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 DU4R2006514Support · corrodedS/O 291018 NR 24233 CORROSION WING TO BODY FAIRING SUPPORT BS 1020 TO BS 1040 LBL 6. FABRICATED AND INSTALLED REPLACEMENT SUPPORT 20" X 3" FROM BAC1505-100049 7075T73 IAW B757-200 SRM 53-40-71, 51-20-01 AND 51-40-02.Jun 24, 2006 · N919DE · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL75K060702Slide · damagedPERFORMING A GENERAL VISUAL INSPECTION FOUND LT OVERWING SLIDE CARRIER HINGE PANEL LOOSE AND NOT SECURED. FURTHER INVESTIGATION FOUND SLIDE LACING UNSECURED AND SLIDE LOOSE IN CARRIER CONTACTING OVERWING SLIDE DOOR. REPLACED LEFT OVERWING EMERGENCY EXIT SLIDJun 23, 2006 · N6701 · Boeing 757232 · Escape SlideSDR DU4R2006501Transition Panel · corrodedS/O 292018 NR 23829 CORROSION AFT PIT RT TRANSITION PANEL 1460 - 1530. REMOVED CORRODED PANEL. DRILLED ATTACHMENT HOLES AND INSTALLED NEW PANEL P/N 146N5391-51 IAW B757 SRM 51-40-2.Jun 23, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006498Transition Panel · corrodedCORROSION ON AFT PIT TRANSITION PANEL BS 1310 - 1380 RT. FABRICATED AND INSTALLED TRANSITION PANEL SPLICE 10 X 10 INCHES FROM 7075-T6 .071" IAW SRM 53-60-53D.Jun 21, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006506Floor Support · corrodedS/O 291018 NR 23848 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1490 TO 1520, RBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 211/2 INCHES FROM BAC1510-1087 AND L-ANGLE 5-1/2 INCHES FROM 7075-T6 .080 B757 SRM 53-60-53 FIG 206.Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006505Floor Support · corrodedS/O 291018 NR 23847 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1523, LBL 3. FABRICATED AND INSTALLED REPAIR CHANNEL 31 INCHES FROM BAC1510-1087 AND L-ANGLE 6 INCHES FROM 7075-T6 .080 B757 SRM 53-60-53 FIG 206.Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006504Floor Support · corrodedS/O 291018 NR 23846 CORROSION AROUND FASTENER HOLES ON FLOOR SUPPORT AFT PIT BS 1500 TO 1520, LBL 7. FABRICATED AND INSTALLED REPAIR CHANNEL 19 INCHES FROM BAC1510-1087 AND L-ANGLE 5 INCHES FROM AND10136-2001 IAW B757 SRM SRM 53-60-53 FIG 206.Jun 20, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060511Compressor · damagedNR 1 ENGINE HAD COMPRESSOR STALL ON TAKEOFF OUT OF LGA. BORO OF COMPRESSOR SHOWED NUMEROUS BLADES DAMAGED BEYOND LIMITS. ENGINE TO BE REPLACED.Jun 19, 2006 · N646DL · Boeing 757232 · Turbine Engine Compressor SectionSDR DU4R2006500Transition Panel · corrodedCORROSION ON RT TRANSITION PANEL IN AFT PIT BS 1530 TO BS 1640. ROUTED OUT CORRODED AREAS IAW B757 MM 53-88-01-801. FABRICATED AND INSTALLED 2 EACH REPAIR DOUBLERS 9.0 X 7.25 AND 6 X 3.0 INCHES FROM 2024-T3 .071" IAW B757 SRM 53-88-01-801.Jun 18, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006509Seat Track · corrodedS/O 291018 NR 23985 CORROSION ON CABIN SEAT TRACK AT OUTBD SIDE FLOOR PANEL ATTACH FLANGE BS 1117 RBL 47. FABRICATED AND INSTALLED SEAT TRACK REPAIR 106 X 3-1/2 FROM BAC1520-792 IAW B757 SRM 51-40-02.Jun 16, 2006 · N630DL · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006503Angle · corrodedS/O 291018 NR 23842 CORROSION IN AFT PIT BS 1470 TO 1475, RBL 12 AROUND NUTPLATE HOLES, ANGLE. REMOVED CORRODED ANGLE. DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED NEW ANGLE IAW B757 SRM SRM 51-40-02, 51-00-53 AND 51-20-01.Jun 15, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006502Intercostal · corrodedS/O 291018 NR 23839 CORROSION IN AFT PIT BS 1478 INTERCOSTAL WEB RBL-11. FABRICATED AND INSTALLED INTERCOSTAL WEB 20.5" X 8.5" FROM 7075-T6 .040 IAW B757 SRM 51-40-02, 53-60-04 FIG. 101.Jun 15, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006510Fitting · corrodedS/O 291018 NR 24021 CORROSION ON CABIN CREASE BEAM UPPER FITTING AT BS 1720 BULKHEAD. REMOVED AND REPLACED FITTING P/N 146N8726U2 IAW B757 SRM 51-40-02.Jun 14, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006499Strap · chafedCABIN FRAME STA 1640 S-10R CHORD/STRAP CHAFED. FABRICATED AND INSTALLED REPAIR STRAP FROM 7075-T6 IAW BOEING DWG 146N8738 REV V DATED 2-12-02 IAW B757 SRM 51-40-2.Jun 14, 2006 · N630DL · Boeing 757232 · Fuselage Main, FrameSDR DL757060498Fitting · misdrilledTHE ATTACH HOLE IN THE SIDE LINK FITTING IS BEYOND ANGULAR TOLERANCE. A TAPERED RADIUS FILLER WAS INSTALLED TO PROPERLY ALIGN THE HOLE.Jun 14, 2006 · N635DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006490Transition Panel · corrodedCORROSION FWD PIT LT TRANSITION PANEL BS 510 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366Y83 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2, 3, 4 AND 51-40-02 PG 2 & 3.Jun 13, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060499Fitting · misalignedINSTALLATION OF MODIFICATION TENSION CLIPS WOULD REQUIRE MORE THAN THE ALLOWED 0.005 INCH SPOT FACE. A TAPERED FILLER WILL BE USED TO INSTALL THE TENSION CLIPS.Jun 13, 2006 · N635DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DL757060496Bushing · looseTHE NR 1 AND NR 2 PYLON WING DRAG FITTINGS HAVE BUSHING MIGRATION. THE BUSHINGS WERE REMOVED, THE HOLES INSPECTED; AND REPLACEMENT BUSHINGS INSTALLED.Jun 13, 2006 · N635DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006496Shim · corrodedCORROSION AT CABIN FLOOR SUPPORT BS 1676 BL 0. REMOVED CORROSION. SHIM OUT OF LIMITS. FABRICATED AND INSTALLED SHIM 2 X 15.75 INCHES FROM 7075-T6 .125" IAW B757 SRM 51-30-01, 51-20-01 AND 51-40-02.Jun 12, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006489Skin · corrodedCORROSION LOWER FUSELAGE EXT SKIN AROUND FWD FASTENER HOLES OF PANEL 191AL BL 0 - LBL 17. FABRICATED AND INSTALLED REPAIR DOUBLER 10.4 X 8.3 INCHES FROM 20-24-T3 .100 IAW B757 SRM 53-00-01 FIG 201 REPAIR 3 AND 51-20-01.Jun 12, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006512Seat Track · corrodedS/O 291018 NR 24041 CORROSION ON CABIN LT I/B SEAT TRACK AT 2 EA PLACES FROM BS 377 TO 395. REMOVED CORRODED SEAT TRACK BS 377 TO BS 440. INSTALLED SEAT TRACK SECTION FROM BAC1520-792 IAW B757 SRM 53-00-52 FIG 101.Jun 10, 2006 · N919DE · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006511Seat Track · corrodedS/O 291018 NR 24028 CORROSION ON CABIN RT I/B SEAT TRACK AT 3 EA PLACES FROM BS 365.25 TO 387. REMOVED CORRODED SEAT TRACK. FABRICATED AND INSTALLED SEAT TRACK SECTION FROM BAC1520-792 IAW B757 SRM 53-00-52 AND 51-40-02.Jun 10, 2006 · N919DE · Boeing 757232 · Fuselage, Seat/Cargo Attach FittingsSDR DU4R2006492Skin · corrodedCORROSION FWD CARGO FUSELAGE INTERNAL SKIN SURFACE B/O 0 BS 660. FABRICATED AND INSTALLED FUSELAGE SKIN REPAIR 8.3 X 7.75 INCHES FROM 2024-T3 .063 IAW B757 SRM 53-30-01 FIG 1, 53-00-01 FIG 101 AND 51-20-01 PG 7.Jun 10, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006497Support Angle · corrodedCORROSION ON CABIN L-4 DOOR SILL SUPPORT ANGLE BS 1681.8. REMOVED DOOR SILL SUPPORT ANGLE. FABRICATED AND INSTALLED ANGLE REPAIR 5 X 1 X 1 INCH FROM 7075-T6 .063 IAW B757 SRM 51-10-03.Jun 8, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060477Power Supply · burnedAFTER LEVEL OFF THE F/A CALL LIGHT AT 30A BEGAN SMOKING. CABIN LIGHTS WERE SECURED AND A DEADHEADING CREW MEMBER OPENED THE PANEL AND DISCONNECTED THE SHORTING LEADS FROM THE LIGHT. FOUND CTR READING LIGHT PWR SUPPLY MODULE BURNT. REPLACED OVHD PSU, CHECKS Jun 8, 2006 · N675DL · Boeing 757232 · Passenger Compartment LightingSDR DU4R2006495Transition Panel · corrodedCORROSION ON AFT PIT LT TRANSITION PANEL BS 1200 TO 1310. REMOVED CORRODED TRANSITION. DRILLED FASTENER HOLES AND INSTALLED P/N 146N539U171 AND INSTALLED NUT PLATES IAW B757 SRM 51-10-01 AND 51-40-02.Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006494Shear Plate · corrodedCORROSION AT CABIN SUB-FLOOR B/O 0 TO RBL 50 BS 1716 (MAIN DECK FLOOR) SHEAR DECK PLATE RBL 25 CORRODED. REMOVED CORROSION RBL 28 TO RBL 50 WITHIN LIMITS. FABRICATED AND INSTALLED EXTERNAL DOUBLER 9 X 5.5 INCHES FROM 2024-T3 .063 IAW B757 SRM 53-60-51 FIG 20Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006493Skin · corrodedCORROSION FWD CARGO PIT IN BILGE AT BS 850 B/O 0 WL 148.5 ON UPPER SURFACE OF THE LOWER SKIN. FABRICATED AND INSTALLED EXTERNAL DOUBLER 10.5 X 8.5 INCHES FROM 2024-T3 .125 IAW B757 SRM 53-30-01 FIG 201 AND 51-20-01.Jun 7, 2006 · N630DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006507Crease Beam · corrodedS/O 291018 NR 23878 CORROSION ON CABIN CREASE BEAM BS 660 TO 760 LT. REMOVED AND REPLACED L/H BS 660 - 760 CABIN CREASE BEAM P/N 143N8328U53 IAW B757 SRM 51-40-02.Jun 6, 2006 · N630DL · Boeing 757232 · Fuselage Main, StructureSDR DU4R2006513Floor Support · crackedS/O 291018 NR 24066 CABIN FLOOR SUPPORT CORRODED AND CRACKED BS 1645 TO BS 1655 RBL 56. CUT OUT CORRODED AND CRACKED SECTION. NDT VERIFIED CRACK CONTAINMENT IAW B757 NDT MNC PART 6. FABRICATED AND INSTALLED DOUBLER FROM 7075-T6 .071 IAW B757-200 SRM 51-70-1Jun 5, 2006 · N919DE · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006491Transition Panel · corrodedCORROSION FWD PIT RT TRANSITION PANEL BS 560 - 644. INSTALLED NEW TRANSITION PANEL P/N 143N366U126 IAW B757 SRM 53-30-53 FIG 1, 53-00-53 FIG 101, 51-40-05 FIG 2, 3, 4 AND 51-40-02 PG 2 & 3.Jun 4, 2006 · N630DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060447Window · crackedFLIGHT DIVERED TO DEN WITH CRACKED L1 WINDOW. INSTALLED NEW CONTROLLER, NEED OP CK AND BITE. REMOVED AND REPLACED L1 WINDOW PER MM. WILL REQUIRE 3RD TORQUE. WIN HEATING SYS CK. WIPER OP CK AND WINDOW HEAT CONTROLLER BITE OK. ALL CK GOOD. APPLIED FINAL TMay 28, 2006 · N604DL · Boeing 757232 · Flight Compartment WindowsSDR DL757060429Apu · shutdownAFTER PASSING THROUGH FL 360, APU QUIT WITH FAULT LIGHT AND WOULD NOT RESTART SINGLE GENERATOR. OPS ON RETURN TO ATL DUE TO LEFT ENG GENERATOR INOP ON MCO AND PLACARD. SERVICED APU OIL TO FULL. ECU BITE SHOWED OVERSPEED FOR AUTO SHUTDOWN. T/S PER FIM 49-11May 25, 2006 · N657DL · Boeing 757232 · Airborne Auxiliary Power Unit (APU) SystemSDR DL75K060401Valve · malfunctionedON T/O FROM LGA, HAD DOOR LIGHT ILLUMINATE AND GEAR DOOR EICAS MSG WITH GEAR HANDLE UP, SAME LIGHT WHEN PUT GEAR DOWN T/S PER M/M CYCLED NOSE GEAR DOOR OPS NML. REPLACED DOOR, SAFETY VALVE PER M/M 32-35-23-004-001 AS PRECAUTIONARY MEASURE NEEDS OPS CHK. REMOMay 17, 2006 · N610DL · Boeing 757232 · Nose/Tail Landing GearSDR DU4R2006445Fitting · wornNR 2 PYLON FOUND LWR FWD OUTBOARD LUG TO BE 2.008, OVERSIZED SHOULD BE > 2.009. REPAIRED BY FABRICATING AND INSTALLING BUSHING 1.748 ID FROM 15-5 PH IAW DELTA ERA 455545-14AD REV ORIGINAL DATED 5-12-06 APPROVED BY FAA FORM 8100-9.May 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon Miscellaneous StructureSDR DU4R2006444Frame · misdrilledNR 2 PYLON INBOARD LOWER CHORD FROM PPS 128 TO PPS 138 HAS 8 EACH DRILL MARKS BESIDE FASTENER HOLES. REPAIRED FASTENER HOLES BY FABRICATING AND INSTALLING FREEZE PLUGS 1 EACH .391 X .225 INCH AND 2 EACH .405 X .225 INCH FROM 15-5 PH IAW DELTA ERA 455398-14 REMay 16, 2006 · N628DL · Boeing 757232 · Nacelle/Pylon, Frame/Spar/RibSDR DU4R2006426Tripler · corrodedCORROSION ON FUSELAGE SKIN TRIPLER BS 1466 TO 1478 WL 138.5 BL 0. REMOVED TRIPLER, FABRICATED AND INSTALLED REPAIR TRIPLER 23 X 12.5 INCHES FROM 2024-T3 .063 IAW B757 SRM 51-40-02, 51-20-01 AND 51-41-00352-013.May 11, 2006 · N628DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DU4R2006443Attach Angle · corrodedCORROSION ON INTERCOSTAL ATTACH ANGLE IN AFT PIT BS 1320 RBL 6. FABRICATED AND INSTALLED INTERCOSTAL ATTACH ANGLE 6.75 X 1.25 X 1.25 INCHES FROM 7075-T6 .063 IAW DELTA B757 SRM 51-30-01, 51-20-01, 51-10-2, 51-40-02 AND 51-00-00D.May 10, 2006 · N628DL · Boeing 757232 · Fuselage Main, Attach FittingsSDR DU4R2006442Intercostal · corrodedCORROSION ON INTERCOSTAL LWR LEG IN AFT PIT BS 1480 - 1500 LBL 24. REMOVED INTERCOSTAL, FABRICATED AND INSTALLED INTERCOSTAL ANGLE 16.25 X 2.25 INCHES FROM 7075-T6 .050 IAW DELTA B757 SRM 51-40-02, 53-60-04, 51-70-11, 51-70-01.May 10, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL75K060395Skin · crackedCRACKS WERE FOUND IN THE FUSELAGE SKIN AT THE EDGE OF THE L1 DOOR OPENING UPPER FORWARD CORNER. A DOUBLER WAS INSTALLED, REF. AD 2004-09-32, 2001-20-12.May 10, 2006 · N609DL · Boeing 757232 · Fuselage Main, Plate/SkinSDR DL75K060364Bulb · missingFOUND SEAT 9D EMERG TRACK SEAT LIGHTING INOP. INSTALLED 2 BULBS AND MISSING LIGHT LENS. FOUND RED LIGHT QUICK DISCONNECT PULLED APART. SECURED CONNECTION. OPEN NOW CKS GOOD. UNDERSEAT BAGGAGE MUST HAVE DISCONNECTED. CONNECTOR AND BAGGAGE MOST LIKELY KNOCMay 9, 2006 · N6709 · Boeing 757232 · Emergency LightingSDR DU4R2006440Shear Tie · corrodedCORROSION ON BS 1400 FRAME SHEAR TIE S-26R. REMOVED SHEAR TIE, FABRICATED AND INSTALLED SHEAR TIE 6.25 X 2.0 INCHES FROM L-ANGLE EXTRUSION 7075-T6 .100" IAW B757 SRM 51-20-01 AND 51-40-02.May 6, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting StructureSDR DU4R2006435Shear Tie · corrodedCORROSION AFT PIT ON FRAME AND FRAME SHEAR TIE BS 1500 S-29L TO S-27L. REMOVED CORROSION ON FRAME, FOUND TO BE WITHIN LIMITS. REMOVED CORRODED SHEAR TIES, FABRICATED AND INSTALLED 2 EACH SHEAR TIES 5.25 X .75 X .75 INCHES FROM 7075-T6 .040 IAW B757 SRM 53-00May 5, 2006 · N628DL · Boeing 757232 · Fuselage Internal Mounting StructureSDR DU4R2006434Intercostal · corrodedCORROSION NOTED ON AFT PIT FLOOR STRUCTURE INTERCOSTAL WEB BS 1460 - 1480 RT. REMOVED CORRODED INTERCOSTAL. FABRICATED AND INSTALLED INTERCOSTAL 19.375 X 7.5 INCHS FROM 7075-T6 .040 IAW B757 SRM 53-60-04 AND 51-40-02.May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006433Panel · corrodedCORROSION NOTED ON AFT PIT PANEL BS 1440 - 1530 RT. REMOVED CORRODED PANEL AND INSTALLED P/N 146N5391-30 IAW B757 SRM 51-10-01 AND 51-40-02.May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006427Angle · corrodedCORROSION ON TRANSITION ANGLE, FROM BS 1310 TO 1380 RT SIDE (ENTIRE LENGTH). REMOVED CORROSION. FABRICATED AND INSTALLED REPAIR DOUBLER 40.75 INCHES FROM 2024-T3. 080", 13 X 6.5 INCHES FROM 7075-T6 .071" AND 33.5 X 1 INCHES AND 7 X 1 INCHES FROM 7075-T6 .063May 5, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006437Intercostal · corrodedCORROSION AFT PIT INTERCOSTAL BS 1540 - BS 1560 LT. FABRICATED AND INSTALLED INTERCOSTAL 19.50 X 3.75 INCHES FROM 7075-T6 .032" IAW BOEING DWG 146N5461-15 AND 51-40-02.May 4, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DU4R2006431Transition Panel · corrodedLEFT TRANSITION PANEL BS 1410 - 1530 CORRODED BA 1410 TO BS 1530 LT. REMOVED CORRODED PANEL. INSTALLED FABRICATED AND INSTALLED REPLACEMENT WEB 20.875 X 2.75 INCHES FROM 7075-T6 .032 IAW B757 SRM 53-00-04 DETAIL 11 FIG 101, 51-40-02, 51-20-01 AND 51-10-02.May 3, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous StructureSDR DL757060351Tire · failedNR 3 MAIN TIRE FAILED DURING RTO. RT SIDE BRAKE TEMP AT 3 HIGHEST. REPLACED NR 3 WHEEL ASSY BRAKE TEMP AT 3 DOES NOT REQUIRE HIGH ENERGY STOP INSP.May 2, 2006 · N662DN · Boeing 757232 · TireSDR DU4R2006436Transition Panel · corrodedCORROSION AFT PIT ON RT TRANSITION PANEL BETWEEN BS 1530 TO 1640. FABRICATED AND INSTALLED TRANSITION PANEL REPAIRS 63 X 1.5 INCHES FROM 2024-T3 .063 AND 64 X 3 INCHES FROM 7075-T6 .071 IAW B757 SRM 51-10-01 AND 53-88-01-801.May 1, 2006 · N628DL · Boeing 757232 · Fuselage Miscellaneous Structure
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