# Service difficulty reports: N716SK

A list on [N716SK](https://openairdocs.org/aircraft/N716SK.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 · 214 reports

- [SDR SWIA2026032976171](https://openairdocs.org/sdr/SWIA2026032976171.md): Intercostal · corroded · Mar 29, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD5 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD5 IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026032976164](https://openairdocs.org/sdr/SWIA2026032976164.md): Intercostal · corroded · Mar 29, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL DD1A AT FS 347.25 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD1A AT FS 347.25 IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026031576188](https://openairdocs.org/sdr/SWIA2026031576188.md): Bearing · flat · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > BOTH INBD LT SLAT TRACK ROLLERS FOR SLAT TRACK 3-2 HAVE FLAT SPOTS REQUIRE REPLACEMENT. REMOVED AND INSTALLED INBD FWD AND INBD AFT SIDE ROLLER ASSYS IAW AMM 27-81-44-000/400-803-A01. REMOVED INBD FWD AND INBD AFT DAMAGED BEARINGS AND INSTALLED NEW BEARINGS
- [SDR SWIA2026031576187](https://openairdocs.org/sdr/SWIA2026031576187.md): Bearing · out of limits · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > ROLLERS AT SLAT TRACK 3-2 IB AFT, OB AFT AND FWD OB REQUIRES REPLACEMENT. REMOVED AND INSTALLED AFT INBD AND AFT OUTBD SIDE ROLLERS IAW AMM 27-81-44-000/400-803-A01. REMOVED AFT INBD AND AFT OUTBD SIDE ROLLERS DAMAGED ROLLER BEARINGS AND INSTALLED NEW ROLLER
- [SDR SWIA2026031576186](https://openairdocs.org/sdr/SWIA2026031576186.md): Bearing · flat · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > ALL 4 ROLLERS AT SLAT TRACK 2-2 HAS FLAT SPOTS REQUIRES REPLACEMENT. REMOVED AND REPLACED THE RT SLAT-TRACK 2-2 FWD INBD AND OTBD SIDE ROLLERS IAW AMM 27-81-44-000/400-802 (CONFIGA01). REFERENCE CONTINUATION CARD FOR WORK PERFORMED.
- [SDR SWIA2026031576185](https://openairdocs.org/sdr/SWIA2026031576185.md): Roller · damaged · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > ALL 4 ROLLERS AT SLAT TRACK 1-2 HAS FLAT SPOTS REQUIRES REPLACEMENT. REMOVED AND INSTALLED THE RT SLAT-TRACK 1-2 FWD AND AFT IB AND OB SIDE ROLLERS IAW AMM 27-81-44-000/400-801(CONFIGA01). REMOVED AFT INBD AND AFT OUTBD DAMAGED BEARINGS AND INSTALLED NEW BE
- [SDR SWIA2026031576184](https://openairdocs.org/sdr/SWIA2026031576184.md): Roller · damaged · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > ALL FOUR LH SLAT TRACK ROLLERS AT SLAT TRACK 2-2 HAVE FLAT SPOTS REQUIRE REPLACEMENT. REMOVED AND REPLACED ALL 4 LT SLAT TRACK ROLLER BEARINGS IAW AMM SW 1631 REMOVED AND INSTALLED THE LT SLAT-TRACK SERVICEABLE 2-2 SIDE ROLLERS IAW AMM 27-81-44-000/400-802 (C
- [SDR SWIA2026031576183](https://openairdocs.org/sdr/SWIA2026031576183.md): Roller · damaged · Mar 15, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > ALL 4 LEFT SLAT TRACK ROLLERS AT 1-2 HAVE FLAT SPOTS REQUIRE REPLACEMENT. REMOVED & INTALLED ALL 4 LT SLAT TRACK ROLLERS AT 1-2 IAW AMM 27-81-44-000-801 (CONFIG A01) & AMM27-81-44-400-801 (CONFIG A01)
- [SDR SWIA2026031476165](https://openairdocs.org/sdr/SWIA2026031476165.md): Former · corroded · Mar 14, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR, FRAME AT FS347.25 BETWEEN DD5 AND DD6 FOUND CORRODED, REQUIRES REPLACEMENT. INSTALLED PAX DOOR AFT FORMER IAW SRM 51-42-06-001-001-A01 AND SRM 51-42-21-001-001-A01.
- [SDR SWIA2026031476146](https://openairdocs.org/sdr/SWIA2026031476146.md): Intercostal · corroded · Mar 14, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD3 FOUND CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD3 IAW SRM TASK 51-42-06-001-001-A01AND SRM TASK 51-42-21-001-001-A01.
- [SDR SWIA2026031076180](https://openairdocs.org/sdr/SWIA2026031076180.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD2 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD2 IAW SRM TASK 51-42-06-001-001-A01, SRM TASK 51-42-21-001-001-A01.
- [SDR SWIA2026031076177](https://openairdocs.org/sdr/SWIA2026031076177.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD INTERCOSTAL DD2 FOUND TO BE CORRODED. REQUIRES REPLACEMENT. INSTALL NEW SERVICEABLE PAX DOOR FWD INTERCOSTAL DD2 IAW SRM TASK 51-42-06-001-001-A01.
- [SDR SWIA2026031076176](https://openairdocs.org/sdr/SWIA2026031076176.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD1A FOUND TO BE CORRODED. REQUIRES REPLACEMENT. INSTALLED SERVICEABLE PAX DOOR MID INTERCOSTAL DD1A IAW SRM TASK 51-42-06-001-001-A01, IAW SRM TASK 51-42-21-001-001-A01.
- [SDR SWIA2026031076175](https://openairdocs.org/sdr/SWIA2026031076175.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL DD4 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026031076172](https://openairdocs.org/sdr/SWIA2026031076172.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD1 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD1 IAW SRM 51-42-06-001-001-A01.
- [SDR SWIA2026031076159](https://openairdocs.org/sdr/SWIA2026031076159.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR AFT INTERCOSTAL DD5 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR AFT INTERCOSTAL DD5 IAW SRM 51-42-06-001-001-A01.,
- [SDR SWIA2026031076149](https://openairdocs.org/sdr/SWIA2026031076149.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD4 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW PAX DOOR MID INTERCOSTAL DD4 IAW SRM 51-42-06-001-001-A01 REFER TO CONTINUATION CARD FOR DETAILS.
- [SDR SWIA2026031076140](https://openairdocs.org/sdr/SWIA2026031076140.md): Intercostal · corroded · Mar 10, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR MID INTERCOSTAL DD6 FOUND TO BE CORRODED, REQUIRES REPLACEMENT. INSTALLED NEW SERVICEABLE PAX DOOR MID INTERCOSTAL DD6 IAW SRM 51-42-06-001-001-A01AND 51-42-21-001-001-A01 REFER TO CONTINUATION CARD FOR DETAILS COMPLETED SKY CARD 51-900-1002-SKY.
- [SDR SWIA2026030976179](https://openairdocs.org/sdr/SWIA2026030976179.md): Slat Track · corroded · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-2 HAS EVIDENCE OF CORROSION IN 2 LOCATIONS. REPAIRED RT SLAT TRACK 1-2 IAW REO 670-57-42-2462 REV -.
- [SDR SWIA2026030976173](https://openairdocs.org/sdr/SWIA2026030976173.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 1-1 IAW REO 670-57-42-1279, REV. B.
- [SDR SWIA2026030976167](https://openairdocs.org/sdr/SWIA2026030976167.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 3-3 IAW REO 670-57-42-2416 REV -.
- [SDR SWIA2026030976163](https://openairdocs.org/sdr/SWIA2026030976163.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-3 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 1-3 IAW REO 670-57-42-2410 REV -.
- [SDR SWIA2026030976162](https://openairdocs.org/sdr/SWIA2026030976162.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-3 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RT SLAT TRACK 3-3 IAW REO 670-57-42-2466 REV -.
- [SDR SWIA2026030976160](https://openairdocs.org/sdr/SWIA2026030976160.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 2-1 IAW REO 670-57-42-2420 REV-.
- [SDR SWIA2026030976157](https://openairdocs.org/sdr/SWIA2026030976157.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-1 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RT SLAT 2-1 IAW REO 670-57-42-2465 REV -.
- [SDR SWIA2026030976156](https://openairdocs.org/sdr/SWIA2026030976156.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RT SLAT TRACK 3-2 IAW MHIRJ REO 670-57-42-2468 REV --.
- [SDR SWIA2026030976155](https://openairdocs.org/sdr/SWIA2026030976155.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-3 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RT SLAT 1-3 IAW REO 670-57-42-2464 REV -.
- [SDR SWIA2026030976154](https://openairdocs.org/sdr/SWIA2026030976154.md): Slat Track · corroded · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 HAS EVIDENCE OF CORROSION IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 1-2 IAW REO 670-57-42-2412 REV -
- [SDR SWIA2026030976153](https://openairdocs.org/sdr/SWIA2026030976153.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RT SLAT TRACK 2-2 IAW REO 670-57-42-2469 REV -.
- [SDR SWIA2026030976151](https://openairdocs.org/sdr/SWIA2026030976151.md): Slat Track · corroded · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1 HAS EVIDENCE OF CORROSION IN 4 LOCATIONS. REPAIRED LT SLAT TRACK 1-1 IAW REO 670-57-42-1279 REV. B.
- [SDR SWIA2026030976150](https://openairdocs.org/sdr/SWIA2026030976150.md): Slat Track · corroded · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LT SLAT TRACK 2-2 HAS EVIDENCE OF CORROSION IN 2 LOCATIONS. REPAIRED LT SLAT TRACK 2-2 IAW REO 670-57-42-24-15 REV --.
- [SDR SWIA2026030976147](https://openairdocs.org/sdr/SWIA2026030976147.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-2 HAS CHAFING DAMAGE IN 2 SPOTS. REPAIRED LT SLAT TRACK 3-2 IAW REO 670-57-42-2413 REV-.
- [SDR SWIA2026030976145](https://openairdocs.org/sdr/SWIA2026030976145.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RT SLAT TRACK 2-3 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RH SLAT TRACK 2-3 IAW REO 670-57-42-2467 REV --.
- [SDR SWIA2026030976143](https://openairdocs.org/sdr/SWIA2026030976143.md): Slat Track · chafed · Mar 9, 2026 · N716SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-1 HAS CHAFING DAMAGE IN 2 LOCATIONS. REPAIRED RH SLAT TRACK 1-1 IAW REO 670-57-42-2463 REV -- DATE 2026-04-15.
- [SDR SWIA2026030876152](https://openairdocs.org/sdr/SWIA2026030876152.md): Angle · corroded · Mar 8, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR KICK PLATE ANGLE IS CORRODED IN 2 SPOTS. PAX DOOR KICK PLATE ANGLE OUT OF LIMITS IAW SRM 53-21-23-101-001-A01 DUE TO MULTIPLE FACTORSINCLUDING PROXIMITY OF DAMAGE TO FASTENERS, MORE THAN 30 PERCENT OF PART DAMAGED, AND MULTIPLE CROSS SECTIONS OF DAMA
- [SDR SWIA2026030876144](https://openairdocs.org/sdr/SWIA2026030876144.md): Hinge · chafed · Mar 8, 2026 · N716SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (FUSELAGE SIDE) HAS CHAFING DAMAGE BETWEEN SEVERAL LUGS. REMOVED AND REPLACED A/C SIDE PAX DOOR HINGE WITH NEW SERVICEABLE HINGE IAW SRM 53-21-23-201-007-A01. PERFORMED REO 670-53-21-2844 REV -A FOR 3EA. DISCREPANT HOLES FOR ACFT SIDE PAX DOOR
- [SDR SWIA2026030776166](https://openairdocs.org/sdr/SWIA2026030776166.md): Bulkhead Web · corroded · Mar 7, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CORROSION ON LT LOWER WEB BULKHEAD BS 280. REMOVED BS 280 LT LOWER WEB AND BUTTSTRAP IAW SRM 51-42-06-001-0010-A01, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-22-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS, BS 280 LT LOWER
- [SDR SWIA2026030776148](https://openairdocs.org/sdr/SWIA2026030776148.md): Bulkhead Web · corroded · Mar 7, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > CORROSION ON RT LOWER WEB BULKHEAD BS 280. REMOVED BS 280 RT LOWER WEB AND BUTTSTRAP IAW SRM 51-42-06-001-001-A01, SRM 51-42-13-001-001-A01. SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01. FABRICATED, LOCATED AND DRILLED NEW REPAIR PARTS, BS 280 RT LOWER
- [SDR SWIA2026030176182](https://openairdocs.org/sdr/SWIA2026030176182.md): Crossbeam · corroded · Mar 1, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Structure
  > RIGHT BS 280 CROSSBEAM HAS MULTIPLE CORROSION PITS ON EDGE CORNER OF BEAM REQUIRES REPLACEMENT. EVALUATED AND FOUND OUT OF LIMITS IAW SRM 53-11-41-201-002-A01, DUE TO SEVERE CORROSION MORE THAN 50% OF THE MATERIAL WAS LOST, RT BS 280 CROSSBEAM NEEDS TO BE REP
- [SDR SWIA2026030176158](https://openairdocs.org/sdr/SWIA2026030176158.md): Crossbeam · corroded · Mar 1, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Structure
  > LEFT BS 280 CROSSBEAM HAS MULTIPLE CORROSION PITS ON EDGE CORNER OF THE BEAM REQUIRES REPLACEMENT. REMOVED LT BS 280 CROSSBEAM IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-13-001-001-A01, SRM 51-42-22-001-001-A01. LOCATED AND DRILLED NEW
- [SDR SWIA2026022776181](https://openairdocs.org/sdr/SWIA2026022776181.md): Former · corroded · Feb 27, 2026 · N716SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FORMER BS 329.41 DD5/DD6 IS CORRODED. INSTALLED NEW PAX DOOR FORMER AT BS 329.41 BETWEEN DD5 AND DD6 IAW SRM 51-42-06-001-001-A01
- [SDR SWIA2026021676178](https://openairdocs.org/sdr/SWIA2026021676178.md): Skin · gouged · Feb 16, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TECH HIT AIRCRAFT WITH MAN LIFT ON RT SKIN PANEL AND DENT AND GOUGED SKIN FROM FS 1108 TO FS 1126 BETWEEN STRG 16R AND STRG 18R. REPAIRED SKIN DAMAGE FROM FS1108 TO FS1126 IAW REO 670-53-61-2684 REV -
- [SDR SWIA2026021576174](https://openairdocs.org/sdr/SWIA2026021576174.md): Skin · ground damage · Feb 15, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > TECH HIT AIRCRAFT WITH MAN LIFT ON RH SKIN PANEL AND DENT AND GOUGED SKIN FROM BS 1000 TO BS 1015 BETWEEN STRG 15R AND 17R. RECEIVED AND COMPLIED WITH FINAL MHIRJ REO 670-53-61-2685 REV -. THE REPAIR OF DAMAGE FROM FS 1000 TO FS 1015 RH SKIN PANEL BETWEEN ST
- [SDR SWIA2026021476169](https://openairdocs.org/sdr/SWIA2026021476169.md): Vane · chafed · Feb 14, 2026 · N716SK · Cndair CL6002C10 · Trailing Edge Flaps
  > LH INBD FLAP VANE LEADING EDGE IS CHAFED AT 4EA. LOCATIONS. REPAIRED LH INBD FLAP VANE IN 4EA LOCATIONS REO 670-57-52-656 REV -.
- [SDR SWIA2026021376161](https://openairdocs.org/sdr/SWIA2026021376161.md): Drag Angle · cracked · Feb 13, 2026 · N716SK · Cndair CL6002C10 · Fuselage, Stabilizer Attach Fittings
  > VERTICAL STAB LEFT DRAG ANGLE SHOWS SIGN OF POSSIBLE CRACK. REPAIRED LT VERTICAL STAB DRAG ANGLE IAW SRM 55-31-00-201-001-A01.
- [SDR SWIA2026012776168](https://openairdocs.org/sdr/SWIA2026012776168.md): Rivet · damaged · Jan 27, 2026 · N716SK · Cndair CL6002C10 · Fuselage Main, Longeron/Stringer
  > RIVET ON STRG 19R. APPROXIMATELY 5 INCH FWD OF FRAME 280 AND APPROXIMATELY 7 INCH AFT OF FRAME 265. 2. RIVET ON STRG 21R. APPROXIMATELY 10" FWD OF FRAME 394 AND APPROXIMATELY 2" AFT OF FRAME 379. 3. RIVET ON STRG 21R. APPROXIMATELY 9" FWD OF FRAME 421 AND APPR
- [SDR SWIA2025121876170](https://openairdocs.org/sdr/SWIA2025121876170.md): Skin · damaged · Dec 18, 2025 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA88272-REO 670-53-00-045-PR1 - COMPLY WITH PERMANENT REPAIR ON RA ID: 88272FUSELAGE SKIN LIGHTNING STRIKE DAMAGE. REF REO 670-53-00-045. COMPLY WITH PERMANENT REPAIR FOR REO 670-53-00-045 REV -K DATED 1/15/2021 PART 2 L
- [SDR SWIA2025121876142](https://openairdocs.org/sdr/SWIA2025121876142.md): Skin · damaged · Dec 18, 2025 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: RA89829-SRM 53-00-00-201-003-A01 TYPE 3-PR1 - COMPLY WITH PERMANENT REPAIR ON RA ID: 89829FOUND LIGHTNING STRIKE DAMAGE TO FUSELAGE SKIN ON THE RH SIDE AROUND A FASTENER AT FS 311.5 WL 57 GREATER THAN 0.005" DEEP. REPAI
- [SDR SWIA2025121876141](https://openairdocs.org/sdr/SWIA2025121876141.md): Fastener · damaged · Dec 18, 2025 · N716SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE PITTING DAMAGE TO A FASTENER ON RT OF BS 383 WL 59 GREATER THAN 20% OF RIVET HEAD SPECIFICED BY SRM. UPON CLEANING FOUND DAMAGE TO COUNTER SINK AREA DEEPER THAT 0.005 IN. REPAIRED DAMAGE TO FASTENER AREA ON RT SIDE OF FUSELAGE AT FS 383 WL 59
- [SDR SWIA2025F01329](https://openairdocs.org/sdr/SWIA2025F01329.md): Jackscrew · damaged · Sep 22, 2025 · N716SK · Cndair CL6002C10 · Flight Control System
  > UPON INSPECTION, FOUND DAMAGE TO THE HSTA RH SCREW JACK TOP ATTACHMENT AND BACKUP STRUCTURE IN MULTIPLE AREAS.DAMAGE UPPER CENTER AREA OF MATING SURFACE "FOOT" MEASURES 0.25" L X 0.062" W BY 0.0010 DEEPDAMAGE ON UPPER RH CORNER OF MATING SURFACE "FOOT" MEASURE

Next page: https://openairdocs.org/aircraft/N716SK/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 = 'N716SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N716SK/reports

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