N498DA, cancelled Dec 10, 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 = 'N498DA' AND deregistration_id = 'N498DA-2012-12-10'
  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 FOTR2011101406609Frame · corrodedTOP OF FRAME BS 727E, S25L CORRODED. REPAIRED ON FASI WO 21142, NR 06609.Oct 14, 2011 · N498DA · Boeing 737232 · Fuselage Main, FrameSDR FOTR2011100406432Frame · corrodedSURFACE CORROSION AT BS 727, FRAME LBL 5 TO RBL 5 , AFT SIDE, LWR AFT CARGO. REPAIRED ON FASI WO 21142, NR 06432.Oct 4, 2011 · N498DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S992769Battery Pack · dischargedON MTC LAYOVER, LT OUTSIDE EMERGENCY EGRESS LIGHTING INOP. REPLACED FWD LIGHT POWER SUPPLY. REPLACED BULBS FOR MID LIGHT AND REPLACED BATTERY PACK ON AFT LIGHT, OPER NOW NORMAL.Dec 16, 1999 · N498DA · Boeing 727232 · Emergency LightingSDR DL72S992252Power Supply · failedCABIN OVERHEAD EMERGENCY LIGHTS INOP ROW 2. REPLACED POWER SUPPLY AND BATTERY PACK.Oct 10, 1999 · N498DA · Boeing 727232 · Emergency LightingSDR DL72S990904Spar Web · crackedWING CENTER SECTION, REAR SPAR WEB, RBL 13. CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK AT RBL 13, JUST BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE SPAR WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PERApr 24, 1999 · N498DA · Boeing 727232 · Wing SparSDR DL72S990610Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACK INDICATIONS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE Mar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990609Skin · crackedLFEC 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 85 CRACKS INCLUDING A 15 INCH LONG CRACK LINK UP BETWEEN FS 640 AND 660. THE ENTIRE SKIMar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990608Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS BETWEEN FS 440 AND 460. THE CRACKED AREA OF SKIN LAP SPLICE WAS CUTOUT AND REMar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990570Skin · crackedLFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 2 CRACKS BETWEEN FS 460 AND 480. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B72Mar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990571Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK BETWEEN FS 580 AND 600. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM Mar 15, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S980807Fitting · crackedFOUND ON B2 LETTER CK, LT INBD VERTICAL STAB TIE BOLT FITTING CRACKED 1 INCH AT THE FIRST FASTENER HOLE AFT OF THE TIE BOLT. REPLACED FITTING PER BOEING DRAWING 65-17509.Apr 14, 1998 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980806Access Panel · crackedFOUND ON B2 LETTER CK, 4 INCH CRACK ON BALANCE BOARD ACCESS PANEL 9114. REPAIRED PER SRM 55-20-3.Apr 14, 1998 · N498DA · Boeing 727232 · Elevator, Plate/SkinSDR DL72S971807Valve · failedAFTER T/O LOST ALL 'A' HYD SYS QTY AND PRESSURE. REPLACED RT MLG LOCK OPERATED SEQUENCING VALVE.Sep 16, 1997 · N498DA · Boeing 727232 · Landing Gear Retraction/Extension SystemSDR DL72S971782Angle · crackedANGLE AT NR 8 SLAT O/B UPSTOP IS CRACKED. REPAIRED PER M/M 57-54-0 PG 816.Sep 11, 1997 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971781Rib · crackedNOSE RIB AT NR 7 SLAT IS CRACKED. REPAIRED PER M/M 57-54-0 PG 819. REPAIRED UPPER CRACK PER M/M 57-54-00 PG 809.Sep 11, 1997 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971759Skin · crackedUPON REMOVAL OF A TIME LIMITED REPAIR ON THE UPPER HINGE CUTOUT OF THE R1 DOOR THE CRACK WAS FOUND TO HAVE LENGTHENED TO 2.75 IN THE REINFORCING STRAP/ DOUBLER WHICH IS BEYOND M/M LIMITS. THIS CRACK WAS REPAIRED WITH A DOUBLER PER ERA 362243-14.Sep 5, 1997 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S972141Skin · crackedCOVE SKIN CRACKED 31 FROM I/B END OF FLAP, REPAIRED PER MM 57-52-0 FIG 809.Aug 28, 1997 · N498DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971761Flap · crackedDOUBLER CRACKED AFT SPAR 19 AND 37S FROM I/B END. REPAIRED PER M/M 57-52-0 PG 802.Aug 27, 1997 · N498DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S971645Stringer · crackedOUTER WING UPPER STRINGER TO RIB ATTACHMENT CRACKED AT LT WING STA 629 STR 13. REMOVED FASTENERS, FILLERS, AND WASHERS, CUT ACCESS HOLE PER FIG 803. DRILLED UP REPAIR ANGLE AND RADIUS BLOCKS. REMOVED FASTENERS AT STRINGER 13, 14, 15, DRILLED UP REPAIR AT STAug 22, 1997 · N498DA · Boeing 727232 · Wing, Longeron/StringerSDR DL72S971949Frame · crackedFRAME AT STA 910 LT CRACKED INSIDE LT W/W. REPAIRED PER M/M 53-11-0 PG 814.Aug 20, 1997 · N498DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S971948Rib · crackedRIB CRACKED INBD END NR 5 L/E SLAT. REPAIRED PER M/M 57-54-0 FIG 814.Aug 20, 1997 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971695Rib · crackedTWO RIBS CRACKED IN NR 6 L/E SLAT. REPAIRED PER M/M 57-54-0 PG 807.Aug 20, 1997 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S971756Bracket · crackedBRACKETS CRACKED THE NR 5 L/E FLAP I/B ACTUATOR BRACKET HAS PREVIOUS REPAIR STOP DRILL CRACKED BEYOND STOP DRILL. THE O/B NR 5 ACTUATOR BRACKET IS ALSO CRACKED AT LOWER RADIUS. REMOVED ACTUATOR REMOVED O/B BRACKET. STOP DRILLED CRACK. CRACK LENGTH AND REPAAug 19, 1997 · N498DA · Boeing 727232 · Leading Edge Slat ActuatorSDR DL72S971722Skin · crackedR-1 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER ERA362243-14 REV. A.Aug 18, 1997 · N498DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S970418Power Supply · inoperativeAFT SECTION OF TRACK LIGHTING SYS INOP. REPLACED BATTERY PACK AND RACK, CKS OK.Mar 6, 1997 · N498DA · Boeing 727232 · Emergency LightingSDR DL72S961840Power Supply · inoperativeDURING TEST, CENTER EMERGENCY LIGHTS FLICKER. REPLACED POWER SUPPY, OPS CHECK NORMAL.Aug 3, 1996 · N498DA · Boeing 727232 · Emergency LightingSDR DL72S961163Web · fatigueTHE AFT VENTRAL STAIRWAY TORQUE BOX RT VERTICAL WEB AT STA 1263 HAD A .75 INCH CRACK AT THE NR 2 ENGINE FUEL LINE CUTOUT. MADE SPLICE REPAIR PER ER/A 303593-14.May 15, 1996 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S961154Skin · crackedA 2 INCH CRACK IN NR 2 ENG INLET OUTER SKIN 3 FT FROM INLET LIP, 2 FT UP FROM FUSELAGE SKIN LT SIDE. REPAIRED PER M/M 54-30-0 FIG 801.May 14, 1996 · N498DA · Boeing 727232 · Nacelle/Pylon, Plate/SkinSDR DL72S961731Rib · crackedRIB NR 18 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961730Rib · crackedRIB NR 12 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961729Rib · crackedRIB NR 12 WAS CRACKED. INSTALLED REPAIR PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961727Rib · damagedRIB NR 11 WAS CRACKED. INSTALLED RIB REPAIR PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S961726Rib · crackedRIB NR 8 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S960881Skin · damagedAT MID-VISIT, THE HORIZ STAB PANEL NR 9215 WAS FOUND TO HAVE A HOLE IN THE TOP SURFACE. THE HOLE WAS REPAIRED PER SRM 55-10-2.Apr 12, 1996 · N498DA · Boeing 727232 · Horizontal Stabilizer, Plate/SkinSDR DL72S960976Blkhd Stiffener · crackedA CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE VERTICAL STIFFENER FS 1183 AT RBL 8. THE CRACK WAS APPROXIMATELY 0.25 INCH IN LENGTH. S/B 727-53-0175, REV 2, WHICH IS REQUIRED BY A.D. 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND REPAIApr 8, 1996 · N498DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S960879Doubler · damagedAT MID-VISIT, A TEMP REPAIR WAS FOUND TO BE INSTALLED ON THE TOP AFT CORNER OF THE L1 DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND REPAIR INSTALLED PER MM 52-11-01 FIG 804.Apr 5, 1996 · N498DA · Boeing 727232 · Passenger/Crew DoorsSDR DL72S960842Frame · crackedAT MID-VISIT, THE R2 DOOR FRAME WAS FOUND CRACKED JUST BELOW UPPER HINGE CUTOUT. THE DAMAGE WAS ROUTED OUT AND DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.Apr 5, 1996 · N498DA · Boeing 727232 · Service DoorsSDR DL72S960841Skin · crackedAT MID-VISIT, THE R2 DOOR UPPER HINGE ARM CUTOUT WAS FOUND TO BE CRACKED. THE DAMAGE WAS ROUTED OUT AND A DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.Apr 5, 1996 · N498DA · Boeing 727232 · Service DoorsSDR DL72S953990Angle · crackedFOUND DURING F-1 LETTER CHECK, .25 INCH CRACK IN RADIUS FROM UNDER BLOCK STA 910 RT MLG UPLOCK H-BRACKET FWD SUPPORT ANGLE. REPAIRED PER M/M 53-11-0 PG 834 AND 835.Oct 12, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S953884Frames · misdrilledDURING ACCOMPLISHMENT OF SI 4-61904-12AD, MAINTENANCE DISCOVERED THAT THE FRAMES AT STA 760.95 LT AND RT AND STA 783.95 LT AND RT HAVE OPEN PILOT HOLES IN THE WEB ABOVE STR 17. THE HOLES WHICH ARE ATTACH POINTS FOR INSULATION BLANKETS, HAVE BEEN INSPECTED ANDAug 22, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951496Rib · crackedDURING SHOP, INSPECTION RT WING NR 5 L/E SLAT WAS FOUNED WITH RIB NR 12 CRACKED. REPAIRED PER MM 57-54-00.Apr 12, 1995 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951407Rib · crackedRIB NR 18 CRACKED NEXT TO NUTPLATE. INSTALLED DOUBLER PER MM 57-54-0 FIGURE 805. DURING SHOP INSPECTION OF RT WING NR 5 L/E SLAT.Apr 4, 1995 · N498DA · Boeing 727232 · Leading Edge DevicesSDR DL72S951335Web · crackedVERT WEB CRACKED .625 INCH AT UPPER FASTENER ROW STA 1273, 48 SEC TORQUE BOX. FOUND AT E-2 LTR CK.Mar 30, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S951334Skin · crackedA 1.25 INCH CRACK IN VERT STAB SKIN RT SIDE AT CUTOUT FOR PANEL 9501 SADDLE PLATE. FOUND DURING E-2 LR CK. REPAIRED PER SRM 55-30-3 PAMM.Mar 30, 1995 · N498DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
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