N672FE

Service difficulty reports · 287

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 = 'N672FE' 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 FDEA202609081286Bottle · low pressureLEFT FWD CREW ENTRY DOOR DAMPER AND EMERGENCY OPERATION CYLINDER REQUIRES SERVICING. SERVICED LEFT FWD DOOR DAMPER AND EMERGENCY OPERATION CYLINDER AS REQUIRES.Sep 8, 2026 · N672FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202602150210Safety Wire · wrong partL1 SLIDE ASSY. REPLACE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 STAINLESS STEEL WIRE AND EJECTOR BAG RELEASE CABLE WIRE WITH MS20995CY16 CAD-PLATED COPPER WIRE. AMM: 25-61-21-04 AMM: 25-61-20-05-01 CMM: 25-60-40 FEA: 6-2560-F0386375 A EA: Feb 15, 2026 · N672FE · Airbus A300F4605R · Escape SlideSDR FDEA202512050001Skin · crackedFWD CARGO COMPT DOOR INNER SKIN CRACK AT FR22A, BEAM1 NEAR LEFT ACTUATOR I/B SIDE. CUT OUT AND INSTALLED REPAIR DOUBLER AT FWD CARGO DOOR INNER SKIN FR22A BEAM1~2 I.A.W FEDEX EA NO: T6-5230-T0381602 P1, SEQ NO:1140, TITLE:DOORS-CARGO DOOR/HYD SYS- FWD CARGJan 2, 2025 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412111817Bracket · crackedFEDEX QA SURVEILLANCE FINDING MDC DOOR CUT OUT AFT SIDE FRAME FOUND 2EA BRACKETS WITH CRACKED AND MISSING PART. REPLACED THE CRACK BRACKETS WITH NEW PART LOCATE AT MAIN DECK SIDE CARGO DOOR CUT OUT AFTER SIDE FRAME I.A.W A300-600F SRM 51-72-10-001 PAGE 2 ADec 11, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202412081840Fork · crackedM/D FLOOR PNL BOTTOM FOUND A LINK FORK CRACK AT FR47, -Y2462 FABRICATED THE NEW LINK FORK AND INSTALLED WITH FASTENER AT M/D FLOOR PNL BOTTOM FR47,-Y2462 I.A.W A300-600F SRM 53-15-15 CONFIG2 FIG 10 PAGE65 ITEM45 & 51-72-10-001 PAGE2 & 51-40-21-001 PARA7 PADec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202412081827Seat Track · wornM/D SEAT TRACK WORN AT FR54.2 PLUS 1", Y0. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR54.2~55, Y0, I.A.W A300-600F SRM 53-10-16-201, PARA.4, PAGE 203~208, FIG.201, THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412081826Seat Track · wornM/D SEAT TRACK WORN AT FR62 PLUS 1", Y1959. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR62~65, Y1959, I.A.W A300-600F SRM 53-10-16-201, PARA.4, PAGE 203~208, FIG.201. THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412081820Seat Track · wornM/D SEAT TRACK WORN AT FR28-1", Y0 POSITION. ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR26~30, Y0, I.A.W A300-600F SRM 53-10-16-201,PARA, 4,PAGE 203~208, FIG.201, THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100.Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412081808Seat Track · wornM/D SEAT TRACK WORN AT FR54.2 PLUS 1", Y0 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR54.2~55,Y0,I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412081807Seat Track · wornM/D SEAT TRACK WORN AT FR62 PLUS 1",Y1959 ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR62~65,Y1959, I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412081806Seat Track · wornM/D SEAT TRACK WORN AT FR28-1",Y0 POSITION ACCOMPLISHED THE SEAT TRACK SPLICE REPAIR AT MAIN DECK SEAT TRACK FR26~30,Y0,I.A.W A300-600F SRM 53-10-16-201,PARA.4,PAGE 203~208, FIG.201,THE REPAIR IS CLASSIFIED AS MAJOR CAT.A PER GMM 6-2-100Dec 8, 2024 · N672FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202412071833Rib · corrodedTHE OUTBD JACK RIB CORRODED ADJACENT TO UPPER BORE AT L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT L5 SPOILER OUTBD JACK RIB ABX 184.625 UPPER BORE. I.A.W FEDEX EA NO: T6-5740-T0381590 P1, SEQ NO: 1134, TITLE: WING-ATTACH FITTINGS-LH WING #5 SPOILER JDec 7, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202412071832Rib · corrodedTHE OUTBD JACK RIB CORROSION ADJACENT TO LOWER BORE AT L5 SPLR. ACCOMPLISHED THE REINFORCEMENT REPAIR AT L5 SPOILER OUTBD JACK RIB ABX 184.625 LOWER BORE. I.A.W FEDEX EA NO: T6-5740-T0381590 P1, SEQ NO: 1134, TITLE: WING-ATTACH FITTINGS-LH WING #5 SPOILER Dec 7, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202412071825Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 PER EO NO : E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 23 LONGN 1~3 PER FEDEX E.O NO :E6-5230-E0378588 A P5 , SEQ NO :1115 , TITLE :DOORS-CARGO DOODec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412071824Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 PER EO NO : E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 LONGN 1~3 PER FEDEX E.O NO :E6-5230-E0378588 A P5 , SEQ NO :1115 , TITLE :DOORS-CARGO DOODec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412071799Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME23 PER EO NO:E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME23 LONGN 1~3 PER FEDEX EO NO:E6-5230-E0378588 A P5 , SEQ NO :1242 , TITLE :DOORS-CARGO DOOR/HYD Dec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412071798Fitting · not reportedREPLACE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME24 PER EO NO:E6- 5230-E0378588A P5. REPLACED MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING AT FRAME 24 LONGN 1~3 PER FEDEX EO NO :E6-5230-E0378588 A P5 , SEQ NO :1242 , TITLE :DOORS-CARGO DOOR/HYDec 7, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412051842Fitting · crackedLOWER LH FRAME 45 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR45. I.A.W FEDEX EO NO: E6-5310-E0330747 D P23, SEQ NO:1120, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202412051841Fitting · crackedLOWER RH FRAME 45 BASE FITTING FOUND AREA 1 CRACK. ACCOMPLISHED THE FRAME FOOT REPAIR AT RH LOWER FRAME FITTING FR45. I.A.W FEDEX EO NO: E6-5310-E0330747 D P24, SEQ NO:1121, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202412051839Fitting · crackedLOWER RH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT RH LOWER FRAME FITTING FR46. I.A.W FEDEX EO NO: E6-5310-E0330747 D P26, SEQ NO:1123, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202412051838Fitting · crackedLOWER LH FRAME 46 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR46. I.A.W FEDEX EO NO: E6-5310-E0330747 D P25, SEQ NO:1122, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202412051837Fitting · crackedLOWER LH FRAME 44 BASE FITTING FOUND AREA 1 CRACK ACCOMPLISHED THE FRAME FOOT REPAIR AT LH LOWER FRAME FITTING FR44. I.A.W FEDEX EO NO: E6-5310-E0330747 D P21, SEQ NO:1119, TITLE: FUSELAGE-MAINFRAME-INSPECTION OF LOWER FRAME BASE FITTING BETWEEN FRAMES 41 Dec 5, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202412041853Door · bentMAIN DECK CARGO DOOR WAS FOUND BULGE ON THE INNER SKIN AND CONNECTION CLIP AT BEARING FITTING FWD OF FR24 BETWEEN LONGERON PT7-PT8. ACCOMPLISHED THE DOUBLER REINFORCEMENT REPAIR AT MAIN CARGO DOOR INNER SKIN AND CONNECTING CLIP FR24 BETWEEN LONGERON PT7~8,Dec 4, 2024 · N672FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202412041834Rib · corrodedFOUND RH #4 SPOILER OUTBOARD UP JACK RIB HOLE CORROSION. ACCOMPLISHED THE REINFORCEMENT REPAIR AT R4 SPOILER OUTBD JACK RIB ABX112.525 UPPER BORE I.A.W FEDEX EA NO:T6-5740-T0381568 P1, SEQ NO:1133, TITLE:WING-ATTACH FITTINGS-RH WING #4 SPOILER JACK RIB AT Dec 4, 2024 · N672FE · Airbus A300F4605R · Wing, Rib/BulkheadSDR FDEA202412041818Strap · crackedFUSELAGE STRUCTURAL FOUND S-33R STRAP CRACK AT FR-85 14" AREA. CRACKED STRAP REPLACED NEW PART INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10- 001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23. THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT FR85 14" Dec 4, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202412031809Floor Support · corrodedM/D FLOOR SUPPORT FOUND CORROSION AT FR14~FR17, -Y1959 REPLACED CORROSION SUPPORT WITH NEW ONE AT M/D FLOOR SUPPORT FR14~FR17,-Y1959, I.W.A A300-600F SRM 51-72-10-001,PAGE 2 & 51-40-21-001,PARA.6,PAGE 7B~23,THE REPAIR IS CLASSIFIED AS MINOR CAT.A PER GMM 6Dec 3, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202412031794Floor Support · corrodedM/D FLOOR SUPPORT FOUND CORROSION AT FR14-9"~FR14, Y730. REPLACED CORROSION FLOOR SUPPORT WITH NEW ONE AT M/D FR14-9"~ FR14, Y730 I.A.W A300- 600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.6, PAGE 7B~23. THE REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100Dec 3, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301835Plate · crackedFWD CGO COMPT UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L, FR21 POSITION. REPLACED FWD CGO COMPT UNDER FLOOR AREA LH SIDE PLATE AT S-43L~S-44L, FR21 POSITION I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-PAGE.23. THIS RNov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301816Floor Support · crackedM/D FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK AT FR80/82, Y300. REPLACED THE 1EA PROFILE-Z WITH NEW ONE AT M/D FLOOR SRTUCTURE FR80/82, Y300. I.A.W A300-600F SRM 51-72-10-001, PAGE.2& 51-40-21-001, PARA.6, PAGE.7B~23. REPIAR CLASSIFIED AS MINOR PER GMM 6-Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301802Floor Support · crackedM/D FLOOR STRUCTURE FOUND 1EA PROFILE-Z CRACK AT FR80/82, Y300. REINSTALLED THE 1EA PROFILE-Z WITH NEW ONE AT M/D FLOOR SRTUCTURE FR80/82, Y300 I.A.W A300-600F SRM 51-72-10-001, PAGE.2. REPIAR CLASSIFIED AS MINOR PER GMM 6-2-100.Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301801Support · crackedM/D OVHD COMPT FOUND A HARNESS SUPPORT CRACK AT FR80/82 POSITION. REPLACED THE DAMAGE HARNESS SUPPORT WITH NEW AT M/D OVHD COMPT FR80/82 POSITION. I.A.W A300-600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301796Support Bracket · crackedAFT CGO COMPT BILGE AREA 1EA ELECTRICAL WIRE SUPPORT BRACKET CRACK AT FR59 CENTER LINE POSITION. REPLACED THE DAMGE 1EA ELECTRICAL WIRE SUPPORT BRACKET WITH NEW ONE AT AFT CGO COMPT BILGE AREA FR59 CENTER LINE POSITION I.A.W A300-600F SRM 51-72-10-001, PAGNov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301795Support Bracket · crackedBULK CGO COMPT BILGE AREA 1EA ELECTRICAL WIRE SUPPORT BRACKET CRACK AT FR63, S-44R POSITION. REPLACED THE DAMAGE WIRE SUPPORT BRACKET WITH NEW ONE AT BULK CGO COMPT BILGE AREA FR63 S-44R POSITION I.A.W A300-600F SRM 51-72-10-001, PAGE 2 REPAIR CLASSIFIED ANov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301782Floor Support · crackedM/D FLOOR STRUCTURE FOUND 1EA SHEAR PLATE CRACK AT FR79 5", Y1600 REPLACED THE DAMAGE SHEAR PLATE WITH NEW ONE AT M/D FLOOR STRUCTURE FR79 5",Y1600 I.A.W A300-600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411301781Floor Support · crackedM/D FLOOR STRUCTURE FOUND 1EA SHEAR PLATE CRACK AT FR79 5", -Y1600 REPLACED THE DAMAGE SHEAR PLATE AT M/D FLOOR STRUCTURE FR79 5", -Y1600 I.A.W A300- 600F SRM 51-72-10-001,PAGE 2,REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100Nov 30, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411261836Plate · crackedAFT CGO COMPT SHEAR PLATE CRACK AT FR68~FR69, S-48L POSITION. INSTALLED THE FABRICATION NEW PART AT BULK CARGO COMPARTMENT AT FR68~69, S-48L I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE.7B~23& AIRBUS DRAWING NO: A53974299 REV.D & FEDEX GMM 7-0-1001. THE Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411261780Crossbeam · corrodedBULK CGO COMPT CROSSBEAM EXTERNAL SURFACE CORRODED AT FR66 ,Y0-2" POSITION CUT OUT DAMAGED CROSSBEAM AREA AND INSTALLED REPAIR PARTS ON REPAIR AREA WITH FASTENERS FOR REPAIR. I.A.W A300-600F SRM 51-40-21-001 PARA6 PAGE7B-23 AND 53-10-15-201 PARA13 P373-P38Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202411261765Bracket · crackedAFT CGO COMPT FWD BULKHEAD LH BRACKET CRACK AT FR54, Y1959 POSITION. REPLACED THE CRACKED LH FWD BULKHEAD BRACKET, AT AFT CARGO COMPT FR54, Y1959 POSITION. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE 7B- PAGE 23 AND 51-72-10-001, PAGE 2. THIS REPAIR IS Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411261764Bracket · crackedAFT CGO COMPT FWD BULKHEAD RH BRACKET CRACK AT FR54, -Y1959 POSITION. REPLACED THE CRACKED AFT CARGO COMPT FWD BULKHEAD RH BRACKET, AT FR54, -Y1959 POSITION. I.A.W A300-600F SRM 51-40-21-001, PARA.6, PAGE 7B - PAGE 23 AND 51-72-10-001, PAGE 2. THIS REPAIR Nov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202411261763Angle · crackedAVIONICS COMPT FLOOR CROSSBEAM PICK UP ANGLE CRACK AT FR10, Y403 POSITION. REPLACED AVIONICS COMPT FLOOR BEAM PICK UP ANGLE WITH NEW ONE AT FR10, Y403 POSITION. I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B~23. THIS REPAIR IS CNov 26, 2024 · N672FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202411211783Skin · damagedAIRCRAFT REPAIR ASSESSMENT: EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW FR31~32, S-49R~52R COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1Nov 21, 2024 · N672FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202409231336Fitting · failedRTO AT 75 KNOTS FOR GENERATOR 1 FAILURE ON ROLL AT KGTF. TAXI BACK TO RAMP FOR MAINTENANCE. RELEASED FOR SERVICE PER MEL 24-11-01-A CATEGORY B. APU GEN MUST BE USED TO POWER AFFECTED BUS THROUGHOUT FLIGHT. MEL: 24-11-01-A DEFERRED PER MEL 24-11-01-A,Sep 23, 2024 · N672FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA202409231335Idg · leakingRTO AT 75 KNOTS FOR GENERATOR 1 FAILURE ON ROLL AT KGTF. TAXI BACK TO RAMP FOR MAINTENANCE. #1 IDG FOUND LEAKING FROM SERVICING PORT. REMOVED AND REPLACED #1 ENG IDG SERVICE FITTING AND PACKING. SERVICED AND OPS CKED IDG IAW ABOVE LISTED REF. OPS AND LEAKSep 23, 2024 · N672FE · Airbus A300F4605R · AC Generator-AlternatorSDR FDEA202406270871Pitot Tube · obstructedON TAKEOFF WHEN SPEED WAS CHECKED AT 80 KNOTS, CAPTAIN AIRSPEED INDICATED 80 AND FO AIRSPEED INDICATED BETWEEN 40 AND 50. REJECTED TAKEOFF AND RETURNED TO RAMP. INSPECTED PITOT DRAIN IN NOSE WHEELWELL . NO WATER FOUND . INSPECTED LINES AT ADC 1 AND ADC Jun 27, 2024 · N672FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA202406180815Pitot Tube · obstructedON TAKEOFF ROLL, FO CALLED 80 KNOTS AND CAPT HAD 60 KNOTS. TAKEOFF REJECTED AT 80 KNOTS ON CAPTAIN SIDE. INSPECTED FO & CAPT PITOT TUBES & FLUSHED LINES FROM ADC 1, ADC2. FO SYS CHECKED GOOD. FOUND CHARRED DEBRIS IN CAPT PITOT PROBE. MM 34-11-15-04, INSJun 18, 2024 · N672FE · Airbus A300F4605R · Pitot/Static SystemSDR FDEA202403260379Lamp · inoperativeLAMP INOP AT 31WL2 (R1 EMERGENCY EXIT SIGN) REMOVED AND REPLACED 1 LAMP AT 31WL2 (R1 EMERGENCY EXIT SIGN) AS REQUIRED, OPS CHECK GOOD.Mar 26, 2024 · N672FE · Airbus A300F4605R · Emergency LightingSDR FDEA202307081184Computer · failedCABIN PRESSURE MANUAL CONTROL. BOTH REGULATORS FAULTED. OPERATED IN MANUAL CONTROL. FOUND BOX LIGHT ILLUMINATED WITH A CODE 70 WHILE TESTING BOX .REMOVED AND REPLACED PDPU 54GB AND TEST OK PER ABOVE REF. PRESSURE CONTROLLERS BOTH TEST OK REF TSM 21-30-00. AJul 8, 2023 · N672FE · Airbus A300* · Cabin Pressure Control SystemSDR FDEA202303080395Strut · damagedNOSE LANDING GEAR DRAG STRUT FAILED REMOVED AND REPLACED TELESCOPING STRUT. IAW AMM 32-31-24-04. OPS CHECK SATISFACTORYMar 8, 2023 · N672FE · Airbus A300* · Main Landing GearSDR FDEA202207161738None · crackedRH FWD PAX DOOR - FRAME SEGMENT AT FR14C FOUND 1EA CRACK PERFORMED THE REPAIR ON RH FWD PAX DOOR FRAME SEGMENT AT FR14C AS PER FEDEX EA# : 6-5210-T0369438 P1 , TITLE: DOORS - PASSENGER / CREW - LOCAL FABRICATION AND REPLACEMENT OF FRAME SEGMENT ON R1 DOOR Jul 16, 2022 · N672FE · Airbus A300* · Passenger/Crew DoorsSDR FDEA202207131713None · delaminatedLH WING 5# SPOILER O/B HINGE ARM O/B END FOUND DELAMINATION SIZE:80MM X 25MM X 1.45MM PERFORMED THE REPAIR ON LH WING 5# SPOILER O/B HINGE ARM O/B END AS PER FEDEX EA # : 6-5750-T0315012 A P2 TITLE: WING - FLIGHT SURFACES - LH WING 5# SPOILER LOWER SURFJul 13, 2022 · N672FE · Airbus A300* · Wing, Control Surfaces
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