Boeing 727-224

Service difficulty reports · 2,252

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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 aircraft_model_key = '727224'
  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 K11A2013070925004Shear Tie · corrodedSHEAR TIE CORRODED BS 990, STR 29R.Jun 5, 2013 · N725CK · Boeing 727224 · Fuselage Internal Mounting StructureSDR K11A20130708001Window Frame · corrodedMAIN DECK WINDOW FRAME CORRODED, BS 980.May 30, 2013 · N725CK · Boeing 727224 · Fuselage Main, StructureSDR K11A2013070925005Skin · crackedSKIN HAS CRACK INDICATIONS AT FOUR LOWER ROW FASTENERS BS 580 - 600, S4R.May 16, 2013 · N725CK · Boeing 727224 · Fuselage Main, Plate/SkinSDR K11A2013090325001Threshold · corrodedAFT CARGO THRESHOLD LOWER CORRODED, (2 X 2)Apr 16, 2013 · N725CK · Boeing 727224 · Fuselage Miscellaneous StructureSDR K11A2012102925001Floorbeam · corrodedFLOORBEAM STA 360 FLANGE CORRODED AT FASTENER HOLE, 1X1 INCHES (NR 0169,0231).Oct 17, 2012 · N725CK · Boeing 727224 · Fuselage Main, Floor BeamSDR K11A2011041872502Smoke Detector · defectiveAT FL280 FIRE BELL SOUNDED, LOWER CARGO LIGHT ILLUMINATED, AFT CARGO MESSAGE ON MX DISPLAY LIGHT EXTINGUISHED DURING DESCENT. RAN LOWER CARGO FIRE CHECKLIST, CONTINUED TO DAL ASKED FOR FIRE TRUCKS TO MEET AIRCRAFT. DAL FIRE AND RESCUE FOUND NO FIRE AND DAMAGApr 18, 2011 · N725CK · Boeing 727224 · Smoke DetectionSDR K11A2011041872501Smoke Detector · dirtyAT FL340 FIRE BELL SOUNDED LOWER CARGO LIGHT ILLUMINATED AND AFT CARGO ON MX DISPLAY LIGHT EXTINGUISHED DESENDING THROUGH APPROX 16,000 FT. INSPECTED AND CLEANED LOWER AFT CARGO SMOKE DETECTORS OF DEBRIS, SYSTEM OP'S CHECKS NORMAL IAW HOLLINGSHEAD / SECURAPLAApr 18, 2011 · N725CK · Boeing 727224 · Smoke DetectionSDR K11A2010021572501Frame · dentedFRAME DENTED 2 EA. 1 INCH DIA. DENTS 6 INCHES APART.Mar 5, 2010 · N725CK · Boeing 727224 · Fuselage Main, FrameSDR K11A2009112572502Floor Support · corrodedM/D FLOOR SUPPORT CORROSION STA 335 RBL 55 1 X 1 INCHES.Nov 25, 2009 · N725CK · Boeing 727224 · Fuselage Miscellaneous StructureSDR K11A2009112572501Floor Support · corrodedM/D FLOOR SUPPORT CORROSION AT STA 335 RBL 45 1 X 1 INCHES.Nov 25, 2009 · N725CK · Boeing 727224 · Fuselage Miscellaneous StructureSDR K11A2009112472502Skin · corrodedRAM AIR DOOR ACTUATOR ACCESS DOOR EXT SKIN CORRODED 1 X 1 INCHES.Nov 24, 2009 · N725CK · Boeing 727224 · Fuselage Main, Plate/SkinSDR K11A2009112472501Web · corrodedWEB CORROSION 1 X 1 INCHES.Nov 24, 2009 · N725CK · Boeing 727224 · Fuselage Miscellaneous StructureSDR K11A2009112372505Angle · crackedAFT PRESSURE BULKHEAD UPPER ANGLE CRACKED 4 INCH CRACK.Nov 23, 2009 · N725CK · Boeing 727224 · Fuselage Main, BulkheadSDR K11A2009112372503Stiffener · crackedAFT PRESSURE BULKHEAD HORIZONTAL STIFFENER CRACKED.Nov 23, 2009 · N725CK · Boeing 727224 · Fuselage Main, BulkheadSDR K11A2009112372504Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER CHORD, AFT LWR FLANGE HAS CORROSION.Nov 23, 2009 · Boeing 727224 · Fuselage Main, Floor BeamSDR K11A2009112372502Attach Angle · corrodedLOWER SPAR CAP FWD ATTACH ANGLE FLANGE HAS CORROSION AT LEFT WING FSS 415.Nov 23, 2009 · N725CK · Boeing 727224 · Wing SparSDR K11A2009112372501Stringer · corrodedSTRINGER HAS CORROSION 8 INCHES.Nov 23, 2009 · N725CK · Boeing 727224 · Fuselage Main, Longeron/StringerSDR K11A2009112072504Window Frame · corrodedRT WINDOW FRAME CORROSION 1 X 1 INCHES.Nov 20, 2009 · N725CK · Boeing 727224 · Fuselage Main, StructureSDR K11A2009112072503Skin · damagedSKIN HAS CREASE 1 X 1 INCHES.Nov 20, 2009 · N725CK · Boeing 727224 · Fuselage Main, Plate/SkinSDR K11A2009112072502Skin · damagedSKIN HAS CREASE 1 X 1 INCHES.Nov 20, 2009 · N725CK · Boeing 727224 · Fuselage Main, Plate/SkinSDR K11A2009112072501Window Frame · corrodedEXTERNAL FUSELAGE STA 610 RT WINDOW FRAME CORRODED 1 X 1 INCHES.Nov 20, 2009 · N725CK · Boeing 727224 · Fuselage Main, StructureSDR DHLA20087451226Angle · crackedUPON VISUALLY INSPECTING THE RT WING A CRACK IN THE FALSE SPAR LOWER CHORD WAS FOUND AT APPROX WBL124.0. THE CRACK IS IN THE RADIUS APPROX 1.5 INCHES IN LENGTH.Dec 26, 2008 · N745DH · Boeing 727224 · Wing Miscellaneous StructureSDR DHLA2008745700Flap Track · corrodedNR 6 FLAP TRACK FWD LUGS CORRODED. REPAIRED FWD LUGS IAW EO COO-2-57-333-08 DATED 10/04/08 AND BAC MSG 1-1000848556-3 DATED 10/02/08. REFERENCE FAA FORM 8100-9 DATED 11/18/08 AND ASTAR EVA B257-00143 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 6-210.Nov 19, 2008 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHLA2008745699Flap Track · corrodedNR 7 FLAP TRACK FWD ATTACH LUGS CORRODED. REPAIRED FWD LUGS IAW COOPESA EO COO-2-57-334-08 DATED 10/04/08 AND BAC MSG 1-1000865923-2 DATED 10/02/08. REFERENCE FAA FORM 8100-9 DATED 11/18/08 AND ASTAR EVA B257-00146 FOR REPAIR APPROVAL. DOCUMENTED ON COOPESANov 19, 2008 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHLA2008745698Flap Track · corrodedNR 6 FLAP TRACK FWD SUPPORT FITTING CORRODED. REPAIRED FITTING ATTACH LUGS IAW COOPESA EO COO-2-57-340-08 DATED 10/07/08 AND BAC MSG 1-1002286730-4 DATED 11/06/08 AND 1-1002286730-11 DATED 11/12/08. REF FAA FORM 8100-9 DATED 11/14/08 AND ASTAR EVA B257-00145Nov 16, 2008 · N745DH · Boeing 727224 · Trailing Edge FlapsSDR DHLA2008745693Attach Fitting · corrodedNR 1 T/E FLAP TRACK FWD ATTACH FITTING OTBD LUG CORRODED. ACCOMPLISHED REPAIR TO LUG BORE IAW COOPESA EO COO-2-57-335-08 DATED 10/04/08 AND BOEING MSG 1-1000885726-2 DATED 10/02/08. REF FAA FORM 8100-9 DATED 11/5/08 AND ASTAR EVA B257-00144 FOR REPAIR APPROVNov 16, 2008 · N745DH · Boeing 727224 · Wing, Attach FittingsSDR DHLA2008745697Support Beam · corrodedLT MLG TRUNNION SUPPORT BEAM OTBD ATTACH LUG BORE CORRODED AND ATTACH FITTING BORE'S SCRATCHED AND CORRODED. ACCOMPLISHED REPAIR TO TRUNNION BEAM BORE AND ATTACH FITTING BORES IAW COOPESA EO COO-2-57-376-08 DATED 10/23/08 AND BAC MSG 1-986112769-7 DATED 10/23Nov 15, 2008 · N745DH · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR DHLA2008745695Lug · corrodedLT WING, NR 2 L/E FLAP, OTBD BULLNOSE ACTUATING MECHANISM, LOWER ROD BEARING LOOSE. ACCOMPLISHED REPAIR TO FLAP BULLNOSE O/B BEARING LUG, DUE TO CORROSION, IAW COOPESA EO COO-2-57-343-08 DATED 10/9/08 AND BAC MSG 1-1006665684-2 DATED 10/7/08. REF FAA FORM 81Nov 15, 2008 · N745DH · Boeing 727224 · Leading Edge DevicesSDR DHLA2008745691Support Beam · corrodedRT MLG TRUNNION SUPPORT BEAM OTBD ATTACH LUG BORE AND ATTACH FITTING BORE CORRODED AND SCRATCHED. REPAIRED RT MLG BEAM OTBD LUG BORE AND ATTACH FITTING (REAR SPAR) BORE IAW COOPESA EO COO-2-57-376-08 DATED 10/23/08 AND BOEING MESSAGE 1-986112769-7 DATED 10/22Nov 15, 2008 · N745DH · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR DHLA2008745692Support Beam · corrodedRIGHT MLG TRUNNION BEAM LOWER FAIRING PANEL ATTACH HOLES CORRODED. ACCOMPLISHED REPAIR TO SUSPECT HOLES IAW EO COO-2-57-391-08 DATED 10/27/08. REF FAA FORM 8110-3 DATED 11/06/08 AND EVA B257-00059 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 1-661.Nov 14, 2008 · N745DH · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR DHLA2008745694Support Beam · corrodedLT MLG TRUNNION SUPPORT BEAM HAS CORROSION IN AND AROUND LOWER PANEL ATTACH HOLES, LWBL 80.5 TO 124.2. ACCOMPLISHED REPAIR TO SUPPORT BEAM AS REQUIRED, IAW COOPESA EO COO-2-57-387-08 DATED 10/27/08. REF FAA FORM 8110-3 DATED 11/06/08 AND ASTAR EVA B257-00060Nov 14, 2008 · N745DH · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR DHLA2008745690Frame · crackedFUSELAGE FRAME AT BS 188, OTBD CHORD CRACKED AT WL 208 AND LBL 36. REMOVED, FABRICATED, AND INSTALLED FRAME OTBD CHORD AND WEB SECTION PER SRM 51-10-1, 51-20-1, AND 51-30-2. DOCUMENTED ON N/R 2-387.Nov 14, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745689Structure · corrodedLWR FUSE, NLG W/WELL HORIZONTAL WALKWAY LOWER LT CHORD CORRODED BETWEEN BS 294.5 AND 348.2. REMOVED, FABRICATED NEW CHORD MEMBER PER BAC DWG 65-18415 REV U DATED 12/15/77, BAC DWG 65-18420 REV M DATED 10/22/81, AND ASTAR EC-01167-001, AND INSTALLED PER SRM 51Nov 14, 2008 · N745DH · Boeing 727224 · Fuselage Miscellaneous StructureSDR DHLA2008745688Floorbeam · corrodedCABIN FLOORBEAM AT BS 1070 LOWER CHORD CORRODED FROM LBL 10 TO RBL 55. ACCOMPLISHED REPAIR TO LOWER CHORD FROM LBL 19 TO RBL 10 PER B727 SRM 53-10-8 FIG 8. ALL OTHER CORROSION CLEANED UP WITHIN SERVICE LIMITS. DOCUMENTED ON N/R 2-164.Nov 13, 2008 · N745DH · Boeing 727224 · Fuselage Main, Floor BeamSDR DHLA2008745685Skin · crackedFUSELAGE SKIN LAP SEAM AT STR 4L HAD CRACK INDICATIONS AT LOWER FASTENER ROW FROM AT BS 391.5, 395, 409, 410, 415.5, 442.5, AND 450, CRACK INDICATIONS DOCUMENTED ON COOPESA N/R'S 2-184, 2-185, AND 2-186. COMPLETE REPAIR DOCUMENTED ON 2-186 ONLY. ACCOMPLISHEDNov 13, 2008 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHLA2008745686Fitting · damagedMODIFICATION OF LMLG TRUNNION SUPPORT BEAM OTBD FITTING, ON REAR SPAR, REQUIRED IN CONJUNCTION WITH FITTING BORE RE-WORK. ACCOMPLISHED MODIFICATION TO FITTING IAW SB 727-57-0153 REV 4 SECTION 3, PART II, DATED 9/10/92. DOCUMENTED ON COOPESA N/R 1-686.Nov 12, 2008 · N745DH · Boeing 727224 · Wing, Landing Gear Attach FittingsSDR DHLA2008745684Pressure Panel · corrodedNLG W/WELL SKIN/WEB CORRODED AT BS 326.5, LBL 17.5. ACCOMPLISHED SKIN REPAIR PER EO COO-2-53-375-08 DATED 10/22/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00161 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 1-666.Nov 11, 2008 · N745DH · Boeing 727224 · Fuselage Main, BulkheadSDR DHLA2008745683Frame · damagedFUSE FRAME AT BS 1090 HAS DOUBLE DRILLED HOLES AT STR 8L, 11L, AND 14L. ACCOMPLISHED NECESSARY FRAME REPAIRS BETWEEN STR 7L AND 9L, AND BETWEEN STR 10L AND 12L PER EO COO-2-53-385-08 DATED 10/27/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00163 FONov 11, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745682Frame · damagedFUSE FRAME AT BS 1090 HAS DOUBLE DRILLED HOLE OVER STR 8R. ACCOMPLISHED FRAME REPAIR BETWEEN STR 7R AND 9R PER EO COO-2-53-379-08 DATED 10/24/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00162 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 2-53.Nov 11, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745681Stringer · damagedFUSELAGE CABIN STR 14R HAS ELONGATED FASTENER HOLES FROM BS 950A TO 950C. ACCOMPLISHED STR 14R SPLICE REPAIR PER EO COO-2-53-369-08 DATED 10/16/2008. REFERENCE FAA FORM 8110-3 DATED 11/6/2008 AND EVA B253-00150 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 2-476.Nov 11, 2008 · N745DH · Boeing 727224 · Fuselage Main, Longeron/StringerSDR DHLA2008745680Bulkhead · corrodedNLG W/WELL TORQUE BOX AREA, BULKHEAD WEB AT BS 351.2 CORRODED BETWEEN LBL 2 AND LBL 4, WL 169. ACCOMPLISHED REPAIR TO WEB PER COOPESA EO COO-2-53-389-08 DATED 10/28/2008. REF FAA FORM 8110-3 DATED 11/6/2008 AND ASTAR EVA B253-00165 FOR REPAIR APPROVAL. DOCUNov 11, 2008 · N745DH · Boeing 727224 · Fuselage Main, BulkheadSDR DHLA2008745676Skin · crackedFUSELAGE SKIN, FASTENER ROW AT STR 4R LAP SEAM FROM BS 691.5 TO 693.5 HAS CRACK INDICATIONS. DURING ACCESS, FOUND FRAME CRACKED AT BS 740, BETWEEN STR 3R AND 5R. ACCOMPLISHED SKIN REPAIR AT LAP SEAM, BS 680 TO BS 740, PER SB 727-53A0222 REV 1, SECT 3, PART INov 10, 2008 · N745DH · Boeing 727224 · Fuselage Main, Plate/SkinSDR DHLA2008745674Frame · damagedCABIN FRAME HAS DOUBLE DRILLED HOLES ON INBD FLANGE AT BS 783.95, BETWEEN STR 16R AND 17R. REPAIRED FRAME INBD CHORD PER EO COO-2-53-292-08 DATED 10/14/08, BAC MSG 1-980377061-3 DATED 10/18/08, BAC MSG 1-980377061-9 DATED 10/13/08, AND EVA B253-00129. REPAIRNov 10, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745673Frame · damagedCABIN FRAME HAS HOLES ON INBD FLANGE THAT ARE WITHIN THE MINIMUM ED OF THE RADIUS AND FLANGE EDGE AT BS 848.95, BETWEEN STR 16L AND 17L. REPAIRED FRAME INBD CHORD PER EO COO-2-53-292-08 DATED 10/14/08, BAC MSG 1-980377061-3 DATED 10/18/08, BAC MSG 1-980377061Nov 10, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745679Shear Tie · crackedFRAME SHEAR TIE CRACKED IN NLG W/WELL TORQUE BOX AT BS 328, BETWEEN STR 26L AND 27L. REPAIRED FRAME SHEAR TIE PER SRM 53-10-4 FIG 15. DOCUMENTED ON N/R 1-683.Nov 8, 2008 · N745DH · Boeing 727224 · Fuselage Internal Mounting StructureSDR DHLA2008745672Frame · crackedFRAME CRACKED IN FWD/LWR CARGO COMPARTMENT AT BS 600, BETWEEN STR 27R AND 28R. REMOVED, FABRICATED NEW FRAME SECTION, AND INSTALLED PER SRM 53-10-2 FIG 3, 51-10-1, AND 51-30-2, REF N/R 1-242.Nov 7, 2008 · N745DH · Boeing 727224 · Fuselage Main, FrameSDR DHLA2008745687Floorbeam · corrodedCABIN FLOORBEAM CORRODED, BS 1130, BETWEEN RBL 34 AND LBL 50, ON UPPER AND LOWER CHORDS. ACCOMPLISHED FLOORBEAM REPAIR TO UPPER CHORD FROM LBL 5.7 TO LBL 54.5, AND TO LOWER CHORD FROM RBL 67 TO LBL 67 DUE TO CORROSION AND POST ACCESS CRACKS DISCOVERED, IAW EONov 6, 2008 · N745DH · Boeing 727224 · Fuselage Main, Floor BeamSDR DHLA2008745678Skin · crackedNR 5 L/E SLAT SKIN CRACKED AT TRACK, SLAT STA 90.25 ACCOMPLISHED REPAIR TO NR 5 SLAT SKIN PER EO COO-2-57-344-08 DATED 10/08/08. REFERENCE FAA FORM 8110-3 DATED 10/12/08 AND EVA B257-00136 FOR REPAIR APPROVAL. DOCUMENTED ON N/R 6-327Nov 3, 2008 · N745DH · Boeing 727224 · Leading Edge DevicesSDR DHLA2008745677Skin · corrodedWING CENTER SECTION, AS ACCESSED THROUGH CABIN, UPPER SKIN CORRODED AT BS 823, BL 0 TO RBL 25. REPAIRED WING CENTER SECTION SKIN DAMAGE AND SPANWISE BEAM BETWEEN RBL 6.5 TO RBL 25 PER EO COO-2-57-284-08 DATED 10/16/08. REFERENCE FAA FORM 8110-3 DATED 10/29/2Nov 3, 2008 · N745DH · Boeing 727224 · Wing, Plate/SkinSDR DHLA2008745589Shear Tie · crackedLOWER FUSELAGE FWD CARGO COMPARTMENT AT BS 640 BETWEEN S26L AND S27L SHEAR TIE CRACKED. REPLACED FUSELAGE SHEAR TIE SECTION AT BS 640 BETWEEN S26L AND S-27L IAW B727SRM 51-10-1 PARA 7A.Oct 22, 2008 · N745DH · Boeing 727224 · Fuselage Internal Mounting Structure
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