Boeing 727-212
Service difficulty reports · 405
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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 = '727212' 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 = '727212' 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 R5KB15546Skin · dentedDENT IN SKIN STA 328 ABOVE FWD ENTRY DOORSDR I5P2008F00000Static Line · kinkedAC DEPARTED AT 1530L AND AIR RETURNED AT 1557L DUE TO CAPTS AND STANDBY A/S INDICATOR 40 TO 50 KNOTS LESS THAN COPILOTS (VERY SLOW TO RESPOND). UPON FURTHER TROUBLE SHOOTING, FOUND KINKED STATIC LINE BEHIND CAPTS VSI WHICH LINKS TO THE CAPT AND STANDBY A/S ISDR 2008003Engine · inoperativeON TAKEOFF, CREW EXPERIENCED A SLIGHT VIBRATION ON NR 3 ENGINE, VERIFIED ALL PARAMETERS NORMAL, CONTINUED WITH TAKEOFF CREW THEN NOTICED A LOSS OF OIL ON NR 3 ENGINE. SHUTDOWN ENGINE AND RETURN TO DEPARTURE. ON INSPECTION, FOUND BLADE DAMAGE, 2ND STAGE FAN BLSDR I5PA2008001Line · brokenAT FLIGHT LEVEL 30K FEET 263 NM OUT OF MAJURO, NR 1 OIL QUANTITY STARTED TO DECREASE FROM 4 GALLONS TO ZERO, CREW THEN SHUT DOWN ENGINE AND DESCENDED TO FL 26K FEET, RETURNED TO MAJURO. WINDMILLING OCCURRED FOR 43 MINUTES WITH OIL PRESSURE AT 17-18 PSI. ON ISDR C1HA200893001Flap System · malfunctionedUPON FLAP RETRACTION, THE INBOARD TRAILING EDGE LEFT WING REMAINED AT 1 DEG OF EXTENSION. COMPLIED WITH COM 2.27.16. DUMPED FUEL COM 228.4. INSPECTED INBD T/E FLAPS PER WO 123219, N/R'S 1 AND 2. NO DEFECTS NOTED. INBD FLAP IND WAS 1 NEEDLE OFF. REMOVED ANSDR C1HA200892001Skin · crackedFOUND CRACKED SKIN AND CORRODED STRINGER AT STA 1089 AT STR 28L. TRIMMED OUT DAMAGED TOP SKIN AND FABRICATED DOUBLER FROM 2024-T3 .060" AND INSTALLED PER SRM 53-30-3 FIG 3 CAT B. REPAIR MUST BE REINSPECTED AT 45000 CYCLES THRESHOLD STARTS AT DATE OF REPAIR. SDR 5700Stiffener · corrodedLEFT WING REAR SPAR VERTICAL STIFFENER CORRODED AT LOWER END W.S. 200SDR C1HA200792002Connector · brokenAFTER GEAR RETRACTION RED GEAR LIGHT FOR NOSE GEAR REMAINED ILLUMINATED REFORMED COM 2.32.22 LIGHT REMAINED ON. REPLACED BOTH NOSE GEAR DOWN LOCK AND GEAR POSITION SWITCHES SWING NOSE GEAR OPS CK NORMAL MM 32-61-71 MM 7-11-00 MM 32-61-01. CONNECTOR D298 NLG SDR C1HA200792001Switch · defectiveAT FL 250 CABIN PRESS STARTED CLIMBING AT 100FT PER MIN PERFORMED COM 2.21.16 UNABLE TO STOP CLIMB. STARTED DESCENT, CABIN WOULD NOT HOLD PRESSURE UNTIL PASSING 17,000 FT CABIN ALT PEAKED AT 9,000 FT RETURNED TO CUN. REMOVED DEFECTIVE PACK SWITCH FOR RT PACKSDR C1HA200793006Stringer · corrodedAFT CARGO COMPT BS 1160 STR 30 AND SPLICE REPAIR CORRODED. REPAIRED STR 30 AT BS 1160 IAW B727 SRM 53-10-3 FIG 1.SDR C1HA200793005Sill · corrodedC2 - DOOR SILL ON FUSELAGE FRAME HAS CORROSION. REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5314-02SDR C1HA200793004Stringer · corrodedFOUND CORROSION ON STR 27L AT BS 737 FWD PIT. REPAIRED AREA AS REQUIRED IAW CHAMPION AIR EO 727-5331-18.SDR C1HA200793003Web · corrodedNOSE WHEEL WELL HAS WEB CORRODED BEHIND NLG LOCK ACTUATOR SUPPORT BRACKET AT BS 351.2. REPAIRED NWW WEB AT BS 351.2 IAW B727 SRM 51-40-2 FIG 1 AND 53-10-2 FIG 1.SDR C1HA200793002Stringer · corrodedFOUND CORROSION ON STR 27R AT BS 737 FWD PIT. REPAIRED STR 27R AT BS 737 - 740 IAW B727 SRM 53-10-3 FIG 1.SDR C1HA200793001Shear Tie · corrodedFOUND CORROSION AT SHEAR TIE AT BS 380 I/B OF STR 28L. REMOVED CORROSION FOUND OUT OF LIMITS FAB DOUBLER REPAIR AND INSTALLED IAW B727 SRM 53-10-4 FIG 13.SDR PCSA10420071Compressor · damagedFLIGHT 743 DURING THE TAKEOFF ROLL FROM MIA THE CREW EXPERIENCED A VIBRATION ON THE NUMBER 3 ENGINE, THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED BACK TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE NR 3 ENGINE AND FOUND THE C-2 COMPRSDR PCSA111706SUPOil Filter · bypassingFLIGHT 858 DEPARTED MAR AND DURING THE CLIMB THE CREW REPORTED THE NR 1 ENGINE LOW OIL FILTER BYPASS LIGHT ILLUMINATED, THE CREW ACCOMPLISHED COMPANY ALTERNATE PROCEDURES, THE NR 1 ENGINE WAS SHUT DOWN AS A PRECAUTIONARY. THE AIRCRAFT RETURNED TO MAR WITHOUT SDR C1HA200692004Duct · leakingAFTER ROTATION ENG 1 BLEED AIR TRIP OFF LIGHT ILLUMINATED. CREW PERFORMED COM 2.36.2 APPROX 1 OR 2 MINS AFTER COMPLETION OF COM PROCEDURE FOR ITEM 1, NR 1 ENG STRUT OVERHEAT LIGHT ILLUMINATED. CREW RAN COM 2.36.9 CONTACTED DISPATCH. FOUND 13TH STAGE SADDLE SDR PCSA7140601Actuator · corrodedTHE NOSE LANDING GEAR MANUAL EXTENSION INBOARD & OUTBOARD SHAFT SEGMENTS WERE FOUND TO HAVE CORROSION, THE DRAG BRACE PIN & FITTING & THE TRANSFER CYLINDER WERE FOUND TO HAVE CORROSION. THE NOSE LANDING GEAR DEFECTIVE COMPONENTS WERE REMOVED AND REPLACED IAW SDR PCSA6130601Compressor · stalledFLIGHT 721 PREPARED TO TAKEOFF FROM MIA; THE CREW REPORTED NR 2 ENGINE COMPRESSOR STALLING AS POWER WAS APPLIED. THE TAKEOFF WAS ABORTED AND THE AIRCRAFT RETURNED TO THE BLOCK. AMERIJET MAINTENANCE ACCOMPLISHED AN ENGINE RUN ON NR 2 ENGINE AND WAS ABLE TO DUSDR PCSA05190601Handle · damagedFLIGHT 741 DEPARTED MIA THE CREW REPORTED DURING CLIMB ON GEAR RETRACTION THE LEFT GEAR DOOR AMBER LIGHT CAME ON, AMERIJET PROCEDURES WERE FOLLOWED AND THE AIRCRAFT RETURNED BACK TO MIA WITHOUT ANY FURTHER INCIDENT. MIA MAINTENANCE TROUBLESHOT THE GEAR LIGHT SDR C1HA200692003Warning Light · illuminatedDURING CLIMBOUT AT 12-13,000 FT THE NR 3 OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED COM 2-72-19 ; 2-72-12 ; 2-28-4. RETURNED TO MMMZ. ALL ENGINE PARAMETERS NORMAL PRIOR TO SHUTDOWN OF NR 3 INFLIGHT. WINDMILLED ENGINE N 12 MINS. OIL PRESS +20 PSI. EMESDR C1HA200692002Actuator · dirtyAFTER TAKEOFF TAIL SKID LIGHT REMIND ILLUMINATED FOLLOWED COM PROCEDURES DUMPED 26.2 FUEL RETURNED FOR LANDING IN ZIH. CLEANED ROLLER ACTUATOR ON BOTH SWITCHES. TESTED TAIL SKID NUMEROUS TIMES IAW 32-71-01, NO DEFECTS NOTED, OK FOR SERVICE.SDR PCSA03030601Switch · false indicationFLIGHT 859 DEPARTED MIA THE CREW REPORTED DURING CLIMB THE NUMBER 3 LEADING EDGE FLAP IN TRANSIT LIGHT STAYED ON AFTER THE FLAPS WERE RETRACTED ON THE FLIGHT ENGINEERS FLAP PANEL LIGHT, AND THE FORWARD PANEL LIGHT. THE AIRCRAFT RETURNED BACK TO MIA AND LANDEDSDR PCSA01310601Nut · looseKMIA-MDSD FLIGHT 871 - CREW REPORTED APPROXIMATELY 20 MINUTES INTO CRUISE, NR 1 ENGINE EGT, N1 AND N2 RAPIDLY APPROACHED THEIR LIMITS. ENGINE NR 1 WAS SHUTDOWN PER AOM. ENGINE WINDMILLED FOR 50 MINUTES AND ENGINE OIL PRESSURE AT 25 PSI DURING WINDMILLING. A/CSDR C1HA200692001Engine · failedON INITIAL CLIMB OUT, AFTER FLAPS UP AND SETTING CLIMB POWER NR 3 ENGINE (BANGED) AND ENGINE GAUGES FLUCTUATED AND AIRCRAFT YAWED. NO FIRE WARNING, NO BOOST PUMP LIGHTS, OIL PRESSURE NORMAL, IGNITION ON, ENGINE ANTI ICE OFF, EPR FLUCTUATED, ENGINE DID NOT OVESDR C1HA200593005Attach Angle · crackedWHILE PERFORMING AD 2005-19-24, FOUND NR 1 ENG PYLON CORD ANGLE CRACKED FWD PYLON FIREWALL P/N 69-16977-1. REMOVED CRACKED ATTACH ANGLE AND INSTALLED NEW ATTACH ANGLE 69-16977-1 REF BAC BWG 65-72772.SDR PCSA12070502Adc · failedFLIGHT 8216 DURING TAKEOFF FROM CUR CREW REPORTED CAPTAIN'S AIRSPEED INDICATION SHOWED NO AIRSPEED INDICATION, THE F/O'S AIRSPEED INDICATOR WAS SHOWING 80 KNOTS, CREW ABORTED THE TAKEOFF AND RETURNED TO THE BLOCK WITHOUT ANY FURTHER INCIDENT. MAINTENANCE TROUSDR PCSA11250501Fuel Heater · failedAT TOP OF DESCENT NR 2 ENGINE OIL TEMP BEGAN TO RISE, NR 2 FUEL HEAT VALVE WAS STUCK OPEN. NR 2 ENGINE FUEL HEAT VALVE WAS CYCLED, BUT WOULD NOT CLOSE, OIL TEMP WENT INTO RED 175 DEG, COULD NOT BE DECREASED, OIL PRESSURE NORMAL. DURING NORMAL ATTEMPT TO SHUTSDR PCSA11030501Engine · vibrationWHILE IN CRUISE, CREW REPORTED VIBRATION ON THE CENTER CONSOLE, WHEN NR 1 ENGINE THROTTLE WAS PULLED BACK VIBRATION SEEMS TO DIMINISH. AIRCRAFT RETURNED AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE INSPECTED ALL 3 ENGINES, INTAKES, AND EXHAUST, NO DAMAGE FSDR MYW2006F00000Wire · burnedDURING FLIGHT, ALL 8 RT READING STATION CB`S POPPED SIMULTANEOUSLY. PA INOPERATIVE ALL STATIONS. NO SMOKING CB POPPED, PASSENGER AND CREW CALL CB POPPED. ATTEMPTED TO RESET CB`S IAW AOM PROCEDURES. CB`S IMMEDIATELY POPPED. DID NOT ATTEMPT TO RESET, AGAIN.SDR C1HA200592004Trunnion · corrodedNOSE LANDING GEAR TRUNNION CAPS CORRODED, LEFT AND RIGHT. REMOVED CORROSION ON LT TRUNNION FITTING TO A FINAL BORE DIAMETER OF 2.602" AND RT 2.727" AND WITHIN LIMITS IN ACCORDANCE WITH 727 SRM 53-40-01, FIGURE 2. REWORKED AREAS TREATED AND PRIMED IN ACCORDANSDR C1HA200592003Pump · failedNR 2 B PUMP FAILED INFLIGHT, REPLACED NR 2 B HYD PUMP, CASE DRAIN AND PRESSURE FILTER, OP'S CHECK GOOD. LEAK CK GOOD REF MM 29-12-3.SDR PCSA7060501Adc · false indicationON TAKEOFF ROLL, CAPT AIRSPEED INDICATOR WENT TO 300 KNOTS AT AROUND 60 KNOTS INDICATED. CREW ABORTED TAKEOFF AND RETURNED TO BLOCKS. NO FURTHER INCIDENT REPORTED. MAINTENANCE INSPECTED AIRSPEED INDICATION AND FOUND SYSTEM ENCOUNTERED A GLICK FROM NR 1 AIR SDR C1HA200592002Actuator · failedON DEPARTURE THE NR 6 L/E FAILED TO RETRACT, COMPLIED WITH COM PROCEDURE 2.27.12 SLAT WAS STILL EXTENDED. CONFERRED WITH DISPATCH/MDC, DECLARED AN EMERGENCY. COMPLIED WITH COM PROCEDURE 2.28.4 AND DUMPED APPROXIMATELY 23K LBS FUEL BEFORE RETURN TO STL. REMOSDR C1HA200593004Power Lever · out of rigUPON APPLICATION OF T/O THRUST, NR 3 ENGINE POWER LEVER TO FORWARD STOP AND EPR ONLY 2.05 FULL T/O EPR = 2.13 T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER ENGINE PARAMETERS IN YELLOW BAND FOR NR 3, PERFORMED STATIC RIG CHECK IAW MSDR C1HA200593003Rod · out of adjustUPON APPLICATION OF FULL T/O THRUST NR 3 ENGINE POWER LEVER WENT TO FORWARD STOP AND EPR ONLY 2.00 (T/O EPR 2.09) T/O ABORTED IAW CHAMPION PROCEDURES. SOC, MX CONTROL NOTIFIED. ALL OTHER PARAMETERS IN YELLOW BAND FOR NR 3, NR 3 ENGINE INTAKE AND EXHAUST INSPSDR PCSA04270501Proximity Switch · out of adjustFLIGHT 881 DEPARTED MIA DURING CLIMBOUT CREW REPORTED AMBER LEADING EDGE FLAP INTRANSIT LIGHT REMAINED ILLUMINATED ON CAPTAINS FWD PANEL, CREW VERIFIED INDICATION ON FLIGHT ENGINEERS PANEL NR 3 LEADING EDGE FLAP INTRANSIT LIGHT ON. AIRCRAFT RETURNED BACK TO MSDR PCSA04260501Outflow Valve · intermittentFLIGHT 710 MID-MIA, DURING CLIMBOUT CREW REPORTED PRESSURIZATION OUTFLOW VALVE WOULD NOT CLOSE IN ANY MODE IN FLIGHT ON DEPARTURE FROM MID. AIRCRAFT RETURNED BACK TO MID WITH NO FURTHER INCIDENT. MAINTENANCE ACCOMPLISHED A PRESSURIZATION CONTROL SYSTEM TEST SDR PCSA05041401Housing · strippedFLT 8414 ON APPROACH TO MIA CREW REPORTED NR 1 ENGINE LOST OIL, ENG. NR 1 WAS SHUTDOWN AS A PRECAUTION. A/C LANDED AT INTENDED DESTINATION WITHOUT FURTHER INCIDENT. MX INSPECTION OF THE NR 1 ENGINE FOUND OIL FILTER & GEARBOX CHIP DETECTORS HAD NO METAL, INSPECSDR C1HA200593002Engine · overtempON TAKEOFF AFTER V1 THE NUMBER 1 ENGINE HAD SEVERE FLUCTUATIONS IN ALL INSTRUMENTS WITH VIBRATIONS ON NUMBER ONE SIDE. HEARD THREE LOUD POPS NR 1 EGT WENT TO 700 DEGREES C, THREE DIFFERENT TIMES IN RAPID SUCCESSION. DUMPED FUEL RETURNED FOR LANDING. FOLLOWESDR C1HA200593001Wire · shortedAFTER T/O RED NOSE GEAR LIGHT ILLUMINATED FOLLOWED BY NOSE GEAR LIGHT (GREEN). RAN COM 2.32,23 SUCCESSFULLY BOTH LIGHTS REMAINED ILLUMINATED ENTIRE FLT. ALSO RAN 2.28.4 (FUEL DUMPING PROCEDURE) FOUND WIRE W1386-023-20 SHORTED TO CONDUIT IN NOSE WHEEL WELL ATSDR PCS2005F00001Controller · intermittentCREW REPORTED AC WILL NOT PRESSURIZE, OUTFLOW VALVE WILL NOT OPERATE IN ANY MODE. AC RETURNED TO DEPARTURE AND LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT PRESSURIZATION AND RERACKED THE CABIN PRESSURE CONTROLLER AND ACCOMPLISHED A FUNCTIONAL TEST OF THSDR 2005F00063Sight Glass · missingFLT - 711 - MIA-MEX - CREW REPORTED UNABLE TO PRESSURIZE IN FLIGHT, DUMPED FUEL AND RETURNED TO MIA. FOUND RIGHT MAIN GEAR DOWNLOCK VIEWING WINDOW MISSING, INSTALLED VIEWING WINDOW (P/N 66-16515-1), REPLACED SEAL (P/N 66-16514-1) AND CLIPS (P/N 66-14269-1) PESDR C1HA200493024Floorbeam · corrodedAFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1090 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED FRAME REPAIR, EA-05-53, MINOR.SDR C1HA200493025Floorbeam · corrodedAFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1070 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED REPAIR STRAP PER EA 10700, MAJOR.SDR C1HA200493023Floorbeam · corrodedAFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1148 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX WAS REMOVED. INSTALLED REPAIR STRAP, EA-10720, MAJOR.SDR C1HA200493022Floorbeam · corrodedAFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1130 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED. INSTALLED REPAIR STRAP, EA-10703, MAJOR.SDR C1HA200493020Floorbeam · corrodedAFT PIT LOWER SIDE OF CABIN FLOORBEAM STA 1110 FROM LBL 60 TO RBL 60 CORRODED NUMEROUS PLACES WHERE RUBITEX TAPE WAS REMOVED, EA-10705, MAJOR.SDR C1HA200493019Floorbeam · corrodedCABIN FLOORBEAM STA 1160 LBL 20 TO RBL 20 CORRODED TOP SIDE EA-10698, MAJOR.
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