# Service difficulty reports: N291WN

A list on [N291WN](https://openairdocs.org/aircraft/N291WN.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 · 278 reports

- [SDR SWAA2026101954853](https://openairdocs.org/sdr/SWAA2026101954853.md): Battery Pack · no test · Oct 15, 2026 · N291WN · Boeing 7377H4 · Emergency Lighting
  > AFT RT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-06.
- [SDR SWAA2026101994927](https://openairdocs.org/sdr/SWAA2026101994927.md): Battery Pack · no test · Oct 15, 2026 · N291WN · Boeing 7377H4 · Emergency Lighting
  > AFT LT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK. REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2026100588776](https://openairdocs.org/sdr/SWAA2026100588776.md): Light · inoperative · Oct 1, 2026 · N291WN · Boeing 7377H4 · Emergency Lighting
  > LEFT OVERWING EXIT, EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHKD GOOD.
- [SDR SWAA2026100589299](https://openairdocs.org/sdr/SWAA2026100589299.md): Light · inoperative · Oct 1, 2026 · N291WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EXTERNAL EMERGENCY LIGHT WAS INOPERATIVE. REMOVED & REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-04-960-801, OPS CHECKED GOOD.
- [SDR SWAA2026090810886](https://openairdocs.org/sdr/SWAA2026090810886.md): Seat · out of adjust · Sep 1, 2026 · N291WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEAT 15D RECLINE INOPERATIVE. ADJUSTED 15D RECLINE ACTUATOR IAW CMM 25-21-42. OPS CHECKED GOOD AT THIS TIME.
- [SDR SWAA2026081973499](https://openairdocs.org/sdr/SWAA2026081973499.md): Engine · no discrepancy · Aug 15, 2026 · N291WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > OTS, NR 1 ENGINE SLOW TO SPOOL ON TAKE OFF ROLL, ABORTED AT 40 KTS. ACCOMPLISHED FDR DOWNLOAD AND UPLOADED FOR POWERPLANT ENGINEERING. IAW MM 31-31-00. ACCOMPLISHED ACCELLERATION TEST 8 PER MM 71-00-00, WITHIN ALLOWABLE LIMITS. ACCOMPLISHED POWER ASSURANCE
- [SDR SWAA2026072396220](https://openairdocs.org/sdr/SWAA2026072396220.md): Stator Vane · leaking · Jul 19, 2026 · N291WN · Boeing 7377H4 · Turbine Engine Compressor Section
  > OTS-#2 ENGINE FUEL LEAK_ REMOVED AND REPLACED THE ENG 2 RH VSV IAW AMM 75-31-01. PERFORMED POWER PLANT TEST IAW AMM 71-00-00 TEST 3A. IDLE LEAK CHECK FAILED. E 202957 C/W RII OF #2 ENG RH VSV INSTALL PER AMM 75-31-01. TEST 3A IDLE LEAK CHECK FAILED. C/W #2 ENG
- [SDR SWAA2026011359676](https://openairdocs.org/sdr/SWAA2026011359676.md): Post · corroded · Jan 9, 2026 · N291WN · Boeing 7377H4 · Fuselage Main, Structure
  > PASSENGER CABIN FWD LAV AFT INBD LOWER POST HAS EVIDENCE OF CORROSION. REMOVED FWD FLIGHT ATTENDANT SEAT TO FOM IAW AMM 25-25-12. FWD FLIGHT ATTENDANT SEAT INSTALLED IAW TASK CARD 725-41-01. REMOVED AND REPLACED THE FWD LAV ASSY IAW TASK 725-41-01.
- [SDR SWAA2026011359698](https://openairdocs.org/sdr/SWAA2026011359698.md): Pan · corroded · Jan 9, 2026 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > PASSENGER CABIN FWD LAV FLOOR PAN HAS EVIDENCE OF CORROSION AT THE THRESHOLD. REMOVED AND REPLACED LAVATORY IAW TASK CARD 725-41-01, FAULT TTG8Q019T2FF.
- [SDR SWAA2025060268070](https://openairdocs.org/sdr/SWAA2025060268070.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT (CRACK 3) 2025-307661<[01] MEASURED CRACK (3) ON VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT: L=2.25? W=1.50? TOOL USED: CALIPER P/N: 500-196-30; S/N: B233750
- [SDR SWAA2025060268072](https://openairdocs.org/sdr/SWAA2025060268072.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT (CRACK 5) 2025-307663<[01] MEASURED CRACK (5) ON VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT: L=1.75? W=1.25? TOOL USED: CALIPER P/N: 500-196-30; S/N: B233750
- [SDR SWAA2025060268073](https://openairdocs.org/sdr/SWAA2025060268073.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT (CRACK 6) 2025-307665<[01] MEASURED CRACK (6) ON VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT: L=1.0? W=0.75? TOOL USED: CALIPER P/N: 500-196-30; S/N: B2337508
- [SDR SWAA2025060268065](https://openairdocs.org/sdr/SWAA2025060268065.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT (CRACK 1). 2025-307658<[01] MEASURED CRACK (1) ON VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT: L=12.0? W=0.75? TOOL USED: CALIPER P/N: 500-196-30; S/N: B23375
- [SDR SWAA2025052968068](https://openairdocs.org/sdr/SWAA2025052968068.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT (CRACK 2) 2025-307657 <[01]. MEASURED CRACK (2) ON VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT L=0.75IN. TOOL USED: CALIPER: P/N: 500-196-30; S/N: A2
- [SDR SWAA2025052968069](https://openairdocs.org/sdr/SWAA2025052968069.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT (CRACK 3) 2025-307659 <[01]. MEASURED CRACK (3) ON VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT L=0.53IN. TOOL USED: CALIPER: P/N: 500-196-30; S/N: A23
- [SDR SWAA2025052968067](https://openairdocs.org/sdr/SWAA2025052968067.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT (CRACK 4) 2025-307662 <[01]. MEASURED CRACK(4) ON VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT L=0.45IN. TOOL USED: CALIPER: P/N: 500-196-30; S/N: A23
- [SDR SWAA2025052968071](https://openairdocs.org/sdr/SWAA2025052968071.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACK VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT (CRACK 5) 2025-307664 <[01]. MEASURED CRACK (5) ON VAPOR VARRIER LOCATED BS 663.75 AND RBL 31 AT MAIN WHEEL WELL COMPARTMENT L=0.64IN. TOOL USED: CALIPER: P/N: 500-196-30; S/N: A2
- [SDR SWAA2025052968066](https://openairdocs.org/sdr/SWAA2025052968066.md): Vapor Barrier · cracked · May 6, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT (CRACK 2). MEASURED CRACK (2) ON VAPOR BARRIER LOCATED BS663 AND LBL 54 AT MAIN WHEEL WELL COMPARTMENT: L=7.5? W=0.87. EVALUATED AND REPAIRED PROCESS IAW SRM 51-70-04-2R-10 REPAIR
- [SDR SWAA2025052966394](https://openairdocs.org/sdr/SWAA2025052966394.md): Support · cracked · May 1, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI INSPECTION. MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO LBL 24.75. 2025-307653 <[01]. MEASURE CRACK IS 1.230 INCHES TOOL USED: ELECTRONIC CALIPER P/N: 500-196-30 S/N: A23048253 DUE DATE: 05/JUN/25. REPLACED FLOOR STRUCTURE SUPPORT (BR
- [SDR SWAA2025052965999](https://openairdocs.org/sdr/SWAA2025052965999.md): Stiffener · cracked · Apr 30, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON VERTICAL STIFFENER LOC BS663 AT LEVEL LBL 25 LOWER SIDE 2025-307647 <[01]. REPLACED VERTICAL STIFFENER AND FASTENERS. LOC BS663 AT LEVEL LBL 25 LOWER SIDE.IAW B737-700 SRM 51-40-02 SRM 51-10-02 ITEM 9 DWG 111A1000 SHEET 259 REV.A. SEE INDIVIDUAL SIGN
- [SDR SWAA2025060265017](https://openairdocs.org/sdr/SWAA2025060265017.md): Angle · cracked · Apr 28, 2025 · N291WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING 2025-274552<[01] REPLACED ANGLE TRAILING EDGE ACCESS PANEL 651FB RT WING IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND MEASURES OF CRACK IS: 1.369? <BR>TOOL USED:<BR>CALIPER P/N: 500-197-30; S/N: A18135
- [SDR SWAA2025052965199](https://openairdocs.org/sdr/SWAA2025052965199.md): Bracket · cracked · Apr 28, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 271 RT WING. REPLACED SUPPORT BRACKET TRAILING EDGE LOCATED ORSS 271 RT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2982; SHEET: 4; REV: -.
- [SDR SWAA2025052928123](https://openairdocs.org/sdr/SWAA2025052928123.md): Frame · cracked · Apr 24, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME ON BS 947.5 AND RBL 8.1 AT AFT CARGO COMPARTMENT 2025-274492 <[01]. REPLACED FRAME LOCATED ON BS 947.5 BETWEEN STR 23 RH TO STR 23 LH AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW B737-700 SRM 51-40-02 AND DRAW
- [SDR SWAA2025052956986](https://openairdocs.org/sdr/SWAA2025052956986.md): Support · corroded · Apr 24, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BS 727 PLUS 15 INCH RBL 21 AND WL 156 AFT CARGO COMPARTMENT 2025-274487 <[01]. REPLACED SUPPORT ZEE ( ZEE CHANNEL SIDE PLATE) AND FASTENERS LOCATED BS 727+4 TO BS 767 RBL 21 AND WL 156 AFT CARGO COMPARTMENT IAW B737-700 DWG 146A7
- [SDR SWAA2025052956981](https://openairdocs.org/sdr/SWAA2025052956981.md): Track · cracked · Apr 24, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TRACK RBBL 13.84 LOCATED BS727E AND BS 747 AFT CARGO COMPARTMENT 2025-274485 <[01]. TOOL USED P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE: 07-OCT-25.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.; [03] PERFORMED PER
- [SDR SWAA2025052956988](https://openairdocs.org/sdr/SWAA2025052956988.md): Angle · cracked · Apr 24, 2025 · N291WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 1 AT LT WING IAW B737-700 SRM 51-40-02
- [SDR SWAA2025052956960](https://openairdocs.org/sdr/SWAA2025052956960.md): Light · broken · Apr 23, 2025 · N291WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY LIGHT ASSY ON HEADER PANEL RH AT FWD GALLEY AREA 2025-274434 <[01]. REPLACED EMERGENCY LIGHT ASSY ON HEADER PANEL RH AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(6)(7). TEST IS OK; [02] CORRECTED STEP 1: REPLACED EMERGENCY
- [SDR SWAA2025052956961](https://openairdocs.org/sdr/SWAA2025052956961.md): Light · broken · Apr 23, 2025 · N291WN · Boeing 7377H4 · Emergency Lighting
  > INCORRECTED EMERGENCY EXIT LIGHT LENS ON LAVATORY A AT FWD GALLEY AREA (1 EA) 2025-274351 <[01]. REPLACED EMERGENCY EXIT LIGHT LENS ON LAVATORY A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(10); [02] REPLACED EMERGENCY EXIT LIGHT LENS ON LA
- [SDR SWAA2025052956967](https://openairdocs.org/sdr/SWAA2025052956967.md): Light · broken · Apr 23, 2025 · N291WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN EMERGENCY EXIT LIGHT ASSY LAVATORY B AT AFT GALLEY AREA (1 EA) 2025-274445 <[01]. REPLACED HOSE AIR DUCK ON LAVATORY A AT FWD GALLEY AREA IAW B737-700 AMM 33-51-01-960-802 STEP 3.C.(5)(D) THRU 3.C.(7);[02] CORRECTED STEP 1: REPLACED HOSE AIR DUCK ON LAV
- [SDR SWAA2025052956975](https://openairdocs.org/sdr/SWAA2025052956975.md): Angle · cracked · Apr 23, 2025 · N291WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACK BLADE ACCESS PANEL 343AT ANGLE RT HORIZONTAL STAB 2025-274463 <[01]. REPLACED BLADE ACCESS PANEL 343AT ANGLE RT HORIZONTAL STAB IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DRAWING 186A3101 SHEET 19 REV. -; [02] TASK COMPLETED.
- [SDR SWAA2025060256946](https://openairdocs.org/sdr/SWAA2025060256946.md): Tie Clip · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN 2025-274293<[01] REPLACED TIE CLIP LOCATED STA277 AND STR10R PASSENGER CABIN IAW B737-700 SRM 51-40-02 AND DWG 141A1110; SHEET: 18 AND REV:?.;[02] CORRECTED STEP 1. <BR>REPLACED TIE CLIP LOCATED STA277 A
- [SDR SWAA2025052956934](https://openairdocs.org/sdr/SWAA2025052956934.md): Stub Frame · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION (2 E/A) ON STUB FRAME LOCATED AT BS 294.5 BETWEEN STR-8 TO STR-9 IN FORWARD GALLEY DOOR RH SIDE; CRACK LENGTH: 0.875 INCHES AND 0.680 INCHES APPROX. 2025-274283 <[01] REPLACED STUB FRAME LOCATED ON BS 294.5 BTW STR 7R TO STR 10R IAW B737-700 S
- [SDR SWAA2025052956947](https://openairdocs.org/sdr/SWAA2025052956947.md): Web · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA 2025-274297 <[01]. REPLACED INTERCOSTAL WEB; STRAP; CLIP AND FASTENERS LOCATED BETWEEN STA294.5 TO STA303.9 AND STR16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02; SRM
- [SDR SWAA2025052956938](https://openairdocs.org/sdr/SWAA2025052956938.md): Access Panel · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ACCESS PANEL 661BB TRAILING EDGE AROUND HOLES AT RT WING 2025-274301<[01]. TOOL USED: HOT BONDER PN:HCS9200B SN:16122983 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 12 ULTRASONIC FLAW DETECTOR P/N: EPOCH 650; S/N: 190776902; CAL DUE DATE: 15-OCT-25; [03]
- [SDR SWAA2025052956939](https://openairdocs.org/sdr/SWAA2025052956939.md): Access Panel · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ACCESS PANEL 661AB AROUND HOLES TRAILING EDGE AT RT WING 2025-274296 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [0
- [SDR SWAA2025052956940](https://openairdocs.org/sdr/SWAA2025052956940.md): Access Panel · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ACCESS PANEL 661CB TRAILING EDGE AROUND HOLES RT WING 2025-274298 <[01].TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03]
- [SDR SWAA2025052956948](https://openairdocs.org/sdr/SWAA2025052956948.md): Access Panel · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ACCESS PANEL 561AB TRAILING EDGE AROND HOLES LT WING 2025-274302 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03] T
- [SDR SWAA2025052956949](https://openairdocs.org/sdr/SWAA2025052956949.md): Access Panel · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ACCESS PANEL 561CB TRAILING EDGE AROUND HOLES LT WING 2025-274303 <[01]. TOOL USED: HOT BONDER PN: HCS9200B-AV SN: 18196127 DUE DATE: 22-FEB-26; [02] TOOL USED ON STEP 13: ULTRASONIC FLAW DETECTOR P/N: EPOCH 600; S/N: 120357005 DUE DATE: 10-JUN-25; [03]
- [SDR SWAA2025052927467](https://openairdocs.org/sdr/SWAA2025052927467.md): Angle · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING SRM 51-10-02 ITEM 9
- [SDR SWAA2025052956943](https://openairdocs.org/sdr/SWAA2025052956943.md): Angle · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE ORSS 281 DEFFLECTION CONTROL RIB SUPPORT BEAM RT WING. REPLACED ANGLE ON TRAILING EDGE ORSS 281 DEFFLECTION CONTROL RIB SUPPORT BEAM AT RT WING IAW SRM 51-10-02 AND SRM 51-40-02. MEASURE OF CRACK IS L=1.182 IN.
- [SDR SWAA2025052956945](https://openairdocs.org/sdr/SWAA2025052956945.md): Floorbeam · cracked · Apr 22, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ANGLE FLOOR STRUCTURE LOCATED STA294.5 AND RBL53 WL208.1 AT FWD GALLEY AREA. REPLACED ANGLE (CLIP) FLOOR STRUCTURE LOCATED STA294.5 AND RBL53 WL208.1 AT FWD GALLEY AREA. IAW SRM 51-10-02 AND DWG 141A8310 SHEET 25 REV.
- [SDR SWAA2025052956933](https://openairdocs.org/sdr/SWAA2025052956933.md): Intercostal · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 AT FWD GALLEY AREA 2025-274281 <[01]. REPLACED WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA344 TO STA360 AND BL0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9 AND INSTALLED FASTE
- [SDR SWAA2025052926644](https://openairdocs.org/sdr/SWAA2025052926644.md): Scuff Plate · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FWD CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT 2025-274244 <[01]. TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23325478; DUE DATE:26-JAN-26.; [02] TOOL USED P/N: XRP-3000; S/N: 1753759; CAL DUE: 30-JUN-25.;[03] REPAIRED FWD CORNER SCUFF PLATE AT AFT C
- [SDR SWAA2025052926778](https://openairdocs.org/sdr/SWAA2025052926778.md): Scuff Plate · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON FWD SERVICE DOOR SCUFF PLATE AT FWD GALLERY AREA 2025-274255 <[01]. TOOL USED DIGITAL CALIPER P/N:500-196-30; S/N:A23325478; DUE DATE:26-JAN-26.; [02] TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N: 1753759; DUE DATE: 30-JUN-25; [03] REPAI
- [SDR SWAA2025052956931](https://openairdocs.org/sdr/SWAA2025052956931.md): Angle · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND RBL1 PASSENGER CABIN 2025-274279 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 28-JAN-26.
- [SDR SWAA2025052956932](https://openairdocs.org/sdr/SWAA2025052956932.md): Angle · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE FLOOR STRUCTURE LOCATED STA695 AND LBL24.75 PASSENGER CABIN 2025-274280 <[01]. TOOLS USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 29-JAN-26; TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 112820025; DUE DATE: 28-JAN
- [SDR SWAA2025052956927](https://openairdocs.org/sdr/SWAA2025052956927.md): Floorbeam · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK FLOOR BEAM LOCATED STA328 AND RBL21 FWD GALLEY AND LAV 2025-274263 <[01]. TOOL USED RADIOMETER/PHOTOMETER KIT P/N: XRP-3000; S/N: 1753759; DUE DATE: 30/JUN/25; [02] TOOL USED ON STEP 18: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 240525411; DUE DA
- [SDR SWAA2025052956929](https://openairdocs.org/sdr/SWAA2025052956929.md): Intercostal · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED STA312 TO STA328 AND RBL31 AT FWD GALLEY AREA 2025-274268 <[01]. REPLACED INTERCOSTAL FLOOR STRUCTURE AND FASTENERS LOCATED STA 312 TO STA 328 AND RBL 31 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM
- [SDR SWAA2025052956926](https://openairdocs.org/sdr/SWAA2025052956926.md): Angle · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING. REPLACED ANGLE LOCATED TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA LT WING IAW SRM 51-10-02 ITEM 9 AND INSTALLED FASTENERS IAW SRM 51-40-02 AND DWG 115A2930 SHEET 7 REV -.
- [SDR SWAA2025052956924](https://openairdocs.org/sdr/SWAA2025052956924.md): Angle · cracked · Apr 21, 2025 · N291WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ANGLE TRAILING EDGE ORSS 281 AT LEVEL DEFLECTION CONTROL RIB SUPPORT BEAM LT WING. REPLACED ANGLE ON TRAILING EDGE ORSS 281 AT LEVEL DEFLECTION CONTROL RIB SUPPORT BEAM AT LT WING IAW SRM 51-10-02 AND SRM 51-40-02. MEASURE OF CRACK IS L=1.687 IN.

Next page: https://openairdocs.org/aircraft/N291WN/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 = 'N291WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N291WN/reports

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