# Service difficulty reports: N283WN

A list on [N283WN](https://openairdocs.org/aircraft/N283WN.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 · 288 reports

- [SDR SWAA2026100570883](https://openairdocs.org/sdr/SWAA2026100570883.md): Ballast · intermittent · Oct 1, 2026 · N283WN · Boeing 7377H4 · Emergency Lighting
  > WING DOOR EMERGENCY EXIT LIGHT, RT SIDE, IS INTERMITTENT. LAMPS OPERATE NORMAL IAW AMM 33-51-00. WINDOW LIGHT AT THIS POSITION IS FOUND TO BE INOPERATIVE. OK TO CONTINUE IAW MEL 33-2-03. SP1B. R & R THE BALLAST IAW AMM 33-21-00. REMOVED MEL.
- [SDR SWAA2026092991980](https://openairdocs.org/sdr/SWAA2026092991980.md): Vapor Barrier · cracked · Sep 25, 2026 · N283WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > FOUND 12 INCH CRACK ON THE VAPOR BARRIER WEB, RBL 40, 40 INCHES DOWN FROM WL. REACCESSED DAMAGE, CRACK FOUND TO BE 18+ INCHES. C/W REPAIR IAW EA 26-157-02619.
- [SDR SWAA2026092125651](https://openairdocs.org/sdr/SWAA2026092125651.md): Wedge · delaminated · Sep 18, 2026 · N283WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT INBD FLAP, AFT OTBD TRAILING EDGE SHOWS EVIDENCE OF DELAMINATION. REMOVED THE FLAP WEDGE. LOCATED & INSTALLED NUTPLATES TO NEW WEDGE IAW SRM 51-40-10. INSTALLED A SERVICEABLE FLAP WEDGE IAW SRM 51-40-02. APPLIED FILLET SEAL TO THE RT INBD MAIN FLAP W
- [SDR SWAA2026082514816](https://openairdocs.org/sdr/SWAA2026082514816.md): Probe · out of tolerance · Aug 23, 2026 · N283WN · Boeing 7377H4 · Engine EGT/TIT Indicating System
  > NR 2 ENGINE RED BOX ON TAKEOFF. C/W ENGINE EXCEEDANCE REVIEW IAW AMM 71-00-00, FOUND EGT MAX OF 965 DEG FOR 5 SECONDS. FOUND S2 EGT PROBE OUT OF TOLERANCE. C/W FIM TASK 77-21, TASK 802 EGT PROBES READING NORMAL. RESET ENG EXCEEDANCE PAGE. ACFT OK FOR SERVI
- [SDR SWAA2026062314238](https://openairdocs.org/sdr/SWAA2026062314238.md): Light · inoperative · Jun 20, 2026 · N283WN · Boeing 7377H4 · Emergency Lighting
  > FOUND EMERGENCY EXIT LIGHT INOP OUTSIDE OF LEFT ENTRY DOOR. RELAMPED EMERGENCY EXIT LIGHT OUTSIDE OF LEFT ENTRY DOOR IAW AMM 33-51-04. OPS CHECKED GOOD. NO FURTHER DEFECTS NOTED.
- [SDR SWAA2025111334131](https://openairdocs.org/sdr/SWAA2025111334131.md): Light · inoperative · Nov 12, 2025 · N283WN · Boeing 7377H4 · Emergency Lighting
  > PASSENGER CABIN LT EMERGENCY EXIT DOOR LIGHT INOPERATIVE. R & R CABIN OVERWING EXIT LIGHT PER AMM 33-51-04.
- [SDR SWAA2025100922994](https://openairdocs.org/sdr/SWAA2025100922994.md): Coalescer Bag · dirty · Oct 8, 2025 · N283WN · Boeing 7377H4 · Humidity Control System
  > PUNGENT DIRTY SOCK SMELL IN COCKPIT DURING CLIMB AND DECENT. R & R CABIN AIR FILTER IAW AMM 21-25-01, UPON FURTHER EVALUATION; FOUND LT COALESCER BAG VERY DIRTY. R & R LT AND RT WATER SEPARATOR COALESCER BAGS IAW AMM 21-51-05. PERFORMED ENG RUN ON BOTH EN
- [SDR SWAA2025090812025](https://openairdocs.org/sdr/SWAA2025090812025.md): Girt Bar · fod · Sep 6, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > FWD SERVICE DOOR GIRT BAR STICKING. CLEANED AND REMOVED DEBRIS ON FWD SERVICE DOOR GIRT BAR PER SIP.
- [SDR SWAA2025042119351](https://openairdocs.org/sdr/SWAA2025042119351.md): Stringer Splice · corroded · Mar 29, 2025 · N283WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CORROSION ON SPLICE LOCATED AT STRINGER 27R BSTA 360 PLUS 2 INCHES AT ELECTRONIC COMPARTMENT. REPLACED SPLICE AND FASTENERS; LOCATED AT STRINGER 27R BSTA 360 PLUS 2 INCHES AT ELECTRONIC COMPARTMENT IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG 140A91
- [SDR SWAA2025042207984](https://openairdocs.org/sdr/SWAA2025042207984.md): Bracket · cracked · Mar 21, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON BRACKET LOC. VAPOR BARRIER BTW LBL54.21 TO LBL 45.64 2025-202969<1. REPLACED BRACKET LOC. ON VAPOR BARRIER STA 663 FWD SIDE AND BTW LBL54.21 TO LBL 45.64 I.A.W B737-700 SRM 51-40-02 AND DWG 111A1001 SHEET 462 REV-.
- [SDR SWAA2025042207594](https://openairdocs.org/sdr/SWAA2025042207594.md): Battery Pack · inoperative · Mar 20, 2025 · N283WN · Boeing 7377H4 · Emergency Lighting
  > INOP BATTERY PACK ON BS 616 LH SIDE AT PASSENGER CABIN. 2025-202955<REPLACED BATTERY PACK ON BS 616 LH SIDE AT PASSENGER CABIN IAW B737-700 AMM 33-51-06-960-805 OLD PART P/N: D717-01-100SWA S/N: WN3725 NEW PART P/N: AD-D717-01-100SWA S/N: BN 591477 TEST IS OK
- [SDR SWAA2025042205789](https://openairdocs.org/sdr/SWAA2025042205789.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA 2025-202752<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TT
- [SDR SWAA2025042205788](https://openairdocs.org/sdr/SWAA2025042205788.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA 2025-202751<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8
- [SDR SWAA2025042205787](https://openairdocs.org/sdr/SWAA2025042205787.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA 2025-202749<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TT
- [SDR SWAA2025042205786](https://openairdocs.org/sdr/SWAA2025042205786.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA 2025-202748<REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0028RSF S
- [SDR SWAA2025042205657](https://openairdocs.org/sdr/SWAA2025042205657.md): Support Angle · cracked · Mar 15, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON SUPPORT ANGLE LOCATED BTW BS 927 TO BS 947.5 BL 0 WL 208.1 AT AFT GALLEY AREA. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED BTW BS 927 TO BS 947.5 BL 0 WL 208.1 AT AFT GALLEY AREA IAW B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9; DWG 147A5400; SHEET 2
- [SDR SWAA2025042205782](https://openairdocs.org/sdr/SWAA2025042205782.md): Bracket · cracked · Mar 15, 2025 · N283WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 11
- [SDR SWAA2025042105784](https://openairdocs.org/sdr/SWAA2025042105784.md): Angle · cracked · Mar 15, 2025 · N283WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202806<[01] INSTALL NEW ANGLE AND PLATE LOC. ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING I.A.W B737-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2930 SHEET 7 REV
- [SDR SWAA2025042114956](https://openairdocs.org/sdr/SWAA2025042114956.md): Support Bracket · cracked · Mar 15, 2025 · N283WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT BRACKET TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING 2025-202807<[01] REPLACE SUPPORT BRACKET ON TRAILING EDGE ORSS 271 DEFLECTION CONTROL RIB AREA RT WING; IAW BOEING 737-700 SRM 51-10-02-0G-0 STEP 9 AND SRM 51-40-02-0G ALSO DWG 11
- [SDR SWAA2025041714960](https://openairdocs.org/sdr/SWAA2025041714960.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA 2025-202748 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK CARD TTG8Q0
- [SDR SWAA2025041714961](https://openairdocs.org/sdr/SWAA2025041714961.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA 2025-202749 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT AFT GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK
- [SDR SWAA2025041714962](https://openairdocs.org/sdr/SWAA2025041714962.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA 2025-202751 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS ENTRY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK C
- [SDR SWAA2025041714963](https://openairdocs.org/sdr/SWAA2025041714963.md): Bracket · deteriorated · Mar 15, 2025 · N283WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA 2025-202752 <[01]. REPLACED HARDWARE GIRT BAR FLOOR BRACKETS GALLEY DOOR SIDE AT FWD GALLEY AREA IAW B737-700 AMM 25-66-02-400-801 THE INSTALLATION IS TO BE ACCOMPLISHED ON TASK
- [SDR SWAA2025042205333](https://openairdocs.org/sdr/SWAA2025042205333.md): Flap · debonded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Trailing Edge Flaps
  > CUSTOMER REQUEST- DEBONDED OB AFT FLAP IB SIDE AT LT WING 2025-202755 <[01]. TOOL USED; CALIPER PN: 500-196-30; SN: A21334230; DUE DATE: 23-MAY-25.; [02] TOOL USED: AUDIBLE BOND TESTER; P/N: S-3; S/N: 064; DUE DATE: 27-AUG-25.; [03] TOOL USED HOT BONDER: P/N:
- [SDR SWAA2025042205331](https://openairdocs.org/sdr/SWAA2025042205331.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202753<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25
- [SDR SWAA2025042205327](https://openairdocs.org/sdr/SWAA2025042205327.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES AT AFT CARGO COMPARTMENT 2025-202744 CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT<
- [SDR SWAA2025042205478](https://openairdocs.org/sdr/SWAA2025042205478.md): Stringer Clip · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA 2025-202770<[01] REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG # 141A1110 SHEET 18 REV -.<BR>SEE INDI
- [SDR SWAA2025042205482](https://openairdocs.org/sdr/SWAA2025042205482.md): Support · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA 2025-202773<1. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G, SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A.
- [SDR SWAA2025042205481](https://openairdocs.org/sdr/SWAA2025042205481.md): Support Angle · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA 2025-202772<[01] REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING 143A5400 REV: A.
- [SDR SWAA2025042205480](https://openairdocs.org/sdr/SWAA2025042205480.md): Support · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA 2025-202771 <[01]. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG 143A5400 SHEET 92. SE
- [SDR SWAA2025042205477](https://openairdocs.org/sdr/SWAA2025042205477.md): Plate · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2025-202769 <[01]. REPLACED PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 1
- [SDR SWAA2025042205485](https://openairdocs.org/sdr/SWAA2025042205485.md): Skin · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781 <[01]. TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE:
- [SDR SWAA2025042205339](https://openairdocs.org/sdr/SWAA2025042205339.md): Web · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT 2025-202766<REPLACED WEB LOCATED CEILING AREA BTW BS 847 TO BS 867 LBL 21 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02, SRM 51-10-02 ITEM 9 AND DWG 149A8100 SHEET 1
- [SDR SWAA2025042205334](https://openairdocs.org/sdr/SWAA2025042205334.md): Web · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT 2025-202762<[01] REPLACED WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 146
- [SDR SWAA2025042205328](https://openairdocs.org/sdr/SWAA2025042205328.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727D PLUS 9 INCHES TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202745<[01] REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:146A
- [SDR SWAA2025042205336](https://openairdocs.org/sdr/SWAA2025042205336.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202750<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25. FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW]
- [SDR SWAA2025042205330](https://openairdocs.org/sdr/SWAA2025042205330.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727A TO BS 727C LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202747<[01] TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25 2. REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22 WL 15
- [SDR SWAA2025042105335](https://openairdocs.org/sdr/SWAA2025042105335.md): Cargo Track · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK TRACK LBBL 17.24 LOCATED STA 727E AFT CARGO COMPARTMENT CRACK TRACK LBL 17.24. PERFORMED PERMANENT REPAIR ON TRACK LBBL 17.24 LOCATED BTW BS 727D+12? TO BS 727E+10.5? AT AFT CARGO COMPARTMENT IAW B737-700 SRM SRM 53-00-53-2R-3; REPAIR 3. FIGURE 203; SH
- [SDR SWAA2025042114947](https://openairdocs.org/sdr/SWAA2025042114947.md): Tie Clip · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ON TIE CLIP LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA. REPLACED TIE CLIP AND FASTENERS LOCATED BS 277 AT LEVEL STR 10R AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 ITEM 9; SRM 51-40-02; DWG # 141A1110 SHEET 18 REV -.
- [SDR SWAA2025042114948](https://openairdocs.org/sdr/SWAA2025042114948.md): Support Angle · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND BL 0 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02-0G AND DWG 143A5400 SHEET 92.
- [SDR SWAA2025042114949](https://openairdocs.org/sdr/SWAA2025042114949.md): Support Angle · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA. REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND RBL AND RBL 10 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02 AND DRAWING 143A5400 REV: A.
- [SDR SWAA2025042114950](https://openairdocs.org/sdr/SWAA2025042114950.md): Support Angle · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA 2025-202773<[01] REPLACED ANGLE - SUPPORT LOCATED BTW STA 380 TO STA 400 AND LBL 13 AT FWD GALLEY AREA IAW B737-700 SRM 51-10-02-0G; SRM 51-40-02 AND DWG 143A5400 SHEET 38 REV A
- [SDR SWAA2025042114946](https://openairdocs.org/sdr/SWAA2025042114946.md): Plate · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT 2025-202769<[01] REPLACED PLATE LOCATED BTW STA 792 TO STA 807 STR 25R AND WL 156.4 AT AFT CARGO COMPARTMENT IAW B737-700 SRM 51-10-02; SRM 51-40-02 AND DRAWING # 146A
- [SDR SWAA2025042114953](https://openairdocs.org/sdr/SWAA2025042114953.md): Skin · cracked · Mar 14, 2025 · N283WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK FOUND ON LH HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT STATION 193.90 RIB; 17.5 INCHES FROM FRONT SPAR; INB SIDE OF RIB LENGTH APPROX= 1.100 INCHES. 2025-202781<[01] TOOL USED ON STEP 5 ET EQUIPMENT: P/N: NORTEC 600D; S/N: 60007161486; CAL DUE DATE: 06-
- [SDR SWAA2025041714936](https://openairdocs.org/sdr/SWAA2025041714936.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES AT AFT CARGO COMPARTMENT 2025-202744 CORROSION SUPPORT ZEE LOCATED BTW BS 727B PLUS 9 INCHES TO BS 727D PLUS 9 INCHES RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT <[01]. FAULT RESOLV
- [SDR SWAA2025041714937](https://openairdocs.org/sdr/SWAA2025041714937.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE LOCATED BTW BS 727D PLUS 9 INCHES TO BS 767 RBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202745 <[01]. REPLACED SUPPORT ZEE LOCATED BS727 TO BS767 AT LEVEL STR25R AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02; SRM 51-40-02 AND DWG:1
- [SDR SWAA2025041714938](https://openairdocs.org/sdr/SWAA2025041714938.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727A TO BS 727C LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202747 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] REPLACED SUPPORT ZEE LOCATED BTW BS 727 TO BS 847 LBL 22
- [SDR SWAA2025041714942](https://openairdocs.org/sdr/SWAA2025041714942.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727C TO BS 727E LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202750 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW];
- [SDR SWAA2025041714939](https://openairdocs.org/sdr/SWAA2025041714939.md): Support · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON SUPPORT ZEE LOCATED BTW BS 727E TO BS 767 LBL 22 WL 156.1 AT AFT CARGO COMPARTMENT 2025-202753 <[01]. TOOL USED IN STEP 3: UT EQUIPMENT; P/N: 45MG; S/N: 130066701 DUE DATE: 12-JUL-25; [02] FAULT WAS RESOLVED ON ANOTHER FAULT SEE [TTG8Q00Z96UW]; [
- [SDR SWAA2025041514941](https://openairdocs.org/sdr/SWAA2025041514941.md): Web · corroded · Mar 14, 2025 · N283WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT 2025-202762<[01] REPLACED WEB LOCATED BTW STA 767 TO STA 792 AND STR 25R WL 156.4 AT AFT CARGO COMPARTMENT I.A.W B737-700 SRM 51-10-02 Ï¿½TEM 9; SRM 51-40-02 AND DWG 146

Next page: https://openairdocs.org/aircraft/N283WN/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 = 'N283WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N283WN/reports

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