# Service difficulty reports: N295WN

A list on [N295WN](https://openairdocs.org/aircraft/N295WN.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 · 291 reports

- [SDR SWAA2026072005218](https://openairdocs.org/sdr/SWAA2026072005218.md): Seat Back · out of adjust · Jul 15, 2026 · N295WN · Boeing 7377H4 · Passenger Compartment Equipment
  > EXIT ROW SEAT 14B RECLINES REMOVED SEAT RECLINE FEATURE AT 14B IAW CMM 25-21-42 IAW CMM 25-21-42. 02.
- [SDR SWAA2026071694829](https://openairdocs.org/sdr/SWAA2026071694829.md): Holder · faulted · Jul 12, 2026 · N295WN · Boeing 7377H4 · Emergency Equipment
  > GIRT BAR STUCK. REMOVED GIRT BAR FROM SLIDE BOX GIRT BAR HOLDER IAW AMM 25-66-01.
- [SDR SWAA2026032582825](https://openairdocs.org/sdr/SWAA2026032582825.md): Ballast · overtemp · Mar 24, 2026 · N295WN · Boeing 7377H4 · Passenger Compartment Lighting
  > PLASTIC BURNING SMELL IN AFT GALLEY. PERFORMED CONDITIONAL INSPECTION 05-51-56. FOUND AFT ENTRY LIGHT BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST AND LAMPS PER AMM 33-29-00
- [SDR SWAA2026032583093](https://openairdocs.org/sdr/SWAA2026032583093.md): Ballast · overtemp · Mar 24, 2026 · N295WN · Boeing 7377H4 · Passenger Compartment Lighting
  > PLASTIC BURNING ODOR IN AFT GALLEY. PERFORMED CONDITIONAL INSPECTION 05-51-56. FOUND AFT ENTRY LIGHT BALLAST OVERHEATED. REMOVED AND REPLACED BALLAST AND LAMPS PER AMM 33-29-00
- [SDR SWAA2025120140670](https://openairdocs.org/sdr/SWAA2025120140670.md): Pressure Switch · faulted · Nov 28, 2025 · N295WN · Boeing 7377H4 · APU Oil System
  > APU LOW OIL PRESSURE LIGHT ILLUMINATED IN CRUISE, RESULTING IN SINGLE ELECTRICAL SOURCE. OVERWEIGHT LANDING PERFORMED IAW AOM 12-1-7. SMLDW EXCEEDED BY 10.3. SERVICED APU OIL & REPLACED LOW OIL PRESSURE SWITCH. CHKD GOOD IAW AMM 49-94-22
- [SDR SWAA2025102226015](https://openairdocs.org/sdr/SWAA2025102226015.md): Handle · loose · Oct 19, 2025 · N295WN · Boeing 7377H4 · Emergency Exits
  > FO SIDE OVER WING EMERGENCY EXIT DOOR HANDLE LOOSE. REINSTALLED STRAP COVER ON FO SIDE EMERGENCY EXIT DOOR IAW AMM 52-22-00.
- [SDR SWAA2025063076680](https://openairdocs.org/sdr/SWAA2025063076680.md): Skin · corroded · May 30, 2025 · N295WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > AAI: AFT CARGO COMPARTMENT; INTERNAL SKIN SURFACE HAS CORROSION BWT STA 747 & STA 767; STR 27L & STR 27R. PERFORMED PERMANENT REPAIR ON AFT CARGO COMPARTMENT INTERNAL SKIN SURFACE BWT STA 747 & STA 767; STR 27L & STR 27R IAW EA 25-153-01624.
- [SDR SWAA2025063076455](https://openairdocs.org/sdr/SWAA2025063076455.md): Floor Support · cracked · May 30, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AAI: MAIN CABIN; FLOOR STRUCTURE SUPPORT HAS CRACK AT STA 540; BL 0 TO RBL 24.75. REPLACED FLOOR STRUCTURE SUPPORT LOCATED PASSENGER CABIN FLOOR STRUCTURE STA540 BL 0 TO RBL 24.75 AND FASTENERS IAW B737-700 SRM 51-40-02;DWG 143A5240 SHEET: 13 REV: - AND 143A0
- [SDR SWAA2025063076575](https://openairdocs.org/sdr/SWAA2025063076575.md): Access Panel · damaged · May 30, 2025 · N295WN · Boeing 7377H4 · Trailing Edge Flaps
  > ELONGATED HOLE ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-335666<[01] TOOL USED CALIPER P/N 500-197-30 S/N B20189334 DUE DATE 26 JAN 26;[02] TOOL USED ON STEP 12:ULTRASONIC EQUIPMENT P/N:EPOCH 650; S/N:201036102; DUE DATE:25-OCT-25.;[03] TOOL USED: HUMID
- [SDR SWAA2025063075332](https://openairdocs.org/sdr/SWAA2025063075332.md): Skin Panel · cracked · May 27, 2025 · N295WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK INDICATION FOUND ON LT HORIZONTAL STABILIZER LOWER SKIN PANEL. LOCATED AT STAB STA 193.9 RIB AND 16.0 INCH. FROM FRONT SPAR. INBOARD SIDE OF RIB. CRACK LENGTH = 0.600 INCH. APPROX. 2025-335643 <[01] TOOL USED ON STEP 5 AND 6: ET EQUIPMENT; PN: NORTEC600D
- [SDR SWAA2025063075152](https://openairdocs.org/sdr/SWAA2025063075152.md): Floor Support · cracked · May 25, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 312 TO BS 328 AND RBL 29 FWD GALLEY AREA. REPLACED INTERCOSTAL LOCATED ON FLOOR STRUCTURE BTW BS 312 TO BS 328 AND RBL 29 FWD GALLEY AREA IAW B737-700 SRM 51-40-02 AND DWG 141A5400 SHEET 39 REV -.
- [SDR SWAA2025063074471](https://openairdocs.org/sdr/SWAA2025063074471.md): Plate · cracked · May 23, 2025 · N295WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK OUTBOARD TRAILING EDGE CORRUGATED PLATE LOCATED AT ORSS 297 AT LT WING 2025-335620<[01] REPLACED CORRUGATED PLATE LOCATED AT ORSS 297 AT LT WING IAW B737-700 SRM 51-10-02-0G ITEM 9 SRM 51-40-02-0G AND DWG 115A3760 SHEET: 15 REV: A. MEASURE CRACK IS 0.650
- [SDR SWAA2025063076453](https://openairdocs.org/sdr/SWAA2025063076453.md): Support Bracket · cracked · May 23, 2025 · N295WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame
  > CRACK OUTBOARD FAN COWL HOLD OPEN ROD SUPPORT BRACKET AFT POSITION ON ENGINE 1. REPLACED SUPPORT BRACKET LOC. FAN COWL HOLD OPEN ROD AFT POSITION ON ENGINE 1 IAW B737-700 SRM 51-40-02-0G-0. MEASURE OF CRACK IS: L= 0.950.
- [SDR SWAA2025062774462](https://openairdocs.org/sdr/SWAA2025062774462.md): Access Panel · cracked · May 23, 2025 · N295WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACK AROUND HOLES OF ACCESS PANEL 661BB TRAILING EDGE AT RT WING 2025-335601<
- [SDR SWAA2025063074220](https://openairdocs.org/sdr/SWAA2025063074220.md): Shield · cracked · May 22, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT 2025-335533 <[01]. REPLACED SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 AT FWD CARGO COMPARTMENT IAW-B737-700-SRM-51-10-02-0G ITEM 9; SRM 51-40-02-0G AND DWG#
- [SDR SWAA2025063074218](https://openairdocs.org/sdr/SWAA2025063074218.md): Web · corroded · May 22, 2025 · N295WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CORROSION WEB DOOR CUT OUT LOCATED STA827 AND RBL64 WL200 AT AFT CARGO COMPARTMENT 2025-335528 <[01]. REPLACED WEB DOOR CUT OUT LOCATED STA 767 AND 847 RBL 64 WL 200 AFT CARGO COMPARTMENT IAW B737-700 SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG 146A81
- [SDR SWAA2025063074223](https://openairdocs.org/sdr/SWAA2025063074223.md): Fairing · cracked · May 22, 2025 · N295WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACK ON INTERNAL SKIN OF ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING 2025-335582<[01] REPAIRED ACCESS PANEL 644BB FLAP SUPPORT FAIRING 8 AT RT WING IAW 25-157-01493-WIP. SEE INDIVIDUAL SIGNOFFS BELOW;[02] REPAIRED ACCESS PANEL 644BB FLAP SUPPORT FAIR
- [SDR SWAA2025063073730](https://openairdocs.org/sdr/SWAA2025063073730.md): Angle · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Aircraft Structures
  > CRACK REAR SPAR ANGLE LOCATED ON IRSS 148 AT MAIN LANDING GEAR AREA AT LT WING 2025-335508 <[01]. REPLACED REAR SPAR ANGLE LOCATED ON IRSS 148 AT MAIN LANDING GEAR AREA AT LT WING IAW B727-700 SRM 51-40-02; SRM 51-10-02 ITEM 9 AND DWG 115A2000 SHEET 21 REV -.
- [SDR SWAA2025063073486](https://openairdocs.org/sdr/SWAA2025063073486.md): Track · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TRACK RBBL 13.84 LOCATED STA747 AFT CARGO COMPARTMENT 2025-335494 <[01] TOOL USED ON STEP 4: EDDY CURRENT EQUIPMENT P/N:NORTEC 600D; S/N:210135503; DUE DATE:24-JUL-25.; [02] TOOL USED P/N: NORTEC 500D; S/N: N500X12101V022235; CAL DUE: 07-OCT-25.; [03] PE
- [SDR SWAA2025063073488](https://openairdocs.org/sdr/SWAA2025063073488.md): Angle · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R AFT POSITION AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN STA 907 TO STA 927 AND STR 25R TO STR 27R AFT POSITION AT AFT CARGO COMPARTMENT IAW-B737-700-SRM- 51-10-02-0G-0;B737-700-S
- [SDR SWAA2025063073484](https://openairdocs.org/sdr/SWAA2025063073484.md): Tie Clip · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK TIE CLIP LOCATED BS 277 AND S-10R PASSENGER CABIN 2025-335493<[01] REPLACED TIE CLIP LOCATED BS 277 AND S-10R PASSENGER CABIN IAW B737-700 SRM 51-40-02-0G-0 DWG 141A1110 SHEET 18 REV- AND DWG 141A8380 SHEET 21 REV-.
- [SDR SWAA2025063073489](https://openairdocs.org/sdr/SWAA2025063073489.md): Angle · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK ANGLE LOCATED BETWEEN STA907 TO STA927 AND STR25R TO STR27R FWD POSITION AT AFT CARGO COMPARTMENT. REPLACED ANGLE LOCATED BETWEEN STA 907 TO STA 927 AND STR 25R TO STR 27R FWD POSITION AT AFT CARGO COMPARTMENT IAW-B737-700-SRM- 51-10-02-0G-0;B737-700-S
- [SDR SWAA2025063073727](https://openairdocs.org/sdr/SWAA2025063073727.md): Rail · corroded · May 21, 2025 · N295WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CORROSION ON RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS449 AT RT WING. REPLACED RAIL NUT PLATES INTERNAL CAVITY LEADING EDGE LOCATED OFSS 449 AT RT WING IAW-B737-700-SRM 51-10-02-0G-0; SRM 51-40-02-0G-0 AND DWG# 112A4402 SHEET 13 REV -.
- [SDR SWAA2025063073729](https://openairdocs.org/sdr/SWAA2025063073729.md): Support Angle · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN. REPLACED SUPPORT ANGLE LOCATED BS 867 BETWEEN S-2R TO S-3R PASSENGER CABIN IAW B737-700 SRM 51-40-02; DWG 146A7901 SHEET: 66 REV: A.
- [SDR SWAA2025063073487](https://openairdocs.org/sdr/SWAA2025063073487.md): Access Panel · cracked · May 21, 2025 · N295WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED SEAL - PLATE ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW B737-700 SRM 51-40-02-0G-0 AND SRM 51-10-02-0G-0 STEP 9.
- [SDR SWAA2025063073239](https://openairdocs.org/sdr/SWAA2025063073239.md): Intercostal · cracked · May 20, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS344 TO BS 360 LBL 12 FWD GALLEY AND LAV 2025-335415 <[01]. REPLACED NEW WEB INTERCOSTAL LOC. ON FLOOR STRUCTURE BS344 TO BS 360 LBL 12 FWD GALLEY IAW B737-700 SRM 51-40-02-0G-0 AND DWG 141A5400 SHEET 46 REV A;
- [SDR SWAA2025063072652](https://openairdocs.org/sdr/SWAA2025063072652.md): Floorbeam · cracked · May 19, 2025 · N295WN · Boeing 7377H4 · Fuselage Floor Panel
  > CRACK FLOOR BEAM LOCATED BS 328 AND RBL 24 FWD GALLEY AND LAV 2025-335317 <[01]. STEP 21 TOOL USED: EDDY CURRENT FLAW DETECTOR. P/N: NORTEC 600D; S/N:190023010; DUE DATE: 05-AUG-25.; [02] REPAIRED FLOOR BEAM LOCATED BS 328 AND RBL 24 FWD GALLEY AND LAV IAW B7
- [SDR SWAA2025063072654](https://openairdocs.org/sdr/SWAA2025063072654.md): Angle · cracked · May 19, 2025 · N295WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK ANGLE TRAILING EDGE ORSS 271 AT LT WING. REPLACED ANGLE TRAILING EDGE ORSS 271 AT LT WING IAW B737-700 SRM 51-40-02; 51-10-02 ITEM 9 AND DWG 115A6200 SHEET:11 REV:B<BR>CRACK LENGH IS 1.700 INCH.
- [SDR SWAA2025063072653](https://openairdocs.org/sdr/SWAA2025063072653.md): Support Beam · cracked · May 19, 2025 · N295WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACK DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 TRAILING EDGE AT LT WING. PERFORMED PERMANENT REPAIR LOC. ON DEFLECTION CONTROL RIB SUPPORT BEAM ORSS 281 TRAILING EDGE AT LT WING IAW SRM 57-51-02-2R-3 REPAIR 3.
- [SDR SWAA2025063072913](https://openairdocs.org/sdr/SWAA2025063072913.md): Stub Frame · cracked · May 19, 2025 · N295WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK INDICATION ON STUB FRAME LOCATED BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA CRACK LENGTH 1.430 IN. APROX.AT PASSENGER CABIN. REPLACED STUB FRAME LOC. BETWEEN BS 294.5 TO BS 296.5 BTW S-8R TO S-9R AT FWD GALLEY DOOR AREA IAW S
- [SDR SWAA2025063072202](https://openairdocs.org/sdr/SWAA2025063072202.md): Nut · deteriorated · May 18, 2025 · N295WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED NUT ASSIST HANDLE AFT SERVICE INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA) 2025-335269 <[01]. REPLACED NUT ASSIST HANDLE AFT SERVICE INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5). FOR THE INSTALLATIO
- [SDR SWAA2025063072201](https://openairdocs.org/sdr/SWAA2025063072201.md): Nut · deteriorated · May 18, 2025 · N295WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED NUT ASSIST HANDLE AFT ENTRY INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA). REPLACED NUT ASSIST HANDLE AFT ENTRY INTERIOR STRUCTURE FWD OF DOOR OPENING (2EA) IAW B737-700 AMM 25-21-25-420-801 STEP 3.B.(5). FOR THE INSTALLATION SEE TTG8Q002EMNQ STEP
- [SDR SWAA2025063072204](https://openairdocs.org/sdr/SWAA2025063072204.md): Nut · deteriorated · May 18, 2025 · N295WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED NUT ASSIST HANDLE FWD ENTRY INTERIOR STRUCTURE AFT OF DOOR OPENING (2EA). REPLACED NUT ASSIST HANDLE FWD ENTRY INTERIOR STRUCTURE AFT OF DOOR OPENING IAW B737-700 AMM-52-11-31-400-802 STEP 3.G. ITEM (2).
- [SDR SWAA2025063072205](https://openairdocs.org/sdr/SWAA2025063072205.md): Nut · deteriorated · May 18, 2025 · N295WN · Boeing 7377H4 · Passenger/Crew Doors
  > DETERIORATED NUT FWD ENTRY DOOR LINER LOWER ASSIST HANDLE (2EA). REPLACED NUT FWD ENTRY DOOR LINER LOWER ASSIST HANDLE (2EA) IAW B737-700 AMM-52-11-31-400-802 STEP 3.G. ITEM (2);[02] TASK COMPLETED
- [SDR SWAA2025063072501](https://openairdocs.org/sdr/SWAA2025063072501.md): Support Angle · cracked · May 18, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE. REPLACED SUPPORT ANGLE AND FASTENERS LOCATED ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19R LOWER FUSELAGE IAW SRM 51-40-02 AND DWG 116A3118 S
- [SDR SWAA2025063072391](https://openairdocs.org/sdr/SWAA2025063072391.md): Support Angle · cracked · May 18, 2025 · N295WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 8 AT RT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 8 AT RT WING IAW SRM 51-40-02-0G AND SRM 51-10-02-0G ITEM 9; DWG 114A5010 SHEET 14 REV C. MEASURE OF CRACK IS: L= 2.019.
- [SDR SWAA2025063072392](https://openairdocs.org/sdr/SWAA2025063072392.md): Support Angle · cracked · May 18, 2025 · N295WN · 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 SRM 51-40-02-0G AND SRM 51-10-02-0G ITEM 9; DWG 114A5010 SHEET 14 REV C. MEASURE OF CRACK IS: L= 2.019.
- [SDR SWAA2025063072396](https://openairdocs.org/sdr/SWAA2025063072396.md): Support Angle · cracked · May 18, 2025 · N295WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACK SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING. REPLACED SUPPORT ANGLE ON INBOARD AUXILIARY TRACK SLAT 2 AT LT WING IAW B737-700 SRM 51-40-02-0G AND SRM 51-10-02-0G ITEM 9.<BR>MEASURE OF CRACK IS: L= 1.870.
- [SDR SWAA2025063072500](https://openairdocs.org/sdr/SWAA2025063072500.md): Support Angle · cracked · May 18, 2025 · N295WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE. REPLACED NEW ANGLE ON WING TO BODY FAIRING STRUCTURE BS 500D AT LEVEL STRINGER 19L LOWER FUSELAGE IAW SRM 51-40-02-0G-0 AND DWG 116A3110 SHEET 8 REV -; DWG 116
- [SDR SWAA2025063072192](https://openairdocs.org/sdr/SWAA2025063072192.md): Panel · corroded · May 17, 2025 · N295WN · Boeing 7377H4 · Fuselage Floor Panel
  > RUST ON LOWER STUD BULKHEAD PANEL 121LW AT FWD CARGO COMPARTMENT (6E/A) 2025-335249 <[01]. REPLACED LOWER STUD BULKHEAD PANEL 121LW AT FWD CARGO COMPARTMENT (6E/A) IAW B737-700 SRM-51-40-02-0G -0; [02] REPLACED LOWER STUD BULKHEAD PANEL 121LW AT FWD CARGO COMP
- [SDR SWAA2025063071696](https://openairdocs.org/sdr/SWAA2025063071696.md): Skin · corroded · May 16, 2025 · N295WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > CUSTOMER REQUEST EVIDENCE OF CORROSION ON EXTERNAL SKIN VACUUM WASTE VENT CUTOUT LOCATED BTW S-21L TO S-22L STA 907 PLUS 10 INCH 2025-335136 <[01]. ON STEP 4; ULTRASONIC THICKNESS GAGE P/N: 45MG; S/N: 221859911; DUE DATE: 19-DEC-25.; [02] TOOL USED EDDY CURREN
- [SDR SWAA2025051970234](https://openairdocs.org/sdr/SWAA2025051970234.md): Battery Pack · failed · May 13, 2025 · N295WN · Boeing 7377H4 · Emergency Lighting
  > L/H AFT EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025051970232](https://openairdocs.org/sdr/SWAA2025051970232.md): Battery Pack · failed · May 13, 2025 · N295WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHTING BATTERY PACK AT THE L/H OVERWING EXIT FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025051970230](https://openairdocs.org/sdr/SWAA2025051970230.md): Battery Pack · failed · May 13, 2025 · N295WN · Boeing 7377H4 · Emergency Lighting
  > L/H FWD EMERGENCY LIGHTING BATTERY PACK FAILED THE CAPACITY CHECK.<[01] REMOVED AND REPLACED BATTERY PACK PER M/M 33-51-06.
- [SDR SWAA2025011686597](https://openairdocs.org/sdr/SWAA2025011686597.md): Light · inoperative · Jan 16, 2025 · N295WN · Boeing 7377H4 · Emergency Lighting
  > L2 DOOR EMERGENCY LIGHT INOP.<[01] R & R L2 DOOR EMERGENCY LIGHT REF AMM 33-51-04. OPS CHK GOOD.
- [SDR SWAA2025011385227](https://openairdocs.org/sdr/SWAA2025011385227.md): Guard · inoperative · Jan 12, 2025 · N295WN · Boeing 7377H4 · Emergency Lighting
  > GUARD ON EMERGENCY LIGHT SWITCH INOP<[01] REMOVED AND REPLACED GUARD IN REF TO SIP
- [SDR SWAA2024120974575](https://openairdocs.org/sdr/SWAA2024120974575.md): Engine · smoke · Dec 5, 2024 · N295WN · Boeing 7377H4 · Power Indicating System
  > EXCESSIVE SMOKE FROM #1 ENGINE TAILPIPE WITH PUDDLING ON GROUND AT REAR OF ENGINE SMOKE ACCOMPANIED BY FLAMES. OIL QUANTITY AT SHUTDOWN 52%. BP AERO JONATHAN NICOLINI (214) 303-7072. THEY ARE ARRIVING ON SWA FLIGHT #3491 AT 2025 IN LAS.<[01] REMOVED ENG#1 PRIM
- [SDR SWAA2024120674339](https://openairdocs.org/sdr/SWAA2024120674339.md): Tailpipe · leaking · Dec 5, 2024 · N295WN · Boeing 7377H4 · Engine Oil Storage (Airframe Furnished)
  > EXCESSIVE SMOKE FROM #1 ENGINE TAIL PIPE REPORTED BY RAMP WITH OIL PUDDLING ON GROUND AT REAR OF ENGINE.<[01] C/W ENGINE VENTS & DRAINS INSPECTION IAW AMM 71-71-00. INSPECTED REAR SEAL FLAME ARRESTOR; NO DEFECTS NOTED. OIL CONSUMPTION WITHIN LIMITS AT 0.42 QTS
- [SDR SWAA2024083031078](https://openairdocs.org/sdr/SWAA2024083031078.md): Flashlight · inoperative · Aug 27, 2024 · N295WN · Boeing 7377H4 · Emergency Equipment
  > 1 FWD CABIN EMERGENCY FLASHLIGHT INOP.<
- [SDR SWAA2024080823926](https://openairdocs.org/sdr/SWAA2024080823926.md): Seat Back · out of adjust · Aug 7, 2024 · N295WN · Boeing 7377H4 · Passenger Compartment Equipment
  > SEATS 11DEF WILL NOT STAY UPRIGHT WHILE OCCUPIED<[01] 11F SEAT RECLINE ACTUATOR NOT LOCKED OUT FOR EMERGENCY EXIT; LOCKED RECLINE ACTUATOR TO UP POSITION AND TIGHTENED ALL HARDWARE OF HINGE POINTS OF ALL 11DEF SEAT PER CMM 25-22-46; ALL SEATS STAY IN UP POSITI

Next page: https://openairdocs.org/aircraft/N295WN/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 = 'N295WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N295WN/reports

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