Boeing 727-247

Service difficulty reports · 2,669

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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 = '727247'
  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 DL72W010572Controller · malfunctionedCLIMBING THROUGH 17,000 FT.IN AUTO MODE AIRCRAFT CABIN ALT. PRESSURE CLIMBED THROUGH 10,000FT RAPIDLY. FOLLOWED LOSS OF PRESSURIZATION, CHECKLISTS AND WAS ABLE TO REGAIN CABIN CONTROL AFTER CYCLING LEFT PACK. STBY.MODE WORKED FINE AFTER THAT.Apr 7, 2001 · N2815W · Boeing 727247 · Air Conditioning SystemSDR UPS01235487Control Cable · out of rigATB-A/C ROLLS DURING FLAP RETRACTION. SUPPLEMENTAL MRR. ADJUSTED INBD AND OUTBD FLAPS FUSELAGE CABLES PER B727 MM-27-51-00Apr 4, 2001 · N207UP · Boeing 727247 · Trailing Edge Flap Control SystemSDR DL72E010529Battery Pack · dischargedFOUND AFT EMERGENCY EXIT BATTERY DEAD. REPLACED BATTERY PACK.Apr 1, 2001 · N282WA · Boeing 727247 · Emergency LightingSDR DL72W010509Gasper Fan · failedPAX REPORTED ELECT SMELL IN CABIN, STRONGEST NEAR ROW 14 OCCURED JUST PRIOR TO LANDING AND DURING TAXI TO GATE.A PAX IN THE VICINITY OF ROW 14 ALSO MENTIONED THE SOUND OF HYD PUMPS GETTING LOUDER JUST PRIOR TO LANDING. FOUND GASPER FAN BAD. REPLACED SAME.Mar 28, 2001 · N2816W · Boeing 727247 · Air Distribution FanSDR DL72E010498Battery Pack · inoperativeINTERIOR L2 DOOR EMER LITE INOPERATIVE - REPLACED POWER SUPPLY BATTERY PACK.Mar 26, 2001 · N830WA · Boeing 727247 · Emergency LightingSDR DL72E010491Battery Pack · dischargedRT OVERWING EMERGENCY EVAC LIGHT INOP. REPLACED BATT PACK OPS NML.Mar 25, 2001 · N2829W · Boeing 727247 · Emergency LightingSDR DL72E010484Actuator · jammedAFTER TAKEOFF NR 3 KRUEGER FLAP DID NOT RETRACT. REPLACED KRUEGER FLAP ACTUATOR AND SHUTTLE VALVE LEAK AND OPS CHECK OK PER OPN 7054.RIIMar 24, 2001 · N283WA · Boeing 727247 · Leading Edge Slat ActuatorSDR DL72W010470Power Supply · inoperativeF/C SEAT ROWS EMER LIGHTS INOP. REPLACED POWER SUPPLY AND BATTERY PACK. OPS CKS NMLMar 22, 2001 · N294WA · Boeing 727247 · Emergency LightingSDR DL72E010468Actuator · leakingDURING APPROACH LOST A SYSTEM HYD PRESS. MANUALLY EXTENDED GEAR. FOUND FLAP HYD MOTOR LEAKING FLUID. REPLACED FLAP HYD MOTOR, AND CASE DRAIN CHECK VALVE PER MM. INSPECTED CASE DRAIN FILTERS, NO METAL FOUND. PERFORMED ENG RUN, OPS CHECKS NORMAL.Mar 22, 2001 · N831WA · Boeing 727247 · Trailing Edge Flap Control SystemSDR DL72W010428Bulkhead · crackedTHE FS 1183 BULKHEAD WEB WAS FOUND WITH A 1 INCH LONG CRACK AT RBL 26 AND WL 169. THE CRACK WAS STOP DRILLED AND REPAIRED WITH A TITANIUM DOUBLER PER ER/A 380315-14.Mar 14, 2001 · N294WA · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W010423Angle · crackedCOVE SKIN ATTACH ANGLE CRACKED BELOW TAI DUCT NBR 8 SLAT. REPAIR PER MM 57-54-000-8Mar 14, 2001 · N294WA · Boeing 727247 · Leading Edge DevicesSDR DL72W010402Frame · crackedCRACKS WERE FOUND IN TWO LOCATIONS OF THE FS 990 FRAME. ONEWAS AT STR 28R AND THE OTHER AT STR 29R. THE CRACKS WERE CUT OUT AND A DOUBLER INSTALLED. THE DAMAGE WAS FOUND AT HMV.Mar 12, 2001 · N2819W · Boeing 727247 · Fuselage Main, FrameSDR DL72W010401Bulkhead · crackedCRACKS WERE FOUND IN THE WEBS AND FAIL SAFE CHORDS OF THE FS294.5 BULKHEAD. CRACKS WERE EMANATING FROM FASTENER LOCATIONS AT WL 180 AND LBL 14. ONE WEB AND THE CHORDS WEREREPLACED AND ONE OF THE WEBS WAS SPLICED. THE DAMAGE WAS FOUND AT HMV.Mar 12, 2001 · N2819W · Boeing 727247 · Fuselage Main, BulkheadSDR DL72W010399Module · failedLOSS OF SYSTEM A FLUID AND PRESSURE SHORTLY AFTER LDG GEAR WAS SELECTED DN. ALL 3 GREEN DN LOCK LGTS ILLUM AND RED DR LGT REMAINED ILLUM. THE L/R GEAR DR AND TAIL SKID AMBER ANNUNCIATORS ON S/O PNL REMAINED ILLUM. FOLLOWED HYD LOSS PRO CEDURES PER POM. UNMar 11, 2001 · N2816W · Boeing 727247 · Hydraulic System, MainSDR UPS01235459Shear Tie · corrodedINSPECTION TYPE:C. DISCOVERED SHEAR TIE AT BS 1148 LBL 10 WL 150 TO BE CORRODED SHEAR TIE FOUND TO BE CORRODED OUT OF LIMITS PER SRM 53-10-1 REMOVED OLD SHEAR TIE AND INSTALLED NEW SHEAR TIE PER SRM 51-30-2 AND 51-10-2Mar 6, 2001 · N212UP · Boeing 727247 · Fuselage Main, StructureSDR DL72W010349Skin · crackedDURING MAINTENANCE VISIT, THE FWD ENTRY DOOR WAS FOUND CRACKED AROUND THE UPPER LATCH CUTOUT. REPAIR PER ER/A 401383-14.Mar 1, 2001 · N2819W · Boeing 727247 · Passenger/Crew DoorsSDR DL72W010354Gusset · crackedINSPECTION OF THE RT TORQUE BOX OF THE VENTRAL STAIRWAY REVEALED A 2 INCH CRACK IN A GUSSET AT FS 1263. THE CRACK IS TYPICAL OF BAC S/B 727-53-0129. THE CRACKED GUSSET WAS REPLACED PER THE REQUIREMENTS OF THE S/B AND PER ER/A 380187-14AD.Feb 28, 2001 · N295WA · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W010340Attach Angle · crackedA .5 INCH VISABLE CRACK O/B END NR 2 SLAT IN COVE SKIN ATTACH ANGLE. REPAIR PER M/M 57-54-000-8.Feb 28, 2001 · N295WA · Boeing 727247 · Leading Edge DevicesSDR UPS01235091Regulator · inoperativeINSPECTION TYPE:N/A, O2 REGULATOR AT F/O POSITION WILL NOT INDICATE FLOW DURING MASK TEST. *S/D* REMOVED AND REPLACED F/O''S REGULATOR O2, OPS CHECKED AND LEAK CHECKED GOOD.Feb 27, 2001 · N210UP · Boeing 727247 · Crew Oxygen SystemSDR 01FDEA00167Web · crackedDURING ROUTINE INSP, AFT AIRSTAIR RT TORQUE BOX WEB LIGHTENING HOLE FOUND CRACKED AT BS 1223. *S/D* STOP DRILL CRACK PER BAC 727 SRM 51-40-2. FAB AND INSTALL PER IAW BAC 727 SRM 51-40-2.Feb 26, 2001 · N233FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 01FDEA00166Tie Clip · crackedDURING ROUTINE INSP THE FUSELAGE TIE CLIP AT BS 1070, STR 8L FOUND CRACKED. *S/D* REMOVED CLIP OUT OF ALLOWABLE LIMITS PER IAW BAC 727 SRM 53-10-1. TREATED AND PRIMED PER IAW BAC 727 SRM 51-10-2.Feb 26, 2001 · N233FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR 01FDEA00165Rib · crackedDURING ROUTINE INSP, LT MLG UPLOCK FRAME REINFORCING RIB AT BS 910 FOUND CRACKED. *S/D* REMOVED DOUBLER, STOP DRILL CRACK. REINSTALL DOUBLER PER IAW BAC 727 SRM 51-30-2.Feb 26, 2001 · N233FE · Boeing 727247 · Fuselage Miscellaneous StructureSDR DL72W010331Stringer · crackedSTRINGER 29R WAS FOUND CRACKED AT FS 950E AND 975. THE STRINGER WAS CUT AT FS 950D +10 AND REPLACED AFT TO THE MFG SPLICE LOCATION. THE DAMAGE WAS FOUND AT MV.Feb 26, 2001 · N2819W · Boeing 727247 · Fuselage Main, Longeron/StringerSDR 01FDEA00164Flange · crackedDURING ROUTINE INSP NR 2 ENG INTAKE FLANGE 1342 BULKHEAD FOUND CRACKED BY LFEC AROUND FLANGE BOLTS IN 16 PLACES FROM 3 O''CLOCK TO 10 O''CLOCK POSITION. *S/D* REMOVED AND REPLACED NR 2 ENG INTAKE DUCT MOUNTING FLANGE PER IAW FEDEX EO 7-5430-7-2303.Feb 25, 2001 · N233FE · Boeing 727247 · Engine Air Intake SystemSDR 01FDEA00159Skin · crackedDURING ROUTINE INSP, NR3 LEAD EDGE FLAP, OTBD GUIDE, WING LEAD EDGE CUTOUT WAS FOUND CRACKED. ** S/D ** STOP DRILL CRACK. FAB & INSTALL PER IAW BAC 727 SRM 57-30-4.Feb 23, 2001 · N233FE · Boeing 727247 · Wing, Plate/SkinSDR 01FDEA00161Skin · crackedDURING ROUTINE INSP, LT WING LEAD EDGE SKIN FOUND CRACKED NEAR NR 3 LEAD EDGE SLAT. ** S/D ** R&R & FAB PER IAW BAC 727 SRM 57-30-4.Feb 23, 2001 · N233FE · Boeing 727247 · Wing, Plate/SkinSDR 01FDEA00160Support Bracket · crackedDURING ROUTINE INSP, NR 1 LEAD EDGE FLAP ACTUATOR, FWD OTBD UPPER FITTING SUPPORT BRACKET FOUND CRACKED.*S/D* REMOVED AND REPLACED BRACKET PER IAW BAC 727 MM 27-81-001-4 AND BAC 727 SRM 51-10-1.Feb 23, 2001 · N233FE · Boeing 727247 · Leading Edge Slat ActuatorSDR UPS01235240Seat Track · corrodedINSPECTION TYPE:C, SEAT TRACK FLANGE CORRODED AT LBL 45, STA 520-529, WL 208. FOUND SEAT TRACK CORROSION TO BE OUT OF LIMITS. REPLACED SEAT TRACK FROM BS 480--BS 530 PER SRM 53-10-05 FIG 1 AND SRM 51-30-2.Feb 22, 2001 · N212UP · Boeing 727247 · Fuselage, Seat/Cargo Attach FittingsSDR DL72E010320Angle · crackedA .25 INCH CRACK AT FWD SIDE OF NR 6 L/E FLAP ACTUATOR MOUNT BOX O/B TRUNNION UPPER ATTACH ANGLE. REPAIRED PER MM.Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge DevicesSDR DL72E010319Stiffener · crackedFWD SPAR STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT O/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge DevicesSDR DL72E010318Stiffener · crackedFWD SPAR VERTICAL STIFFENER CRACKED AT I/B SIDE OF NR 6 SLAT I/B TRACK. REPLACED STIFFENER PER MM 57-20-021-8.Feb 22, 2001 · N283WA · Boeing 727247 · Leading Edge DevicesSDR DL72W010313Door Frame · misdrilledTHE RT AFT ENTRY DOOR FRAME SPLICE INSTALLED PER S/B 727-53-0210 WAS FOUND TO HAVE SHORT EDGE DISTANCE. THE AREA WAS MODIFIED PER S/B AT HMV.Feb 22, 2001 · N2819W · Boeing 727247 · Fuselage Main, StructureSDR DL72W010302Battery · dischargedL1 DOOR OVERHEAD EMERGENCY LIGHT BATTERY DEAD. REPLACED LIGHT ASSY.Feb 20, 2001 · N296WA · Boeing 727247 · Emergency LightingSDR DL72E010301Attach Angle · crackedA .5 INCH VISIBLE CRACK AT I/B STOP ATTACH ANGLE ON NR 7 L/E SLAT. REPAIRED PER MM 57-54-000-8.Feb 20, 2001 · N830WA · Boeing 727247 · Leading Edge DevicesSDR DL72W010283Pin · backed outAFT CARGO EMERGENCY LIGHT INOP ON CARGO DOOR. PIN PUSHED BACK IN D5024P. RESEATED PIN, CKS GOOD.Feb 18, 2001 · N293WA · Boeing 727247 · Emergency LightingSDR DL72W010278Window · crackedUPON LANDING, NOTICED R-1 WINDOW CRACKED. REPLACED R-1 WINDOW AND WINDOW HEAT CONTROLLER.Feb 16, 2001 · N294WA · Boeing 727247 · Flight Compartment WindowsSDR DL72W010273Frame · crackedTHE INNER CHORD OF THE FS 1303 RT FRAME WAS FOUND WITH A CRACKED FLANGE AT A HYDRAULIC BRACKET ATTACH POINT JUST ABOVE THE AFT VENTRAL STAIRWAY TORQUE BOX. THE CRACKED PORTION OF FLANGE WAS TRIMMED OUT AND REPAIRED WITH AN ALUMINUM REPAIR ANGLE PER EFeb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, FrameSDR DL72W010271Skin · crackedTHE UPPER AFT CORNER OF THE R5 COCKPIT WINDOW WAS FOUND WITHA .25 INCH LONG CRACK IN THE SKIN. THE CRACK WAS STOP DRILLED AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 380034-14, REV A.Feb 13, 2001 · N2816W · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72E010269Skin · crackedTHE FUSELAGE SKIN AROUND THE L1 DOOR CUTOUT WAS FOUND WITH A CRACK IN THE LOWER HINGE CUTOUT. THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER INSTALLED PER ER/A 380012-14, REV A.Feb 13, 2001 · N283WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010257Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 480 & 681 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED 11 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN ALONG THE LENGTH OF THE LAP JOINT. THE ENTIRE SKIN LAP WAS CUTOUT AND REPAIREDFeb 12, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010254Skin · crackedLFEC INSPECTION OF THE STRINGER 26L SKIN LAP JOINT BETWEEN FS 480 & 680 INDICATED CRACKS. INTERNAL MFEC INSPECTION CONFIRMED MULTIPLE CRACKS IN THE LOWER SKIN AT THE LOWER FASTENER ROW. THE ENTIRE LAP JOINT WAS CUTOUT TO REMOVE ALL CRACKS. THE JOINT WAS RFeb 12, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010250Stiffener · crackedWING L/E SPAR STIFFENER CRACKED O/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-21-8.Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W010249Stiffener · crackedWING L/E SPAR STIFFENER CRACKED I/B SIDE NR 3 SLAT O/B TRACK. REPAIR PER M/M 57-20-021-8.Feb 12, 2001 · N2816W · Boeing 727247 · Leading Edge DevicesSDR DL72W010248Skin · crackedA 1 INCH CRACK NR 2 L/E FLAP OUTER SKIN AT LOWER LIP INBD HINGE CUTOUT. REPAIR PER M/M 57-53-000-8.Feb 12, 2001 · N2816W · Boeing 727247 · Trailing Edge FlapsSDR DL72W010232Skin · crackedLFEC INSPECTION OF THE STRINGER 4R SKIN LAP JOINT INDICATED CRACKS BETWEEN FS 680 & 740. INTERNAL MFEC INSPECTION CONFIRMED 5 CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. THE ENTIRE SKIN LAP SPLICE WAS CUT AWAY TO REMOVE ALL DAMAGE. THE LAP WAS RESTOFeb 8, 2001 · N296WA · Boeing 727247 · Fuselage Main, Plate/SkinSDR DL72W010231Frame · damagedTHE FS 720D FUSELAGE FRAME WEB WAS DAMAGED BY TOOLING JUST BELOW STRINGER 25R AND THE EXISTING FRAME SPLICE. THE DAMAGE WAS REMOVED WITH A 2 INCH CUTOUT IN THE WEB. THE DAMAGE WAS REPAIRED BY REMOVING THE EXISTING FRAME SPLICE AND FABRIACTING A LARFeb 8, 2001 · N2816W · Boeing 727247 · Fuselage Main, FrameSDR DL72W010225Indicator · inaccurateA/C DIVERSION DUE OUTBOARD FLAPS LOCKED OUT. INSPECTED T/E FLAPS. NO DEFECTS NOTED. OPERATED FLAPS. OP CK NML. SWAPPED INDICATORS AS PRECAUTION. FLAP IND AND OPN NML.Feb 8, 2001 · N2820W · Boeing 727247 · Trailing Flap Position Indicating SystemSDR 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/Skin
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