N929L, cancelled Aug 22, 2013

Service difficulty reports · 59

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 = 'N929L' AND deregistration_id = 'N929L-2013-08-22'
  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 TWAA0016004Skin · corrodedDURING CHECK-C MAINT, FOUND SKIN BULGING AND SIGNS OF CORROSION FROM LONGERON 26R TO 26L, STA 996. REPAIRED SKIN PER SRM 53-03, FIG 9.Oct 11, 2000 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA0015712Bulkhead · crackedDURING CHECK-C MAINT AN EDDY CURRENT CHECK OF THE BULKHEAD T-CAP SHOWED A CRACK APPROXIMATELY 1 INCH LONG IN RADIUS AT LONGERON 28L. INSTALLED NEW T-CAP PER SRM 53-03 FIG 37A AND BOEING DRAWING SERIES 5911425.Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA0015711Bulkhead · corrodedDURING CHECK-C MAINT, THE AFT PRESSURE BULKHEAD SKIN WAS CORRODED ALONG THE BOTTOM EDGE AT ''T'' CAP, STA 996 FROM LONGERON 27L TO 28R, 23 INCHES LONG BY 2.25 IN HIGH. REPAIRED PRESSURE BULKHEAD SKIN PER SRM 53-05 FIG 9.Oct 3, 2000 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA0012107Longeron · crackedFOUND A .5 INCH CRACK ON THE I/B FLANGE OF LONGERON 2R, STA 680. SPLICED LONGERON PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.Jul 31, 2000 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA0012106Longeron · crackedFOUND A .5 INCH CRACK IN I/B AND O/B FLANGE OF LONGERON 2R AT STA 756. SPLICED NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 7-20-99 STL.Jul 31, 2000 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9914603Fuel Pump · failedABORTED TAKEOFF ROLL, DUE TO RT ENG COMPRESSOR STALL. FOUND RT ENG FUEL PUMP OUT PUT SHAFT SHEARED. REPLACED FUEL PUMP ASSY. CC00 7-20-99 STL.Oct 27, 1999 · N929L · Doug DC932 · Engine Fuel PumpSDR TWAA9809303Fitting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT PYLON WITH CORROSION ON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 54-04, FIG 13, AND PLATED PER SRM 54-04, PAGE 53, ITApr 30, 1998 · N929L · Doug DC932 · Nacelle/Pylon StructureSDR TWAA9806512Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT HOLE IN FRONT SPAR CRACKED BEYOND LIMITS. REPLACED FRONT SPAR PER SRM 51-01 AND ARA 15277. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Apr 22, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR TWAA9806511Spar Cap · rustyMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT LT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACHMENT TO CENTER SECTION WAS VERY RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. INSTALLED NEW LT HORIZONTAL STABILIZER UPPER SPAR CAP. IApr 22, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Spar/RibSDR TWAA9806510Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT FASTENER IN WING LE RIB ABOVE LE LOWER PANEL 1113. REMOVED AND REPLACED WITH NEW RIB AND INSTALLED DOUBLER PER SRM 57-01, PG 8, AND SRM 51-01 PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TApr 22, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9806509Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LOWER PANEL NR 1112. INSTALLED NEW RIB PER SRM 51-01. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Apr 22, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9806508Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT WING LE WITH CRACK AT AFT LOWER FASTENER IN WING LE RIB ABOVE LE LOWER PANEL NR 1111. INSTALLED NEW RIB PER SRM 51-01, PG 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Apr 22, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9806616Panel · tornMCI - DURING OP 16 MAINTENANCE CHECK, FOUND TOP TE PANEL ON RUDDER SEPARATED AND TORN AT JOINT SEAMS. REPAIRED PER SRM 51-90-0. (M)Apr 16, 1998 · N929L · Doug DC932 · Rudder, Plate/SkinSDR TWAA9806601Skin · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE WITH CRACK AT LOWER AFT FASTENER IN LE ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01 PAGE 1. (M)Apr 16, 1998 · N929L · Doug DC932 · Wing, Plate/SkinSDR TWAA9806515Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED RIB PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9806514Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND AT STA 937 TO STA 965, CABIN FLOORBEAM CAP WITH METAL REMOVED BEYOND LIMITS FOR CORROSION REMOVAL. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, ITEM 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TCApr 16, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9806413Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT TOP AFT FASTENER IN RT WING LE RIB ABOVE LE PANEL 1213A. REPLACED PART PER SRM 51-01, PG 1 ITEM C. ACFT TT: 75,041 HOURS. ACFT TC: 81,086.Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9806412Barrel Nut · rustedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZONTAL STABILIZER UPPER AFT RT BARREL NUT IN FRONT SPAR FOR STABILIZER ATTACH TO CENTER SECTION WAS RUSTY AND EMITTING RUST FROM BOTTOM OF HOLE. REMOVED BOLT AND BARREL NUT AND CLEANED. REAMED AND BUSHED HOLE PApr 16, 1998 · N929L · Doug DC932 · Horizontal Stabilizer StructureSDR TWAA9806410Support · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND METAL REMOVED BEYOND LIMIT FOR CORROSION REMOVAL AT CABIN STA 937 TO STA 965, CENTER FLOOR CAP. INSTALLED NEW SECTION AT FLOOR SUPPORT PER SRM 53-05, P21, 6A, AND ARA 10993. ACFT TT: 75,041 HOURS. ACFT TC: 81,08Apr 16, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9806409Rib · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING LE HAD CRACK AT LOWER AFT FASTENER IN LE RIB ABOVE LE PANEL NR 1211A. INSTALLED NEW RIB PER SRM 51-01, PAGE 1. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Apr 16, 1998 · N929L · Doug DC932 · Wing, Rib/BulkheadSDR TWAA9809304Bulkhead · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND 1104 CANTED BULKHEAD AT NR 3 LONGERON RT AND LT SIDE, WITH 2 EACH FASTENERS MISSING. HFEC AREA FOUND 2 INCH CRACK. REPAIRED PER SRM 53-05, PAGE 49. (X)Apr 14, 1998 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9809301Bulkhead Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LT PYLON UPPER AFT BULKHEAD ANGLE CRACKED AT INBOARD AND OUTBOARD ENDS. MADE AND INSTALLED NEW ANGLE PER SRM 51-01, PAGE 1, ITEM C. (X)Apr 14, 1998 · N929L · Doug DC932 · Nacelle/Pylon, Bulkhead/FirewallSDR TWAA9807320Fitting · flat spotMCI - DURING OP 16 MAINTENANCE CHECK, FOUND HORIZ STABILIZER LEFT PIVOT BEARING LUG, IN LT SIDE OF STAB CENTER SECTION RIB, WITH FLAT SPOT IN BEARING BORE AT APPROX 3 O'CLOCK POSITION, .017 IN DEEP AND LUG IS .010 IN THICKER AT TOP 12 O'CLOCK POSITION AT SPOT Apr 14, 1998 · N929L · Doug DC932 · Horizontal Stabilizer, Attach FittingsSDR TWAA9807319Bulkhead Casting · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FOOT CASTING AFT INBOARD SIDE OF 965 BULKHEAD, CRACKED. REMOVED AND REPLACED CASTING PER SRM 51-01 AND STANDARD PRACTICES. (M)Apr 13, 1998 · N929L · Doug DC932 · Fuselage Main, BulkheadSDR TWAA9807312Block · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING TE FLAP INSIDE FLAP OUTBOARD FLAP HINGE TO FORWARD MOUNT BOLT, RT AND LT SIDE MOUNT WEBS CRACKED OUT FROM BOLT HOLES. REPLACED MOUNT BLOCK PER STANDARD PRACTICES AND SRM 51-01. (M)Apr 13, 1998 · N929L · Doug DC932 · Wing, Control Surface Attach FittingsSDR TWAA9807306Horiz Stab · gougedMCI - DURING OP16 MAINTENANCE CHECK, FOUND ON LT HORIZ STAB TOP AFT 2 BARREL NUT HOLES GOUGED. REAMED HOLES AND INSTALLED BUSHING AND REDRILLED .562 IN PER ARA 15267. (M)Apr 7, 1998 · N929L · Doug DC932 · Horizontal Stabilizer StructureSDR TWAA9809305Fitting · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION ON NR 1 PYLON FRONT SPAR LOWER BEAVER TAIL FITTING. REMOVED CORROSION ON BEAVER TAIL FITTING PER SRM 54-04, FIG 13. ROTOPEENED REWORKED AREA PER SRM 5-04, FIG 13 AND PLATED PER SRM 54-04, PAGE 53, ITEM 4.Apr 3, 1998 · N929L · Doug DC932 · Nacelle/Pylon StructureSDR TWAA9809307Skin · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CLASS III REPAIR INSTALLED ABOVE AND JUST FORWARD OF EXTERNAL POWER RECEPTACLE. INSTALLED CLASS I REPAIR PER SRM 53-04, FIGURE 12 B. (X)Mar 31, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809302Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN FUSELAGE SKIN RT SIDE AFT OF AFT CARGO DOOR. FOUND INTERIM REPAIR INSTALLED. INSTALLED CLASS 1 REPAIR PER SRM 53-04, FIG 12B. (X)Mar 30, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809309Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 43 INDICATING CRACK WITH HFEC, RT WING LOWER REAR SPAR STA XRS 154. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)Mar 27, 1998 · N929L · Doug DC932 · Wing SparSDR TWAA9809308Spar · crackedMCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING HOLE 71 INDICATING CRACKED, LOWER REAR SPAR RT XRS 200. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (X)Mar 27, 1998 · N929L · Doug DC932 · Wing SparSDR TWAA9809306Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND NR 1 PYLON LOWER END CHORD ANGLE CRACKED, 60 INCHES AFT OF LEADING EDGE, 4 INCHES INBOARD AT OUTBOARD END. INSTALLED DOUBLER PER SRM 54-01, FIG 2, PAGE 7. (X)Mar 27, 1998 · N929L · Doug DC932 · Nacelle/Pylon, Frame/Spar/RibSDR TWAA9807315Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CORROSION BEYOND LIMIT ON FLOORBEAM CAP FROM STATION 196 TO 218 OBL. FABRICATED AND INSTALLED NEW BEAM CAP PER SRM 51-01 PAGE 1. (M)Mar 27, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9807311Pivot Arm · wornMCI - DURING OP16 MAINTENANCE CHECK, FOUND LT TE FLAP CENTER HINGE PIVOT BEARING OUTBOARD LUG WORN AND CORRODED INBEARING BORE. INBOARD BEARING BORE WORN OVERSIZE. INSTALLED NEW HINGE CASTING PER MM 27-50-1. (M)Mar 27, 1998 · N929L · Doug DC932 · Trailing Edge FlapsSDR TWAA9807310Pivot Arm · wornMCI - DURING OP 16 MAINTENANCE CHECK, FOUND RT WING FLAP CENTER HINGE PIVOT BEARING INBOARD AND OUTBOARD LUGS WITH WORN GROOVES AND PITTING CONDITION IN BEARING BORES. INSTALLED NEW CENTER HINGE PIVOT ARM PER MM 27-50-01. (M)Mar 27, 1998 · N929L · Doug DC932 · Trailing Edge FlapsSDR TWAA9807305Spar · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 104 INDICATING CRACK RT WING LOWER SPAR STATION XRS 268. REPAIRED PER SERVICE REWORK DRAWING J060173 AND TWA STD PRACTICES. (M)Mar 27, 1998 · N929L · Doug DC932 · Wing SparSDR TWAA9806502Seat Track · corrodedMCI - DURING OP 16 MAINTENANCE CHECK FOUND CORROSION BEYOND LIMITS IN CHAIR TRACK AT STA 570 TO STA 617, LBL 45 IN. REMOVED AND REPLACED SEAT TRACK AT STA 570 TO STA 617, LBL 45 IN, PER SRM 53-05, PG 10G. ACFT TT: 75,041 HOURS. ACFT TC: 81,086. (X)Mar 25, 1998 · N929L · Doug DC932 · Fuselage, Seat/Cargo Attach FittingsSDR TWAA9809310Frame · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FUSELAGE FRAME STA 89 WITH CRACK IN OUTBOARD RADIUS BETWEEN LONGERONS 18 AND 19. STOP DRILLED CRACK PER SRM 51-10 AND REPAIRED PER SRM 53-01, PAGE 10, FIGURE 2. (X)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, FrameSDR TWAA9807318Spar Cap · crackedMCI - DURING OP 16 MAINTENANCE CEHCK, FOUND RT WING TE UPPER REAR SPAR CAP CRACKED AT INBOARD FLAP HINGE UPPER ATTACH HOLES. STOP DRILLED CRACK, REPAIRED PER DAC DWG J060271 AND STD PRACTICES. (M)Mar 23, 1998 · N929L · Doug DC932 · Wing SparSDR TWAA9807317Longeron · brokenMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L BROKEN JUST FORWARD OF FORMER 160. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807316Longeron · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 4L CRACKED AT STATION 200. REPAIRED PER SRM 53-02, FIG 18 PAGE 48. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Longeron/StringerSDR TWAA9807309Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND SURFACE CORROSION ON FLOORBEAM CAP AT FS 160 FROM OL-288. REPLACED FLOORBEAM CAP PER SRM 51-01, PAGE 1 ITEM 1C. SEALED PER SRM 91-20-0. (M)Mar 23, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9809108Floorbeam · corrodedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND FLOORBEAM CAP AT FS 160 TO 196, RBL 44, CORRODED BEYOND LIMITS. INSTALLED NEW FLOORBEAM PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9809106Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK IN FORWARD FUSELAGE INTERCOSTAL TO FS 69.55 FORMER ATTACH 'T' ANGLE AT LBL 13 INCH. REPLACED 'T' ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9809104Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK,F OUND DENT ON LEFT SIDE BELOW AFT CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1 INCH BY .045 INCH DEEP. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9809103Skin · dentedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND DENT IN LEFT SIDE BELOW FORWARD CORNER OF EXTERNAL POWER RECEPTACLE, 1 INCH BY 1.25 INCH BY .055. INSTALLED DOUBLER REPAIR PER SRM 53-01, PAGE 18. (M)Mar 17, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807314Floorbeam · wornMCI - DURING OP 16 MAINTENANCE CHECK, FOUND CABIN FLOORBEAM WITH WEAR AREA AT STATION 237, LBL 4 INCHES. REPAIRED FLOORBEAM PER SRM 53-05 FIG 30. (M)Mar 12, 1998 · N929L · Doug DC932 · Fuselage Main, Floor BeamSDR TWAA9807313Angle · crackedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND BELOW RT AFT LAVATORY FLOOR, ANGLE AT STATION 996 BELOW LONGERON 18R, AT CUST LINE, CRACKED. REPLACED ANGLE PER SRM 51-01, PAGE 1 ITEM C. (M)Mar 12, 1998 · N929L · Doug DC932 · Fuselage Miscellaneous StructureSDR TWAA9807308Skin · damagedMCI - DURING OP 16 MAINTENANCE CHECK, FOUND UNFILLED HOLES IN FUSELAGE SKIN AT STATION 965, BELOW LONGERON 14R. REPAIRED PER ARA 15017A. (M)Mar 7, 1998 · N929L · Doug DC932 · Fuselage Main, Plate/SkinSDR TWAA9807307Spar · crackedMCI - DURING OP16 MAINTENANCE CHECK, FOUND HOLE 44 INDICATING CRACK IN RT WING LOWER REAR SPAR STATION XSR 155. REWORKED PER SERVICE REWORK DRAWING JO60173 AND TWS STD PRACTICES. (M)Mar 7, 1998 · N929L · Doug DC932 · Wing Spar
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