# Service difficulty reports: N290WN

A list on [N290WN](https://openairdocs.org/aircraft/N290WN.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 · 257 reports

- [SDR SWAA2026080308795](https://openairdocs.org/sdr/SWAA2026080308795.md): Cartridge · cracked · Jul 29, 2026 · N290WN · Boeing 7377H4 · Trailing Edge Flaps
  > LEFT WING OUTBOARD AFT FLAP INBOARD CLOSURE RIB CARTRIDGE ASSEMBLY IS CRACKED ON AFT LOWER SURFACE. REMOVED AND REPLACED LT OTBD AFT FLAP IAW AMM 27-51-22. VERIFIED ADJUSTMENT ADJUSTMENT GOOD. OP CHECKED GOOD. VERIFIED WORK ACCOMPLISHED IAW AMM 27-51-22.
- [SDR SWAA2026080381075](https://openairdocs.org/sdr/SWAA2026080381075.md): Fastener · missing · Jul 28, 2026 · N290WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR GIRT BAR RETAINER MISSING FASTENER. COMPLIED WITH EA M-23-125-01839 FWD ENTRY GIRT BAR SECURED.
- [SDR SWAA2026031077270](https://openairdocs.org/sdr/SWAA2026031077270.md): Battery Pack · inoperative · Mar 6, 2026 · N290WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS LEFT IN THE ON POSITION, BATTERIES DEPLETED, LIGHTS INOPERATIVE. REPLACED THE EMERGENCY LIGHT BATTERY PACKS IAW AMM 33-51-06.
- [SDR SWAA2025123055923](https://openairdocs.org/sdr/SWAA2025123055923.md): Battery · inoperative · Dec 26, 2025 · N290WN · Boeing 7377H4 · Emergency Equipment
  > FWD FA FLASHLIGHT NOT BLINKING. REMOVED & REPLACED THE FWD FA FLASHLIGHT BATTERY IAW AMM 25-64-00. OPS CHECKED GOOD. ACFT GOOD TO GO.
- [SDR SWAA2025102025044](https://openairdocs.org/sdr/SWAA2025102025044.md): Spring · broken · Oct 17, 2025 · N290WN · Boeing 7377H4 · Emergency Lighting
  > FA REPORT IN AFT GALLEY THE EMERGENCY EXIT LIGHT SWITCH SPRING IS BROKEN AND CUTS ON FINGERS WHEN WORK LIGHT SWITCH IS BEING USED. ADJUSTED SPRING ON SWITCH COVER REF SWPM 20-83-11
- [SDR SWAA2025081399953](https://openairdocs.org/sdr/SWAA2025081399953.md): Unknown · odor · Aug 9, 2025 · N290WN · Boeing 7377H4 · Air Distribution System
  > BAD SMELL AFT GALLEY<[01] PERFORMED ENGINE RUN #1 & #2 SEPARATELY ISOLATING LH AND RH PACKS. NO SMELLS NOTED. OPERATED PACKS WITH APU. NO SMELLS NOTED. PER AMM 71-00-00. GVI OF AFT GALLEY NOTHING WET OR SMELLY. NO SMELLS IN AFT CARGO COMPARTMENT.<BR><BR>134062
- [SDR SWAA2025081299944](https://openairdocs.org/sdr/SWAA2025081299944.md): Drain · odor · Aug 8, 2025 · N290WN · Boeing 7377H4 · Waste Disposal System
  > FLIGHT ATT. REPORTS SEWAGE SMELL COMING FROM AFT GALLEY. CLEANED AFT GALLEY DOOR DRAINS IAW AMM38-31-00.
- [SDR SWAA2025080798501](https://openairdocs.org/sdr/SWAA2025080798501.md): Air Filter · odor · Aug 4, 2025 · N290WN · Boeing 7377H4 · Air Distribution System
  > STRONG SEWAGE SMELL DURING CLIMB OUT FROM ROW 20 TO AFT OF AIRCRAFT. FA AND PASSENGER COMPLAINTS. INSPECTED AFT TOILET SYSTEM AND POTABLE WATER SUPPLY / GRAY WATER DRAIN LINE. NO LEAK AND ANY ABNORMALITY NOTED PER AMM 38-32-00. FURTHER T/S REQ'D. INSPECTED
- [SDR SWAA2025050565841](https://openairdocs.org/sdr/SWAA2025050565841.md): Handle · loose · Apr 30, 2025 · N290WN · Boeing 7377H4 · Service Doors
  > FWD GALLEY AREA R1 DOOR ASSISTANCE HANDLE LOOSE 2025-232442<[01] INSTALLED CORRECTLY DOOR ASSISTANCE HANDLE IAW B737-700 STEP 3 F(2);[02] CORRECTED STEP 1. INSTALLED CORRECTLY IN FWD GALLEY AREA R1 DOOR ASSISTANCE HANDLE IAW B737-700 STEP 3 F(2);[03] CORRECTED
- [SDR SWAA2025050565847](https://openairdocs.org/sdr/SWAA2025050565847.md): Handle · loose · Apr 30, 2025 · N290WN · Boeing 7377H4 · Service Doors
  > AFT SERVICE AREA LEFT AND RIGHT DOORS ASSISTANT HANDLE LOOSE 2025-232467<[01] INSTALLED CORRECTLY AFT SERVICE AREA LEFT AND RIGHT DOORS ASSISTANT HANDLE IAW B737-700 AMM 52-41-31-400-802 STEP 3 F(2);[02] TASK COMPLETED
- [SDR SWAA2025050554065](https://openairdocs.org/sdr/SWAA2025050554065.md): Elevator · out of limits · Apr 13, 2025 · N290WN · Boeing 7377H4 · Elevator Miscellaneous Structure
  > DURING BALANCE PROCEDURE WAS FOUND CBM OF RT ELEVATOR -73.94 LBFIN IS OUT OF LIMIT IAW B737-700 SRM 51-61-04-0G-0 2025-232426<[01] PERFORMED SECONDARY STATIC BALANCE JIG CHECK AT RT ELEVATOR IAW B737-700 SRM 51-61-04-0G-0; STEPS 5.A (3)(B)1); 5.A (4);5.A (5)(A
- [SDR SWAA2025050554055](https://openairdocs.org/sdr/SWAA2025050554055.md): Floorbeam · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2025-232404<[01] REPLACED FLOOR STRUCTURE SUPPORT LOCATED STA 540; BL 0 TO RBL 24.75. IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV-SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPL
- [SDR SWAA2025050554056](https://openairdocs.org/sdr/SWAA2025050554056.md): Floor Support · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2025-232405<[01] REPLACED FLOOR STRUCTURE BRACKET LOCATED STA 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRE
- [SDR SWAA2025050522849](https://openairdocs.org/sdr/SWAA2025050522849.md): Floorbeam · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2025-232404<[01] REPLACED FLOOR STRUCTURE SUPPORT LOCATED STA 540; BL 0 TO RBL 24.75. IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV-SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPL
- [SDR SWAA2025050522850](https://openairdocs.org/sdr/SWAA2025050522850.md): Floorbeam · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2025-232405<[01] REPLACED FLOOR STRUCTURE BRACKET LOCATED STA 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRE
- [SDR SWAA2025050538275](https://openairdocs.org/sdr/SWAA2025050538275.md): Floorbeam · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. 2025-232404<[01] REPLACED FLOOR STRUCTURE SUPPORT LOCATED STA 540; BL 0 TO RBL 24.75. IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV-SEE INDIVIDUAL SIGN OFFS BELOW.;[02] REPL
- [SDR SWAA2025050538276](https://openairdocs.org/sdr/SWAA2025050538276.md): Floorbeam · cracked · Apr 8, 2025 · N290WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > AAI MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75 2025-232405<[01] REPLACED FLOOR STRUCTURE BRACKET LOCATED STA 540; BL 0 TO LBL 24.75 IAW B737-700 SRM 51-40-02 DWG 143A0060 SHEET 46 REV- SEE INDIVIDUAL SIGN OFFS BELOW.;[02] CORRE
- [SDR SWAA2025050554053](https://openairdocs.org/sdr/SWAA2025050554053.md): Access Panel · damaged · Apr 7, 2025 · N290WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 551ET (6 EA) 2025-232399<[01] TOOL USED ON STEP 10 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25;[02] SCALE P/N CR5200; S/N: 8343110809; DUE DATE: 06-MAR-26.;[03] TOOL USED: HOT BONDER PN:HCS92
- [SDR SWAA2025050521876](https://openairdocs.org/sdr/SWAA2025050521876.md): Access Panel · damaged · Apr 5, 2025 · N290WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON PLATE LOCATED ACCESS PANEL 644BB AT RT WING 2025-232389<[01] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.;[02] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2025050538272](https://openairdocs.org/sdr/SWAA2025050538272.md): Access Panel · elongated · Apr 5, 2025 · N290WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON PLATE LOCATED ACCESS PANEL 644BB AT RT WING 2025-232389<[01] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.;[02] REPLACED PLATE LOCATED ACCESS PANEL 644BB AT RT WING IAW B737-700 SRM 51-40-02-0G-0.
- [SDR SWAA2025050554046](https://openairdocs.org/sdr/SWAA2025050554046.md): Battery Pack · inoperative · Apr 3, 2025 · N290WN · Boeing 7377H4 · Emergency Lighting
  > DOES NOT WORK BATTERY PACK LOCATED ON CEILING PANEL AT FWD GALLEY AREA 2025-232381<[01] REPLACED BATTERY PACK LOCATED ON CEILING PANEL AT FWD GALLEY AREA IAW B737-700 AMM 33-51-06-960-805 STEP 4.A THRU 4.E (6)(B) PERFORMED OPERATIONAL TEST; TEST IS OK;[02] COR
- [SDR SWAA2025050254042](https://openairdocs.org/sdr/SWAA2025050254042.md): Bracket · worn · Apr 2, 2025 · N290WN · Boeing 7377H4 · Escape Slide
  > WORN HARDWARE OF FLOOR MOUNTEDESCAPE SLIDE BRACKETS AT FWD SERVICE DOOR AND AFT SERVICE DOOR 2025-232365<[01] REPLACED HARDWARE OF FLOOR MOUNTED ESCAPE SLIDE BRACKETS AT FWD SERVICE DOOR AND AFT SERVICE DOOR IAW B737-700 AMM 25-66-02-400-801 WILL BE INSTALLED
- [SDR SWAA2025050254043](https://openairdocs.org/sdr/SWAA2025050254043.md): Bracket · worn · Apr 2, 2025 · N290WN · Boeing 7377H4 · Escape Slide
  > WORN HARDWARE OF FLOOR MOUNTEDESCAPE SLIDE BRACKETS AT FWD ENTRY DOOR AND AFT ENTRY DOOR 2025-232366<[01] REPLACED HARDWARE OF FLOOR MOUNTEDESCAPE SLIDE BRACKETS AT FWD ENTRY DOOR AND AFT ENTRY DOOR THE INSTALLING WILL BE ON OTHER MAINTENANCE PROCEDURE TTG8Q00
- [SDR SWAA2025050554038](https://openairdocs.org/sdr/SWAA2025050554038.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25;
- [SDR SWAA2025050554039](https://openairdocs.org/sdr/SWAA2025050554039.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28
- [SDR SWAA2025050520674](https://openairdocs.org/sdr/SWAA2025050520674.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28
- [SDR SWAA2025050538259](https://openairdocs.org/sdr/SWAA2025050538259.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON RH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 184.70 RIB; 10.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.900 INCHES 2025-232357<[01] TOOL USED ON STEP 7: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:200048001; DUE DATE: 28
- [SDR SWAA2025050520673](https://openairdocs.org/sdr/SWAA2025050520673.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25
- [SDR SWAA2025050538258](https://openairdocs.org/sdr/SWAA2025050538258.md): Skin · cracked · Apr 1, 2025 · N290WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 9.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 0.940 INCHES 2025-232356<[01] TOOL USED: EDDY CURRENT EQUIPMENT; PN: NORTEC 600D; SN: 60007161486; DUE DATE: 06-SEP-25
- [SDR SWAA2025050554031](https://openairdocs.org/sdr/SWAA2025050554031.md): Angle · cracked · Mar 31, 2025 · N290WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 AT RT WING 2025-232325<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WIN IAW B737-700 SRM 51-40-02-0G AND DWG 115A2930 SHEET 8 REV -;[02] REPLACED ANGLE TRAILING EDGE ORSS 271 AT RT WIN IAW B737-700 SRM 51-40-02-0G AND DWG
- [SDR SWAA2025050554032](https://openairdocs.org/sdr/SWAA2025050554032.md): Angle · cracked · Mar 31, 2025 · N290WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 280 RT WING 2025-232326<[01] REPLACED ANGLE LOC TRAILING EDGE ORSS 280 RT WING IAW B737-700 SRM 51-40-02-0G AND DWG 115A6200 SHEET 11 REV B;[02] CORRECTED STEP 1 REPLACED ANGLE LOC TRAILING EDGE ORSS 280 RT WING IAW B737-700 SRM
- [SDR SWAA2025050554030](https://openairdocs.org/sdr/SWAA2025050554030.md): Angle · cracked · Mar 31, 2025 · N290WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 LT WING 2025-232328<[01] REPLACED ANGLE TRAILING EDGE ORSS 271 LT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9 AND DWG: 115A2930 SHEET: 7 REV - MEASURES OF CRACK L: 0.3950? TOOL USED DIGITAL CALIPER P/N: 500-197-
- [SDR SWAA2025050554034](https://openairdocs.org/sdr/SWAA2025050554034.md): Plate · cracked · Mar 31, 2025 · N290WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK CORRUGATED PLATE TRAILING EDGE IRSS 216 AT LT WING 2025-232329 CORRECTED FAULT NAME: CRACK CORRUGATED PLATE TRAILING EDGE ORSS 216 AT LT WING<[01] REPLACED CORRUGATED PLATE TRAILING EDGE IRSS 216 AT LT WING IAW B737-700 SRM-51-40-02; SRM-51-10-02 ITEM 9
- [SDR SWAA2025050554033](https://openairdocs.org/sdr/SWAA2025050554033.md): Web · cracked · Mar 31, 2025 · N290WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK WEB TRAILING EDGE ORSS 270 FIXED PANEL DEFLECTION CONTROL RIB BEAM AT RT WING 2025-232327<[01] REPLACED WEB TRAILING EDGE ORSS 270 FIXED PANEL DEFLECTION CONTROL RIB BEAM AT RT WING IAW B737 SRM 51-10-02 AND SRM 51-40-02 DWG 115A2512 SHEET 14 REV-A;[02]
- [SDR SWAA2025050554021](https://openairdocs.org/sdr/SWAA2025050554021.md): Web · cracked · Mar 30, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED ON BS 1040 LBL 33.80 WL 208.1 AFT GALLEY AREA 2025-232285<[01] REPLACED NEW WEB AND FASTENERS LOCATED ON BS 1040 LBL 33.80 WL 208.1 AFT GALLEY AREA IAW B737-700 SRM 51-40-02 AND 51-10-02 ITEN 9. AND DWG 148A0922 SHEET 23 REV - SEE INDIVIDU
- [SDR SWAA2025050254022](https://openairdocs.org/sdr/SWAA2025050254022.md): Shield · corroded · Mar 30, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SHIELD WEB LOCATED BTW BS 492TO BS 500A RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT 2025-232287<[01] REPLACED NEW SHIELD WEB AND FASTENERS LOCATED BTW BS 492 TO BS 500A RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SMR 51-10-02
- [SDR SWAA2025050254023](https://openairdocs.org/sdr/SWAA2025050254023.md): Support · corroded · Mar 30, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 500A TO BS 500C RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT 2025-232289<[01] EVALUATED CORROSION ON SUPPORT ZEE LOCATED BTW BS 500A TO BS 500C RBL 25 WL 156.1 AT FWD CARGO COMPARTMENT AND FOUND OUT OF THE LIMITS; SUPPORT ZE
- [SDR SWAA2025050553999](https://openairdocs.org/sdr/SWAA2025050553999.md): Nut Plate · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 722 AT LT WING 2025-232245<[01] REPLACED RAIL NUT PLATE AND FASTENERS LOCATED ON LEADING EDGE FROMT SPAR OFSS 722 AT LT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 STEP 9 AND DWG: 112A4402 SH
- [SDR SWAA2025050554000](https://openairdocs.org/sdr/SWAA2025050554000.md): Nut Plate · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 571 AT LT WING 2025-232247<[01] REPLACED RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 571 AT LT WING IAW B737-700 SRM 51-40-02 AND DWG: 112A4402 SHEET: 14 REV: -. <BR>LENGTH OF CRACK: 0.439<BR>T
- [SDR SWAA2025050554011](https://openairdocs.org/sdr/SWAA2025050554011.md): Nut Plate · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 482 AT RT WING 2025-232255<[01] REPLACED RAIL NUT PLATE LEADING EDGE FROMT SPAR LOCATED LOCATED OFSS 482 AT RT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG: 112A4402 SHEET: 13; REV: -
- [SDR SWAA2025050554012](https://openairdocs.org/sdr/SWAA2025050554012.md): Nut Plate · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 503 AT RT WING. REPLACED RAIL NUT PLATE LEADING EDGE FROMT SPAR LOCATED OFSS 503 AT RT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG: 112A4402; SHEET: 13; REV: - LENGTH OF CRACK: 0.425
- [SDR SWAA2025050554013](https://openairdocs.org/sdr/SWAA2025050554013.md): Nut Plate · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing, Attach Fittings
  > CRACK RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 572 AT RT WING. REPLACED RAIL NUT PLATE LEADING EDGE FRONT SPAR LOCATED OFSS 572 AT RT WING IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 AND DWG: 112A4402; SHEET: 14; REV: - LENGHT OF CRACK: 0.475
- [SDR SWAA2025050554004](https://openairdocs.org/sdr/SWAA2025050554004.md): Cargo Track · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK ON CARGO TRACK LOCATED BS 727E RBL 13.84 WL 208.1 AT AFT CARGO COMPARTMENT 2025-232254<[01] FAULT RESOLVED ON OTHER FAULT DUE TO REPAIR IS COMPLETED ON TTG8Q00ZK0SQ;[02] CORRECTED STEP 1 <BR><BR>FAULT RESOLVED ON OTHER FAULT DUE TO REPAIR IS COMPLETED ON
- [SDR SWAA2025050554017](https://openairdocs.org/sdr/SWAA2025050554017.md): Cargo Track · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBL 13.84 LOCATED. BS 747 WL 156.1 AT AFT CARGO COMPARTMENT 2025-232270<[01] FAULT RESOLVED ON OTHER FAULT DUE TO REPAIR IS COMPLETED ON TTG8Q00ZK0SQ. SEE INDIVIDUAL SIGN OFF BELOW;[02] TASK COMPLETED
- [SDR SWAA2025050554008](https://openairdocs.org/sdr/SWAA2025050554008.md): Angle · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE LOCATED ORSS 272 CONTROL RIB AREA AT LT WING 2025-232249<[01] REPLACED ANGLE TRAILING EDGE LOCATED ORSS 272 CONTROL RIB AREA AT LT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-10-02-0G ITEM 9 AND DWG: 115A2930 SHEET: 6 REV - MEASURES OF
- [SDR SWAA2025050253997](https://openairdocs.org/sdr/SWAA2025050253997.md): Web · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 19 AT AFT CARGO COMPARTMENT 2025-232244<[01] REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 19 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET
- [SDR SWAA2025050253998](https://openairdocs.org/sdr/SWAA2025050253998.md): Support Angle · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED CEILING AREA BS 727B LBL 51 AT AFT CARDO COMPARTMENT 2025-232246<[01] ON STEP 7; TOOL USED: EDDY CURRENT: PN: NORTEC 600D; SN: 210138503; DUE DATE: 05-AUG-25;[02] PERFORMED REPAIR SUPPORT ANGLE LOC. ON CEILING AREA BTW BS 727B TO
- [SDR SWAA2025050254003](https://openairdocs.org/sdr/SWAA2025050254003.md): Cargo Track · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK RBBL 13.84 LOCATED. BS 767 WL 156.1 AT AFT CARGO COMPARTMENT 2025-232253<[01] EQUIPMENT P/N PHASEC 3D; S/N CZ1026/09; DUE DATE 31-MAY-25 WAS USED ON STEP 4 AND STEP 5;[02] PERFORMED PERMANENT REPAIR ON CARGO TRACK RBL 13.84 LOCATED ON BS 767 WL 156
- [SDR SWAA2025050254006](https://openairdocs.org/sdr/SWAA2025050254006.md): Support · corroded · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 747 TO BS 787LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-232261<[01] REMOVED CORROSION ON SUPPORT ZEE LOCATED BTW BS 747 TO BS 787 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT. EVALUATED REWORKED AREA AND FOUND OUT OF THE
- [SDR SWAA2025050254015](https://openairdocs.org/sdr/SWAA2025050254015.md): Web · cracked · Mar 29, 2025 · N290WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT 2025-232265<[01] REPLACED WEB AND FASTENERS LOCATED BTW BS 927 TO BS 947.5 AT LEVEL STR 25R WL 156.1 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02. I.A.W B737

Next page: https://openairdocs.org/aircraft/N290WN/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 = 'N290WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N290WN/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.