Boeing 757-212

Service difficulty reports · 377

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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 = '757212'
  ORDER BY difficulty_date DESC"

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SDR DL75A040945Control Cable · wornHMV-3 VISIT IN DFW. CABLE WORN, AILERON CABLE WORN AT LEFT WING OVERRIDE QUADRANT. CABLE FOUND TO BE IN POSITION A1B-4 AND PN BACC2C4AD06518FG. REPLACED CABLE PER OPN 2000 AND INSTALLED RECOMMENDED OPTIONAL CABLE PN BACC2C4CD06518FG ON RC 1388-1392 WITH RIISep 29, 2004 · N750AT · Boeing 757212 · Aileron Control SystemSDR DL75A040884Bear Strap · crackedFUSELAGE BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR. REPAIRED IAW ERA 093001-14AD.Sep 16, 2004 · N757AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A040878Skin · corrodedFUSELAGE SKIN AT STATION 1510 BETWEEN STR 28L - 29L CORRODED. REPAIRED IAW ERA 092820-14.Sep 14, 2004 · N757AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A040872Switch · incorrectGAP INCORRECT. GAP BETWEEN AUTOFIRE SWITCH ROLLER AND CAM INCORRECT IN RIGHT AFT OVERWING EXIT CUTOUT. REPLACED ADJUSTED GAP BETWEEN AUTO FIRE SWITCH ROLLER AND CAM IN RIGHT AFT OVERWING EXIT PER AMM 25-26-11-404-010. TEST NOW CORRECT PER AMM.Sep 5, 2004 · N757AT · Boeing 757212 · Door Warning SystemSDR DL75A040871Bracket · damagedSTA 333.45 STR 7L PULLEY EMERGENCY POWER ASSIST PASSENGER DOOR L-1. PULLEY BRACKET DAMAGED. REMOVED DAMAGED PULLEY BRACKET. REMOVED FASTENER, DRILLED MOUNT HOLES. REPLACED PULLEY BRACKET PER BAC 141N6322. EMERGENCY POWER ASSIST SYSTEM RIGGED ON OPN 7899.Sep 3, 2004 · N757AT · Boeing 757212 · Fuselage Miscellaneous StructureSDR DL75A040874Cam · corrodedCAM CORRODED RIGHT OVERWING EXIT HATCH CUTOUT AUTO FIRE SWITCH CAM FWD POSITION. CLEANED CAM AND HAND BURNISHED PAINT AND DIRT RESIDUE. NO CORROSION FOUND PER SRM 51-10-02. CW VISUAL PER SRM 51-10-02, NO CORROSION FOUND. OK TO TREAT AND PAINT. RESTORED FIAug 31, 2004 · N757AT · Boeing 757212 · Door Warning SystemSDR DL75A040873Switch · corrodedRIGHT AFT OVERWING EXIT CUTOUT AUTOFIRE SWITCH CAM CORRODED. REMOVED CORROSION PER SRM 53-00-00D FIG 1. OK TO CHECK LIMITS. RIGGED SWITCH PER AMM. FOUND CAM OUT OF LIMITS PER BAC DWG 284N1508 AND REPLACED SWITCH ASSY.Aug 19, 2004 · N757AT · Boeing 757212 · Door Warning SystemSDR DL75A040662Skin · crackedFUSELAGE, SKIN L1 DOOR CUTOUT, UPPER FWD CORNER REPAIR OF CRACK FATIGUE CRACK FOUND DURING INSPECTION OF THE L1 DOOR CUTOUT. ERA WAS GENERATED INSTALLING A REPAIR DOUBLER, TRIPLER AND QUADRUPLER TO REPAIR THE DAMAGE. ERA 097855-14AD REVISION ORIGINALJul 15, 2004 · N750AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A040390Controller · inoperativeAT 37,000 FT CABIN ALTITUDE HORN CAME ON. SWITCHED TO AUTO 2 WITH NO IMMEDIATE ALT MOVEMENT, SO SWITCHED TO MANUAL. REPLACED NR 1 AUTO PRESSURE CONTROLLER.May 3, 2004 · N757AT · Boeing 757212 · Cabin Pressure ControllerSDR DL75A040333Skin · dentedTHE FUSELAGE SKIN WAS FOUND DENTED AT FS 1645, JUST BELOW STRINGER 19R. THE DENT WAS REMOVED WITH A 3.5 X 3.2 INCH CUTOUT. THE CUTOUT WAS REPAIRED WITH TWO EXTERNAL ALUMINUM DOUBLERS PER ER/A 089688-14, REV A.Apr 10, 2004 · N752AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A040287Tire · separatedNR 4 AND NR 8 MAIN TIRES BLOWN/DEFLATED CONFIRMED BY GROUND PERSONNEL ON TAKEOFF AT LGA. NR 8 TIRE LOST CAP, NR 4 TIRE FLAT. REPLACED ALL 4 WHEEL ASSYS ON RIGHT TRUCK. ALSO REPLACED NR 8 BRAKE LINE AND NR 4 AND 8 BRAKE ASSYS DAMAGED BY TIRE CAP. REPLACED Apr 1, 2004 · N750AT · Boeing 757212 · TireSDR DL75A031068Bottle · defectiveNOTICED AFTER COCKPIT INDICATOR LIGHTS TEST, CARGO BOTTLE 1 DISCHARGE LIGHT REMAINED ILLUMINATED WITH ASSOCIATED MESSAGE ON EICAS. REPLACED BOTTLE.Dec 2, 2003 · N757AT · Boeing 757212 · Fire Bottle, FixedSDR DL75A030811Inverter · failedSTANDBY INVERTER INOP. REPLACED STANDBY INVERTER.Sep 4, 2003 · N751AT · Boeing 757212 · AC InverterSDR DL75A030629Wire · burnedIRR: FWD AND AFT CARGO DOORS INOPERATIVE. FOUND BURNT WIRE BEHIND AFT CARGO DOOR SWITCH. REPLACED SAME. REPLACED K101 AND PSEU. SLACK IN WIRES ENOUGH WHEN CUT BACK TO REINSTALL ON NEW SWITCH. K101 AND PSEU DAMAGED WHEN WIRE SHORTED OUT.Jul 12, 2003 · N751AT · Boeing 757212 · Door System WiringSDR DL75A030590Wire · brokenEMERGENCY PATH LIGHT INOP AT ROW 40DEF. REPAIRED BROKEN WIRE UNDER SEAT TRACK, OPS NORMAL.Jun 26, 2003 · N757AT · Boeing 757212 · Light System WiringSDR DL75A030391Light · inoperativeEMERGENCY LIGHT AT SEAT 40 DEF INOP. RELAMPED SAME.Apr 27, 2003 · N757AT · Boeing 757212 · Emergency LightingSDR DL75A021210Ballast · failedAPPROXIMATELY 3 PLUS HOURS FROM ATL DURING FLT ELECTRICAL ODOR IN FIRST CLASS CABIN - REPLACED 2CD BALLAST AND LAMPSOct 18, 2002 · N752AT · Boeing 757212 · Passenger Compartment LightingSDR DL75A021141Odor · detectedON CRUISE F/A SMELT ODOR SIMILAR TO BURNT POPCORN NEAR ROW 33. ENG A/I WAS ON. SMELL DISSIPATED AFTER A/I AND LIGHTS WERE TURNED OFF. OPERATED PACKS BOTH INDEPENDENTLY AND TOGETHER IN FULL HOT POSITION. ALSO RAN BOTH ENG USING INDIVIDUAL ENGS ANTI ICE NO BSep 26, 2002 · N757AT · Boeing 757212 · Air Distribution SystemSDR DL75A020353Bulkhead · corrodedFUSELAGE / BULKHEAD / FS 900 / STRG. 28L-28R / LOWER CHORD AND WEB : CORROSION REPAIR THE LOWER CHORD AND WEB OF THE FS 900 BULKHEAD WAS FOUND CORRODED BETWEEN STRINGERS 28L & 28R. THE DAMAGED SECTION OF WEB WAS CUTOUT ANMar 20, 2002 · N752AT · Boeing 757212 · Fuselage Main, FrameSDR DL75A020352Skin · corrodedFUSELAGE / SKIN / FS 900 / STRG. 28L-28R : CORROSION REPAIR THE FUSELAGE SKIN WAS FOUND BADLY CORRODED AT FS 900 AND BETWEEN STRINGERS 28L & 28R. THE SKIN WAS CUT AT FS 885 AND THE AFT SECTION Mar 20, 2002 · N752AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A020349Skin · gougedFUSELAGE / SKIN / FS 676 / STRG. 23R : GOUGE CUTOUT REPAIR THE FUSELAGE SKIN WAS BADLY GOUGED BY A WORK STAND AT FS 676 NEAR STRINGER 23R. THE GOUGE WAS REMOVED WITH A 7.9" X 3" CUTOUT. THE CUTOMar 20, 2002 · N752AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A020348Skin · corrodedFUSELAGE / SKIN / FS 426 / STRG. 1-2R / TCAS ANTENNA CUTOUT CORROSION REPAIR CORROSION WAS FOUND AROUND THE TCAS ANTENNA CUTOUT AT FS 426 BETWEEN STRINGERS 1 AND 2R. THE EXISTING TCAS DOUBLER WAS REMOVED AND DISCMar 20, 2002 · N752AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A020347Skin · corrodedTHE FUSELAGE SKIN AND UNDERLYING BEAR STRAP WERE FOUND WITH AREAS OF CORROSION NEAR THE C2 DOOR CUTOUT AT FS 1440 AND STRINGERS 25R-26R. THE CORROSION WAS REMOVED FROM THE BEAR STRAP AND ANOTHER IN THE SKIN. THE CUTOUTS WERE REPAIRED WITH EXTERNAL DOUBLERS PMar 20, 2002 · N752AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A020335Floorbeam · corrodedTHE UPPER CAP OF THE FS 1681 FLOORBEAM WAS FOUND WITH SEVERAL AREAS OF CORROSION. THE UPPER CAP WAS TRIMMED OFF TO REMOVE ALL AREAS OF CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED PER ER/A 382554-14, REV A.Mar 18, 2002 · N752AT · Boeing 757212 · Fuselage Main, Floor BeamSDR DL75A020334Door Frame · corrodedC1 DOOR OPENING LOWER CHORD CORRODED, THE FS 620 OPENING FRAME OUTER CHORD AND WEB WERE CUT AND THE LOWER SECTIONS REMOVED TO ALLOW ACCESS TO THE CHORD. AFTER REPLACEMENT OF THE CHORD, THE LOWER SECTION OF FRAME CHORD AND WEB WERE REINSTALLED AND SPLICE WITH Mar 18, 2002 · N752AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A020336Trunnion · corrodedINSPECTION OF THE RT MLG FWD TRUNNION SUPPORT FITTING FUSE PINS PER AD 2000-07-13 REVEALED CORROSION IN THE FUSE PIN LUG BORES OF THE FITTING. THE CORROSION WAS REMOVED BY OVERSIZING THE LUG BORES AND INSTALLING OVERSIZED BUSHINGS. THE REPAIR WAS ACCOMPLISHEMar 16, 2002 · N752AT · Boeing 757212 · Main Landing Gear Attach SectionSDR DL75A020192Flap · corrodedLEFT MAIN FLAP, LWR CHORD WAS FOUND CORRODED. REPAIR PER ER/A 410943-14.Feb 15, 2002 · N752AT · Boeing 757212 · Trailing Edge FlapsSDR DL75A020074Connector · not seatedLEFT HYD ELECT PUMP EICAS MSG CAME ON AND PRESS LIGHT IN THE LEFT HYD PUMP SWITCH ILLUMINATED. FOUND PUMP OPN NORMAL. RESEATED PRESSURE SWITCH PLUG. PUMP, LIGHT, AND MSG ALL CHECK OK. REPLACED OVERHEAD HYD CONTROL PANEL AND LEFT SYS HYD ELECT PUMP LOW PRESJan 21, 2002 · N750AT · Boeing 757212 · Hydraulic Pressure SensorSDR DL75A011861Bear Strap · corrodedFUSELAGE / SKIN / C2 DOOR CUTOUT / FS 1440 / STRG. 25R-26R: CORROSION BLEND REPAIR THE INTERNAL BEAR STRAP AROUND THE C2 DOOR CUTOUT WAS FOUND WITH AN AREA OF CORROSION NEAR THE AFT EDGE OF THE DOOR AT FS 1440 BETWEEN STRINov 22, 2001 · N757AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A011838Spar · gougedTHE FWD UPPER SPAR WEB OF THE NR 2 PYLON WAS FOUND WITH A DEEP GOUGE AT NAC STA 128 AT RBL 2. THE WEB WAS CUT FWD AND AFT OF THE DAMAGE AND THE DAMAGED SECTION OF WEB WAS REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH ALUMINUM DOUBLERS PER ER/A 381993-14,Nov 20, 2001 · N757AT · Boeing 757212 · Nacelle/Pylon, Frame/Spar/RibSDR DL75A011837Sill · corrodedTHE LOWER DOOR SILL OF THE C2 DOOR OPENING WAS BADLY CORRODED AND NEEDED TO BE REPLACED.Nov 20, 2001 · N757AT · Boeing 757212 · Fuselage Miscellaneous StructureSDR DL75A011665Fseu · malfunctionedIN CRUISE RECEIVED EICAS MSG LEADING EDGE SLAT ASYMMETRY WITH LEADING EDGE INDICATOR LIGHT. FLAPS INDICATED BETWEEN UP AND 1 POSITION. HANDLE WAS IN UP OR 0 POSITION. VISUAL CHECK CONFIRMED LEADING EDGE SLATS IN UP POSITION. CYCLED FLAPS AND SLATS AFTER CLOct 14, 2001 · N750AT · Boeing 757212 · Trailing Edge Flap Control SystemSDR DL75A011670Floorbeam · corrodedTHE UPPER CAP OF THE FS 1681 PASSENGER FLOORBEAM WAS FOUND CORRODED IN SEVERAL AREAS. THE ENTIRE CAP WAS CUT OFF TO REMOVE ALL CORROSION. A NEW CAP WAS FABRICATED AND INSTALLED IN PLACE OF THE REMOVED CAP PER ER/A 381633-14, REV A.Oct 12, 2001 · N750AT · Boeing 757212 · Fuselage Main, Floor BeamSDR DL75A011657Door Frame · corrodedTHE FWD FRAME OF THE C2 DOOR OPENING AT FS 1380 WAS FOUND WITH CORROSION ON THE OUTER FRAME CAP NEAR STRINGER 27R. THE CHORD WAS CUT JUST ABOVE THE DAMAGE AND THE LOWER SECTION REMOVED. A NEW SECTION OF CHORD WAS FABRICATED AND SPLICED IN WITH REPAIR ANGLES.Oct 11, 2001 · N750AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A011648Skin · dentedFUSELAGE / SKIN / FS 690 / STRG. 24R-25R : SKIN CUTOUT REPAIR AN EXISTING SKIN REPAIR DOUBLER WAS DAMAGED AND REMOVED. THE UNDERLYING SKIN WAS CLEANED UP WITH A 8" X 4" CUTOUT. THE CUTOUT WAS REPAIOct 10, 2001 · N750AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A011649Door Frame · corrodedTHE LOWER SILL BEAM OF THE C2 DOOR OPENING WAS BADLY CORRODED AND REQUIRED REPLACEMENT. TO REMOVE AND INSTALL A NEW SECTION, THE OUTER CHORD OF THE FS 1440 OPENING FRAME WAS CUT AT STRINGER 26R AND THE WEB CUT AT STRINGER 23R. THE LOWER SECTIONS WERE REMOVEDOct 8, 2001 · N750AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A011563Skin · dentedFUSELAGE / SKIN / FS 278 / WL 208 : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND DENTED NEAR FS 278 AT WL 208. THE DENT WAS REMOVED WITH A 5" X 4" CUTOUT. THE CUTOUT WAS REPAIRED WITH ANSep 19, 2001 · N750AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A011210Cooler · leakingACFT DIVERTED TO MIA EN ROUTE TO BOG DUE TO RT ENG LOW OIL QTY. FOUND ENG FUEL OIL COOLER. F/O COOLER LEAKING AT ENG OIL INLET ELBOW ADAPTER. REPLACED F/O COOLER. LEAK CHECK NORMAL.Jul 17, 2001 · N751AT · Boeing 757212 · Engine Fuel/Oil CoolerSDR DL75A011160Bear Strap · corrodedTHE C2 DOOR SURROUND BEARSTRAP AT FS 1380 WAS FOUND WITH TWO AREAS OF CORROSION AT STRINGERS 22R AND 23R.Jul 12, 2001 · N751AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A011159Skin · dentedFUSELAGE / SKIN / FS 620 / STRG. 16L-17L : DENT CUTOUT REPAIR THE FUSELAGE SKIN WAS FOUND WITH SEVERAL DENTS NEAR FS 620 AND STRINGERS 16L & 17L. THE DENTS WERE REMOVED WITH A 7" X 6" CUTOUT AND AJul 12, 2001 · N751AT · Boeing 757212 · Fuselage Main, Plate/SkinSDR DL75A011154Frame · cutFUSELAGE / C1 DOOR OPENING / FRAME / FS 620 / STRG. 25R-26R:FRAME WEB AND OUTER CHORD SPLICE REPAIR THE C1 DOOR OPENING LOWER SILL OUTER CHORD REQUIRED REPLACEMENT DUE TO CORROSION. TO FACILITATE REMOVAL AND INSTALLATION OF A NEJul 10, 2001 · N751AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A011118Door Frame · corrodedTHE LOWER SILL CAP OF THE C2 DOOR SURROUND STRUCTURE WAS BADLY CORRODED AND REQUIRED REPLACEMENT.Jul 5, 2001 · N751AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A011001Bulkhead · gougedFUSELAGE / SKIN & BULKHEAD / FS 1700-1780 / STRG. 26L-26R : GROUND DAMAGE REPAIR THE FUSELAGE SKIN FWD AND AFT OF THE FS 1720 BULKHEAD WAS GOUGED AND PUNCTURED FROM A TAIL STRIKE DURING LANDING. THEBULKHEAD WEB WAS SLIJun 15, 2001 · N750AT · Boeing 757212 · Fuselage Main, StructureSDR DL75A010605Slide · dislodged3L ENTRY DOOR OPENED WHILE ARMED, SLIDE DID NOT DEPLOY, IT FELL ON SERVICE TRUCK - REPLACED SAMEApr 12, 2001 · N752AT · Boeing 757212 · Escape SlideSDR DL75A010409Wire · brokenEMERGENCY LIGHT INOP AT SEAT ROW 33DEF. REPAIRED BROKEN WIRE AT SEAT ROW 33DEF, EMERGENCY LIGHT OPS CK. GOODMar 12, 2001 · N750AT · Boeing 757212 · Emergency LightingSDR DL75A000975Engine · flamed outRT ENGINE ROLLED BACK AND QUIT DURING DESCENT INTO ATL PASSING THRU 21,000 FT. REPLACED RT ENGINE.May 16, 2000 · N752AT · Boeing 757212 · Engine (Turbine/Turboprop)SDR DL75A000687Jackscrew · damagedON FINAL FLAPS STUCK AT 17 DEGREES. TRAILING EDGE LIGHT ON. VISUAL INSPECTION SHOWS RIGHT INBOARD T/E FLAPS NOT EXTENDED WITH DAMAGE ON INBOARD SIDE. REPLACED RT I/B FLAP CARRAIGE ROLLER BEARING. REPLACED RIGHT I/B FLAP CARRIAGE JACKSCREW AND GIMBAL ASSY PApr 7, 2000 · N757AT · Boeing 757212 · Trailing Edge Flap Control SystemSDR DL75A000623Actuator · inoperativeAFTER TAKEOFF, NOSE GEAR DID NOT RETRACT. RETURNED TO SLC. REPLACED NG ACTUATOR AND BYPASS SEQ VALVE.Apr 2, 2000 · N751AT · Boeing 757212 · Landing Gear ActuatorSDR DL75A000337Indicator · intermittentSTRONG ACID ODOR IN COCKPIT JUST PRIOR TO TAKEOFF WHEN TRANSPONDER WAS TURNED ON. RETURNED TO GATE. FOUND WEATHER RADAR INDICATOR INTERMITTENT PER CREW. REMOVED AND REPLACED WEATHER RADAR INDICATOR AND TRANSCEIVER CK OK. INSPECTED FWD AND MAIN E AND E COMPFeb 18, 2000 · N752AT · Boeing 757212 · Weather Radar SystemSDR DL75A992796Pwr Supply · inoperativeFWD CABIN FLOOR TRACK EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.Dec 18, 1999 · N750AT · Boeing 757212 · Emergency Lighting
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