N871AS

Service difficulty reports · 156

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 = 'N871AS' 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 SWIA2019082746225Fire Warning · false indicationRECEIVED R ENG FIRE WARNING MESSAGE IN FLIGHT FOR APPROXIMATELY 4 SECONDS. MESSAGE SELF CLEARED BEFORE QRC PROCEDURE STARTED. ALL ENGINE INDICATIONS REMAINED NORMAL. ALL SYSTEM INDICATIONS REMAINED NORMAL. REMOVED AND REPLACED THE RH ENG FIRE DETECTION LOOP Aug 27, 2019 · N871AS · Cndair CL6002B19 · Fire DetectionSDR ASOA2019042433026Bulb · inoperativeTHE CREW REPORTED OVERHEAD EMERGENCY LIGHTING INOPERATIVE AT ROW 10. MAINTENANCE REMOVED AND REPLACED LIGHT BULB AT ROW 10. OPERATIONAL CHECKS WERE GOODApr 23, 2019 · N871AS · Cndair CL6002B19 · Emergency LightingSDR SWIA201744070Structure · dentedDENT AT FS STATION 310 BETWEEN STR 11R AND 10R. (C-CHECK) COMPLIED WITH DENT REPAIR AT FS 310 BETWEEN STR 11R AND 10R IAW REO. PRESSURIZATION CHECK GOOD AT THIS TIME.Dec 11, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744068Structure · dentedFOUND DENT WITH GOUGE AT FS 409+96 STR 22L. (C-CHECK) REPAIRED DENT WITH GOUGE AT FS 409+96 STRINGER 22L IAW REO.Nov 20, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744078Doubler · damagedCIRCULAR WEB REPAIR DOUBLER TO NOSE WHEEL WELL RIGHT HAND SIDE DAMAGED. (C-CHECK) REPAIRED CIRCULAR WEB REPAIR DOUBLER AT NLG WHEEL WELL RT SIDE IAW REO.Nov 17, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744073Floor Support · corrodedFLOORBOARD SUPPORT ANGLE IS CORRODED AT FS 621.00 BETWEEN RBL 9.0 AND RBL 27.0. (C-CHECK) REPAIRED CORROSION ON FS 621 FLOOR SUPPORT ANGLE BETWEEN RBL 9 AND 27 IAW REO.Nov 11, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744072Floor Support · corrodedFLOORBOARD SUPPORT ANGLE IS CORRODED AT FS 621.00 BETWEEN LBL 27.0 AND LBL 45.0. (C-CHECK) REPAIRED FLOORBOARD SUPPORT ANGLE AT FS 621.00 BETWEEN LBL 27.0 AND LBL 45.0 IAW REO.Nov 11, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744077Floor Support · corrodedFLOORBOARD SUPPORT BEAM CAP AT LBL-9 IS CORRODED BETWEEN FS 409.00+128 AND FS 559.00. (C-CHECK) REPAIRED FLOORBOARD SUPPORT CAP AT LBL -9 AT FS 409.00+128 AND FS 559.00 IAW REO.Nov 10, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744075Door Sill · corrodedRT FLOOR SILL IS CORRODED BETWEEN FS 310 AND FS 319.70. (C-CHECK) REMOVED AND REPLACED RT FLOOR SILL BETWEEN FS310 AND FS319.70 IAW SRM.Nov 10, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744074Floorbeam · corrodedFS 349 FLOORBEAM CORRODED RT BETWEEN RBL 27 AND RBL 36. (C-CHECK) REPAIRED FS 349 FLOORBEAM RT BETWEEN RBL 27 AND 36 IAW REO.Nov 10, 2017 · N871AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR SWIA201744071Door Sill · corrodedRT PRESSURE FLOOR SILL IS CORRODED IN 6EA LOCATIONS AROUND FASTENER HOLES BETWEEN FS 424.00 AND FS 484.00. (C-CHECK) REPAIRED RT PRESSURE FLOOR SILL PANEL CORROSION AT SIX LOCATIONS COMMON TO THE NUTPLATE HOLES AT FS-429: FS 435.5: FS441: FS447: FS452: AND FSNov 10, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201744076Bulkhead · damagedINDICATION NOTED AT FS621.00 REAR PRESSURE BULKHEAD FWD FACE AT RBL27.50 WL97.50-WL102.75 APPROX. 5.25" IN LENGTH 50% FULL SCREEN HEIGHT. (C-CHECK) REPAIRED FS 621 BULKHEAD WEB AT RBL 27 IAW REO.Nov 9, 2017 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201744069Structure · dentedDENT FOUND BETWEEN FS 250.00 AND 265.00, BETWEEN STRINGERS 24L AND 25L. (C-CHECK) COMPLIED WITH DENT REPAIR FOUND BETWEEN FS 250.00 AND 265.00 BETWEEN STRINGERS 24L AND 25L IAW REO. PRESSURE CHECK GOOD AT THIS TIME.Nov 7, 2017 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015082113575Plate · damagedEXTERNAL POWER RECEPTACLE DOOR TOP LAND DAMAGED, ON FUSELAGE SIDE. CUT AWAY DAMAGED SECTION OF EXTERNAL POWER RECEPTACLE DOOR UPPER LAND, ON FUSELAGE SIDE, CLEANED UP CUTLINES REF EC/TC REO 601R-53-11-009. FABRICATED, DRILLED AND DEBURRED JOGGLED PLATE, PN Aug 21, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015081413574Skin · dentedFUSELAGE HAS SEVERAL DENTS AT BS 593 BETWEEN STRINGERS 25-26R AND STRINGERS 24-25R. REO 601R-53-61-5529 HAS BEEN ACCOMPLISHED AND ALL STEPS HAVE BEEN DOCUMENTED AND SIGNED FOR ON A NON-ROUTINE WORK CARD.Aug 14, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2015081013566Sign · damagedSERVICE DOOR EXIT SIGN DAMAGED, NEEDS REPLACED. REMOVED DAMAGED SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-000-801. INSTALLED NEW SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-400-801. OPS TEST OF THE "EXIT" SIGN ABOVE THE SERVICE DOOR IS GOOD IAW AMM TASK 33-51-00-Aug 10, 2015 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015080713573Intercostal · damagedUPON REMOVAL OF TOP PLATE, PN 601R38669-73, FOUND 2 EA FASTENER HOLES ELONGATED IN TOP PLATE AND IN UNDER LYING INTERCOSTAL, PN 601R38669-39. REMOVED INTERCOSTAL PT 601R38669-39 AT RBL 38.45, FS 280 IAW SRM 51-42-06. INTERCOSTAL REQUIRES REPLACEMENT. FABRICAAug 7, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080413565Floor Support · corrodedFLOOR SILL DOUBLER FWD OF SERVICE DOOR HAS CORROSION. REMOVED FLOOR SILL DOUBLER FWD OF SERVICE DOOR IAW SRM 51-42-06. INSTALLED NEW SERVICEABLE FLOOR SILL ANGLE FWD OF SERVICE DOOR IAW SRM 51-42-06 & SRM TR 51-32.Aug 4, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015080313564Skin · crackedRIGHT LOWER WING PLANK HAS MULTIPLE INDICATIONS NOTED AT DRAIN HOLE NEAR BOOST PUMP 50 PERCENT FSH AROUND ENTIRE CIRCUMFERENCE, FAILED NDT INSPECTION. BLENDED AREA AROUND DRAIN HOLE .006" MAX MATERIAL REMOVED. AREA MEASURES 2.1" X 2.3". BLENDED AREA IAW SRMAug 3, 2015 · N871AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015080313563Skin · crackedLT LOWER WING PLANK HAS ONE INDICATION NOTED AT WS 87, DRAIN HOLE FWD SIDE .400" LONG BY 90 PERCENT FSH, FAILED NDT INSP. PERFORMED CUTOUT OF DAMAGE TO LT LOWER WING PLANK AT WS 87 DRAIN HOLE FWD SIDE IAW REO NR 601R-57-21-2346. CHAMFER WING PLANK CUTOUT AS RAug 3, 2015 · N871AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2015080113562Frame · corrodedFRAME FS 310, STR 23 & 22R HAS CORROSION AT ATTACHED ANGLE. DAMAGED SECTION OF FS 310, FRAME BETWEEN STR 22R & 23R WAS REPLACED DURING ACCOMPLISHMENT OF REO 601R-53-21-2644.Aug 1, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015073113561Sign · damagedSERVICE DOOR EXIT SIGN DAMAGED, NEEDS REPLACED. REMOVED DAMAGED SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-000-801. INSTALLED NEW SERVICE DOOR EXIT SIGN IAW AMM 33-51-13-400-801. OPS TEST OF THE "EXIT" SIGN ABOVE THE SERVICE DOOR IS GOOD IAW AMM TASK 33-51-00-Jul 31, 2015 · N871AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015073013560Bulkhead · crackedINDICATIONS NOTED AT 621 REAR PRESSURE BULKHEAD, BL 0.00, WL 110.00 APPROXIMATELY 1.700" IN LENGTH VERTICALLY 50 PERCENT FULL SCREEN HEIGHT FAILING NDT. COMPLIED WITH EC/TC REO 601R-53-61-1285 AND GREO 601R-53-61-1285, REV D, DATED 10/31/2011 AS WRITTEN. REO Jul 30, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2015072913559Floor Support · corrodedCARGO FLOOR SUPPORT RIGHT EDGE MEMBER HAS CORROSION FROM FS 559+80 TO FS 559+112. DURING REPAIR OF CABIN FLOOR SILL BETWEEN FS 559+80 TO FS 559+112 RT, FOUND CORROSION TO BE OUT OF LIMITS IAW REO 601R-53-00-526, REV-DATED 22 MAY 13. C/W ECTC REO 601R-53-00-5Jul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072913558Floor Support · corrodedFLOOR SUPPORT TOP PLATE ON RBL 9 HAS CORRSION FROM FS 589 TO FS 621. BLENDED CORROSION FROM FLOOR SUPPORT TOP PLATE AT RBL 9, FS 589 TO FS 621. MAX MATERIAL REMOVED .013. FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005 RIG B. UPON FURTHER INVESTIGATION FOUJul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072913553Seat Track · corrodedFLOOR SUPPORT TOP PLATE ON LBL 9 HAS CORROSION FROM FS 589 TO FS 621. BLENDED FLOOR SUPPORT TOP PLATE AT LB 9, FS 559-FS 621. MAX MATERIAL REMOVED .011. FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005, DETAIL B. UPON FURTHER INVESTIGATION FOUND OUT OF LIMJul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072913552Seat Track · corrodedFLOOR SUPPORT TOP PLATES INBD AND OTBD ON LBL 27 FROM FS 574 TO FS 621 HAS CORROSION ON IT. BLENDED FLOOR SUPPORT TOP PLATE AT RBL 9, FS 589-FS 621 MAX MATERIAL REMOVED .012". FOUND TO BE OUT OF LIMITS IAW REO 601R-53-00-005, DETAIL B. REMOVED CORRODED LBL Jul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072913551Door Sill · corrodedCARGO DOOR SILL IS CORRODED. CLIP AT FS 589 UNDER CARGO DOOR SILL FOUND TO BE CRACKED. REMOVED CLIP IAW SRM 51-42-21. LOCATED NEW FASTENER HOLES ON NEW SERVICEABLE CLIP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-21. DID NOT FABRICATE FLJul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072913550Frame · corrodedFS 589 FRAME IS CORRODED FROM STR 26R TO 23L. UNDER FURTHER INVESTIGATION FOUND DAMAGED AREA TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. INSTALLED NEW FRAME SECTOR AT FS 589 IAW SRM 51-42-06, PN 601R36025-61. REMOVED STR 23R FROM FS 589.00 TO 60Jul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072913549Frame · corrodedFS 605.00 FRAME HAS CORROSION FROM STR 26R TO 22L. UNDER FURTHER INVESTIGATION FOUND DAMAGED AREA TO BE OUT OF LIMITS IAW SRM 53-00-00, FIG 102, SHEET 2. INSTALLED NEW SERVICEABLE FS 605.00 FRAME, PN 601R36026-27 IAW SRM 51-42-06/51-40-11/51-42-21. REMOVED LJul 29, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072813548Vertical Support · crackedFOUND FS 409.00+128, VERTICAL POST BL 0.0, RT SIDE HAS INDICATION NOTED APPROX .250" LONG 60 PERCENT FSH AT AFT FLANGE RADIUS. FAILED NDT INSPECTION. REMOVED FS 409+128 VERT POST ASSY IAW SRM 51-42-06, 51-42-21. C/W ECTC REO 601R-53-41-889 AND MET ALL THE REJul 28, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072813547Intercostal · crackedFS 621 BULKHEAD AFT SIDE INTERCOSTAL IS CRACKED AT STR 14L. DRILLED, LOCATED FASTENERS AS REQUIRED ON NEW INTERCOSTAL. WORK PERFORMED IAW SRM 51-42-06, 51-42-21 & 51-77-00. INSTALLED NEW INTERCOSTAL AT STR 14L IAW SRM 51-42-06, 51-42-21 & 51-77-00.Jul 28, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072713572Hinge · chafedPAX DOOR HINGE ON ACFT SIDE IS CHAFED BY ROLL PIN ON LAST LUG AFT. COMPLIED WITH REO 601R-53-21-814, REPAIR TYPE IV DISPOSITION FOR DAMAGE TO THE HINGE LUG LAND. PASSENGER DOOR HINGE PIN WORN TO LIMITS, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PASSENJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Door HingeSDR ASOA2015072713571Retainer · bentLOWER EDGE OF PAX DOOR SKIN AND SEAL RETAINER IS BENT AT AREA ADJACENT TO PROXIMITY SWITCH. REMOVED LOWER CENTER PAX DOOR SEAL RETAINER IAW SRM 51-42-13. LOCATED, DRILLED & INSTALLED PAX DOOR SEAL RETAINER IAW SRM 51-40-11-00, 51-42-13-00 & REO 601R-52-11-91Jul 27, 2015 · N871AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR ASOA2015072713557Seat Track · corrodedLT FLOOR SEAT RAIL FROM FS 409+112-FS 559+4 HAS SEVERAL AREAS OF CORROSION AROUND SCREWS. REMOVED LT FLOOR SEAT RAIL FROM FS 409+112 TO FS 559+4 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, P/O W35264, FS 409+112-FJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072713556Floor Support · corrodedRT PRESSURE FLOOR SILL PANEL HAS MULTIPLE LOCATIONS OF CORROSION SURROUNDING NUTPLATES FROM FS 409+128 TO FS 559. FOUND QTY 2 BLEND REPAIRS TO FLOOR SILL LOCATED LESS THAN 5" AWAY FROM EACH OTHER. LIMITATION IAW REO 601R-53-41-666-01 IS MINIMUM OF 5" APART. Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072713546Seat Track · corrodedLT AND RT FLOOR SEAT TRACKS FROM FS 559-FS 559+80 HAVE SEVERAL AREAS OF CORROSION AROUND SCREW HOLES. REMOVED LT AND RT FLOOR SEAT TRACKS FROM FS 559 TO FS 559+80 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, PO W35Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072713545Seat Track · corrodedRT FLOOR SEAT RAIL FROM FS 409+112-559+4 HAS SEVERAL AREAS OF CORROSION AROUND SCREW AND AT LEAST 1 AREA OF INTERGRANULAR. REMOVED RT FLOOR SEAT RAIL FROM FS 409-112 TO FS 559+4 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN:N12Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072713544Seat Track · corrodedLT FLOOR SEAT RAIL FROM FS 399-409+112 HAS SEVERAL AREAS OF CORROSION, SOME SEVERE INTERGRANULAR. REMOVED LT FLOOR SEAT RAIL FROM FS 399 TO FS 409 IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN N126-2075, PO W35264, FS 399-FS 4Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072713541Frame · corrodedFS 310 FRAME HAS CORROSION BETWEEN 26L AND 25L ON FWD FACE. REMOVED CORROSION FRAME 601R32002-69 AT STS 310 BETWEEN 25L STR & 25R STR IAW SRM 51-42-06 & SRM 51-42-21. FOUND TO BE OUT OF LIMIT. RECEIVED NEW SERVICEABLE FRAME SECTOR 601R32002-69. LOCATED & DRJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072713542Frame · corrodedFS 295, FRAME HAS CORROSION BETWEEN 26L AND 25L ON AFT SIDE. REMOVED AVIONICS BAY FLOOR SUPPORT BRACKET AT FS 295, BETWEEN STR 25L & 25R IAW SRM 51-42-06. INSTALLED SERVICEABLE AVIONICS BAY FLOOR SUPPORT BRACKET AT FS 295 IAW SRM 51-42-06. REMOVED FS 295, FJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072713540Frame · corrodedFS 310, FRAME IS CORRODED BETWEEN STRS 23R AND 22R. COMPLIED WITH BSC REO 601R-53-21-2644, REV A, DATED 2015/08/11.Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, FrameSDR ASOA2015072713539Floorbeam · crackedFS 280 CROSSBEAM IS CRACKED IN MULTIPLE LOCATIONS. REMOVED 4 EA CLIPS FROM FS 280 AT LBL 9 INBD AND OTBD AND RBL 9 INBD AND OTBD IAW SRM 51-42-06 AND 51-42-21. INSTALLED NEW CLIPS IAW SRM 51-42-06, 51-42-21 AND REO 601R-53-11-171, REV D, 13 FEB 07. CUT AWAYJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA2015072713538Floor Support · corrodedLEFT FLOOR SILL ANGLE HAS CORROSION IN MULTIPLE LOCATIONS BETWEEN FS 409+128 TO FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C, DATED 11/06/12 AS WRITTEN.Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072713537Floor Panel · corrodedLEFT FLOOR SILL PANEL HAS CORROSION AROUND NUTPLATES BETWEEN FS 439 TO FS 461. R & R NUTPLATES BETWEEN FS 439.00 TO FS 461 IAW SRM 51-45-00 AND 51-42-06. COMPLIED WITH EC/TC REO:601R-53-41-666 01 AND REO:601R-53-41-666, REV C.Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Floor PanelSDR ASOA2015072713536Floor Support · corrodedRT PRESSURE FLOOR SUPPORT ANGLE HAS NUMEROUS LOCATION OF CORROSION, FILIFORM, FROM FS 409+128 TO FS 559. COMPLIED WITH EC/TC REO 601R-53-41-666 01 AND REO 601R-53-41-666, REV C.Jul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072713535Seat Track · corrodedRT FLOOR SEAT TRACK FROM BS 399 - 409+112 HAS SEVERAL AREAS OF CORROSION, SOME SEVERE INTERGRANULAR. REMOVED THE SEAT TRACK IAW AMM 53-01-11-000-802 AND SRM 51-41-02. LOCATED HOLES IN BULK MATERIAL, PN: N126-2075, P/O: W35264, FS 399 TO FS 409+112 RT IAW SJul 27, 2015 · N871AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR ASOA2015072613543Angle · corrodedSERVICE DOOR LOWER SILL ANGLE IS CORRODED IN SEVERAL AREAS. REMOVED SERVICED DOOR LOWER SILL ANGLE IAW SRM 51-40-11. INSTALLED NEW LOWER SILL ANGLE AT SERVICE DOOR IAW SRM 51-42-13, 51-42-21, PN 601R38303-253. RECEIVED NEW LOWER SILL ANGLE, PN 601R38303-253Jul 26, 2015 · N871AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2015072513570Cable · chafedLT PYLON, WHITE AND GREEN IDG CABLES ARE CHAFED OTBD OF FEED THRU. REPAIRED WHITE AND GREEN IDG CABLES IN THE LT PYLON IAW REO 601R-24-21-004. COMPLIED WITH EC/TC REO 601R-24-21-004 AND GREO 601R-24-21-004, REV A DATED 07/14/2011 AS WRITTEN.Jul 25, 2015 · N871AS · Cndair CL6002B19 · Nacelle/Pylon, Main FrameSDR ASOA2015072513569Cable · chafedRIGHT PYLON, GREEN IDG CABLE IS CHAFED, APPROXIMATELY 6"-7" OTBD OFF FEED THRU. REPAIRED GREEN 1DG CABLE IN THE RT PYLON IAW REO 601R-24-21-004. COMPLIED WITH EC/TC REO 601R-24-21-004 AND GREO 601R-24-21-004, REV A DATED 07/14/2011 AS WRITTEN.Jul 25, 2015 · N871AS · Cndair CL6002B19 · Nacelle/Pylon, Main Frame
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