N246PS

Service difficulty reports · 172

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 = 'N246PS' 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 SWIA202156406Seat Track · corrodedLEFT PASSENGER SEAT TRACK HAS CORROSION FROM FS 546.00 - FS 559+10. (C-CHECK) RO 2/21/2021. LT PASSENGER SEAT TRACK BETWEEN FS 546.00 - FS 559+10 HAS BEEN REPAIRED AND REPLACED WITH A SERVICEABLE UNIT IAW REO 601R-53-00-485 REV -D DATE 2018-01-29.Jan 12, 2021 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202156405Seat Track · corrodedLEFT PASSENGER SEAT TRACK HAS CORROSION FROM FS 559+16 - FS 559+80. (C-CHECK) RO 2/21/2021. LT PASSENGER SIDE SEAT RAIL BETWEEN FS 559.00+16 - FS 559+80 HAS BEEN REPLACED WITH A SERVICEABLE UNIT IAW REO 601R-53-00-055 REV C DATED 2017-03-21.Jan 12, 2021 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202156375Skin · puncturedBETWEEN FS 625.30 FS 640.00 AND BETWEEN STRG 25, STRG 26 IS PUNCTURE IN THE SKIN APPROXIMATELY .500 LONG AND .250 WIDE. (C-CHECK) RO 2/21/2021. COMPLIED WITH REO 601R-53-61-7544 REV-- DATED 2021-01-29. REFERENCE THE CONTINUATION CARD FOR THE WORK PERFORMED.Jan 10, 2021 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202056387Stop Fitting · crackedMAIN PAX DOOR UPPER LATCH MECHANISM AFT STOP FITTING CRACKED. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED MAIN PAX DOOR UPPER LATCH MECHANISM AFT STOP FITTING AS REQUIRED IAW CRJ 200 CMM 52-11-00. SEE ATTACHED CONTINUATION CARD FOR WORK PERFORMED.Dec 29, 2020 · N246PS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056408Hinge Bracket · chafedRIGHT WING FLAP HINGE ARMS (BOTH WS80.50 AND WS127.25) FAIRING PLATE PANELS HAVE CHAFE MARKS IN RADIUS OF BRACKET INTO BARE METAL. (C-CHECK) RO 2/21/2021. REMOVED AND INSTALLED NEW SERVICEABLE SIDE PLATES AND BRACKET IAW CRJ 200 SRM 51-42-06,51-42-15 AND 51-Dec 28, 2020 · N246PS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056404Seat Track · corrodedRIGHT SIDE SEAT RAIL CHANNEL HAS AREAS OF CORROSION FROM FS 409+128-559+16. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED RT SIDE SEAT RAIL DUE TO CORROSION IAW REO 601R-53-00-055 REV-C DATE 2017-03-21.Dec 28, 2020 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056403Seat Track · corrodedRIGHT SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FS 409+112 - 409+128. (C-CHECK) RO 2/21/2021. RT SIDE SEAT RAIL BETWEEN FS 409+112 - FS 409+128 WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW REO 601R-53-00-055 REV-C DATE 2017-03-21.Dec 28, 2020 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056402Seat Track · corrodedRIGHT SIDE SEAT RAIL HAS AREAS OF CORROSION FROM FS 409+36 - 409+112. (C-CHECK) RO 2/21/2021. RT SIDE SEAT RAIL BETWEEN FS 409+36 - FS 409+112 WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW REO 601R-53-00-055 REV C DATE 2017-03-21.Dec 28, 2020 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056401Seat Track · corrodedRIGHT SIDE SEAT RAIL HAS CORROSION FROM FS 409+16-409+36. (C-CHECK) RO 2/21/2021. RT SIDE SEAT RAIL BETWEEN FS409+16 - FS409+36 WAS REMOVED AND REPLACED WITH A SERVICEABLE UNIT IAW REO 601R-53-00-055 REV-C DATE 2017-03-21.Dec 28, 2020 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056400Door Sill · corrodedPAX DOOR LOWER SILL ANGLE IS CORRODED AT THE PAX DOOR BONDING JUMPER LOCATION AND JUST FORWARD OF THE PAX DOOR AFT HANDRAIL ARM FITTING. (C-CHECK) RO 2/21/2021. PAX DOOR LOWER SILL ANGLE WAS REMOVED AND REPLACED IAW CRJ 200 SRM 51-42-21, SEE ATTACHED CONTINUDec 27, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056399Bonding Jumper · corrodedLEFT AND RIGHT ELEVATORS NR 1 HINGE BONDING JUMPERS AND HARDWARE ARE CORRODED. (C-CHECK) RO 2/21/2021. REMOVED REPLACED LT RT ELEVATORS NR 1 HINGE BONDING JUMPERS AND HARDWARE IAW CRJ 200 AMM 51-80-00-400-803 BOND CHECK GOOD MEGGER USED WVACT 9519 CALL DUE 1Dec 26, 2020 · N246PS · Cndair CL6002B19 · Elevator StructureSDR SWIA202056398Bolt · corrodedRIGHT WING SPOILERON O/B ACTUATOR LOWER MOUNT HARDWARE CORRODED RWS 255.36. (C-CHECK) RO 2/21/2021. REPLACED LOWER MOUNTED HARDWARE WITH SERVICEABLE HARDWARE AT RT WING O/B ACTUATOR IAW CRJ-200 AMM TASK 27-62-01-400-801.Dec 24, 2020 · N246PS · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA202056397Bolt · corrodedRIGHT WING I/B SPOILERON ACTUATOR LWR HDWR CORRODED RWS 246.93. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED R/W I/B SPOILERON ACTUATOR LWR HDWR IAW CRJ 200 AMM 27-62-01-400-801.Dec 24, 2020 · N246PS · Cndair CL6002B19 · SpoilersSDR SWIA202056379Bulkhead Web · failedFOUND REAR PRESSURE BULKHEAD WEB AT RBL 27.50 WL112 HAS MULTIPLE INDICATIONS NOTED 7 INCHES LONG 90%FSH FAILED NDT INSPECTION. (C-CHECK) RO 2/21/2021. PERFORMED REPAIR OF FS 621 PRESSURE BULKHEAD IAW REO 601R-53-61-1240 REV D DATED 2016-10-31. REFERENCE CONDec 24, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA202056409Floorbeam · damagedFLOOR BEAM AT LBL 33, FS 559+112 HAS FLOOR BOLT CEASED IN NUTPLATE. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED 2 (EA) NUT PLATES AT LBL 33, FS 559+112 IAW CRJ 200 SRM 51-45-00 REFERENCE CONTINUATION CARD FOR WORK PERFORMED.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202056396Crossbeam · corrodedCROSSBEAM CAP AT FS 589 HAS MINOR CORROSION BETWEEN RBL 27 AND RBL 45. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED THE CAP STRIP AT FS 589 BETWEEN RBL 27 AND RBL 45 IAW CRJ 200 SRM 51-42-06. APPLIED PRIMER TO CAP STRIP IAW CRJ 200 SRM 51-25-06. APPLIED TOPDec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056395Stringer · corrodedSTRINGER 26L HAS MULTIPLE SPOTS OF CORROSION FROM FS 364.00 TO FS 349.00. (C-CHECK) RO 2/21/2021. FOUND DAMAGE TO INTERCOSTAL 27L FS 349 TO 364 TO BE OUT OF LIMITS, REMOVED INTERCOSTAL AND INSTALLED A NEW INTERCOSTAL IAW CRJ 200 SRM 51-42-06 AND 51-42-21.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202056394Stringer · corrodedSTRINGER 26R HAS MULTIPLE SPOTS OF CORROSION FROM FS 364.00 TO FS 349.00. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED INTERCOSTAL IAW CRJ 200 SRM 51-42-21 , 51-42-21.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202056393Angle · corrodedFS 280.00 FWD J ANGLE HAS CORROSION AROUND NUTPLATES. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED FS 280.00 FWD J ANGLE AS REQUIRED IAW CRJ 200 SRM 51-40-11.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202056386Floorbeam · crackedFS 280.00 BEAM SPLICE CRACKED AT APPROX. RBL11. (C-CHECK) RO 2/21/2021. REMOVED DAMAGED SPLICE AT FS 280.00 RBL 9 AND INSTALLED A NEW SPLICE ANGLE IAW REO 601R-53-11-171 REV D DATED 13-FEB-07.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA202056385Bracket · crackedFS 280 2 EA ANGLE BRACKETS AT RBL 9 ARE CRACKED. (C-CHECK) RO 2/21/2021. REMOVED DAMAGED BRACKETS AND INSTALLED SERVICEABLE BRACKETS IAW CRJ 200 SRM 51-42-21.Dec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056378Floor Support · corrodedLEFT SIDE FLOOR SUPPORT STRUCTURE HAS MULTIPLE AREAS OF CORROSION FS 559+80 TO FS 621, LBL42.90. (C-CHECK) RO 2/21/2021. REPAIRED LEFT SIDE FLOOR STRUCTURE AT FS 559+80 TO FS 621 LBL 42.90 IAW REO 601R-53-61-690 REV D DATED 29 SEP 05. REFERENCE CONTINUATIODec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056372Floor Support · corrodedRIGHT FLOOR SILL MEMBER FS409+128 TO FS 559 HAS MULTIPLE AREAS OF CORROSION (C-CHECK) RO 2/21/2021. REPAIRED RIGHT FLOOR SILL MEMBER FS409+128 TO FS 559 AS REQUIRED IAW REO 601R-53-41-666 REV C DATED 2012-11-06. SEE ATTACHED CONTINUATION CARD FOR WORK PERFDec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056371Crossbeam · corrodedMINOR CORROSION ON CROSSBEAM AT FS 349.00 AND APPROX. RBL45. C-CHECK RO 2/21/2021. REPAIRED MINOR CORROSION ON CROSSBEAM AT FS 349.00 AND APPROX. RBL45 AS REQUIRED IAW REO 601R-53-21-2745 REV-- DATED 2016-11-18. SEE ATTACHED CONTINUATION CARD FOR WORK PERFODec 22, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056374Floor Support · corrodedLEFT FLOOR SILL HAS MULTIPLE CORROSION AREAS FS409+128 TO FS559 (C-CHECK) RO 2/21/2021 CORROSION WAS REMOVED AND TREATED IAW BOMBARDIER REO 601R-53-41-666 REV C DATED 2012-11-06. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY COMPLETED AND ATTACHED. Dec 21, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056407Skin · chafedRIGHT AILERON LOWER MID LE SKIN IS CHAFED. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED LOWER L/E SKIN ON RT AILERON WITH NEW SKIN IAW CRJ 200 SRM 51-42-21 PAR 6 C AND SRM 51-42-06 PAR 6 A AND APPLIED TOP COAT TO MATCH PAINT IAW CRJ 200 SRM 51-25-21 PAR 6 A-Dec 19, 2020 · N246PS · Cndair CL6002B19 · AileronsSDR SWIA202056384Hinge Fitting · gougedRIGHT AILERON NR 2 HINGE IB AND OB LUGS ARE GOUGED. (C-CHECK) RO 2/21/2021. REPAIRS WERE ACCOMPLISHED IAW MHIRJ REO 601R-57-61-768 REV -- DATED 2021-01-22 AND REO 601R-57-61-324 DATED 2011/11/22 REV. A. FORM 337 AND MAJOR REPAIR TASK CARD 51-900-1003-SKY CODec 19, 2020 · N246PS · Cndair CL6002B19 · AileronsSDR SWIA202056373Skin · chafedRIGHT AILERON UPPER LE SKIN IS CHAFED IN NUMEROUS LOCATIONS IB TO OB. (C-CHECK) RO 2/21/2021. REMOVED DAMAGED RT AILERON UPPER SKIN PANEL AND INSTALLED A NEW SERVICEABLE PANEL IAW CRJ 200 SRM 51-42-06 AND 51-42-21.Dec 19, 2020 · N246PS · Cndair CL6002B19 · AileronsSDR SWIA202056392Nut · corrodedLEFT OB GROUND SPOILER OUTBD MOUNT BOLT NUT IS CORRODED. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED SPOILER OUTBOUND BOLT NUT IAW CRJ200 AMM REF 27-63-01.Dec 18, 2020 · N246PS · Cndair CL6002B19 · SpoilersSDR SWIA202056391Nut · corrodedLEFT SPOILERON MOUNT HINGE MOUNT BOLT NUTS AND KEEPER BOLTS ARE CORRODED. (C-CHECK) RO 2/21/2021. DAMAGED HARDWARE WAS REMOVED IAW CRJ 200 AMM 27-64-01-000-801 AND NEW HARDWARE INSTALLED IAW CRJ 200 AMM 27-64-01-400-801.Dec 18, 2020 · N246PS · Cndair CL6002B19 · SpoilersSDR SWIA202056390Nut · corrodedRIGHT FLIGHT SPOILER IB MOUNT BOLT NUT AND KEEPER BOLTS ARE CORRODED. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED CORRODED HARDWARE ON RT FLIGHT SPOILER IB SIDE IAW CRJ AMM 27-64-05-000-801 AND 27-64-05-400-801.Dec 18, 2020 · N246PS · Cndair CL6002B19 · SpoilersSDR SWIA202056389Nut · corrodedFORWARD KEEL BEAM LT AND RT LINK FWD ATTACH HARDWARE IS CORRODED. (C-CHECK) RO 2/21/2021. REMOVED AND REPLACED ALL CORRODED HARDWARE ON LT AND RT FWD KEEL BEAM LINKS FWD END IAW BOMBARDIER RII. NR 3418 REV A DATED 13 JUN 2020.Dec 18, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, KeelSDR SWIA202056377Intercostal · corrodedFWD JACKING FITTING LT INTERCOSTAL IS CORRODED LOCATED AT FS278 BETWEEN STGR27 AND STGR26L. (C-CHECK) RO 2/21/2021. REPLACED FWD JACK FITTING LT INTERCOSTAL LOCATED AT FS 278 BETWEEN STGR 27 AND STGR 26L IAW REO 601R-53-11-3656 REV -- DATED 2021-01-30 AND CRDec 11, 2020 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056376Skin · dentedCOMPLY WITH SCHEDULED MAINTENANCE CODE: RA56729-601R-53-61-7299 N246PS MXCODEID50918-PR - DURING ALLOWABLE DAMAGE INSPECTION; FOUND DENT AT FUSELAGE STA 626.3, ABOVE RT STR 21, MEASURING 1.34" DIAMETER BY .044" DEEP. COMPLIED WITH REO 601R-53-61-7299. PERMANNov 2, 2020 · N246PS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR VNAA2019010711101Vane · lack of lubeAT ROTATION, THE CREW OBSERVED THE STICK SHAKER AND RECEIVED AN AURAL WARNING AND A STALL FAIL CAUTION MESSAGE. THE CREW DECLARED AN EMERGENCY AND RETURNED TO FIELD. THE AIRCRAFT LANDED WITHOUT FURTHUR INCIDENT. MAINTENANCE LUBRICATED BOTH ANGLE OF ATTACK VANEJan 7, 2019 · N246PS · Cndair CL6002B19 · Stall Warning SystemSDR VNAA2018111699920Seat Track · corrodedLBL9 SEAT TRACK HAS AREA OF CORROSION FROM FS464-FS469 CA REPLACED SEAT TRACKNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699919Seat Track · corrodedLBL 9 SEAT TRACK FROM FS399 TO FS408 HAS SEVERAL AREAS OF CORROSION. CA REPLACED SEAT TRACKNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699918Seat Track · corrodedLBL9 SEAT TRACK FROM FS364-399 HAS SEVERAL AREAS OF CORROSION CA REMOVED AND REPLACED SEAT TRACK IAW CRJ 200 REO 601R-53-00-485.Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699917Floor Support · corrodedFLOORBEAM AT LBL 27 HAS NUMEROUS FASTENER HOLES CORORDED DAMAGED BETWEEN FS 559.00+64 AND FS 621.00. CA REMOVED AND REPLACED DAMAGED AREA OF FLOORBEAMNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018111699916Seat Track · corrodedSEAT RAIL @LBL9 APPROX FS 559.00+112 CORRODED CA REMOVED AND REPLACED CORRODED SEAT TRACK WITH NEW SEAT TRACK IAW CRJ200 AMM 53-00-44-400-801Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699915Seat Track · corrodedSEAT RAIL @RBL9 APPROX. FS559.00 TO 559.00+80 CORRODED CA REMOVED AND REPLACED WITH NEW SERVICEABLE SEAT RAIL AT F.S. 559Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699914Seat Track · corrodedSEAT RAIL @LB9 APPROX. FS 559.00 TO 559.00+80 CORRODED CA REPLACED SEAT TRACKNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699913Bulkhead Web · corrodedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT BLO WL113 5 INCHES LONG 50%FSH FAILED NDT INSPEC-TION CA REPAIRED CRAKCED FS621 BULKHEAD WEB AT BLO, WL113 PER BOMBARDIER REO 601R-53-61-1285, REV E VIEW RNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018111699912Bulkhead Web · crackedFOUND REAR PRESSURE BULKHEAD WEB HAS MULTIPLE INDICATIONS NOTED AT RBL27.50 WL87 2 INCHES LONG 50%FSH FAILED NDT INSPECTION CA REPAIRED CRAKCED FS621 BULKHEAD WEB AT RBL27.50, WL87 PER BOMBARDIER REO 601R-53-61-1285, REV E VIEW RNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018111699911Stiffener · cracked621 BULKHEAD STIFFENER ANGLE BETWEEN LBL36 AND LBL48 AT WL 78.5 IS CRACKED CA REPLACED ANGLENov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR VNAA2018111699910Doubler · corrodedWARDROBE MOUNT DOUBLER LBL36 CORRODED CA R&R DOUBLER.Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR VNAA2018111699909Crossbeam · corrodedFS.280 CROSSBEAM FWD "J" CHANNEL IS CORRODED BETWEEN LBL9 AND RBL9 CA REPLACED CROSSBEAMNov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR VNAA2018111699908Seat Track · corrodedCO: 79201118 JOB 27920115 OP 56 DISCREPANCY: FOUND(CRACK) INDICATION ON L/H 2ND HOLE FROM AFT EDGE OF STRAP 65% FSH APPEOX .5 UP THE TRUNION FAILS NDT. ----------------------------------------------------------------------------------------------------Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699907Seat Track · corrodedCO: 79201118 JOB 27920111 OP 157, 158, 159, AND 160. DISCREPANCY: LH SIDE SEAT TRACKS CORRODED AT THE FOLLOWING F.S.: 364-409+17, 409+17-409+112, 529, AND 545. --------------------------------------------------------------------------------------Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR VNAA2018111699906Seat Track · corrodedCO: 79201118 JOB 27920111 OP 156 DISCREPANCY: RH SIDE SEAT TRACK F.S. 454-F.S. 499 HAS EXFOLIATION CORROSION. ----------------------------------------------------------------------------------------------------------------------------------------Nov 16, 2018 · N246PS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach Fittings
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