N650FE

Service difficulty reports · 219

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 = 'N650FE' 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 FDEA201708302414Fitting · crackedAFT CARGO DOOR ACTUATOR SUPPORT BEAM IS CRACKED. REMOVED AFT CARGO DOOR IAW AMM 52-32-11-04-01. REMOVED CRACKED FITTING, AND INSTALLED A NEW FITTING IAW SRM 51-40-21. REINSTALLED THE AFT CARGO DOOR IAW AMM 52-32-11-04-01. MAJOR REPAIR.Aug 30, 2017 · N650FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201708232330Web · crackedAFT CARGO DOOR WEB AROUND DOOR ACTUATOR CRACKED. REPAIRED AREA IAW FINAL EA 6-5230-T0334976 P1 DOORS - CARGO DOOR / HYD SYS - AFT CARGO DOOR, INNER SKIN WEBS CRACKED - DOUBLER REPAIR. MAJOR REPAIR.Aug 23, 2017 · N650FE · Airbus A300F4605R · Cargo/Baggage DoorsSDR FDEA201708182272Seat Track · gougedMAIN DECK AREA LEFT SIDE BETWEEN FRAMES 48 & 49, Y1456, SEAT TRACK GOUGED ON CROWN. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 51-40-21. MAJOR REPAIR.Aug 18, 2017 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708182271Floor Panel · delaminatedMAIN CABIN FLOOR PANEL 241FJ DELAMINATED. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 06-41-53-00. MAJOR REPAIR.Aug 18, 2017 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708182270Floor Panel · delaminatedDELAMINATION ON FLOOR PANEL 251PG IN MAIN DECK. REMOVED AND REPLACED THE FLOOR PANEL IAW AMM 06-41-53-00. CLASSIFIED AS A MAJOR REPAIRAug 18, 2017 · N650FE · Airbus A300F4605R · Fuselage Floor PanelSDR FDEA201708172250Seat Track · gougedGOUGES ON THE SEAT TRACK SCALOPS IN THE MAIN DECK CARGO BAY BETWEEN FRAMES 58 TO 60, BL 0. REMOVED DAMAGE IAW SRM 53-10-16 FIG 102. CHECKED LIMITS, DIMENSION L=0.5 D=.065 W=.815 MAX D ALLOWED .016. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-16. CUT OUT THE DAAug 17, 2017 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708162239Seat Track · corrodedCORROSION ON SEAT TRACK SCALOP IN MAIN DECK CARGO BETWEEN FRAMES 76 AND 77, Y450. REPAIRED THE SEAT TRACK IAW SRM 53-10-16, FIG 201. MAJOR REPAIR.Aug 16, 2017 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201708142201Seat Track · corrodedCORROSION AND GOUGES ON SEAT TRA CK SCALOP IN MDC BETWEEN FRAMES 74 AND 75, Y1140. REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-10-16, FIG 201 AND DWG A53279232. MAJOR REPAIR.Aug 14, 2017 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201701050046Girt Bar · out of adjustAFTER THE R1 DOOR WAS CLOSED AND SLIDE ARMED, AN INDICATION WENT TO YELLOW & UNARMED. FIRST OFFICER DISARMED DOOR TO OPEN & CLOSE DOOR. DOOR WILL NOT ARM. INSPECTED THE R1 DOOR ASSY, AND FOUND THE GIRT BAR OUT OF POSITION. PLACED THE GIRT BAR INTO PROPEJan 5, 2017 · N650FE · Airbus A300F4605R · Emergency EquipmentSDR FDEA201606232130Transmitter · leakingDURING CRUISE FLIGHT GREEN SYSTEM HYD RESERVOIR LOW LEVEL. GRAVITY GEAR EXTENSION DUE TO LOSS OF GREEN HYDRAULICS. IDENTIFIED PARTS MPN: 64250-005-2, CPN: 2910415, QTY: 1. FOUND GREEN SYSTEM PRESSURE TRANSMITTER LEAKING, REF IPC 29-32-03-01, ITEM 060B. REJun 23, 2016 · N650FE · Airbus A300F4605R · Hydraulic Quantity SensorSDR FDEA201604191312Rod End · failedDURING PREFLIGHT WALK AROUND FOUND NR 2 RT GND SPOILER EXTENDED. FURTHER TROUBLESHOOTING FOUND BROKEN ROD END ON SPOILER TO ACTUATOR. DURING FURTHER INSPECTION FOUND BELL CRANK HAD GOUGES WHERE ROD WAS HITTING AGAINST IT. ROD ASSEMBLY & RT LEVER ASSEMBLY REApr 19, 2016 · N650FE · Airbus A300F4605R · Drag Control SystemSDR FDEA201510163261Wire · chafedL1 & R1 DOOR ARMED, CHIME DOES NOT PRESS TO TEST. FOUND SLIDES HORN CB 2WN POPPING WHEN FWD RT DOOR PTT PB 40WN PRESSED. REMOVED DOOR LINING FOR ACCESS, FOUND UNIDENTIFIABLE WIRE SHORTING AGAINST DOOR STRUCTURE, CAUSING BREAKER TO POP, IMAGES UPLOADED. FUROct 16, 2015 · N650FE · Airbus A300F4605R · Door System WiringSDR FDEA201505221618Crossbeam · crackedMDCC FRAME 58 -Y700 SUSPECTED CRACK ON CROSSBEAM DID HFEC INSPECTION OF THE AFFECTED AREA IAW NTM 51-10-08, FOUND A CRACK ABOUT 8MM IN LENGTH. REPAIRED THE CRACKED CROSSBEAM IAW EA 6-5310-T0317748 PT 1. MAJOR REPAIR IAW GMM 6-2-100.May 22, 2015 · N650FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201505111471Pressure Deck · crackedMAIN DECK CARGO, HORIZONTAL PRESSURE DECK WEB CRACKED AT FRAME 47, Y0 - Y450. REPAIRED IAW SRM 53-15-15-201 CONFIG 2 FIG 201.May 11, 2015 · N650FE · Airbus A300F4605R · Fuselage Main, BulkheadSDR FDEA201505031365Frame · crackedLEFT FRAME 40 AT UPPER SKIN LEVEL, TENSION BOLT JUNCTION, LOWER HOLE CRACKED. REPAIRED LT SIDE FRAME 40 CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION. THE CRACKED LOWER HOLE IAW EA 6-5710-T0317493 PT 1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2015 · N650FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201505031364Frame · crackedLEFT FRAME 40 SKIN LEVEL TENSION BOLT JUNCTION MID HOLE CRACKED. REPAIRED LT SIDE FRAME 40 CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, THE CRACKED MID HOLE IAW EA 6-5710-T0317493 PT 1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2015 · N650FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201505031363Frame · crackedLEFT FRAME 40 UPPER SKIN LEVEL TENSION BOLT JUNCTION, UPPER HOLE CRACKED. REPAIRED LT SIDE FRAME 40 CTR WING JOINT AT UPPER SKIN LEVEL TENSION BOLT JUNCTION, THE CRACKED UPPER HOLE IAW EA 6-5710-T0317493 PT 1. MAJOR REPAIR IAW GMM 6-2-100.May 3, 2015 · N650FE · Airbus A300F4605R · Fuselage Main, FrameSDR FDEA201408032043Warning System · false activationAT 30,000 FT R1 DOOR ARMING SLIDE WARNING LIGHT & BUZZER CAME ON. STAYED ON UNTIL PASSING 15,000 FT IN DESCENT. CREW DEBRIEF IS DURING ENTIRE FLT, ECAM SHOWED DOOR SLIDE ARMED ONLY BUZZER WARNING WAS GOING OFF. ALL OTHER INDICATIONS OF DOOR WERE NORMAL. TAug 3, 2014 · N650FE · Airbus A300F4605R · Door Warning SystemSDR FDEA201306181338Lug · corrodedLEFT MLG, RIB 5, FWD LUG HAS EVIDENCE OF PITTING ON FWD AND AFT FACE AND SLIGHT CORROSION IN BORE. LT MAIN GEAR REMOVAL, REWORK, REPAIR IAW MFG INSTRUCTIONS AND RECOMMENDATIONS CARRIED OUT ON RIB 5. LEFT GEAR REFITTED IAW AMM 32-11-11-04. REFER TO STAJun 18, 2013 · N650FE · Airbus A300F4605R · Wing, Attach FittingsSDR FDEA201306181337Lug · corrodedRIGHT MLG, RIB 5 FWD LUG HAS EVIDENCE OF SLIGHT CORROSION IN BORE. RIGHT MAIN GEAR REMOVAL, REWORK, REPAIR IAW MFG INSTRUCTIONS AND RECOMMENDATIONS CARRIED OUT. RIGHT GEAR REFITTED IAW AMM 32-11-11-04. REFER TO STAGE SHEETS ON JPF ITEMS 1-41 . FUNCTIONAL CHJun 18, 2013 · N650FE · Airbus A300F4605R · Wing, Landing Gear Attach FittingsSDR FDEA201306141286Skin · damagedRIGHT WING INBD T/E FLAP DAMAGED AFT EDGE.Jun 14, 2013 · N650FE · Airbus A300F4605R · Trailing Edge FlapsSDR FDEA201306131282Floorbeam · misrepairedMCD FLOORBEAM FR29 MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 212.Jun 13, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201306131280Floorbeam · misrepairedMCD FLOORBEAM FR28 MISREPAIRED, REPAIRD IAW SRM 53-10-15, FIG 212.Jun 13, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201306131277Skin · dentedLOWER SKIN DENTED FR 89-90, 12 INCHES LT OF CENTRELINE. DAMAGE OUT OF LIMITS IAW EA 6-5330-113345, REPAIR CARRIED OUT IAW SRM 53-10-12, FIG 210. REPAIR CLASSED AS MAJOR CAT B.Jun 13, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201306111246Floorbeam · misrepairedFLOORBEAM FR 33 MISREPAIRED. REPAIRED IAW SRM 53-10-15, FIG 212.Jun 11, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201306111248Seat Track · misrepairedSEAT TRACK Y-1959 BETWEEN FR 26-33 MISREPAIRED. REPAIRED IAW SRM 53-10-16, FIG 201 CAT A REPAIR.Jun 11, 2013 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201306111254Skin · dentedFUSELAGE DENT AT FR 26-27 BETWEEN STR35-36 LT, INVESTIGATE AND RECTIFY. FUSELAGE DENT AT FR26-27 BETWEEN STR 35-36L ASSESSED AND SENT TO MFG. JPF PAGE 1, ITEMS 1-3 AND ATTACHING EA 6-5310-167424 AND RAS/70578099/003/2013. REPAIR CLASSED AS MINOR CAT B WITHJun 11, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201306111252Skin · dentedDENT ON EMPENNAGE AT FR 80/82-83, STR 40-41 RT. PLEASE INVESTIGATE AND RECTIFY DENT. REPAIR CARRIED OUT ON EMPENNAGE AT FR80/82 -83, STR 40-41 RT IAW SRM 53-10-12, FIG 210. SEE JPF STAGES 1-2 FOR WORK CARRIED OUT. THIS REPAIR REMOVES DAMAGE LISTED ON NRC NJun 11, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201306101244Crossbeam · crackedCROSSBEAM FOUND CRACKED LOCATED AT Y812 OTBD. REPAIRED IAW EA 6-5300-167423. REPAIR CLASSIFIED AS MAJOR.Jun 10, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201306101243Skin · damagedLIGHTNING STRIKE DAMAGE FR 8 . REPAIRED IAW SRM 53-10-12 P, BLOCK 201, PARA 5 AND EA 6-5311-167426. REPAIR CLASSED AS MAJOR CAT B.Jun 10, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, Plate/SkinSDR FDEA201306081231Crossbeam · crackedCROSSBEAM SPLICE REPAIR AT FR.30 BETWEEN SEAT TRACK STA Y450 TO Y1456. REPAIRED IAW EA 6-5310-167428 AND SRM 53-10-15 FIG 207 SHEET 28. REPAIR CLASSED AS MAJOR.Jun 8, 2013 · N650FE · Airbus A300F4605R · Fuselage Main, StructureSDR FDEA201306071223Seat Track · corrodedSEAT TRACK FOUND CORRODED AT FR 44/45 AREA SEAT TRACK AT FR 40 TO FR 44/45 -Y953\8. REPLACED IAW SRM 51-40-21 DWG A53810296.Jun 7, 2013 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201306041193Plate · crackedLEFT PYLON, VERTICAL PLATE AT AFT FAIRING TO MAIN PYLON JUNCTION ON LT SIDE CRACKED AT TOP AND WORN THROUGH SIDE STRUCTURE OF AFT FAIRING ASSY. PLATE REPLACED AND DAMAGED AFT FAIRING STRUCTURE REPAIRED IAW EA 6-5751-167425 AND TD-J2-S1-03624-2013 FUCTIONALJun 4, 2013 · N650FE · Airbus A300F4605R · Nacelle/Pylon, Main FrameSDR FDEA201306031180Cargo Track · damagedMAIN CARGO TRACK BADLY DAMAGED, FR30 Y1456-Y1959. REPLACED IAW SRM 51-40-21.Jun 3, 2013 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201306031179Cargo Track · wornMAIN CARGO TRACK UPPER SURFACE DAMAGED, FR 31, Y1456-Y1959. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-15, FIG 107, CARGO TRACK REPLACED IAW SRM 51-40-21.Jun 3, 2013 · N650FE · Airbus A300F4605R · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201305070924Proximity Switch · failedLOST EVERYTHING BUT THIS TIME ON GEAR RETRACTION LOST ATS (LEVER TRIPPED OFF) NR 2 TRANSPONDER AT 1500 FT FINAL LAX CAPT HOOK DISAPPEARED THEN CAME ON AT 1000 FT AGL AND 30 KNOTS DIFFERENCE LOWER THAT F/O HOOK F/O CORRECT IAW WEIGHT NOT ANTI-SKID RELEASE ON May 7, 2013 · N650FE · Airbus A300F4605R · Landing Gear Position and WarningSDR FDEA201302230421Regulator · failedBOTH AUTO PRESSURIZATION REGULATORS FAILED MULTIPLE TIMES DURING CLIMBOUT. ELECTED TO CONTINUE FLIGHT USING MANUAL PRESSURIZATION. FACT MEM U NO HISTORY. PERFORMED CABIN PRESS CTL TEST. NO FAULTS FOUND. R & R NR 1 PRESS CONTROLLER AS PRECAUTION BECAUSE ITFeb 23, 2013 · N650FE · Airbus A300F4605R · Pressure Regulator/Outflow ValveSDR FDEA201212204347Windshield · failedDURING CRUISE, AT FL 320, LT WINDOW HEAT FAULT LIGHT ILLUMINATED, TURNED OFF IAW ECAM. R & R WINDSHIELD IAW MM 56-11-11-04, TO INSTALLATION, STEP 12. OPS CHECKED NORMAL REF AMM 30-42-00-05.Dec 20, 2012 · N650FE · Airbus A300F4605R · Flight Compartment WindowsSDR FDEA201212154309Landing Gear · failedLANDING GEAR FAILED TO RETRACT ON DEPARTURE. R & R LT MLG PROXIMITY SENSOR IAW MM 32-00-00-04. DESERVICED PITCH DAMPNERS AND VERIFIED BOGIE BEAM FREE TO PIVOT. LUBRICATED BOGIE BEAM IAW 12-22-32. SERVICED PITCH DAMPNERS IAW 12-12-32-00 Dec 15, 2012 · N650FE · Airbus A300F4605R · Landing Gear Retraction/Extension SystemSDR FDEA201211073899Indicator · failedNR 2 ENGINE INOP DURING T/O ROLL. ATTEMPTED TWICE, RTO , 80 KTS. R & R NR 2 ENGINE N1 INDICATOR AND TORQUED SCREWS IAW AMM 20-21-12-00. MAX POINTER PRESS TO TEST CARRIED OUT, TESTS NORMAL. ENG NR 2 RUN IAW JRH ENG NR2 N1 INDICATION NORMAL. .Nov 7, 2012 · N650FE · Airbus A300F4605R · Engine RPM Indicating SystemSDR FDEA201206302424Flex Line · failedLOST GREEN HYD ON LANDING. REPLACED YELLOW AND BLUE HYD SYSTEM PRESSURE FLEX LINES ON RT INBD AILERON ACTUATORS, LEAK CHECKED NORMAL IAW AMM 27-14-12-04.Jun 30, 2012 · N650FE · Airbus A300F4605R · Hydraulic System, MainSDR FDEA201112035137Slide · unwanted deployRT DOOR SLIDE DEPLOYED WHEN ARMING DOOR. R & R R1 DOOR SLIDE IAW MM 25-61-21-04, ACFT OK FOR SERVICE.Dec 3, 2011 · N650FE · Airbus A300F4605R · Escape SlideSDR FDEA201110274668Slide · unwanted deploySLIDE DEPLOYED ON RT DOOR. R & R R1 DUAL ESCAPE SLIDE IAW AMM 25-61-21-04. REPLACED DIAPHRAM IN EMERGENCY OPERATING CYLINDER AND RECHARGED CYLINDER IAW AMM 52-10-14-03-02. OPS CKS AND LEAK CKS GOOD. ACFT OK FOR SERVICE. FINAL CLOSED.Oct 27, 2011 · N650FE · Airbus A300F4605R · Escape SlideSDR FDEA201104201540Skin · crackedRT WING BOTTOM SKIN, BOTTOM SURFACE AT T/E 13.5IN INBD OF RIB 9 HAS A CRACK. ABOUT 1.25 IN LONG. REPAIRED CRACKED SKIN IS ACCOMPLISHED ON E6-5710-7-5013, REV 01, PT6.Apr 20, 2011 · N650FE · Airbus A300F4605R · Wing, Plate/SkinSDR FDEA201104201539Track · gougedAFT CARGO COMPARTMENT R2 ROLLER TRACK IS GOUGED ON INBD AND OTBD END RADIUS FROM FRAME 54 TO FR 54.3. DAMAGE EXTENDS TO THE TRACK LEG ON BOTH INBD AND OTBD ENDS AND THE MEASURE MAX IS 8 IN X 0.040 IN. TRACK HAS MULTIPLE GOUGES THAT ARE NOT SEVERE. SMOOTApr 20, 2011 · N650FE · Airbus A300F4605R · Fuselage Miscellaneous StructureSDR FDEA201103251176Floorbeam · crackedFWD CARGO COMPARTMENT MAIN DECK FLOORBEAM AT FRAME 25 HAS A 0.25 IN CRACK ON THE UPPER END OF THE VERTICAL STIFFENER BETWEEN SEAT TRACKS R3 AND R2. REMOVED DAMAGED AREA, AND REPAIRED IAW SRM 53-10-15 PAGE 393 THRU PAGE 399. FIG 212.Mar 25, 2011 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201103251175Floorbeam · crackedFWD CARGO COMPARTMENT FLOORBEAM AT FR23 HAS A 0.5 IN CRACK AT UPPER END OF VERTICAL STIFFENER BETWEEN SEAT TRACKS R1 AND R2. REMOVED DAMAGED AREA, NDT CHECKED FOR CRACKS-CHECKED GOOD, FABRICATED REPAIR ANGLE AND REPAIRED DAMAGED AREA.Mar 25, 2011 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201103251174Floorbeam · crackedFWD CARGO COMPARTMENT FLOORBEAM AT FR 21 HAS A CRACK AT VERTICAL (UPPER END) BETWEEN SEAT TRACKS R2 AND R3, CRACK MEASURES APPROX .75 IN LONG. REF AMM 53-13-11-06-0. CRACK IS ON VERT STIFFENER. REMOVED DAMAGED AREA, NDT CHECKED FOR CRACKS-CHECKED GOOD, FABRICMar 25, 2011 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201103221128Floorbeam · crackedFWD CARGO COMPT MAIN DECK FLOORBEAM AT FR31 HAS A .25 INCH CRACK ON VERTICAL STIFFENER BETWEEN SEAT TRACKS L3 AND L4. REPAIRED FLOORBEAM AT FR31 BETWEEN SEAT TRACK 3L AND 4L IAW SRM 53-10-15, FIG 212.Mar 22, 2011 · N650FE · Airbus A300F4605R · Fuselage Main, Floor BeamSDR FDEA201012144663Gearbox · failedON TAKEOFF, FLAP SYS 1 AND SYS 2. FLAPS STUCK BETWEEN 15 AND 20. OCCURRED AT TEMP -4 MX UPDATE FOUND TORQUE LIMITER POPPED IN LT WHEEL WELL. WOULD NOT RESET. FOUND BOTH SFCC'S INDICATING A JAM.Dec 14, 2010 · N650FE · Airbus A300F4605R · Trailing Edge Flap Control System
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