Boeing 757-222
Service difficulty reports · 15,539
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 = '757222' 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 = '757222' 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 FDEA202002140337Filter · defectiveAFTER LANDING TOWARD END OF ROLLOUT, GOT FIRE EICAS MESSAGE AND FIRE MASTER WARNING INDICACTIONS. NO OTHER FIRE INDICATIONS. AS WE PULLED OFF RWY COCKPIT FILLED UP WITH SMOKE. FIRE INDICATION CLEARED. SHUT DOWN JET, RAN QRH FOR EMERG EVAC, AND EXITED LT SIDE VSDR CALA2020021600425Skin · crackedLH INBD DIAGONAL BRACE FITTING HAS 2 FASTENER HOLE CRACK INDICATIONS MARKED. REF: AAR N/R 9756230 SEE ECRA 5720-03163 L/H WING UPPER SKIN, FWD DRAG FITTINGS, AND SHIM REPLACEMENT INTERIM REPAIR. ON OR BEFORE JAN 23 2022 OR THE ACCUMULATION OF 21975 TOTAL FLT CSDR CALA2020021600424Skin · crackedLH DRAG BRACE FITTING SKIN HAS FASTENER HOLE CRACK INDICATION AT FASTENERS 5, 9, 14, 17 & 18. REF. A EE ECRA 5720-03163 L/H WING UPPER SKIN, FWD DRAG FITTINGS, AND SHIM REPLACEMENT INTERIM REPAIR. ON OR BEFORE JAN 23 2022 OR THE ACCUMULATION OF 21,975 TOTAL A/SDR CALA2020021600421Skin · crackedDURING ROTO INSP CRACK INDICATIONS NOTED AT PYLON (#13 FASTENER HOLE) RIGHT WING SKIN DRAG FITTINGS AREA, CRACK POSITION :- 7:O''CLOCK; CRACK DEPTH :- 0.323"; CRACK SIZE :- 0.030" REF. AAR N/R 9756220 SEE ECRA 5720-03164 R/H WING UPPER SKIN, FWD DRAG FITTINSDR CALA2020021600420Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #2 PYLON UPPER SKIN AT DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #9 - CRACK POSITION :- 7:O''CLOCK; CRACK DEPTH :-0.315"; CRACK SIZE :-0.060" REF. AAR N/R 9756199 SEE ECRA 5720-03164 R/H WSDR CALA2020021600419Skin · crackedDURING NDT HFEC ROTO INSPECTION OF #2 PYLON UPPER SKIN AT DRAG FITTING IAW NDTM PART 6, 51-00-16 CRACK INDICATIONS WERE FOUND AT HOLE #3 - CRACK POSITION :- 10:O''CLOCK; CRACK DEPTH :- 0.394"; CRACK SIZE :- 0.030" REF. AAR N/R 9756198 SEE ECRA 5720-03164 R/HSDR FDEA2020031740223Battery · dischargedMDIS 790 33-50 3426 24JAN20 GSO FACT U L1 DOOR EXTERIOR EMERGENCY LIGHT AND L1 DOOR INTERIOR EXIT SIGN WON'T ILLUMINATE WHEN EMERGENCY LIGHTS ARE TESTED. R/I 24JAN20 05:26 GSO U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 2013-SDR FDEA202001240214Charger · failedR1 DOOR EXTERIOR EMERGENCY LIGHT INOP. R1 INDOOR EMERGENCY LIGHT OPS NORMALLY. EMERGENCY BATTERY VOLTAGE GOOD, RELAMPED, NO HELP. NO POWER AT SOCKET. REF SSM 33-51-01 PG101 SH2, VERIFIED GOOD WIRING FROM BULB CONTACT AT L30 BACK TO CONNECTOR D66 AT EMERG LSDR FDEA2020012320196Controller · malfunctionedDIVERTED INTO EWRZONE TEMP DROPPED TO 38/49/26. TRIM AIR WAS MEL'D FL 370, NO A/ICE, TRIED AUTO, N, W ON PACK CONTROLLER. TEMP CONTINUED TO DROP IN ALL SETTINGS. LOST 30 DEGREES IN 50 MINS. ETURNED TRIM AIR PRESSURE REGUALTING VALVE TO NORMAL CONFIG. REMOVED ASDR CALA2020011000111Skin · chafedB757-53-3-6075 SUPPORT CHAFING INTO AFT FUSELAGE SKIN PANEL STA 1797 STR 17R BLENDED AND CHECKED LIMITS ON CHAFING AT AFT FUSELAGE SKIN PANEL STA 1797 STR 17R; L=2.3 IN W=.70 IN D=.031,ORIGINAL MATERIAL THI CKNESS .056 IN. BLENDED AREA FOUND TO BE OUT OF LIMITSDR CALA2020010600098Engine · flamed outENGINE 2 FAILURE LEVEL AT 4000FT BASE TO FINAL TURN FLIGHT CREW REPORTED THE ENGINE FLAMED OUT ON IT''S OWN. THEY HEARD A MUFFLED BOOM SOUND AND FELT THE AIRCRAFT YAW. THEY HAD R ENG STATOR AND R ENG FAIL EICAS MESSAGES DISPLAYED. ENGINE WINDMILLED FOR APPROX.SDR CALA2020010600069Skin · dentedDENT ON ENTERIOR SKIN FROM INSIDE OUT FED OF AFT DRAIN MAST APPROX STSTION 1590 C/W HFEC PER NDT MANUAL PART 6, OF FUSELAGE DENT , EXTERIOR SKIN- INSIDE OUT , FWD OF AFT DRAIN MAST AT APPROX STA-1590. NO CRACK INDICATIONS NOTED AT THIS TIME. PERFORMED INTERIMSDR FDEA2019123103330Sensor · failedAFTER TAKEOFF THE LANDING GEAR HANDLE WOULD NOT RAISE TO RETRACT. RAN QRH. LANDING GEAR RETRACTED WITH LOCK OVERRIDE QRH. REMOVED AND REPLACED LEFT FORWARD MAIN GEAR TRUCK TILT SENSOR IAW AMM 32-09-07-2. OPS CHECK GOOD. AIRCRAFT OK FOR SERVICE. SDR INFO:SDR CALA2020010600047Skin · chafedB757-53-3-6075 SUPPORT BRACKET CHAFING INTO AFT FUSELAGE SKIN PA NEL STA 1797 STR 17L. RL030 REF ST ENG N/R 0079023 BLENDED AND CHECKED LIMITS TO CHAFING AT AFT FUSELAGE SKIN PANEL STA 1797 S-17L L=2.5 W=.75 D=.030 OUT OF LIMITS IAW B757-2 SRM 53-80-70 PG 106 SDR CALA2020010600014Pan · gougedB757-06-3-2303 L-2 PASSENGER DOOR,EXTERNAL HANDLE PAN IS GOUGED. (96-32) REF.ST. ENGINEERING N/R 0079201 BLENDED AND CHECKED LIMITS TO L2 PASSENGER DOOR EXTERNAL HANDLE PAN: L=1.3",W=.10" D=.008". OUT OF LIMITS IAW B757-200 SRM 52-10 -01 AD1,FIG 101,DETAIL VISDR CALA2020010600016Depressor · dentedB757-52-3-6063 FWD CARGO DOOR,AFT DEPRESSOR IS DENTED IN 2EA PLA CES.(96-18) REF. ST. ENGINEERING N/R 0079119 FOUND 2EA DENTS OUT OF LIMITS.REMOVED AND REPLACED FWD CARGO DOO R AFT DEPRESSOR IAW B757-200 SRM 51-40-02 AND SRM 51-70-11,AREA FOD FREE AND BOEING DSDR CALA2019122102256Housing · damagedSUPPORT TASK SECONDARY FINDING UPON REMOVAL OF L1 DOOR HANDLE ME CHANISM BOX FOUND 2EA DAMAGE (GOUGE) AT CENTER HOLE SLEEVE. REF ST ENG N/R 0079475SDR FDEA2019122083258Strap · dentedMAIN EQUIPMENT CENTER CEILING AREA,, MAIN FLOOR STRUCTURE ATTACH STABILIZER STRAP HAS A CRACK AT FASTENER HOLE ABOUT 1.5" LONG, BS.480 RBL. 24.75 CUT DAMAGED AT STABILIZER STRAP IAW B757 SRM 51-10-02-0G AND SRM 53-00-51-2R FIG 201 DETAILV REP 12, FABSDR CALA2020010600005Door Frame · dentedB757-52-3-6063 FWD CARGO DOOR,AFT CORNER FRAME IS DENTED IN CENT ER. (96-19) REF. ST. ENGINEERING N/R 0079120 CHECKED LIMITS TO DENT AT FWD CARGO DOOR AFT CORNER FRAME; L=.70 ", W=.40",D=.023" OUT OF LIMITS IAW B757-200 SRM 52-30-02 AD1,DE TAIL V.REOVED AND RESDR CALA2020010600004Depressor · dentedB757-52-3-6065 AFT CARGO DOOR,AFT DEPRESSOR IS DENTED AND HAS CH AFING ALONG ENTIRE EDGE.(96-09) REF. ST. ENGINEERING N/R 0079110 REMOVED AND REPLACED AFT CARGO DOOR AFT DEPRESSOR P/N: 146N6603- 114,BATCH NO 0003589133,PO NO. SOS1920224 IAW BOEING DRAWING 143 SDR FDEA201912133241Stringer Splice · corrodedLOWER FUSELAGE SKIN BULGE AT BS 1464 STR29L APPROX. SUSPECT OF CORROSION EVALUATED AREA AT LWR FUSE SKIN FOUND STR SPLICE CORROSION OUT OF LIMITS. REMOVED, FABRICATED AND INSTALLED NEW STRINGER SPLICE AS PER SRM 51-40-02-0G, 51-10-02-0G AND DWG 146N3820 REV CSDR FDEA2019121323230Angle · corrodedUPON REMOVAL OF APU INTAKE DUCT FOUND ANGLE CORRODED APPROX STA 1787 TO 1800 RBL6. FOUND ANGLE AT APU INTAKE DUCT TO BE 100% MATERIAL LOSS OUT OF LIMITS IAW SRM 53-80-15. REMOVED, FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-40-02 AND DWG 148N3152 REV -.SDR CALA2019121302177Coffeemaker · leakingWATER LEAKING FROM MID GALLEY COFFEE MAKER. WOULD NOT STOP WITH SHUTOFF VALVE IN OFF REPLACED COFFEE REPLACED COFFEE MAKER.OPS GOOD. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1118399 SN OFF 0340 COFFEEMAKER, IN OFF 31-2534-9-0001 0340 ON 31-2534-9-0001 1504SDR FDEA2019120653189Gust Lock · brokenL1 DOOR GUST LOCK BROKEN. REMOVED AND REPLACED L1 GUSSETT LOCK IAW AMM 52_11_08_8_0 OPS CHECK GOOK, AC OK FOR SERVICE, THIS CLEARS MEL #720992SDR FDEA201911263107Warning Message · false activationPDIS 786 36-11 3853 26NOV19 GSO OPEN U LOGPAGES:3166516 REJECTED T/O BECAUSE OF "LEFT ENG BLEED AIR" AT 80 KTS. CLEARED EICAS WITH QRH AND CHECK LIST. RAN LEFT AND RIGHT ENGINES TO 80 PERCENT N2 WITH BOTH ENGISDR CALA2019111601977Frame · dentedB757-53-3-6043 SECONDARY FINDING DENT ON FWD CARGO LH FRAME UPPE R FLANGE AT STA 540 ABOVE STR 24L REF. ST. ENGINEERING N/R 0076173 CHECK LIMITS TO DENT ON FWD CARGO LH FRAME AT STA 540 ABOVE S-24 L;L=.92",W=.90",D=.024".OUT OF LIMITS IAW B757-200 SRM 53-00-07SDR CALA2019111601975Web · crackedB757-52-3-6087 (SECONDARY FINDING)WHILE WORKING N/R NO. 0075848 FOUND A CRACK ON R4 DOOR INTERIOR WEB AT LIGHTNING HOLE RADIUS J UST ABOVE LOWER HINGE FITTING REF. ST. ENGINEERING N/R 0076244 REPAIRED CRACK L=.250 AT R4 DOOR INTERIOR WEB AT LIGHTING HOLE R ADISDR CALA2019111601974Web · crackedWHILE WORKING N/R NO 0075848 FOUND A CRACK ON R4 DOOR INTERIOR W EB AT A LIGHTNING HOLE RADIUS. REF. ST. ENGINEERING N/R 0076242 REPAIRED CRACK L=.250 AT RH DOOR INTERIOR WEB AT LIGHTING HOLE R ADUIS IAW ECRA 5210-03043. COMPLETED AND ACCEPTEDSDR CALA2019111601986Girt Bar · damaged(SUPPORT TASK EA 5210-01360 REV. J SEQ NO 888)DURING L1 DOOR GIR T BAR ADJUSTMENT TEST FOUND GIRT BAR LEAF SPRING NOT HOLDING THE SLIDER. REF. ST. ENGINEERING N/R 0076336SDR CALA2019111101959Skin · damagedSUPPORT TASK EA 5300-02572 REV A OP 002 DURING VIASAT AFT DOUBLE R INSTALLATION P/N AR230-2502-02,1EA HOLE MIS-DRILLED THROUGH DO UBLER AND CROWN SKIN AT STA 625.5 ABOVE I/B SIDE OF STR 2R.REF S T. ENGINEERING N/R ACCOMPLISHED EC/RA 5300-02664 ON CROWN STRUCTUSDR CALA2019111101958Skin · damagedSUPPORT TASK EA 5300-02572 REV A OP 002 DURING VIASTAT FWD DOUBL ER INSTALLATION P/N AR230-2502-01, 2EA HOLES WERE MIS-DRILLED TH ROUGH DOUBLER AND CROWN SKIN AT STA 575 JUST I/B OF STR 2R. REF ST ENG N/R 0076290 ACCOMPLISHED EC/RA 5300-02664 ON CROWN STRUCTURSDR CALA2019111101957Stringer · damagedSUPPORT TASK EA 5300-02572 REV A OP 002 DURING VIASAT AFT DOUBLE R HOLE LOCATING,STRINGER 2R WAS NICKED WITH DRILL BIT AT STA 625 .5 AT I/B UPPER RADIUS REF. ENGINEERING N/R ACCOMPLISHED EC/RA 5300-02664 ON CROWN STRUCTURE INSTALLATION SE E LOG PAGE 3783598 FOSDR FDEA2019110762898Slide · damagedL1 DOOR SLIDE FELL OUT OF BUSELL, FLIGHT CREW FAILED TO FULLY DISARM PRIOR TO OPENING. ASSIST BOTTLE DISCHARGED. L1 INOP SLIDE REMOVED AND PLACED IN MAIN DECK CARGO BEHIND BARRIER. REMOVED AND REPLACED L1 DOOR EMERGENCY POWER ASSIST CYLINDER PER MM 52-11-3SDR CALA2019110501911Gate · corrodedSUPPORT TASK EA 5210-01360 REV J OP 001 L-1 DOOR, LWR GATE HAS C ORROSION ON PREVIOUS BLEND, ALONG EDGE.(96-17) REF ST N/R 007605 6 BLENDED AND CHECKED LIMITS TO CORROSION ON L1 DOOR LOWER GATE L= 8.0 W=.260 D=.125. OUT OF LIMITS IAW B757-2 SRM 52-10-02 AD1 FISDR FDEA201910312800Unknown · malfunctionedR1 DOOR NOT OPENING AND CLOSEING PROPERLY USING OUTSIDE HANDLE. UPPER AND LOWER FLAPS NOT FAIRING PROPERPLY. OPEN AND CLOSES CORRECTLY USING INSIDE DOOR HANDLE. SDR CALA2019110501910Strap · corrodedB757-55-3-6021 INTERIOR STRAP CORRODED AT FUSELAGE STA 1825 AT A FT SIDE OF APU AIR INLET DOOR HOUSING CUTOUT.REF. VT SAN ANTONIO AEROSPACE N/R 0076275 BLENDED CORROSION AND CHECKED LIMITS ON INTERIOR STRAP AT STA 18 25 AFT SIDE OF APU AIR INLET DOOR HOUSING CSDR CALA2019110501909Depressor · dentedB757-52-3-6063 FWD CARGO DOOR,AFT DEPRESSOR IS DENTED/CREASED IN 2EA AREAS.(96-26).REF VT SAN ANTONIO AEROSPACE N/R 0076116 REMOVED DAMAGED DEPRESSOR AND INSTALLED NEW SEAL DEPRESSOR P/N 1 43N6603-105 ON AFT SIDE OF AFT CARGO DOOR IAW BOEING DWG NO. 14N 6603 ASDR CALA2019110101881Slider · wornSUPPORT TASK EA 2560-02123 REV D L4 DOOR FWD GIRT BAR SLIDER FAI LED MINIMUM MEASUREMENT CHECK. VT SAN ANTONIO AEROSPACE N/R 0075 735SDR CALA2019110101866Frame · dentedB757-53-3-6043 SECONDARY FINDING DENT ON FWD CARGO LH FRAME UPPE R FLANGE AT STA 580 BETWEEN STR 24L-25L.REF VT SAN ANTONIO AEROS PACE N/R 0076172 DENT,L=1.0",W=.60",D=.016",ON FWD CARGO LH FRAME UPPER FLANGE AT 53-00-07 AD1,PG101,FIG101,REPAIR FRAME IAW B757-SDR CALA2019110501904Angle · corroded(B757-55-3-6021) APU AIR INLET DOOR HOUSING ASSY TO FUSELAGE CUT OUT LANDING HAS CORROSION. REF ST-SAA NR 0076006. AFTER CORROSION REMOVAL FOUND FWD STRAP AND LWR ANGLE OUT OF LIM ITS IAW B757-200 SRM 53-80-13 L=21.0, W=1.0, D=.015 AND L=2.0, W =1.0, D=.023, RSDR CALA2019102981843Skin · dentedB757-53-3-6037 AFT LOWER HALF OF FUSELAGE LEFT SIDE BETWEEN STA 1580 AND STA 1600 PROTRUDING DENT. MARKED CVC210-018 REF ST ENG N/R 0075751 REF. N/R#0075751 FOUND DENT OUT OF LIMITS. ACCOMPLISHED ZONE A C AT B REP. IAW 757 SRM#53-00-01 REPAIR 29. INITIATE D DSDR CALA2019102501800Oven · smokeSMOKE AND FUMES COMING FROM AFT GALLEY OVENS DURING CLIMBOUT. AF T LAV SMOKE ALARMS BEGAN FLT ATT VERIFIED SMOKE SOURCE WAS OVEN 411. MEAL CONTAINED IN PLASTIC TOUCHING UPPER METAL PORTION OF MEAL CARIER. CONTROLLERS REPLACEMENTS ARE REQUIRED. REMOVED DIRTY OVSDR FDEA2019102192699Structure · crackedR2 UPPER HINGE DOOR CUT OUT IS CRACKED. CUT OUT DAMAGE ON THE R-2 DOOR UPPER HINGE CUT OUT , FABRICATED DOUBLER AND INSTALLED IAW B757 SRM 52-10-02-2R FIG 201 REPAIR 1 DET III , FEDEX EA# F-5210-T0350260 P1. TITLE : DOORS - PASSENGER/CREW - R-2 DOOR FWD FRSDR FDEA201910152647Angle · crackedFOWARD LOWER CARGO COMPARTMENT DOOR UPPER CHORD, AFT GUSSET ANGLE CRACKED IN RADIUS REMOVED FWD LWR CARGO DOOR UPPER AFT ANGLE (BRACKET) IAW B757 SRM 51-40-02. FORMED, LOCATED, DRILLED AND INSTALLED NEW ANGLE (BRACKET) IAW BOEING DWG 69- 53919 AND B757 SSDR FDEA2019101422616Terminal · dirtyON WALKAROUND, FOUND L1 DOOR SLIDE EMERGENCY LAMP ON EXTERIOR WAS INOPERATIVE. RELAMPED TWICE WITH NO HELP. REMOVED L1 DOOR SLIDE EMERGENCY LIGHT ASSY IAW AMM 33-51-06-2-1. INSPECTED LIGHT ASSY, WIRES AND TERMINALS FOR ANY DEFECTS. FOUND CENTER TEMINAL ON TSDR FDEA2019101412606Seat Track · corrodedMAIN DECK COURIER AREA FLOOR SEAT TRACK RBL 12 IN STA 355 TO 377 UPPER SURFACE HAS 10 SQ IN CORROSION. REMOVED CORR ON SEAT TRACK STA 355 TO 377 RBL 12 IAW B757 SRM 51-10-02. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK IAW B757 SRM 51-40-05, 51-40-0SDR CALA2019101101737Fan · failedSTRONG ELECTRICAL ODOR IN CABIN. NO SMOKE NOTED. MIDS TURNOVER WAS THAT THE REPORTED SMELL HAD DISSIPATED PRIOR TO THEIR ARRIVAL AND THEY WERE UNABLE TO DUPLICATE IT. REF LOG PAGES 3517649, 3511722 AND 3514642. REPLACED RT RECIRC FAN AND FILTERS. UNABLE TO DUPSDR CALA2019101101733Gcu · malfunctionedDURING FLIGHT, LEFT GENERATOR DROPPED OFF LINE /PLANE JERKED BUT AP WORKED. REF LOG PAGE 3482718, R AND R LEFT ENGINE GCU. LP 3482718- NO RESET ON LEFT GEN, DIVRT TO DEN SINCE NO APU. VERIFIED OIL SVC LEVEL ON #1 ENG IDG, RESET IDG, R AND R ENG GCU, REF AMM 2SDR FDEA2019100312380Solenoid Valve · leakingRIGHT HYD QTY EICAS MESSAGE INFLIGHT. COMPLIED WITH QRH. FOUND LEAK AT RT SYSTEM APCS ELECTROHYDRAULIC SOLENOID VALVE WHERE IT MATES TO THE SOLENOID. REMOVED AND REPLACED METAL GASKET ON SOLENOID VALVE IAW MM 22-12-02-2. PERFORMED OPS AND LEAK CHECKS. OPSSDR CALA2019093001676Flex Duct · tornACFT AIR RETURN DUE TO PRESSURIZATION ISSUES, PLEASE DEBRIEF CREW FOR DETAILS. SEE LOG PAGES 3397569,3397548,3397874, FOR CORRECTIVE ACTION. FOUND TORN FLEX DUCT ON RH ACM CHECK VALVE. RPLD DUCT REF AMM 21-51-15-434-018. NO LEAKS NOTED. PRESSURIZED ACFT, REF
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