Boeing 727-222
Service difficulty reports · 1,723
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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 = '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 FDEA2020072316538Seat Track · corrodedSEAT TRACK, RBL 58.22 HAD LIGHT SURFACE CORROSION AROUND NUT PLATES AT BS 1180. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52-1A, FIG 101, DET VII, AND DET I, CUT OUT SECTION OF SEAT TRACK FROM BS 1180 TO 1310, FABRICATED AND INSTALLED A NSDR UALA2013070804751Girt Bar · obstructedFOUND LANYARD UNDER GIRT BAR. SECURED LANYARD AND DOOR OPS NORMAL.SDR UALA2013051303297Floorbeam · corrodedFWD PAX COMPARTMENT, BS 324, RBL 41 TO 43, FLOORBEAM HAS CORROSION ON FWD EDGE. REMOVED CORROSION AND LOSS OF .030 IS OOL CUT AND REPAIRED DMG SECTION IAW SRM 53-10-08, REPAIR 1. FABRICATED PTS IAW SRM 53-10-08. INSTALLED REPAIR PARTS IAW 53-10-08 AND GNMSDR FDEA201011284515Floorbeam · corrodedCORROSION TOP "T" CAP FLOORBEAM STA 440, BL 0 - LBL 25, MAIN CABIN CUTOUT DAMAGE AREA AT FLOORBEAM BS 440, LBL 10 IAW SRM 53-10-8 FIG 8, FABRICATED (2) ANGLES REPAIR IAW SRM 53-10-8 FIG 8, & INSTALLED NEW ANGLES REPAIR AT LBL 5 - LBL 13 BS 440 IAW SRM 53-1SDR 2007UALA05002Lamp · brokenSEAT 1E AFT EMERGENCY LIGHT ON ARMREST BROKEN OFF. RELAMPED.
SDR 2007UALA04566Line · leakingHYD QTY LOW C CENTER HYDRAULIC SYSTEM LOW RESERVOIR QUANTITY. FOUND LT MLG SIDE BRACE DOWNLOCK ACTUATOR HOSE LEAKING REF IPC 32-32-04 ITEM 30. REPLACED HYDRAULIC LINE, CLEANED AREA, PRESSURIZED HYD SYSTEM &
LEAK CHECKED OK.SDR GAIA0710Wire · shortedDURING DESCENT, THE NR 3 ENGINE FIRE LIGHT FLICKERED ON AND OFF. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED A SHORTED WIRE IN THE NR 3 ENGINE PYLON AT PLUG AT PLUG D4184P. THE WIRE WAS REPAIRED AND THE ENGINE AND FIRE WARNING OPS CHECKED GOOD ON TSDR GAIA0708Wire · shortedDURING DECENT, THE NR 3 ENGINE HAD A FIRE INDICATION. THE FLIGHT CREW ACCOMPLISHED THE CHECK LIST AND SHUTDOWN THE ENGINE AND FIRED BOTH FIRE BOTTLES. THE ENGINE FIRE LIGHT NEVER EXTINGUISHED. AN UNEVENTFUL LANDING WAS MADE. INSPECTION REVEALED A SHORTED WSDR 2007UALA01236Light · missingAFT EEL LIGHT AT SEAT 14D IS MISSING. REPLACED LIGHT ASSY. OPS CHECKS GOOD.SDR BMAC06013Csd · overspeedAN ELECTRICAL MALFUNCTION OCCURRED CAUSED BY THE NR 1 AC GEN ISOLATED THE (3) BUS TIES AND DISCONNECTED THE NR 1 CSD. ALSO, NOTED ALL (8) BOOST PUMP CB'S HAD OPENED. MAINT DEFERRED THE NR 1 GEN AND CSD. LATER REPLACED NR 1 AC GEN AND CSD, OPS CHECKED GOOSDR BMAC06009Battery Pack · failedDURING SERVICE CHECK, FOUND RIGHT HAND OVERWING EMERGENCY LIGHT NOT ILLUMINATING. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW UAL MM 33-50-19, OPS CHECKED GOOD.SDR C7WA200600009Valve · failedAIR RETURN, LOST A-SYSTEM HYDRAULIC SYSTEM ON TAKEOFF ZERO QUANITY AND PRESSURE. COMPLETED CHECK LIST, NORMAL LANDING FOUND LT MLG DOOR SEQUENCE VALVE BLOWN. REMOVED AND REPLACED SEQUENCE VALVE. OPERATIONAL AND LEAK CHECKS GOOD. (K)SDR C7WA200600007Control Box · false indicationNR 1 ENGINE FIRE WARNING LIGHT ILLUMINATED SHUTDOWN ENGINE AND RETURNED TO DEPARTURE. REMOVED AND REPLACED NR 1 ENGINE FIRE DETECTION CONTROL BOX OPS CHECK GOOD IAW MM. (K)SDR C7WA200600008Clamp · looseNR 1 ENGINE FIRE WARNING LIGHT AND BELL ILLUMINATED IN FLIGHT. PERFORMED ENGINE SHUTDOWN AND RETURNED TO DEPARTURE. INSPECTED ENGINE FOR LEAKS AND DAMAGE. TIGHTENED CLAMPS ON BLEED AIR DUCTS AND REPOSITIONED FIRE LOOP IN PYLON. RAN ENGINE OPERATIONAL CHECKSDR BMAC06006Battery Pack · failedL/H EMERGENCY LIGHT INOP, FOUND ON INSPECTION.REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK IAW UAL MM 33-50-28. OPS CHECKED GOOD.SDR C7WA200600006Smoke Warning · activatedCARGO SMOKE LIGHT ILLUMINATED IN FLIGHT. RAN PROCEEDURE AND DIVERTED. COULD NOT DUPLICATE. TESTED SYSTEM IAW MM. (K)SDR C7WA200600004Regulator · intermittentNR 1 GENERATOR EXPERIENCED AN UNDER VOLTAGE CAUSING A VERTICAL TRIP. NR3 GENERATOR ALREADY ON DMI. REMOVED AND REPLACED NR1 POSITION VOLTAGE REGULATOR SYSTEM OPERATIONAL CHECKS GOOD IAW MM. (K)SDR C7WA200600003Engine · fodIN FLIGHT, AT FL 28.0, NR 2 ENGINE COMPRESSOR STALLED. ENGINE WAS IN STABLE OPERATION, NO BLEED AT 1.80 EPR. EPR DROPPED TO 1.4 EGT RUNS 80 TO 100 HOTTER THAN ENGINES 1 AND 3 IN ALL PARAMETERS OF FLIGHT. INSPECTION ON NR 2 ENGINE REVEALED HEAVY FOD DAMAGE. SDR BMAC060005Battery Pack · failedEMERGENCY LIGHTS M955 AND M957 FOUND INOPERATIVE ON DAILY CHECK. BATTERY PACKS WILL NOT HOLD CHARGER, PACKS REMOVED AND REPLACED.SDR C7WA200600001Seal · leakingENGINE NR 1 LOSS OIL DURING FLIGHT. INSTALLED NEW OIL LINE DONUT SEALS ON GEARBOX OIL LINES. NO LEAKS NOTED DURING ENGINE RUNS IAW MM. (K)SDR BMAC060004Wire · brokenCRUISE TRIM INOPERATIVE IN MANUAL AND AUTO-PILOT MODE. FOUND AND REPAIRED BROKEN WIRE PIN 7 TO CRUISE TRIM MOTOR.SDR BMAC060003Transmitter · faultyASYMMETRY ON OUTBOARD FLAPS. REPLACED RT OUTBOARD FLAP POSITION INDICATOR.SDR C7WA200500126Sequence Valve · intermittentDURING APPROACH, RT MLG AND NOSE GEAR INDICATION SHOWED UNSAFE. ON SECOND ATTEMPT GEARS CAME DOWN NORMALLY. ON GEAR OPERATIONAL CHECK RT MLG FAILED TO EXTEND, NOSE GEAR OPERATION NORMAL. REMOVED AND REPLACED RT MLG DOOR SEQUENCE VALVE. SYSTEM OPERATIONAL CSDR GAIA05024OPSkin · crackedNO FLIGHT; DURING INSPECTION A SMALL CRACK WAS FOUND ON THE L1 DOOR UPPER AFT BEARING WHICH CAUSED THE DOOR FRAME TO CRACK. REMOVED AND REPLACED L1 DOOR. AIRCRAFT WAS RETURNED TO SERVICE. (K)SDR BMAC050012Controller · malfunctionedUNABLE TO MAINTAIN AND CONTROL CABIN ALTITUDE IN AUTO, STBY OR MANUAL. OUTFLOW VALVE SHOWS FULLY CLOSED, HOWEVER, CABIN ALTITUDE CONTINUED TO CLIMB. REMOVED AND REPLACED PRESSURE CONTROLLER AND SAFETY VALVE.SDR BMAC050011Actuator · leakingAFTER TAKEOFF, NR 1 SLAT WOULD NOT RETRACT. SYSTEM "A" HYDRAULIC QUANTITY DECREASED TO 0.3 GALLONS. MAINTENANCE REMOVED AND REPLACED NR 1 L/E SLAT ACTUATOR, LEAK AND OPS CHECK GOOD.SDR C7WA200500110Overheat Loop · groundedLOWER AFT BODY OVERHEAT LIGHT ON. COMPLETED EMERGENCY PROCEDURE, FOUND IT TO BE NR 2 ENGINE. INSPECTED NUMBER 2 ENGINE FOUND LOOP TOUCHING BLEED AIR DUCT. REPOSITIONED LOOP OPERATIONAL CHECKS GOOD PER MM 26-14-0. (M)SDR C7WA200500108Brake · seizedAIR RETURN, ON CLIMBOUT AT 14,000 FT WHEEL WELL FIRE LIGHT ILLUMINATED. RAN CHECK LIST FIRE LIGHT WENT OUT. FOUND NR 2 BRAKE ASSEMBLY. SEIZED. REMOVED AND REPLACED NR 2 BRAKE ASSEMBLY. (SO29200506401) (K)SDR BMAC050007Slide · deployedL1 EMERGENCY DOOR SLIDE ACTIVATED WHEN DOOR WAS OPENED, GIRT BAR WAS NOT ATTACHED. HOLDING CONTAINER MALFUNCTIONED. REMOVED AND REPLACED SLIDE ASSEMBLY.SDR C7WA200500095Warning System · malfunctionedAPU FIRE BELL SOUNDS OFF AND CANNOT BE SILENCED. NO WARNING LIGHTS OR OTHER INDICATIONS THAT A PROBLEM EXISTS. REMOVED, CLEANED AND REINSTALLED APU FIRE DETECTOR POWER UNIT. SYSTEM OPS. CHECK NORMAL IAW MM. (K)SDR C7WA200500098Pump · inoperativeAIR RETURN: NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS FAILED. REMOVED AND REPLACED NR 1 AND NR 2 (B) SYSTEM HYDRAULIC PUMPS. REMOVED AND REPLACED (B) SYSTEM CASE DRAIN FILTERS. (K)SDR C7WA200500094Switch · out of adjustCARGO DOOR LIGHT ILLUMINATED AFTER TAKEOFF. ADJUSTED MAIN CARGO DOOR VENT LIGHT SWITCH IAW MM. OPS CHECK GOOD. (K)SDR C7WA200400081Accessory Unit · inoperativeRT MLG UNSAFE LIGHT ILLUMINATED IN FLIGHT. REMOVED AND REPLACED LANDING GEAR ACCESSORY UNIT. OPERATIONAL CHECK IAW MM. OPS CHECK NORMAL. (K)SDR C7WA200300077Connector · dirtyAIR RETURN, UPON FLAP RETRACTION ON CLIMB-OUT, NR 1 SLAT FAILED TO RETRACT. CLEANED CONNECTOR IAW 20-80-01, OPS CHECKED FLAPS AND SLATS PER MM 27-80-0. ALL INDICATIONS NORMAL. OK FOR CONTINUED SERVICE. (M)SDR C7WA200300075Wire · shortedIN FLIGHT SHUTDOWN NR 3 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN ALT AT 12,000 FEET, PERFORMED ABNORMAL CHECKLIST AS REQUIRED. FOUND WIRES SHORTED IN CONNECTOR D8002 TO NR 3 ENGINE START VALVE PRESSURE SWITCH. REMOVED AND REPLACED CONNECTOR, OPS CHECK PESDR C7WA200400072Warning Light · illuminatedLOWER AFT BODY OVERHEAT LIGHT ILLUMINATED THEN EXTINGUISHED ON ITS OWN INFLIGHT. INSPECTED DUCTING IN AFT AIRSTAIR AREA AND RAN ENGINES AT TAKEOFF POWER. UNABLE TO DUPLICATE PROBLEM, NO LEAKS NOTED. SYSTEM OPERATIONAL, CHECK GOOD IAW MM. (K)SDR C7WA200400073Sensing Element · erraticIN FLIGHT, LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED, RT DUCT PRESSURE INDICATED 80 PSI. MADE PRECAUTIONARY LANDING. TIGHTENED ALL CLAMPS IN AIRSTAIR AREA. REPLACED LT AND RT PURGE LINE COUPLING SEALS. REMOVED AND REPLACED LOWER AFT BODY OVERHEAT LOOP DETESDR C7WA200400068Pressure Switch · inoperativeNR 3 ENGINE START VALVE LIGHT CAME ON DURING FLIGHT. FOUND NR 3 ENGINE START VALVE PRESSURE SWITCH INOPERATIVE. REMOVED AND REPLACED PRESSURE SWITCH IAW MM.SDR C7WA200400061Flap Track · corrodedRT WING IB FLAP OB TRACK AFT MOUNT PAD HAS CORROSION. RT WING IB FLAP OB. TRACK NR 6 PN 65192493, CORROSION ON AFT MOUNT PAD REMOVED. MATERIAL REMOVED WAS 0.020. REPAIR ACOMPLISHED IAW EO.SDR C7WA200400060Keelbeam · corrodedAFT CARGO COMPARTMENT, STA 1007 RT KEELBEAM CHORD HAS CORROSION. INSTALLED INTERNAL SPLICE REPAIR ON RT HEELBEAM CHORD SECTION BETWEEN BS 980 AND BS 1007. DAMAGED KEELBEAM CHORD SECTION REMOVED. NEW KEELBEAM CHORD SECTION FABRICATED IAW SAMPLE AND MFG DWG 6SDR C7WA200400059Structure · damagedRT HORIZONTAL STABILIZER BALANCE PANELS NR 2, NR 3, AND NR 4 CAVITIES T/E LOWER BEAM RUB BLOCKS ADJUSTMENT SCREW SAFETY WIRE HOLES CRACKED. INSTALLED SPLICE REPAIR ON RT HORIZONTAL STABILIZER T/E BEAM BALANCE PANELS CAVITIES NR 2, NR 3, AND NR 4. DAMAGED CHOSDR C7WA200400057Floorbeam · corrodedFLOOR TRAVERSE BEAM AT STA 600 HAS LIGHT CORROSION BETWEEN BL0 AND RBL 24.5 AND BETWEEN LBL 45.5 AND LBL50. INSTALLED INTERNAL FLOORBEAM REPAIR ON DAMAGE LOCATED AT BS 600 BETWEEN BL0 AND LBL 24.50. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DISDR C7WA200400056Floorbeam · corrodedTRAVERSE FLOORBEAM STA 720 HAS CORROSION BETWEEN BL0 AND LBL 24.5. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 720A, BETWEEN BL0.0 AND LBL 24.5. DAMAGED FLOORBEAM CHORD PORTION REMOVED. FINAL TRIM OUT DIMENSION WAS 6.00 INCH X 2.00 INCH. REPAIR SECTION FABRSDR C7WA200400055Shear Tie · crackedSHEAR TIE CRACKED AT FRAME STA 930 BETWEEN STRINGER 13 RT AND STRINGER 14 RT. INSTALLED INTERNAL REPAIR ON SHEAR TIE AT BS 930 BETWEEN STRINGER 13 RT AND 14 RT. DAMAGED SHEAR TIE REMOVED. REPAIR PART FABRICATED FROM 7075-T6, X .063. REPAIR PARTS AND BARE ESDR C7WA200400054Beam · corrodedBULKHEAD STA 1183 HAS A 6 INCH CRACK IN THE VERTICAL BEAM AT LBL 24.5, WL 250. INSTALLED INTERNAL REPAIR ON DAMAGED VERTICAL BEAM AT BS 1183 AT LBL 24.50, WL 250. DRILLED STOP HOLE .250. REPAIR CHANNEL 65C33556-45 AND SHIMS INSTALLED IAW SB. REPAIR PARTS ASDR C7WA200400053Floorbeam · corrodedFLOORBEAM AT BS 660 RBL 45.50 HAS LIGHT CORROSION. INSTALLED INTERNAL FLOORBEAM REPAIR AT BS 660, RBL 45.50. REMOVED DAMAGED CHORD PORTION, FINAL TRIM OUT WAS 2.00 INCH. FABRICATED REPAIR SECTION FROM ALUM 7075-0 X 0.090 INCH X 16 INCHES. HEAT TREATED TO TSDR C7WA200400052Skin · crackedNR 3 RT COCKPIT WINDOW UPPER SKIN (EXTERIOR) HAS AN APPROXIMATELY 1 INCH CRACK. INSTALLED EXTERNAL SKIN REPAIR ON RT NR 3 WINDOW UPPER SKIN. REMOVED DAMAGED SKIN PORTION. SKIN TRIM OUT 4.00 X 5.00. FABRICATED AND INSTALLED REPAIR FILLER PLATE FROM 2024-T3 SDR GAIA04139Skin · crackedDURING C-CHECK INSPECTION FOUND LT WING L/E CAVITY WS110-130 FWD. SKIN BUCKLED AND CRACKED. REF FASI NR 86706, STOP DRILLED CRACK, INSTALLED DOUBLER REPAIR IAW SRM 57-50-3, FIG 12.SDR GAIA04138Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME AT BS 660 ABOVE STR17,16 RT, DENTED. REF FASI NR 86687, CUT OUT DAMAGED AREA DIM 1.0 X 2.25 AND 1.0 X 2.25. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.SDR GAIA04137Frame · dentedDURING C-CHECK INSPECTION FOUND MAIN CABIN FRAME BS 640 ABOVE STR 17, STR 16, RT DENTED. REF FASI NR 86686 CUT OUT DAMAGED AREA DIM 1.0 X 3.50. INSTALLED ANGLE REPAIR IAW SRM 51-40-3, FIG 1.
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