Boeing 757-2G5

Service difficulty reports · 557

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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 = '7572G5'
  ORDER BY difficulty_date DESC"

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SDR FDEA201109123854Battery Pack · inoperativeEMERGENCY EXIT LIGHTS WILL NOT COME ON DURING A TEST. R & R RT EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.Sep 12, 2011 · N943FD · Boeing 7572G5 · Emergency LightingSDR FDEA201108253488Reservoir · emptyON ARRIVAL DURING L1 DOOR OPENING DOOR BOTTLE WAS DISCHARGED BUT SLIDE WAS NOT DEPLOYED. R & R L-1 DOOR EMERGENCY ASSIST POWER RESERVOIR IAW MM 52-11-30-4. OK FOR SERVICE.Aug 25, 2011 · N944FD · Boeing 7572G5 · Passenger/Crew DoorsSDR U2RA227DHN044Floor Support · corrodedMAIN CABIN, BETWEEN STA 1640 TO 1681 RT OF BUTTE LINE 56", FLOOR SUPPORT HAS CORROSION AROUND SEVERAL SCREW HOLES.Jun 16, 2011 · N151GX · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR U2RA227DHN043Control Cable · nickedMAIN PASSENGER CABIN CABLE RUN A2B, APROX 6 INCHES FWD OF STA BS460 HAS A NICK.Apr 4, 2011 · N151GX · Boeing 7572G5 · Aileron Control SystemSDR U2RA227DHN042Angle · corrodedINBD LANDING FOR WING ACCESS PANEL NR 611JB HAS CORROSION AT FWD SECTION.Apr 4, 2011 · N151GX · Boeing 7572G5 · Wing Miscellaneous StructureSDR U2RA227DHN041ASkin · misrepairedFUSELAGE REPAIR AT STA BS1520, BETWEEN S8L AND S10L REQUIRES REWORK. DOES NOT MEET THE REQUIREMENTS OF SRM 53-00-01, REPAIR NR 2.Mar 21, 2011 · N151GX · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201102010446Skin · damagedEXISTING FUSELAGE SKIN REPAIR AT STA 1713-1717, BETWEEN S-18L TO S-19L REQUIRES REWORK IAW EA F-5330-142277 COMPLIED WITH EA F-5330-142277 FUSELAGE-PLATES AND SKIN (AD2006-11-11) EO F-5100-7-5001, EXISTING REPAIR STA 1713 S-18L, MAJOR REPAIR.Feb 1, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201101310430Channel · damagedSRM 53-00-03, REPAIR NR1 OF N/R N00148, REPAIR REQUIRES REPLACEMENT AT "BS 310.5- 324, S4R". REMOVED HAT SECTION STA 340, STR 4R IAW SRM 51-40-02. R & R HAT SECTION STA 340 STR 4R IAW SRM 53-00-03, FIG 201, R2. THIS IS A CAT A REPAIR IAW NOTES, REF IN SRM Jan 31, 2011 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201101310429Channel · damagedREPAIR NR1 OF NR N00239, REPAIR REQUIRES REPLACEMENT AT FWD PIT SIDEWALL, BS 755, S24L. REMOVED EXISTING HAT SECTION STA 755, S24L IAW SRM 51-40-02. REPAIRED STRINGER STA 755, 24L IAW SRM 53-00-03 FIG 201 R2. THIS IS A CAT "A" REPAIR. MAJOR REPAIR.Jan 31, 2011 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201101280404Crease Beam · gougedMAIN DECK BS 550, RBL 64, OTBD CREASE BEAM DOUBLER REPAIR. C/W ATTACHMENT "B" OF EO F-5100-7-5001, PT 1 LOWER SURFACE OF OTBD CHORD, BS 556, GOUGED JUST AFT OF -3 REPAIR SPLICE. ACCOMPLISHED EA F-5310-142282. MAJOR REPAIRJan 28, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201101250352Skin · misrepairedFUSELAGE SKIN DENT BS 1480-1500, S25R, DUE TO INCORRECT REPAIR INSTALLED. REMOVED REPAIR DOUBLER AT BS 1480-1500, S25R, IAW SRM 51-40-02. INSTALLED NEW REPAIR DOUBLER AT BS 1480-1500, S25R, IAW SRM 53-00-01, FIG. 201, REPAIR NR 15. THIS IS A CAT "B" REPAIR WJan 25, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201101250351Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 1610, S17L, DOES NOT MEET CURRENT SRM REQUIREMENTS AND REQUIRES NEW REPAIR. (ORIGINALLY ON N00019, WHICH WAS EVALUATION-ONLY). REMOVED SKIN REPAIR AT BS 1610, S17L, THAT DID NOT MEET CURRENT SRM REQUIREMENTS IAW SRM 51-40-02. INSTJan 25, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201101240343Skin · misrepairedFUSELAGE SKIN REPAIR AT BS 650, S21R / 22R, DOES NOT MEET CURRENT SRM RQUIREMENTS. REMOVED EXISTING DOUBLER, STA 650, S21R- 22R, IAW SRM 51-40-02. INSTALLED REPAIR DOUBLER STA 650, B/T S21R- 22R, IAW SRM 53-00-01 FIG 201R,NR16. THIS IS A CAT "B" REPAIR WITJan 24, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201101130171Skin · dentedNR 1 SLAT UPPER SURFACE, WS 711.5, HAS A TEMP REPAIR OR A DENT. (CURRENT SRM REQUIRES PERM. REPAIR AT C-CHECK) REPAIRED NR1 L/E SLAT IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSION IS 3" DIAMETER. SLAT ASSY PN IS: 114N4002-133, SN: A1-0143. REPAIR WAJan 13, 2011 · N943FD · Boeing 7572G5 · Leading Edge DevicesSDR FDEA201101130170Wedge · damagedNR 5 L/E SLAT UPPER SURFACE, T/E WEDGE, BETWEEN INBD TRACK AND MID-TRACK HAS A TEMP. REPAIR OF A DENT. (CURRENT SRM REQUIRES PERM. REPAIR AT C-CHECK) REPAIRED NR5 SLAT IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSION IS 3" DIAMETER. THE SLAT ASSY P/N IJan 13, 2011 · N943FD · Boeing 7572G5 · Standard Practices/StructuresSDR FDEA201101060059Frame · misalignedSHORT EDGE MARGIN CONDITION ON 657N3227-8 FRAME DOUBLER CHORD AT STA 680 S-4R . AT STA 680, STR 4 R , A SHORT EDGE MARGIN CONDITION EXIST ON THE 657N3227-8 FRAME DOUBLER CHORD. A REPAIR WAS ACCOMPLISHED ON STAM EA757-5332-16-F2980 REV- DATED 10/18/2010. Jan 6, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, FrameSDR FDEA201101060057Fitting · damagedPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161-12 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640, S 17R TO S 18R AT STA 1640, STRINGER 17 AND 18 R. A REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON STAM W/C 1Jan 6, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201101060048Fitting · misalignedPOTENTIAL SHORT EDGE MARGIN CONDITIONS IN THE 657N3161 FITTING DUE TO INCOMING FASTENER HOLE LOCATIONS AT STA 1640 S-17L TO S-18L AT STA 1640, STR 17 AND 18L A REPAIR WAS ACCOMPLISHED DUE TO DISCREPANCY EFFECTING THE PTF CONVERSION ON STAM PTF W/C 118350399EJan 6, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201101060046Tear Strap · damagedINCOMING FASTENER HOLES IN 140N2311-4, TEAR STRAP AT S-4R STA 680 AND STA 700 DO NOT COMPLY WITH DWG 657N3242, SHEET 7, REV A REQUIREMENT AT STA'S 680 AND 700; STR 4R, 4 EA ADDITIONAL FASTENER HOLES AT BOTH STA'S DO NOT COMPLY WITH DWG 657N3242 EFFECTING PTFJan 6, 2011 · N943FD · Boeing 7572G5 · Fuselage Main, StructureSDR FDEA201012294764Bushing · gougedRT PYLON INBD SIDE LOAD BUSHING GOUGED REPAIRED NR2 PYLON INBD SIDE BUSHING IAW EA F-5720-143207. WING-FITTINGS-AD 2004-4-12-07/ EO 5450-7-5003. NR2 PYLON INBD SIDE LOAD FITTING BUSHING OS. MAJOR REPAIR.Dec 29, 2010 · N943FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201012294763Bushing · gougedRT PYLON OTBD WING TO PYLON MID SPAR SUPPORT FITTING HAS A GOUGED BUSHING. REPAIRED DAMAGE ON NR2 PYLON IAW EA F-5720-142296. WINGS FITTINGS-AD2004-12-07-EO F- 5450-7-5003. NR2 ENG PYLON OTBD SIDE LOAD FITTING OS HOLE. MAJOR REPAIR.Dec 29, 2010 · N943FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201012144664Skin · misrepairedEXISTING REPAIR ON R1 DOOR INNER SKIN , DOES NOT CONFORM TO PREVIOUS OPERATOR DATA (REF 8110-3 ). ACCOMPLISHED EA F-5210-146201. DOORS- CREW AND PASSENGER-- R1 ENTRY DOOR INNER SKIN REPAIR. THIS IS A CAT A. REPAIR MAJOR REPAIR WITH 8100-9.Dec 14, 2010 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201012134649Skin · corrodedAPU INLET DOOR ATTACH STRUCTURE STA 1825 B/T STR'S 3R- 6R CORRODED ACCOMPLISHED EA F-5330-142280, FUSELAGE-PLATES SKIN- SECTION 48 APU INLET STRAP CORROSION REPAIR PN 148N3138-8000. THIS IS A MAJOR REPAIR.Dec 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201012124644Skin · dentedNR4 SLAT T/E OTBD SIDE LWR SURFACE HAS A DENT. REPAIRED NR4 SLAT T/E IAW SRM 51-70-10, SLAT NR4 PN: 114N4005-159, SN : A1-0144, DAMAGE WAS REPAIRED ON LOWER SKIN APPROX 2" FROM OTBD END, FINAL DIMENSION OF REPAIR IS 3" IN DIAMETER. F-5740-146203 GENERATED FDec 12, 2010 · N943FD · Boeing 7572G5 · Leading Edge DevicesSDR FDEA201012074610Skin · dentedFUSELAGE EXTERIOR SKIN WITH DENT AT BS 1701 TO BS 1720, AT STR 20R. DENT REPAIRED IAW EA F-5330-142379. (FUSELAGE SKIN DENT AT S-20R LAP JOINT BETWEEN BS 1701 AND BS 1720). REPAIR IS CLASSIFIED AS MAJOR.Dec 7, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201012074609Fitting · misalignedRT WING INBD FWD FLAP TRACK FAIRING BRACKET ATTACHMENT HOLES ON AFT LANDING GEAR TRUNNION HSG MISALIGNED. BRACKET FOR RT WING INBD FWD FLAP TRACK FAIRING REPAIRED IAW EA F-5740-142375. (WING ATTACH FITTINGS - 1 FASTENER HOLE MISALIGNED ON 113N1159-1 FITTING).Dec 7, 2010 · N944FD · Boeing 7572G5 · Trailing Edge FlapsSDR FDEA201012064599Skin · dentedAFT CARGO DOOR EXTERNAL SKIN, HAS A DENT, APPROX BS 1435. EVALUATED DENT IAW SRM 52-30-01,DETAIL 6 AND FOUND OUT OF LIMITS IAW SRM 52-30-01, FIG 101, DETAIL 6; A/Y=20. HFEC NOTED NO CRACKS. CUT OUT SKIN IAW SRM 52-30-01,STEP 3. REMOVED FASTENERS IAW SRM 51-40Dec 6, 2010 · N943FD · Boeing 7572G5 · Cargo/Baggage DoorsSDR FDEA201012064593Floor Support · corrodedFWD CARGO COMPT FLOOR DECK SPLICE STRAPS FOUND CORRODED AND BENT AT STA 550, STA 653.80 AND STA 749.40. CORRODED STRAPS IN FWD CARGO COMPARTMENT. R & R IAW AMM 25-50-04, REV 89. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 6, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201012064592Floor Support · corrodedAFT CARGO COMPT FLOOR DECK SPLICE STRAPS FOUND CORRODED AND BENT AT STA 1330, STA 1470 AND STA 1510. CORRODED AFT CARGO COMPARTMENT FLOOR DECK SPLICE STRAPS R & R IAW AMM 25-50-04, REV 89. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 6, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201012034554Attach Fitting · corrodedFWD CARGO COMPT LT CARGO TIE-DOWN FITTINGS AT STA 760, STA 780, STA 800, STA 820 AND STA 840 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360. FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIEDec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034553Attach Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 680, STA 700, STA 720, STA 740, FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJDec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034552Attach Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1560, STA 1580, STA 1600 AND STA 1620 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN AFT CARGO COMPT REPAIRED IAW EA F-5340-142364. (AFT CARGO TIE DOWN FITTINGS CORROSION REPAIR) REPAIR IS CLASSIFDec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034551Attach Fitting · corrodedFWD CARGO COMPT RH CARGO NET TIE-DOWN FITTINGS AT STA 520 AND STA 540 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360. (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR) REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-Dec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034550Attach Fitting · corrodedFWD CARGO COMPT RT CARGO NET TIE-DOWN FITTINGS AT STA 660, STA 680, STA 700, STA 720 AND STA 740 FOUND WITH CORROSION. CORRODED FITTINGS IN FWD CARGO COMPT REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MDec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034549Attach Fitting · corrodedFWD CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 600, STA 620, STA 640 AND STA 660 FOUND WITH CORROSION. CORRODED FITTINGS REPAIRED IAW EA F-5340-142360 (FWD CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Dec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034548Attach Fitting · corrodedAFT CARGO COMPT RH CARGO NET TIE-DOWN FITTINGS AT STA 1560, STA 1580, STA 1600 AND STA 1620 FOUND WITH CORROSION. REPAIR CARRIED OUT ON CORRODED FITTINGS IAW F-5340-142364 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMMDec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012034547Attach Fitting · corrodedAFT CARGO COMPT LT CARGO NET TIE-DOWN FITTINGS AT STA 1240, STA 1300, STA 1320 AND STA 1340 FOUND WITH CORROSION. REPAIR CARRIED OUT ON CORRODED FITTINGS AT STA 124, 1300, 1320 AND 1340 IAW F-5340-142364 (AFT CARGO TIE-DOWN FITTINGS CORROSION REPAIR). REPADec 3, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012024544Support · crackedAFT CARGO COMPT RH FLOOR DECK PLATE SUPPORT AT STA 1506 RBL 10.5 FOUND CRACKED. CRACKED SUPPORT AT STA 1506, RBL 10.5. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 2, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201012024542Attach Fitting · corrodedAFT CARGO COMPT RI CARGO NET TIE-DOWN FITTINGS AT STA 1360, STA 1377, STA 1383 AND STA 1400 FOUND WITH CORROSION. CORRODED TIE-DOWN FITTINGS AT STA 1360, 1377, 1383 AND STA 1400. R & R IAW SRM 51-40-02 REV 101. REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100.Dec 2, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201012024540Threshold · crackedAFT CARGO COMPT THRESHOLD PLATE FOUND WITH CRACKS AND DENTS. CRACKED THRESHOLD PLATE IN AFT CARGO COMPT. R & R IAW AMM 53-33-01, REV 89. REPAIR IS CLASSIFED AS MINOR IAW GMM 6-2-100.Dec 2, 2010 · N944FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201011304516Rib · corrodedLT AILERON NR2 BALANCE WEIGHT SUPPORT RIB FROM OTBD HAS CORROSION. REMOVED CORROSION ON LT AILERON NR 2 BALANCE WEIGHT SUPPORT RIB IAW SRM 51-10-02 BLEND OUT DIM = L .50,W .50, D.05 ORIGINAL MATERIAL THICKNESS .125, FOUND OUT OF LIMITS IAW SRM 57-60-0Nov 30, 2010 · N943FD · Boeing 7572G5 · AileronsSDR FDEA201011304521Skin · dentedLT FUSELAGE SKIN HAS A DENT AT BS 1715, S16L, ACCOMPLISHED EA F-5330-142297; "FUSELAGE-PLATES AND SKIN-SECTION 46-FUSELAGE SKIN, SMOOTH DENT REPAIR, BS 1715, S16L" REF FAA FORM 8110-3, DATED 11/18/2010; "FIRST STAGE APPROVAL", DTE PENDING NOT TO EXCEED 12 MONNov 30, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201011284505Skin · corrodedRT WING TOP SKIN - AFTER REMOVAL OF OVERWING FILL PORT ADAPTOR, FOUND CORROSION ON SKIN CUTOUT. CORROSION REPAIR CARRIED OUT ON RT WING TOP SKIN IAW EA F-5730-137696 (RT WING TOP SKIN FUEL PORT CORROSION REPAIR). REPAIR IS CLASSIFIED AS MAJOR IAW GMM 6-2-100.Nov 28, 2010 · N944FD · Boeing 7572G5 · Wing, Plate/SkinSDR FDEA201011284504Bracket · crackedNR1 ENG OTBD FAN COWL UPPER HINGE HEAT SHIELD COVERS 4 EA FOUND WITH CRACKS. CRACKED NR1 ENGINE OTBD FAN COWL UPPER HINGE REPAIRED IAW EA F-7110-142348 (NR1 AND NR2 ENGINE FAN COWLING SHIELD HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAWNov 28, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon, Attach FittingsSDR FDEA201011284503Bracket · crackedNR 2 ENG INBD FAN COWL HAS 4EA UPPER HINGE COVER PLATES WITH CRACKS. CRACKED NR2 ENG INBD FAN COWL HINGE COVER PLATES REPAIRED IAW EA F-7110-142348 (NR1 AND NR2 ENG FAN COWLING SHIELD - HINGE BRACKET WELDING REPAIR). REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2Nov 28, 2010 · N944FD · Boeing 7572G5 · Nacelle/Pylon Miscellaneous StructureSDR FDEA201011264493Skin · damagedRT WING NR 10 L/E SLAT T/E LOWER SURFACE PUNCTURED. REPAIRED RT WING NR 10 SLAT T/E WEDGE IAW SRM 51-70-10. MAJOR REPAIR.Nov 26, 2010 · N943FD · Boeing 7572G5 · Leading Edge DevicesSDR FDEA201011264491Skin · delaminatedNR5 SLAT T/E LOWER SURFACE OTBD CORNER SIDE DELAMINATED. REPAIRED NR 5 SLAT IAW SRM 51-70-06. MAJOR REPAIR.Nov 26, 2010 · N943FD · Boeing 7572G5 · Leading Edge DevicesSDR FDEA201011254488Floorbeam · corrodedCABIN, EXISTING REPAIR AT STA 324, RBL 51 TO RBL 40, TO FLOORBEAM CAP. EVALUATE AND RECTIFY. CABIN STA 324 FLOORBEAM UPPER CAP PN 141N2932-23, R & R IAW SRM 51-40-02, REV 101. THIS REPAIR IS CLASSIFIED AS MINOR IAW GMM 6-2-100 CRITERIA.Nov 25, 2010 · N944FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201011234469Skin · corrodedRT WING NR9 L/E SLAT, OTBD AREA, CORROSION RUNS UNDER BOTH FASTENERS. ACCOMPLISHED EA F-5740-141230; WING L/E SLAT NR9, NOSE SKIN CORROSION REPAIR. REF. FAA FORM 8100-9, DATED 11/12/2010. REPAIR ACCOMPLISHED ON SLAT ASSY. PN; 141N4003- 174, SN; A2-0122. CONov 23, 2010 · N943FD · Boeing 7572G5 · Leading Edge DevicesSDR FDEA201011234468Skin · dentedEXTERNAL FUSELAGE SKIN HAS DENT AT STA 1705 S-15L. ACCOMPLISHED ON EA F-5330-143215, STA 1705 SKIN REAPIR AT STR 15L CAT B, REPAIR OF FAA FORM 8100-9 JAN 6, 2011 A NEW FAA APROVAL WHICH MUST BE ISSUED FINDING COMPLIANCE WITH 14 CFR 26.43 (D) AND 25.571 PRIORNov 23, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/Skin
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