# Service difficulty reports: N8938A, cancelled May 21, 2024

A list on [N8938A, cancelled May 21, 2024](https://openairdocs.org/deregistered/N8938A-2024-05-21.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Page 1 of 2 · 74 reports

- [SDR REXA2017032100392](https://openairdocs.org/sdr/REXA2017032100392.md): Pbe · inoperative · Mar 21, 2017 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > ALL 3 PBE BARRIER POUCHES SPONGY. REPLACED THE COCKPIT WARDROBE AND AFT CABIN PBE SMOKE HOODS IAW AMM 35-30-00.
- [SDR REXA2016101101924](https://openairdocs.org/sdr/REXA2016101101924.md): Stowage Box · leaking · Oct 11, 2016 · N8938A · Cndair CL6002B19 · Crew Oxygen System
  > PILOT OXYGEN MASK STOWAGE BOX TEST BUTTON LEAKING. REPLACED PILOT OXYGEN MASK STOWAGE BOX IAW AMM 35-11-15. NO LEAKS NOTED. OPS CHECKED GOOD.
- [SDR REXA2016070601249](https://openairdocs.org/sdr/REXA2016070601249.md): Oxygen Mask · unwanted deploy · Jul 6, 2016 · N8938A · Cndair CL6002B19 · Passenger Oxygen System
  > OXYGEN MASKS IN SEAT 8 C/D ARE DEPLOYED. REPACKED THE OXYGEN MASKS FOR SEAT 8 C,D AND PERFORMED OPS CHECKED IAW AMM 35-21-09.
- [SDR REXA2016030700349](https://openairdocs.org/sdr/REXA2016030700349.md): Inverter · inoperative · Mar 7, 2016 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > DURING WAKE UP CHECK, NOTED EMER FLOOR LIGHTS AT ROW 2 - 5 & LT EMER EXIT LIGHT AT ROW 7 INOPERATIVE. R & R NR 2 INVERTER WITH SERVICEABLE UNIT, PN ON & OFF 5925-7 & SN N/A IAW AMM 33-51-07-04. ALL CHECKED GOOD.
- [SDR REXA2016022500258](https://openairdocs.org/sdr/REXA2016022500258.md): Light · disconnected · Feb 25, 2016 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > FLOOR EMER EXIT STRIPS, SEATS 2 - 5 NOT LIT. CONNECTED FLOOR EMER LIGHTS, CHECKED GOOD IAW AMM 33-51-01. OK FOR SERVICE.
- [SDR REXA2016012900120](https://openairdocs.org/sdr/REXA2016012900120.md): Light · inoperative · Jan 29, 2016 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > FLIGHT ATTENDANT EMER SWITCH TURNED ON WILL NOT ILLUMINATE, ROWS 2 - 5 ON FLOOR TRACK LIGHTING. PERFORMED ADJUSTMENT & TEST OF ROWS 2 - 5 FLOOR TRACK LIGHTING IAW AMM 33-51-01. OPERATIONS CHECKED GOOD.
- [SDR REXA2015120801184](https://openairdocs.org/sdr/REXA2015120801184.md): Oxygen Mask · defective · Dec 8, 2015 · N8938A · Cndair CL6002B19 · Crew Oxygen System
  > CAPTAINS SIDE OXYGEN MASK NOT TESTING PROPERLY. WHILE HOLDING PRESS TO TEST, O2 FLOW CONTINUES WHEN IT SHOULD NOT, & MARKER REMAINS YELLOW, NOT BLACK. SWAPPED CAPTAINS SIDE 02 MASK WITH OBSERVERS SIDE 02 MASK, PROBLEM FOLLOWED DEFERRED OBSERVERS MASK IAW MEL
- [SDR REXA2015111101101](https://openairdocs.org/sdr/REXA2015111101101.md): Bulkhead · damaged · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > AFT FUSELAGE PRESS BULKHEAD, APPROX 32" UP FROM FLOOR, 7 EA CHAFE & GOUGES FROM SCREWS, APPROX.180 DIA X.002 DEEP. REPAIRED AFT FUSELAGE PRESS BULKHEAD IAW REO 601R-53-61-2155..002"" MAX MATERIAL REMOVED AT ALL LOCATIONS. SCREW LENGTHS REQUIRE ADJUSTMENT
- [SDR REXA2015111101100](https://openairdocs.org/sdr/REXA2015111101100.md): Life Vest · unserviceable · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Life Jacket
  > INFANT LIFE VEST OUTER PACKING IS TORN OPEN, UNSERVICEABLE. REMOVED UNSERVICEABLE INFANT LIFE VEST FROM LT FWD CLOSET. INSTALLED SERVICEABLE INFANT LIFE VEST IN LT FWD CLOSET AT PLACARD LOCATION.
- [SDR REXA2015111101099](https://openairdocs.org/sdr/REXA2015111101099.md): Flashlight · inoperative · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > COPILOT FLASHLIGHT IS NOT BLINKING & DOES NOT COME ON WHEN PULLED FROM HOUSING. WARDROBE FLASHLIGHT, EMER USE ONLY STRAP IS BROKEN. R & R TAMPER STRAP ON WARDROBE FLASHLIGHT IAW AMM 20-21-00-910-801, PN A1-18-1030.
- [SDR REXA2015111101098](https://openairdocs.org/sdr/REXA2015111101098.md): Connector · missing · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Light System Wiring
  > ELECTRICAL CONNECTS FOR FLOOR TRACK EMER LIGHTS ARE MISSING IN MULTIPLE LOCATIONS. REPAIRED ELEC CONNECTORS FOR FLOOR TRACK EMER LIGHTS IAW ESPM 20-11-00. OPERATIONS TESTED GOOD IAW AMM 33-51-00-710-801.
- [SDR REXA2015111101097](https://openairdocs.org/sdr/REXA2015111101097.md): Wire · broken · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Light System Wiring
  > WIRE BROKEN TO EMER EXIT LIGHT IN BOTTOM OF WARDROBE. UPON INVESTIGATION, FOUND CONNECTOR BROKE OFF END OF WIRE. INSTALLED NEW SERVICEABLE CONNECTOR FOR EMER LIGHT IAW ESPM 20-17-31. OPERATIONS TEST OF THE EMER LIGHTS DUE. OPERATIONS TEST OF EMER LIGHTS GO
- [SDR REXA2015111101096](https://openairdocs.org/sdr/REXA2015111101096.md): Wire · broken · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Light System Wiring
  > EMERGENCY TRACK LIGHTING WIRING UNDER FLOORBOARD 251CLF BROKEN. R & R EMER TRACK LIGHT CONNECTOR PIN PL29LY IAW ESPM 20-17-10. OPERATIONS CHECK DUE. REF AMM 33-51-00-710-801. OPERATIONS TEST OF FLOOR TRACK EMER LIGHTING GOOD IAW AMM 33-51-00-710-801.
- [SDR REXA2015111101095](https://openairdocs.org/sdr/REXA2015111101095.md): Skin · corroded · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Wing, Plate/Skin
  > RIGHT WING LOWER PLANK HAS MULTIPLE INDICATIONS NOTED NEXT TO FOOTPRINT OF DRAIN HOLE FITTING AT BOOST PUMP 55% FSH. FAILED NDT INSPECTION. COMPLIED WITH WORK PACKAGE DRAIN HOLE SURFACE INSPECTION. REMOVED LIGHT SURFACE CORROSION IAW SRM 51-21-06. ENGINEER
- [SDR REXA2015111101094](https://openairdocs.org/sdr/REXA2015111101094.md): Post · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, BULKHEAD VERTICAL POSTS CRACKED AT BOTTOM INBD CORNERS LBL 27 & RBL 27. REMOVED SUPPLY AIR FILTER IAW AMM 21-24-01-000-801. REINSTALLED SUPPLY AIR FILTER IAW AMM 21-24-01-400-801. REMOVED SUPPLY AIR FILTER DUCT BY REMOVING & SCREWS FROM THE STRU
- [SDR REXA2015111101093](https://openairdocs.org/sdr/REXA2015111101093.md): Stringer · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Longeron/Stringer
  > FORWARD LT SIDE OF FUSELAGE, STRINGER 3L, CRACKED AT FS 280. REMOVED LT FWD STRINGER 31 AT FS 280 IAW SRM 51-42-06 & 51-42-21. DRILLED NEW SERVICEABLE STRINGER 3L CLIP IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE CLIP IAW SRM 51-42-06 & 51-42-21.
- [SDR REXA2015111101092](https://openairdocs.org/sdr/REXA2015111101092.md): Bulkhead · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > PRESSURE BULKHEAD FS 202.75 AT BL 23.75, FOUND MULTIPLE INDICATIONS EXTENDING A MAXIMUM OF.45"" LONG BY 100%FSH AROUND PARKING BRAKE PASS THROUGH HOLE FROM 6 O'CLOCK POSITION TO 2 O'CLOCK POSITION. LEAKING AFT, FAILED NDT. COMPLIED WITH STEP 1 & 2 OF REO 60
- [SDR REXA2015111101091](https://openairdocs.org/sdr/REXA2015111101091.md): Bulkhead · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESS BULKHEAD WEB THAT SURROUNDS THE LINTEL ATTACHMENT FITTING HAS INDICATION NOTED APPROX.400 IN LENGTH 70% FSH. REPAIRED FS 621 BULKHEAD WEB AT THE LINTEL ATTACHMENT FITTING IAW REO 601R-53-61-1230 REV F DATED 10 31 1. THIS IS A MAJOR REPAIR.
- [SDR REXA2015111101090](https://openairdocs.org/sdr/REXA2015111101090.md): Bulkhead · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Bulkhead
  > FOUND REAR PRESS BULKHEAD WEB HAS INDICATION NOTED AT LBL 27.50, WL 130, APPROX.500 INCHES IN LENGTH 50% FSH. FAILED NDT INSPECTION. REPAIRED CRACK IN FS 621, REAR PRESS BULKHEAD WEB AT LBL 27.50, WL 130 IAW REO 601R-53-61-1541 REV F DATED 11 12 14.
- [SDR REXA2015111101089](https://openairdocs.org/sdr/REXA2015111101089.md): Attach Angle · corroded · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > SERVICE DOOR LOWER SILL ANGLE & DRAIN HOSE AFT ATTACH ANGLE CORRODED, BETWEEN FS 319 & 349, STRINGER 18R. REMOVED SERVICE LOWER SILL ANGLE BY REMOVING RIVETS, CHERRYMAX & HI-LITES IAW SRM 51-42-06/10/21. INSTALLED NEW LT WING SIDE SILL ANGLE AT SERVICE DOOR
- [SDR REXA2015111101088](https://openairdocs.org/sdr/REXA2015111101088.md): Intercostal · corroded · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INTERCOSTAL CORRODED, BETWEEN FS 333 & FS 349, STRINGER 20R. REMOVED CORRODED INTERCOSTAL IAW SRM 51-42-06 & 51-42-11. LOCATED & DRILLED NEW INTERCOSTAL IAW SRM 51-40-11. NEW INTERCOSTAL REQUIRES INSTALL. INSTALLED NEW INTERCOSTAL & INSTALLED BETWEEN FS 33
- [SDR REXA2015111101087](https://openairdocs.org/sdr/REXA2015111101087.md): Post · damaged · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128 VERTICAL POST HAS ONE INDICATION.3"" LONG BY 90% FSH ON THE BL 0.0 LT VERTICAL POST AFT RADIUS. FAILED NDT INSPECTION. REMOVED Y DUCT & UNDER FLOOR AC DUCT BY REMOVING 3 EA ADEL CLAMP, 3 EA WORM CLAMP. REINSTALLED Y DUCT & UNDER FLOOR AC DUCT BY
- [SDR REXA2015111101086](https://openairdocs.org/sdr/REXA2015111101086.md): Frame · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Frame
  > FS 333.00 FRAME CRACKED APPROX 2""L AT STRINGER 1L. R & R CRACKED FRAME AT FS 333, BETWEEN STRINGER 0 & STRINGER 3L IAW SRM 61-42-06 & 51-12-21. REMOVED CRACKED FRAME AT FS 333, BETWEEN STRINGER 0 & 3L IAW SRM CH 51-42-06 & SRM CH 51-42-21. REPLACE FRAME PN
- [SDR REXA2015111101085](https://openairdocs.org/sdr/REXA2015111101085.md): Angle · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > INBD & OTBD ANGLES ON INTERCOSTAL IS CRACKED AT FS 484, RBL 27 & 36. REMOVED CABLE GUIDE TO ACCESS CRACKED ANGLE FOM, BY REMOVING BOLTS & NUTS IAW SRM 51-41-00. REINSTALLED SAME SERVICEABLE CABLE GUIDE IAW AMM 20-21-00-910-801 & 20-24-00-910-801. R & R INBD
- [SDR REXA2015111101084](https://openairdocs.org/sdr/REXA2015111101084.md): Skin · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Ailerons
  > RIGHT AILERON UPPER LE SKIN HAS 2 CHAFED AREAS AT OTBD HINGE. INBD DAMAGE MEASURES APPROX 1.2"" LONG X 0.6"" WIDE X 0.010"" DEEP. OTBD DAMAGE MEASURES APPROX.9"" LONG X 0.6"" WIDE X 0.020"" DEEP. R & R UPPER LE SKIN IAW SRM 51-42-06 & 51-42-20. LE PN CC67
- [SDR REXA2015111101083](https://openairdocs.org/sdr/REXA2015111101083.md): Attach Angle · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 280 CROSSBEAM HAS 2 ATTACH ANGLE CRACKED AT LBL 9 & RBL 9. INSTALLED TWO EACH CABLE BLOCKS, TOOL 201175 & 201174, AT FS 280 - 295 ON MLG ALT RELEASE FOR BRACKET REMOVAL TO FOM. REMOVED TWO EACH CABLE BLOCKS, TOOL 201175 & 201174, FROM MLG ALT EXTENSION CA
- [SDR REXA2015111101082](https://openairdocs.org/sdr/REXA2015111101082.md): Handle · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR INTERNAL HANDLE HAS A CRACK. REMOVED CRACKED PAX DOOR INTERNAL HANDLE IAW AMM 52-11-21-000-801 SUB TASK 52-11-21-020-012, STEP N5. LOCATED NEW FASTENER HOLES TO NEW SERVICEABLE HANDLE IAW SRM 51-40-11. INSTALLED NEW SERVICEABLE PAX DOOR INTER
- [SDR REXA2015111101081](https://openairdocs.org/sdr/REXA2015111101081.md): Bracket · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Main, Attach Fittings
  > RIGHT MLG WW HYD TRANSDUCER BRACKET CRACKED. R & R RT MLG WW HYD TRANSDUCER BRACKET IAW SRM 51-42-06 & SRM 51-40-11.
- [SDR REXA2015111101080](https://openairdocs.org/sdr/REXA2015111101080.md): Bracket · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > RIGHT FWD FUSELAGE POWER RECEPTACLE STRUCTURE CRACKED. REMOVED ACFT POWER RECEPTACLE BRACKET IAW SRM 51-42-06 & SRM 51-42-21. INSTALLED ACFT POWER RECEPTACLE BRACKET IAW SRM 51-42-06 & 54-42-21. LOCATED & DRILLED NEW AC POWER BRACKET RECEPTACLE IAW SRM 51-4
- [SDR REXA2015111101079](https://openairdocs.org/sdr/REXA2015111101079.md): Post · damaged · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Fuselage Miscellaneous Structure
  > FS 409+128, VERTICAL POSTS HAVE ONE EACH INDICATION.2" LONG BY 95% FSH ON THE BL 0.0 RT VERTICAL POST AFT RADIUS, RBL 18.0 OTBD VERTICAL POST.25" LONG BY 95% FSH AFT RADIUS, INBD VERTICAL POST.3" LONG BY 98% FSH AFT RADIUS. FAILED NDT INSPECTION. REINSTAL
- [SDR REXA2015111101078](https://openairdocs.org/sdr/REXA2015111101078.md): Drag Angle · cracked · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Passenger/Crew Doors
  > PASSENGER DOOR AFT SIDE DRAG ANGLE CRACKED, PREV REPAIR. FOUND PREV REPAIR TO BE 601R-52-11-513 REPAIR TYPE, DISREGARD PREV REPAIR & ACCOMPLISH 601R-52-11-513 REPAIR TYPE 11. REPAIRED AFT PAX DOOR AFT DRAG ANGLE IAW REO 601R-52-11-513. REMOVED PAX DOOR POWE
- [SDR REXA2015111101077](https://openairdocs.org/sdr/REXA2015111101077.md): Panel · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Engine Cowling System
  > LEFT ENG, LOWER FAN COWL PANEL 432AB, TE IS CHAFED IN SEVERAL AREAS. R & R LT ENG LOWER FAN COWL TE IAW CMM 71-14-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090, REQUIR
- [SDR REXA2015111101076](https://openairdocs.org/sdr/REXA2015111101076.md): Skin · damaged · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Trailing Edge Flaps
  > THE LT FLAP STUB FAIRING IS CHAFED ON THE OUTER SKIN & FWD BRACKET IS DAMAGED. UPON FURTHER INVESTIGATION FOUND FWD FITTING ON LT WING TO BE DAMAGED, REQUIRES REPLACEMENT. REMOVED UNSERVICEABLE FITTING ON LT WING & REPLACED WITH NEW SERVICEABLE FITTING, PN 6
- [SDR REXA2015111101075](https://openairdocs.org/sdr/REXA2015111101075.md): Separator · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > LEFT ENG, LOWER PYLON, PN 412DB, FWD SEPARATOR IS CHAFED. R & R LT ENG, LOWER PYLON PANEL 412DB SEPARATOR WITH NEW SERVICEABLE SEPARATOR IAW SRM 51-40-11, 51-42-06 & 51-42-13.
- [SDR REXA2015111101074](https://openairdocs.org/sdr/REXA2015111101074.md): Bracket · broken · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Trailing Edge Flaps
  > BONDING JUMPER BRACKET BROKEN ON LT FLAP HINGE BOX, STATION 127.25. REPLACED ANGLE BRACKET, BONDING WIRE JUMPER, LT FLAP HINGE BOX, PN 600-14500-9 IAW EA CRJ257-03796 & SRM 51-42-21.
- [SDR REXA2015111101073](https://openairdocs.org/sdr/REXA2015111101073.md): Fitting · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT ENG UPPER PYLON, PN 422BT, TWO INBD CLIPS ARE CHAFED. REMOVED NO STEP PLACARD FOR ACCESS IAW AMM 11-20-00-000-801. APPLIED NO STEP PLACARD TO PANEL 422BT IAW AMM TASK 11-20-00-400-801. REMOVED TWO EACH UNSERVICEABLE INBD CLIPS FROM RT ENG UPPER PYLON
- [SDR REXA2015111101072](https://openairdocs.org/sdr/REXA2015111101072.md): Cowling · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Engine Cowling System
  > RIGHT ENG UPPER FAN COWL HAS SEVERAL CHAFED AREAS ALONG TE. R & R RT ENG UPPER FAN COWL TE IAW CMM 71-41-01-300-814-A01 REPAIR SRS091. UPON FURTHER INVESTIGATION, FOUND CHAFE DAMAGE TO BE OUT OF LIMITS OF CMM TASK 71-14-01-300-813-A01 SRS090. REQUIRES AFT E
- [SDR REXA2015111101071](https://openairdocs.org/sdr/REXA2015111101071.md): Flow Divider · chafed · Nov 11, 2015 · N8938A · Cndair CL6002B19 · Nacelle/Pylon Miscellaneous Structure
  > RIGHT ENG LOWER PYLON, PN 422DB, FWD DIVIDER IS CHAFED. R & R DISCREPANT DIVIDER ON PANEL 422DB IAW SRM 51-42-06.
- [SDR REXA2015050500464](https://openairdocs.org/sdr/REXA2015050500464.md): Light · inoperative · May 5, 2015 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE IN ROWS 5. PLACED EMER FLOOR TRACK LIGHTING AT ROW 5 ON DEFERRAL IAW MEL 33-51-17. REPLACED EMER LIGHT LAMP STRAP IAW 33-51-01. OPERATIONS CHECKED GOOD. OK FOR SERVICE. THIS CLEARS DM 1267, MM02 UPDATED & PLA
- [SDR REXA2015032600348](https://openairdocs.org/sdr/REXA2015032600348.md): Connector · damaged · Mar 26, 2015 · N8938A · Cndair CL6002B19 · Light System Wiring
  > FLOOR LEVEL EMER LIGHT STRIP HAS DAMAGED CONNECTOR, MALE, SIDE OF THE TWO WIRES THAT COME THROUGH THE FLOORBOARD. AFT PORTION OF EMER LIGHT STRIP NEEDS REINSTALLED. FOUND NO DAMAGE TO CONNECTOR, PIN WAS BENT. STRAIGHTENED PIN, RECONNECTED WIRES & REINSTALLE
- [SDR REXA2015011500054](https://openairdocs.org/sdr/REXA2015011500054.md): Proximity Sensor · out of adjust · Jan 15, 2015 · N8938A · Cndair CL6002B19 · Landing Gear Position and Warning
  > RIGHT MLG AFTER GEAR DISAGREE MASTER CAUTION QRH COMPLETE. DURING TROUBLESHOOTING FOR DISC 1 ON AML 3180474 FOUND RT MLG UPLOCK TARGET LOOSE. REFER TO CORRECTIVE ACTION NR 2 ON AML 3180474 PREFORMED GEAR SWING CHECK IAW AMM 32-30-00. OPERATIONS CHECKED GOOD
- [SDR REXA2014100100894](https://openairdocs.org/sdr/REXA2014100100894.md): Skin · dented · Sep 27, 2014 · N8938A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > DENT WAS NOTED IN THE FUSELAGE SKIN BETWEEN FS 582 & FS 588 STRINGER 20L & 21L MEASURING 6 INCHES X 1 INCH X 0.010 INCHES DEEP. REPAIRED IAW EA CRJ253-02952.
- [SDR REXA2014092600893](https://openairdocs.org/sdr/REXA2014092600893.md): Skin · dented · Sep 26, 2014 · N8938A · Cndair CL6002B19 · Fuselage Main, Plate/Skin
  > MAINTENANCE FOUND TWO DENTS IN THE FUSELAGE SKIN BETWEEN FS 667 & 681 BETWEEN STRINGER 18L & 19L. THE FWD DENT MEASURES 3.00 INCHES X 1.0 INCHES X 0.002 INCHES DEEP & THE AFT DENT MEASURES 8.0 INCHES X 1.25 INCHES X 0.005 INCHES DEEP. REPAIRED IAW EA CRJ253-
- [SDR REXA2014090300862](https://openairdocs.org/sdr/REXA2014090300862.md): Battery Pack · discharged · Sep 3, 2014 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > DURING ROUTINE CHECK FOUND SEVERAL EXTERIOR & INTERIOR EMER LIGHTS OUT. R & R NR 1 & NR 4 EMER BATTERY PACKS IAW AMM 33-51-04. OPERATIONS CHECKED GOOD AT THIS TIME.
- [SDR REXA2014072400736](https://openairdocs.org/sdr/REXA2014072400736.md): Lens · cracked · Jul 24, 2014 · N8938A · Cndair CL6002B19 · Emergency Lighting
  > BULKHEAD EMERGENCY LIGHT LENS CRACKED. R & R LENS IAW CMM 33-21-38.
- [SDR REXA2014071900708](https://openairdocs.org/sdr/REXA2014071900708.md): Smoke Goggles · inoperative · Jul 19, 2014 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > OBSERVERS SMOKE GOGGLES INOPERATIVE. R & R OBSERVERS GOGGLES IAW AMM 25-61-00. MM02 UPDATED & PLACARD REMOVED.
- [SDR REXA2014071900707](https://openairdocs.org/sdr/REXA2014071900707.md): Smoke Goggles · defective · Jul 19, 2014 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > CAPTAINS SMOKE GOGGLES ELASTIC ADJUSTABLE STRAP WORN OUT. SWAPPED OBSERVERS WITH CAPTAINS SEAT SMOKE GOGGLES. DEFER OBSERVERS IAW MEL 25-12-11 IAW MOC JD, ADDED TO MEL LOGBOOK, PLACARD INSTALLED.
- [SDR REXA2014071200695](https://openairdocs.org/sdr/REXA2014071200695.md): Pbe · damaged · Jul 12, 2014 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > TWO PBE'S DAMAGED. R & R COCKPIT PBE & GALLEY CLOSET PBE IAW AMM 35-30-00.
- [SDR REXA2013073001392](https://openairdocs.org/sdr/REXA2013073001392.md): Pbe · damaged · Jul 30, 2013 · N8938A · Cndair CL6002B19 · Emergency Equipment
  > CREW REPORTS DAMAGE PBE. R & R PBE IAW AMM 25-61-00.
- [SDR REXA2013072001378](https://openairdocs.org/sdr/REXA2013072001378.md): Warning Message · false activation · Jul 20, 2013 · N8938A · Cndair CL6002B19 · Drag Control System
  > FLIGHT SPOILER FAULT STATUS MESSAGE READ-441, COMPLIED WITH READ-441. SPOILER FAULT STATUS MESSAGE IAW FIM 27-60-00. NO SPOILER FAULT STATUS MESSAGE INDICATED AT THIS TIME. OK FOR SERVICE.

Next page: https://openairdocs.org/deregistered/N8938A-2024-05-21/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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 = 'N8938A' AND deregistration_id = 'N8938A-2024-05-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N8938A-2024-05-21/reports

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