Boeing 727-2F9
Service difficulty reports · 219
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 = '7272F9' 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 = '7272F9' 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 PCSA2011082530Beam · corrodedRIGHT HORIZONTAL STABILIZER TRAILING EDGE LOWER BEAM ELEVATOR STATION 17.20-209.96 CORRODED. REPLACED BEAM SECTION.SDR PCSA2011082529Beam · corrodedRIGHT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM ELEVATOR STATION 17.20-209.96 CORRODED. REPLACED BEAM SECTION.SDR PCSA2011082528Beam · corrodedLEFT HORIZONTAL STABILIZER TRAILING EDGE UPPER BEAM ELEVATOR STATION 17.20-39.50 CORRODED. REPAIRED WITH DOUBLER.SDR PCSA2011082527Floorbeam · corrodedFLOORBEAM LOWER CHORD BS 720 LBL 55 RBL 57 EXISTING REPAIR CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082526Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 1110 LBL 70 RBL 70 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082525Floorbeam · corrodedFLOORBEAM LOWER CHORD BS 970 RBL 23 RBL 44 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082524Floorbeam · corrodedFLOOR BEAM UPPER CHORD BS 1130 LBL 24 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082523Support Angle · corrodedPRESSURE SEAL RETAINER SUPPORT ANGLE BS 870 LBL 62-RBL 62 CORRODED. REPLACED SUPPORT ANGLES.SDR PCSA2011082522Support Angle · corrodedPRESSURE SEAL RETAINER SUPPORT ANGLE BS 870 LBL 62-RBL 62 CORRODED. REPLACED SUPPORT ANGLES.SDR PCSA2011082522AFloorbeam · corrodedFLOORBEAM UPPER CHORD BS 950E RBL 8-RBL 47 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082521Floorbeam · corrodedFLOOR BEAM UPPER CHORD BS720A LBL 18.5-LBL 30.5 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082520Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 620 LBL 18-RBL 45 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082519Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 620 LBL 18-RBL 45 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082518Floorbeam · corrodedFLOORBEAM UPPER CHORD BS 540 LBL 27-LBL 43 CORRODED. REPLACED FLOORBEAM SECTION.SDR PCSA2011082517Skin · damagedFUSELAGE SKIN FORWARD ENTRY DOOR LOWER HINGE CUTOUT. REPAIRED TO SATISFY AD2007-12-14.SDR PCSA2011082516Skin · damagedFUSELAGE SKIN FORWARD ENTRY DOOR UPPER HINGE CUTOUT. REPAIRED TO SATISFY AD2007-12-14.SDR PCSA2011082515Frame · dentedFUSELAGE FRAME BS 380 S5R-S7R DENTED. REPLACED FRAME SECTION.SDR PCSA2011082514Stringer · corrodedFUSELAGE STRINGER 12R BS 312-BS 328 CORRODED. REPLACED STRINGER SECTION.SDR PCSA2011082513Frame · dentedFUSELAGE FRAME BS 440 S15L-S17L DENTED. REPLACED DENTED FRAME SECTION.SDR PCSA2011082512Frame · dentedFUSELAGE FRAME BS 420 S15L-S17L DENTED. REPLACED DENTED FRAME SECTIONSDR PCSA2011082511Frame · dentedFUSELAGE FRAME BS 360 S15L-S17L DENTED. REPLACED DENTED FRAME SECTION.SDR PCSA2011082510Frame · damagedFUSELAGE FRAME BS 360 S3L-S9L DAMAGED. REPLACED DAMAGED FRAME SECTION.SDR PCSA2011082509Skin · damagedFORWARD GALLEY DOOR SKIN LOWER AFT JAMB BS 400-BS 430 S15R DAMAGED. REPAIRED WITH EXTERNAL DOUBLERSDR PCSA2011082508Skin · corrodedFUSELAGE SKIN BETWEEN BS 1030-BS 1110 S27L-S26R CORRODED. REPAIRED WITH EXTERNAL DOUBLER.SDR PCSA2011082507Frame · corrodedFRAME ST BS 1110 S24L-S28L CORRODED. REPLACED FRAME SECTION.SDR PCSA2011082506Frame · dentedFRAME REPAIR AT BS 580 S20L-S26L DENTED. REPLACED FRAME SECTION.SDR PCSA2011082505Frame · dentedFRAME REPAIR AT BS 560 S20L-S26L DENTED. REPLACED FRAME SECTION.SDR PCSA2011082504Frame · dentedFRAME REPAIR AT BS 520 S20L-S26L DENTED. REPLACED FRAME SECTION.SDR PCSA2011082503Stringer · corrodedSTRINGER S29L BS 1051-BS 1115 CORRODED. REPLACED DAMAGED STRINGER SECTION.SDR PCSA2011082502Stringer · corrodedSTRINGER S27R BS 1053-BS 1086.5 CORRODED. REPLACED DAMAGED STRINGER SECTION.SDR PCSA2011082501Angle · damagedFRAME REINFORCEMENT ANGLE BS 1130 S27L-S27R DAMAGED. REPLACED DAMAGED SECTION.SDR PCSA2009111701Shim · damagedENGINE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED CLIMBING THROUGH FL260. THE STRUT OVERHEAT PROCEDURE WAS ACCOMPLISHED IAW THE AOM AND THE LIGHT EXTINGUISHED. MAINTENANCE REPLACED THE DAMAGED 6TH STAGE DUCT SHIMS AND THE OVERHEAT DETECTION ELEMENT, RETORQUED THESDR PCSA2009111501Modulating Valve · leakingDURING CLIMBOUT PASSING 28000 FEET ENGINE 1 ENG STRUT OVERHEAT ILLUMINATED. ACCOMPLISHED ABNORMAL PROCEDURE, NO FURTHER OCCURRENCE. MAINTENANCE FOUND ENGINE 1 HIGH PRESSURE MODULATING VALVE LEAKING, REPLACED THE VALVE IAW THE B727 AMM, PERFORMED A LEAK CHECKSDR PCSA2009072201Clamp · leakingIN CLIMBOUT OF POS NR 1 STRUT OVERHEAT LIGHT ILLUMINATED IN FLT, EXTINGUISHED WHEN THROTTLE BROUGHT BACK TO IDLE. FLT 82320 WAS CANCELLED UPON RETURN TO POS. MAINTENANCE REMOVED AND REPLACED FWD CLAMP AT NR 1 ENGINE BLEED VALVE. RAN ENGINE TO TAKEOFF POWER SDR PCSA2009072002Clamp · looseIN FLIGHT FROM GND TO GEO - NR 1 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED AT CRUISE. THROTTLE BROUGHT TO IDLE, LIGHT EXTINGUISHED. THE FLIGHT DIVERTED TO POS. MAINTENANCE DISCOVERED A LOOSE CLAMP ON THE NR 1 STRUT PRECOOLER DUCT. THE CLAMP WAS RETORQUED ANDSDR PCSA2008111101Transmitter · failedON DESCENT IN SDQ OIL QUANTITY GAUGE NR 3 BLED SLOWLY DOWN TO ZERO QUANTITY. OIL PRESSURE AND TEMPERATURE NORMAL BUT WERE VERY LIGHT SO A PRECAUTIONARY ENGINE SHUTDOWN WAS DONE. A NORMAL LANDING WAS PERFORMED. AFTER LANDING OIL QUANTITY CHECKED FULL. ENGINSDR 706200701Engine · damagedFLIGHT 743 DEPARTED, WHEN THE CREW REPORTED, DURING CLIMBOUT, THE NR 3 ENGINE STARTED TO VIBRATE ABOUT FL340, ENGINE INDICATIONS WERE ERRATIC, NR 3 FUEL QTY GAUGE SHOWED 1700 LBS. DIFFERENCE WITH NR 1 FUEL TANK, THEN NR 3 ENGINE FLAMED OUT. THE CREW ACCOMPLISHSDR 0607200701Duct Clamp · looseFLIGHT 845 DEPARTED MIA AND CLIMBED TO CRUISE ALTITUDE, THE CREW REPORTED THE NR 1 STRUT OVERHEAT LIGHT ILLUMINATED, THE AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. IN MIA MAINTENANCE FOUND A LOOSE CLAMP AT THE NR 1 ENGINE BLEED VALVE, THE CSDR PCSA2062007SUCompressor · damagedFLIGHT 713 ABORTED THE TAKEOFF AFTER THE FLIGHT CREW EXPERIENCED A VIBRATION COMING FROM THE NR 1 ENGINE, THE AIRCRAFT RETURNED TO THE GATE WITHOUT ANY FURTHER INCIDENT. MAINTENANCE INSPECTED THE ENGINES AND FOUND THE NR 1 ENGINE SHOWING EVIDENCE OF DAMAGE TOSDR PCSA12070601Actuator · failedFLIGHT 8413 DEPARTED MIA AND DURING THE CLIMB THE CREW REPORTED THE NOSE LANDING GEAR DID NOT RETRACT WITH THE GEAR LEVER IN THE UP POSITION, THE COCKPIT INDICATION SHOWED THE RED NOSE LANDING GEAR LIGHT AND THE GREEN NOSE LANDING GEAR LIGHT REMAINED ILLUMINATSDR PCSA1016061SUSwitch · malfunctionedABORTED TAKEOFF AT 135 KTS. ENGINE FAIL LIGHTS CAME ON, ALL PARAMETERS WORKED NORMAL. TRANSFERRED AUTO PACK TRIP SYSTEM TO DMI 14808. A HIGH ENERGY STOP CONDITION INSPECTION WAS PERFORMED. NO DISCREPANCIES WERE NOTED. SUPPLEMENTAL ADD ON INFO, FOLLOW-UP RSDR PCSA07120601Engine · leakingFLIGHT 8315 DURING THE DESCENT, 25 MINUTES OUT, THE CREW REPORTED NR 2 ENGINE QUANTITY INDICATION WENT TO (0) AND NR 2 ENGINE OIL PRESSURE WENT TO (0), THE CREW REPORTED THE NR 2 ENGINE WINDMILLED FOR 25 MINUTES AT 6-10 PSI. THE AIRCRAFT LANDED WITHOUT FURTHERSDR PCSA022401Annunciator · malfunctionedAFTER TAKEOFF HAD TAIL SKID LIGHT AND RIGHT GEAR DOOR INDICATION WITH HANDLE OFF HAD GEAR GREEN LIGHT ON. AIRCRAFT RETURN TO MIA AND LANDED WITH NO INCIDENT. MAINTENANCE PERFORMED JACKED AIRCRAFT IAW B727 MM 07-11-0. PERFORMED EXTENSION AND RETRACTION OPERASDR PCSA12070501Compressor · stalledFLIGHT 723 DEPARTED MIA AND CLIMBED TO 34,000 FT CRUISE ALTITUDE, CREW REPORTED NUMBER 2 ENG COMPRESSOR STALLED, POWER WAS REDUCED AND NR 2 ENG CONTINUED TO COMPRESSOR STALL. THE CREW PERFORMED A PRECAUTIONARY ENGINE SHUTDOWN, ALL FLIGHT CONDITIONS WERE NORMASDR PCSA11040501Adi · spinningFLT 8419 AFTER DEPARTURE FROM MIA AND WHILE IN CRUISE THE CREW REPORTED CAPTAINS VG ATTITUDE FLAG IN VIEW CONTINUOUSLY AND RAPID SPINNING OF THE ADI TO THE RIGHT, AUX VG SELECTION AND C/B RESET, NO HELP. AIRCRAFT RETURNED BACK TO MIA AND LANDED WITHOUT ANY FUSDR PCSA10120501Engine · overheatedAFTER DEPARTURE ENGINE NR 3 OIL TEMPERTURE INCREASED TO 160, PERFORMED ALTERNATE PROCEDURE, NO HELP. SHUT DOWN ENGINE, DUMPED FUEL TO LAND. MX INSPECTED INLET & EXHAUST OF NR 3 ENGINE; INLET OK, EXHAUST SHOWS EVIDENCE OF OIL LEAK, SUSPECT NR 6 BEARING SEAL. SDR PCSA10100501Controller · malfunctionedFLIGHT 751 MIA TO MEX CREW REPORTED, PRESSURIZATION WOULD NOT LEVEL OFF ON CLIMBOUT, JETTISONED FUEL BELOW LANDING WEIGHT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND FLOW CONTROL VALVE NOT OPERATING PROPERLY. REMOVED ANDSDR PCSA09170501Controller · malfunctionedFLIGHT 857 DURING CLIMBOUT FROM MIA FLIGHT CREW REPORTED AIRCRAFT WOULD NOT PRESSURIZE & IT SEEMED BOTH PACKS WERE NOT WORKING AT ALL. AIRCRAFT RETURNED TO MIA & LANDED WITHOUT ANY FURTHER INCIDENT. MAINTENANCE CHECKED BOTH LEFT & RIGHT PACKS IAW B-727 MM CHSDR 07260501Controller · misoverhauledFLIGHT 711 KMIA/MMMX, DURING CLIMB AUTO PRESSURIZATION FAILED, WENT TO STANDBY, OUTFLOW VALVE WENT FULL OPEN. UNABLE TO HOLD CABIN PRESSURE IN MANUAL AC OR DC. AIRCRAFT RETURNED TO KMIA AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND CABIN PRESSURE CONTSDR PCS2005F00002O-Ring · leakingCREW REPORTED NR2 ENG OIL QUANTITY DROPPED IN FLIGHT, THEN ENGINE OIL PRESSURE DROPPED, THEN OIL TEMP ROSE. CREW SHUTDOWN NR2 ENGINE AND AC RETURNED TO DEPARTURE, AC LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND NR2 ENGINE GEARBOX LEAKING OIL FROM THE F
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