Boeing 757-224
Service difficulty reports · 3,821
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 CALA2025112111377Anti-Ice Valve · no discrepancyTIA VALVE LIGHT WITH EICAS WHEN THRUST IS BELOW 30 N1 ON TAXI NORMAL INDICATION PER CONDITIONS DESCRIBED. NO FURTHER ACTION NEEDED. IAW AMM 30-21-00.SDR CALA2025112011370Fitting · corrodedL4 DOOR EXTERIOR HANDLE BOX HAS EVIDENCE OF CORROSION. REMOVED AND REPLACED NEW L4 DOOR EXTERIOR HANDLE BOX IAW B757-200 AMM 52-11-13-902-015 SFR NUMBER 2418 REF.138842SDR CALA2025112411424Pan · dentedREMOVED AND REPLACED HANDLE PAN AT L4 DOOR EXTERIOR IAW SRM 51-40-02-0G-0, DRAWING 146N6100. REMOVED AND REPLACED HANDLE PAN WITH P/N: 146N6201-5, BATCH:NUMB ER 0004442259 AT L4 DOOR EXTERIOR LAW SRM 51-40-01-0G-D , DRAWING 146N6100.SDR CALA2025112411422Web · corrodedAFT CARGO COMP. RT BS 1380 S23R TO S20R FOUND WEB WITH CORROSION. REMOVED AND REPLACED WEB BTW BS 1380 TO 1360 S22R IAW SRM 51-40-02-0G-0 AND DWG 146N8533 DOOR.SDR CALA2025112011358Mechanism · out of adjustL2 BOARDING DOOR WILL NOT CLOSE KNUCKLE KNOCKER HANGS UP. OTHERWISE DOOR 2L OPERATES AND SLIDE ARMS NORMALLY. REQUEST MEL. DDP COMPLIED WITH. MEL APPROVED FOR KNUCKLE KNOCKER HANGS UP HANGS UP AT DOOR 2L. PLACED IN MEL. *DM* SEE AMM TASK 52-11-20-825-001 & 52-SDR CALA2025111811323Pan · groovedL4 DOOR EXT DOOR HANDLE PAN HAS GROOVE WORN IN THE SURFACE, 3.5 INCHES LONG AND 1/32" DEEP. ALSO ONE GROOVE FWD OF THE HANDLE 2.5" LONG AND 1/64" DEEP BACKSIDE HANDLE HARDWARE. GROOVE DEPTH MEASUREMENT ACCOMPLISHED BY SKILL 105. AFT GOUGE DEPTH MEASURES AT A SDR CALA2025112011361Fitting · corrodedWHILE WORKING NR 138452 FOUND EXTRA HOLE AND EXCESSIVE CORROSION ON FITTING BENEATH ANCHOR PLATE STA 620 FWD CARGO DOOR ENTRY SILL. REF NR 138507. ESFR CREATED. REMOVED AND REPLACED FITTING IAW B757-200, SRM 51-40-02-06-0SDR CALA2025111811286Bracket · corrodedLOWER FUSELAGE BS 900 APPROX LBL 6, TEE CHORD AND BRACKET HAVE CORROSION. CORROSION ON BRACKET AND TEE CHORD WAS REMOVED, BRACKET FOUND WITH IN LIMITS IAW SRM 53-00-71-1A AND TEE CHORD WAS REPAIRED IAW SRM 51-70-12-0G.SDR CALA2025111711274Stiffener · corrodedEXFOLIATION DAMAGE ON THE LOWER END AFT SIDE OF THE BS 1180 WHEEL WELL BULKHEAD STIFFENER, LOCATED AT LBL 53.96. THE REPAIR INCORPORATED VIA ECRA 5340-02246 FUSELAGE BULKHEAD STATION 1180 WHEEL WELL STIFFENER. REMOVED THE AIRCRAFT FROM SERVICE.SDR CALA2025112011353Girt Bar · fodR2 DOOR WILL NOT ARM. REMOVED FOD FROM UNDER GIRT, SLIDE ARMS AND DISARMS NORMAL. IAW AMM 52-11-01.SDR CALA2025111711273Frame · dentedONE DENT ON THE BS 1560 FRAME BOTTOM, BETWEEN S26L & S27L. THE DENT MEASURES 0.750 INCH LONG, 0.600 INCH WIDE, AND 0.020 INCH DEEP. THIS DENT IS THE SUBJECT OF EA 5310-07582 AND ALSO AD 2020-05-25 PERFORM INSPECTIONS PER PART 2 OF THE LATEST REVISION OF ECRA SDR CALA2025111411216Inlet Door · corroded(SDR)(B757-MP-2000-53-1-0026) THROUGH ACCESS PANEL 311AL APU INL ET DOOR LOWER STRAP BETWEEN 1787 TO 1825 WITH EXFOLIATION DOT 07 -024. REF NR 134577. SFR REPORTING ONLY FABRICATED APU INLET DOOR STRAP IAW SRM 53-80-15-2R. REPLACED NE W INLET DOOR APU STRAP IASDR CALA2025111311168Light · brokenFOUND EMERGENCY EXIT PATH LIGHT PANEL BROKE ON ROW 32 ABC. ADJUSTED EMERGENCY EXIT PATH PANEL AS REQ, OPS CHECK GOOD. OK TO CONT.SDR CALA2025111111136None · no discrepancyFWD CABIN CALL LIGHT ON OVERHEAD PANEL NOT LIGHTING UP WHEN CALLED, ALSO NO EICAS CABIN CALL RESET FLIGHT ATTENDANCE PHONE L1 DOOR LIGHT, AND EICAS MESSAGE IN FLIGHT DECK OPERATE CORRECTLY IAW AMM 23-19-00NSDR CALA2025111111133Cam · out of adjustLEFT FWD ENTRY DOOR ARMING LEVER IS VERY STIFF, HARD TO ARM COMPARED TO RT IAW.AMM TASK 52-25-825-01, CHECKED L1 DOOR ARMING MECHANISM. CHECKED GIRT BAR SLIDE LOCKS, BOTH OPERATED NORMALLY WHEN ARMING AND DISARMING. GIRT INSTALLED CORRECTLY. SUSPECT LINKAGESDR CALA2025111111104Fuel Tank · corrodedDURKING OK TO INSTALL OF FLOOR PANEL, FOUND BETWEEN BS 984 - 996 BELOW ACCESS PANEL 242BF, EXFOLIATION IN THE LOWER SURFACE. REF NRC 135215. REMOVED CORROSION ON UPPER SURFACE OF FUEL TANK SKIN BETWEEN BS 989 - 996 IAW SRM 51-10-02, SRM 57-10-01, REPAIR APB-1SDR CALA2025111711272Fitting · crackedCRACK DAMAGE ON THE OTBD SIDE, FWD LOWER FLANGE OF MID BULKHEAD FITTING OF THE NR 2 STRUT ASSY AT PPS 174.30. THE CRACK EXTENDS FROM THE FWD EDGE OF FLANGE TO THE FWD FASTENER HOLE THROUGH ENTIRE MATERIAL THICKNESS.SDR CALA2025111711271Frame · dentedONE DENT REPORTED DURING C CHECK ON THE LT BS 680 FRAME, BETWEEN S23L & S24L. THE DENT MEASURES 0.700 INCH LONG, 0.500 INCH WIDE, AND 0.015 INCH DEEP. INTERIM REPAIR PERFORMED AS PER ECRA 5330-07645 PART1.SDR CALA2025111711270Frame · dentedDURING C-CHECK, REPORTED ONE DENT ON BS 1280 FRAME BOTTOM, BETWEEN S26R AND S27R. THE DENT MEASURES 1.20 INCH LONG, 0.92 INCH WIDE, AND 0.024 INCH DEEP. INTERIM REPAIR PERFORMED AS PER ECRA 5360-02051 PART1.SDR CALA2025111711269Frame · crackedWHILE ACCOMPLISHING INSPECTION PER EA 5311-01827, NOTED CRACK ON THE LT BS 1640 FRAME BETWEEN S14L AND S15L. THE CRACK STARTS AT FREE FLANGE OF THE INBD CHORD AND PROPAGATES INTO THE WEB. PERFORMED INSPECTIONS PER PART 2 OF THE LATEST REVISION OF ECRA 5360-SDR CALA2025111111128Line · out of positionDOOR 1R WONT ARM SURVIVAL STATIC LINE GOT TANGLED IN THE GIRTBAR MECHANISM. UNTANGLED AN STOWED PER AMM 25-66-10-402-022, FIG 204.SDR CALA2025111211165Frame · dentedFWD CARGO BAY FRAME BS 680, DENTED. REPAIRED FWD CARGO FRAME AT BS 680, S23L IAW EC/RA 757-5330-13 -A4168.SDR CALA2025111211155Frame · dentedAFT CARGO BAY BS 1280 BETWEEN STRINGERS 26R TO 27R DENTED. REPAIRED THE FRAME BS 1280 S26R-27R IAW EA 757-5360-13- A4160.SDR CALA2025111211153Frame · dentedBULK CARGO BAY, FRAME HAS A DENT ON LOWER LOBE, BS 1560, LT SIDE, NEAR S26L. REPAIRED BULK CARGO IAW EA 757-5360-13- A4162.SDR CALA2025111011098Fitting · crackedNUMBER 2 PYLON OTBD SIDE THROUGH ACCESS PANEL 443CR, LOWER CORNER OF PP STA 174 WITH EVIDENCE OF A CRACK. REPAIRED THE PYLON OTBD SIDE BULKHEAD FITTING IAW EA 757-5450-13-A4151 AND EC/RA 5450-03064 REV-.SDR CALA2025111011049Tee Angle · corrodedEXTERNAL LOWER FUSELAGE BS 900 TEE ANGLE LBL 6 WITH CORROSION. TEE ANGLE BS 900 WAS REPLACED IAW SRM 51-70-11- OG.SDR CALA2025111011047Fitting · crackedL4 DOOR UPPER FITTING CRACKED. REMOVED AND REPLACED UPPER FITTING ON L4 DOOR IAW SRM 51-40-02-06-0SDR CALA2025111011045Floor Support · crackedAFT CARGO COMPARTMENT CEILING AREA BS 1420- 1440, RBL. 0.05 INTERCOSTAL FLOOR SUPPORT CRACKED. REMOVED AND REPLACED CLIP ANGLE ON AFT PIT STA 1420 TO STA 1440 BL.0.SDR CALA2025110710988Bulb · inoperativeEMERGENCY LIGHTS LH WING EXIT FOUND LIGHT NOT ILLUMINATING REPLACED 2 BULBS PN 1317 REF 33-50-00.SDR CALA2025111011036Bracket · crackedDURING REMOVAL OF TEE FITTING AT BS 900, FOUND ONE ANGLE BRACKET WITH A CRACK AT LBL 5. REMOVED AND REPLACED BRACKET (CLIP) ON TEE FITTING IAW SRM 51-40-02-OG AND DWG 149N7130.SDR CALA2025110610966Intercostal · corrodedFWD CARGO BAY BETWEEN BS 740 - 760, STR 28L-29L, INTERCOSTAL HAS EVIDENCE OF CORROSION. R & R THE INTERCOSTAL IAW SRM 51-40-02-06 & DWG 143N5355.SDR CALA2025110510925Fanwheel · seizedENG EGT 941 2 MIN AFTER NORMAL ENG START. LOCKED FOR POSITIVE FIX PER CREW COMMENT, #1 ENGINE STARTED NORMALLY, THEN 2 MINUTES AFTER ENGINE START EGT SPIKED. CREW IMMEDIATELY SHUTDOWN ENGINE. ON VISUAL EXAMINATION, EXHAUST HAS NO DEBRIS, THE FAN DISK IS SSDR CALA2025110410867Sensor · out of adjustSENSOR ON TOP OF FLIGHT DECK DOOR NEEDS ADJUSTMENT. CAUSES DIFFICULTY OPE NING AND CLOSING. ADJUSTED MAGNETIC SENSOR TRAGET AND VERIFIED FWD ENTRY LIGHT CHECK GOOD, REF AMM 52-52-01-800-801-C10.SDR CALA2025110610960Skin · crackedLEFT WING, SLAT NR 1, INNER SURFACE, ABOVE INBD TRACK, CLOSE TO WS 735, SKIN CRACKED. REMOVED, FABRICATED, & INSTALLED LT WING INNER SKIN IAW SRM 51-40-02, REINSTALLED SLAT NR 1 IAW AMM 27-81-02-424-021.SDR CALA2025110610958Skin · crackedLEFT WING, SLAT NR 2, INNER SURFACE, ABOVE OTBD TRACK, CLOSE TO WS 675, SKIN HAS A CRACK. REMOVED AND REPLACED THE INNER SKIN IAW SRM 51-40-02-0G-0. REINSTALLED THE NR 2 SLAT IAW AMM 27-81-02-024-001, & 27-81-02 424-021.SDR CALA2025110610956Stiffener · corrodedAFT CARGO COMP, FWD BULKHEAD, REAR SIDE, STIFFENER BS 1180, LBL 53.96 HAS EXFOLIATION ON LOWER AREA. REPAIRED IAW EC/RA 5340-02246 AND EA 757-5340-13-A4169 REV-.SDR CALA2025110610954Skin · crackedLEFT WING, SLAT 3, INNER SURFACE, ABOVE INBD TRACK, SKIN CRACKED. REMOVED, FABRICATED & INSTALLED LH WING SLAT #3 INNER SURFACE SKIN IAW SRM 51-40-02, & MAE TRAVELER T25/1836170. REMOVED AND REINSTALLED THE SLAT IAW AMM 27-81-02-024-001, & 27-81-02-424-021SDR CALA2025110410902Warning Message · illuminatedRIGHT CENTER FUEL PUMP STILL DISPLAYS ON FLOW BAR WHEN DESELECTE D PRESS LIGHT NOT ON MECHANICAL WINDOW THAT SHOWS/HIDES FLOW BAR INOP. PULLED AND COLLARED R FUEL OVRD PUMP BREAKER ON P6. INSTALLED TAPE OVER CENTER FUEL PUMP RIGHT SWITCH, WHEN CLEARING DEFERRASDR CALA2025110310854Girt Bar · out of adjustR1 DOOR SLIDE INDICATOR LIGHT NOT ILLUMINATED. ADJUSTMENT GIRT BAR MECHANISM AND CLEANED THE R1 DOOR IAW AMM 25-66-00. OPS CHECKED ARMED - DISARMED LEVER. POSITION SATISFACTORY. OK TO CONTINUE.SDR CALA2025110210826Intercostal · corrodedFWD CARGO BAY, BETWEEN BS 740 - 760, S27L-28L, INTERCOSTAL HAS EVIDENCE OF CORROSION. REMOVED CORROSION IAW SRM 51-10-02-OG, EVALUATED DAMAGE (ORIGINAL THICKNESS 0.032") REMAING TH 0.022" FOUND TO BE OUT OF LIMITS IAW SRM 53-30-04-01-1 T88093, INTERCOSTAL ANDSDR CALA2025110310852Girt Bar · out of adjustL4 DOOR WILL NOT ARM, GIRT BAR WAS CLEANED ON FLOOR AND ADJUSTED MECHANISM IAW AMM 25-66-00. OPS CHECKED ARMED-DISARMED LEVER, DOOR SLIDE WAS SATISFACTORY. OK TO CONTINUE.SDR CALA2025111211139Strap · crackedEA 5311-01827 REV F - CRACK FOUND AT FLANGE RADIUS LOCATED AT THE INTERCOSTAL STRAP AT S14L AT FR 1640. ACCOMPLSIHED EC/RA 5360-02050 AND EA 757-5360-13 A4156 PRELIMINARY 1.SDR CALA2025103110790Service Door · missingLEFT LAVATORY SERVICE DOOR MISSING, DEFERRED REF LOGPAGE CDL 6683578.SDR CALA2025103010737Computer · failedFLIGHT CONTROLS TOO HARD IN FLIGHT.DEBRIEF CREW ON ARRIVAL FLIGHT CREW REPORTED ON TAKE OFF THE ELEVATOR WAS HARD TO PULL BACK ALSO THE AILERONS AND RUDDER HARDER THAN NORMAL TO MOVE. NO EICAS MSG OR OTHER FAULTS SHOWING IN FLT OR ON GND FOLLOWING CONSULTATIONSDR CALA2025102810630Light · no discrepancyEMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCH PROCEDURE - EMERGENCY LIGHT INOP ABOVE SEAT 3DEF/ 4DEF. REPLACED LIGHT ASSY NO HELP, NEED MORE TIME TO T/S, REQUEST MEL 3351A APPROVED COMPLIED MEL 3351A, STICKER APPLIED. PERFORMED EMERGENCY LIGHTS OPERSDR CALA2025102810621Arming Lever · stiffDOOR 4L ARM LEVER DOESNT MOVE FULLY INTO DISARM POS. DOOR SHOWS DISARMED CREW REPORTED DOOR 4R HARD TO DISARM. CYCLED GIRT BAR, NO DEFECT NOTED REF AMM 25-66-01SDR CALA2025102710576Floor Support · crackedE/E FLOOR STRUCTURE OF THE PASSENGER CABBIN BETWEEN BS 395 TO 418 CROSSBEAM 0, SUPPORT CHANNEL WITH EVIDENCE OF A CRACK. REMOVED AND REPLACED SUPPORT P/N141N5191-1 IAW SRM 51-4 0-02-0G, RESTORED SURFACE PROTECTION AT SUPPORT IAW AMM 51-21-15-370-801, & AMMSDR CALA2025102410483Lever · unknownDOOR 2L ARM LEVER WOULD NOT FLIP TO ARM AFTER DOOR CLOSED BUT WORKED AFTER CREW CYCLED DOOR. L2 DOOR SLIDE ARMED/DISARMED SATIS ON GND IAW AMM 52-11-00.SDR CALA2025102310453Target · lack of lubeDOOR 1L NOT INDICATING OPEN, LUBERCATED DOOR 1L PROXIMITY SWITCH TARGET PLATE SHAFT. OPS CHKD GOOD.SDR CALA2025102310440Support Strap · corrodedAFT CARGO COMP, BEHIND RH SIDE PANEL, BTW STA 1360 AND STA 1380, STRAP SUPPORT HAS CORROSION AROUND NUTPLATES. REMOVED SUPPORT ANGLE BTW BS 1360 - 1380 IAW SRM 51-4 0-02. REMOVED FOR ACCESS TRANSITION PANEL IAW SRM 51-40-02. INSTALLED NEW PART IAW SRM 5 1
Back to Boeing 757-224