AT MID GALLEY AND ROW 18 TO 23, RT SIDE. FOUND LIGHTS WET. REMOVED AND DRIED THE LAMPS AND ALL CONNECTIONS. CHECK-C 6-4-00 LAX.Jun 25, 2000 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA0010004Light · inoperativeTHE OUTSIDE EMERGENCY LIGHT AT THE LEFT SIDE FWD CABIN DOOR WAS INOPERATIVE. REPLACED THE LAMP. CHECK-C 6-4-00 LAX.Jun 24, 2000 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA0009003Skin · misrepairedDURING CHECK-C MAINT, FOUND PREVIOUS 7 INCH BY 12.5 INCH REPAIR ON RT WING O/B FLAP, O/B END LOWER SURFACE LOCATED 32 INCHES FROM O/B END. APPLIED HOT BOND REPAIR 12 INCHES BY 8 INCHES ON O/B FLAP PER SRM 57-53-01 AND 51-70-07.Jun 7, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0009002Stringer · corrodedDURING CHECK-C MAINT, FOUND .375 INCH CORROSION AT FUSELAGE STA 456, STRINGER 33R. INSTALLED 14 INCH STRINGER DOUBLER REPAIR PER SRM 53-00-03, PAGE 215. CUT OUT CORROSION IN STRINGER 33R. PRIMED AND TREATED AREAS.Jun 7, 2000 · N650TW · Boeing 767205 · Fuselage Main, Longeron/StringerSDR TWAA0005603Light · inoperativeTHE EMERGENCY LIGHT AFT OF THE AFT CARGO DOOR, LT COACH EGRESS LIGHTS, AND TWO OVERWING ESCAPE DOORS EXIT SIGNS WERE INOPERATIVE. REPLACED THE LAMPS AND CLEANED FLOOR TRACK CABLES AND LAMPS. CHECK-C 2-21-00 LAX.Apr 12, 2000 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA0005102Battery Pack · inoperativeTHE RT SIDE CABIN OVERHEAD EMERGENCY LIGHTS WERE INOPERATIVE BETWEEN ROW 30 AND THE AFT GALLEY. REPLACED THE BATTERY PACK. CHECK-C 2-21-00 LAX.Apr 2, 2000 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA0003706Skin · dentedDURING CK-C 2C, FOUND THE INBOARD AFT FLAP TOP SURFACE HAS A DENT 33.5 INCH FROM THE INBOARD END, 3 INCH FROM THE TRAILING EDGE. FILLED THE DENT WITH HYSOL 934, INSTALLED A 3 INCH BY 4 INCH DOUBLER PER THE SRM 51-70-10. SEALED THE EDGES AND PRIMED.Feb 20, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0003028Skin · delaminatedDURING CHECK-C MAINT, THE RT WING OTBD FLAP 4 FEET 4 INCHES FROM OTBD END, 10.5 INCHES FROM TE HAD DELAMINATION .75 INCH BY 0.5 INCHES. CLEANED UP DAMAGED AREA AND FILLED AND INSTALLED 3 IN BY 5 IN HOT BOND REPAIR PER SRM 51-70-07.Feb 20, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0003027Skin · damagedDURING OP 16 MAINT CHECK, THE RT WING INBD FLAP LE OTBD OF AFT FLAP ACTUATOR ROD, BULLNOSE WAS WORN. REMOVED MULTIPLE LAYERS OF PAINT TO MATERIAL SURFACE. FOUND NO DAMAGE. APPLIED PROTECTIVE COATING PER SRM 51-24-13 AND PAINTED REPAIR.Feb 20, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0003026Skin · damagedDURING CHECK-C MAINTENANCE, THE RT WING INBD FLAP OTBD END FWD BULLNOSE WAS WORN. REMOVED MULTIPLE LAYERS OF PAINT TO MATERIAL SURFACE. FOUND NO DAMAGE. APPLIED PROTECTIVE COATING PER SRM 51-24, AND PAINTED.Feb 20, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0003025Skin · damagedDURING CHECK-C MAINTENANCE, THE RT WING INBD AILERON UPPER SURFACE, 38.75 IN FWD OF TE, 16 INCHES OTBD OF INBD END, HAD A DENT. INSTALLED 2 LAYER GRAPHITE 4.5 INCH DIAMETER HOT BOND PER SRM 51-70-05. PRIMED AND PAINTED AREA.Feb 20, 2000 · N650TW · Boeing 767205 · AileronsSDR TWAA0003024Skin · damagedDURING CHECK-C MAINT, THE RT WING OTBD FLAP INBD END, TOP SURFACE 36 INCHES FWD OF THE TE AND 1.25 INCHES FROM THE INBD END, A FLAP REPAIR WAS WORN THROUGH. REMOVED MULTIPLE LAYERS OF PAINT TO MATERIAL SURFACE. APPLIED PROTECTIVE COATING PER SPM 51-24-13. NFeb 20, 2000 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA0002802Wire · cutTHE EGRESS LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN ROWS 27 TO 35. REPLACED THE FEEDER CABLE. CHECK-C 11-12-99 LAX.Feb 16, 2000 · N650TW · Boeing 767205 · Light System WiringSDR TWAA9917102Battery · dischargedTHE EMERGENCY CEILING LIGHTS WERE INOPERATIVE ON RT SIDE OF CABIN, ROW 22 AFT. REPLACED POWER SUPPLY. CHECK-C 11-7-99 LAX.Dec 16, 1999 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA9915806Skin · delaminatedDURING CHECK-C MAINT, FOUND AT LOWER O/B SURFACE OF NUMBER 8 SLAT, THE T/E WEDGE HAD DELAMINATION 6 INCHES FROM THE T/E. INSTALLED HOT BOND REPAIR PER SRM 51-70-10, A 3 INCH BY 5 INCH PATCH.Nov 10, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9915303Skin · delaminatedDURING CHECK-C MAINT, THE NUMBER 11 LE SLAT HAD DELAMINATION AT LOWER INBD SURFACE, 6 INCHES FROM THE TE. INSTALLED METAL HOT BOND REPAIR PER SRM 51-70-10, PER BOEING SERVICE BULLETIN 767-57A0057 REV 2.Nov 10, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9915304Skin · misrepairedDURING CHECK-C MAINT, THE LEFT WING NUMBER 3 LE SLAT, TOP SIDE AT OTBD END, FOUND THE PATCH COVER HAD COME OFF OF THE METAL SURFACE. INSTALLED A 3.5 INCH IN BY 5.5 IN HOT BOND REPAIR PER BOEING SERVICE BULLETIN 767-57A0057 REV 2, AND SRM 51-70-10.Nov 7, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9906005Skin · crackedTHE TOP SURFACE OF NR 4 LE SLAT, AFT EDGE WEDGE, HAD A 2 IN CRACK WITH .125 IN HOLE APPROX 42 IN INBD AND 9 IN FROM TE. INSTALLED DOUBLER REPAIR PER 767 SRM 51-70-10, PAGE 20, AND SEALED EDGES. CHECK-C 2-10-99 LAX.Apr 19, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9902302Skin · delaminatedDURING CHECK-C, MAINTENANCE FOUND NR 5 L/E SLAT INBD TOP DELAMINATED 3 INCH BY 3 INCH. REMOVED DELAMINATED SKIN AND INSTALLED FILLER AND METAL HOT BOND REPAIR PER SRM 51-70-10.Feb 7, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9901401Skin · damagedTHE NR 6 LE SLAT PANEL TRAILING EDGE AT INBD TOP END HAD REPAIR BLOWN OFF. INSTALLED HOT BOND REPAIR AS REQUIRED BY SRM 51-70-10, PAGE 26 FIG 10. CHECK-C 10-28-98 LAX.Jan 15, 1999 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9818808Skin · delaminatedFOUND 12 INCH BY 12 DELAMINATION ON UPPER SURFACE OF NR 6 L/E DEVICE, AT O/B END. INSTALLED METAL TO METAL HOT BOND REPAIR PER 767 SRM 51-70-10. CHECK-C 10-28-98 LAX.Nov 24, 1998 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9818409Skin · delaminatedDURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT, O/B SIDE REPAIR DELAMINATED. REPLACED CORRODED HONEYCOMB AND INSTALLED 12.5 IN BY 13 IN METAL OVERLAY PER SRM 51-70-10.Nov 1, 1998 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9818410Skin · delaminatedDURING CHECK-C MAINT, FOUND RT WING NR 10 LEADING EDGE SLAT TOP DELAMINATED O/B OF CENTER, AND I/B OF OLD PATCH, 2 IN WIDE BY 4 IN LONG. REMOVED PREVIOUS REPAIR AND ADDITIONAL DELAMINATED SKIN. REMOVED DAMAGED CORE. MADE 10 IN BY 25 IN CORE AND SKIN METAL TOct 31, 1998 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9818412Skin · delaminatedDURING CHECK-C MAINT, FOUND REPAIR COMING LOOSE ON THE LEADING EDGE OF LT WING, AFT OF OF NR 6 LEADING EDGE SLAT I/B SIDE. REMOVED DELAMINATED REPAIR, REPLACED WITH 7 BY 7 IN HOT BONDED REPAIR PER SRM 51-70-07.Oct 30, 1998 · N650TW · Boeing 767205 · Wing, Plate/SkinSDR TWAA9818411Skin · delaminatedDURING CHECK-C MAINT, FOUND NR 6 LEADING EDGE SLAT I/B REPAIR HAD DELAMINATION. REMOVED DELAMINATED DOUBLER AND REPAIRED DAMAGED CORE AND INSTALLED 10 BY 12 IN HOT BOND REPAIR PER 51-70-10.Oct 30, 1998 · N650TW · Boeing 767205 · Leading Edge DevicesSDR TWAA9812703Battery Pack · dischargedMAINT FOUND EMERGENCY LIGHT EQUIPMENT NRS L308, L311, L333 WERE INOPERATIVE ON TEST. REPLACED BATTERY PACK. CHECK-C 7-21-98 LAX.Aug 4, 1998 · N650TW · Boeing 767205 · Emergency LightingSDR TWAA9812130Skin · crackedDURING CHECK-C MAINT, FOUND LT WING O/B FLAP LOWER SKIN WITH 2 IN CRACK APPROX 18 IN FROM I/B END AND APPROX 12 IN FROM T/E. CUT OUT DAMAGED AREA AND INSTALLED FIBER GLASS 250 DEG CURE HOT BOND REPAIR PER SRM 57-53-01 AND 51-70-07.Jul 24, 1998 · N650TW · Boeing 767205 · Trailing Edge FlapsSDR TWAA9812131Skin · tornDURING CHECK-C MAINT, FOUND NR 5 SPOILER T/E 1.5 IN TEAR IN SPOILER PANEL. REPAIRED PER SRM. INSTALLED LAYER ADHESIVE AND LAYER FABRIC AND HOT BOND 6 BY 6 PER SRM 51-70-17, FIG 19 ITEM 3H.Jul 21, 1998 · N650TW · Boeing 767205 · SpoilersSDR TWAA9802203Oil Regulator · leakingSTL - FLT 842 - AIRCRAFT WAS OPERATING WITH THE LT GENERATOR PLACARDED INOPERABLE PER MEL. IN-FLIGHT, THE APU AUTO SHUTDOWN WITH EICAS MSG - APU LOW OIL PRESS. DIVERTED TO STL. REPLACED THE LEFT IDG AND PLACARDED THE APU INOP PER MEL. AIRCRAFT OPERATED TO Feb 11, 1998 · N650TW · Boeing 767205 · APU Oil SystemSDR TWAA9716004Vane Bleed Contl · out of adjustJFK - DURING CRUISE, NR 2 ENGINE SUFFERED COMPRESSOR STALL. ADJUSTED ENGINE VANE BLEED CONTROL (EVBC). OPERATIONAL CHECK AND ENGINE RUN NORMAL. (M)Feb 1, 1997 · N650TW · Boeing 767205 · Compressor Bleed Control
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