# Service difficulty reports: N732SK

A list on [N732SK](https://openairdocs.org/aircraft/N732SK.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 · 190 reports

- [SDR SWIA2026031875949](https://openairdocs.org/sdr/SWIA2026031875949.md): Skin · damaged · Mar 18, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > UPON REMOVING FASTENERS ON RT SLAT NR 2 TRAILING EDGE, FOUND 1EA HOLE ELONGATED. REPAIRED 1 EA FASTENER IAW REO 670-57-42-2441 REV-.
- [SDR SWIA2026030775951](https://openairdocs.org/sdr/SWIA2026030775951.md): Angle · cracked · Mar 7, 2026 · N732SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CRACKED ANGLE AFT OF BS 280 AT LBL 9 OTBD. REMOVED CRACKED ANGLE, FABRICATED A NEW ANGLE AND INSTALLED IAW REO 670-53-11-579, REV B. MAJOR REPAIR.
- [SDR SWIA2026030775950](https://openairdocs.org/sdr/SWIA2026030775950.md): Angle · cracked · Mar 7, 2026 · N732SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > FOUND CRACKED ANGLE AFT OF BS 280, LBL.12. REPLACED CRACKED ANGLE WITH NEW IAW SRM 51-42-21-001-001-A01, DWG BA670-31057, REV L, AND DWG CC670-34010, REV K.. MAJOR REPAIR.
- [SDR SWIA2026030775916](https://openairdocs.org/sdr/SWIA2026030775916.md): Floorbeam · damaged · Mar 7, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > LEFT FLOORBEAM AT BS 280 SHOWS SIGNS OF EXFOLIATION. REMOVED AND INSTALLED A NEW FLOORBEAM IAW SRM 51-42-06-001-001-A01, DWG CC670-34010, REV K, AND DWG CC670-33052, REV G. COMPLIED WITH SKYWEST TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026030675917](https://openairdocs.org/sdr/SWIA2026030675917.md): Doubler · damaged · Mar 6, 2026 · N732SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > UPON REMOVAL DAMAGED AFT CARGO DOOR HANDLE ASSY, FOUNDED 10EA ELONGATED FASTENER HOLES ON INNER HANDLE DOUBLER. REPLACED INNER HANDLE DOUBLER ON AFT CARGO DOOR IAW SRM 51-42-06-001-001-A01 AND DWG CC670-38702 REV. -F. LEAK CHECK GOOD. COMPLIED WITH TASK CARD
- [SDR SWIA2026030575928](https://openairdocs.org/sdr/SWIA2026030575928.md): Bulkhead Web · damaged · Mar 5, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Bulkhead
  > LEFT BS 280 LOWER INBD WEB SHOWS SIGNS OF EXFOLIATION. REMOVED AND INSTALLED NEW FABRICATED REPAIR LT LOWER BULKHEAD WEB IAW SRM 53-11-10-201-004-A01. COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026030575918](https://openairdocs.org/sdr/SWIA2026030575918.md): Channel · corroded · Mar 5, 2026 · N732SK · Cndair CL6002C10 · Fuselage Miscellaneous Structure
  > CHANNEL ASSY BETWEEN BS 1031 - 1051.30, STR 26 - 27R CORRODED. REMOVED AND INSTALLED A NEW CHANNEL ASSY IAW SRM 51-42-06-001-001-A01 AND DWG MM670-43200, REV N. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECKS GOOD.
- [SDR SWIA2026030175929](https://openairdocs.org/sdr/SWIA2026030175929.md): Slat Track · worn · Mar 1, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-2 HAS WORN SPOT ON LOWER SIDE. LIGHTLY BLENDED LT SLAT TRACK 3-2 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2403 REV-.
- [SDR SWIA2026022875953](https://openairdocs.org/sdr/SWIA2026022875953.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1 HAS WORN SPOT ON UPPER SIDE. BLENDED WORN AT LH SLAT TRACK 1-1 ON UPPER SIDE IAW SRM 51-12-00-001-001-A01, FOUND TO BE OUT OF LIMITS IAW SRM 57-41-25-001-001-A01 AND REMOVED AND REPLACED LT SLAT TRACK 1-1 ON JOB HN00298053.
- [SDR SWIA2026022875952](https://openairdocs.org/sdr/SWIA2026022875952.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-1 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT LH SLAT TRACK 1-1 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01 FOUND TO BE OUT OF LIMITS IAW SRM 57-41-25-001-001-A01, AND REMOVED AND REPLACED LT SLAT TRACK 1-1 IAW AMM 27-81-41-400-801-A01 AND
- [SDR SWIA2026022875938](https://openairdocs.org/sdr/SWIA2026022875938.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 3-3 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT LT SLAT TRACK 3-3 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2405, REV -.
- [SDR SWIA2026022875937](https://openairdocs.org/sdr/SWIA2026022875937.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-1 HAS WORN SPOT ON LOWER SIDE. LIGHTLY BLENDED 2 EACH SPOTS ON LT SLAT TRACK 2-1 LOWER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2400 REV-.
- [SDR SWIA2026022875936](https://openairdocs.org/sdr/SWIA2026022875936.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS WORN SPOT ON INBD SIDE. BLENDED WORN AT LT SLAT TRACK 2-2 ON INBD SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2399, REV -. CHECKS GOOD.
- [SDR SWIA2026022875935](https://openairdocs.org/sdr/SWIA2026022875935.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 2-2 HAS WORN SPOT ON OTBD SIDE. BLENDED WORN AT LT SLAT TRACK 2-2 ON OTBD SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF REO 670-57-42-2399, REV -.
- [SDR SWIA2026022875934](https://openairdocs.org/sdr/SWIA2026022875934.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-2 HAS WORN SPOT ON OTBD SIDE. BLENDED WORN AREA OF RH SLAT TRACK 2-2 ON OUTBOARD FORWARD EDGE AND 3EA WORN AREAS ON AFT FACE OF RH SLAT TRACK 2-2 IAW SRM 51-12-00-001-001-A01. FOUND TO BE WITHIN LIMITS REF REO 670-57-42-2401, REV --, COMP
- [SDR SWIA2026022875933](https://openairdocs.org/sdr/SWIA2026022875933.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 1-1 HAS WORN SPOT ON LOWER SIDE. BLENDED 4 EACH SPOTS RH SLAT TRACK 1-1 LOWER SIDE IAW SRM 51-12-00-001-001-A01, COMPLIED WITH ALL STEPS OF REO 670-57-42-2383 REV-.
- [SDR SWIA2026022875932](https://openairdocs.org/sdr/SWIA2026022875932.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 2-3 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 2-3 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2384 REV-. CHECKED GOOD.
- [SDR SWIA2026022875931](https://openairdocs.org/sdr/SWIA2026022875931.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-2 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 3-2 ON LOWER SIDE IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2398, REV --,CHECKED GOOD.
- [SDR SWIA2026022875930](https://openairdocs.org/sdr/SWIA2026022875930.md): Slat Track · worn · Feb 28, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT SLAT TRACK 3-1 HAS WORN SPOT ON LOWER SIDE. BLENDED WORN AT RT SLAT TRACK 3-1 ON LOWER SIDE. IAW SRM 51-12-00-001-001-A01. PERFORMED REPAIRS IAW REO 670-57-42-2393, REV -A CHECKED GOOD.
- [SDR SWIA2026022775939](https://openairdocs.org/sdr/SWIA2026022775939.md): Shroud · chafed · Feb 27, 2026 · N732SK · Cndair CL6002C10 · Ailerons
  > RIGHT AILERON UPPER LEADING EDGE CHAFED. REMOVED AND REPLACED RT AILERON UPPER LEADING EDGE SKIN SHROUD WITH NEW SKIN SHROUD IAW SRM 51-42-06-001-001-A01, SRM 51-42-21-001-001-A01, SRM 51-42-22-001-001-A01 & DWG CC670-13000, REV D.
- [SDR SWIA2026022675948](https://openairdocs.org/sdr/SWIA2026022675948.md): Floorbeam · cracked · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Floor Beam
  > CRACKED BS 280 FLOORBEAM OTBD OF RBL 9. REPLACED CRACKED BRACKET AT ON THE FLOORBEAM WITH NEW IAW SRM 51-42-21-001-001-A01, DWG BA670-31057, REV L, AND DWG CC670-34010, REV K. MAJOR REPAIR.
- [SDR SWIA2026022675947](https://openairdocs.org/sdr/SWIA2026022675947.md): Fitting · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR FITTING CORRODED BETWEEN BS 280 - 295. RBL18. REPLACED CORRODED GALLEY FLOOR MOUNT FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.
- [SDR SWIA2026022675946](https://openairdocs.org/sdr/SWIA2026022675946.md): Fitting · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > GALLEY FLOOR FITTING CORRODED BETWEEN BS 280 - 295 APPROX. RBL36. REPLACED CORRODED GALLEY FLOOR FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.
- [SDR SWIA2026022675945](https://openairdocs.org/sdr/SWIA2026022675945.md): Skin · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > INTERNAL SKIN AFT OF BS 280 BETWEEN STR 19L - 20L CORRODED. REMOVED, FABRICATED NEW REPLACEMENT SEALING DOUBLER, AND INSTALLED THE NEW DOUBLER IAW DWG BA670-31051, REV NC, DWG BA670-31057, REV -L AND SRM 51-42-06-001-001-A01. CHECKED GOOD.
- [SDR SWIA2026022675944](https://openairdocs.org/sdr/SWIA2026022675944.md): Fitting · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Attach Fittings
  > ENTRANCE STORAGE FLOOR FITTING CORRODED AT FS310 LBL18. REPLACED ENTRANCE STORAGE FLOOR FITTING AT BS 310, LBL18 WITH NEW IAW SRM 51-42-21-001-001-A01, AND SH670-32120, REV D. MAJOR REPAIR.
- [SDR SWIA2026022675943](https://openairdocs.org/sdr/SWIA2026022675943.md): Fitting · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Passenger/Crew Doors
  > PAX DOOR FWD HANDRAIL CLOSING FITTING CORRODED. REMOVED AND INSTALLED NEW PAX DOOR FWD HANDRAIL CLOSING FITTING IAW SRM 51-42-06-001-001-A01, DWG SH670-31810, REV AE, AND DWG SH670-31840, REV A.
- [SDR SWIA2026022675942](https://openairdocs.org/sdr/SWIA2026022675942.md): Mount · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage, Equipment Attach Fittings
  > GALLEY FLOOR FITTING AT BS 382, RBL 36 CORRODED. REPLACED THE CORRODED GALLEY FLOOR MOUNT FITTING WITH NEW IAW SRM 51-42-21-001-001-A01, AND DWG SH670-32120, REV D. MAJOR REPAIR.
- [SDR SWIA2026022675941](https://openairdocs.org/sdr/SWIA2026022675941.md): Frame · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORROSION ON FRAME AT BS 310 BETWEEN STR 26L - 26R. PERFORMED SPLICE REPAIR AT BS 310 BETWEEN STR 26L TO 26R IAW SRM 53-00-06-201-006-A01. LEAK CHECK GOOD.
- [SDR SWIA2026022675940](https://openairdocs.org/sdr/SWIA2026022675940.md): Frame · corroded · Feb 26, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Frame
  > CORRODED FRAME AT BS 295 BETWEEN STR 26 - 27R. REPAIRED BS 295 LOWER FRAME SECTOR BETWEEN STR 25L TO 25R IAW SRM 53-00-06-201-006-A01. LEAK CHECKED GOOD.
- [SDR SWIA2026022475956](https://openairdocs.org/sdr/SWIA2026022475956.md): Roller · worn · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > FOR RIGHT SLAT TRACK 3-2 ROLLERS FOUND WORN. INSTALLED FOUR RIGHT SLAT TRACK 3-2 ROLLERS IAW AMM 27-81-44-400-803-A01. GAP CHECK GOOD, RETRACTION TEST GOOD.
- [SDR SWIA2026022475955](https://openairdocs.org/sdr/SWIA2026022475955.md): Roller · worn · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > (4 EACH) RIGHT HAND SLAT TRACK 2-2 ROLLERS FOUND WORN. INSTALLED (4 EACH) RIGHT HAND SLAT TRACK 2-2 ROLLERS REF AMM 27-81-44-400-802-A01. GAP CHECK GOOD, RETRACTION TEST GOOD.
- [SDR SWIA2026022475954](https://openairdocs.org/sdr/SWIA2026022475954.md): Roller · worn · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > LEFT SLAT TRACK 1-2 ALL SIDE ROLLERS WORN. INSTALLED FOUR LT SLAT TRACK 1-2 ROLLERS IAW AMM 27-81-44-400-801-A01. GAP AND EXTENSION CHECKS GOOD.
- [SDR SWIA2026022475927](https://openairdocs.org/sdr/SWIA2026022475927.md): Doubler · chafed · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Aerodynamic Fairings
  > DOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL & 196DR JUST AFT OF FS985 BETWEEN BL5L & BL4R IS CHAFED. REPAIRED DOUBLER UNDER TRAILING EDGE OF FUSELAGE TO WING FAIRINGS 195DL AND 196DR JUST AFT OF FS985 BETWEEN BL5L AND BL4R REF REO 670-53-00
- [SDR SWIA2026022475926](https://openairdocs.org/sdr/SWIA2026022475926.md): Skin · chafed · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Fuselage Main, Plate/Skin
  > EXTERNAL SKIN REPAIR CHAFED FS975 BL0. REPAIRED CHAFED DAMAGE ON EXTERNAL SKIN PREVIOUS REPAIR COVER PLATE AT FS 975 & BL 00 IAW REO 670-53-00-815 REV -. DIMENSION OF BLEND: L=1.500" W=1.115" THICKNESS FOUND= 0.043".COMPLIED WITH SKY CARD 51-900-1002-SKY S
- [SDR SWIA2026022475925](https://openairdocs.org/sdr/SWIA2026022475925.md): Stand Off · cracked · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust Reverser
  > LH LWR TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED CRACKED INBD -A- BRACKET STANDOFF FROM LT LOWER TRANSCOWL, LOCATED, DRILLED AND DEBURRED NEW INBD -A- BRACKET STANDOFF, INSTALLED THE NEW INBD -A- BRACKET STANDOFF ON LT LOWER TRANSCOWL AND MAR
- [SDR SWIA2026022475924](https://openairdocs.org/sdr/SWIA2026022475924.md): Bracket · cracked · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RIGHT LOWER TRANSCOWL INBD -A- BRACKET STANDOFF IS CRACKED. REMOVED AND REPLACED INBD STAND-OFF ANGLE ON RT LOWER TRANSCOWL, IAW REO 670-54-21-971, REV. B. SKY CARD 51-900-1002-SKY.
- [SDR SWIA2026022475923](https://openairdocs.org/sdr/SWIA2026022475923.md): Bracket · loose · Feb 24, 2026 · N732SK · Cndair CL6002C10 · Engine Thrust Reverser
  > RIGHT UPPER TRANSCOWL INBD A BRACKET HAS LOOSE SPINNING FASTENER ( WORN "A" BRACKET HOLE) INSTALLED A NEW RT UPPER TRANSCOWL INBD A BRACKET REF REO 670-564-21-971, REV -B, COMPLIED WITH TASK CARD 51-900-1002-SKY.
- [SDR SWIA2026021975919](https://openairdocs.org/sdr/SWIA2026021975919.md): Skin · gouged · Feb 19, 2026 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > RIGHT WING LEADING EDGE, NR 2 SLAT, CENTER UPPER AFT IS GOUGED, REMOVED DAMAGE ON THE RT SLAT NR 2 LEADING EDGE AFT UPPER SIDE IAW SRM 51-12-00-001-001-A01. COMPLIED WITH STEPS OF REO 670-57-42-2441 REV-- FOR TRIM/BLENDED AREAS. COMPLIED WITH SKYWEST TASK CAR
- [SDR SWIA2026021775920](https://openairdocs.org/sdr/SWIA2026021775920.md): Door · chafed · Feb 17, 2026 · N732SK · Cndair CL6002C10 · Cargo/Baggage Doors
  > AFT CARGO DOOR CHAFED AND GOUGED IN MULTIPLE LOCATIONS AROUND OUTER HANDLE HOUSING. REMOVED AND INSTALLED NEW AFT CARGO DOOR HANDLE ASSY IAW SRM 51-42-21-001-001-A01 AND DWG CC670-38702 REV. -F. LEAK CHECK AND OPS TESTED GOOD. COMPLIED WITH TASK CARD 51-900-1
- [SDR SWIA2025111375922](https://openairdocs.org/sdr/SWIA2025111375922.md): Skin · gouged · Nov 13, 2025 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH PERMANENT REPAIR ON RA ID: 94134RH SLAT NR 1, TWO AREAS OF GOUGE DAMAGE BETWEEN SS58.75 - TRACK 1-1 DATUM, AND BETWEEN SS 142.25 - SS 155.25. COMPLIED WITH TEMP REPAIR IAW REO 670-57-42-1734 REV A. PERFORM PERMANENT REPAIR BEFORE 3250 FLT HRS IAW
- [SDR SWIA2025111375921](https://openairdocs.org/sdr/SWIA2025111375921.md): Skin · damaged · Nov 13, 2025 · N732SK · Cndair CL6002C10 · Leading Edge Devices
  > COMPLY WITH PERMANENT REPAIR ON RA ID: 94135 RT SLAT NR 2 HAS NEW DAMAGE OF A BLENDED REPAIR ON THE TRAILING EDGE SKIN 48 INCHES FROM THE INBOARD EDGE OF THE SLAT. TEMPORARY REPAIR OF RT SLAT NR 2 COMPLIED WITH PER REO 670-57-42-1742 REV A, ON LOWER EDGE SURF
- [SDR SWIA20241113](https://openairdocs.org/sdr/SWIA20241113.md): Pylon · damaged · Nov 13, 2024 · N732SK · Cndair CL6002C10 · Nacelle/Pylon, Plate/Skin
  > SKIN UNDER NUTPLATE FOR THE DETACHABLE TRAILING EDGE ASSY ON THE LH PYLON IS DAMAGED (FILED CLOSED) REPAIRED LANDING FOR THE DETACHABLE TRAILING EDGE ASSY ON THE LH PYLON IAW REO 670-54-51-077, REV. -- DATED 11/13/24
- [SDR SWIA20240722](https://openairdocs.org/sdr/SWIA20240722.md): Bolt · worn · Jul 22, 2024 · N732SK · Cndair CL6002C10 · Engine Mount Section
  > RIGHT ENGINE BACKUP THRUST LINK MOUNT BOLT IS WORN BEYOND SERVICABLE LIMITS (FILED - CLOSED)REMOVED AND REPLACED RIGHT ENGINE BACKUP THRUST LINK MOUNT BOLT IN REFERENCE TO GE CF34-8C ESM 71-20-00- ASSEMBLYTORQUE WRENCH SN 5060772342 DUE 12/2024
- [SDR SWI20240606000486](https://openairdocs.org/sdr/SWI20240606000486.md): Window · warning message · Jun 5, 2024 · N732SK · Cndair CL6002C10 · Windshield/Door Rain/Ice Removal
  > TRANSFER FROM EAML 1362735: L WINDOW HEAT CAUTION CAME ON A FEW MINUTES AFTER SELECTING LOW ON THE WINDOW HEAT SWITCH (FLIGHT 4829 FILED CLOSED)REMOVED AND REPLACED LEFT WINDOW IN REF TO CRJ 700 AMM 56-12-01.TORQUE WRENCH 642260CAL DATE 2/6/2024CAL DUE
- [SDR SWIA202266726](https://openairdocs.org/sdr/SWIA202266726.md): None · cracked · Nov 1, 2022 · N732SK · Cndair CL6002C10 · Window/Windshield System
  > LEFT PILOT WINDOW SHIELD CRACKED (FLIGHT 3090 - FILED CLOSED) REMOVED AND REPLACED LT WINDSHIELD PER TASK CARD 56-220-100-SKY AND CRJ700 AMM 56-11-01. OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA202266480](https://openairdocs.org/sdr/SWIA202266480.md): None · damaged · Sep 14, 2022 · N732SK · Cndair CL6002C10 · Wing Structure
  > ON PUSHBACK TUG PUSHED AIRCRAFT LEFT WING TIP INTO CART: DAMAGE TO THE LT WINGLET L/E SKIN, WINGLET T/E WEDGE, WINGLET LOWER FILLET FAIRING AND WINGLET OUTBD SKIN DUE TO IMPACT WITH THE CART / * THIS HAS BEEN DETERMINED TO BE A MAJOR REPAIR, FORM M-337 IS R
- [SDR SWIA202266460](https://openairdocs.org/sdr/SWIA202266460.md): None · damaged · Sep 13, 2022 · N732SK · Cndair CL6002C10 · Wing Structure
  > FOUND DAMAGE TO THE LT WINGLET L/E SKIN (DWG CC670-15350 REF), WINGLET T/E WEDGE (DWG CC670-15309 REF), WINGLET LOWER FILLET FAIRING (DWG CC670-15305 REF), AND WINGLET OUTBD SKIN (DWG CC670-15114 REF), LHS, DUE TO IMPACT WITH THE CART. 1 SCRATCH:. 006€? MAX
- [SDR SWIA202264959](https://openairdocs.org/sdr/SWIA202264959.md): None · corroded · Feb 9, 2022 · N732SK · Cndair CL600* · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON LBL9.0 FLOOR BEAM CAP BETWEEN FS1025 AND FS1035. (C-CHECK RO 3/11/2022) REMOVED AND REPLACED CORRODED FLOOR BEAM SECTION WITH NEW FABRICATED FLOOR BEAM SECTION AT LBL9.0 BETWEEN FS1025.00 AND FS1035.00 WITH ALL NEW HARDWARE PER CRJ700
- [SDR SWIA202264957](https://openairdocs.org/sdr/SWIA202264957.md): None · corroded · Feb 9, 2022 · N732SK · Cndair CL6002C10 · Fuselage Internal Mounting Structure
  > CORROSION FOUND ON RBL9.0 FLOOR BEAM CAP BETWEEN FS1025 AND FS1035. (C-CHECK RO 3/11/2022) REMOVED AND REPLACED CORRODED FLOOR BEAM SECTION WITH NEW FABRICATED FLOOR BEAM SECTION AT RBL9.0 BETWEEN FS1025.00 AND FS1035.00 WITH ALL NEW HARDWARE PER CRJ700
- [SDR SWIA202264952](https://openairdocs.org/sdr/SWIA202264952.md): None · corroded · Feb 9, 2022 · N732SK · Cndair CL6002C10 · Fuselage Main, Keel
  > CORROSION FOUND ON STRINGER 26R BETWEEN FS1015 AND FS1031 (C-CHECK RO 3/11/2022) REMOVED DAMAGED AREA AND INSTALLED REPAIR ON STGR26R BETWEEN FS1015.00 AND FS1051.00 REF CRJ700 SRM 53-00-03-201-001-A01 FIGURE 53-00-03-991-805. NO NDT DEFECTS NOTED. REST

Next page: https://openairdocs.org/aircraft/N732SK/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 = 'N732SK' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N732SK/reports

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