N606FE
Service difficulty reports · 403
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 = 'N606FE' 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 = 'N606FE' 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 04FDEA02011Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.020; REMAINING THICKNESS: 0.486 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-767SDR 04FDEA02010Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.408; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-767SDR 04FDEA02009Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.406; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.404 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76SDR 04FDEA02008Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062"; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBSDR 04FDEA02007Hinge Bracket · corrodedOUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062; FINAL DIAMETER: 1.189 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-76783, LEFT AND RIGHT OUTBOARD FLAP - INBOASDR 04FDEA02005Seat Track · crackedFWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 FOUND CRACKED AT THE BOTTOM SIDE. FWD CABIN - SEAT TRACK AT STA 635, LBL 47.5 SEAT TRACK REPAIRED AS PER SRM 53-70-00 FIGURE 1 VOLUME 1.SDR 04FDEA02014Hinge · corrodedLEFT WING OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76783, WINGS - LEFT AND RIGHT OUTBOARD FLAP - INBSDR 04FDEA01998Seat Track · wornSEAT TRACK CROWN AT STA 1171, LBL 47.5 FOUND WORN. REPAIR CARRIED OUT AS PER SRM 53-70-00 FIG. 1 VOL. I.SDR 04FDEA01985Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.195. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOSDR 04FDEA01984Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.196. COMPLIED WITH FEDEX EA# 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOASDR 04FDEA01983Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.399; MATERIAL REMOVED 0.004; REMAINING THICKNESS: 0.395 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-SDR 04FDEA01981Hinge Bracket · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.506; MATERIAL REMOVED 0.002"; REMAINING THICKNESS: 0.504 AND REPAIR CARRIED OUT AS PER FEDEX EASDR 04FDEA01982Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.407; MATERIAL REMOVED 0.002; REMAINING THICKNESS: 0.405 AND REPAIR CARRIED OUT AS PER FEDEX EA 1-5750-7SDR 04FDEA01980Hinge Bracket · corrodedLEFT WING - OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.495; MATERIAL REMOVED 0.032"; REMAINING THICKNESS: 0.463 AND REPAIR CARRIED OUT AS PER FEDSDR 04FDEA01979Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062, FINAL DIAMETER = 1.094. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARD HSDR 04FDEA01978Hinge Bracket · corrodedOUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093", FINAL DIAMETER = 1.127. COMPLIED WITH FEDEX EA 1-5750-76784, WINGS - LEFT AND RIGHT OUTBOARD FLAP - OUTBOARSDR 04FDEA01961Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.218 INCH AND RESDR 04FDEA01960Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.217 INCH AND SDR 04FDEA01959Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.414 INCH; MATERIALSDR 04FDEA01958Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.415 INCH; MATERISDR 04FDEA01957Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.482 INCH; MATERIAL REMOSDR 04FDEA01956Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL THICKNESS: 0.514 INCH; MATERIAL RESDR 04FDEA01955Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.062 INCH; FINAL DIAMETER: 1.126 INCH AND REPAIRSDR 04FDEA01954Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 20-11-02 PAGE 2-4. ORIGINAL DIAMETER: 1.093 INCH; FINAL DIAMETER: 1.147 INCH AND REPAIR CSDR 04FDEA01953Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGE 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.130 INCH. COSDR 04FDEA01952Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.093 INCH, FINAL DIAMETER = 1.127 INCH. COMPLSDR 04FDEA01951Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.505 INCH, MATESDR 04FDEA01950Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.497 INCH, MATERIAL SDR 04FDEA01949Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.405 INCH, SDR 04FDEA01948Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE SPOT SURFACE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL THICKNESS = 0.404 INCH, MATESDR 04FDEA01947Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCHSDR 04FDEA01946Hinge Bracket · corrodedRT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP OUTBOARD AFT HINGE, INBOARD ACTUATOR HOLE ORIGINAL DIAMETER = 1.062 INCH, FINAL DIAMETER = 1.223 INCH. CORROSION REMOVED PER CMM 20-11-02, PAGES 2 - 4. SDR 04FDEA01940Splice · crackedCTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R CRACKED. CTR CARGO, BETWEEN BS 5-113 TO 1541, LONGERON SPLICE 48R. REMOVED PER SRM 51-33-01 VOLUME II. NEW LONGERON SPLICE FABRICATED AS PER DWG: A5A7124, INSTALLED PER SRM 51-33-01 VOLUME II AND PASDR 04FDEA02001Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 1090, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS SDR 04FDEA02000Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 6-80, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 6-40 TO STA 7-0, LBL 47.5 CUT AND REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRM 51-31-01 VOLUME II. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 53-70-00 SDR 04FDEA01999Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 1119, LBL 47.5 FOUND WORN. MAIN DECK, SEAT TRACK FROM STA 1049 TO 1129, LBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR PARTS FABRICATED AND REWORKED AS PER SRM 51-21-01 VOLUME II. REPAIR PARTS INSTALLED AS SDR 04FDEA01997Seat Track · gougedMAIN DECK - SEAT TRACK CROWN AT STA 1251, LBL 47.5 FOUND WITH GOUGED MARK. MAIN DECK - DAMAGED SEAT TRACK CROWN AT STA 1251, LBL 47.5 REMOVED FROM STA 1268 TO 7 - 0 LBL 47.5 PER SRM 53-70-00 FIGURE 1 VOLUME I AND 51-31-01 VOLUME 2. REPAIR PARTS FABRICATED ANSDR 04FDEA01994Seat Track · gougedMAIN DECK - SEAT TRACK CROWN AT STA 1129, RBL 28 FOUND WITH GOUGED MARK. MAIN DECK - SEAT TRACK FROM STA 1129 TO 7 - 0, RBL 28 REMOVED AS PER SRM 51-31-01 VOLUME 2. SEAT TRACK REWORKED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REWORKED TRACK INSTALLED AS PER 5SDR 04FDEA01991Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 1090, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2.SDR 04FDEA01990Seat Track · wornMAIN DECK - SEAT TRACK CROWN AT STA 1020, RBL 47.5 FOUND DAMAGED. MAIN DECK - SEAT TRACK AT STA 999 TO STA 1129, RBL 47.5 REPLACED PER SRM 53-70-00 FIGURE 1 VOLUME I AND PER 51-31-01 VOLUME 2.SDR 04FDEA01989Seat Track · wornMAIN DECK, SEAT TRACK CROWN AT STA 870 - STA 890, RBL 47.5 FOUND DAMAGED. MAIN DECK, SEAT TRACK FROM STA 850 TO STA 950, RBL 47.5 REMOVED AS PER SRM 53-70-00 FIGURE 1 VOLUME I. REPAIR TRACK REWORKED AND INSTALLED AS PER SRM 53-70-00 FIGURE 1 VOLUME I AND SRMSDR 04FDEA01988Hinge Bracket · corrodedRT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. RT WING, INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.254 INCH, AND RESDR 04FDEA01987Hinge Bracket · corrodedLEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE FOUND CORRODED. LEFT WING - INBOARD FLAP OUTBOARD AFT HINGE, INBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.326 INCHSDR 04FDEA01986Hinge Bracket · corrodedLEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE FOUND CORRODED. LEFT WING, INBOARD FLAP OUTBOARD AFT HINGE, OUTBOARD PIVOT HOLE CORROSION REMOVED AS PER CMM 57-52-03 PAGES 442-443. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.248 INCH, ANSDR 04FDEA01977Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERSDR 04FDEA01975Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETERSDR 04FDEA01974Hinge Bracket · corrodedLEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. LEFT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= SDR 04FDEA01970Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, OUTBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1.SDR 04FDEA01969Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, INBOARD ACTUATOR HOLE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL DIAMETER= 1.187 INCH, FINAL DIAMETER= 1SDR 04FDEA01968Hinge Bracket · corrodedRT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE FOUND CORRODED. RT WING, OUTBOARD FLAP INBOARD FORWARD HINGE, LOWER MOUNT MATING SURFACE CORROSION REMOVED AS PER CMM 57-44-08 PAGES 402-407. ORIGINAL THICKNESS=0.470 INCH, MATERIAL R
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