# Service difficulty reports: N490WN, cancelled Oct 29, 2024

A list on [N490WN, cancelled Oct 29, 2024](https://openairdocs.org/deregistered/N490WN-2024-10-29.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 6 · 294 reports

- [SDR SWAA2024031463130](https://openairdocs.org/sdr/SWAA2024031463130.md): Cable · loose · Mar 14, 2024 · N490WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT RECLINE BUTTON LOOSE SEAT 10A (EXIT ROW)<[01] RESECURED RECLINE CABLE AT 10A SEAT REF CMM 25-21-42
- [SDR SWAA2023121129398](https://openairdocs.org/sdr/SWAA2023121129398.md): Battery Pack · inoperative · Dec 8, 2023 · N490WN · Boeing 7377H4 · Emergency Lighting
  > LEFT SIDE (CAPTAINS SIDE) ROW 1 AND 4 BIN EMERGENCY AISLE EXIT LIGHTS DO NOT ILL LEFT SIDE (CAPTAINS SIDE) ROW 1 AND 4 BIN EMERGENCY AISLE EXIT LIGHTS DO NOT ILLUMINATE<[01] REMOVED AND REPLACED FWD GALLEY LEFT SIDE BATTERY PACK IAW AMM 33-51-06; EMERGENCY LIG
- [SDR SWAA2023111622153](https://openairdocs.org/sdr/SWAA2023111622153.md): Slide · out of limits · Nov 15, 2023 · N490WN · Boeing 7377H4 · Emergency Equipment
  > AFT SERVICE DOOR SLIDE NOT IN GREEN<[01] REMOVED + REPLACED AFT SERVICE SLIDE PACK IAW M/M 25-66-01 + MT#725-61-06-AS
- [SDR SWAA2022103166170](https://openairdocs.org/sdr/SWAA2022103166170.md): Fuse · inoperative · Oct 29, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION; RECONNECTED SIGN. OPS CHECK GOOD REF MM
- [SDR SWAA2022103166430](https://openairdocs.org/sdr/SWAA2022103166430.md): Battery Pack · inoperative · Oct 29, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION; RECONNECTED SIGN. OPS CHECK GOOD REF MM
- [SDR SWAA2022103166431](https://openairdocs.org/sdr/SWAA2022103166431.md): Charger · inoperative · Oct 29, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > R OVERWING EXIT EMERGENCY LIGHTS INOP / [01] REMOVED AND REPLACED POWER SUPPLY FUSES; BATTERY PACK AND BATTERY CHARGER ASSY PER AMM 33-51-06 NO HELP.;[02] DISCONNECTED R OVER WING EMERGENCY EXIT SIGN; CLEANED CORROSION; RECONNECTED SIGN. OPS CHECK GOOD REF MM
- [SDR SWAA2022082242405](https://openairdocs.org/sdr/SWAA2022082242405.md): Light · inoperative · Aug 17, 2022 · N490WN · Boeing 7377H4 · Emergency Equipment
  > RH EXIT DOOR UPPER AND LOWER AFT EMERGENCY LIGHTS INOP / [01] REPLACED DAMAGED FUSE ON BATTERY CHARGER M1669 AND PERFORMED GOOD TEST PER AMM 33-51-06-690-804.<BR>-COMPLETED STEP 1.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.<BR>VERIFIED STEP 1.
- [SDR SWAA2022082242019](https://openairdocs.org/sdr/SWAA2022082242019.md): Battery Pack · inoperative · Aug 15, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ASSOCIATED WITH BATTERY PACK M1673 ARE INOP / [01] REPLACED EMERGENCY EXIT LIGHTS BATTERY PACK M1673 AND PERFORMED GOOD TEST PER AMM 33-51-06-960-805.;[02] VERIFIED ITEM 1 CORRECTIVE ACTIONS.
- [SDR SWAA2022082339225](https://openairdocs.org/sdr/SWAA2022082339225.md): Floor Panel · damaged · Aug 6, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241ABF HAS 3 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE=R/H SIDE; AFT INBOARD AFT 3 HOLES / REMOVED DAMAGE FROM UPPER SURFACE MEASURING 13'X3' APPLIED BMS5-28 TY19 LOT#AK2DP3091K POTTING COMPOUND TO (3EA) FASTENER HOLE
- [SDR SWAA2022082239226](https://openairdocs.org/sdr/SWAA2022082239226.md): Floor Panel · out of position · Aug 6, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AAF HAS 1 EACH INSERT THAT DOES NOT ALIGN WITH HOLE IN STRUCTURE=L/H SIDE; AFT OUTBOARD CORNER HOLE / [01] IDENTIFIED FLOOR PANEL 241AAF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6. FLOOR PANEL PROVIDED FROM STOCK WAS BAD. TH
- [SDR SWAA2022082239227](https://openairdocs.org/sdr/SWAA2022082239227.md): Floor Panel · misaligned · Aug 6, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > DUE TO REPAIR OF BS 986 FLOORBEAM; AT SPLICE LOCATION;PASSENGER CABIN FLOOR PANEL 242VF HAS 2 EACH INSERTS THAT DOES NOT ALIGN WITH HOLES IN STRUCTURE= FWD EDGE OF PANEL-MARKED / [01] IDENTIFIED PANEL 242VF IAW SRM 53-00-50-0I-1 FIGURE 6 TABLE 6<BR><BR>DAMAGED
- [SDR SWAA2022082338534](https://openairdocs.org/sdr/SWAA2022082338534.md): Panel · delaminated · Aug 4, 2022 · N490WN · Boeing 7377H4 · Wing, Fuselage Attach Fittings
  > 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 SWAA2022082241966](https://openairdocs.org/sdr/SWAA2022082241966.md): Wire · broken · Jul 31, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN WIRE AT AFT PASSENGER CABIN BS947+5 S-2R. MARKED. / [01] REPAIRED WIRE W3058-0147-22 WITH SPLICE IAW SWPM 20-10-13 AND SWPM 20-30-12; AS WELL AS WDM 23-42-11. TOOLING: ID: ATS1543 DUE: 10/2022;[02] PERFORMED GOOD CONTINUITY CHECK OF W3058-0147-22 IAW WD
- [SDR SWAA2022082236518](https://openairdocs.org/sdr/SWAA2022082236518.md): Baffle · cracked · Jul 30, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD CARGO BAY L/H BAFFLE UNDER FLOOR TO SIDEWALL SUPPORT AT BS 460-480 LBL 23 IS CRACKED / [01] VERIFIED APPLICABILITY FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT;PER SRM 51-10-02 PARA#9.;[02] REMOVED FWD CARGO BAY L/H BAFFLE UNDE
- [SDR SWAA2022082335082](https://openairdocs.org/sdr/SWAA2022082335082.md): Floor Panel · damaged · Jul 26, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 242UF HAS 2 RIPPED OUT INSERTS ALONG THE AFT EDGE. (MARKED) / OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4B REMOVED DAMAGE TO 2 FACESHEETS AND CORE AT 2EA INSERT HOLES ON AFT EDGE OF PANEL AND CLEANED REPAIR AREA. FABRICATE
- [SDR SWAA2022082333626](https://openairdocs.org/sdr/SWAA2022082333626.md): Web · cracked · Jul 26, 2022 · N490WN · Boeing 7377H4 · Trailing Edge Flaps
  > RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB IS CRACKED / [01] FOUND NO APPLICABLE SRM REPAIR FOR CRACKED RT WING T/E SEAL WEB TO DEFLECTION CONTROL RIB ANGLE; THEREFORE REPAIRED BY REPLACEMENT PER SRM 51-10-02-0G-0 PARAGRAPH 9. REMOVED AND REPLACED CRACKED
- [SDR SWAA2022082235080](https://openairdocs.org/sdr/SWAA2022082235080.md): Access Panel · corroded · Jul 26, 2022 · N490WN · Boeing 7377H4 · Service Doors
  > AFT ENTRY DOOR LOWER HINGE ACCESS PANEL 834DZ HAS CORROSION AT INNER SURFACE LOWER EDGE; 9' FROM AFT EDGE. / [01] RECEIVED NEW AFT ENTRY DOOR LOWER HINGE ACCESS PANEL 834DZ; TO BE INSTALLED ON TASK CARD TTG8Q00CULFB;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03]
- [SDR SWAA2022082233362](https://openairdocs.org/sdr/SWAA2022082233362.md): Battery Pack · inoperative · Jul 24, 2022 · N490WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT BATTERY CHARGER AT M1669 WON'T CHARGE BATTERY / [01] REPLACED EMERGENCY EXIT BATTERY CHARGER AT M1669 PER AMM 33-51-06-960-806; STEP 5.E.(4).;[02] VERIFIED CORRECTIVE ACTION ITEM 1.;[03] COMPLETED STEP 1.;[04] VERIFIED STEP 1 COMPLETE.
- [SDR SWAA2022082332989](https://openairdocs.org/sdr/SWAA2022082332989.md): Web · corroded · Jul 23, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT AFT CARGO BAY BS807+4 RBL20. / [01] CORRECTED STEPS 1 & 2.;[02] REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 807+4 RBL 20 IAW SRM 51-10-02 MEASURES: L=1' W=1' <BR><BR> REQUIRES NDT FOR REMAINING THICKNESS;[03] UT INSPECTED BLENDED AREA IAW
- [SDR SWAA2022082332992](https://openairdocs.org/sdr/SWAA2022082332992.md): Web · corroded · Jul 23, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT AFT CARGO BAY BS787+11 RBL20. / REMOVED CORROSION ON WEB AT AFT CARGO BAY BS 787+11 RBL 20 IAW SRM 51-10-02 MEASURES: L= 10' W= 3' REQUIRES NDT FOR REMAINING THICKNESS;[03] UT INSPECTED BLENDED AREA IAW 737 NDTM PART 4 51-00-00 PROCEDURE
- [SDR SWAA2022082332672](https://openairdocs.org/sdr/SWAA2022082332672.md): Floorbeam · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT AFT CABIN BS986 RBL40 - RBL43. / CUT AND REMOVED THE DAMAGED FLANGES OF THE UPPER CHORD OF THE FLOOR BEAM FROM L/H END TO R/H END IAW SRM 53-70-51-2R-4 REPAIR 4 STEP 4B; INSTALLED BACR15CE8AD DOUBLE FLUSH RIVET TO PLUG THE INITIAL TOO
- [SDR SWAA2022082332678](https://openairdocs.org/sdr/SWAA2022082332678.md): Sidewall Support · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY LBL23 BS400 - BS500D. / [01] REMOVED CORROSION ON FWD CARGO BAY FLOOR TO SIDEWALL SUPPORT AT LBL 23 WL 156 BS 400 DIMENSIONS L=1' W= 0.750 DEPTH:0.010' IAW SRM 51-10-02 PARAGRAPH 15; EVALUATED REWORKED A
- [SDR SWAA2022082332679](https://openairdocs.org/sdr/SWAA2022082332679.md): Sidewall Support · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23. / [01] REMOVED SIDEWALL SUPPORT AT FWD CARGO BAY BS400 - BS420 RBL23 IAW 51-40-02;[02] REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT CARGO BAY BS400-BS420 RBL 23 AT DISCREPANCY AR
- [SDR SWAA2022082231824](https://openairdocs.org/sdr/SWAA2022082231824.md): Floor Panel · cracked · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > AFT CABIN FLOOR PANEL 241ADF AFT O/B CORNER IS CRACKED. / [01] IDENTIFIED FLOOR PANEL 241ADF IAW SRM 53-00-50-0I-1 TABLE 6 FIG 6DAMAGED NOTED IS OUT OF ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARA 4 DAMAGE TO BE REPAIRED IAW SRM 53-00-50-2R-6 REMOVED ALL
- [SDR SWAA2022082232662](https://openairdocs.org/sdr/SWAA2022082232662.md): Channel · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT R/H MOPSILL HAS CORROSION BS 957-986; RBL 47-50; WL 208 / [01] REMOVED CORROSION ON PASSENGER CABIN MOP SEAL AT RBL 47-50 BS 957- BS 986 W.L 208.1 P/N 147A8540-8;AREA OT=0.080;RT=0.068;L=30.000'W=1.200'';X=0.012;FOUND TO BE OUT LIMITS I.A.W SRM 53-70-15-
- [SDR SWAA2022082232663](https://openairdocs.org/sdr/SWAA2022082232663.md): Channel · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT L/H MOPSILL HAS CORROSION BS 947-996; LBL 45-50; WL 208 / [01] REMOVED CORROSION ON AFT SERVICE DOOR MOP SILL AT B.S. 947-996 LBL45-50 W.L 208.1 P/N 147A8540-7;AREA OT=0.080;RT=0.068;L=26.700'W=1.700'';X=0.012 WITH DEPTH GAGE ID:ATS2678<BR>S/N:UNKNOWN<B
- [SDR SWAA2022082232670](https://openairdocs.org/sdr/SWAA2022082232670.md): Floorbeam · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986 FLOORBEAM LBL 44; WL 208 / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOORBEAM BS 986 LBL 44; WL 208 IN AREA OF 1' X 1'X 0.110' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE IN LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C<BR>TOOLS
- [SDR SWAA2022082232671](https://openairdocs.org/sdr/SWAA2022082232671.md): Floorbeam · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON BS 986 FLOORBEAM; RBL 35; WL 208 / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOORBEAM BS 986 RBL 35; WL 208 IN AREA OF 1.5' X 1'X 0.09' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE IN LIMIT IAW SRM 53-70-51-1A-1 DET. 4H; FIG 103-C TOOLS
- [SDR SWAA2022082232675](https://openairdocs.org/sdr/SWAA2022082232675.md): Gusset · cracked · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FWD CARGO BAY AFT BULKHEAD SUPPORT GUSSET IS CRACKED BS500D S-19L WL193. MARKED / [01] PRIOR TO REMOVAL;FOUND PART TO HAVE NO SRM LIMITS AND SO PART IS REPAIRABLE BY REPLACEMENT PER SRM 51-10-02 STEP#9. REMOVED GUSSET CRACKED AT BS500D;STR 19L;WL 193 AT FWD C
- [SDR SWAA2022082232680](https://openairdocs.org/sdr/SWAA2022082232680.md): Attach Angle · cracked · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CRACKED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. / [01] REMOVED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155 IAW SRM 51-40-02;[02] LOCATED AND DRILLED INTERCOSTAL ATTACH ANGLE AT FWD CARGO BAY BS400 LBL25 WL155. IAW SRM 51-40
- [SDR SWAA2022082232681](https://openairdocs.org/sdr/SWAA2022082232681.md): Floor Support · elongated · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > FCB FLOOR SUPPORT HAS ELONGATED FASTENER HOLE BS492 RBL17 WL156. / [01] VERIFIED APPLICABILITY NO ALLOWABLE DAMAGE FOR THIS PART TO BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02 PARA#9;[02] REMOVED FCB FLOOR SUPPORT HAS ELONGATED FASTENER HOLE BS492 RBL17 WL156.
- [SDR SWAA2022082232673](https://openairdocs.org/sdr/SWAA2022082232673.md): Floorbeam · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT AFT CABIN BS986 RBL5; LBL5. MARKED. / [01] REMOVED CORROSION FROM PASSENGER CABIN FLOOR BEAM BS 986 RBL 5; WL 208 IN AREA OF 1' X 1' X 0.08' DEEP ORIGINAL MATERIAL THICKNESS 0.150' FOUND TO BE OUT OF LIMIT IAW SRM 53-70-51-1A-1 DET. 4
- [SDR SWAA2022082232666](https://openairdocs.org/sdr/SWAA2022082232666.md): Tension Tie · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TENSION STRAP AT AFT WET AREA LBL3 BS1016; BS1026. / [01] PARTIAL STEP 1 AND 2.;[02] VERIFIED CORRECTIVE ACTION 1 AND 2 PARTIAL AND VERIFIED OUT OF LIMITS;[03] REMOVED TENSION STRAP AT BS 989 TO 1026 RBL 11 WL 208 PER SRM 51-10-02.-;[04] RECIVED N
- [SDR SWAA2022082232667](https://openairdocs.org/sdr/SWAA2022082232667.md): Tension Tie · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON TENSION STRAP AT AFT WET AREA RBL3 BS1026; BS1029. / [01] CORROSION ON TENSION STRAP AT AFT WET AREA RBL3 BS1026; BS1029 WITH NEXT DIMENSION L=3.00'' W=0.800 X= 0.010 OT=0.050 RT=0.040 WL 208 P/N 147A5744-1 WITH NEXT TOOL DEPTH GAGE ID:ATS2678 S/N
- [SDR SWAA2022082232668](https://openairdocs.org/sdr/SWAA2022082232668.md): Web · corroded · Jul 22, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON WEB AT AFT CABIN BS989 RBL37. / [01] CORROSION ON WEB AT AFT CABIN BS989 RBL37 WL 208 P/N 147A5744-14 WITH NEXT DIMENSION L=0.950'' W=0.800 X= 0.010 OT=0.050 RT=0.040 WITH NEXT TOOL DEPTH GAGE ID:ATS2678 S/N:UNKNOWN DATE:04/2022 DUE:04/2023; FOUND
- [SDR SWAA2022082331814](https://openairdocs.org/sdr/SWAA2022082331814.md): Rail · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS727C+7; BS767+6 LBL8. / [01] [1]REMOVED (1EA) NUTS PLATE FOR ACCESS IAW SRM 51-40-02. REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS 727C+ 7 LBL 8 IAW SRM 51-10-02-0G-0 MEASURE: L= 1.5' X W=.9' X D= 0.003' REWORKED AREA FOU
- [SDR SWAA2022082331815](https://openairdocs.org/sdr/SWAA2022082331815.md): Rail · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON RAIL AT AFT CARGO BAY BS727D+6; BS767+6 LBL3. / [01] [1]REMOVED (2EA) NUTS PLATE FOR ACCESS IAW SRM 51-40-02. REMOVED CORROSION ON RAIL AT AFT CARGO BAY BS 727D+ 6 LBL 3 IAW SRM 51-10-02-0G-0 MEASURE: L= 2.' X W=.8' X D= 0.003' REWORKED AREA FOUN
- [SDR SWAA2022082331813](https://openairdocs.org/sdr/SWAA2022082331813.md): Sidewall Support · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY LBL21 BS727B+10; BS727C+10; BS727C+14; BS727D+6; BS727E+2; BS727E+10; BS747 - BS787. / REMOVED CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY LBL 21 BS 727B+10 REMOVED CORROSION EVALUATED AS FOLL
- [SDR SWAA2022082331790](https://openairdocs.org/sdr/SWAA2022082331790.md): Stringer Clip · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRINGER CLIP AT AFT CARGO BAY BS767 S-26R. / [01] CORROSION ON CLIP AT AFT CARGO BAY BS767 S-26R FOUND TO BE OUT LIMITS DUE NO ALLOWABLE DAMAGE ON SRM PART WILL REPLACEMENT PER SRM 51-40-02-0G-0 PARA 9C;[02] REMOVED CLIP AT AFT CARGO BAY BS767 S-
- [SDR SWAA2022082231780](https://openairdocs.org/sdr/SWAA2022082231780.md): Frame · cracked · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > BS 312 FRAME IS CRACKED AT STRINGER 5L / [01] REMOVED DAMAGE FROM FRAME BS 312 STR 5L; WL 283 IAW SRM 51-10-02-0G-0;[02] REMOVED DAMAGE FROM FRAME BS 312 STR 5L; WL 283 IAW SRM 53-10-07-2R-1 STEP 4C;[03] INSPECTED AND VERIFIED CORRECTIVE ACTIONS 1 AND 2. HFEC
- [SDR SWAA2022082231778](https://openairdocs.org/sdr/SWAA2022082231778.md): Floor Panel · broken · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Floor Panel
  > FWD CABIN FLOOR PANEL 221BF IS BROKEN ON THE AFT O/B END / [01] IDENTIFIED FLOOR PANEL 221BF MATERIAL IAW SRM 53-00-50-0I-1 FIGURE 2 TABLE 2. DAMAGE AT DISCREPANT LOCATION EXCEEDS ALLOWABLE DAMAGE LIMITS IAW SRM 53-00-50-1A-1 PARAGRAPH 4.F. DAMAGE IS REPAIRABL
- [SDR SWAA2022082231783](https://openairdocs.org/sdr/SWAA2022082231783.md): Intercostal · cracked · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FLOOR SUPPORT IS CRACKED AT BS 284; BL 0; WL 208 / [01] VERIFIED APPLICABILITY AS PER SRM 53-10-51-1A-1 AFTER EVALUATION; DISCREPANCY WAS FOUND OUT OF LIMIT AS PER SRM 53-10-51-1A-1; STEP 4.B(1)A FIGURE 105; DETAIL A.<BR><BR>LOCATED AND DRILLED NEW INTERCOSTA
- [SDR SWAA2022082231789](https://openairdocs.org/sdr/SWAA2022082231789.md): Tie Down · cracked · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACKED TRACK AT AFT CARGO BAY BS727E RBL13. / [01] CARGO TIE DOWN TRACK CRACKED AT BS 727 E RBL 13 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2 ALLOWABLE DAMAGE 2. THE STRUCTURAL ITEM TO BE REPAIRED BY REPLACEMENT PER SRM 53-00-53-2R-3 REPAIR 3 AND PER DWG
- [SDR SWAA2022082231801](https://openairdocs.org/sdr/SWAA2022082231801.md): Support Angle · cracked · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS914 RBL11. / [01] DAMAGE FOUND AT ACB WATER SERVICE PANEL SUPPORT ANGLE BS 914; RBL 11; FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C
- [SDR SWAA2022082231802](https://openairdocs.org/sdr/SWAA2022082231802.md): Support Angle · cracked · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE BEHIND WATER SERVICE PANEL AT ACB BS918 RBL11. / [01] DAMAGE FOUND AT ACB WATER SERVICE PANEL SUPPORT ANGLE BS 918; RBL 11; FOUND TO BE OUT OF LIMIT DUE TO NO LIMIT ON SRM PARTS WILL BE REPAIRED BY REPLACEMENT IAW SRM 51-10-02-0G-0 PAR 9C
- [SDR SWAA2022082231785](https://openairdocs.org/sdr/SWAA2022082231785.md): Track · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON TRACK AT AFT CARGO BAY RBL13 BS727+10 - BS727B; BS727D; BS787; BS787+12. / [01] REMOVED MULTIPLE CORROSION AREAS ON THE TIE DOWN TRACK FROM BS 727+10 - BS787+12 RBL 13 IAW SRM 51-10-02. MAX. MATERIAL REMOVED IN AREA OF 1.3'X0.9'X0.04'DEPTH FROM AN
- [SDR SWAA2022082231817](https://openairdocs.org/sdr/SWAA2022082231817.md): Rail · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Internal Mounting Structure
  > CORROSION ON RAIL AT AFT CARGO BAY BS767+6 LBL12. / [01] CORRODED SPLICE REPAIR; ON UPPER FLANGE AT A JOGGLE; LOCATED AT AFT CARGO BAY BS 767 + 6 LBL12 NOT HAVE ENTRIES IN SRM BY ALLOWABLE DAMAGE MUST BE REPAIR BY REPLACEMENT IAW SRM 51-10-02 ITEM 9.C.;[02] V
- [SDR SWAA2022082231818](https://openairdocs.org/sdr/SWAA2022082231818.md): Shield · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+8; BS767+12 RBL22. / [01] CORROSION ON FWD SHIELD AT AFT CARGO BAY BS767+8; BS767+12 RBL22; FOUND TO BE OUT OF LIMITS DUE NO ALLOWABLE DAMAGE ON SRM;PART WILL BE REPAIRED BY REMPLACEMENT IAW 51-10-02-0G-0 PAR 9
- [SDR SWAA2022082231791](https://openairdocs.org/sdr/SWAA2022082231791.md): Attach Fitting · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FWD SHIELD ATTACH FITTING AT AFT CARGO BAY BS767 RBL23. / [01] REMOVED FWD SHIELD ATTACH FITTING AT AFT CARGO BAY BS767 RBL23.FOUND TO BE OUT LIMITS DUE NO ALLOWABLE DAMAGE ON SRM PART WILL REPLACEMENT PER SRM 51-40-02-0G-0 PARA 9C. RECEIVED NEW
- [SDR SWAA2022082231797](https://openairdocs.org/sdr/SWAA2022082231797.md): Sidewall Support · corroded · Jul 21, 2022 · N490WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT AFT CARGO BAY BS867+9 RBL21. / [01] VERIFIED APPLICABILITY OF SRM 53-60-53-01-2 FOR IDENTIFICATION AND SRM 53-60-15-1A-1 FOR ALLOWABLE DAMAGE;[02] SRM FOR ALLOWABLE DAMAGE 53-00-53-1A-2;[03] REMOVED CORROSION ON FLOOR

Next page: https://openairdocs.org/deregistered/N490WN-2024-10-29/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 = 'N490WN' AND deregistration_id = 'N490WN-2024-10-29'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N490WN-2024-10-29/reports

---
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, except the copies of manufacturers’ service documents, which belong to their rights holders.