N943FD

Service difficulty reports · 118

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
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 n_number = 'N943FD' AND registry_match = 'registration'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201412054075Gust Lock · failedL1 DOOR LEVER ASSEMBLY HOLD OPEN LOCK MECHANISM INOPERATIVE. R & R THE GUST LOCK IAW AMM: 52-11-08-8. OPS CHECKED NORMAL.Dec 5, 2014 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201409112566Gearbox · lowON APPROACH TE FLAP DISAGREE EICAS WARNING WHEN SELECTING FLAPS 25. FLAPS REMAINED AT 20 RAN QRH PROCEDURE, LANDED UNEVENTFULLY AT FLAPS 20. AMM SMP FOUND FAULT MSG FLAP DISAGREE 305 IN NR 1 FSEU. PROCEEDED TO TROUBLESHOOT IAW FIM 27-5 1 FT 808 FOUND OVERLOSep 11, 2014 · N943FD · Boeing 7572G5 · Trailing Edge Flap Control SystemSDR FDEA201402030241Control Box · failedDESCENDING FROM FL 380 TO APPROXIMATELY 12000', LT ENG THROTTLE STUCK. THROTTLE FREED UP & WORKED NORMAL FOR THE ARRIVAL & LANDING. R&R LT ENG LOWER CONTROL BOX ASSEMBLY IAW AMM 76-11-10-4. OPERATIONS CHECKED GOOD, RAN ENG IAW JRH & HAD GOOD THROTTLE RESPFeb 3, 2014 · N943FD · Boeing 7572G5 · Power LeverSDR FDEA201309192248Rod · wornRECEIVED A "RT REV ISLN VAL" ON TAKEOFF ROLL AT 80 KTS. REJECTED TAKEOFF. DURING TROUBLESHOOTING IAW MTSI 78-30/2705 PARA A. FOUND WORN BEARING AT END OF DIRECTION CONTROL VALVE ROD ASSEMBLY AND CAM IAW AMM 76-11-00-5 FIG 501 SHEET 1 AND SHEET 2. CAUSING GASep 19, 2013 · N943FD · Boeing 7572G5 · Engine Thrust ReverserSDR FDEA201308101827Unknown · smokeAFTER TAKEOFF, NOTICED HAZE IN COCKPIT WHICH DEVELOPED INTO LIGHT SMOKE EMINATING FROM BEHIND THE INSTRUMENT PANEL. DECLARED AN EMERGENCY & STARTED DESCENT. PERFORMED SMOKE, FIRE, FUMES CHECKLIST. AFTER STEP 10, NOTICED LIGHT SMOKE ABATED AND LEFT RESIDUALAug 10, 2013 · N943FD · Boeing 7572G5 · Air Distribution SystemSDR FDEA201301190150Stringer Clip · crackedCRACK NOTED ON BS 487, S1R FORWARD HOLE FOR STRINGER CLIP. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 53-00-03 REPAIR 2 FIG 201 AND SRM 53-00-00.Jan 19, 2013 · N943FD · Boeing 7572G5 · Fuselage Main, Attach FittingsSDR FDEA201112085216Lock · brokenDOOR HOLD OPEN LOCK LEVER ASSY IS BROKEN/DISASSEMBLED IN DOOR HINGE. PREVENTING DOOR FROM LATCHING. INSTALLED LOCK COLLAR AT L1 DOOR. OPS CHECKED GOOD IAW AMM 52-11-08-4, AND MM 52-11-08.Dec 8, 2011 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201112085215Latch · brokenDOOR OUTSIDE BUTTERFLY HANDLE HOLD DOWN LATCH ASSY BROKEN. BUTTERFLY LOCKDOWN LATCH SPRING BROKEN. INSTALLED SPRING ON L1 DOOR OUTSIDE BUTTERFLY HANDLE. REF ABOVE ENTRY FOR RII ACTION REQUIRED. FINAL CLOSED.Dec 8, 2011 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201109214009Cam · out of adjustCAPTAIN`S SLIDING WINDOW DOES NOT STAY CLOSED WHEN CRANK HANDLE IS RELEASED. WINDOW CRANK MOVES TOWARDS OPEN AND OVER CENTER INDICATOR MOVES TOWARD OPEN. CAPT'S SLIDING WINDOW FOUND UPPER CAM BLOCK, AND WINDOW OPERATING CLUTCH OUT OF ADJUSTMENT. ADJUSTED ANSep 21, 2011 · N943FD · Boeing 7572G5 · Flight Compartment WindowsSDR FDEA201109143886Battery Pack · failedEMERGENCY EXIT LIGHTS WILL NOT TEST. R & R L1 EMERGENCY EXIT LIGHT BATTERY PACK IAW MM 33-51-07-2. OPS CHECKED NORMAL.Sep 14, 2011 · N943FD · Boeing 7572G5 · Emergency LightingSDR 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 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 FDEA201101130169Skin · noneNR3 L/E SLAT UPPER SURFACE WS 509.5 HAS A TEMP REPAIR. (CURRENT SRM REQUIRES PERM REPAIR AT C-CHECK) REPAIRED NR3 SLAT ASSY IAW SRM 57-43-02, REPAIR NR1. FINAL REPAIR DIMENSIONS ARE 3" DIAMETER. THE SLAT PN IS: 114N4004-165A, SN: A1-0122. THE REPAIR WAS PJan 13, 2011 · N943FD · Boeing 757222 · Leading Edge DevicesSDR 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 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 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 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 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/SkinSDR FDEA201011224463Frame · corrodedCORROSION ON BOTTOM FRAME FROM LBL 10 TO LBL 23, STA 1040. WTB FRAME CONSIDERED SECONDARY STRUCTURE.Nov 22, 2010 · N943FD · Boeing 7572G5 · Fuselage Miscellaneous StructureSDR FDEA201011184418Floorbeam · corrodedMAIN CARGO COMPARTMENT, FLOORBEAM UPPER CHORD HAS CORROSION AT BS 1640. REMOVED CORROSION IAW SRM 51-10-02. BLENDED AREAS; L=5.0",W=2.0",D=.035", ORIG. MATL. .125", REMAINING .090", OUT OF LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3. R & R BS 1640 FLOORBEAM FNov 18, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201011124327Stringer · corrodedFWD PITT, LT SIDEWALL, BS 755, S24L, CORROSION BETWEEN SKIN AND DOME NUT STRIP. REMOVED CORROSION FROM STRINGER IAW SRM 51-10-02. BLENDED AREA; L=2.5", W=1.1", D=.030", ORIG. MATL. .080", AFTER REWORK; .050" REMAINING, OUT OF LIMITS IAW SRM 53-00- 03, FIG 1Nov 12, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Longeron/StringerSDR FDEA201011084284Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOORBEAM UPPER CHORD HAS CORROSION BS 345 BLENDED UPPER CHORD STA 345 IAW SRM 51-10-02, ORIGINAL MATERIAL .125 AFTER REWORK .106 OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL III. EXCEEDS MAX MAT LOSS OF 10 PERCENT OF ORIGINAL MANov 8, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor BeamSDR FDEA201011084283Skin · crackedR4 DOOR HAS TWO LIGHTENING STRIKES WITH CRACKS, BS 1260-1270, S16R. REPAIRED AND ACCOMPLISHED EA F-5210-141228; DOORS 2 EA CRACKS ON R4 DOOR INNER SKIN REPAIR. THIS IS A CAT"A" MAJOR REPAIR IAW FORM 8100-9, DATED 11/01/2010. DOOR ASSY PN: 146N6100-12, SN: 003Nov 8, 2010 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201011034242Skin · dentedFUSELAGE SKIN DENT, BS 1480-1500, S25R. (FROM PREVIOUS OPERATOR). MEASURED DENT A=1.256, Y=.023, A/Y=54. DISTANCE FROM DENT TO S25R IS .320, OUT OF LIMITS IAW SRM 53-00-01, P.104, FIG.101, DETAIL 3. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR NR 2. THIS IS A CNov 3, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Plate/SkinSDR FDEA201011034243Seat Track · gougedBS 418-440, LBL 45, SEAT TRACK GOUGED. REMOVED GOUGE MARK IAW SRM 51-10-02. AFTER REWORK, FOUND OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 4; L=2", W=1", ORIGINAL MATERIAL; .071", AFTER REWORK; .051", LOSS; .020". FABBED NEW SEAT TRACK, BAC 1520-792, BATCNov 3, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010264169Seat Track · chafedSEAT TRACK HAS CHAFED MARK GOUGES AND CORRODED AROUND HOLES BS 440 TO 640 RBL 45.50 REMOVED CORROSION AND GOUGES IAW SRM 51-10-02 . CHECKED LIMITS OF BLENDED AREA STA 450-660 RBL 45 MAT, LOSS .019 ON TOP OF CROWN AND .010 IN BOTTOM OF CROWN WITH IN LIMITS IAWOct 26, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010264172Skin · gougedL4 DOOR INTERNAL SKIN PANEL AT APPROX STA 1660, STR 13-L HAS A GOUGE. REMOVED DAMAGE IAW SRM51-10-02. REMOVED GOUGE BY BLENDING IAW 52-10-01 PG 104 FIG 101, DETAIL V, L=2.0 W=1.0 D=0.008. ORIG MAT 0.063, AFTER REWORK 0.055 -OUT OF LIMITS IAW SRM52-10-01 PGOct 26, 2010 · N943FD · Boeing 7572G5 · Passenger/Crew DoorsSDR FDEA201010214136Seat Track · gougedSTA 418-440, RBL 45, SEAT TRACK GOUGED. REMOVED GOUGE, AFTER REWORK OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL 7 ORIG MATL, .91, AFTER BLEND OUT, .37, ONLY 20 PERCENT OF MATL ALLOWED. REMOVED SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02. FABRICATED NOct 21, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010214135Seat Track · gougedSTA. 418-440, RBL 24, SEAT TRACK GOUGED. REMOVED GOUGE, AFTER REWORK OUT OF LIMITS IAW SRM 53-00-52, FIG.101, DETAIL 7, ORIG MATL .91, AFTER BLEND OUT, .30, LOST MORE THAN 20 PERCENT ALLOWED. REMOVED SEAT TRACK BS 418-440, RBL 24, IAW SRM 51-40-02. FABBED NEWOct 21, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010154077Seat Track · gougedMAIN DECK SEAT TRACK STA 440- 680 LBL 45.5 GOUGED & CORRODED. REMOVED GOUGES AND CORROSION PER SRM 51-10-02. BLENDED AREA ; L=13.0",W=1.0",D=.030". OUT OF LIMITS, EXCEEDS THE MAX DEPTH OF .020", GIVEN IN SRM 53-00- 52, FIG.101, DETAIL 1. FABRICATED NEW SEOct 15, 2010 · N943FD · Boeing 7572G5 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201010134040Floorbeam · corrodedMAIN CARGO COMPARTMENT FLOOR BEAM UPPER CHORD HAS CORROSION ENTIRE LENGTH BS 1660 CHECKED LIMITS STA 1660 FLOORBEAM AT LBL 55. TO RBL 59 L=6.0 W = 2.0 AND D = .038, FOUND TO BE OUT OF ALLOWABLE LIMITS IAW SRM 53-00-51, FIG.101, DETAIL 3 . REMOVED AND REPOct 13, 2010 · N943FD · Boeing 7572G5 · Fuselage Main, Floor Beam
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