Boeing 757-222

Service difficulty reports · 15,539

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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 = '757222'
  ORDER BY difficulty_date DESC"

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SDR FDEA201410123120Angle · corrodedBS 320 - 360 R1 DOOR LOWER SILL ANGLE FOUND CORRODED. CORROSION REMOVED IAW SRM 51-20- 01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53- 10-15 FIG 101 ALLOWABLE DAMAGE 1 REV 113. SILL ANGLE REMOVED AND REPLACED IAW SRM 51-40-02 REV 113 AND DWG 141N8422 SHT Oct 12, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR CALA2014101692458Stringer · corrodedCORROSION ON AFT CARGO FLOOR STRINGER BS 1460 STRINGER 26L. FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 1 01 DETAIL II. REPAIRED STRINGER 27L BS 1433 TO 1460 IAW SRM 53-00-03 FIG 201 REPAIR 1.Oct 12, 2014 · N544UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR CALA2014101692457Stringer · corrodedCORROSION ON AFT CARGO STRINGER AT BS 1440 STRINGER 27L STRINGER SPLICE. FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 1 01 DETAIL II. REPAIRED STRINGER 27L BS 1433 TO 1460 IAW SRM 53-0 0-03 FIG 201 REPAIR 1.Oct 12, 2014 · N544UA · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201410113113Strap · corrodedEMPENNAGE APU AIR INLET DOOR CUT OUT FWD STRAP HAS CORROSION AT BS 1787 STRINGER 3 - 6R. STRAP REMOVED AND REPLACED IAW SRM 51-40-02 REV 112. AND SRM 51-40-02 REV 113 AND DWG148N3105 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.Oct 11, 2014 · N780FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR CALA2014101692441Floorbeam · corrodedCORROSION MAIN CABIN FLOORBEAM UPPER SURFACE BS 365 RBL 4. REPAIRED MAIN CABIN FLOORBEAM UPPER CHORD AT BS 365 RBL 10 TO LBL 70 IAW ECRA 5310-05536, ECRA 5100-01844 & ECRA 5310 -06277. THIS IS A CATEGORY A REPAIR.Oct 10, 2014 · N544UA · Boeing 757222 · Fuselage Main, Floor BeamSDR CALA2014101692439Floorbeam · crackedMAIN CABIN FLOORBEAM CRACKED TOP FLANGE BS 700 LBL 24.75 & LBL 46.5. REPAIRED MAIN CABIN FLOORBEAM TOP FLANGE AT BS 700 LBL 24.75 & LBL 46.5 IAW ECRA 5310-06274. THIS IS A CATEGORY A REPAIR.Oct 10, 2014 · N544UA · Boeing 757222 · Fuselage Main, Floor BeamSDR CALA2014101692436Frame · corrodedCORROSION AFT CARGO COMPARTMENT FRAME AT BS 1400 BETWEEN STRINGER 27L & 29L. R & R LOWER FRAME SECTION AT BS 1400 BETWEEN STRINGER 25L & 28R IAW SRM 51-40-02 PARA 4 & 7 FIG 3 & 12.Oct 10, 2014 · N544UA · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410103072Stringer · corrodedAFT CARGO BAY BS 1460, STRINGER 29L CORRODED. REMOVED CORROSION FROM STRINGER IAW SRM 51-10-02. REPAIRED IAW SRM 53-00-03 FIG 201.Oct 10, 2014 · N784FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201410103075Skin · dentedFUSELAGE SKIN HAS A DENT BS 1701 - 1720 STRINGER 28 - 30R. REPAIRED IAW EA F5330-T0310832. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Oct 10, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410103108Skin · dentedLEFT WING INBD FLAP OTBD BOTTOM SIDE DENT 6 INCHES FROM BOTTOM EDGE 29 INCHES FROM INBD EDGE. REPAIRED IAW SRM 51-70-10 REPAIR NR 2 FINAL REPAIR. DIMENSIONS DOUBLER 4.75 INCHES IN DIAMETER. COMPLIED WITH EA F-5750-T0312306 WINGS FLIGHT SURFACES LT WING INBDOct 10, 2014 · N784FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201410093041Floorbeam · damagedBS 345 RBL 23 - 60 FLOORBEAM UPPER TEE FOUND DAMAGED. FLOORBEAM TEE REPAIRED IAW SRM 53-00-51 REPAIR 8 REV 113 REPAIR CLASSIFIED AS MAJOR.Oct 9, 2014 · N780FD · Boeing 757222 · Fuselage Main, Floor BeamSDR CALA2014101692433Frame · corrodedCORROSION AFT CARGO COMPARTMENT FRAME AT BS 1420 BETWEEN STRINGER 27L & 29L. R & R IAW SRM 51-40-02 PARA 4 & 7 FIG 3 & 12. FABRICATED LOWER FRAME SECTION IAW SRM 51-30-01 PARA & FIG 7 & DWG 146N1028.Oct 9, 2014 · N544UA · Boeing 757222 · Fuselage Main, FrameSDR FDEA201410083006Floorbeam · corrodedFLOORBEAM AT BS 1661 CORRODED. FLOORBEAM TEE REMOVED BETWEEN RBL 70 - LBL 70 IAW SRM 51-40-02 REV 113. NEW FLOORBEAM TEE FABRICATED IAW DWG 146N5110 SHT 3 REV B AND INSTALLED IAW DWG 146N5090 SHT 6 REV. REPAIR CLASSIFIED AS MAJOR.Oct 8, 2014 · N780FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201410083009Crease Beam · corrodedBS 960 - 984 RT CREASE BEAM WEB FOUND CORRODED. CORROSION REMOVED IAW SRM 51-10-02 REV 112. REWORKED AREA EVALUATED AND FOUND MATERIAL LOSS OF 0.021" OUT OF 10% LIMIT OF ORIGINAL THICKNESS OF 0.063" IAW SRM 53-40-13 ALLOWABLE DAMAGE 1 FIG 101 REV 113 DETAILOct 8, 2014 · N780FD · Boeing 757222 · Fuselage Main, StructureSDR FDEA201410083010Floorbeam · corrodedBS 377.7 LBL 55 - 60 FLOORBEAM UPPER TEE FOUND CORROED ON LOWER SURFACE. FLOORBEAM TEE REMOVED AND REPLACED IAW DWG 141N5113 SHT 1 REV F. DWG 141N5123 SHT 1 REV A AND EA F-5310-T0311051 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 8, 2014 · N785FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201410072992Skin · damagedFUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26 LT & 26 RT AT BS 580- 600. DAMAGE REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II REV 113 AND REPAIRED IAW EA F-5330-T0312729 PART 1. REPAIR CLASSIFIED AS MAJOR.Oct 7, 2014 · N780FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014102192527Skin · dentedDENT AT STATION 1705 BETWEEN STRINGER 17L & 18L. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 3.Oct 7, 2014 · N544UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410072997Skin · damagedFUSELAGE SKIN HAD NUMEROUS NICKS & SCRATCHES BETWEEN STRINGER 26L & 26R BETWEEN BS 1701 - 1720. DAMAGE REMOVED AND TREATED IAW SRM 51-10-02 REV 112. FOUND ONE SPOT OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112, REPAIRED OUT OF LIOct 7, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR CALA2014101392393Structure · dentedRE INSPECTION IAW SRM 53-00-01 TABLE V USING LOW FREQ METHOD IAW NDT PART 6 51-00-06. RAMP REPORTED A DENT AT STATION 1680 APPROX 3 FEET BEHIND DOOR 4L. ALL RE INSPECTION COVERED ON CF9067. VERIFIED DENT IS FREE OF CRACKS USING HFEC. DENT LOCATED AT STATIONOct 7, 2014 · N544UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR CALA2014101392392Structure · dentedDENT AT STATION 1705 BETWEEN STRINGER 17L & 18L. REPAIRED IAW SRM 53-00-01 FIG 201 REPAIR 3.Oct 7, 2014 · N544UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201410073000Stringer Splice · corrodedAFT CARGO PIT STATION 1470 STRINGER 9R CORROSION ON AFT END OF STRINGER SPLICE. R & R STRINGER SPLICE AT STATION 1470 STRINGER 29R IAW SRM 51-40-02. MAJOR REPAIR.Oct 7, 2014 · N784FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201410032953Stringer · corrodedAFT CARGO COMPARTMENT UNDER THE FLOOR BILGE AREA SKIN STRINGER CORRODED, STRINGER 28L OTBD FLANGE STATION 1400. REMOVED CORROSION IAW SRM 51-10-02. NO ALLOWED DAMAGE IN 757-200 SRM. REPAIRED STRINGER FROM STATION 1386 - 1419 STRINGER 28L IAW SRM 53-00-03 REOct 3, 2014 · N784FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201410022892Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1654 STRINGER 28 - 29L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 AND SRM 51-20-01 REV 112, FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CAROct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022891Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1622 STRINGER 27 - 28L. THE DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. PART 1Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022890Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1627 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00-01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 11 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CAOct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022889Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1630 STRINGER 27 - 28L. DAMAGE WAS REMOVED AND TREATED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIROct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022888Skin · damagedFUSELAGE EXTERIOR SKIN HAS A LIGHTNING STRIKE AT BS 1653 STRINGER 28 - 29L. DAMAGE REMOVED IAW SRM 53-00- 01 REPAIR 6 REV 112 AND 51-20-01 REV 112 AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE I REV 112. REPAIR CARRIED OUT IAW EOct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022913Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1581 STRINGER 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022912Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1576 STRINGER 27 - 28L. BLENDED THE DAMAGE AND FOUND OUT OF LIMITS IAW SRM 53- 00-01 FIG 101 DETAIL II ALLOWABLE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410022914Skin · damagedFUSELAGE EXTERIOR SKIN HAD A LIGHTNING STRIKE AT BS 1571 STRINGERS 27 - 28L. DAMAGE BLENDED AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II ALLOWANCE DAMAGE 1 REV 112. REPAIR CARRIED OUT IAW EA F-5330-T0311361. REPAIR CLASSIFIED AS MAJOR.Oct 2, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201410012879Frame Splice · gougedAFT CARGO BAY BS 1520 STRINGER 24 - 25R, FRAME SPLICE FOUND DAMAGED. REMOVED AND REPLACED IAW SNRM N04012. REPAIR CLASSIFIED AS MAJOR.Oct 1, 2014 · N785FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014100292354Crease Beam · corrodedCORROSION MULTI AREAS AS MARKED. MAIN CABIN CREASE BEAM BS 1000 - 1040. INSTALLED NEW CREASE BEAM IAW SRM 51-40-02 PAR 4 FIG 3 PAR 7 FIG 12 & PAR 5 FIG 9 I.Sep 29, 2014 · N544UA · Boeing 757222 · Fuselage Main, StructureSDR FDEA201409282844Skin · damagedMULTIPLE TOOL DAMAGE ON THE INTERIOR SKIN AT BS 1420 - 1423, STRINGER 25L - 26L. REPAIRED IAW EA F-5330-T0311215 PART 1. REPAIR CLASSIFIED AS MAJOR.Sep 28, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201409262791Frame · gougedAFT CARGO BAY FRAME BS 1360 STRINGER 23 - 24L OUTER FLANGE GOUGED. REPAIRED IAW EA F5310-T0311806 P1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Sep 26, 2014 · N785FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201409262793Skin · crackedTHERE IS A CRACK AT FWD CARGO DOOR EXTERIOR SKIN AT LOWER AFT CORNER BS 600 - 620 STRINGER 25 - 26R. REPAIRED IAW EA F-5230-T0311723. REPAIR CLASSIFED AS MAJOR.Sep 26, 2014 · N785FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201409262810Skin Panel · damagedINCOMING STRUCTURE INTERFERES WITH CABLE SHROUD INSTALLATION BETWEEN 1340 STRINGER 4L TO 4R. FUSELAGE SKIN REPAIR WAS ACCOMPLISHED DUE TO EFFECTING THE P TO F CONVERSION ON EA 757-5361-16-F4656 REV DATED SEPT. 16, 2014 & NR 60002686700001. THIS NR IS FOR TRASep 26, 2014 · N798FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201409252761Skin · crackedL4 DOOR INTERNAL HANDLE BOX CUT OUT AFT EDGE INNER SKIN FOUND CRACKED AT EDGE. REPAIRD IAW EA F-5210-T0311310 PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Sep 25, 2014 · N785FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201409252789Floorbeam · damagedMAIN DECK CARGO FLOORBEAM UPPER TEE AT BS 1640 SCRATCHED, NICKED & CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL III. R & R FLOORBEAM IAW DWG 146N5089 & SRM 51-40-02. MAJOR REPAIR.Sep 25, 2014 · N783FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201409252783Seat Track · gougedMAIN CABIN BETWEEN BS 900 - 1080 LBL 45.5 SEAT TRACK HAS GOUGES, NICKS & CORROSION IN SEVERAL PLACES. R & R SEAT TRACK WITH NEW TRACK IAW SRM 51-40-02. SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL II. MAJOR REPAIR.Sep 25, 2014 · N784FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409242758Frame · misrepairedAFT CARGO BAY BS 1440 STRINGER 26L. FRAME MISREPAIRED. FRAME REPAIR R & R IAW SRM 51-40-02 & DWG 146N1013. MAJOR REPAIR.Sep 24, 2014 · N798FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201409232722Skin · gougedEXISTING REPAIR FINDING FUSELAGE THERE IS GOUGE ON THE INTERIOR SURFACE OF THE DOUBLER OF THE EXISTING REPAIR AT STATION 1350 STRINGER 29L - 28R. REMOVED BY HAND CLEAN & TREATED PER SRM 51-10-01 REV 112 AND SRM 51-20-01 REV 112. NEW REPAIR CARRIED OUT PER FSep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201409232711Frame · corrodedAFT CARGO COMPARTMENT STATION 1380 RBL 10 FRAME UPPER CHORD FOUND CORROSION DURING REMOVING CORROSION AT FRAME FLANGE IAW SNRM N03563. COMPLIED AS PER EA F-5310-T0311624 P1 TITLE: FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FSep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201409232709Frame · corrodedAFT CARGO COMPARTMENT STATION 1380 BL0 - RBL 15 FRAME FLANGE HAS CORROSION. COMPLIED AS PER EA F-5310 - T0311624 PT 1. TITLE : FUSELAGE - MAINFRAME - REPAIR FOR OUT OF LIMIT BLEND OUT CORROSION AT FREE FLANGE OF STA 1380 146N1028-88 BOTTOM FRAME AND 146N8511Sep 23, 2014 · N785FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2014092992322Line · chafedRIGHT OFF WING SLIDE PRESS LINE FOUND CHAFING WHERE IT PENETRATES FUSELAGE THROUGH CLOTH BRAID ON LINE. REPAIRED PRESS LINE GNMM 1-0-0-006.Sep 23, 2014 · N594UA · Boeing 757222 · Escape SlideSDR FDEA201409232740Seat Track · gougedLEFT UPPER LOBE FLOOR SUPPORT STRUCTURE SEAT TRACK HAS NICKS, GOUGES & SCRATCHES LOCATION STATION 1180 - 1320 LBL 45.5. R & R SEAT TRACK WITH A NEW ONE IAW SRM 51-40-02. PREVIOUS SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL II. MAJORSep 23, 2014 · N784FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232739Seat Track · gougedMAIN CABIN BETWEEN BS 1080 - 1180 LBL 24.75 SEAT TRACK HAS GOUGES, NICKS & CORROSION IN SEVERAL PLACES. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED & INSTALLED NEW TRACK IAW DWG 144N5021 & IAW SRM 51-40-02. MAJOR REPAIR.Sep 23, 2014 · N784FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409232738Seat Track · gougedMDC FLOOR SEAT TRACK RBL 24.75 GOUGED & SCRATCHED BETWEEN STATION 1075 - 1180. REMOVED SEAT TRACK IAW SRM 51-40-02. FABRICATED NEW TRACK IAW DWG 144N5021 BATCH 2645495 & INSTALLED NEW SEAT TRACK IAW SRM 51-10-02 & DWG 144N5021. MAJOR REPAIR.Sep 23, 2014 · N784FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201409222698Web · chafedNUMBER 2 PYLON OTBD SIDE FAN COWL SUPPORT WEB AFT SIDE EXISTING REPAIR. THERE IS WEAR MARK IN THE DOUBLER. SUPPORT WEB REPAIRED IAW EA F-5450-T0312881 PART 1. TITLE NACELLES & PYLON, PYLON STRUCTURES, RE-ACCOMPLISH EXISTING REPAIR AT NR 2 PYLON OTBD SIDE, FSep 22, 2014 · N780FD · Boeing 757222 · Nacelle/Pylon Miscellaneous StructureSDR CALA2014092292253Battery · dischargedEMERGENCY EXIT LIGHT SECTION BETWEEN SEAT ROW 21ABC & 27ABC INOPERATIVE. REPLACED BATTERY & CHARGER IAW MM 33-51-07 AT ROW 23. EMERGENCY EXIT LIGHT OPERATIONS NORMAL.Sep 20, 2014 · N565UA · Boeing 757222 · Emergency LightingSDR FDEA201409192687Stringer Splice · corrodedAFT CARGO UNDER THE FLOOR BILGE AREA SKIN STRINGER 29L CORRODED AT STATION 1460. REMOVED CORROSION IAW SRM 51-10- 02. NO ALLOWED DAMAGE ON SRM. R & R STRINGER SPLICED IAW SRM 51-40-02. MAJOR REPAIR.Sep 19, 2014 · N784FD · Boeing 757222 · Fuselage Main, Longeron/Stringer
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