# Service difficulty reports: N282WN

A list on [N282WN](https://openairdocs.org/aircraft/N282WN.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 · 297 reports

- [SDR SWAA2025092316551](https://openairdocs.org/sdr/SWAA2025092316551.md): Pressure Deck · cracked · Sep 20, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Structure
  > FLIGHT DECK AFT FLOOR WEB DENT WITH CRACKS AT STATION 255 AND LBL 3. REMOVED AND REPLACED WEB SECTION PER SRM 51-40-02 AND IAW EA M-21-153-00734 WHICH HAD BEEN INITIALLY REPLACED ON NR TTG8Q0100AU9 DURING ACCOMPLISHMENT OF EA M-21-153-00734.
- [SDR SWAA2025062785439](https://openairdocs.org/sdr/SWAA2025062785439.md): Lamp · inoperative · Jun 25, 2025 · N282WN · Boeing 7377H4 · Emergency Lighting
  > L/H OVER WING EMERGENCY EXIT SIGN AREA LIGHTS INOP<[01] REVAMPED L/H OVER WING EMERGENCY EXIT SIGN AREA LIGHTS & OPS CHECK GOOD REF AMM 33-51-01.
- [SDR SWAA2025051671198](https://openairdocs.org/sdr/SWAA2025051671198.md): Girt Bar · out of adjust · May 14, 2025 · N282WN · Boeing 7377H4 · Emergency Equipment
  > INSTALL CORRECTLY GIRT BAR ESCAPE SLIDE FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA 2025-242657<[01] INSTALL CORRECTLY GIRT BAR ESCAPE SLIDE FLOOR BRACKET SERVICE DOOR AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801. INSTALLATION TEST IS OK.;[02] CORREC
- [SDR SWAA2025051956321](https://openairdocs.org/sdr/SWAA2025051956321.md): Web · cracked · Apr 18, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INDICATION IN HOLE ON LOWER SILL LOCATED BS 294.5 PLUS 1 INCH AT LEVEL STR 17R AT FWD GALLEY AREA. CRACK DIRECTION IS: 6 0 CLOCK VIEW LOOKING FWD. 2025-242620<[01] REPLACED WEB LOC. ON LOWER SILL BS 294.5 PLUS 1 INCH AT LEVEL STR 17R AT FWD GALLEY AREA I
- [SDR SWAA2025051956307](https://openairdocs.org/sdr/SWAA2025051956307.md): Angle · cracked · Apr 13, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INNER CHORD LOCATE BS 294.5 RBL 53 WL 208.1 AT FWD GALLEY AREA. REPLACED INNER CHORD LOC. BTW BS 259.50 TO BS 360 RBL 53 WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8310 SHEET 25 REV; DWG 140A9810 SHEET 22 REV B; DWG 140A9
- [SDR SWAA2025051956303](https://openairdocs.org/sdr/SWAA2025051956303.md): Plate · cracked · Apr 12, 2025 · N282WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED AT LEVEL ORSS 465 TRAILING EDGE AT LT WING 2025-242575<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 465 TRAILING EDGE AT LT WING I.A.W B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 115A3710 SHEET 3 REV -.;[02] COR
- [SDR SWAA2025051956298](https://openairdocs.org/sdr/SWAA2025051956298.md): Plate · cracked · Apr 12, 2025 · N282WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED AT LEVEL IRSS 218 TRAILING EDGE AT LT WING 2025-242568<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL IRSS 218 TRAILING EDGE AT LT WING IAW B737 SRM 51-40-02-0G AND DWG 115A2001 SHEET 45 REV -;[02] TASK COMPLETED
- [SDR SWAA2025051956305](https://openairdocs.org/sdr/SWAA2025051956305.md): Plate · cracked · Apr 12, 2025 · N282WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK ON CORRUGATED PLATE LOCATED AT LEVEL ORSS 297 TRAILING EDGE AT LT WING 2025-242574<[01] REPLACED CORRUGATED PLATE LOCATED AT LEVEL ORSS 297 TRAILING EDGE AT LT WING IAW B737-700 SRM 51-10-02-0G-0 STEP 9; SRM 51-40-02-0G-0 AND DWG 115A3700 SHEET 38 REV-.;
- [SDR SWAA2025051923757](https://openairdocs.org/sdr/SWAA2025051923757.md): Angle · cracked · Apr 11, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED TRAILING EDGE ON IRSS 140 RIGHT WING 2025-242538<[01] REPLACED ANGLE (CLIP) LOCATED TRAILING EDGE ON IRSS 140 RIGHT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0 AND DWG: 115A2000 SHEET: 22 REV A MEASURES OF CRACK L: 1.3640'
- [SDR SWAA2025051956289](https://openairdocs.org/sdr/SWAA2025051956289.md): Support Angle · cracked · Apr 11, 2025 · N282WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED ON TRAILING EDGE ORSS 271 RT WING 2025-242547<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDITIONAL DAMAGES AND INSTALLED NEW SUPPORT ANGLE (WEB ASSY) LOCATED ON TRAILING EDGE ORSS 271 RT WING IAW B737-700 SRM 51-40-02-0G; SRM 51-1
- [SDR SWAA2025051923880](https://openairdocs.org/sdr/SWAA2025051923880.md): Support Bracket · cracked · Apr 11, 2025 · N282WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING. 2025-242544<[01] REPLACED SUPPORT BRACKET LOC. ON TRAILING EDGE ORSS 271 RT WING IAW-B737-700-SRM 51-10-02-0G-0 ITEM 9 AND 51-40-02-0G-0 TOOK MEASURE OF CRACK IS: 0.121 INCHES TOOL USED ELECTRONI
- [SDR SWAA2025051956291](https://openairdocs.org/sdr/SWAA2025051956291.md): Angle · cracked · Apr 11, 2025 · N282WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON ANGLE LOCATED ON TRAILING ORSS 281 RT WING 2025-242548<[01] REPLACED ANGLE (CLIP) LOCATED ON TRAILING ORSS 281 RT WING IAW B737-700 SRM 51-10-02-0G-0 ITEM 9 SRM 51-40-02-0G-0 AND DWG: 115A6200 SHEET: 11 REV B MEASURES OF CRACK L: 0.4080' TOOL USED DIG
- [SDR SWAA2025051956297](https://openairdocs.org/sdr/SWAA2025051956297.md): Angle · cracked · Apr 11, 2025 · N282WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ACCESS PANEL 551FB ON ANGLE AT LT WING 2025-242556<[01] REPLACED ANGLE ON ACCESS PANEL 551FB AT LT WING IAW B737-700 SRM 51-40-02-0G 51-10-02-0G-0 STEP 9 AND DWG 115A2710 SHEET 9 REV- A. AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE ON SRM. MEASURE
- [SDR SWAA2025051956277](https://openairdocs.org/sdr/SWAA2025051956277.md): Support Angle · cracked · Apr 10, 2025 · N282WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED AT LEVEL ORSS 261 DEFLECTION CONTROL RIB AREA TRAILING EDGE AT LT WING 2025-242530<[01] REMOVED AND PERFORMED GVI; NO FOUND ADDITIONAL DAMAGES AND INSTALLED NEW SUPPORT ANGLE (WEB ASSY) LOCATED AT LEVEL ORSS 261 DEFLECTION CONTRO
- [SDR SWAA2025051956272](https://openairdocs.org/sdr/SWAA2025051956272.md): Access Panel · cracked · Apr 9, 2025 · N282WN · Boeing 7377H4 · Passenger/Crew Doors
  > CRACK ACCCESS PANEL 834DZ ENTRY DOOR AFT BRACKET AT AFT GALLEY AREA. REPLACED ACCCESS PANEL 834DZ ENTRY DOOR AFT BRACKET AT AFT GALLEY AREA;IAW B737-700 SRM 51-40-02 AND DWG 411A2119; SHEET 72; REV -.<
- [SDR SWAA2025051956250](https://openairdocs.org/sdr/SWAA2025051956250.md): Lens · broken · Apr 8, 2025 · N282WN · Boeing 7377H4 · Emergency Lighting
  > BROKEN LIGHT EXIT LENS ON SIDEWALL PANEL 232YJW AT PASSENGER CABIN 2025-242400<[01] REPLACED LIGHT EXIT LENS ON SIDEWALL PANEL 232YJW AT PASSENGER CABIN IAW B737-700 AMM 33-51-01-960-802 STEP 3.C(5)(C) AND STEP 3.C(10);[02] REPLACED LIGHT EXIT LENS ON SIDEWALL
- [SDR SWAA2025051956252](https://openairdocs.org/sdr/SWAA2025051956252.md): Access Panel · cracked · Apr 8, 2025 · N282WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK ACCESS PANEL 333AT PLATE AT LT HORIZONTAL STABILIZER 2025-242408<[01] REPLACED ACCESS PANEL 333AT PLATE AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. TOOL USED CALIPER P/N: 500-196-30 S/N: A23400724 DUE DATE: 11-SEP-25;[0
- [SDR SWAA2025051922884](https://openairdocs.org/sdr/SWAA2025051922884.md): Rib · cracked · Apr 8, 2025 · N282WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK ACCESS PANEL 331B LEADING EDGE RIB LOCATED LE STA 105.26 AT LT HORIZONTAL STABILIZER 2025-242429<[01] REPLACED RIB LOC. ON LEADING EDGE STA 105.26 AT LT HORIZONTAL STABILIZER IAW B737-700 SRM 51-40-02-0G-0 AND DWG 186A1352 SHEET 1 REV- AND DWG 186A1304 S
- [SDR SWAA2025051956227](https://openairdocs.org/sdr/SWAA2025051956227.md): Floorbeam · corroded · Apr 7, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CORROSION ON FLOOR BEAM LOCATED BS 986.5 RBL 43 WL 208.1 AT AFT GALLEY AREA 2025-242324<[01] STEP 8 TOOL USED: EDDY CURRENT FLAW DETECTOR. P/N: NORTEC 600D; S/N: 210138503; DUE DATE: 05-AUG-25.;[02] PERFORMED REPAIR ON FLOOR BEAM LOC. ON BS 986.5 RBL 43 WL 208
- [SDR SWAA2025051956234](https://openairdocs.org/sdr/SWAA2025051956234.md): Access Panel · cracked · Apr 7, 2025 · N282WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK AROUND HOLES ACCESS PANEL 561BB TRAILING EDGE AT LT WING 2025-242338<[01] TOOL USED: SCALE PN: CR5200 SN: 8343110809 DUE DATE: 06-MAR-26.;[02] TOOL USED: HOT BONDER P/N: HCS9200B; S/N: 18185847; DUE DATE: 01-OCT-25;[03] TOOL USED P/N: EPOCH 600; S/N: 120
- [SDR SWAA2025051956242](https://openairdocs.org/sdr/SWAA2025051956242.md): Floor Support · cracked · Apr 7, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT 2025-242368<[01] REPLACED WEB - INTERCOSTAL LOCATED BTW BS927 TO BS947.5 AND RBL21 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0 AND DWG 147A7500 SHEET 29 REV- AND S
- [SDR SWAA2025051956243](https://openairdocs.org/sdr/SWAA2025051956243.md): Keelbeam · cracked · Apr 7, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Keel
  > CRACK INTERNAL STRUCTURE KEEL BEAM LOCATED BTW BS727 TO BS727A AND STR27L AT AFT CARGO COMPARTMENT 2025-242372<[01] ON STEPS 4 AND 5; TOOL USED P/N: NORTEC 500D; S/N: N500X12101U102020; CAL DUE: 07-OCT-25.;[02] TOOLS USED TEMPERATURE CONTROLLED P/N: P3015GOES0
- [SDR SWAA2025051956206](https://openairdocs.org/sdr/SWAA2025051956206.md): Floorbeam · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ON FLOOR BEAM LOCATED BS 294.5 RBL 56 WL 208.1 AT FWD GALLEY AREA 2025-242295<[01] TOOL USED P/N: NORTEC 500D; S/N: N500X11290U021704; CAL DUE: 14-APR-25.;[02] REPAIRED FLOOR STRUCTURE BEAM LOCATED ON BS 294.5 RBL 20 TO RBL 64 WL 208.1 AT FWD GALLEY AREA
- [SDR SWAA2025051956204](https://openairdocs.org/sdr/SWAA2025051956204.md): Floorbeam · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACK ON ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX 2025-242293<[01] REPLACED ANGLE LOCATED BS 540 AND RBL 6 AT CENTER WING BOX IAW-B737-700-SRM-51-40-02-0G-0 AND EVALUATED CRACK AND NOT FOUND ALLOWABLE DAMAGE IAW-B737-700-SRM-51-10-02-0G-0 ANGLE MUST B
- [SDR SWAA2025051956208](https://openairdocs.org/sdr/SWAA2025051956208.md): Intercostal · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA 2025-242297<[01] REPLACED INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 15L AT FWD GALLEY AREA IAW B737-700 SRM 50-10-02-0G-0 ITEM 9 AND DWG 141A8180 SHEET 29
- [SDR SWAA2025051956201](https://openairdocs.org/sdr/SWAA2025051956201.md): Stub Frame · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATIONS(2EA) ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA.CRACK LENGTHS 1.812 IN. AND 0.437 IN. APROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD
- [SDR SWAA2025051956205](https://openairdocs.org/sdr/SWAA2025051956205.md): Stub Frame · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON STUB FRAME LOCATED BS 294.5 AT LEVEL STR 17R WL 208.1 AT FWD GALLEY AREA PERFORMED REPAIR ON STUB FRAME LOC. BS 294.5 AT LEVEL STR 17R WL 208.1 AT FWD GALLEY AREA IAW B737-700 SRM 53-10-15-2R-7 REPAIR 7. SEE INDIVIDUAL SIGN OFF BELOW.;[04] TASK COMPLE
- [SDR SWAA2025051956207](https://openairdocs.org/sdr/SWAA2025051956207.md): Intercostal · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON INTERCOSTAL LOCATED BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA 2025-242296<[01] REPLACED INTERCOSTAL LOC. BTW BS 294.5 TO BS 303.9 AT LEVEL STR 16L AT FWD GALLEY AREA IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A8180 SHEET 27 REV C; DW
- [SDR SWAA2025051956202](https://openairdocs.org/sdr/SWAA2025051956202.md): Support Angle · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN 2025-242298<[01] REPLACED NEW SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 10 WL 208.1 AT PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 AND DWG 143A5400 SHEET 38 REV A.SE
- [SDR SWAA2025051956203](https://openairdocs.org/sdr/SWAA2025051956203.md): Support Angle · cracked · Apr 6, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN 2025-242299<[01] REPLACED SUPPORT ANGLE LOCATED BTW BS 380 TO BS 400 RBL 41 WL 208.1 AT PASSENGER CABIN IAW-B737-700-SRM 51-40-02-0G-0 AND DWG # 143A5400 SHEET 38 REV- A. SE
- [SDR SWAA2025051956159](https://openairdocs.org/sdr/SWAA2025051956159.md): Angle · cracked · Apr 5, 2025 · N282WN · Boeing 7377H4 · Aerodynamic Fairings
  > CRACK ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L TO S-20L AT LOWER FUSELAGE 2025-242251<[01] REPLACED NEW ANGLE LOCATED BS 500D BODY FAIRING BETWEEN S-18L TO S-20L AT LOWER FUSELAGE IAW B737-700 SRM 51-40-02-0G-0 AND DWG 116A3110 SHEET 5 REV B; DWG 116A3
- [SDR SWAA2025051956156](https://openairdocs.org/sdr/SWAA2025051956156.md): Scuff Plate · cracked · Apr 5, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT. REPAIRED THE AFT CORNER SCUFF PLATE AT FWD CARGO COMPARTMENT IAW BOEING 737-700 SRM 53-30-15-2R-1 REPAIR 1 AND BAC 5975.
- [SDR SWAA2025051956183](https://openairdocs.org/sdr/SWAA2025051956183.md): Pressure Deck · cracked · Apr 5, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK INDICATION FOUND ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAIN WHEEL WELL COMPARTMENT. CRACK LENGTH: 0.250 IN. APPROX. PERFORMED PERMANENT REPAIR ON HORIZONTAL PRESSURE DECK WEB AT LBL 31 BETWEEN STA 663 TO STA 675 AT MAI
- [SDR SWAA2025051956151](https://openairdocs.org/sdr/SWAA2025051956151.md): Vapor Barrier · cracked · Apr 4, 2025 · N282WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK VAPOR BARRIER WEB LOCATED BS 663.75 RBL 25 AT MAIN WHELL WELL 2025-242190<[01] TOOL USED: CALIPER P/N: 500-197-30; S/N: A21147758; DUE DATE: 05 JAN 25.;[02] CORRECTED STEP 1 <BR>TOOL USED: CALIPER P/N: 500-197-30; S/N: A21147758; DUE DATE: 05 JAN 26.;[03
- [SDR SWAA2025052220787](https://openairdocs.org/sdr/SWAA2025052220787.md): Vapor Barrier · cracked · Apr 2, 2025 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK VAPOR BARRIER WEB LOCATED BS 663.75 RBL 25 AT MAIN WHELL WELL COMPARTMENT 2025-242107.
- [SDR SWAA2025051921217](https://openairdocs.org/sdr/SWAA2025051921217.md): Access Door · cracked · Apr 2, 2025 · N282WN · Boeing 7377H4 · Doors
  > CRACK ON ACCESS DOOR 732 ON LT MAIN LANDING GEAR 2025-242142<[01] ON STEP 6. TOOL USED: ET INSTRUMENT. P/N: NORTEC 600D. S/N: 210138503. DUE DATE: 05-AUG-25.;[02] TOOL USED ON STEP 10. ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-SEP-25;[
- [SDR SWAA2025032609517](https://openairdocs.org/sdr/SWAA2025032609517.md): Handle · broken · Mar 26, 2025 · N282WN · Boeing 7377H4 · Emergency Equipment
  > CREW REPORTS FWD MEGAPHONE HANDLE IS BROKEN.<[01] REMOVED AND REPLACED FWD MEGAPHONE PER AMM 25-64-00.
- [SDR SWAA2025022699969](https://openairdocs.org/sdr/SWAA2025022699969.md): Motor · inoperative · Feb 26, 2025 · N282WN · Boeing 7377H4 · Stabilizer Control System
  > ELECTRIC STAB TRIM INOP MANUAL TRIM NORMAL<[01]. REMOVED AND REPLACED STABILIZER TRIM MOTOR PER AMM 27-41-71. OPS CHECK GOOD.
- [SDR SWAA2025021094168](https://openairdocs.org/sdr/SWAA2025021094168.md): Battery Pack · inoperative · Feb 8, 2025 · N282WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTS FWD SECTION DOES NOT ILLUMINATE.<[01] REMOVED AND REPLACED EMERGENCY LIGHTS POWER SUPPLY BATTERY PACK IAW AMM 33-51-06. OP-CHECK GOOD.
- [SDR SWAA2025021094169](https://openairdocs.org/sdr/SWAA2025021094169.md): Panel · delaminated · Feb 8, 2025 · N282WN · Boeing 7377H4 · Aerodynamic Fairings
  > LEADING EDGE; EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BR EDGE EROSION AND DELAMINATION TO WING TO BODY FAIRING PANEL 192BR LEADING EDGE<[01] REMOVED 3 EA.CAMLOCK FASTENERS AND 1 EA. CAM LOCK GROMET TO F.O.M.;[02] REMOVED DAMAGE AT PANEL
- [SDR SWAA2024102551403](https://openairdocs.org/sdr/SWAA2024102551403.md): Threshold · cracked · Oct 21, 2024 · N282WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO REAR THRESHOLD CAP CRACKED<[01] UPDATED STEP 1;[02] REPLACED AFT CARGO REAR THRESHOLD CORNER CAP. DRILLED FASTENER HOLES IAW SRM 51-40-05
- [SDR SWAA2024072415237](https://openairdocs.org/sdr/SWAA2024072415237.md): Battery Pack · inoperative · Jul 22, 2024 · N282WN · Boeing 7377H4 · Emergency Lighting
  > MULTIPLE EMERGENCY LIGHTS INOP ON LH AFT SIDE.<[01] REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK M1673 PER AMM 33-51-06; OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024031563936](https://openairdocs.org/sdr/SWAA2024031563936.md): Vapor Barrier · cracked · Mar 15, 2024 · N282WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > RH WHEEL WELL FWD BULKHEAD VAPOR BARRIER PANEL HAS 2 CRACKS. ONE APPROXIMATELY 2 THE OTHER 4<[01] REPAIRED PER M-21-157-00675-REPREF.
- [SDR SWAA2024030860727](https://openairdocs.org/sdr/SWAA2024030860727.md): Bulb · inoperative · Mar 8, 2024 · N282WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AFT OF THE AFT ENTRY DOOR DOES NOT ILLUMINATE<[01] REMOVED AND REPLACED EMEGENCY LIGHT BULB ON LH EXTERIOR AFT OF L2 DOOR IN REFERENCE WITH AMM 33-51-04. OPS CHECK GOOD AT THIS TIME.
- [SDR SWAA2024021552518](https://openairdocs.org/sdr/SWAA2024021552518.md): Lamp · inoperative · Feb 15, 2024 · N282WN · Boeing 7377H4 · Emergency Lighting
  > AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOP.<[01] RELAMPED EXIT LIGHT PER AMM 33-51-04.
- [SDR SWAA2024010437683](https://openairdocs.org/sdr/SWAA2024010437683.md): Unknown · unknown · Jan 3, 2024 · N282WN · Boeing 7377H4 · Fuel Quantity Indicator
  > #1 FUEL TANK SHOWS APROX 2000 LBS LOWER FUEL QTY THAN #2 TANK IN CRUISE PERFORMED AMM 28-11-00 NO LEAKS NOTED. PERFORMED AMM 28 28-41-00 NO FAULTS AND QTY INDICATIONS ARE CORRECT. FUEL QTY MATCHES WITH PLANNED FUEL LOAD. C/W COND INSP 05-51-48 NO DEFECTS NOTED
- [SDR SWAA2023120728915](https://openairdocs.org/sdr/SWAA2023120728915.md): Idg · sheared · Dec 7, 2023 · N282WN · Boeing 7377H4 · AC Generator-Alternator
  > IN CRUISE #1 DRIVE LIGHT; #1 SOURCE LIGHT; & #1 GEN OFF BUS LIGHT ILLUMINATED; FOLLOWED PROCEDURE IN QRH. DISCONNECTED #1 DRIVE. DIVERTED TO MCI. PERFORMED NORMAL LANDING. ('NO OVERWEIGHT LANDING')<[01] TROUBLESHOT PER FIM 24-11 TASK 801. FOUND IDG FAULT. REMO
- [SDR SWAA2023071277411](https://openairdocs.org/sdr/SWAA2023071277411.md): Lens · out of adjust · Jul 12, 2023 · N282WN · Boeing 7377H4 · Emergency Lighting
  > 1ABC OVERHEAD BIN EMERGENCY LIGHT LENS IS PUSHED INTO BULLNOSE AND LOOSE.<[01] REPOSITION EMERGENCY LIGHT LENS COVER <BR>REF AMM 33-51-03;[02] C/W
- [SDR SWAA2023062170112](https://openairdocs.org/sdr/SWAA2023062170112.md): Pin · out of position · Jun 21, 2023 · N282WN · Boeing 7377H4 · Landing Gear Retraction/Extension System
  > LANDING GEAR LEVER WOULD NOT RAISE TO UP POSITION AFTER TAKEOFF. RAN QRH CHECKLIST. TAKEOFF WARNING HORN CONTINUED TO SOUND AFTER FLAPS UP. TAKEOFF WARNING CUTOUT CB PULLED IN ACCORDANCE WITH QRH RA N ALL APPROPRIATE CHECKLISTS (BRAKES ON SPD AT 65KTS)<[01] TR
- [SDR SWAA2023050124475](https://openairdocs.org/sdr/SWAA2023050124475.md): Bracket · elongated · Apr 6, 2023 · N282WN · Boeing 7377H4 · Aerodynamic Fairings
  > ELONGATED HOLES ON NEW BRACKET LOCATED ON WING TO BODY FAIRING AT LOWER FUSELAGE RH 2023-212859<[01] PERFORMED OVERSIZE HOLE ON BRACKET LOC WING TO BODY FAIRING RH SIDE AT LOWER FUSELAGE IAW B737-700 SRM 51-40-05 TABLE B; DIAMETER OF FASTENER NOT EXCEED MAXIMU

Next page: https://openairdocs.org/aircraft/N282WN/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 = 'N282WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N282WN/reports

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