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 CALA2024070300112Stringer · handler errorJET BRIDGE MALFUNCTIONED AND CONTACTED FUSELAGE, FOUND DENT AT STRINGER 16L APPROX 4 FEET FROM LEFT WING INSPECTION LIGHT PICS UPDATE WITH MEASUREMENTS DAMAGE IS FORWARD OF THE L2 DOOR. DENT FOUND TO BE ON STRINGER 16L @ STATION 611 (SEE SRM 53-00-01-1A-1 SHESDR CALA2024071102004Adc · inoperativeFO AIRSPEED + 5KTS AND ALTITIDE +200 FEET DIFFERENCE FROM THE CAPTAIN. CREW BELIEVES THE CAPTAIN SIDE IS CORRECT CREW DEBRIEF 1ST OFFICER SELECTED ALT. AIR DATA SOURCE SELECT F/O,CAPT,STBY INDICATED SAME. VISUAL INSPECTED PITOT AND STATIC PORTS NO FAULT NOTE, SDR CALA2024070300113Flap System · faultedTE FLAP DISAGREE EICAS B A FLAP POSITION DOES NOT AGREE WITH THE FLAPS POSITION SELECTION FLAPS AT 20 WHEN HANDLE SELECTED TO 25 SDR SELECTED FOR GO AROUND FOR FLAP ISSUE TROUBLESHOOTED PER B757 FIM 27-51 FAULT TREE 808. FSEU BITE C/OU T. NO EXISTING FAULTS ONSDR CALA2024070101935Adc · intermittentLEFT AND RIGHT EEC INS IN THE ALTERNATE MODE EEC BIT #1&2 BOTH HAVE F0 D6 ED. PERFORM FIM 73-21TREE802 AND AMM 73-21-00-902-001-R01 #1&2 EEC BITE BOTH #1&2 NO FO FAULTS NOW F1 FAULT D6. ENGINES BOTH FO D6 FAULT INDICATES DIFFERENCE OF 252 FT. ALT L/R ADC''S RSDR CALA2024070201952Transmission · trippedTE FLAP DISAGREE EICAS B A FLAP POSITION DOES NOT AGREE WITH THE FLAPS POSITION SELECTION FLAPS AT 20 WHEN HANDLE SELECTED TO 25 SDR SELECTED FOR GO AROUND FOR FLAP ISSUE TROUBLESHOOTED PER B757 FIM 27-51 FAULT TREE 808. FSEU BITE C/OU ANSMISSION. RESET OVERLOSDR CALA2024070101940Gate · corrodedEA 5210-03219 REV A - CORROSION ON DOOR GATE 4L DOOR. NO DOT.() REMOVED AND REPLACED LOWER GATE AT DOOR L4 IAW B757 AMM 52-11-38 -004-001 AND B757 AMM 52-11-38-404-009.SDR CALA2024070101941Gate · corrodedEA 5210-03219 REV A - CORROSION ON DOOR GATE, DOOR 4R. REMOVED AND REPLACED LOWER GATE AT DOOR R4 IAW B757 AMM 52-11-38 -004-001 AND B757 AMM 52-11-38-404-009.SDR CALA2024062801923Fmc · faultedAUTO PIILOT/ A/T FMC FAILURE MULTI TIME CURRENT FAULTS PER MCDP BITE FOR PREV FLT FAULTS ARE A/P CTN FMC L-R CH PERFORMED MCDP TEST 1 (FCC), 10 (A/T) AND 30 WITH NO DEFECTS - 34-61-00 WITH NO DEFECTS. A/C REMAINS FULL CAT QUALIFIED. T/S DIAG CODES 110081, 120SDR CALA2024062701911Transition Panel · corrodedSUPPORT TASK: AFT CARGO COMPT, L/H TRANSITION PANEL AT 1360, FOU ND EXFOLIATED CORROSION REMOVED AND REPLACED TRANSITION PANEL STA 1310 TO 1410 LH 526L D UE TO EXCEED ALLOWABLE DAMAGE LIMITS IAW B757-200 SRM 53-00-5-1A -1, SRM 51-40-02-0G, BOEING BWG 146N5391,SDR CALA2024062500098Warning Message · illuminatedCABIN ALT MSG RECEIVED AT FL370. STARTED DESCENT BUT PUT MODE S ELECT TO AUTO 2. GOT CABIN BACK. *DM* MX NOTE. NO FAULTS FOUND ON #1 & #2 CABIN PRESSURE CNTLS REF AMM 21-30-802. PRESSURISED A/C IN MANUAL MODE. OPERATION TEST GOOD IN MANNUAL MODE REF 21-31-00-SDR CALA2024062501889Tee Angle · corrodedWING TO BODY STA 900 T CHORD BTW RBL 10 TO LBL 10 FOUND EXFOLIATING CORROSION REPAIR COMPLETED ON ST ENGINEERING N/R 102148 PER SRM 51-70-12-09-0SDR CALA2024062701910Spring · brokenPDA 1 REFERENCE 8393440, DURING ETOPS CHECK FOUND R/H MAIN LANDING GEAR DOWNLOCK SPRING BROKEN. HOOK END OF R-MLG DOWN-LOCK ASSY BROKEN SPRING DEPARTED AIRCRAFT SIZE IS ABOUT 3/16 IN DIA AND 2 IN HOOK END LENGTH. ITEM TO BE REPLACED UNDER LOGPAGE 8393440. CLOSSDR CALA2024062601899Spring · brokenREFERENCE 8393440, DURING ETOPS CHECK FOUND R/H MAIN LANDING GEAR DOWNLOCK SPRING BROKEN. NEED TO REPLACE REF AMM INSTALL THE DOWNLOCK SPRINGS FOR THE MAIN LANDING GEAR REFERENCE: TASK 32-11-22-404-007 R/H MAIN LDG DOWNLOCK SPRING REPLCED IAW AMM REF 32-11-22SDR CALA2024062500088Spring · defectiveDURING ETOPS CHECK FOUND R/H MAIN LANDING GEAR DOWNLOCK SPRING BROKEN HOOK END OF R-MLG DOWN-LOCK SPRING BROKEN OFF. MAJOR REPAIR.SDR CALA2024062401882Aileron Sys · unknownAILERON AND AILERON TRIM CONTROL AILERON (01=L,02=R,03=L&R) PROBLEM WAS ENCOUNTERED BY THE FLIGHT CREW WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS 03 AILERON CONTROL INPUT FORCE SEEMS EXCESSIVE DURING TAKEOFF ROLL AND IN FLIGHT PILOT STATES FORCE IS ESPECISDR CALA2024062400064Skin · canningDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR, PERFORMED INTERIM REPAIR PER ECRA 5330-07276 PART 1 STEPS 1-4. REF EC/RA 5330-07276 PERFORMED HFEC SURFACE INSPECTION IAW NDT PART 6 51-00-19, NO CRACKS DETECTED. PERMANENT REPAIR COMPLETED SDR CALA2024061901874Heat Shield · damagedAMES NR 171629-0400-0013. REMOVED, REPAIRED, AND REINSTALLED #2 PYLON AFT MOST HEAT SHIELD IAW EX/RA 5452-01005 AND B757 SRM 51- 40-02 PARA 4. SEE PARTIAL WORK ON BACK AND PARTIAL WORK SHEET 16 PAGE 1 OF 1 FOR WORK COMPLETION.SDR CALA2024061801856Skin · dentedREF AMES NON ROUTINE 171629-0100-0043. GENERATING ITEM:19-0640-1 -2100.DENT ON FUSELAGE SKIN AT STA 1400 S-25LSDR CALA2024062601905Skin · dentedDURING WALK AROUND FOUND DENT IN A PREVIOUS REPAIR FWD OF L2 DOOR. ACCOMPLISH PART 3 PERMANENT REPLAIR WITHIN 2 FLIGHT CYCLES PER ECRA 5330-07276. PER ECRA 5330-07276 "ACCOMPLISH PART 3 PERMANENT REPAIR WITHIN 2 TOMC-APPROVAL FROM SC1ELBYC COMMENT FLIGHT CYCLSDR CALA2024060701733Indicator · bindingTE FLAP DISAGREE STUCK AT 20 UPON CREW DEBRIEF FLAP INDICATOR STUCK AT 20 AT SHUTDOWN POWER FSEU # 28N011-40, NO FAULTS FOUND ON 2/3. FSEU 1 FLAP DISAGREE INSTALLATION TEST AMM 27-58-02-704-010.ALL CHECKED GOOD. X-FER INDICATOR WENT TO PILOT REQUESTED 25. INSPSDR CALA2024060701712Stiffener · buckledREF AMES NON ROUTINE 171415-0400-0044. GENERATING ITEM:ZONE 430 OPEN.FEED BACK CABLE COVER PLATE IS BENT AND CRACKED TAG#6936. REPAIRED NO.1 ENGINE O/B T/R FEEDBACK CABLE SUPPORT STIFFENER P/ N LJ70309 IAW AMES DOCUMENT 47618REA03, DATED 6/4/2024 UNITED EC /RASDR CALA2024060701713Strap · crackedREF AMES NON ROUTINE 171415-0100-0024.GENERATING ITEM B757-06-3- 0228: FLOORBEAM STRAP IS CRACKED, LOCATED IN LEFT TUNNEL OF MEC, FRAME STA. 377.7 AND LBL 26 (MARKED WITH STREAMER 70878). CATEGORY A REPAIR. NO ADDITIONAL SUPPLEMENT INSPECTIONS REQUIRED . REMOVSDR CALA2024060301665Radome · delaminatedREVIEW ALL DISCREPANCIES RECORDED AND INITIATE SFR/SDR REPORTS AS REQUIRED. {B757-05-3-0003} - SDR TO BE RAISED POST RADOME REPLACEMENT DUE AIRCRAFT BEING OUT OF SERVICE PER GMM 04-20-16 PER GMM 04-20-16 SDR BEING RAISED DUE TO AIRCRAFT BEING OUT OF SERVICE SDR CALA2024060301664Coupling · leakingR HYD QTY EICAS DURING CRUISE F360. RAN CHKLST THEN GOT R HYD SY S PRESS R QTY IS NOW .14 FOUND SELF SEALING COUPLING LEAKING HYDRALIC ON ENGINE 2, REMOVED REPLACED SELF SEALING COUPLING PER AMM 29-11-00. OPS CHECK GOOD, NO LEAKS.SDR CALA2024053101653Warning Message · illuminatedON CLIMBOUT RECEIVED YELLOW REV ICON ABOVE RIGHT ENGINE EPR GAUG E REQUEST MEL FOR RIGHT ENG THRUST REVERSER INOP. PLACED RIGHT ENG T/R ON MEL DDP CW. RIGHT ENGINE THRUST REVERSER DEACTIVATED I.A.W. MEL 7831F. MEL AND DDP REQUIREMENTS CONTAINED IN 7831F COMPSDR CALA2024060301671Lamp · inoperativeEMER LIGHT NEAR AFT DOOR R NOT ON DURING TEST RELAMPED 767 BULB. WORKS OK NOW.SDR CALA2024052901600Warning System · false indicationGEAR DOORS CAUTION ON GEAR EXTENSION. THREE GREEN LIGHTS. GEAR DOORS WENT AWAY AFTER GO AROUN CREW DEBRIEF REPORTS GEAR DOOR CAUTION LIGHT ILLUMINATED ON GEAR EXTENSION. ALL THREE GREEN LIGHTS ILLUMINATED. GEAR DOOR CAUTION LIGHT EXTINGUISHED ON GO AROUND. REPSDR CALA2024060401696Bracket · brokenNUMBER 2 INBOARD TR FWD HOLD OPEN SUPPORT CLIP BROKEN. REMOVED BROKEN CLIP (BRCKET) ASSY AND INSTALLED NEW BRACKET ASSY IAW SRM 51-40-02.SDR CALA2024060401698Plate · crackedREF AMES NON ROUTINE 171415-0500-0009. GENERATING ITEM: 171415- 0500-0001. RT WING TE TRANSITION WIGGLE PLATE CRACKED. LOCATED JUST I/B OF #8 SPOILER. TAG# 34152 REMOVED OLD AND INSTALLED NEW WIGGLE PLATE IAW BH757-200 SRM 51-40-02.SDR CALA2024060401697Plate · crackedLEFT WING TE TRANSITION WIGGLE PLATE CRACKED. LOCATED JUST I/B AND BELOW #5 SPOILER. REMOVED OLD AND INSTALLED NEW WIGGLE PLATE IAW B757-200 SRM 51-40-02.FOR MORE DETAILS UNITED FORM # 46-0024 SSFR C/W.SDR CALA2024052301565Steering Sys · faultedA/C PULLED HARD RIGHT ON INITIAL T/O ROLL AROUND 35 KTS REPEAT W RITE UP CALM WINDS. STEERING IS NORMAL AND SMOOTH ON TAXI. ON TAKE OFF SHIP REACHING CLOSE TO 40KNOTS, AIRCRAFT PULLED HARD RIGHT. USED FULL LEFT RUDDER- NO HELP. ULTIMATELY, APPLIED BRAKES. BRAKSDR CALA2024053101652Metering Valve · inoperativeON TAXI AND T/O ROLL AIR CRAFT HAD STRONG LEFT TU RN BIAS. T/O R OLL REQRD ABNORM AMT RT RUDR/0WI PER FIM 32-51 FAULT TREE 802 STEP 1 LUBRICATED THE NOSE LANDING TAXIED AIRCRAFT WHEN TILLER IS RELEASED AC DRIFTS TO THE LEFT STEERING COLLAR , AND CHECKD ALL LANSDR CALA2024052001510Landing Gear · lack of lubeLOW SPEED REJECT APPROX 60 KNTS. A/C PULLED SIGN IFICANTLY TO TH E RIGHT. ENG SPOOL CLOSE TO EVE PER FIM 32-51 FAULT TREE 802 STEP 1 LUBRICATED THE NOSE LANDING AIRPLANE TAKEN OUT TO TAXI, NO NOTICED PULLING LEFT OR RIGHT. STEERING COLLAR , AND CHECKD ALL LANSDR CALA2024052001517Warning Message · illuminatedL ENG BLEED OFF CAS AFTER ENG START BLEED PSI PULSING UP AND DO WN 15 PSI DEBRIEF CREW. LEFT ENG BLEED PULSING AT ENG START WITH BLEED OFF INDICATION. EVEN WHEN ADDING POWER STILL PULSING. EVENTUALLY BLEED OFF INDICATION EXTINGUISHED BUT ENGINE BLEED STILL FLSDR CALA2024052001504Sensor · faultedCOCKPIT AND CABIN UNCONTROLABLE 100DEG TO 16 DEG LOCKED FOR POSITIVE FIX TOOK RESISTANCE VALUES FOR TS198, TS200 AND TS01, ALL VALUES T/S IAW 757 FIM 21-51 FT 803 COMPLETED UPTO AND INCLUDING BLOCK COMPARABLE TO RIGHT SENSORS. SINCE LEFT PACK CONTROLLER STILL SDR CALA2024051401469Oven · odorMID GALLEY OVEN #305 HAS A BURNING SMELL WHEN OPERATING. MID GALLEY OVEN HAS A BURNING SMELL WHEN IS WORKING. NO SMOG COMPLIED WITH NEF DISPOSITION. OVEN AT MID GALLEY INOP AND DETECTED. REQUEST NEF PLACED ON NEF NOC DATE: 13-MAY-24- TOMC APPROVES NEF 2520P OVSDR CALA2024051301432O-Ring · wornON TAKE OFF ROLL LOST LEFT HYDRAULIC SYSTEM QUANTITY FROM UPPER 90S TO .43 AND DROPPING. FOUND FLAP AND SLAT DEPRESSURIZATION MODULE PLUG LEAKING. REF 40-0595-3-1985,QTY :1 IPC 27-51-29-01 ITEM 160. REMOVED AND REPLACED PACKING ITEM 165TORQUED TO SPECS AS REF SDR CALA2024050701389Fuse · blownEXIT/SALIDA EMERGENCY LIGHT INOP AT LAV S. VERIFIED OPS OF LIGHTS CHECKS GOOD. REMOVED AND REPLACED EMERGENCY LIGHT LAMPS REF AMM 33-51-10 REMOVED AND REPLACED FUSE ON M10919 REF AMM 33-51-07-962-071,SDR CALA2024050601326None · noneBIRD STRIKE NOTED DURING WALK AROUND ON LH WING ROOT, JUST BESIDE LANDING LIGHT BIRDSTRIKE CLEANED AND AREA INSPECTED IAW AMM 05-51-18 REV 133 20JAN24. NO DAMAGE NOTEDSDR CALA2024050801411Compressor · stalledL ENGINE COMPRESSOR STALL ON DEPARTURE AMM TASK 71-00-00-715-049-R03 & TEST NO 13 PER TASK 71-00-00-715-223-R03. ESCPP ROHAN ATTACHED PIC OF E1 EGT AUTO EVENT. ENGINEERING UPDATE: PERFORM FIM TASK 71-06 FAULT TREE 812, "ENGINE SURGE AND RECOVERY". PERFORM BLOSDR CALA2024042601246Lamp · inoperativeFLIGHT ATTENDANT CALL LIGHT FOR AFT RIGHT LAV DOES NOT STAY ILLU MINATD RE-LAMPED OPS CHECKS GOODSDR CALA2024042401221Transition Panel · dentedDURING OK TO INSTALL AFT CARGO TRANSITION PANEL S26LH AND STA 14 00 UPPER SKIN FRAME WITH DENT. EVALUATED FRAME AT STA 1400 S26LH IAW B757-200 SRM 53-00-07-1A1, INSTALL NEW REPAIR SECTION AT STA1400 526 LA IAW B757-200 SRM 53 NO DENTS ALLOW ON FLANGE THEREFORESDR CALA2024042201184Oil Cap · leakingL ENG LOST OIL QTY. COUPLE OF SECONDS LATER L EG OIL PRESS LIGHT CAME ON. OFF. REPLACEMENT. NEW OIL FILLER CAP LOCKS SECURELY. CREW DEBRIEF HE STATED HE NOTICE ON CLIMBOUT OIL QTY STARTED TO SUSPECTED LOOSE OIL CAP, SUGGEST REPLACEMENT OF THE GRAVITY ALSO SUGGSDR CALA2024042201183Oil Cap · detachedLEFT ENG LOST OIL QTY. COUPLE OF SECS LATER LT ENG OIL PRESS LIGHT CAME ON. NEW OIL FILLER CAP LOCKS SECURELY. CREW STATED, NOTICE ON CLIMBOUT OIL QTY STARTED TO SUSPECTED LOOSE OIL CAP, SUGGEST REPLACEMENT OF THE GRAVITY ALSO SUGGESTED REPLACE OF HOUSING FISDR CALA2024042901263Sense Line · leakingL ENG BLEED OFF EICAS MSG ON TO ROLL REJECT TO AT APPROX 75KTS PERFORMED HEALTH CHECK ON FAN AIR MODULATING VALVE REF. TO AMM 36-00-23-705-153-001. FAN AIR TEMPERATURE SENSOR FAILED THE HEALTH CHECK. RECOMMENED CHANGING THE FAN AIR TEMPERATURE SENSOR. FOUND SESDR CALA2024042301203Handle · bindingDOOR-MOUNTED ESCAPE SYSTEM DOOR 1R - A EVACUATION SLIDE PROBLEM WAS ENCOUNTERED WHICH IS NOT COVERED IN THE FAULT CODE DIAGRAMS ARMING LEVER BINDING. EXCESSIVE FORCE NEEDED TO MOVE LEVER TO AR MED POSITION CLEANED DEBRIS FROM BOTTOM DOOR SILL WHERE GIRT BAR ENSDR CALA2024042201163Oil System · low quantityON THE TAKE OFF ROLL WE RECEIVED A L GEN DRIVE LIGHT ON STATIS MESSAGE. PER FLIGHT CREW REJECTED TAKEOFF SPEED WAS 85 KT. LEFT GEN. LIGHT STAYED ON. RETURN TO GATE FOUND LEFT IDG OIL LEVEL LOW WITH EICAS MESSAGE DISPLAYING THE SAME . SERVICED WITH 1.5 QTS PER SDR CALA2024041701120Oxygen Bottle · low pressureOXY PRESS 890PSI AT CRUISE. NEEDS SERVICING SDR FLAGGED BOTTLE, OXY, AI OFF 29-3511-9-9001 0589 ON 0000 BOTTLE, OXY, AI OFF 29-3511-9-9001 0589 ON 29-3511-9-9001 4831 DUE PREVIOUS HISTORY OF MULTIPLE CREW OXYGEN SERVICING, REPLACED CREW OXYGEN CYLINDER ASSY RESDR CALA2024041701115Skin · damagedNOSE FUSELAGE SKIN BETWEEN STA 333 TO STA 350 AND NEXT TO S23R WITH LIGHTNING STRIKE MARK. ACCOMPLISH PERMANENT REPAIR IAW B757-200 SRM 53-00-01-2R-28, REP AIR 28 FIG 202, NOSE FWD FUSELAGE SKIN, BETWEEN STA 333 TO STA S TA 350, AT S23R.SDR CALA2024041601112Oven · smokeAFT CENTER OVEN SMOKING IN FLIGHT SOURCE OF OVEN SMOKE IDENTIFIED GO TO STEP E (DISPOSITION OF EVENT). STEPS C AND D DO NOT NEED TO BE ACCOMPLISHED REF AMM SMOKE/ODOR IN THE FLIGHT DECK AND/OR CABIN CONDITIONAL INSPECTION (ADDED BY EC0500-01014) REFERENCE: TAS
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