Boeing 727-200

Service difficulty reports · 2,835

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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 = '727200'
  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 03FDEA00064Frame · dentedAFT CARGO BAY BS 1130 FRAME IS DENTED AT LBL 27 UPPER FLANGE. DENT IN FRAME BS 1130 AFT CARGO BAY LBL 27 UPPER FLANGE TO BE OUT OF LIMITS. FABRICATED DOUBLER. INSTALLED REPAIR DOUBLER IAW SRM 53-10-1, SRM 51-30-2, SRM 51-40-3 FIG 1.Jan 22, 2003 · N479FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00063Web · corrodedCORROSION, FORWARD CARGO DOORWAY LOWER SILL BEAM WEB, STA 560-620 STR 26R, NUMEROUS AREAS OUTBOARD SIDE. REMOVED, FABRICATED, AND INSTALLED FORWARD CARGO DOOR LWR BEAM WEB IAW SRM 53-10-1, 51-20-1, 51-30-2.Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 03FDEA00065Floorbeam · corrodedCORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE STA 1130, RBL 4, WL 201. REMOVED CORROSION ON FLOORBEAM LOWER CHORD UPPER SURFACE BS 1130, RBL 1-RBL 8, WL 201, IAW SRM. 100 PERCENT MATERIAL LOSS, FOUND TO BE OUT OF LIMITS IAW SRM. REPAIRED LOWER FLANGE OFJan 22, 2003 · N479FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00062Seat Track · corrodedCORROSION ON SEAT TRACK OUTBOARD FLANGE BS 720D - 720D+10 LBL 25 WL 208. REMOVED AND REPLACED NEW SEAT TRACK IAW SRM 51-30-2.Jan 22, 2003 · N263FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00060Odor · detectedLEFT PACK CAUSES FUMES IN COCKPIT WHEN SELECTED TO MOMENTARY WARM TEMP. TWO CREW MEMBERS NOTICED DULL HEADACHE AND ONE CREW MEMBER COMPLAINED OF BURNING EYES. RAN LEFT PACK WARM POSITION WITH NO FUMES OR OTHER DEFECTS NOTED PER B727- 200MM 21-55-000-5. OK FJan 21, 2003 · N487FE · Boeing 727200 · Air Distribution SystemSDR 03FDEA00051Frame · crackedFRAME CRACKED IN THE FWD CARGO BAY. REMOVED DAMAGED FRAME FLANGE. FABRICATED, & INSTALLED REPAIR PARTS IAW SRM 51-40-3 FIG 1.Jan 20, 2003 · N479FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00055Seat Track · corrodedCORROSION IB-FLANGE ON SEAT TRACK NUT PLATE HOLE STA 514 LBL 25 WL 208. R&R SEAT TRACK PER SRM 51-30-2.Jan 20, 2003 · N263FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00054Seat Track · corrodedCORROSION ON SEAT TRACK OB FLANGE BS 650-660 LBL 25 WL 208. R&R SEAT TRACK PER SRM 51-30-2.Jan 20, 2003 · N263FE · Boeing 727200 · Fuselage, Seat/Cargo Attach FittingsSDR 03FDEA00052Frame · crackedFRAME CRACKED IN THE FWD CARGO BAY STA 660 RBL 3 WL 148 UNDER FLOOR SUPPORT. FWD CARGO FRAME CRACKED AT BS 660 RBL 3 WL 148 OUT OF LIMITS PER SRM 53-10-4. FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3Jan 20, 2003 · N479FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00050Floorbeam · corrodedCORROSION ON FLOORBEAM LWR CHORD UPPER SURFACE STA 1130 RBL 4 WL 201.Jan 20, 2003 · N479FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00053Duct · blownDURING CLIMBOUT WITH STANDARD TAKEOFF POWER SET, NR 1 ENGINE FIRELIGHT ILLUMINATED WITH HORN ON. SHUT DOWN ENGINE IAW WITH CHECKLIST. REMOVED AND REPLACED MAIN OIL STRAINER DUE TO INFLIGHT SHUT DOWN OF NR 1 ENGINE. ENGINE WINDMILLED FOR APPROXIMATELY 10 MINJan 18, 2003 · N257FE · Boeing 727200 · Pneumatic Distribution SystemSDR 03FDEA00044Keelbeam · corrodedCORROSION ON FLANGE AND BEAM OB SIDE OF LT KEELBEAM STA 950A AFT CARGO BAY. REPAIRED KEELBEAM BS 950A + 2 STR 29L IAW SRM 27-53-023A.Jan 16, 2003 · N263FE · Boeing 727200 · Fuselage Main, KeelSDR 03FDEA00035Floorbeam · damagedMECHANICAL DAMAGE ON FLOORBEAM BS 990, RBL 37.5, WL 207. REPAIRED FLOORBEAM BS 990 RBL 37.5 WL 207 IAW SRM 53-10-8.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00031Lead · out of positionSTRINGER 20L CHAFED BY GENERATOR LEAD, BS 374, AT LT END OF E1 RACK. REPAIRED STR 20L BS 360-390 IAW SRM.Jan 15, 2003 · N263FE · Boeing 727200 · Electrical Power System WiringSDR 03FDEA00029Hydraulic Line · out of positionHYDRAULIC LINE CHAFING ON STRUCTURE STA 1150, STR 22L, AFT CARGO REPAIRED FRAME IAW EA 7-5310-68161, SRM 51-40-3 FIG 1.Jan 15, 2003 · N263FE · Boeing 727200 · Hydraulic System, MainSDR 03FDEA00027Floorbeam · corrodedCORROSION ON LOWER FLOORBEAM CHORD, AROUND NUTPLATES, STA 1130 0 BL, RBL 48, WL 200. REPAIRED FLOORBEAM BS 113 WL 200 IAW EA 7-5310-68165.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00023Skin · dentedDENT IN EXTERNAL SKIN BS 1033 STR 22-23R. REPAIR PER SRM 53-30-3, SKIN AT BS 1033 STR 22-23R.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00033Frame · damagedMECHANICAL DAMAGE ON FRAME, BS 980, STR 7R. REMOVED MECHANICAL DAMAGE. FABRICATED, DRILLED, ALOINDED, PRIMED, AND INSTALLED REPAIR DOUBLER IAW SRM.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00026Frame · dentedBS 500, FRAME IS DENTED ABOVE STR 22L UPPER FLANGE. REMOVED DAMAGE AREA OF BS 500 FRAME AND FABRICATED REPAIR DOUBLER AND INSTALLED REPAIR DOUBLER IAW SRM.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA000034Floorbeam · corrodedCORROSION ON FLOORBEAM, BS 1030 LBL 9 WL 208. REPAIRED IAW SRM.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00032Frame · dentedFRAME DENTED AT BS 1030 ABOVE STR 26R. REPAIRED DAMAGED FRAME AT BS 1030 ABOVE STR 26R PER SRM AND EA.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00028Floorbeam · corrodedCORROSION ON LOWER FLOORBEAM CORD, AROUND NUTPLATES, STA 1070, 0 BL - RBL 45, WL 200. BLENDED CORROSION ON BS 1070 LOWER CHORD AND FOUND OUT OF LIMITS AT RBL 11 TO RBL 34. REMOVED LOWER CHORD FROM RBL 11 TO RBL 34. FABRICATED REPAIR PARTS AND INSTALLED REPAJan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00030Frame · dentedFRAME, BS 1050 LBL 26 WL 155 HAS A DENT. DENT FOUND TO BE OUT OF LIMITS PER SRM. REPAIRED AREA IAW SRM, E.A.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00039Floorbeam · corrodedCORROSION ON FLOORBEAM BS 312 AT FASTENER HOLES WL 207.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 03FDEA00042Indicator · erraticON TAKEOFF ROLL, JUST PRIOR TO V1, ALL 3 FUEL FLOW INDICATIONS BECAME ERRATIC. AFTER TAKEOFF ALL 3 FUEL FLOW INDICATORS WERE READING APPROX CORRECT BUT FLUCTUATIONS +/- 2000 LBS. AFTER 10 MINUTES ALL THREE FUEL FLOW GAUGES BECAME COMPLETELY ERRATIC AND UNUSAJan 15, 2003 · N206FE · Boeing 727200 · Fuel Flow IndicatingSDR 03FDEA00025Skin · chafedAFT NR 2 LWR CARGO DOOR CHAFING IN EXTERIOR SKIN 3-12 INCHES FROM FORWARD EDGE 0-3 INCHES FROM UPPER EDGE. REPAIRED IAW EA.Jan 15, 2003 · N263FE · Boeing 727200 · Cargo/Baggage DoorsSDR 03FDEA00024Skin · dentedEXTERIOR FUSELAGE SKIN HAS 2 DENTS, BS 1090, 3 INCHES ABOVE STR 7R. REPAIRED SKIN IAW SRM.Jan 15, 2003 · N263FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 2003F00109Light · inoperativeDURING PREFLIGHT TRANSIT CHECK, FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED COCKPIT EMERGENCY LIGHT ASSEMBLY IAW MM 33-40-0. (M)Jan 14, 2003 · N211DB · Boeing 727200 · Emergency LightingSDR 03FDEA00009Skin · dentedOIL CAN DENT IN SKIN AT BS 190, RBL 22, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER, AND INSTALLED REPAIR IAW SRM 53-30-3.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00010Skin · dentedOIL CAN DENT IN SKIN AT BS 211, RBL 23, WL 182. REMOVED DAMAGED AREA OF SKIN. FABRICATED REPAIR DOUBLER. INSTALLED REPAIR IAW SRM 53-30-3.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 03FDEA00007Frame · dentedDENT IN FRAME, BS 950C STR 26L. REPAIR FRAME IAW SRM.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, FrameSDR 03FDEA00006Motor · failedCOMPLETE LOSS OF SYSTEM A HYDRAULIC FLUID JUST PRIOR TO FLAP EXTENSION. SPOILERS HAD BEEN USED JUST PRIOR TO LOSS. REPLACED RIGHT OUTBOARD FLAP MOTOR IAW MM, SERVICED HYDRAULIC SYSTEM TO FULL LEVEL. OPERATED FLAPS UP AND DOWN SEVERAL TIMES, ALL INDICATIONS Jan 8, 2003 · N244FE · Boeing 727200 · Trailing Edge Flap ActuatorSDR 03FDEA00008Skin · corrodedCORROSION UNDER EDGE OF RIGHT RAM AIR DOOR ACTUATOR PANEL. CORROSION OUT OF LIMITS, REPAIRED IAW EA 7-5330-68147.Jan 8, 2003 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00975Skin · damagedFUSELAGE SKIN DAMAGED AT BS 1050, STR 19R, JUST BELOW THE LAP. REPAIRED SKIN IAW SRM.Dec 26, 2002 · N489FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 02FDEA00964Floorbeam · gougedLONGITUDINAL FLOORBEAM OUTBOARD, LOWER FLANGE, UPPER SIDE IS GOUGED, JUST BELOW FASTENER HOLES FROM BS 740-848, RBL 51, WL 208. FABRICATED AND REPLACED LONGITUDINAL BEAM UPPER CHORD IAW SRM.Dec 23, 2002 · N212FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00960Flap · missingFOUND APPROXIMATELY 5.5 FT INBOARD SECTION OF THE LEFT FORE FLAP MISSING ON POST FLIGHT INSPECTION. REMOVED LEFT INBOARD FORE FLAP ASSEMBLY IAW MM. INSTALLED LEFT INBOARD FORE FLAP IAW M/M, SYSTEMS OPS, CHECK NORMAL.Dec 21, 2002 · N468FE · Boeing 727200 · Trailing Edge FlapsSDR 02FDEA00957Frame · corrodedCORROSION, BS 720A, FWD SIDE OF FRAME AT STR 8L.Dec 18, 2002 · N212FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00956Support Angle · corrodedCORROSION FLOORBEAM SUPPORT ANGLE, UPPER FLANGE, LWR SURFACE BS 825, RBL 62, 207.5. REMOVED, FABRICATED AND REPLACED FLOORBEAM SUPPORT ANGLE IAW SRM AT BS 825, RBL 62.Dec 18, 2002 · N212FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 02FDEA00952Stringer · crackedFOUND CRACK IN STR 21 LT AT BS 540.Dec 17, 2002 · N477FE · Boeing 727200 · Fuselage Main, StructureSDR 2003F00165Wire · shortedUPON ENTRY INTO COCKPIT FOUND RIGHT DUCT PRESSURE NEEDLE FLUCTUATING W/WPU OFF, NR 2 FUEL HEAT VALVE C/B POPPING, NR 2 ENGINE OIL PRESSURE INDICATOR FLUCTUATING. NR 3 WING ANTI-ICE VALVE C/B POPPING. NR F/F AND NR 2 EPR POPS C/B. SHORTED WIRES FOUND BURNED ADec 14, 2002 · N894AA · Boeing 727200 · Electrical Power System WiringSDR 02FDEA00936Skin · corrodedFOUND CORROSION ON INNER SURFACE OF SKIN BS 965 LBL 17 WL 139.Dec 11, 2002 · N477FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR P9R2002F00019Light · looseFORWARD GALLEY EMERGENCY FLOOR DIRECTIONAL TRACK LOOSE. RESCURED EMERGENCY FLOOR DIRECTIONAL TRACK IAW MM.Dec 7, 2002 · N919PG · Boeing 727200 · Emergency LightingSDR 02FDEA00934Crease Beam · corrodedN00836 CORROSION C53-224-02 CREASE BEAM BS 500 RBL 67. CORROSION ON CREASE BEAM AT BS 600, RBL 67, WL208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED CREASE BEAM BS 445-525, RBL 67,WL 208. FABRICATED REPLACEMENT CREASE BEAM FROM BAC 1515-531 7075-T6 LODec 6, 2002 · N477FE · Boeing 727200 · Fuselage Main, StructureSDR 02FDEA00929Skin · crackedRT VERTICAL FIN SKIN HAS 2 POSSIBLE CRACKS EMANATING FROM FASTENERS AT BS 1214 COMMON TO SPAR ** SD ** DAMAGE TO RT VERTICAL FIN SKIN AT BS 1214 COMMON TO FRONT SPAR FORGING JUST ABOVE FUSELAGE IS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-01, REPAIRED DAMAGE IDec 6, 2002 · N262FE · Boeing 727200 · Vertical StabilizerSDR 02FDEA00932Frame · dentedFUSELAGE FRAME BS 500 UPPER FLANGE HAS SEVERAL DENTS LBL 33-47. REMOVED EXISTING FRAME SPLICE BS 500, LBL 33. CUT OUT DAMAGED AREAS AT LBL 33 TO LBL 47. FABRICATED AND DRILLED UP NEW FRAME SPLICE. INSTALLED NEW FRAME SPLICE AND FASTENERS IAW B727 SRM AND EDec 6, 2002 · N477FE · Boeing 727200 · Fuselage Main, FrameSDR 02FDEA00930Frame · bentFUSELAGE FRAME BS 500 UPPER FLANGE IS BENT RBL 33 WL 160. REMOVED DAMAGE AND REPAIRED IAW SRM.Dec 6, 2002 · N477FE · Boeing 727200 · Fuselage Main, FrameSDR P9R2002F00018Light · missingPHOTOLUMINESCENT STRIP MISSING IN FORWARD GALLEY. INSTALLED PHOTOLUMINESCENT STRIP IAW MM.Dec 5, 2002 · N919PG · Boeing 727200 · Emergency LightingSDR 02FDEA00924Wire · damagedON CLIMBOUT, DURING FLAP RETRACT, MOVED HANDLE FROM FLAP 5 TO FLAP 2 AND 6. LEADING EDGE FLAP SHOWED IN TRANSIT ON S/O AUX PANEL WITH AMBER LEADING EDGE FLAP LIGHT ON FOWARD PANEL. INSTALLED JUMPER CABLE ON NR 6 LEADING EDGE FLAP IAW MM. MAINTENANCE ANDDec 5, 2002 · N221FE · Boeing 727200 · Flight Control System WiringSDR 02FDEA00922Floorbeam · corrodedCORROSION ON FLOORBEAM, BS 720D, LBL 5. BLENDED CORROSION ON FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM. CUT OUT DAMAGE FROM BS 720-720F, BL 0. FABRICATED AND INSTALLED REPAIR IAW EA.Dec 4, 2002 · N477FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 02FDEA00915Stringer · corrodedCORROSION AT STA 617-624, WL 151, RBL 15, ON STRINGER 27 RT. INSPECTION OF STRINGER 27 RT, WL 151, BS 617 - 624 FOUND IT TO BE OUT OF LIMITS PER BOEING SRM REMOVED DAMAGED AREA AND REPLACED PER BOEING SRM 53-10-3.Dec 4, 2002 · N477FE · Boeing 727200 · Fuselage Main, Longeron/Stringer
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