Boeing 757-224
Service difficulty reports · 3,824
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 = '757224' 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 = '757224' 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 CALA2024082602271Support Angle · crackedCEILING AREA INTEROSTAL UPPER SUPPORT ANGLE CRACKED BETWEEN BS 1320 AND BS 1340 BL 0. REPLACED UPPER ANGLE SUPPORT AT STA 1320-1340 BLO IAW B757-200 S RM 51-40-02-0G-0 PARA 4 AND 7.SDR CALA2024082302259Frame · dentedGEN ITEM: GENERATING ITEM /// SUPPORT TASK FRAME DENTED AT STA 620 STRINGER 25L FOUND ON AGING AIRCRAFT INSPECTION.SDR CALA2024081902237Intercostal · corrodedINTERCOSTAL ANGLE AT STA 1480-1500 STR 27-26L FOUND CORRODED.SDR CALA2024081600442Pressure Switch · faultyCHECK LIGHTBULB IN OVHD BY ENTRY OF FLIGHT DECK LIGHT INOP AT THRESHOLD LIGHT OUTSIDE FLIGHT DECK. PHOTOS ADDED FOR LOC REF. REQUEST MEL 3321B FOR THRESHOLD LT OUTSIDE FWD LAV APPROVED MEL 3321B COMPLIED WITH RELAMPED (FWD LAV OUTSIDE CEILING BULB), OPS CHECSDR CALA2024081602229Skin · corrodedGENERATING ITEM: 19-5310-1-2576 APU DOOR EXTERNAL SURROUND STRUCTURE LIFTED AFT LWR.SDR CALA2024081902234O-Ring · leakingRIGHT HYD SYS PRESSURE LIGHT AND EICAS ELECTRIC HYDRAULIC PUMPS. ALL HYDRAULIC QUANTITIES NORMAL. AUTO EVENT ATTACHED, SHOWS RSVR PRESS HIGH ON ALL 3 SYSTEMS. DURING CLIMB OUT AT FL180, RIGHT HYDRAULIC PRESSURE LIGHT INDICATOR ILLUMINATED AND EICAS MESSAGE. NOSDR CALA2024081602227Pan · gougedL4 DOOR HANDLE PAN IS GOUGE ON THE INSIDE RADIUS REF AMES NR 172653-0800-0117 REMOVED AND REPLACED L4 DOOR HANDLE PAN IAW B757 CMM 52-11-25. I NSTALLED IAW B757 CMM 52-11-25 AND SRM 51-40-02 PARA 4 SEE BACK FOR PARTIAL WORK COMPLETED TAG #12486SDR CALA2024081502226Bracket · crackedPER CUSTOMER REQUEST FLC CLIP CRACKED @BS 840 BETWEEN STR 21L AND STR 22L. DOT 45014. MARINE V931875SDR CALA2024081502225Bracket · crackedFOUND FLC CLIP CRACKED @BS840 BETWEEN STR 21R AND STR 22R.SDR CALA2024081402206Intercostal · corrodedALC INTERCOSTAL HAS CORROSION BETWEEN BS 1480 AND BS 1500 STR 26R AND STR 27R.SDR CALA2024080900395Lavatory · fullAFT LAVS FLUSHED BROWN WATER WITH ODOR. ALL 4 LAVATORIES SERVICED AND PERFORMED OPS CHECK SATIS PER B757 AMM 12-17.SDR CALA2024080700386Adc · failedL AIR DATA COMP FAIL REPLACED LEFT ADC,,OPS CKS NORMAL..REF MM 34-12-01 AND 34-12-00..ALL TESTS AND INDICATIONS ARE NORMAL ACCOMPLISHED IDT PER GMM 09-10-05.SDR CALA2024081200406Unknown · unknownLOW SPEED REJECTED TO NO MORE THAN 35KTS FOR A/T DISC AT MCP ENG A AND TO DATA DELETED. PERFORMED AUTOFLIGHT FLIGHT FAULT BITE PROCEDURE AMM REFERENCE: 22-02 TASK 801 TEST 30 FOR AUTO THROTTLE DISC . NO FAULTS FOUND . AIRCRAFT REMAIN FULL CAPABILITY. ALSO PERFSDR CALA2024080800394Filter · leakingR HYD QTY EICAS DURING CRUISE. .45 QTY WITH RF FLAG SEE LOGPAGE 8848118 FOR DEFECT TROUBLESHOOTING AND RECTIFICATION.HYD LEAK FROM RIGHT PYLON. HYD SYSTEM IS AT .37% AFTER LANDING FOUND LARGE LEAK FROM RH PYLON. OPEN RH PYLON HYD BAY DOOR AND FOUND AREA VERY WSDR CALA2024080802181Gate · out of alignmentAFT ENT DOOR EICAS MESSAGE FL 360 PRESSURIZATION NORMAL HANDLE NOT IN NORM POS AFT ENTRY DOORS BOTH OUT OF RIGGED .HANDLE LOOSE ON BOTH DOORS . DOOR 4L. FOUND LOWER GATE CONTACTING SILL PLATE AT FORWARD TRIMMED 4L DOOR LOWER FWD CORNER TO OBTAIN PROPER CLEARENSDR CALA2024080700383Sensor · faultyINFLIGHT RT ENGINE BLEED OFF. RT CTR FUEL PUMP INOP. RT ENGINE N3 INDICATING 0 REMOVED AND REPLACED E2 TACHOMETER REF 77-12-02 AND FIM 77-12-805 PARTS USED: 19-7712-9-9001,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1928849 SN OFF 7761. INFLIGHT RT ENSDR CALA2024080702174Actuator · failedLEADING EDGE SLAT DISAGREE AFTER TAKEOFF, FLAPS STUCK BETWEEN UP & 1 UNTIL ALT SYS USE. PERFORMED T/S WITH TECH SUPPORT AND FIM 27-51 FAULT TREE 805 SLAT DISAGREE, FOUND MESSAGE #310, DURING INSPECTION FOUND L/E PDU OVERLOAD INDICATOR ON LT & RT PDU TORQUE LISDR CALA2024080500356Controller · faultyLEFT HYD ELEC PUMP EICAS C THE LEFT ELECTRICAL PUMP OUTPUT PRESSURE IS LOW EICAS MESSAGE. LT HYD ELEC PUMP OVRHD L ELEC HYD PUMP PRESS LT SPOKE WITH CREW, L/H HYD. PUMP PRESSURE IS AT 3010PSI, BUT L HYD ELEC PUMP MESSAGE POPPED UP ON EICAS AND ASSOCIATED "PRSDR CALA2024080602164Scuff Plate · damagedL4 DOOR FWD SCUFF PLATE CORNER FLATTENED ON RIDGE. DOESN''T ALLOW DOOR GATE TO CLOSE PROPERLY. (REF N/R 0800-0022). QC ACCEPTED. NOTE: THIS LOG PAGE WAS MARKED RII INADVERTENTLY. REMOVED AND REPLACED L4 DOOR FWD SCUFF PLATE WITH NEW P/N 146N610Y83 IAW B757 AMMSDR CALA2024080602162Scuff Plate · crackedL4 DOOR AFT SCUFF PLATE CORNER FLATTENED AND CRACKED ALONG TOP RIDGE. DOESN''T ALLOW DOOR GATE TO CLOSE PROPERLY. (REF N/R 0800-0022). REMOVED AND REPLACED L4 DOOR AFT SCUFF PLATE WITH NEW P/N 146N6104-59 IAW B757 AMM 53-13-01-424-003. SEE PARTIAL WORK ACCOMPSDR CALA2024080602168Pan · damagedL1 EXTERIOR DOOR HANDLE PAN GOUGED,AS MARKED AMES INSPECTOR V921207 BOUGHT THE FINAL INSPECTION. NONE L1 EXTERIOR DOOR HANDLE PAN DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED REPLACED AND INSTALLED PAN PN141N6302U3 IAW B757 SRM 51-40-02 PARA 4 AND 9. BOEING DRASDR CALA2024080602166Pan · damagedL4 DOOR EXTERNAL HANDLE PAN IS GOUGED IN MULTIPLE AREAS TO INCLUDE AT THE PRESS TO RELEASE BUTTON. L4 DOOR EXTERNAL HANDLE PAN DAMAGE FOUND TO BE OUT OF LIMITS DETAILS. REMOVED AND REPLACED AND INSTALLED PAN P/N -146N6201-7. IAW SRM 51-40-02 PARA 4 AND 9 AND SDR CALA2024080602163Skin · corrodedREPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC #47625REA02. REPAIRED CORROSION ON INTERNAL SKIN DOUBLER AT CUTOUT FOR PANEL 154AR IAW UNITED EC/RA 5300-03134 AND AMES DOC 47625REA02. SEE PARTIAL SDR CALA2024080202151Transmitter · faultyON APPROACH TE FLAP DISAGREE EICAS CAUTION DISPLAYED. FLAPS 25 S ELECTED.FLAPS AT 20. FLAP DISAGREE, INTERMITTENT TYPE, MESSAGE 305. PERFORMED GROUND VISUAL INSPECTION OF FLAPS, NO DEFECTS NOTED, HYDRAULICALLY RAN FLAPS TO ZERO & CYCLED DOWN TO 30 & BACK TO ZESDR CALA2024073100336Flex Line · faultyFLIGHT CREW STATES ON T/O WHILE BRINGING UP FLAP HANDLE NOTICED LT HYD QTY DECREASING, SELECTED BOTH LT EDP & LT ACMP OFF. LT HYD FLUID QTY NOW AT .15 PERCENT ON EICAS. AMM 29-11-00/201 CONDITION 1 TABLE 1. FOUND LEAK COMING FROM LT MLG DOOR ACTUATOR. FLEX LINSDR CALA2024080202150Selector Valve · faultedLEFT HYD QTY LT ON /AT .45 TURNED L ENG/ELEC OFF FAILED. HYD LEAKS FROM SAME LOCATION BETWEEN UNION AND SELECTOR VALVE. SUSPECT FAULTY SELECTOR VALVE. ACFT ARRIVED WITH .14 HYD QTY NO PUMPS ON. REMOVED LT HYD SYS PRESSURE IAW AMM 29-11-00. R & R UNION & PACKISDR CALA2024080100344Idg · faultyLEFT GEN OFF. RESET PER CHECKLIST AND GEN CAME BACK OFF AFTER RESETMX ENGINE IDLE RUN, FOUND L GENERATOR UNABLE TO ENGAGE, ATTEMPTS TO SWITCH TO L GEN POWER BUT KICKS BACK TO APU POWER AFTER A FEW SECONDS. PERFORMED BPCU BITE REF. FIM 24-20 FAULT TREE 801. MSDR CALA2024080100343Computer · faultyACFT DIVERTED WITH MULTPLE GPWS RELATED FAULTS REMOVED AND REPLACED THE GPWS COMPUTER REF AMM 34-46-01 LOADED CURRENT TERRAIN DB VERSION 640 REF AMM 34-46-00 OPS CHECKS NORMAL.PARTS USED: 64-3446-9-0002,QTY :1 PARTS USED: 64-3446-9-0002,QTY :1 ROTABLE PARTS CSDR CALA2024073000313Control Box · faultyRETURN TO FIELD. EPR WOULD NOT GO ABOVE 1.44 ON CLB CREW SAID THERE FELT TENSION ON THE TAKE OF POSITION ON THE LEFT THRUST HANDLE AND WHEN THE PILOT REMOVED HIS HAND THE THROTTLE PUSHED BACK ABOUT A KNOB, WHEN CHECKED HANDLE FELT TENSION ABOUT 3/4 OF THE WAY SDR CALA2024072902131Hydraulic Line · rupturedFLIGHT CREW STATES ON T.O. WHILE BRINGING UP FLAP HANDLE NOTICED LEFT HYD QTY DECREASING : SELECTED BOTH LEFT EDP AND LEFT ACMP OFF. LEFT HYD FLUID QTY NOW AT .15 PERCENT ON EICAS. SEE AMM 29-11-00/201 CONDITION 1 TABLE 1. FOUND LEAK COMING FROM LEFT MLG DOOR SDR CALA2024080602165Angle · corrodedLIGHT CORROSION FORMING AROUND NUTPL ATES ON LOWER SIDE OF ALC RT TRANSITION ANGLE FLOOR TO SLOPING SIDE WALLS, BS 1300 TO 1360 RBL 24. REMOVED AND REPLACED DAMAGED ALC RT TRANSITION PANEL BS 1300-1360 WITH NEW P/N 146N5391U182 IAW SRM 51-40-02 PARA 4 AND 7SDR CALA2024072900296Proximity Sensor · inoperativeEA 5210-03219 REV A, OPERATION 001 - DURING EMERGENCY LIGHT SLIDE MECHANISM CHECK GIRT BAR BREAKER POPPED OUT NONE PERFORMED TROUBLESHOOTING AND CONTINUED CHECK FOUND P/N 1 IN CONNECTOR D41706P GROUNDED FROM SLIDE LIGHT L1 RECONNECTED SLIDE LIGHT L1 DOOR IAW BSDR CALA2024080602169Bracket · corrodedCORROSION ON BOTH OF THE BRACKETS THAT HOLD THE LEFT OVERWING ESCAPE SLIDE RELEASE PIN INSIDE OF THE LEFT SLIDE COMPARTMENT.#3653 REMOVED AND REPLACED L/H OVERWING EXCAPE SLIDE RELEASE PIN BRACKET ASSY IAW B757 SRM 51-40-02 PARA 7. SEE PARTIAL WORK ACCOMPLISHESDR CALA2024072900301Limit Switch · faultySTAB TRIM CAUTIO ON CLMB OUT. AUTOPILOT CAUTION EICAS FOLLOWED 3 TIMESDEBRIEFED CREW AND WAS INFORMED THAT STAB TRIM CAUTION CAME ON PRIOR TO A/P ENGAGEMENT ON CLIMB. PERFORMED MCDP BITE IAW AMM 22-02 TASK 801; FOUND SEVERAL PREVIOUS FLIGHT LEGS A/P CAUTION MESDR CALA2024072402093Wedge · dentedB757-06-3-0324, RH WING SLAT #9 EDGE WEDGE UPPER SKIN INB AREA W ITH TWO DENTS. REPAIRED THE #9 SLAT IAW B757 SRM 51-70-10-2R-0SDR CALA2024072500283Hinge · damagedNOISE AND VIBRATION HEARD FROM 2L AFTER TAKEOFF UPON ARRIVAL WE FOUND THE LAV SERVICE DOOR BELOW DR2 L TO BE OPEN AND ONE HINGE IS DAMAGED. SEE PICTURES. MID LAV ACCESS PANEL DOOR WHICH IS LOCATED BELOW DOOR 2R HAS BEEN REMOVED. DRAIN VAVLE IS IN THE CLOSED SDR CALA2024072400277Light · intermittentAUTO LIGHT IN LAV 1L INTERMITENT REQUIRES TOO MUCH FORCE WHEN LOCKING DOOR TO TURN ON SUSPECT DOOR SWITCH, AUX AND DOME LIGHT OPERABLE. APPROVED NEF 3320AS COMPLY WITH DDP. FOUND LIGHT IN LAV 1L AND LOCKING MECHANISM TO BE OPERATING NORMALLY.SDR CALA2024080602167Bracket · corrodedTHERE IS CORROSION ON THE 2 STOWAGE BRACKETS FOR THE RIGHT OVERWING ESCAPE SLIDE RELE ASE CABLE PIN NO 3650. REMOVED AND REPLACED R/H OVERWING EXCAPE SLIDE CABLE RELEASE BRACKET ASSY P/N 416N2826-80 IAW B757 SRM 51-40-02 PARA 4. SEE AMES NON ROUTINE 173487-01SDR CALA2024072300272Hose · failedFOUND LH MLG DOWNLOCK ACT PRESSURE FLEX HOSE LINE FAILED AT ACT B NUT. (REF LP #8664494) REPLACED HYD PRESSURE LINE ON LH MLG DOWNLOCK ACT PER AMM 32-32-02-404-010 FOR HOSE REPLACEMENT. STILL REQUIRES FUNCTIONAL CHECK PER ITEM 3E (12).PARTS USED: 19-3232-3-00SDR CALA2024071600202Wire · unsecureCOACH CABIN, ALL FLOOR EMERGENCY PATH LIGHTS INOP. FOUND POWER SUPPLY M10919 SUPPLYING POWER TO ALL ROWS. FOUND WIRE L9043A18 FROM BATTERY M10699 STOWED BEHIND 12 ABC DADO PANEL. RE ROUTED TO 32ABC TO CONFORM TO DRAWING BR2013-P-7572C0-5 AND DRAWING BR2013-PSDR CALA2024071502017Computer · unserviceableLEFT AUTOPILOT INOP CENTER, NO FAULTS. PERFORMED TEST 30 IAW MM:22-00-02, NO FAULTS AT THIS TIME. PER FLIGHT CREW VERBAL, ALSO STATED THAT THE CENTER A/P ALSO NOTE, PSEU BOX HAD NO POWER AT THE SAME TIME THE MCDP GROUND DISCONNECTED THEN CAME BACK. MCDP GROUNDSDR CALA2024071502033Pump · damagedPER FLIGHT CREW DURING GEAR EXTENSION ON APPROACH LEFT HYDRAULIC SYSTEM WENT TO ZERO. DECLARED EMERGENCY. UPON ARRIVAL AT GATE FOUND LT HYD SYS ENG DRIVEN PUMP CASE DRAIN FILTER ASSY BROKEN OFF OF HOUSING. STARTED REMOVAL OF LT EDP (P/N# 7588587-103), REF REMOSDR CALA2024071102006Tire · failed#5 MLG TIRE BLOWN ON LANDING. REMOVED AND REPLACED #5 MAIN TIRE IAW BOEING 757 AMM 32-45-01.SDR CALA2024071001998Transition Panel · corrodedB757-53-3-0495 - CORROSION ON TRANSITION PANEL BS 640 STR26 (BELOW PANEL ON NUTPLATE AREA) DOT 46-27 CHECKED LIMITS FOUND EXFOLIATED CORROSION 100% MATERIAL LOST IAW AND AMM 51-00-59. B757-200 SRM 53-00-53-1A-1 NOTE C DETAIL V. REMOVED AND REPLACED SIDE PANEL SDR CALA2024071800249Tire · unknownPDA 1 REF LP 8545126: LAX REPORTED A MLG GEAR TIRE MAY HAVE DEPARTED THE AIRCRAFT. CREW OBSERVED AN ANTISKID EICAS ON TAKEOFF THEN WENT AWAY. CABIN CREW FELT A SHUDDER ON TAKEOFF PICS ONLY FLAGGED AS SDR SDR HAS BEEN CREATED REF SDR# 1036734 OIL SERVICE ACCOMPSDR CALA2024071102005Wheel · detachedPDA 1 REF LP 8545126: LAX REPORTED A MLG GEAR TIRE MAY HAVE DEPARTED THE AIRCRAFT. CREW OBSERVED AN ANTISKID EICAS ON TAKEOFF THEN WENT AWAY. CABIN CREW FELT A SHUDDER ON TAKEOFF.SDR CALA2024070801974Channel · crackedBROKEN STRUCTURE THAT ATTACHES CEILING PANEL RH SIDE OF AFT GALL EY AREA. REMOVED AND REPLACED SUPPORT CHANNEL IAW B757-200 SRM 51-40-02. TREATED AND PRIMED SUPPORT CHANNEL IAW SRM 51-20-01.SDR CALA2024070800157Heat Exchanger · damagedDEPARTED DEN WITH 90* TEMPS. JETBRIDGE AIR WAS NOT ADEQUATE TO COOL FD AND CABIN. USED APU AND PACKS. IN FLIGHT, FD AND AFT CABIN TEMPS WHERE IN TH HIGH 80'S. CREW RAN NON-NORMALS CABIN TEMP HOT 2.20.22 STEP 1 THROUGH 29 AND TEMPS DROPPED ABOUT 5* IN ABOUT 30 SDR CALA2024070300108Pressure Switch · unknownL HYD QTY 0 L SYS PRESS 0 L RSVR MSG ON HYD PG FLAGGING FOR SDR R&R L ENGINE HYD SYSTEM PRESSURE SWITCH REF B757 FIM 27-21 FAULT TREE 809, AMM 29-11-17-004-001. PERFORMED L ENGINE OPPS AND LEAK CHECK OF LEFT HYD SYSTEM, OPS CHECK GOOD. CLEANED LH HYD QTY INDISDR CALA2024070501965Hose · leakingFO ALTIMETER SPLIT FROM CAPTAIN. CAPTAIN SIDE IS CORRECT LOCKED UNLOCKED. PERFORMED FULL RANGE PITOT-STATIC LEAK CHECK & FOUND FO STATIC E2 RACK AFT SIDE DRAIN VLV LEAKING. REMOVED DRAIN VLV HOSE & CAPPED STATIC LINE, LEAK CHECK PASSED. REINSTALLED THE DRAIN
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