Boeing 727-222
Service difficulty reports · 1,723
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 = '727222' 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 = '727222' 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 GAIA04160Beam · crackedDURING C-CHECK INSPECTION FOUND AFT CABIN VERTICAL BEAM BS 1183, LBL24 INCH, WL 269, CRACKED. REF FASI NR 86945 INSTALLED REPAIR KIT 65C33556-41 IAW SB 727-53-0182, REV 1.SDR GAIA04159Skin · bulgedDURING C-CHECK INSPECTION FOUND C-2 DOOR SKIN BULGE IN LOWER SECTION. REF FASI NR 86950, INSTALLED SKIN REPAIR DOUBLER IAW SRM 52-00-3.SDR GAIA04158Stringer · dentedDURING C-CHECK INSPECTION FOUND STRINGER 21 RT AT BS 410, DENTED. REF FASI NR 86948, ACCOMPLISHED STRINGER REPAIR IAW SRM 53-10-2, FIG 2.SDR GAIA04157Pressure Panel · crackedDURING C-CHECK INSPECTION FOUND ELECT. COMPARTMENT BS 288, LBL24, PRESSURE WEB FOR NOSE WW CRACKED. REF FASI NR 86933, INSTALLED DOUBLER REPAIR IAW SRM 53-10-2, FIG 1.SDR GAIA04156Skin · crackedDURING C-CHECK INSPECTION, FOUND L-1 DOOR EXTERIOR SKIN AFT UPPER CORNER BENT. REF FASI NR 86903 REWORKED SKIN TO ORIGINAL CONTOUR, FOUND SKIN CRACKED, INSTALLED DOUBLER REPAIR IAW SRM 52-10-2, FIG 1.SDR GAIA04155Skin · dentedDURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED, STA 1303, LT SIDE. REF FASI NR 86890 ACCOMPLISHED DOUBLER REPAIR IAW SRM 53-30-3.SDR GAIA04154Skin · crackedDURING C-CHECK INSPECTION, FOUND RT WING L/E AT NR 5 SLAT GUIDE CUTOUT CRACKED. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4.SDR GAIA04153Floorbeam · mismanufacturedDURING C-CHECK INSPECTION FOUND CABIN FLOORBEAM IS NOT IAW DWG NR 2902. REF FASI NR 86793 REMOVED AND REPLACED FLOORBEAM IAW DWG NR 2902 AND SRM 53-10-2, FIG 7.SDR GAIA04151Seat Track · misinstalledDURING C-CHECK INSPECTION FOUND SEAT TRACK NOT INSTALLED IAW DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902.SDR GAIA04150Seat Track · mismanufacturedDURING C-CHECK INSPECTION, FOUND CABIN SEAT TRACK BS 344-480, RBL45.5 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902.SDR GAIA04149Seat Track · wrong partDURING C-CHECK INSPECTION FOUND SEAT TRACK, STA 344-480, RBL 24.75 NOT IN COMPLIANCE WITH DWG NR 2902. REF FASI NR 86790, REMOVED AND REPLACED SEAT TRACK IAW DWG NR 2902.SDR GAIA04148Seat Track · mismanufacturedDURING C-CHECK INSPECTION FOUND MAIN CABIN SEAT TRACK BS 344-480 LBL 45.5 NOT IN COMPLIANCE WITH DWG 2902. REMOVED AND REPLACED SEAT TRACK BS 344-480, LBL 45.5 WITH PN BAC 1520-792 IAW SRM 53-10-2, FIG 7 AND DWG 2902.SDR GAIA04147Seat Track · wrong partDURING C-CHECK INSPECTION FOUND CABIN SEAT TRACK STA 344-480, LBL 24.75 IS NOT IN COMPLIANCE WITH DRW NR 2902. REF FASI NR 86788 REMOVED AND REPLACED SEAT TRACK IAW DRW NR 2902.SDR GAIA04146Skin · damagedDURING C-CHECK INSPECTION FOUND SKIN FASTENERS LOOSE AND PULLED THROUGH SKIN AT STA 1342. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 54-30-3, FIG 7.SDR GAIA04145Skin · dentedDURING C-CHECK INSPECTION FOUND FUSELAGE SKIN DENTED AT BS 1342. REF FASI NR ACCOMPLISHED DOUBLER REPAIR IAW SRM 54-30-3, FIG 7.SDR GAIA04144Skin · tornDURING C-CHECK INSPECTION FOUND C1 DOOR CUT OUT AFT. FRAME STA 620 INNER SKIN TORN. REF FASI NR 86767 REMOVED DAMAGED AREA, INSTALLED REPAIR IAW SRM 51-40-2, FIG 1.SDR GAIA04143Angle · crackedDURING C-CHECK INSPECTION FOUND KEELBEAM PANEL COVER ANGLE CRACKED LT SIDE BS 870. REF FASI NR 86737 CUT OUT DAMAGED AREA DIM 1 X 8 INSTALLED ANGLE REPAIR IAW SRM 51-40-3.SDR GAIA04142Skin · crackedDURING C-CHECK INSPECTION FOUND NR 2 ENGINE INLET INTERIOR RT SIDE STA 1183 CRACKED. REF FASI NR 86722 CUT OUT DAMAGED AREA, INSTALLED DOUBLER REPAIR IAW SRM 54-10-3, FIG 9.SDR GAIA04141Skin · crackedDURING C-CHECK INSPECTION FOUND LT WING UPPER L/E SKIN NR 3 SLAT HOOK CUT OUT CRACKED. REF FASI N/R ACCOMPLISHED DOUBLER REPAIR IAW SRM 57-30-4.SDR GAIA04140Skin · crackedDURING C-CHECK INSPECTION, FOUND LT WING L/E SKIN WS549 CRACKED. REF FASI NR 86708 STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-30-4.SDR C7WA200400041Transmitter · frozenEXPERIENCED FLAP PROBLEM ON EXTENSION, PERFORMED CHECK LIST. LANDED WITHOUT INCIDENT. FOUND LT IB FLAP POSITION TRANSMITTER FROZEN. REMOVED AND REPLACED TRANSMITTER AND REPAIRED WIRES AT D224 IB FLAP INDICATOR CONNECTOR OPERATIONAL CHECK GOOD IAW MM.SDR C7WA2004000BBAccessory Unit · inoperativeRED LT GEAR, RT GEAR, NOSE GEAR AND AMBER TAIL SKID LIGHTS ON PILOTS FRONT PANEL REMAINED ILLUMINATED AFTER GEAR HANDLE WAS RAISED ON TAKEOFF. FLIGHT ENGINEERS ANNUNCIATOR LIGHTS REMAINED OUT. REMOVED AND REPLACED LANDING GEAR ACCESSORY BOX IAW MM. OPS CHECSDR C7WA2004000CCDuct · brokenAFTER TAKEOFF NR 3 ENGINE FIRE WARNING WENT OFF. EMERGENCY CHECK LIST ACCOMPLISHED. WHEN NR 3 THROTTLE WAS RETARDED FIRE WARNING LIGHT WENT OUT. RETURNED TO AIRPORT. FOUND NR 3 ENGINE ANTI-ICE DUCT BROKEN. REMOVED AND REPLACED NR3 ENGINE ANTI-ICE DUCT IAWSDR C7WA2004000AASwitch · inoperativeENGINE SHUTDOWN: IN CRUISE NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED AT THE SAME TIME THE RT DUCT OVERHEAT LIGHT CAME ON. ACCOMPLISHED ASSOCIATED EMERGENCY PROCEDURE IAW AOM. LIGHTS STAYED ON UNTIL ENGINE SHUTDOWN ON THE GROUND. REMOVED AND REPLACED NSDR 278229Accessory Unit · inoperativeDURING CLIMB, EXPERIENCED MULTIPLE WARNINGS FOR UNSAFE RT MAIN GEAR. ALTITUDE WARNING HORN SOUNDED AT 2000 FT, INADDITION TO WINDSHEAR LIGHT AND STICK SHAKER (NO SHEAR NOTED). AIRCRAFT RETURNED TO MSY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED LANDINSDR 2004F00187Skin · damagedDURNG WALK AROUND INSPECTION FOUND, SKIN DAMAGE WITH SKIN PEELED AND MISSING ON LOWER FORWARD RIGHT SIDE CENTER ENGINE AIR INLET DUCT HOUSING, BETWEEN FUSELAGE STATION 1183 AND 1233. REMOVED SKIN DAMAGE AS NECESSARY. INSTALLED EXTERNAL DOUBLER REPAIR AT LOWESDR 2004F00163Skin · delaminatedAT C-CHECK, FOUND LEFT WING INBOARD MID FLAP LOWER SURFACE TRAILING EDGE WITH DELAMINATION. FABRICATED FILLER AND DOUBLER. CUT NEW CORE. BONDED, CURED, SANDED, CLEANED, TREATED, PRIMED AND SEALED. (M)SDR 2004F00173Doubler · crackedAT C-CHECK, FOUND RIGHT WING NR 8 SLAT ACTUATOR ATTACH OUTER OUTBOARD FRAME LAYER IS CRACKED WING LEADING EDGE CAVITY. FABRICATE, PRIMED AND INSTALL NEW DUOBLER REPAIR AT RIGHT WING NR 8 SLAT ACTUATOR. (M)SDR 2004F00172Accessory Unit · faultyON APPROACH INTO DAY, UNSAFE RIGHT MAIN LANDING GEAR INDICATION. RED LIGHT WAS ILLUMINATED. GEAR WS VISUALLY VERIFIED DOWN BY THE TOWER. ACCOMPLISHED APPROPRIATE CHECKLIST FOR UNSAFE GEAR. RECYCLED GEAR SECOND TIME AND ALL INDICATIONS WERE NORMAL. AIRCRAFSDR 2004F00167Duct · crackedON TAKEOFF ROLL OUT OF ICT, NR 3 ENGINE FIRE WARNING CAME ON. SHUTDOWN NR 3 ENGINE IAW RYAN PROCEDURES AND RETURNED ICT. AIRCRAFT LANDED ICT WITHOUT INCIDENT. REMOVED AND REPLCED NR 3 ENGINE 13 STAGE SADDLE DUCT. GROUND OPERATIONAL CHECK NORMAL. (M)SDR 2004F00074Connector · damagedON LANDING INTO MSY, THE FORWARD PILOT PANEL INDICATOR LIGHT FOR THE LT MAIN LANDING GEAR SHOWED A RED UNSAFE LIGHT ILLUMINATED WITHOUT THE GREEN DOWN AND LOCKED INDICATION. THE FLIGHT ENGINEER'S PANEL SHOWED ALL THREE GEAR DOWN AND LOCKED. FLIGHT CREW DECLASDR 2004F00075Skin · tornIN CRUISE FLIGHT, CABIN CLIMBS 1000 FPM IN BOTH AUTO AND STANDBY MODES. FOUND FOUR INCH CRESCENT TEAR IN FUSELAGE SKIN ON RIGHT SIDE OF FUSELAGE AT STATION 420, BETWEEN STRINGERS 20R AND 21R. REMOVED DAMAGED SKIN SECTION AND REPAIRED USING AN EXTERNAL REPAIRSDR 2004F00110Generator · failedDURING TAKEOFF FROM BNA, AIRCRAFT LOST NR 3 GENERATOR, EPR WENT TO 1.6 AND OIL PRESSURE FELL TO REDLINE. PERFORMED ENGINE SHUTDOWN PROCEDURES AND DECLARED EMERGENCY. AIRCRAFT RETURNED TO BNA AND LANDED WITHOUT INCIDENT. DURING GROUND RUN OF ENGINES, FOUND NSDR 2004F00034Helicoil · damagedDURING CRUISE, ENGINE NR 3 LOST ALL OIL PRESSURE AND ALL OIL QUANTITY. PERFORMED NR 3 ENGINE INFLIGHT SHUTDOWN CHECKLIST. DIVERTED TO STL. EMERGENCY DECLARED. AIRCRAFT LANDED WITHOUT FURTHER INCIDENT. REMOVED AND REPLACED HELICOIL AT OIL FILTER BYPASS UNISDR RYN76394ASkin · corrodedDURING A SCHEDULED INSPECTION FOUND FUSELAGE SKIN AT STA 303 STR 17-18R, UNDER FORWARD LAV SERVICE PANEL, HAS EXFOILIATED CORROSION.SDR 2004F00069Switch · malfunctionedDURING FLIGHT, AIRCRAFT DECLARED EMERGENCY ON DESCENT TO PHX. AUTOPILOT FAILED TO DISCONNECT. AIRCRAFT LANDED AT PHX WITHOUT FURTHER INCIDENT. CLEANED AUTOPILOT DISENGAGE SWITCH ON YOKE AND OPERATIONAL CHECK NORMAL. (M)SDR 2004F00072Hinge · crackedAT B-CHECK, FOUND AFT SECTION OF MAIN CARGO DOOR HINGE CRACKED AT AFT END AIRFRAME SIDE. REMOVED CRACKED SECTION OF MAIN CARGO DOOR HINGE. FABRICATE, TREAT, PRIME AND INSTALLED NEW HINGE SEGMENT. MAIN CARGO DOOR OPERATIONAL CHECKED NORMAL. (M)SDR 2004F00057Angle · crackedAT B-CHECK, FOUND NR 2 SPOILER ACTUATOR IB MOUNT BRACKET CRACKED. REMOVED AND REPLACED NR 2 SPOILER ACTUATOR IB MOUNT BRACKET. RIGG AND LEAK CHECKED NORMAL. (M)SDR RYN2004F00027Module · failedAFTER TAKEOFF, RETRACTED FLAPS AND RECEIVED AN A-HYDRAULIC LOW PRESSURE INDICATION AT FLIGHT ENGINEER PANEL AND PILOTS FWD PANEL. FOLLOWED HYDRAULIC LOSS PROCEDURES. AIRCRAFT RETURNED TO DEPARTURE AIRPORT WITHOUT INCIDENT. REMOVED AND REPLACED (A) SYSTEM HYSDR RYN2004F00024Flap · maladjustmentAFTER TAKEOFF, ACCELRATED TO 300 KNOTS. CREW EXPERIENCED MODERATE VIBRATION. AIRCRAFT RETURNED TO DEPARTURE AIRPORT. ADJUSTED LT AND RT AFT FLAPS. REMOVED AND REPLACED AILERON HINGE SUPPORT FITTING.SDR RYN2004F00023Smoke Detector · false activationAC DEPARTED, ENROUTE, MAIN CARGO COMPARTMENT SMOKE DETECTOR LIGHT ILLUMINATED. AC DIVERTED WITHOUT INCIDENT. INSPECTED AC FOR EVIDENCE OF BURNED WIRES AND FLUIDS. NO EVIDENCE FOUND. INSPECTED CARGO SMOKE DETECTORS AND PERFORMED FUNCTIONAL TEST OF CARGO SMOSDR RYN2004F00022Line · chafedON CLIMB OUT, LOST HYDRAULIC A-SYSTEM. ACCOMPLISHED APPROPRIATE CHECK LIST AND MANUALLY EXTENDED THE LANDING GEAR. EMERGENCY DECLARED AND AIRCRAFT RETURNED. AIRCRAFT LANDED MDT WITHOUT INCIDENT. REPLACED NR 2 ENGINE HYDRAULIC PUMP FLEX PRESSURE LINE. LEAKSDR RYN2004F00021Actuator · leakingAFTER TAKEOFF, DURING ASCENT TO FLIGHT LEVEL 24.0 NR 7 FLAP LED AND YELLOW LIGHTS STAYED ILLUMINATED DURING FLAP RETRACTION. IMPLEMENTED PROCEDURES IAW MM FOR TROUBLESHOOTING. MANUAL STATED TO PROCEED WITH FLIGHT IF LIGHT EXTINGUISHED. LIGHTS EXTINGUISHED.SDR 2003F00479Cooling Fan · malfunctionedAFTER 'BLOCK-IN', THERE WAS SMOKE IN THE COCKPIT. (M)SDR 2003F00469Retainer · damagedAT C-CHECK, FOUND C2 DOOR PRESSURE SEAL RETAINER AT TOP CENTER OF DOOR DAMAGED. REMOVED AND REPLACED C2 DOOR PRESSURE SEAL RETAINER AT TOP CENTER OF DOOR. (M)SDR 2003F00470Bearing · crackedAT C-CHECK, FOUND RIGHT FIN UPPER STABILIZER HINGE FITTING BEARING CRACKED AND BOTH RETAINERS CORRODED AT BS 1586. REMOVED AND REPLACED RIGHT STABILIZER HINGE BEARING ASSEMBLY. (M)SDR 2003F00455Compressor · stalledFROM 31,000 FEET, ON DESCENT INTO BWI, NR 2 ENGINE COMPRESSOR STALL. ALL ENGINE READINGS APPEARED NORMAL. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 ENGINE. OPERATIONAL AND LEAK CHECKED NORMAL. (M)SDR 2003F00249Connector · damagedDURING LANDING AT WICHITA, THE NOSE LANDING GEAR SAFE LIGHT FAILED TO ILLUMINATE WHEN GEAR WAS EXTENDED. EMERGENCY CHECKLIST PROCEDURES WERE FOLLOWED WITH A CONFIRMED VISUAL DOWN INDICATION. AIRCRAFT LANDED AT ICT WITHOUT INCIDENT. SECURED LOOSE PIN AND RELSDR 2003F00420Floor Support · dentedAT C-CHECK, FOUND DENT ON AFT CARGO FLOOR SUPPORT, STATION 950F, RBL 17. FABRICATE REPAIR DOUBLER AND FILLER. TREATED AND PRIMED PARTS AND AREA. INSTALLED DOUBLER AND FILLER AT AFT CARGO FLOOR SUPPORT RBL 17 STATION 950F PLUS 2 INCHES. (M)SDR 2003F00419Frame · crackedAT C-CHECK, FOUND CRACK ON FORWARD CARGO FRAME AT BS 660, STRINGER 23R/24R. FABRICATE REPAIR ANGLE. TREATED, PRIMED AND INSTALLED REPAIR ANGLE ON FORWARD CARGO FRAME STATION 660 STRINGER 23R AND 24R. (M)
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