# Service difficulty reports: N788SK

A list on [N788SK](https://openairdocs.org/aircraft/N788SK.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 SWIA2025121200028](https://openairdocs.org/sdr/SWIA2025121200028.md): Floorbeam · corroded · Oct 28, 2025 · N788SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > UNDER FLOORBOARD 232BRF RT FLOOBEAM FROM RBL 12 TO OTBD SILL SIGNS OF CORROSION AT BS 333. PERFORMED REPAIR ON THE RT FLOORBEAM IAW AMM 20-70-00, SRM 51-42-21, 51-21-06, REO 670-53-21-2733, REV--(P1) & REO 670-53-21-2733 REV-. PERFORMED INSPECTION.
- [SDR SWIA202512121025](https://openairdocs.org/sdr/SWIA202512121025.md): Post · corroded · Oct 25, 2025 · N788SK · Cndair CL6002C11 · Fuselage Main, Structure
  > AVIONICS BAY LEFT FLOOR POST AT LBL12 AND FS280.00 THERE IS SIGNS OF CORROSION WHERE THE POST CONNECTS TO FRAME 280. PERFORMED REPAIR AT LT FLOOR POST AT LBL 12 AND FS280.00 IAW SRM 53-00-00, 53-11-43, 51-42-06, 51-42-21, 51-42-10, 51-24-21, 51-40-11, 51-21-1
- [SDR SWIA2025121200004](https://openairdocs.org/sdr/SWIA2025121200004.md): Floorbeam · corroded · Oct 4, 2025 · N788SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > SIGNS OF CORROSION NOTED AT FLOORBEAM FS280 RBL12. R & R THE FLOORBEAM IAW SRM 53-00-00, AMM 20-70-00, SRM 51-42-06, SRM 51-42-21, SRM 51-42-13, SRM 53-11-10, SRM 51-24-21, SRM 51-40-11, SRM 51-21-11, SRM 51-25-06, AND SRM 51-25-16. PERFORMED NDT INSPECTION,
- [SDR SWIA202512120904](https://openairdocs.org/sdr/SWIA202512120904.md): Web · corroded · Sep 4, 2025 · N788SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > LEFT COCKPIT LOWER WEB CORRODED AT BOTTOM NEXT TO FLOOR. PERFORMED REPAIR ON LT COCKPIT LOWER WEB AT THE BOTTOM NEXT TO THE FLOOR IAW REO 670-53-11-594 REV.-A. AND AMM 20-70-00, SRM 51-42-06, AND SRM 51-25-16. PERFORMED NDT INSPECTION. COMPLETE INSTALLATI
- [SDR SWI2025F01824](https://openairdocs.org/sdr/SWI2025F01824.md): Floor Support · corroded · Aug 29, 2025 · N788SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > LEFT FLOOR SUPPORT CORRODED FROM BS 280 - 310. R & R THE FLOOR SUPPORT FROM BS 280 - 310 IAW SRM 51-26-01, 53-00-00, 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-12-00, 51-21-11, 51-25-06, 51-25-16, AND AMM 21-31-00.
- [SDR SWI2025F01823](https://openairdocs.org/sdr/SWI2025F01823.md): Floor Support · corroded · Aug 29, 2025 · N788SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT CORRODED FROM BS 280 TO 310. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FS280-FS319.70 IAW AMM 20-70-00, SRM 51-42-15, 51-12-00, 51-42-06, 51-42-13, 51-42-21, 51-40-11, 51-21-11, 51-25-06, 51-25-16, ESPM 20-12-00, AND AMM 21-31-00.
- [SDR SWIA2025121200829](https://openairdocs.org/sdr/SWIA2025121200829.md): Floorbeam · corroded · Aug 29, 2025 · N788SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > COCKPIT AFT FLOORBEAM CORRODED. REMOVED AND REPLACED ANGLE ON COCKPIT FLOOR AND LT FLOORBEAM IAW SRM 51-12-00, 53-00-00, 51-42-06, 51-42-21, 51-40-11, 51-25-06, 51-42-13, 51-21-11, 51-25-16, AND AMM 20-70-00.
- [SDR SWI2025F01822](https://openairdocs.org/sdr/SWI2025F01822.md): Web · corroded · Aug 29, 2025 · N788SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > RIGHT COCKPIT LOWER WEB CORRODED AT THE BOTTOM NEXT TO THE FLOOR. REPAIRED THE COCKPIT LOWER WEB IAW REO REO 670-53-11-594, REV -A. AMM 20-70-00, SRM 51-42-06, SRM 51-42-13, SRM 53-11-10, SRM 51-42-21, SRM 51-42-20, SRM 51-42-24, SRM51-41-02, SRM 51-21-11, SR
- [SDR SWIA202512120828](https://openairdocs.org/sdr/SWIA202512120828.md): Floorbeam · cracked · Aug 28, 2025 · N788SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > RBL 12 COCKPIT FLOORBEAM IS CRACKED ON OTBD SIDE WHERE IT ATTACHES TO BS 280. PERFORMED REPAIR OF FLOORBEAM IAW AMM 20-70-00, SRM 51-42-06, 51-42-21, 51-40-11, 51-21-11, 51-25-06, & REO 670-53-11-896, REV -. PERFORMED NDT ET INSPECTION. SEE REPORT FOR DETAI
- [SDR SWI2025F01821](https://openairdocs.org/sdr/SWI2025F01821.md): Floorbeam · cracked · Aug 28, 2025 · N788SK · Cndair CL6002C11 · Fuselage Floor Panel
  > LBL 12 COCKPIT FLOORBEAM CRACKED ON OTBD SIDE, WHERE IT ATTACHES TO BS 220. PERFORMED REPAIR IAW SRM 51-42-06, 51-42-21, 53-00-00, 51-21-11, 51-25-06, 51-40-11, 51-25-16, & REO 670-53-11-896, REV -. PERFORMED NDT ET INSPECTION.
- [SDR SWIA202512120825](https://openairdocs.org/sdr/SWIA202512120825.md): Rib · cracked · Aug 25, 2025 · N788SK · Cndair CL6002C11 · Wing, Rib/Bulkhead
  > RIGHT WING LEADING EDGE RIB AT WS 58.41 CRACKED NEAR THE TOP. PERFORMED REPAIR LEADING EDGE RIB WS 58.41 AT RT WING IAW REO 670-57-41-644 REV-, SRM 57-41-12, NDT PERFORMED.
- [SDR SWIA202512120823](https://openairdocs.org/sdr/SWIA202512120823.md): Striker · corroded · Aug 23, 2025 · N788SK · Cndair CL6002C11 · Service Doors
  > SERVICE DOOR LOWER SEAL STRIKER HAS SIGNS OF CORROSION AROUND FASTENER HOLES. REPAIRED THE DAMAGE TO SERVICE DOOR LOWER SEAL STRIKER IAW REO 670-53-21-2752, REV-, AND SRM 53-21-23.
- [SDR SWIA202512120818](https://openairdocs.org/sdr/SWIA202512120818.md): Web · cracked · Aug 18, 2025 · N788SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > RIGHT FWD EQUIPMENT BAY FLOOR WEB HAS A CRACK AFT OF DOOR. PERFORMED REPAIR ON RT EQUIPMENT BAY FLOOR WEB IAW AMM 20-70-00, SRM 550 51-42-06, SRM 51-21-11, SRM 51-25-06, SRM 51-25-16, REO 670-53-11-509, REV -E, AND REO 670-53-11-2193, REV -, NDT PERFORMED
- [SDR SWIA2023032900025](https://openairdocs.org/sdr/SWIA2023032900025.md): Unknown · damaged · Feb 25, 2023 · N788SK · Cndair CL6002C10 · Wing, Plate/Skin
  > TRANSFER FROM EAML 1089110: PULLING INTO GATE, LEFT WING TIP HIT BELT LOADER RAIL. DAMAGE TO LEFT WING TIP. INSPECTED THE LT WINGTIP AND FOUND SEVERAL DAMAGED COMPONENTS IN THE LT WINGTIP AREA. PLEASE SEE REO 670-57-00-104 REV A TABLE 1- DAMAGED PARTS SUMMA
- [SDR SWIA202055300](https://openairdocs.org/sdr/SWIA202055300.md): Angle · corroded · Dec 13, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON PAX DOOR LOWER SILL FWD CAP ANGLE. C-CHECK RO 1/5/2021. REPAIRED CORROSION DAMAGE TO PAX DOOR SILL UPPER SUPPORT ANGLE (FWD-CAP) BY REPLACING WITH NEW PART, IAW CRJ700 SRM 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND DWG SH670-31810 REV
- [SDR SWIA202055299](https://openairdocs.org/sdr/SWIA202055299.md): Intercostal · corroded · Dec 8, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CORROSION FOUND ON INTERCOSTAL AT STGR 21L FS 333-FS 349. C-CHECK RO 1/5/2021. REMOVED AND REPLACED NEW INTERCOSTAL P/N SH670-31823-1S AT FS 333.00 TO FS 349.00 STGR 21L, REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31810 REV Y. COMPLIED WITH TASK CARD
- [SDR SWIA202055311](https://openairdocs.org/sdr/SWIA202055311.md): Bolt · corroded · Dec 6, 2020 · N788SK · Cndair CL6002C10 · Elevator Control System
  > LT ELEVATOR POSITION TRANSMITTER HAS CORRODED HARDWARE. C-CHECK RO 1/5/2021. REPLACED ELEVATOR POSITION TRANSMITTER HARDWARE LT, PER CRJ 700 AMM 27-34-10-400-801-A01. INSTALLED NEW 2 EA BOLTS, 3 EA WASHERS, 2 EA NUTS. OPERATIONAL TEST GOOD.
- [SDR SWIA202055310](https://openairdocs.org/sdr/SWIA202055310.md): Floorbeam · corroded · Dec 6, 2020 · N788SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FLOOR CROSS BEAM AT APPROXIMATELY FS 1069.75 AT FLOOR SILL HAS CORROSION, MARKED. C-CHECK RO 1/5/2021. CORROSION ON CROSS BEAM AND RT FLOOR SILL AT FS 1069.75 REMOVED CORROSION, PER CRJ-700 SRM 51-21-06-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-53-61-
- [SDR SWIA202055309](https://openairdocs.org/sdr/SWIA202055309.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT TRACK MOUNTING CHANNEL, LT CORRODED AT APPROXIMATELY FS 797.00. C-CHECK RO 1/5/2021. REMOVED CORROSION AND FOUND SIDE SEAT TRACK MOUNTING CHANNEL TO BE OUT OF LIMITS. REPLACED CHANNEL, REF CRJ-700 SRM 51-41-02-001-001-A01.
- [SDR SWIA202055308](https://openairdocs.org/sdr/SWIA202055308.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK SECTION FS 581.00 TO FS 677.00, LBL 9.0 CORRODED SEVERAL PLACES. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK RBL 9 AT FS 581.00-FS 677.00, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055307](https://openairdocs.org/sdr/SWIA202055307.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK SECTION FS 485.00 TO FS 581.00, RBL 9.0 CORRODED SEVERAL PLACES. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK LBL 9 AT FS 485.00-FS 581.00, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055306](https://openairdocs.org/sdr/SWIA202055306.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK SECTION FS 581.00 TO FS 677.00, RBL 9.0 CORRODED SEVERAL PLACES. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK RBL 9 AT FS 581.00-FS 677.00, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055305](https://openairdocs.org/sdr/SWIA202055305.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK SECTION FS 485.00 TO FS 581.00, LBL 9.0 CORRODED SEVERAL PLACES. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK LBL 9 AT FS 485.00-FS 581.00, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055298](https://openairdocs.org/sdr/SWIA202055298.md): Tie Down · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > TIE DOWN BRACKET PLATE AT FS 581.00, AT STRINGER 27.00 HAS EVIDENCE OF CORROSION. C-CHECK RO 1/5/2021. TIE DOWN BRACKET PLATE AT FS 581.00, AT STRINGER 27.00 REMOVED AND REPLACED WITH NEW, REF CRJ 700 SRM 51-42-21-001-001-A01 AND DRAWING SH670-33600 REV AD.
- [SDR SWIA202055297](https://openairdocs.org/sdr/SWIA202055297.md): Tie Down · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > TIE DOWN BRACKET PLATE, BETWEEN FS 549.00 TO FS 565.00 AT STRINGER 25L, HAS EVIDENCE OF CORROSION. C-CHECK RO 1/5/2021. REMOVED AND REPLACED TIE DOWN BRACKET PLATE BETWEEN FS 549 TO FS 565 AT STRINGER 25L, REF CRJ 700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-
- [SDR SWIA202055296](https://openairdocs.org/sdr/SWIA202055296.md): Tie Down · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > TIE DOWN BRACKET PLATE AT FS 533.00, AT STRINGER 27.00 HAS EVIDENCE OF CORROSION. C-CHECK RO 1/5/2021. REMOVED AND REPLACED TIE DOWN BRACKET AT FS 533 STINGER 27, REF CRJ 700 SRM 51-42-21-001-001-A01 CRJ 700 SRM 51-42-24-001-001-A01 BOMBARDIER DWG SH670-3360
- [SDR SWIA202055295](https://openairdocs.org/sdr/SWIA202055295.md): Support Channel · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > AFT DRAIN MAST SUPPORT CHANNEL IS CORRODED. C-CHECK RO 1/5/2021. REPLACED AFT DRAIN MAST SUPPORT CHANNEL, REF CRJ-700 SRM 51-42-06-001-001-A01 AND DWGMM670-43200 REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. LEAK CHECK GOOD.
- [SDR SWIA202055294](https://openairdocs.org/sdr/SWIA202055294.md): Seat Track · corroded · Dec 5, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > SIDE SEAT TRACK MOUNTING CHANNEL, RT CORRODED AT APPROXIMATELY FS 797.00. C-CHECK RO 1/5/2021. REMOVED CORROSION AND FOUND REWORKED AREA TO BE OUT OF LIMITS. REPLACED RT SIDE SEAT TRACK MOUNTING CHANNEL FS 785-FS 857, REF SNIEO SH670-30017 S16 2020.12.18.
- [SDR SWIA202055304](https://openairdocs.org/sdr/SWIA202055304.md): Support Angle · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > SERVICE DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION AT FWD NUT PLATE HOLE. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SERVICE DOOR SILL UPPER FLOOR SUPPRT ANGLE, REF CRJ 700 SRM 51-42-06-001-001-A01 AND CRJ 700 SRM 51-42-21-001-001-A01.
- [SDR SWIA202055293](https://openairdocs.org/sdr/SWIA202055293.md): Floor Support · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > PAX DOOR SILL UPPER FLOOR SUPPORT ANGLE HAS EVIDENCE OF CORROSION, AS MARKED. C-CHECK RO 1/5/2021. REPAIRED CORROSION DAMAGE TO PAX DOOR SILL UPPER SUPPORT ANGLE (MID-CAP) BY REPLACING WITH NEW PART, IAW CRJ700 SRM 51-40-11-001-001-A01, 51-41-02-001-001-A01,
- [SDR SWIA202055292](https://openairdocs.org/sdr/SWIA202055292.md): Floorbeam · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > FRAME FS 333 CABIN FLOOR CROSS BEAM HAS EVIDENCE OF CORROSION AT NUT PLATE HOLE AT APPROXIMATELY BL 18RT. C-CHECK RO 1/5/2021. REMOVED CORROSION BY CUTTING OUT DAMAGE AT FS 333 APPROXIMATELY BL 18RT CABIN FLOOR CROSS BEAM AND REPAIRED AREA, REF REO 670-53-21
- [SDR SWIA202055291](https://openairdocs.org/sdr/SWIA202055291.md): Intercostal · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID DOOR FWD INTERCOSTAL BELOW LATCH PIN HAS POSSIBLE CORROSION, AS MARKED. C-CHECK RO 1/5/2021. REPLACED PAX DOOR MID DOOR FWD INTERCOSTAL BELOW LATCH PIN, REF CRJ-700 SRM 51-42-06-001-001-A01 AND BOMBARDIER DWG: 601R31702-101 REV N DATE 2010-07-20
- [SDR SWIA202055290](https://openairdocs.org/sdr/SWIA202055290.md): Former · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER AT FS 311.75 IS CORRODED IN SEVERAL SPOTS. C-CHECK RO 1/5/2021. REPLACED PAX DOOR FORMER AT FS 311.75, REF CRJ-700 SRM 51-42-06-001-001-A01, CRJ-700 SRM 51-42-13-001-001-A01, CRJ-700 CRJ-700 SRM 51-42-21-001-001-A01, AND DWG: 601R31702 REV N.
- [SDR SWIA202055289](https://openairdocs.org/sdr/SWIA202055289.md): Intercostal · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 21L INTERCOSTAL BETWEEN FS 310 AND FS 319 HAS EVIDENCE OF CORROSION. C-CHECK RO 1/5/2021. REMOVED AND REPLACED NEW INTERCOSTAL P/N SH670-31822-1 AT STGR 21L BETWEEN FS 310.00-FS 319.00, REF CRJ700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 5
- [SDR SWIA202055288](https://openairdocs.org/sdr/SWIA202055288.md): Frame · corroded · Dec 4, 2020 · N788SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME FS 319 HAS EVIDENCE OF CORROSION ON WEB BETWEEN STRINGERS 19L TO 21L. C-CHECK RO 1/5/2021. REMOVED AND REPLACED NEW FRAME P/N SH 670-31891-3S AT FS 319.00 STGR 18L TO 21L, REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-21-001-001-A01. COMPLI
- [SDR SWIA202055303](https://openairdocs.org/sdr/SWIA202055303.md): Seat Track · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9 SEAT TRACK FROM APPROXIMATELY FS 349 TO FS 485 HAS EVIDENCE OF CORROSION AT APPROXIMATELY FS 415 AND FS 473. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK RBL 9 AT FS 349.00-FS 485.00, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055302](https://openairdocs.org/sdr/SWIA202055302.md): Seat Track · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 9 SEAT TRACK FROM APPROXIMATELY FS 377 TO FS 485 HAS EVIDENCE OF CORROSION ALONG ENTIRE LENGTH. C-CHECK RO 1/5/2021. REMOVED AND REPLACED SEAT TRACK LBL 9 AT FS 377.00-FS 485.00 WITH NEW HADWARE, REF CRJ700 AMM 53-00-49-400-801-A03.
- [SDR SWIA202055287](https://openairdocs.org/sdr/SWIA202055287.md): Intercostal · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > STRINGER 20R INTERCOSTAL HAS EVIDENCE OF CORROSION BETWEEN FS 310 AND FS 319. C-CHECK RO 1/5/2021. REMOVED AND REPLACED NEW INTERCOSTAL P/N SH670-32047-1 AT STGR 20R BETWEEN FS 310.00-FS 319.00, REF CRJ700 SRM 51-42-06-001-001-A01 AND DWG SH670-31950 REV Y.
- [SDR SWIA202055286](https://openairdocs.org/sdr/SWIA202055286.md): Floor Support · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT FLOOR SILL HAS EVIDENCE OF CORROSION AT APPROXIMATELY FS 280, FS 313 AND FS 319. C-CHECK RO 1/5/2021. REMOVED AND REPLACED NEW FLOOR SILL P/N SH670-32172-11 APPROXIMATELY FS 280.00-FS 319.00, REF CRJ700 SRM 51-42-06-001-001-A01 AND CRJ700 SRM 51-42-10-001
- [SDR SWIA202055285](https://openairdocs.org/sdr/SWIA202055285.md): Angle · cracked · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > ANGLE BETWEEN FS 280 BEAM AND FLOOR BEAM BOX STRUCTURE AT BL 12 LT HAS EVIDENCE OF CRACK IN RADIUS AT UPPER END. C-CHECK RO 1/5/2021. REMOVED CRACKED ANGLE, REPLACED WITH NEW ANGLE, PER CRJ 700 SRM 51-42-21-001-001-A01 AND DRAWING CC670-34010 REV K. COMPLIE
- [SDR SWIA202055284](https://openairdocs.org/sdr/SWIA202055284.md): Intercostal · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > RT INTERCOSTAL JUST RIGHT OF STR 27 BETWEEN FS 364.00 AND FS 349.00 CORRODED. C-CHECK RO 1/5/2021. NO DAMAGE ALLOWED AT LOCATION. REPLACED AVIONICS BAY DOOR FWD RT LATCH PIN INTERCOSTAL, REF CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA202055283](https://openairdocs.org/sdr/SWIA202055283.md): Intercostal · corroded · Dec 3, 2020 · N788SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > LT INTERCOSTAL JUST LEFT OF STR 27 BETWEEN FS 364.00 AND FS 349.00 CORRODED. C-CHECK RO 1/5/2021. NO DAMAGE ALLOWED AT LOCATION. REPLACED AVIONICS BAY DOOR FWD LT LATCH PIN INTERCOSTAL, REF CRJ-700 SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA202055317](https://openairdocs.org/sdr/SWIA202055317.md): Seal Plate · corroded · Dec 2, 2020 · N788SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD BAGGAGE BAY DOOR LOWER SEAL PLATE HAS MULTIPLE CORRODED AREAS, P/N LE670-39647-1. C-CHECK RO 1/5/2021. REMOVED AND REPLACED FWD BAG BAY DOOR LOWER SEAL PLATE, REF CRJ 700 SRM 51-42-06-001-001-A01.
- [SDR SWIA202055282](https://openairdocs.org/sdr/SWIA202055282.md): Structure · corroded · Dec 2, 2020 · N788SK · Cndair CL6002C10 · Emergency Exits
  > RT EMERGENCY EXIT DOOR HAS 2 AREAS OF CORROSION AROUND FASTENER HOLES ON LOWER SIDE OF DOOR, MARKED. C-CHECK RO 1/5/2021. REPAIRED CORROSION DAMAGE ON LOWER SECTION OF RT EMERGENCY DOOR, REF REO 670-52-21-066 REV- 2020-12-20. COMPLIED WITH TASK CARD 51-900-
- [SDR SWIA202055316](https://openairdocs.org/sdr/SWIA202055316.md): Lever · chafed · Nov 30, 2020 · N788SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > FWD BAGGGE BAY DOOR, FWD OUTER LEVER IS CHAFED, MARKED. C-CHECK RO 1/5/2021. FBBD, FWD OUTER LEVER REPLACED WITH NEW PART, AS PER CRJ 700 AMM 52-35-02-400-801-A01.
- [SDR SWIA202055301](https://openairdocs.org/sdr/SWIA202055301.md): Angle · corroded · Nov 30, 2020 · N788SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR BOTTOM ANGLE CORRODED AROUND FASTENER HOLES. C-CHECK RO 1/5/2021. REMOVED AND INSTALLED NEW PAX DOOR BOTTOM ANGLE PN: 601R317726-3, REF-CRJ-700 SRM 51-42-06-001-001 A01 AND SRM 51-42-13-001-001 A01.
- [SDR SWIA202055281](https://openairdocs.org/sdr/SWIA202055281.md): Striker · dented · Nov 30, 2020 · N788SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR SEAL STRIKER DENTED AT FWD UPPER SECTION, MARKED. C-CHECK RO 1/5/2021. REMOVED DENT/DAMAGE AND INSTALLED REPAIR DOUBLER AT PAX DOOR SEAL STRIKER AT FWD UPPER SECTION, PER CRJ 700 SRM 51-21-23-201-006-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. L
- [SDR SWIA202055280](https://openairdocs.org/sdr/SWIA202055280.md): Drag Angle · cracked · Nov 25, 2020 · N788SK · Cndair CL6002C10 · Vertical Stabilizer
  > LEFT SIDE VERTICAL STABILIZER, AFT DRAG ANGLE APPEARS CRACKED, MARKED. C-CHECK RO 1/5/2021. REPAIRED LEFT SIDE VERTICAL STABILIZER AFT DRAG ANGLE, REF CRJ700 SRM 55-31-00-201-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA202055315](https://openairdocs.org/sdr/SWIA202055315.md): Link · corroded · Nov 23, 2020 · N788SK · Cndair CL6002C10 · Aileron Control System
  > LT AILERON OUTBOARD PCU OUTPUT LINK IS CHAFED. C-CHECK RO 1/5/2021. LT AILERON REMOVED, OUTBOARD PCU OUTPUT LINK REMOVED AND REPLACED WITH NEW PART AND HARDWARE. OPERATIONAL TEST PERFORMED OK, NO CHAFING CONDITION NOTICED. WORK DONE AS PER CRJ 700 AMM 27-1
- [SDR SWIA202055314](https://openairdocs.org/sdr/SWIA202055314.md): Link · corroded · Nov 23, 2020 · N788SK · Cndair CL6002C10 · Aileron Control System
  > LT AILERON INBOARD PCU OUTPUT LINK IS CHAFED. C-CHECK RO 1/5/2021. LT AILERON REMOVED, INBOARD PCU OUTPUT LINK REMOVED AND REPLACED WITH NEW PART AND HARDWARE. OPERATIONAL TEST PERFORMED OK, NO CHAFING CONDITION NOTICED. WORK DONE AS PER CRJ 700 AMM 27-14-

Next page: https://openairdocs.org/aircraft/N788SK/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 = 'N788SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N788SK/reports

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