N661FE
Service difficulty reports · 318
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 = 'N661FE' 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.
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 = 'N661FE' AND registry_match = 'registration' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR FDEA202404020542Skin · damaged1EA WATER TRAPPED AREA(110MM X 150MM) WAS FOUND AT R/H ELEVATOR UPPER SKIN PANEL T/E NO.26 SCREW AREA. ACCOMPLISHED THE CAT.A MAJOR COMPOSITE REPAIR AT RH ELEVATOR UPPER SKIN PANEL NO.26 T/E SCREW PER GMM 6-2-100 I.A.W A300-600F SRM 55-21-12-201, PARA 5J, SDR FDEA202404020537Seat Track · gougedMAIN DECK FLOOR - SEAT TRACK CROWN AREA GOT A GOUGE LOCATION AT FR28 PLUS 3" AND - Y953 ACCOMPLISHED THE CAT.A MAJOR SEAT TRACK SPLICE REPAIR PER GMM 6-2-100 AT MAIN DECK FR 28 AND -Y953 IAW SRM 53-10-16-201, PARA.4, PAGE 203-208, FIG 201.SDR FDEA202404010584Support · crackedAVIONICS COMP'T ACCESS DOOR OMEGA STOP FITTING CRACK AT FR6 POSITION. REPLACED THE DAMAGE STOP FITTING WITH NEW PART. AT AVIOICS ACCESS DOOR I.A.W A300-600F SRM 51-72-10-001 PAGE2. THIS REPAIR IS CLASSIFIED AS MINOR PER GMM 6-2-100 (AT FR 6, Y0)SDR FDEA202404010547Seat Track · crackedAVIONICS COMP'T UNDER FLIGHT DECK SEAT TRACK ANGLE CRACK AT FR10 ,Y953 POSITION. REPLACED THE ANGLE FITTING WITH NEW ONE IAW A300-600F SRM 51-72-10-001 PAGE2 THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 AT FR10 ,Y953SDR FDEA202403310590Adapter · gougedMAIN DECK FLOOR CLS ADAPTER CROWN GOUGE AT FR59 Y1736 REPLACED THE DAMAGE ADAPTER WITH NEW ONE AND INSTALLED WITH FASTENERS AT MAIN DECK FR59 Y1736, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 I.A.W A300-600F SRM 51- 72-10-001, PAGE 2 AND 51-40-21-001, PSDR FDEA202403310588Adapter · gougedMAIN DECK FLOOR CLS ADAPTER CROWN GOUGE AT FR61 Y1566 REPLACED THE DAMAGE ADAPTER WITH NEW ONE AND INSTALLED WITH FASTENERS AT MAIN DECK FR61 Y1566, THE REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100 I.A.W A300-600F SRM 51- 72-10-001, PAGE 2 &51-40-21-001, PARASDR FDEA202403310586Adapter · gougedMAIN DECK FLOOR CLS ADAPTER CROWN GOUGE AT FR57.2 Y1736 AT F57.2 Y1736 DAMAGED ADAPTER REPLACED NEW PART,INSTALLED WITH FASTENERS.IAW A300- 600F SRM51-40-21 PARA7-PAGE24-50 AND 51-72-10-001.PAGE 2 THIS REPAIR CLASSIFIED AS MINOR PER GMM 6-2-100.SDR FDEA202403280669Fitting · crackedTHE MDC DOOR ACTUATOR YOKE FWD SUPPORT FRAME WAS FOUND CRACK ACCOMPLISHED THE REPLACEMENT OF BEARING FITTING AT MAIN DECK CARGO DOOR FR23 LONGN1~LONGN3 I.A.W FEDEX EA NO:T6-5230-T0378797 P1, SEQ NO:1121, TITLE:DOORS-CARGO DOOR /HYD SYS-MAIN CARGO ACTUATOR SDR FDEA202307071176Unknown · unknownPDIS 661 29-01 5576 30JUN23 MEM FACT U GREEN RESERVOIR OVERHEAT WARNING DURING CLIMB OUT. FOLLOWED THE ECAM AND QRH PROCEDURES. GRAVITY EXTENDED GEAR AND NO NOSE WHEEL STEERING AS A RESULT. OVERSPEED THE KRUGER FLAP AS A RESULT OF BEING ABOSDR FDEA197706301134Unknown · unknownGREEN RESERVOIR OVERHEAT WARNING DURING CLIMB OUT. FOLLOWED ECAM & QRH PROCEDURES. GRAVITY EXTENDED GEAR & NO NOSE WHEEL STEERING AS A RESULT. OVERSPEED KRUGER FLAP AS A RESULT OF BEING ABOVE 300 & .65 MACH AT THE TIME OF FAILURE. KRUGER FLAP WAS OVERSPESDR FDEA202211102751Spoiler · faultedON TAXI OUT THE NUMBER 6 SPLR FAULTED. RAN CHECK LIST. RESET CB. FAULT RETURNED. PERFORMED T/S PER A310 TSM27-61-00, NO BITE FAULT CODE DISPLAYED ON BOTH EFCU. UNABLE TO DUPLICATE SPOILER FAULT ON GROUND. SWAPPED NR 1 EFCU WITH NR 2 EFCU FOR TROUBLESHOOTSDR FDEA202211102750Spoiler · faultedON TAXI OUT THE NUMBER 6 SPLR FAULTED. RAN CHECK LIST. RESET CB. FAULT RETURNED. IAW AMM: 27-61-34-04, PERFORMED T/S IAW TSM27-61-00, NO BITE FAULT CODE DISPLAYED ON BOTH EFCU. UNABLE TO DUPLICATE SPOILER FAULT ON GROUND.HOWEVER, SWAPPED NR 1 EFCU WITH NR SDR FDEA202202220347None · noneUNABLE TO DISARM SLIDE L1 DOOR. FOUND FOREIGN DEBRIS NEAR GIRT BAR AT FLOOR ATTACHMENT. REMOVED DEBRIS. SLIDE ARM HANDLE NOW MOVES FREELY TO ARM AND DISARM POSITION PER MM 25-61-20-02. OK FOR SERVICE.SDR FDEA202110262621Seat Track · noneMAIN DECK FR20-FR21 Y1456 SEAT TRACK DEFORMED COMPLIED WITH EA: 6-5310-T0365068 P1. TITLE: FUSELAGE - MAINFRAME - MCD Y1456 SEAT TRACK BENT BETWEEN FR20 AND FR21 - REPAIR. REPAIRED THE MAIN DECK FR20-FR21 Y1456 DEFORMED SEAT TRACK. THIS IS A PERMANENT CASDR FDEA202110262620Seat Track · noneMAIN DECK FR20-FR21 Y953 SEAT TRACK DEFORMED COMPLIED WITH EA: 6-5310-T0365066 P1. TITLE: FUSELAGE - MAINFRAME - MCD Y953 SEAT TRACK BENT BETWEEN FR20 AND FR21 - REPAIR. REPAIRED THE MAIN DECK FR20-FR21 Y953 DEFORMED SEAT TRACK. THIS IS A PERMANENT CATEGSDR FDEA202110252610None · noneCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 RH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P2 STEP 5.D-5.E. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM SDR FDEA202110252609None · noneCENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM PANEL AT JUNCTION WITH FUSELAGE FR47 LH SIDE, FASTENER "I" HOLE FOUND CRACK SIGNAL COMPLIED WITH EO 6-5710-E0342809 B P1 STEP 5.D-5.E. TITLE: WINGS - CENTER WING BOX - INSPECTION OF REAR SPAR AND BOTTOM SDR FDEA202110252608None · noneRH WING #5 SPOILER CENTER I/B HINGE ARM O/B SIDE FOUND DELAMINATION. SIZE: 25MM*20MM, DEPTH: 2.0MM COMPLIED WITH EA: 6-5750-T0364810 P1. TITLE: WING - FLIGHT SURFACES - RH 5# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE RH WING #5 SPSDR FDEA202110252607None · noneLH WING #5 SPOILER CENTER O/B HINGE ARM O/B SIDE FOUND DELAMINATION. SIZE: 40MM*20MM, DEPTH: 1.0MM COMPLIED WITH EA: 6-5750-T0364812 P1. TITLE: WING - FLIGHT SURFACES - LH 5# SPOILER CENTER HINGE ARM OUTSIDE SURFACE DELAMINATION. REPAIRED THE LH WING #5 SPSDR FDEA202107201827Skin · gougedR/H I/B FLAP UPPER SURFACE IS GOUGED. COMPLIED WITH EA 6-2780-T0363087 L/E SLATS AND FLAPS REPAIR UPPER SKIN R/H INBD FLAP.SDR FDEA202102160384Seal · failedMDIS 661 52-10 3182 DOOR 1L EMERGENCY OPERATION CYLINDER NITROGEN BOTTLE WILL NOT TAKE AIR. IT HAS A BLOWN DIAPHRAGM THAT NEEDS REPLACED PER AMM 52-10-14-03-02. REPLACED FWD DOOR DAMPER SEALS PERCUSSION MECHANISM DIAPHRAGM. REF. A300-600 M/M 52SDR FDEA202011112826Smoke Detector · false activationAVIONICS SMOKE WARNING ON APPROACH INTO MEMPHIS MULTIPLE RESETS NO HELP SNIFFER FAN SHOWED NO SMOKE, QRH PROCEDURES, DECLARED EMERGENCY. CAPTAIN RAN BOTH ENGINES AND PRESSURIZED A/C, REF A300-600 AMM 21-31-00-05. DURING PRESSURIZATION SMELLED HYD FLUID. AFSDR FDEA202010272658Window · burnedPDIS 661 56-10 2873 27OCT20 MEM OPEN U LOGPAGES:3227955 DURING DESCENT OBSERVED FLAMES ON LOWER LEFT CORNER OF FO WINDSHIELD (OUTSIDE). SHORTLY THEREAFTER FO WINDSHIELD CRACKED. FACT 27OCT20 19:16 MEM SDR FDEA2020090822153Unknown · odorDUSTY/METALLIC SMOKE SMELL IN COCKPIT DURING TAKEOFF ROLL UP TO 5000FT. AT THE SAME TIME THE AURAL ALTITUDE WARNING WAS CONSISTENTLY BLARING, THEN COMPLETELY STOPPED. NO AURAL WARNING ABOVE 20K. CREATED NEW WRI 22-XX-XXXX FOR ALTITUDE ALERT AURAL WARNING POSDR FDEA201906281480Fitting · crackedDURING PERFORMING ROTOTEST INSPECTION OF FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, LT MID HOLE FOUND CRACK SIGNAL COMPLIED WITH EA: 6-5710-T0347503 PT1, EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE MIDDLE HOLE AT FR40 LHSDR FDEA201906281475Fitting · crackedDURING PERFORMING ROTOTEST INSPECTION OF FRAME 40 TO CENTER WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, RH UPPER HOLE FOUND CRACK SIGNAL COMPLIED WITH FEDEX EA: 6-5710-T0347502 PT1, EA TITLE: WINGS - BASIC WING STRUCTURE - CRACK IN THE UPPER HOLESDR FDEA201906271483Hinge · delaminatedSDI FOUND LT WING #3 SPOILER CENTER HINGE LOWER SURFACE FOUND DELAMINATION COMPLIED WITH EA: 6-5750-T0347580 PT1, EA TITLE: WING - FLIGHT SURFACES - LT 3# SPOILER CENTER HINGE ARM LOWER SURFACE DELAMINATION. REPAIRED LT WING #3 SPOILER CENTER HINGE ARM LOWER SSDR FDEA201906251484Skin · unknownEXISTING REPAIR ON RH WING 1# SLAT LOWER SKIN BETWEEN RIB9 AND RIB10 REQUIRES EVALUATION FOR CONFORMITY THE
EXISTING REPAIR ON RH WING 1# SLAT LOWER SKIN BETWEEN RIB9 AND RIB10 WAS EVALUATED AND FOUND NO REPAIR
RECORD WAS AVAILABLE. THE EXISTING REPAIR PITCHSDR FDEA201906251457Crossbeam · crackedEXISTING REPAIR ON MDCC CROSSBEAM AT FR30, BETWEEN Y-450 AND Y-953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR30, BETWEEN Y-450 AND Y-953 WAS EVALUATED AND FOUND DID NOT CONFORMED TO PREVIOUS REPAIR RECORD. THE EXISTING REPAISDR FDEA201906251454Crossbeam · crackedEXISTING REPAIR ON MDCC CROSSBEAM AT FR28, BETWEEN Y-450 AND Y-953 REQUIRES EVALUATION FOR CONFORMITY THE EXISTING REPAIR ON MDCC CROSSBEAM AT FR28, BETWEEN Y-450 AND Y-953 WAS EVALUATED AND FOUND DID NOT CONFORMED TO PREVIOUS REPAIR RECORD. THE EXISTING REPAISDR FDEA2019061701311Stiffener · corrodedLH LOWER FUSELAGE SKIN ATTACHED STIFFENER - FWD TOILET SERVICE PANEL FWD LWR CUTOUT CORRODED, BETWEEN FR12 AND FR12ASDR FDEA2019061301287Web · crackedMAIN DECK - UNDERFLOOR VERTICAL WEB CRACKED, AT FR47, BETWEEN Y953 AND Y1456 REPAIRED THE CRACKED VERTICAL WEB (MAIN DECK - UNDERFLOOR VERTICAL WEB, AT FR47, BETWEEN Y953 AND Y1456) PER A300-600F SRM53-15-15 FIGURE 201. THIS REPAIR CATEGORY "B". INSPECTIOSDR FDEA2019061301286Web · crackedMAIN DECK - UNDERFLOOR VERTICAL WEB CRACKED, AT FR47, BETWEEN Y0 AND Y-450 REPAIRED THE CRACKED VERTICAL WEB (MAIN DECK - UNDERFLOOR VERTICAL WEB, AT FR47, BETWEEN Y0 AND Y-450) PER A300-600F SRM53-15-15 FIGURE 201. THIS REPAIR CATEGORY "B". INSPECTION THSDR FDEA2019061301285Web · crackedMAIN DECK - UNDERFLOOR VERTICAL WEB CRACKED, AT FR47, BETWEEN Y0 AND Y450 REPAIRED THE CRACKED VERTICAL WEB (MAIN DECK - UNDERFLOOR VERTICAL WEB, AT FR47, BETWEEN Y0 AND Y450) PER A300-600F SRM53-15-15 FIGURE 201. THIS REPAIR CATEGORY "B". INSPECTION THRESDR FDEA2019062801421Crossbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR60, BTW Y-1456 AND Y-1959 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR60, BTW Y-1456 AND Y-1959) PER A300-600F SRM53-10-15-201 FIGURE SDR FDEA2019061181260Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR32, BTW Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR32, BTW Y1456 AND Y1959) PER A300-600F SRM53-10-15-201 FIGURE 212.SDR FDEA2019061181259Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR27, BTW Y-450 AND Y-953 REPAIRED THE CRACKED CROSSBEAM IAW SRM 53-10-15-201 FIGURE 212. THIS REPAIR CATEGORY "A". MAJOR REPAIR IAW GMM 6-2-100.SDR FDEA2019061361282Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR75, BETWEEN STGR10L AND STGR11L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR75, BETWEEN STGR10L AND STGR11L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR FDEA2019061361284Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR59, BETWEEN STGR13L AND STGR14L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR59, BETWEEN STGR13L AND STGR14L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR FDEA2019061361283Frame · dentedMAIN DECK - FUSELAGE MAIN FRAME DEFORMED, AT FR58, BETWEEN STGR13L AND STGR14L REPAIRED THE DEFORMED FRAME(MAIN DECK - FUSELAGE MAIN FRAME, AT FR58, BETWEEN STGR13L AND STGR14L) PER A300-600F SRM53-10-13 FIGURE 202. THIS REPAIR CATEGORY "B". FIRST INSPECTISDR FDEA201906041481Coupling · chafedMAIN DECK - FUSELAGE MAINFRAME COUPLING CHAFFED, AT FR29, BETWEEN STR 12R AND STR 13R REPLACED THE MAINFRAME COUPLING (MAIN DECK - FUSELAGE MAINFRAME COUPLING, AT FR29, BETWEEN STR 12R AND STR 13R ) PER SRM51-40-21. THIS REPAIR CATEGORY "A". MAJOR REPAIR IAW SDR FDEA2019060631214Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR31, BTW Y1456 AND Y1959 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR31, BTW Y1456 AND Y1959) PER SRM53-10-15-201 FIGURE 212. THIS REPASDR FDEA2019060631215Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BTW Y-1456 AND Y-1959 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR64, BTW Y-1456 AND Y-1959) PER SRM53-10-15 FIGURE 211. THIS REPASDR FDEA201906031213Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR66, BTW Y-953 AND Y-1456 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR66, BTW Y-953 AND Y-1456) PER SRM53-10-15 FIGURE 211. THIS REPAIRSDR FDEA201906031212Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR66, BTW Y953 AND Y1456 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR66, BTW Y953 AND Y1456) PER SRM53-10-15 FIGURE 211. THIS REPAIR CATSDR FDEA2019060631211Floorbeam · crackedMAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM CRACKED, AT FR64, BTW Y-953 AND Y-1456 REPAIRED THE CRACKED CROSSBEAM (MAIN DECK CARGO COMPARTMENT FLOOR STRUCTURE - CROSSBEAM, AT FR64, BTW Y-953 AND Y-1456) PER SRM 53-10-15 FIGURE 211. THIS REPAISDR FDEA201812013411Gcu · malfunctionedOPERATING UNDER MEL 49-33-12 (NO APU GEN AVAILABLE) DURING TAKEOFF AT V1 FO PFD FLICKERED, ALT FLAT. AT APPROXIMATELY 1000 AGL GEN 2 FAULT AND AC BUS 2 FAIL ON ECAM AND OVERHEAD PANEL. GEN 2 DID NOT RESET AND COULD NOT POWER AC BUS 2. ATB TO KDEN. DURING ATBSDR FDEA2018100272719Detector Loop · malfunctionedMAIN DECK CARGO SMOKE DETECTION LOOP TEST IS INOP. CYCLED DETECTION CONTROL C/B'S PER M/M 26-19-34-04. OP'S NORMAL.SDR FDEA201708312440Smoke Detector · malfunctionedDURING TAKEOFF ROLL AT 50KIAS, AVIONICS SMOKE WARNING, REJECTED TAKE OFF, NO SMOKE ON SNIFFER FAN, RETURNED BACK TO GATE. REMOVED AND REPLACED AV3 SMOKE DETECTOR IAW AMM 26-15-12-04. OPS CHECKED GOOD.SDR FDEA201704221254Smoke Warning · false activationDURING TAXI GOT MULTIPLE AVIONICS SMOKE WARNINGS WITH NO SMOKE SMELL . THE WARNING WOULD COME AND GO. DURING TAXI, RECEIVED MULTIPLE AVIONICS SMOKE WARNINGS, WITH NO SMOKE ODOR. THE WARNING WOULD COME & GO WORKED WITH MTSI 53-21/9289. WHILE ACCOMPLISHING M
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