Boeing 727-277

Service difficulty reports · 627

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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 = '727277'
  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 AUS20040111Switch · out of adjust(AUS) MAIN CARGO DOOR NR 1 AND NR 7 LATCH INDICATOR MICROSWITCHES OUT OF ADJUSTMENT.Feb 13, 2004 · Boeing 727277 · Door Warning SystemSDR AUS20031147Fitting · corroded(AUS) NR 1 ENGINE FORWARD SUPPORT FITTING TOP SURFACE CORRODED IN AREA BETWEEN FITTING AND UPPER STRUT SKINS. FOUND DURING INSPECTION IAW AD/B727/151.Nov 12, 2003 · Boeing 727277 · Engine Mount SectionSDR AUS20031093Shaft · sheared(AUS) MAIN CARGO DOOR FORWARD AND AFT ACTUATOR PIVOT SHAFTS SHEARED. SECONDARY DAMAGE CAUSED TO AFT ACTUATOR MAIN SUPPORTS.Oct 27, 2003 · Boeing 727277 · Cargo/Baggage DoorsSDR AUS20030855Switch · faulty(AUS) TRAILING EDGE FLAP 27.5 SWITCH (S294) FAULTY. FOUND DURING INSPECTION IAW AD/B727/105.Aug 21, 2003 · Boeing 727277 · Trailing Flap Position Indicating SystemSDR AUS20030562Wheel · disintegrated(AUS) NR 3 MAIN WHEEL ASSEMBLY INBOARD HUB DISINTEGRATED IN AREA AROUND THE INBOARD BEARING HUB. BRAKE ASSEMBLY DAMAGED.Jun 10, 2003 · Boeing 727277 · Wheel/Ski/FloatSDR AUS20030501Switch · out of adjust(AUS) MAIN CARGO DOOR AFT AUXILIARY LATCH SWITCH OUT OFADJUSTMENT.May 9, 2003 · Boeing 727277 · Door Warning SystemSDR 03FDEA00338Warning System · false activationDESCENDING THROUGH 10,000 FT, APU FIRE LIGHT CAME ON. PULLED FIRE HANDLE AND LIGHT WENT OUT.Mar 19, 2003 · N242FE · Boeing 727277 · Smoke DetectionSDR 03FDEA00172Compressor · stalledUPON LEVELING AT FL310 WITH CRUISE POWER SET AND AFTER CLOSING ENGINE, ANTI-ICE COMPRESSOR STALLS. NR 2 ENGINE EPR DROPPED FROM 1.8 TO 1.2,EGT STARTING TO CLIMB, NR 2 THROTTLE TO IDLE. SLOWLY RESTORED NR 2 POWER AND CYCLED ENGINE ANTI-ICE BACK TO OFF, COMPREFeb 22, 2003 · N245FE · Boeing 727277 · Fuel Control/Turbine EnginesSDR AUS20030257Bleed Valve · fractured(AUS) NR 1 ENGINE THIRTEENTH STAGE BLEED VALVE SEPARATED.Feb 19, 2003 · Boeing 727277 · Compressor Bleed ValveSDR AUS20030303Panel · corroded(AUS) AFT CARGO DOOR THRESHOLD PANEL CONTAINED LEVEL 2 CORROSION ANDREQUIRED REPLACEMENT DUE TO BEING WORN BEYOND LIMITS. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Plate/SkinSDR AUS20030302Frame · corroded(AUS) FUSELAGE FRAME BS 950E CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA LOCATED BETWEEN STRINGER 28L AND STRINGER 29L. FOUNDDURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030301Stringer · corroded(AUS) STRINGER 29L CONTAINED LEVEL 2 CORROSION ON THE OUTBOARD LEG ON THE FORWARD AND AFT SIDES OF FRAME 950E. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030300Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS 950B BETWEEN STRINGER 27R AND STRINGER 28R CONTAINED LEVEL 2 CORROSION ON THE LOWER FLANGE. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030299Intercostal · corroded(AUS) INTERCOSTAL IN AFT CARGO AREA CONTAINED LEVEL 2 CORROSION BETWEEN BS1070 TO BS1090 AND STRINGER 30. FOUND DURING CPCP INSPECTIONIAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030298Stringer · corroded(AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREA LOCATED BETWEEN BS 1070 TO BS 1090. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030297Stringer · corroded(AUS) STRINGER 27L CONTAINED LEVEL 2 CORROSION AT LOCATION BS 1128.FOUND DURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030296Bracket · corroded(AUS) CLIP BRACKET JOINING STRINGER 27L TO FRAME AT LOCATION BS 1130 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INVESTIGATION IAWC53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030295Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS1130 CONTAINED LEVEL 2 CORROSION ON LOWER FLANGE IN AREA BETWEEN STRINGER 28L AND 29L. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030294Frame · corroded(AUS) FUSELAGE FRAME LOCATED IN BILGE AREA AT BS 970 BETWEEN STRINGER28R AND STRINGER 29R CONTAINED LEVEL 2 CORROSION ON THE LOWER LEG. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030293Frame · corroded(AUS) FRAME FORMER LOCATED AT BS 1090 BETWEEN STRINGER 28R AND STRINGER29R CONTAINED LEVEL 2 CORROSION ON AFT FACE. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030292Bracket · corroded(AUS) ANGLE BRACKET LOCATED AT CARGO FLOOR LEVEL BS 720D BL 21L CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030291Floorbeam · corroded(AUS) AFT CARGO FLOORBEAM ANGLE CONTAINED LEVEL 2 CORROSION IN AREALOCATED AT BS 1166 ABOVE STRINGER 27L BETWEEN BL16L AND BL23L. FOUND DURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Floor BeamSDR AUS20030290Stringer · corroded(AUS) STRINGER 30 CONTAINED LEVEL 2 IN AREA LOCATED AT BS1010. FOUNDDURING INSPECTION IAW CPCP C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030289Stringer · corroded(AUS) AFT CARGO STRINGER 27L CONTAINED LEVEL 2 CORROSION IN AREALOCATED BETWEEN BS950D AND BS1030. FOUND DURING CPCP INSPECTION IAW C53-013-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030288Frame · corroded(AUS) FUSELAGE FRAME LOCATED AT BS 1050 STRINGER 27R CONTAINED LEVEL 3 CORROSION ON THE TOP FLANGE. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030287Stringer · corroded(AUS) STRINGER 27R CONTAINED LEVEL 2 EXFOLIATION CORROSION AT BS 480. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030286Frame · corroded(AUS) FUSELAGE FRAME LOWER FLANGE CONTAINED LEVEL 2 CORROSION AT BS 660 BETWEEN STRINGER 26R AND STRINGER 27R. FOUND DURING CPCPINSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030285Stringer · corroded(AUS) STRINGER SPLICE ON STRINGER 27L LOCATED AT BS 680 CONTAINED LEVEL2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030284Frame · corroded(AUS) FUSELAGE FRAME FLANGE LOCATED AT BS 720A CONTAINED LEVEL 2 CORROSION IN AREA BETWEEN STRINGER 27R AND 28R. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030283Frame · corroded(AUS) FUSELAGE FRAME LOWER LEG LOCATED AT ZONE 1 BS 580 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURINGCPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030282Frame · corroded(AUS) FUSELAGE FRAME LOWER LEG SHEAR TIES LOCATED AT BS 600 BETWEEN STRINGER 27 RT AND STRINGER 28 RT CONTAINED LEVEL 2 CORROSION.FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030281Intercostal · corroded(AUS) INTERCOSTAL LOCATED IN FORWARD CARGO AREA BETWEEN FRAME BS 580 AND FRAME BS 600 AT STRINGER 28 RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-113-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, FrameSDR AUS20030280Skin · corroded(AUS) NR 3 CARGO DOOR CUTOUT AFT LOWER CORNER CONTAINED LEVEL 2CORROSION IN THE AREA LOCATED BETWEEN SKIN LAMINATIONS AT STA 1140 TO 1148 AND BETWEEN STRINGER 26 RT AND STRINGER 27 RT. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, Plate/SkinSDR AUS20030279Strap · corroded(AUS) INTERNAL SKIN REINFORCING STRAP LOCATED ON THE AFT SIDE OF FUSELAGE FRAME AT STA 1090 BETWEEN STRINGERS 26RT AND 27RT CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Main, StructureSDR AUS20030271Angle · corroded(AUS) VERTICAL ANGLE LOCATED IN THE AVIONICS COMPARTMENT BILGE AT STA 368 LBL 15 CONTAINED LEVEL 2 CORROSION. FOUND DURING CPCP INSPECTION IAW C53-111-01.Feb 12, 2003 · Boeing 727277 · Fuselage Miscellaneous StructureSDR AUS20030152Hose · leaking(AUS) NR 2 ENGINE OIL PRESSURE TRANSMITTER SUPPLY LINE HOSE LEAKING.Feb 12, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030153Filter · damaged(AUS) NR 1 ENGINE OIL FILTER THREAD STRIPPED. PERSONNEL/MAINTENANCE ERROR.Feb 11, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030151Relief Valve · faulty(AUS) NR 1 ENGINE OIL PRESSURE RELIEF VALVE FAULTY.Feb 10, 2003 · Boeing 727277 · Turbine Engine Oil SystemSDR AUS20030268Flap Track · corroded(AUS) LT OUTBOARD FLAP OUTBOARD TRACK FORWARD ATTACHMENT FITTINGCONTAINED LEVEL 2 CORROSION. FOUND DURING INSPECTION IAW CPCP C57-581-06.Feb 8, 2003 · Boeing 727277 · Trailing Edge FlapsSDR AUS20030269Stringer · corroded(AUS) FUSELAGE STRINGER 18A LOCATED AT STN 930 RT CONTAINED LEVEL 2 CORROSION BETWEEN THE FASTENERS ON THE LOWER LEG OF THE TEE SECTION. FOUND DURING INSPECTION IAW CPCP C53-100-01.Feb 7, 2003 · Boeing 727277 · Fuselage Main, Longeron/StringerSDR AUS20030118Clamp · loose(AUS) NR 3 ENGINE THIRTEENTH STAGE MODULATING VALVE LEAKING FROM REAR DUCT CLAMP.Feb 5, 2003 · Boeing 727277 · Engine Bleed Air SystemSDR AUS20030267Skin · corroded(AUS) WING CENTER SECTION UPPER SKIN CONTAINED LEVEL 2 CORROSION AT SECTION 46 STN 825 RBL 13. FOUND DURING INSPECTION IAW CPCP C53-224-05.Jan 8, 2003 · Boeing 727277 · Wing, Plate/SkinSDR AUS20030304Stiffener · corroded(AUS) FORWARD SPAR LEADING EDGE VERTICAL STIFFENER CONTAINED LEVEL 2CORROSION LOCATED AT STN236. FOUND DURING CPCP INSPECTION IAW C57-562-02.Jan 2, 2003 · Boeing 727277 · Wing Miscellaneous StructureSDR AUS20030270Spar · corroded(AUS) LT WING REAR LOWER SPAR CONTAINED LEVEL 3 CORROSION AT WS 200. FOUND DURING CPCP INSPECTION IAW C57-581-03.Jan 2, 2003 · Boeing 727277 · Wing SparSDR 02FDEA00937Stringer · dentedFUSELAGE STRINGER 24L HAS DENT DAMAGE AT BS 565.Dec 11, 2002 · N477FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 02FDEA00938Stringer · corrodedFOUND CORROSION ON STR 27L BS 965. REPAIRED DAMAGED STRINGER 27L BS 965 PER SRM 53-10-3 FIG 1Dec 11, 2002 · N477FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 02FDEA00939Frame · dentedFUSELAGE FRAME BS 520 UPPER FLANGE HAS SEVERAL DENTS RBL 33-42.Dec 11, 2002 · N477FE · Boeing 727277 · Fuselage Main, FrameSDR 02FDEA00940Stringer · crackedSTR 15R AT BS 720B+4 CRACKED. REPAIRED PER SRM 53-10-3 FIG 5.Dec 11, 2002 · N477FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 02FDEA00941Skin · gougedGOUGE IN SKIN BS 1070, STR 25R, WAS FOUND OUT OF LIMITS. REPAIRED SKIN AT BS 1070, STR 25R PER SRM 53-30-3, FIGURE 3.Dec 11, 2002 · N477FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR AUS20021306Panel · separated(AUS) NO2 ENGINE RH FORWARD COWL BLOWOUT PANEL MISSING. PANEL WAS FOUND ON RUNWAY.Nov 14, 2002 · Boeing 727277 · Engine Cowling System
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