Boeing 727-225
Service difficulty reports · 4,226
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 = '727225' 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 = '727225' 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 20010214SG004Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND RIGHT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M)SDR CA010212011Engine · failed(CAN) ENROUTE TO CPH FROM EMA NR 1 ENGINE OIL QUANTITY SLOWLY DECREASED TO 1 GALLON AT WHICH POINT THE INFLIGHT SHUT DOWN WAS PERFORMED. THE A/C LANDED WITHOUT INCIDENT AT CPH. THE ENGINE MAINTAINED POSITIVE OIL PRESSUE FOR THE 20-25 MINUTE PERIOD OF WINDMILL SDR DL72S010078Control Unit · leakingDURING CRUISE B-SYSTEM HYD QTY DECREASED. FOUND UPPER RUDDER POWER CONTROL UNIT LEAKING. REPLACED UPPER RUDDER POWER CONTROL UNIT.SDR SCNA01317Plate · corrodedDURING HEAVY MAINTENANCE CHECK, CORROSION WAS DISCOVERED OUT OF LIMITS ON THE LEFT HAND WING FRONT SPAR LOWER FORWARD CHORD PLATE, WS 360 TO WS 450. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 513002. FABRICATED NEW CHORD FROSDR SCNA01009Door · out of adjDURING CLIMB THE FORWARD ENTRY DOOR EXIBITED AN EXTREMELY LOUD SQUEAL IN FLIGHT, THE SOUND DID NOT ALTER DUE TO CHANGES IN AIRSPEED, ALTITUDE OR CABIN PRESSURE. THE FLIGHT CREW ELECTED TO RETURN TO MSP, THE POINT OF ORIGIN. REPOSITIONED THE DOOR SNUBBER, ANDSDR 20010214SG003Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND LEFT MID EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED LEFT MID OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-22-101. OPS CHECK GOOD. (M)SDR 20010214SG005Battery Pack · dischargedON PREFLIGHT TRANSIT, FOUND FORWARD EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REMOVED AND REPLACED RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-50-22. OPS CHECK GOOD. (M)SDR 20010124SG003Computer · malfunctionedAUTO PILOT PORPOISES IN CRUISE MODE ''A'' CONTINUOUSLY TRIMS STAB UP AND DOWN. REMOVED AND REPLACED AUTO PILOT PITCH COMPUTER. OPS CHECK OK IAW MM 22-11-12. (M)SDR SCNA01316Sign · will not testDURING HEAVY MAINTENANCE CHECK, THE LT FWD EMERGENCY HATCH EXIT SIGN FAILED LUMINESCENCE CHECK. REMOVED AND REPLACED IAW B727 335031.SDR SCNA01315Sign · failedDURING HEAVY MAINTENANCE INSPECTION THE LT AFT EMERGENCY EXIT HATCH SIGN FAILED TEST. REMOVED AND REPLACED IAW B727 MM 335031.SDR SCNA01314Sign · failedDURING HEAVY MAINTENANCE CHECK THE RT AFT EMERGENCY EXIT SIGN FAILED TEST. REMOVED AND REPLACED RT AFT EMERGENCY EXIT SIGN IAW B727 MM 335031.SDR SCNA01308Floorbeam · damagedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS AT F/B SCREW HOLES ON TOP OF FLOORBEAM AT STA 360 LBL 24 TO RBL 24. REMOVED CORROSION IAW B727 SRM 511006. TRIMMED DAMAGED AREA IAW B727 SRM 531008. FABRICATED REPAIR DOUBLER AND ANGLE FRSDR SCNA01313Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK FROM STA 440 TO 480 RBL 45. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK FROM BAC 1520792 7075 T6 PER SAMPLE. SDR SCNA01312Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT STA 344 TO 440 RBL 45. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK FROM BAC 1520792 7075 T6 PER SAMPLE. TREASDR SCNA01311Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE UNDERSIDE OF THE FLOORBEAM SUPPORT AT FS 1070 RBL 6. REMOVED CORROSION 511006. REMOVED FLOORBEAM SUPPORT IAW B727 SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 7075 T6 .063.SDR SCNA01309Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM SUPPORT AT FS 1070 RBL 10. REMOVED CORROSION IAW B727 SRM 511006. REMOVED FLOOR SUPPORT BEAM IAW B727 SRM 513002. FABRICATED NEW SUPPORT FROM BAC 15064417 7075 T6 .063 PESDR SCNA01307Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE UPPER FLOOR BEAM SUPPORT AT FS 1070 RBL 46. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 511001. FABRICATED DOUBLER ADN FILLER IAW B727 SRM 514002 FROM 202SDR SCNA01306Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOOR BEAM SUPPORT AT FS 1050 RBL 8. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGE AREA IAW B727 SRM 531001. FABRICATED DOUBLER FROM AND1071371011. TREATED AND PRIMED IAW B727SDR SCNA01305Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND TO BE OUT OF LIMITS ON SEAT TRACK AT ST 344 TO STA 460 RBL 24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK FROM BAC 1520792 7075 T6 PER SAMPLE.SDR SCNA01304Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE UNDERSIDE OF THE FLOOR SUPPORT BEAM AT FS 1166 RBL 5. REMOVED CORROSION IAW B727 SRM 511006. REMOVED FLOOR BEAM SUPPORT IAW B727 SRM 513002. FABRICATED NEW SUPPORT FROOM BAC 15064417 SDR SCNA01303Floorbeam · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOOR SUPPORT BEAM AT STA 1050 LBL 5. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED AREA IAW B727 SRM 531001. FABRICATED DOUBLER FROM 101371011 AND FILLER FROM 7075 T6 .06SDR SCNA01301Floor Support · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SUPPORT BEAM AT FS 166 RBL 5. REMOVED CORROSION IAW B727 SRM 511006. REMOVED FLOOR SUPPORT BEAM IAW B727 SRM 513002. FABRICATED NEW SUPPORT FORM BAC 15064417 7075 T6 .063. TREATSDR EISA20000230Smoke · detectedAT FL 330, PUFF OF SMOKE CAME OUT FROM CAPTAINS INSTRUMENT PANEL. SMOKE STOPPED ON INITIAL DESCENT. ALL REQUIRED CHECKLIST COMPLETED. MADE PRECAUTIONARY LANDING AT ELP. REMOVED CAPTAINS INST PANEL, PERFORMED A VISUAL INSP OF ELECTRICAL COMPONENTS AND WIRINSDR SCNA01310Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT FS 950F RBL 45. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 512002. ISDR SCNA01302Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK AT FS870 LBL45. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TREATED AND PRIMED IAWSDR SCNA01300Seat Track · corrodedDURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE SEAT TRACK LOCATED AT FS779 TO FS850 RBL24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 15201429. INSTSDR 20010125SG017Fuel Control · malfunctionedON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT IAW 73-21-1. OPERATIONAL CHECKED NR 3 ENGINE IAW 71-00-00. (M)SDR 20010124SG004Fuel Control · malfunctionedON TAKEOFF ROLL, ENGINE NR 3 DID NOT PRODUCE RATED TAKEOFF THRUST. CAPTAIN ABORTED TAKEOFF AT 80 KNOTS. A/C WEIGHT 180.8. REMOVED AND REPLACED FUEL CONTROL UNIT IAW 73-21-1. OPS CHECKED NR 3 ENGINE IAW 71-00-00. OPS NORMAL. (M)SDR 20010406SG008Beam · crackedDURING C-CHECK, FOUND 1 INCH CRACK IN RADIUS OF AFT CHORD OF BS 1183 VERTICAL BEAM RBL 36, 29 INCHES FROM CABIN FLOOR. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR IAW SB 727-53-192. (M)SDR 20010406SG005Control Cable · out of adjIN CRUISE FLIGHT, NOSE GEAR DOOR LIGHTS COMES ''ON'' AT 310 KNOTS COMES BACK ''OFF'' AT 293 KNOTS. INSPECTED NOSE GEAR WW DOORS AND FOUND CABLES TO BE OUT OF TOLERANCE. ADJUSTED CABLES IAW 32-22-1. OPERATION CHECK GOOD. PERFORMED RETRACTION, SYSTEM OPS CHESDR EISA20000231Light · inoperativeL-1 ENTRY DOOR EMERGENCY LIGHT INOP IN EMERGENCY MODE. REMOVED AND REPLACED LIGHT ASSEMBLY.SDR EISA20000229Regulator · failedUNABLE TO MAINTAIN CABIN ALTITUDE BELOW 10,000 FT AUTO OR MANUAL AIR TURNBACK TO AUS. REPLACED LEFT PRESSURE REGULATOR PER MM 36-12-51.SDR 20010406SG003Seat Track · corrodedDURING C-CHECK, FOUND LEFT OUTBOARD SEAT TRACK UPPER SURFACE OUTBOARD FLANGE CORRODED BS 1020. REMOVED AND REPLACED TRACK SECTION LEFT OUTBOARD TRACK BS 990 TO 1070 LBL 45 IAW SRM 53-10-5 FIG 7. (M)SDR DHL2000743001Indicator · unserviceableNR 2 EGT READ BELOW 0 ON PUSH BACK JUST BEFORE START. NO START ATTEMPTED. RETURNED TO THE BLOCKS. R & R NR 2 EGT INDICATER, CHKS OK PER M/M 77-21-51.SDR 20010406SG002Seat Track · corrodedDURING C-CHECK, FOUND CABIN SEAT TRACK CORRODED BS 344 TO 360 RBL 45. REMOVED AND REPLACED SEAT TRACK SECTION FROM BS 344 TO BS 480 IAW SRM 53-10-5 FIG 7. (M)SDR EISA20000220Unknown · odorELECTRICAL ODOR IN COCKPIT DURING DESCENT. CORRECTIVE ACTION: INSPECTED E&E BAY, FORWARD E&E BAY, LEFT AND RIGHT PACK SYSTEM AND COCKPIT, NO DEFECTS NOTED. COULD NOT DUPLICATE AT THIS TIME.SDR EISA20000218Lockpin · installedON TAKE OFF NOSE GEAR DOES NOT RETRACT AIR TURN BACK TO (SEA). CORRECTIVE ACTION: REMOVED NOSE GEAR SAFTEY LOCK PIN.SDR SCNA00131Battery · dischargedDURING A MAINTENANCE LINE INSPECTION THE EMERGENCY EXIT SIGN ABOVE L2 WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE BATTERIES FOR THE L2 DOOR EMERGENCY EXIT SIGN LIGHTING, OPERATIONAL CHECKS GOOD.SDR EISA20000210Outflow Valve · inoperativeON DEPARTURE CABIN PRESSURIZED TO APRROX 5000' TO 6000' BELOW SEA LEVEL, AND SHORTLY AFTER STABILIZING, DURING CLIMB CABIN WAS CLIMBING AND DESCENDING GREATER THAN 2000FPM, PRESSURIZATION ERRATIC. CORRECTIVE ACTION: REMOVED AND REPLACED RIGHT OUTFLOW VALVE PSDR 00FDEA00820Adi · faulty00-332 DURING T/O 1ST OFFICER ADI HAD RED GYRO FLAG APPEAR. ADI WENT TO 2 DEG NOSE DOWN WHEN AC WAS AT 15 DEG. CIRCUIT BREAKERS ALL IN. R&R NR 2 ADI PER MM 34-62-011. OPS CK GOOD.SDR GAIA00720Flap · malfunctionedFLT 1804 - LAX - AT FL 270, THE AMBER LEADING EDGE FLAP LIGHT ILLUMINATED, WITH CORRESPONDING NR 5 KRUEGER INDICATOR ON THE LEADING EDGE ANNUNCIATOR PANEL. THE LIGHT STAYS ON CONTINUOUSLY. AIRCRAFT MADE AN UNEVENTFUL RETURN TO LAX. REMOVED AND CLEANED CONNESDR CA001201009Bearing · binding(CAN) FLIGHT CREW REPORTED THAT THE AILERON SYSTEM HAD BECOME PROGRESSIVELY STIFFER DURING THEIR FLIGHT. MAINTENANCE INSPECTED THE AIRCRAFT, CLEANED AND LUBRICATED PULLEYS AND BEARINGS IAW THE MM THE AIRCRAFT WAS RELEASE FOR A FERRY FLT. MAINTENANCE FOUND BESDR GAIA00719Flap · malfunctionedFLT 1804 - LAX - OUT OF 24,000 FT THE LEADING EDGE AMBER LIGHT ILLUMINATED, CORRESPONDING WITH THE NR 5 KRUEGER LIGHT ILLUMINATED ON THE LEADING EDGE ANNUNCIATOR PANEL. AIRCRAFT MADE AN UNEVENTFUL RETURN TO LAX. CYCLED FLAPS AND LEADING FLAPS TWO TIMES. CANSDR 20010119SG003Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-71, OPS CHECK GOOD. (M)SDR 20010112SG035Accumulator · rupturedUPON LANDING AT PHL LOST HYD BRAKE PRESSURE FROM SYSTEM A/B. UTILIZED PNEUMATIC SYSTEM TO STOP AIRCRAFT. ON INSPECTION FOUND RUPTURED HYD BRAKE ACCUMULATOR IN RIGHT WHEEL WELL WITH SUBSEQUENT STRUCTURAL DAMAGE TO RT MAIN GEAR DOOR, HYD LINES ABOVE ACUMULATORSDR 20010112SG018Battery Pack · dischargedDURING PREFLIGHT TRANSIT, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-71. OPS CHECK GOOD. (M)SDR 00FDEA00754Web · corrodedCORROSION (C53-224-04) BS 1148, LBL 1.5 TO LBL 5, WL 208 AT NUT PLATE HOLE IN SHEAR WEB PREVIOUS BLEND. *S/D* REMOVED AND REPLACED PER EA 7-5310-52471 AND FEDEX SRM 51-40-2.SDR 00FDEA00751Stringer · corrodedCORROSION (C53-113-01,1) ON STRINGER 26 RT AT BS 720F+16 INCHES. *S/D* REMOVED AND REPLACED PER FEDEX SRM 53-10-3 USING MATERIAL BAC 1498-147, LOT 381472, BAC 1498-131 LOT 269814.SDR EISA20000198Relief Valve · inoperativeCLIMBING OUT OF 1000 FT HYDRAULIC A SYSTEM PRESSURE FAILED, RAN APPROPRIATE CHECKLIST AND RETURNED TO (TUS). REPLACED A SYSTEM PRESSURE RELIEF VALVE. LEAK AND OP CHECK GOOD IAW M/M 29-11-64.SDR SCNA00116Light · damagedDURING A MAINTENANCE LINE CHECK, THE EMERGENCY TRACK LIGHTING WAS FOUND TO BE PULLED ON ONE END. REPLACED MISSING AND DAMAGED SECTIONS OF EMERGENCY TRACK LIGHTING, OPERATIONAL CHECKS GOOD.
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