N654FE

Service difficulty reports · 237

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 = 'N654FE' 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 FDEA202607100898Glide Slope · malfunctionedON RNAV APPROACH RW 21, ON GLIDEPATH AND CONFIGURED FOR LANDING GOT GLIDESLOPE GLIDESLOPE REPEATEDLY STARTING AT 100 FEET UNTIL TOUCHDOWN.Jul 10, 2026 · N654FE · Airbus A300F4605R · Glide Slope SystemSDR FDEA202604290521Power Supply · failedON POST FLIGHT FOUND L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. DURING TEST, BOTH ASSOCIATED WARNING BUZZERS OPERATE NORMALLY. MEL 52-73-01-01: L1 & R1 CREW ENTRY DOOR ESCAPE SLIDE WARNING SYSTEM LIGHTS - INOP. REMOVED AND REPLACEApr 29, 2026 · N654FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202512022217Battery · failedWITH R1 ENTRY DOOR ARMED NO ECAM INDICATION PRESENT. RELEASED FOR SERVICE PER MEL 52-30-04. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR INOPERATIVE. DOOR ESCAPE SLIDE ARMING SYS IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE. R & R TWO BATTERIESDec 2, 2025 · N654FE · Airbus A300F4605R · Door Warning SystemSDR FDEA202511192195Girt Bar · fodR1 DOOR SLIDE WILL NOT ARM. ECAM SLIDE INDICATION SYSTEM FOR R1 DOOR - INOP. DOOR ESCAPE SLIDE ARMING SYSTEM IS TO BE VERIFIED AS FULLY ARMED PRIOR TO EACH DEPARTURE.MSN DID A GVI OF GIRT BAR FOR DEBRIS & OPERATION IAW AMM 25-61-21-04, NO DEFECTS NOTED. Nov 19, 2025 · N654FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202508291567Door · crackedMAIN DECK CARGO DOOR UPR EDGE AT PT1 BETWEEN FR22 AND FR25 FOUND CRACK SIGNAL ON 6EA FASTENER HOLES REPAIRED THE MAIN DECK CARGO DOOR UPR EDGE PT1 BETWEEN FR22 AND FR25 6EA CRACKED FASTENER HOLES PER EA 6-5230-T0384742 P1, TITLE: DOORS - CARGO DOOR / HYD SAug 29, 2025 · N654FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202508131418Frame · crackedCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0384526 P1. TITLE: WINGS - BASIC WING STRUCTURE - FR47 RH REAR SPAR HOLE C CRACK REPAIR - SB AAug 13, 2025 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202508131417Frame · crackedCENTER BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "C" HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0384530 P1. REPAIRED THE CENTER BOX REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SAug 13, 2025 · N654FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA202508121408Skin · crackedNDT INSP FOUND RH WING CENTER FLAP TOP SKIN FLANGE RIB26 STGR2.7 AND STGR 2.8 CRACKED COMPLIED WITH EA: 6-5750-T0384484 P1, TITLE: WINGS - FLIGHT SURFACES - RH CENTER FLAP - CRACK IN UPPER FLANGES OF RIB 26 REPAIRED THE CRACKED RIB UPR FLANGE AT RH WING Aug 12, 2025 · N654FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202508111404Actuator · faultedCARGO DOOR, HYD SYS, DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR ACTUATOR BEARING FITTINGS AT FRAME 23 AND 24. COMPLIED WITH EO 6-5230-E0378588 B P5. TITLE: DOORS - CARGO DOOR/HYD SYS - DETAILED VISUAL INSPECTION OF THE MAIN DECK CARGO DOOR (MDAug 11, 2025 · N654FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA202507231298Check Valve · leakingCRUISING, FL340. ODOR IN FLT DECK. SMELLED LIKE A WET DOG, MUSTY TOWEL, OR DIRTY DIAPER. GOT STRONGER. OPENED C/P DOOR & SAW A CLOUD IN BACK. BURNING IN NOSTRILS. PUT ON OXY MASKS. DIDN`T RECEIVE FIRE - SMOKE WARNINGS. DIVERTED, COULDN`T DETERMINE SOURCE. Jul 23, 2025 · N654FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA202507221289Smoke Warning · activatedMAIN DECK CARGO SMOKE ECAM PASSING 32K LEVELED OFF COMPLIED WITH ECAM. ATB DESCENDING THROUGH 20K RECALLED ECAM ALL RED ECAM CLEARED CONTINUED MEM NORMAL APP LANDING FIRE RESCUE CONFIRMED NO SMOKE. EMERGENCY DECLARED. REMOVED AND REPLACED SMOKE DETECTIJul 22, 2025 · N654FE · Airbus A300F4605R · Smoke DetectionSDR FDEA202505230794Oxygen Mask · inoperativeON PREFLIGHT FOUND CREW COCKPIT O2 WALK AROUND BOTTLE MASK UNSERVICEABLE. REMOVED AND REPLACED COCKPIT CREW 02 MASK PER REF ABOVE. OPS CHECK GOOD. A/C OK FOR SERVICE.May 23, 2025 · N654FE · Airbus A300F4605R · Passenger Oxygen SystemSDR FDEA202505210771Flap System · stuckON DEPARTURE ON A SLATS/FLAPS 15/20 TAKEOFF AT COMMENCEMENT OF ATTEMPTED FLAP RETRACTION WE RECEIVED ECAM FOR FLAPS SYS 1 AND 2 FAULT/FLAPS STUCK. WE FOLLOWED THE ECAM AND SUBSEQUENT QRH PROCEDURE WITH NO SUCCESS WITH CYCLING. THE SLATS AND FLAPS REMAINEMay 21, 2025 · N654FE · Airbus A300F4605R · Trailing Edge Flap Control SystemSDR FDEA202502140230Battery · no testDURING MX PREFLIGHT: JUMPSEAT AREA EMERGENCY LIGHTS INOP. AMM 33-51-14-04 REPLACED PSU EMERG. BATTERY IAW A300-600 AMM CH. REF. LISTED ABOVE. OPS CKS GOOD. A/C OK FOR SERVICE.Feb 14, 2025 · N654FE · Airbus A300F4605R · Emergency LightingSDR FDEA202502080253Power Supply · faultedRIGHT ENTRY DOOR WILL NOT ARM. FACT 08FEB25 13:52 OMA AMM: 52-73-18-04 RESET AUTOMONOMOUS POWER SUPPLY REF AMM 52-73-18-04, OP'S CHECK NORMAL. OK FOR SERVICE.Feb 8, 2025 · N654FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202407211039Altimeter · failedAT CRUISE RECEIVED CAPT ALTI FAULT ECAM WITH COMMENSURATE INDICATIONS ON THE PRIMARY ALTIMETER INCLUDING OFF FLAG FOLLOWED BY ERRATIC ALTITUDE INDICATIONS VARYING BY UP TO APPROXIMATELY 1000 FEET FROM FO ALTIMETER. REFERENCE QRH FOR REQUIRED RVSM EQUIPMENJul 21, 2024 · N654FE · Airbus A300F4605R · Altimeter, Barometric/EncoderSDR FDEA202405030570Bottle · overservicedFOUND RH CREW ENTRY DOOR DAMPER CYLINDER SLIGHTLY OVERSERVICED. FACT 03MAY24 19:29 LRD AMM: 52-10-14-03-02 SERVICED RH CREW DOOR DAMPER CYLINDER AS REQUIRED IN REF WITH PLACARD AND AMM 52-10-14-03-02 STEP 3.D.(12).May 3, 2024 · N654FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA202404230271Warning Horn · false activationDURING CLIMBOUT, L1 DOOR INDICATED CONSTANT AUDIBLE ALARM AND FLASHING RED LIGHT. ATTEMPTED TO SEAT DOOR HANDLE WITH NO RESULT. REMAINED ON THROUGH CLIMB AND CRUISE. ADJ AND TEST IAW AMM STEP C. (1)-(6) NO FAULTS NOTED AT THIS TIME.Apr 23, 2024 · N654FE · Airbus A300F4605R · Passenger/Crew DoorsSDR FDEA202305270964Flap · dentedLH WING CTR FLAP L/E GOT A DENT AT RIB11-2" PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIRED AREA. I.A.W A300-600F SRM 57-50-00-201, PARA.4H, P201-P236, FIG.208. THIS REPAIR IS CAT B REPAIR REFER CHAPTER TO SRI:57-50-00-201,IIR:57-50-0May 27, 2023 · N654FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202305200962Skin · dented1EA DENT ON FUSELAGE SKIN, AT FR98~99, STGR2L~3L CUT OUT THE DAMAGED DENT, FABRICATED THE REPAIR DOUBLER AND INSTALLED WITH BLIND RIVETS, SEALANT I.A.W A300-600F SRM 53-19-12-201, PARA.6, FIG.202, PAGE.213~218, THIS REPAIR IS CLASSIFIED AS A MAJOR CATEGORYMay 20, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202305190993Unknown · unknownLH WING TIP FWD NAV LIGHT CUTOUT UPPER & LOWER CORNER RIBS GOT ABRASION REPLACED THE UPPER AND LOWER CORNER RIBS WITH NEW PARTS IAW A300-600F SRM 51-72-10- 001 , PAGE.2 & 51-40-21-001 , PARA.6 , PAGE7B~PAGE23May 19, 2023 · N654FE · Airbus A300F4605R · Wing StructureSDR FDEA202305180903Seat Track · unknownEXISTING SPLICE REPAIR ON MAIN DECK SEAT TRACK BETWEEN FR19~21, Y2462. EVALUATE TO DETERMINE WHETHER IT IS MAJOR OR MINOR AND WHETHER ACCOMPLISHED PER APPROVED DATA COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-AMay 18, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305150972Frame · noneAGING AIRCRAFT ASSESSMENT : EXISTING FRAME REPAIR FOUND ON M/D AT FR 22, STGR 8R~9R 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, INSPECTION OMay 15, 2023 · N654FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202305131027Crossbeam · unknownAGING AIRCRAFT ASSESSMENT : EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 31 BTW Y1456 ~ Y1959 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, May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305131026Crossbeam · unknownAGING AIRCRAFT ASSESSMENT : EXISTING CROSSBEAM REPAIR FOUND ON M/D AT FR 32 BTW Y1456 ~ Y1959 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, May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305130978Seat Track · corrodedMAIN DECK CGO COMP'T SEAT TRACK FOUND CORROSION AT FR15A, -Y953 AREA REPLACED THE NEW SEAT TRACK I.A.W A300-600F SRM 51-72-10-001, PAGE.2May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305130971Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 39~41L, FR 57.3~58 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 12May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305130970Skin · noneN00400 AGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 51~54R, FR 60~61 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CMay 13, 2023 · N654FE · Airbus A300F4605R · Standard Practices/StructuresSDR FDEA202305130963Flap · dentedRH WING CTR FLAP L/E LWR SURFACE DENT AT O/B EDGE-11", D NOSE T/E -3.125". PFM CUT OUT REPAIR AND MADE THE REPAIR PARTS TO INSTALLED ON REPAIR AREA I.A.W A300- 600F SRM 57-50-00-201, PARA .4H, P201-P236 ,FIG 208. THIS IS CAT B REPAIR REFER CHAPTER TO SRI: 5May 13, 2023 · N654FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA202305130936Skin · unknownAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON FUSELAGE SKIN BTW STGR 35~37R, FR26~27 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.7May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA202305130902Seat Track · noneAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 57.1~57.2, Y1456 COMPLIED WITH ATTACHMENT B OF EO:E6-5100-7-5000 D7 PT1, TITLE:STRUCTURES-REPAIR CATALOG-A300/A310 REPAIR IDENTIFICATION & TRACKING REQUIREMENTS 14 CFR 121.7May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305130901Floor Support · noneAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D FLOOR SUPPORT BTW FR 14A~16A, -Y1456 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.May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305130892Seat Track · unknownAGING AIRCRAFT ASSESSMENT : EXISTING SPLICE REPAIR FOUND ON M/D SEAT TRACK, BTW FR 31~33, 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 121.707, May 13, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305120980Profile · crackedMAIN DECK CGO COMP'T FLOOR FOUND Z-PROFILE CRACKED AT FR80/82, -Y1475 REPLACED WITH NEW Z-PROFILE I.A.W A300-600F SRM 51-72-10-001, PAGE 2May 12, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305100905Web · noneAGING AIRCRAFT ASSESSMENT : EXISTING DOUBLER REPAIR FOUND ON M/D WEB AT FR 47 BTW Y953 ~ Y1456 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, May 10, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305090883Dummy Rail · wornFR54/FR54.2 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. REPAIRED THE RH NO2 FR54~FR54.2 DUMMY SEAT TRACK AND REINSTALLED O.K I.A.W A300-600 SRM:53-15-16 PARA 5A P201-P210 FIG.201 & AMM:20-21-12-00.May 9, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305090882Dummy Rail · wornFR38.2/FR40 RH NO.2 DUMMY SEAT TRACK FOUND GAP OVER 1.0MM AND LESS THAN 2.15MM. REPAIRED THE DUMMY SEAT TRACK WITH REINSTALLATION O.K I.A.W A300-600 SRM:53-15-16 PARA 5A P201~P210 FIG.201 & AMM:20-21-12-00.May 9, 2023 · N654FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA202305071020Shear Web · crackedMAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACK AT FR77 NEAR STGR26R AREA REPLACED THE CRACK WEB WITH NEW ONE. I.A.W A300-600F SRM 51-72-10-001, PAGE2 & 51-40-21- 001, PARA.6, PAGE.7B-PAGE.23May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305070982Shear Web · crackedMAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACK AT FR79 PLUS 3" NEAR STGR26R AREA REPLACED THE CRACKED SHEAR WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE.2May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305070981Shear Web · crackedMAIN DECK CGO COMP'T FLOOR FOUND SHEAR WEB CRACKED AT FR79 PLUS 3" NEAR STGR26L AREA REPLACED THE CRACKED SHEAR WEB WITH NEW PART I.A.W A300-600F SRM 51-72-10-001, PAGE 2May 7, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305051021Fitting · crackedAVIONICS COMP'T PICK UP FITTING CRACK AT FRAME 10 FWD SIDE -Y953 POSITION REMOVED CRACK FITTING,THEN INSTALLED NEW ONE WITH FASTENERS,I.A.W A300-600F SRM 51- 72-10-001,PAGE.2 & 51-40-21-001,PARA.6, PAGE.7B~23May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA202305050992Unknown · unknownLH WING FIXED T/E ARROW EXTRUSION GOT CORROSION BETWEEN RIB26 & RIB28 REPLACED THE DAMAGED SECTION WITH NEW PART AND FASTENERS. I.A.W A300-600F SRM 51- 72-10-001, PAGE 2. AND 51-40-21-001, PARA 13, PAGE 149 - 156May 5, 2023 · N654FE · Airbus A300F4605R · AileronsSDR FDEA202305050984Fitting · crackedAVIONICS COMP'T ANGLE FITTING CRACK AT FRAME10 FWD SIDE Y-953 POSITION CRACKED ANGLE FITTING REPLACED NEW PART, INSTALLED WITH RIVETS, I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA .6, PAGE.7B-23May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305050983Fitting · crackedAVIONICS COMP'T PICK UP FITTING CRACK AT FRAME10 FWD SIDE Y403 POSITION CRACKED ANGLE FITTING REPLACED NEW PART, INSTALLED WITH RIVETS I.A.W A300-600F SRM 51-72-10-001, PAGE.2 AND SRM 51-40-21-001, PARA.6, PAGE.7B-23May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA202305050977Stringer · corrodedFWD CGO COMP'T BAY AFT AREA 1EA BONDING WIRE CONNECTION AREA GOT CORROSION AT S- 44R ,FR38.2 POSITON. CUT OUT DAMAGED STRINGER, FABRICATED THE NEW REPAIR STRINGER AND COUPLING AND WET INSTALLED REPAIR PARTS WITH FASTENERS. I.A.W A300-600F SRM 53-10-14-201, May 5, 2023 · N654FE · Airbus A300F4605R · Fuselage Main, Longeron/StringerSDR FDEA202207081697Transmitter · unknownGREEN RSVR LO LEVEL ECAM COMPLIED WITH ECAM AND QRH. NO GREEN HYD SYSTEM , NO AUTO BRAKE , NO NOSE WHEEL STEERING. MANUAL GREER EXTENSION. LANDED KLBB VFR 17R. NO FURTHER EVENT. EMERGENCY DECLARED COMPLETED REQUIRED TSI 29-30/4488 AND REPLACED GREEN HJul 8, 2022 · N654FE · Airbus A300F4605R · Hydraulic Indicating SystemSDR FDEA202207031678None · unknownPDIS 654 29-30 4470 02JUL22 MEM OPEN U DURING DESCENT, ECAM FOR GREEN RSVR LO LEVEL. LOW QUANTITY INDICATED ON ECAM AND OVERHEAD PANEL GAUGE. IN TERMINAL AREA AT KMEM, DECLARED AN EMERGENCY, RAN THE L/G GRAVITY EXTENSION CHECKLIST. LANDED ONJul 3, 2022 · N654FE · Airbus A300* · Hydraulic Indicating SystemSDR FDEA202010312730Bulkhead · corrodedFWD CARGO FR 39, Y-450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSUREOct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA202010312729Bulkhead · corrodedFWD CARGO FR 39, Y450 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y450 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROSION ON PRESSURE FOct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA202010312728Bulkhead · corrodedFWD CARGO FR 39, Y-1959-Y-2164 BULKHEAD PANEL WITH HEAVY CORROSION. REPAIRED FWD CARGO FR 39, Y-1959-Y-2164 CORRODED BULKHEAD PANEL, PER A300-600F SRM51-40-21 & EA: 6-5310-T0357303 P1 & DWG: R53810840 ISSUE B. TITLE: FUSELAGE-MAINFRAME-HEAVY EXFOLIATED CORROct 31, 2020 · N654FE · Airbus A300F4605R · Fuselage Main, Bulkhead
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