N729FD

Service difficulty reports · 228

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 = 'N729FD' 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 FDEA202405240796Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER10 PLUS 4", T/E-27" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMEMay 24, 2024 · N729FD · Airbus A300B4622R · Elevator StructureSDR FDEA202405240795Elevator · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON RH ELEVATOR LWR SKIN AT ER13 6", T/E-8" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS May 24, 2024 · N729FD · Airbus A300B4622R · Elevator StructureSDR FDEA202405240774Skin · noneAIRCRAFT REPAIR ASSESSMENT: EXISTING COMPOSITE REPAIR FOUND ON LH ELEVATOR UPR SKIN AT ER6~7, T/E-39" COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES - REPAIR CATALOG - A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CMay 24, 2024 · N729FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202405230993Skin · corrodedRH WING UPPER SKIN LOWER SURFACE FOUND CORRODED BEHIND REAR SPAR BETWEEN RIB27 AND RIB28 ACCESS FROM 690BB ACCOMPLISHED THE REINFORCING DOUBLER REPAIR AT RH WING UPPER SKIN PANEL NO.3, REAR SPAR, RIB25~29 I.A.W FEDEX EA NO:T6-5730-T0379408 P1, SEQ NO:1260,May 23, 2024 · N729FD · Airbus A300B4622R · Wing, Plate/SkinSDR FDEA202405230812Plate · crackedFWD CARGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L,FR21 POSITION INSTALLED THE NEW PLATE WITH FASTENERS AT FWD CARGO FLOOR AREA FR20-21 S-43L~44L I.A.W A300-600 SRM 51-72-10-001, PAGE.2 & 51-40-21-001, PARA.7, PAGE.24~50, THE REPAIR CLASSMay 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230784Floor Support · crackedMAIN DECK FLOOR STRUCTURE SUPPORT PROFILE-Z CRACK AT FR80 PLUS 4", Y1450 POSITION REPLACED SUPPORT PROFILZ-Z WITH FASTENERS AT FR80 PLUS 4", Y1450 POSITION I.A.W A300- 600 SRM 51-72-10-001,PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B~23 NOTE:SDR (NO:24-0734 & 24May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230782Bracket · crackedAFT CARGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT CENTER LINE,FR54 POSITION. CRACKED SUPPORT BRACKET REPLACED NEW PART. INSTALLED WITH RIVETS I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001,PARA.6, PAGE.7B-23, THIS REPAIR CLASSIFIED May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230781Support · crackedAFT CARGO COMP'T CEILING PANEL SUPPORT CRACK AT ENTRY AREA BETWEEN FR60~FR61 POSITION. CRACKED SUPPORT REPLACED NEW PART. INSTALLED WITH RIVETS I.A.W A300-600 SRM 51-72-10- 001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23, THIS REPAIR CLASSIFIED AS MINOR PEMay 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230780Bracket · crackedAFT CARGO COMP'T FWD PRESSURE BULKHEAD SUPPORT BRACKET CRACK AT -Y1959,FR54 POSITION. CRACKED SUPPORT BRACKET REPLACED NEW PART. INSTALLED WITH RIVETS I.A.W A300-600 SRM 51-72-10-001, PAGE.2 AND 51-40-21-001,PARA.6 PAGE.7B-23, THIS REPAIR CLASSIFIED AS MMay 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230779Bracket · corrodedNOSE LANDING GEAR BAY FOUND HYD TUBE 1EA CLAMP SUPPORT BRACKET CORROSION AT FWD-RH AREA. REPLACED CORROSION SUPPORT BRACKET AT NOSE LANDING GEAR BAY WITH FASTENERS I.A.W A300-600 SRM 51-72-10-001,PAGE.2 & 51-40-21-001, PARA.6, PAGE.7B~23, THE REPAIR CLASSIMay 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230778Skin · delaminated1EA WATER STRAPPED AREA (50MMX60MM)WAS FOUND AT ER5 OF LH ELEVATOR TOP SKIN. REPAIRED THE DAMAGE AREA WITH CORE AND PLIES AT ER5 OF LH ELEVATOR TOP SKIN I.A.W A300-600 SRM 55-21-12-201-2, PARA.5J, PAGE.266-269,FIG.212(SHEET 2) & 51-77-12-201, PARA.2A(2), PMay 23, 2024 · N729FD · Airbus A300B4622R · Elevator, Plate/SkinSDR FDEA202405230766Fitting · crackedAVIONICS COMP'T CABIN FLOOR CROSSBEAM OF PICK UP FITTING CRACK AT FR10,Y-953 POSITION REPLACED THE NEW BRACKET. I.A.W A300-600 SRM 51-72-10-001,P2(POS:CABIN FLOOR CROSSBEAM AT FR10,Y-953).THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230739Profile · crackedMAIN DECK FLOOR STRUCTURE SUPPORT PROFILE-Z CRACK AT FR80 PLUS 4", Y1450 POSITION REPLACED SUPPORT PROFILZ-Z WITH FASTENERS AT FR80 PLUS 4", Y1450 POSITION, I.A.W A300- 600 SRM 51-72-10-001,PAGE.2 & 51-40-21-001, PARA.6, PAGE 7B~23 THE REPAIR CLASSIFIED AS May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230737Shear Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK AT FR79 PLUS 5" ,-Y1620 POSITION REPLACED SHEAR WEB WITH FASTENERS AT FR79 PLUS 5",-Y1620 POSITION, I.A.W A300-600 SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.7,PAGE 24~50, THE REPAIR CLASSIFIED AS MINOR PER GMM 6May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230736Profile · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK AT FR79 PLUS 5",-Y1620 POSITION REPLACED SHEAR WEB WITH FASTENERS AT FR79 PLUS 5",-Y1620 POSITION, I.A.W A300-600 SRM 51-72-10-001,PAGE 2 & 51-40-21-001, PARA.7,PAGE 24~50 THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230735Profile · crackedMAIN DECK FLOOR STRUCTURE SUPPORT PROFILE-Z CRACK AT FR80 PLUS 4",-Y1450 POSITION REPLACED SUPPORT PROFILE-Z WITH FASTENERS AT FR80 PLUS 4",-Y1450 POSITION, I.A.W A300- 600 SRM 51-72-10-001, PAGE 2 & 51-40-21-001, PARA.6, PAGE 7B~23 THE REPAIR CLASSIFIED AS May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230734Support · crackedMAIN DECK FLOOR STRUCTURE SUPPORT PROFILE-Z CRACK AT FR80 PLUS 4", Y1450 POSITION REPLACED SUPPORT PROFILZ-Z WITH FASTENERS AT FR80 PLUS 4", Y1450 POSITION, I.A.W A300- 600 SRM 51-72-10-001,PAGE.2 & 51-40-21-001, PARA.6, PAGE 7B~23 THE REPAIR CLASSIFIED AS May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405230733Web · crackedMAIN DECK FLOOR STRUCTURE SHEAR WEB CRACK AT FR79 5", -Y1620 POSITION REPLACED SHEAR WEB WITH FASTENERS AT FR79 5",-Y1620 POSITION, I.A.W A300-600 SRM 51-72- 10-001,PAGE 2 & 51-40-21-001, PARA.7,PAGE 24~50May 23, 2024 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202405180962Fitting · crackedTHE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT F23 ACCOMPLISHED THE REPLACEMENT OF BEARING FITTINGS AT MAIN DECK CARGO DOOR FR23-24 LONGN1~LONGN3 IAW FEDEX EA NO:T6-5230-T0379211 P1, SEQ NO:1252, TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CAMay 18, 2024 · N729FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202405180948Fitting · crackedTHE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTING WAS FOUND CRACK AT F23. ACCOMPLISHED THE REPLACEMENT OF BEARING FITTINGS AT MAIN DECK CARGO DOOR FR23-24 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0379211 P1, SEQ NO:1252, TITLE:DOORS-CARGO DOOR/HYD SYS-MAINMay 18, 2024 · N729FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202302010192Cylinder · not enteredL-1 DOOR ASSIST BOTTLE BLOWN RELEASED FOR SERVICE PER MEL : 52-XX-XX CREW ENTRY DOOR L1 - INOP." (EMERGENCY DOOR OPENING BOTTLE BLOWN DURING F.O.M. OF L1 DOOR NOT DISENGAGING SLIDE BY FLIGHT CREW. MX WILL REQUIRE REPLACEMENT OF BOTTLE DIAPHRAM FOR SERVICFeb 1, 2023 · N729FD · Airbus A300* · Passenger/Crew DoorsSDR FDEA202302010189Mechanism · dirtyL-1 DOOR WILL NOT DISARM. RELEASED FOR SERVICE PER MEL : 52-XX-XX INOP. SLIDE REMAINS INSTALLED ON DOOR." MEL: 52-XX-XX. - (REPORTED ON SEPERATE SDR) DURING MX, L1 DOOR EMERGENCY ASSIST BOTTLE WAS BLOWN DURING MX ACTION TO RELEASE SLIDE GIRT BAR MECAHNISFeb 1, 2023 · N729FD · Airbus A300* · Passenger/Crew DoorsSDR FDEA202210182592Line · crackedDURING FLIGHT, BLUE RESERVOIR LOW. TURNED OFF PUMP. COMPLIED WITH QRH. EMERGENCY DECLARED. REMOVED OVAL LT AND RT PYLON PANEL NR 1 ENG. FOUND CASE DRAIN LINE CRACKED OR HAS A HOLE. WILL HAVE TO REMOVE TOP PYLON PANEL & REMOVE INTERCOOLER TO GAIN ACCESS. Oct 18, 2022 · N729FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202208181995Selector Valve · failedDURING FLIGHT, GREEN HYD SYSTEM QUANTITY DROPPED TO THE RED DOT. FOLLOWED QRH. CRANKED THE GEAR. STOPPED ON RWY. APPEARS THE HYD LEAK IS COMING FROM THE BOTTOM ELBOW OF LANDING GEAR SELECTOR 3GA. WE WILL REPACK ELBOW WITH NEW BACK UP WASHER AND O-RING. WIAug 18, 2022 · N729FD · Airbus A300B4622R · Hydraulic Indicating SystemSDR FDEA202208171989O-Ring · damagedPASSING 22,000 FT, ECAM DIRECTED GREEN PUMPS OFF AND GREEN SYSTEM PRESSURE INDICATED ZERO ON BOTH ECAM SCHEMATIC PAGE AND OVERHEAD HYDRAULIC GAGE. RAN QRH HYD SYS LO PR FOLLOWED BY HYD RSVR LO LEVEL CHECKLISTS, USED FREE FALL EXTENSION CHECKLIST, DECLAREAug 17, 2022 · N729FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202112063089Floor Panel · damagedMAIN DECK CARGO COMPT #241LK FLOOR PANEL WAS EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600 SRM 53-10-20-201 PARA. 9A, P. 205-206 FIG. 201.Dec 6, 2021 · N729FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202112063088Floor Panel · damagedMAIN DECK CARGO CARGO COMPT #232EF FLOOR PANEL WAS EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600 SRM 53-10-20-201 PARA. 9A, P. 205-206 FIG. 201.Dec 6, 2021 · N729FD · Airbus A300* · Fuselage Floor PanelSDR FDEA202112063086Floor Panel · damagedMAIN DECK CARGO COMPT #231RH FLOOR PANEL WAS EDGE DAMAGED. ACCOMPLISHED THE FLOOR PANEL REPAIR I.A.W. A300-600 SRM 53-10-20-201 PARA. 9A, P. 205-206 FIG. 201.Dec 6, 2021 · N729FD · Airbus A300* · Fuselage Floor PanelSDR FDE2022F00000None · crackedDURING E.A NO.T6-5710-114908 B P2 FOUND HOLE 6 LHS DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P4 (SEQ NO: 000895) AND A300-600 SRM 5Nov 29, 2021 · N729FD · Airbus A300* · Wing StructureSDR FDEA202111292949None · crackedDURING E.A NO.T6-5710-114908 B P2 FOUND HOLE 6 LHS DEVIATION. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P4 (SEQ NO: 000895) AND A300-600 SRM 5Nov 29, 2021 · N729FD · Airbus A300* · Wing StructureSDR FDEA202111263130None · cracked1EA CRACK INDICATION WAS FOUND AT L/H SIDE HOLE 166 ON THE INTERNAL ANGLE ON FR47. (DEPTH LENGTH 16MM) ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-11490Nov 26, 2021 · N729FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202111263124None · cracked1EA CRACK INDICATION WAS FOUND AT HOLE H ON THE INTERNAL ANGLE ON FR47. ACCOMPLISHED THE WORK: REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE/FRAME 47 FASTENER HOLE REPAIRS (RH AND LH SIDES) I.A.W. EA NO: T6-5710-114908 C P6 (SEQ NO: 000897) AND A300Nov 26, 2021 · N729FD · Airbus A300* · Wing Main, Frame StructureSDR FDEA202111242982Seat Track · corrodedTHE Z220 FLOOR SEAT TRACK FR14-FR19 Y-953 WAS FOUND CORROSION. REPLACED THE CORROSION SEAT TRACK WITH NEW PART. I.A.W. A300-600 SRM 51-72-10-001 PAGE.2, 51-40-21-001 PARA.7 PAGE.24-50.Nov 24, 2021 · N729FD · Airbus A300* · Fuselage Structure (General)SDR FDEA202111233093Skin · dentedTHE RH FUSELAGE WAS FOUND 1EA DENT AT FR 55 5.5" STRG 36R ACCOMPLISHED DENT SKIN CAT.B REPAIR I.A.W A300-600 SRM 53-10-12-201, PARA5 PAGE.343-346 FIG224(SHEET1) AND SRI 53-10-12-201, IIR 53-10-12-2-004-00, PARA3D TABLE208 FIG204Nov 23, 2021 · N729FD · Airbus A300* · Fuselage Main, Plate/SkinSDR FDEA202111162986None · damagedRUDDER R/H SIDE PANEL NO.39 SCREW FOUND STAGNANT WATER 2EA WATER TRAPPED AREAS (120MM*185MM & 35MM*160MM) WERE FOUND AT NO.39 SCREW OF RH RUDDER SIDE PANEL ACCOMPLISHED THE CAT.B REPAIR I.A.W FEDEX EA NO:6-5540-T0365512 P1(SEQ888) TITLE:STABILIZERS-RUDDENov 16, 2021 · N729FD · Airbus A300* · Rudder StructureSDR FDEA202111162985None · damagedRUDDER R/H SIDE PANEL NO.20 FOUND STAGNANT WATER 1EA WATER TRAPPED AREA (50MM*100MM) WAS FOUND AT NO.20 SCREW OF RH RUDDER SIDE PANEL ACCOMPLISHED THE CAT.B REPAIR OF SKIN DAMAGE AT SCREW LINE IN REPAIR ZONE.P I.A.W A300-600 SRM 55-41-12-201, PARA31B, P3Nov 16, 2021 · N729FD · Airbus A300* · Rudder StructureSDR FDEA2020021470326Flap · damagedPDIS 729 27-80 5120 07FEB20 IAD OPEN U LOGPAGES:3206390 ON APPROACH TO IAD, WHEN SLATS EXTENDED, RECEIVED KRUGER NOT EXTENDED, COMPLIED WITH QRH. FACT 16FEB20 19:39 MEM REMOVED AND REPLACFeb 7, 2020 · N729FD · Airbus A300B4622R · Leading Edge DevicesSDR FDEA202001020004Uplock · malfunctionedAFTER SELECTING LANDING GEAR UP, LEFT GEAR DOOR WOULD NOT CLOSE. ALSO HAD RED "UNLK" ON LEFT GEAR. GEAR EXTENDED NORMALLY. PER CREW DEBRIEF, POSITION SYS 1 WAS NEVER SELECTED. SYSTEM 2 WAS SELECTED THE WHOLE TIME. SYSTEM 2 HAS HISTORY. R/R LT MLG DOOR UPJan 2, 2020 · N729FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA201907161621Smoke Detector · failedPDIS 729 26-12 4562 16JUL19 MEM OPEN U LOGPAGES:2907154 AVIONICS SMOKE MASTER WARNING AT 40 KNOTS. REJECTED THE TAKEOFF REPEAT GRIPE. REMOVED AND REPLACED AVIONICS SMOKE DETECTOR 13WA PER MM CH. 26-15-12-04.Jul 16, 2019 · N729FD · Airbus A300B4622R · Smoke DetectionSDR FDEA2019062751406Support · corrodedAFT CARGO BAY FRAME 58, Y1470 ROLLER TRAY SUPPORT WAS CORRODED. REMOVED THE CORROSION, MATERIAL REMOVED WAS OVER 50% OUT OF LIMITS IAW SRM 51-22-00, REPAIRED IAW SRM 53-10-15, FIG 207. MAJOR REPAIR.Jun 25, 2019 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA2019062751405Attach Fitting · corrodedAFT CARGO COMPARTMENT FRAME 56 ROLLER TRAY -Y1470 ATTACHMENT STRUCTURE HAD CORROSION. REMOVED CORROSION, MATERIAL REMOVED WAS OVER 50% OUT OF LIMITS IAW SRM 51-22-00, REPAIRED IAW SRM 53-10-15 FIG 207, MAJOR REPAIR.Jun 25, 2019 · N729FD · Airbus A300B4622R · Fuselage Main, Attach FittingsSDR FDEA2019062091368Floor Panel · damagedFLOOR PANEL 131HG FWD PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL ON TRAVELER T19/1418730 IAW SRZ-25-005. MAJOR REPAIRJun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091374Floor Panel · damagedFLOOR PANEL 151KF AFT PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL 151KF ON TRAVELER T19/1418778 IAW SRZ-25-005 MAJOR REPAIRJun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091371Floor Panel · damagedFLOOR PANEL 137ZF FWD PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL 131ZF ON TRAVELER T19/1418845 IAW SRZ-25-005. MAJOR REPAIR.Jun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091373Floor Panel · damagedFLOOR PANEL 132YF FWD PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL 132YF ON TRAVELER T19/1418842 IAW SRZ-25-005. MAJOR REPAIR.Jun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091372Floor Panel · damagedFLOOR PANEL 131QF FWD PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL 131QF ON TRAVELER T19/1418774 IAW SRZ-25-005. MAJOR REPAIR.Jun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091370Floor Panel · damagedFLOOR PANEL 152HF AFT CARGO PIT IS DAMAGED. FABRICATED NEW FLOOR PANEL ON TRAVELER T19/1418844 IAW SRZ-25-005. MAJOR REPAIRJun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019062091367Floor Panel · damagedFLOOR PANEL 152GF AFT CARGO IS DAMAGED. FABRICATED NEW FLOOR PANEL 152GF ON TRAVELER T19/1418779 IAW SRZ-25-005. MAJOR REPAIRJun 19, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA201906071258Floor Panel · damagedMAIN DECK CARGO COMPT 231VG FLOOR PANEL BROKEN. FABRICATED 231VG FLOOR PANEL ON VT MAE TRAVELER T19/1418726 IAW DWG SRZ-25-005. CAT "A" MAJOR REPAIRJun 7, 2019 · N729FD · Airbus A300B4622R · Fuselage Floor PanelSDR FDEA2019060301192Profile · crackedMAIN DECK CARGO COMPT PROFILE - Z CRACKED BETWEEN Y0 AND Y-450 AT FR80 REMOVED PROFILE -Z AT MAIN DECK CARGO COMPT Y0 TO Y-450 FR80 IAW SRM 51-40-21. LOCATED AND DRILLED NEW PROFILE - Z IAW SRM 51-40-44. INSTALLED PROFILE - Z IAW SRM 51- 40-21. CAT "A" MAJOMay 30, 2019 · N729FD · Airbus A300B4622R · Fuselage Miscellaneous Structure
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