Boeing 727-231
Service difficulty reports · 840
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 = '727231' 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 = '727231' 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 95ZZZZ229Stringer · crackedMCI - DURING CHECK-C, FOUND A ONE-INCH LONG CRACK IN STRINGER 16, STA 656.5. REPAIRED PER SRM 57-20-201 FIG 207. TOTAL CYCLES 45,150. (Z)SDR 95ZZZW601Frame · crackedMCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN FUSELAGE FRAME, FS 783.95. REPAIRED PER SERVICE BULLETIN 727-53-0197, DRAWING NR 65C36280 AND EMLR 65639.SDR 95ZZZW600Stringer · crackedMCI - DURING C-CHECK, FOUND A ONE INCH LONG CRACK IN STRINGER 16, STATION 656.5. REPAIRED PER SRM 57-20-201, FIGURE 207.SDR 95ZZZW268Controller · malfunctionedSTL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PSDR 95ZZZW267Controller · malfunctionedSTL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PSDR 95ZZZW266Outflow Valve · malfunctionedSTL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PSDR 95ZZZW265Outflow Valve · malfunctionedSTL - DURING CRUISE, CABIN PRESSURE BEGAN CLIMBING WITHOUT ABILITY TO CONTROL, AND PASSENGER OXYGEN MASK DEPLOYED. THE FLIGHT MADE AN UNSCHEDULED LANDING. REPLACED BOTH OUTFLOW VALVES, (P/N 103280-5-1), AUTO PRESSURE CONTROLLER, (P/N 763810-1), AND MANUAL PSDR 95ZZZW643Deck · crackedMCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940. STOP DRILLED CRACK AND REPAIRED PER ARA 9117A. TOTAL CYCLES 45,150.SDR 95ZZZW597Deck · crackedMCI - DURING C-CHECK, FOUND A .25 INCH CRACK IN PRESSURE DECK OUTBOARD END, STATION 940. STOP DRILLED CRACK AND REPAIRED PER ARA 9117A.SDR 95ZZZW263Duct · rupturedSTL - DURING CLIMB, NR 3 ENGINE FIREWARNING SOUNDED. REDUCED POWER ON THE NR 3 ENGINE AND FIREWARNING CEASED. FOUND 13TH STAGE DUCT AND PERFORMED A HIGH POWER LEAK CHECK. CHECKED NORMAL. CHECK C-1 11-21-94 - MCI.SDR 95ZZZW231Skin · crackedMCI - DURING OP-17, FOUND A 1.5 INCH CRACK IN VERTICAL STABILIZER SKIN FUSELAGE, STA 1333. REPAIRED PER ARA 9113. TOTAL CYCLES 22210.SDR 95ZZZW641Stringer · corrodedMCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990. REPAIRED PER ARA 9054. TOTAL CYCLES 22,210.SDR 95ZZZW640Stringer · crackedMCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000. REPAIRED PER ARA 9054. TOTAL CYCLES 22,210.SDR 95ZZZW599Stringer · crackedMCI - DURING OP-17 FOUND A SIX INCH LONG CRACK IN AFT CARGO BIN, STRINGER 29L, FS 1000. REPAIRED PER ARA 9054.SDR 95ZZZW596Stringer · corrodedMCI - DURING OP-17, FOUND CORROSION IN AFT CARGO BIN, ON LEG OF STRINGER 29L, AROUND TWO HI-LOCKS, FS 990. REPAIRED PER ARA 9054.SDR 95ZZZW232Stringer · corrodedMCI - DURING OP-17, FOUND CORROSION IN AFT CARGO STRINGER/STRINGER SPLICE 29R AND 29L, FS 990. REMOVED CORROSION PER SRM 51-10-6 AND REPAIRED PER ARA 8682 AND STANDARD PRACTICES. TOTAL CYCLES 22210.SDR 95ZZZW219Stringer · crackedMCI - DURING OP-17 FOUND A 6 INCH CRACK AT AFT CARGO STRINGER 29, IN RT VERTICAL LEG INBOARD SIDE, FS 1000 TO FS 1010. REPAIRED PER ARA 8682 AND STANDARD PRACTICES. TOTAL CYCLES 22,210.SDR 95ZZZW216Ring · bentMCI - DURING OP-17, FOUND FORMER RING BENT BETWEEN STRINGERS 23L AND 24L, FS 520. REPAIRED PER ARA 9106. TOTAL CYCLES 22,210.SDR 95ZZZW220Skin · crackedMCI - DURING CHECK C-1D, FOUND A 1.5 INCH CRACK IN FORWARD FUSELAGE, RUNNING FORWARD TO FASTENER HOLE UPPER HINGE CUTOUT, FORWARD ENTRY DOOR. REPAIRED BY INSTALLING DOUBLER PER S/B 727-53-0198. TOTAL CYCLES 25,548.SDR 95ZZZW218Skin · crackedMCI - DURING C-CHECK, FOUND A ONE INCH CRACK IN EXTERIOR SKIN AT TOP AFT CORNER OF FORWARD ENTRY DOOR. CUT OUT CRACKED AND DAMAGED AREA, REPAIRED PER SRM 5-30-03. TOTAL CYCLES 33,173.SDR 95ZZZX857Actuator · malfunctionedSTL - FLT 297 - AFTER TAKEOFF WHEN LANDING GEAR WAS RETRACTED, THE RIGHT MAIN WHEELWELL DOOR LIGHT REMAINED ILLUMINATED; CYCLED LANDING GEAR. FOUND DOOR HYDRAULIC ACTUATOR, MFG 7-3141-4, BYPASSING. REPLACED RIGHT MLG DOOR ACTUATOR. LANDING GEAR DOOR AND DOOSDR 95ZZZX878Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.SDR 95ZZZX1399Skin · crackedJFK - DURING SPECIAL CHECK, FOUND A 4 INCH CRACK IN RT WING NR 5 LEADING EDGE SLAT, ON INBOARD LOWER SURFACE, RT SIDE. STOP DRILLED CRACK AND REPAIRED PER SRM 57-50-3, FIGURE 1, PAGE 2A. AIRCRAFT TOTAL TIME: 37,178 HOURS; 24,066 CYCLES.SDR 95ZZZX879Fuel Tank · crackedMCI - DURING OP-17, FOUND CRACK IN LT WING FUEL TANK IN TOP AFT NR 3 STRINGER, WS 656.50, AT RIB NR 6 ATTACH POINT. REPAIRED PER SSRM 57-20-201, PAGE 215, FIGURE 207. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES.SDR 95ZZZX1398Stringer · crackedMCI - DURING OP-17, FOUND CRACK IN LT WING FUEL TANK IN TOP AFT NR 3 STRINGER, WS 656.50, AT RIB NR 6 ATTACH POINT. REPAIRED PER SSRM 57-20-201, PAGE 215, FIGURE 207. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES.SDR 95ZZZW123Skin · crackedMCI - DURING SPECIAL CHECK, FOUND CRACK IN LT LOWER LAP FUSELAGE SKIN, STA 490, LT STRINGER LAP 26L. CUT OUT CRACK AND CORROSION PER SRM 53-30-03 AND REPAIRED PER SRM 53-30-3 FIG 14. TOTAL CYCLES 42,197.SDR YAUA9502Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 1 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR 95ZZZX854Skin · corrodedDURING OP-17, FOUND FUSELAGE TOP SKIN AT STA 1110 TO STA 1120 DENTED LEFT AND RIGHT OF BL 0. REPAIRED PER SRM 53-30-3, FIGURE 3. AIRCRAFT TOTAL TIME: 36,843 HOURS; 22,210 CYCLES.SDR 95ZZZX1046Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 8 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR 95ZZZX1045Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 5 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR 95ZZZX1044Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 4 L/E SLAT STRUCTURAL STOP WITH 1 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR 95ZZZX1043Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 3 L/E SLAT STRUCTURAL STOP WITH 3 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR 95ZZZX1042Bolts · looseCOMPLY WITH INSPECTION FOR LOOSE OR BROKEN BOLTS IAW SB 727-57-171. INSPECTION FOUND NR 2 L/E SLAT STRUCTURAL STOP WITH 2 EACH BOLTS LOOSE. IN ORDER TO COMPLY FULLY WITH SB 727-57-171, REMOVED ALL SLATS INCLUDING NR 6 AND NR 7 SLATS MODIFIED IAW SB USING KITSDR YAUA9501Window Post · crackedTYPE SERVICE '2B' CHECK. X-RAY OF WINDOW POST N-F, AD 93-05-17, REF. SB 737-53-0086. FOUND CRACK AT 6TH FASTENER DOWN TO EDGE OF POST N-F, RIGHT HAND. EDDY CURRENT USED TO VERIFY CRACK. MODIFICATION/REPAIR DONE IAW SB 727-53-0086, REV 2, PART II, PAGE 24, SDR 95ZZZX852Tie · corrodedMCI - DURING CHECK C-2D, FOUND CORROSION AT END OF LONGERON TIE TO STR 29R. REMOVED CORROSION PER SRM 51-10-6, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440. AIRCRAFT TOTAL TIME: 37,342 HOURS; 24,204 CYCLES.SDR 95ZZZX850Stringer · crackedMCI - DURING CHECK C-2D, FOUND A 6 INCH CRACK AT STR 29R, BS 990, OUTBOARD SIDE OF BOTTOM RADIUS. STOP DRILLED CRACK PER SRM 51-10-1, PAGE 6A, AND REPAIRED PER SSRM 53-10-213 AND TWA DWG. C03440. ACFT TOTAL TIME: 37,342 HOURS; 24,204 CYCLES.SDR 95ZZZX711Skin · crackedMCI - DURING CHECK 'C', FOUND .3750 INCH CRACK IN FORWARD GALLEY DOOR OUTER SKIN, FROM FASTENER TO EDGE OF DOOR CUT-OUT, LOWER AFT CORNER. INSTALLED REPAIR PER SSRM 53-30-206, PAGE 201 AND PAGE 204. AIRCRAFT TOTAL TIME: 66,258 HOURS; 45,561 CYCLES.SDR 96ZZZM190Door Frame · crackedMCI - DURING C-CHECK, FOUND A 1.5 INCH CRACK IN CABIN FORWARD DOOR FRAME RIGHT SIDE. REPAIRED PER SRM 51-40-3, FIGURE 1 AND TWA STANDARD PRACTICES. (M)SDR 95ZZZX712Casting · crackedMCI - DURING CHECK C-2D, FOUND .75 INCH CRACK IN TOP INBOARD CORNER OF NR 1 ENGINE AFT ENGINE MOUNT CASTING. REPAIRED BY INSTALLING DOUBLERS PER BOEING DWG 65C34994. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES.SDR 95ZZZX546Bulkhead · crackedDURING CHECK C-2D, FOUND CRACK APPROXIMATELY TWO INCHES IN BULKHEAD BELOW APU FLOW CONTROL VALVE, IN RT MLG WHEELWELL. STOP DRILLED CRACK AND INSTALLED DOUBLER PER TWA DWG C03242 AND TWA STANDARD PRACTICES. AIRCRAFT TOTAL TIME: 61,014 HOURS; 40,930 CYCLES.
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