N671FE

Service difficulty reports · 189

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 = 'N671FE' 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 FDEA202410091666Fitting · crackedREMOVE MAIN CARGO DOOR ACTUATOR YOKE FOUND FR23 FRAME FITTING CRACK. I.A.W A300-600 AMM 52-36-27-04 REPLACED MAIN CARGO DOOR ACTUATOR YOKE AT FR23, LONGN 1~3 & FEDEX EO NO: E6-5230-E0378588 A P5, SEQ NO:1229, TITLE: DOORS- CARGO DOOR/HYD SYS- DETAILED VISUOct 9, 2024 · N671FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202410091633Seat Track · unknownEXISTING SPLICE REPAIR FOUND ON MAIN DECK CARGO COMPARTMENT SEAT TRACK BETWEEN FRAME 52~53, -Y956, EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA. DUE TO NO LEGACY DOCUMENTATION SUPPORTING THIS EXISTING REPAIROct 9, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410041586Seat Track · corrodedMAIN DECK FLOOR STRUCTURE FOUND SEAT TRACK CORROSION AT FR15A 2" AND Y953 AREA REPLACED THE DAMAGE SEAT TRACK WITH NEW ONE AT MAIN DECK FLOOR STRUCTURE FR15A PLUS 2" AND Y953 AREA I.A.W A300-600F SRM 51-72-10-00, PAGE 2 & 51-40-21-001, PARA.6 PAGE 7B- PAGOct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202410041585Plate · bentTAIL FUSELAGE INTERNAL FOUND 2EA SUPPORT AND WEB GOT DEFORM AT FR86-87 S33R AND S39R REPLACED THE DEFORM STRAPS AND WEBPLATE WITH NEW PARTS ON TAIL FUSELAGE BETWEEN FR86 TO FR87, S-33R AND S-39R I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40- 21-001,Oct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202410041470Crossbeam · corrodedMAIN DECK FLOOR STRUCTURE FOUND CROSSBEAM CORROSION AT FR47 AND Y370 AREA. REMOVED CORROSION CROSSBEAM AND INSTALLED NEW CROSSBEAM I.A.W A300-600F SRM 51- 72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT Oct 4, 2024 · N671FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202410021661Skin · gougedLH WING SPOILER #3 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #3 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381100 P1, SEQ NO:1248, TITLE:WINGS-FLIGHT SURFACES-LH #3 SPOILER-OUTER HINGE ARMSOct 2, 2024 · N671FE · Airbus A300F4605R · SpoilersSDR FDEA202410021659Skin · gougedRH WING SPOILER #4 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPR SURFACE FOUND 4EA NICKS ACCOMPLISHED THE EDGE BAND REPAIR AT RH #4 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381096 P1, SEQ NO:1247, TITLE:WINGS-FLIGHT SURFACES-RH #4 SPOILER-OUTER Oct 2, 2024 · N671FE · Airbus A300F4605R · SpoilersSDR FDEA202410021658Skin · gougedLH WING SPOILER #7 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #7 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO:T6-5750-T0381092 P1, SEQ NO:1246, TITLE:WINGS-FLIGHT SURFACES-LH #7 SPOILER-OUTER HINGE ARMSOct 2, 2024 · N671FE · Airbus A300F4605R · SpoilersSDR FDEA202410021656Skin · gougedLH WING SPOILER #6 BOTH I/B AND O/B HINGE ARMS FWD SECTION UPPER SURFACE NICK. ACCOMPLISHED THE EDGE BAND REPAIR AT LH #6 SPOILER BOTH HINGE ARMS I.A.W FEDEX EA NO: T6-5750-T0381085 P1, SEQ NO:1245, TITLE: WINGS-FLIGHT SURFACES-LH #6 SPOILER-OUTER HINGE AROct 2, 2024 · N671FE · Airbus A300F4605R · SpoilersSDR FDEA202409301494Crossbeam · brokenMAIN DECK FLOOR STRUCTURE FOUND FR61 CROSS BEAM CROWN BROKEN BETWEEN Y1456 AND Y1959 AREA REPLACED THE CROSS BEAM ADAPTER OF THE MAIN DECK CARGO FLOOR STRUCTURE AT FR 61 BETWEEN Y1456 AND Y1959 AREA. I.A.W A300-600F SRM 51-72-10-001, PAGE 2. THIS REPAIR ISSep 30, 2024 · N671FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202409291662Shear Web · crackedFWD CARGO COMPT RH CHORD CRACK AT FR38 POSITION UNDER FLOOR PANEL (RBL59) REPLACED THE DAMAGED SHEAR WEB WITH NEW PART AT FWD CARGO COMPARTMENT BETWEEN FR38~38.1, S-44R. I.A.W A300-600F SRM 51-72-10-001, PAGE.2. THIS REPAIR IS CLASSIFIED AS CAT.A MINOR PERSep 29, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202409271469Support Bracket · damagedLOWER BEACON LIGHT POWER SUPPLY UNIT 4LV WIRE BUNDLE 1EA SUPPORT BRACKET BROKEN AT AFTER CARGO UNDER FLOOR PANEL 162DF REPLACED BROKEN SUPPORT BRACKET WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE 2 & 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFSep 27, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202409261468Profile · crackedMAIN DECK FLOOR STRUCTURE FOUND T-PROFILE CRACK AT FR80/82,-Y1580 AREA. REMOVED CRACK T-PROFILE AND INSTALLED NEW T-PROFILE I.A.W A300-600F SRM 51-72-10-001, PAGE2 AND 51-40-21-001 PARA6 PAGE7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT MAIN DESep 26, 2024 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202409251657Spar · wornRH WING NR 2 SPOILER O/B SIDE FWD SKIN WORN CUT OUT THE DAMAGE AREA AND INSTALLED REPAIR PARTS AT RH #2 SPOILER FWD OF RIB 18 IAW EA NO:T6-5750-T0381047 P1, SEQ NO:1251, TITLE:WING-FLIGHT SURFACES-RH NR 2 SPOILER-WEAR DAMAGE AT OUTBOARD FACE OF FRONT SPAR AT RSep 25, 2024 · N671FE · Airbus A300F4605R · SpoilersSDR FDEA202409251631Seat Track · damagedMAIN DACK FLOOR STRUCTURAL FOUND SEAT TRACK CROWN BROKEN AT FR63 AND -Y2400 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR62~FR64 PLUS 10.5" I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPAIR CLSep 25, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409251592Seat Track · damagedMAIN DACK FLOOR STRUCTURAL FOUND SEAT TRACK CROWN BROKEN AT FR63 AND -Y2400 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR62~FR64 PLUS 10.5" I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203 ~ 208. THIS REPAIR Sep 25, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409231660Rib · gougedLH WING LE CAVITY RIB GOUGE ABOVE ANTI-ICE DUCT AT WOFX -259.4 NEAR KRUEGER FLAP. TRIMMED OUT THE DAMAGE AREA AND INSTALLED THE REPAIR ANGLE AT LH WING LE CAVITY RIB WOFX259.4 I.A.W FEDEX EA NO:T6-5710-T0380996 P1, SEQ NO:1243, TITLE:WING-BASIC WING STRUCTSep 23, 2024 · N671FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202409231630Seat Track · crackedMAIN DACK FLOOR STRUCTURE FOUND Y1456 SEAT TRACK CRACK AT FR 57.2 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57.1 PLUS 10"~FR58 PLUS 10", Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS REPASep 23, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409231591Seat Track · crackedMAIN DACK FLOOR STRUCTURE FOUND Y1456 SEAT TRACK CRACK AT FR 57.2 AREA. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK FLOOR SEAT TRACK FR57.1 PLUS 10"~FR58 PLUS 10", Y1456. I.A.W A300-600F SRM 53-10-16-201, PARA.4, FIG.201, PAGE.203~208. THIS RESep 23, 2024 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202409201353Skin · no discrepancyAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER5-12", T/E-22.5" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTSSep 20, 2024 · N671FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202409201665Repair · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING FLUSH DOUBLER REPAIR FOUND ON LH CTR FLAP NOSE SKIN BTW RIB 23~24 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14Sep 20, 2024 · N671FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202409201636Skin · no discrepancy00089009N00135 AIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP LWR SKIN BTW RIB 14~14A, T/E-21" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING RSep 20, 2024 · N671FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202408061088Transmitter · failedENROUTE TO MEM GOT A GREEN HYDRAULIC SYSTEM LOW LEVEL. PER ECAM TURNED OFF GREEN HYDRAULIC PUMPS. DECLARED AN EMERGENCY AND RECOVERED TO MEMPHIS. LOWERED THE GEAR VIA EMERGENCY EXTENSION AND LANDED STRAIGHT AHEAD ON 36C. UPON LANDING, HYDRAULIC QUANTITY SAug 6, 2024 · N671FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202403010225Feel Unit · faultedON LANDING AIRCRAFT ELEVATOR CONTROLS ARE VERY HEAVY TO PULL AFT. CONTROL WILL NOT RETURN TO NEUTRAL POSITION WITHOUT PUSHING IT INTO PLACE ON GROUND. INSTALLED PUSH-PULL TOOL ON PILOT'S YOKE AND CHECKED ELEVATOR OPS LOAD PER A300-600 AMM 27-33-00-05 Mar 1, 2024 · N671FE · Airbus A300F4605R · Elevator Control SystemSDR FDEA202312051925Switch · inoperativeFOUND DOOR INTERIOR EMERGENCY EXIT LIGHTS ALWAYS ILLUMINATED. NOTICED RED EMERGENCY LIGHT SWITCH FWD OF L1 DOOR IS STUCK INSIDE. RELEASED FOR SERVICE PER MEL : 33-XX-XX-XX CAT: C EXP: 15DEC23 "MEL 33-XX-XX-XX: COURIER COMPARTMENT INTERIOR EMERGENCY LIGHTSDec 5, 2023 · N671FE · Airbus A300* · Emergency LightingSDR FDEA202306211077Psu · failedON PRE-DEPARTURE CHECK FOUND THAT COUIER COMPARTMENT INTERIOR EMERGENCY EXIT LIGHTS ARE INOP, WILL NOT TEST. RELEASED FOR SERVICE PER MEL : 33-XX. INSTALLED NEW BATTERY, NO HELP. REINSTALLED ORIGIONAL BATTERY. A300 AMM 33-XX. RELAMPED PER IPC. NO HELP. PJun 21, 2023 · N671FE · Airbus A300* · Emergency EquipmentSDR FDEA202302040234Transformer · failedWHILE ATTEMPTING TO START APU, GOT AN APU FAULT, THEN ELECTRICAL FUMES AND SMOKE IN COCKPIT PULLED APU/ START C/B. OPEN FRONT PANEL OFF OF 120 VU, INSPECTED WIRING, AND APU START CONTACTOR 5KA, APPEARS TO BE IN GOOD SHAPE, NO DAMAGE, 50 AMP BREAKER 10XH POFeb 4, 2023 · N671FE · Airbus A300* · APU Start/Ignition SystemSDR FDEA202205171405None · damagedSTABILIZER - RUDDER RH PANEL FOUND WATER INGRESS AROUND FASTENER #36, #37, #38 AND #39 COMPLIED WITH FEDEX EA: 6-5540-T0332902 A PT3, EA TITLE: STABILIZERS - RUDDER - RH - WATER INGRESS - AIRBUS SERVICE BULLETIN A300-55-6050 INSPECTIONS/EO 6-5540- E031936May 17, 2022 · N671FE · Airbus A300* · Rudder StructureSDR FDEA202205161404None · crackedRH FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK COMPLIED WITH FEDEX EA: 6-5210-T0368735 PT1, EA TITLE: DOORS - PASSENGER/CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR - RSC TRACKING. REPAIRED RH FWD PAX DOOR - FRAME SEGMENT May 16, 2022 · N671FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202205161395Seat Track · crackedMAIN DECK CARGO COMPARTMENT FLOOR SUPPORT STRUCTURE - SEAT TRACK CRACKED, BETWEEN FR20 AND FR21, Y1959 COMPLIED WITH FEDEX EA: 6-5310-T0368594 PT1, EA TITLE: FUSELAGE - MAINFRAME - MCD Y1959 SEAT TRACK BENT AND CRACKED BETWEEN FR20 AND FR21 - REPAIR. REPAMay 16, 2022 · N671FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202107241856Power Supply · no testEMERGENCY LIGHTS PUSH TO TEST SWITCH IN COURIER AREA DOES NOT ILLUMINATE DURING TEST. DURING LIGHTING TEST, ALSO NOTED RED LED ON FRONT FACE OF POWER SUPPLY UNIT (29WL1) WAS ILLUMINATED.REMOVED AND REPLACED POWER SUPPLY UNIT (29WL1) REF AMM 33-51-14-04. OPJul 24, 2021 · N671FE · Airbus A300F4605R · Emergency LightingSDR FDEA202104080854Pawl · out of alignmentL1 DOOR ESCAPE SLIDE HANDLE DIFFICULT TO DISARM HANDLE STIFF AND WE COULDN'T MOVE IT FAR ENOUGH INTO THE DISARM POSITION TO PIN IT. . RELEASED FOR SERVICE PER MEL : 52-XX-XX-XX CATEGORY : C EXP "MEL 52-XX-XX-XX: CREW ENTRY DOOR ESCAPE SLIDE L1 - INOP. SLIApr 8, 2021 · N671FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202104060831Hose · wornLOST GREEN HYDRAULIC SYSTEM PASSING THROUGH FL290. FLUID LEVEL DECREASED TO RED DOT ALMOST IMMEDIATELY. LEVELED A\C AT FL330, SLOWED TO GREEN DOT. COMPLIED WITH QRH. DESCENDED TO FL310 AND MAINTAINED .65 MACH. CONTINUED TO MEMPHIS, EMERGENCY DECLARED Apr 6, 2021 · N671FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202012203192Mount · crackedON SLAT EXTENSION ON APPROACH GOT ECAM "KREUGER NOT EXTENDED" REMAINED NOT EXTENDED THROUGH LANDING. ON POSTFLIGHT WALKAROUND FOUND LEFT KRUEGER FLAP VANE OUTBOARD BRACKET MOUNT CRACKED AND INBOARD BRACKET BROKEN. REMOVED KRUEGER FLAP MOVEABLE VANE, PER MM Dec 20, 2020 · N671FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA2020040370586Indication Sys · malfunctionedPDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR Mar 17, 2020 · N671FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2020031970586Indication Sys · inoperativePDIS 671 52-70 0953 17MAR20 IND OPEN U LOGPAGES:3230401 R1 DOOR SLIDE WILL NOT ARM MEL 17MAR20 00:00 IND U RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 27MAR20 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR Mar 17, 2020 · N671FE · Airbus A300F4605R · Door Warning SystemSDR FDEA2019111532941Skin · crackedFR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE NDT HFEC INSPECTION FOUND CRACK SIGNAL. FR40 CTR WING JOINT AT UPPER SKIN LEVEL LH MIDDLE HOLE CRACK. COMPLIED WITH FEDEX EA:6-5710-T0350731 P1. TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MINov 13, 2019 · N671FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201911082907Crossbeam · crackedMDC FLOOR - FR64 Y-1456 - Y-1959, CROSSBEAM CRACKED APPROX 0.5 INCH IN LENGTH. MDC FLOOR FR64 B/W Y-1456 AND Y-1959 CROSSBEAM CRACKED APPROX 0.5 INCH . REPAIRED THE CRACKED CROSSBEAM PER A300-600F SRM53-10-15 FIGURE211. THIS REPAIR CATEGORY IS A. MAJONov 8, 2019 · N671FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201911082906Rib · crackedRH WING - MID FLAP RIB21 AFT AREA FOUND CRACK ON X-RAY INSPECTION. RH WING - MID FLAP RIB21 UPPER FLANGE CRACK BETWEEN STGR2.7 AND STGR2.8 . REPAIRED THE CRACKED RIB FLANGE PER A300-600F SRM57-50-00-201 FIG.201. TRACKING EA:6-5750-T0350993 HAS BEEN ISSUED Nov 8, 2019 · N671FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201705101390Skin · gougedRIGHT INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. ACCOMPLISHED EA 6-5750-T0333072, PART 1. MAJOR REPAIR.May 10, 2017 · N671FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201705101388Skin · gougedLEFT WING INBD FLAP UPPER SURFACE HAS SEVERAL GOUGES. REPAIRED THE FLAP UPPER SURFACE IAW EA 6-5750-T0332914, PART 1. MAJOR REPAIR.May 10, 2017 · N671FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201705061364Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION AT Y0 BETWEEN FRAMES 33 AND 34. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16, 51-4-21, AND SRM 51-40-44. MAJOR REPAIR.May 6, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201705061363Seat Track · wornSEAT TRACK IS HEAVILY WORN IN MAIN CABIN JUST AFT OF FRAME 78, Y852. REMOVED AND REPLACED THE SEAT TRACK SECTION IAW SRM 53-10-16. MAJOR REPAIR.May 6, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201705041356Floor Panel · brokenMAIN CABIN FLOOR PANEL 251VF IS BROKEN. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.May 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201705041355Floorboard · dentedMAIN CABIN FLOOR PANEL 241TH HAS SEVERAL DENTS AND MISSING EDGE FILLER. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005. MAJOR REPAIR.May 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201705041354Floor Panel · delaminatedFLOOR PANEL 161AF HAS DELAMINATION ON BOTTOM SIDE. FABRICATED A NEW FLOOR PANEL IAW DWG SRZ 25-0005, REV M. MAJOR REPAIRMay 4, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704301336Support · crackedMAIN CABIN SUPPORT WEB IS CRACKED AT FRAME 45. REMOVED AND REPLACED THE SUPPORT WEB IAW SRM 51-40-21 AND SRM 51-40-44. MAJOR REPAIRApr 30, 2017 · N671FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201704291296Seat Track · corrodedMAIN CABIN SEAT TRACK HAS CORROSION BETWEEN FRAME 54.1 -Y1959. REMOVED AND REPLACED MAIN CABIN SEAT TRACK BETWEEN FR 54.1 -Y1959 IAW SRM 51-40- 21. THIS IS A MAJOR REPAIR.Apr 29, 2017 · N671FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201704271284Floor Panel · crackedMAIN CABIN FLOOR PANEL 241DF HAS IMPACT DAMAGE. FABRICATED MAIN CABIN FLOOR PANEL 241DF REF 70013348480001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.Apr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201704271283Floor Panel · dentedMAIN CABIN FLOOR PANEL 242UJ HAS SEVERAL DENTS. FABRICATED MAIN CABIN FLOOR PANEL 242UJ REF 70013348500001 AND DWG SRZ 25-005 REV M. THIS IS A MAJOR REPAIR.Apr 27, 2017 · N671FE · Airbus A300F4605R · Fuselage Floor Panel
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