N663FE

Service difficulty reports · 264

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 = 'N663FE' 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 FDEA202604090418Handle · faultedMLG RETRACT INOP, RAISING MLG LEVER AFTER TAKE-OFF. EMERGENCY DECLARED. AFTER BRIEF W/ CREW MLG RETRACT INOP IN SYS 1, CREW DID NOT ATTEMPT TO RETRACT IN SYS 2 DUE TO A MLG WARNING MESSAGE IN SYS 1. ALL DOORS SHOWED UNLOCKED WHEN MLG HANDLE MOVED UP & MLGApr 9, 2026 · N663FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA202604020396Seat Track · damagedRAMP REPORTED BROKEN LOCK ON MAIN DECK POS 12R. LOCK PN [MT1584]. B/R LOCK REMOVED AND STOWED IN FLIGHT DECK CLOSET. PLND: DATE: 27MAR26 ENT BY: 779762 ON: 27MAR26 17:39 Z AT: IND-HVMX PLNTXT27MAR26 12:39 SEAT TRACK DAMAGE MEL 27MAR26 09:07 IND RApr 2, 2026 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202602140197Safety Wire · wrong partPACKBOARD RELEASE CABLE SAFETY WIRE REQUIRES REPLACEMENT PER FEA 6-2560-F0386375 A P1 L1 DOOR FEA: 6-2560-F0386375 A P1 CMM: 25-60-40 SAFTIED L1 DOOR SLIDE PACKBOARD RELEASE CABLE WITH .015 STAINLESS WIRE.Feb 14, 2026 · N663FE · Airbus A300F4605R · Escape SlideSDR FDEA202407211044Skin · gougedFOUND GOUGE AT TAIL CONE LOWER SURFACE FR92 PLUS 5.6", S-17R PLUS 3" CUT OUT THE DAMAGE AREA, FABRICATED THE REPAIR DOUBLER WET INSTALLED REPAIR DOUBLER WITH BLIND RIVETS AT TAIL CONE LOWER SURFACE FR92~93, S-17R~18R I.A.W A300- 600F SRM 53-19-12-201, PARA.Jul 21, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202407161033Fitting · crackedPERFORM BEARING FITTING REPLACEMENT AT MAIN DECK CARGO DOOR FR23, LONGN1~3 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23 LONGN1~LONGN3 I.A.W FEDEX EA NO: T6-5230-T0379479 A P1, SEQ NO:775, TITLE: DOORS-CARGO DOOR/HYD SYS-MAINJul 16, 2024 · N663FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202407111003Skin · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON RH I/B FLAP UPPER SKIN BETWEEN RIB16~17, S2.1~S2.2 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIRJul 11, 2024 · N663FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202407061002Angle · chafedQA SURVEILLANCE ITEM AFT CGO COMP'T RH SIDE PROFILE CORNER GOT SCRATCH AT FR58- FR59A POSITION. REPLACED THE SCRATCHED CORNER PROFILE WITH A NEW ONE. I.A.W A300-600F SRM 51-72-10-001 PAGE 2. AT AFT CARGO COMPARTMENT RH SIDE, FR58~FR59A POSITION. REPAIR IS Jul 6, 2024 · N663FE · Airbus A300F4605R · Fuselage Structure (General)SDR FDEA202407050995Seat Track · wornMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WORN AT FR41~FR41 PLUS 3",Y0 POSITION DAMADED SEAT TRACK REPLACED WITH NEW PART, INSTALLED WITH FASTENERS. I.A.W A300- 600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 7, PAGE 24-50. REPAIR CLASSIFIJul 5, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202406190986Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPPER SKIN AT ER7 PLUS 10", FRONT SPAR-18.3" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKINJun 19, 2024 · N663FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202406190985Support Web · deformedAFT FUSELAGE FOUND 2EA SUPPORT WEB GOT DEFORM AT FR86 S35R AND S38R REPLACED THE NEW SUPPORT WEBS WITH RIVETS. I.A.W A300-600F SRM 51-72-10-001 PAGE.2 AND 51-40-21-001 PARA.6, PAGE.7B~23, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100, AT AFT FUSELAGE FR86Jun 19, 2024 · N663FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202406190919Skin · damagedAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR UPPER SKIN AT ER7 10", FRONT SPAR-18.3" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQJun 19, 2024 · N663FE · Airbus A300F4605R · Elevator, Plate/SkinSDR FDEA202406171040Crossbeam · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE CROSS BEAM SURFACE WAS FOUND CORROSION AT FR54.2,-Y70~-Y140 I.A.W A300-600 AMM:20-21-12-00 REPLACED MAIN DECK CARGO COMPATEMENT FLOOR STRUCTURE CROSS BEAM AT FR54.2-Y70-Y140, REPAIR IS CLASSIFIED AS MAJOR PER GMMJun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA202406170994Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WAS FOUND CORROSION AT FR53 PLUS 14"~FR54, Y453 ACCOMPLISHED THE SPLICE REPAIR AT MAIN CARGO SEAT TRACK AT Y450 BETWEEN FR52 AND FR53 I.A.W FEDEX EA NO:T6-5310-T0379554 P1, SEQ NO:000771, TITLE :FUSELJun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202406170964Cargo Track · wornMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WORN AT FR54 PLUS 8"~FR54 PLUS 11", -Y953 INSTALLED THE NEW DUMMY SEAT TRACK AT MAIN DECK FR 54~54.2, -Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24-50. THE REPAIR CLASSJun 17, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202406161028Rib · crackedRH WING SLAT 1 SKELETON RIB 24, 1EA WEB LOWER EDGE CRACK AT FOLDING NOSE O/B SIDE ACCOMPLISHED THE ANGLE REPAIR AT RH WING SLAT #1 RIB24 I.A.W FEDEX EA NO:T6-5750- T0379841 P1, SEQ NO:000778, TITLE:WINGS-FLIGHT SURFACES- RH #1 SLAT-RIB24 LEADING EDGE WEB PLJun 16, 2024 · N663FE · Airbus A300F4605R · Leading Edge DevicesSDR FDEA202406150997Seat Track · corrodedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SEAT TRACK WAS FOUND CORROSION AT FR18 PLUS 10"~FR18 PLUS 15",Y953 REPLACED THE CORRODED SEAT TRACK WITH NEW PART AT FR15A~ FR19, Y953 I.A.W A300-600F SRM 51-72-10-001, PAGE 2 AND 51-40-21-001, PARA 6, PAGE 7B~PAJun 15, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202406150981Rib · cracked1. 1EA CRACK (15MM) WAS FOUND AT R/H WING CENTER FLAP RIB25 AFT AREA OF TOP SURFACE RIB FLANGE. 2. 2EA CRACKS (5MM & 20MM) WERE FOUND AT R/H WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. 3. 1EA CRACK (50MM) WAS FOUND AT R/H WING CENTER FLAP Jun 15, 2024 · N663FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202406140998Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT WAS FOUND CRACK AT FR38 PLUS 4",-Y2462 POSITION CRACKED SUPPORT REPLACED NEW PART. INSTALLED WITH FASTENERS I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7, PAGE.24- PAGE.50. THE REPJun 14, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202406140996Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE SUPPORT WAS FOUND CRACK AT FR38 PLUS 4",-Y2462 POSITION CRACKED SUPPORT REPLACED NEW PART. INSTALLED WITH FASTENERS I.A.W A300-600F SRM 51- 72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.7, PAGE.24- PAGE.50. THE REJun 14, 2024 · N663FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA202406140982Rib · cracked1.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB11 AFT AREA OF TOP SURFACE RIB FLANGE. 2.1EA CRACK (5MM) WAS FOUND AT L/H WING CENTER FLAP RIB12 AFT AREA OF TOP SURFACE RIB FLANGE. 3.1EA CRACK (25MM) WAS FOUND AT L/H WING CENTER FLAP RIB19 AFT AREJun 14, 2024 · N663FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202406131019Seat Track · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR58 ~ 61, Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1Jun 13, 2024 · N663FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202406131018Seat Track · bentAIRCRAFT REPAIR ASSESSMENT : EXISTING SLPIECE REPAIR FOUND ON MDCC SEAT TRACK BTW FR58 ~ 61, Y953 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 1Jun 13, 2024 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202406071031Fitting · crackedTHE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT FR24 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR24 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0379479 A P1, SEQ NO:775, TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CAJun 7, 2024 · N663FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202404190474Pbe · failedDURING SERVICE CHECK FOUND PBE IN COURIER AREA DUE DATE OF 04/24 . INSTALLED ONLY NEW PBE IN COURIER AREA PER AMM 35-31-01-02.Apr 19, 2024 · N663FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202303160447Unknown · unknownMDIS 663 24-40 5174 14MAR23 LAX OPEN U AIRCARFT EXTERNAL POWER RECEPTACLE ARCED AT PLUG AND EXTERNAL POWER CONNECTION. SHGN 14MAR23 16:21 LAX U AMM: 24-41-15-04 REF AMM 24-41-15-04 BEGAN EXTERNAL POWER RECEPTACLE REMOVAL BY COMPLETING Mar 16, 2023 · N663FE · Airbus A300* · Electrical Power SystemSDR FDEA202201300161Dummy Rail · wornFR54/FR54.2 LH NO.3 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300160Dummy Rail · wornFR54/FR54.2 LH NO.2 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300159Dummy Rail · wornFR54/FR54.2 CENTER NO.1 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300158Dummy Rail · wornFR54/FR54.2 RH NO.3 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300157Dummy Rail · wornFR54/FR54.2 RH NO.2 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W SRM 53-15-16-201 PARA 5A PAGE 201-216 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300156Dummy Rail · wornFR38.2/FR40 LH NO.4 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300155Dummy Rail · wornFR38.2/FR40 RH NO.5 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201300154Dummy Rail · wornFR38.2/FR40 RH NO.4 DUMMY SEAT TRACK GAP OVER 1MM. I.A.W A300-600 SRM 53-15-16-201 PARA 5A P201-210 FIG.201 PFM REPAIR ACCOMPLISHED.Jan 30, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201260230Floor Support · corrodedMAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR11 ~ FR13A , Y730MM ACCOMPLISHED THE SUPPORT REPLACED I.A.W A300-600F SRM 51-72-10-001 P2Jan 26, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201230285Crossbeam · corrodedMDCC FLOOR STRUCTURE CROSSBEAM UPR SURFACE WAS FOUND CORROSION AT FR46,FROM - Y330MM TO -Y370MM REPLACED THE CORROSION CROSSBEAM WITH FABRICATED NEW PART I.A.W AIRBUS DRAWNING NUMBER : A53812936 SHEET.A & A300-600F SRM 51-72-10-001, PAGE2 & 53-15-15-001-2Jan 23, 2022 · N663FE · Airbus A300* · Fuselage Floor PanelSDR FDEA202201220242Floor Support · corrodedMAIN DECK LONGITUDIAL FLOOR STRUCTURE UPR SURFACE WAS FOUND CORROSION AT FR12A ~ FR13A , Y1450MM REPAIRED THE DAMAGE AREA WITH TEE SPLICE REPAIR I.A.W. A300-600F SRM 53-12-15-201-2 PARA.5.G P.239-244 FIG.207Jan 22, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202201170275Shear Web · crackedN00253 MAIN DECK FLOOR STRUCTURE'S SHEAR WEB CRACKED AT FR79 160MM,-Y1630MM POS. REPLACED THE WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001 P.2.Jan 17, 2022 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA202108071994Seat Track · brokenSEAT TRACK AT -Y953 AND FR 27 HAS BROKEN LIP. REMOVED AND REPLACED SEAT TRACK -Y953 FR27- FR29 IAW SRM 53-10-16 FIG 201 PARAGRAPH 4. CATEGORY "A" MAJOR REPAIRAug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202108071993Seat Track · shearedSEAT TRACK AT Y0 AND FR 27 HAS BROKEN LIP. EVALUATED DAMAGED SEAT TRACK Y 0 FR 27, FOUND OUT OF LIMITS, IAW SRM 53-10-16, REPAIRED SEAT TRACK IAW SRM 53-10-160 FIGURE 201, FR 26.5 TO FR 27.5. CATEGORY "A" MAJOR REPAIRAug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202108071992Seat Track · shearedSEAT TRACK AT Y450 AND FR 27 HAS BROKEN LIP. EVALUATED DAMAGED SEAT TRACK Y450, FOUND OUT OF LIMITS IAW SRM 53-10-16, REPAIRED SECTION SEAT TRACK Y450 FROM FR 26.5 TO FR 29.5 IAW SRM 53-10-16 FIGURE 201 CATEGORY "A" MAJOR REPAIRAug 7, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202106201574Seat Track · damagedMAIN DECK, ARTICULATING SEAT TRACK IS DAMAGED @ CENTERLINE GUIDE. REPLACED ARTICULATING SEAT TRACK SECTION IAW AIRBUS DWG A53813187000Jun 20, 2021 · N663FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202103150653Cylinder · low pressureAFTER L1 DOOR SLIDE INSTALLATION FOUND L1 DOOR EMERG OP CYL PRESS LOW. SHEAR PIN IN BAD & NIS PDX. ORDERING PART. IDENTIFIED PARTS SHEAR MPN: FE127-100-04 CPN: 5210791 QTY: 1 PART 15MAR21 06:48 PDX U ORDER PART MPN: FE127-100-04 CPN: 5210791 QTYMar 15, 2021 · N663FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202103150654Bottle · low pressureUPON SERVICE CHECK FOUND R1 DOOR SLIDE IN RED BAND. RELEASED FOR SERVICE PER MEL : 52-11-01-01. CREW ENTRY DOOR ESCAPE SLIDE R1 INOP. SLIDE REMAINS INSTALLED ON DOOR. PRESSURE NEEDLE IS ALIGNED WITH THE 'MOVABLE GREEN CURSOR'.Mar 15, 2021 · N663FE · Airbus A300F4605R · Escape SlideSDR FDEA202007301718Coupling · failedDURING DEPARTURE, ECAM FOR HIGH NAC 250 DEG C, TROUBLSHOT NR 2 ENG IAW QRH. NO CHANGE WITH THROTTLE MOVE OR BLEED VALVE OFF. REACHED TOP OF CLIMB FL290 & TEMP DID NOT REDUCE, LOWEST 215, ONCE THROTTLE FWD 240 DEG AT 290. RETURNED TO DEPART, NR 2 MOTORED, RUJul 30, 2020 · N663FE · Airbus A300F4605R · Pneumatic Distribution SystemSDR FDEA201909112202Switch · failedPDIS 663 32-20 1528 11SEP19 MEM OPEN U LOGPAGES:2636365 AFTER GEAR RETRACTION THE NG DOOR LIGHT REMAINED ILLUMINATED. VIBRATION INDICATED THAT THE DOOR WAS OPEN. PER GOC RETURNED TO BASE AFTER RUNNING QRH SHGN 11SEP19 11:28 MEM U DEBRIEFED CSep 11, 2019 · N663FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA2019080761800Floorbeam · crackedMDCC - FR16 -Y1456, FLOOR SUPPORT CRACKED APPROX 1.5 INCH IN LENGTH REPAIRED THE MAIN DECK CRACKED FLOOR SUPPORT AT FR16 -Y1456 PER SRM 53-12-15 FIG 207. THE REPAIR WAS CATEGORY B AND WAS CLASSIFIED AS MAJOR PER GMM 6-2-100.Aug 6, 2019 · N663FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201907291734None · noneEXISTING REPAIR ON MDCC FR29 Y-750 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR29 Y-750 CROSSBEAM WAS EVALUATED AND FOUND NO REPAIR DOCUMENT AND NOT CONFORM ANY REPAIR SCHENE IN CURRENT SRM, REPAIRED IT AGAIN PER A300-600F SRM Jul 29, 2019 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA201907261706Door Frame · noneEXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FR20A BTW S-37R AND S-41R REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON FWD CARGO DOOR FWD CUTOUT FR20A BTW S-37R AND S-41R WAS EVALUATED AND FOUND IN CONFORMITY WITH FEDEX DRAWING SR30-53-001 REV.D,FEJul 26, 2019 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA201907241675Beam · damagedEXISTING REPAIR ON MDCC FR30 Y-750 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR30 Y-750 CROSSBEAM WAS EVALUATED AND FOUND NO REPAIR DOCUMENT AND NOT CONFORM ANY REPAIR SCHENE IN CURRENT SRM, REPAIRED IT AGAIN PER FEDEX EA #: 6-Jul 24, 2019 · N663FE · Airbus A300* · Fuselage Main, StructureSDR FDEA201907241673Beam · unknownEXISTING REPAIR ON MDCC FR60 Y-2462 CROSSBEAM REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC FR60 Y-2462 CROSSBEAM WAS EVALUATED AND FOUND IN CONFORMITY WITH FEDEX EA #: 6-2550-53566A , TITLE: FUSELAGE-MAINFRAME-MIAN DECK CARGO COMPARTMENT FLJul 24, 2019 · N663FE · Airbus A300* · Fuselage Main, Structure
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