Boeing 757-232

Service difficulty reports · 15,843

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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 = '757232'
  ORDER BY difficulty_date DESC"

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SDR DL757080865Skin · chafedLT WING NR 3 SLAT AT T/E AREA HAS CHAFING 2 EA LOCATIONS. REPAIRED CHAF IAW SRM 51-70-10.Jun 12, 2008 · N647DL · Boeing 757232 · Leading Edge DevicesSDR DL757080864Floorbeam · corrodedMAIN CABIN STA 1640 LBL FLOOR STRUCTURE "T" CHORD REPAIR EXFOLIATED AT FASTENER HOLE. REPLACED DAMAGED FLOOR STRUCTURE IAW SRM 53-00-51.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Main, Floor BeamSDR DL757080863Frame · dentedAFT CARGO PIT STA 1540 LT FRAME AT STR 23L HAS A DENT. REPAIRED DENT IAW SRM 53-00-07.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Main, FrameSDR DL757080862Angle · corrodedAFT CARGO PIT STA 1360-1380 WEB "L" ANGLE BETWEEN S 27R AND 26R CORRODED. REPLACED "L" ANGLE IAW SRM 51-10-01 AND 53-60-04.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757080861Skin · dentedDENT ON LT SIDE FUSELAGE STA 408 GOES ACROSS STR 16L AND 2 BAYS. REPAIRED DAMAGE IAW SRM 53-00-01.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080860Doubler · corrodedMAIN CABIN FLOOR STRUCTURE DECK PLATE REPAIR DOUBLER HAS CORROSION STA 1715 LBL 12. REPLACED DOUBLER IAW SRM 51-40-02.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757080859Seat Track · corrodedMAIN CABIN SEAT TRACK STARTING AT FS 630 LBL 45 TO FS 790 HAS NUMEROUS AREAS OF CORROSION DAMAGE. REPAIRED SEAT TRACK IAW SRM 53-30-52.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR DL757080858Web · corrodedRT SIDE MAIN CABIN FLOOR STRUCTURE IS CORRODED AT FS 1420-1440 LOWER WEB FWD END. REPLACED DAMAGED WEB IAW SRM 51-40-02.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757080857Stringer · corrodedUPON REMOVAL OF DOME NUT PLATE, FOUND EXFOLIATION CORROSION IN CHANNEL OF S 20R STA 758. REPLACED DAMAGED SECTION OF STRINGER IAW SRM 53-30-03 FIG 201.Jun 12, 2008 · N647DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080846Skin · damagedFUSELAGE SKIN LIGHTNING DAMAGE AT FS 330, S-26R. DAMAGE CUT OUT AND REPAIRED WITH DOUBLERS.Jun 9, 2008 · N689DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080875Ground Wire · looseSQUIB AND SWITCH TEST P61 PANEL FAILS TEST 1. TROUBLESHOT L EMERGENCY ESCAPE SLIDE SQUIB AND NR 1 TEST SWITCH ON P61 PANEL IAW WDM 25-65-01. FOUND LOOSE GROUNDS ON CONNECTOR D5544. RECONNECTED LOOSE GROUND WIRES ON CONNECTOR D5544 IAW SWPM 20-20-00. PERFORJun 6, 2008 · N647DL · Boeing 757232 · Equipment/Furnishings WiringSDR DL757081676Structure · unknownSUPPLEMENTAL SDR RT WING NR 7 SLAT TRAILING EDGE WEDGE REPAIR IAW ERA 468804-14, C/W ERA 468804-14.Jun 5, 2008 · N616DL · Boeing 757232 · Leading Edge DevicesSDR C8GA20080017Eec · malfunctionedFLT P0002 FROM PTY TO MFA. DURING CLIMB OPERATION OIL PSI WENT TO -4, N1=0, N2=0 ENG SHUTDOWN. ACFT RETURNED TO PTY WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND EEC TO BE AT FAULT. REMOVED AND REPLACED EEC, OPS CHECKS GOOD. NO FURTHER DEJun 4, 2008 · N620DL · Boeing 757232 · Fuel Controlling SystemSDR C8G2008F00001Eec · inoperativeDURING CLIMB OPERATION, OIL PSI WENT TO -4, N1=0, N2=0, ENGINE SHUTDOWN. AC RETURNED TO DEPARTURE WHERE IT LANDED WITHOUT INCIDENT. TROUBLESHOT SYSTEM AND FOUND EEC TO BE AT FAULT. REMOVED AND REPLACED EEC, OPS AND LEAK CHECKS GOOD. NO OTHER DEFECTS NOTED.Jun 4, 2008 · N620DL · Boeing 757232 · Fuel Controlling SystemSDR DALA1103880689Actuator · unknownHORIZONTAL STABILIZER TRIM ACTUATOR REPLACED IAW EA 06-086621-03, ME03.Jun 1, 2008 · N689DL · Boeing 757232 · Stabilizer Position IndicatingSDR DL757080807Stringer · corrodedSTA 1710 STR 27L HAS EXFOLIATING CORROSION AFT CARGO BAY. REPLACED STR SECTION PER SRM 53-00-03 FIG 201 REF NR 78981650001.May 31, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080806Channel · corrodedAFT CARGO STA 1720 STR 21L IS CORRODED/SPLICED IN NEW HAT CHANNEL PER SRM 53-00-03 FIG 201 REF NR78980200001.May 31, 2008 · N641DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757080805Stringer · corrodedAFT OF AFT CARGO BAY CORROSION AT STR 24L STA 1710/SPLICED STR HAT SECTION FROM STA 1690 TO 1720 PER SRM 53-00-03 FIG 201 AND 51-20-01 ON SAA N/R 78980240001.May 31, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080813Stringer · corrodedSTR 23L AT STA 1700, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080811Stringer · corrodedSTR 22L AT STA 1710, FOUND CORROSION. REPAIRED PER SRM 53-00-03 FIG 201.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080810Stringer · corrodedSTR 26L AT STA 1710 WAS FOUND TO HAVE CORROSION UNDER STRINGER. REPAIRED PER SRM 53-80-08 FIG 201.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080809Stringer · corrodedSTR 28 L HAS 2 AREAS OF CORROSION BETWEEN STA 1460 AND 1480/SRM 51-40-05. REPAIR REPORTED PER SRM 53-00-03.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080808Skin · dentedDENT ON STR BETWEEN STR 28R AND 29R AT STA 192. REPAIRED DENT PER SRM 53-00-01 REF SAA N/R 78986200001.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080804Structure · corrodedDURING HMV FOUND AFT CHORD CORRODED AROUND SEVERAL HOLES AFTER STR STR 27L TO 20L. REPLACED A SECTION OF THE CHORD PER SMR 53-80-08D REF SAA N/R 78986090001.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, BulkheadSDR DL757080793Structure · corrodedDURING HMV AT SAA, CORROSION WAS FOUND ON THE HORIZONTAL AFT CHORD OF THE AFT PRESSURE BULKHEAD, FORWARD SIDE AT STA 1720, S-19L. THE CORROSION WAS REPAIRED PER BOEING INSTRUCTIONS AS DOCUMENTED IN ER/A 06-468363-14.May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, BulkheadSDR DL757080812Stringer · corrodedSTR 20L AT 1680 AND STA 1700 FOUND CRACKED AND CORRODED. REMOVED DAMAGE, FABRICATED STRINGER, SPLICED, TREATED, IAW 757 SRM 51-40-05 F 201,May 30, 2008 · N641DL · Boeing 757232 · Fuselage Main, Longeron/StringerSDR DL757080782Fitting · damagedDURING HMV AT SAA, A HOLE WAS MISDRILLED COMMON TO THE NR 2 PYLON MIDSPAR FITTING, WEB, CHORD AND DOUBLER. THE HOLE WAS REAMED, BUSHED, AND REDRILLED PER BOEING INSTRUCTIONS.May 28, 2008 · N641DL · Boeing 757232 · Nacelle/Pylon, Plate/SkinSDR DL757080779Bulkhead · wornTHE NR 1 PYLON AFT BULKHEAD O/B VERTICAL FLANGE AT NAC STA 203 WAS FOUND WITH WEAR. THIS WEAR WAS CAUSED BY THE RUBBING OF THE PYLON AFT FAIRING UPPER SPAR FLANGE. THIS WEAR WAS FOUND DURING ACCOMPLISHMENT OF THE SIP MOD, S/B B757-54-0034. REPAIR WAS ACCOMPMay 28, 2008 · N641DL · Boeing 757232 · Nacelle/Pylon, Bulkhead/FirewallSDR DL757080781Fitting · damagedDURING ACCOMPLISHMENT OF THE SIP MOD PER S/B 757-54-0034 REV 1, THE NR 2 PYLON MID SPAR FITTING UPPER HORIZONTAL TANGE WAS MISDRILLED IN A FORWARD MOST HOLE LOCATION. THE FINAL CLEANUP SIZE HOLE WAS 0.704". A BUSHING AND RETENTION WASHER WERE INSTALLED AS A May 27, 2008 · N641DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/RibSDR DL757080780Brace · damagedDURING ACCOMPLISHMENT OF THE SIP MOD, S/B 757-54-0034 REV 1, THE DIAGONAL BRACE LOWER/FWD I/B LUG WAS INADVERTENTLY OVERSIZED TO 2.003" INSTEAD OF THE REQUIRED 2.000" MAXIMUM. AN OVERSIZED BUSHING WAS INSTALLED. AD 2003-18-05 APPLIES.May 27, 2008 · N641DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DL757080717Duct · obstructedON TAXI OUT HAD ELECTRICAL SMELL IN COCKPIT. FOUND BLOCKAGE IN COOLING TUBE TO CAPT'S VOR/DME CONTROL PANEL. CLEARED BLOCKAGE. ALSO, REPLACED CAPT'S VOR/DME CONTROL PANEL WHICH WAS CAUSE OF SMOKE FROM OVERHEAT. PANEL REPLACED WAS MFG NR 285T0554-5, S/N DO3May 10, 2008 · N666DN · Boeing 757232 · Air Distribution SystemSDR DL757080680Fan · overheatedON APPROACH TO LANDING, NOTICED A STRONG BURNING ELEC SMELL, DISSIPATED ON TAXI IN ALL IND INST NORMAL. REMOVED AND REPLACED NR 1 FWD EQUIPMENT COOLING FAN PER MM. OPN NML. ALSO, REPLACED EQUIPMENT COOLING FILTER.May 6, 2008 · N682DA · Boeing 757232 · Air Distribution FanSDR DL757080677Skin · damagedFUSELAGE SKIN FOUND WITH LIGHTNING STRIKES AT STA 1337, 1358, 1385 AT STR 25L. THE DAMAGE WAS CUTOUT AND REPAIR DOUBLERS WERE INSTALLED.May 5, 2008 · N690DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080833Duct · crackedAT FLT LVL 240 WITH ENGINE AND WING ANTI-ICE ON LEFT ENG BLEED LIGHT ILLUMINATED. FOLLOWED QRH SHUT BLEED SW OFF. OPENED ISOLATION VLV AT FLT LVL 260 RIGHT ENGINE BLEED LIGHT ILLUM. CABIN PRESSURE CLIMBED THROUGH 10K DEPLOYED MASKS. DECLARED EMERGENCY INTOMay 4, 2008 · N610DL · Boeing 757232 · Pneumatic Distribution SystemSDR DL757080659Skin · damagedFUSELAGE/SKIN/FS 1010 - 1038, S-1 TO S-3R, LIGHTNING STRIKES TOO CLOSE TOGETHER FOR SRM REPAIRS, AND ONE REPAIR ON FS 1040 FRAME WHICH REQUIRED NON-SRM REPAIR. DAMAGE CUTOUT OUT, DOUBLERS INSTALLED.May 4, 2008 · N621DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080643Fitting · damagedDURING HMV, AN ELONGATED HOLE WAS FOUND IN THE AFT BULKHEAD FITTING OF THE NR 2 PYLON. THE HOLE WAS REPAIRED PER BOEING INSTRUCTIONS.Apr 25, 2008 · N646DL · Boeing 757232 · Nacelle/Pylon, Bulkhead/FirewallSDR DL757080641Structure · damagedDURING HMV AT SAA, THE NR 1 PYLON INBOARD SIDE HAD AN ELONGATED HOLE IN THE UPPER CHORD AT N STA 128. THE ELONGATED HOLE WAS REPAIRED PER BOEING INSTRUCTIONS.Apr 25, 2008 · N646DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DL757080640Structure · crackedHMV AT SAA, A CRACK WAS FOUND IN THE UPPER CHORD OF THE NR 1 PYLON, RT SIDE, AT NACELLE STA 136. THE CRACK WAS REPAIRED PER BOEING INSTRUCTIONS.Apr 25, 2008 · N646DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DL757080631Frame · corrodedDURING HMV AT SAA, CORROSION WAS FOUND ON THE STA 1640 FRAME AT WL 210. THE CORRODED SECTION WAS REMOVED AND A REPAIR WAS INSTALLED PER BOEING DIRECTIONS.Apr 24, 2008 · N646DL · Boeing 757232 · Fuselage Main, FrameSDR DL757080630Skin · crackedDURING HMV AT SAA, A CRACK WAS DISCOVERED IN THE SKIN LAP JOINT AT STA 532, S-26L. THE CRACK WAS REMOVED AND A PERMANENT REPAIR WAS INSTALLED PER BOEING INSTRUCTIONS. REPETITIVE INSPECTIONS FOR FURTHER DAMAGE WILL BEGIN AT 37,500 TOTAL AIRCRAFT CYCLES AND EVApr 23, 2008 · N646DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DALA1121490624Gear · defectiveTRAILING EDGE FLAP TRANSMISSION GEAR REPLACED IAW EA 06-097281-03, ME02, ME04.Apr 19, 2008 · N624DL · Boeing 757232 · Trailing Edge Flap Control SystemSDR DL757080581Lamp · inoperativeEMERGENCY LIGHT OUT AFT OF LEFT WING. RELAMPED SAME, CKS OK.Apr 10, 2008 · N699DL · Boeing 757232 · Emergency LightingSDR DL757080580Light · inoperativeEMERGENCY LIGHT OUT RT AFT OVERWING POSITION. RELAMPED SAME.Apr 10, 2008 · N699DL · Boeing 757232 · Emergency LightingSDR DL757080579Lamp · inoperativeEMERGENCY LIGHT OUT AT R4 DOOR EXTERIOR, RELAMPED CKS OK.Apr 10, 2008 · N699DL · Boeing 757232 · Emergency LightingSDR DL757080578Connector · brokenEMERGENCY LIGHT OUT AT SEAT 4D, DEF PER MEL 33-51-03. FOUND WIRE BROKEN BETWEEN SEAT LEG CONNECTOR AND WALL CONNECTOR. REPLACED SAME. OPS CKS GOOD. MCO AND PLACARD REMOVED.Apr 10, 2008 · N699DL · Boeing 757232 · Light System WiringSDR DL757080567Skin · corrodedDURING HMV AT SAA, CORROSION WAS FOUND ON THE EXTERNAL SKIN AT STA 1510 BETWEEN S-28R AND S-29R WHERE AN AIRPHONE ANTENNA HAD PREVIOUSLY BEEN MOUNTED. SINCE THE ANTENNA IS NO LONGER USED, THE CORRODED SKIN WAS CUT OUT AND AN EXTERNAL REPAIR DOUBLER WAS INSTALApr 8, 2008 · N644DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080552Skin Panel · corrodedHMV AT SAA, CORROSION WAS FOUND ON THE EXTERNAL SKIN AT THE DME ANTENNA MOUNT AT STA 690, BL 0. THE CORROSION WAS REMOVED AND A REPAIR WAS INSTALLED WITH BOEING APPROVAL. LFEC INSPECTIONS ARE REQUIRED BEGINNING AT 37,500 CYCLES AND EVERY 3000 CYCLES THEREAFTApr 4, 2008 · N644DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080442Frame · dentedTHE STA 345 FUSELAGE FRAME WAS DAMAGED BETWEEN S-18L AND S-20L. THE DAMAGE SECTION OF FRAME WAS REMOVED AND A NEW FRAME SECTION WAS SPLICED IN.Mar 27, 2008 · N659DL · Boeing 757232 · Fuselage Main, FrameSDR DL757080441Skin · dentedFUSELAGE SKIN HAS A DENT AT STA 345 BETWEEN S-18L AND S-20L. THE DAMAGED SKIN WAS CUTOUT AND A REPAIR DOUBLER/TRIPLER WAS INSTALLED.Mar 27, 2008 · N659DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL757080403Unknown · smokeAFTER STARTING RT ENGINE AND PUTTING ON PACKS, COCKPIT FILLED WITH SMOKE. RAN LT AND RT PACKS OFF APU AIR. NO SMOKE OR ODOR. STARTED ENG OFF APU AIR CROSSBLEED STARTED LT ENG. RAN PACKS FULL H TO FULL COLD 3 TIMES. NO SMOKE OR ODOR. RAN ENG TO TAKEOFF PWMar 22, 2008 · N693DL · Boeing 757232 · Air Distribution System
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