N876AS

Service difficulty reports · 267

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 = 'N876AS' 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 SWIA202056227Seat Track · corroded* MOST FWD RIGHT BL9 SEAT RAIL FROM JUST AFT OF APPROX. FS409.00 GOING FORWARD IS CORRODED ON MULTIPLE ELEMENTS AND AROUND FASTENER HOLES IN NUMEROUS LOCATIONS ALONG ITS ENTIRE LENGTH. (MARKED) (C-CHECK) RO 2/9/2021 INSTALLED NEW SEAT RAIL AT RBL9 FROM F.SDec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA202056226Nut · corrodedLH WING IB AND OB GROUND SPOILERS MOUNTING HARDWARE OB NUTS CORRODED. (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED 2 EACH NEW NUTS P/N MS17825-5 AND 2 EACH NEW COTTER PINS P/N MS24665-155 ON THE LEFT HAND WING INBOARD AND OUTBOARD GROUND SPOILERS, OUTBOARDDec 9, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056222Nut · corrodedRH WING OB GROUND SPIOLER PCU CONNECTING HARDWARE NUTS CORRODED. (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED NEW NUTS AND COTTER PINS ON THE RH OUTBOARD GROUND SPOILER PCU ATTACH LINK. REF - CRJ 200 AMM 27-65-01-000-801 STEP3B (1-2) AND CRJ 200 AMM 27-65-0Dec 9, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056221Nut · corrodedRH WING GROUND SPIOLER IB AND OB MOUNTING HAARDWARE NUTS CORRODED. (C-CHECK) RO 2/9/2021 REMOVED AND INSTALLED 2 EACH NEW NUTS P/N MS17825-5 AND 3 EACH NEW COTTER PINS P/N MS24665-231 ON RH OTBD GROUND SPOILER, INBD AND OTBD HINGES. REF - CRJ 200 AMM 27-65Dec 9, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056220Nut · corrodedRH WING SPOILERON IB AND OB MOUNTING HARDWARE NUTS CORRODED. (C-CHECK) RO 2/9/2021 INSTALLED NEW HARDWARE FOR RH WING SPOILERON INBOARD AND OUTBOARD HINGE POINTS. REF. CRJ200 AMM 27-64-01-400-801. SEE CONTINUE CARD FOR DETAILS.Dec 9, 2020 · N876AS · Cndair CL6002B19 · SpoilersSDR SWIA202056212Rib · cracked*RH WING BATT RIB CAP AT WS 48.30 BETWEEN APPROX. FS 529.00 - 544.00 IS CRACKED (C-CHECK) RO 2/9/2021 REMOVED CRACKED RH WING BATT RIB CAP AND REPLACED WITH NEW AT WS 48.30 BETWEEN APPROX. FS 529.00 - 544.00 IAW CRJ SRM 51-42-21Dec 9, 2020 · N876AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA202056175Stringer Splice · corroded*SPLICE ANGLE FOR STGR26R AT THE AFT SIDE OF THE FS409 JOINT IS CORRODED. (MARKED) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED SPLICE ANGLE FOR STGR 26R AT THE AFT SIDE OF THE F.S 409 JOINT REF. DWG 601R31057 REV J, CRJ-200 SRM 51-42-06 AND CRJ-200 SRM 51-4Dec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202056174Intercostal · corroded*INTERCOSTAL TO THE RIGHT OF STGR27, BETWEEN FS394 AND FS409, HAS CORROSION. (MARKED) (C-CHECK) RO 2/9/2021 BLENDED CORROSION ON INTERCOSTAL TO THE RIGHT OF STGR27, BETWEEN FS394 AND FS409 WITHIN LIMITS IAW MHI REO 601R-53-21-3381 REV -- DATED 2020-12-31. Dec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056173Skin · corroded*FREEZE PLUG IN THE SKIN IS CORRODED BETWEEN FS295 AND FS310, AND STGR25L AND STGR24L. (MARKED) (C-CHECK) RO 2/9/2021 REPAIRED SKIN AREA BETWEEN F.S 295 AND F.S 310, STR25L AND 24L REF. MHIRJ REO 601R-53-21-3376 REV. -- DATED 2021-01-06. COMPLIED WITH TASKDec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202056172Floor Support · corroded*RIGHT BL9 FLOOR BEAM FROM APPROX. FS 409.00+16 TO APPROX. FS409.00+128 HAS CORROSION. (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED FLOOR BEAM CAP AT RBL9 FLOOR BEAM APPROX. FS409.00+16 - FS409.00+128 REF CRJ200 SRM 51-42-22, SRM 51-42-21, DWG 601R31005 REVDec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056171Floor Support · corroded*LEFT BL9 FLOOR BEAM FROM APPROX. FS 409.00+32 TO APPROX. FS409.00+128 HAS CORROSION. (C-CHECK) RO 2/9/2021 BLENDED CORROSION ON THE LBL9 FLOOR BEAM FROM APPROX. FS.409+32 TO FS.409+128 AND FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED FLOOR BEAM CAP ODec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056170Cap · cracked*LH WING BATT RIB CAP AT WS 48.30 BETWEEN APPROX. FS 529.00 - 544.00 IS CRACKED (C-CHECK) RO 2/9/2021 LH WING BATT RIB CAP AT WS48.30 REMOVED AND REPLACED. REF CRJ200 SRM 51-42-21 AND DWG 601R10204 REV J / COMPLIED WITH TASK CARD 51-900-1003-SKY.Dec 9, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, StructureSDR SWIA202056219Hinge Arm · corrodedRH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND 264.00 MOUNTING HARDWARE IS WORN AND CORRODED (C-CHECK) RO 2/9/2021 ODERED, RECEIVED AND INSTALLED NEW HARDWARE ON RH OUTBOARD- FLAP HINGE ASSEMBLY AT WS178.00 WS220.00 AND WS264.00. 15 BOLTS, 12 NUTSDec 8, 2020 · N876AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056218Hinge Arm · corrodedLH OTBD FLAP HINGE ARM ASSY'S AT WS178.00, WS220.00 AND 264.00 MOUNTING HARDWARE IS WORN AND CORRODED (C-CHECK) RO 2/9/2021 ORDERED AND RECEIVED NEW HARDWARE. SEE CAMP 21866107 JOB 2757660 OP 553 FOR INSTALL. 1 PIN, 14 NUTS, 14 BOLTS, 37 WASHERS.Dec 8, 2020 · N876AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056211Stringer · cracked* IN THE AFT EQUIPMENT BAY, THE INTERCOSTAL THAT RUNS ADJACENT TO STRINGER 14R BETWEEN FS 621 TO FS 625 IS CRACKED IN THE RADIUS ON ITS AFT END. (MARKED WITH ORANGE FLAG TAPE) (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED NEW INTERCOSTAL P/N 601-3501252 ADJACDec 8, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Longeron/StringerSDR SWIA202056169Fitting · chafedL/H WING TO FUSELAGE FITTING - FS 473 - LOWER ATTACH FITTING SHOWS EVIDENCE OF CHAFFING ON EXTERIOR PANEL 2 PLACES AS MARKED (C-CHECK) RO 2/9/2021 REMOVED CHAFFING AT THE LH WING TO FUSELAGE FITTING FS.473 LOWER ATTACH FITTING REF CRJ 200 SRM 51-12-00 FOUNDec 8, 2020 · N876AS · Cndair CL6002B19 · Fuselage, Wing Attach FittingsSDR SWIA202056168Skin · corroded* THE LOWER FUSELAGE SKIN'S EXTERNAL SURFACE HAS CORROSION AND CHAFING UNDER ACCESS PANEL 195BB, BETWEEN FS 559+112 AND FS 574, AND BETWEEN STRINGERS 21L AND 21R. (C-CHECK) RO 2/9/2021 REMOVED THE CORROSION AND CHAFFING UNDER ACCESS PANEL 195BB BETWEEN FS.Dec 8, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR SWIA202056242Attach Angle · gouged* THE VERTICAL STABILIZER'S LH AND RH FRONT SPAR TO FUSELAGE SPLICE STRAP RIB ATTACH ANGLES ARE GOUGED ON THEIR OUTBOARD SIDES. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 2/9/2021 REMOVED GOUGED DAMAGE ON VERTICAL STAB FRONT SPAR TO FUSELAGE SPLICE STRAPDec 7, 2020 · N876AS · Cndair CL6002B19 · Vertical Stabilizer, Attach FittingsSDR SWIA202056225Link · corrodedRH AILERON FLUTTER DAMPER SHEAR LINK IS SEIZED HAS EVIDENCE OF PITTING CORROSION (C-CHECK) RO 2/9/2021 REPLACED R/H AILERON FLUTTER DAMPER SHEAR PIN LINK IAW CRJ 200 AMM 27-15-05-400-802 SEE CONTINUATION CARD FOR WORK ACCOMPLISHEDDec 7, 2020 · N876AS · Cndair CL6002B19 · AileronsSDR SWIA202056224Link · seizedLH AILERON FLUTTER DAMPER SHEAR LINK IS SEIZED HAS EVIDENCE OF PITTING CORROSION. (C-CHECK) RO 2/9/2021 REPLACED L/H AILERON FLUTTER DAMPER SHEAR PIN LINK IAW CRJ 200 AMM 27-15-05-400-802 SEE CONTINUATION FOR WORK ACCOMPLISHEDDec 7, 2020 · N876AS · Cndair CL6002B19 · AileronsSDR SWIA202056167Splice · gouged* THE VERTICAL STABILIZER'S RH FRONT SPAR TO FUSELAGE SPLICE STRAP IS GOUGED ON ITS OUTBOARD SIDE. (MARKED WITH RED GREASE PENCIL) (C-CHECK) RO 2/9/2021 REMOVED THE GOUGE ON THE V-STAB RH FRONT SPAR TO FUSELAGE SPLICE STRAP ON THE OTBD SIDE AND FOUND TO BEDec 7, 2020 · N876AS · Cndair CL6002B19 · Vertical StabilizerSDR SWIA202056223Vane · corrodedLH INBOARD FLAP INBOARD FLAP VANE ACTUATOR INNER SPRING AND HARDWARE HAS CORROSION. (C-CHECK) RO 2/9/2021 REPLACED L/H I/B FLAP VANE ACTUATOR INNER SPRING HARDWARE IAW CRJ 200 AMM 27-54-16-400-801Dec 4, 2020 · N876AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202056166Skin · chafedRH AILERON HAVE CHAFING DAMAGE ALONG LEADING EDGE AS MARKED (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED THE R/H AILERON LEADING EDGE SKIN (P/N 601R13031-166) REF CRJ-200 SRM 51-12-00, CRJ-200 SRM 57-60-00, REO 601R-57-61-577 REV--, DATED 2017-05-24, CRJ-200Dec 4, 2020 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202056165Skin · chafedRH INBOARD FLAP VANE LEADING EDGE IS CHAFED AT CNETER LOCATION AS MARKED. (C-CHECK) RO 2/9/2021 REMOVED AND REPLACED R/H INBD FLAP VANE CENTER LEADING EDGE. REF CRJ200 SRM 51-42-13 & DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKYDec 3, 2020 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR SWIA202056217Threshold · crackedSERVICE DOOR THRESHOLD HAS EXFOLIATED CORROSION (C-CHECK) RO 2/9/2021 ORDERED AND RECEIVED SERVICABLE SERVICE DOOR THRESHOLD SEE CAMP#21866078 JOB 0 OP 513 FOR INSTALLATION. SEE CONTINUE CARD FOR WORK PERFORMED.Dec 2, 2020 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA202056164Angle · damaged* PASSENGER DOOR FRAME SEAL ANGLE DAMAGED AT PREVIOUS REPAIR AT FS 349 MARKED (C-CHECK) RO 2/9/2021 REMOVED EXISTING REPAIR ON THE PAX DOOR FRAME AT FS.349, INSTALLED A NEW REPAIR AND COMPLIED WITH ALL APPLICABLE STEPS OF REO 601R-53-22-033 REV -D DATED 2Dec 2, 2020 · N876AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA202056163Bulkhead · crackedCOMPLY WITH SCHEDULED MAINTENANCE CODE: AD 2019-08-04/02 40000 FC - COMPLY WITH PARAGRAPH (J) OF AD 2019-08-04 BY: (J)(1) DOING A NONDESTRUCTIVE INSPECTION FOR CRACKING OF THE FORWARD FACE OF THE FUSELAGE STATION (FS) 621 PRESSURE BULKHEAD, IN ACCORDANCE WITHNov 5, 2020 · N876AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2019080646138O-Ring · leakingHYD 3 LO PRESS MESSAGE IN FLIGHT. DIVERTED. (FLT#5440) REMOVED AND REPLACED THE FAULTY O-RING AND BACKUP RING IAW AMM. LEAK CHECK SATISFACTORY. SERVICED AND BLED THE HYDRAULIC SYSTEM #3 IAW AMM. NO LEAKS NOTED AND NO DEFECTS NOTED AT THIS TIME.Aug 6, 2019 · N876AS · Cndair CL6002B19 · Hydraulic System, MainSDR ASOA201902055033Skin · dentedFWD RIGHT SIDE FUSELAGE SKIN HAS A DENT AT APPROXIMATELY FS234 BETWEEN STRINGERS 14R AND 15R. REPAIRED DAMAGE IAW EA 45-2019-003.Feb 5, 2019 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201902045032Bearing · wornRT AILERON FAILED BACKLASH ON SYSTEM NR 2 AT 0.113 AND SYSTEM NR 3 AT 0.105, MAX IS 0.085. REPAIRED IAW REO 601R-57-61-004 REV E DATED 2014-12-08 AND ECTC REO 601R-57-61-004.Feb 4, 2019 · N876AS · Cndair CL6002B19 · AileronsSDR ASOA201902035030Skin · dentedFORWARD RT SIDE FUSELAGE SKIN HAS A DENT AT APPROX FS260 BETWEEN STRINGERS 16R AND 17R. REPAIRED DAMAGE IAW EA 45-2019-002 DATED 2019-01-22.Feb 3, 2019 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201902035029Skin · chafedWING ACCESS HOLE 550EB HAS AREAS OF CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-030 REV L DATED 2014-02-05 AND ECTC EO600-57-81.Feb 3, 2019 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201901295026Hinge · corrodedELEVATOR HINGE P/N 600-24043 AT ES 16.520 CORRODED IN THE BORE. REPAIRED IAW EC/TC RIL0183.Jan 29, 2019 · N876AS · Cndair CL6002B19 · Elevator StructureSDR ASOA5201901135017Door Sill · corrodedREF: CO 7576618 JOB 757668 OP 4: CARGO DOOR FLOOR SILL CORRODED BETWEEN FS 574.00 AND FS 621.00. C/A: REPAIRED DAMAGE IAWREO 601R-53-61-1574 REV.B, DATED 2012-04-15 AND EC/TC REO 601R-53-61-1574 REV.A, DATED 2018-08-31.Jan 13, 2019 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201901135016Skin · gougedREF: CO 7576618 JOB 757661 OP 78: EXTERNAL SKIN IS GOUGED WITH HIGH METAL JUST AFT OF APU EXHAUST, FS 672.00. C/A: REPAIRED DAMAGE IAW EA 45-2019-007 REV.--, DATED 01/06/2019 AND EC/TC EA 45-2019-007 REV.0, DATED 2019-01-10.Jan 13, 2019 · N876AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA201901135015Door Sill · corrodedREF: CO 7576618 JOB 757668 OP 8: LT PRESSURE FLOOR SILL HAS CORROSION AROUND 2(EA) SCREW HOLES. LOCATED AFT OF FS 449.00 IN THE SILL WEB. C/A: REPAIRED DAMAGE IAW REO 601R-53-41-666 REV.C, DATED 2012-11-06 AND EC/TC REO 601R-53-41-666 01 REV.A, DATED 2013-10-2Jan 13, 2019 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA201901105028Skin · chafedWING ACCESS HOLE 650BB HAS AREAS OF CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-030 REV L DATED 2014-02-05 AND ECTC EO600-57-81.Jan 10, 2019 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201901105027Skin · chafedWING ACCESS HOLE 55HB HAS AREAS OF CHAFING DAMAGE. REPAIRED DAMAGE IAW REO 601R-57-21-030 REV L DATED 2014-02-05 AND ECTC EO600-57-81.Jan 10, 2019 · N876AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA201901105014Roll Pin · migratedREF: CO 7576618 JOB 757661 OP# 53: PAX DOOR HINGE PIN ROLL PIN MIGRATED AND GOUGED THE HINGE. C/A: REPAIRED DAMAGE IAWREO 601R-53-21-814 REV C, DATED 2017-08-02 AND EC/TC REO 601R-53-21-814 REV.A2018-08-30, DATED 2019-01-03.Jan 10, 2019 · N876AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA201901055031Bulkhead · chafed7 EA CHAFES ON THE FORWARD FACE OF FS 621 BULKHEAD BELOW ENGINE BEAM LBL 36 - RBL 36. REPAIRED CHAFES IAW ECTC REO 601R-53-61-2155.Jan 5, 2019 · N876AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201743394Panel · chafedLEFT AILERON PANEL 599AB CHAFED. REPLACED THE AILERON PANEL IAW SRM.Jun 1, 2017 · N876AS · Cndair CL6002B19 · AileronsSDR SWIA2017062043392Hinge · wornFOUND PIANO HINGE ON FUSELAGE SIDE WITH WORN HOLES FOR PIN. REMOVED AND REPLACED PASSENGER DOOR HINGE FUSELAGE SIDE IAW SRM AND REO. PRESSURE CHECK OF REPAIRED AREA WAS FOUND TO BE GOOD NO LEAKS WERE NOTED IAW AMM.May 19, 2017 · N876AS · Cndair CL6002B19 · Fuselage, Door HingeSDR SWIA2017062043393Bulkhead Web · gougedGOUGES NOTED ON THE BS 621 BULKHEAD WEB, FWD FACE, BELOW CARGO DOOR TRACK ALONG LBL 36.2. REPAIRED THE BULKHEAD WEB IAW REO.May 13, 2017 · N876AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA2017062043391Bulkhead Web · crackedCRACK NOTED ON THE BS 621 BULKHEAD WEB, FWD FACE, ALONG LBL 27.5, UPPER CARGO DOOR TRACK FITTING TO WEB INTERFACE. PERFORMED PERMANENT REPAIR IAW REO. PRESSURE CHECK OF REPAIRED AREA WAS FOUND TO BE GOOD, NO LEAKS WERE NOTED IAW AMM.May 13, 2017 · N876AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015060513066Battery Pack · inoperativeLT AND RT WING EMERGENCY EXIT MID LIGHTS ARE INOPERATIVE. TROUBLESHOT SYS IAW WM 33-52-00 AND ESPM 20-12-01 AND FOUND EMERGENCY LIGHTS BATTERY PACK BAD. REMOVED BATTERY PACK AND INSTALLED SERVICEABLE EMERGENCY LIGHTS BATTERY PACK 3 IAW AMM 33-51-04-000/400-8Jun 4, 2015 · N876AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015060513065Light · brokenGALLEY PANEL EMERGENCY EXIT FLOODLIGHT BROKEN. REPLACED THE FLOODLIGHT IAW AMM 33-51-00-400-801. OPS TESTED GOOD IAW AMM 33-51-00-710-801.Jun 4, 2015 · N876AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015060913072Structure · corrodedFOUND A DENT WITH CORROSION ON LT PRESSURE SILL AT FS 499, LBL 47, TOP AND BOTTOM . REPAIRED IAW REO:601R-53-41-1913.May 28, 2015 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015060413029Floorbeam · corrodedFLOORBOARD SUPPORT ANGLES 2 EA ON FRAME 333 CORRODED. FABRICATED NEW ANGLE, PN 600-32004-50101 IAW SNIEO S03, DWG 601R32004, STEP 1. LOCATED & DRILLED 2 EA FLOOR SUPPORT ANGLES, PN 601R32004-S03 & 600-32004-113 IAW SRM 51-40-11. COMPLIED WITH EC/TC SNIEO 60May 26, 2015 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015060413025Intercostal · corrodedINTERCOSTAL ON STR 26R BETWEEN FS 349 & FS 364 IS CORRODED BEYONG LIMITS. REMOVED INTERCOSTAL IAW SRM 51-42-06. INSTALLED NEW INTERCOSTAL, PN:601R31049-120 IAW SRM 51-42-06 AND 51-42-21.May 24, 2015 · N876AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015060413024Floorbeam · corrodedFS 349, FLOORBOARD SUPPORT BRACKET IS CORRODED BEYOND LIMITS. REMOVED FLOORBOARD BRACKET FROM FS 349 IAW SRM 51-42-06. LOCATED AND DRILLED HOLES IN NEW SERVICEABLE FLOORBOARD SUPPORT, PN:601R32085-71 IAW SRM 51-42-06. INSTALLED NEW FLOORBOARD SUPPORT BRACKEMay 23, 2015 · N876AS · Cndair CL6002B19 · Fuselage Main, Floor Beam
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