N432AW

Service difficulty reports · 229

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 = 'N432AW' 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 A6WA202206208193Engine · overtempAT APROX 80 KTS THE RH ITT WENT RED LINE AT 900 DEG PLUS. REDUCED THROTTLE TO IDLE, ABORTED TO. RH ENG ITT RETURNED TO NORMAL IAT IDLE. BTMS READ 9557. INTERROGATED MDC NO EXCEEDANACES SHOWN THIS DATE. ***AIRCRAFT REMOVED FROM SERVICE *** C/W ENGINE INSPECTJun 20, 2022 · N432AW · Cndair CL6002B19 · Engine Temperature Indicating SystemSDR A6WA202203288156None · gougedIAD MX FOUND TWO GOUGES IN THE CARGO DOOR OUTER SKIN UPPER EDGE. AIRCRAFT WAS FERRIED TO DAY FOR REPAIR. OUTER SKIN WAS REPAIRED WITH REO 601R-52-31-366. DAMAGE WAS MOST LIKELY CAUSED BY INCORRECT HARDWARE INSTALLED IN THE CARGO LINERS ABOVE THE DOOR. WHENMar 28, 2022 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202111157968Doubler · damagedLH WINGLET DOUBLER PN 600-10380-59 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-59, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 33, MATERIAL 0.071Ï¿½ CLAD 202Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111157964Strap · damagedLH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 6, MATERIAL 0.071Ï¿½ CLAD Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111157965Strap · damagedLH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 3, MATERIAL 0.040Ï¿½ CLAD 20Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111157966Strap · damagedLH WINGLET LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET LOWER STRAP PN 600-15108, REF CRJ200 SRM 57-31-31 REV 38, PG5, FIGURE 1, SHT 1, ITEM 8, MATERIAL 0.040Ï¿½ CLAD 20Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111157967Doubler · damagedLH WINGLET DOUBLER PN 600-10380-63 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO LH WINGLET DOUBLER PN 600-10380-63, REF CRJ200 SRM 57-31-31 REV 38, PG6, FIGURE 1, SHT 2, ITEM 34, MATERIAL 0.071Ï¿½ CLAD 202Nov 8, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111057975None · corrodedCORROSION FOUND ON BRACKET ASSEMBLY COMMON TO PASSENGER DOOR SURROUND STRUCTURE FS 318.00 LBL 40. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 318.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.200W X .008D (P2) 2.5L X Nov 5, 2021 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202111197974None · corrodedCORROSION FOUND ON FLOOR STRUCTURE COMMON TO PASSENGER DOOR SURROUND STRUCTURE AT FS 333.00 TO FS 349.00 LBL 36 TO LBL 40. ***AIRCRAFTY REMOVED FROM SERVICE*** BLENDED CORROSION ON BRACKET ASSY 601R31527-149 AT FS 333.00 AT 4 EACH LOCATIONS. (P1) 2.100L X 1.Nov 5, 2021 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202111197977None · dentedAFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .600"L X .500"W X .025"D AT FS 621, 3.7" O/B OF RBL 36.20, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .011"D. CUTOUT DAMAGED AREANov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111227979None · corrodedCORROSION DAMAGE COMMON TO L/H WING ACCESS PANEL #540AT AT LOWER WING PLANK LAND AROUND ENTIRE AREA OF LAND. ***AIRCRAFT REMOVED FROM SERVICE*** REMOVED CORROSION ON LOWER WING PLANK LAND COMMON TO L/H WING ACCESS PANEL #540AT. BLEND DIMENSIONS ARE 19.50"L XNov 4, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111197978None · dentedAFT PRESSURE BULKHEAD HAS DENT WITH A GOUGE .500"L X .300"W X .015"D AT FS 621, LBL 9.5 TO LBL 18.00, AND 2.0" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED GOUGE FROM DENTED AREA. GOUGE MEASURES: .250"L X .050"W X .013"D. CUTOUT DAMAGED AREA Nov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111197976None · dentedAFT PRESSURE BULKHEAD HAS DENT .400"L X .300"W X .010"D AT FS 621 IN BETWEEN LBL 27.50 AND LBL 36.20 AND 1.70" ABOVE WL 73.50. ***AIRCRAFT REMOVED FROM SERVICE*** DRESSED BACK DENT ON AFT PRESSURE BULKHEAD TO ORIGINAL CONTOUR. HFEC WAS PERFORMED AT REWORK ARNov 4, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111127963Doubler · damagedRH WINGLET INNER SKIN LOWER STRAP PN 600-15108 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET INNER SKIN LOWER STRAP PN 600-15108. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ANov 4, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111127962Doubler · damagedRH WINGLET DOUBLER PN 600-10388-60 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET DOUBLER PN 600-10388-60. PERFORMED HFEC WITH NO INDICATIONS. RESTORED PROTECTIVE FINISH. ALL WORK WITHIN LIMITS WNov 4, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111127961Strap · damagedRH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. ***AIRCRAFT REMOVED FROM SERVICE*** RH WINGLET LOWER OUTBOARD FAIRING STRAP PN 600-10388 HAS SEVERAL TOOL MARKS. BLENDED DAMAGE TO A SMOOTH CONTOUR TO RH WINGLET LOWER OUTBOARD FAIRNov 4, 2021 · N432AW · Cndair CL6002B19 · Wing StructureSDR A6WA202111227980Skin · dentedAIRCRAFT HAS 2EA DENTS LOCATED ON R/H FUSELAGE SKIN EXTERIOR BETWEEN FS 589+5 TO FS 589+8 JUST BELOW S25R. DENT DIMENSIONS (D1) 1.100L X .900W X .003D (D2) 1.100L X .900W X .009D. (P1) AND (P2) ARE NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111227981Skin · dentedAIRCRAFT HAS OUTWARD DENT ON R/H FUSELAGE SKIN EXTERIOR AT FS 379.00 +3 AT S18R+4. DIMENSIONS = .200"L X .100"W X .003"D. DENT NOT WITHIN ALLOWABLE LIMITS IAW CRJ200 SRM 53-00-31 REV 38. ********AIRCRAFT REMOVED FROM SERVICE*********** PERFORMED CUTOUT (.400Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Internal StairsSDR A6WA202111227982Skin · dentedAIRCRAFT R/H SKIN EXTERIOR HAS 5 EACH DENTS AT FS 589.00 TO FS 605.00 AND S24R - S25R. DENT DIMENSIONS ARE: (P1) .500L X .400W X .006D; (P2) .450L X .400W X .004D; (P3) .200L X .200W X .001D; (P4) .350L X .200W X .001D; (P5) .350L X .300W X .003D. EVALUATED DENov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111517971Skin · dentedDENTS (11 TOTAL) ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED 11 DENTS ON AFT FUSELAGE SKIN AT FS654.5 - FS672.20 AND S22R - S24R. DENTS DIMENSION: FS654.50 Ï¿½ FS672.2 AND S22R Ï¿½ S23R: P1= L = Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111217960Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT ON AFT FUSELAGE SKIN AT FS625.3 - FS640.00 AND S25R - S26R DENT DIMENSIONS P1- L = 1.200Ï¿½ X W = 0.900Ï¿½X D = 0.006Ï¿½. PERFORMED HFEC WNov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111117959Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R. ***AIRCRAFT REMOVED FROM SERVICE*** EVALUATED DENT ON AFT FUSELAGE SKIN AT FS625.30+13 - FS640.00 AND S22R - S23R AND FOUND TO BE ACCEPTABLE PER EA. DENT DIMENSIONS P1- L = 0.900Ï¿½ X W = Nov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202111107956Skin · dentedDENT ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. ***AIRCRAFT REMOVED FROM SERVICE*** HAND DRESSED DENT TO RE-FORM ORIGINAL CONTOUR ON AFT FUSELAGE SKIN AT FS682.00+4Ï¿½ AND S19R - S20R. DENT DIMENSION L = 0.500Ï¿½ X W = 0.400Ï¿½ X D = 0.008Ï¿½. PNov 1, 2021 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA202110207987Web · crackedPASSENGER DOOR HAS CRACK ON INNER WEB AT FS 338.9 DOOR HAS EXISTING REPAIR IAW GREO 601R-52-11-402 REV H. ********************AIRCRAFT REMOVED FROM SERVICE*********************** EXTENDED CUTOUT ON INNER WEB PN:601R31902-537 AT FS 338.9 TO 13.300"L X 6.800"WOct 20, 2021 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202110207986None · gougedPASSENGER DOOR ROLLER BRACKET PN: 600-31471-9 HAS A GOUGE 0.400"L X 0.165"W X 0.020"D ON OUTSIDE EDGE OF BRACKET. ***************AIRCRAFT REMOVED FROM SERVICE******************* BLENDED THE DAMAGE TO A SMOOTH CONTOUR. HFEC PERFORMED WITH NO INDICATIONS. ROTOOct 20, 2021 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202111247985Web · crackedPASSENGER DOOR HAS A CRACK .375"L ON INNER WEB P/N:601R31902-537 AT FS 320 AT UPPER FORWARD CORNER. **************AIRCRAFT REMOVED FROM SERVICE********************** DURING INCORPORATION OF GENERIC REO 601R-52-11-402 REV H, HFEC INSPECTION FOUND CRAOct 20, 2021 · N432AW · Cndair CL6002B19 · DoorsSDR A6WA202012087452Angle · corrodedT CAP CORRODED BEYOND LIMITS AT FS 621 TO FS 559+112 LBL 27. AIRCRAFT REMOVED FROM SERVICE. REMOVED AND REPLACED TCAP AT FS 559+112 TO FS 621, IAW CRJ SRM 51-42-21 AND BOMBARDIER DWG 601R35031.Dec 2, 2020 · N432AW · Cndair CL6002B19 · Fuselage Main, BulkheadSDR A6WA2020031047221Wire Harness · defectiveDURING TAKE OFF CLIMB, WHEN SELECTING GEAR UP, RECEIVED NOSE GEAR DISAGREE WITHIN 6 SECONDS OF SELECTION. LH+RH GEAR INDICATED GEAR UP AND LACKED. NOSE GEAR WHITE IN TRANSIT. DECLARED EMERGENCY. LANDING WAS BELOW MAX LANDING WEIGHT @ 146 KNOTS. Mar 8, 2020 · N432AW · Cndair CL6002B19 · Landing Gear System WiringSDR A6WA2019122347077Transducer · malfunctionedPRESSURE INDICATOR ON HYD 1 FROM 200-1800 PSI. C/W QRH. QTY AND TEMPS NORMAL AT 15-20 DEG AND 60% QTY. NEVER RECEIVED LOW PRESS CAUTION. AIRCRAFT REMOVED FROM SERVICE R&R HYD SYS #1 PRESSURE TRANSDUCER. OPS CHECK GOOD.Dec 20, 2019 · N432AW · Cndair CL6002B19 · Hydraulic System, MainSDR A6WA2019121047046Selector Valve · abnormalSUPPLIMENTAL INFORMATION, AT 170 KTS APROX 2200 FT AGL RECEIVED GEAR DISSAGREE WARNING ON GEAR EXTENSION. NLG SHOWS DOWN AND LOCKED. MLG SHOW UP AND LOCKED. PER QRH CYCLED GEAR HANDLE CONDITION PERSISTS. PER QRH PULLED MANUAL GEAR EXTENSION. ALL SHOW DOWN AND Dec 7, 2019 · N432AW · Cndair CL6002B19 · Landing Gear SelectorSDR A6WA2019120647040Sealant · looseSUPPLEMENTAL INFORMATION, AFTER TAKE-OFF, FIRST OFFICER'S WINDSHIELD SEALANT CAME LOOSE. STARTED MAKING LOUD SOUNDS AGAINST FIRST OFFICER'S WINDSHIELD THEN DEPARTED AIRCRAFT. MX INSPECTED AND FOUND FIRST OFFICER'S WINDSHIELD MISSING APPROXIMATELY 18" OF MOISDec 3, 2019 · N432AW · Cndair CL6002B19 · Flight Compartment WindowsSDR A6WA2019112647034Support Beam · crackedANGLE AT FS 621 BAGGAGE DOOR UPPER SUPPORT BEAM IS CRACKED AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT ANGLE FROM 2024 T-3 .040" AND INSTALLED REFERENCE CRJ 200 SRM 51-42-20, 51-24-21, AND 53-61-23 REV 37.Nov 20, 2019 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2019112647032Bracket · crackedBRACKET ASSY AT FS 574.00 & S6L HAS A CRACK AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2024 T-3 .050" REF CRJ 200 SRM 51-24-21 AND 53-61-15 REV 37. AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.Nov 19, 2019 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019112647033Bracket · crackedBRACKET ASSY AT FS 621.00 & S6L IS CRACKED. AIRCRAFT REMOVED FROM SERVICE FABRICATED REPLACEMENT BRACKET FROM 2014 T-3 .050" REF CRJ 200 SRM -51-24-21 AND 53-61-15 REV 37 AND INSTALLED REF CRJ 200 SRM 51-42-21 AND 51-23-00 REV 37.Nov 19, 2019 · N432AW · Cndair CL6002B19 · Fuselage Main, Attach FittingsSDR A6WA2019112047022Structure · damagedR/H O/B FLAP T/E DAMAGED 14" O/B FROM I/B CORNER. DAMAGE WAS INDUCED DURING MAINTENANCE. AIRCRAFT REMOVED FROM SERVICE REPAIRED DAMAGE ON R/H O/B FLAP T/E AT APPROX 14" O/B FROM I/B CORNER WITH A REPAIR DOUBLER THAT MEASURES 5.6" X 3.1" REF CRJ 200 SRM 57-53Nov 13, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019112247029Fitting · crackedFOUND CRACK ON MICRO SWITCH MOUNTING BRACKET INSTALLED ON THE SERVICE DOOR. AIRCRAFT REMOVED FROM SERVICE REMOVED AND REPLACED MOUNTING BRACKET ON R1 SERVICE DOOR REF CRJ 200 SRM 51-42-20 REV 37.Nov 8, 2019 · N432AW · Cndair CL6002B19 · Service DoorsSDR A6WA2019112147027Fitting · chafedR/H WING O/B FOREFLAP / AFT FLAP FITTING WORN DUE TO SEIZED ROLLER.AT FZ 189.57. AIRCRAFT REMOVED FROM SERVICE BLENDED CHAFE DAMAGE AREA ON R/H WING O/B FLAP O/B FOREFLAP FITTING AND AFT FLAP FITTING IN AN AREA OF 4.2"L X .20"W X .005"D WITHIN LIMITS REF ASANov 7, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019112647035Panel · crackedPANEL 433AB HAS A CRACK AIRCRAFT REMOVED FROM SERVICE REPLACED WITH SERVICEABLE PANEL 433AB REF CRJ200 SRM 52-41-02 REV 37.Nov 6, 2019 · N432AW · Cndair CL6002B19 · Nacelle/Pylon, Plate/SkinSDR A6WA2019112047024Hinge Fitting · chafedR/H WING O/B FLAP HINGE BOX AT WS 264.00 HAS 2 AREAS OF CHAFING DAMAGE. DAMAGE AREA 1 IS TO THE I/B FLAP HINE ARM FITTING DWG 601R10910 WITH DAMAGE DIMENSIONS OF .20"L X .15"W X .032"D. DAMAGE 2 IS TO THE AFT SIDE PLATE DWG 601R10180 WITH DAMAGE DIMENSIONS OF Nov 4, 2019 · N432AW · Cndair CL6002B19 · Trailing Edge FlapsSDR A6WA2019081446789Spoiler Sys · malfunctionedGROUND LIFT DUMP SYSTEM DID NOT DEPLOY ON INITIAL TOUCHDOWN CAUSING BOUNCE. DEPLOYED ON 2ND TOUCHDOWN. NO ASSOCIATED MSGS.Aug 13, 2019 · N432AW · Cndair CL6002B19 · Drag Control SystemSDR A6WA2019061246657Cabin Pressure · malfunctionedDURING CLIMB, THE CABIN WOULD NOT PRESSURIZE. THE FLIGHT LEVELED OFF AND THE CREW RAN THE QRH. THE FLIGHT RETURNED TO ORD AND LANDED WITHOUT FURTHER ISSUES.Jun 11, 2019 · N432AW · Cndair CL6002B19 · Cabin Pressure Control SystemSDR A6WA2019030146448Warning System · false activationON CLIMBOUT, RECIEVED NOSE DOOR WARNING MESSAGE AND GEAR DISAGREE WARNING MESSAGES, C/W QRH, MESSAGE CLEARED, THEN DIVERTED.Feb 19, 2019 · N432AW · Cndair CL6002B19 · Landing Gear Position and WarningSDR A6WA2018052945853Connector · unsecureDURING OPERATIONAL TEST OF PAX O2, PSU AT ROW 6CD FAILED TO DEPLOY. RESECURED CONNECTOR TO DEPLOY SOLENOID. SUBSEQUENT OPS TEST OF PAX O2 SYSTEM, AMM 35-20-00 PROVES GOOD.May 27, 2018 · N432AW · Cndair CL6002B19 · Oxygen System WiringSDR A6WA2017101645361Frame · crackedFRAME BS 333, OTBD OF STRINGER 0, FOUND CRACKED. REPLACED THE FRAME.Oct 12, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017101345356Skin · chafedLEFT WING UPPER INBD AFT TE TO BODY (APRON SKIN) HAS LARGE CHAFE AREA. REPAIREDOct 12, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, Plate/SkinSDR A6WA2017101345360Angle · corrodedPRESSURE FLOOR SUPPORT ANGLES AT BS 409+128 TO 559, LBL 36 - 47 CORRODED. REPAIRED.Oct 11, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017101345359Frame · crackedFRAME BS 333 HAS CORROSION ON THE FWD AND AFT SIDE BETWEEN STRINGERS 26L AND 26R. A .14 INCH CRACK WAS DISCOVERED DURING CORROSION REMOVAL. REPLACED.Oct 11, 2017 · N432AW · Cndair CL6002B19 · Fuselage Main, FrameSDR A6WA2017101145350Floor Support · corrodedMAIN CABIN L1 DOOR CUT OUT LOWER SILL VERTICAL FLOOR SUPPORT IS CORRODED BS 310 - 349, LBL 42Oct 9, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous StructureSDR A6WA2017101145343Stiffener · crackedSTIFFENER CRACKED BEHIND PANEL 326ER.Oct 6, 2017 · N432AW · Cndair CL6002B19 · Fuselage Structure (General)SDR A6WA2017101345337Support Angle · crackedINTERCOSTAL SUPPORT ANGLE COMMON WITH SKIN CRACKED AT BS 621 TO 625.3, STRINGER 15L.Oct 4, 2017 · N432AW · Cndair CL6002B19 · Fuselage Miscellaneous Structure
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