Boeing 757-251

Service difficulty reports · 4,707

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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 = '757251'
  ORDER BY difficulty_date DESC"

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SDR DALA1126835501Skate Angle · crackedRT WING OUTBD OF RT PYLON T/E SKATE ANGLE CRACKED. PERFORMED HFEC INSP IAW NTM 51-00-19 PT 6. STOP DRILLED CRACK IAW SRM 54-52-01-801. REMOVED PNL 455BR IAW SRM 51-40-02. REMOVED SKATE ANGLE IAW SRM 51-40-02. RECEIVED FABBED SKATE ANGLE WITH TRAVELER T11/Apr 17, 2011 · N501US · Boeing 757251 · Nacelle/Pylon Miscellaneous StructureSDR DALA1126435531Intercostal · corrodedFLOORBEAM VERTICAL, INTERCOSTAL AT STA 395 RBL 19.5 HAS CORROSION. REMOVED CORROSION IAW SRM 51-10-01 OUT OF LIMITS IAW SRM 53-00-51 ORIG MAT. .040. NEW PART FABBED ON STAM TRAVELER T11/878529 MAT BAC-1508-238/70 75-T-65H, BATCH 3 0001962671. LOCATED & DRApr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1126425531Sill · corrodedAFT CARGO COMPT AT STA 1420 UPPER FRAME ADJACENT TO DOOR SILL CHANNEL SUPPORT HAS CORROSION. REMOVED SHEAR CLIP IAW SRM 51-40-02, REMOVED CORR ORIG .040, REMOVED .020, .020 REMAINING OUT OF LIMITS IAW SRM 53-00-53, FABBED NEW SHEAR CLIP ON TRAVELER T11/878861Apr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1126415531Intercostal · corrodedFLOORBEAM VERTICAL INTERCOSTAL AT STA 365-377 RBL 44 UPPER SURFACE HAS CORROSION AT MARKED. FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 ORIGINAL MAT'L .053 LOSS MAT'L .014, REMAINING MAT'L .039, REMOVED BEAM & ANGLES. RECEIVED PART (BEAM) DA-141N5185-24 ON Apr 16, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1126845501Wedge · damagedRT WING SLAT NR 8 LOWER T/E WEDGE PUNCTURED AS MARKED. REMOVED DAMAGE AREA AND FABRICATED DOUBLER REPAIR IAW SRM 51-70-10 PER WORKCARD 5742-01022-02H. DOUBLER FABBED FROM 2024T3-.020. AREA PAINTED IAW MM 51-21-10.Apr 15, 2011 · N501US · Boeing 757251 · Leading Edge DevicesSDR DALA1126405531Vertical Support · corrodedAFT CARGO DOOR LOWER INNER STRUCTURE NR 2 FROM FWD VERT SUPPORT BRACKET INR & OUTER SKIN CORRODED. REMOVED BRACKET IAW SRM 51-40-02, REMOVED CORR IAW SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 52-30-02 FIG 101. FABBED PART IAW TRAVELER T11/878611 DWG 14Apr 15, 2011 · N531US · Boeing 757251 · Cargo/Baggage DoorsSDR DALA1125725654Skin Panel · dentedREF SCEPTRE LOG 0261723 - REPAIR COMPLETED IAW ERA491662-14 REV ORIG.Apr 14, 2011 · N554NW · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1125785501Seat Track · crackedCOCKPIT AREA, CAPTAINS SEAT, OTBD AFT SEAT TRACK CRACKED AT AFT POSITION, AS MARKED. CONFIRMED CRACK L=0.5" NOT PERMITTED PER SRM 53-00-52, FIG 1, PAGE 101. R & R SEAT TRACK IAW SRM 51-40-02 AND AMM 25-11-01-201-925A-A.Apr 13, 2011 · N501US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1125525531Floor Support · corrodedFLOOR SUPPORT ANGLE AT STA 433-LBL 63 UPPER SURFACE HAS CORROSION, AS MARKED. REMOVED SUPPORT ANGLE IAW SRM 51-40-02. FABRICATED SUPPORT ANGLE ON STAM TRAVELER T11/878440. LOCATED AND DRILLED SUPPORT ANGLE IAW SRM 51-490-08. TREATED, PRIMED AND TOP COATED SUApr 12, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1125405531Plate · corrodedCABIN FLOOR SUPPORT METAL PLATE AT STA 365 RBL 26.5 UPPER SURFACE HAS CORROSION, AS MARKED. REMOVED CORROSION IAW SRM 51-10-02.CHECKED LIMITS: L=4.0 W=4.0 D=0.012. ORIGINAL OUT OF LIMITS IAW SRM 53-00-51. REMOVED METAL PLATE IAW SRM 51-40-0 2. FABBED NEW Apr 11, 2011 · N531US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1124745523Fairing · damagedDAMAGE TO LEFT BODY FAIRING PANEL 191AL IAW ER/A 491594-14 MADE TEMP REPAIR. REFERENCE LOG PAGE 0332195. ER/A 491594 SECTION I ISSUED FOR WING TO BODY FAIRING DAMAGE, PANEL 191AL AT BS 800. ASSOCIATED ER/A CHANGED FROM 13-491594 TO 14-491594 FOR AC 5523 APPApr 7, 2011 · N523US · Boeing 757251 · Aerodynamic FairingsSDR DALA1125475635Skin · damaged2 X 2 PUNCTURE LT SIDE OF FUSELAGE APROX 2 FT AFT AND 2 FT BELOW LAV SVC DOOR PANEL. REM DAMAGE IAW SRM 53-00-01, FIG 201 HFEC SURFACE SCAN OF CUTOUT IAW NDT MANUAL 51-00-19. NO DEFECTS. HFEC BOLT HOLE INSP OF EXISITING FASTENERS IAW NDT MANUAL 51-00-16. NOApr 5, 2011 · N535US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1123735521Sill · corrodedON REMOVAL OF AFT CARGO DOOR SIDE PANEL FOUND CORROSION ON AFT CARGO DOOR SILL. BLENDED CORR AREAS PER SRM 51-10-02. OUT OF LIMITS IAW SRM 53-60-15 FIG 101. REMOVED AND REPLACED DOOR SILL T-CHORD IAW SRM 51-40-02 & SRM 51-40-05. SPLICE SIDE PNL AT STA1485Apr 1, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1123725521Panel · corrodedAFT CARGO BETWEEN STA 1380 TO 1440 RBL 22 TO 25 TOP SURFACE OF SIDE PANEL HAS SEVERAL SPOT OF CORROSION AS MARKED. REMOVED CORROSION TOP & UNDERSIDE IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS PER SRM 53-00-53 FIG 101. REMOVED FWD SPLICE OF TRANS PANEL. ANApr 1, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1123715521Sill · corrodedAFT CARGO BETWEEN STA 1380 T0 1440 RBL 19 TO 25 UNDERNEATH OF DOOR SILL & SIDE PNL FASTENER & NUT PLATE HAS SURFACE CORROSION. BLENDED CORRODED AREAS ON LWR AREA OF DOOR SILL PER SRM 51-10-02. OUT OF LIMITS PER SRM 53-60-15 FIG 101. DOOR SILL REPLACED ON N/Apr 1, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1123515521Frame · corrodedAFT CARGO COMPT FLOOR FRAME AT STA 1460 BILGE FROM S-29L- S-29R AS CORROSION. BLENDED CORRODED IAW SRM 53-00-07. OUT OF LIMITS IAW SRM 53-00-07, FIG 101. TRIMMED DAMAGED AREA IAW ER/A 490233-14, FIG 1. NO CRACKS, FABRICATED REPAIR PARTS IAW ER/A490233-14. Mar 31, 2011 · N521US · Boeing 757251 · Fuselage Main, FrameSDR DALA1123175521Support Angle · corrodedANGLE SUPPORT AFT OF FRAME STN 1440 BETWEEN STR 27R AND S28R EXFOLIATED. REMOVED & INSTALLED NEW CLIP, P/N 146N8515-1, FABRICATED IAW STAM TR T11/876899, IAW SRM 51-40-02.Mar 30, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1123165521Stiffener · corrodedVERTICAL STIFFENER AT FRAME BS 1440 BETWEEN STR 27R AND 28R CORRODED NEAR AFT DOOR SILL. REMOVED & INSTALLED NEW CLIP, FABRICATED IAW STAM TRAVELER #T11/876864. P/N 146N5393-28 IAW SRM 51-40-02.Mar 30, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1122445523Intercostal · corrodedFWD CARGO INTERCOSTAL CORRODED STA 540-560 BETWEEN STR 26-27 R. FABRICATED AND REPLACED FWD CARGO INTERCOSTAL AT STA 540-560 STR 26-27R IAW SRM 51-40-02 PG:1, 2 AND 7.Mar 27, 2011 · N523US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1122435523Fitting · corrodedL-1 DOOR LWR SILL THRESHOLD SUPPORT STRUCTURE WEB FITTINGS AND ANGLES LITE CORROSION STA 333-377 LBL 63. ORIGINAL MATERIAL WAS .050" LENGTH WAS 15"WIDTH 1" DEPTH WAS .011". GAINED ACCESS PER B757 SRM 51-40-02. FABRICATED, LOCATED, DRILLED AND INSTALLED V CHMar 27, 2011 · N523US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1122425523Guide · corroded1 DOOR SLIDE GIRT BAR ALIGNMENT GUIDE IS EXFOLIATED. REMOVED AND REPLACED L1 DOOR SLIDE GIRT BAR ALIGNMENT GUIDE (RETAINER PLATE) PER CARD 2561-01257-01A, STEP 12 C.Mar 26, 2011 · N523US · Boeing 757251 · Emergency EquipmentSDR DALA1121805521Doubler · corrodedFWD CARGO COMPT STA 508 S-27R DOUBLER HAS SURFACE CORROSION AS MARKED. REMOVED CORRODED DOUBLER AND SHEAR TIE, RECEIVED NEW SHEAR TIE FABBED EXT REPAIR DOUBLER IAW SRM 53-00-01. LOCATED AND DRILLED NEW SHEAR TIE AND DOUBLER IAW SRM 51-40-05 TREATED & PRIMED Mar 23, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1121595534Switch · miswiredDURING A LINE CHECK, MAINTENANCE FOUND THE FLIGHT ATTENDANT EMERGENCY LIGHT TEST SWITCH INOPERATIVE. MAINTENANCE CORRECTED THE SWITCH WIRING. OPERATIONAL CHECK WAS GOOD.Mar 22, 2011 · N534US · Boeing 757251 · Light System WiringSDR DALA1121345639Wire · disconnectedSEAT - MOUNTED EMERGENCY LIGHTS FROM 20ABC TO 23ABC WOULD NOT ILLUMINATE. MAINTENANCE RECONNECTED THE WIRE. OPERATIONAL CHECK IS NORMAL.Mar 21, 2011 · N539US · Boeing 757251 · Light System WiringSDR DALA1119845521Floor Support · corrodedFLOOR SUPPORT AT BL 0 BETWEEN STN 1640 AND STN 1661 CORRODED AS MARKED. REMOVED CORR IAW SRM 51-10-02. ORIGINAL MAT THICKNESS=.050" OUT OF LIMITS IAW SRM 53-00-51. REMOVED FLOOR SUPPORT AND STIFFENER IAW SRM 51-40-02. FABBED NEW CHANNEL SUPPORT IAW DWG 146Mar 17, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119835521Floorbeam · corrodedAT RBL 13 BET FLOORBEAM STA 365TO STA 377 BOX BEAM HAS CORROSION AS MARKED. REMOVED BOX BEAM IAW SRM 51-40-02, FABRICATED NEW BOX BEAM AND ANGLES PER DWG 141N5162. LOCATED AND DRILLED NEW PARTS IAW SRM 51-40-05, TREATED & PRIMED IAW SRM 51-20-01, TOP COATED Mar 17, 2011 · N521US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1119205521Floor Support · corrodedAFT CARGO COMPARTMENT FLOOR SUPPORT AT STA 1456-1483 RBL 13.0 HAS CORROSION. REMOVED AND INSTALLED FLOOR SUPPORT SPLICERS IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119195521Floor Support · corrodedR4 DOOR FWD FLOOR SUPPORT CORRODED AT MANY LOCATIONS AS MARKED. REMOVED, FABRICATED, AND INSTALLED NEW FLOOR SUPPORT AT R4 DOOR FWD SUPPORT IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119185521Sill · corrodedLT DOOR SILL WEB AT STN 1663 CORRODED AS MARKED. REMOVED, FABRICATED, AND INSTALLED CHANNEL IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119175521Sill · corrodedLT DOOR SILL WEB AT STN 1655 CORRODED AS MARKED. REMOVED, FABRICATED, AND INSTALLED CHANNEL IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119165521Sill · corrodedLT DOOR SILL WEB AT STN 1772 CORRODED AS MARKED. REMOVED, FABRICATED, AND INSTALLED CHANNEL IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119155521Sill · corrodedL4 DOOR SILL WEB AT STN 1660 EXFOLIATED. FOUND TO BE OUT OF LIMITS IAW SRM 53-60-15 FIG 101. REMOVED, FABRICATED, AND INSTALLED NEW SILL WEB (CHANNEL) IAW SRM 51-40-02.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119145521Floor Support · corrodedR4 DOOR AFT FLOOR SUPPORT CORRODED AT MANY LOCATIONS AS MARKED. REMOVED, FABRICATED, AND INSTALLED IAW SRM 51-40-02.RETAIN FOR RECORDS.Mar 15, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1119135521Support Fitting · corrodedCABIN AREA STA 700 NR 3 FROM FWD SCUFF PLATE SUPPORT FITTING AT L2 DOOR SILL HAS CORROSION AS MARKED. REMOVED CORROSION AT BRACKET. BRACKET FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG 101 DETAIL IV (TR14295). REMOVED, FABRICATED, AND INSTALLED BRACKET IAMar 14, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1118715523Seat Track · corrodedSEAT TRACK AREAS OF LITE CORROSION STA 700 TO 780 LBL-45. SEAT TRACK CROWN AT STA 762 IS OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02, RECEIVED NEW SEAT TRACK LOCATED & DRILLED SEAT TRACK IAW SRM 51-40-05. INSTALLED SEAT TRACK IAW SRMMar 14, 2011 · N523US · Boeing 757251 · Fuselage, Seat/Cargo Attach FittingsSDR DALA1118705523Intercostal · corrodedFWD CARGO INTERCOSTAL CORRODED STA 740-760 O/B OF STR. REMOVED CORROSION OUT OF LIMITS IAW B757 SRM 53-00-04. REMOVED INTERCOSTAL AND CUT OUT DAMAGED AREA PER 757 SRM 51-40-02 AND 51-70-11, FABBED DOUBLER REPAIR LOCATED, DRILLED, DEBURRED INSTALLED INTERCOSTMar 14, 2011 · N523US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1118695523Web · corrodedAFT GALLEY AREA FLOOR WEBB HAS CORROSION STA 1680 TO 1720 BETWEEN BL-0 TO LBL-60. REMOVED CORR IAW SRM 53-60-51. NDT NO CRACKS AND MAT LOSS ON STA 1716, STA 1716-1707, STA 1685, STA 1683 LBL 38 ,LBL 28 ,STA 1682 LBL 17, STA 1700-1694 LBL 25-18 AND STA 1698Mar 14, 2011 · N523US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1118685523Web · corrodedAFT GALLEY AREA FLOOR WEB HAS CORROSION STA 1680 TO BL-0 TO RBL-60. REMOVED CORROSION ON STA 1680 TO 1720 BETWEEN BL-0 TO RBL-60 IAW SRM 53-60-51 PG 201. NDT FOUND NO CRACKS AND FOUND MAT LOSS AT STA 1716 RBL 2 STA 1682 RBL 19 TO 24 WITHIN LIMITS IAW SRM 53Mar 14, 2011 · N523US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1120235640Wire · damagedDURING A LINE CHECK, MAINTENANCE FOUND AN EMERGENCY PATH LIGHT AT LAV 2L INOPERATIVE. MAINTENANCE REPAIRED THE WIRING. OPERATIONAL CHECK WAS GOOD.Mar 12, 2011 · N540US · Boeing 757251 · Light System WiringSDR DALA1118165521Floor Support · corrodedCABIN AREA BETWEEN STA 700 TO 740 LBL 64-50 FLOOR ANGLE SUPPORT HAS CORROSION. REMOVED CORROSION BETWEEN IAW SRM 51-10-02 ORIGINAL THICKNESS 0.080 L=.500" W=450" D=0.012 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15 FIG 101 DETAIL III, IV. REMOVED FLOOR 0002008Mar 12, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1118155521Floor Support · corrodedFLOORBEAM STA 365 AND BET BL 0 TO RBL 50, PREVIOUSLY REPAIRED FLOOR SUPPORT HAS CORROSION AS MARKED. REMOVED SURFACE CORROSION DEPTH TO BE .027 OUT OF LIMITS PER SRM 53-00-51 FIG 101. REPAIRED IAW SRM 53-00-51 FIG 201 R3. REMOVED REPAIR. FABBED T-CHORD BAC Mar 12, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1118145521Floor Support · corrodedBETWEEN FLOORBEAM STA 345 TO STA 365, LBL 25 FLOOR SUPPORT HAS CORROSION AS MARKED. BLENDED CORROSION PER SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-04, FIG 101 DETAIL II. REM AND REP SHIM IAW SRM 51-40-02, 51-40-05 AND TRAVELERT11/873556, MAT 707Mar 11, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1117075521Box Beam · corrodedAT RBL 41 BET STA 324 TO STA 345 BOX BEAM HAS CORROSION AS MARKED. BLENDED AREA PER SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101. REMOVED AND REPLACED BEAM BOX IAW SRM 51-40-02, SRM 51-40-05. PART FABRICATED ON TRAVELER T11/873823 MAT. BMar 10, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1117065521Floorbeam · corrodedAT LBL 62 BET FLOORBEAM STA 365 TO STA 377 BOX BEAM HAS CORROSION AS MARKED. REMOVED CORROSION, AFTER REWORK, DEPTH (.014) ORIGINAL MAT (.050) OUT OF LIMITS PER SRM 53-00-51, FIG 101 FABRICATED NEW BOX BEAM PER STAM TRAVELER T11/873094. INSTALLED BOX BEAM SUMar 10, 2011 · N521US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1116915523Skin · dentedDURING INSP OF LOG PAGE 2969760 FOUND DENT OVER S16L AT STA 414. CUT OUT DAMAGE AREA ON SKIN FROM B STA 409-414 STR 16L AND INST .071" THK REPAIR DOUBLER AND FILLER .06 3" THK PER SRM 53-00-01. INSP TO START AT 69,509 FLIGHT CYCLES WITH REPEAT INSP EVERY 300Mar 9, 2011 · N523US · Boeing 757251 · Fuselage Main, Plate/SkinSDR DALA1116745521Structure · corrodedPREVIOUS REPAIR AT STN 1640 CORRODED AT 4 LOCATIONS BETWEEN LBL 15 AND RBL 60. BLENDED AREA PER SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED UPPER CHORD IAW SRM 53-00-51, REPAIR 3 FIGURE 201. REMOVED AND REPLACED 2Mar 9, 2011 · N521US · Boeing 757251 · Fuselage Miscellaneous StructureSDR DALA1116735521Floorbeam · corrodedPREVIOUS REPAIR AT BS 1640 CORRODED AT 4 LOCATIONS BETWEEN LBL 15 AND LBL 60. REMOVED CORROSION AT STN 1640 FLOORBEAM PER SRM 51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED UPPER CHORD AT BS 1640 FROM LBL 64 TO LBL 15 IAW Mar 9, 2011 · N521US · Boeing 757251 · Fuselage Main, Floor BeamSDR DALA1114415523Bushing · wornLT ELEVATOR OTBD HINGE TO SPAR ATTACH BOLTS AND BUSHINGS WORN. REMOVED AND REPLACED OTBD HINGE AT LT ELEVATOR OTBD POSITION PER AMM 27-31-01-401-926A-A. OPS CHECK TO BE C/W ON TC NR 2910-4001.Mar 1, 2011 · N523US · Boeing 757251 · Elevator StructureSDR DALA1116705528Pin · not seatedEMERGENCY TRACK LIGHTS OUT BETWEEN 23F AND 32F. RESEATED PIN 1 PLUG D9043 ON POWER SUPPLY M9003. TESTED NORMAL.Feb 28, 2011 · N528US · Boeing 757251 · Emergency LightingSDR DALA1116765523Support · corrodedSEAT TRACK SUPPORT STRUCTURE EXISTING REPAIR HAS CORROSION STA 365, RBL24. REMOVED AND REPLACED EXISTING REPAIR ON SEAT TRACK SUPPORT STRUCTURE STA 365, RBL 24, IAW B757-A-53-15-01-801-663A-A.Feb 20, 2011 · N523US · Boeing 757251 · Fuselage, Seat/Cargo Attach Fittings
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