Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 UALA2012010400091Blade · damagedON WALKAROUND, FOUND BLADE DAMAGEED ON ENGINE NR 2. REPAIRED NR 2 ENGINE FAN BLADE PER AMM.SDR UALA2012010300037Floor Panel · damagedAFT GALLEY FLOORING PEELING UP NOT ALLOWING CARTS TO BE PULLED OUT. MAINT TEXT: APPEARS TO BE LOTS OF MOISTURE UNDER FLOOR PAN AT REAR CART NEXT TO AFT LAV, REMOVING FLOOR PAN TO DETERMINE CONDITION OF FLOORBOARD UNDERNEATH. ALSO LOOSE FLOOR PAN UNDER 2ND CASDR UALA2012010300021Slide · dislodgedR3 DOOR SLIDE FELL DOWN ON DOOR SILL. DOOR SLIDE INSTALLED PER AMM. INSPECTED INSTALLATION PER AMM. OBSERVED ALL STEPS OF INSTALLATION FOLLOWED PROPERLY. DOOR ARMING AND DISARMING OBSERVED TO BE WORKING PROPERLY.SDR UALA2012010300020Thermocouple · openFOUND NR 2 ENGINE EGT THERMOCOUPLE T4.9 PROBE AT 10 O'CLOCK POSITION OPEN. REPLACED THERMOCOUPLE PROBE PER AMM.SDR UALA2012010400104Blade · damagedLEFT ENGINE HAS DAMAGE ON LEFT FAN BLADE. INSPECTED FAN BLADE-NO CRACKS OR TEARS. DAMAGE IS 5.25" IN FROM MID-SPAN. DAMAGE IS .031 DEEP. FIGURE 603 DAMAGE IS IN AREA 8. PER PAGE 609. BLENDED DAMAGED BLADE AS REQUIRED.SDR UALA2012010300025Bonding Strap · looseBONDING WIRE BROKE LOOSE ON T/E FLAP. REMOVED DAMAGED SEAL FROM LT INBD CANOE. REPLACED SEAL.SDR UALA2012010300068Sign · missingR4 DOOR MISSING EXIT SIGN. REPLACED EXIT SIGN LENS COVER.SDR UALA2012010300067Lanyard · out of positionL4 DOOR WILL NOT ARM. MOVED LANYARD OUT OF WAY OF DOOR. DOOR ARMS NORMALLY.SDR UALA2012010300006Coupling · leakingFUEL LEAKING FROM NR 1 ENGINE. FOUND FUEL LEAKING FROM COUPLING O-RING. REMOVED GAMA COUPLING FOUND SEALING SURFACES GALLED. MM 28-22-07 PG 617 ITEM (D). REMOVED FUEL LINE FROM FWD SPAR TO THE NEXT FWD COUPLING. INSTALLED TUBE ASSY WITH NEW PACKINGS. LEAK SDR UALA2012010300005Feeder Cable · damagedEMERGENCY LIGHTS INOPERATIVE. REPAIRED EMERGENCY LIGHT FEEDER CABLE AND LIGHTS CHECKED OKAY.SDR UALA2012010300002Light · inoperativeONE GREEN EEL STRIP LIGHT SEAT ROW 11 INOPERATIVE. FOUND PINS BROKEN ON LIGHT STRIP. REPLACED PART #36262-4 PCN 560-0806 LIGHT STRIP AND CHECKED OPERATION.SDR UALA2012010300063Socket · dirtyENGINE BOTTLE 1 DISCHARGE LIGHT STILL NOT TESTING CORRECTLY. SWAPPED LIGHT CAPS, PROBLEM STAYS WITH NR 1 BOTTLE, CHECKED SECURITY OF CONNECTORS AT FIRE CONTROL PANEL, ALL SECURE. RETURNED LIGHT CAPS TO ORIGINAL POSITION. CLEANED SOCKET AND PIN CONTACTS ON LISDR UALA2012010300062Sensor · malfunctionedAIRCRAFT FAILED ALTERNATE EXTEND TEST. RIGHT NEEDLE GOES TO APPROXIMATELY 12 DEGREES WHEN KNOB TURNED TO 1 DEGREE POSITION. TEST THAT FAILS IS JOB CARD 5-5010-B STEP 6D3. THE REST OF TEST PASSED. CHANGED RELAY K1024 4. SWAPPED & RETURNED FSEU2 AND FSEU3. SDR UALA2012010300061Light · looseEMERGENCY EXIT LIGHT PULLED UP FROM FLOOR IN FRONT OF FWD CLOSET. SECURED EMERGENCY LIGHT, CHECKED OK.SDR UALA2011123007165Switch · dirtyCREW REPORTS SLIDE ARM LIGHT AT DOOR 1R IS INOPERATIVE. CLEANED SWITCH AND OPS CHECKED NORMAL.SDR UALA2011123007167Packing · leakingLEFT WING FILL VALVE LEAKING 6 DROPS PER MINUTE AT THE MOUNT OF THE VALVE. REPLACED PACKING'S, OP'S AND LEAK CHECKED NORMAL, NO DEFECTS NOTED, PER AMM.SDR UALA2012120407046Skin · damagedEXTERNAL FUSELAGE SKIN CREASED BETWEEN BS 1380 TO 1400 AND STR 27R-28R. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER AND INSTALLED BETWEEN BS 1380 TO 1390 AND AFT CARGO DOOR FORWARD LOWER CORNER OF CUTOUT PER REO G14379,SDR UALA2011122907154Skin · damagedEXTERNAL FUSELAGE SKIN CREASED BETWEEN BS 1380 TO 1400 AND STR 27-28R. MAJOR REPAIR ACCOMPLISHED. REMOVED DAMAGED SKIN AND FABRICATED A REPAIR DOUBLER, STRUCTURAL FILLER, AND FILLER AND INSTALLED PER REO G14379, REV. C.SDR UALA2011122807141Arm · out of adjustL1 DOOR UPPER FORWARD TORQUE TUBE ROLLER IS HITTING HARD ON THE UPPER FWD LATCH CAM AND NEARLY FALLING OUTSIDE OF CAM, FALSE LATCHING. ADJUSTED GUIDE ARM AND OPS CHECK GOOD.SDR UALA2011122807140Engine · making metalAFTER NR 1 ENGINE START, LT ENGINE OIL FILTER EICAS AND STATUS MESSAGES, FOLLOWED FM PROCEDURES. MX REPORTED METAL IN MAIN OIL FILTER, ANGLE GEARBOX CD, MAIN GEARBOX CD AND ON NR 1, 2, & 3 BEARING CD, REPLACED LEFT ENGINE PER AMM.SDR UALA2011123007162Wire · brokenSLIDE LIGHT EXTINGUISHED IN CRUISE DOOR 1R. ALL OTHER ARMING INDICATIONS NORMAL. REPLACED LIGHT ASSSY, NO HELP. SUSPECT GIRT BAR PROXIMITY SWITCHES. FOUND WIRE W3682-B-PA BROKEN IN SIDE WALL APPROXIMATELY 24 INCHES DOWN. OBSERVED CORROSION ON BROKEN END. RESDR UALA2012010300049Relay · failedCOCKPIT AIR NOISE IS VERY LOUD. CHECKED FLIGHT DECK NOISE LEVEL PER SERVICE TIP 21- 22-00 PAGE 902 STEP 7. NOISE LEVEL INDICATED A GREATER THAN 3DB CHANGE WHEN RT RECIRCULATION FAN WAS SELECTED. FOUND THE RIGHT PACK STUCK IN HIGH FLOW. REPLACED CONTROL VASDR UALA2011122907151Angle · corrodedAFT FUSELAGE INTERNAL ABOVE CONSTANT BOX UPPER BULKHEAD, LOWER ANGLE, JUST BELOW APU DUCT IS CORRODED AT BS 1862, AND RBL 17 TO RBL 19. REMOVED BS 1862.7 LATERAL STRUCTURE AND REMOVED CORROSION BETWEEN RBL 10 AND RBL 17 ON UPPER SURFACE OF THE HORIZONTAL FLANSDR UALA2011122707115Oil System · overservicedAPU QUIT AFTER ONE ENGINE START WITH FAULT ILLUMINATION. FOUND OIL OVER SERVICED. PROPERLY SERVICED, OPS CHECKED GOOD.SDR UALA2011122807134Control Unit · malfunctionedAT 6500 FT LE DEVICES WOULD NOT EXTEND. RETRACTED FLAPS ELECTRICALLY. SELECTED ALTERNATE TO MOVE FLAPS WITH NO L/E MOVEMENT. REPLACED FSEU-2 PER MM, SYSTEM OPERATES.SDR UALA2011122707116Engine · hung startHUNG START ON LEFT ENGINE. SECOND START UNSATISFACTORY. 3RD ATTEMPT MADE WITH IGNITION IN BOTH. ENGINE HANGS AT 60% N2 AND WILL NOT ACCELERATE TO IDLE. NO LIMITS EXCEEDED. STARTER CUTOUT WAS NORMAL. REFER TO MM 73-21-00 FIG 111 ON PG125 FOR FAULT ISOLATION. FSDR UALA2011122707114Feeder Cable · burnedNR 1 ENGINE IDG PHASE C, FEEDER CABLE AND THRU LEAD FOUND BURNED DURING PRELIMINARY INSPECTION. REMOVED & REPLACED IDG. REPLACED NR 1 IDG POWER FEEDER CABLE PHASE C TERMINAL LUG & HEAT SLEEVE. OPS CHECKED IAW AMM.SDR UALA2011122707119Feeder Cable · damagedEMERGENCY LIGHTS INOPERATIVE. SPLICED FEEDER CABLE AND SECURED. OPS CHECKED OKAY.SDR UALA2011122707118Threshold · damagedCARGO DOOR SCUFF PLATE HAS DENT AND CRACK BETWEEN THE 5TH AND 6TH SCREW ATTACHMENT FROM FRONT OF AIRCRAFT AT TOP OF SCUFF PLATE. DENT IS 1. BY .50 WITH A CRACK IN THE DIAMETER OF THE DENT MEASURING .75 INCHES LONG. THRESHOLD REMOVED. TRANSFERRED ALL HOLES SDR UALA2011122707117Adc · malfunctionedALTITUDE AND IAS DISAGREE. CAPTAIN`S AIR DATA SWITCH SELECTED RESTORES PROPER INDICATIONS. FOUND LEFT ADC FAULTING LEFT AOA, FOUND LEFT AOA STIFF, AND BINDING. REPLACED LEFT AOA AND LEFT ADC, OPS CHECKED GOOD. COMPLETED CAT III TEST 30, TESTED GOOD.SDR UALA2011122707113Pan · gougedDOOR 1 LEFT HANDLE PAN IS GOUGED BELOW EXTERIOR DOOR HANDLE. FOUND IT OUT OF LIMITS OF SRM. REMOVED & REPLACED HANDLE PAN ASSEMBLY.SDR UALA2011122707112Pan · gougedDOOR 4 LEFT HANDLE PAN IS GOUGED BELOW EXTERIOR DOOR HANDLE. FOUND IT OUT OF LIMITS. REMOVED & REPLACED HANDLE PAN ASSEMBLY.SDR UALA2011122307094Compressor · stalledRT ENG COMPRESSOR STALL, RTFL. RIGHT ENGINE HAD COMPRESSOR STALL DURING T-O CLIMB AND LANDING (REVERSE) SAMC TEXT: ESN 726514. CHECK PER FIM. SEAMM REPORTS DURING HPC BORESCOPE EXTENSIVE DAMAGE TO HPC-6 (1EA. HALF THE BLADE MISSING AND DAMAGE TO SUBSEQUENT SSDR UALA2011122307092Control Unit · faultyAC YAW AT HIGH SPEED. REPLACE RUDDER AND MONITOR PRINTED CIRCUIT UNIT CARD ASSY DUE TO BOTTOM RUDDER PCA FAILING TEST. RPLC'D CARD ASSY PER MM & TESTED SYSTEM. OPERATES PROPERLY. IN ADDITION, LOWER RUDDER PCU IS STILL NOT PASSING. CARD WAS CHANGED AS A PRESDR UALA2011122707129Compressor · stalledAIR RETURN DUE TO RIGHT ENGINE COMPRESSOR STALL DURING TAKE OFF, CLIMB AND LANDING. CHECKED PER MM. REPLACED ENGINE.SDR UALA2011122207055Blades · damagedFAN BLADES ON NR 2 ENGINE ARE DAMAGE. ACCOMPLISHED BLEND REPAIR ON FAN BLADE LE TIP.SDR UALA2011122307081Floorbeam · corrodedPAX CABIN MAIN DECK FLOORBEAM 324 RBL 42 HAS CORROSION. MAJOR REPAIR ACCOMPLISHED. INSTALLED SPLICE REPAIR ON UPPER CHORD REF ECRA 5310-05426. WORK ACCOMPLISHED ON SCAL NR 9955650.SDR UALA2011122307079Structure · corrodedPAX CABIN MAIN DECK FLOOR CORROSION AT STA 365 BL 0 TO RBL 63. MAJOR REPAIR ACCOMPLISHED. ACCOMPLISHED UPPER CHORD SPLICE REPAIR REF EC-RA 5310-05427. WORK ACCOMPLISHED ON SCAL NR 9955656.SDR UALA2011122307080Pan · gougedDOOR 2 LEFT HANDLE PAN IS GOUGED BELOW THE EXTERIOR HANDLE. FOUND GOUGE TO BE OUT OF LIMITS PER B757 SRM 52-10-01. INSTALLED NEW HANDLE PAN IAW B767 SRM.SDR UALA2011122207074O-Ring · failedLEFT HYD SYS INOPERATIVE, RETURNED TO FIELD. LOW QUANTITY. REPLACED LE SLAT BYPASS VALVE. FOUND O-RING ON FITTING DESTROYED. SERVICED HYD TO FULL CYCLED ALL FLIGHTS CONTROLS, NO LEAKS NOTED.SDR UALA2011122207073Bottle · failedEMERGENCY ESCAPE RIGHT SQUIB DOES NOT ILLUM ON TEST TWO. MAINT TEXT: SHOULD READ, FAILED TEST 2 BOTTLE PRESSURE TEST. VERIFIED RIGHT OVERWING ESCAPE BOTTLE PRESSURE IN AFT CARGO PIT FWD WALL PER MM. VERIFIED PRESSURE AT 2700 PSI. TO BE REPAIRED WITHIN 50 FSDR UALA2011122207064Fuse · defectiveNR 2 REAR BRAKE COLD ON ARRIVAL. DE-ACTIVATED NR 6 BRAKE PER MEL 3241A. ANTISKID MODULE CAP STOWED IN FLIGHT DECK WITH LANDING GEAR PINS. REPLACED HYD FUSE, OPS CHECK GOOD PER MM AND RE-ACTIVATED SYSTEM FROM MEL3241A.SDR UALA2011122207060Slide · unserviceableLT OVERWING SLIDE IS UNRAVELED. RMV'D & RPLC'D LT OVERWING SLIDE PER MM ON NON ROUTINE 29126.SDR UALA2011122107030Slide · detachedDOOR 4R SLIDE IS DETACHED FROM DOOR. SLIDE HAS NOT DEPLOYED. REPLACED SLIDE ASSY PER AMM (PRECAUTIONARY).SDR UALA2011122107016Light · inoperativeNR 4 LT MAIN ENTRY DOOR EMER EXT LIGHT, INOPERATIVE. RELAMPED, OPERATES NORMAL.SDR UALA2011122107015Light · inoperativeNR 2 MAIN ENTRY DOOR EXT EMER LIGHT INOPERATIVE. RELAMPED (RT) OPERATES NORMAL.SDR UALA2011122107008None · noneDOOR 1L ENTRY HANDLE RISES INFLIGHT APPROX 2 INCHES". PERFORMED DOOR LATCHING INSPECTION PER AMM. ALL CHECKED GOOD. CHECKED DOOR LOCKING AND GIRT BAR OPERATION ALL CHECKS GOOD.SDR UALA2011122107014Unknown · leakingCREW REPORT: DARK FLUID DRIPPING 1 DROP EVERY 10 SECONDS FROM LEFT ENGINE. SAMC TEXT: REF AMM 71-71-00 (601) FOR ENGINE DRAINS LEAK RATE LIMITS, IDENTIFY LEAKY COMPONENT, NOTIFY OPBLM TOMC-EMC WITH FINDINGS. OPBLM EMC 20DEC11. CREW ACCOMPLISHED LEFT ENGINESDR UALA2011121906962Engine · power lossABORTED TAKEOFF AT 140 KIAS FOR NR 1 ENGINE ROLLBACK WITH FUEL FLOW FLUCTUATIONS. CAPTAIN NOTICED THE NR 1 FUEL FLOW DROPPING OFF JUST PRIOR TO PULLING THROTTLE BACK. DID NOT NOTICE ANY OTHER PARAMETER FLUCTUATION.SDR UALA2011121906980Screw · missingSCREW MISSING ON OTBD FLAP ASSY OTBD SIDE AFT PART ON LEFT WING. REPLACED MISSING SCREW ON RIGHT O/B TE FLAP FAIRING.
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