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 TWAA9711801Bearing · failedSTL - FLT 572 - DURING CRUISE, NR 3 ENGINE, SN 1509, EXPERIENCED VIBRATIONS FOLLOWED BY FULL SCALE DEFLECTION OF NR 3 AVM METER. ALSO, NR 3 ENGINE OIL FILTER BYPASS LIGHT ILLUMINATED. SHUT DOWN ENGINE IN-FLIGHT. ENGINE TOTAL TIME: 43,228 HOURS; 27,505 CYCLSDR TWAA9711601Actuator · malfunctionedSTL - FLT 173 - DURING GEAR RETRACTION THE LEFT MAN GEAR FAILED TO RETRACT ON THE FIRST ATTEMPT, SECOND ATTEMPT WAS SUCCESSFUL. REMOVED AND REPLACD THE LEFT MAIN GEAR ACTUATOR, MFG P/N 65-17830-13, MANUFACTURED BY BOEING. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9804108Screws · brokenMCI - DURING C-CHECK MAINTENANCE, FOUND RT WING LOWER TRAPEZOIDAL PANEL OUTBOARD OF MAIN GEAR TRI-WING SCREWS BROKEN LOOSE AT FORWARD OUTBOARD END. INSTALLED DOUBLER PER SRM 51-40-2 AND FASTENER PR SRM 51-30-3. (M)SDR TWAA9711503Case · crackedDURING TAKEOFF, THE NR 3 ENGINE FIRE LIGHT ILLUMINATED. INTERNAL ENGINE CASE CRACKED BELOW RT 13TH STAGE BLEED DUCT APPROX 3 INCHES. REMOVED AND REPLACED ENGINE. REPAIRED ENGINE AND RETURNED TO SERVICE. (M)SDR EISA97212Seat Track · corrodedMAIN CABIN LEFT INBOARD SEAT TRACK HAS CORROSION FS 360 TO 480. REPLACED SEAT TRACK SECTION FROM FS 360 TO 480 IAW SRM 53-10-05. (M)SDR TWAA9804401Stringer · corrodedMCI - DURING C-CHECK MAINTENANCE, A CORRODED STRINGER WAS FOUND AT FS 350 TO 360, STRINGER 27R. REMOVED CORROSION PER 51-10-6 AND REPLACED STRINGER PER 51-10-1. (M)SDR TWAA9804003Stringer · corrodedMCI - DURING C-CHECK MAINTENANCE, STRINGER 28R WAS CORRODED FS 350 TO FS 360. REMOVED CORROSION PER SRM 51-10-6 AND REPLACED STRINGER PER 51-10-1. (M)SDR TWAA9711101Fuel Heat Vlv · malfunctionedMCI - FLT 712 - DURING CRUISE, THE NR 2 ENGINE, S/N 3954 OIL TEMPERATURE INDICATED HIGH. REMOVED AND REPLACED THE NR 2 ENGINE FUEL HEAT VALVE, MFG P/N 320115, MANUFACTURED BY WHITTAKER CONTROLS. OPERATIONAL CHECK NORMAL. (M)SDR EISA97217Seat Track · crackedMAIN CABIN LEFT OUTBOARD SEAT TRACK HAS CRACKS FS 1050. SEAT TRACK SECTION REPLACED FROM FS 1050 TO 1090 IAW SRM 53-10-05. (M)SDR TWAA9711004Test Card · failedSTL - FLT 146 - DURING LANDING, THE LEFT MAIN GEAR UNSAFE LIGHT ILLUMINATED. REMOVED AND REPLACED THE MASTER DIM TEST CARD, MFG P/N 69-48272-3, MANUFACTURED BY BOEING COMPANY. OPERATIONAL CHECK NORMAL. (M)SDR EISA97214Seat Track · corrodedMAIN CABIN, RIGHT INBOARD SEAT TRACK HAS CORROSION ON BOTH FLANGES FROM FS 360 TO 400. REPLACED SEAT TRACK SECTION FROM FS 360 TO 480 IAW SRM 53-10-05. (M)SDR TWAA9804304Casting · corrodedMCI - DURING OP 17 MAINTENANCE CHECK, THE RT LANDING GEAR AFT DRAG BRACE MOUNT CASTING HAD DEEP PITTING CORROSION BETWEEN BUSHINGS. REPLACED DRAG BRACE MOUNT CASTING PER SRM 51-10-1 AND TWA STD PRACTICES. (M)SDR TWAA9804006Rib · crackedMCI - DURING OP17 MAINTENANCE CHECK, THE LEFT WING WS 738.5 RIB CHORD WAS CRACKED ON LOWER CHORD AT STRINGER 6 AND 8, IN THE RADIUS. INSTALLED NEW RIB PER SRM 51-10-1 AND 51-30-2. (M)SDR TWAA9804005Splice · crackedMCI - DURING OP 17 MAINTENANCE CHECK, A CABIN STRINGER SPLICE WAS CRACKED AT STATION 440 STRIGNER 19R. REPLACED STRINGER SPLICE PER SRM 53-10-3 AND INSTALLED STRINGER REPAIR PER SRM 53-10-3. (M)SDR TWAA9710901Bulb · failedLGA - DURING SCHEDULED MAINTENANCE, THE EMERGENCY LIGHT ADJACENT TO THE AFT LEFT AND RIGHT LAVS WOULD NOT ILLUMINATE. RELAMPED OPERATIONAL CHECK NORMAL. (M)SDR TWAA9803815Stringer · crackedMCI - DURING C-CHECK MAINTENANCE, CRACKS WERE INDICATED AT THE TWO FORWARD HOELS AT BS 760L STRINGER 18 IND IS AT 6 AND 12 O'CLOCK POS IN HOLES. REPAIRED PER SERVICE BULLETING 727-57-0112 AND ARA 11403. (M)SDR TWAA9799001Actuator · leakingSTL - FLT 228 - DURING CLIMB FOLLOWING GEAR RETRACTION THE 'A' SYSTEM HYDRAULIC QTY WENT TO ZERO. REMOVED AND REPLACED THE NR 6 LEADING EDGE FLAP ACTUATOR, MFG PN 1U-1110, MANUFACTURED BY DOWTY AERO SPACE CORPORATION. OPS CHECK NORMAL. (M)SDR TWAA9798001Actuator · failedSTL - FLT 67 - DURING CLIMB, THE LEFT MAIN LANDING GEAR LIGHT REMAINED ON. REMOVED AND REPLACED LEFT MAIN GEAR ACTUATOR, MFG P/N 65-17830-13, MANUFACTURED BY BOEING COMPANY. (M)SDR TWAA9803813Stringer · crackedMCI - DURING OP 17 MAINTENANCE CHECK, THERE WAS A CRACK INDICATION AT THE TWO FORWARD HOLES STATION 760 STRINGER 18, BOTH 6 AND 12 O'CLOCK POSITION. REPAIRED PER ARA 11406 AND SB 727-57-0112. (M)SDR TWAA9803812Former · crackedMCI - DURING OP 17 MAINTENANCE CHECK, A CRACK WAS FOUND ON THE RT SIDE FS 760 FORMER 3, .5 INCH UP FROM CENTER TANK. REPAIRED PER ARA 11406, SB 727-53-0197. (M)SDR TWAA9784005Wheel · vibrationABQ - FLT 160 - DURING TAKEOFF ROLL JUST PRIOR TO ROTATION, A NOSE GEAR VIBRATION WAS NOTED. REMOVED AND REPLACED RIGHT NOSE GEAR TIRE AND WHEEL ASSEMBLY, MFG P/N 3-1395, MANUFACTURED BY B.F. GOODRICH, CO. OPS CHECK NORMAL. CHECK C - 10-30-97 - MCI. (X)SDR TWAA9781004Bushing · failedSTL - FLT 299 - DURING CRUISE, NR 1 ENGINE, SN 3903, WAS SHUT DOWN DUE TO DROP IN OIL QUANTITY. REMOVED AND REPLACED BUSHING, MFG PN 313594, MANUFACTURED BY PRATT & WHITNEY, AND SEAL IN GEARBOX, MFG PN M3248-1-908. ENGINE TOTAL TIME: 63,867 HOURS; 44,078 CYCSDR TWAA9803807Chord · crackedMCI - DURING CORROSION CONTROL CHECK, FUOND UPPER CHORD LBL 70.5 STATION 760 WITH CRACKS INDICATED PER HIGH FREQUENCY EDDY CURRENT CHECK. CRACKS WERE IN UPPER AND LOWER BOLT HOLES 6 AND 12 O'CLOCK POSITION. REPAIRED PER ARA 11749. CHECK - 2-25-97 MCI. (M)SDR TWAA9775003Light Socket · failedPHX - FLT 179 - DURING APPROACH UPON GEAR EXTENSION, RIGHT GEAR DOWN AND LOCK LIGHT FAILED TO ILLUMINATE. REMOVED AND REPLACED RIGHT GEAR LIGHT SOCKET, MFG PN 30413-21-035, MANUFACTURED BY JAY EL PRODUCTS, INC. OPS CHECK NORMAL. CHECK C - 8-23-96 - MCI. (XSDR TWAA9804004Skin · crackedMCI - DURING C-CHECK, THE UPPER L-1 DOOR HINGE CUTOUT SKIN ON FUSE BELOW STRINGER 14L HAD 1.16 INCH LONG CRACK. INSTALLED STAINLESS STEEL DOUBLER REF SSRM 53-10-219. (M)SDR TWAA9803820Skin · crackedMCI - DURING C-CHECK MAINTENANCE, THE LOWER L1 DOOR HINGE CUTOUT ON FUSELAGE SKIN FORWARD WAS FOUND WITH A 1.1666 INCH LONG CRACK. CONFIRMED BY DYE CHECK. INSTALLED STAINLESS STEEL DOUBLER REF SSRM 53-10-219 FIG 202. (M)SDR TWAA9772004Transfer Cyl · failedSTL - FLT 633 - DURING GEAR EXTENSION, NOSE GEAR FAILED TO EXTEND. CYCLED LANDING GEAR TWICE AND NOSE GEAR EXTENDED AND LOCKED. REMOVED AND REPLACED WORN NOSE GEAR HYDRAULIC TRANSFER CYLINDER, MFG P/H 69-14106-5, MANUFACTURED BY BOEING. OPS CHECK NORMAL. (MSDR TWAA9772002Sensing Line · crackedSTL - DURING CRUISE, MADE EMERGENCY DESCENT DUE TO UNCONTROLLABLE CABIN PRESSURIZATION. REMOVED AND REPLACED CRACKED LEFT OUTFLOW VALVE AIR CONDITIONING SENSING LINE. OPS CHECK NORMAL. (M)SDR TWAA9769001Uplock Actuator · failedJFK - FLT 519 - DURING CLIMB EXPERIENCED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE. REMOVED AND REPLACED LEFT MAIN GEAR UPLOCK ACTUATOR AND HOSES. ALSO, REPLACED CASE DRAIN AND MAIN HYDRAULIC FILTERS. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9768002Fuel Pump · failedSTL - FLT 179 - DURING TAKEOFF, NR 3 ENGINE WENT TO BELOW IDLE POWER. REMOVED AND REPLACED FUEL PUMP AND JFC. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9768001O-Ring · wornSTL - FLT 300 - DURING DESCENT LOST 'A' SYSTEM HYD PRESSURE AND FLUID. REMOVED AND REPLACED WORN O-RING IN THE 'A' SYSTEM HYD FILTER PACK. OPERATIONAL CHECK NORMAL. (M)SDR TWAA9803818Angle · crackedMCI - DURING C-CHECK MAINTENANCE, THE RT MLG WHEEL WELL STATION 910 GEAR UPLOCK SUPPORT ANGLE WAS FOUND CRACKED .5 INCH ABOVE THE RADIUS BLOCK. STOP DRILLED CRACK TWO PLACES PER SRM 51-10-1. REPAIRED PER BOEING SB 727-53-165 FIG 2 AND SSRM 53-50-217 FIG 201.SDR TWAA9803817Fasteners · crackedMCI - DURING C-CHECK, FOUND LEFT INBOARD MID FLAP TOP ROW INBOARD FASTENERS, 3 INCIDCATED CRACKED WITH LOW FREQ EDDY CURRENT. COLD WORKED HOLES AND INSTALLED FASTENERS PER SERVICE BULLETING 727-57-160. (M)SDR TWAA9803811Skin · corrodedMCI - DURING C-CHECK MAINTENANCE, THE FUSELAGE REPAIR AT THE AFT LAV SERVICE AREA WAS FOUND BULGED. REPAIRED PER ARA 11727. REMOVED CORROSION PER SRM 51-10-6. REPAIRED PER SRM 53-30-3. (M)SDR TWAA9762001Light · failedSTL - FLT 151 - DURING LAYOVER MAINTENANCE, AFT AIRSTAIR EMERGENCY LIGHT WOULD NOT ILLUMINATE. REMOVED AND REPLACED WORN EMERGENCY LIGHT ASSEMBLY, MFG P/N 11-0283-7, MANUFACTURED BY GRIMES AEROSPACE CO. OPS CHECK NORMAL. (M)SDR TWAA976100Valve · leakingJFK - FLT 191 - DURING CLIMB 'A' SYSTEM HYDRAULIC QTY WENT TO ZERO. REMOVED AND REPLACED LEAKING LEFT MAIN GEAR DOOR SAFETY VALVE, MFG P/N 1372-579788, MANUFACTURED BY PARKER HANNIFIN CORP. OPS CHECK NORMAL.SDR TWAA9760003O-Ring · splitMCI - FLT 117 - DURING DESCENT LOST 'B' SYSTEM HYDRAULIC QTY. REMOVED AND REPLACED SPLIT O-RING AT NR 5 SPOILER ACTUATOR PLUG. OPS CHECK NORMAL. (M)SDR TWAA9756002O-Ring · leakingJFK - FLT 304 - DURING CRUISE EXPERIENCED LOSS OF HYDRAULIC SYSTE 'A' FLUID. REMOVED AND REPLACED O-RING DUE TO HYDRAULIC PRESSURE MODULE O-RING LEAKING. OPS CHECK NORMAL. (M)SDR TWAA9804706Frame · crackedDURING OP17 MAINTENANCE CHECK, FOUND A CRACKED INNER FRAME AT 760 CASTING, LEFT, 6 INCHES INBOARD OF 70.5 WING RIB. REPAIRED PER SERVICE BULLETIN 727-53-0197 AND BOEING DWG 65C36279 AND ARA 11715. (M)SDR TWAA9804705Rib · crackedMCI - DURING OP 17 MAINTENANCE CHECK, EDDY CURRENT SHOWED CRACKS IN FWD UPPER AND LWR FASTENER HOLES IN RIB CHORD UPPER VERTICAL FLANGE, 6 AND 12 O'CLOCK POSITION, FS 760, LBL 70. REPAIRED PER ARA 11715. (M)SDR TWAA9804402Frame · crackedMCI - DURING OP 17 MAINTENANCE CHECK, A CRACKED INNER FRAME 760 CASTING WAS FOUND RT 6 INCH INBOARD OF 70.5 WING RIB. CONFIRMED WITH EDDY CURRENT. REPAIRED PER BOEING DWG NR 65C36279 AND SERVICE BULLETIN 727-53-0197. (M)SDR TWAA9803816Frame · bentMCI - DURING OP 17 MAINTENANCE CHECK, THE FORMER RING AT STATION 1030 STRINGER 25L WAS FOUND BENT. REPAIRED THE FRAME AS PER SSRM 53-60-202 PARA B, SPLICED FRAME REPAIR. (M)SDR TWAA9803806Casting · crackedMCI - DURING OP 17 MAINTENANCE CHECK, EDDY CURRENT INDICATED A CRACK ON FORWARD HOLES ON CASTING BS 760 RBL 70.5. CRACK RUNNING FROM 12 O'CLOCK TO 6 O'CLOCK IN BOTH HOLES. REPAIRED CRACK AT STATION 760 PREVENTATIVE MODIFICATION PER ARA 11713. (M)SDR TWAA9804201Skin · crackedMCI - DURING C-CHECK MAINTENANCE, THE SKIN ON TOP OF LEFT WING FORWARD OF FLUX VALVE WAS FOUND WITH 2 INCH CRACK. CONFIRMED WITH HIGH FREQ EDDY CURRENT. STOP DRILLED PER SRM 51-10-1 AND INSTALLED REPAIR DOUBLER PER SRM 51-40-2. (M)SDR TWAA9803814Chord · crackedMCI - DURNG C-CHECK MAINTENANCE, CURRENT INDICATED A CRACK IN THE FORWARD TWO HOLES IN UPPER RIB CHORD VERT FLANGE STATION 759 RBL 70.5. REPAIRED UPPER AS PER AD94-07-08 AND ARA 11640. REPAIRED LOWER AS PER M27-AD-FD AND ARA 11640. (M)SDR TWAA9751004Connector · contaminatedMCI - FLT 323 - DURING LAYOVER MAINTENANCE, AFT EMERGENCY EGRESS LIGHT WAS INOP. REMOVED MOISTURE FROM TRACK AND CONNECTOR, FUNCTIONAL CHECK NORMAL. (M)SDR TWAA9750002Oven · dirtyLGA - FLT 45 - DURING CRUISE, AFT GALLEY OVEN EMITTED SMOKE INTO PASSENGER CABIN. CLEANED FOOD DEBRIS FROM OVEN AND OPERATIONAL CHECK OF ALL AFT GALLEY OVENS NORMAL. (M)SDR TWAA9749001Oil Line · failedSTL - DURING DESCENT NR 1 ENGINE, S/N 3981, WAS SHUT DOWN DUE TO OIL QTY FALLING TO ZERO. REMOVED AND REPLACED NR 6 BEARING OIL PRESSURE LINE, MFG P/N B02206-1, DUE TO LEAK. (M)SDR TWAA9804001Rib · crackedMCI - DURING C-CHECK MAINTENANCE, THE LEFT WING EDDY CURRENT SHOWED CRACK INDICATION AT 6 AND 12 O'CLOCK POSITION IN RIB CHORD TOP FORWARD HOLE. LEFT BOTTOM FWD HOLE HAD 2 CRACKS IN VERTICAL LEG 2 AND 7 'CLOCK. STOP DRILLED CRACKS PER SRM 51-10-01 FIG 6A. ISDR TWAA9803902Stringer · corrodedMCI - DURING C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER 30 FROM STATION 1010 TO STATION 1183. REPLACED STRINGER PER SRM 51-10-01. (M)
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