N881AS

Service difficulty reports · 206

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 = 'N881AS' 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 SWIA2021073059844Seat Track · corroded* RIGHT SIDE SEAT RAIL STRUCTURE IS CORRODED FORWARDOF FS409.0 +128 MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RIGHT SIDE SEAT RAIL TRACK (P/N 601R38312-31) OF FS364.00 TO FS409.00+16, AND SEAT RAIL TRACK(P/N601R38312-29) OF FJun 1, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021073059843Seat Track · corroded* RH SIDE SEAT RAIL U CHANNEL IS CORRODED. SIDE SEAT RAIL STRUCTURE FORWARD OF FS409.0 +128 IN AREA'S. CIRCLED WITH GREASE PENCIL. (C-CHECK RO 7/27/2021) REMOVED AND REPLACEDRH SIDE SEAT RAIL U CHANNEL (P/N 601R38312-89) FWD AT FS364.00 TO FS409.00+1Jun 1, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021073059842Seat Track · corroded* LH SIDE SEAT RAIL IS CORRODED IN AREA OF FS409+128 AND FWD. MARKED WITH GREASE PENCIL (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED TWO NEW L/H SIDE SEAT TRACKS FWD OF FS409.00+128. REF CRJ200 AMM 53-01-11-000-802 & CRJ200 AMM 53-01-11-400-802.Jun 1, 2021 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA2021073059808Rib · cracked* L/H BATT RIB WEB CRACKED AT UPPER FASTENERS WS 53.60 (C-CHECK RO 7/27/2021) REPAIRED CRACKED LH BATT RIB AT WS5.6 REF BOMBARDIER REO 601R-57-51-046 REV B DATED 2002-02-28 SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SKY, COMPLETED FORMJun 1, 2021 · N881AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2021073059807Hinge · gouged* RH OTBD FLAP HINGE BOX AFT ATTACH FITTING AT WS220.00 GOUGED (C-CHECK RO 7/27/2021) BLENDED DAMAGE ON R/H OTBD FLAP HINGE BOX AFT ATTACH FITTING AT WS220.00 TO A SMOOTH CONTOUR AND RESTORED FINISH. REMAINING MATERIAL IN REWORKED AREA IS WITHIN LIMITS.May 28, 2021 · N881AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA202159806Rib · crackedR/H BATT RIB ANGLE P/N 601R10203-25 CRACKED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED R/H BATT RIB ANGLE P/N 601R10203-25. REF DWG 601R10203 REV -G AND CRJ200 SRM 51-42-21. COMPLIED WITH TASK CARD 51-900-1003-SKY.May 27, 2021 · N881AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2021073059805Intercostal · crackedPOTENTIAL CRACK ON PAX DOOR INTERCOSTAL AT DD1 AFT SIDE OF DOOR. (MARKED) (C-CHECK RO 7/27/2021) REMOVED DAMAGED INTERCOSTAL. REPLACED AND INSTALLED NEW DD1 INTERCOSTAL P/N 601R31902-318 REF. CRJ200 SRM 51-42-06, AND DWG# 601R31702 REV -N. COMPLIED WITHMay 27, 2021 · N881AS · Cndair CL6002B19 · Passenger/Crew DoorsSDR SWIA2021073059860Hinge · corroded* RH INBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED R/H I/B GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059859Hinge · corroded* RH OTBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HINGE HARDWARE RIGHT OUTBOARD GROUND SPOILER REF CRJ 200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-65-01-400-801. OPERATIONAL TEST GOOD REMay 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059858Pcu · corroded* RH OTBD GROUND SPOILER TO PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT OUTBOARD GROUND SPOILER TO PCU REF CRJ 200 AMM 27-65-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-65-01-400-801. OPERATIONAL TEST GOOD RMay 26, 2021 · N881AS · Cndair CL6002B19 · Drag Control SystemSDR SWIA2021073059857Hinge · corroded* RH FLIGHT SPOILER HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HINGE HARDWARE RIGHT FLIGHT SPOILER HINGE REF CRJ 200 AMM 27-64-05-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-64-05-400-801. OPERATIONAL TEST GOOD REF CRJ May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059856Pcu · corroded* RH FLIGHT SPOILER INBD AND OTBD PCU€™S HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED HARDWARE RIGHT FLIGHT SPOILER INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62-01-400-801. May 26, 2021 · N881AS · Cndair CL6002B19 · Drag Control SystemSDR SWIA2021073059855Pcu · corroded* RH SPOILERON INBD AND OTBD PCU€™S LOWER ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED CORRODED LOWER ATTACH HARDWARE RIGHT SPOILERON INBOARD AND OUTBOARD PCUS REF CRJ 200 AMM 27-62-01-000-801 AND INSTALLED NEW HARDWARE REF CRJ 200 AMM 27-62May 26, 2021 · N881AS · Cndair CL6002B19 · Drag Control SystemSDR SWIA2021073059854Hinge · corroded* RH SPOILERON HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED RH SPOILERON IB AND OB HINGE ATTACHING HARDWARE IAW CRJ-200 AMM 27-64-01-000-801 AND 27-64-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILSMay 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA202159853Hinge · corroded* LH INBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH INBD GROUND SPOILER HINGE HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059852Pcu · corroded* LH INBD GROUND SPOILER PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH INB GROUND SPOILER PCU HARDWARE REF CRJ-200 AMM 27-63-01-000-801, AND 27-63-01-400-801May 26, 2021 · N881AS · Cndair CL6002B19 · Drag Control SystemSDR SWIA2021073059851Hinge · corroded* LH OTBD GROUND SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH OTBD GROUND SPOILER HINGE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059850Pcu · corroded* LH OTBD GROUND SPOILER PCU HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH OTBD GROUND SPOILER PCU HARDWARE IAW CRJ-200 AMM 27-65-01-000-801 AND 27-65-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR DETAILS.May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059849Attach Fitting · corroded* LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED LH FLIGHT SPOILER OTBD PCU ATTACH HARDWARE IAW CRJ-200 AMM 27-62-01-000-801 AND 27-62-01-400-801, OPERATIONAL TEST CHECKED GOOD, SEE CONTINUATION CARD FOR May 26, 2021 · N881AS · Cndair CL6002B19 · Wing, Attach FittingsSDR SWIA2021073059848Hinge · corroded* LH FLIGHT SPOILER HINGE HARDWARE CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED 4 BOLTS, 4 NUTS, 12 WASHERS AND 4 COTTER PINS. REF. CRJ200 AMM 27-64-05-000-801 AND CRJ200 AMM 27-64-05-400-801 CALIBRATED TOOL USED TUC 5659 CAL DUE DATE 28 FEB 22May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059847Hinge · corroded* LH SPOILERON HINGE HARDWARE IS CORRODED (C-CHECK RO 7/27/2021) REMOVED AND REPLACED 4 BOLTS, 4 NUTS, 12 WASHERS AND 4 COTTER PINS ON LH SPOILERON HINGE. REF. CRJ200 AMM 26-64-01-000-801 AND CRJ200 AMM 27-64-01-400-801 CALIBRATED TOOL USED TUC5659 CAL May 26, 2021 · N881AS · Cndair CL6002B19 · SpoilersSDR SWIA2021073059804Rib · cracked*R/H BATT RIB WEB CRACKED AT UPPER FASTENERS WS53.60 (C-CHECK RO 7/27/2021) REMOVED DAMAGED R/H BATT RIB. REPLACED AND INSTALLED NEW BATT RIB P/N 601R10203-28 AT WS53.60 REF. CRJ200 SRM 51-42-21, AND DWG 601R10203 REV -G. COMPLIED WITH TASK CARD 51-900May 26, 2021 · N881AS · Cndair CL6002B19 · Wing, Rib/BulkheadSDR SWIA2021073059803Fastener · damagedRH OUTBOARD FLAP HAS 9EA SMOKING RIVETS AT APPROX WS226.51. (C-CHECK RO 7/27/2021) REPAIRED RH OUTBOARD FLAP 9EA SMOKING RIVETS AT APPROX WS226.51 BY COMPLYING WITH REO 601R-57-53-1220 REV-- DATED 2021-06-21, COMPLIED WITH TASK CARD 51-900-1003-SKY, SEEMay 26, 2021 · N881AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021073059802Frame · bent* AFT EQUIPMENT BAY FS700.00 FRAME BENT BETWEEN STGR 1L & STGR 1R (MARKED) (C-CHECK RO 7/27/2021) HAND DRESSED FS700.00 FRAME LWR LIP TO ORIGINAL CONTOUR AND INSTALLED REINFORCEMENT REPAIR ANGLE. REO 601R-53-61-7661 REV -- DATED 2021-06-21. COMPLIED WITMay 25, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, FrameSDR SWIA2021073059801Angle · cracked* L/H WING CAP ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS 48.30 CRACKED (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW LH WING CAP ATTACHED AT LOWER SIDE OF UPPER WING SKIN AT WS4.830 REF CRJ 200 SRM 51-42-21 AND BOMBARDIER DWG 601R10204 REV J CMay 25, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2021073059800Attach Angle · cracked* R/H WING CAP ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED DAMAGED CAP ANGLE, REPLACED AND INSTALLED NEW R/H WING CAP ANGLE P/N 600-10389-2 ATTACHED TO LOWER SIDE OF UPPER WING SKIN PANEL AT WS48.30May 24, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2021073059799Attach Angle · cracked* R/H WING ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED DAMAGED ANGLE, REPLACED AND INSTALLED NEW ANGLE P/N 600-10204-28 REF. CRJ200 SRM 51-42-21, CRJ200 SRM 51-42-06, AND DWG 600-10204 REV -M. COMPLMay 24, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2021073059798Attach Angle · cracked* L/H WING ANGLE ATTACHED TO LOWER SIDE OF UPPER WING SKIN AT WS48.30 CRACKED. (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW LH WING ANGLE ATTACHED TO UPPER SIDE OF WING SKIN AT WS48.3 REF CRJ 200 SRM 51-42-06 AND DWG 600-10204 REV M. COMPLIED WITH 5May 24, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR SWIA2021073059797Bracket · cracked* LH MLG WHEEL WELL BRACKET P/N 601R75262-159 IS CRACKED (MARKED) (C-CHECK RO 7/27/2021) REMOVED AND INSTALLED NEW BRACKET IN THE LH MLG WHEEL WELL. REF CRJ200 SRM 51-42-06 SEE CONTINUATION CARD FOR FURTHER DETAILSMay 24, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2021073059796Vane · chafedLH INBOARD FLAP VANE REPAIR STRIP INBOARD SIDE IS CHAFED THROUGH (C-CHECK RO 7/27/2021) CHAFE DAMAGE IS 100% THROUGH REPAIR STRIP AND NO ALLOWABLE LIMITS PROVIDED FOR STRIP IN CRJ200 SRM CHAPTER 57. PER SKYWEST REQUEST REPLACE L/H FLAP VANE L/E SKIN INMay 21, 2021 · N881AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2021073059795Skin · chafed* LEFT SIDE AILERON UPPER LEADING EDGE SKIN IS CHAFFED ALONG ITS ENTIRE LENGTH. (C-CHECK RO 7/27/2021) REPLACED LEFT SIDE AILERON UPPER LEADING EDGE SKIN P/N 601R13031-165 REF CRJ 200 SRM 51-42-06 AND DWG 601R13031 REV K. REO 670-57-61-194 REV -C DATEMay 19, 2021 · N881AS · Cndair CL6002B19 · AileronsSDR SWIA2021073059794Housing · chafed* GALLEY SERVICE DOOR EXTERIOR HANDLE HOUSING HAS CHAFFES. (C-CHECK RO 7/27/2021) REPAIRED GALLEY SERVICE DOOR EXTERIOR HANDLE HOUSING PER BOMBARDIER REO 601R-52-41-235 REV -A 2017-06-07 AND MHIRJ REO 601R-52-41-468 REV -- 2021-06-11 / BLEND OUT OF DAMMay 9, 2021 · N881AS · Cndair CL6002B19 · Galley DoorsSDR SWIA2021073059793Web · cracked* LEFT SIDE TRU BAY FLOOR WEB HAS SUSPECTED CRACK NEAR ACCUMULATOR PRESSURE GAUGES. (C-CHECK RO 7/27/2021) REPAIRED LEFT SIDE TRU BAY FLOOR WEB REF REO 601R-53-11-081 REV NC DATED 97-07-02. SEE CONTINUATION CARD FOR DETAILS. COMPLIED WITH 51-900-1003-SMay 9, 2021 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA2021073059792Skin · dentedADM#N881AS-6539. 26 BLENDS FOUND ON LOWER FUSELAGE, FS265.00- FS295.00 STGR24R FOR REPAIR REFERENCE REO 601R-53-00-733 FOR MEASUREMENTS OF BLENDS. PERMANENT REPAIR REQUIRED AT C CHECK. (C-CHECK RO 7/27/2021) EVALUATED, HAND DRESSED 26 IDENTIFIED DENTS, May 6, 2021 · N881AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2018123126081Acm · weakTHE CREW REPORTED STRONG ODOR OF FUEL FROM LEFT PACK WITH BLEEDS ON ENGINE OR APU. APPEARS TO BE STRONGER WITH LEFT PACK OUTPUT SET TO ABOVE 40 DEGRESS C. MAINTENANCE PLACED LEFT PACK ON MEL. SUPPLEMENT TO FOLLOW.Dec 26, 2018 · N881AS · Cndair CL6002B19 · Cabin Cooling SystemSDR ASOA201812035349Bulkhead · damagedREPAIR DAMAGE TO RT 9G BULKHEAD AFT SIDE INSERT/RIVNUT LOCATIONS. REPAIRED DAMAGE IAW EO CL-600-2B19-53-L05915 DATED 11/21/2018 AND EC/TC EO CL-600-2B19-53-L05915.Dec 3, 2018 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA201812035348Bulkhead · damagedREPAIR DAMAGE TO CENTER 9G BULKHEAD AFT SIDE AT INSERT/RIVNUT LOCATIONS. REPAIRED DAMAGE IAW EO CL-600-2B19-53-L05914 DATED 11/21/2018 AND EC/TC EO CL-600-2B19-53-L05914 REV 0, DATED 2018-11-26.Dec 3, 2018 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018121935347Bulkhead · damagedREF: CO# 7496618 JOB# 7749663 OP# 1: REPAIR DAMAGE TO L/H SIDE 9G BULKHEAD AFT SIDE AT INSERT/RIVNUT LOCATIONS.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER EO# CL-600-2B19-53-L05913 DATED 11/21/2018 AND EXPRESSJET EC/TC EO# CL-600-2B19-53-L05913 REV.0, DATED 2018-1Dec 3, 2018 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR ASOA2018121935346Skin · dentedREF: CO# 7496618 JOB# 7749665 OP# 30: 2EA DENTS ON FUSELAGE SKIN BETWEEN F.S.235.00 AND F.S.250.00, STRINGER 24L AND STRINGER 25L.C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER REO 601R-53-11-3352 REV.A, DATED 2018/11/29 AND EXPRESSJET EC/TC REO 601R-53-11-3352 REV.ADec 3, 2018 · N881AS · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR ASOA2018121935345Skin · crackedREF: CO# 7496618 JOB# 7749665 OP# 35: LOWER WING PLANK CUTOUT FOR R/H BOOST PUMP HAS AN INDICATION NOTED ON THE LOWER SURFACE OF THE WNG PLANK ON THE AFT SIDE OF CUT OUT. INDICATION IS .150" LONG BY 100% FSH. FAILED NDT INSPECTION.C/A: REPAIRED DAMAGE I.A.W. Dec 3, 2018 · N881AS · Cndair CL6002B19 · Wing, Plate/SkinSDR ASOA2018121935344Floorbeam · damagedREF: CO# 7496618 JOB# 7749668 OP# 4: FOUND TWO ELONGATED HOLES NEAR F.S. 574.00 L/H SIDE. (1EA) HOLE ON INBD ANGLE OF FWD TIE DOWN AND ANOTHER ON THE FLOOR SUPPORT BEAM AT ANGLE ATTACHING POINT. HOLE ON ANGLE MEASURES .223" AND HOLE ON FLOOR SUPPORT BEAM MEADec 3, 2018 · N881AS · Cndair CL6002B19 · Fuselage Main, Floor BeamSDR ASOA201812145337Skin · dentedREF: CO# 7496618 JOB# 7749661 OP# 28: DENT ON L/H INBOARD FLAP, LOWER SURFACE APPROX. 3.50" FROM INBOARD EDGE AND 1.00" FROM TRAILING EDGE. .500" IN DIAMETER, .020" DEEP. C/A: REPAIRED DAMAGE I.A.W. BOMBARDIER CRJ200 SRM 57-20-00, REPAIR #3 - INBOARD FLAP ANov 24, 2018 · N881AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA2018051444654Wire Harness · defectiveGEAR DISAGREE ON CLIMB OUT JUST PRIOR TO FL180. NOSE GEAR POSITION INDICATION MISSING (HASHED OUT). BTMS CAME UP ALSO. LASTED FOR 10 SECONDS AND WARNING AND GEAR INDICATIONS WENT AWAY. SHORTLY AFTER, THE GEAR INDICATION CAME UP AGAIN WITH A MISSING NOSE GEAR IMay 14, 2018 · N881AS · Cndair CL6002B19 · Landing Gear System WiringSDR SWIA201743426Bulkhead Web · no testFOUND REAR PRESSURE BULKHEAD WEB HAS 9 AREAS THAT FAILED NDT INSPECTION. REPAIRED THE PRESSURE BULKHEAD WEB.May 16, 2017 · N881AS · Cndair CL6002B19 · Fuselage Main, BulkheadSDR SWIA201743430Floor Support · corrodedCARGO BAY FLOOR SUPPORT AT LBL 9 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.May 12, 2017 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR SWIA201743429Cargo Track · corrodedCARGO TRACK AT RBL 9 BETWEEN BS 559+80 AND 570 CORRODED. REMOVED AND REPLACED IAW AMM.May 12, 2017 · N881AS · Cndair CL6002B19 · Fuselage, Seat/Cargo Attach FittingsSDR SWIA201743428Skin · dentedRIGHT INBD FLAP UPPER SKIN DENTED. REPAIRED THE FLAP SKIN IAW SRM.May 12, 2017 · N881AS · Cndair CL6002B19 · Trailing Edge FlapsSDR SWIA201743427Floor Support · corrodedCARGO BAY FLOOR SUPPORT AT BS 570 - 621, LBL 27 CORRODED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW REO.May 12, 2017 · N881AS · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR ASOA2016071415089Light · brokenON ENTERING ACFT, FOUND WHITE EMERGENCY EXIT LIGHT, DETACHED FROM BULKHEAD. REMOVED AND REPLACED THE LIGHT IAW AMM 33-51-19. OPS CHECKED GOOD.Jul 14, 2016 · N881AS · Cndair CL6002B19 · Emergency LightingSDR ASOA2015041512603Battery Pack · inoperativeF/A FLASHLIGHT INOPERATIVE. REPLACED BATTERIES IN FLASHLIGHT IAW 25-60-00.Apr 11, 2015 · N881AS · Cndair CL6002B19 · Emergency Equipment
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