Boeing 727-221
Service difficulty reports · 149
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 = '727221' 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 = '727221' 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 EISA98040Fire Loop · inoperativeNR 2 FIRE WARNING WILL NOT TEST. REPLACED CONNECTOR AND FIRE LOOP. (M)SDR EISA98013Aural Warning · malfunctionedFIRE BELL SOUNDED EN ROUTE FROM HDN TO DFW. REMOVED AND REPLACED AURAL WARNING UNIT. TT: 31,095:9 HOURS. TC: 16,292. (X)SDR EISA98012Fire Bell · soundedFIRE BELL SOUNDED IN-FLIGHT WITH BOTH PILOT AND COPILOT MASTER FIRE WARNING LIGHTS ILLUMINATED. NO AREA OR POSITION LIGHT ILLUMINATED. INSPECTED ENGINE FOR LEAKS. ALSO, INSPECTED FIRE LOOPS FOR WEAR AND DAMAGE AND DEFECTS. NONE NOTED. OPS CHECK GOOD. (X)SDR EISA98006Fire Bell · soundedDURING CLIMB-OUT, FIRE BELL SOUNDED AND NO LIGHT. RERACKED FIRE DETECTOR UNIT. OPS CHECK GOOD IAW MM 26-00-00. (M)SDR EISA98001Engine · failedNR 2 ENGINE FAILED ON GO AROUND. REMOVED AND REPLACED NR 2 ENGINE. (M)SDR EISA97286Wire · brokenNR 2 OIL TEMP ABOVE RED LINE ON TAKEOFF ENGINE SHUTDOWN. REPAIRED BROKEN WIRE AT TEMP BULB ON NR 2 ENGINE, OPS CHECK NORMAL. (M)SDR EISA97225Mix Valve · stuckON CLIMB-OUT, LEFT AIR MIXING VALVE STUCK TOWARD HOT RESULTING IN DUCT TRIP AND PACK TRIP, CABIN ALTITUDE WOULD NOT HOLD AT 25,000 CABIN ALTITUDE AT 11,000, ON RETURN TO MSP WAS 9,000. REMOVED AND REPLACED LEFT MIXING VALVE, OPS CHECK GOOD IN MANUAL MODE IAW SDR EISA97175Seal · tornPRESSURE LEAK IN FORWARD ENTRY DOOR. CLEANED ENTIRE SEAL SURFACE AND REPAIRED DOOR SEAL. TT: 30,451.24 HOURS. TC: 15,923. (X)SDR EISA97140Fire Detector · dirtyNR 1 FIRE DETECTOR LOOP LIGHT ILLUMINATED. CLEANED AND RESECURED CONNECTION ON FIRE LOOP, OPS CHECK NORMAL. (M)SDR EISA97106Switch · inopL/E FLAP NR 5 FAILED TO RETRACT AFTER TAKEOFF. REPLACED L/E NR 5 FLAP SWITCH PER MM 27-80. (M)SDR EISA97137Connector · burnedDURING ROUTINE C-CHECK, FOUND PITOT TUBE ON VERTICAL STABILIZER WITH BURNED ELECTRICAL CONNECTOR, INSIDE PANEL NR 9504. REMOVED AND REPLACED CONNECTOR PER STANDARD WIRING PRACTICES. (M)SDR EISA97136Carriage · corrodedDURING ROUTINE C-CHECK, FOUND RT OUTBOARD FLAP, INBOARD TRACK CARRIAGE, AFT SPINDLE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED CARRIAGE AND REPLACED WITH SERVICEABLE UNIT PER MM 27-51-13. (M)SDR EISA97134Skin · crackedDURING ROUTINE C-CHECK, FOUND SKIN CRACKED AT TOP, FORWARD, OUTBOARD CORNER OF RIGHT ELEVATOR. REMOVED AND SENT TO OUTSIDE REPAIR FACILITY FOR REPAIR, UNIT REINSTALLED WITH FORM 8130-3. (M)SDR EISA97133Tab · delaminatedDURING ROUTINE C-CHECK, FOUND LEFT ELEVATOR TAB DELAMINATED IN TWO AREAS. REPAIRED TAB PER SRM 51-40-8, REPAINTED AND BALANCE CHECKED. (M)SDR EISA97132Tab · delaminatedDURING ROUTINE C-CHECK, FOUND RIGHT ELEVATOR TAB DELAMINATED IN TWO AREAS. REPAIRED TAB PER SRM 51-40-8, REPAIRED AND BALANCE CHECK. (M)SDR EISA97120Carriage · corrodedDURING C-CHECK, FOUND LEFT OUTBOARD FLAP, INBOARD CARRIAGE AFT SPINDLE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED CARRIAGE AND REPLACED WITH SERVICEABLE UNIT PER MM 27-51-3. (M)SDR EISA97127Bracket · crackedDURING ROUTINE C-CHECK INSPECTION, FOUND FORWARD CARGO COMPARTMENT DOOR BRACKET CRACKED AT TOP AFT DOOR STRUCTURE. FABRICATED AND INSTALLED NEW BRACKET IAW SRM 52-00-01. (M)SDR EISA97099Receiver · inopON DEPART NR 1 VHF NAV INOP, RETURNED TO DFW. REPLACED NR 1 NAV RECEIVER. (M)SDR EISA97128Stiffener · crackedDURING ROUTINE C-CHECK, FOUND 3RD STIFFENER AFT OF LEFT WING LEADING EDGE AT WS 92.8 CRACKED AT UPPER END. STOP DRILLED CRACK FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)SDR EISA97126Bulkhead Angle · crackedDURING ROUTINE C-CHECK INSPECTION OF AFT PIT, AFT BULKHEAD UPPER RT SIDE, FOUND 7 INCH CRACK ON VERTICAL ANGLE FS 1183. REMOVED CRACKED ANGLE, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 53-10-2. (M)SDR EISA97135Web · crackedDURING ROUTINE C-CHECK, FOUND TORN WEB AT UPPER END OF VERTICAL STABILIZER LEADING EDGE. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-30-02. (M)SDR EISA97131Elevator · crackedDURING ROUTINE C-CHECK, X-RAY INSPECTION REVEALED A 2 INCH CRACK IN RIGHT ELEVATOR. REMOVED ELEVATOR AND REPLACED WITH A SERVICEABLE UNIT PER MM 27-30-01. (M)SDR EISA97130Stiffener · crackedDURING ROUTINE C-CHECK, X-RAY INSPECTION REVEALED MISSING MATERIAL AND 6.5 INCH CRACK AS SHOWN IN SHOT NR 1 ON RT ELEVATOR. REMOVED DAMAGED STIFFENER AND REPLACED WITH NEW STIFFENER PER SRM 51-10-1. (M)SDR EISA97129Stiffener · crackedDURING ROUTINE C-CHECK, FOUND 3RD STIFFENER AFT OF RIGHT WING LEADING EDGE AT WS 92.8 CRACKED AT UPPER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER PER SRM 51-40-3. (M)SDR EISA97125Duct · crackedDURING ROUTINE C-CHECK, FOUND NR 1 ENGINE 8TH STAGE BLEED DUCT CRACKED. REMOVED DUCT AND REPLACED SERVICEABLE UNIT. (M)SDR EISA97124Angle · crackedDURING ROUTINE C-CHECK, FOUND REINFORCING ANGLE WITH 1 INCH CRACK AT FS 804.5, ADJACENT TO STRINGER 14R. STOP DRILLED CRACK, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-03. (M)SDR EISA97123Support · corrodedDURING ROUTINE C-CHECK, FOUND RIGHT AFT LAV FLOOR SUPPORT CRACKED AND CORRODED. REMOVED CORROSION, FABRICATED AND INSTALLED REPAIR PER SRM 51-10-06 ADN 51-40-03. (M)SDR EISA97122Slat · dentedDURING ROUTINE C-CHECK, FOUND NR 8 SLAT DENTED FROM SLAT STATION 391-401. REMOVED SLAT AND INSTALLED SERVICEABLE UNIT PER MM 27-81-11. (M)SDR EISA97121Stiffener · crackedDURING ROUTINE C-CHECK, FOUND 4TH STIFFENER AFT OF LEADING EDGE OF LEFT WINGS AT WS 92.8, CRACKED AT LOWER END. STOP DRILLED CRACK, FABRICATED AND INSTALLED DOUBLER REPAIR PER SRM 51-40-3. (M)SDR EISA97083O-Ring · damagedNR 3 ENGINE HAD OIL LOSS ON FINAL. INDICATIONS AT SHUT DOWN, QTY 0, PRESSURE IN YELLOW BAND AND YELLOW OIL LIGHT ILLUMINATED. REPLACED DAMAGED O-RING ON OIL RETURN LINE ABOVE OIL SCREEN. LEAK CHECKED OK PER CHAPTER 71. (M)SDR EISA97077Light · malfunctionedEMERGENCY EXIT LIGHT ABOVE R1 DOOR IS FLICKERING ON AND OFF. RE-INSTALLED EMERGENCY EXIT LIGHT ABOVE R1 DOOR. SYSTEM OPS CHECK GOOD. (M)SDR EISA97041Bulb · failedAFT OVERWING EMERGENCY EXIT LIGHT ON LEFT SIDE. ONE BULB INOP. REPOSITION LIGHT BULB. (M)SDR EISA97040Light · inoperativeEMERGENCY EXIT LIGHTS AT R1 EXIT DO NOT ILLUMINATE. REPLACED EMERGENCY LIGHTS. (M)SDR EISA97039Light · inoperativeEMERGENCY EXIT LIGHTS AT L-1 EXIT DO NOT ILLUMINATE. REPLACED EMERGENCY LIGHTS. (M)SDR EISA97038Lamp · failedEMERGENCY EXIT SIGN FOR OVERWING EXITS LEFT SIDE WILL NOT ILLUMINATE. RELAMPED EMERGENCY EXIT SIGN, OPS CHECK GOOD. (M)SDR EISA97037Light · looseFOUND EMERGENCY EXIT LIGHTS AT L1 AND R1 DOORS DO NOT ILLUMINATE. RESEATED LIGHTS INTO CHARGING BASE, AFTER SUFFICIENT CHARGING TIME LIGHTS, OPS CHECKED NORMAL. (M)SDR EISA97036Seal · looseFLT ATTENDANT REPORTED, THAT THE L2 GALLEY DOOR HAD A HOLE AND AIR LEAK. R/E CONFIRMED, RETURN TO DFW (ATB). FOUND L2, DOOR FORWARD LOWER SEAL LOOSE, REINSTALLED SEAL TRACK PER MM 52-00-1. (M)SDR EISA97032Battery Pack · dischargedAFT SLIDE EMEGENCY LIGHTS INOP. REPLACED EMERGENCY LIGHT BATTERY PACK. (M)SDR EISA97004Oil Press Switch · inoperativeNR 2 ENGINE OIL FILTER BYPASS/LOW PRESS LIGHT ILLUMINATED DURING FLIGHT. REMOVED AND REPLACED NR 2 LOW PRESS SWITCH. (M)SDR EISA96285Adi · inopF/O'S ADI GYRO FLAG IN VIEW IN BOTH NORMAL AND ALTERNATE. REMOVED AND REPLACED F/O'S ADI. OPS CHECK GOOD IAW MM 34-23-11. (M)SDR EISA96286Relief Valve · out of adjustDURING TAKEOFF, NR 2 OIL PRESSURE ROSE ABOVE RED LINE (APPROX 80 PSPSI). TROUBLESHOT ENGINE OIL PRESSURE RELIEF VALVE AND ADJUSTED PER MM, LEAK AND OPS CHECK GOOD. (M)SDR EISA96282Outflow Vlv · inoperativeCABIN PRESSURE CONTROL SYSTEM MALFUNCTIONED IN CLIMB. FAILED IN STANDBY MODE TO FULL CABIN DESCENT, SWITCHED TO MANUAL DC FAILED OPS PER AOM VOL 1. REMOVED AND REPLACED OUTFLOW VALVE PER MM. OPS CHECK GOOD PER GROUND OPS PROCEDURE. (M)SDR EISA96196Fitting · looseENGINE NR 3 OIL QTY BEGAN RAPIDLY DROPPING ON APPROACH AND OIL TEMPERATURE ENTERED YELLOW BAND. ENGINE SHUTDOWN ACCOMPLISHED APPROXIMATELY 1/4 GALLON REMAINING UPON LANDING. OIL SYSTEM INSPECTED, BANJO FITTING ON SYSTEM RETURN FOUND LOOSE. THREAD PITCH CHECSDR EISA96102Filter · cloggedENGINE NR 2 OIL PRESSURE FILTER BYPASS LIGHT ILLUMINATED IN FLIGHT. REDUCED POWER LIGHT REMAINED ILLUMINATED WITH POWER AT IDLE. ENGINE SHUT DOWN AND RETURNED TO EWR. REPLACED NR 2 MAIN OIL SCREEN, RUN-UP AND LEAK CHECK OK. OIL PRESSURE LIGHT OPS CHECK NORSDR EISA96100Crossfeed · inoperativeNR 3 ENGINE FUEL CROSSFEED VALVE INTRANSIT LIGHT REMAINED ILLUMINATED AFTER CROSSFEED OPERATIONS DIVERTED TO 'ICT'. DEFERRED PER MEL 24-2 PLACARD NR 966. (M)SDR EISA96099Turbine · failedON TAKEOFF ROLL AT 60 KIAS AND AT TAKEOFF EPR 25 DEGREES CELSIUS. NR 2 ENGINE EGT BECAME EXCESSIVE AND A COMPRESSOR STALL OCCURRED. TAKEOFF WAS ABORTED. REPLACED NR 2 ENGINE IAW MM. (M)SDR EISA96098Clamp · looseENGINE NR 1 FIRE WARNING LIGHT ILLUMINATED AFTER TAKEOFF. ENGINE NR 1 SHUTDOWN, LIGHT EXTINGUISHED UPON THROTTLE CLOSING. FOUND CLAMP ON 8TH STAGE DUCT LEAKING AIR ON FIRE WALL LOOP. REMOVED AND INSPECTED CLAMP AND DUCT FOR CRACKS, NO DEFECTS NOTED. RAN ENSDR EISA96089Evac Slide · failedR-1 DOOR SLIDE DID NOT DEPLOY AUTOMATICALLY WHEN DOOR WAS OPENED FOR MINIEVACUATION DEMONSTRATION. REMOVED AND REPLACED R-1 DOOR SLIDE IAW MM 25-10-11. (M)SDR EISA96088Wire · brokenRIGHT EXTERIOR EMERGENCY LIGHT AFT OVERWING INOP. REPAIRED BROKEN WIRE AT LAMP IAW MM 33-20-00. OPS CHECK GOOD. (M)SDR EISA95431Channel · dentedAFT CARGO LOWER BILGE HAT CHANNEL DENTED, AT STATION 967 ABOVE AND BETWEEN STRINGER 30 AND 29L. REMOVED HAT CHANNEL AND DENT, FABRICATED REPAIR PER SRM 51-40-1 TREATED AND PRIMED PER 51-10-2. INSTALLED HAT CHANNEL PER SRM 51-10-2. (M)
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