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 TWAA0003103Seat Track · corrodedDURING CHECK-C MAINTENANCE, FOUND TOP OF CABIN CHAIR TRACK CORRODED UNDER FLOOR PANELS STA 1030 TO 1070, NUMBER 2 TRACK. REMOVED CORRODED TRACK STA 1030 TO 1070. MADE SECTION OF CHAIR TRACK PER BOEING DRAWING 65-19601 AND INSTALLED TRACK PER SRM 53-10-5.SDR TWAA0002702Rivet · crackedDURING CHECK-C MAINT, FOUND CRACK AT RIVET HEAD ON LT O/B SIDE OF THE NUMBER 2 ENGINE INLET, 17 INCHES UP FROM THE FUSELAGE AND 28 ICHES AFT OF THE INLET L/E. FABRICATED REPAIR PER SRM 54-30-3 AND INSTALLED.SDR TWAA0002803Skin · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON SKIN AND SPLICE PLATE AT STA 680, O/B OF STRINGER 28L. REPAIRED PER SRM 53-30-03, PAGE 14E. REMOVED A 4 IN BY 5 IN SECTION OF SKIN AND CORROSION ON STRINGER. CUT TEMPLATE FOR PLUG. SOLD CORROSION/CLEAN UP TO INSPECTSDR TWAA0002606Stringer · corrodedDURING CHECK-C MAINT, THERE WAS A BULGE IN THE FUSELAGE SKIN AT STA 660, STRINGER 28L. REPLACED STRINGER FROM STA 657 TO 680 PER SRM 53-10-3, PAGE 3.SDR TWAA0002605Bulkhead · crackedDURING CHECK-C MAINT, FOUND A 2 INCH CRACK IN PRESSURE WEB, RT MLG WHEEL WELL AT STA 940, RBL 55. CONFIRMED CRACK WITH HIGH FREQ EDDY CURRENT. INSTALLED REPAIR DOUBLER PER BOEING PRINT 65-89360, AND AD 92-19-11.SDR TWAA0002604Skin · gougedDURING CHECK-C MAINT, FOUND DENT AND GOUGE IN FUSELAGE SKIN AT STA 312, BELOW STRINGER 24R. DENT 1.75 IN BY 2 IN BY 0.046 IN DEEP. NO CRACK FOUND PER PART 6-51-00-03. BLENDED AREA PER SRM 51-10-1. DENT WITHIN LIMITS PER SRM 53-30-1.SDR TWAA0002603Skin · delaminatedDURING CHECK-C MAINT, THE LEFT WING NUMBER 2 AFT FLAP WAS DELAMINATED TOP SKIN 65 IN FROM O/B END. REMOVED AND REPLACED LEFT I/B TRAILING EDGE AFT FLAP PER MM 27-51-02. SAFTIED AND OP CHECK OK.SDR TWAA0002414Torque Box · crackedDURING CHECK-C MAINT THE RT TORQUE BOX VERTICAL WEB (AFT AIRSTAIRS) REPAIR DOUBLER CRACKED ALONG TOP ROW, STR 1273 TO 1269. REPLACED CRACKED WEB USING 7075T6, 0.032 IN METAL, AND MS20470D5, AND MS20470D6 RIVETS AND SSRM 50-80-211.SDR EISA2000011Light · inoperativeEMERGENCY EXIT LIGHT IN COCKPIT INOPERATIVE. REMOVED AND REPLACED EMERGENCY EXIT LIGHT IAW MM 33-50. OPS CHECK GOOD. (M)SDR TWAA0002413Structure · crackedDURING CHECK-C MAINT NUMBER 6 LE SLAT HAD A CRACK AT RIVET UNDER ACTUATOR ATTACH FITTING. FABRICATED A REPAIR PER SRM 57-50-3.SDR TWAA0002412Torque Box · crackedDURING CHECK-C MAINT FOUND 1.5 INCH LONG CRACK IN RT TORQUE BOX UPPER BEAM AFT SIDE OF STA 1273, 3 INCHES O/B OF VERT WEB. REPLACED BEAM (P/N 65-17518-6) AND INSTALLED GUSSET 69-67881-1 AND STIFFENER ANGLE 65-17518-15 USING BACB 3088 8 AND BACB 3088 6 HI-LOKSSDR TWAA0002006Skin · delaminatedDURING CHECK-C MAINTENANCE, THE RT HORIZ STAB TE WAS DELAMINATED, 26 IN INBD OF THE OTBD END TO 69 IN INBD OF THE OTBD END. REPAIRED TE OF RT ELEVATOR PER ARA 16277. RECHECKED BALANCE PER SRM 51-80-7 AND FOUND WITHIN MOMENT ARM REQUIRED. MOMENT 119.240.SDR EISA2000008Switch · shortedDURING CLIMB, DUCT USING RIGHT PACK ONLY, WERE UNABLE TO MAINTAIN PRESSURIZATION ABOVE FL 20,000. AIR TURN BACK TO BRUSSELS. REMOVED AND REPLACED PACK SWITCH. (M)SDR TWAA0002005Stringer · crackedDURING CHECK-C MAINTENANCE, FOUND RIB STA 686.5 STRINGER 10 CRACKED AT UPPER STRINGER TO RIB ATTACHMENT. STOP DRILLED CRACK AND INSTALLED REPAIR PER SSRM 57-20-210, PAGE 213 AND SERVICE BULLETIN 57-A159.SDR TWAA0001404Fitting · crackedDURING CHECK-C MAINT AT AFT AIR STAIRS RT SIDE, FOUND CRACK UNDER ACTUATOR FITTING MOUNT, FWD SIDE, INBD UPPER CHORD, ON PREVIOUS REPAIR. REMOVED REPAIRED ANGLES AND OLD CRACKED ANGLES. REPLACED WITH NEW PARTS PER BOEING DWG 65C13874.SDR TWAA0001403Fitting · crackedDURING CHECK-C MAINT AT AFT AIRSTAIRS THE RT SIDE HAD CRACK UNDER ACTUATOR FITTING MOUNT, AFT SIDE, RUNNING LONGATUDINALLY ALONG CHORD ANGLE. REMOVED CRACK ANGLE AND MADE NEW ANGLE AND INSTALLED PER BOEING DRAWING 65C13874.SDR TWAA0001402Frame · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON FORMER AT STA 1148, BETWEEN STRINGER 24L AND 25L. REMOVED FASTENERS FOR CORROSION REMOVAL. REMOVED CORROSION PER SRM 51-10-6. TREATED CORROSION PER SRM 51-10-6, PAGE 31. PAINTED AND REINSTALLED FASTENERS PER 51-30.SDR TWAA0001401Stringer · corrodeddDURING CHECK-C MAINT, FOUND CORROSION IN THE AFT CARGO COMPT ON STRINGER 27L, AT STA 990. REPLACED 14 INCH SECTION OF STRINGER PER SRM 53-01-1.SDR TWAA0001004Skin · puncturedTHE LT FUSELAGE HAD PUNCTURE HOLE 21 INCHES BELOW CAPTAIN SLIDING WINDOW. REPAIRED PER SRM 53-30-3, FIG 13 SHEET 3. CHECK-C 9-7-99 MCI.SDR TWAA0000302Duct · failedNUMBER 3 ENGINE FIRE WARNING SOUNDED DURING FLIGHT. ENGINE WAS SHUT DOWN AND FIRE WARNING STOPPED. REPLACED 13TH STAGE AIR DUCT AND THE SUBSEQUENTLY DAMAGED EIGHTH STAGE MANIFOLD AND ENGINE COWLING. CHECK-C 9-8-99 MCI.SDR TWAA0001003Skin · puncturedGROUND DAMAGE CAUSED A PUNCTURE HOLE AND DENT AT APPROX STA 229, LT OF AIRCRAFT 21 IN BELOW WINDOW. REPAIRED PER SRM 53-30-03, PAGE 28 FIG 7, AND ENGINEERING. CHECK-C 9-7-99 MCI.SDR TWAA0000102Unknown · smokeSMOKE IN THE CABIN WAS REPORTED IN FLIGHT. APPEARED ONLY WHEN ENGINE ANTI-ICE WAS ON. SMOKE HAD NO ODOR. MAINTENANCE RAN ENGINES AND ACCOMPLISHED OTHER CHECKS BUT WAS UNABLE TO DUPLICATE THE PROBLEM. CHECK-C 5-20-99 JFK.SDR EISA2000033Bleed Valve · wornDURING ENGINE RUN ACCELERATION PRIOR TO TAKEOFF ROLL ENGINES WERE STABILIZED ABOUT 1.4 EPR AND WE HEARD A LOUD BANG. AT ABOUT 1.7 EPR AFTER CHECKING ALL THREE ENGINES WE HEAR THE SAME BANG AND COMPRESSOR STALL ON NR 2 ENGINE WHICH WHICH WE SHUT DOWN AND RETURSDR TWAA0000809Frame · crackedDURING CHECK-C MAINT, FOUND CRACK ON UPPER CORD OF VENTRAL STAIRWELL, AT STA 1273 RT SIDE. INSTALLED REPAIR ANGLE PER SSRM 53-80-211.SDR TWAA0000808Flange · corrodedDURING CHECK-C MAINT, FOUND RT AFT OVERWING EMERGENCY EXIT, PRESSURE SEAL FLANGE BOTTOM SIDE WITH CORROSION FROM 6 INCHES UP ON EACH SIDE TO BOTTOM. REMOVED CORROSION BY SANDING PER SRM 51-10-6, PAGE 147. ALODINED AND PRIMED BARE AREA PER SRM 51-10-2 PAGE 1.SDR TWAA0000807Retainer · corrodedDURING CHECK-C MAINT, FOUND THE FWD RT EMERGENCY EXIT, FWD RT EMERGENCY EXIT BOTTOM SEAL RETAINER HAD CORROSION FROM FWD BOTTOM STOP TO AFT BOTTOM STOP. REMOVED CORROSION BY SANDING PER SRM 51-16-6, PAGE 147.. ALODINED AND PRIMED PER SRM 51-16-2, PAGE 1.SDR TWAA0000412Rib · crackedDURING CHECK-C MAINT, FOUND LT WING NUMBER 3 SPOILER RIB ATTACHED TO OTBD CASTING WAS CRACKED. REPLACED PART PER SRM 57-10-1 AND 51-30-2 FASTENER INSTALLATION. -SDR 2000ZZZX209Frame · corrodedDURING A C-CHECK, CORROSION NOTED ON FRAME AT STA 228.5, BL ZERO.SDR TWAA9916801Light · inoperativeTHE LAST SECTION OF CABIN EGRESS LIGHTS AT ROW 30 WERE INOPERATIVE. REPAIRED THE TRACK FEEDER CABLE. CHECK-C 9-8-99 MCI.SDR 2000ZZZM84Coupler · damagedMIA - ON CLIMB-OUT, WITH AUTO PILOT ENGAGED AT 10000 PLUS 250-260 KTS RUDDER SPLIT AND AUTO PILOT COULD NOT CONTROL AIRCRAFT. DISCONNECTED AUTO PILOT AND FOUND IT TOOK 4 DEGREES RIGHT TRIM TO KEEP AIRCRAFT FROM YAWING. RETURNED TO MIA. TROUBLE SHOT SYSTEM, SDR TWAA0000406Stringer · corrodedDURING CHECK-C MAINT, FOUND CORROSION ON LOWER OTBD EDGE OF STRINGER 29R AT STA 1111. REPLACED S29R FROM STA 1110 TO 1130 PER SRM 53-10-3.SDR 2000ZZZX474Buffet · detectedON TAKEOFF FROM ACA WHILE CLIMBING THROUGH 18,000 FEET, FELT AIRCRAFT JOLT. RETURNED TO ACA FOR GROUND INSPECTION. RETURNED TO ACA AFTER DUMPING FUEL TO OBTAIN PROPER WEIGHT FOR LANDING. INSPECTED AIRCRAFT PER INSTRUCTIONS FROM MIAMI AIR MAINTENANCE CONTROLSDR TWAA9916705Skin · crackedDURING CHECK-C MAINT, THE FORWARD LEFT CABIN ENTRY DOOR, UPPER HINGE CUTOUT WAS CRACKED, GOING FORWARD 1.375 INCH LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED CRACK 0.250 INCH PER SRM 51-10-1, PAGE 6 TO 8. INSTASDR TWAA9916704Skin · crackedDURING CHECK-C MAINT, THE FORWARD LT CABIN ENTRY DOOR, LOWER HINGE CUTOUT WAS CRACKED GOING FORWARD, 1.5 INCHES LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DOUBSDR TWAA0000701Skin · crackedDURING CHECK-C MAINT, THE FWD ENTRY DOOR LOWER HINGE CUT OUT WAS CRACKED, FWD 1 1/2 INCHES IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-01, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10-219, SDR TWAA0000417Skin · crackedDURING OP 16 MAINT CHECK, THE FWD ENTRY DOOR LOWER HINGE CUT-OUT WAS CRACKED OUT, FWD 1.5 IN LONG IN FUSELAGE SKIN. ACCOMP HIGH FREQ EDDY CURRENT AND MARKED END OF CRACK. STOP DRILLED 0.250 IN PER SRM 51-10-1, PAGE 6. INSTALLED REPAIR DOUBLER PER SSRM 53-10SDR TWAA9916001Battery Pack · dischargedTHE AFT AIRSTAIR EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 8-8-99 MCI.SDR TWAA9915503Line · failedTHE NUMBER 1 ENGINE HYDRAULIC PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT AND THE -A- HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. IT WAS NECESSARY TO MANUALLY EXTEND THE LANDING GEAR. THE NUMBER 1 ENGINE PUMP PRESSURE LINE HAD RUBBED THROUGH AT THE PYLON PASS THROSDR TWAA9915201Line · rupturedTHE 'A' HYDRAULIC SYSTEM DEPLETED WHEN THE LANDING GEAR WAS LOWERED. WAS NECESSARY TO MANUALLY CRANK DOWN THE RT MAIN LANDING GEAR. REPLACED FAILED HYDRAULIC LINE FOR THE RT GEAR DOOR ACTUATOR. CHECK-C 7-18-99 MCI.SDR CA991103058Battery · failed(CAN) ON ARRIVAL WITH LOW BATTERY VOLTAGE DEFECT WRITTEN UP IN THE LOG BOOK. THE BATTERY WAS BEING CHARGED BY ELECTRICAL BATTERY CHARGER ON GROUND SERVICE. GROOMING CREW NOTICED FUMES AND SMOKE IN THE CABIN AND EVACUATED AIRCRAFT. BATTERY REMOVED. BATTERY SDR TWAA9914501Power Supply · inopTHE LEFT AFT OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED POWER SUPPLY. CHECK-C 1-29-99 MCI.SDR EISA99208Wire · damagedALL EMERGENCY LIGHTS INOPERATIVE. REPAIRED DAMAGED WIRES BEHIND CONTROL PANEL, OPS CHECK GOOD. (M)SDR TWAA9913801Line · rupturedDURING FLIGHT THE 'B' HYDRAULIC SYSTEM FLUID WAS LOST RESULTING IN LOSS OF THE SYSTEM HYDRAULIC PUMPS. USED PNEUMATIC BRAKES DURING LANDING. REPLACED TWO HYDRAULIC LINES, MFG AE1008787H290 AND AE3660130K0290. CHECK-C 1-29-99 MCI.SDR EISA99175Actuator · malfunctionedON TAKEOFF, WHEN FLAPS AND LEADING EDGE DEVICES WERE RETRACTING, NR 7 SLAT FAILED TO RETRACT, RECYCLED BUT REMAINED EXTENDED. AIR TURN BACK TO (VIT). UPON LANDING FLAPS WERE RETRACTED AND NR 7 SLAT RETRACTED. INSPECTED SLAT, NO DEFECTS NOTED. (M)SDR EISA99173Actuator · malfunctionedON TAKEOFF, WHEN FLAPS AND LEADING EDGE DEVICES WERE RETRACTING, NR 7 SLAT FAILED TO RETRACT, RECYCLED BUT REMAINED EXTENDED. AIR TURN BACK TO (VIT). UPON LANDING FLAPS WERE RETRACTED AND NR 7 SLAT RETRACTED. INSPECTED SLAT, NO DEFECTS NOTED. (M)SDR TWAA9911401Hyd Lines · leakingDURING GEAR RETRACTION AFTER TAKEOFF HAD COMPLETE LOSS OF THE -A- HYDRAULIC SYSTEM. MANUALLY EXTENDED GEAR AND USED ALTERNATE FLAP EXTENSION. RETURNED TO SAT. FOUND THE RT LANDING GEAR DOOR OPEN AND CLOSE HYD LINES LEAKING. REPLACED THE OPEN LINE BACH8A06NSDR TWAA9911103Wire · failedUNABLE TO RAISE, THE GEAR HANDLE AFTER TAKEOFF AT JFK WAS NECESSARY TO TO USE THE OVERRIDE LEVER LATCH TO RAISE THE GEAR. FOUND WIRE W31203922 WAS OPEN. SPLICED THE WIRE. REF WDM 32-31-01 PAGE 1. CHECK-C 10-29-98 MCI.SDR TWAA9910801Light · failedTHE AFT SECTION OF THE CABIN EMERGENCY EGRESS LIGHTS FAILED TO ILLUMINATE. REPLACED THE EGRESS LIGHT STRIP. CHECK-C 2-26-99 MCI.SDR TWAA9910401Plug · failedABOUT 15 MINUTES INTO FLIGHT LOST B HYDRAULIC SYSTEM FLUID. RETURNED TO STL. THE NUMBER 5 SPOILER PLUG BLEW OUT OF THE ACTUATOR. REPLACED THE PLUG. CHECK-C 12-13-98 MCI.SDR TWAA9910101Motor · leakingTHE A-HYDRAULIC SYSTEM QUANTITY WENT TO ZERO. MANUALLY EXTENDED THE LANDING GEAR AND RETURNED TO STL. REPLACED THE O/B FLAP DRIVE MOTOR DUE TO LEAKAGE. CHECK-C 8-24-98 MCI.
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