N918FD

Service difficulty reports · 190

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 = 'N918FD' 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 FDEA200902090485Skin · damagedWS 776.5, RT WING LOWER SKIN, HAS A .185 INCH DIAMETER MIS-DRILLED HOLE IN THE -466 SKIN PANEL. REPAIRED DAMAGED AREA, WS 776.5, RT LOWER SKIN, IAW EA 757-5724-16-A1813 AND EA F- 5724-124060, DOUBLER REPAIR. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REFeb 9, 2009 · N918FD · Boeing 75723A · Wing, Plate/SkinSDR FDEA200902040456Frame · dentedAFT CARGO COMPARTMENT FRAME AT STA 1220 STR 26R HAS DENT. REPAIRED FRAME IAW EA NR F-5310-124030 AND EA 757-5342-16-F1807. THIS REPAIR IS CATEGORY "A" MAJOR REPAIR.Feb 4, 2009 · N918FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200902040455Fitting · wornL-2 DOOR TOP DOOR STOP HOUSING AFT SIDE HAS WORN SPOT FROM CHAFING. BLENDED L2 DOOR TOP STOP FITTING, AFT SIDE, FOUND TO BE OUT OF LIMITS IAW SRM 52-10-02 FIG 101 DET. XI. REMOVED DOOR STOP FTG IAW SRM 51-40-02. FABRICATED NEW DOOR STOP FITTING. INSTALLFeb 4, 2009 · N918FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA200901280348Skin · crackedL4 DOOR INNER SKIN IS CRACKED, JUST BELOW HANDLE PAN. REPAIR ACCOMPLISHED IAW FEDEX EA F-5210-123960 AT L4 DOOR INNER SKIN. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.Jan 28, 2009 · N918FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA200901270328Web · crackedR1 DOOR INNER WEB CRACKED, FWD SIDE, BELOW HANDLE. COMPLIED WITH MAE EA 757-5211-16-A1817, EA F-5210-124059, ON THE R1 DOOR, BS 332.05, AT BEAM NR 3. THIS DOUBLER REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.Jan 27, 2009 · N918FD · Boeing 75723A · Passenger/Crew DoorsSDR FDEA200901230313Floorbeam · damagedEXISTING FLOORBEAM REPAIR AT BS 1640, LBL 52, WL 208, UPON EVALUATION OF EO F-5100-7-5001, PART 1, ATTACHMENT "B", DOES NOT MEET SRM REQUIREMENTS AND INTERFERES WITH PTF MODIFICATION. PERMANENT FLOORBEAM CAT "A" MAJOR REPAIRS ACCOMPLISHED PER MAE EA'S 757-536Jan 23, 2009 · N918FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200812175194Stringer · corrodedMAIN EQUIPMENT CENTER, ZONE 119, STA 420, S23L HAS CORROSION. REMOVED AND FABRICATED NEW STRINGER SECTION ON MAE TRAVELER NR T8/759394, DRILLED, TREATED, PRIMED AND INSTALLED NEW STRINGER SECTION ON S23L BETWEEN STA 395 TO 436 IAW SRM 51-40-02, SRM 53-00-03, Dec 17, 2008 · N918FD · Boeing 75723A · Fuselage Main, Longeron/StringerSDR FDEA200812035072Shear Web · corrodedBS 1020, RBL 65, CREASE BEAM WEB IS CORRODED. REMOVED CORROSION, BS 1020, RBL 65, ON CREASE BEAM WEB IAW SRM 51-10-02 AND FOUND TO BE OUT OF LIMITS IAW SRM 53-60-13. L=.50, W=.50, D=.015. FABRICATED NEW WEB ON MAE TRAVELER T8/759905, TREATED, PRIMED WEB IAW Dec 3, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200812025046Floor Support · corrodedCABIN FLOOR, BS 310-324, RBL 43, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT/CHANNEL IAW SRM 51-40-02. FABRICATED NEW SUPPORT/CHANNEL ON MAE TRAVELER T8/759071. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IAW SRM 51-20-01 AND AMM Dec 2, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200812025044Floor Support · corrodedCABIN FLOOR, BS 297-310.5, RBL 30, CHANNEL CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT, BS 301-310.5, RBL 30, IAW SRM 51-40-02. FABRICATED NEW FLOOR SUPPORT (CHANNEL) ON MAE TRAVELER T8/759040. TREATED, PRIMED AND TOP COATED NEW SUPPORT/CHANNEL IADec 2, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200812025042Floor Support · corrodedCABIN FLOOR, BS 297, RBL 20-36.2, CHANNEL IS CORRODED AROUND FASTENER HOLES. REMOVED FLOOR SUPPORT AT BS 297, RBL 20-36.2, IAW SRM 51-40-02. FABRICATED NEW SUPPORT ON MAE TRAVELER T8/759390. TREATED, PRIMED AND TOP COATED SUPPORT IAW SRM 51-20-01 AND AMM 51Dec 2, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200811184916Floorbeam · corrodedAFT CARGO COMPT, FLOORBEAM 1360, AT S-26L, IS CORRODED AND GOUGED. REPAIRED FLOORBEAM IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT. "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP REQUIREMENTS: INITIAL AT 37,500 FC; THEREAFTER EVERY 12,0Nov 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, Floor BeamSDR 08FDEA04918Skin · damagedPREVIOUSLY INSTALLED REPAIR, WS 823, WBL 740, TANK INTERNAL, RT WING, LOWER SURFACE, IDENTIFIED AS A TIME-LIMITED REPAIR. COMPLY WITH ATTACHMENT "B" OF EO F-5100-7-5100, PART 1. COMPLIED WITH ATTACHMENT "B" OF EO F-5100-7-5001, PART 1. REPLACED RT WING, LNov 18, 2008 · N918FD · Boeing 75723A · Wing, Plate/SkinSDR 08FDEA04916Frame · corrodedAFT CARGO COMPT, FRAME 1360, AT S-26L, IS CORRODED AND GOUGED. REPAIRED FRAME, AFT CARGO COMPT, BS 1360, AT S-26L, IAW SRM 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP REQUIREMENTS, INITIAL AT 37Nov 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200811114855Frame · gougedAFT CARGO COMPT, BS 1480, S-23R - S-24R, BEAM HAS DEEP GOUGES. REPAIRED FRAME AFT CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,5Nov 11, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04855Frame · damagedAFT CARGO COMPT, BS 1480, S-23R - S-24R, BEAM HAS DEEP GOUGES. REPAIRED FRAME/BEAM, BS 1480, S-23R - S-24R, AFT CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5, DETAIL 3. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKINov 11, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200811104839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 EA NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIA AT APPROX PPS 132 AND 1 EA HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 EA HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH EA F-5450-124034 ANDNov 10, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811104838Skin · damagedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR1 PYLON SIP MOD F-5450-7-5003 A4 PT.5 1 EA. HOLE WAS OVERSIZED TO 0.390 DIA. AND COUNTERSUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH EA F-5450-124034, 11/07/08 AND REPAIRED OVERSIZED HONov 10, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04839Skin · damagedWHILE DRILLING THE 311N5046-31 NR 1 PYLON OTBD SKIN 2 NUTPLATE ATTACH HOLES WERE OVERSIZED TO .250 DIAMETER AT APPROX PPS 132 AND 1 HOLE WAS ELONGATED AT APPROX PPS 205.65 AND 2 HOLES DAMAGED IN LOWER CHORD AT PPS 174.30. COMPLIED WITH FED EX EA NR F-5450-124Nov 10, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04838Skin · misrepairedWHILE REAMING THE -31 OTBD SKIN AND OTBD BATHTUB FITTING FOR THE NR 1 PYLON SIP MOD F- 5450-7-5003 A4 PT.5 1 HOLE WAS OVERSIZED TO 0.390 DIA AND COUNTERUNK FOR A BACB30NW12K(*) X FASTENER. COMPLIED WITH FEDEX EA NR F-5450-124034 11/07/08 AND REPAIRED OVERSIZNov 10, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811094822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APROX AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL PN 311N5046-33 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811094821Skin · corrodedNR1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCES PANEL 433CL REMOVED AND REPLACED WITH NEW SKIN PN 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811094820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON . REMOVED AND REPLACED NEW SKIN PN 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04822Skin · corrodedNR 2 NACELLE STRUT INTERNAL, INBD SKIN EXFOLIATED AT PP STA 166 APPROXIMATELY AND HAS CORROSION FROM PP STA 174-100 AT ACCESS DOORS CUT-OUTS. REMOVED AND REPLACED WITH A NEW SKIN PANEL P/N 311N5046-33 "A" MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04821Skin · corrodedNR 1 STRUT OTBD SIDE SKIN CORRODED INSIDE ACCESS PANEL 433CL. REMOVED AND REPLACED WITH NEW SKIN P/N 311N5046-31 IAW SRM 51-40-02 AND DWG 311N5002, "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04820Skin · corrodedNR 2 NACELLE STRUT, OTBD INTERNAL SKIN HAVE CORRODED SPOTS ALONG PYLON. REMOVED AND REPLACED NEW SKIN P/N 311N5446-32 "A" MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Nov 9, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811084814Skin · corrodedNR1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. R & R INBD SIDE SKIN PANEL ASSY. IAW DWG N311N5002 AND SRM 51-40-02. OLD CONTROL NR: 08FDEA04814Nov 8, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR 08FDEA04814Skin · corrodedNR 1 STRUT CORROSION ON INNER AFT SKIN INBD SIDE. REMOVED AND REPLACED INBD SIDE SKIN PANEL ASS'Y IAW DRAWING N311N5002 AND SRM 51-40-02.Nov 8, 2008 · N918FD · Boeing 75723A · Nacelle/Pylon, Plate/SkinSDR FDEA200811064773Support Channel · corrodedFWD MAIN CABIN LT- INTERCOSTAL PLATE ABOVE FLIGHT CONTROL PULLEYS AT LBL 24.75 BAE STA 333.45 AND STA 350.00 IS CORRODED . REMOVED AND REPLACED FLOOR SUPPORT PN 141N5170-30 IAW SRM 51-40-02 FROM STA 324.0 - 345.0 LBL 24.75 "A" MAJOR REPAIR NO FOLLOW-UP REQUIRENov 6, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR 08FDEA04773Floor Support · corrodedFWD MAIN CABIN LT, INTERCOSTAL PLATE ABOVE FLIGHT CONTROL PULLEYS AT LBL 24.75 BS 333.45 AND STA 350.00 IS CORRODED. REMOVED AND REPLACED FLOOR SUPPORT P/N 141N5170-30 IAW SRM 51-40-02 FROM STA 324.0 - 345.0 LBL 24.75 "A" MAJOR REPAIR NO FOLLOW-UP REQUIRED.Nov 6, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200810314649Frame · dentedFWD CARGO PIT, BS 720, AT S-23L, FRAME IS DENTED ON TOP SIDE. REPAIRED FRAME IAW SRM 53-00-07, REPAIR NR 5. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOOct 31, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04649Frame · dentedFWD CARGO PIT, BS 720, AT S-23L, FRAME IS DENTED ON TOP SIDE. REPAIRED BS 720 FRAME AT S-23L, IAW SRM 53-00-07, REPAIR NR 5. REPAIR PARTS FABRICATED ON MAE TRAVELER T8/763002 AND INSTALLED IAW SRM 51-40-02 AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIEDOct 31, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810304620Frame · dentedFWD CARGO BAY BS 760, STR -24L FRAME UPPER J-ANGLE DENTED. REPAIRED FRAME STA 760, STR -24L IAW SRM 53-00-07, 51-40-02. NOTE: SUBSEQUENCT INSPECTIONS ARE REQUIRED IAW SRM 53-00-07, PAGE 208, REPAIR 5, DETAIL III AND PAGE 210, TABLE II . THIS IS A CLASS "B" ROct 30, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810304639Frame · corrodedAFT CARGO COMPT, BS 1320, S26L, IS CORRODED. REPAIRED FRAME IAW SRM 53-00-07, REPAIR NR 5. INSTALLED REPAIR IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITIAL AT 37,500 FC FROMOct 30, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810304638Frame · dentedFWD CARGO COMPT., BS 760, S-24L, FRAME UPPER J-ANGLE IS DENTED. REPAIRED FRAME, BS 760, S-24L, FWD CARGO COMPT, IAW SRM 53-00-07, REPAIR 5. INSTALLED REPAIR PARTS IAW SRM 51-40-02. THIS REPAIR I CLASSIFIED AS A CATEGORY 'B" MAJOR REPAIR WITH THE FOLLOWING FOLLOct 30, 2008 · N918FD · Boeing 757236 · Fuselage Main, FrameSDR 08FDEA04639Frame · corrodedAFT CARGO COMPT, BS 1320, S-26L, IS CORRODED. REPAIRED FRAME, BS 1320, S-26R, IAW SRM 53-00-07, REPAIR NR 5. INSTALLED REPAIR IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CATEGORY "B" MAJOR REPAIR WITH THE FOLLOWING FOLLOW UP TRACKING REQUIREMENTS: INITOct 30, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04638Frame · dentedFWD CARGO COMPT, BS 760, S-24L, FRAME UPPER J-ANGLE IS DENTED. REPAIRED FRAME, BS 760, S-24L, FWD CARGO COMPT, IAW SRM 53-00-07, REPAIR NR 5. INSTALLED REPAIR PARTS IAW SRM 51-40-02. THIS REPAIR I CLASSIFIED AS A CATEGORY 'B" MAJOR REPAIR WITH THE FOLLOWIOct 30, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR 08FDEA04620Frame · dentedFWD CARGO PIT STA 760 STR -24L FRAME UPPER J ANGLE DENTED. REPAIRED FRAME STA 760 STR -24L IAW SRM 53-00-07,51-40-02. SUBSEQUENT INSPECTIONS ARE REQUIRED PER SRM 53-00-07, PAGE 208, REPAIR 5, DETAIL III AND PAGE 210, TABLE II. THIS IS A CLASS "B" REPAIR WITOct 30, 2008 · N918FD · Boeing 75723A · Fuselage Main, FrameSDR FDEA200810224475Seat Track · damagedMAIN CABIN SEAT TRACK, BS 1540-1640, LBL 45, I/B FLANGE HAS SEVERAL MIS-DRILLED HOLES. REMOVED AND REPLACED SEAT TRACK ASSY, IAW SRM 51-40-02. REPLACEMENT SEAT TRACK WAS DRILLED UP AND SCALLOPED ON MAE TRAVELER NR T8/758323.Oct 22, 2008 · N918FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR FDEA200810224474Channel · gougedRT UPPER LOBE, INTERNAL, BS 1280, RBL 60, FRAME AT S-10R, FWD SIDE IS GOUGED. CUT OUT DAMAGED AREA IAW SRM 53-00-07, REPAIR AT 1. FABRICATED CHANNEL, LOCATED AND DRILLED IAW SRM 51-40-05, 53-00-07, REPAIR NR 1. INSTALLED FABRICATED CHANNEL IAW SRM 51-40-02 AOct 22, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR 08FDEA04477Seat Track · corrodedMAIN CABIN SEAT TRACK, BS 377.7-440, LBL 45, HAS CORROSION AND SCRATCHES. REMOVED SEAT TRACK ASSY AT CUSTOMER REQUEST IAW SRM 51-40-02. REPLACEMENT SEAT TRACK WAS DRILLED UP AND SCALLOPED ON MAE TRAVELER NR T8/760225. INSTALLED REPLACEMENT SEAT TRACK ASSY, Oct 22, 2008 · N918FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04475Seat Track · damagedMAIN CABIN SEAT TRACK, BS 1540-1640, LBL 45, I/B FLANGE HAS SEVERAL MIS-DRILLED HOLES. REMOVED AND REPLACED SEAT TRACK ASSY, BS 1540-1640, LBL 45, IAW SRM 51-40-02. REPLACEMENT SEAT TRACK WAS DRILLED UP AND SCALLOPED ON MAE TRAVELER NR T8/758323.Oct 22, 2008 · N918FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04474Channel · gougedRT UPPER LOBE, INTERNAL, BS 1280, RBL 60, FRAME AT S-10R, FWD SIDE IS GOUGED. CUT OUT DAMAGED AREA IAW SRM 53-00-07, REPAIR NR 1. FABRICATED CHANNEL ON MAE TRAVELER NR T8/763184, LOCATED AN DRILLED IAW SRM 51-40-05, 53-00-07, REPAIR NR 1. INSTALLED FABRICATOct 22, 2008 · N918FD · Boeing 75723A · Fuselage Miscellaneous StructureSDR FDEA200810184427Floorbeam · damagedMAIN CABIN FLOORBEAM, STA 1620 LBL25-45 HAS MISDRILLED SCREW HOLES. REPAIRED FLOORBEAM IAW SRM 53-00-51 REPAIR NR 1 FIG 201 AND SRM 51-40-02. MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, Floor BeamSDR FDEA200810184425Window Frame · damagedLIGHTNING STRIKE, LT CABIN WINDOW CUT OUT BS 395- BS 418. REPAIRED LIGHTNING STRIKE IAW SRM 56-20-02 REPAIR NR 1 FIGURE 201 SHT-3 MAJOR REPAIR NO FOLLOW-UP INSP REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, StructureSDR FDEA200810184424Panel · crackedNR 2 L/E SLAT COVE PANEL, INBD OF OTBD MAIN TRACK IS CRACKED. REMOVED AND REPLACED COVE PANEL IAW SRM 51-40-02 AND DRAWG NR 114N4076.Oct 18, 2008 · N918FD · Boeing 75723A · Leading Edge DevicesSDR FDEA200810184426Seat Track · corrodedMAIN CABIN, SEAT TRACK BS 377.7- BS 440 LBL 24.75 CROWN HAS CORROSION AND GOUGES. REMOVED AND REPACED SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIR NO FOLLOW-UP, INSP REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04427Floorbeam · damagedMAIN CABIN FLOORBEAM, STA 1620 LBL25-45 HAS MISDRILLED SCREW HOLES. REPAIRED FLOORBEAM IAW SRM 53-00-51 REPAIR NR 1 FIG 201 AND SRM 51-40-02 MAJOR REPAIR NO FOLLOW-UP INSPECTION REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, Floor BeamSDR 08FDEA04426Seat Track · corrodedMAIN CABIN, SEAT TRACK BS 377.7- BS 440 LBL 24.75 CROWN HAS CORROSION AND GOUGES. REMOVED AND REPLACED SEAT TRACK IAW SRM 51-40-02 MAJOR REPAIR, NO FOLLOW-UP INSPECTION REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA04425Window Frame · damagedLIGHTNING STRIKE, LT CABIN WINDOW CUT OUT BS 395- BS 418. REPAIRED LIGHTNING STRIKE IAW SRM 56-20-02 REPAIR NR 1 FIGURE 201 SHT, 3 MAJOR REPAIR. NO FOLLOW-UP INSPECTION REQUIRED.Oct 18, 2008 · N918FD · Boeing 75723A · Fuselage Main, Structure
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