Boeing 727-22

Service difficulty reports · 1,282

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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 = '72722'
  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 04FDEA03074Spar · corrodedCORROSION LT HORIZONTAL STAB UPPER FRONT SPAR CHORD INTERNAL SURFACE IN AREAS FROM STAB STA 4.45 TO STAB STA 33. REPAIRED IAW SRM 51-10-6. 51-30-2, 51-10-2, 55-10-5.Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03073Spar · corrodedCORROSION ON LT HORIZONTAL STAB INTERNAL UPPER FRONT SPAR CHORD STAB STA 64. REPAIRED IAW SRM 51-10-6, 51-30-2, 51-10-2, 55-10-5.Nov 11, 2004 · N166FE · Boeing 72722 · Horizontal Stabilizer, Spar/RibSDR 04FDEA03072Beam · corrodedCORROSION ON LONGITUDINAL BEAM BS 750 - 840, RBL 25, WL 208. REPAIRED PER SRM 53-10-1, 51-20-4, 51-30-2, 51-70-1.Nov 10, 2004 · N233FE · Boeing 72722 · Fuselage Main, StructureSDR 04FDEA03071Floorbeam · corrodedCORROSION AT FLOORBEAM UPPER AND LOWER SURFACE BS 344 LBL 10 - RBL 10. REPAIRED FLOORBEAM BS 344 LBL 10 - RBL10 PER SRM 53-10-1 AND FEDEX SR 27-53-007.Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03068Floorbeam · damagedMECHANICAL DAMAGE ON FLOORBEAM STA 700 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8Nov 10, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03062Hinge Fitting · corrodedCORROSION ON RT WING O/B AILERON I/B CTR FITTING A/C SIDE IS CORRODED ON LOWER SURFACE. REPAIRED PER MM 27-10-031-2, SRM 51-30-2, 51-30-5.Nov 9, 2004 · N166FE · Boeing 72722 · Wing, Control Surface Attach FittingsSDR 04FDEA03056Frame · dentedFRAME BS 1030 LT AT STR 24 AND 25, DENTED. REPAIRED FRAME PER SRM 51-40-3.Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03055Floorbeam · damagedMECHANICAL DAMAGE ON FLOORBEAM BS 720 TOP CHORD LWR SURFACE LBL 64. REJECTED DUE TO DAMAGE STILL EXISTS. REPAIRED PER SRM 53-10-8Nov 9, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03029Frame · dentedAFT CARGO FRAME DENTED AT BS 1030, STR 26R. REPAIRED PER SRM 51-40-3.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03028Frame · dentedAFT CARGO FRAME DENTED AT BS 990 STR 26 LT. REPAIRED PER SRM 51-40-3, 51-10-2 AND 51-30-2.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, FrameSDR 04FDEA03027Skin · dentedBS 294, STR 21 RT, DENTS AROUND 3 FASTENERS. REPAIRED PER SRM 53-30-1, 53-30-3.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 04FDEA03045Floorbeam · corrodedFOUND CORROSION ON FLOORBEAM AT BS 620 BL O - LBL 8 (C53-111-01(3)). CORROSION REMOVED ON FLOORBEAM FOUND TO BE OUT OF LIMITS. FLOORBEAM TO BE REPAIRED ON N00920.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03044Web · crackedFUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED AT STA 880-890, LBL 47, WL 206. REPLACED VERTICAL WEB PER SRM 51-10-2, 51-30-2 & SRM 51-30-5.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 04FDEA03047Floorbeam · corrodedCORROSION (C53-224-01) AT FLOORBEAM UPPER CHORD AT BS 620, LBL 45-65, WL 208.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03046Floorbeam · corrodedCORROSION FLOORBEAM STA 620 LWR CHORD LWR SURFACE CORRODED LBL 8 AROUND NUTPLATE HOLE. REPAIRED PER SRM 53-10-1, 53-10-8Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 04FDEA03043Stringer · gougedMAIN CARGO BAY HAS GOUGE ON STRINGER 9R AT BS 600.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 04FDEA03042Web · crackedFUEL FEED LINE PRESSURE BOX INBOARD VERTICAL WEB CRACKED, STA 880-890 RBL 47, WL 206. REPAIRED PER SRM 51-30-2, 51-30-5, 51-10-3, 51-10-2Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 04FDEA03041Stringer Clip · crackedSTRINGER CLIP CRACKED, STR 5L, BS 1010. REPLACED PER SRM 51-30-2, 51-30-5Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage Main, Attach FittingsSDR 04FDEA03040Seat Track · gougedSEAT TRACK GOUGED AT BS 740, RBL 45, WL 208. REPAIRED SEAT TRACK PER SRM 53-10-5.Nov 8, 2004 · N166FE · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 04FDEA03016Stringer · damagedSTR L23 DAMAGED AT BS 376 TO 388. REPAIRED PER SRM 53-10-3.Nov 4, 2004 · N166FE · Boeing 72722 · Fuselage Main, Longeron/StringerSDR 04FDEA03014Skin · gougedAFT CARGO DOOR EXTERNAL SKIN GOUGED AT LWR EDGE, 17 INCH FROM AFT EDGE. REPAIRED SKIN IAW SRM 52-00-3.Nov 3, 2004 · N166FE · Boeing 72722 · Cargo/Baggage DoorsSDR CA030805003Support · cracked(CAN) DURING 'C' CHECK INSPECTION, NOSE WHEEL WELL SUPPORT FOUND CRACKED BS 294 RBL 12. REPAIR CARRIED OUT AS PER SRM.Jul 22, 2003 · Boeing 72722 · Fuselage Miscellaneous StructureSDR CA030729012Control Cable · frayed(CAN) DURING INSPECTION OF THE STATION 870 AREA AT C-CHECK IT WAS FOUND THAT THE NR 3 ENGINE THRUST CABLE WAS FRAYED TO THE POINT OF 1 (ONE) STRAND REMAINING. THE CAUSE WAS IMPROPER ROUTING OF THE CABLE. THE CABLE WAS NOT ON THE PULLEY AND WAS CHAFING ON THEJul 2, 2003 · Boeing 72722 · Power LeverSDR CA030805004Control Cable · frayed(CAN) DURING INSPECTION OF THE STATION 870 AREA AT 'C' CHECK, IT WAS FOUND THAT THE NR 3 ENGINE THRUST CABLE WAS FRAYED TO THE POINT OF ONE (1) STRAND REMAINING. THE CAUSE WAS IMPROPER ROUTING OF THE CABLE. THE CABLE WAS NOT ON THE PULLEY AND WAS CHAFING ON THJul 2, 2003 · Boeing 72722 · Power LeverSDR C1HA200396006Seat Track · gougedLT OTBD SEAT TRACK GOUGED BETWEEN BS 954 & 956May 20, 2003 · N696CA · Boeing 72722 · Fuselage, Seat/Cargo Attach FittingsSDR 02FDEA00869Floorbeam · corrodedCORROSION ON LWR CHORD OF BS 950F AT NUT PLATEHOLE, RBL 24, WL 200.Nov 10, 2002 · N264 · Boeing 72722 · Fuselage Main, Floor BeamSDR 02FDEA00786Bushing · out of adjustMODERATE AIRFRAME FLUTTER ABOVE 280 KNOTS, GOES AWAY WITH SPEED BRAKE HANDLE PULLED TO ABOVE 5 DEGREES WHEN SLOWED DOWN, FLUTTER RETURNS DURING LEFT TURNS. FOUND RIGHT OUTBOARD TRAILING EDGE FLAP, ECCENTRICS REQUIRED ADJUSTMENT. ADJUSTED AFT FLAP ECCENTRIC BOct 31, 2002 · N148FE · Boeing 72722 · Trailing Edge FlapsSDR 02FDEA00539Frame · corrodedCORROSION ON FRAME AT BS 680 STR 25R. REMOVED AND REPLACED FRAME PER EA 7-5310-65004 & SRM 53-10-9 FIG 11.Jul 31, 2002 · N465FE · Boeing 72722 · Fuselage Main, FrameSDR 02FDEA00541Skin · chafedEXTERNAL SKIN CHAFED AT STR 19R BS 720D+13. REMOVED AND REPLACED SKIN PER SRM 53-30-3 FIG 14.Jul 31, 2002 · N465FE · Boeing 72722 · Fuselage Main, Plate/SkinSDR 02FDEA00540Stringer Clip · crackedINTERIOR CABIN HAS CRACKED STR CLIP AT BS 680 STR 4L. REMOVED AND REPLACED CLIP PER SRM 51-30-2.Jul 26, 2002 · N465FE · Boeing 72722 · Fuselage Miscellaneous StructureSDR 02FDEA00542Floorbeam · corrodedCORROSION ON FLOORBEAM AROUND 2 FASTENER HOLES BS 480 RBL 10 WL 208. REMOVED AND REPLACED FLOORBEAM PER SRM 53-10-8 FIG 8.Jul 26, 2002 · N465FE · Boeing 72722 · Fuselage Main, Floor BeamSDR 02FDEA00528Floorbeam · corrodedCORROSION ON FLOORBEAM AT NUT CLIP LOCATION BS 950F LBL 10.5 WL 208. REMOVED AND REPLACED FLOORBEAM AT BS 950F, LBL 10.5, WL 208 PER SRM 53-10-8 FIG 8.Jul 25, 2002 · N465FE · Boeing 72722 · Fuselage Main, Floor BeamSDR DHL2002707003Accessory Unit · malfunctionedAFTER GEAR RETRACTION MOVED GEAR HANDLE TO OFF, GEAR DOOR LIGHT FORWARD PANEL AND RIGHT MAIN GEAR DOOR LIGHT S/O PANEL ILLUMINATED. MOVED GEAR HANDLE TO UP, LIGHTS OUT, HANDLE TO OFF, LIGHTS OUT NORMAL OPS. ACCOMPLISHED POWER OFF RERACK OF LDG ACCY UNIT, CLEApr 30, 2002 · N707DH · Boeing 72722 · Landing Gear Retraction/Extension SystemSDR 02FDEA00289Altimeter · failedCAPT'S ALTIMETER GOT OFF FLAG ON CLIMBOUT, ALSO GOT OFF FLAG IN ALTITUDE ALERT BOX, WHEN OFF FLAG SHOWING, ALTIMETER DIDN'T MOVE. REMOVED AND REPLACED CAPT'S ALTIMETER PER MM 34-12-011-5.Apr 25, 2002 · N151FE · Boeing 72722 · Altimeter, Barometric/EncoderSDR 02FDEA00290Hydraulic Line · leakingHYDRAULIC A-QTY TO ZERO IN FLT. REMOVED AND REPLACED NR 1 ENG A-SYSTEM HYDRAULIC PRESS LINE. REMOVED AND REPLACED 1 & 2 ENGINE HYD PUMP CASE DRAIN FILTERS PER MM 29-11-041-2.Apr 25, 2002 · N169FE · Boeing 72722 · Hydraulic System, MainSDR DHL2002707002Switch · inoperativeFIRE ALARM BELL DOES NOT WORK FOR ANY ALARM FUNCTION. REMOVED AND REPLACED THE S41 CUTOFF SWITCH WITH SERVICEABLE SWITCH, OPS CHECK GOOD IAW BOEING WM 26-11-01.Jan 30, 2002 · N707DH · Boeing 72722 · Fire DetectionSDR 02FDEA00059Connector · dirtyCARGO DOOR SMOKE LIGHT ILLUMINATED. PRESSED BOTTLE NR 1 DISCHARGE PER QRHB. CLEANED CONNECTORS.Jan 23, 2002 · N149FE · Boeing 72722 · Smoke DetectionSDR DHL2002707001Sensor · failedAPU FIRE TEST INOP. REMOVED AND REPLACED FIRE DETECTOR SENSOR IAW DHL 727 MM 26-15-002. SYSTEM OPS CHECKED GOOD.Jan 22, 2002 · N707DH · Boeing 72722 · Fire DetectionSDR 02FDEA00032Window · defectiveAFTER T/O ELECT FIRE BY CAPT'S SEAT. APPEARED TO BE WINDOW HEAT WIRE. REMOVED AND REPLACED SLIDING WINDOW, HARNESS, CIRCUIT BREAKER C153, TRANSFORMER T48 AND BACKSHELL OF CONNECTOR D9489.Jan 8, 2002 · N148FE · Boeing 72722 · Flight Compartment WindowsSDR TX22002F00000Bearing · failedDURING REMOVAL OF THE HORIZONTAL STABILIZER HINGE PINS TO COMPLY WITH THE AD AND SB. FOUND RIGHT HINGE BEARING TO HAVE FAILED WITH PIECES MISSING. LEFT BEARING WAS CRACKED. DURING FURTHER INSPECTION FOUND NUMEROUS BUSHINGS AND ATTACH HARDWARE IN THE HORIZONDec 27, 2001 · N400RG · Boeing 72722 · Vertical StabilizerSDR 01FDEA01098Actuator · failedDURING T/O, NR 7 LEADING EDGE FAILED TO RETRACT. REMOVED AND REPLACED SLAT ACT PER MM 27-81-032-4.Dec 20, 2001 · N198FE · Boeing 72722 · Leading Edge Slat ActuatorSDR 01FDEA01092Module · bypassingAPPROX 10 MIN AFTER T/O NR 1 & 2 ENG DRIVEN HYS SYS A PUMPS LOW PRESS LIGHTS ILLUM'D HYD QTY REMAINED STEADY 3.5 GAL ALL HYD C/B WERE IN SYS A PRESS WENT TO ZERO AND SYS A FLT CONT LOW PRESS LIGHTS ILLUM'D. REPLACED SYS A MODULAR UNIT IAW AMM 29-11-061-4. RDec 20, 2001 · N189 · Boeing 72722 · Hydraulic System, MainSDR DHL2001707015Autopilot Sys · malfunctionedWHILE ON FINAL APPROACH COURSE WITH BOTH LOCALIZERS AND GLIDESLOPE INITIALLY CAPTURED ON AUTOPILOT, THE AUTOPILOT WAS NOT CAPABLE OF FLYING THE GLIDESLOPE. AIRCRAFT DOVE FOR THE GROUND. PERFORMED OPERATIONAL CHECK OF AUTOPILOT SYSTEM IAW 727 MM CH 22-00 AND Dec 14, 2001 · N707DH · Boeing 72722 · Autopilot SystemSDR DHL2001707014Windshield Wiper · out of adjRANGE OF MOTION ON WINDSHIELD WIPERS, BOTH CAPT AND F/O ARE INADEQUATE FOR NORMAL FIELD OF VISION (DO NOT COME UP HIGH ENOUGH). WINDSHIELD WIPERS NEED REPLACING (BLADES). TESTED AND ADJUSTED NR 1 AND NR 2 WIPER ASSB IAW 727 MM CHP 30-42. GROUND CKS NORMAL ADec 14, 2001 · N707DH · Boeing 72722 · Windshield/Door Rain/Ice RemovalSDR 01FDEA01027Downlock Switch · faulty1-387 AFTER T/O UNSAFE GEAR LIGHT ILLUMINATED. R&R R/H LAND GEAR DOWNLOCK SWITCH & ACCESSORY UNIT PER MM 32-61-021-4, 32-09-111-4.Dec 4, 2001 · N193FE · Boeing 72722 · Landing Gear Position and WarningSDR 01FDEA01013Receiver · faultyRADAR INTERMITTENT GIVES GOOD PRESENTATION THEN GETS DISTORTED. REMOVED AND REPLACED WEATHER RADAR RECEIVER/ TRANSMITTER AND COLOR IND PER MM 34-41-041-4.Nov 29, 2001 · N149FE · Boeing 72722 · Weather Radar SystemSDR 01FDEA00966Line · blownNR 1 ENGINE STRUT OVERHEAD LIGHT CAME ON. REMOVED AND REPLACED BLOWN T/R HOSE IN NR 1 PYLON AREA. NO LEAKS NOTED. OK FOR SERVICE.Nov 6, 2001 · N151FE · Boeing 72722 · Pneumatic Distribution SystemSDR 01FDEA00964Clamp · looseNR 1 ENG STRUT OVERHEAD LIGHT ILLUM. SECURED CLAP AND CONNECTOR PER MM 36-00-000-5. OPS CHECK OK.Nov 2, 2001 · N151FE · Boeing 72722 · Pneumatic Distribution SystemSDR 01FDEA00951Clamp · loose01-357 #1 ENG STRUT OVERHEAT ILLUM IN GLT. TIGHTENED CLAMP ON HIGH PRESS MODULATING VALVE (SHUTOFF).Nov 1, 2001 · N151FE · Boeing 72722 · Overheat DetectionSDR 01FDEA00892Outflow Valve · failedAIRCRAFT FAILED TO PRESS. REMOVED AND REPLACED LEFT OUTFLOW VALVE PER MM 21-30-051-4.Oct 16, 2001 · N149FE · Boeing 72722 · Pressure Regulator/Outflow Valve
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