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 FDEA201606162029Fmc · failedDURING DESCENT, RECEIVED EICAS MESSAGE, RT FMC FAIL, COMPLIED WITH QRH AND CONTINUED FLIGHT WITH LT FMC ONLY. R & R RT SIDE FMC IAW AMM 34-61-01-4-2, SYSTEM OPS CHECK NORMAL.Jun 16, 2016 · N787FD · Boeing 757222 · Flight Management Computing Hardware SystemSDR FDEA201606141997Frame · gougedAFT CARGO COMPARTMENT, BS 1520, STR 22R-STR 23R. FRAME WEB HAS GOUGE MARKS.Jun 14, 2016 · N782FD · Boeing 757222 · Fuselage Main, FrameSDR CALA2016061595450Floor Support · corrodedSUPPORT TASK, MAIN CABIN FLOOR CENTER SECTION FROM STA 900 TO STA 1020 AND RBL 63 FLOOR SUPPORT ANGLE HAS EVIDENCE OF SURFACE CORROSION. R & R NEW FLOOR SUPPORT ANGLE, PN BAC1515-551, PO 1402636, STA 900-1020, RBL 63, IAW SRM 51-40-02.Jun 13, 2016 · N595UA · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201606131978Skin Panel · delaminatedRT WING, INBD T/E MAIN FLAP UPPER INTERSPAR PANEL FOUND DELAMINATION AT MF STA 175, 18" FROM L/E. COMPLIED WITH PART 1 OF EA F-5750-T0327826. SRM REPAIRS ON RT WING INBD MAIN FLAP UPPER BONDED SKIN OUTER AND INNER FACESHEETS, STA 160-180, RSC TRACKING, REPAJun 13, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201606131977Skin Panel · delaminatedRIGHT WING-INBD T/E MAIN FLAP UPPER INTERSPAR PANEL FOUND DELAMINATION AT MF STA 165, 20" FROM L/E. COMPLIED WITH PART 1 OF EA F-5750-T0327826, SRM REPAIRS ON RT WING INBD FLAP UPPER BONDED SKIN, OUTER & INNER FACESHEETS, MF STA 160-180, RSC TRACKING. REPAIRJun 13, 2016 · N790FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201606101939Skin · damagedINCOMING SKIN BLEND OUTS AT FASTENER LOCATIONS BETWEEN BS 350-BS 365, 23L. EVALUATED BLEND OUT AREAS BS 350-BS 365, STR 23L AREA FOUND TO BE OUT OF LIMITS, IAW-SRM-53-00-01-1A FIG 101 DET II, REPAIRED SKIN DAMAGED AREA IAW-SRM-53-00-01-2R, FIG 201, R15, THIS IJun 10, 2016 · N781FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201606091905Frame · corrodedAFT CARGO COMPARTMENT, BS 1460, STR 26R-28L, FRAME WEB CORROSION. R & R WITH NEW FABRICATED FRAME WEB IAW DWG 146N1014, SHT 6 REV D. REPAIR CLASSIFIED AS MAJOR.Jun 9, 2016 · N782FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201606091896Skin · damagedFUSELAGE RT SIDE, THERE IS A LIGHTNING STRIKE AT BS 680 - BS 700 BETWEEN STR 24- STR 25. LIGHTNING STRIKE REMOVED, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 101, DETAIL II, REV 118. REPAIR CARRIED OUT IAW SRM 53-00-01, FIG 201, REPAIR 15, REV 118. THIS IS AJun 9, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201606071858Stringer · corrodedAFT CARGO COMPARTMENT STATION 1510 - 1530, STRINGER 29R, STRINGER CORROSION. CORROSION OUT OF LIMITS, R & R WITH NEW STR STA 1460-STA 1620, STR 29R IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F IN REF TO JOB CARD N02233 IAW WORK DETAIL ATTACHED. Jun 7, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201606071857Stringer · corrodedAFT CARGO COMPARTMENT STATION 1460 - 1480, STRINGER 29R, STRINGER CORROSION. AFT CARGO COMPARTMENT OUT OF LIMIT, STR STA 1460-STA 1620, STR 29R. R & R WITH NEW STR STA 1460-STA 1620 IAW SRM 51-40-02, REV 118 AND DWG 146N3400, SHT 03, REV F. REPAIR CLASSIFIJun 7, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201606061855Skin · damagedFUSELAGE RIGHT SIDE THERE IS A LIGHTNING STRIKE AT BS 500 - 520 BETWEEN STRINGER 25 - 26 WITH STICKER 633. LIGHTNING STRIKE MARK REMOVED AREA FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX, AD REPAIR CARRIED OUJun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201606061854Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 480 - 500, BETWEEN STRINGER 25 - 26 WITH STICKER 630. FUSELAGE EXTERIOR SKIN AT BS 480-500, STR 25R-26R LIGHTING STRIKE MARK. REMOVED AREA, FOUND OUT OF LIMIT IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTJun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201606061853Skin · damagedFUSELAGE RT SIDE THERE IS A LIGHTNING STRIKE AT BS 460 - 480, BETWEEN STRINGER 25 - 26 WITH STICKER 613. REMOVED AREA, FOUND OUT OF LIMITS IAW SRM 53-00-01, FIG 201, DET II, REV 118, DEPTH OF CLEAN UP 15 PERCENT MAX AND REPAIR CARRIED OUT IAW SRM 53-00-01, FIJun 6, 2016 · N782FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201606051849Frame · corrodedAFT CARGO COMPARTMENT STATION 1560, STRINGER 30 - 29L, FRAME WEB CORROSION.Jun 5, 2016 · N782FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201606051848Skin · chafedRIGHT WING OTBD TE MAIN FLAP, NOSE SKIN FOUND CHAFE MARK AT 2.5" FROM OTBD EDGE.Jun 5, 2016 · N782FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201606041812Fitting · corrodedWHILE WORKING THE INBD AFT FLAP RT SIDE, THE OTBD FITTING WAS FOUND WITH PITTING CORROSION. AFTER CORROSION REMOVAL, FOUND OUT OF LIMITS IAW DWG 113N2801 SHT 1 REV. COMPLIED WITH EA F-5750-T0325349 PT 1 DATED 05 27 16. CAT A MAJOR REPAIR FAA FORM 8100-9 ISSJun 4, 2016 · N789FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201606031806Panel · delaminatedVERTICAL STAB AUXILIARY SPAR TO FRONT SPAR RT FIXED PANEL FROM STATION 195 - 270 HAS SEVERAL SPOTS OF DELAMINATION ON EXTERNAL & INTERNAL SURFACE. R & R VERTICAL STAB RT FIXED PANEL 175N2001-4 IAW SRM 51-40-02 -0G & DWG 175N2001 SH1 REV B. PN 175N2001-4 REPJun 3, 2016 · N789FD · Boeing 757222 · Vertical Stabilizer Miscellaneous StructureSDR FDEA201606031800Shear Tie · corrodedAFT PIT STATION 1620, TWO EACH SHEAR TIES HAVE CORROSION BETWEEN STRINGER 29L - 29R. REMOVED CORROSION IAW SRM 51-10-02-OG. NO ALLOWABLE DAMAGE IAW SRM. R & R TWO EACH SHEAR TIES, PN 140N2002-252 & PN 140N2002-307, BATCH 0002974391 IAW SRM 51-40-02-0G CATJun 3, 2016 · N781FD · Boeing 757222 · Fuselage Internal Mounting StructureSDR FDEA201606031793Engine · malfunctionedRIGHT ENGINE FAILED AT 4000 FT. COMPLIED WITH QRH, SHUTDOWN ENGINE. OIL PRESSURE WAS 25 PSI AT SHUTDOWN. EGT INCREASED BUT WAS NOT IN THE RED. NR 1 ENGINE OPERATED NORMALLY, NO EXCEEDANCE. RUMBLING NOISE FROM RT ENGINE. RT ENGINE PARAMETERS BEGAN TO ROLLJun 3, 2016 · N793FD · Boeing 757222 · Engine (Turbine/Turboprop)SDR CALA2016060695429Skin · corrodedWING CTR FUEL TANK SECTION. UPPER SKIN HAS EVIDENCE OF CORROSION UNDER INTERCOSTAL FITTING BS 930, RBL 61. REPAIR AT CTR FUEL TANK UPPER SKIN PANEL, STATION 980, RBL 61 APPROX IAW RES 2010587-23.Jun 2, 2016 · N595UA · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201605311770Skin · dentedFORWARD CARGO DOOR OUTER SKIN AT BOTTOM HAS A DENT. EVALUATED & DETERMINED DENT TO BE OUT OF LIMITS IAW SRM 52-30-01-1A FIG 101 DET VIII. INSTALLED REPAIR DOUBLER IAW SRM 52-30-01-2R FIG 201 REPAIR 4, CAT B. REPAIR REF EA F-5230-TO325627 ISSUED FOR RSC TRACMay 31, 2016 · N789FD · Boeing 757222 · Cargo/Baggage DoorsSDR FDEA201605311764Channel · damagedCABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD CHANNEL, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CHANNEL REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD CHANNEL FABRICATED IAW DWG 146N5317, SHT 1, REV AND INSTALLED IAW DWG 146N5300, SHT 23May 31, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201605311763Angle · damagedCABIN STATION 1720, LBL 65 - RBL 65, DECK PLATE ATTACHED CHORD ANGLE, FOUND HOLE ELONGATED AFTER DECK PLATE REMOVAL. CABIN, STA 1720, LBL 65-RBL 65 DECK PLATE ATTACHED CHORD ANGLE WITH ELONGATED HOLE REMOVED IAW SRM 51-40-02, REV 117. NEW CHORD ANGLE INSTALLMay 31, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201605261739Stringer Splice · corrodedAFT CARGO COMPARTMENT, STATION 1460, STRINGER 28L, STRINGER SPLICE HAS CORROSION. R & R WITH NEW FABRICATED STA 1460, STR 28L, STRINGER SPLICE IAW DWG 146N3400, SHT 02, REV C. NEW STRINGER FABRICATED IAW DWG 146N3820, SHT 01, REV C.May 26, 2016 · N782FD · Boeing 757222 · Fuselage Main, Longeron/StringerSDR FDEA201605261738Frame Splice · gougedAFT CARGO COMPARTMENT, STATION 1520, STRINGER 24R, FRAME SPLICE HAS GOUGE MARKS. FRAME SPLICE REMOVED AND REWORKED AREA TREATED IAW SRM 51-10-02 AND SRM 51-20-01, REV 118. MATERIAL REMOVED 0.027" OUT OF LIMIT. FRAME SPLICE R & R WITH NEW FABRICATED FRAME SPMay 26, 2016 · N782FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201605251733Unknown · odorTHREE TIMES DURING FLIGHT WE SMELLED AN ACRID ELEC BURNING SMELL. NO SMOKE NOTED & UNABLE TO ISOLATE. FIRST OFFICER ALWAYS SMELLED IT FIRST. ALWAYS WENT AWAY IN 1 MIN. NO SMELL IN COURIER AREA. IAW FIM 21-00 PROC 4, SINCE FAULT CAN'T BE DUPLICATED & ALL EMay 25, 2016 · N785FD · Boeing 757222 · Air Distribution SystemSDR FDEA201605201693Skin · dentedLEFT HORIZONTAL STAB FWD TORQUE BOX, INBD LOWER PANEL HAS LIMITED DENT REPAIR FOR 3 DENTS AT STATION 192 & 8.5" AWAY FROM PREVIOUS REPAIR & 1.25" AWAY FROM THE 3RD DENT, STAB STATION 195, 10.34" AFT OF THE AUX SPAR. REPAIRED LT HORIZONTAL STAB FWD TORQUE BOX May 20, 2016 · N789FD · Boeing 757222 · Horizontal Stabilizer, Plate/SkinSDR FDEA201605191664Skin · dentedFUSELAGE EXTERIOR SKIN LT SIDE, THERE IS AN EXISTING DENT. COMPLIED WITH PART 1 OF EA F-5310-T0324962A. REPAIR CLASSIFIED AS MAJOR.May 19, 2016 · N792FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201605191671Frame · corrodedAFT PIT STATION 1260, CORROSION ON FRAME UPPER FLANGE AT FLOOR STRINGER LBL 2.29. REMOVED CORROSION IAW SRM 51-10-02-0G. AFTER REWORK AREA WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A.FIG 101 DET V, ORIG MAT .063, .016 MAT LOSS. R & R FRAME IAW SRM 51-May 19, 2016 · N789FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201605171650Shear Tie · corrodedAFT PIT STATION 1500, BETWEEN STRINGER 29L - 30, SHEAR TIE HAS CORROSION. R & R SHEAR TIE IAW SRM-51-40-02-0G. REMOVED CORROSION IAW SRM-51-10-02, NO ALLOWABLE DAMAGE FOUND IN CHAPTER 53 OF SRM. REPAIR CATEGORIZED AS A MAJOR REPAIR.May 17, 2016 · N789FD · Boeing 757222 · Fuselage Internal Mounting StructureSDR FDEA201605161608Light · intermittentL1 DOOR SLIDE LIGHT INTERMITTENTLY ILLUMINATING WHEN ARMING L1 DOOR. R & R L1 DOOR SLIDE & ARMED LIGHT ASSEMBLY IAW SRM. OPERATIONS CHECKED NORMAL.May 16, 2016 · N787FD · Boeing 757222 · Door Warning SystemSDR FDEA201605141582Floorbeam · corrodedCABIN STATION 1681, RBL 10 - 47, FLOORBEAM UPPER FLANGE FOUND CORROSION AFTER DECK PLATE REMOVAL. CABIN, STA 1681, RBL 10-47 FLOORBEAM UPPER FLANGE CORROSION REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA ORIGINAL THICKNESS 0.158" MATERIAL THICKNESS. REMAMay 14, 2016 · N782FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201605131545Skin · chafedRIGHT OTBD MAIN FLAPS LE, JUST IN FRONT OF NR 11 SPOILER HAS CHAFED MARK. EVALUATED CHAFE MARK, OUT OF LIMITS IAW SRM 57-53-01 FIG 101 DETAIL VI. REPAIRED IAW SRM 57-53-01-2R REPAIR 2 FIG 201 & SRM 51-40-02-0G, REF EA F-5750-T0325268 ISSUED FOR TRACKING. MAMay 13, 2016 · N789FD · Boeing 757222 · Trailing Edge FlapsSDR FDEA201605101523Skin · unknownFUSELAGE EXTERIOR SKIN THERE IS A RIVET THAT IS NOT FLUSH AT BS 1520, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0324711B PART 1. REPAIR CLASSIFIED AS MAJOR.May 10, 2016 · N792FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201605101522Skin · damagedFUSELAGE EXTERIOR SKIN THERE IS A RIVET WITH AN ELONGATED HOLE AT BS 1600 - 1620, BETWEEN STRINGER 29 LT & 29 RT. REPAIR CARRIED OUT IAW EA F-5330-T0325043A PART 1. REPAIR CLASSIFIED AS MAJOR.May 10, 2016 · N792FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201605091517Strap · corrodedRIGHT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRCIATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer StructureSDR FDEA201605091515Strap · corrodedLEFT SIDE EMPENNAGE LOWER OUTER HORIZONTAL STAB PIVOT STRAP FOUND CORRODED. PIVOT STRAP REMOVED AND NEW FABRICATED IAW DWG 182N1608 SHT 1 REV A AND INSTALLED IAW DWG 182N1601 SHT 1 REV C. REPAIR CLASSIFIED AS MAJOR.May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer StructureSDR FDEA201605091516Strap · corrodedEMPENNAGE, RT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP. FOUND CORROSION RT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP REMOVED AND NEW PIVOT FABRICATED IAW DWG NR: 182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601, SHT 1, REV C. May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Miscellaneous StructureSDR FDEA201605091514Strap · corrodedEMPANNAGE, LEFT SIDE, LOWER INNER HORIZONTAL STABILIZER PIVOT STRAP FOUND CORROSION LT LOWER INNER HORIZONTAL STABILIZER CORRODED PIVOT STRAP. REMOVED AND NEW PIVOT STRAP FABRICATED IAW DWG NR:182N1608, SHT 1, REV A AND INSTALLED IAW DWG NR 182N1601 SHT, REV May 9, 2016 · N782FD · Boeing 757222 · Horizontal Stabilizer Miscellaneous StructureSDR FDEA201605081512Skin · chafedLEFT WING LOWER INTERSPAR SKIN, EXTERIOR SURFACE FOUND CHAFING MARK AT FUEL TANK PANEL 541CB. CUT OUT BOTH FWD & AFT AREA, ALONG NR 1 PYLON UPPER INBD EDGE. LT WING LOWER INTERSPAR SKIN EXTERIOR SURFACE CHAFING MARK REMOVED & COMPLETED IAW EA F-5730-T0324554May 8, 2016 · N792FD · Boeing 757222 · Wing, Plate/SkinSDR FDEA201605071494Intercostal · corrodedCABIN STATION 1621, STRINGER 13L INTERCOSTAL WEB FOUND CORROSION. INTERCOSTAL WEB CORROSION REMOVED IAW SRM 51-12-02 REV 117. FOUND 50% MATERIAL LOSS. INTERCOSTAL WEB R & R WITH FABRICATED WEB IAW SRM 51-40-02 REV 117 & DWG 146N8734 SHT 1 REV C. INTERCOSTMay 7, 2016 · N782FD · Boeing 757222 · Fuselage Miscellaneous StructureSDR FDEA201605051472Frame · corrodedAFT PIT STATION 1500, FRAME AT FLOOR STRINGER RBL 7.55, CORRODED AT FLANGE. R & R FRAME AT STATION 1500, STRINGER 25L - 25R IAW SRM-51-40-02-0G & DWG 146N1030. REPAIR CLASSIFIED AS CAT A MAJOR REPAIR. CORROSION WAS REMOVED IAW-SRM-51-10-02. AFTER REWORK, AMay 5, 2016 · N789FD · Boeing 757222 · Fuselage Main, FrameSDR FDEA201605041457Deck Plate · corrodedBS 1681 LBL 10 - 17 DECK PLATE UPPER SURFACE FOUND CORRODED. COMPLIED WITH EA F-5310-T0325421 PART 1 P1. REPAIR CLASSIFIED AS MAJOR.May 4, 2016 · N782FD · Boeing 757222 · Fuselage Floor PanelSDR FDEA201605041453Pan · chafedCABIN L1 DOOR EXTERNAL HANDLE PAN FOUND CHAFED. REMOVED IAW SRM 51-10-02 REV 117. FOUND EXCEEDS LIMIT IAW SRM 52-10-01-1A REV 117. HANDLE PAN REMOVED IAW SRM 51-40-02 REV 117 & REPLACED IAW DWG 141N6100 SHT 8 REV K & SHT 14 REV F. REPAIR CLASSIFIED MAJOR IMay 4, 2016 · N782FD · Boeing 757222 · Passenger/Crew DoorsSDR FDEA201605031446Skin · damagedINCOMING LIGHTNING STRIKE REPAIR ON FUSELAGE SKIN AT STATION 1240, ABOVE STRINGER -8L, FOUND OUT OF LIMITS BY SRM, REQUIRES REPAIR. ACCOMPLISHED EA F-5330-T0324536 PT 1. CATEGORY A MAJOR REPAIR.May 3, 2016 · N789FD · Boeing 757222 · Fuselage Main, Plate/SkinSDR FDEA201605031445Seat Track · chafedCABIN STATION 1550 - 1570, LBL 24.75 SEAT TRACK CROWN CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEAN UP DEPTH ON THE LIP OF SEAT TRACK CROWN 0.040" AFTER REMOVAL THE MAXIMUM DIAMETER BETWEEN THE LIPS 0.504" EXCEED THE MAXIMUM LIMIT 0.48May 3, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201604281420Floorbeam · damagedCABIN STATION 1440, RBL 19, FLOORBEAM UPPER FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-51-2R FIG 201 REPAIR 5 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM.Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage Main, Floor BeamSDR FDEA201604281419Seat Track · damagedCABIN STATION 1316, RBL 45.5, SEAT TRACK OTBD FLANGE HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 OPTION 1 REV 117. REPAIR CLASSIFIED AS MAJOR.Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201604281418Seat Track · damagedCABIN STATION 1475, LBL 24.75, SEAT TRACK INBD FLANGE FASTENER HOLE ELONGATED. REPAIR CARRIED OUT IAW SRM 53-00-52-2R FIG 201 REPAIR 1 REV 117. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100.Apr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201604281417Seat Track · chafedCABIN STATION 1590, RBL 45.5 SEAT TRACK INBD FLANGE CHAFED. CHAFE REMOVED IAW SRM 51-10-02, REV 117. REWORKED AREA CLEANED UP DEPTH OF 0.021" MATERIAL ORIGINAL, THICKNESS 0.080" AND REMAINING THICKNESS 0.059" FOUND EXCEED 10 PERCENT LIMIT IAW SRM 53-00-52-1AApr 28, 2016 · N782FD · Boeing 757222 · Fuselage, Seat/Cargo Attach Fittings
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