# Service difficulty reports: JASC 5741

A list on [JASC 5741](https://openairdocs.org/jasc/5741.md).

Reports filed under 5741 · Wing, Fuselage Attach Fittings, newest first.

Page 1 of 11 · 544 reports

- [SDR IPXA2026052012545](https://openairdocs.org/sdr/IPXA2026052012545.md): Former · cracked · May 10, 2026 · N394UP · Boeing 767381
  > CRACKED FORMER, RT WING OUTBD FXD LE NOSE SKIN, OSS 456.98. INSTALL NEW FORMER I.A.W SRM 51-40-02-0G REV.55 AND BOEING DWG 114T2202 SH 1 REV D AND UPS SREO-57209-REQ001 REV2
- [SDR 2025FA0000771](https://openairdocs.org/sdr/2025FA0000771.md): Wing Root · corroded · Nov 19, 2025 · N313QS · Cessna 680CE
  > CORROSION FOUND WHERE LT AND RT WING AND FUSELAGE MEET.
- [SDR SWIA2025F01331](https://openairdocs.org/sdr/SWIA2025F01331.md): Attach Fitting · gouged · Aug 1, 2025 · N461SW · Cndair CL6002B19
  > L/H WING AFT ATTACHMENT FITTING AT WS220.0 HAS GOUGING ON THE I/B OF THE TWO CENTER LUGS. (MARKED) (S/N#00605) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON L/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS220.0 AT I/B CENTER LUG REF. CRJ2
- [SDR SWIA2025F01362](https://openairdocs.org/sdr/SWIA2025F01362.md): Attach Fitting · gouged · Aug 1, 2025 · N461SW · Cndair CL6002B19
  > L/H WING AFT ATTACHMENT FITTING AT WS178.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00604) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON L/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS178.0 AT I/B AND O/B CENTER LUGS REF. CRJ200 SR
- [SDR SWIA2025F01361](https://openairdocs.org/sdr/SWIA2025F01361.md): Attach Fitting · gouged · Aug 1, 2025 · N457SW · Cndair CL6002B19
  > L/H WING AFT ATTACHMENT FITTING AT WS264.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00603) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON L/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS264.0 AT I/B AND O/B CENTER LUGS. REF. CRJ200 S
- [SDR SWIA2025F01360](https://openairdocs.org/sdr/SWIA2025F01360.md): Attach Fitting · gouged · Aug 1, 2025 · N461SW · Cndair CL6002B19
  > R/H WING AFT ATTACHMENT FITTING AT WS220.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00601) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON R/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS220.0 AT I/B AND O/B CENTER LUGS REF. CRJ200 SR
- [SDR SWIA2025F01359](https://openairdocs.org/sdr/SWIA2025F01359.md): Attach Fitting · gouged · Aug 1, 2025 · N461SW · Cndair CL6002B19
  > R/H WING AFT ATTACHMENT FITTING AT WS178.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON R/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS178.0 AT I/B AND O/B CENTER LUGS REF. CRJ200 SRM 51-
- [SDR SWIA2025F01352](https://openairdocs.org/sdr/SWIA2025F01352.md): Attach Fitting · gouged · Aug 1, 2025 · N461SW · Cndair CL6002B19
  > R/H WING AFT ATTACHMENT FITTING AT WS264.0 HAS GOUGING ON THE CENTER TWO LUGS. (MARKED) (S/N#00602) (C-CHECK RO 09/24/2025)BLENDED-OUT DAMAGES TO SMOOTH CONTOUR ON R/H WING AFT ATTACHMENT FITTING FOR HINGE BOX WS264.0 AT I/B AND O/B CENTER LUGS. REF. CRJ200 S
- [SDR SWI2025F01533](https://openairdocs.org/sdr/SWI2025F01533.md): Slat Track · damaged · Jul 15, 2025 · N249LR · Cndair CL6002D24
  > RH SLAT TRACK 1-2 HAS AREAS WITH SIGNS OF PITTING ON UPPER AND LOWER SURFACES (C-CHECK RO 11/07/2025)REPAIRED DAMAGED RH SLAT TRACK 1-2 UPPER AND LOWER SURFACE IAW CRJ900 SRM 51-12-00 AND REO 690-57-42-1269 REV-- DATE 2025-07-28. NDT PERFORMED.
- [SDR SWIA20251110715](https://openairdocs.org/sdr/SWIA20251110715.md): Slat Track · damaged · Jul 15, 2025 · N249LR · Cndair CL6002D24
  > LH SLAT TRACK 2-2 HAS SIGNS OF PITTING ON LOWER SURFACE (C-CHECK RO 11/07/2025)PERFORMED REPAIR LWR SURFACE AT L:H SLAT TRACK 2-2, MATERIAL LOSS.004", FOUND WITHIN LIMITS IAW REO 690-57-42-1276 REV-- DATE: 2025-08-11, CRJ900 SRM 51-12-00, AMM 57-42-26, NDT
- [SDR SWI2025F01916](https://openairdocs.org/sdr/SWI2025F01916.md): Roller · out of limits · Jun 20, 2025 · N820SK · Cndair CL6002D24
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: TRACK ROLLER SLAT 2-2 900 LH - COMPLY WITH TASK CARD 27-530-809 LT TRACK ROLLER SEALED, TRACK 2-2, TOP FORWARD - SLAT 2. REMOVED AND REPLACED THE LT SLAT TRACK 2-2 UPPER FORWARD TRACK ROLLER IAW AMM 27-81-43-400-801-A01.
- [SDR JGVR202504007001](https://openairdocs.org/sdr/JGVR202504007001.md): Attach Fitting · chafed · Apr 7, 2025 · N305QS · Cessna 680CE
  > MECHANICALLY REMOVED CHAFFING MARKS ON RH MIDDLE WING ATTACHMENT FITTING, PERFORMED NDT, REPORTED FOR REPAIR DISPOSITION, CLEANED, TREATED, AND, PRIMED PER NETJETS REQUEST FOR TECHNICAL SERVICES REPORT.
- [SDR SWIA2025F00468](https://openairdocs.org/sdr/SWIA2025F00468.md): Roller · out of limits · Feb 19, 2025 · N710SK · Cndair CL6002C10
  > R/H SLAT TRACK 3-2 HAS 2 TRACK ROLLERS OUT OF LIMIT FLAT SPOTS. IB AND OB FWD ROLLERS. (C-CHECK RO 04/16/2025)REMOVED AND REPLACED BOTH I/B AND O/B FWD SIDE ROLLERS ON SLAT RECK 3-2 AS REQUIRED IAW CRJ 700 AMM 27-81-44-400-801-A01.
- [SDR SWIA202507220103](https://openairdocs.org/sdr/SWIA202507220103.md): Roller · out of date · Jan 2, 2025 · N825SK · Cndair CL6002D24
  > COMPLY WITH SCHEDULED MAINTENANCE CODE: SIDE ROLLER SLAT TRACK 2-2 900 RH - RH SIDE ROLLER ASSY 0.750 DIA. SLAT TRACK PN CC670-12027-3 (QTY 2) AND SIDE ROLLER ASSY 0.875 DIA. SLAT TRACK PN CC670-12048-3 (QTY 2) ARE DUE LIFE LIMIT. REMOVE AND DISCARD. REPLACE W
- [SDR SWIA2024102500004](https://openairdocs.org/sdr/SWIA2024102500004.md): Rib · chafed · Oct 24, 2024 · N929SW · Cndair CL6002B19
  > L/H INBOARD FLAP INBOARD CLOSING RIB AND INBOARD VANE ARE CHAFED. (FILED CLOSED)REMOVED AND REPLACED L/H INBOARD FLAP IAW AMM 27-54-01AND TASK 27-900-1006-SKY OPS CHECK GOOD AT THIS TIME.
- [SDR SWIA20240920037](https://openairdocs.org/sdr/SWIA20240920037.md): Slat Track · cracked · Aug 12, 2024 · N784SK · Cndair CL6002C10
  > SUSPECTED CRACK AT LH SLAT TRACK FUEL CANISTER 1-3 (C-CHECK RO 9/19/2024) PERFORMED REPAIR AT LH SLAT TRACK FUEL CANISTER 1-3 CRACKED BRACKET, REF REO 670-57-42-577 REV-- DATE: 2016-12-02. COMPLIED WITH TASK CARD 51-900-1002-SKY. ALL CHECK GOOD, LEA
- [SDR SWI2024F00719](https://openairdocs.org/sdr/SWI2024F00719.md): Slat Track · corroded · May 29, 2024 · N758SK · Cndair CL6002C10
  > R/H #1 SLAT MID SLAT TRACK HAS SEVERAL AREA'S OF PITTING CORROSION (S/N 00526) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 1-2 REF-CRJ-700 SRM 51-12-00-001-001 A01,REPAIRED REF REO 670-57-42-1598 REV -- DATE 2024-06-27, DWG CC670
- [SDR SWI2024F00718](https://openairdocs.org/sdr/SWI2024F00718.md): Slat Track · corroded · May 29, 2024 · N758SK · Cndair CL6002C10
  > R/H # 2 SLAT MID SLAT TRACK HAS PITTING CORROSION AND SEVERAL AREA'S OF WEAR (S/N 00521) (C-CHECK RO 8/22/2024) BLENDED PITTING FROM RH WING SLAT TRACK 2-2 REF. CRJ-700 SRM 51-12-00-001-001-A01, DWG CC670-12050 REV.-C, AND COMPLIED WITH REO 670-57-42-
- [SDR SWI202404290329](https://openairdocs.org/sdr/SWI202404290329.md): Slat Track · worn · Feb 29, 2024 · N752SK · Cndair CL6002C10
  > RIGHT WING LEADING EDGE SLAT TRACK ASSEMBLY NO. 3-3 HAS WARE MARKS, HN00142274 (C-CHECK RO 4/26/2024) REPAIRED RH WING SLAT TRACK ASSEBLY 3-3. PER REO 670-57-42-1495 REV -- DATED 2024-03-07 STEPS 1-8. ALL CHECKS GOOD. COMPLIED WITH TASK CARD 51-900
- [SDR IPXA2023110154296](https://openairdocs.org/sdr/IPXA2023110154296.md): Unknown · unknown · Nov 1, 2023 · N391UP · Boeing 767304
  > *SDR FILED OPEN* DURING WAI FOUND INSPECTIONPANEL, 2 FEET OUTBOARD OF RIGHT ENGINE, HINGES BROKEN BUT PANEL STILL ATTACHED. PANEL REMOVED AND PANEL DEFERRED IAW CDL 57-41-2.<BR>PLACKARD INSTALLED.
- [SDR SWI2023F00586](https://openairdocs.org/sdr/SWI2023F00586.md): Unknown · corroded · Oct 10, 2023 · N743SK · Cndair CL6002C10
  > * LH WING SLAT TRACK AT 1-1 POSITION HAS SPOTS OF CORROSION (MARKED). 27279750 (C-CHECK RO 12/23/2023) BLENDED CORROSION AT LH WING SLAT TRACK. RECIEVED REO 670-57-42-1451 REV. -- DATED 2023-11-01 AND COMPLIED WITH ALL STEPS. SEE CONTINUATION FOR DETAILS.B
- [SDR IPXA2023091871606](https://openairdocs.org/sdr/IPXA2023091871606.md): Unknown · unknown · Aug 29, 2023 · N433UP · Boeing 75724APF
  > **SDR FILED OPEN**FAULT RT WING L/E BETWEEN SLAT#9 AND SLAT#10 HAS CRACK SHOWING COMPOSITE DOT #47-06 VERIFIED TOPCOAT.
- [SDR SWIA202310060728](https://openairdocs.org/sdr/SWIA202310060728.md): Unknown · scratched · Jul 28, 2023 · N728SK · Cndair CL6002C10
  > L/H WING - INBD FLAP - FLAP VANE ACTUATORS #1 AND #2 HAVE SCRATCHED THE INNER FLAP SKIN TO BASE METAL (C-CHECK RO 10/4/2023) BLENDED AND RESTORED L/H WING INBOARD FLAP SKIN BY #1 AND #2 ACTUATORS IAW CRJ700 REO-670-57-52-352 REV-- DATE 2017-03-28 ALL STEPS
- [SDR SWIA2023082300706](https://openairdocs.org/sdr/SWIA2023082300706.md): Unknown · damaged · Jul 6, 2023 · N758SK · Cndair CL6002C10
  > RH LOWER AUX SPAR (PN CC670-10742-4) WAS FOUND TO BE DAMAGED AFTER REMOVING THE LOWER SKIN PANEL. (FILED OPEN)PERFORMED TEMPORARY REPAIR OF RH LOWER AUX SPAR FLANGE BETWEEN WS24.00 - WS34.00 IN REF TO REO 670-57-21-952, REV--, DATED 2023-07-15. COMPLIED WITH T
- [SDR SWI2023F00264](https://openairdocs.org/sdr/SWI2023F00264.md): Unknown · cracked · Jun 27, 2023 · N738SK · Cndair CL6002C10
  > RH WING SLAT CANISTER BRACKET 1-3 IN FUEL TANK CRACKED (C-CHECK RO 8/31/2023) COMPLIED WITH REPAIR OF RH WING SLAT 1-3 CANISTER BRACKET REF REO 670-57-42-577 REV -- DATED 2016-12-02 OPS CHECK GOOD LEAK CHECK GOOD. COMPILED WITH SKYWEST TASK CARD 51-900-
- [SDR SWI2023F00260](https://openairdocs.org/sdr/SWI2023F00260.md): Unknown · worn · Jun 27, 2023 · N738SK · Cndair CL6002C10
  > R/H SLAT TRACK 3-3 HAS NOTICABLE RUB AND WEAR MARKS WORN INTO SLAT TRACK BOTTOM SIDE (C-CHECK RO 8/31/2023) BLENDED WEAR MARKS ON RH 3-3 SLAT TRACK BOTTOM SIDE AT 4 LOCATIONS REF CRJ700 SRM 51-12-00-001-001-A01 AND COMPLIED WITH ALL STEPS OF DISPOSITION
- [SDR SWI2023F00258](https://openairdocs.org/sdr/SWI2023F00258.md): Unknown · worn · Jun 27, 2023 · N738SK · Cndair CL6002C10
  > L/H SLAT TRACK 3-3 HAS NOTICABLE RUB AND WEAR MARKS WORN INTO SLAT TRACK ON BTM SIDE (C-CHECK RO 8/31/2023) BLENDED WEAR MARKS ON LH 3-3 SLAT TRACK BOTTOM SIDE AT 2 LOCATIONS REF CRJ700 SRM 51-12-00-001-001-A01. COMPLIED WITH ALL STEPS OF DISPOSITION FO
- [SDR SWIA202306210007](https://openairdocs.org/sdr/SWIA202306210007.md): Unknown · cracked · May 26, 2023 · N870DC · Cndair CL6002C10
  > *SLAT CANISTER SUPPORT BRKT CRACKED UNDER FUEL PANEL #651AB (MARKED) (C-CHECK RO 6/19/2023) REPAIRED R/H SLAT TRACK 1-3, SLAT CANNISTER #3 SUPPORT BRACKET. REF. BOMBARDIER REO 670-57-42-577 REV. --, DATED 2016-12-02 AND MHIRJ REO 670-57-42-1418 REV--, D
- [SDR SWIA2023051700004](https://openairdocs.org/sdr/SWIA2023051700004.md): Unknown · delaminated · May 14, 2023 · N262SY · Emb ERJ170200LL
  > TRANSFER FROM EAML 1136127: CREATED FROM FORWARD DISCREPANCY. PLEASE REFERENCE AML 1135826. RH AFT INBOARD FLAP, LOWER SKIN ON LEADING EDGE APPROXIMATELY 1 ½€™ INBOARD ON RIB 4 HAS DELAMINATION DAMAGE MEASURING 2 5/8 INCHES BY 1 ¼ AND THROUGH DAMAGE 33MM
- [SDR ABXA2023041857](https://openairdocs.org/sdr/ABXA2023041857.md): Rib · gouged · Mar 9, 2023 · N763CK · Boeing 7673P6
  > WHILE IN C-CHECK AT KALITTA IN OSC. IT WAS FOUND THAT RIGHT WING LEADING EDGE BULL NOSE PANEL GOUGED AT APPROX LES 500.10, TD10. AFTER BLENDING IT WAS FOUND TO BE BEYOND ALLOWABLE LIMITS. ENGINEERING WAS CONTACTEDFOR A REPAIR. AN FAA-DER APPROVED AND REPAIR
- [SDR GTIA2023020136964](https://openairdocs.org/sdr/GTIA2023020136964.md): Bracket · cracked · Feb 9, 2023 · N605NK · Airbus A320232
  > CRACK BRACKET TELESCOPIC DUCT OUTBOARD OF FIXED LEADING EDGE ON LH WING RAF-01 3102849-02 GENERATED-PERFORMED PERMANENT REPAIR ON LH WING LE UPPER SKIN TELESCOPIC DUCK BRACKET OB RIB IAW E.A.# 57-0031-23 AND EC NO. EA 5741-2311. REPAIR CATEGORY "A" INSPECTION
- [SDR SWAA2023031300553](https://openairdocs.org/sdr/SWAA2023031300553.md): Panel · broken · Feb 8, 2023 · N277WN · Boeing 7377H4
  > RIGHT WING LEADING EDGE SERVICE PANEL 621GB HANDLE BROKEN<[01] REMOVED AND REPLACED RIGHT-WING LEADING-EDGE SERVICE PANEL 621GB AS PER AMM 52-49-21;[02] CORRECTION STEP 1: REMOVED AND REPLACED RIGHT-WING LEADING-EDGE SERVICE PANEL 621 GB DOOR HOLD OPEN ROD AS
- [SDR UIEA2022103101182](https://openairdocs.org/sdr/UIEA2022103101182.md): Strap · none · Oct 30, 2022 · N780BA · Boeing 747
  > CORROSION-STRAP, LH WING INBD FIXED LE CAVITY LOWER SKIN PNL SPLICE, ILES 380(<P>1) REMOVE DAMAGE PARTS I.A.W SRM 51-40-02, REV=52 2) FABRICATE PARTS I.A.W SRM 51-40-02, REV=52 2) FABRICATE PARTS I.A.W EI=T2022P57M-3119, REV=0. 3) INSTALL FABRICATE PARTS I.A.W
- [SDR SWAA2022102161711](https://openairdocs.org/sdr/SWAA2022102161711.md): Panel · delaminated · Oct 20, 2022 · N757LV · Boeing 7377H4
  > LEFT WING PANEL 521 YB OUTBOARD EDGE DELAMINATED. 2INCHES FROM LEADING EDGE. 1.5 INCH WIDE BY 3 INCH LONG / [01] ACCOMPLISHED TEMP REPAIR PER EA-GENERAL CLEANED; TAP TESTED;INSTALLED 2 LAYERS OF SPEED TAPE AND REINSTALLED PANEL.;[02] COMPLIED WITH EA; #TTG8Q00
- [SDR CALA2022100302600](https://openairdocs.org/sdr/CALA2022100302600.md): Panel · damaged · Oct 2, 2022 · N227UA · Boeing 777222
  > LEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511CB HAS THE FOLLOWING DISCREPANCIES: OUTER SIDE SCREW HOLES HAVE SOME COMPOSITE SHOWING NEAR HOLES( MARKED IN RED) INNER SIDE HAS NUMEROUS AREAS OF MISSING, PEELING, AND BLISTERED TAPE.
- [SDR CALA2022100302599](https://openairdocs.org/sdr/CALA2022100302599.md): Panel · damaged · Oct 2, 2022 · N227UA · Boeing 777222
  > LEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511AB HAS NUMEROUS AREAS OF BLISTERING, PEELING, AND MISSING ALUMINUM FOIL TAPE. UPDATED TO REFLECT MAJOR REPAIR STATUS. C/W RII INSPECTION FOR PERMANENT REPAIR TO THE BONDED ALUMINUM FO
- [SDR CALA2022100302598](https://openairdocs.org/sdr/CALA2022100302598.md): Panel · damaged · Oct 2, 2022 · N227UA · Boeing 777222
  > LEFT WING LEADING EDGE PANELS FOIL/MESH INSPECT {B777-20-3-7002} - PANEL 511EB HAS THE FOLLOWING DISCREPANCIES: INNER SIDE HAS NUMEROUS AREAS OF PEELING AND BLISTERING TAPE WITH SOME COMPOSITE MATERIAL SHOWING ALONG THE EDGE; OUTER SIDE HAS A SCREW HOLE SHOWIN
- [SDR CALA2022092302460](https://openairdocs.org/sdr/CALA2022092302460.md): None · none · Sep 21, 2022 · N796UA · Boeing 777
  > REF. LP 9580500, 9580486, 9580475, 9579508, 9579463, AND 9579452 WING LEADING EDGE PANELS REPAIRED HAVE NOT BEEN FLAGGED AS MAJOR REPAIR, RII ACCOMPLISHMENT RECORDED ON LOGPAGE 9583494. LOCKED FOR DISPOSITION. RII AND MAJOR REPAIR DOCUMENTED. SFOIQ PHIL DUMAS
- [SDR SWIA202266758](https://openairdocs.org/sdr/SWIA202266758.md): None · damaged · Sep 15, 2022 · N913EV · Cndair CL6002B19
  > DAMAGE HOLES ON PLUG FLAP END ATTACH RH I/B FLAP VANE SKIN AT PANEL 684MB (C-CHECK RO 11/8/2022) REMOVED AND REPLACED RH IB FLAP VANE END PLUG REF CRJ200 SRM 51-42-13 & DWG 601R14302 REV E. COMPLIED WITH 51-900-1003-SKY. SEE CONTINUATION CARD FOR WORK P
- [SDR SWIA202266757](https://openairdocs.org/sdr/SWIA202266757.md): None · chafed · Sep 15, 2022 · N913EV · Cndair CL6002B19
  > THE L-H WING INBD FLAP, THE OUTBD LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED WITH NEW LEADING EDGE VANE CAP REF CRJ200 SRM 51-42-13 AND DRAWING #601R14302 REV: E / COMPLIED WITH SKYWEST YASK CARD 51-900-1003-SKY (CL6
- [SDR SWIA202266756](https://openairdocs.org/sdr/SWIA202266756.md): None · chafed · Sep 15, 2022 · N913EV · Cndair CL6002B19
  > THE L-H WING INBD FLAP, THE MID LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED WITH NEW MID LEADING EDGE VANE CAP. P/N 601R14303-51 ON ON L-H WING INBD FLAP PER CRJ200. SRM 51-42-13 REV. 39 DATE MAR 10/21 AND DRAWING. 6
- [SDR SWIA202266755](https://openairdocs.org/sdr/SWIA202266755.md): None · chafed · Sep 15, 2022 · N913EV · Cndair CL6002B19
  > THE L-H WING INBD FLAP, THE INBD LEADING EDGE VANE CAP, HAS CHAFFING (C-CHECK RO 11/8/2022) REMOVED AND REPLACED LH IB FLAP, INBD LE VANE CAP WITH NEW, REF CRJ 200 SRM 51-42-13 AND DWG 601R14303 REV J. / COMPLIED WITH SKYWEST TASK CARD 51-900-1003-SKY
- [SDR CALA2022080801992](https://openairdocs.org/sdr/CALA2022080801992.md): Rivet · missing · Aug 7, 2022 · N16732 · Boeing 737
  > THIS IS A SUPPLEMENTAL REPORT FOR THE SAME CONTROL NUMBER SUBMITTED ON 8/08/22. PDA 3 RIGHT WING INBOARD FIXED LEADING EDGE HAS ONE RIVET BROKEN OFF AT OUTBOARD END NEAR PYLON. REMOVED FASTENER AND REPLACE WITH NEW FASTENER.
- [SDR SWAA2022082338534](https://openairdocs.org/sdr/SWAA2022082338534.md): Panel · delaminated · Aug 4, 2022 · N490WN · Boeing 7377H4
  > R/W FUELING PANEL 621GB HAS DELAMINATIONS TO INNER SURFACE (MARKED) / [01] IDENTIFIED PANEL IAW SRM 57-41-01-0I-4 FIG 1; DRAWING 116A8500 PL SHT 15; DRAWING 116A8520 & 116A8501; AND AIPC 57-40-00-51 ITEM 100. DAMAGE IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 5
- [SDR SWAA2022082637353](https://openairdocs.org/sdr/SWAA2022082637353.md): Panel · delaminated · Aug 1, 2022 · N560WN · Boeing 737790
  > R/W L/E PANEL 621CB HAS CORNER DELAMINATION ON CORNER (MARKED) / [01] IDENTIFIED PANEL IAW SRM 57-41-01-0I-4 TABLE 5; FIG.5; ITEM 3. CORNER EROSION DAMAGE TO L/E IS BEYOND ALLOWABLE DAMAGE LIMITS IAW SRM 57-41-01-1A-1 PARA 4.A(5)(C) DAMAGE TO BE REPAIRED IA
- [SDR U5OA_N960DP](https://openairdocs.org/sdr/U5OA_N960DP.md): None · corroded · Jun 1, 2022 · N960DP · Gulstm GIV
  > LH WING TO FUSELAGE AFT BL 33.187 CLOTHESPIN FITTING WAS FOUND TO HAVE CORROSION DURING INSPECTION REQUIRING EXTENSIVE SHEET METAL REPAIRS.
- [SDR A6WA202205108510](https://openairdocs.org/sdr/A6WA202205108510.md): Unknown · unknown · May 10, 2022 · N434AW · Cndair CL6002B19
  > RIGHT-WING LEADING-EDGE SHOWS SIGNS OF ROUGHNESS ********AIRCRAFT REMOVED FROM SERVICE********* RE-SKIN OTB SECTION OF RH WING OUTB LEADING EDGE AND INSTALLED 1 EA RIB AND 1 EA STRAP
- [SDR QXEA2022051000189](https://openairdocs.org/sdr/QXEA2022051000189.md): Panel · dented · May 10, 2022 · N644QX · Emb ERJ170200LR
  > 2 SMALL DENTS FOUND ON RIGHT WIND INBOARD LEADING EDGE SLAT. REMOVED FROM SERVICE. FOUND TWO DENTS ON THE RHIB SLAT LEADING EDGE THAT ARE 2.15" APART. OB DENT: 0.258 X 0.425" DEPTH 0.015" IB DENT: 0.235 X 0.91, DEPTH 0.02". DENTS ARE 28.5" INBOARD FROM THE OUT
- [SDR SWAA2022061401323](https://openairdocs.org/sdr/SWAA2022061401323.md): Slat · cracked · Apr 30, 2022 · N286WN · Boeing 7377H4
  > RT WING #7 SLAT LWR SURFACE HAS A SUSPECTED CRACK AT I/B AFT HILOCK SLAT STA 322. 8-10 / [01] PERFORMED HFEC AT SUSPECTED CRACK IAW NDTM PART 6; 51-00-00 PROCEDURE 23. CRACK CONFIRMED EMANATING FROM I/B FURTHEST AFT FASTENER. CRACK LENGTH: 0.118';[02] REMOVED
- [SDR SWIA202265997](https://openairdocs.org/sdr/SWIA202265997.md): None · dented · Apr 29, 2022 · N607SK · Cndair CL6002C10
  > LH INBD FLAP HAS 2EA DENTS ON BOTTOM INBD SIDE (C-CHECK RO 7/8/2022) L/H I/B FLAP LOWER I/B SKIN HAS BEEN REPAIRED REF CRJ 700 SRM 57-52-01-201-005-A01, FIG 57-52-01-995-801.C/W SKY CARD 51-900-1002-SKY

Next page: https://openairdocs.org/jasc/5741/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 jasc_code = '5741'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/jasc/5741/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.