N2821W, cancelled Aug 27, 2012

Service difficulty reports · 44

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 = 'N2821W' AND deregistration_id = 'N2821W-2012-08-27'
  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 DL72W010107Windshield · crackedR-1 OUTER WINDOW PANE IS CRACKED. REPLACED R-1 WINDOW PER M/M.Jan 21, 2001 · N2821W · Boeing 727247 · Flight Compartment WindowsSDR DL72W002227Web · crackedNR 2 SLAT ACT O/B MOUNT WEB BROKEN. REPAIR PER MM 57-42-0.Nov 14, 2000 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W002174Engine · failedENG SHUT DOWN IN FLT AFTER OIL CLOG LIGHT AND OIL TEMP RISE OF 130 DEG. FOUND METAL IN GEARBOX CHIP DET AND MAIN OIL FILTER. REPLACED NR 1 ENG.Nov 6, 2000 · N2821W · Boeing 727247 · Turbine Engine Accessory DriveSDR DL72W001305Engine · failedON CLIMB, NR 3 ENG HAD VIBRATION, LOUD BANG, AND LOSS OF THRUST. NO FIRE WARNING. REPLACED NR 3 ENGINE.Jul 10, 2000 · N2821W · Boeing 727247 · Engine (Turbine/Turboprop)SDR DL72W001299Switch · failedAUTO PACK TRIP LIGHT FAILED TO ILLUMINATE ON TAKEOFF. RETURN TO GATE. REPLACED AUTO PACK TRIP SWITCHES.Jul 9, 2000 · N2821W · Boeing 727247 · Cabin Cooling SystemSDR DL72W001199Skin · crackedTHE FUSELAGE SKIN AT FS 303 BELOW THE FWD LAVATORY SERVICE DOOR CUTOUT (BETWEEN STRINGERS 21R_& 22R) WAS FOUND WITH A 1INCH CRACK DUE TO CORROSION. THE CORRODED AREA OF SKIN WAS REMOVED WITH A 4.5 INCH X 4 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTEJun 22, 2000 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W000696Angle · crackedANGLE CRACKED IN RADIUS ABOVE UPPER RADIUS BLOCK ON FWD ANGLE AT FS 910 O/B OF H BRACKET. REPAIRED PER MM 53-11-0.Apr 11, 2000 · N2821W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W000695Angle · crackedNR 8 SLAT I/B ACT ATTACH ANGLE CRACKED. REPAIRED PER MM 57-20-21.Apr 11, 2000 · N2821W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W992561Battery · dischargedROW 28 OVERHEAD EMERGENCY LIGHT INOP. REPLACED BATTERIES.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W992560Battery · dischargedR1 DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W992559Battery Pack · dischargedAFT CABIN DOOR EXIT EMERGENCY LIGHT INOP. REPLACED BATTERY PACK.Nov 21, 1999 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W991958Skin · crackedRT ELEVATOR LOWER SKIN CRACKED. REPAIRED PER SRM 55-20-3.Sep 3, 1999 · N2821W · Boeing 727247 · Elevator, Plate/SkinSDR DL72W991957Bracket · crackedNR 5 L/E FLAP ACTUATOR I/B MOUNT BRACKET CRACKED BELOW LOWER MOUNT BOLT. REPAIRED PER M/M 57-20-21 PAGE 811.Sep 3, 1999 · N2821W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W991494Ballast · failedAT DEPARTURE TIME, BURNING SMELL IN CABIN AND RT AFT CEILING LIGHT CIRCUIT BREAKER POPPED. FOUND CEILING BALLAST BAD AT SEAT 17. REPLACED SAME. .Jul 2, 1999 · N2821W · Boeing 727247 · Passenger Compartment LightingSDR DL72W990907Skin · crackedFUSELAGE CK REPAIR, LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 680 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 21 CRACKS ALONG THE PANEL LENGTH. THE ENTIRE SKIN LAP WAS CUTOUT ANApr 25, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990906Skin · crackedFUSELAGE SKIN FS 481-681,STRINGER 4R, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 13 CRACKS ALONG THApr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990901Skin · crackedFUSELAGE SKIN FS 440-460 STRINGER 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION OF THE ENTIRE PANEL CONFApr 24, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990607Skin · corrodedTHE FUSELAGE SKIN WAS FOUND CORRODED AT THE FS 680 BUTT SPLICE BETWEEN STRINGER 28L AND 28R. AN EXISTING LOCAL REPAIR WAS REMOVED AT THIS LOCATION AND ALL CORROSION AREAS WERE CUT OUT OF THE SKIN WITH A 1 X 3 CUTOUT AND A 10 X 5 CUTOUT. BOTH CUTOUTS WERE REPMar 19, 1999 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W990583Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 629 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990582Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 656.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990581Stringer · crackedA .25 INCH VISIBLE CRACK AT UPPER STRINGER 10 AT WS 686.5 AT ATTACH BOLT. REPAIRED PER MM 57-13-0.Mar 9, 1999 · N2821W · Boeing 727247 · Wing, Longeron/StringerSDR DL72W990476Angle · crackedCRACK ORIGINATING UNDER I/B UPSTOP PAD ON NR 7 SLAT ANGLE RUNNING I/B .25 INCH. REPAIRED PER MM 57-40-0 PAGE 816.Mar 1, 1999 · N2821W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W981379Beam · chafedMLG CHAFFING FWD SIDE OF MLG BEAM BELOW STR 18A. REPAIR PER M/M 57-43-0.Jul 1, 1998 · N2821W · Boeing 727247 · Wing Miscellaneous StructureSDR DL72W981378Web · crackedVERT WEB CRACKED AT LIGHTENING HOLES STA 1280 AND 1303 LT. REPAIRED PER MM 53-11-0 P 828.Jul 1, 1998 · N2821W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W981377Web · crackedCRACK IN RT AIR STAIR WEB AT STA 1240 VERTICAL WEB. REPAIRED PER MM 53-11-0 P 832.Jul 1, 1998 · N2821W · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W980163Battery Pack · dischargedAFT AISLE OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD.Jan 19, 1998 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W980162Battery Pack · dischargedAFT OVERHEAD LIGHTED SIGN EMERG LIGHT INOP. REPLACED RACK AND BATT PACK, OPN CK GOOD.Jan 19, 1998 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W972458Bracket · crackedA .125 INCH VISIBLE CRACK NR 1 L/E FLAP ACTUATOR I/B MOUNT BRACKET. REPAIR PER MM 57-20-21.Nov 24, 1997 · N2821W · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W972457Baffle · crackedA .75 INCH CRACK NR 3 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACT AND .5 INCH CRACK NR 2 L/E FLAP HEAT BAFFLE AFT SIDE BELOW ACTUATOR. REPAIR PER MM 57-54-0.Nov 24, 1997 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W970476Indicator · inoperativeOUTBOARD FLAPS IND. 25/25 FLAPS 30 SELECTED. AT APPROXIMATELY 200 FEET, GPWS WARNING FLAPS. PERFORMED GO AROUND I.A.W. DELTA PROCEDURES AND COMPLIED WITH P.O.M. NOTE ALT FLAP MASTER USED. REPLACED OUTBOARD FLAP IND AND RESET. CKS OK PER MM CHAPT. 27.Mar 13, 1997 · N2821W · Boeing 727247 · Trailing Flap Position Indicating SystemSDR DL72W962711Skin · corrosionFOUND CORROSION ON FUSELAGE SKIN AT STA 486. REPAIRED IN ACCORDANCE DAL ER/A 258313-14, REV A.Dec 8, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W962712Skin · corrosionFOUND CORROSION ON THE LOWER EDGE OF THE C-1 DOOR CUTOUT AT STATION 580. REPAIRED PER DAL ER/A 304497-14, REV A.Dec 3, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W962651Frame · crackedR-1 DOORS 550 HAS A 1.5 INCH CRACK IN AFT LOWER FRAME AT CUTOUT FOR LOCK MECHANISM. DRILLED UP REPAIR DOUBLER PER M/M 52-12-0 PG 807, INSTALLED DOUBLER PER M/M 52-12-0 PG 807, CLOSED WEB.Dec 2, 1996 · N2821W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W962650Frame · crackedA .375 INCH CRACK R-2 DOOR FRAME AT UPPER HINGE CUTOUT. REMOVED DOOR FROM A/C, REPAIRED DOOR FRAME PER SRM 52-40-2.Nov 25, 1996 · N2821W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W960576Skin · crackedDURING LETTER CHECK AT TAMPA, A .5 INCH CRACK IN THE FUSELAGE SKIN AT STA 1098 ALONG S-1. CRACK WAS REPAIRED PER B727 SRM 53-30-3, FIGURE 3.Mar 8, 1996 · N2821W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W960519Angle · crackedFOUND DURING B-2 LETTER CHECK - NR 8 L/E SLAT COVE SKIN ATTACH ANGLE CRACKED AT OUTBOARD UPSTOP PAD. REPAIRED PER M/M 57-54-0, PAR 5A.Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W960518Angle · crackedFOUND DURING B-2 LETTER CHECK - 1 INCH CRACK NR 1 L/E SLAT COVE SKIN ATTACH ANGLE BELOW TAI DUCT. REPAIRED PER M/M 57-54-0 PAR 12.Mar 7, 1996 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W954158Eel Power Supply · failedIRREG - CABIN EMERG EXIT LIGHT AT AIRSTAIR DOOR INOP. CORRECTIVE ACTION - REPLACED PWR SUPPLY AND BATTERY.Oct 31, 1995 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W954071Lines · crackedFUEL VENTED OUT OF RT VENT BOX ON ACTIVE RUNWAY, FUEL MIGRATING FROM OTHER TANK CAUSING THE NR 3 TANK TO OVERFILL. FOUND CRACK LINES MFG (P/N 65-22731-2 AND 65-16710-52) REF IPC 28-30-0-16 ITEMS 120 AND 140. BOTH LINES SENT TO SHOP FOR REPAIRS.Oct 18, 1995 · N2821W · Boeing 727247 · Aircraft Fuel Distribution SystemSDR DL72W953950Frame · misdrilledDURING ACCOMPLISHMENT OF E.O. 4-61904-3AD FOR THE LT STA 783.95 FRAME, MTC FOUND THAT ONE OF THE FASTENERS INSTALLED THROUGH FRAME AND RING DOUBLER (65-16236-35) FELL OUT IN THE RADIUS OF THE 65C36280-3 REPAIR ANGLE. REPAIRS ACCOMPLISHED PER DL ERA 302567-14ASep 29, 1995 · N2821W · Boeing 727247 · Fuselage Main, FrameSDR DL72W953842Eel Pack · dischargedRIGHT FWD OVERWING EMERGENCY EXIT SIGN INOP. REPLACED BATTERY PACK, OPS CK NORMAL.Sep 28, 1995 · N2821W · Boeing 727247 · Emergency LightingSDR DL72W953208Stiffner · crackedI/B SPAR STIFFENER CRACKED LWR END AT NR 7 SLAT I/B TRACK. FOUND DURING B-1 LTR CK TPAMM. REPAIRED PER MM 57-20-21 PG 813.Jul 27, 1995 · N2821W · Boeing 727247 · Leading Edge DevicesSDR DL72W953005Overheat Loop · cutAT FL 270, 25 MIN INTO FL, LOWER AFT BODY O/H LIGHT ILLUM INTERMITTENTLY FOR APPROX 1 MIN, THEN STEADY. C/W POM PROC AND LIGHT REMAINED ILLUM FOR 15 TO 20 MIN WITH NR 2 THROTTLE AT IDLE. AFTER 20 MIN WITH NR 2 THROTTLE AT IDLE LIGHT EXT WITH A COUPLE OF FLICJul 9, 1995 · N2821W · Boeing 727247 · Overheat DetectionSDR DL72W951928Skin · crackedFUSELAGE SKIN CRACKED 1 INCH LONG STA 684 ONE INCH ABOVE STR 18R. CUT OUT SKIN DAMAGE 2.5 LONG BY 1.0625 WIDE, .5 INCH RAD TYP, USING THE SRM 53-30-3 PAGES 6 AND 7.May 7, 1995 · N2821W · Boeing 727247 · Fuselage Main, Plate/Skin
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