Boeing 727-2J7
Service difficulty reports · 117
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 = '7272J7' 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 = '7272J7' 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 97ZZZX4688Coupler · shortedLOG BOOK ENTRY: EXCESSIVELY HARD LOWER RUDDER INPUTS LEFT AND RIGHT INDEPENDANT OF PILOT ACTION OR INPUT. VISUAL INDICATION OF SAME ON COCKPIT RUDDER INDICATOR. FOUND LOWER YAW DAMPENER RACK CONNECTOR WET WITH WATER. GALLEY FLOOR DRAIN SYSTEM AT FAULT. RESDR 97ZZZM1117Seat Track · corrodedSEAT TRACK NR 4 STATION 500-600 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)SDR 97ZZZM1116Seat Track · corrodedSEAT TRACK CORRODED BEYOND LIMITS STATION 1010-1130 NR 4. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0, 51-30-2. (M)SDR 97ZZZM1115Floorbeam · corrodedFLOORBEAM AT STATION 344 CORRODED BEYOND LIMITS END TO END. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-6, 51-30-2 AND 51-10-01 AND 53-10-8. (M)SDR 97ZZZM1114Seat Track · corrodedSEAT TRACK NR 5 CORRODED FROM STATION 344-380 BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)SDR 97ZZZM1113Floorbeam · corrodedFLOORBEAM AT STATION 380 CORRODED BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-6, 51-30-2, 51-10-01 AND 53-10-8. (M)SDR 97ZZZM1112Seat Track · corrodedSEAT TRACK NR 3 FROM STATION 344-480 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-10-6, 51-20-0 AND 51-30-2. (M)SDR 97ZZZM1111Skin · corrodedLEFT AND RIGHT RAM AIR PLENUM CAVITY SKINS CORRODED BEYOND LIMITS AT STATION 772.45 TO 848.95. REPAIRED IAW BOEING DOC DWG MAJR970919 AND B727 SRM 57-30-3 FIG 9 DETAIL 1 AND 53-30-10 FIG 1. (M)SDR 97ZZZM1110Seat Track · corrodedSEAT TRACK NR 4 FROM STATION 344-500 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)SDR 97ZZZM1109Seat Track · corrodedSEAT TRACK NR 1 FROM STATION 344-480 CORRODED BEYOND LIMITS. REMOVED AND REPLACED SEAT TRACK IAW BOEING SRM 51-10-0, 51-10-2, 51-20-0 AND 51-30-2. (M)SDR 97ZZZM1108Floorbeam · corrodedFLOORBEAM CORRODED END TO END AT STATION 400 BEYOND LIMITS. REMOVED AND REPLACED FLOORBEAM IAW BOEING SRM 51-10-2, 51-10-0, 51-10-6, 51-30-2 AND 53-10-8. (M)SDR C8GA977103Engine · failedFLT 224 - KPAP-KMIA - ON TAKEOFF ROLL, AT APPROXIMATELY 65 KTS, ENGINE NR 2 FAILED. WITH PRONOUNCED VIBRATION IN POWER QUADRANT AND ENGINE FAIL LIGHT ILLUMINATED. ENGINE READINGS, EPR 0, N1 22 PERCENT, N2 45 PERCENT, FF 1200, EGT 570 DEGREES. (M)SDR 96ZZZX6181Fuel Control · failedFLT PT 301 DEPARTED MIAMI, FL FOR CUARAZAO (CUR) ON THIS DATE. TAKEOFF WAS NORMAL UP TO THE TIME OF THE FIRST POWER REDUCTION. POWER REDUCTION WAS NORMAL FOR NR 2 AND NR 3 ENGINES; BUT, NR 1 ENGINE REMAINED AT HI POWER WITH NO RESPONSE TO THROTTLE MOVEMENT. SDR 96ZZZX6148Downlock Switch · inoperativeAFTER TAKEOFF FROM TPA WITH THE GEAR HANDLE IN THE GEAR UP POSITION, BOTH THE RED AND GREEN NOSE GEAR LIGHTS REMAINED ILLUMINATED. THE GEAR HANDLE WAS PLACED IN THE GEAR DOWN POSITION AND THE AIRCRAFT RETURNED TO TPA WITHOUT INCIDENT. TROUBLESHOOTING OF THE SDR 97ZZZX1467Floor Beam · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON LOWER FLOOR BEAM CHORD AT FS 1166 AT BL ZERO.SDR 97ZZZX1466Skin · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON SKIN PANEL AT FS 340 BETWEEN S22F AND S23R.SDR 97ZZZX1461Channel · crackedDURING C-10 INSPECTION, A CRACK WAS NOTED IN THE NOSE GEAR LOCK ACTUATOR CHANNEL.SDR 97ZZZX1458Stringer · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON STR 26L AT FS 328 UNDER FLOOR WEB.SDR 97ZZZX1465Skin · dentedDURING C-10 INSPECTION, A DENT WAS NOTED ON FUSELAGE EXTERNAL AT STA 1090 AT S18L AND S19L.SDR 97ZZZX1464Web · crackedDURING C-10 INSPECTION, A 3.50 INCH CRACK WAS NOTED IN FS 870 WEB, FORWARD SIDE OF LT MAIN WHEELWELL. REF: C53-100-01.SDR 97ZZZX1463Angle · crackedDURING C-10 INSPECTION, A CRACK WAS NOTED IN ANGLE BELOW AFT AIRSTAIR ACTUATOR SUPPORT FITTING AT FS 1273. REF: C53-137-01.SDR 97ZZZX1462Skin · damagedDURING C-10 INSPECTION, 6 EACH FASTENER HOLES FOUND KNIFE-EDGED THROUGH SKIN AT LAP SEAM, STA 344, S23R. REF: C53-100-01.SDR 97ZZZX1460T Chord · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON LOWER T-CHORD, FLOOR BEAM STA 1070 AT LBL 30.SDR 97ZZZX1459Seat Track · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON CABIN SEAT TRACK FROM STA 1030 TO STA 1110 AT LBL 40.SDR 97ZZZX1457Web · corodedDURING C-10 INSPECTION, CORROSION WAS NOTED AT L-2 DOOR FRAME CUT-OUT, LOWER AFT SIDE, STA 1070 AT S17L.SDR 97ZZZX1456Stringer · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED ON S23R AT STA 340.SDR 97ZZZX1455Skin · corrodedDURING C-10 INSPECTION, CORROSION WAS NOTED IN EXTERNAL SKIN AT FS 344 AT S24L.SDR 97ZZZM520Cowl · corrodedEXFOLIATED CORROSION ON NR 1 ENGINE FIXED COWL FORWARD SKIN. CORROSION BETWEEN HEAT SHILL AND SKIN. REMOVED FASTENERS AND SKIN. FABRICATED NEW SKIN FROM 2024-T3 .032 INCH 21.75 INCH BY 30.5 INCH. DRILLED, COUNTERSUNK AND DEBURRED. ALODINED AND PRIMED NEW SDR 97ZZZM515Control Valve · chafedNR 1 ENGINE STARTER CONTROL VALVE CHAFED AND COVER BROKE AT CORNERS. REMOVED AND REPLACED STARTER CONTROL VALVE IAW B727 80-11-11. LEAK CHECKED OK. LOG PAGE 6465.SDR 97ZZZM519Rib · crackedFIN STATION 35, STRINGER NR 4 SECOND BAY UP FROM THE BOTTOM, RIB CRACKED WITH PREVIOUS ANGLE REPAIR, STOP DRILL IS NET .25 INCH AND CRACKED ON FORWARD SIDE OF RIB RUNS TO THE SIDE OF STOP DRILL. CRACK RUNS PAST ANGLE DOUBLER RT SIDE OF VERTICAL STABILIZER. RSDR 97ZZZM523Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 520 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.SDR 97ZZZM522Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 420 L/E FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMITS.SDR 97ZZZM521Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RIGHT WING STATION 410.0 L/E FORWARD LOWER SPAR CAP CORRODED. MECH REMOVED CORROSION BOTTOM OF FORWARD CHORD AT RIGHT WING STATION 410 IAW B727 SRM 51-10-6. CORROSION REMOVAL WENT OUT OF LIMITSSDR 97ZZZM516Fitting · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND LT WING NR 5 SPOILER ACTUATOR FITTING IS CRACKED 2 PLACES. REMOVED AND REPLACED FITTING IAW SRM 51-30-2 AND 51-10-1. REMOVED AND REINSTALLED SPOILER PANEL TO FOM IAW MM 27-10-2. OPS CHECKED GOSDR 97ZZZM514Rib · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT WING STATION 738.5 LOWER RIB FLANGE IS CRACKED AT STRINGER NR 8 ATTACH POINT. STOP DRILLED CRACK IAW B 727 SRM 51-10-1. FABRICATED CHANNEL FROM 7075-0 .080 4 INCH BY 15 INCH IAW B727 SRM 57-SDR 97ZZZM511Spar · corrodedDURING SCHEDULED INSPECTION AT AERO COP IN LAKE CITY, FL, FOUND LT WING STATION 491.5 L/E SPAR AFT OF NR 4 SLAT ACTUATOR CORRODED APPROX 6 INCHES IN LENGTH. MECH REMOVED CORROSION AT WS 491.5 L/E SPAR IAW B727-SRM 51-10-6. REMOVED AT .091 METAL 14 INCHES ORISDR 97ZZZM510Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND LT WING STATION 383 L/E SPAR AT NR 4 SLAT FORWARD OF ACTUATOR ROD CORRODED APPROXIMATELY 18 INCHES IN LENGTH. MECH REMOVED CORROSION AT LEFT WING L/E SPAR IAW SRM 51-10-6. REMOVED AT .058 18 INCSDR 97ZZZM508Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RIGHT WING STATION 546.5 L/E SPAR CORRODED FORWARD OF NR 4 SLAT ACTUATOR ARM. FOUND TO BE IN LIMITS.SDR 97ZZZM507Spar · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 629, L/E SPAR CORRODED AT ACTUATOR ARM NR 7. FOUND TO BE IN LIMITS.SDR 97ZZZM505Fitting · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND NLG ACTUATOR ATTACH FITTING (AIRFRAME) CORRODED LT SIDE OUTBOARD. REMOVED NLG ATTACH FITTING FROM 2.799 TO 2.845. FABRICATED BUSHINGS TO 2.84700 (.002 INTERFENCE FIT). INSTALLED BUSHING WET WITSDR 97ZZZM503Spar Cap · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL FOUND RT WING STATION 738.5 LEFT FORWARD LOWER SPAR CAP CORRODED. FOUND TO BE IN LIMIT.SDR 97ZZZM504Cowl · crackedNR 3 ENGINE FIXED COWL FORWARD UPPER OUTER SKIN IS CRACKED 3 INCHES IN LENGTH 3H. REMOVED SECTION OF UPPER FORWARD OUTER SKIN 21 INCHES BY 1.3125 INCHES BY 11.25 INCHES FROM NR 3 ENGINE FIXED COWLING. FABRICATED NEW SECTION OF SKIN OUT OF 2024-T3 .032. DRILSDR 97ZZZM513Skin · corrodedRIGHT WING LEADING EDGE 5 SLAT HAS CORROSION UNDER PANEL SS128. MECH REMOVED CORROSION AND TR WING LEADING EDGE SPAR IAW SRM 51-10-6. REMOVED AT .088 METAL ORIGINAL THICKNESS .360 MATERIAL ALLOWABLE .012 OUT OF LIMIT IAW SRM 57-10-1. NO CRACKS NOTED BY EDDYSDR 97ZZZM512Skin · delaminatedON THE UPPER SURFACE T/E OF THE INBD MID-FLAP ON ITS OUTBD T/E THE FLAP HAS BECOME DELAMINATED. ALSO, AT TWO OTHER SMALLER SPOTS ON ITS MIDDLE T/E OF THE SAME FLAP. REMOVED LT INBD FLAP IAW MM 27-51-31. REMOVED DELAMINATED SKIN AND CRUSHED HONEYCOMB IAW SRMSDR 97ZZZM509Spar · corrodedWING STATION LEADING EDGE SPAR JUST FORWARD OF NR 2 SLAT ACT ROD HAS CORROSION AT 3 INCHES LONGERON. MECH REMOVED CORROSION AT WING STATION 616.5 LE SPAR IAW SRM 51-10-6. REMOVED AT .024 METAL 6 INCHES LONG ORIGINAL THICKNESS .225 MAX OUT ALLOWABLE .012 OUT SDR 97ZZZM506Skin · corrodedRIGHT WING UPPER LEFT END SKIN CORRODED AT MOUNT SCREWS FROM WS 170-760 FORWARD AND AFT CHORD. ACCOMPLISHED CORROSION REMOVAL ON RIGHT WING UPPER LT SPAR IAW SRM 51-10-6. INSTALLED TWO REPAIRS AT W/S NR 3 AND NR 4, 16 AND 18 BETWEEN W/S 190 AND 332. REPAIR SDR 97ZZZM517Skin · corrodedRIGHT WING OUTBOARD FLAP, THE AFT FLAP HAS A CORRODED AREA AT 9 FEET FROM THE OUTBOARD END. REMOVED CORROSION, REVEALED PUNCTURE HOLE IN FLAP FULL OF FILLER. CUT OUT CORRODED AREA. REQUIRES COMPOSITE REPAIR. CLEANED OUT OLD POTTING MATERIAL. PRIMED AREA ISDR 97ZZZM518Fitting · damagedREMOVED AND REPLACED LT NOSE GEAR FITTING PER B727 MM 32 AND S/B 727-53-0119R2 PART 3. REMOVED AND REPLACED LT NOSE GEAR FITTING PER B727 M32 AND SB 727-53. (M)SDR 96ZZZX5201Pitot Tube · blockedMIAMI - ON TAKEOFF ROLL, THERE WAS NO AIRSPEED INDICATION ON THE CAPTAIN'S AIRSPEED INDICATOR. DISCONNECTED PITOT PRESSURE LINE, APPLIED NITROGEN PRESSURE AND FOUND INSECTS (BEES) CLOGGING CAPTAIN'S PITOT TUBE. CLEARED AL INSECTS FROM CAPTAIN'S PITOT LINES, SDR 96ZZZX4866Hose · rupturedFLIGHT RETURN. LOST A-SYSTEM HYDRAULICS IN-FLIGHT DUE TO LOSS OF FLUID. FOUND NR 1 ENGINE HYDRAULIC CASE DRAIN LINE RUPTURED. THE PUMP AND CASE DRAIN LINE WERE BOTH REPLACED TO CORRECT PROBLEM.
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