# Service difficulty reports: N296WN

A list on [N296WN](https://openairdocs.org/aircraft/N296WN.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 · 272 reports

- [SDR SWAA2026092187992](https://openairdocs.org/sdr/SWAA2026092187992.md): Light · inoperative · Sep 15, 2026 · N296WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT SEAT 16FED IS INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IAW AMM 33-51-03-960-801. OP CHKD GOOD.
- [SDR SWAA2026060810077](https://openairdocs.org/sdr/SWAA2026060810077.md): Engine · failed · Jun 7, 2026 · N296WN · Boeing 7377H4 · Engine (Turbine/Turboprop)
  > NR 2 ENGINE FAILURE ON TAKE OFF ROLL AT APPROX 40 KTS; N1 & N2 BOTH INDICATED ZERO. AS SOON AS TOGA WAS SELECTED, THERE WAS A LOUD BANG FOLLOWED BY AN AGGRESSIVE YAW TO THE RT CONT: ABORTED TO AT THIS TIME. REFER TO MT# 771-00-01 FOR NR 2 ENGINE R & R. REFE
- [SDR SWAA2026031177605](https://openairdocs.org/sdr/SWAA2026031177605.md): Lamp · inoperative · Mar 8, 2026 · N296WN · Boeing 7377H4 · Emergency Lighting
  > L2 EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. R & R THE L2 EXTERIOR EMERGENCY EXIT LAMP IAW AMM 33-51-04. R & R THE BATTERY PACK & CHARGER ASSY IAW AMM 33-51-06; OPS CHECKED GOOD.
- [SDR SWAA2026021670373](https://openairdocs.org/sdr/SWAA2026021670373.md): Barrel Nut · broken · Feb 13, 2026 · N296WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER BROKEN. REPLACED FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER. IAW AMM 52-11-31.
- [SDR SWAA2026021671268](https://openairdocs.org/sdr/SWAA2026021671268.md): Retainer · broken · Feb 13, 2026 · N296WN · Boeing 7377H4 · Escape Slide
  > FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER BROKEN. REPLACED FWD ENTRY DOOR SLIDE BARREL NUT AND RETAINER IAW AMM 52-11-31.
- [SDR SWAA2025073091271](https://openairdocs.org/sdr/SWAA2025073091271.md): Plate · cracked · Jul 15, 2025 · N296WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKS ON PLATE ASSY- AT IRSS 199+17; FOR ATTACHMENT OF ACCESS PANEL 651EB INBOARD SIDE. REMOVED AND REPLACED THE RT WING I/B SIDE WIGGLE PLATE AT IRSS 199+17 FOR ACCESS PANEL 651EB IAW SRM 51-40-02-0G-0 STEP 4 AND IPC 57-50-00-22A. REMOVED AND REPLACED TH
- [SDR SWAA2025072990095](https://openairdocs.org/sdr/SWAA2025072990095.md): Fairing · cracked · Jul 11, 2025 · N296WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > NUMBER 1 ENG STRUT AFT FAIRING TRAILING EDGE IS CRACKED. R & R NR 1 ENG STRUT AFT FAIRING TRAILING EDGE IAW SRM 51-40-02-0G-0, & DWG 313A2400 REV A. ALL STEPS COMPLETE.
- [SDR SWAA2025072989360](https://openairdocs.org/sdr/SWAA2025072989360.md): Insert · damaged · Jul 9, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PANEL 241ABF AFT GIRT FITTING, AFT FASTENER HOLE 2-PIECE INSERT IS DAMAGED. REMOVED AND REPLACED DAMAGED INSERT FOR AFT GIRT FITTING ON PANEL 241ABF IAW SRM 53-00-50-2R-0 PARA 5B(2); PARA 5S AND DWG 147A5810-88.
- [SDR SWAA2025072988395](https://openairdocs.org/sdr/SWAA2025072988395.md): Seat Track · corroded · Jul 4, 2025 · N296WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 45, WL 208, BS 360+9 ON WELL, BS 360+14 ON CROWN BS 360+16 ON WELL, BS 380 ON CROWN & WELL, BS 400+1 ON CROWN & WELL, BS 420+11 ON CROWN. REMOVED CORROSION ON SEAT TRACK IAW SRM 53-00-52-1A-1. FOUND TO BE OUT OF
- [SDR SWAA2025072988004](https://openairdocs.org/sdr/SWAA2025072988004.md): Doubler · corroded · Jul 3, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > WIFI ANTENNA AREA; EXTERIOR FUSELAGE CROWN SKIN DOUBLER FOUND CORROSION AT STA 727C BTWN STGR 1 AND 2 RH AT SEVERAL FASTENERS. RESOLVE FAULT ON TTG8Q013J793 WHERE EA 25-153-01827.
- [SDR SWAA2025073187674](https://openairdocs.org/sdr/SWAA2025073187674.md): Seat Track · corroded · Jul 2, 2025 · N296WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 45 BS 360+9, 360+14, 360+16, 380, 400+1, 420+11, & 500A+4. WL 208. TASK TO BE ACCOMPLISHED ON CUSTOMER CARDS TTG8Q013JXQ1 AND TTG8Q013JWFT.
- [SDR SWAA2025072987675](https://openairdocs.org/sdr/SWAA2025072987675.md): Doubler · cracked · Jul 2, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > DURING OK TO INSTALL RT BS 663 RBL 6-32 LWR DOUBLER; FOUND DOUBLER CRACKED AT THE CORNER. REMOVED AND REPLACED ON FAULT TTG8Q013CQB6.
- [SDR SWAA2025072987671](https://openairdocs.org/sdr/SWAA2025072987671.md): Seat Track · corroded · Jul 2, 2025 · N296WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON PASSENGER SEAT TRACK AT RBL45 BS380+13 ON CROWN, BS400+10 ON CROWN, BS480+6 ON CROWN, BS500A+14 ON CROWN, BS520 ON WELL WL208. ACCOMPLISHED ON TASK CARDS TTG8Q013KMBX AND TTG8Q013KMB3.
- [SDR SWAA2025072987350](https://openairdocs.org/sdr/SWAA2025072987350.md): Seat Track · corroded · Jul 1, 2025 · N296WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION FOUND ON PASSENGER SEAT TRACK AT LBL 25 BS 360+10 ON CROWN AND WELL, BS 400 ON CROWN, BS 480+13 ON CROWN AND WELL, BS 500A+6 ON WELL; BS 500B+11 ON CROWN AND WELL AT WL 208 ACCOMPLISHED ON CUSTOMER CARDS TTG8Q013JXQP AND TTG8Q013JWGG.
- [SDR SWAA2025072986999](https://openairdocs.org/sdr/SWAA2025072986999.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 767, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1132 REV -.
- [SDR SWAA2025072987000](https://openairdocs.org/sdr/SWAA2025072987000.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727E, S5R. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1112 REV-.
- [SDR SWAA2025072987001](https://openairdocs.org/sdr/SWAA2025072987001.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727C, S6L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1103 REV. -
- [SDR SWAA2025072987002](https://openairdocs.org/sdr/SWAA2025072987002.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S7L. REMOVED AND REPLACED THE STRINGER CLIP IAW SRM 51-40-02 AND DWG 146A1102 REV.-.
- [SDR SWAA2025072987003](https://openairdocs.org/sdr/SWAA2025072987003.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN BS727E S-6L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1112 REV.-.
- [SDR SWAA2025072987004](https://openairdocs.org/sdr/SWAA2025072987004.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727E, S-5L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1112 REV.-.
- [SDR SWAA2025072987005](https://openairdocs.org/sdr/SWAA2025072987005.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN BS727D S-7L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1111 REV.-.
- [SDR SWAA2025072987006](https://openairdocs.org/sdr/SWAA2025072987006.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727B, S-6L. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-40-02 AND DWG NBR 146A1102 REV.-.
- [SDR SWAA2025072987007](https://openairdocs.org/sdr/SWAA2025072987007.md): Stringer Clip · cracked · Jun 30, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED STRINGER CLIP AT PAX CABIN, BS 727A S-7L. REMOVED AND REPLACED STR CLIP AT PAX CABIN BS 727A S-7L PER REF SRM 51-40-02 AND DWG NBR 146A1101 REV. -.
- [SDR SWAA2025072986189](https://openairdocs.org/sdr/SWAA2025072986189.md): Stiffener · cracked · Jun 27, 2025 · N296WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > CRACKED LOWER SIDE STIFFENER 3 AT INSPAR RIB 3 (STAB STA 111.10) - L/H HORIZONTAL STABILIZER. REPAIRED LOWER SIDE OF STIFFENER #3 AT INSPAR RIB #3(STAB STA 111.10) L/H HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-4.
- [SDR SWAA2025072993051](https://openairdocs.org/sdr/SWAA2025072993051.md): Flap Track · worn · Jun 27, 2025 · N296WN · Boeing 7377H4 · Trailing Edge Flaps
  > RIGHT WING I/B AFT FLAP O/B TRACK WORN ON LOWER FLANGE. REMOVED AND RE-INSTALLED RIGHT WING I/B AFT FLAP TO REPLACE WORN O/B TRACK IAW AMM 27-51-12-000-801; AMM 27-51-16-400-801 AND AMM 27-51-12-400-801.
- [SDR SWAA2025072986191](https://openairdocs.org/sdr/SWAA2025072986191.md): Floor Panel · delaminated · Jun 27, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241VF UPPER SKIN HAS AREAS OF DELAMINATION. REPLACED DAMAGED 241VF FLOOR PANEL WITH A NEW FLOOR PANEL IAW SRM 51-40-02-0G-0 PARA 9 AND AIPC 53-21-00-22 ITEM #161.
- [SDR SWAA2025073085564](https://openairdocs.org/sdr/SWAA2025073085564.md): Panel · delaminated · Jun 26, 2025 · N296WN · Boeing 7377H4 · Wing, Plate/Skin
  > PANEL 521CB FWD I/B CORNER DELAMINATED. REPAIRED PER [SRM 51-70-05-2R-6-A00737 (REPAIR 6 - REPAIR OF DAMAGE TO THE EDGEBAND OF A HONEYCOMB PANEL - AIRFRAME - PERMANENT) VERIFIED COMPLETE.
- [SDR SWAA2025073085852](https://openairdocs.org/sdr/SWAA2025073085852.md): Web · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > LEFT WING TRAIING EDGE TRANSVERSE WEB OTBD ATTACH ANGLE CRACKED. REMOVED & REPLACED A NEW ATTACH ANGLE AT LT WING T/E TRANSVERSE WEB OTBD SIDE IAW SRM 51-40-02 & DWG 115A6200 SH 11 REV:B.
- [SDR SWAA2025072985848](https://openairdocs.org/sdr/SWAA2025072985848.md): Floorbeam · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Floor Beam
  > CRACKED ON FLOORBEAM AT BS 328; RBL 18.5; WL208. REMOVED AND REPAIRED DAMAGE PART OF THE UPPER FLANGES FLOOR BEAM BS328 FROM RBL1-RBL60 WL208 I.A.W SRM 53-10-51-2R-7 REPAIR 7 ALTERNATIVE 2.
- [SDR SWAA2025072985850](https://openairdocs.org/sdr/SWAA2025072985850.md): Intercostal · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ON INTERCOSTAL AT BS 393; RBL 10; WL 208. REMOVED AND REPLACED INTERCOSTAL BS380-BS400 RBL8.2 WL208 I.A.W SRM 51-10-02-0G-0 PAR 9.C; SRM 51-40-02-0G-0 AND DWG 143A5400 REV:A.
- [SDR SWAA2025072985837](https://openairdocs.org/sdr/SWAA2025072985837.md): Scuff Plate · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FWD ENTRY DOOR FWD LOWER SCUFF PLATE IS CRACKED ON AFT EDGE. REPAIRED CRACKED FED FWD SCUFF PLATE PER EA 25-153-01771-WIP1; ACCOMPLISHED ON TASK ID TTG8Q013H6V.
- [SDR SWAA2025072985841](https://openairdocs.org/sdr/SWAA2025072985841.md): Bulkhead Web · corroded · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > 1016 BULKHEAD WEB HAS CORROSION BS 1020; LBL 9; WL 208. REMOVED DAMAGE ON BULKHEAD WEB BS 1029 LBL 9+ WL 208 2.0'X1.0'WITH.003' MATERIAL REMOVED. ORIGINAL MATERIAL THICKNESS OF.040. NO ALLOWABLE LIMITS. REPAIRED PER EA 25-153-01785 ON TTG8Q0013MR43.
- [SDR SWAA2025072985563](https://openairdocs.org/sdr/SWAA2025072985563.md): Beam · corroded · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Structure
  > BS 986 BEAM PREVIOUS REPAIR IS CORRODED ON UPPER SURFACE AND BETWEEN REPAIR PARTS FROM RBL 42 TO RBL 45, WL 207.9 TO WL 208.1. DISCREPANCY AREA TO BE REMOVE AND REPAIRED FROM BS 986, RBL 25-RBL 50, WL208 ON CCN TTG8Q013DS97 DUE TO ADJACENT DAMAGE REPORTED EXC
- [SDR SWAA2025072985834](https://openairdocs.org/sdr/SWAA2025072985834.md): Scuff Plate · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO BAY AFT CORNER SCUFF PLATE IS CRACKED. REPAIRED IAW SRM 53-60-15-2R-1. SCUFF PLATE WILL BE INSTALLED ON CUSTOMER CARD TTG8Q013BV69.
- [SDR SWAA2025072985845](https://openairdocs.org/sdr/SWAA2025072985845.md): Tail Cone · cracked · Jun 26, 2025 · N296WN · Boeing 7377H4 · Aerodynamic Fairings
  > PERFROM PERMENANT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE. ACCOMPLISHED PERMANENT REPAIR TO 1 INCH CRACK ON TOP LEFT SIDE OF TAILCONE IAW SRM 51-70-05-2R-2.
- [SDR SWAA2025073185555](https://openairdocs.org/sdr/SWAA2025073185555.md): Attach Angle · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CORROSION AFT CARGO BAY ATTACH ANGLE UNDER SHIELD, HAS MULTIPLE AREAS UNDER NUT PLATES BS 767 TO BS 787, RBL21, WL156. CORROSION ON AFT CARGO BAY ATTACH ANGLE UNDER SHIELD FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS AS GIVEN IN SRM. REMOVED, REPLACED, & INS
- [SDR SWAA2025072985369](https://openairdocs.org/sdr/SWAA2025072985369.md): Floor Panel · delaminated · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241TF HAS DELAMINATION. REMOVED CABIN FLOOR PANEL 241TF IAW AMM 53-21-00-000-801. REPAIRED AND REINSTALLED FLOOR PANEL 241TF PER AMM 53-21-00-400-801.
- [SDR SWAA2025072985368](https://openairdocs.org/sdr/SWAA2025072985368.md): Floor Panel · delaminated · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241SF HAS DELAMINATION. REMOVED CABIN FLOOR PANEL 241SF IAW AMM 53-21-00-000-801. DUE TO THE EXTENT OF DAMAGE; REPLACED PASSENGER CABIN FLOOR PANEL 241SF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-22 ITEM 121.
- [SDR SWAA2025072985365](https://openairdocs.org/sdr/SWAA2025072985365.md): Floor Panel · delaminated · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 242AF HAS DELAMINATION. REPLACED WITH A SERVICEABLE FLOOR PANEL PER SRM 51-10-02-0G-0 PARA 9.A.1 DUE TO AMOUNT OF ALL DAMAGE.
- [SDR SWAA2025072985366](https://openairdocs.org/sdr/SWAA2025072985366.md): Floor Panel · delaminated · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241BF HAS DELAMINATION. DUE TO THE EXTENT OF DAMAGE, REPLACED THE FLOOR PANEL 241BF IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM 65.
- [SDR SWAA2025072985556](https://openairdocs.org/sdr/SWAA2025072985556.md): Support Plate · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION FWD CARGO BAY LT FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS 400 TO BS 500D LBL22 WL156, FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW L/H FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0 AND DWG 143
- [SDR SWAA2025072985553](https://openairdocs.org/sdr/SWAA2025072985553.md): Support Plate · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 LBL22 WL156. EVALUATED; LOCATED; DRILLED; REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0; SRM 51-40
- [SDR SWAA2025072985554](https://openairdocs.org/sdr/SWAA2025072985554.md): Support Plate · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY R/H FLOOR TO SIDEWALL SUPPORT PLATE HAS MULTIPLE AREAS AROUND NUT PLATE HOLES BS727B TO BS767 RBL22 WL156, FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED; AND INSTALLED NEW FLOOR TO SIDEWALL SUPPORT PLATE IAW SRM 51-40-02-0G-0 AND DWG 14
- [SDR SWAA2025072985557](https://openairdocs.org/sdr/SWAA2025072985557.md): Shield · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY SHIELD FWD OF CARGO DOOR AROUND MULTIPLE NUT PLATE HOLES BS767+3 TO BS794 RBL22 WL156, FOUND TO BE OUT OF LIMITS DUE TO NO LIMITS ARE GIVEN IN THE SRM. REMOVED; REPLACED AND INSTALLED NEW SHIELD IAW SRM 51-40-02-0G-0; AND DWG 146A0081
- [SDR SWAA2025072985558](https://openairdocs.org/sdr/SWAA2025072985558.md): Strap · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION AFT CARGO BAY ON TIE STRAP BS 787+16, RBL 20, WL 156, FOUND TO BE OUT OF LIMITS. REMOVED; REPLACED AND INSTALLED NEW TIE STRAP IAW SRM 51-40-02-0G-0; DWG 146A8340 REV -, DWG 146A0081, REV A, AND DWG 146A8120, REV -.
- [SDR SWAA2025072985356](https://openairdocs.org/sdr/SWAA2025072985356.md): Attach Angle · cracked · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > LANDING GEAR MANUAL EXTENSION CONTROL DRUM BOX ATTACH ANGLE CRACKED AT BS 253, RBL 7, WL 207. REMOVED AND REPLACED LANDING GEAR MANUAL EXTENSION CONTROL DRUM ATTACH ANGLE IAW SRM 51-40-02-0G-0 AND DWG 141A0631 REV D, DWG 141A5100 REV C.
- [SDR SWAA2025072985560](https://openairdocs.org/sdr/SWAA2025072985560.md): Strap · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT BS719; RBL66; WL203. REMOVED AND TREATED PER EA 25-153-01775-WIP1; TASK ID TTG8Q013HMEX; AND WIP2; TASK ID TTG8Q013QUEY.
- [SDR SWAA2025072985561](https://openairdocs.org/sdr/SWAA2025072985561.md): Strap · corroded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON STRAP AT MID CABIN BS696 LBL66 WL203. IAW EA 25-153-01786; THE REWORK IS ACCEPTABLE AS A CONTINUE-IN-SERVICE CONDITION WITHOUT REPETITIVE INSPECTIONS AND NO TERMINATING ACTION REQUIREMENTS.
- [SDR SWAA2025072985562](https://openairdocs.org/sdr/SWAA2025072985562.md): Attach Angle · cracked · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Attach Fittings
  > CRACKED ATTACH ANGLE AT MID CABIN BS 691, RBL1, WL206. REMOVED, FABRICATED, AND REPLACED ATTACH ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, BOEING 111A6000 REV -, DWG 273A9112, REV -, DWG 273A9112, REV H.
- [SDR SWAA2025072985125](https://openairdocs.org/sdr/SWAA2025072985125.md): Panel · debonded · Jun 25, 2025 · N296WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > PANEL 193AR OUTER SKIN IS DISBONDED. REPAIRED IAW SRM 51-70-05-2R-4.

Next page: https://openairdocs.org/aircraft/N296WN/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 = 'N296WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N296WN/reports

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