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 CALA2016012000062Skin · dentedAFT CARGO DOOR DENT LOCATED 12" FROM BOTTOM & 18" FROM AFT SIDE, IS OUT LIMITS IAW SRM 52-30-01. DENT LOCATED ON TOP OF FRAME. CUT OUT DAMAGE & INSTALLED REPAIR DOUBLER IAW SRM 52-30-01 REPAIR 4. INITIATED DIP TO PERFORM LFEC INSPECTION AT 37,500 TOTAL DOORSDR CALA2016012000061Frame · crackedEVIDENCE OF CRACKED FRAME, ACFT DISTRIBUTION RAIL ATTACHMENT BRACKET AROUND INBD RIVET, AT STATION 760L. MARKED CUT OUT DAMAGE FRAME SECTION & INSTALLED REPAIR DOUBLER IAW ECRA 5310-06731 PART 1. INITIATED DIP TO ACCOMPLISH A PERMANENT REPAIR ON OR BEFORE THSDR CALA2016012000060Frame · wornCABIN FRAME STATION 1640, AT UPPER L1 DOOR ARE WORN. INSTALLED REPAIR IAW ECRA 5310-06722 PART 1 STEPS 1 - 18.I.SDR CALA2016012000059Frame · wornCABIN FRAME STATION 1640, AT UPPER R1 DOOR AREA WORN. REPAIRED IAW ECRA 5310-06723, STEPS 1 - 17.SDR CALA2016011500054Strap · corrodedCORROSION ALONG APU INLET DOOR AFT SUPPORT AT STATION 1825, BETWEEN STRINGER 3R - 6R. CUT OUT DAMAGED INNER STRAP, FABRICATED REPAIR PIECES, TREATED, PRIMED & INSTALLED IAW SRM 53-80-15 REPAIR 1 & ECRA 5380 -01117.SDR CALA2016011500053Strap · crackedFORWARD CARGO CEILING STRAP CRACKED, STATION 720, LBL25. REPAIRED STRAP IAW ECRA 5310-06729.SDR CALA2016011500052Strap · crackedFORWARD CARGO CEILING AT STATION 600, RBL 45,5, STRAP CRACKED. REPAIRED FWD CARGO CEILING STRAP IAW ECRA 5310-06730.SDR CALA2016011500050Circuit Breaker · poppedONCE AUTO THROTTLE WAS SELECTED, RT IRU EICAS ON DC WITH RT FMC FAILURE. CB BUS RT SECT 2 POPPED U080913 FOR INPUT ONLY NORMAL AFTER RESET. REPLACED CB P6 PANEL 115VAC BUS R SECT 2 PRECAUTIONARY WDM 24-51-22.SDR CALA2016011200049Frame · wornRIGHT BELT FRAME AT STATION 1640, STRINGER 6 RT, SHOWS WEAR MARK. REPAIRED FRAME IAW ECRA 5310-06728. PLACED ON DIP, CONT 95720 IAW STEP 17 OF ECRA 5310-06728. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 37,000 TOTAL FLIGHT CYCLES. PLSDR CALA2016011200047Indicator · poppedTRAILING EDGE FLAP DISAGREE ON APPROACH. FLAPS STUCK JUST BEYOND 15 DEGREES, ABLE TO EXTEND TO 20 DEGREES WITH ALTERNATE METHOD. TROUBLE SHOT IAW FIM TASK 27-51-00-815-808. FOUND LT WING, OTBD FLAP, OTBD TRANSMISSION INDICATOR POPPED, RESET SAME. OPERATED FSDR CALA2016010800040Floorbeam · corrodedFORWARD WET AREA FLOORBEAM AT STATION 377.5, LBL 0 TO 12 INCHES HAS CORROSION. REPAIRED FWD WET AREA FLOORBEAM IAW ECRA 5300-02286.SDR CALA2016010800030Frame · crackedCABIN STATION 760, BETWEEN STRINGER 8L & 9L, BELT FRAME CRACKED AT INBD RIVET. INSTALLED FUSELAGE FRAME REPAIR. PLACED IN DIP TO DO VISUAL INSPECTION EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, OR 50,000 AIRFRAME CYCLES, WHICHEVER CAME FIRST IAW SRMSDR CALA2016010400025Windshield · crackedCAPTAIN FRONT WINDOWS, OUTSIDE PANEL SHATTERED IN FLIGHT. REPLACED L1 WINDOWS IAW MM 56-11-01-004-001 & EA 3040-01164 WINDOW CHANGE WIRE UPGRADE. OPERATIONS NORMAL ROTABLE PARTS CHANGE WAS INDICATED. TT 1470906, SN OFF 09429 WINDSHIELD, B75 OFF 19-5611-9-90SDR CALA2016010400021Frame · crackedBELL FRAME LOCATED AT BS 1120 LT HAS CRACK AROUND FASTENER HOLE LOCATED BETWEEN STRINGER 6L & 9L. CUT OUT DAMAGED SECTION FRAME & INSTALLED REPAIR. INITIATED A ZONE 3 DIP OF A RIVETED FRAME REPAIR TO RE-INSPECT AT 12000 FLIGHT CYCLES FROM REPAIR INSTALLATIONSDR CALA2016010400013Frame · crackedCABIN INTERNAL STRUCTURE FRAME CRACKED AT FASTENER LOCATION WHERE A/C DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME AT STATION 1580, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR SDR CALA2016010400010Engine · malfunctionedDURING ATTEMPTED NR 1 ENG START, ENG STARTED & OVERTEMPED AT 577 UNTIL TOLD WE HAD AN ENG TAIL PIPE FIRE. NO FIRE WARNING IN COCKPIT. DISCHARGED NR 1 ENG NR 1 BOTTLE. NEW ENG INSTALLED. SEE WC 19-7100-1-0900 DEC 31 2015 FOR DETAILS.SDR CALA2016010400003Charger · inoperativeL4 DOOR SLIDE LIGHT ON FUSELAGE INOPERATIVE. REPLACED BATTERY CHARGER IAW AMM 33-51-07-862-054. OPERATIONS CHECKED GOOD. ACFT RELEASED FOR FLIGHT.SDR CALA2015123001051Floorbeam · corrodedCABIN AFT WET ENTRY FLOOR STRUCTURE, FLOORBEAM UPPER CAP HAS AREAS OF CORROSION AT STATION 1640 FROM LBL 2 TO LBL 8. CUT & REMOVED DAMAGED SECTION OF UPPER T CHORD ON FLOORBEAM. FABRICATED & INSTALLED REPAIR IAW ECRA 5310-06716 & SRM 53-00-51 REPAIR 10.SDR CALA2015123001050Beltframe · crackedCABIN STATION 760, BETWEEN STRINGER 8R & 9R, BELT FRAME CRACKED AT INBD RIVET. INSTALLED FUSELAGE FRAME REPAIR. PLACED IN DIP TO DO A VISUAL INSPECTION EVERY 12,000 FLIGHT CYCLES FROM REPAIR INSTALLATION, OR 50,0000 AIRFRAME CYCLES, WHICHEVER COMES FIRST IAWSDR CALA2015122801035Wire · damagedDURING 2 SVC, FOUND ON SEAT EMER LIGHTS FOR ROWS 22 - 30 INOPERATIVE. DAMAGED WIRING FOUND SEAT TO SEAT CABLE BETWEEN SEATS 27 - 28 ABC. DAMAGED CABLES CUT OUT & SPLICE REPAIR CARRIED OUT IAW WPM 20-30-21 P15. ALL EMER LIGHTING NOW OPERATES NORMALLY.SDR CALA2015122801032Frame · crackedBELL FRAME LOCATED AT BS 1120 RT HAS CRACK AROUND FASTENER HOLE, LOCATED BETWEEN STRINGER R8 & R9. REPAIRED IAW SRM 53-00-07 REPAIR 1. INITIATE DIP 53, DIP CONTROL 95343 FOR THRESHOLD DVI AT 12000 CYCLES & 50000 TOTAL CYCLES WHICHEVER COMES FIRST. REPETITIVSDR CALA2015122401027Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1520, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. SDR CALA2015122401026Frame · crackedCABIN STATION 800, STRINGER 8R & 9R, BELT FRAME CRACKED AT INBD RIVET. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR. INITIATED A ZONE 3 DIP OF A RIVETED FRAME REPAIR TO RE-INSPECT AT 12 ,000 FLIGHT CYCLES FROM INSTALLATION OR 50,000 AIRFRAME CYCLES, WSDR CALA2015122401025Light · inoperativeOVERHEAD BIN AISLE EMER LIGHTS INOPERATIVE AT POSITIONS 4R, 12L, 12R, 37R & 35L. RELAMPED OVERHEAD BINS AISLE EMER LIGHTS IAW AMM 33-51-05 & TESTED NORMAL.SDR CALA2015122401024Light · inoperativeEPL LIGHTS AT SEAT ROWS 7L, 20L, 24L, 32L, 33L, 35L, 36L & 37L INOPERATIVE. EPL LIGHTS RELAMPED LIGHTS IAW AMM 33-51-11 & TESTED NORMAL.SDR CALA2015122401023Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1480, BETWEEN STRINGER 8L & 9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1.SDR CALA2015122401022Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1540, BETWEEN STRINGER 8R & 9R. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. INITIATED DISDR CALA2015122301020Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1520, BETWEEN STRINGER -8L & -9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07, REPAIR SDR CALA2015122301019Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1540, BETWEEN STRINGER 8L & 9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07 REPAIR 1. SDR CALA2015122301018Frame · crackedCABIN INTERNAL STRUCTURE, FRAME CRACKED AT FASTENER LOCATION WHERE AC DISTRIBUTION DUCT SUPPORT BRACKET IS SECURED TO FRAME, STATION 1580, BETWEEN STRINGER -8L & -9L. MARKED CUT OUT DAMAGE SECTION OF FRAME & INSTALLED REPAIR DOUBLERS IAW SRM 53-00-07, REPAIR SDR CALA2015122101013Crease Beam · corrodedOUTER CREASE BEAM CORRODED STATION 430 RT. R & R CREASE BEAM RT SIDE, BETWEEN BS 430 - BS 450 IAW SRM 51-40-02, PN BAC1515-53 2024 T35.SDR CALA2015122101016Unknown · odorBURNING RUBBER ODOR IN COCKPIT AFTER ENG START, AS TAXING OUT SEEMED TO DISSIPATE. AS ACFT TOOK RUNWAY FOR TAKEOFF, ODOR CAME BACK VERY STRONG, AGAIN IT SMELLED LIKE BURNING RUBBER. PERFORMED CONDITIONAL INSPECTION FOR SMOKE & ODOR IAW AMM 05-51-58. NO ODOSDR CALA2015122101014Floorbeam · corrodedAFT CABIN PAX AT WET AREA ON BS 1681, LBL 40, FLOORBEAM UPPER FWD FLANGE HAS EXFOLIATION CORROSION. REMOVED CORROSION ON FLOORBEAM, FOUND BEYOND LIMITS. FABRICATED REPAIR STRAP, ANGLES & FILLER. TREATED, PRIMED & TOP COATED PARTS. REWORKED AREAS & INSTALLESDR CALA2015122101008Attach Bracket · crackedLEFT PSU RAIL ATTACH BRACKET AT BELT FRAME SHOWS CRACK AT FASTENER STATION 1580. CUT OUT DAMAGED SECTION OF FRAME & INSTALLED REPAIR.SDR CALA2015121801005Floorbeam · corrodedFLOORBEAM AT STATION 365, RBL-10, FWD FLANGE HAS CORROSION ON UPPER & LOWER SIDES. COMPLETED INSTALLATION OF REPAIR ON CABIN FLOORBEAM, STATION 365, RBL-10, FWD FLANGE IAW SRM 53-00-51 REPAIR 5.SDR CALA2015121300991Angle · corrodedZ ANGLE AT L2 DOOR HAS CORROSION. R & R Z ANGLE AT L2 DOOR IAW SRM 51-40-02.SDR CALA2015120400968Deck Plate · corrodedAFT CABIN FLOOR STRUCTURE & AREA BELOW THE FLOOR LT STATION 1681, BETWEEN LBL 0 & LBL 60, SUBFLOOR SHOWS EVIDENCE OF SURFACE CORROSION. REMOVED CORROSION ON DECK PLATE, STATION 1681, LBL 12, LBL 24, LBL 40 X LBL 48, MAT LOST LBL 12 .031, LBL24, .016,LBL 40 .0SDR CALA2015120400963Light · inoperativeSEAT 1B EMER LIGHT, 1 OF 2, INOPERATIVE. ITEM PLACED ON MEL IAW 3351H. THIS FORM RAISED FOR SDR REPORTING.SDR CALA2015120400961Oven · odorGATE RETURN FOR OVEN ODOR. PERFORMED AMM 05-51-58 INSPECTION. VERIFIED OVEN 305 AS CAUSE REF 8326266 FOR OVEN 305. MEL FORMS 46-6020 FAXED TO MOC. IAW FORMS NO SMOKE OR BURNING ODOR PRESENT, ONLY OVEN SMELL. INSPECTED OVEN NO OVERHEAT CONDITION NOTICED.SDR CALA2015112000938Oven · shortedFORWARD GALLEY OVEN 204, SHORTED, WITH OVEN TURNED OFF. UTILITY BUSES WERE TURNED OFF & CB PULLED, OVEN THEN COOLED DOWN. PERFORMED SMOKE & ODOR IN FLIGHT DECK & OR CABIN INSPECTION IAW AMM 05-51- 58, NO DEFECTS NOTED. R & R NR 204 & 205 OVENS IAW AMM 25-34SDR CALA2015111800934Heater · inoperativeEXPERIENCED SMOKE IN THE CABIN. COMPLIED WITH QRH & DIVERTED. FOUND NR 2 HEATER POPPING BREAKER ON P70 PANEL. DURING REMOVAL OF HEATER IT WAS INOPERATIVE WITH BURNT DEBRIS INSIDE OF IT. REPLACED NR 2 DOOR HEATER. RAN ENG & PACKS TO CONFIRM SMOKE NO LONGERSDR CALA2015111600933Splice Plate · corrodedLEFT HORIZONTAL STAB LOWER SURFACE PIVOT FITTING STRAP APPROX AT STAB STATION 81 & 15 INCHES FWD OF AFT SPAR IS CORRODED. REPLACED UPPER SPLICE PLATE, PN 182N1608-5, AT LOWER SURFACE PIVOT FITTING IAW SRM 51-40-02 & DWG 182N1601. SEE ENTRIES BELOW FOR ALL WOSDR CALA2015111600932Intercostal · corrodedCENTER INTERCOSTAL WEB ANGLE ATTACHES ON AFT CARGO DOOR LOWER END IS CORRODED. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. INSTALLED NEW CTR INTERCOSTAL WEB AT AFT CARGO DOOR IAW DWG 146N6 603 & SRM 51-40-02.SDR CALA2015111600931Stiffener · corrodedAFT CARGO DOOR LOWER END, AFT TEE STIFFENER IS CORRODED. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. R & R AFT CARGO DOOR LOWER END AFT TEE STIFFENER IAW DWG 146N6603 & SRM 51-40-02.SDR CALA2015111600930Intercostal · corrodedCENTER INTERCOSTAL ANGLE ON AFT CARGO DOOR LOWER END IS CORRODED OUT OF LIMITS. FOR PREVIOUS WORK ACCOMPLISHED SEE WIPS ABOVE. INSTALLED NEW CTR INTERCOSTAL ANGLE ASSEMBLY IAW DWG 146N6603 & SRM 51-40-02.SDR CALA2015111300918Skin · crackedL4 DOOR UPPER HINGE, INNER SKIN CRACKED. REPAIRED L4 DOOR UPPER SKIN CRACKS IAW SRM 52-10-01 REPAIR 7 & ECRA 5210-02675.SDR CALA2015111000909Frame · chafedMAIN CABIN 1640 FRAME & STRINGER 6R HAS CHAFING MARK. BLENDED OUT DAMAGE & INSTALLED REPAIR DOUBLER IAW ECRA 5310-CONT. TOTAL AIRFRAME FLIGHT CYCLES FOR THE INSPECTION REQUIREMENT 06643 REV A PART 1, STEPS 1 - 17. INITIATED DIP TO ACCOMPLISH TROUBLESHOOTINGSDR CALA2015111000908Frame · crackedFORWARD CARGO COMPARTMENT, RT FRAME DENTED AT STATION 680, ABOVE STRINGER 24L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO REINSPECT AT 25K FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVSDR CALA2015111000907Frame · dentedFORWARD CARGO COMPARTMENT, LT FRAME IS DENTED AT STATION 800 ABOVE STRINGER 24L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 1 DIP TO REINSPECT AT 37,500 AFTER REPAIR INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVER COMES SDR CALA2015111000906Frame · dentedFORWARD CARGO COMPARTMENT, LT FRAME IS DENTED AT STATION 700 ABOVE STRINGER 23L. CUT OUT DAMAGED AREA OF FRAME & INSTALLED REPAIR DOUBLER & INITIATED A ZONE 2 DIP TO REINSPECT AT 25K FLIGHT CYCLES AFTER INSTALLATION OR 50K AIRFRAME FLIGHT CYCLES, WHICHEVER CO
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