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 UALA2013032501838Door · out of adjustL2 DOOR HARD TO ARM. ADJUSTED DOOR LINER ALSO LOWER FOOTBALL CAMS AND LWR LINKAGE.SDR UALA2013032501867Skin · dentedDENT IN UPPER CROWN AREA BS 653.8 2.5 INCHES BELOW S3R. REPAIRED IAW ECRA5331-01700.SDR UALA2013032501866Skin · dentedDENT FOUND AROUND RIVET BS 646 BETWEEN STR 3-4R, FOUND TO BE OUT OF LIMITS PER SRM 53-00-01 FIG 101 PG102. REPAIRED DAMAGE PER ECRA 5331-01700.SDR UALA2013032501875Fcu · faultyREPLACED APU FLOW SENSING MODULE REF DF676 APU AUTO SHUTDOWN. REPLACED FLOW SENSING MODULE, NO HELP ACC. APU DEEP BITE TEST FAULTS SHOW DELTA P, FUEL CONTROL UNIT, DE-OILER SOLENOID, HOT SENSOR AND P2 SENSORSDR UALA2013032501823Circuit Breaker · trippedDOOR GIRT BAR ENTRY DIM CIRCUIT BREAKER R34 TRIPPED. CYCLED SYSTEM POWER. OPS CHECKED ARM DISARM LEVER OF ALL MED DOORS FEW TIME, CIRCUIT BREAKER R34 NOT POPPED.SDR UALA2013032201810Blade · damagedNR 2 ENGINE LPT FAN BLADE HAS A NICK APPROXIMATELY 4 INCHES FROM LEADING EDGE BLADE TIP. ACCOMPLISHED EDDY CURRENT IAW NDTM 72-31-401, NO CRACKS DETECTED.SDR UALA2013032101773Control Panel · defectiveNR 1 VHF COMM CONTRL PANEL HAS MECHANICAL DEFECT: BROKEN, MISSING OR LOOSE PARTS. VHF CONTROL PANEL RIGHT FREQ WINDOW HAS THE LEFT SIDE INTERNAL LIGHT INOPERATIVE. REPLACED RADIO CONTROL PANEL. OPS CHECKED GOOD.SDR UALA2013032101755Filter · dirtyFWD CAB TRIM AIR INOPERATIVE. CLEANED CABIN TEMP SENSOR FILTERS. OPS CHECKED NORMAL.SDR UALA2013032201809Ground Wire · unsecureGROUND WIRE HANGING OUT OF 1ST FLAP TRACK CANOE OUTBOARD OF LF ENG PYLON SECURED GROUND WIRE IN CANOE FAIRING.SDR UALA2013032201788Floorbeam · corrodedBS 324 FLOORBEAM TEE CAP CORRODED AT RBL 50. FABRICATED AND INSTALLED NEW TEE CAP AND SPLICE IAW SRM 53-10-08, REPAIR 1.SDR UALA2013032201786Floorbeam · corrodedAFT CABIN BS 1640, LBL 2 - RBL 10 TOP OF FLOORBEAM HAS CORROSION. FABRICATED AND INSTALLED NEW FLOORBEAM UPPER TEE IAW EC-RA 5310-05536.SDR UALA2013032201785Cusp Web · corrodedMAIN CABIN, RT CUSP WEB CORRODED BS 1020 - 1027, RBL 65 - 69. FABRICATED NEW WEB IAW DWG 144N5140. INSTALLED WEB IAW SRM 51-40-02.SDR UALA2013032201802Skin · dentedSKIN DENTED BS 1420-1440, BETWEEN STRINGERS 16 - 17L. HFEC INSPECTION IAW NDT PT 6, 51-00-19, NO CRACKS NOTED. DENT SMOOTH AND CRACK FREE. REMOVED DAMAGE IAW SRM 53-00-01 FIG 201. FABRICATED AND INSTALLED DOUBLER IAW 53-00-01 FIG 201.SDR UALA2013032201789Skin · dentedDENT IN FUSELAGE SKIN ABOVE STR17L BTWN BS 1420 AND 1440. REMOVED DAMAGE IAW SRM 53-00-01. FABRICATED AND INSTALLED DOUBLER IAW SRM 53-00-01 FIG, 201 REPAIR 3.SDR UALA2013032101761Door Frame · corrodedR1 DOOR AFT CUTOUT FRAME HAS CORROSION AT WL 207. REMOVED DAMAGED SECTION OF FRAME AND INSTALLED SLICE DOUBLER RPR SRM 53-10-15 AND EA 130272.SDR UALA2013032101760Floorbeam · corrodedFLOORBEAM UPPER AND LOWER SURFACE AT FLOORBOARD ATTACH HOLES CORRODED STA 365, RBL 10- RBL 50. TRIMMED UPPER SECTION OF DAMAGED TEE CAP AND INSTALLED ANGLE STRAP REPAIR PER ECRA 5310-05536.SDR UALA2013032101759Skin · dentedSKIN DENTED BS 820, ABOVE STRINGER 17L. INSTALLED DOUBLER REPAIR PER EA 130246, ECRA 5330-04465.SDR UALA2013032101758Floorbeam · corrodedCABIN FLOORBEAM TEE CAP HAS CORROSION BS 1661, BL 0 TO LBL 25. INSTALLED TEE CAP SECTION FILLER ANGLE REPAIR PER ECRA 5310-05536 AND SRM 53-00-51.SDR UALA2013032101757Stringer · damagedSTRINGER 16L IS DAMAGED AT BS 607. INSTALLED STRINGER SPLICE REPAIR PER EA 130227 REV IR AND ECRA 5330- 04460.SDR UALA2013032101756Skin · dentedSKIN DENTED BS 607, BELOW STRINGER 16L. INSTALLED SKIN DOUBLER REPAIR PER ECRA 5330-04460, AND EA 130227 REV IR.SDR UALA2013032201784Unknown · unknownLAVATORY AND POTABLE WATER ISSUE, FLIGHT DIVERTED.SDR UALA2013032101764Skin · dentedEXTERNAL FUSELAGE SKIN HAS A DENT AT BS 1694, STR 12L- 13L. EVALUATED DENT AND FOUND TO BE WITHIN LIMITS OF SRM 53-00-01, FIG 101, SHT 4, DETAIL III. HFEC ACCOMPLISHED PER NDT 6-51-00-19 AND NO CRACKS NOTED.SDR UALA2013032101762Smoke Goggles · faultyCAPTAIN'S SMOKE GOGGLES ELASTIC HEADBAND STRETCHED OUT, DOES NOT PROVIDE SNUG FIT. REPLACED SMOKE GOGGLES.SDR UALA2013032101772Control Unit · faultedECU FAULT WAS "FIRE EMERG " CYCLED BOTH FIRE HANDLE IN FLT DECK AND REMOTE SHUTDOWN SW AT NOSE GEAR. AFTER ECU RESET FULLY, OPS NOW NORMAL. 3 SUCCESSIVE GOOD STARTS.SDR UALA2013032001730Skin · dentedDENT BELOW L1 DOOR APPROXIMATELY BS 340 S18 AT SKIN LAP 8.5L BY 7.5W BY .150 DEEP. REMOVED SHEAR TIE. COMPLIED WITH REPAIR PER ECRA 5330 04470 AND AVO ESC 130317-5426-1A, 130317-5426-1, 130316-5426-1.SDR UALA2013032101770Apu · failedAPU INOPERATIVE. REPLACED SURGE VALVE, BATTERY AND STARTER. APU STILL HANGS AT 30 TO 40 PERCENT. SWAPPED ECU AND BATTERY CHARGER, NO HELP. INSTALLED OLD CHARGER AND ECU. REPLACED APU.SDR UALA2013032001736Cover · looseEMERGENCY EXIT LIGHTING COVER ROW 38 LOOSE. ACCOMPLISHED INTERIM REPAIR SECURED FLOOR TRACK LIGHT COVER AT ROW 38 PER GMM 05-30-06. REPLACED EMERGENCY LIGHTING COVER AT ROW 38, OPS CHECKED GOOD.SDR UALA2013032001749Lens · unsecureEXIT SIGN INOP AT SEATS 9CD. SECURED EXIT SIGN LENS AT 9CD, OPS CHECK OKAY.SDR UALA2013032001747Cover · unsecureEMERGENCY LIGHT NEAR CLOSET AT 1L NOT SECURE. SECURED LIGHT COVER, OPS GOOD.SDR UALA2013032101771Bonding Wire · brokenBONDING WIRE ON PC AIR DOOR BROKEN. REPLACED BONDING WIRE ON AC AIR DOOR.SDR UALA2013032001706Exciter · failedAPU NO START. REPLACED EXCITER, LEAD AND IGNITER PLUG. OPS NORMAL.SDR UALA2013032001705Slat System · malfunctionedWHEN FLAPS SELECTED TO POS 1, RECEIVED A LEADING EDGE SLAT DISAGREE EICAS AND FLAP INDICATION SHOW FLAP BETWEEN UP AND POS 1. TRIED TO MOVE FLAPS WITHIN ALTERNATE WITH BOTH LEADING AND TRAILING EDGE FLAPS SELECTED, NO MOVEMENT OCCURED. RECEIVED A LEADING EDSDR UALA2013032001739Skin · damagedRIGHT WING INBOARD AFT FLAP UNDERSIDE SKIN OUT OF CONTOUR. REMOVED AND REPLACED RT INBOARD AFT FLAP.SDR UALA2013032001729Connector · shortedEXTERNAL EMERGENCY LIGHT AT L1 DOOR DOES NOT WORK. FOUND PIN 10 ON CONNECTOR SHORTED TO GROUND. ISOLATED PIN 10 FROM CONNECTOR LIGHT WORKS. CAPPED AND STOWED WIRE 35 320-110-20 FROM CONNECTOR D68 AT POWER SUPPLY M731. EMERGENCY LIGHTS OP CHECKED GOOD.SDR UALA2013032001728Wire · damagedNR 1 LEADING EDGE SLAT ASYM MESSAGE ON EICAS. PER TROUBLESHOOTING FIM TASK 27-81-05 REMOVED AND REPLACED LT OUTBOARD SLAT LOSS SENSOR SWITCH PER AMM. REPAIRED WIRE WITH ENVIRONMENTAL SPLICE PER SWPD 20-10- 12. SYSTEM OPS CHECKED OKAY.SDR UALA2013032101774Cap · missingL2 WINDOW HT WIRES-CAPS MISSING. REPLACED CAPSDR UALA2013032001721Ace · malfunctionedFORWARD CARGO LOADING NESTING SYSTEM WILL NOT EXTEND. THE ACE CARGO LOADING SYSTEM IS THE SUBJECT OF AD2000-20-16, WHEN CLEARING THE DEFERRED ITEM REMOVE QUICK RELEASE PINS AND RETURN TO VINYL POUCH IF INSTALLED IN LOB BIN CARGO LOADING SYSTEM MUST BE REACTIVSDR UALA2013031901688Fan · inoperativeHOT ODOR FOR 2-3 MINUTES AFTER TAKEOFF, WENT AWAY BY ITSELF, DE ICE WAS NOT AN ISSUE. ACCOMPLISHED AC SYSTEM CHECK. REF MM 21-00-01-301 PROCEDURE 1. BEGAN FIM UP TO PROCEDURE 13A. INSPECTED LEFT RECIRCULATION FAN IN FORWARD CARGO FOR BURNED WIRES AND ODOR. SDR UALA2013032001723Display · failedLOWER EICAS SCREEN RED. REPLACED SCREEN.SDR UALA2013032001750Light · inoperativeLEFT AFT OVERWING EMERGENCY LIGHT INOP. REPAIRED L562 LIGHT ASSY FOR BROKEN CONTACT-TAB REPLACED M10770 BATTERY CHARGER FOR NO OUTPUT FROM PIN 9. LEFT AFT OVERWING EMERGENCY LIGHT, OPS CHECK OK.SDR UALA2013032001738Light · unsecureEMERGENCY LIGHT STRIP COMING UP AT 25C. SECURED LIGHT.SDR UALA2013032001737Cap · separatedEMERGENCY LIGHT END CAP SEPARATING FROM PLASTIC STRIP AT 8C. SECURED END CAP, CHECKED OKAY.SDR UALA2013032001725Fcu · failedNR 1ENG FLAME OUT. REMOVED AND REPLACED FUEL PUMP AS PER AMM, FUEL CONTROL AS PER AMM AND ALSO EEC AS PER MM 73-21-04.SDR UALA2013032001701Strap · crackedAFT CARGO COMPARTMENT AT BS 1380 WL 199 RBL 46 STABILIZER STRAP IS CRACKED & BROKEN. INSTALLED STABILIZER STRAP REPAIR IAW ECRA 5315-01063.SDR UALA2013032001746Cover · damagedEMERGENCY LIGHT COVER DAMAGE BY 8C. REPLACED COVER.SDR UALA2013032001722Liner · puncturedR1 DOOR UPPER LINING HAS A PUNCTURE. NO DAMAGE NOTED BEHIND UPPER LINING. FILLED HOLE AND SANDED SMOOTH.SDR UALA2013032001748Duct · dirtyRIGHT RECIRCULATION FAN EXTREMELY LOUD. CLEANED DUCTS AT FLIGHT DECK. WINDSHIELD DECIBEL READING DIFFERENCE LESS THEN 3 DB AND READING AT 68.9 DB, OK FOR FLIGHT.SDR UALA2013032001703Wedge · dentedLEFT WING NR 1 SLAT TRAILING EDGE WEDGE AT 38 INCH INBOARD FROM OUTBOARD EDGE AND 4 INCH, FWD OF TRAILINGE EDGE IS DENTED. DENT IS WITHIN LIMITS BUT DUE TO BEING IN EXCESS OF 2 INCH IN DIAMETER, REQUIRES REPAIR SRM 57-43-01 FIG101 SHEET 4 NOTEJ AND FIG101 SSDR UALA2013032001699Frame · damagedFRAME WEB IS PARTIALLY CUT ON FWD SIDE BS 365.25 S17R. REMOVED DAMAGED FRAME BS 365.25 FABRICATED SPLICE AT RT WL190. ACCOMPLISHED REPAIR IAW EA 130272 AND ECRA 5310- 05704.SDR UALA2013032001743Cap · missingEMERGENCY FLOOR TRACK LIGHT END CAPS MISSING ROWS 8 AND 12. REPLACED END CAPS.
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