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 04FDEA02922Skin · corrodedCORROSION ON INNER SKIN BS 720C LBL 5 WL 136. BLENDED CORROSION ON INNER SKIN AT BS 720C BL 0 AND ON SHEARTIE BS 720C RBL 5 - LBL5 W/L 136. BOTH AREAS FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 FIG 1 AND 53-30-1 FIG 1. FABRICATED REPLACEMENT SHEARTIE BAC1490SDR C8GA20040023Pitot Head · bird strikeFLT 717 FORM KELP TO KSTL, ABORTED TAKEOFF DUE TO NO AIRSPEED INDICATION ON THE CAPTAIN AIRSPEED INDICATOR. AIRCRAFT RETURNED TO BLOCKS AND UPON INSPECTION FOUND A BIRD STRIKE ON THE CAPTAIN PITOT PROBE. REMOVED FEATHERS AND PERFORMED A BIRD STRIKE INSPECTIOSDR DHL2004742007Controller · malfunctionedON GROUND STALL WARNING, STICK SHACKER AND AUTOPILOT DISCONNECT WARNING CAME ON AND COULD SMELL ELECTRICAL SMOKE IN COCKPIT. ADJUSTED AOA IAW 34-18-01, INSPECTED WIRING IN EE BAY NO SIGN OF SMOKE DETECTED SUSPECTED SMOKE FROM APU, INSPECTED APU IAW 21-20-01. SDR PCS2004F00001Stabilizer · out of adjustCREW REPORTED, THROUGH FL 270 AIRCRAFT STARTED PORPOISING, TURNED AUTOPILOT OFF, PORPOISE CONTINUED SLOWED TO .76 MACH, THEN DISAPPEARED. AIRCRAFT DIVERTED BACK AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED HORIZONTAL STABILIZER ADJUSTMENT/TESDR C7WA200400051Stringer · corrodedSTR 27 RT CORRODED STA 620. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED STRINGER REPAIR IAW SRM 53-10-4 FIG 1, DETAIL 2.SDR C7WA200400046Support Angle · corrodedSUPPORT ANGLE CORRODED AT STA 1030 TO 1050 BETWEEN STR 29 AND 30 RT. REPAIR ANGLE FABRICATED IAW SAMPLE IAW SRM 51-20-1 AND 51-40-3. MATERIAL USED 7075-T6 X .050 INCH.SDR C7WA200400043Skin · corrodedFUSELAGE LOWER SKIN AT STA 990 STR 28 RT. CORRODED AND TWO RIVETS MISSING. INSTALLED EXTERNAL SKIN REPAIR IAW SRM. 53-30-3 FIG 3. DOUBLER MATERIAL USED, 2024-T3 X .125 INCH X 17 INCHES X 11 INCHES.SDR C7WA200400042Door Frame · corrodedELECTRONIC COMPARTMENT DOOR CUTOUT AFT FRAME CORRODED STA 450 BETWEEN STRINGER 27 RT AND 27 LT. REMOVED AND REPLACED FRAME SECTION. FABRICATED NEW FRAME SECTION IAW SAMPLE. MATER USED 7075-0, .050, HEAT TREATMENT TO 7075-T6 IAW BAC 5602.SDR C7WA200400044Stringer · corrodedSTRINGER 28 RT CORRODED AT STA 990. REPLACED DAMAGED KEELBEAM SECTION IAW EO NR 1M-727-53-0236 AND DRAWING 65-56441-8.SDR C7WA200400045Skin · corrodedFUSELAGE LOWER SKIN AT STA 720B, STR 28 RT CORRODED. INSTALLED EXTERNAL SKIN REPAIR IAW SRM 53-30-3, FIG 1 DOUBLER MATERIAL USED, 2024-T3 X.160 INCH X 27 INCHES X 28.5 INCHES.SDR C7WA200400050Stringer · corrodedSTRINGER 29 RT CORRODED AT STA 950A. REMOVED CORROSION IAW SRM 51-10-6 AND INSTALLED REPAIR ON RT FLANGE IAW SB 727-0170.SDR C7WA20040922Shear Tie · corrodedSHEAR TIE CORRODED AT STA 950A BETWEEN STR 28 AND STR 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11 MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR C7WA200400048Shear Tie · corrodedSHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 LT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11, MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR C7WA200400047Shear Tie · corrodedSHEAR TIE CORRODED AT STA 970 BETWEEN STR 28 AND 29 RT. REPAIRED SHEAR TIE IAW SRM 53-10-4 FIG 11. MATERIAL USED 7075-T6 X .050 INCH X 6 INCHES X 11 INCHES.SDR 04FDEA02770Angle · crackedRT MLG WHEEL WELL VERTICAL L-ANGLE CRACKED BS 870 RBL 6 FWD OF APU LWR CORNER . REMOVED AND REPLACED RT WHEEL WELL VERTICAL L-ANGLE BS 870 RBL 6 IAW SRM 51-30-5, 51-30-2, AND 51-10-2.SDR C1HA2004006Accessory Unit · malfunctionedON GEAR RETRACTION LEFT MAIN GEAR RED LIGHT REMAINED ILLUMINATED. COM PROCEDURES FOLLOWED. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT IAW M/M 32-09-121, OPS CHECK IAW M/M 32-09-121 PG 501. OK FOR SERVICE.SDR C8GA20040020Engine · defectiveFLT 1721 FROM FLL TO TOL, AT FL140, AT CLIMB POWER THE NR 1 ENG LOW OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED. FOLLOWED AOM PROCEDURES A2-10 AND THE NR 1 ENG IN-FLIGHT SHUTDOWN AS A PRECAUTIONARY AND AIR TURN BACK TO FLL. A/C WAS INSPECTED AND THE LOW OIL PSDR C1HA200479005Uplock Sensor · malfunctionedAFTER DEPARTURE THE LEFT MAIN LANDING GEAR UNSAFE LIGHT (RED) REMAINED ILLUMINATED. COMPLIED WITH COM PROCEDURES AND LIGHT REMAINED ON DURING FLIGHT. REMOVED AND REPLACED LT UPLOCK SENSOR IAW MM 32-61-81. OPS CHECK GOOD.SDR C7WA200400038Transducer · inoperativeAIR RETURN: DURING CLIMBOUT UPPER RUDDER DEFLECTED TO FULL RT YAW DAMPER POSITION THEN BEGAN OSCILLATING LT TO RT CONTINUOUSLY. REMOVED AND REPLACED UPPER YAW DAMPER TRANSDUCER. SYSTEM OPERATIONAL CHECKS NORMAL.SDR C1HA200479004Warning Light · illuminatedUPON LANDING, GEAR EXTENSION, NOSE LEFT & RIGHT MAIN LANDING GEAR RED UNSAFE LIGHTS ILLUMINATED WITH ALL GREEN DOWN AND LOCKED LIGHT. PERFORMED COM PROCEDURES. ALL INDICATIONS NORMAL. PERFORMED GEAR INDICATION FUNCTIONAL TEST IAW MM 31-09-121. COULD NOT DUSDR DHL2004748006Light · inoperativeDURING PRE-DEPARTURE CHECK FOUND L1 DOOR EMERGENCY EXIT LIGHT INOPERATIVE.REMOVED AND REPLACED L1 DOOR EMERGENCY LIGHT ASSY IAW MM 33-50-71/SYST, OPS CHECKED GOOD.SDR DHL2004743006Seal · failedLOWER AFT BODY OVERHEAT LIGHT ILLUM INFLIGHT. ABNORMAL PROCEDURE COMPLETED, DECLARED AN EMERGENCY AND DIVERTED TO MEM. REMOVED AND REPLACED SEALS P/N 24366-100 ON PURGE VALVE AIR SUPPLY TUBE AFT OF PRECOOLER VALVE ON RIGHT SIDE. RESECURED SLIPPED PNSDR DHL2004742006Light · inoperativeCOCKPIT EMERGENCY EXIT LIGHT WILL NOT COME ON WHEN SWITCH TURNED ON. RESEATED COCKPIT EMERGENCY EXIT LIGHT ASSY, OPS CHECKS NORMAL IAW B727 M/M 33-50-01.SDR C1HA200478004Slide · tornL-2 DOOR SLIDE INADVERTANTLY DEPLOYED DUE TO DOOR BEING ARMED. SLIDE INFLATED CORRECTLY AN THEN DEFLATED DUE TO A TEAR IN THE SLIDE. REMOVED AND REPLACED L-2 EVAC SLIDE IAW MM 25.60.15.SDR C8GA20040017O-Ring · leakingIN CRUISE, NR 1 ENGINE LOST 2 QTS OF OIL EVERY 10 MINUTES. THE NR 1 ENGINE WAS SHUTDOWN AS A PRECAUTION. AN EMERGENCY WAS DECLARED, THE AIRCRAFT DIVERTED TO AND LANDED WITHOUT INCIDENT. FOUND INLET PRESSURE LINE LEAKING. TIGHTENED LINE, OPS AND LEAK CHECK SDR DHL2004748005Bulb · inoperativeEMERGENCY EXIT LIGHTS UNARMED LIGHT FLICKERS. RELAMPED UNARMED LIGHT. EMERGENCY EXIT LIGHT SYS OP'S NORMAL IAW B-MM 33-50-01. INSTALLED 1EA BULB P/N CM313.SDR C1HA200476005Floorbeam · corrodedCORROSION ON FLOORBEAM STA 1010 LBL 0 - 15 LBL. CLEANED, TREATED & INSTALLED REPAIR DOUBLER.SDR DHL2004742005Warning Light · illuminatedGEAR UNSAFE LIGHT INDICATION.SDR CA040720003Compressor · odorDURING TAKEOFF, THE CREW REPORTED A RUSH OF HOT AIR IN THE COCKPIT AND A BURNING ODOR. THE CREW DECIDED TO RETURN TO BASE. AIRCRAFT LANDED WITHOUT INCIDENT. MX APPLIED MEL 36-06 WITH THE NR 1 BLEED CLOSED AND THE LT NR 2 ENGINE/APU BLEED OPENED AFTER TAKEOFSDR C8GA20040012O-Ring · leakingDURING CRUISE, THE NR 1 ENGINE LOSS OIL QUANTITY FOLLOWED BY LOSS OF OIL PRESSURE. REFERENCE AOM CHECKLIST FOLLOWED BY NR 1 ENGINE IN-FLIGHT SHUTDOWN, ADVISED ATC AND DECLARED AN EMERGENCY AND LANDED AT OUR FINAL DESTINATION IN KTOL WITHOUT INCIDENT. AIRCRAFSDR CA040713011Switch · failed(CAN) AFTER TAKEOFF WHEN THE GEAR WAS RETRACTED, THE LEFT MAIN GEAR DOOR LIGHT ON THE ENGINEERS PANEL AND THE DOOR UNSAFE LIGHT REMAINED ILLUMINATED. THE CREW CYCLED THE GEAR AND THE LIGHT REMAINED ON, THE CREW ELECTED TO RETURN TO THE POINT OF ORIGIN. THE SWSDR C1HA200479003Panel · delaminatedRIGHT WING APU EXHAUST PANEL DELAMINATED AND CORRODED AT EXHAUST CUTOUT.SDR C1HA200479001Bulkhead · crackedLEFT MAIN GEAR WHEEL WELL AFT PRESSURE BULKHEAD UPPER CHORD IS CRACKED AT O/B CORNER, STA 950 BL 60L.SDR C1HA200479002Intercostal · corrodedINTERCOSTAL BETWEEN STA 1148-1166 AND STR 28L TO 27L IS CORRODED.SDR DHL2004742004Element · out of adjustNR 3 FIRE PROTECTION SYSTEM GROUND DETECTOR CIRCUIT ANNUNCIATOR PULSES FAINTLY. ADJUSTED NR 3 FIRE PROTECTION SENSING ELEMENTS PER MM 26-11-01, OP'S CHECK NORMAL.SDR DHL2004742008Brake · lockedLT BRAKE REMAINS LOCKED AFTER PARKING BRAKE RELEASED. REF. ITEM 4M L/P 003102. NR 2 BRAKE CHANGED. ALSO REPLACED NR 1 BRAKE IAW B-727 M/M 32-41-32. OPS AND LEAK CHECKS SERVICEABLE. TAXI CHECK IAW JRH 9.1. OPS SERVICEABLE.SDR DHL2004755014Actuator · malfunctionedNR 6 SLAT FAILED TO RETRACT AFTER TAKEOFF. ABNORMAL PROCEDURES COMPLIED WITH, WOULD NOT RETRACT. UPON CHECK AT ARRIVAL FOUND NR 7 SLAT AMBER LIGHT WOULD NOT EXTINGUISH. REMOVED AND REPLACED NR 7 SLAT ACTUATOR IAW MM 27-81-32. CHECKED OPERATION OF NR 6 CLEANSDR CA040624008Engine · malfunctioned(CAN) DURING TAKE-OFF, THE CREW REPORT THAT THEY HAD HEARD A BANG. ALL ENGINE PARAMETERS WERE NORMAL. THE AIRCRAFT MADE AN UNSCHEDULED LANDING. ALL ENGINES WERE PHYSICALLY INSPECTED WITH NO APPARENT DAMAGE. ALL 3 ENGINES WERE STARTED, POWERED UP AND REVERSDR C8GA20040008Pitot Line · obstructedDURING TAKE-OFF ROLL, THE FIRST OFFICER’S AIRSPEED INDICATOR READ 80 KNOTS AND THE CAPTAIN’S INDICATOR INDICATED ZERO KNOTS. ABORTED TAKE-OFF, CONTACTED ATC TO ADVISE THEM OF AN AIRSPEED INDICATION PROBLEM AND RETURNED TO RAMP WITH NO FURTHER INCIDENT. INSPECTSDR C1HA200478003Skin · corrodedCENTER WING LOWER SKIN IS CORRODED ON RT SIDE AT STA 535. REPAIRED IAW EO-727-57-10-01.SDR DHL2004748003Fire Loop · out of positionNR 1 FIRE DETECTOR CIRCUIT GROUND LIGHT ON C/B PANEL ILLUMINATED IN FLIGHT. DOES NOT ILLUMINATE ON GROUND. DEFERRED NR 1 FIRE WARNING GROUND FAULT DETECTOR SYS. PER MEL 26-9-1 DMI 16886 PLACARD INSTALLED. REPOSITIONED NR 1 ENG FIRE LOOP PER DHL B727 MM 26-SDR CA040611005Switch · inoperative(CAN) AFTER TAKE OFF AND DURING CLIMB IT WAS OBSERVED THAT THE LT OB KRUGER FLAP WAS NOT RETRACTED. BOTH INDICATIONS SHOWED THE KRUGER WAS STILL EXTENDED. THE AIRCRAFT MADE AN UNSCHEDULED LANDING WITHOUT INCIDENT. JUMPER ASSY WAS INSTALLED IAW B727-27-80-02SDR MYW2004F00006Generator · fluctuatesDURING TAKE OFF ROLL, GENERATOR DROPPED OFF LINE FOLLOWED BY NR 3 GEN LIGHT. REJECTED TAKE OFF AT 75 KNOTS. ACCOMPLISHED AOM PROCEDURE GENERATOR CHECKLIST ZA9-1 AND REJECTED TAKEOFF. RETURNED TO GATE WITHOUT INCIDENT. FOUND NR 3 GENERATOR FREQUENCY FLUCTUASDR C1HA200474004Retainer · looseNR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT 26.0. FOLLOWED COM PROCEDURE, LIGHT WENT OUT. PERFORMED DUCT INSPECTION AND LOOP INSPECTION DID 2 HIGH POWER ENGINE RUNS. OVERHEAT NOT DUPLICATED HOWEVER AIR LEAK WAS FOUND IN 8TH STAGE DUCT. NR 3 ENG 8TH STASDR C1HA200474003Compressor · stalledCOMPRESSOR STALLS NR 2 ENGINE 350 LEVEL OFF, PWR REDUCTION, NR 2 EPR DROPPED. THRUST LEVER TO IDLE INDICATIONS NORMAL. LEFT IN IDLE FOR REMAINDER OF FLIGHT. PERFORMED CENTER ENGINE COMPRESSOR STALL CHECK, GROUND CHECK FOR BLEED OPERATION AND ACEL/DECEL CHECSDR CA040531001Actuator · damagedDURING A SCHEDULED ROUTINE MAINTENANCE CHECK IT WAS OBSERVED THAT THE LEFT HAND OUTBOARD SLAT ACTUATOR WAS DAMAGED. THE CORNER OF THE SLAT WAS GROUNDED OFF EXPOSING A SECONDARY STRUCTURAL EXTRUSION. THE AIRCRAFT WAS GROUNDED A SUSPECTED A WING TIP STRIKE ON LSDR DHL2004743004Rib · crackedLT WING NR 2 LEADING EDGE SLAT RIBS AT ROD END HAS 2 SMALL CRACKS. ONE ON EACH SIDE OF ROD END. REPAIRED BRACKETS IAW B-727 SRM 51-40-3, MATERIAL USED 2024T3, .051, RIVETS USED: CR3223-5-2, 10 EA, NAS 517-3-5 SCREWS, 2 EA. PO NR 400004986. .SDR 2004F00186Connector · damagedDURING CLIMB-OUT, THE NR 8 LEADING EDGE SLAT LIGHT ON THE FORWARD PANEL STAYED ILLUMINATED WHEN THE SLATS WERE RETRACTED. AIRCRAFT RETURNED TO SEATTLE AND LANDED WITHOUT INCIDENT. REPAIRED RECESSED PIN IN CONNECTOR AT NR 8 LEADING EDGE SLAT. (M)SDR DHL2004755013Module · malfunctionedAPU FIRE LIGHT AND BELL CAME ON. FIRE HANDLE PULLED LIGHT OUT AND BELL SILENCED. TRANSFERRED TO DMI NR 16580 IAW MEL 49-1 CAT. (C) PLACARD INSTALLED FIRE HANDLE PULLED. APU FIRE LIGHT AND BELL CAME ON FIRE HANDLE PULLED. LIGHT OUT AND BELL SILENCED. REMOSDR DHL2004755012Fire Loop · looseAPU FIRE BELL DURING T/O. TRANSFERRED TO DMI LOG 16554 CAT-C REF MEL 49-1. PLACARD INSTALLED. RTO 40 KIAS 11 DEG C, 155,900 LBS 1000FT PA NORMAL ZONE DUE TO APU FIRE WARNING. PER BRAKING CHART NO FURTHER INSPECTION REQUIRED. DURING ROLL OUT. APU FIRE BEL
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