N914FD

Service difficulty reports · 168

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 = 'N914FD' 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 FDEA201001140148Seat Track · damagedEXISTING SEAT TRACK HAS SCALLOPS PREVIOISLY REMOVED AT STA 1635-1640 LBL 24 WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. R & R SEAT TRACK AT LBL 24, STA 1540 TO 1640 IAW SRM 51-40-02 AND 51-40-05. SEAT TRACK FABRICATED ON MAE FAB TRAV, T10/8Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001140147Seat Track · damagedEXISTING SEAT TRACK HAS SCALLOPS PREVIOUSLY REMOVED AT STA 1635-1640, RBL 24 WHICH WILL INTERFERE WITH INSTALLATION OF CARGO HANDLING SYS. R & R SEAT TRACK BETWEEN STA 1540 TO 1640, RBL 24.75 IAW SRM 51-40- 02. MAJOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001140145Crease Beam · corrodedMAIN CABIN STA 1140 I.B CREASE BEAM CORRODED. REMOVED DAMAGED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 51-40-02. INSTALLED NEW CREASE BEAM AT RT STA 1040 TO 1180, IAW SRM 51-40-02 AND 51-20-05. MAJOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001140135Support · corrodedNR 2 CARGO DOOR LWR SILL SUPPORT FRAME STA 1380-1440 HAS CORROSION UNDER NUTPLATES. REMOVED CORROSION IAW SRM 53-60-15 CHECKED LIMITS ORIG 0.220 MAT REMAIN 0.190, LOSS 0.030 AT LOWEST FOUND OUT OF LIMITS IAW SRM 53-60-15. REMOVED AND REPLACED TEE FITTING IAJan 14, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001140132Floor Support · corrodedMCD FLOOR SUPPORT WEB SURFACE IS CORRODED BETWEEN STA 700 TO STA 720 AT LBL 64. R & R GUTTER SUPPORT. CHECKED LIMITS, FOUND OUT OF LIMITS IAW SRM 53-00-51, PG. 103, FIG. 101, DETAIL II. MINOR REPAIR.Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA201001140131Crease Beam · corrodedCORROSION FOUND ON LOWER SURFACE OF MCD CREASE BEAM BETWEEN STA 680 TO STA 700 AT LBL 64. ORIG MAT THICKNESS .050 MAT LOSS .008 MAT REMAIN .042, FOUND AREA OUT OF LIMITS IAW SRM 53-00-51, FIG 01, DETAIL VI, PAG 103. R & R CHANNEL PN 143N5410-1, IAW SRM 51-40-Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001140130Floorbeam · corrodedFLOORBEAM 1681.18 UPPER CAP LOWER SURFACE BOTH FWD AND AFT FLANGES HAVE CORROSION ON AND AROUND NUTPLATE ASSY. REMOVED NUT PLATE ASSY IAW SRM 51-40-02. FABRICATED NEW NUT PLATE ASSY IAW SRM 51-40-01. INSTALLED NEW NUT PLATE ASSY STA 1681.8, IAW SRM 51-40-0Jan 14, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201001130101Floorbeam · corrodedCABIN FLOORBEAM, STA 377 UPPER T-CHORD BL 0 TO LBL 65 HAS CORROSION AT FASTENER HOLES. CORROSION REMOVED, FOUND OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DET 3 , REMOVED PREVIOUS REPAIR FROM LBL 70-RBL 41 FABED TEE, RECEIVED NEW REPAIR ANGLES -2 AND -3, AND STRAJan 13, 2010 · N914FD · Boeing 75728A · Fuselage Main, Floor BeamSDR FDEA201001130097Seat Track · corrodedMCD SEAT TRACK CROWN HAS NUMEROUS GOUGES BETWEEN STA 780 TO STA 820 AT LBL 46. REMOVED AND REPLACED SEAT TRACK FROM SPLICE AT STA 780, TO SPLICE AT STA 879, LBL 46, IAW SRM 51-40-02. CATEGORY "A", MAJOR REPAIR.Jan 13, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001130096Seat Track · corrodedMCD SEAT TRACK CROWN HAS NUMEROUS CORROSIONS BETWEEN STA 980 TO STA 1005 AT LBL 46. CAPTURED THE CLASS "A" MAJOR REPAIR THAT R & R SEAT TRACK PN BAC1520841 IAW SRM'S 53-00-52, 51-40-02, 51-20-01. SEAT TRACK CORROSION WAS OUT OF LIMITS, MAT LOSS WAS MORE THAN Jan 13, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001130095Seat Track · corrodedNUMEROUS GOUGES AND CORROSION FOUND ON MCD SEAT TRACK BETWEEN STA 900 TO STA 1076 AT LBL 25. R & R SEAT TRACK IAW SRM 51-40-02/ 51-20-05. GOUGES AND CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101. NEW SEAT TRACK FABRICATED ON SHOP TRAVELER NR Jan 13, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001130094Window Frame · corrodedCABIN RT WINDOW FRAME STA 990 HAS CORROSION. RT CABIN WINDOW FRAME, AT STA 990, FOUND TO BE OUT OF LIMITS IAW SRM 56-20-02, FIG 101, TABLE 1. R & R WINDOW FRAME , RT STA 990, PN 144N3250Y4, BATCH NR 0001791095, IAW SRM 51-40-02. REF EA F-5620-131588. MAJOR RJan 13, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001120086Skin · dentedDENT IN ACFT SKIN APROX STA 1345 BETWEEN STR 25R AND 26R. CHECKED LIMITS ON DENT STA 1345 STR 25R-26R ORIG .070, DEPTH OF DAMAGE .020. FOUND OUT OF LIMITS IAW SRM 53-00-01 DET 3 FIG 101, DENT 0.5 X 1.0, REMOVED DAMAGE SKIN STA 1345 IAW 53-00-01 HFEC DENT CUJan 12, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001110081Skin · dentedAFT FUSELAGE UPPER LT EXTERNAL SKIN AT APPROX STA 1645 - 1652 AND JUST BELOW STRINGER 4L HAS 2 (EA) DENTS. (MARKED). MEASURED DENT NR 1 Y=.003, A=.780 A/Y=260.0. MEASURED DENT NR 2 Y=.003, A=.780 A/Y=260.0 DENTS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01,FIJan 11, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001110080Skin · dentedLWR FUSELAGE BS 399 BTW STRS 21 AND 22R SKIN DENTED. INSP FINDINGS MEASURED DENT Y=.012, A=.905 A/Y = 75.4. DENT FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL III. DENT LOCATED DIRECTLY UNDER FRAME LWR TEE CHORD. UPON FURTHER INVESTIGATION DETEJan 11, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090066Crease Beam · corrodedMCD LT CREASE BEAM FLOOR SUPPORT AND NUMEROUS DOME NUTS HAS CORROSION APPROX BETWEEN STA 900 TO STA 1040. R & R CREASE BEAM IAW SRM 51-40-02. CREASE BEAM OUT OF LIMITS IAW SRM 54-40-13 FIG 101, DETAIL VII, PAGE 104. INSTALLED NEW NUT PLATES IAW SRM 51-40-Jan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001090063Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA APPROX FS 1180 TO 1320, BTW S-16R TO S-20R SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG 101Jan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090062Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-20R APPROX FS 1327 HAS "2EA" SCRATCH DAMAGE AREAS IN ZONE "A" WHICH IS NOT PERMITTED THAT CROSS INTO ZONE "B". SKIN IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL IV. COMPLIED WITH EJan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090061Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA APPROX. F.S. 1340 TO 1360, BTW S-21R AND S-23R SKIN HAS SCRATCH DAMAGE AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG 101, DETAIL II. AFTER FURTHER EVALUATION, ABOVE NOTED AREA WJan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090060Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA APPROX FS 1280 TO 1300, BTW S-27L TO S-27R SKIN HAS SCRATCH DAMAGE AREA GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL II. AFTER FURTHER EVJan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090059Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA APPROX FS 1340 TO 1360, BTW S-21L AND S-25L SKIN HAS SEVERAL GOUGES AND SCRATCH DAMAGE AREA THAT IS GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101,Jan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090058Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-20L, APPROX FS 1327 HAS SCRATCH DAMAGE IN ZONE "B" WHICH IS OUT OF LIMITS IAW SRM 53-00- 01, FIG. 101, DETAIL IV. FILLET SEAL IS NOT PERMITTED TO COVER DAMAGE AREA. COMPLIED WITH EA F-533Jan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001090057Skin · damagedAFT WTB FAIRING EDGE SEALENT AREA APPROX FS 1180 TO 1320, BTW S-16L TO S-20L SKIN HAS SEVERAL GOUGES AND SCRATCH DAMAGE AREAS THAT ARE WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL II. AFTER FURTHER EVALUATJan 9, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080056Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 780 TO 860, BTW S-16R TO S-18R SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080055Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 760 TO 780, BTW S-19R TO S-18R SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101,Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080054Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-19R HAS SCRATCH DAMAGE IN ZONE "A" WHICH IS NOT PERMITTED THAT CROSS INTO ZONE "B". SKIN IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL IV.Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080053Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 750 TO 770, BTW S-19R TO S-26R SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101,Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080052Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-26R HAS SCRATCH DAMAGE IN ZONE "A" WHICH IS NOT PERMITTED THAT CROSS INTO ZONE "B". SKIN IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL IV.Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080051Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 768 TO 775, S-26L TO S-26R SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETJan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080050Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-26L HAS SEVERAL SCRATCHES AND GOUGE IN ZONE "B" WHICH IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL IV. FILLET SEAL IS NOT PERMITTED TO COVER THE DAMAGE AREA.Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080049Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 750 TO 770, BTW S-19L TO S-26L SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080048Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA AND LAP SEAM CROSS SECTION AREA AT S-19L SKIN HAS SEVERAL SCRATCHES IN ZONE "A" WHICH IS NOT PERMITTED THAT CROSS INTO ZONE "B". AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAIL IV.Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080047Skin · damagedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 760 TO 780, BTW S-19L TO S-18L HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101, DETAJan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080046Skin · gougedFWD WTB FAIRING EDGE SEALENT AREA APPROX FS 780 TO 860, BTW S-16L TO S-18L SKIN HAS MULTIPLE GOUGES AND SCRATCH DAMAGE AREAS THAT ARE GREATER THAN 10" IN LENGTH, AND IS WITHIN THE "20X" DAMAGE AREA OF FASTENER. AREA IS OUT OF LIMITS IAW SRM 53-00-01, FIG. 101Jan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, Plate/SkinSDR FDEA201001080045Crease Beam · corrodedRT CABIN CREASE BEAM BET STA 1380 AND 1400 HAS CORROSION. REMOVED DAMAGED SECTION IAW SRM 51-40-02. RECEIVED NEW SECTION IAW TRAV NR T10/815242, LOCATED/DRILLED IAW SRM 51-40-05. INSTALLED SECTION, IAW SRM 51-40-02, AND 51-20-05. CATEGORY "A", MAJOR REPAIRJan 8, 2010 · N914FD · Boeing 75728A · Fuselage Main, StructureSDR FDEA201001060024Frame · corrodedAFT PIT FUSELAGE FRAME STA 1480 HAS CORROSION FROM S-27R TO S-25R. REMOVED CORROSION IAW SRM 51-10-02. CHECKED LIMITS AND FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, FIG 101, DETAIL 3; L=.025",W=.025",D=.012", AT BS 1480, S25R-27R. FABRICATED REPAIR PARTS OJan 6, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA201001060020Seat Track · gougedCABIN SEAT TRACK STA 1180 TO 1225 RBL45.5 GOUGED ON CROWN. REMOVED CORROSION MATERIAL LOSS .030 AREA FOUND TO BE OUT OF LIMITS TAW SRM 53- 00-52 FIG. 101, DETAIL I REMOVED SEAT TRACK STA 1180 TO 1280 RBL 45.5 IAW SRM 51-40-02. FABRICATED NEW SEAT TRACK IAWJan 6, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001060019Seat Track · gougedUPPER CABIN FS 900 TO 1040 SEAT TRACK RBL 45.5 HAS NUMEROUS GOUGES, SCRATCHES AND AREAS OF CORROSION. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-50, FIG 101. REMOVED DAMAGED SEAT TRACK IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON TRAVELER NR T10/816705. LOCATED,Jan 6, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001060018Seat Track · corrodedNUMEROUS CORROSION FOUND ON SEAT TRACK FLANGE UPPER AND LWR SURFACES AT FASTENER HOLES FROM STA 680 TO STA 780 AT LBL 46. REMOVED DAMAGED SEAT TRACK, WAS OUT OF LIMITS, IAW SRM 53-00-52, IAW SRM 51-40-02. RECIVED NEW SEAT TRACK PER TRAV T10/817022. INSTALLEJan 6, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001060017Seat Track · gougedNUMEROUS GOUGES FOUND ON SEAT TRACK BETWEEN STA 440 TO 480 AT LBL 25. REMOVED GOUGES AND FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02, 53-00-52. FABBED REPLACEMENT SEAT TRACK MAE TRAV NR T10/816680. INSTALLED SEAT TRACK STA 440-680, LBL 25, IAW SRM 51-40-02. Jan 6, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001050016Frame · damagedFUSELAGE FRAME UPPER EXPOSED FLANGE HAS TOOL MARK DAMAGE "DRILL MARK", FRAME STA 1640, BTW S-26L AND 27L. DAMAGED FRAME FLANGE STA 1640, BTW S-26L AND S-27L FOUND TO BE OUT OF LIMITS IAW SRM 53-00-07, PG 103, FIG. 101, DETAIL II. ORIG MAT .063, MAT. LOSS .020Jan 5, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA201001050015Frame · corrodedFUSELAGE FRAME UPPER CHORD HAS CORROSION STA 1640, S-22L. AFTER FURTHER EVALUATION IAW DWG NR 146N1023 FRAME THICKNESS IS .080, AFTER BLEND OUT FOR CORROSION REMOVAL, MAT REMAIN IS .077, FRAME IS WITHIN LIMITS IAW SRM 53-00-07 FIG. 101 DET. 2 AND IS A MINOR RJan 5, 2010 · N914FD · Boeing 75728A · Fuselage Main, FrameSDR FDEA201001040007Seat Track · damagedUPPER CABIN SEAT TRACK FS 1320-1540 RBL 45.5 HAS SCRATCHES AND TOOL MARKS WITH CORROSION IN NUMEROUS AREAS. BLEND OUT SCRATCHES, TOOL MARKS AND CLEAN UP CORRODED AREAS PREVIOUSLY MARKED ON TOP FLANGE SURFACES OF SEAT TRACK, FOUND 3 EA SPOTS OUT OF LIMITS STAJan 4, 2010 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201001020001Support Angle · corrodedCABIN RH FLOOR CREASE BEAM SUPPORT ANGLE STA 1610 HAS COROSION . REMOVED CREASE BEAM IAW SRM 51-40-02. FABRICATED NEW CREASE BEAM IAW SRM 51-40-05. INSTALLED NEW CREASE BEAM STA 1610, IAW SRM 51-40-02. CATEGORY "A". MAJOR REPAIR.Jan 2, 2010 · N914FD · Boeing 75728A · Fuselage Miscellaneous StructureSDR FDEA200912314574Seat Track · scratchedUPPER CABIN RT SIDE FS 843 TO 823 SEAT TRACK 24.75 HAS SCRATCHES. REMOVED SCRATCHES ON SEAT TRACK STA 823 TO 843 RBL24.75 IAW SRM 53-00-52. MAX CLEAN UP 0.020 AT STA 823 MAT LOSS .025 AT STA 843 MAT LOSS .029 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REDec 31, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912314573Seat Track · gougedNUMEROUS GOUGES FOUND ON SEAT TRACK FROM STA 1120 TO STA 1180 AT LBL 25. FOUND OUT OF LIMITS IAW SRM 53-00-52 FIG. 101, DET I, PG 102. R & R SEAT TRACK IAW SRM 51-40-02 CLASSIFIED AS MAJOR REPAIRDec 31, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912304568Seat Track · corrodedUPPER CABIN FS 900 TO 1040R SEAT TRACK RBL 24.75 HAS AREAS OF SCRATCHES GOUGES AND AREAS OF CORROSION. R & R SEAT TRACK IAW SRM 51-40-02 / 51-20-05. GOUGES AND CORROSION WERE OUT OF LIMITS IAW SRM 53-00-52, FIG. 101. NEW SEAT TRACK FABRICATED ON SHOP TRAVELEDec 30, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912304567Seat Track · damagedUPPER CABIN SEAT TRACK RBL 45.5 FS 680 TO 730 HAS TOOL MARKS AND SCRATCHES. REMOVED AND REPLACED SEAT TRACK AT RBL 45.5 FS 640 TO 780 IAW SRM 51-40-02. REPAIR CLASSIFIED AS MAJOR.Dec 30, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912304565Seat Track · corrodedNUMEROUS CORROSION FOUND ON SEAT TRACK FLANGE UPPER AND LWR SURFACES FROM STA 680 TO STA 780 AT LBL 25. REMOVED CORROSION AND CHECKED LIMITS FO SEAT TRACK IAW SRM 53-00-52 / 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. BEFORE REWORK; .145"/AFTER REWODec 30, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200912304564Seat Track · corrodedSEAT TRACK HAS GOUGES AND CORROSION FROM STA 820 TO 839 AT LBL 25. REMOVED GOUGES & CORROSION FROM MCD SEAT TRACK STA 820-839, LBL 25 IAW SRM 51-10-02. ORIG MAT THICKNESS= .145, MAT LOSS .045. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101, DETAIL I, PG Dec 30, 2009 · N914FD · Boeing 75728A · Fuselage, Seat/Cargo Attach Fittings
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