# Service difficulty reports: N765SK

A list on [N765SK](https://openairdocs.org/aircraft/N765SK.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 4 · 185 reports

- [SDR SWIA2025112400018](https://openairdocs.org/sdr/SWIA2025112400018.md): Skin · dented · Nov 18, 2025 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > REF AML 1751235: UPON INSPECTION FOUND: 3-OFF AREAS OF DENT DAMAGE TO LHS FUSELAGE SKIN PANEL (DWG: MM670-35146, 0.080€? ±0.005€? NOMINAL PAD UP THK, 0.050€? ±0.005€? & 0.060€? ±0.005€? CHEM-MILLED POCKET THICKNESS, REF) BETWEEN FS1015.00 -FS1047.00 A
- [SDR SWIA2025111900008](https://openairdocs.org/sdr/SWIA2025111900008.md): Skin · dented · Nov 18, 2025 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > REF AML# 1751235: UPON INSPECTION FOUND: 3-OFF AREAS OF DENT DAMAGE TO LT FUSELAGE SKIN PANEL (DWG: MM670-35146, 0.080€? ±0.005€? NOMINAL PAD UP THK, 0.050€? ±0.005€? & 0.060€? ±0.005€? CHEM-MILLED POCKET THICKNESS, REF) BETWEEN FS1015.00 -FS1047.00 A
- [SDR SWI2025F00664](https://openairdocs.org/sdr/SWI2025F00664.md): Windshield · sparks · May 23, 2025 · N765SK · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > D:DURING CLIMB OUT THROUGH 4000 HEARD A LOUD POP, SPARK AND GREY SMOKE, WHICH QUICKLY CLEARED, OUT OF THE RIGHT WINDSHIELD HEATER. RECEIVED RIGHT WINDSHIELD CAUTION. RAN QRH.C: MEL 30-41-1ACAT C DUE ON 06/02/2025DURING CLIMB OUT THROUGH 4000 HEARD A LOUD POP,
- [SDR SWI2025F00612](https://openairdocs.org/sdr/SWI2025F00612.md): Slat Track · out of limits · Mar 26, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING L/E SLAT #3, INBD TRACK REQUIRES REPLACEMENT DUE TO DAMAGE EXCEEDING THE ALLOWABLE LIMITS PER MHI ENGINEERING (C-CHECK RO 04/30/2025)REMOVED AND INSTALLED NEW L/E #3 I/B SLAT TRACK PER CRJ 700 AMM 27-81-41-000-801-A01,27-81-41-400-801-A01,27-81-25-000
- [SDR SWIA20250430326](https://openairdocs.org/sdr/SWIA20250430326.md): Slat Track · out of limits · Mar 26, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > RH WING L/E SLAT #2, INBD TRACK REQUIRES REPLACEMENT DUE TO DAMAGE EXCEEDING THE ALLOWABLE LIMITS PER MHI ENGINEERINGÂ (C-CHECK RO 04/30/2025)REMOVED AND INSTALLED REPAIRED L/E #2 I/B SLAT TRACK PER CRJ 700 AMM 27-81-41-000-801-A01,27-81-41-400-801-A01,27-8
- [SDR SWI2025F00622](https://openairdocs.org/sdr/SWI2025F00622.md): Guide Fitting · chafed · Jan 22, 2025 · N765SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH OUTBOARD WING TRAILING EDGE, INBOARD FLAP ROLLER GUIDE FITTING IS CHAFED. (C-CHECK RO 04/30/2025)CLEANED UP CHAFE DAMAGE & EVALUATED. DAMAGE FOUND TO BE WITHIN LIMITS OF REO 670-57-51-594 REV. -- DATED: 2025-04-18.OPS CHECK GOOD AT THIS TIME. REF. CRJ 700
- [SDR SWIA20250430122](https://openairdocs.org/sdr/SWIA20250430122.md): Floorbeam · corroded · Jan 22, 2025 · N765SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > L/H SIDE OF CROSS BEAM AT FS 280.00 LBL 9, WL 72.00 HAS 100% MATERIAL LOSS DUE TO CORROSION, REQUEST REPAIR (C-CHECK RO 04/30/2025)REMOVED AND REPLACED L/H CROSS BEAM AT FS 280.00 WL 72.00 IAW CRJ 700 SRM 51-42-06-001-001-A01, CRJ 700 SRM 51-42-21-001-001-A01
- [SDR SWIA20250430109](https://openairdocs.org/sdr/SWIA20250430109.md): Pad · worn · Jan 9, 2025 · N765SK · Cndair CL6002C10 · Service Doors
  > GALLEY SERVICE DOOR FWD EXTERNAL SURROUND STRUCTURE AND FITTINGS HAVE WORN STOP PADS, CHAFFED GUIDE FITTINGS (C-CHECK RO 04/30/2025)CLEANED AND RESTORED FINISH ON GUIDE FITTINGS IAW CRJ200 51-26-00-001-004-A01 FOUND TO BE MISSING PAINT ONLY AND REWORKED DOOR S
- [SDR SWI2025F00607](https://openairdocs.org/sdr/SWI2025F00607.md): Slat Track · worn · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 3-2 IB AFT ROLLER WORN OUT OF LIMITS (C-CHECK RO 04/30/2025)REMOVED AND REPLACED LH SLAT TRACK 3-2 PER CRJ 700 AMM 27-81-44-000-803 AND 27-81-44-400-803 OPS CHECK WILL BE PERFORMED ON JOB CARD HT405-20353 CAMP# 2971144-1
- [SDR SWI2025F00606](https://openairdocs.org/sdr/SWI2025F00606.md): Slat Track · worn · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 2-2 OB AFT ROLLER WORN OUT OF LIMITS (C-CHECK RO 04/30/2025)REAMOVED AND REPLACED LH SLAT TRACK 2-2 OB AND AFT ROLLER PER CRJ 700 AMM 27-81-44-000-802 AND 27-81-44-400-802 OPS CHECK WILL BE PERFORMED ON HT 405-20353 CAMP # 29071144-1
- [SDR SWI2025F00605](https://openairdocs.org/sdr/SWI2025F00605.md): Slat Track · worn · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > LH SLAT TRACK 1-2 BOTH IB ROLLERS AND AFT OB ROLLER WORN OUT OF LIMITS (C-CHECK RO 04/30/2025)REMOVED AND REPLACED LH SLAT TRACK 1-2 BOTH I/B ROLLERS AND AFT O/B ROLLER BER CRJ700 AMM 27-81-44-000-801-A01 AND AMM 27-81-44-400-801-A01 OPS CHECK PERFORMED ON W
- [SDR SWI2025F00604](https://openairdocs.org/sdr/SWI2025F00604.md): Slat Track · worn · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 2-2 AND 0B FWD ROLLERS WORN OUT OF LIMITS (C-CHECK RO 04/30/2025)REMOVED AND REPLACED RH SLAT TRACK I/B AND O/B FWD ROLLERS PER CRJ 700 AMM 27-81-44-000-802(CONF A01) AND AMM 27-81-44-400-802(CONFIG A01)OPS CHECK PERFORMED ON HT405/10098 CAMP # 2
- [SDR SWI2025F00603](https://openairdocs.org/sdr/SWI2025F00603.md): Slat Track · worn · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > RH SLAT TRACK 1-2 FWD AND AFT 0B ROLLERS WORN OUT OF LIMITS (C-CHECK RO 04/30/2025)REMOVED AMD REPLACED RH SLAT TRACK 1-2 FWD AND AFT O/B ROLLERS PER CRJ 700 AMM TASK 21-81-44-000-801-A01 AND 27-81-44-400-801-A01 OPS CHECK PERFORMED ON CARD 405-10098 CAMP 2907
- [SDR SWIA20250430106](https://openairdocs.org/sdr/SWIA20250430106.md): Skin · chafed · Jan 6, 2025 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > LH EXTERNAL FUSELAGE, CHAFFING ON SKIN PANEL, FS961, BETWEEN LH STR# 23-24 (C-CHECK RO 04/30/2025)COMPLIED WITH REO N# 670-53-51-339 REV. -- 2025-02-15, AT L/H EXTERNAL FUSELAGE SKIN BLENDED CORROSION DAMAGE BTW FS 953.00 - FS 969.00 & STR 23- STR 24L. (FOR WO
- [SDR SWIA20250430103](https://openairdocs.org/sdr/SWIA20250430103.md): Hinge Arm · loose · Jan 3, 2025 · N765SK · Cndair CL6002C10 · Trailing Edge Flaps
  > R/H WING O/B FLAP O/B HINGE ARM AFT FITTING (ON FLAP) FWD FAIRING MOUNT BRACKET LOOSE (C-CHECK RO 04/30/2025)ACCOMPLISHED REO NO 670-57-53-401 REV --. 2025-02-22. AT BLENDED CORROSION DAMAGE TO R/H WING I/B & O/B HIGNE FITTING HALF AT WS 264.00 (FOR WORK INPR
- [SDR SWI2025F00602](https://openairdocs.org/sdr/SWI2025F00602.md): Slat Track · worn · Dec 28, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT N0.3 O/B TRACK LOWER SURFACE WORN 7" ABOVE ECCENTRIC PIN. (C-CHECK RO 04/30/2025)PERFORMED ADJUSMENT AND RIGGING CHECK,CHECK GOOD NO DEFECT NOTED THIS TIME PER REO 670-57-42-2031 REV --- DATED: 2025-03-25 PERFORMED BLEND OUT ON R/H WING L/E
- [SDR SWI2025F00601](https://openairdocs.org/sdr/SWI2025F00601.md): Slat Track · damaged · Dec 28, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT N0.3 O/B TRACK I/B AND O/B SURFACES PITTED ALONG LENGTH OF TRACK. (C-CHECK RO 04/30/2025)PERFORMED ADJUSMENT AND RIGGING CHECK,CHECK GOOD NO DEFECT NOTED THIS TIME PER REO NUMBER 670-57-42-2031 REV-- PG 5 STEP 6-7.OPS CHECK GOOD NO
- [SDR SWIA202504301228](https://openairdocs.org/sdr/SWIA202504301228.md): Slat Track · worn · Dec 28, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT N0.3 CENTER TRACK UPPER AND LOWER SURFACES WORN (UPPER SURFACE WORN 1.5" & 5" ABOVE ECCENTRIC PIN) (LOWER SURFACE WORN 1.5",5.5" & 7.5" ABOVE ECCENTRIC PIN.) (C-CHECK RO 04/30/2025)-PERFORMED BLENDOUTS ON RH WING LE SLAT #3 CENTER TRACK UP
- [SDR SWI2025F00600](https://openairdocs.org/sdr/SWI2025F00600.md): Slat Track · worn · Dec 26, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT NO.1 CENTER TRACK LOWER SURFACE WORN 3", 13" & 14.5" ABOVE ECCENTRIC PIN AND UPPER SURFACE WORN 1" & 12" ABOVE UPPER STOP TAB (C-CHECK RO 04/30/2025)REWORK PERFORMED ON R/H WING L/E SLAT #1 SLAT TRACK 1-2 IS STRUCTUALLY & FUNCTIONALLY ACCEP
- [SDR SWI2025F00599](https://openairdocs.org/sdr/SWI2025F00599.md): Slat Track · worn · Dec 26, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT NO. 1 I/B TRACK LOWER SURFACE BORN 1.5", 11.75" & 14" ABOVE STOP FITTING AND UPPER SURFACE WORN 1" & 12" ABOVE UPPER STOP TAB (C-CHECK RO 04/30/2025)-PERFORMED BLENDOUT ON RH WING LE SLAT NO.1 I/B TRACK LOWER SURFACE IAW REO 670-57-42-1989RE
- [SDR SWI2025F00598](https://openairdocs.org/sdr/SWI2025F00598.md): Slat Track · worn · Dec 26, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT NO.2 O/B TRACK UPPER SURFACE WORN 2" & 9.5" ABOVE ECCENTRIC PIN (C-CHECK RO 04/30/2025)PERFORMED ADJUSTMENT AND RIGGING CHECK,CHECKED GOOD NO DEFECTS NOTED AT THIS TIME PER REO # 670-57-42-2016 REV -- PAGE 7 STEPS 6 & 7. OPS CHECK GOOD NO DE
- [SDR SWIA202504301226](https://openairdocs.org/sdr/SWIA202504301226.md): Slat Track · worn · Dec 26, 2024 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > R/H WING L/E SLAT NO.2 CENTER TRACK UPPER AND LOWER SURFACES WORN (UPPER SURFACE WORN 1" & 7" ABOVE UPPER STOP TAB) (LOWER SURFACE WORN 2.5", 8.5" & 11" ABOVE ECCENTRIC PIN) AND I/B AND O/B SURFACE WORN (I/B SURFACE WORN 7" ABOVE ECCENTRIC PIN) (O/B SURFACE W
- [SDR SWIA202504301223](https://openairdocs.org/sdr/SWIA202504301223.md): Vane · gouged · Dec 23, 2024 · N765SK · Cndair CL6002C10 · Trailing Edge Flaps
  > RH WING I/B FLAP FOUR FLAP VANE ACTUATOR ROLLER TRACKS (4EA) MULTIPLE AREA GOUGES, DAMAGED AS MARKED (C-CHECK RO 04/30/2025)R/H WING, INBD FLAP VANE ACTUATORS WITHIN LIMITS (4 EA) IAW MHIRJ REO 670-57-52-598 DATED: 2025-03-03. REWORKED AREAS REFINISHED PER SAM
- [SDR SWIA202157362](https://openairdocs.org/sdr/SWIA202157362.md): Skin · corroded · Mar 22, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS CORROSION JUST AFT OF FS985 BETWEEN STGR 26L-26R (C-CHECK RO 4/3/2021) BLENDED CORROSION ON EXTERNAL FUSELAGE SKIN AFT OF FS985 BETWEEN STGR 26L-26R REF CRJ700 SRM 51-21-06-001-001-A01. BLEND-OUT IS STRUCTURALLY ACCEPTABLE PER M
- [SDR SWIA202157377](https://openairdocs.org/sdr/SWIA202157377.md): Angle · corroded · Mar 21, 2021 · N765SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER SILL ATTACHING MID CAP ANGLE HAS CORROSION (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW REPLACEMENT PAX DOOR LOWER SILL MID CAP ANGLE (P/N SH670-31825-9S) WITH NEW HARDWARE, REF CRJ700 SRM 51-41-02-001-001 A01. OPERATIONAL TEST GOOD.
- [SDR SWIA202157361](https://openairdocs.org/sdr/SWIA202157361.md): Fitting · corroded · Mar 21, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > FWD CLOSING FITTING AT FS314.00 AND STGR18L CORRODED. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED CORRODED FWD CLOSING FITTING WITH NEW FITTING (P/N SH670-31840-3) AT FS314.00 AND STGR18L WITH NEW HARDWARE. REF BOMBARDIER DWG#SH670-31810 REV Y AND CRJ700
- [SDR SWIA202157360](https://openairdocs.org/sdr/SWIA202157360.md): Fitting · corroded · Mar 21, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > AFT CLOSING FITTING AT FS342.00 AND STGR18L CORRODED. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED CORRODED AFT CLOSING FITTING WITH NEW FITTING (P/N SH670-32475-3) AT FS342.00 AND STGR18L WITH NEW HARDWARE. REF BOMBARDIER DWG#SH670-31810 REV Y AND CRJ700
- [SDR SWIA202157359](https://openairdocs.org/sdr/SWIA202157359.md): Angle · corroded · Mar 21, 2021 · N765SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR LOWER SILL KICK ANGLE HAS CORROSION (C-CHECK RO 4/3/2021) REMOVED AND REPLACED CORRODED PAX DOOR LOWER SILL KICK ANGLE WITH NEW SERVICEABLE PART(P/N SH670-31875-7S) WITH ALL NEW HARDWARE, REF BOMBARDIER DWG# SH670-31810 REV Y AND CRJ700 SRM'S 51-
- [SDR SWIA202157376](https://openairdocs.org/sdr/SWIA202157376.md): Seat Track · corroded · Mar 14, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON FLOOR SEAT TRACK AT LBL9 BETWEEN APPROX FS379.00 AND FS485.00. (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW FLOOR SEAT TRACK ON LBL 9.0 BETWEEN APPROX FS379.00-FS485.00 SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL
- [SDR SWIA202157358](https://openairdocs.org/sdr/SWIA202157358.md): Stringer Clip · misaligned · Mar 14, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > WHILE REPLACING FS 333.0 UPPER FRAME SECTION, FOUND 7 EA EXISTING STRINGER CLEATS PN SH670-31249-1 MIS-ALIGHNED RIVET HOLES WITH NEW FRAME. FABRICATE 7 EA NEW CLEATS. (C-CHECK RO 4/3/2021) REMOVED AND REPLACED 7 EA STRINGER CLEATS PN SH670-31249-1 CO
- [SDR SWIA202157357](https://openairdocs.org/sdr/SWIA202157357.md): Hinge · chafed · Mar 14, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > PAX DOOR HINGE (DOOR SIDE) HAS CHAFES ON MULTIPLE LANDINGS. (C-CHECK RO 4/3/2021) REPAIRED PAX DOOR HINGE (DOOR SIDE) WITH IN LIMITS REF CRJ700 SRM 52-11-01-201-007-A01 REPAIR TYPE IV / COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY
- [SDR SWIA202157356](https://openairdocs.org/sdr/SWIA202157356.md): Skin · chafed · Mar 12, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL FUSELAGE SKIN HAS CHAFE APPROX. BET. FS977.00 AND FS985.00 AT STGR 27 (C-CHECK RO 4/3/2021) COMPLIED WITH REO 670-53-00-652 REV -- DATED 2021-03-30 REPAIR TO FUSELAGE SKIN FS953-985 STR26L-STR26R LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 5
- [SDR SWIA202157375](https://openairdocs.org/sdr/SWIA202157375.md): Torque Tube · corroded · Mar 8, 2021 · N765SK · Cndair CL6002C10 · Passenger/Crew Doors
  > * PASSENGER DOOR LOWER TORQUE TUBE STOP BOLT FITTING IS CORRODED (C-CHECK RO 4/3/2021) REMOVED CORRODED STOP FITTING AND INSTALLED NEW LOWER STOP FITTING REF CRJ700 SRM 51-42-06-001-001-A01.
- [SDR SWIA202157374](https://openairdocs.org/sdr/SWIA202157374.md): Torque Tube · corroded · Mar 8, 2021 · N765SK · Cndair CL6002C10 · Passenger/Crew Doors
  > * PASSENGER DOOR UPPER TORQUE TUBE STOP BOLT FITTING IS CORRODED (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW STOP BOLT FITTING ON PASSENGER DOOR UPPER TORQUE TUBE REF CRJ-700 SRM 51-42-06-001-001-A01
- [SDR SWIA202157355](https://openairdocs.org/sdr/SWIA202157355.md): Canister · cracked · Mar 8, 2021 · N765SK · Cndair CL6002C10 · Leading Edge Devices
  > LH WING SLAT CANNISTER 1-3 HAS CRACK IN BRACKET (MARKED) (C-CHECK RO 4/3/2021) COMPLIED WITH LH WING SLAT CANNISTER 1-3 REPAIRED PER REO 670-57-42-577 REV-- DATED: 2016-12-02, LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASKCARD 51-900-1002-SKY.
- [SDR SWIA202157354](https://openairdocs.org/sdr/SWIA202157354.md): Frame · cracked · Mar 8, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Frame
  > FRAME AT FS333 AT APPROXIMATELY STR1R HAS CRACK AT LIGHTENING HOLE (C-CHECK RO 4/3/2021) REMOVED AND REPLACED FRAME SECTION AT FS333 BETWEEN STR0.00-STR9R REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, AND DWG SH670-31950 REV. Y. LEAK CHECK GOOD.
- [SDR SWIA202157380](https://openairdocs.org/sdr/SWIA202157380.md): Track · gouged · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > * AFT CARGO DOOR, AFT TRACK GOUGED (C-CHECK RO 4/3/2021) REMOVED GOUGED AFT CARGO DOOR TRACK AND INSTALLED NEW AFT CARGO DOOR TRACK. REF CRJ 700 AMM 52-31-00-400-801-A01. SEE CONTINUATION CARD FOR DETAILS.
- [SDR SWIA202157379](https://openairdocs.org/sdr/SWIA202157379.md): Bracket · gouged · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > * BRACKET AT APPROXIMATELY FS1030 STGR5R IS GOUGED (C-CHECK RO 4/3/2021) REMOVED AND REPLACED DAMAGED BRACKET AT APPROXIMATELY FS1030 STGR5R, FOUND TO BE OUT OF LIMITS AFTER BLEND IAW CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202157378](https://openairdocs.org/sdr/SWIA202157378.md): Bracket · gouged · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > * BRACKET AT APPROXIMATELY FS1030 STGR2R IS GOUGED (C-CHECK RO 4/3/2021) REMOVED AND REPLACED DAMAGED BRACKET AT APPROXIMATELY FS1030 STGR2R, FOUND TO BE OUT OF LIMITS AFTER BLEND IAW CRJ700 SRM 51-42-21-001-001-A01
- [SDR SWIA202157373](https://openairdocs.org/sdr/SWIA202157373.md): Seat Track · corroded · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK FROM APPROX. FS581-FS693 RBL9 HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW SEAT TRACK, SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL IAW CRJ700 AMM 53-00-49-400-801-A17
- [SDR SWIA202157372](https://openairdocs.org/sdr/SWIA202157372.md): Seat Track · corroded · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK FROM APPROX. FS477-FS581 LBL9 HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW LBL 9 FLOOR SEAT TRACK FROM APPROX FS477-FS581 IAW CRJ700 AMM 53-00-49-400-801-A17
- [SDR SWIA202157371](https://openairdocs.org/sdr/SWIA202157371.md): Seat Track · corroded · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > FLOOR SEAT TRACK FROM APPROX. FS477-FS581 RBL9 HAS SEVERAL AREAS OF CORROSION (C-CHECK RO 4/3/2021) INSTALLED NEW FLOOR SEAT TRACK FROM APPROX. FS477-FS581 RBL9 REF CRJ700 AMM 53-00-49-400-801-A17
- [SDR SWIA202157363](https://openairdocs.org/sdr/SWIA202157363.md): Stop · cracked · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > * AFT CARGO DOOR, AFT TRACK UPPER STOP IS CRACKED/SPLIT (C-CHECK RO 4/3/2021) REMOVED AND REPLACED AFT CARGO DOOR, AFT TRACK UPPER STOP REF CRJ-700 AMM52-31-23-000-801-A01 AND 52-31-23-400-801-A01 TORQUE WRENCH USED TUC 8619 CAL DUE 31 OCT 2021
- [SDR SWIA202157353](https://openairdocs.org/sdr/SWIA202157353.md): Bracket · corroded · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > MACHINED BRACKET AT FS581 BETWEEN STR22L-STR23L HAS SEVERAL AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/3/2021) REPLACED MACHINED BRACKET PN SH670-33390-2 AT FS581 BETWEEN STR22LSTR23L PER CRJ700 SRMS 51-42-06-001-001-A01, 51-42-21-001-001-A01, AND 51-42
- [SDR SWIA202157352](https://openairdocs.org/sdr/SWIA202157352.md): Bracket · corroded · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > MACHINED BRACKET AT FS533 BETWEEN STR26L AND STR27 HAS SEVERAL AREAS OF CORROSION. (MARKED) (C-CHECK RO 4/3/2021) REMOVED CORROSION ON THE MACHINED BRACKET ATFS533 BETWEEN STR 26L AND 27 REF CRJ 700 SRM 700 51-21-06-001-001-A01. EVALUATED AND FOUND TO BE
- [SDR SWIA202157351](https://openairdocs.org/sdr/SWIA202157351.md): Hinge · chafed · Mar 7, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Door Hinge
  > * PASSENGER DOOR HINGE HALF ( FUSELAGE SIDE) HAS AFT HINGE LUG LAND CHAFED FROM CONTACT WITH ROLL PIN. (C-CHECK RO 4/3/2021) REPLACED PAX DOOR HINGE (FUSELAGE SIDE) REF CRJ700 SRM 53-21-23-201-007-A01 LEAK CHECK GOOD. COMPLIED WITH SKYWEST TASK CARD 51-9
- [SDR SWIA202157370](https://openairdocs.org/sdr/SWIA202157370.md): Seat Track · corroded · Mar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > RBL 9.0 FLOOR TRACK HAS AREAS OF LITE CORROSION FROM APPROX FS 349 TO APPROX FS477.0 (C-CHECK RO 4/3/2021) REMOVED AND REPLACED SEAT TRACK, SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL IAW CRJ700 AMM 53-00-49-400-801-A17
- [SDR SWIA202157369](https://openairdocs.org/sdr/SWIA202157369.md): Seat Track · corroded · Mar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage, Seat/Cargo Attach Fittings
  > LBL 27 FLOOR SEAT TRACK HAS ARES OF LIGHT CORROSION FROM APPROX FS 477.0 TO FS 349.0 (C-CHECK RO 4/3/2021) REMOVED AND REPLACED SEAT TRACK, SEAT TRACK FOUND TO BE OUT OF ALLOWABLE LIMITS AFTER CORROSION REMOVAL IAW CRJ700 AMM 53-00-49-400-801-A17
- [SDR SWIA202157350](https://openairdocs.org/sdr/SWIA202157350.md): Frame · corroded · Mar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage Main, Frame
  > *CORROSION ON AFT SURFACE OF FRAME FS 333.00 BETWEEN STGR 25L €“ 24L (C-CHECK RO 4/3/2021) REMOVED AND INSTALLED NEW FRAME SECTOR AND ALL FABRICATED REPAIR PARTS AT FS 333.00 FRAME REPAIR REF CRJ 700 SRM 53-00-06-201-006-A01, CRJ 700 SRM 51-42-06-001-00
- [SDR SWIA202157349](https://openairdocs.org/sdr/SWIA202157349.md): Intercostal · corroded · Mar 6, 2021 · N765SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > *CORROSION ON INTERCOSTAL BETWEEN FS 349.00 €“ 364.00, STGR 27 €“ 26L (C-CHECK RO 4/3/2021) REPLACED LATCH PIN INTERCOSTAL BETWEEN FS349-FS364 STR27-26L REF SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01 AND DWG SH670-32050 REV.J. LEAK TEST GOOD. CO

Next page: https://openairdocs.org/aircraft/N765SK/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 = 'N765SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N765SK/reports

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