N751FD

Service difficulty reports · 308

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 = 'N751FD' 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 FDEA202602100164Cable · incorrectDURING INSPECTION OF THE L1 DOOR SLIDE (PN: D30546-509, SN: C1384) FOUND THE BREAKAWAY WIRE ON THE RELEASE CABLE INCORRECT. CMM: 25-61-39 REPLACED THE PACKBOARD RELEASE CABLE SAFETY WIRE WITH MS20995C15 REFERENCE FEA: 6-2560-F0386261 REV A P1 AND CMM 25Feb 10, 2026 · N751FD · Airbus A300B4622R · Escape SlideSDR FDEA202512192262Battery Pack · inoperativeDURING POST FLIGHT NONE OF THE EMEGENCY LIGHTING WILL TEST. REMOVED AND REPLACED BATTERY FOR POWER SUPPLY 29WL, ALL EMERGENCY LIGHTING OPS CHECKED GOOD, REF AMM 33-51-14-04. OK TO CONTINUE SERVICE.Dec 19, 2025 · N751FD · Airbus A300B4622R · Emergency LightingSDR FDEA202509041616Pitot Tube · cloggedON TAKEOFF ROLL, CAPTAIN S AIRSPEED SHOWED 95 KTS WHILE FO SIDE SHOWED 60 KTS. TAKEOFF REJECTED. PERFORMED FLIGHT ENVIRONMENT DATA BITE TEST PER A300 AMM 34-10-00-05, TEST PASSED, NO FAULTS NOTED. PERFORMED VISUAL INSPECTION OF F/O PITOT TUBE PER A300 AMMSep 4, 2025 · N751FD · Airbus A300B4622R · Pitot/Static SystemSDR FDEA202506261054Hydraulic Line · damagedDURING CLIMB OUT OF KMEM GOT ECAM YELLOW HYD SYS LO PRESSURE. THE YELLOW RESERVOIR SHOWED ZERO QUANTITY. COMPLETED THE ECAM AND QRH PROCEDURES. CONSULTED GOC, AND THEY HAD US CONTINUE TO KMSN. COMPLETED THE FLIGHT. FOUND YELLOW SYS PRESSURE FLEX LINE TO LH AIJun 26, 2025 · N751FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202404050466Web · bentTHSA COMPARTMENT FOUND 1EA SUPPORT WEB GOT DEFORM AT FR85-86, S-33R REPLACED THE DAMAGED SUPPORT WEB WITH NEW ONE. I.A.W A300-600 SRM 51-72-01-001, PAGE.2 AND 51-40-21-001, PARA.6, PAGE.7B-23 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT FR85~86, S-33R.Apr 5, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202404040291Rib · crackedPFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB 19 BTWN REAR SPAR ~ STRG 2.8 . ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-57Apr 4, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202404040479Skin · crackedPFM E.A #:6-5750-T0378613 P1 FOUND NEW CRACK AT LH WING CTR FLAP RIB19 BTWN REAR SPAR ~ STRG2.8. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.19 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-Apr 4, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190293Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190292Rib · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190290Rib · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613 Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190289Rib · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT SMar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190288Rib · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190287Rib · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE: WINGS-FLIGHT SURFACES-RH CENTER FLAP; CMar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190481Skin · cracked2EA CRACKS WERE FOUND AT RH WING CENTER FLAP RIB26 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE CAT.A MAJOR FLANGES REPAIR AT RH CENTER FLAP RIB26 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS-FLIGHT SURFACES-RH CENTER FLAP; Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190480Skin · cracked1EA CRACK WAS FOUND AT RH WING CENTER FLAP RIB27 FWD AREA OF TOP SURFACE RIB FLANGE ACCOMPLISHED THE CAT.A MAJOR FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT RH CENTER FLAP RIB27 I.A.W FEDEX EA NO:T6-5750-T0378627 A P1, SEQ NO:1171, TITLE:WINGS- FLIGHT SUMar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190478Skin · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB26 AFT AREA OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.26 S-2.7~S-2.8, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR I.A.W FEDEX EA NO:T6-5750- T0Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190477Skin · cracked1EA CRACK WAS FOUND AT LH WING CENTER FLAP RIB18 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGE REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.18 S-2.8~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FMar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190476Skin · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB12 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AT LH CENTER FLAP RIB.12 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5750-T0378613Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403190475Skin · cracked2EA CRACKS WERE FOUND AT LH WING CENTER FLAP RIB11 AFT AREAS OF TOP SURFACE RIB FLANGE. ACCOMPLISHED THE FLANGES REPAIR AND EXTERNAL DOUBLER REPAIR AT LH CENTER FLAP RIB.11 S-2.7~REAR SPAR, THE REPAIR CLASSIFIED AS CAT.A MAJOR REPAIR PER GMM 6-2-100 I.A.W Mar 19, 2024 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202403150438Rib · gougedLH WING SPOILER #6 ACTUATOR INBD JACK RIB LOWER HOLE GOUGE ACCOMPLISHED THE CAT.A REINFORCEMENT REPAIR AT LH WING #6 SPOILER JACK RIB STA SP1X 31.675, THIS REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 I.A.W FEDEX EA NO:T6-5740- T0378536 P1, SEQ NO:1164, TITLEMar 15, 2024 · N751FD · Airbus A300B4622R · Wing, Rib/BulkheadSDR FDEA202403140339None · none00087567N00574 AIRCRAFT REPAIR ASSESSMENT : EXISTING COMPOSITE REPAIR FOUND ON AFT CGO FLOOR PNL 152FF TOP SIDE BTW FR56~57.1, -Y805 TO -Y1470 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIMar 14, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403140324Floor Panel · noneEXISTING COMPOSITE REPAIR FOUND ON AFT CGO FLOOR PNL 152EF TOP SIDE BTW FR56~57, -Y140 TO -Y805 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, INSPECTION OF EXISTING REPAIR DETERMINED IT TO BE CURRENT WITH FAA APPROVED DATA: A300-600 SRM 53-10-20Mar 14, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403130420Adapter · gougedMAIN DECK FLOOR STRUCTURE FOUND 1EA CLS T-ADAPTER GOT SOME GOUGED MARKS LOCATION AT FR61 , Y1456 THRU Y1959 REPLACED THE DAMAGED ADAPTER WITH NEW ONE.I.A.W A300-600 SRM 51-72-10-001, PAGE2 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 (AT FR61, Y1456 TO Y1959Mar 13, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403120422None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON STRINGER BTW FR57.2~57.3, S-35L COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403120418Adapter · gougedMAIN DECK FLOOR ADAPTER GOUGE 2EA AT FR62 -Y700 AND -Y875 REPLACED THE GOUGE ADAPTER WITH NEW PART. AT MAIN DECK FLOOR FR62 -Y700 AND -Y875. I.A.W A300-600 SRM 51-72-10-001 PAGE2 & 51-40-21-001 PARA7 PAGE24~PAGE50. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-1Mar 12, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403120360None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR63-64, S-49L. COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403120344None · none00087567N00360 AIRCRAFT REPAIR ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON FWD CARGO COMPT FLOOR CROSSBEAM BTW Y805 TO -Y805, FR38.2 COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION Mar 12, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403110278Support Frame · crackedTHE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK AT FR23 FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO: T6- 5230-T0378435 P1, SEQ NO:1175 TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ALTUATOR BEARING FITTING REPLMar 11, 2024 · N751FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202403110340None · noneAIRCRAFT REPAIR ASSESSMENT : EXISTING COUPLING REPAIR FOUND ON STRINGER BTW FR62- 64, S-48L COMPLIED WITH ATTACHMENT B OF EO: E6-5100-7-5000 D7 PT1, TITLE: STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.707, IMar 11, 2024 · N751FD · Airbus A300B4622R · Standard Practices/StructuresSDR FDEA202403100421Support Angle · corrodedFWD CGO COMP'T UNDER ROLLER TRACK SUPPORT ANGLE TOP SKIN CORRODED AT FR31-FR32, S-43L POSITION. REMOVED DAMAGE ANGLE AND INSTALLED NEW ONE. IAW A300-600 SRM 51-40-21-001, PARA.6 PAGE 7B-PAGE23 & 51-72-10-001, PAGE2. THIS REPAIR CLASSIFIED AS MINOR PER GMM Mar 10, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403090419Floor Support · corrodedMAIN DECK COURIER AREA FOUND 1EA FLOOR SUPPORT CORRODED POSITION AROUND SEVERAL OF ATTACHMENT HOLES LOCATION FROM FR11 TO FR15A AND Y953 ACCOMPLISHED THE REPLACEMENT OF FLOOR SUPPORT AT FR11 TO FR15A AND Y953, REPAIR CLASSIFIFED AS MINOR PER GMM 6-2-100 I.Mar 9, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403080417Beam · corrodedREAR FUSELAGE L/H HORIZONTAL STAB CUTOUT EDGE BEAM GOT A PROFILE CORRODED AT FR89 PLUS 8", S-27L REPLACED THE DAMAGED BEAM WITH NEW ONE. I.A.W A300-600 SRM 51-72-10-001, PAGE 2 AND 51-40-21-001 PARA7 P24-P50 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 ( AMar 8, 2024 · N751FD · Airbus A300B4622R · Fuselage Main, StructureSDR FDEA202403060463Plate · crackedFWD CGO COMP'T UNDER FLOOR AREA LH SIDE PLATE CRACK AT S-43L~S-44L AND FR21 POSITION. REPLACED THE SIDE PLATE WITH NEW PART AT FR21 AND S-43L~44L, REPAIR CLASSIFIED AS MINOR REPAIR IAW SRM 51-72-10-001, PAGE 2 & 51-40-21-001, PARA 6~7, PAGE 7B~50Mar 6, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403060412Floor Support · corrodedBULK CGO COMP'T FLOOR BEAM TOP SKIN CORROSION BTW FR66-FR68,Y140 POSITION. REPLACED THE NEW PROFILE, LONGITUDINAL BTW FR66~FR68, Y140. I.A.W A300-600 SRM 51-72-10-001, P2. THIS REPAIR CLASSIFIED AS MINOR, PER GMM 06-2-100Mar 6, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403040411Header · bentAFT CGO COMP'T CEILING PNL SUPPOPRT DEFORM AT ENTRY AREA BTWFR60-FR61 POSITION. REPLACED THE DEFORM CEILING PNL SUPPORT WITH NEW PART. AT AFT CGO COMPONENT CEILING PANEL. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100. I.A.W A300-600 SRM 51-72-10-001 PAGE2Mar 4, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403030434Floor Support · crackedMAIN DECK FLOOR ONE SUPPORT CRACK NEAR FR38.1 PLUS 5" STGR26R. REPLACED THE NEW SUPPORT. I.A.W A300-600 SRM 51-72-10-001,P2 NEAR FR38.1 PLUS 5" STGR 26R. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403030414Adapter · gougedMAIN DECK FLOOR ADAPTER GOUGE AT FR64 -Y1456 TO -Y1959 REPLACED THE DAMAGED ADAPTER WITH NEW ONE.I.A.W A300-600 SRM 51-72-10-001, PAGE2 REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 (AT FR64, Y1456 TO -Y1959)Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403030413Shear Web · damagedMAIN DECK FLOOR SHEAR WEB BROKEN AT FR79 5" Y1630 REPLACED THE NEW PLATE, SHEAR. I.A.W A300-600 SRM 51-72-10-001,P2 NEAR FR79 5" Y1630. THIS REPAIR CLASSIFIED AS MINOR PER GMM 06-2-100.Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403030252Profile · crackedMAIN DECK FLOOR Z-PROFILE CRACK AT FR80/82 -Y1480 REPLACED THE NEW PROFILE-Z AT FR80/82 -Y1480.I.A.W A300-600 SRM 51-72-10-001,P2, THIS REPAIR CLASSIFIED AS MINOR PER GMM06-2-100Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202403030251Profile · crackedMAIN DECK FLOOR Z-PROFILE CRACK AT FR80/82 Y1480 [TS3RJ00C7E0U] REPLACED THE NEW PROFILE-Z AT FR80/82 Y1480 .I.A.W A300-600 SRM 51-72-10-001, P2, THIS REPAIR CLASSIFIED AS MINOR PER GMM06-2-100Mar 3, 2024 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202402290277Support Frame · crackedTHE MDC DOOR ACTUATOR YOKE AFT SUPPORT FRAME WAS FOUND CRACK FABRICATED NEW SUPPORT FRAMES AND INSTALLED WITH FASTENERS I.A.W FEDEX EA NO: T6- 5230-T0378435 P1, SEQ NO:1175 TITLE:DOORS-CARGO DOOR/HYD SYS-MAIN CARGO DOOR ALTUATOR BEARING FITTING REPLACEMENT Feb 29, 2024 · N751FD · Airbus A300B4622R · Cargo/Baggage DoorsSDR FDEA202305080824Structure · damagedDURING ULTRASONIC INSPECTION IAW A300 NTM 57-0-45 PT 4. PROCEDURE A R/H LOWER WING BOX HOLE #1 CRACKED ON THE FWD SIDE OF THE FASTENER APPROXIMATELY 1/8" LONG. MARKED FASTENER WITH A "X" FOR IDENTIFICATION REAMED HOLE TO .593" AND INSTALLED A EN 6114-9-Y29 HMay 8, 2023 · N751FD · Airbus A300* · Standard Practices/StructuresSDR FDEA202206161443Sensor · failedPDIS 751 32-30 3421 16JUN22 YMX OPEN U LANDING GEAR LEVER INTERLOCKED CAUTION ON SYS 1 RIGHT AFTER CAPT TAT AND PITOT PROBE HEAT FAULTS. NO ISSUES ON SYS 2.MEL 16JUN22 12:44 YMX U RELEASED FOR SERVICE PER MEL : 32-30-01-B CATEGORY : C EXPIJun 16, 2022 · N751FD · Airbus A300* · Landing Gear Retraction/Extension SystemSDR FDEA202109062223Floor Support · corrodedMAIN DECK FR12A-FR14 -Y1959 FLOOR SUPPORT CORRODED REPAIRED THE MAIN DECK FR12A-FR14 -Y1959 CORRODED FLOOR SUPPORT PER A300-600 SRM53-12-15-201. PARA.G. FIG207. THIS IS CATEGORY B REPAIR. THE REPAIR MUST BE INSPECTED AT DEFINED INTERVALS PER A300-600 SRISep 6, 2021 · N751FD · Airbus A300B4622R · Fuselage Miscellaneous StructureSDR FDEA202105261403Transmitter · crackedPDIS 751 29-30 2383 26MAY21 MEM OPEN U PASSING FL330 ON DESCENT TO MEM GREEN SYS RESERVOIR LOW LEVEL ILLUMINATED. GREEN SYSTEM SHOWED AT THE RED DOT. COMPLIED WITH ALL ECAM AND QRH PROCEDURES INCLUDING GRAVITY GEAR EXTENSION. FACT 26MAY21May 26, 2021 · N751FD · Airbus A300B4622R · Hydraulic Indicating SystemSDR FDEA202105201316Skin · dentedR/H IINBOARD FLAP, OUTBOARD TRAILING EDGE, LOWER SURFACE, HAS DENT MWT REPAIR PER SRM 57-50-00 FIG. 205May 20, 2021 · N751FD · Airbus A300B4622R · Trailing Edge FlapsSDR FDEA202105041100B-Nut · looseAFTER TAKEOFF, GEAR RETRACTED AND FLAPS RETRACTED GOT ECAM GREEN PRESSURE LOW, FOLLOWED BY GREEN FLUID QUANTITY LOW. FOLLOWED ECAM, MANUALLY EXTENDED GEAR. STOPPED ON THE RUNWAY AND TOWED TO THE GATE FOUND HYD FLUID POURING FROM #1 ENG, OPENED ENG AND May 4, 2021 · N751FD · Airbus A300B4622R · Hydraulic System, MainSDR FDEA202105031081Actuator · leakingMOMENTS AFTER GEAR RETRACTION WE HAD AN INDICATION OF A TOTAL LOSS OF GREEN HYDRAULIC FLUID. BOTH ECAM HYDRAULIC PAGE AND ANALOG GAUGE SHOWED ZERO. EMERGENCY DECLARED. MOCC AND GOC NOTIFIED. COMPLIED WITH ECAM AND QRH FOR MANUAL GEAR EXTENSION. AFTER GEARMay 3, 2021 · N751FD · Airbus A300B4622R · Landing Gear Retraction/Extension SystemSDR FDEA202103250778Indication Sys · inoperativeWHEN ARMING SLICED FOR DEPARTURE, R1 DOES NOT INDICATE ARMED RELEASED FOR SERVICE PER MEL : 52-30-04 CATEGORY : C EXPIRATION : 04APR21 "MEL 52-30-04: ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS Mar 25, 2021 · N751FD · Airbus A300B4622R · Door Warning SystemSDR FDEA202010152513Power Supply · damagedBOTH LT AND RT MAIN CABIN ENTRY DOORS ESCAPE SLIDE RELEASE WARNING SYSTEM LIGHTS INOPERABLE. RELEASED FOR SERVICE PER MEL: 52-XX-XX-XX CATEGORY: C "MEL 52-XX-XX-XX: L1 AND R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS INOPERABLE. FACT 15OCT20 18:37Oct 15, 2020 · N751FD · Airbus A300B4622R · Door Warning System
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