N523DA, cancelled Apr 2, 2013

Service difficulty reports · 73

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 = 'N523DA' AND deregistration_id = 'N523DA-2013-04-02'
  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 DL72S030222Bulkhead · crackedINSPECTION OF THE FS 1183 BULKHEAD AFT ENTRY DOOR FRAME AT RBL 17.8 PER AD 99-18-05 REVEALED A CRACKED FASTENER HOLE AT WL 273. THE CRACKED HOLE WAS OVERSIZED TO REMOVE ALL CRACK INDICATIONS AND AN ADDITIONAL OVERSIZING INSURANCE CUT WAS MADE. AN OVERSIZE FMar 5, 2003 · N523DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S030211Mount · crackedINSPECTION OF THE NR 1 ENGINE FWD MOUNT SUPPORT FITTING ATTACH HOLES PER AD 97-05-08 REVEALED A CRACK INDICATION IN THE HOLE G-LOCATION. THE HOLE WAS OVERSIZED TO REMOVE THE CRACK INDICATION AND AN INSURANCE CUT APPLIED. AN OVERSIZE FASTENER WAS THEN INSTALLMar 5, 2003 · N523DA · Boeing 727232 · Engine Mount SectionSDR DL72S030185Light · malfunctionedCOCKPIT EMERGENCY LIGHT FAILS TO COME ON DURING EMERGENCY POWER CHECK. REPLACED EMERGENCY LIGHT ASSY, OPS CHECK GOOD.Feb 24, 2003 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S030110Warning Light · illuminatedNR 1 ENG OIL FILTER BYPASS LIGHT PER POM SHUT ENGINE DOWN. CLEANED CONNECTOR FOR MASTER DIM AND TEST MODULE AND PERFORMED ENGINE WINDMILL INSP PER M/M.Jan 29, 2003 · N523DA · Boeing 727232 · Engine (Turbine/Turboprop)SDR DL72S021302Torque Box · crackedFUSELAGE / VENTRAL STAIRWAY / RH TORQUE BOX STRUCTURE / FS 1263 : CRACK REPAIR THE VENTRAL STAIRWAY ACTUATOR ON THE RH TORQUE BOX AT FS 1263 WAS FOUND PULLED THROUGH THE UPPER WEB OF THE TORQUE BOX, RESULTING IN CRNov 5, 2002 · N523DA · Boeing 727232 · Fuselage Main, StructureSDR DL72S021175Battery · dischargedLT SIDE OVERWING EMERGENCY LIGHTS DID NOT ILLUMINATE DURING LAYOVER TEST. REPLACED BATTERY PACK PER M/M. CKS OK.Oct 8, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S021133Battery · dischargedAFT OVERHEAD ISLE EMERGENCY LIGHT INOP. REPLACED BATTERY OPS CHECK GOOD.Sep 24, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S021079Charger · inoperativeOVERWING EMERGENCY EXIT LIGHTS INOP IN EMERGENCY MODE. REMOVED AND REPLACED CHARGER ON RIGHT SIDE, BATTERY ON LEFT SIDE AND EMERGENCY LIGHT ASSEMBLY ON RIGHT OVERWING EXIT.Sep 13, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S020890Skin · crackedDURING LAYOVER, MAINTENANCE FOUND A 1 INCH LONG CRACK IN THE FUSELAGE SKIN BETWEEN TWO FASTENERS AT S-30 BETWEEN FS 990 AND 1009. THE SUBJECT CRACK WAS REMOVED AND AN EXTERNAL DOUBLER INSTALLED. THE REPAIR INCORPORATED AN EXISTING REPAIR INSTALLED PER PREVIOJul 27, 2002 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S020866Battery Pack · dischargedLEFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK.Jul 23, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S020865Battery · dischargedEMERGENCY EXIT LIGHT OVER AFT RT DOOR INOP. REPLACED BATTERY AND RACK. ALSO SECURED GROUND.Jul 23, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S020860Skin · crackedTHE LT BOX SKIN OF THE VERTICAL STABILIZER WAS FOUND WITH A CRACK EMANATING FROM A FASTENER COMMON TO THE REAR SPAR LOCATED 1 INCH ABOVE THE FUSELAGE SKIN INTERFACE. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 383575-14,Jul 20, 2002 · N523DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S020832Angle · crackedFOUND ON E1 LETTER CK. 1 INCH CRACK AT COVE SKIN ATTACH ANGLE NBR 6 SLAT BELOW ACTUATOR ROD REPAIRED PER M/M 57-54-000-8 FIG 805A,Jul 18, 2002 · N523DA · Boeing 727232 · Wing StructureSDR DL72S020831Angle · crackedFOUND ON E1 L/C 1.25 INCH CRACK NBR 5 SLAT COVE SKIN ATTACH ANGLE AT INBD END REPAIRED PER M/M57-54-000-8 FIG 805AJul 18, 2002 · N523DA · Boeing 727232 · Wing StructureSDR DL72S020828Skin · crackedFOUND ON E-1 LETTER CK SKIN CRACKED AT BASE OF VERTICAL STAB RT SIDE ABOVE FWD END OF NUMBER 2 ENG CUTOUT AT STR 10. REPAIR PER MM 55-30-000-8.Jul 18, 2002 · N523DA · Boeing 727232 · Vertical Stabilizer, Plate/SkinSDR DL72S020521Battery Pack · dischargedFOUND FORWARD BULLNOSE EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.May 8, 2002 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S020308Wire · brokenEMERGENCY LIGHTS OUT, ROWS 12 - 19. REPAIRED BROKEN WIRE.Mar 15, 2002 · N523DA · Boeing 727232 · Light System WiringSDR DL72S011941Battery · dischargedL2 DOOR EMERGENCY EXIT OVERHEAD LIGHT BATTERIES DEAD. REPLACED BATTERIES.Dec 15, 2001 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S010758Control Unit · overheatedON DESCENT, LIGHT SMOKE NOTICED BELOW PILOT''S L-2 WINDOW. WINDOW HEAT TURNED OFF AND SMOKE STOPPED.May 13, 2001 · N523DA · Boeing 727232 · Windshield/Door Rain/Ice RemovalSDR DL72S010706Stringer · crackedSTRINGER 18A LT AT STA 940 HAS A 3/4 INCH VISIBLE CRACK FROM RADIUS BLOCK LOWER BOLTS AND A 1 INCH CRACK FROM RADIUS BLOCK UPPER BOLTS. REPAIRED PER M/M 53-12-000-8 AND ERA 380727-14 ORIGINAL ISSUE. TIME LIMITED LEVEL 2 REPAIR RESTRICTIONS APPLY. REINSPECT REPApr 17, 2001 · N523DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72S010696Stringer · crackedSTRINGER 18A RT STA 940 CRACKED 1 INCH. REPAIRED PER MM 53-12-000-8 TIME LIMITED I REPAIRApr 17, 2001 · N523DA · Boeing 727232 · Fuselage Main, Longeron/StringerSDR DL72K001643Skin · corrodedTHE FUSELAGE SKIN AT FS 1050 AND STRINGER 28R WAS FOUND WITH TWO AREAS OF CORROSION. THE CORROSION WAS REMOVED WITH TWO 8 X 1 INCH CUTOUTS IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH A SINGLE EXTERNAL ALUMINUM DOUBLER INSTALLED PER ER/A 378309-14, REV A.Aug 24, 2000 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72K001633Web · crackedFOUND ON C2 LETTER CK, 1.25 INCH CRACK STA 1303 RT WEB ABOVE THE S-DUCT. A .75 INCH CRACK IN STA 1303 LT WEB ABOVE THE S-DUCT. REPAIRED PER B727 DRD 53-10-4D FIG 802D.Aug 23, 2000 · N523DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72K001632Angle · crackedFOUND ON C2 LETTER CK,1 INCH CRACK IN BULKHEAD TO STR ATTACH ANGLE INSIDE VERT STAB AT STR 9L. REPAIRED PER MM 55-30-0.Aug 23, 2000 · N523DA · Boeing 727232 · Vertical StabilizerSDR DL72K001365Battery Pack · malfunctionedRT WING EMERGENCY LIGHT FWD BLINKS. REPLACED RT FWD BATTERY PACK, CHECKS GOOD.Jul 19, 2000 · N523DA · Boeing 727232 · Emergency LightingSDR DL72K000997Battery Pack · dischargedCENTER AISLE OVERWING EMERG EXIT LIGHT INOP. REPLACED BATTERY PACK.May 21, 2000 · N523DA · Boeing 727232 · Emergency LightingSDR DL72K000878Power Supply · intermittentFWD CTR AISLE EMERGENCY LIGHT WON''T TEST. REPLACED RACK, CHECKS OK.May 3, 2000 · N523DA · Boeing 727232 · Emergency LightingSDR DL72K000597Light · inoperativeRIGHT FWD OVRWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY RACK M655, OPS CHECKS GOOD.Mar 29, 2000 · N523DA · Boeing 727232 · Emergency LightingSDR DL72K000507Slide · dischargedL2 DOOR SLIDE LOW PRESSURE. REPLACED SAME.Mar 13, 2000 · N523DA · Boeing 727232 · Escape SlideSDR DL72K991940Battery Pack · dischargedEMERGENCY LIGHT BATTERY PACK RACK ROW 16 OVERHEAD TEST BAD. REPLACED BATTERY PACK RACK.Aug 31, 1999 · N523DA · Boeing 727232 · Emergency LightingSDR DL72K991538Power Supply · inoperativeEMERGENCY EXIT SIGN AT ROW 4 FAILED TO ILLUMINATE DURING TEST BY CREW MEMBER. REPLACED POWER SUPPLY.Jul 9, 1999 · N523DA · Boeing 727232 · Emergency LightingSDR DL72S990809Skin · crackedFUSELAGE SKIN FS 680-740, STRINGER 4R, SKIN LAP SPLICE, CRACK 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 45 CRACKS ALONG TApr 11, 1999 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990808Skin · crackedFUSELAGE SKIN FS 481-68, STRG 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 8 CRACKS ALONG THE PANApr 11, 1999 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990807Skin · crackedFUSELAGE SKIN FS 360-481 STRG 4R SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 6 CRACKS IN 3 SEPARATE Apr 11, 1999 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990806Skin · crackedFUSELAGE SKIN FS 420-440 STRINGER 4L, SKIN LAP SPLICE, CRACK REPAIR. LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 481 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED A SINGLE CRACK BEApr 11, 1999 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S990589Stringer · crackedVERT FIN STR 10L CRACKED AT STA 180.600. INSTALLED DOUBLER PER M/M 55-30-0.Mar 18, 1999 · N523DA · Boeing 727232 · Vertical StabilizerSDR DL72S990587Frame · crackedFOUND AT B-2 LETTER CK, .5 INCH CRACK AFT ENTRY DOOR CUTOUT LT FRAME AT 2ND FROM UPPER STOP CASTING. REPAIR PER SRM 53-10-9.Mar 18, 1999 · N523DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S981614Frame · corrosionCORROSION WAS FOUND ON THE O/B FLANGE OF THE O/B CHORD OF THE C2 DOOR SILL. APPROX 0.060 OF MATERIAL FROM THE UPPER SURFACE OF THE FLANGE WAS REMOVED. REPAIRED PER ERA 331905-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S981613Skin · crackedL1 DOOR SURROUND BEAR STRAP WAS FOUND CRACKED IN THE LWR AFT CORNER OF THE DOOR. CRACK WAS TRIMMED OUT THRU THE SKIN, BONDED DOUBLER AND BEAR STRAP. REPAIRED PER ERA 331987-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, Plate/SkinSDR DL72S981612Frame · crackedA CRACK WAS FOUND IN THE FRAME AT FS 380 AND WL 280, JUST ABOVE THE R1 DOOR CUTOUT. REPAIRED PER ERA 331909-14.Aug 6, 1998 · N523DA · Boeing 727232 · Fuselage Main, FrameSDR DL72S981579Rib · crackedNR 7 SLAT O/B ACTUATOR ATTACH RIB HAS BEEN STOP DRILLED TWICE INDICATING THAT CRACK HAS CONTINUED TO GROW. REMOVED ACCESS PANELS TO RIB. FABRICATED DOUBLER. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER MM 57-54-0 FIG 804. REPAIR OK PER M/M. OK TO CLOSE SJul 29, 1998 · N523DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981578Angle · crackedNR 5 SLAT ANGLE CRACKED AT O/B SIDE OF ACTUATOR ATTACH RIB. REMOVED PANELS 6501, 6573 AND 6502 FOR ACCESS. REPAIRED PER MM 57-54-0, FIG 804. INSTALLED PANELS 6501, 6573 AND 6502.Jul 29, 1998 · N523DA · Boeing 727232 · Leading Edge DevicesSDR DL72S981577Bulkhead Angle · corrodedFWD B/B STA 740 BLKH LWR ANGLE/CORRODED LOC BETWEEN STA 27R AND 28R. NOTE, FOUND DURING OK TO INST STG 27R REPAIR N/R 1349. BEGAN REMOVING ANGLE, CONT REMOVING ANGLE. REMOVED ANGLE BEGAN INSTALLATION OF NEW ANGLE. DRILLED UP NEW ANGLE. DRILLED UP ANGLE DOJul 22, 1998 · N523DA · Boeing 727232 · Fuselage Main, BulkheadSDR DL72S981573Skin · repairedDURING SHOP VISIT, THE COVE SKIN WAS FOUND CRACKED 31 FROM IB END OF FLAP. THE SKIN WAS REPAIRED PER 727 MM 57-52-0, FIG 809, BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER AND FILLER.Jul 2, 1998 · N523DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981572Angle · repairedDURING SHOP VISIT, THE REAR CHORD ANGLE WAS FOUND CRACKED 17 AND 22 FROM IB END OGF FLAP. THE ANGLE WAS REPAIRED PER 727MM 57-52-0 BY INSTALLING A DOUBLER.Jul 2, 1998 · N523DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981571Angle · crackedTHE MIDFLAP REAR CHORD ANGLE WAS FOUND CRACKED 37 AND 31 FROM IB END DURING SHOP VISIT. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A DOUBLER.Jul 2, 1998 · N523DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981570Angle · repairedDURING SHOP VISIT, THE NR 3 MIDFLAP, SN DL15, WAS FOUND WITH A CRACKED REAR CHORD ANGLE. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0, FIG 802 BY INSTALLING A DOUBLER.Jul 2, 1998 · N523DA · Boeing 727232 · Trailing Edge FlapsSDR DL72S981556Former · bentFORMER BENT AND DAMAGED, STA 970, ABOVE 26L. REMOVED DAMAGE PER SRM 53-10-4. FABRICATED REPAIR PER SRM 53-10-4. DYE CHECKED REMOVED AREA FOR CRACKS, NO CRACKS FOUND PER PS 900-6-3. INSTALLED REPAIR DOUBLER PER SRM 53-10-3.Jul 2, 1998 · N523DA · Boeing 727232 · Fuselage Miscellaneous StructureSDR DL72S980595Stringer · crackedFOUND .75 INCH CRACK IN VERT STAB STRINGER 8R AT THIRD BULKHEAD ABOVE CRAWLWAY OPENING FIN STA 133.8. REPAIRED PER MM 55-30-0 FIG 803.Mar 17, 1998 · N523DA · Boeing 727232 · Vertical StabilizerSDR DL72S980593Web · crakcedFOUND .375 INCH CRACK RT VERT WEB UPPER LIGHTENING HOLE STA 1235, .5 INCH CRACK RT VERT WEB UPPER LIGHTENING HOLE STA 1243. REPAIRED PER MM 53-11-0 P 828.Mar 17, 1998 · N523DA · Boeing 727232 · Fuselage Miscellaneous Structure
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