# Service difficulty reports: N566WN

A list on [N566WN](https://openairdocs.org/aircraft/N566WN.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 · 237 reports

- [SDR SWAA2026082118837](https://openairdocs.org/sdr/SWAA2026082118837.md): Cover · detached · Aug 17, 2026 · N566WN · Boeing 7377CT · Emergency Lighting
  > EXIT ROW LIGHT COVER DETACHED. SECURED AS REQUIRED IAW SIP.
- [SDR SWAA2026050895813](https://openairdocs.org/sdr/SWAA2026050895813.md): Lens · damaged · May 6, 2026 · N566WN · Boeing 7377CT · Emergency Lighting
  > PASSENGER CABIN SEAT ROW 1DEF PHOTOLUMINESCENT STRIP HAS MOISTURE UNDER LENS. R&R CABIN PHOTO LUMINESCENT STRIP PER AMM 33-51-15
- [SDR SWAA2026041790067](https://openairdocs.org/sdr/SWAA2026041790067.md): Battery Pack · inoperative · Apr 16, 2026 · N566WN · Boeing 7377CT · Emergency Lighting
  > LEFT OVERWING EXIT EMERGENCY LIGHTS ARE INOPERATIVE. REMOVED AND REPLACED LT OVERWING EXIT EMERGENCY LIGHTS BATTERY PACK IAW AMM 33-51-06. OP CHECKS GOOD IAW AMM 33-51-06.
- [SDR SWAA2025040220605](https://openairdocs.org/sdr/SWAA2025040220605.md): Seat · loose · Apr 2, 2025 · N566WN · Boeing 7377CT · Passenger Compartment Equipment
  > PASSENGER SEAT LOOSE IN TRACK AT 12DEF.<[01] RESECURED SEAT ROW 12DEF IN FLOOR TRACK REF AMM 25-22-00
- [SDR SWAA2025030699109](https://openairdocs.org/sdr/SWAA2025030699109.md): Scuff Plate · cracked · Feb 24, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > FCB FWD SCUFF PLATE CRACKED<[01] REPLACED FCB FWD SCUFF PLATE PER SRM 51-10-02-0G-0; LOCATED AND DRILLED AND COUNTERSUNK PER SRM 51-40-02-0G-0; SRM 51-40-08-0G-0; REF IPC 53-13-00-08.;[02] INSTALLED ON BAR CODE TTG8Q00YP6R7;[03] VERIFIED CORRECTIVE ACTION ITEM
- [SDR SWAA2025031098253](https://openairdocs.org/sdr/SWAA2025031098253.md): Panel · cracked · Feb 21, 2025 · N566WN · Boeing 7377CT · Fuselage Main, Plate/Skin
  > FSD FWD SURROUND PANEL IS CRACKED AT THE OUTLET CUTOUT<[01]. REPAIRED FSD FWD SURROUND PANEL CRACK AT OUTLET CUTOUT IAW CMM 25-00-66 REPAIR 1-1 SECTION 4.B.; REPAIR 2-1 SECTION 4.B; AND ENG. DWG 25200003 PG. 11 ITEM 1.12.
- [SDR SWAA2025031097012](https://openairdocs.org/sdr/SWAA2025031097012.md): Angle · cracked · Feb 18, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > DURING OPEN HOLE HFEC; 1 EA HOLE CRACKED; TITANIUM ANGLE UPPER FLANGE; BS 663; LBL 36; MARKED.<[01] REPAIRED CRACKED HOLE BY REAMING HOLE TO FIRST OVERSIZE PER SRM 53-40-51-2R-2 PARAGRAPH 2. J. AND SRM 51-10-02-0G-0 STEP 11. B. NDI ACCOMPLISHED PER 737 NDTM PA
- [SDR SWAA2025031096409](https://openairdocs.org/sdr/SWAA2025031096409.md): Vapor Barrier · cracked · Feb 15, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > R/H BS 663 LOWER VAPOR BARRIER CRACKED RBL 53 WL 159 <[01]. APPLIED INTERIM REPAIR AT THE LOWER VAPOR BARRIER RBL 53 BS663 WL 159 IAW SRM 57-10-10-2R-2; [02] VERIFIED ALL STEPS CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2025030695755](https://openairdocs.org/sdr/SWAA2025030695755.md): Floor Panel · pulled · Feb 14, 2025 · N566WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 231XF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 231XF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025030695757](https://openairdocs.org/sdr/SWAA2025030695757.md): Floor Panel · pulled · Feb 14, 2025 · N566WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 241AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 241AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025030695759](https://openairdocs.org/sdr/SWAA2025030695759.md): Floor Panel · pulled · Feb 14, 2025 · N566WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 241DF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 241DF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025030695760](https://openairdocs.org/sdr/SWAA2025030695760.md): Floor Panel · pulled · Feb 14, 2025 · N566WN · Boeing 7377CT · Fuselage Floor Panel
  > FLOOR PANEL 242AF UPPER SKIN HAS AREAS OF PULLED STRANDS.<[01] DAMAGE FOUND TO BE OUT OF ECONOMICAL REPAIR; FABRICATED NEW 242AF FLOOR PANEL IAW SRM 53-00-50-2R-0.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025030696150](https://openairdocs.org/sdr/SWAA2025030696150.md): Seat Track · corroded · Feb 14, 2025 · N566WN · Boeing 7377CT · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON PAX CABIN SEAT TRACK BS372 LBL25 WL208. MARKED<[01] REMOVED CORROSION FROM CABIN SEAT TRACK BS372 LBL25 WL208.<BR>WELL: L= 7' W:.90' D:.030' CROWN: L=4'W:.45' D:.025'<BR>FOUND SEAT TRACK OUT LIMITS PER SRM 53-00--52-1A-1 PAR. 4 A. (2) FIG. 103
- [SDR SWAA2025030696222](https://openairdocs.org/sdr/SWAA2025030696222.md): Panel · cracked · Feb 14, 2025 · N566WN · Boeing 7377CT · Wing, Plate/Skin
  > R/W T/E PANEL 651FB HAS A CRACKED L-CLIP ON FWD SIDE 27' FROM O/B END<[01] REMOVED CRACKED L-CLIP AND REPLACED WITH NEW IAW SRM 51-40-02-0G-0 AND DWG 115A2710 REV. B.;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025031095754](https://openairdocs.org/sdr/SWAA2025031095754.md): Panel · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Fuselage Floor Panel
  > PANEL BREAK CRACKED AT HARDWARE - BS 540; RBL 47 AND RBL 63. <[01] REMOVED AND REPLACED PANEL BREAK AT BS 540; RBL 47 AND RBL 63 PER SRM 51-40-02-0G-0 AND DWG 143A5240 REV: -; [02] JOB COMPLETE.
- [SDR SWAA2025031095752](https://openairdocs.org/sdr/SWAA2025031095752.md): Web · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK IN MAIN CABIN ABOVE MLG WHEEL WELL - BS 663; LBL 35; WL 196. <[01] THIS CARD WILL BE ATTENDED ON CUSTOMER CARD TTG8Q00YPFZ9; [02] VERIFIED. CARD COMPLETE.
- [SDR SWAA2025030695751](https://openairdocs.org/sdr/SWAA2025030695751.md): Stiffener · corroded · Feb 13, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION NEAR FASTENER; BS 697; RBL 67; WL 203.5.<[01] CORROSION NEAR FASTENER; BS 697; RBL 67; WL 203.5 REPAIRED PER 25-153-00436-WIP1;[02] VERIFIED CORRECTIVE ACTION. CARD COMPLETE.
- [SDR SWAA2025030695750](https://openairdocs.org/sdr/SWAA2025030695750.md): Skin · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.9; 17' FROM FWD EDGE; 0.5' IN LENGTH (MARKED)<[01] DUPLICATE WRITE UP. ALL WORK TO BE PERFORMED ON FAULT TTG8Q00YQ0L1;[02] VERIFIED. CARD COMPLETE.
- [SDR SWAA2025030695749](https://openairdocs.org/sdr/SWAA2025030695749.md): Skin · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Horizontal Stabilizer, Plate/Skin
  > CRACK ON LH LOWER HORIZONTAL STABILIZER SKIN. AT STAB STA 193.90; 17' FROM FWD EDGE; 0.5' IN LENGTH (MARKED)<[01] REPAIRED L/H HORIZONTAL STABILIZER LOWER SKIN IAW SRM 51-40-02-0G-0 AND SRM 55-10-01-2R-11; REPAIR 11; FIG. 204; DETAIL B AND TABLE 202.;[02] VERI
- [SDR SWAA2025030695375](https://openairdocs.org/sdr/SWAA2025030695375.md): Pressure Deck · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK IN LH HORIZ PRESSURE DECK BS 665 LBL 34 WL 202;.790' LONG. MARKED ENDS.<[01] REMOVED THE DAMAGE WEB; CUT AND REMOVED THE DAMAGED PART OF THE WEB PER SRM 53-40-51-2R-2 PAR. 4. C. (1)(2)(3)(B) FIG. 203. <BR><BR>INSTALLED L/H PRESSURE DECK BS663- BS773; L
- [SDR SWAA2025030695743](https://openairdocs.org/sdr/SWAA2025030695743.md): Scuff Plate · cracked · Feb 13, 2025 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > AFT CARGO FWD CORNER SCUFF PLATE CRACKED<[01] REPAIRED AFT CARGO FWD CORNER SCUFF PLATE PER SRM 53-60-15-2R-1 PARA 4.B.(2); SOPM 20-30-02; SOPM 20-43-03; AMM 51-21-72-370-804.;[02] VERIFIED CORRECTIVE ACTION STEP 1.
- [SDR SWAA2025031095371](https://openairdocs.org/sdr/SWAA2025031095371.md): Bulkhead · cracked · Feb 12, 2025 · N566WN · Boeing 7377CT · Fuselage Main, Keel
  > B.S. 663 LOWER COMPOSITE BULKHEAD IS CRACKED AT L.B.L. 19; W.L. 152. <[01] APPLIED INTERIM REPAIR AT THE LOWER VAPOR BARRIER LBL 19 BS663 WL 152 IAW SRM 57-10-10-2R-2; [02] VERIFIED ALL STEPS CORRECTION ACTION ITEM 1 MEASUREMENT FIELD COMPLETE; CARD COMPLETE.
- [SDR SWAA2025030695365](https://openairdocs.org/sdr/SWAA2025030695365.md): Angle · cracked · Feb 12, 2025 · N566WN · Boeing 7377CT · Fuselage Main, Bulkhead
  > B.S. 663 LOWER COMPOSITE BULKHEAD UPPER ATTACH ANGLE IS CRACKED AT R.B.L. 45; W.L. 167.<[01] UPDATED STEPS 1-3;[02] REMOVED AND REPLACED BS 663 R/H LOWER COMPOSITE BULKHEAD UPPER ANGLE IAW SRM 51-40-02 AND DWG 111A1000 REV:;[03] VERIFIED COMPLETION CORRECTIVE
- [SDR SWAA2024111859296](https://openairdocs.org/sdr/SWAA2024111859296.md): Vapor Barrier · cracked · Nov 13, 2024 · N566WN · Boeing 7377CT · Fuselage Main, Bulkhead
  > L/H CENTER WING SECTION VAPOR BARRIER IS CRACKED APPROXIMATELY 2.5 INCHES LONG 3 INCHES O/B OF KEEL BEAM<[01] PERFORMED LH CENTER WING VAPOR BARRIER REPAIR REF SRM 57-10-10.
- [SDR SWAA2024102852674](https://openairdocs.org/sdr/SWAA2024102852674.md): Unknown · odor · Oct 24, 2024 · N566WN · Boeing 7377CT · Air Distribution System
  > FLIGHT ATTENDANT REPORTED ELECTRICAL BURNING SMELL; NOT IN GALLEY; ROW 22; NO SMOKE; DISTINCT. TURNED RECIRC FAN ON; DISSIPATED. POST FLIGHT CHECK STILL HAD LINGERING ODOR. TALKED TO THE FLIGHT ATTENDANT BURNING SMELL WAS PRETTY BAD PASSENGERS WERE RINGING TH
- [SDR SWAA2024082628422](https://openairdocs.org/sdr/SWAA2024082628422.md): Cover · misinstalled · Aug 21, 2024 · N566WN · Boeing 7377CT · Emergency Lighting
  > R/H OVER WING EXIT; EMERGENCY EXIT ARROW ON LIGHT POINTING WRONG DIRECTION<[01] REMOVED AND REPLACED R/H OVERWING EXIT LENS COVER WITH CORRECT ORIENTATED LENS REF M/M 33-51-03
- [SDR SWAA2024021651671](https://openairdocs.org/sdr/SWAA2024021651671.md): Bracket · cracked · Feb 13, 2024 · N566WN · Boeing 7377CT · Leading Edge Devices
  > LEFT WING #2 SLAT INBOARD AUX TRACK SKIN TAB BRACKET CRACKED<[01] R&R LEFT WING #2 SLATE INBOARD AUX TRACK SKIN TAB BRACKET PER AMM 20-50-11.
- [SDR SWAA2024021551661](https://openairdocs.org/sdr/SWAA2024021551661.md): Battery Pack · no test · Feb 13, 2024 · N566WN · Boeing 7377CT · Emergency Lighting
  > EMX BATT PACK M01675 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01675 PER AMM 33-51-06
- [SDR SWAA2024021551660](https://openairdocs.org/sdr/SWAA2024021551660.md): Battery Pack · no test · Feb 13, 2024 · N566WN · Boeing 7377CT · Emergency Lighting
  > EMX BATT PACK M01672 FAILS CAPACITANCE CHECK<[01] REMOVED AND REPLACED EMX BATT PACK M01672 PER AMM 33-51-06
- [SDR SWAA2023091399008](https://openairdocs.org/sdr/SWAA2023091399008.md): Sign · missing · Sep 11, 2023 · N566WN · Boeing 7377CT · Emergency Lighting
  > EXIT SIGN ABOVE REAR SERVICE DOOR MISSING<[01] REPLACED AFT L/H SERVICE DOOR EMERGENCY EXIT SIGN OPS CHECK GOOD AMM 3-51-01
- [SDR SWAA2023050242760](https://openairdocs.org/sdr/SWAA2023050242760.md): Megaphone · broken · Apr 28, 2023 · N566WN · Boeing 7377CT · Emergency Equipment
  > AFT MEGAPHONE HANDLE BROKE OFF<[01] R&R MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2023031617047](https://openairdocs.org/sdr/SWAA2023031617047.md): Girt Bar · out of adjust · Mar 15, 2023 · N566WN · Boeing 7377CT · Escape Slide
  > PAX CABIN LH FWD ENTRY DOOR SLIDE GIFT BAR DOES NOT FIT CORRECTLY ON GIFT BAR FITTING 2023-106436<[01] INSTALLED CORRECTLY PAX CABIN LH FWD ENTRY DOOR SLIDE GIFT BAR GIRT BAR FITTING IAW B737-700 AMM 25-66-02-400-801 STEP 3.E. TEST IS OK;[02] TASK CARD COMPLET
- [SDR SWAA2023032012431](https://openairdocs.org/sdr/SWAA2023032012431.md): Web · cracked · Mar 4, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Plate/Skin
  > CRACK WEB LOCATE BETWEEN BS500B TO BS500C AT LEVEL STR26L 2023-106381<[01] REPLACED NEW WEB LOCATED BETWEEN BS500B TO BS500C AT LEVEL STR26L IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG 143A7505 SHEET 5 REV B. PART USED 143A7510-11 P.O: 2022 216488 SEE INDIVIDUAL
- [SDR SWAA2023031711749](https://openairdocs.org/sdr/SWAA2023031711749.md): Channel · cracked · Mar 2, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK CHANNEL LOCATED BETWEEN BS188 TO BS203.8 RBL 3.5 FWD NOSE COMPARTMENT 2023-106380<[01] TOOL USED TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE: 25-JAN-24.;[02] REPLACED CHANNEL LOCATED BETWEEN BS188 TO BS203.8 RBL 3.5 FWD NOSE COMP
- [SDR SWAA2023032009530](https://openairdocs.org/sdr/SWAA2023032009530.md): Bracket · cracked · Feb 23, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK BRACKET LOCATED BS259.5 TO BS277 AT LEVEL STR 8 AT PASSENGER CABIN 2023- 106360<[01] TOOL USED: TEMPERATURE CONTROLLER: P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED BRACKET AND FASTENERS LOCATED BS259.5 TO BS277 AT LEVEL STR 8 AT PASSE
- [SDR SWAA2023032009531](https://openairdocs.org/sdr/SWAA2023032009531.md): Bracket · cracked · Feb 23, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK BRACKET LOCATED BS259.5 TO 277 AT LEVEL STR 10L AT PASSENGER CABIN 2023-106361<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: 48VFL11; S/N: AE-31448; DUE DATE: 14-JUN-23.;[02] REPLACED BRACKET LOCATED BS259.5 TO 277 AT LEVEL STR 10L AT PASSENGER CABIN IAW B
- [SDR SWAA2023032002014](https://openairdocs.org/sdr/SWAA2023032002014.md): Frame · cracked · Feb 11, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK FRAME 259.5 AT LEVEL STR8L AT PASSENGER CABIN 2023-106328<[01] TOOL USED EDDY CURRENT INSTRUMENT P/N NORTEC500D S/N N500X12101V022235 DUE DATE 03-AUG-2023.;[02] REPAIRED FRAME ON BS259.5 AT LEVEL STR8L AT PASSENGER CABIN I.A.W. EA 23-153-00632 AND EA 23-
- [SDR SWAA2023032002013](https://openairdocs.org/sdr/SWAA2023032002013.md): Plate · cracked · Feb 11, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK PLATE LOCATED BS907 TO BS927 AT LEVEL STR26R TO STR27R AT AFT CARGO COMPARTMENT 2023-106327<[01] REPLACED PLATE LOCATED BS907 TO BS927 AT LEVEL STR26R TO STR27R AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 AND DWG 147A7221 SHEET: 1
- [SDR SWAA2023032002012](https://openairdocs.org/sdr/SWAA2023032002012.md): Support Angle · cracked · Feb 11, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS 947 AT LEVEL STR25L AT AFT CARGO COMPARTMENT 2023-106325<[01] REPLACED SUPPORT ANGLE LOCATED BS 947 AT LEVEL STR25L AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9;[02] CORRECTIVE STEP 1 <BR>REPLACED SUPPORT ANGLE LOCAT
- [SDR SWAA2023032001651](https://openairdocs.org/sdr/SWAA2023032001651.md): Panel · cracked · Feb 10, 2023 · N566WN · Boeing 7377CT · Leading Edge Devices
  > CRACK ACCESS PANEL 623GB LOCATED SLAT 6 AT RT WING 2023-106320<[01] TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 01-FEB-24.;[02] TOOL USED: PO
- [SDR SWAA2023031701650](https://openairdocs.org/sdr/SWAA2023031701650.md): Frame · cracked · Feb 10, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Frame
  > CRACK FRAME 787 BETWEEN S-8R AND S-9R WL 270 AT PASSENGER CABIN 2023-106322<[01] REPAIR FRAME 787 BETWEEN S-8R AND S-9R WL 270 AT PASSENGER CABIN IAW EA 1-A53-12114.;[02] CORRECTED STEP 1:<BR>PERFORMED REPAIR ON FRAME 787 BETWEEN S-8R AND S-9R WL 270 AT PASSEN
- [SDR SWAA2023032001191](https://openairdocs.org/sdr/SWAA2023032001191.md): Support Angle · elongated · Feb 9, 2023 · N566WN · Boeing 7377CT · Fuselage Internal Mounting Structure
  > ELONGATED HOLE FLOOR STRUCTURE SUPPORT ANGLE LOC BTW BS 847 TO BS 867 AND BTW LBL 24.5 TO LBL 12.5AT AFT CARGO COMPARTMENT 2023-106303<[01] REPLACED SUPPORT ANGLE LOC BTW BS 847 TO BS 867 AND BTW LBL 24.5 TO LBL 12.5AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51
- [SDR SWAA2023032001189](https://openairdocs.org/sdr/SWAA2023032001189.md): Frame · cracked · Feb 9, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Structure
  > CRACK FRAME ON BS 312 BTW STR 5L TO 6L FWD GALLEY AND LAV 2023-106300<[01] REPAIRED LOCATED FRAME ON BS 312 BTW STR 5L TO 6L FWD GALLEY AND LAV IAW B737-700 EA NO:M-22-153-01244 REV: B.<BR>SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPAIRED LOCATED FRAME ON BS 312 BTW
- [SDR SWAA2023032001192](https://openairdocs.org/sdr/SWAA2023032001192.md): Support · corroded · Feb 9, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LBL 24.9 WL 152.7 BTW BS 747 TO BS 807AT AFT CARGO COMPARTMENT 2023-106311<[01] REPAIRED SUPPORT ZEE LOCATED BETWEEN 747 TO BS 807 AND LBL21; WL156 AFT CARGO COMPARTMENT IAW B737-700 SRM 53-00-53-2R-6 REPAIR 6; SEE INDIVIDUAL SIGN OFFS BE
- [SDR SWAA2023032001193](https://openairdocs.org/sdr/SWAA2023032001193.md): Angle · corroded · Feb 9, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION ANGLE-SUPPORT RBL 24 BTW BS 767 TO BS 787; WL 152.7 AT AFT CARGO COMPARTMENT 2023-106314<[01] REPLACED ANGLE-SUPPORT LOC RBL 24 BTW BS 767 TO BS 787; WL 152.7 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #146A8123 SHEET 16 REV -.
- [SDR SWAA2023032000605](https://openairdocs.org/sdr/SWAA2023032000605.md): Web · corroded · Feb 8, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BS492 TO BS500A RBL21.80 AND WL156 AT FWD CARGO COMPARTMENT 2023-106291<[01] REPLACED NEW WEB LOCATED BS492 TO BS500A RBL21.80 AND WL156 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 AND SRM 51-40-02 PART USED: 143A8126U3
- [SDR SWAA2023032000604](https://openairdocs.org/sdr/SWAA2023032000604.md): Angle · cracked · Feb 8, 2023 · N566WN · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK FRONT SPAR ANGLE LOC FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT RT WING 2023-106290<[01] REPLACED ANGLE ON FRONT SPAR LOC FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT RT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #112A2004 SHEET 5 REV AND DW
- [SDR SWAA2023032000603](https://openairdocs.org/sdr/SWAA2023032000603.md): Angle · cracked · Feb 8, 2023 · N566WN · Boeing 7377CT · Wing Miscellaneous Structure
  > CRACK ANGLE FRONT SPAR WEB LOC FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT LT WING 2023-106289<[01] REPLACED ANGLE FRONT SPAR WEB LOC FUEL BOOST PUMP IFSS 120 APPROX AND WBL 94.24 AT LT WING IAW B737-700 SRM 51-10-02 ITEM 9 AND DWG #112A2004 SHEET 5 REV -
- [SDR SWAA2023032000175](https://openairdocs.org/sdr/SWAA2023032000175.md): Support Angle · corroded · Feb 7, 2023 · N566WN · Boeing 7377CT · Fuselage Miscellaneous Structure
  > CORROSION ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR25L TO STR26L AND WL156 FWD CARGO COMPARTMENT 2023-106272<[01] TOOL USED: ULTRASONIC EQUIPMENT; P/N: 45MG; S/N: 130063701; DUE DATE: 16 JUN 23.;[02] REPLACED ANGLE - SUPPORT LOCATED BS500D AT LEVEL STR25L TO
- [SDR SWAA2023031699660](https://openairdocs.org/sdr/SWAA2023031699660.md): Stringer · cracked · Feb 7, 2023 · N566WN · Boeing 7377CT · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 25R AT LEVEL BS540 AT FWD CARGO COMPARTMEN 2023-106199<[01] UT TOOL USED PN: 45MG; SN: 221859911. DUE DATE: 07-NOV-23;[02] TOOLS USED: TEMPERATURE CONTROLLER: P/N: P3015GOES00000; S/N: 112031023; DUE DATE: 01-FEB-24; TEMPERATURE CONTROLLER: P/N

Next page: https://openairdocs.org/aircraft/N566WN/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 = 'N566WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N566WN/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.