Boeing 727-227
Service difficulty reports · 5,082
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 = '727227' 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 = '727227' 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 FDEA201206202280Web · crackedAFT AIR STAIR AREA FWD LT LIGHTNING HOLE CRACKED, BS 1227. CUT OUT DAMAGED AREA OF L/H AFT TORQUE BOX VERTICAL WEB STA 1227, FABRICATED, AND INSTALLED REPAIR DOUBLER IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1SDR FDEA201206192259Wire Harness · sparksNOTICED SPARKS COMING FROM WINDSHIELD HEAT SUPPLY WIRE NEXT TO CAPTAIN'S MIKE CONNECTOR. FOLLOWED QRH, PULLED WINDSHIELD HEAT C/B. REMOVED AND REPLACED WINDOW AND WIRE HARNESS IAW MM 56-12-011-4.SDR PCSA2012060501Engine · power lossDURING CLIMBOUT THE NR 2 ENGINE LOSS POWER.SDR FDEA201205302011Battery · dischargedESSENTIAL IN STANDBY POWER-EMERGENCY LIGHTS IN GALLEY AND FLIGHT DECK DO NOT ILLUMINATE. R & R EMERGENCY EXIT UNIT BATTERIES IAW AMM 33-56-01-2. OPS CK GOOD. ACFT OK FOR SERVICE.SDR FDEA201205261972Skin · dentedDENT IN SKIN AT BS 1129 S29L. CUT OUT DAMAGED AREA IAW SRM 53-30-3, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-30-3, FIG 1 AND SRM 53-30-2, FIG 2.SDR FDEA201205231941Skin · damagedSKIN DENTED AND GOUGED BS 1050 TO 1060 BETWEEN STRINGERS 26-28R. CUT OUT DAMAGED AREA IAW IAW SRM 53-30-3, FIG 1. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-30-3, FIG 1 AND SRM 51-30-2.SDR FDEA201205231945Shaft · wornMAIN ENTRY DOOR HARD TO SHUT FROM INSIDE AND NOT POSSIBLE TO CLOSE AND STORE HANDLE FROM OUTSIDE. FOUND ENTRY DOOR HANDLE SPLINE SHAFT WORN. R & R SHAFT IAW MM 52-11-001-5. OPS CHECKED GOOD.SDR FDEA201205221932Frame · crackedCRACK AT NR 1 CARGO DOOR AFT FRAME BS 620, S25R. CUT OUT DAMAGED AREA IAW SRM 51-40-3, FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-10-2, FIG 3 AND SRM 51-40-2, FIG 1.SDR FDEA201205221927Web · dentedDENT ON LT AIRSTAIR TORQUE BOX WEB AT BS 1313. DENT OUT OF LIMITS IAW SRM 53-10-1, FIG 1. CUT OUT DAMAGED AREA IAW SRM 51-40-02, FIG 1. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 51-40-02, FIG 1.SDR FDEA201205221920Stringer · damagedON REMOVAL OF DAMAGED STRINGER 28L FOUND SKIN CORRODED AT BS 585. CUT OUT DAMAGED SKIN IAW SRM 51-10-1 AND EA 7-5330-143992. FABRICATED FILLER, STRUCTURAL FILLER AND DOUBLER IAW SRM 53-30-3 FIG 3 AND EA 7-5330-143992. INSTALLED IAW SRM 51-30-2, 53-30-3 FIG SDR FDEA201205191887Frame · crackedSTATION 720 FRAME CRACKED AT SKIN ATTACH FASTENER HOLE BETWEEN STR 28L AND 27L. CUT OUT DAMAGED AREA IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-10-4, FIG 15 AND EA 7-5310-143991.SDR FDEA201205191886Stringer · corrodedCORROSION ON STRINGER 28L FROM BS 580 TO 600. CUT OUT CORRODED PORTION OF STRINGER IAW SRM 51-10-1. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. INSTALLED STRINGER REPAIR PARTS IAW SRM 51-30-2, REV 103.SDR FDEA201205191885Retainer · damagedESCAPE SLIDE GIRT BAR RETAINER CLIPS ON COVER DO NOT HOLD GIRT BAR. R & R ESCAPE SLIDE GIRT BAR RETAINER CLIPS ON COVER. REINSTALLED SLIDE IAW MM 25-60-015-2-0. MEL CLEARED.SDR FDEA201205081765Gauge · out of positionESCAPE SLIDE AIR BOTTLE PRESSURE GAUGE CAN NOT BE SEEN THROUGH COVER DOOR WINDOW. ADJUSTED ESCAPE SLIDE IN DOOR.SDR FDEA201205081764Switch · out of adjustON A TEST FLIGHT, AFT ENTRY DOOR LIGHT ON S/O PANEL COMES ON AFTER A NORMAL LANDING. ADJUSTED AFT ENTRY DOOR SWITCH TO ACTUATE AT APPROX 5 DEG OF HANDLE TRAVEL AND PERFORMED SATISFACTORY. OPS CHECKED IAW AMM 52-70-001-5.SDR FDEA201204251589Battery Pack · inoperativeDURING SERVICE CHECK, FOUND EXTERIOR EMERGENCY EVACUATION SLIDE LIGHT INOPERATIVE. REMOVED & REPLACED EMERGENCY ESCAPE SLIDE LIGHT BATTERY PACK ASSY. IAW MM 33-50-051-2-0. OPS CHECKED NORMAL.SDR FDEA201204251588Light · inoperativeMX PREFLIGHT REVEALED ENTRY DOOR O/H EMERGENCY LIGHT NOT ILLUMINATED DURING TEST. R & R FWD ENTRY DOOR EMERGENCY LIGHT ASSY AND BATTERIES. OPS CHECKED NORMAL REF MM 33-50-101-2-0. PREMATURE REMOVAL/INSTALLATION.SDR FDEA201204201503Hinge Fitting · crackedEXTERIOR FUSELAGE AFT MOST FUSELAGE MOUNTED MAIN CARGO DOOR HINGE SEGMENT HAS CORNER CRACKED SECOND LUG FWD OF AFT END VERIFIED WITH HFEC. REMOVED CRACKED HINGE IAW SRM 51-30-2. FABRICATED AND INSTALLED NEW HINGE IAW DWG 52FX1433 REV E AND SRM 51-30-2.SDR FDEA201204191492Floor Support · damagedMISDRILLED AND ELONGATED FASTENER HOLES IN FLOOR SUPPORT WEB BS 1148 TO 1183 BL0. AREA OUT OF LIMITS IAW SRM 53-10-1, FIG 1. REMOVED DAMAGED WEB, FABRICATED NEW AND INSTALLED IAW DWG 65-19606 AND SRM 51-30-2.SDR FDEA201204171451Stringer · corrodedCORROSION ON STRINGER 29L FROM BS 950E TO 950F. FABRICATED REPAIR STRAP AND SHIM IAW EA 7-5310-143984. INSTALLED REPAIR STRAP IAW EA 7-5310-143984 AND SRM 51-30-02 REV 103.SDR FDEA201204171453Seat Track · corrodedCORROSION AROUND FASTENER ON FLOATING SEAT TRACK SUPPORT ANGLE, BS 740 RBL 25. FOUND CORROSION OUT OF LIMITS IAW SRM 53-10-1, FIG 3. REMOVED DAMAGED SEAT TRACK IAW SRM 51-30-2 AMD MM 20-80-01-002. FABRICATED NEW SEAT TRACK SECTION IAW DWG 69-4121. INSTALLEDSDR FDEA201204131396Skin · dentedSKIN DENTED STA 238 ABOVE STR 24R. FOUND OUT OF LIMITS IAW SRM 53-30-1, FIG 1. CUT OUT DAMAGED AREA, FABRICATED REPAIR DOUBLER AND STRAP AND INSTALLED IAW SRM 53-30-3, FIG 1.SDR FDEA201204111364Shear Tie · corrodedCORROSION ON STUB FRAME SHEAR TIE AT BS 950E PLUS 4 INCHES, AFT SIDE, BETWEEN STRINGERS 29 AND 30R. REMOVED SHEAR TIE IAW SRM 51-30-02. FABRICATED NEW SHEAR TIE IAW DWG NR 65-56129 AND SRM 51-30-05 AND 51-20-1, FIG 7 & INSTALLED IAW SRM 51-30-02, REV 103.SDR FDEA201204111363Line · leakingTOTAL LOSS OF "A" SYS HYD QTY AND PRESSURE WHEN GEAR RETRACTED FOLLOWING TAKEOFF. ON POST FLIGHT DEBRIEF CREW REPORTED THAT WHEN THEY RETRACTED THE GEAR THEY LOST HYD FLUID AND PRESSURE AND THAT THEY HAD TO EXTEND THE GEAR MANUALLY. OPENED ACCESS PANEL 8505SDR FDEA201204101346Seat Track · corrodedMAIN CABIN SEAT TRACK CORRODED ON INBD FLANGE AT BS 1118, RBL 24.75. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED A NEW SECTION AND INSTALLED IAW SRM 53-10-5, FIG 1.SDR FDEA201204101348Seat Track · corrodedCORROSION ON SEAT TRACK BS 1130-1176 BL 0. CORROSION OUT OF LIMITS IAW SRM 53-10-1 FIG 3. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED NEW SECTION AND INSTALLED IAW SRM 53-10-2 FIG 7A, SRM 51-30-2 AND DWG 53FX939, REV F.SDR FDEA201204091331Stringer · corrodedCORRODED STRINGER 27L BS 700. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 51-10-1. FABRICATED NEW STRINGER SECTION AND 2 EACH STRINGER SPLICES IAW SRM 53-10-03 FIG 1. INSTALLED REPAIR IAW SRM 51-30-02 FIG 1 REV 103.SDR FDEA201204091327Skin · damagedEXTERIOR FUSELAGE BS 720A BELOW STR 15L HAS A PREVIOUS BLEND OUT. FOUND OUT OF LIMITS IAW IAW SRM 53-30-1 FIG 1, CUT OUT DAMAGED AREA, FABRICATED AND INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 53-30-3, FIG 3, SRM 53-30-2, FIG 2 AND SRM 51-30-2.SDR FDEA201204091336Web · damagedFOUND ELONGATED FASTENER HOLES IN AFT LOWER TORQUE BOX WEB BS 1323, LBL 17.5. WEB REPLACED.SDR FDEA201204051273Skin · gougedSKIN GOUGED BS 720D 10" STR 19L. REPAIRED IAW SRM 51-30-2, CUT OUT LOWER SKIN IAW SRM 53-30-3, FIG 5. FABRICATED NEW DOUBLER, STRUCTURAL FILLER AND FILLER IAW SRM 53-30-3, FIG 5. INSTALLED NEW DOUBLER, STRUCTURAL FILLER AND FILLER IAW SRM 53-30-3, FIG 5.SDR FDEA201204051272Skin · dentedDENT IN SKIN BS 490 ABOVE STRINGER 25R. CUT OUT DAMAGED AREA ON FUSELAGE SKIN IAW SRM 53-30-3, FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-30-01, FIG 1. INSTALLED REPAIR DOUBLER IAW SRM 51-30-02.SDR FDEA201204041250Seat Track · crackedCRACK ON SEAT TRACK SCALLOP BL 0 AT BS 1130. REMOVED DAMAGED SEAT TRACK IAW SRM 53-10-5, FIG 1. FABRICATED NEW SEAT TRACK AND INSTALLED IAW P-F SRM 53-10-5, FIG 1 AND SRM 53-10-5, FIG 1.SDR FDEA201204031240Web · crackedAFT AIRSTAIR AREA CRACKS IN WEB AT LT LOWER TORQUE BOX, BS 1323. REMOVED AFT WEB AT LT LOWER TORQUE BOX AND ATTACH ANGLES IAW SRM 51-30-2. FABRICATED NEW WEB IAW DWG 65-17510. INSTALLED NEW WEB AND ATTACH ANGLES IAW SRM 51-30-2.SDR FDEA201204031239Web · crackedAFT AIRSTAIR AREA LT LOWER TORQUE BOX WEB IS CRACKED AT PNEUMATIC LINE, STAND OFF BRACKET BS 1223. REPAIRED IAW SRM 51-40-02SDR FDEA201203231070Fitting · leakingNR 3 ENGINE SHUTDOWN DUE TO OIL QUANTITY LOSS, CRUISING AT FL 330. NR 3 OIL QUANTITY STARTED TO DECREASE APPROX 1 QT PER 2 MINUTES. AT FIRST INDICATION OF SECONDARY CONFIRMATION COMPLETED SHUTDOWN CHECKLIST AND DIVERTED. SHUTDOWN TO LANDING WINDMILL 15 MINSDR FDEA201203160985Cover · brokenAFTER BLOCK-IN AND OPENING MAIN ENTRY DOOR, FOUND EMERGENCY EXIT LIGHT ASSY ON FLOOR NEXT TO CREW MEAL BOX. INSPECTED PORTABLE EMERGENCY LIGHT ASSY FROM ABOVE THE MAIN ENTRY DOOR. FOUND LIGHT ASSY BENT AND WARPED. FOUND LIGHT LATCH LEVER LOCKING PINS SHEARESDR FDEA201203160979Battery Pack · looseEMERGENCY EXIT LIGHT ABOVE L1 ENTRY DOOR DOES NOT ILLUMINATE. FOUND BATTERY PACK FOR EMERGENCY EXIT L1 ENTRY DOOR LOOSE, REPOSITIONED EMERGENCY BATTERY PACK FOR L1 ENTRY DOOR, PERFORMED OPS CHECK IN REF AMM 33-50-101-2. OPS CHECKED OK. ACFT OK FOR SERVICE.SDR FDEA201203120905Battery Pack · inoperativeEMERGENCY LIGHTS INOPERATIVE WHEN ESS POWER SWITCHED TO STANDBY MODE AND EMERGENCY EXIT LIGHT SWITCHING TO ARM. PLACED SWITCH TO ON AND STILL LIGHTS DID NOT TURN ON . REPLACED BATTERIES IN EXIT LIGHTS. OPS CHECKED GOOD.SDR FDEA201202280709Slide · dislodgedON POST FLIGHT INSPECTION, FOUND L1 DOOR SLIDE COMING OUT AND COVER NOT SECURE. REINSTALLED DOOR SLIDE AND COVER IAW DOOR COVER PLACARD.SDR FDEA201201260351Slide · dislodgedTHE SLIDE WAS OUT OF ITS CONTAINER WHEN S/O ARRIVED FOR PREFLIGHT. REINSTALLED SLIDE ON L1 DOOR IAW MM REF 25-60-015-2-0. OK FOR FLIGHT.SDR FDEA201201200279Control Unit · failedAT ALTITUDE, RECEIVED WHEELWELL LIGHT & BELL, PERFORMED PHASE 1, LOWERED GEAR & OPENED MAIN GEAR DOORS, LIGHT REMAINED ON, ON TEST, BELL DID NOT SOUND. AFTER ACFT PULL IN THE GATE, INSPECTED WHEEL WELL TIRES AND BRAKES NO DISCREPANCY FOUND. INSPECTED FIRESDR FDEA201201190271Controller · malfunctionedPRIOR TO TAKEOFF, WHEEL WELL FIRE LIGHT AND BELL CAME ON INTERMITTENTLY APPROX 5 TIMES. AFTER WHICH WHEEL WELL FIRE WARNING WOULD NOT TEST. CHECKED MLG WW WIRING & SENSING ELEMENTS IAW WDM 26-12-01 & MM 26-12-001, ALL CHECKED GOOD. POWER & GROUND TO FIRE &SDR FDEA201201180273Light · dislodgedCOCKPIT EMERGENCY EXIT LIGHT FELL OUT OF POSITION IN TURBULENCE AFTER TAKEOFF. CHECKED MOUNTING BASE AND LIGHT ASSY, NO DEFECTS NOTED. REINSTALLED EMERGENCY EXIT LIGHT ASSY, OPS CHECKED GOOD MM 33-50-101-2.SDR FDEA201201180270Light · dislodgedCOCKPIT EMERGENCY EXIT LIGHT FELL OUT OF POSITION IN TURBULENCE AFTER TAKEOFF. CHECKED MOUNTING BASE AND LIGHT ASSY, NO DEFECTS NOTED. REINSTALLED EMERGENCY EXIT LIGHT ASSY,OPS CHECKED GOOD.SDR FDEA201201170208Controller · malfunctionedUPON LEVELING AT FL360, "CAB ALT" WARNING HORN SOUNDED. CAB ALT WAS 10,000' & CLIMBING. ACCOMPLISHED PHASE 1'S, RAN QRH, & WAS UNABLE TO REMEDY LACK OF PRESSURIZATION. ELECTED TO RETURN. CREW REPORTED DURING DEBRIEF THAT THEY COULD NOT CONTROL THE RT PACSDR FDEA201201170274Light · dislodgedEMERGENCY EXIT LIGHT ABOVE CABIN ENTRY DOOR FELL OUT OFF SOCKET. INSTALLED & SECURED CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY IAW MM 33-50-101-2. LIGHT OPS CHECKED GOOD.SDR CA120119013Switch · out of adjust(CAN) WHILE ENROUTE, THE MAIN CARGO DOOR WARNING LIGHTS ILLUMINATED IN FLIGHT DECK WITH AN ASSOCIATED AMBER, DOOR NOT CLOSED, LIGHT ILLUMINATED ON THE MCD CONTROL PANEL. CREW NOTED NO CHANGE IN PRESSURIZATION. ACFT DIVERTED. WHILE PASSING THROUGH FL260 THE SDR R5KB2012011446657Seat Track · corrodedRBL 46, SEAT TRACK CORRODED AT STA 1080-1090.SDR FDEA201201130142Sensor · failedDURING CRUISE FLIGHT WITH AUTOPILOT ELEVATOR SERVO "A" ENGAGED, ACFT HAD PITCH OSCILLATIONS GREATER THAN PLUS/MINUS 2 DEGREES INTERMITTENTLY. OSCILLATIONS SEEMED MORE PRONOUNCED DURING TURBULENCE OR WHEN ELEVATOR WAS LOADED IN A TURN. A/P SERVO INDICATOR SSDR R5KB2012010946570Seat Track · corrodedLBL 24, STA 1135, SEAT TRACK CORRODED.
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