Boeing 757-2Q8

Service difficulty reports · 2,798

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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 = '7572Q8'
  ORDER BY difficulty_date DESC"

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SDR FDEA201101050013Spar · gougedBETWEEN AFT SPAR AND RUDDER RIB STA 97.354 LT SIDE HAS 2 GOUGES. REPAIRED DAMAGE IAW EA F-5530-143212. STABILIZER-VERTICAL-ELONGATED HOLES IN TRAILING RIB. MAJOR REPAIR.Jan 5, 2011 · N993FD · Boeing 7572Q8 · Vertical Stabilizer, Spar/RibSDR FDEA201101030003Skin · gougedRT WING INBD MAIN FLAP OTBD END AREA T/E LOWER SIDE HAS CHAFED AREA. REMOVED GOUGE ON RT WING I/B MAIN FLAP O/B END AND FOUND OUT OF LIMITS IAW SRM 57- 53-01 FIG 101 DETAIL V. REPAIRED FLAP IAW SRM 57-53-01 REPAIR 2. EA F-5750-146241. MAJOR REPAIRJan 3, 2011 · N993FD · Boeing 7572Q8 · Trailing Edge FlapsSDR FDEA201012294762Skin · damagedSCRIBE LINE FOUND AT STA 664.438-668.813 S26L. DURING LAP SEAM INSP, REPAIRED DAMAGE TO SKIN STA 664-668 S-26L PER EA F-5330-142243 FUSELAGE -PLATES AND SKIN - AD2007-19-07/EO F-5330-7-5000-SCRIBE LINE FINDINGS. MAJOR REPAIRDec 29, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR DALA1100726804Light · inoperativeDURING LAYOVER CHECK, FOUND MID GALLEY EMERGENCY PATH LIGHT INOPERATIVE. MX REPLACED LIGHT ASSY.Dec 26, 2010 · N706TW · Boeing 7572Q8 · Emergency LightingSDR FDEA201012094627Skin · gougedGOUGE ON RT FUSELAGE SKIN NEAR R-2 DOOR UPPER FWD CORNER, STA 686,STR 7R. REPAIR ACCOMPLISHED IAW EA 757-5331-16-F2978 REF FAA FORM 8110-3, DATED NOV 22, 2010. (FIRST STAGE APPROVAL DTA PENDING) REF EA F-5330-1432220. THIS NR IS FOR TRACKING PURPOSES ONLY. Dec 9, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201012074605Floor Support · corrodedMAIN CARGO COMPARTMENT FLOOR SUPPORT HAS CORROSION BS 324 TO BS 350, RBL 40 TOP SIDE. REMOVED CORROSION IAW SRM 51-40-02. ORIG MAT THICKNESS .100 MAT LOSS .031 MAT REMAINING .069 FOUND AREA OUT OF LIMITS IAW SRM 53-00-51, PAG 103, DETAIL III, FIG 101. R & Dec 7, 2010 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201011224461Skin · dentedEXTERNAL FUSELAGE SKIN, FOUND DENTED AT BS 1120-1139.819, STRINGER 8R. FOUND TO BE OUT OF LIMITS DUE TO PROXIMITY TO STR IAW SRM 53-00-01, FIG 101, DETAIL. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FIG 201, REPAIR 2. CLASSIFIED CATEGORY "B" MAJOR REPAIR WITHNov 22, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR DALA1033216803Engine · flamed outDURING CRUISE FLIGHT THE NR 2 ENGINE FLAMED OUT. FLIGHT CREW DIVERTED THE AIRCRAFT TO SNN AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE REPLACED THE NR 2 ENGINE. (2010-D1391) (DL75E103239)Nov 20, 2010 · N704X · Boeing 7572Q8 · Engine (Turbine/Turboprop)SDR FDEA201011174407Gate · corrodedL-4 DOOR UPPER GATE HAS CORROSION. R & R L-4 PASSENGER ENTRY DOOR UPPER GATE IAW MM 52-11-38-4 AND SRM 51-10-02, FIG 101. PERFORMED ADJUSTMENT CHECK IAW MM 52-11-00-5. MAJOR REPAIR.Nov 17, 2010 · N993FD · Boeing 7572Q8 · Service DoorsSDR FDEA201011164399Skin · dentedDENTS ON FUSELAGE SKIN STA 580-600 BETWEEN STR 27L-28L EVLAUATED DENT AT STA 580-600 BETWEEN S-27L TO S28L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101 DETAIL III, DUE TO DENT BEING LESS THAN .5 FROM FRAME. REPAIRED DAMAGED AREA IAW SRM 53-00-01, FNov 16, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201011154379Seat Track · misalignedMAIN CARGO COMPARTMENT SEAT TRACK TOP HAS DOUBLE HOLES. BS 740 TO 760 RBL 45.50. FOUND DOUBLE HOLES AT FLANGE OUT OF LIMITS IAW SRM 53-00-52, DETAIL "G", FIG 101 PG 101. R & R SEAT TRACK IAW SRM 51-40-02 AND 51-20-05 AT BS 640- 780, RBL 45.50. MAJOR REPAIRNov 15, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011154378Frame · crackedMCD UPPER LOBE- FRAME AT STA 1520, S3L CRACKED. REMOVED DAMAGED AREA IAW SRM 51-10-02. FABRICATED NEW FRAME SECTION ON TRAV T10/854913, CHANNEL NR1 (2EA) TRAV T10/854912 & CHANNEL NR2 (2EA) TRAV T10/854911. LOC & DRILLED IAW SRM 53-00-07. TREATED & PRIMED Nov 15, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201011114319Skin · damagedACFT SKIN STA, 686 DAMAGED AT STRINGER 7R AT STA 686 STR 7R A MAJOR REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE P TO F MOD ON STAM W/O 11850045JUPR07 AND STAM EA 757-5331-16-2978, REV NEW DATED NOV 3, 2010. THIS NR IS FOR TRACKING PUPOSES ONLY ANNov 11, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201011114318Frame · crackedMCD UPPER FRAME AT STA 1560 CRACKED AT STR 2R. REMOVED DAMAGED FRAME SECTION IAW SRM 53-00-07, REPAIR 1 FABRICATED NEW FRAME SECTION AND REPAIR PARTS ON TRAVELERS T10/854916, T10/854914 AND T10/854915. LOCATED AND DRILLED IAW SRM 53-0007 COLD WORK HOLES IAW Nov 11, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201011074269Seat Track · gougedMAIN CARGO COMPT. SEAT TRACK HAS CHAFFED MARKS, GOUGES, AND NICKS STA 640-780 RBL 24.75 REMOVED DAMAGE ON SEAT TRACK STA 640-780 RBL 24.75 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. ORIG MATERAIL .265 REMOVED .025. MAX MATERIAL LOSS Nov 7, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201011054262Crease Beam · corrodedMAIN CARGO COMPARMENT CREASE BEAM HAS CORROSION RBL 62, BS 1260-1290. BLENDED CORROSION IAW SRM 51-10-02, CHECKED LIMITS ORIG MAT .070 MAT. REMAINING .059 FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13, PG 105, FIG 101, DET. VIII, R & R CREASE BEAM FROM STA 11Nov 5, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201011014204Skin · damagedNR1 PYLON LT SIDE SKIN 1 EA AND RT SIDE SKIN HAS 2 EA ELONGATED HOLES AT AFT BULKHEAD. COMPLIED WITH STAM EA 757-5450-16 F2907 REV - ELONGATED FASTENER HOLE FOUND IN THE RT AND LT SKIN OF NR1 PYLON COMMON TO BULKHEAD AT PP STA 201.5. EA F-5450-14227 NACELLENov 1, 2010 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Plate/SkinSDR FDEA201010294195Structure · corrodedL-2 DOOR INNER CHORD HAS SURFACE CORROSION BET BSTA 700-720 LBL 64. BLENDED AREA & REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS, MATERIAL THICKNESS .080", MAT LOST .010" MATERIAL REMAINING .070" WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15, PAG 106, DOct 29, 2010 · N993FD · Boeing 7572Q8 · Passenger/Crew DoorsSDR FDEA201010284187Floorbeam · dentedMAIN CARGO COMPARTMENT FLOORBEAM HAS DENT BS 310.5. DENTS ON FLOOR BEAM STA 310.5 NOT PERMITTED IAW SRM 53-00-51 FIG 101. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02. CLASSIFIED CAT "A" MAJOR REPAIROct 28, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201010264173Structure · damagedNR1 PYLON 1EA CODE L HOLE INCOMING DIA. .312, EO F-5450-7-5010 P5 CALLS FOR .2651-.2661 COMPLIED WITH EA F-5450-141205. NACELLES/PYLON-NR 1-INCOMING OVERSIZED HOLES. CLASSIFED CATEGORY "A" MAJOR REPAIR.Oct 26, 2010 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Main FrameSDR DALA1029846804Wire · burnedDURING FLIGHT, A FLIGHT ATTENDANT NOTICED AN ELECTRICAL SMELL IN THE AFT GALLEY NEAR THE COFFEEMAKER AREA. CREW SHUT OFF POWER TO SEVERAL GALLEY ITEMS AND THE SMELL DISSIPATED. MAINTENANCE FOUND THE COFFEEMAKER WIRES BURNED, DISABLED THE COFFEEMAKER. NEF COOct 25, 2010 · N706TW · Boeing 7572Q8 · Equipment/Furnishings WiringSDR FDEA201010244158Bulkhead · gougedNR 2 PYLON AFT BULKHEAD GOUGED INBD AND OTBD LOWER CORNERS. MACHINED DAMAGED AREAS, FABRICATED & INSTALLED REPAIR FILLERS AND GUSSETS IAW EA F-5450-141204 AND TRAVLERS T10/852810, T10/852831, T10/852832. MAJOR REPAIR.Oct 24, 2010 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201010234153Skin · dentedDENT ON FUSELAGE SKIN STA 33.45 BETWEEN S-21L TO S-22L. FOUND OUT TO BE OUT OF LIMIT IAW SRM 53-00-01, PG 101. DETAIL IV HFEC ON CUT- OUT & INITIAL FUSELAGE HOLES IAW NTM 51-00-19PT 6, NO CRACK NOTED. FABRICATED DOUBLER AND FILLER IAW SRM 53-00-01 PG 201, TABOct 23, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201010224146Bulkhead · chafedNR 1 PYLON AFT BULKHEAD RT BOTTOM CORNER SIDE HAS CHAFED MARK NAC STA 201.02. MACHINED DAMAGED AREA, FABRICATED & INSTALLED REPAIR FILLER IAW EA F-5450-142253 AND TRAVLERS T10/852836 & T10/852837. MAJOR REPAIR.Oct 22, 2010 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201010224145Bulkhead · chafedNR 1 PYLON AFT BULKHEAD LT BOTTOM CORNER SIDE AND EDGE HAS CHAFED MARK, NAC STA 201.02. MACHINED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR FILLER IAW EA F5450-142253, AND TRAVLERS T10/852834, T10/852833. MAJOR REPAIR.Oct 22, 2010 · N993FD · Boeing 7572Q8 · Nacelle/Pylon, Bulkhead/FirewallSDR FDEA201010214134Seat Track · corrodedSEAT TRACK CORRODED STA 1640, RBL45. REMOVED CORROSION ON STA RBL 45.5 IAW SRM 51-10-02 ORIG MAT=.100" AFTER REWORKED 0.050" FOUND OUT OF LIMIT IAW SRM 53-00-52, FIG 101, SH3 T0 6 DETAIL V L=6" W=2" D=0.050", R & R SEAT TRACK FROM STA 1540-1640 RBL 45.5 FAOct 21, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010204120Skin · damagedEXTERNAL SKIN BS 1140 TO 1360 16R/28R HAS SCRATCHES, CORROSION(COMMON TO WTB FAIRINGS). REMOVED CORROSION FROM SKIN STA 1140-1360 S-16R TO S-28R AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL II. ORIG MAT .055 AFTER REWORK .023. REPAIRED SKIN Oct 20, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Plate/SkinSDR FDEA201010194109Seat Track · damagedMAIN CARGO COMPARTMENT SEAT TRACK HAS CHAFFED MARK AND GOUGES.BS 418 TO 440, RBL 45.50. REMOVED CORROSION FROM CROWN, REMOVED .031 MAT (NO THICKNES), FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52 FIG 101 DET I. FABRICATED NEW SEAT TRACK OF PN BAC1520-792, BATCH Oct 19, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010164083Stringer · corrodedCORROSION ON STRINGER 26L BS 760-780 INSIDE FWD CGO COMPARTMENT. REMOVED DAMAGE IAW SRM 51-10-02 CHECKED LIMITS ON STA 760 S-26L SKIN ATTACHMENT (STRINGER) FOUND TO BE EXFOLIATED AROUND HOLES FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53 FIG 101 SHEET 1 PG 105Oct 16, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201010164084Seat Track · gougedMAIN DECK SEAT TRACK GOUGE IN SEVERAL AREAS FROM STA 1540 TO 1640, LBL 45.5. REMOVED GOUGE AREA IAW SRM 51-10-02, ORG MAT THINESS .180" AFTER REWORKED FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, FIG 101, SH2 PAGE 102 L=6" W=1" D=0.050" R & R SEAT TRACK FROM SOct 16, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010164082Stringer Splice · corrodedFWD CARGO PIT, STA 770, S27L, WL 138 CORRODED. REMOVED DAMAGED AREA OF STR IAW SRM 53-00-03, FABRICATED FILLER AND SPLICE ON TRAV NR T10/856553 AND T10/856554 BATCH NR 0001611893, 7075-0.090C LOCATED , DRILLED, AND INSTALLED SPLICE AND FILLER IAW SRM 53-00-0Oct 16, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Longeron/StringerSDR FDEA201010144067Seat Track · misalignedSTA 418, RBL-45 AFT SEAT TRACK FITTING IS MISLOCATED (INCOMING). REMOVED FITTING AT RBL 45, STA 418, SEAT TRACK SPLICE IAW SRM 51-40-02, RECEIVED NEW FITTING PN 14N2504-1 BATCH 1923858, INSTALLED FITTING AT RBL 45 STA 418 SEAT TRACK SPLICE IAW SRM 51-40-02. MOct 14, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010134034Seat Track · gougedSEAT TRACK GOUGE IN SEVERAL AREA FROM STA 1540 TO 1640 LBL 24. GOUGES ON SEAT TRACK STA 1540-1640 LBL 24 MEASURED OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL I. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIROct 13, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010134037Floor Support · corrodedMAIN DECK FLOOR SUPPORT ANGLE CORRODED AT STA 374, LBL 58. REMOVED COPRROSION ON CHANNEL IAW SRM 51-10-03 CHECKED LIMITS ORIGINAL MAT .050. REMAINING .042 LOSS .008 FOUND OUT OF LIMITS DETAIL FIG 101 PG 103 W=2.00 L=3.00 DEPTH .008 IAW SRM 53-00-51 R & R IAWOct 13, 2010 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201010063958Seat Track · gougedMAIN CARGO COMPARTMENT SEAT TRACK HAS CHAFFED MARK AND GOUGES BS 418 TO 440 RBL 25.75. REMOVED .023 MATERIAL FROM SEAT TRACK CROWN AT STA 418-440,RBL 25.75,OUT OF LIMITS IAW SRM 53- 00-52 FIG 101 DET I REMOVED SEAT TRACK FABRICATED NEW SEAT TRACK FROM MATEOct 6, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010053939Frame · gougedRH CABIN FRAME AT B STA 1280 BETWEEN S-10R THRU S-12R HAS AREAS GOUGED AND SCRATCHED. REMOVED GOUGES STA 1280 BETWEEN S-10R TO S-12R AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. ORIG MATERIAL .071 AFTER REWORK .058. REMOVED DAMAGE AND Oct 5, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201010053938Frame · gougedMCD FRAME WITH 3EA GOUGES STA 1280 STR 10L,11L AND 13L. EMOVED GOUGES STA 1280 BETWEEN S-10L TO S-13L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL II. ORIG MATERIAL .071 AFTER REWORK .062. REMOVED DAMAGE AND INSTALLED REPAIR PARTS IAW SRMOct 5, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201010053935Shear Web · corrodedMAIN CARGO COMPARTMENT FLOOR SHEAR WEB HEAVY CORRROSION BS 1680 TO BS 1720 LBL 51.5 TO RBL 51.5. REMOVED CORROSION AT STA 1681-1720, LBL 51.5 TO RBL 51.5 ON SHEAR WEB 5 EA PLACES. NR 1 ORIG MAT .071 MAT. LOSS .019, REMAINING .052, NR 2. ORIG MAT .071, MAT LOct 5, 2010 · N993FD · Boeing 7572Q8 · Fuselage Miscellaneous StructureSDR FDEA201009293791Crease Beam · corrodedRH MAIN DECK CREASE INNER CHORD AT STA 1420 BOTTOM SURFACE NEAR SCREW HOLES CORRODED. RT SIDE CREASE BEAM IB CHORD STA 1420 MEASURED OUT OF LIMITS IAW SRM 53-60-15 FIG 101 DETAIL III. REMOVED AND REPLACED CHORD IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJORSep 29, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, StructureSDR FDEA201009293794Support · crackedSEAT TRACK SUPPORT STA 365-418 RBL 24 CRACKED. REMOVED SEAT TRACK SUPPORT, FABRICATED NEW SEAT SUPPORT IAW SRM 53-10-52 PG3,DETAIL II INSTALLED NEW SEAT TRACK SUPPORT AT RBL 24 STA 365-418 IAW SRM 51-40-02. MAJOR REPAIRSep 29, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009283776Seat Track · corrodedSTA 365-418, RBL 45, SEAT TRACK SUPPORT CORRODED. REMOVED CORROSION, ORIGIN MAT .070, MAT REMOVED .028, MAT REMAINING .042 FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52 FIG 101 DET VII. REMOVED DAMAGED SEAT TRACK SUPPORT IAW SRM 51-40-02, FABRICATED NEW SEAT Sep 28, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009273740Failsafe · corrodedFAIL SAFE CHORD HAS SURFACE CORROSION BET BSTA 700-BSTA 720 RBL 64 (NEAR R-2 DOOR). REMOVED CORROSION FROM CHORD STA 600-720 ORIGINAL MAT .080 REMOVED .030 FOUND TO BE OUT OF LIMITS IAW SRM 53-30-15 DET III, PAG 106. R & R CHORD, PN 143N8328U54, MAJOR REPSep 27, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, FrameSDR FDEA201009203575Seat Track · gougedMAIN CARGO COMPARTMENT UNDER SEAT TRACK WEB HAS GOUGE BS 780 TO 879 RBL 45.50. REMOVED GOUGE UNDER SEAT TRACK WEB BS 780 TO 879 RBL 45.50 IAW SRM 51-10-50 CHECKED LIMITS MATERIAL THICKNESS .145" MATERIAL LOST .015" MATERIAL REMAINING .130" FOUND TO BE OUT Sep 20, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009203567Seat Track · gougedSEAT TRACK LBL 45.50 FROM BS 1075 TO 1180 HAS GOUGES, CHAFE MARKS AND WORN SCALLOPS. BLENDED DAMAGED AREA IAW SRM 51-10-02 ORIGINAL THICKNESS .230 MAX CLEAN UP DEPTH ON TOP SURFACE .020 MATERIAL REMOVED .03 FOUND TO BE OUT OF LIMITS IAW 53-00-52 FIG 101 DETASep 20, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009183538Seat Track · corrodedMAIN DECK SEAT SUPPORT CORRODED AT STA 377.5, LBL24. REMOVED .024" FROM .070" ORIGINAL MATERIAL,OUT OF LIMITS IAW SRM 53-0052 FIG 101 DET VII REMOVED SEAT TRACK SUPPORT, FABRICATED NEW SEAT TRACK SUPPORT IAW SRM 53-10-52 DET III INSTALLED NEW SEAT TRACK AT Sep 18, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009183539Seat Track · gougedMAIN CARGO COMPARTMENT SEAT TRACK HAS GOUGED AND CHAFED MARKS BS 1075 TO 1180 RBL 45.50. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 NOTE "G". R & R ON SEAT TRACK IAW SRM 51-40-02.Sep 18, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009163508Floorbeam · corrodedINSIDE CABIN STA 1640 LBL 58" FLOORBEAM HAS CORROSION AT FASTENER HOLE. REMOVED CORROSION IAW SRM 51-10-02, CHECKED LIMITS FOUND REMAINING MAT 0.095", OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DET VI. REMOVED FLOORBEAM AT STA 1640 IAW SRM 51-40-02, RECEIVED Sep 16, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Floor BeamSDR FDEA201009153494Seat Track · gougedMAIN DECK SEAT TRACK GOUGED AT STA 418 LBL 45. REMOVED 0.025" GOUGED MATERIAL FROM SEAT TRACK CROWN. OUT OF LIMITS IAW SRM 53-00-52 DET.I AND SRM 51-10-02. REMOVED SEAT TRACK . FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 DET I INSTALLED NEW SEAT TRACK AT LBSep 15, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153493Seat Track · gougedMAIN DECK SEAT TRACK GOUGES AT STA. 418 LBL24. REMOVED 0.032" GOUGED MATERIAL FROM SEAT TRACK CROWN. OUT OF LIMITS IAW SRM 53-00- 52 DET.I AND SRM 51-10-02. MAJOR REPAIRSep 15, 2010 · N993FD · Boeing 7572Q8 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201009153421Stringer · corrodedFWD PIT STRINGER CORRODED 26L AT FRAME STA 600. REMOVED CORROSION ON STRINGER STA 600 S-26L AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03, FIG 101, DETAIL II. R & R STRINGER IAW SRM 51-40-02. CLASSIFIED CATEGORY "A" MAJOR REPAIR.Sep 15, 2010 · N993FD · Boeing 7572Q8 · Fuselage Main, Longeron/Stringer
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