Boeing 727-200

Service difficulty reports · 2,835

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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 = '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 06FDEA2910Floorbeam · corrodedCORROSION (C53-224-01(2) BS 740 FLOORBEAM UPPER CHORD EMANATING FROM UNDER NUT PLATE RBL 5 WL 208. FLOORBEAM BS 740 UPPER CHORD WAS BLENDED IN AN AREA 4 X 1.5 INCHES RBL 5 WL 208 WITH REMAINING THICKNESS OF .115 FLAP PEENED BLENDED AREA, ALODINED AND PRIMED IAug 9, 2006 · N201FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2909Stringer · damagedSTRINGER DAMAGED AT BS 1090 STR 7R. REPAIRED DAMAGED STRINGER PER SRM 53-10-3.Aug 9, 2006 · N201FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2908Stringer Clip · crackedSTRINGER CLIP CRACKED STA 1090 STR 7R. REMOVED AND REPLACED STRINGER CLIP PER SRM 51-30-02.Aug 9, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2912Skin · unknownN01454 EXISTING EXTERNAL DOUBLER REPAIR APPROX. 9.50 INCHES X 14.50 INCHES AT STA. 494 LT STRINGER NR 19 (DOT NR 16) REQURIES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR AND INSAug 9, 2006 · N201FE · Boeing 727200 · Standard Practices/StructuresSDR 06FDEA2887Skin · dentedDENT IN SKIN AT BS 361 JUST BELOW STR 17L CUT OUT & REMOVED DAMAGE IN SKIN BS 361 BELOW STR 17L. FABRICATED & INSTALLED REPAIR IAW FED EX EA 7-5330-100574. REPAIR IS CONSIDERED A MAJOR REPAIR.Aug 8, 2006 · N201FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2850Indicator · failedMOMENTARY SPEED FLAGS IN VIEW PRIOR TO TAKEOFF ON CAPT AND F/O ADI. ON TAKEOFF ROLL, AFTER INITIAL INCREASE OF AIRSPEED ON F/O AIRSPEED INDICATOR, GOT A FLAG IN THE AIRSPEED WINDOW. AFTER REJECT, FLAG WENT AWAY. REMOVED AND REPLACED F/O'S ELECTRIC AIRSPEED Aug 5, 2006 · N211FE · Boeing 727200 · Airspeed/Mach IndicatorSDR C8GA20060010Window · failedFLT 705 FROM YYC TO MSP. ON CLIMB, AT APPROXIMATELY FL30.0, AIRCRAFT EXPERIENCED SEVERE TURBULENCE AND HAIL DAMAGE. CREW DECLARED AN EMERGENCY AND RETURNED TO YYC. AIRCRAFT LANDED WITHOUT INCIDENT. FOUND NOSE RADOME WITH APPROXIMATELY 24 INCH DIAMETER HOLEAug 4, 2006 · N708AA · Boeing 727200 · Flight Compartment WindowsSDR 06FDEA2848Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950D STR 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 950D, STR 7R IAW SRM 51-30-2 AND 51-30-5.Aug 4, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2847Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 1070 STR 7R. REMOVED AND REPLACED STRINGER CLIP AT STA 1070, STR 7R IAW SRM 51-30-2 AND 51-30-5.Aug 4, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2846Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950D STR 7L. REMOVED AND REPLACED STRINGER CLIP AT STA 950D, STR 7L IAW SRM 51-30-2 AND 51-30-5.Aug 4, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2845Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 970 STR 9R. REMOVED AND REPLACED STRINGER CLIP BS 970 STR 9R IAW SRM 51-30-2.Aug 4, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2832Frame · dentedFUSELAGE UPPER LOBE, FRAME IS DENTED, BS 520, 5 INCHES ABOVE STR 17R. REPAIRED FUSELAGE UPPER LOBE FRAME AT BS 520 5 INCHES ABOVE STR 17R IAW SRM 51-40-3.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2831Frame · dentedFUSELAGE UPPER LOBE, FRAME IS DENTED, BS 500, 5 INCHES ABOVE STR 17R. REPAIRED UPPER LOBE FRAME AT SB 500 5 INCHES ABOVE STR 17R IAW SRM 51-40-3.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2830Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950F, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2829Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 1030, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2828Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 990, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2827Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 1090, STR 7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 AND 51-30-5.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2826Frame · corrodedFUSELAGE UPPER LOBE, CORROSION ON FRAME INNER AND OUTER FLANGE, AT BS 720A BETWEEN STR 1 TO STR 4 RT. REPAIRED FRAME PER SRM 53-10-4.Aug 3, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2789Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950E, STRL 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.Aug 2, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2787Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950B, STR 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.Aug 2, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2788Stringer Clip · crackedSTRINGER CLIP CRACKED AT STA 950C, STR 7L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.Aug 2, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2791Skin · damagedEXTERNAL FLUSH REPAIR ON LT LWR FUSELAGE APPROX 3 X 2 INCHES STA 260, S21L TO 22L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED SKIN PER FED EX EA 7-5330-100558.Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2790Stringer · corrodedCORROSION FWD CARGO BAY: ON STRINGER 28 AT BS 506, LBL 6. REPAIRED STRINGER PER SRM 53-10-3 FIG 1 DETAIL II.Aug 2, 2006 · N281FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2765Door · damagedEXTERNAL DOUBLER REPAIRS, 6 EACH AT NR 3 CARGO DOOR REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED NR 3 CARGO DOOR PER SRM 51-30-2 AND FED EX MM 52-35-051-4.Aug 1, 2006 · N281FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA2746Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 18 X 12 INCHES AT STA 1185 RT STRINGER NR 5 ON UPPER FUSELAGE. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING REPAIR DOUBLER AT STAJul 31, 2006 · N201FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2750Threshold · crackedAFTER REMOVAL OF STUB FRAME FOUND GALLEY DOOR THRESHOLD WEB CRACKED BS 376 WL 208 RBL 65. REPAIRED THRESHOLD PER FED EX DWG 65-56153 AND SRM 51-30-2.Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA2749Door Frame · crackedMAIN CARGO BAY, FWD SERVICE DOOR CUTOUT FWD FRAME IS CRACKED AT BS 380 RBL 65 WL 209. REPAIRED FRAME PER SRM 51-40-3.Jul 31, 2006 · N281FE · Boeing 727200 · Fuselage Main, StructureSDR 06FDEA2748Skin · damagedEXISTING EXTERNAL DOUBLER REPAIR APPROX 2 X 2 INCHES ON RT HORIZONTAL STABILIZER UPPER SURFACE T/E AREA, ELEVATOR STA 99.79 NR 2 BALANCE BAY UPPER PANEL. REPAIR REQUIRES EVALAUTION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPJul 31, 2006 · N201FE · Boeing 727200 · Horizontal Stabilizer, Plate/SkinSDR 06FDEA2747Skin · chafedEXTERNAL SKIN IS CHAFED, AT BS 950E, STR 26R. REPAIRED PER FED EX EA 7-5330-100567.Jul 31, 2006 · N201FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2728Hydraulic System · malfunctionedTHE FLIGHT CREW PERFORMED AIR TURNBACK, INVOKED BY LOSS OF A-SYSTEM HYDRAULIC FLUID INFLIGHT, DURING CLIMBOUT FOR SCHEDULED FLIGHT 0307 FROM MEM, ON 07/28/2006.Jul 28, 2006 · N493FE · Boeing 727200 · Hydraulic System, MainSDR 06FDEA2722Stringer · crackedFWD PIT FS 720-720A, APPROX RBL 17 FLOOR STRINGER CRACKED.Jul 28, 2006 · N242FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA2721Compressor · stalledPDIS 484, 72-00 0008702 27JUL06 SDF OPEN R LOGPAGES: 01298762 REJECTED TAKEOFF AFTER ENGINE FAILURE LIGHT ILLUMINATION AND ASSOCIATED BANG NOISE AND VIBRATION. ENT BY: 188726 RPT BY: 251618 FACT 29JUL06, 14:32 SDF R IAW FLT DATA RECORDER NR 3 ENG COMPRESSORJul 27, 2006 · N484FE · Boeing 727200 · Turbine Engine Compressor SectionSDR 06FDEA2712Skin · chafedEXTERNAL SKIN CHAFED, AT RT WING L/E AND UNDER WING TO BODY FAIRING FWD, WRAP AROUND PANEL, BS 720D 13, STR 19R. REMOVED DAMAGE, AND REPIAR IAW SRM 53-30-3, 53-30-1 AND M/M 51-20-021, 51-20-151.Jul 27, 2006 · N201FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2689Frame · dentedN01255 FUSELAGE UPPER LOBE, FRAME IS DENTED, BS 540, 5 INCHES ABOVE STR 17R. REMOVED DAMAGE AND REPAIRED IAW SRM 53-10-2, 51-20-1, 51-30-5, 51-10-2, 51-40-3, 53-10-4 AND 51-30-2.Jul 26, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2688Frame · dentedFUSELAGE UPPER LOBE, FRAME IS DENTED, BS 580, 5 INCHES ABOVE STR 17R. REMOVED DAMAGE AND REPAIRED FRAME IAW SRM 53-10-2, 51-20-1, 51-40-3, 53-10-4, 51-30-5 AND 51-30-2.Jul 26, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2687Skin · damagedEXTERNAL DOUBLER REPAIR AT NR 3 CARGO DOOR CUTOUTS, 13 INCHES X 5.5 INCHES STA 1148, STRINGER 23R TO 24R REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA REPAIRED SKIN PER FEDEX EA 7-5330-100561.Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2685Skin · damagedN01370 EXTERNAL DOUBLER REPAIR APP. 8.5 X 6.5 ON LT LWR FUSELAGESTA 203 STR 23L. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPARIED SKIN IAW SRM 53-30-3 FIG 24.Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2686Skin · damagedN01354 EXTERNAL DOUBLER REPAIR APPROX 6 INCHES X 8 INCHES ON RT LOWER FUSELAGE STA 294, WL 168. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER INSTALLED PER FED EX EA 7-5Jul 26, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2679Skin · damagedEXTERNAL DOUBLER REPAIR APPROX 22 X 19 INCHES ON RIGHT HAND LOWER FUSELAGE STA 195 - STA 220, STR 19R. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER FED EX EA 7-5330-100557.Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2678Floorbeam · corrodedWHILE WORKING OK TO CLOSE MAIN CARGO AREA FLOORBOARDS, FOUND CORROSION ON PREVIOUS BLEND ON TOP OF FLOORBEAM, AND ONE MISDRILLED HOLE AT; BS 1030, LBL 9, WL 208. CUT OUT CORROSION DAMAGE AND REPAIRED UPPER CHORD OF FLOORBEAM PER SRM 53-10-8 FIG 3.Jul 25, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2681Union · looseTHE A-SYSTEM HYDRAULIC LEAK. COMPLIED WITH QRH AND MADE A NORMAL LANDING. A 1.5 GALLON REMAINED AT BLOCK-IN. REMOVED SEVERAL LEADING EDGE PANELS. NO LEAK FOUND AS OF YET. FOUND UNION LOOSE ON LINE THAT GOES TO OUTBOARD LEFT WING SLAT ACT. TIGHTEN PER B7Jul 25, 2006 · N266FE · Boeing 727200 · Hydraulic System, MainSDR 06FDEA2680Union · looseA-SYSTEM HYDRAULIC LEAK. COMPLIED WITH QRH AND MADE A NORMAL LANDING, 1.5 GALLONS REMAINED AT BLOCK-IN. REMOVED SEVERAL LEADING EDGE PANELS. NO LEAK FOUND AS OF YET. FOUND UNION LOOSE ON LINE THAT GOES TO OUTBOARD LEFT WING SLAT ACT, TIGHTENED PER B727-20Jul 25, 2006 · N266FE · Boeing 727200 · Hydraulic System, MainSDR 06FDEA2670Floorbeam · corrodedFUSELAGE INTERIOR FLOOR STRUCTURE, BS 312 LBL 19 WL 208, FLOORBEAM CORRODED. REPAIRED FLOOR BEAM IAW SRM 53-10-1.Jul 24, 2006 · N201FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2672Frame · dentedDENTED FRAME AT BS 1148 STRINGER 25R. REMOVED DAMAGED AND REPAIR FRAME PER SRM 51-40-3.Jul 24, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2674Repair · misinstalledEXISTING EXTERNAL CIRCULAR DOUBLER REPAIR APPROX 6 INCHES AT STA 950C PLUS 15 INCHES RT STRINGER NR 23. REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXISTING EXTERIOR REPAIR DOUBLER BS 950C PLUJul 24, 2006 · N201FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 06FDEA2667Frame · dentedFRAME DENTED BETWEEN STR 23 AND 24 RT, STA 680. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-40-3 FIG 1.Jul 24, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2666Frame · dentedFRAME DENTED BETWEEN STR 23 AND 24 LT, STA 520. CUT OUT DAMAGE AND FABRICATED REPAIR IAW SRM 51-10-3 FIG 1.Jul 24, 2006 · N201FE · Boeing 727200 · Fuselage Main, FrameSDR 06FDEA2665Floorbeam · corrodedCORROSION ON UPPER CHORD OF FLOORBEAM AT BS 1030, RBL 10, WL 208. REMOVED DAMAGE, FABRICATED, AND INSTALLED REPAIR PARTS PER SRM 53-10-8 FIG 3.Jul 24, 2006 · N281FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA2627Stringer Clip · corrodedCORROSION BS 720C, STR 2L CLIP. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.Jul 19, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 06FDEA2628Stringer Clip · corrodedCORROSION (C53-224-01) BS 720, STR CLIP 4L. REMOVED AND REPLACED STR CLIP IAW SRM 51-30-2.Jul 19, 2006 · N201FE · Boeing 727200 · Fuselage Main, Attach Fittings
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