# Service difficulty reports: N703SK

A list on [N703SK](https://openairdocs.org/aircraft/N703SK.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 5 · 246 reports

- [SDR SWIA2026082076936](https://openairdocs.org/sdr/SWIA2026082076936.md): Sensor · faulted · Aug 20, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Slat Control System
  > IN FLT RECEIVED A SLATS FAIL CAUTION MSG. FAILED AT 1 DEGREE. WHEN THE FLAPS TO 45 FOR LANDING, SLATS WENT TO 25. (FLT 4325) TROUBLESHOT IN FLIGHT SLATS FAIL CAUTION MSG ON LANDING IAW FIM 27-81-03. NO CURRENT FAULTS. PERFORMED MULTIPLE OPS CHKS OF SLATS/FL
- [SDR SWIA2026061476258](https://openairdocs.org/sdr/SWIA2026061476258.md): Intercostal · gouged · Jun 14, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > AFT EQUIPMENT BAY RT INTERCOSTAL GOUGED AT RT 9 STRINGER APPROX. FS 1144. REPAIRED AFT EQUIPMENT BAY RT INTERCOSTAL AT RT 9 STRINGER APPROX. BS 1144 IAW REO 670-53-61-2736 DATED 2026-06-16 REV-- ALL STEPS COMPLIED WITH. COMPLIED WITH SKYWEST TASK CARD 51-900
- [SDR SWIA2026061376293](https://openairdocs.org/sdr/SWIA2026061376293.md): Slat Track · chafed · Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT WING SLAT TRACK 3-1 IS CHAFED. REPAIRED LT WING SLAT TRACK 3-1 IAW REO 670-57-42-2474 REV -.
- [SDR SWIA2026061376285](https://openairdocs.org/sdr/SWIA2026061376285.md): Slat Track · chafed · Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT WING SLAT TRACK 1-3 IS CHAFED. COMPLIED WITH REPAIR OF LT WING SLAT TRACK 1-3 IAW REO 670-57-42-2473 REV -.
- [SDR SWIA2026061376250](https://openairdocs.org/sdr/SWIA2026061376250.md): Slat Track · chafed · Jun 13, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT WING SLAT TRACK 2-1 IS CHAFED. COMPLIED WITH REPAIR OF LH WING SLAT TRACK 2-1 IAW REO REO 670-57-42-2485 REV--. COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2026052376260](https://openairdocs.org/sdr/SWIA2026052376260.md): Floorbeam · corroded · May 23, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > FLOORBEAM ANGLE AT BS 280, RBL 11 CORRODED. REPLACED FLOOR BEAM ANGLE/CLIP AT BS 280, RBL 11 WITH NEW. IAW SRM 51-42-06-001-001-A01 & DWG CC670-34191, REV NC, DWG CC67033052 REV -G AND DWG CC670-34010 REV -J. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-
- [SDR SWIA2026051976257](https://openairdocs.org/sdr/SWIA2026051976257.md): Striker · corroded · May 19, 2026 · N703SK · Cndair CL6002C11 · Service Doors
  > SERVICE DOOR LOWER SEAL STRICKER IS CORRODED. REPLACED SERVICE DOOR LOWER SEAL STRIKER IAW DWG SH670-31950, REV Y, & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY. NO LEAKS NOTED.
- [SDR SWIA2026051876269](https://openairdocs.org/sdr/SWIA2026051876269.md): Door Sill · corroded · May 18, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > GALLEY SERVICE DOOR LOWER SILL IS CORRODED JUST FORWARD OF THE FORWARD DOOR FITTING. REPLACED ANGLE LOWER SILL REF DWG SH670-31950 REV Y & SRM 51-42-06-001-001-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY
- [SDR SWIA2026042576295](https://openairdocs.org/sdr/SWIA2026042576295.md): Tie Bar · gouged · Apr 25, 2026 · N703SK · Cndair CL6002C11 · Nacelle/Pylon, Main Frame
  > LEFT ENGINE FAN COWL, PYLON TIE BAR HAS A GOUGE ON FWD SIDE WHERE IT ATTACHES TO THE PYLON. REPAIRED LT ENGINE FAN COWL, PYLON TIE BAR IAW REO 670-54-12-895, REV -.
- [SDR SWIA2026042576284](https://openairdocs.org/sdr/SWIA2026042576284.md): Tie Bar · chafed · Apr 25, 2026 · N703SK · Cndair CL6002C11 · Nacelle/Pylon, Main Frame
  > LEFT HAND FAN COWL - PYLON TIE BAR, UPPER ATTACHMENT POINT ON PYLON BRACKET CHAFED. REMOVED CHAFE FROM L/H FAN COWL PYLON TIE BAR UPPER ATTACHMENT POINT ON PYLON BRACKET PER IAW SRM 51-12-00-001-001-A01, REWORKED AREA FOUND TO BE WITHIN LIMITS IAW REO 670-54-
- [SDR SWIA2026042376299](https://openairdocs.org/sdr/SWIA2026042376299.md): Angle · out of limits · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > REMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME. REPLACED NEW ANGLE AT BS 280 LT IAW SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01, DWG CC670-33199, REV B, AND DWG CC670-33052, REV-F
- [SDR SWIA2026042376297](https://openairdocs.org/sdr/SWIA2026042376297.md): Doubler · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR AFT PULL IN CAM DOUBLER. REMOVED AND INSTALLED NEW PAX DOOR AFT PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG 601R31702, REV N.
- [SDR SWIA2026042376286](https://openairdocs.org/sdr/SWIA2026042376286.md): Intercostal · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR FWD DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV. N. PRESSURIZED AIRCRAFT IAW AMM 21-31-0
- [SDR SWIA2026042376281](https://openairdocs.org/sdr/SWIA2026042376281.md): Intercostal · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR AFT DD7 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702 REV N, PRESSURIZED AIRCRAFT IAW AMM 21-31-00-9
- [SDR SWIA2026042376276](https://openairdocs.org/sdr/SWIA2026042376276.md): Intercostal · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR FWD DD1 INTERCOSTAL. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. INSTALLED A NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01, AND DWG 601R31702, REV N. PRESSURIZED AIRCRAFT IAW AMM 21-
- [SDR SWIA2026042376268](https://openairdocs.org/sdr/SWIA2026042376268.md): Doubler · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR FWD PULL IN CAM DOUBLER. REMOVED AND INSTALLED NEW PAX DOOR FWD PULL IN CAM DOUBLER IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N, COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2026042376251](https://openairdocs.org/sdr/SWIA2026042376251.md): Intercostal · cracked · Apr 23, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > SUSPECTED CRACK ON PAX DOOR AFT DD1 INTERCOSTAL MX 32130057. DRILLED AND LOCATED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. INSTALLED NEW INTERCOSTAL IAW SRM 51-42-06-001-001-A01 AND DWG 601R31702, REV. N. PRESSURIZED AIRCRAFT
- [SDR SWIA2026042276265](https://openairdocs.org/sdr/SWIA2026042276265.md): Skin · cracked · Apr 22, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > UPON REMOVAL OF PAX DOOR INNER SKIN FOUND AFT FORMER CRACKED. INSTALLED NEW AFT FORMER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG 601R31702 REV. N.
- [SDR SWIA2026042176253](https://openairdocs.org/sdr/SWIA2026042176253.md): Floor Support · out of limits · Apr 21, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > REMOVE AND DISCARD OLD ANGLE ASSEMBLY. REPLACE WITH NEW SAME AS CC670-33199(-4 OPP) REMOVED AND REPLACED L/H COCKPIT FLOOR SUPPORT ANGLE (CC670-33199-4) WITH NEW PER REF CRJ 550 SRM 51-42-06-001-001-A01 DWG# CC670-33052, REV -G. COMPLIED WITH TASK CARD 51-900
- [SDR SWIA2026041876277](https://openairdocs.org/sdr/SWIA2026041876277.md): Crossbeam · cracked · Apr 18, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > RIGHT CROSSBEAM AT BS 280 CRACKED ON UPPER FLANGE. REPLACED RT CROSSBEAM AT BS 280 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01, AND DWG CC670-34010, REV K.
- [SDR SWIA2026041576271](https://openairdocs.org/sdr/SWIA2026041576271.md): Web · corroded · Apr 15, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > RIGHT LOWER WEB AT FS 280 HAS CORROSION. REMOVED AND INSTALLED NEW FABRICATED RT LOWER WEB AT BS 280 IAW SRM 53-11-10-201-003-A01, REV 38.
- [SDR SWIA2026041376287](https://openairdocs.org/sdr/SWIA2026041376287.md): Floorbeam · cracked · Apr 13, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM BS 280, LBL 12.00 CRACKED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM IAW SRM 53-11-43-201-003-A01.
- [SDR SWIA2026041276298](https://openairdocs.org/sdr/SWIA2026041276298.md): Floor Support · corroded · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > PASSENGER DOOR FLOOR SILL ANGLE BETWEEN BS 310 TO BS 349 HAS MULTIPLE SPOTS OF CORROSION. INSTALLED NEW MID CAP ANGLE TO PAX DOOR LOWER SILL ANGLE REF DWG. SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01.
- [SDR SWIA2026041276291](https://openairdocs.org/sdr/SWIA2026041276291.md): Floorbeam · cracked · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Floor Beam
  > COCKPIT FLOORBEAM AT BS 280, RBL 12 CRACKED AND CORRODED. REMOVED AND REPLACED DAMAGED AREA OF THE COCKPIT FLOORBEAM AT BS 280, RBL 12 IAW SRM 53-11-43-201-003-A01.
- [SDR SWIA2026041276266](https://openairdocs.org/sdr/SWIA2026041276266.md): Stringer · corroded · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 20L BETWEEN BS 319 AND 333. REMOVED AND REPLACED STRINGER 20L BETWEEN BS 310 AND 349 IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01 AND DWG SH67031810 REV. Y. INSTALLED FASTENERS TO NEW STRINGER 20L BETWEEN BS 319 AND 333 IAW
- [SDR SWIA2026041276255](https://openairdocs.org/sdr/SWIA2026041276255.md): Frame · cracked · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Frame
  > CRACK AT BS 333 BETWEEN S1R AND S2R. CRACK AT BS 333 BETWEEN S1R & S2R. REPAIRED BS 333 FRAME BETWEEN STRINGERS 1R - 2R. IAW REO 670-53-21-2863, REV -. ALSO COMPLIED WITH 51-900-1002-SKY.
- [SDR SWIA2026041276254](https://openairdocs.org/sdr/SWIA2026041276254.md): Cup · corroded · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > PASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS342.00 CORRODED. INSTALLED NEW AFT CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG SH670-31810, REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY
- [SDR SWIA2026041276252](https://openairdocs.org/sdr/SWIA2026041276252.md): Fitting · corroded · Apr 12, 2026 · N703SK · Cndair CL6002C11 · Passenger/Crew Doors
  > PASSENGER DOOR CABIN FLOOR HAND RAIL CUP AT APPROXIMATELY FS 314 CORRODED. INSTALLED A NEW FWD CUP FITTING TO PAX DOOR LOWER SILL AND MID CAP ANGLE REF DWG.SH670-31810 REV AE, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01. COMPLIED WITH 51-900-1002-SKY TA
- [SDR SWIA2026041076282](https://openairdocs.org/sdr/SWIA2026041076282.md): Crossbeam · cracked · Apr 10, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > DURING AUDIT OF 1C TASK CARD 53-140-509, DETAILED INSPECTION OF THE BS 280 CROSSBEAM, DRAIN PANS AND DRAIN TUBES, FOUND A SUSPECTED CRACKED ANGLE ON THE AFT SIDE OF THE BS 280 CROSSBEAM OTBD OF RBL 9 SHEAR BOX. REMOVED OLD ANGLE & REPLACED WITH 1 EA OF NEW AN
- [SDR SWIA2026040776290](https://openairdocs.org/sdr/SWIA2026040776290.md): Roller Guide · dented · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Cargo/Baggage Doors
  > AFT CARGO DOOR UPPER GUIDE ROLLER TRACKS DENTED IN MULTIPLE SPOTS. COMPLIED WITH SRM 53-61-58-201-002-A01 TRACK REPAIR, INSTALLED NEW LOWER TRACK SECTION REF REO 670-53-61-1296, REV --.
- [SDR SWIA2026040776288](https://openairdocs.org/sdr/SWIA2026040776288.md): Door Sill · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > AFT CARGO DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS AROUND SCREW HOLES. REPLACED AFT CARGO LOWER SILL. IAW DWG MM670-35085 REV K, SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01, & SRM 51-42-21-001-001-A01.
- [SDR SWIA2026040776283](https://openairdocs.org/sdr/SWIA2026040776283.md): Mount Bracket · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 BETWEEN STRG 23-24. REPLACED FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE APROX BS 581 BETWEEN S23-24. IAW DWG SH670-33600, REV AD, & SRM 51-42-21-001-001-A01.
- [SDR SWIA2026040776275](https://openairdocs.org/sdr/SWIA2026040776275.md): Floor Support · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > RIGHT FLOOR SUPPORT FROM BS 280 - 319.70 WAS CORRODED. REMOVED AND INSTALLED NEW RT FLOOR SUPPORT BS280 - 319.70, STRINGER 17R IAW DWG SH670-32172, REV E, DWG SH670-32170, REV V, SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND SRM 51-42-13-001-001-A
- [SDR SWIA2026040776273](https://openairdocs.org/sdr/SWIA2026040776273.md): Mount · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > FORWARD CARGO BAY, AFT CARGO NET MOUNTING PLATE CORRODDED APROX FS 581 CENTER STRG 27. REMOVED AND REPLACED WITH NEW FWD CARGO BAY AFT CARGO NET MOUNTING PLATE. COMPLIED WITH ALL STEPS OF TASK CARD 51-900-1002-SKY. IAW DWG SH670-33600 REV AD, SRM 51-40-11-001
- [SDR SWIA2026040776263](https://openairdocs.org/sdr/SWIA2026040776263.md): Floor Support · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Miscellaneous Structure
  > LEFT SIDE FLOOR SUPPORT BS 280 - 310 CORRODED. REMOVED AND INSTALLED NEW LT FLOOR SILL FROM BS 280 TO 310 IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-40-11-001-001-A01, SRM 51-42-13-001-001-A01, AND DWG SH670-32170, REV V.
- [SDR SWIA2026040776261](https://openairdocs.org/sdr/SWIA2026040776261.md): Door Sill · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > PAX DOOR LOWER SILL CORRODED IN MULTIPLE SPOTS. INSTALLED NEW PAX DOOR LOWER SILL ANGLE REF BOMBARDIER DWG SH670-31810 REV AE, SRM 51-42-21-001-001-A01, SRM 51-42-06-001-001-A01. COMPLIED WITH 51-900-1002-SKY TASK CARD.
- [SDR SWIA2026040776259](https://openairdocs.org/sdr/SWIA2026040776259.md): Mount · corroded · Apr 7, 2026 · N703SK · Cndair CL6002C11 · Fuselage, Equipment Attach Fittings
  > FORWARD CARGO BAY, FWD CARGO NET MOUNTING PLATE CORRODDED APROX FS 533 BETWEEN S23-24 LT. REPLACED AND INSTALLED NEW BRACKET SH670-33389-1, IAW DWG.SH670-33600 REV AD, SRM.51-42-10-001-001-A01 AND SRM 51-42-21-001-001-A01, AND SRM 51-42-22-001-001-A01. ALSO
- [SDR SWIA2026040276296](https://openairdocs.org/sdr/SWIA2026040276296.md): Slat Track · gouged · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT SLAT TRACK 3-2 HAS GOUGES ON INBOARD EDGE AND LOWER SURFACES. REPAIRED LEFT SLAT TRACK 3-2 PER REO 670-57-42-2475, REV --, STEPS 1-7. OPS AND RIG CHECKED GOOD.
- [SDR SWIA2026040276289](https://openairdocs.org/sdr/SWIA2026040276289.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 CHAFED ON LOWER SIDE REWORKED THE RT SLAT TRACK 1-3 IAW REO 670-57-42-2480, REV-.
- [SDR SWIA2026040276279](https://openairdocs.org/sdr/SWIA2026040276279.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 CHAFED ON LOWER SURFACE. REPAIRED LT SLAT TRACK 3-3 PER REO 670-57-42-2476, REV-,
- [SDR SWIA2026040276272](https://openairdocs.org/sdr/SWIA2026040276272.md): Slat Track · gouged · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS GOUGES ON INBOARD EDGE AND LOWER SURFACE. REPAIRED LT SLAT TRACK 2-2 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2477 REV--.
- [SDR SWIA2026040276270](https://openairdocs.org/sdr/SWIA2026040276270.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-3 CHAFED ON LOWER SIDE. REPAIRED RH SLAT TRACK 3-3 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2478 REV-.
- [SDR SWIA2026040276267](https://openairdocs.org/sdr/SWIA2026040276267.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 CHAFED ON LOWER SIDE. REWORKED RT SLAT TRACK 1-2 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2481 REV--.
- [SDR SWIA2026040276262](https://openairdocs.org/sdr/SWIA2026040276262.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 CHAFED ON LOWER AND INBD SIDE. REPAIRED RT SLAT TRACK 2-2 LOWER INBD SIDE IAW SRM 51-12-00-001-001-A01, REO 670-57-42-2479, REV --.
- [SDR SWIA2026040276256](https://openairdocs.org/sdr/SWIA2026040276256.md): Slat Track · chafed · Apr 2, 2026 · N703SK · Cndair CL6002C11 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-1 CHAFED ON LOWER SIDE. BLENDED SLAT TRACK REWORKED RH SLAT TRACK 2-1 PER INSTRUCTIONS OF REPAIR ENGINEERING ORDER REO 670-57-42-2472 REV --, ALL STEPS COMPLIED WITH.
- [SDR SWIA2026033176294](https://openairdocs.org/sdr/SWIA2026033176294.md): Stand Off · cracked · Mar 31, 2026 · N703SK · Cndair CL6002C11 · Engine Thrust Reverser
  > RIGHT UPPER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED THE CRACKED STANDOFF AND INSTALLED A NEW STANDOFF ON R/H UPPER TRANSCOWL, IAW GREO #670-54-21-971, REV -B, STEP 1-3.
- [SDR SWIA2026032876300](https://openairdocs.org/sdr/SWIA2026032876300.md): Plate · cracked · Mar 28, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Structure
  > FORWARD EQUIPMENT COMPARTMENT RIGHT SIDE ADG PUMP REINFORCEMENT PLATE CRACKED. PERFORMED REPAIR TO FORWARD EQUIPMENT COMPARTMENT RIGHT SIDE ADG PUMP REINFORCEMENT PLATE & INSTALLED NEW DOUBLER IAW SRM 53-11-43-201-001-A01. REVISION 38,
- [SDR SWIA2026032776278](https://openairdocs.org/sdr/SWIA2026032776278.md): Lug · damaged · Mar 27, 2026 · N703SK · Cndair CL6002C11 · Fuselage, Door Hinge
  > PASSENGER DOORS DOOR SIDE OF THE HINGE LUG 27 ROLL PIN HOLE IS ELONGATED. DRILLED AND LOCATED NEW PAX DOOR PIANO HINGE DOOR SIDE IAW SRM 52-11-01-201-002-A01, STEPS E, F, G, H, I AND SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, & DWG 601R31702, REV N.
- [SDR SWIA2026032776274](https://openairdocs.org/sdr/SWIA2026032776274.md): Skin · scratched · Mar 27, 2026 · N703SK · Cndair CL6002C11 · Fuselage Main, Plate/Skin
  > MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO BS 1051.30 BETWEEN S27R AND S24R. REPAIRED MULTIPLE NICKS AND SCRATCHES ON EXTERIOR SKIN BETWEEN BS 1000 TO 1051.30 BETWEEN S27R AND S24R. IAW REO 670-53-61-2715 REV -.
- [SDR SWIA2026032676280](https://openairdocs.org/sdr/SWIA2026032676280.md): Receptacle · cracked · Mar 26, 2026 · N703SK · Cndair CL6002C11 · Electrical/Electronic Compartment Doors
  > RIGHT TRU LANDING AFT LATCH RECEPTACLE CRACKED. INSTALLED NEW RIGHT TRU LANDING IAW REO 670-53-11-2304 REV-.

Next page: https://openairdocs.org/aircraft/N703SK/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 = 'N703SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N703SK/reports

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OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.