Boeing 727-227
Service difficulty reports · 5,082
Newest first. General aviation reporting is voluntary.
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 = '727227' 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.
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 = '727227' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 06FDEA1803Stringer Clip · damagedFOUND MECHANICAL DAMAGE TO STRINGER CLIP, BS 680 STRINGER 9 LEFT. REPLACED STRINGER CLIP PER SRM 51-30-2.SDR 06FDEA1789Shear Tie · corrodedFOUND CORROSION ON FRAME SHEAR TIE STA 990 BETWEEN STR 28L - 29L. REPLACED FRAME SHEAR TIE PER SRM 53-10-1, 53-10-4.SDR 06FDEA1802Frame · dentedFOUND FRAME DENT AT BS 720 LBL 8 WL 156. REPAIRED FRAME BS 720 LBL 8 IAW SRM 51-40-3.SDR 06FDEA1829Wedge · chafedFOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 12" FROM UPPER T/E EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 12" FROM UPPER EDGE IAW FED EX EA 7-5530-100549.SDR 06FDEA1828Wedge · chafedFOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 12" FROM UPPER T/E. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX. 12" FROM UPPER EDGE IAW FEDEX EA 7-5530-100549.SDR 06FDEA1822Wedge · chafedFOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 39" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE APPROX. 39" FROM BOTTOM IAW FED EX EA 7-5530-100549.SDR 06FDEA1821Wedge · chafedFOUND UPPER RUDDER, RT T/E WEDGE CHAFED APPROX 69" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER RT TE WEDGE CHAFF APPROX 69" FROM BOTTOM IAW FED EX EA 7- 5530-100549.SDR 06FDEA1820Wedge · chafedFOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 69" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE CHAFF APPROX 69" FROM BOTTOM IAW FED EX EA 7- 5530-100549.SDR 06FDEA1816Wedge · chafedFOUND UPPER RUDDER, LT T/E WEDGE CHAFED APPROX 24" FROM BOTTOM EDGE. REPAIRED UPPER RUDDER LT TE WEDGE APPROX 24" FROM BOTTOM IAW FED EX EA 7-5530-100549.SDR 06FDEA1798Support Angle · corrodedFOUND FUSELAGE BS 336 RBL 9 WL 148, LONGITUDINAL CHORD SUPPORT L ANGLE CORRODED. REPLACED SUPPORT ANGLE PER SRM 51-30-2.SDR 06FDEA1797Structure · corrodedFOUND FUSELAGE BS 336 LBL 18 WL 148, LONGITUDINAL CHORD ATTACH CLIP CORRODED. REPLACED ATTACH ANGLE PER SRM 51-30-2.SDR 06FDEA1796Attach Fitting · corrodedFOUND FUSELAGE BS 336 RBL 18 WL 148, LONGITUDINAL CHORD AND SUPPORT ANGLE ATTACH CLIP CORRODED. REPLACED ATTACH CLIP PER SRM 51-30-2.SDR 06FDEA1795Frame · dentedFOUND FRAME AT BS 540 IS DENTED AND GOUGE BETWEEN STR 22-24LT. REPARIED FRAME PER SRM 51-40-3.SDR 06FDEA1794Frame · dentedFOUND FRAME AT BS 580 BETWEEN STR 22L-24L HAS DENT. REPAIRED FRAME PER SRM 51-40-3.SDR 06FDEA1790Shear Tie · corrodedFOUND CORROSION ON FRAME SHEAR TIE STA 990 BETWEEN STR 29L - 30. REPLACED SHEAR TIE PER SRM 53-10-1, 53-10-4.SDR 06FDEA1792Frame · damagedFOUND AFT CARGO BAY DOUBLE HOLE IN FRAME WEB STA 990 2" ABOVE STR 26R. REPAIRED DOUBLE HOLE IN FRAME IAW FED EX EA 7-5310-100553.SDR XN0A1327Flap System · unknownINBOARD FLAPS WOULD NOT EXTEND. REMOVED INBOARD FLAP INDICATOR. CYCLED FLAPS. RESEATED CONNECTOR ON INDICATOR. CYCLED FLAPS SEVERAL TIMES AND INSPECTED FLAP SYSTEM. NO DAMAGE OR DEFECTS NOTED. CYCLED FLAPS BACK TO ZERO DEGREES. OPERATIONAL CHECK GOOD IASDR 06FDEA1757Skin · corrodedFOUND CORROSION EMANATING FROM UNDER STRINGER R027 AT BS 676, ALSO FASTENER HEAD IS DISHED. REMOVED AND REPLACED STR 27R BS 673-680 PER SRM 53-10-3.SDR 06FDEA1761Stringer Clip · crackedFOUND STRINGER CLIP AT BS 600 LT STR 23 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-5 .SDR 06FDEA1759Stringer · crackedFOUND STRINGER CLIP AT BS 600 LT STR 24 CRACKED. REPLACED STR CLIP PER SRM 53-10-1, 51-30-5.SDR 06FDEA1758Flap Track · corrodedNR 7 FLAP TRACK FORWARD SUPPORT FITTING HAS CORROSION PITTING ON INBOARD FACE. REMOVED FITTING, REPAIRED IAW FED EX DWG SR27-57-020 REV A AND SOPM 20-10-03 AND REINSTALLED FITTING IAW OHM 20-50-01.SDR 06FDEA1756Floorbeam · corrodedFOUND CORROSION ON LWR FLANGE OF FLOORBEAM BS 1130 BETWEEN RBL 6 - 53 WL 200. REPAIRED LOWER CHORD OF FLOOR BEAM IAW FED EX EA 7-5310-102253.SDR 06FDEA1755Stringer · corrodedCORROSION FOUND AT STRINGER 26R BETWEEN STA 700 TO STA 720 WAS OUT OF LIMITS AFTER CORROSION REMOVAL. REMOVED DAMAGED AREA (SECTION OF STRINGER) IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR PART IAW SRM 53-10-3, INSTALLED ALL REPAIR PARTS IAW SRM 51-30-2. REPASDR XN0A1335Hydraulic System · contaminatedON TAXI OUT -A- SYSTEM DROPPED BELOW REQUIRED MINS. FOUND AIR TO BE IN SYSTEM FROM PREVIOUS HYDRAULIC LEAK. CYCLED ALL SYSTEMS NUMEROUS TIMES TO BLEED AIR AND SERVICED -A- HYDRAULIC SYSTEM IAW B727 MM CHAPTER 12-12-00 USING 2 GALLONS. NO LEAKS NOTED AT THISSDR 06FDEA1725Skin · chafedFUSELAGE SKIN CHAFED FROM BODY FAIRINGS BS 950D PLUS 10 BS 990 BTWN STR 27L AND 23L. REPAIRED CHAFFED SKIN IAW SRM 53-30-01.SDR 06FDEA1695Repair · unknownEXTERNAL DOUBLER AT BS 695, STR 28L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED AND REPAIRED EXTERNAL DOUBLER AT BS 695 STR 28L IAW SRM 53-30-3 FIG 3A.SDR 06FDEA1691Skin · gougedFOUND FUSELAGE SKIN GOUGED, BS 720D PLUS 12, STR 19L, MARKED. REPAIRED SKIN PER SRM 53-30-3 FIG 14.SDR 06FDEA1694Repair · misrepairedEXTERNAL DOUBLER AT BS 660, STR 30 REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. EXTERNAL DOUBLER AT BS 660, STR 30 WAS FOUND NOT TO BE ACCOMPLISHED IAW APPROVED DATA. REMOVED DOUBLER, REPAIRESDR 06FDEA1692Stringer Clip · crackedFOUND STRINGER CLIP AT BS 500 LT STR 23 CRACKED. REMOVED AND REPLACED STR CLIP BS 500 STR 23L IAW SRM 51-30-02.SDR 06FDEA1693Stringer Clip · crackedFOUND STRINGER CLIP AT BS 500 LT STR 22 CRACKED. REMOVED AND REPLACED STR CLIP BS 500 STR 22L IAW SRM 51-30-02.SDR 06FDEA1661Engine · failedATTEMPTED TAKEOFF ON 18L HAD SLIGHT COMPRESSOR STALL ON POWER APPLICATION. ABORTED TAKEOFF AND CHECKED ENGINE CONDITIONS ELECTED SECOND ATTEMPT DUE TO CROSSWINDS. ON SECOND ATTEMPT HAD ANOTHER COMPRESSOR STALL. 1ST STALL OCCURRED AT 1.5 EPR AND SECOND STALLSDR 06FDEA1558Stringer · dentedREWORK REQUIRED ON STRINGER 3R BS 401 HAS OPEN HOLE, BS 367 STRINGER IS DENTED. REPAIRED PER EA 7-5310-96627.SDR XN0A1320Brake Assy · draggingON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD.SDR XN0A1920Brake Assy · draggingON TAXI OUT AIRCRAFT BRAKES SEEMED TO DRAG, AIRCRAFT CAME TO A STOP. REMOVED AND REPLACED NR 1 BRAKE ASSY IAW B727 MM CHAPTER 32-41-32. REMOVED AND REPLACED NR 1 MLG WHEEL ASSY IAW B727 MM CHAPTER 32-45-01, OPS CHECKS AND LEAKS GOOD.SDR 06FDEA1560Skin · damagedFWD LOWER RT EXTERIOR FUSELAGE HAVE MULTIPLE LIGHTNING STRIKES BETWEEN BS 480-700 FROM STR 27R TO STR 30R, FURTHER EVALUATION FOUND DAMAGE AT STA 500 BETWEEN STR 28R TO STR 29R IS OUT OF LIMIT. REMOVE SKIN, INTERCOSTAL IAW SRM 51-30-2. FABRICATED DOUBLER, FISDR 06FDEA1531Skin · bulgedFOUND FWD LOWER RT EXTERNAL FUSELAGE BETWEEN BS 500-520 STR 28R, SKIN BULGING. REPAIRED IAW SRM 53-10-1 AND 53-10-3 FIG 1, REPAIR CLASSIFIED AS MAJOR.SDR 06FDEA1485Repair · misinstalledFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1166 STR 30 IS NOT CONFORMED TO FAA APPROVED DATA. REMOVED EXISTING REPAIR, FABRICATED AND INSTALLED REPAIR IAW SRM 53-30-3, FIG 3. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.SDR 06FDEA1467Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1050 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR ISSDR 06FDEA1466Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 988 STR 29L WAS ACCOMPLISHED IAW SB 727-53-0179 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CLASDR 06FDEA1465Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ON STA 700 STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3. BASED ON AN EXTERNAL VISUAL EVAUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP, REPAIR IS SDR 06FDEA1464Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ON STA 660 STR 26L WAS ACCOMPLISHED IAW EA 7-5330-55769A BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS CSDR 06FDEA1463Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 265 STR 17L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 1 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR IS SDR 06FDEA1462Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED FWD OF BOTH HINGE CUTOUTS OF THE LT MAIN ENTRY DOOR WAS ACCOMPLISHED IAW EO 7-5330-7-2345 PT2 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SIZE AND SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESDR 06FDEA1461Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED ON NR 4 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP, REPAIR IS CLSDR 06FDEA1460None · noneFOUND PREVIOUSLY REPAIR INSTALLED ON NR 5 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3 BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS. GENERAL WORKMANSHIP AND REPAIR ISDR 06FDEA1459Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 6 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3. BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL TYPE AND THICKNESS, GENERAL WORKMANSHIP AND REPAIR IS CLASSDR CA060412003Bracket · cracked(CAN) WHILE INVESTIGATING A STIFF THRUST REVERSER SNAG, MAINTENANCE DISCOVERED THE NR 3 ENGINE CONTROL QUADRANT BRACKET CRACKED. BRACKET WAS REPLACED AND AIRCRAFT RETURNED TO SERVICE. (TC NR 20060412003)SDR 06FDEA1377Panel · missingFOUND NR 1 PYLON FWD BLOWOUT PANEL MISSING AFTER TEST FLIGHT. REPLACED MISSING PANEL AND CORRECTED DUCT LEAK AT PRE-COOLER.SDR 06FDEA1365Panel · missingNR 1 ENGINE PYLON MISSING FWD BLOWOUT PANEL. INSTALLED NEW BLOW OUT PANEL IN NR 1 ENGINE PYLON PANEL NR 5402 IAW FED EX MM 54-30-011-8.SDR 06FDEA1364Switch · out of adjustFWD ENTRY DOOR LIGHT CAME ON DURING FLIGHT. ADJUSTED FWD ENTRY DOOR WARNING SWITCH REF MM 52-70-001-5. SWITCH FUNCTIONAL, TESTED OK. PRESSURIZED AIRCRAFT TO SIMULATE FLIGHT LOADS AT 5.5. PSI, SWITCH OPERATION REMAINED NORMAL.
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