N653FE

Service difficulty reports · 221

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 = 'N653FE' 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 FDEA201112145260Splice · dentedMAIN DECK CARGO RT FRAME 22 AT L8-9R BRACKET SPLICE FOUND DENTED. DENTED BRACKET REMOVED AS PER SRM 51-40-21 REVISION 21. FABRICATED AS PER DWG A5377090321000 ISSUE "E" AND INSTALLED AS PER SRM 51-40-21 REVISION 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 Dec 14, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201112135253Fitting · damagedFOUND EXTERNAL COUPLING DAMAGED. CARRIED OUT REPAIR IAW EA 6-5310-155852, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Dec 13, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201112085214Crossbeam · misrepairedCROSSBEAM MISREPAIRED AT FRAME 66 APPROX Y=960. REPAIRED IAW SRM 53-10-15, FIG 211, REV 21 AND EO E6-5100-7-5000D PT1.Dec 8, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201112055158Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR 131PG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6Dec 5, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201112055157Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR 132SG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-Dec 5, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201112055156Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR 132LG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM Dec 5, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201112045147Floor Panel · damagedFORWARD CARGO COMPARTMENT FLOOR PANEL NR 132NG FOUND DAMAGED. DAMAGED FLOOR PANEL REMOVED IAW AMM 53-10-29-04, REV 52.0. NEW FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J AND INSTALLED IAW AMM 53-10-29-04, REV 52.1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-Dec 4, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201112045142Skin · crackedRIGHT WING L/E PANEL NR 613AB CUT-OUT FOUND CRACKED. CARRIED OUT REPAIR IAW SRM 53-15-63, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Dec 4, 2011 · N653FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201111305089Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 4.5 INCHES FROM FRAME 1 AND 10.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT IAW SRM 51-40-41 REVISION 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111305087Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH A LIGHTNING STRIKE APPROX.4.5 INCHES FROM FRAME 1 AND 10.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT IAW SRM 51-40-41, REVISION 2. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111305086Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 1.75 INCHES FROM FRAME 1 AND 10.0 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED OUT ON FASTENER HOLE IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111305085Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE FROM FRAME 1 AND 9.0 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111305084Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE APPROX 2.75 INCHES FROM FRAME 0 AND 8.5 INCHES FROM BOTTOM CENTER LINE. REPAIR CARRIED IAW SRM 51-40-41, REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111305083Skin · damagedLOWER FORWARD FUSELAGE RT LOWER SKIN FOUND WITH LIGHTNING STRIKE. REPAIR CARRIED OUT IAW SRM 51-40-41 REV 21. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 113.Nov 30, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201111295071Floor Panel · damagedAFT CARGO BAY FLOOR PANEL NR 152XF FOUND DAMAGED. R & R IAW AMM 53-10-33-04, REV 52.1. FLOOR PANEL FABRICATED IAW DG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 29, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111295072Floor Panel · corrodedCARGO BAY FLOOR PANEL NR 162EF FOUND LOWER SURFACE CORRODED. R & R IAW AMM 53-10-35-04, REV 52.1. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REVISION J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 29, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111295070Floor Panel · damagedAFT CARGO BAY FLOOR PANEL NR 152WF FOUND DAMAGED. R & R IAW AMM 53-10-33-04 REV 52.1. FLOOR PANEL FABRICATED IAW DWG SRZ-25-005, REV J. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 29, 2011 · N653FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201111255044Floorbeam · crackedFOUND AT MAIN DECK FLOORBEAM AT FR 28 APPROX - Y= 700 CRACKED. CARRIED OUT REPAIR IAW EA 6-5310-155850& EO 6-5100-7-5000D-PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255027Cargo Track · corrodedMAIN DECK CARGO TRACK CROWN AREA AT FR66, Y = 17.5 FOUND CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-16, FIG 201, REV 21 BETWEEN FRAME 65.6 TO FRAME 67.5. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255046Floorbeam · crackedFOUND MAIN DECK FLOORBEAM AT FRAME 29 APPROX Y=700 CRACKED. CARRIED OUT REPAIR IAW EA 6-5310-155850 & EO E6-5100-7-5000D-PT1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255045Floorbeam · crackedFOUND AT MAIN DECK FLOORBEAM AT FR 30 APPROX - Y = 700 CRACKED. CARRIED OUT REPAIR IAW EA NR 6-5310-155850 & EO E6-5100-7-5000D-PT1 . REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255043Frame · damagedAFTER THE REMOVAL OF REPAIR SPLICE AT RT FRAME 22 L8-9, FOUND UNDERLYING STRUCTURAL DAMAGE. DAMAGED FRAME REMOVED IAW SRM 51-40-21, REV 21. FABRICATED IAW DWG A5377169420300, ISSUE B AND INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSFIED MAJOR IAW GMM 6-2-Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201111255042Frame · damagedAFTER THE REMOVAL OF REPAIR SPLICE AT FRAME 23 L8-9, FOUND UNDERLYING STRUCTURE DAMAGE. DAMAGED FRAME REMOVED IAW SRM 51-40-21, REV 21. FABRICATED IAW DWG A53770911200 ISSUE B AND INSTALLED IAW SRM 51-40-21, REV 21. REPAIR CLASSFIED MAJOR IAW GMM 6-2-100, RNov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201111255040Seat Track · wornSEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 5 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.020IN). REPAIR CARRIED OUT IAW 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255038Seat Track · wornSEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 2 RT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.026IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255036Seat Track · wornSEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 3 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.019IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255035Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 32, LBL 67 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 53-10-15, FIG 212, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255032Seat Track · wornSEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 4 LT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.027IN). REPAIR CARRIED OUT IAW SRM 53-15-16, FIG 201, REV 21. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255031Seat Track · wornSEAT TRACKS AND DUMMY SEAT TRACK ATTACHMENT FITTING NR 6 RT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.032IN). REPAIR CARRIED OUT IAW 53-15-16 FIG 201, REV 21 REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201111255033Floorbeam · crackedMAIN DECK FLOORBEAM AT FR 67, LBL 63 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG 211 REV 21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255030Floorbeam · crackedMAIN DECK FLOORBEAM AT FR64, RBL 65 FOUND CRACKED. REPAIR CARRIED OUT AS PER SRM 53-10-15 FIG.211 REV21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201111255041Attach Fitting · wornSEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 2, RT AT FR 38.2 TO FR 40 FOUND WORN AND OUT OF GAP VALUE (0.020 INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111255039Attach Fitting · wornSEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 5 RT AT FR 38.2 TO FR 40. FOUND WORN AND OUT OF GAP VALUE (0.022 INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111255037Attach Fitting · wornSEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 2 LT AT FR 54 TO FR 54.2. FOUND WORN AND OUT OF GAP VALUE (0.031INCH). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111255034Attach Fitting · wornSEAT AND DUMMY TRACK ATTACHMENT FITTINGS NR 3 RT AT FRAME 38.2 TO FRAME 40 FOUND WORN AND OUT OF GAP VALUE (0.022IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG 201 REV.21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111255029Attach Fitting · wornSEAT AND DUMMY TRACK ATTACH FITTING NR 6 LT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.020IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG. 201 REV. 21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111255026Attach Fitting · wornSEAT AND DUMMY TRACK ATTACH FITTING NR 5 LT AT FRAME 54 TO FRAME 54.2 FOUND WORN AND OUT OF GAP VALUE (0.023IN). REPAIR CARRIED OUT AS PER SRM 53-15-16 FIG.201 REV.21 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISION 113.Nov 25, 2011 · N653FE · Airbus A300F4605R · Fuselage Main, Attach FittingsSDR FDEA201111235008Structure · damagedLEFT INBD FLAP, 5 INCHES FROM INBD EDGE FOUND LOWER SURFACE DRAIN HOLE ELONGATED. CARRIED OUT REPAIR IAW EA NR 6- 5750-155851, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 113.Nov 23, 2011 · N653FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201110074371Battery · dischargedR1 DOOR NO ECAM SLIDE LIGHT WHEN DOOR IS ARMED. R & R ASPSU BATTERY'S 1 AND 2 REF AMM 52-73-18-04. SYS TEST'S GOOD. ACFT OK FOR SERVICE. R & R ASPSU BATTERY'S 1 AND 2 REF AMM 52-73-18-04. SYS TEST'S GOOD. ACFT OK FOR SERVICE. FINAL CLOSED.Oct 7, 2011 · N653FE · Airbus A300F4605R · Escape SlideSDR FDEA201108233433Cylinder · gougedLT MLG ACTUATING CYLINDER GOUGED ON UPPER BODY. REMOVED LT MLG ACTUATING CYLINDER AND INSTALLED SERVICEABLE CYLINDER PN C23129004-4 ON 32T0007.Aug 23, 2011 · N653FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201106072140Light · no testDURING SERVICE CHECK EMERGENCY LIGHTS DID NOT TEST PROPERLY FROM SWITCH AT DOOR 1L. RED LIGHT ON POWER SUPPLY UNIT ILLUMINATED WHEN TEST BUTTON PUSHED. COMPLIED WITH EPSU OPS CHECK IAW MM 33-50-00-00. OPS CHECKED OK. NO FAULTS NOTED. GREEN LIGHT ILLUMINATEJun 7, 2011 · N653FE · Airbus A300F4605R · Emergency LightingSDR FDEA201104171510Tire · failedNR 4 TIRE BLEW ON LANDING, REPLACED TIRE.Apr 17, 2011 · N653FE · Airbus A300F4605R · TireSDR FDEA201102220675Coalescer Bag · odorAFTER LANDING AT APPROX 60KTS, GOT A SMOKE INDICATIONS IN THE EQUIPMENT BAY FOLLOWED BY MAIN DECK SMOKE INDICATIONS. THERE WAS SMOKE IN THE COCKPIT. R & R NR 1 AND NR 2 PACK COALESCER SOCKS IAW MM 21-51-16-03. R & R AVIONICS COOLING FILTER IAW MM 21-21-1Feb 22, 2011 · N653FE · Airbus A300F4605R · Humidity Control SystemSDR FDEA200907082540Web · crackedRT WING NR 1 SLAT VERTICAL WEB AT RIB 24 HAS A 0.30 INCH CRACK. REMOVED DAMAGED VERTICAL WEB, FABRICATED REPLACEMENT WEB AND INSTALLED ON NR 1 SLAT RIB 24 IAW DWG A57863063 AND A300-600 SRM 57-42-11 AND SRM 51-72-10.Jul 8, 2009 · N653FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA200904241399Duct · contaminatedSMOKE IN COCKPIT ON GROUND AFTER AIR COND PACK TURNED ON. ACFT RELEASED FOR SERVICE PER MEL/CDL: 49-10-01. SMOKE WAS NOTED DURING FIRST PACK OPERATION FOLLOWING COMPRESSOR WASH OF THE NR 2 ENGINE, SUSPECT WATER FROM WASH IN BLEED DUCT. OPERATED APU PER JRHApr 24, 2009 · N653FE · Airbus A300F4605R · APU Bleed Air SystemSDR FDEA200901070067Unknown · odorON FINAL 1500' AGL, MASTER CAUTION EQUIP BAY SMOKE INDICATION. DECLARED EMERGENCY RAN ECAM & LANDED. INDICATION WENT AWAY SHORTLY INTO PROCEDURE & NO SMOKE SEEN OR SMELLED. INSPECTED E/E BAY & NO EVIDENCE OF SMOKE OR FUMES. 12WA REPLACED. FOUND NO EVIDENCEJan 7, 2009 · N653FE · Airbus A300F4605R · Air Distribution SystemSDR 07FDEA03008Skin · crackedRT WING LOWER SKIN CRACKED AT T/E ACCESS PANEL 675FB CUTOUT. FORWARD O/B CORNER AREA TOTAL CRACKED LENGTH 1.25 APPROX REF A300-600 SRM 51-10-00. COMPLIED WITH EA 6-5730-110509 REF SB'S A300-600 57-6064 AND 57-6029 DWG R57340199, SMALL REPAIR PLATE.Aug 21, 2007 · N653FE · Airbus A300F4605R · Wing, Plate/SkinSDR 07FDEA03007Spar · crackedA 1.5 INCH CRACK EXIST AT LT WING REAR SPAR BETWEEN RIBS 8/9 ACCESS PROVISIONS THROUGH PNL 575FB REF 57-00-00-6 ZONE 500. INSTALLED S/B NR A300-57-6064 DOUBLERS AT RIB NR 9 AFT OF REAR SPAR (REINFORCEMENT DOUBLERS) COMPLIED WITH EA 6-5730-110509.Aug 21, 2007 · N653FE · Airbus A300F4605R · Wing SparSDR 07FDEA02884Floorbeam · crackedLATE FIND FLOORBEAM FR 30 BETWEEN SEAT TRACK NR 2L AND 3L HAS A .5 INCH CRACK AT STIFFENER. CUT OUT DAMAGED SECTION OF FLOORBEAM IAW A300-600 FREIGHTER SRM 53-10-15. FABRAICATED AND INSTALLED REPAIR ANGLE AND FILLER IAW A300-600 FREIGHTER SRM 53-10-15. ALODAug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR 07FDEA02883Frame · gougedMDCC AT FR 22 BETWEEN STG 17R AND STG 9R HAS 7 GOUGES APPROX 4" ZONE 230 REF A300-600 SRM 51-10-00. BLENDED 7 GOUGES FR 22 BETWEEN STR 7 AND 17R IAW A300-600 SRM 51-73-10 1EA AREA OUT OF LIMITS IAW A300 SRM 53-10-00 PG 101 B=.063 A=.046 L=.017. FABRICATED ANAug 14, 2007 · N653FE · Airbus A300F4605R · Fuselage Main, Frame
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