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 CALA2021012000059Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1701 BETWEEN STRINGERS S-20R AND S-21R. FOUND A PREVIOUS REPAIR OVER STRINGER 19R AFT OF STA 1701 APPROXIMATELY AND ABOVE TO DMG AREA. REMOVED REPAIR FOR ACCESS. COMPLIED WITH AVO 8767 STEPS 1 THRU 5 TO CONTINUE. HFEC CSDR CALA2021011500046Stringer · deformedSTRINGER S-21R IS DEFORMED AND DENTED BETWEEN STA 1701 AND 1720. CUT AND REMOVED STRINGER S-21R FROM STA 1681.8 +17 TO STA 1720, REFERENCE NEEDS TO BE UPDATED. AVO 8767 REV A STEP 17. REMOVED STRINGER CLIP AND SHEAR TIE FOR ACCESS. CUT AND REMOVED STRINGERSDR CALA2021011500045Stringer · damagedSTRINGER S-20R IS COMPLETELY SEVERED BETWEEN STA 1701 AND 1720 CUT AND REMOVED STRINGER S-20R FROM STA 1682.8 +17 TO STA 1720. REFERENCE NEEDS TO BE UPDATED AVO 8767 REV A STEP 16. REMOVED STRINGER CLIP AND SHEAR TIE FOR ACCESS. CUT AND REMOVED STRINGER S-2SDR CALA2021011100036Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1620 ABOVE S-20R. DAMAGE BETWEEN STRINGERS S-19R AND S-20R. REMOVED 25 EXISTING FASTENERS AROUND THE PERIMETER OF DAMAGE FOR REPAIR. COMPLIED WITH STEPS 1 THRU 5 OF AVO 8768. PERFORMED HFEC ON TRIM OUT, PER PT 6 51-00-SDR CALA2021011100035Skin · damagedA/C SUSTAINED DAMAGE JUST AFT OF STA 1701 BETWEEN STRINGERS S-20R AND S-21R. FOUND A PREVIOUS REPAIR OVER STRINGER 19R AFT OF STA 1701 APPROXIMATELY AND ABOVE TO DAMAGE AREA. REMOVED REPAIR FOR ACCESS. COMPLIED WITH AVO 8767 STEPS 1 THRU 5 TO CONTINUE. HFESDR CALA2021010600016Exhaust Valve · faultedLEVEL FL390 CABIN ALT SLOWLY CLIMBED TO 14000 AND CABIN PRESS WARNING CAME ON/MASKS DEPLOYED LEFT PACK OUTLET DUCT CLAMP LOOSE AT AT FWD END OF PACK, SECURED CLAMP. LEFT PACK OUTLET DUCT CLAMP LOOSE AT AT FWD END OF PACK, SECURED CLAMP. EQUIPMENT COOLING EXHSDR CALA2021010400007Pressure Switch · faultedAPU OIL QTY EICAS S THE APU OIL QUANTITY IS LOW NOTE: APU AUTO EVENT ALSO-APU OIL ADD ON EICAS STATUS PAGE ON ARRIVAL SERVICED APU OIL, RAN APU AND TWICE WAS AUTO SHUTDOWN. BITE THE CONTROLLER FAULTED LOW OIL PRESSURE SWITCH. REPLACE OIL PRESSURE SWITCH AND SDR CALA2021010100001Smoke Detector · faultedLAV SMOKE EICAS INFLIGHT. STILL SOUNDING AT GATE. NO VISIBLE SMOKE OR FIRE. RESET SMOKE DETECTOR IN FWD LAV, CHECKED GARBAGE BIN HEAT INDICATOR, NO DEFECTS NOTED. OK FOR SERVICE. REFRENCE L/P 5675559 FOR THE REPEAT WRITE UP, PREV WRITEUP FWD LAV SMK DET ASDR CALA2020120901353Pressure Switch · inoperativeRECEIVED C HYD SYSTEM PRESSURE LIGHT APPROXIMATELY 45 MINS INTO FLIGHT NORMAL C QTY AND PRESSURE. REMOVED AND REPLACED PRESSURE SWITCH S10003 SSM 29-00-04 AND AMM 29-11-00. OPERATIONS CHECK GOOD.SDR CALA2020112501302Filter · damagedPER FLIGHT CREW RIGHT HYD SYSTEM LIGHT ON, HYD QTY WENT TO 20% AT TAKE OFF. FOUND RIGHT HYD ENGINE DRIVEN PUMP CASE DRAIN FILTER HOUSING SEPARATED FROM MODULE. NEED MODULE ASSEMBLY. PRESSURE & CASE DRAIN OF THE ENGINE DRIVEN PUMP RIGHT SYSTEM, REF AMM 29-11SDR CALA2020110401243Seal · looseWHILE CLB THRU FL265 VERY LOUD PIERCING SQUEAL OCCURRED FROM CENTER LOWER AREA OF L2/L3 WINDOWS DEBRIEFED CREW. PER CAPTAIN LOUDEST SQUEAL IS EMINATING FROM LOWER PART OF L2 /L3 WINDOW HIGH PITCHED SQUEAL. REMOVED AND REPLACED L2 WINDOW PRESSURE SEAL, PER AMSDR CALA2020102301213Transmission · inoperativeON APPROACH WHEN FLAPS 1 WAS SELECTED WE GOT T/E DISAGREE EICAS. DID QRC LOCKED LP DUE TO TWO FLIGHTS IN A ROW HAVE DECLARED EMERGENCY ON LANDING FOR T/E DISAGREE. TOMC UNLOCK LOG FOR MAINT UPDATE, AS PER CREWS BRIEF, WHEN SELECT FLAPS FROM 0 TO 1 OPS NORMASDR CALA2020072001056Fairing · brokenPDA UPPER LEFT GENERATOR COMPESSOR GAS FAIRING BROKE OFF NR 2 ENGINE. DISCOVERED AFTER FLIGHT 675.SDR CALA2020071201048Transmitter · malfunctionedREPEAT WRITE UP - NO 2 EPR WENT BLANK W/ LOSS OF AUTOTHROTTLES.. DURING T/O ROLL T/S AIRCRAFT. CONFIRMED EPR INDICATION WENT OUT, CHECKED PREVIOU S WORK OF PE25 AT TB1 IS GOOD AT PIN2 D1368P OF EPR TRANSMITTER. SHOOK WIRES FROM EPR TRANSMITTER ALL ALONG TB1 ANSDR CALA2020040600790Skin · dentedFOUND DENT ON FUSELAGE ABOUT 3FT AFT OF L2 DOOR STA. 750 BETWEEN STR. 15L AND 14L DENT MEASURES TO BE W= 1.7 L=1.3 D= 0.67 REVISED DMG DIMENSIONS ARE L:4.5", W:4.0", D:0.112 DENT WITH GOU GE. ACCOMPISHED UT INSP TO DETERMINE SKIN THKNESS AFTER BLENDING TO BE ASDR CALA2020040300784Girt Bar · damaged(B757-52-3-0120) L-4 PASSENGER DOOR, GIRT BAR LEAF SPRING IS BEN T AND WILL NOT HOLD THE SLIDER FITTING. REF ST-SAA NR 0090239SDR CALA2020040300761Girt Bar · worn(SUPPORT TASK EA 2560-02123 REV D) R1 DOOR GIRT BAR FWD LEAF SPR ING FAILED MOVEMENT TEST - REF ST-SAA NR 0090035.SDR CALA2020032700718Frame · dented(B757-20-3-0082) DENT ON AFT CARGO FRAME UPPER FLANGE AT STA 150 0 BETWEEN STR 25L - 26L. REF ST-SAA NR 0090312 MEASURED DENT L= 1" W= .700" Y= .025 FOUND TO BE OUT LIMITS PER B757-200 SRM 53-00-07 FABRICATED AND FORMED 1 EA REPAIR J SECTIO N, LOCATED AND DRILSDR CALA2020032700706Stringer Clip · not reported(B757-20-3-0082) STRINGER CLIP 26L AT STA 1500 AFT CARGO REQUIRE FABRICATION IAW B757-2 SRM 53-00-07 REPAIR 5 FIG 201 PG204. REF ST-SAA NR 0090472. FABRICATED STR CLIP 26L AFT CARGO COMP STA 1500 PER DWG 140N2001 AND B757-2 SRM 53-00-07 LOCATED AND DRILLED STRSDR CALA2020032700704Stringer Clip · not reported(B757-20-3-0082) STRINGER CLIP 25L AT AFT CARGO STA 1500 REQUIRE FABRICATION IAW B757-2 SRM 53-00-07 REPAIR 5 FIG 201 PG204. REF ST-SAA NR 0090471 FABRICATED STR CLIP 25L AFT CARGO COMP STA 1500 PER DWG 140N2001 AND B757-2 SRM 53-00-07 LOCATED AND DRILLED STR SDR CALA2020032700695Angle · corroded(B757-53-3-0593) APU AIR INLET HOUSING FUSELAGE CUTOUT STRUCTURE HAS CORROSION AS VIEWED THRU ACCESS 311AL. REF ST-SAA NR 009004 9. REMOVED CORROSION AT APU AIR INLET HOUSING FUSELAGE CUTOUT STRUC TURE; UPPER ANGLE L=1.5 W=.30 D=.063. LOWER ANGLE L=2.0 W=.50 DSDR CALA2020032100681Girt Bar · defective(SUPPORT TASK EA 2560-02123 REV D) L2 DOOR GIRT BAR FWD SLIDER F AILED MEASUREMENT CHECK. REF ST-SAA NR 0090036 REMOVED AND REPLACED L2 DOOR GIRT BAR PN 140N2762-17 IAW B757-2 AMM 25-66-10-002-001 AND AMM 25-66-10-402-022. OPS CHECK GOOD AN D ADJUSTMENT IAW B7SDR CALA2020032100670Stringer · dentedREFERENCE LOGPAGE 8418473 - UPON DVI FOUND FUSELAGE STRINGER AT STA 750 L-15 DENTED BEHIND L-2 DOOR. REF ST-SAA NR 0090408. DENT AT FUSELAGE STRINGER 15L STA 750 MEASURED L=2.5 W=1 D=.040 A/Y=25. FOUND TO BE OUT OF LIMITS IAW B757-2 SRM 53-00-03 FIG 10 1 DETAISDR CALA2020032100662Transmitter · faultyAUXILIARY POWER UNIT EICAS MESSAGE APU OIL QTY DISPLAYED AND OIL QTY READS ADD (ON AIRPLANES WITH OIL QUANTITY TRANSMITTER) INDICATION ON STATUS PAGE ON CLIMBOUT THEN 0.25 OIL QUANTY SHOWS AT CRUISE REQUEST MEL 4994B. APU OIL VERIFIED FULL AT SIGHT GLASS APU VSDR FDEA2020031760574Skin · gougedFUSELAGE EXT SKIN STA 1400 TO 1440 AND FROM S30 TO S26L HAS SEVERAL PREVIOUS BLENDS AREA REPAIRED PER EA # F-5310-T0352664 P1SDR CALA2020032100658Pan · gouged(B757-06-3-0358) L1 PASSENGER DOOR, EXTERNAL HANDLE PAN IS GOUGE D. REF ST-SAA NR 0090255. MEASURED DEPTH OF GOUGE ON L1 PASSENGER DOOR EXTERNAL HANDLE PAN TO BE .020" FOUND OUT OF LIMITS IAW B757-2 SRM 52-10-01 FIG 101 AD1. REMOVED AND REPLACED L1 DOOR PAN HASDR CALA2020032100646Seal Depressor · dentedB757-06-3-0354 FWD CARGO DOOR, AFT SEAL DEPRESSOR IS DENTED, AS MARKED. REF: ST-SAA NR 0090285 REMOVED AND REPLACED SEAL DEPRESSOR OF FWD CARGO DOOR AFT SIDE I AW B757-2 DWG 143N6603 REV B AND SRM 51-40-02 PG2 & 3. WORK ACCO MPLISHED. INSPECTED.SDR CALA2020032100647Pan · cracked(B757-52-3-0122) R1 PASSENGER DOOR EXTERNAL HANDLE PAN IS GOUGED . REF ST-SAA NR 0090204. DUE TO CRACK, REMOVED AND REPLACED R-1 DOOR EXTERNAL HANDLE PAN IAW B757-200 SRM 51-40-05 AND B757-200 SRM 51-40-02 PAGE 21 FIG 4 AND DWG 141N6200 REV F. THIS IS TRANSCRISDR CALA2020030600571B-Nut · looseL HYD QTY EICAS C THE LEFT HYDRAULIC RESERVOIR QUANTITY IS LOW NOTE: HYD AUTO EVEN T W/ L PUMPS OFF IAW CHKLST QTY HELD AT 0.37 FOUND #3 SPOILER RETURN LINE B NUT LOOSE,TIGHTENED B NUT OP CHECKED FLIGHT CONTROLS NO LEAK NOTEDSDR CALA2020022900548Valve · inoperativeFLT DECK TEMP EXCEEDS 99 DEGREE. TRIM AIR SWITCH POSITION OFFN O HELP REMOVED AND REPLACED TRIM AIR PRESSURE REGULATING VALVE REF AMM TASK 21-61-06-404-036 OPS CHECK AND LEAK CHECK REQUIRED. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1400978 SN OFF 1554 VALVSDR CALA2020022400492Line · leakingGEAR DOOR EICAS MESSAGE LOST L HYD RESEVOIR FOUND RH MLG TRUCK POSITION PRESSURE LINE LEAKING. LINE LOCATED NIS SFO. TOP OF LANDING GEAR. M&E 19-3232-3-0118. P/N BACH8A04EE0557B. REF IPC 32-32-51-16A ITEM 247. REMOVED HYDRAULIC LINE AND CLEANED AREA. OPTIONALSDR CALA2020022400469Skin · dentedTHE LOWER FUSELAGE HAS A DENT AT THE 6 O CLOCK POSITION BELOW THE FORWARD CARGO DOOR S-29L TO 29R (BETWEEN STA 580 - 600) DOT 48-003 REF AAR N/R 9733007 EVALUATED DENT AT LOWER FUSELAGE SKIN BETWEEN STA 580 & STA 600 S-29L TO S-29R DENT MEASURES L=2.300" W=1.6SDR CALA2020022400461Skin · corrodedFWD LAVATORY SERVICE PANEL IS BULGING AT RIGHT AFT CORNER AND ALSO HAS A RIVET HEAD PULLING THROUGH. REMOVED FWD LAVATORY SERVICE PANEL AFT R/H CORNER HAS CORROSION,BURNISHED CORROSION REF SRM 51-10-10. SKIN IS .080 THICK REF SRM 53-10-10 . NEED TO VERIFY HOW SDR CALA2020021200399Skin · damagedWHILE PERFORMING WALK AROUND, ON NO.2 ENGINE PYLON NEAR EXHAUST AREA FOUND PULLED PANEL, HEADS OF SCREWS UNABLE TO SECURE IT. PULLED PANEL IS LOCATED ON OUTBOARD AREA ON ENGINE NO.2 ENGINE UPON FURTHER INSPECTION, DIAMETER OF HOLES ON PANEL ARE ENLARGED CAUSINSDR CALA2020020300310Unknown · unknown#6 BRAKE REQUIRES CHANGE DUE ANTI SKIP REMOVED AND REPLACED #6 BRAKE IAW AMM 32-41-10 NO DEFECTS NOTED AIRCRAFT OK TO CONTINUE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1015201 SN OFF 0901 BRAKE, MLG, ATA OFF 53-3241-9-0002 0901 ON 53-3241-9-0002 1120 INSPESDR CALA2020020200281Frame · dentedB757-06-3-0230 DENT ON FWD CARGO FRAME UPPER FLANGE STA 660BETWE EN STRINGER 24 AN STRINGER 25 (034-038) LH SIDE REF ST ENG N/R 0 085668 FOUND DENT OUT OF LIMITS IAW B757-200 SRM 53-00-07 FIG 101 L=1.1 0, W=.90, D=.047. CUT OUT DAMAGE AND ACCOMPLISHED CATEGORYSDR CALA2020020100269Web · dentedB757-06-3-0366 L-4 PASSENGER DOOR, INTERNAL WEB IS PUNCTURED AT UPPER HINGE CAVITY. (96-03) REF ST ENG N/R 0085414 REPAIRED L4 PASSENGER DOOR INTERVAL WEB SKIN AT HINGE CAVITY IAW ECRA 5210-03049.SDR CALA2020012600224Pan · dentedSUPPORT TASK EA 5210-01360 REV J OP 001 SECONDARY FINDING UPON R EMOVAL OF THE L-1 EXTERNAL DOOR HANDLE, DISCOVERED A DEEP GOUGE ON THE PAN. (96-30) REF ST ENG N/R 0085800 CHECKED LIMITS TO GOUGE AT L1 DOOR HANDLE PAN L=.30 W=.20 D=.011 ORIGINAL MAT THICKNESS SDR CALA2020012000206Check Valve · failedRIGHT ENGINE COMPRESSOR STALL CLIMBING THROUGH 1000 FEET ON DEPA RTURE. RIGHT ENGINE ITT 900. COMPRESSOR STALLED CONSECUTIVELY FOUR TIMES (PER PAX VIDEO). CREW REPORTED ENGINE REMAINED AT IDLE POWER THE REMAINER OF THE FLIGHT(NEVER SHUTDOWN). ENG EXCD PAGE SHOSDR CALA2020011300144Charger · inoperativeEMERGENCY ESCAPE PATH AISLE LIGHTING IS INOPERATIVE FROM SEAT 07C TO 20C. FOUND BATTERY PACK POWER SUPPLY INOPERATIVE FOR LEFT SEAT SECTION ROW 07 TO 20. REPLACED POWER SUPPLY BATTERY CHARGER ASSY PER AMM 33-51-07-862-054. OPS CHECK OF EMERGENCY LIGHTS NOW NSDR CALA2020011000123Unknown · malfunctionedAFTER TAKEOFF LFT FUEL TANK IMMEDIATELY LOST 3000 LBS. FUEL CONF IG LIGHT. FLUX BETWEEN 1000 REF FUEL QTY BITE FOLLOWING ARE PRESENT LEG FAULTS-LM DENS CONTA M OR RESISTOR A03, LM HIZ WIRE LOW RESISTENCE A05, LM COMPENSATO R G01. CENTER 10.8. DRIP STICK READINSDR CALA2020010600036Tank Unit · inoperativeTOTAL FUEL QTY INDICATION INOP TOTAL FUEL QUANTITY HAS BEEN DEFERRED IN COMPLIANCE WITH MEL CAR D 28130, TOMCQC REV PERFORMED .SDR CALA2020010600010Skin · dentedDENT ON FUSELAGE LEFT SIDE BETWEEN PRESSURE RELIF VALVE AND ELEV.STATIC PORT ABOUT 36" BELOW PUNCTURE THROUGH FUSELAGE SKIN AT APPROX STA 1445 AND 1" ABOVE S-25L REMOVED DAMAGE TO THE AFFECTED SKIN AERA STA 1445 AND STR 25 L REF 53-00-01. INSPECTION WILL NEEDSDR CALA2019121602215Selector · malfunctionedPRESSURIZATION CONTROL EICAS MESSAGE CABIN ALTITUDE SHOWN. CABIN ALT & CABIN ALTITUDE LIGHTS ON. COULD NOT CONTROL THE CABIN PRESSURE IN THE MANUAL MODE (DESCRIBE CAUSE OF DEPRESSURIZATION , IF KNOWN) TALKED TO THE CREW AFTER LANDING AND THEY TRIED BOTH AUSDR CALA2019121602211Unknown · noiseCREW REPORTS LOUD NOISE UNDER FLOOR JUST AFT OF FLIGHT DECK DOOR. TRIED TURNING OFF RH AND LH RECIRC FANS NO HELP OPBLM HANN FLIGHT CREW REPORTED VERBALLY TO TECH SOUND COMING FWD OF FLT DECK DOOR. INSPECTED BOTH E&E COMPARTMENTS FOUND NO OBVIOUS DAMAGE WHEN RSDR CALA2019121302195Girt Bar · failedSUPPORT TASK EA 2560-02123 REV D R1 DOOR FWD AND AFT OF GIRT BAR FAILED MINIMUM ENGAGEMENT CHECK REF. ST. ENGINEERING N/R 0080969SDR CALA2019121302188Girt Bar · failedSUPPORT TASK EA 2560-02123 REV D R4 DOOR FWD GIRT BAR FAILED MIN IMUM ENGAGEMENT CHECK.SDR CALA2019120902174Stringer · corrodedSUPPORT TASK ECRA 2011-0100 AFTER CLEANING OF BLUE WATER IN FWD CARGO LH SIDE FOUND CORROSION DURING DVI ON STR 23L AT STA 750 R EF ST ENG N/R 0081164 REMOVED CORROSION AND CHECKED LIMITS TO FWD CARGO S25L AT STA 75 0; L=5.2" W=1.5" D=.063", ORIGINAL MATERIAL SDR CALA2019120702160Girt Bar · no testSUPPORT TASK EA 2560-02123 REV D R2 DOOR AFT GIRT BAR FAILED MIN IMUM ENGAGEMENT CHECK REF ST ENG N/R 0080970 REMOVED AND REPLACED R2 DOOR GIRT BAR P/N 140N2762-17 IAW B757-2 AMM 25-66-10-402-022 ADJUSTMENT AND TEST WILL BE ACCOMPLISHED A T EA 25600-02123 REV SDR CALA2019121702219Gate · corrodedSUPPORT TASK EA 5210-01364 REV G (ON WING INSPECTION) R4 DOOR LO WER GATE HAS CORROSION OFF S/C PART. REF VT-SAA N/R: 0081207 REMOVED CORROSION AND CHECKED LIMITS TO R4 DOOR LOWER GATE; L=3. 1, FIG 101, DETAIL IV. REMOVED AND REPLACED R4 DOOR LOWER GATE, P/N:
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