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 EISA20000165Skin · corrodedT/H FWD E&E COMPARTMENT AT FS 294 - 312, RBL 20 CORRODED TOP WHEEL WELL. REMOVED, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED DOUBLER IAW B727-200 SRM 51-10-6, 51-10-2 AND 51-20-1 AND 51-30-2.SDR EISA20000178Beam · crackedPERFORMED HFEC LOCATED CRACK AT BS1050 AND STR 26R. CORRECTIVE ACTION: REMOVED, FABRICATED, REPAIR DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 51-30-2, 53-10-2 AND 53-10-4.SDR EISA20000177Floorbeam · gougedFLOORBEAM AT STA 990 LBL 70, UPPER CHORD, AFT FLANGE GOUGED. REMOVED, FABRICATED REPAIR DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-8.SDR EISA20000174Angle · crackedNR 1 ENGINE NOSE COWL AFT SECTION AT BULKHEAD FLANGE CRACKED. REMOVED, FABRICATED REPAIR ANGLE AND FILLER, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 54-10-3.SDR EISA20000157Clip · crackedSTR 8L END TIE IS CRACKED AT STA 950. REMOVED AND REPLACED END TIE IAW B727-200 SRM, 51-10-1, AND 51-30-2.SDR EISA20000173Fitting · crackedPERFORMED BHFEC AT FLAP TRACK LANDING GEAR DOOR FED HINGE FITTING ATTACHMENT HOLES LT AND RT SIDE 7 HOLES TOTAL. REAMED HOLES PER BOEING SB 727-32-0340.SDR EISA20000160Skin · separatedLEFT WING O/B AILERON O/B TRAILING EDGE CORNER METAL SEPARATED. REMOVED, FABRICATED SKIN DOUBLERS AND FILLERS, BONDED, ALODINED, AND PRIMED SKIN DOUBLERS AND FILLERS IAW B727-200 SRM 51-10-, 51-20-1, 51-40-5, 51-40-6, 57-50-2 AND B727-200 MM 51-20-151.SDR EISA20000159Skin · gougedLT WING O/B AILERON T/E LOWER SURFACE HAS GOUGE. REMOVED, FABRICATED REPAIR DOUBLERS AND FILLERS, BONDED, ALODINED, PRIMED IAW B727-200 SRM 51-10-2, 51-20-1, 51-40-5, 51-40-6, 57-50-2, AND B727-200 MM 51-20-151.SDR EISA20000175Fitting · crackedPERFORMED HFEC ON FWD LANDING GEAR DOOR HINGE FITTING FOUND CRACKS TOTAL OF 8 HOLES LT AND RT SIDE. REAMED ALL SIDES, CLEANED, SHOT PEENED FITTINGS, ALODINED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2, SOPM 20-10-03 AND SB 727-32-0340.SDR 20010111SG025Longeron · crackedDURING C-CHECK, FOUND AFT CARGO COMPARTMENT BS 950E AT STRINGER 29R HAS CORROSION. REMOVED CORROSION FROM STRINGER AND FOUND CRACK IN STRINGER AT STATION 950E. REMOVED AND REPLACED STRINGER FROM STATION 950 TO 1110. INSTALLED DOUBLER TRIPLER AND QUADRUPLER WSDR EISA20000169Floorbeam · corrodedFLOORBEAM SUPPORT STRAP AT BS 1030 TO BS 1070 BL 72R CORRODED. REMOVED, FABRICATED STRAP SPLICE, ALODINED, PRIMED AND INSTALLED STRAP SPLICE IAW B727-200 SRM 51-10-2 AND 53-10-3.SDR TWAA0013404Bottle · dischargedTHE LEFT SIDE NUMBER 2 CABIN DOOR SLIDE HAD LOW BOTTLE PRESSURE. REPLACED THE SLIDE ASSEMBLY. CHECK-C 11-18-99 MCI.SDR TWAA0013401Cable · out of rigDURING CLIMB APPROXIMATELY 1 MINUTE AFTER GEAR HANDLE PLACED IN THE OFF POSITION THE LANDING GEAR EXTENDED. GEAR HANDLE WAS PLACED IN THE UP POSITION, FOR GEAR RETRACTION, AND WAS LEFT THERE WHILE THE FLIGHT PROCEEDED AT REDUCED AIR SPEED. RIGGED LGVB AND LGSDR EISA20000189Doubler · crackedBS 560 CRACKED B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR DOUBLER AND FILLER ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.SDR EISA20000188Angle · crackedBS 580 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED, FABRICATED REPAIR ANGLE ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.SDR EISA20000187Doubler · crackedBS 620 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED FABRICATED PLATES AND FILLER, ALODINED, PRIMED AND INSTALLED PLATES AND FILLER IAW B727-200 SRM 51-10-2 AND 51-40-4.SDR EISA20000186Doubler · crackedBS 640 CRACKED B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR DOUBELR, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.SDR EISA20000170Splice · crackedSTR 22R BETWEEN BS 380 - 400, CRACKED. REMOVED FABRICATED SPLICE, ALODINED, PRIMED AND INSTALLED REPAIR SPLICE IAW B727-200 SRM 51-10-2, 51-10-6 AND 53-10-3.SDR EISA20000176Angle · crackedBS 540 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED SECTION, FABRICATED ANGLE REPAIR, ALODINED, PRIMED AND INSTALLED ANGLES REPAIR IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.SDR TWAA0013303Battery · inoperativeTHE OVERHEAD EMERGENCY LIGHT AT THE BOTTOM OF THE AIRSTAIRS WAS INOPERATIVE. REPLACED THE BATTERIES. CHECK-C 11-18-99 MCI.SDR EISA20000185Doubler · misdrilledBS 720E DRILLED HOLE IN RADIUS B/T CUSP AND STR 16R ON FRAME. REMOVED FABRICATED DOUBLER AND FILLER, FORMED, DRILLED, DEBURRED, ALODINED AND PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2 AND 53-10-4.SDR EISA20000184Angle · misdrilledBS 950F DRILLED HOLES IN RADIUS B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2 AND 53-10-4.SDR EISA20000183Frame · misdrilledBS 970 DRILLED HOLE IN RADIUS B/T CUSP AND 16R ON FRAME. ROUNDED HOLE IN RADIUS, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727-200 SRM, 51-10-2, 51-40-3 AND 53-10-2.SDR EISA20000182Angle · misdrilledBS 1110 TRIPLE DRILLED HOLE BT CUSP AND STR 16R ON FRAME. REMOVED, FABRICATED REPAIR ANGLE AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2 AND 53-10-4.SDR EISA20000181Doubler · misdrilledBS 950D DRILLED HOLE IN RADIUS B/T CUSP AND STR 16L /IB FRAME. REMOVED, FABRICATED DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2 AND 53-10-4.SDR EISA20000180Angle · misdrilledBS 1110 DRILLED HOLE IN RADIUS B/T CUSP AND STR 16L I/B FRAME. REMOVED, FABRICATED ANGLE REPAIR, ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.SDR TWAA0013001Light · inoperativeTHE EMERGENCY EXIT LIGHT ABOVE THE AFT HOSTESS JUMP SEAT, AND AT CABIN ROW 3 WERE INOPERATIVE. REPLACED THE BATTERY PACK AND POWER SUPPLY, (P/N 50202-090), FOR THE HOSTESS SEAT, AND REPLACED THE LAMP, (P/N 1315) AT ROW 3. CHECK-C 12-12-99 MCI.SDR 20010111SG029Seat Track · crackedDURING C-CHECK, FOUND SEAT TRACK LEFT, OUTBOARD OF CENTER, TRACK CORRODED AT OUTER EDGES BETWEEN BS 1030 AND 1070. REMOVED CORROSION FROM TRACK, FOUND TRACK CRACKED. REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-2 AND 53-10-5. (M)SDR 20010111SG026Seat Track · corrodedDURING C-CHECK, FOUND SEAT TRACK LEFT OUTBOARD BETWEEN BS 1110-1130 CORRODED ON UPPER FACE. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-10-2, 51-30-2 AND 53-10-5. (M)SDR EISA20000125Door · not closedAIRCRAFT WOULD NOT MAINTAIN PRESSURE. AIR TURNBACK TO (CVG). VISUALLY INSPECTED EXTERIOR DOORS FOR SECURITY, FOUND VAULT DOOR HANDLE CLOSED, BUT DOOR NOT FULLY CLOSED. CYCLED DOOR SEVERAL TIMES, LIGHT AND DOOR OPS CHECK NORMAL.SDR EISA20000105Accumulator · leakingTEN MINUTES AFTER TAKEOFF A SYSTEM HYDRAULIC PRESSURE DROPPED TO 1000 PSI AND SYSTEM FLUID QUANTITY DROPPED TO O, SEE LOG PAGE 60983 REPEAT WRITE UP. REMOVED AND REPLACED A SYSTEM ACCUMULATOR, NR 1, NR 2, ENGINE HYDRAULIC PUMPS, IAW M/M 29-00, OPS CHECK NORMASDR EISA20000104Accumulator · lowAFTER 25 MINUTE OF FLIGHT A HYDRAULIC SYSTEM FLUID LEVEL WENT TO ZERO, BOTH PUMP LOW PRESSURE LIGHTS CAME ON. AIR TURN BACK TO ELP. REMOVED AND REPLACED A SYSTEM PUMP FILTERS, NO CONTAMINATION FOUND. REPLACED A SYSTEM ACCUMALATOR IAW M/M 29-00, OPS CHECK NOSDR TWAA0012501Relay · failedTHE EMERGENCY EXIT AND EGRESS LIGHTING CAME ON INTERMITTENTLY. REPLACED THE R70 RELAY. CHECK-C 10-25-99 MCI.SDR 20010111SG028Stringer · corrodedDURING C-CHECK, FOUND LEFT FUSELAGE STATION 1160 TO 1183 STRINGER 22L HAS SURFACE CORROSION. REMOVED AND REPLACED DAMAGED STRINGER 24.5 INCHES AT LT FS 1160-1183 IAW SRM 53-10-3 PAGE 4B AND 4A. (M)SDR 20010117SG001Structure · damagedDURING C-CHECK, FOUND 1 INCH DAMAGE TO LEFT HORIZONTAL STAB LOWER FORWARD CHORD OF FORWARD SPAR STATION 101. CUT OUT DAMAGED SECTION OF CHORD. FABRICATED AND INSTALLED ANGLE AND FILLER IAW SRM 51-10-3, 51-10-2 AND 55-10-5 FIG 1. (M)SDR TWAA0012102Light · inoperativeTHE EMERGENCY LIGHT WAS INOPERATIVE AFT OF THE AFT STAIRWAY, AND ON THE FUSELAGE EXTERIOR ON RT SIDE BELOW THE OVERWING EXIT. TIGHTENED LOOSE BATTERY CLIPS FOR THE AFT STAIRWAY, AND REPLACED THE LAMP FOR THE OVERWING EXIT. CHECK-C 9-29-99 MCI.SDR TWAA0012002Power Supply · wornTHE AFT AIRSTAIR AND RT WING FWD EMERGENCY LIGHTS WERE INOPERATIVE. REPLACED THE POWER SUPPLY. CHECK-C 9-29-99 MCI.SDR C8GA200000008Circuit Breaker · trippedFLIGHT BX719 FROM MCO TO TOL. DURING CLIMBOUT, NR 2 BUSS TIE LIGHT ILLUMINATED. 15 SECONDS LATER NR 2 GENERATOR AND FIELD TRIPPED, YAW DAMP LIGHT ILLUMINATED, AND CAPT''S AND F/O LOST ALL INSTRUMENTS. CLOSED BUSS TIE AND CAPT''S INSTRUMENT POWER RETURNED EXCSDR 20010111SG027Web · crackedDURING C-CHECK, FOUND FUSELAGE UPPER LOBE INTERIOR AFT LEFT FLOOR PLATE BETWEEN STATION BS 1050 AND BS 1183 AND BETWEEN LEFT OUTBOARD OF CENTER TRACK TO THE WALL, HAS CORROSION ON SEVERAL PLACES AND IS CRACKED FORWARD OF BS 1183. REMOVED CORROSION FROM FUSELASDR C8GA200000007Roller · out of adjFLIGHT 207 FROM HSV TO DAY. DURING CLIMBOUT, AT APPROXIMATELY 10,000 FT, THE FORWARD ENTRY DOOR WAS LEAKING AND MADE A LOUD NOISE. AIRCRAFT RETURNED TO HSV AND LANDED WITHOUT FURTHER INCIDENT. INSPECTED DOOR AND FOUND ROLLER CAMS HAD NOT ENGAGED PROPERLY INSDR TWAA0011501Battery · dischargedTHE RT FWD OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 9-29-99 MCI.SDR TWAA0011503Battery · dischargedTHE LT WING EXTERIOR OVERWING EMERGENCY EXIT LIGHT WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 10-25-99.SDR TWAA0010601Light · inoperativeTHE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS INOPERATIVE. REPLACED THE BULB. CHECK-C 11-18-99 MCI.SDR TWAA0010201Connector · dirtyTHE FWD CABIN LT AND RT SLIDE LIGHTS WERE INOPERATIVE. CLEANED CONNECTORS AT THE BATTERY PACK. CHECK-C 9-7-99 MCI. ---CLOSED--SDR C8GA200000004Pump · inoperativeFLT 216 KDAY-KHSV WITH ENG POWER SET AT REDUCED TAKEOFF POWER SETTING OF 2.0 EPR AND 95 PERCENT N1 NR 1 ENG WENT TO 2.4 EPR, RETARDED THROTTLE AND EPR QUICKLY DROPPED TO 1.8. TRIED TO RESET POWER AND NO EPR RESPONSE TO THROTTLE MOVEMENT OCCURRED. ABORTED TAKSDR TWAA0009201Battery Pack · inoperativeTHE RT FWD AND LT FWD EMERGENCY SLIDE LIGHTS WERE INOPERATIVE, AND THE AFT SECTION OF EGRESS LIGHTS WERE VERY DIM. CLEANED DIRTY PINS AT THE BATTERY PACK FOR THE SLIDE LIGHTS, AND CLEANED AND DRIED THE EGRESS LIGHT STRIP AND CONNECTIONS. CHECK-C 9-7-99 MCI.SDR TWAA0009103Power Supply · inoperativeTHE EMERGENCY LIGHTS AT ROW 18 EMERGENCY EXIT WERE INOPERATIVE. REPLACED THE POWER SUPPLY IN AFT AIRSTAIR. CHECK-C 12-12-99 MCI.SDR C8GA200000003Radar · malfunctionedFLT.514 FROM KBWI TO KROC. ON FOURTH (4TH) LEG OF THE DAY''S OPERATION, WEATHER (WX) RADAR WAS TURNED ON BUT DID NOT OPERATE NORM. THE DISPLAY SCREEN WOULD NOT PAINT ANY WEATHER, GROUND OR RADAR SYMBOLOGY. IMC CONDITIONS WERE IN EXISTANCE ALONG ROUTES OF FLISDR TWAA0009001Light · wornTHE RT FWD OVERWING EMERGENCY LIGHT AND THE LIGHT AT THE BOTTOM OF THE AIRSTAIRS WERE INOPERATIVE. REPLACED THE BULB FOR THE OVERWING LIGHT, AND TIGHTENED SCREWS ON THE AFT STAIR LIGHT. CHECK-C 9-29-99 MCI.SDR TWAA0008901Battery Pack · inoperativeTHE EMERGENCY CEILING AREA LIGHT AT CABIN ROW 3 WAS INOPERATIVE. REPLACED THE BATTERY PACK. CHECK-C 2-20-00 MCI.
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