N2813W, cancelled May 3, 2001

Service difficulty reports · 84

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 = 'N2813W' AND deregistration_id = 'N2813W-2001-05-03'
  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 DL72W010233Skin · corrodedAN AREA OF CORROSION WAS FOUND IN THE FUSELAGE SKIN AT FS 660 NEAR STRINGER 30. THE CORROSION WAS JUST FWD OF AN EXISTING SKIN REPAIR. THE EXISTING REPAIR WAS REMOVED, THE UNDERLYING SKIN INSPECTED, AND THE NEW CORROSION REMOVED WITH A 2.5 INCH CUTOUT. THE Feb 7, 2001 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010211Skin · crackedFROM E-2 LTR CK N/R 55, SHEARED RIVET AND CRACKS EXTENDING FROM A FASTENER WITH VISIBLE CORROSION AT STG 26L LAP JOINT 8 INCHES AFT OF STA 680. REPAIR PER SRM 53-30-3.Feb 6, 2001 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010209Skin · crackedFROM E-2 LTR CK, FUSELAGE SKIN IS CRACKED AT R-4 COCKPIT WINDOW CUTOUT. REPAIR PER SRM 53-30-3.Feb 6, 2001 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W002452Battery Pack · inoperativeAFT CARGO DOOR EMERG LIGHT INOP. REPLACED POWER PACKDec 15, 2000 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W002087Battery Pack · inoperativeEXTERIOR EMERGENCY LIGHT INOP. REPLACED BATTERY AND POWER SUPPLY.Oct 22, 2000 · N2813W · Boeing 727247 · Exterior LightingSDR DL72W002086Power Supply · inoperativeOUTBOARD AFT LEFT OVERWING EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AND POWER SUPPLY.Oct 22, 2000 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W001961Actuator · failedON TAKEOFF NR 2 SLAT ON LEFT WING DID NOT RETRACT. REPLACED NR 2 SLAT ACTUATOR, VISUALLY INSPECTED AND ALL CHECKS OK. SLAT ACTUATOR LEAK AND OPS CKS OK. NR 2 L/E SLAT ACTUATOR INSTALLATION, LEAK CK AND OPS CK OK PER M/M.Oct 9, 2000 · N2813W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W001268Stiffener · crackedSPAR STIFFENER CRACKED I/B OF I/B TRACK NR 2 SLAT. REPLACED STIFFENER PER MM 57-20-21.Jul 5, 2000 · N2813W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W001267Stiffener · crackedNR 7 SLAT I/B TRACK I/B SPAR STIFFENER FOUND CRACKED. DURING E-1 LETTER CHECK.Jul 5, 2000 · N2813W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W001243Battery Pack · inoperativeRT FWD EXTERIOR EMERGENCY LIGHT INOPERATIVE. R/R RT FWD BATTERY PACK OPS CK GOOD.Jun 30, 2000 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W001154Bulkhead · crackedA 1 INCH CRACK FOUND ON THE WEB OF THE STA 178 BULKHEAD AT RBL 3 AND WL 197. DAMAGE FOUND ADJACENT TO EXISTING REPAIR. EXISTING REPAIR REMOVED AND NEW REPAIR INSTALLED FOR CUTOUT MEASURING 7.5 UP/DWN BY 12.5 IB/OB. ER/A 334537-14 REV A.Jun 12, 2000 · N2813W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W000873Actuator · failedON DEPARTURE CLIMB WHEN FLAPS RETRACTED FROM 5 DEG TO 2 DEG, NR 8 LED REMAINED EXTENDED. REPLACED NR 8 SLAT ACT PER M/M, OPS AND LEAK CHECK GOOD.May 2, 2000 · N2813W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W992703Skin · corrodedTHE FUSELAGE SKIN BELOW THE LAVATORY SERVICE PANEL WAS FOUND WITH AN AREA OF SKIN CORROSION AT STRINGER 20R BETWEEN FS 300 & FS 312. THE CORROSION WAS REMOVED WITH AN 8 X 2 SKIN CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A Dec 9, 1999 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W992672Bracket · crackedNR 5 L/E FLAP ACTUATOR O/B ATTACH BRACKET CRACKED TOP AND BOTTOM RADIUS. REPAIRED PER MM 57-20-21.Dec 7, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W991679Insulation · splitON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN RT 48 SEC TO FIREWALL DISC WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-24-026-Jul 16, 1999 · N2813W · Boeing 727247 · Electrical Power System WiringSDR DL72W991678Insulation · splitON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48 SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SERVICE LETTER 727-SL-2Jul 16, 1999 · N2813W · Boeing 727247 · Electrical Power System WiringSDR DL72W991046Angle · crackedTPA - LTR CHK D-1, NR 3 SPOILER I/B ACTUATOR ATTACH ANGLE CRACKED AT LWR BOLT. REPLACED ANGLE PER MM 57-42-0.May 12, 1999 · N2813W · Boeing 727247 · SpoilersSDR DL72W991045Bracket · crackedNR 1 L/E FLAP ACT O/B AND I/B MOUNT BRACKETS CRACKED AT UPPER AND LOWER MOUNT BOLTS. REPAIRED PER MM 57-20-21.May 12, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W991044Angle · crackedNR 2 SLAT LWR COVE SKIN ATTACH ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0.May 12, 1999 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W982073Skin · corrodedFUSELAGE SKIN FS 720 S-28L-28R, REPAIR FOR SKIN CORROSION. THE FUSELAGE SKIN WAS FOUND CORRODED AT FS 720 BETWEEN STRINGERS 28L AND 28R, DURING ROUTINE INSPECTIONS PER AD 91-09-09. THE CORRODED AREA OF SKIN WAS CUTOUT AN REPAIRED WITH AN EXTERNAL ALUMINUM Oct 7, 1998 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W980550Stringer · corrodedTHE FUSELAGE STRINGER AND SKIN AT S-29R WERE FOUND BADLY CORRODED BETWEEN FS 720A+10 AND 720C+10. THE SKIN DAMAGE WAS CUTOUT AND A DOUBLER AND TRIPLER INSTALLED. THE DAMAGED AREA OF STIFFENER WAS REMOVED AND A NEW SECTION SPLICED IN. THE REPAIR WAS ACCOMPLIMar 7, 1998 · N2813W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W980500Skin · corrodedAN AREA OF CORROSION WAS DISCOVERED ON THE SKIN PANEL AT FS 700, BL 0. THE CORROSION WAS CUTOUT OVER A 7.75 X 6.75 AREA. THE REQUIRED SKIN REPAIR WAS GOING TO INFRINGE ON TWO PREVIOUSLY ACCOMPLISHED SKIN REPAIRS, SO THE PREVIOUS REPAIRS WERE REMOVED AND A NEFeb 27, 1998 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W980483Web · crackedFOUND ON MV1 CHECK, TWO .375 INCH CRACKS UPPER END OF TORQUE BOX VERTICAL WEB STA 1243. FABRICATED/INSTALLED DOUBLER PER M/M 53-11-0.Feb 27, 1998 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980476Skin · crackedFUSELAGE SKIN R1 DOOR CUTOUT UPPER HINGE CUTOUT, REPAIR FOR CRACK IN REINFORCING DOUBLER (BEAR STRAP). THE UPPER HINGE CUTOUT OF THE R1 DOOR CUTOUT WAS FOUND TO HAVE A TYPICAL CRACK IN THE REINFORCING DOUBLER (BEAR STRAP) THE CRACK WAS IN LOCATION D PER BOEINFeb 23, 1998 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W980025Engine · failedNR 3 ENG OIL STRAINER CLOG LIGHT ON / ENG SHUT DOWN. DIVERTED TO DFW. FOUND METAL ON CHIP DETECTOR AND FILTER. MTC IN PROGRESS, REPLACING ENG.Jan 5, 1998 · N2813W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W972298Skin · crackedFOUND ON L/O CK, NUMBER 1 L/E FLAP CRACKED AT THE INBD HINGE CUTOUT. REPAIRED PER MM 57-30-0 AND ERA 363182-14.Nov 9, 1997 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W971660Light · inoperativeAFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WOULD NOT TEST. REPLACED LIGHT ASSY.Aug 25, 1997 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W971439Skin · crackedA 3.75 INCH CRACK IN LOWER SKIN OF LT HORIZONTAL STABILIZER NR 2 BALANCE BOARD ACCESS PANEL. INSTALLED DOUBLER PER SRM 55-20-3 FIG 5.Jul 23, 1997 · N2813W · Boeing 727247 · Horizontal Stabilizer, Plate/SkinSDR DL72W970039Bolt · shearedTHE INBOARD TENSION TIE BOLT AT LT S-3A WAS FOUND SHEARED. THE BOLT WAS REPLACED AND THE TENSION TIE FITTING INSPECTED IN ACCORDANCE WITH S/B 727-53-0178, REV 2.Dec 18, 1996 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W962705Bracket · crackedFOUND ON B1 LETTER CK, .5 INCH CRACK AT NR 1 L/E FLAP ACTUATOR MOUNT BRACKET UPPER INBD CORNER. REPAIRED PER MM 57-20-21.Dec 17, 1996 · N2813W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W962704Stiffener · crackedA 1.75 INCH CRACK AT FRONT SPAR VERTICAL STIFFENER NR 3 SLAT I/B TRACK. REPAIRED PER MM 57-20-21.Dec 17, 1996 · N2813W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W962008Light · inoperativeAFT AREA EMERGENCY EXIT LIGHT INOP. REPLACED LIGHT ASSY EMERGENCY LIGHTS, CK OK.Aug 29, 1996 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W961488Bulkhead · crackedA .5 INCH CRACK WAS FOUND IN THE 1183 BULKHEAD AT RBL 8 AND WL 172. REPAIRED PER DELTA ER/A 303629-14AD.May 23, 1996 · N2813W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W961289Bulkhead · crackedA .5 CRACK FOUND IN 1183 BULKHEAD AT RBL 8 AND WL 172. THIS ERA WILL GIVE INSTRUCTIONS TO ACCOMPLISH A REPAIR UNTIL THE FULL MODIFICATION REQUIRED BY AD 90-06-09 IS ACCOMPLISHED. THE REPAIR WILL BE INSTALLED ON THE FORWARD SIDE OF THE 1183 BULKHEAD.May 23, 1996 · N2813W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W961489Channel · crackedFOUND A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. REPAIRED PER DELTA ER/A 303628-14AD.May 22, 1996 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961294Traverse Beam · crackedCRACK IN ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AD 94-07-08 WHICH REQUIRES INSPECTION PER S/B 53-0129. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/BMay 22, 1996 · N2813W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W961258Hinge Cutout · crackedFOUND DURING A-2 LETTER CHECK, L-2 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER SRM 52-40-2.May 22, 1996 · N2813W · Boeing 727247 · Service DoorsSDR DL72W961257Skin · crackedFOUND DURING A-2 LETTER CHECK, TWO .25 INCH CRACKS AT CONSECUTIVE RIVET HOLES LT SIDE OF VERT STAB 10 FT AFT OF NR 2 ENG INLET. REPAIRED PER M/M 54-30-0 FIG 801.May 22, 1996 · N2813W · Boeing 727247 · Vertical Stabilizer, Plate/SkinSDR DL72W961256Stringer · crackedFOUND DURING A-2 LETTER CHECK, 1 INCH CRACK AT STRINGER TO BULKHEAD ATTACH BOLT AT FIN STA 180.6 STR 8 LT SIDE. REPAIRED PER M/M 55-30-0 FIG 803.May 22, 1996 · N2813W · Boeing 727247 · Vertical StabilizerSDR DL72W954093Angle · crackedFOUND ON A1 LETTER CK, NR 2 SLAT COVE SKIN ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER MM 57-54-0.Oct 24, 1995 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W954092Angle · crackedFOUND ON A1 LETTER CK, .5 INCH CRACK AT INBD STOP PAD NUMBER 7 SLAT. REPAIRED PER MM 57-54-0.Oct 24, 1995 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W953841Eel · inoperativeAFT STAIRWAY EMERGENCY LIGHT INOP. REPLACED BATTERIES, NO HELP. FWD TO MCO AND PLACARD. REPLACED LIGHT ASSEMBLY, OPERATION NORMAL.Sep 27, 1995 · N2813W · Boeing 727247 · Emergency LightingSDR DL72W952126Oven · smokingDURING CRUISE, FLT ATTENDANT REPORTED FWD GALLEY OVEN EMITTED SMOKE AS SOON AS IT WAS TURNED ON. OVEN WAS INSPECTED, PROBLEM COULD NOT BE DUPLICATED, RETURNED TO SERVICE.Apr 29, 1995 · N2813W · Boeing 727247 · Buffet/GalleysSDR DL72W951592Stair · crackedDURING SHOP INSP, A HOLE IN STR (CTR CHANNEL) 1.5 INCHES FROM THE AFT END WAS FOUND IN AFT AIRSTAIR ASSEMBLY. REPAIRED PER SRM 53-10-8 FIG 1.Apr 18, 1995 · N2813W · Boeing 727247 · Entrance StairsSDR DL72W951358Downstop · crackedFOUND AT HMV, NR 2 SLAT DOWNSTOP HAS CRACK WHERE DOWNSTOP CONTACTS. ADJACENT TO DOWNSTOP ON SLAT CORNER, AT UPSTOP. REPAIRED PER MM 57-54-0 PG 820 AND 821, REF NR CARD NR 1672.Mar 30, 1995 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W951301Doubler · misinstalledAT HMV, FOUND DOUBLERS INSTALLED BACKWARDS ON UPPER T/E SKIN OF NR 4 SLAT, NOT AERODYNAMICALLY SMOOTH. INSTALLED DOUBLERS PER SRM 57-50-3 PG 27.Mar 26, 1995 · N2813W · Boeing 727247 · Leading Edge DevicesSDR DL72W951299Skin · dentedAT HMV, FOUND FUS SKIN DENTED AT STA 1061 STR 21L. FABRICATED AND INSTALLED NEW DOUBLER AND FILLER PER SRM 53-30-3 PG 12.Mar 25, 1995 · N2813W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W951316Stringer · corrodedDURING HMV, FOUND CORROSION ON STR 27L AND END FITTING AT STA 740. REPAIRED PER SRM 53-10-3 PG 3.Mar 14, 1995 · N2813W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W951170Stringer · corrodedAT HMV FOUND CORROSION ON STR 26R AT STA 740 FWD BB. TRIMMED AND DRILLED UP STR SPLICE PER SRM 53-10-3.Mar 14, 1995 · N2813W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR DL72W951163Aileron · gougedAT HMV FOUND LWR SKIN GOUGED/DENTED LT WING INBD AILERON. REMOVED DAMAGE AND FABRICATED REPAIR PER SRM 57-50-5.Mar 14, 1995 · N2813W · Boeing 727247 · Ailerons
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