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 2001UALA01594Valve · failedNR 1 OIL TEMP IN YELLOW BAND FOR 15 MIN. ENGINE SHUTDOWN AND DIVERTED TO COS. THE FUEL HEAT VALVE FAILED. REPLACED FUEL HEAT VALVE AND DRAINED, REPLACED OIL AND SCREEN. THE MOTOR IN THE ACTUATOR OF THE VALVE ASSEMBLY WAS FOUND TO BE BAD.SDR 2001UALA01511Bypass Switch · failedAIRCRAFT DIVERTED DUE TO A NR 1 OIL FILTER BYPASS LIGHT. REPLACED THE OIL FILTER BYPASS SWITCH.SDR 2001UALA01513Battery · failedAFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT IS INOPERABLE. SUPPLEMENTAL DATA UPDATE BATTERY FAILED. REPLACED BATTERY. OPERATIONS CHECK NORMAL.SDR 2001UALA01462Skin · crackedFUSELAGE SKIN CRACK LOCATED JUST AFT OF NR 2 VHF ANTENNA, LEFT OUTBOARD BETWEEN 4TH AND 5TH ROW OF RIVETS. CRACK IS APPROX. 1.75 INCHES LONG. FUSELAGE SKIN CRACK BETWEEN STATION 1030 AND 1070 STR 28L. DAMAGE CUTOUT, EDDY CURRENT, AND DOUBLER INSTALLED PER SSDR 2001UALA01470Pump · leakingCREW REPORTS LOSS OF B-SYSTEM BRAKE PRESSURE, ALSO REPORTS FLUID COMING FROM THE GEAR ON TAXI OUT. REPLACED NR 2 ENGINE B-SYSTEM HYDRAULIC PUMP. SYSTEM TESTS NORMAL.SDR 2001UALA01469Controller · failedCABIN PRESSURE CAN NOT BE MAINTAINED (CABIN ALTITUDE RISES) IN DESCENT. BOTH AUTO & STANDBY THIS HAPPENS EVEN AT 5000 FEET. DUCT PRESSURE NORMAL. REPLACED THE NR 3 ENGINE 13TH STAGE MODULATOR VALVE, AND THE PRESSURE CONTROLLER.SDR GAIA01284Switch · inoperativeDURING PERIODIC SERVICE CHECK, THE EMERGENCY EXIT LIGHT 'ARM AND ON' SWITCH WOULD NOT TURN LIGHTS OFF. MAINTENANCE REMVOED AND REPLACED EMERGENCY EXIT LIGHT 'ARM AND ON' SWITCH. SYSTEM WAS OPERATINOAL CHECKED OK PER BOEING 727 MM CHAP 33-50. (M)SDR 2001UALA01468Controller · malfunctionedAT FL240 WHEN THROTTLES PULLED BACK TO FLIGHT IDLE, CABIN PRESSURE STARTED CLIMBING AT 2000 FPM. WHEN CARGO HEAT VALVE CLOSED, CABIN PRESSURIZATION RETURNED TO NORMAL.SDR 2001UALA01466Aileron · out of adjCREW REPORTS RIGHT HAND WING OUTBOARD AILERON, INBOARD TRAILING EDGE MAKING CONTACT. CHECKED ADJUSTMENT OF FLAP AND ADJUSTED AILERON. OPERATIONS CHECK NORMAL.SDR 2001UALA01443Skin · delaminatedFLIGHT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. FLT SPOILER LEFT WING NR 3 DELAMINATED NEAR TRAILING EDGE. SPOILER PANEL WAS CHECKED FOR CRACKS OR SCRATCHES AND NONE WERE NOTED. AN INTERIM REPAIR WAS ACCOMPLISHED WITH THE REQUIREMENT THAT THE SSDR 2001UALA01445Skin · corrodedRIGHT SIDE OF FUSELAGE 6 INCHES AFT OF FORWARD LAV SERVICE PANEL, PAINT IS BUBBLING AND SKIN IS BULGING IN A 6 INCH DIAMETER AREA.SDR 2001UALA01463Control Panel · failedCABIN PRESSURIZATION ELECTRONIC SYSTEM IN MANUAL THERE IS NO OUTFLOW VALVE INDICATOR MOVEMENT WITH FUNCTION SWITCH IN AC MANUAL. VALVE VISUALLY OBSERVED AND IS NOT MOVING. THE CONTROL PANEL FAILED. REPLACED CONTROL PANEL. OPERATIONS CHECK NORMAL.SDR 2001UALA01465Engine · malfunctionedNR 3 ENG EGT LIMITED T/O FROM DEN. COMMAND EPR 2.06. TARGET N1 X-CK 98.1. AT 2.06 EPR, NR 3 ENG N1 95 PERCENT AND EGT REACHED 630 DEG FOR 2 SEC. REDUCED POWER TO KEEP EGT IN LIMITS. A CHECK OF THE INLET AND EXHAUST AND PERFORM THE MAX EGT CHECK PER JRH 2-7-3SDR 2001UALA01444Cowling · crackedNR 2 ENGINE LOWER FORWARD COWLING MATING FLANGE, FOUND 3 CRACKS, ONE 8 INCHES LONG, THE OTHERS 3.5 INCHES LONG. ALSO, THERE IS A HOLE WORN THRU COWL MATING FLANGE. REPAIRED COWL AND SPLICED IN NEW FLANGE. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01422Screw · missingLOSS OF HYDRAULIC FLUID IN THE 'A' SYSTEM. FOUND FLAP DRIVE MOTOR SHAFT SEAL PLATE MISSING SCREWS AND O-RING POPPED OUT. REPLACED FLAP DRIVE MOTOR AND SERVICED HYD SYS. OPERATIONS AND LEAK CHECK NORMAL.SDR 2001UALA01430Brake · fireLEFT OUTBOARD LANDING GEAR BRAKES CAUGHT ON FIRE APPROX 3 MINUTES AFTER PARKING BRAKES SET. *S/D* INSPECTION ACCOMPLISHED WITH NR 1 & NR 2 BRAKES REMOVED, NO DEFECTS FOUND. REPLACED NR 1 AND NR 2 BRAKES AS PRECAUTIONARY. OPERATIONS CHECK NORMAL.SDR 2001UALA01427Connector · faultyNOSE GEAR RED LIGHT ON WHEN GEAR EXTENDED. *S/D* REPLACED CONNECTOR D298. OPERATIONS CHECK NORMAL.SDR 2001UALA01424Engine · fireUPON LANDING FLAMES CAME OUT OF NR 1 ENGINE THRUST REVERSERS WHEN THRUST REVERSERS WERE MOVED TO STOWED POSITION. *S/D* REPORT OF FLAMES OUT OF THE THRUST REVERSER WAS REPORTED BY OPERATIONS VEHICLE AND NO CAUSE HAS BEEN FOUND. THE THRUST REVERSER WAS OPERASDR 2001UALA01464Light · inoperativeAFT AIRSTAIR EMERGENCY LIGHT HAS ONE BULB BURNED OUT RELAMPED. OPERATIONAL CHECK GOODSDR 2001UALA01446Nut Plate · looseVIBRATION AT M .80, INCREASES WITH AIRSPEED, AND LEFT TURNS, STAYS THE SAME WITH SPOILERS EXTENDED. FOUND NUTPLATES ON TAIL CONE REQUIRING REPLACEMENT. NUTPLATES ALLOWED TAIL CONE TO VIBRATE.SDR 2001UALA01473Connector · intermittentRADIO ALTIMETER FAULT WITH ASSOCIATED GPWS FAIL. INTERMITTENT CONNECTION CAUSED THE FAULT. REMOVED AND REINSTALLED ANT RAD ALT TX ANTENNAS. SECURED SOFT MATE CONNECTOR RAD ALT. OPERATIONS CHECK NORMAL.SDR 2001UALA01472Shear Tie · corrodedAFT PIT BILGE, CORROSION IN SHEAR TIE FORWARD SIDE BETWEEN STR 28L AND 29L AT FRAME STA 1010. REPAIRED SHEAR TIE PER MM 53-10-29. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01471Shear Tie · corrodedAFT PIT BILGE, CORROSION IN SHEAR TIE AFT SIDE OF FRAME 1130 BETWEEN STR 27L AND 28L. REPAIRED SHEAR TIE PER MM 53-10-29. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01407Proximity Switch · malfunctionedLEFT MAIN GEAR INDICATION LIGHT ILLUMINATED DURING DESCENT. LANDED WITHOUT INCIDENT. REPLACED A9 CARD AND DOWNLOCK POSITION PROXIMITY SWITCH. OPS CHECK CHECKED NORMAL. NO OTHER OBVIOUS DISCREPANCIES.SDR 2001UALA01467Skin · corrodedAFT PIT BILGE AREA CORROSION IN SKIN LT SIDE, BETWEEN STR 28L AND 29L, STA 970-990.SDR 2001UALA01410Battery Pack · dischargedEMERGENCY EXIT LIGHTS ABOVE BOTH LEFT OVERWING EXIT DOORS ARE INOPERABLE. SUPPLEMENTAL DATA UPDATE REPLACED BATTERY PACK, OPERATIONS CHECK NORMAL.SDR 2001UALA01411Pcu · failedCREW REPORTS AILERONS EXPERIENCED AN UNCOMMANDED JERKING MOVEMENT WHEN MAKING TURNS TO THE RIGHT. REPLACED AILERON PCU. SYSTEM CHECKS NORMAL.SDR 2001UALA01406Motor · leakingINBOARD FLAPS INDICATION LIGHT ILLUMINATED WHILE RAISING FLAPS. AIRCRAFT RETURNED TO DEN. FOUND INBD FLAP HYD MOTOR LEAKING. REMOVED AND FOUND BEARINGS ROUGH, REPLACED WITH NEW REF MM27-53-19. CYCLED FLAPS SEVERAL TIMES, SYSTEM OPERATION NORMAL.SDR 2001UALA01408Brake · smokeTOWER REPORTED SMOKE COMING FROM THE LANDING GEAR DURING LANDING. *S/D* NR 2 BRAKE HAD BEEN REPLACED FLIGHT PRIOR. POSSIBLE THAT SMOKE DUE TO RESIDUAL HYD FLUID FROM ACCOMPLISHMENT OF BRAKE CHANGE. BRAKE INSPECTED AND TESTED NORMAL. NO FURTHER ACTION TAKESDR 2001UALA01405Switch · failedLEADING EDGE FLAP AMBER LIGHT INDICATION OCCURRED AFTER CLIMBOUT. AIRCRAFT CONTINUED TO MIA. SUPPLEMENTAL DATA UPDATE FOUND #2 LEADING EDGE FLAP SWITCH FAULTY AND REPLACED SWITCH.SDR 2001UALA01409Audio Panel · failedCREW REPORTS INTERMITTENT FAILURE OF NR 1 AND NR 2 RADIOS. AIRCRAFT RETURNED TO DEN. CAPTAIN'S AUDIO PANEL FAILED. REPLACED CAPTAIN AUDIO SELECT PANEL PER MM. OPERATIONS CHECK NORMALSDR 2001UALA01404Switch · faultyNR 2 ENGINE SHUT DOWN IN FLIGHT DUE TO LOW OIL PRESSURE INDICATION. AIRCRAFT DIVERTED TO COS. *S/D* ENGINE WAS SHUT DOWN DUE TO LOW OIL PRESSURE LIGHT INDICATION. ALL ENGINE PARAMETERS INDICATED NORMAL AND OIL PRESSURE WAS ABOVE 35 PSI. LOW OIL PRESSURE LSDR 2001F00177Hydraulic Line · cracked'A' SYSTEM HYDRAULIC FAILURE AFTER TAKEOFF. EMERGENCY DECLARED. COMPLIED WITH ALL CHECK LISTS. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED HYDRAULIC PRESSURE TUBE ON RIGHT ELEVATOR POSITION CONTROL UNIT. LEAK AND OPERATIONAL CHECK GOOD. (M)SDR 2001UALA01340Skin · dentedFOUND DENT ON LEFT SIDE OF FUSELAGE BEHIND RADOME AT 7 O'CLOCK POSITION, STATION 188. REPAIRED EXTERNAL FUSELAGE DENT PER SRM 53-30-03. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01341Battery · dischargedLT CENTER OVER WING EMERGENCY EXIT LIGHT IS INOPERABLE. BATTERY WAS DISCHARGED. RECHARGED BATTERY, GROUND TEST NORMAL.SDR 2001UALA01345Light · inoperativeFWD LOWER LEFT DOOR EXIT LIGHT IS INOPERABLE. EEL CABLE AND EXIT LIGHT WAS DAMAGED. REPAIRED DAMAGED EEL CABLE AND REPLACED INOPERABLE EXIT LIGHT ASSEMBLY. EMERGENCY EXIT OPERATIONS CHECK NORMAL.SDR 2001UALA01342Stringer · corrodedSTRINGER 27R IS CORRODED. REPAIRED STRINGER PER SRM 53-10-03. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01343Actuator · failedCREW REPORTS A GRINDING NOISE HEAR WHEN CRUISE TRIM ENGAGED. MANUAL TRIM WAS JAMMED IN THE NOSE UP POSITION. AIRCRAFT RETURNED TO DEN. REPLACED THE MAIN STAB TRIM ACTUATOR, CRUISE STAB TRIM ACTUATOR AND STAB BRAKE ASSY. SYSTEM OPERATIONS CHECK NORMAL.SDR 2001UALA01344Skin · crackedRT ELEVATOR LOWER SKIN IS CRACKED AT STATION 183. REPAIRED SKIN WITH EXTERNAL DOUBLER PER SRM 55-20-03 AND CALCULATED NEW MOMENT PER SRM 51-80-07. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01309Skin · crackedRT ELEVATOR LOWER SKIN IS CRACKED AT STA 183. REPAIRED SKIN WITH EXTERNAL DOUBLER REPAIR PER SRM 55-20-03. CALCULATED NEW MOMENT PER SRM 51-80-07. FOUND MOMENT WITHIN LIMITS. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01335Transceiver · failedLOST WEATHER RADAR DURING CRUISE. AIRCRAFT DIVERTED TO ORD. TRANSCEIVER FAILED. REPLACED WEATHER RADAR. OPERATIONS CHECK NORMAL.SDR 2001UALA01308Valve · failedCABIN PRESSURE CANNOT BE MAINTAINED IN DESCENT. *S/D* SUSPECT NR 3 ENG HIGH PRESSURE MODULATING VALVE. REPLACED HIGH PRESSURE MODULATING VALVE.SDR 2001UALA01307Light · damagedEMERGENCY EXIT LIGHTING FROM ROW 23 TO AFT ENTRY DOOR IS INOPERABLE. EEL STRIP IS DAMAGED. REPLACED LAMPS AND COVER. OPERATIONS CHECK NORMAL.SDR 2001UALA01306Battery · missingTHE R1DOOR EMERGENCY EXIT EXTERIOR LIGHT IS INOPERABLE. BATTERY ASSY IS MISSING. INSTALLED MISSING BATTERY ASSY. OPERATIONS CHECK NORMAL.SDR 2001UALA01193Channel · crackedLT ELEVATOR INTERNAL SUPPORT CHANNEL IS CRACKED IN HALF AT STA 120. REPLACED CHANNEL PER GNMM 1-0-0-23. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01190Roller · shearedCREW RECEIVED A SPLIT FLAP INDICATION WHILE RETRACTING FLAPS AFTER CLIMBOUT. AIRCRAFT DIVERTED TO EWR. FOUND ROLLERS ON TOGGLE ASSEMBLY FOR THE RT INBOARD FLAP TRACK SHEARED OFF. REPLACED TOGGLE ASSY.SDR 2001UALA01189Light · inoperativeFORWARD LOWER CEILING EMERGENCY LIGHT IS INOPERABLE. EMERGENCY LIGHT ASSY FAILED. REPLACED BATTERIES AND LAMPS, NO HELP, REPLACED LIGHT. ASSEMBLY OPERATION IS NOW NORMAL.SDR 2001UALA01188Control Valve · failedAIRCRAFT UNABLE TO MAINTAIN PRESSURIZATION DURING CRUISE AT FL250. *S/D* RIGHT FLOW MODULATING VALVE WOULD NOT CLOSE. REPLACED FLOW CONTROL MODULATING VALVE. OPERATIONS CHECK NORMAL.SDR 2001UALA01191Strap · tornTEAR STRAP UNDER SKIN IS TORN JUST FORWARD OF RT FUSELAGE JACK POINT. FABRICATED TEAR STRAP DOUBLER AND TRIPLER PER SRM 53-30-04 FIG 6. LOCATED STA 351 AND STRINGER 21R. CORRODED SKIN SUPPORT BRACKET REPLACED DURING REPAIR. MAJOR REPAIR ACCOMPLISHED.SDR 2001UALA01078Battery · dischargedAFT EMERGENCY FLASHLIGHT INOPERABLE. REPLACED BATTERIES. OPERATIONAL CHECK NORMAL.
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