# Service difficulty reports: N276WN

A list on [N276WN](https://openairdocs.org/aircraft/N276WN.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 · 286 reports

- [SDR SWAA2026091549653](https://openairdocs.org/sdr/SWAA2026091549653.md): Lamp · inoperative · Sep 11, 2026 · N276WN · Boeing 7377H4 · Emergency Lighting
  > AFT CARGO BAY EMERGENCY LIGHT INOP. REMOVED AND REPLACED RH OVERWING ESCAPE GROUND ILLUMINATION LIGHT LAMP IAW B737 AMM 33-51-04-960-801 TEST PASSED VERIFIED REMOVED AND REPLACED RH OVERWING ESCAPE GROUND ILLUMINATION LIGHT LAMP IAW B737 AMM 33-51-04-960-801
- [SDR SWAA2026090379831](https://openairdocs.org/sdr/SWAA2026090379831.md): Lamp · inoperative · Aug 30, 2026 · N276WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY LIGHT AT FWD ENTRY DOOR INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-51-03, OPS CHKD GOOD.
- [SDR SWAA2026062515460](https://openairdocs.org/sdr/SWAA2026062515460.md): Brake · smoke · Jun 24, 2026 · N276WN · Boeing 7377H4 · Landing Gear Brake System
  > POST FLIGHT, FOUND SMOKE COMING FROM LEFT MAIN WHEEL BRAKE ASSY. BRAKE TEMP READINGS UNABLE TO BE TAKEN PRIOR TO 15 MINUTES AFTER ACFT ARRIVED AT GATE. ACFT BRAKES REQUIRED TO COOL MINIMUM GROUND TIME. IAW MPM 53.5.2.2
- [SDR SWAA2026061713176](https://openairdocs.org/sdr/SWAA2026061713176.md): Handle · broken · Jun 17, 2026 · N276WN · Boeing 7377H4 · Passenger/Crew Doors
  > CLOSE ASSIST HANDLE BROKE F/E DOOR. REPLACED ASSIST HANDLE ON FORWARD ENTRY DOOR IAW AMM 25-21-31.
- [SDR SWAA2026052605371](https://openairdocs.org/sdr/SWAA2026052605371.md): Isolator · cracked · May 22, 2026 · N276WN · Boeing 7377H4 · Escape Slide
  > PASSENGER CABIN FORWARD SERVICE DOOR AFT SLIDE MOUNT ISOLATOR CRACKED.<[01] R&R AFTER SLIDE MOUNT ISOLATOR PER SRM 51-40-02;[02] INSPECTION VERIFIED CORRECTIVE ACTION TAKEN IN STEP 1.
- [SDR SWAA2026022472730](https://openairdocs.org/sdr/SWAA2026022472730.md): Attach Bracket · cracked · Feb 21, 2026 · N276WN · Boeing 7377H4 · Wing, Attach Fittings
  > RIGHT WING UPPER PANEL SUPPORT, FWD ATTACH BRACKET CRACKED. REMOVED AND REPLACED IAW SRM 51-40-02-0G-0-A00729.
- [SDR SWAA2025121243658](https://openairdocs.org/sdr/SWAA2025121243658.md): Smoke Detector · false activation · Dec 7, 2025 · N276WN · Boeing 7377H4 · Smoke Detection
  > AFTER LAV SMOKED ALARM ACTIVATED INTERMITTENTLY DURING FINAL DESCENT AND AT THE GATE. NO SIGNS OF SMOKE. OK TO CONTINUE PER MEL 26-16-01 XB;AFT LAVATORY SMOKE DETECTION SYSTEM. WITH SP 1B & 3 AND AUTHORIZATION NUMBER 296463. R & R AFT LAVATORY SMOKE DETECTO
- [SDR SWAA2025112438111](https://openairdocs.org/sdr/SWAA2025112438111.md): Handle · unsecure · Nov 21, 2025 · N276WN · Boeing 7377H4 · Passenger/Crew Doors
  > FWD ENTRY DOOR ASSIST HANDLE STRAP WILL NOT SECURE TO DOOR TRIM<[01] REPLACED HANDLE ?WARNING? STRAP PER SIP OPS CHECKS GOOD
- [SDR SWAA2025082206113](https://openairdocs.org/sdr/SWAA2025082206113.md): Cam Plate · loose · Aug 20, 2025 · N276WN · Boeing 7377H4 · Service Doors
  > FWD SERVICE DOOR HANDLE CAM PLATE IS LOOSE, TIGHTENED HARDWARE. PER AMM 20-50-11.
- [SDR SWAA2025050165087](https://openairdocs.org/sdr/SWAA2025050165087.md): Control Module · faulted · Apr 28, 2025 · N276WN · Boeing 7377H4 · Fire Detection
  > ENG #1 OVERHEAT DURING CLIMB THROUGH 9K COMPLETED QRC/QRH LIGHT EXTINGUISHED<[01] PERFORMED FIM TASK 26-10 TASK 810 NO FAULTS FOUND. REMOVED AND REPLACED ENGINE & APU FIRE DETECTION CONTROL MODULE AS PER AMM 26-10-01. AIRCRAFT STILL REQUIRES HIGH POWER ENGINE
- [SDR SWAA2025040722315](https://openairdocs.org/sdr/SWAA2025040722315.md): Connector · failed · Apr 3, 2025 · N276WN · Boeing 7377H4 · Electrical Power System Wiring
  > ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARE
- [SDR SWAA2025040722314](https://openairdocs.org/sdr/SWAA2025040722314.md): Wire · corroded · Apr 3, 2025 · N276WN · Boeing 7377H4 · Electrical Power System Wiring
  > ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARE
- [SDR SWAA2025040721566](https://openairdocs.org/sdr/SWAA2025040721566.md): Gcu · failed · Apr 3, 2025 · N276WN · Boeing 7377H4 · AC Generator-Alternator
  > ENROUTE NOTICED ELECTRICAL BURN SMELL THEN RECEIVED A 'TRANSFER BUS OFF' LIGHT AND 'SOURCE OFF' LIGHT ON NO.2 SIDE. RAN QRH AND DURING CHECKLIST GOT A 'DRIVE' LIGHT ON NO2 SIDE. COMPLIED WITH QRH AND FA'S CALLED TO SAY CABIN HAD SMOKE. RAN QRH AND SMOKE CLEARE
- [SDR SWAA2025040721301](https://openairdocs.org/sdr/SWAA2025040721301.md): Gcu · burned · Apr 2, 2025 · N276WN · Boeing 7377H4 · AC Generator-Alternator
  > AT CRUISE; A NOTICEABLE ELECTRICAL SMELL WAS NOTICED THROUGHOUT ENTIRE PLANE. SHORTLY AFTER; TRANSFER BUS LIGHT ILLUMINATED; FOLLOWED BY SOURCE OFF LIGHT; FOLLOWED BY DRIVE LIGHT - ALL CHECKLISTS WERE FOLLOWED AND COMPLIED WITH<[01] WHILE PERFORMING FIM TASK 0
- [SDR SWAA2025012889827](https://openairdocs.org/sdr/SWAA2025012889827.md): Lamp · inoperative · Jan 27, 2025 · N276WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR HAS INOP BULBS<[01] RELAMPED EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR; PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025012889826](https://openairdocs.org/sdr/SWAA2025012889826.md): Bulb · inoperative · Jan 27, 2025 · N276WN · Boeing 7377H4 · Emergency Lighting
  > EMERGENCY EXIT LOCATOR FWD OF L/H OWE HAS INOP BULBS<[01] RELAMPED EMERGENCY EXIT LOCATOR FWD OF FWD SERVICE DOOR; PERFORMED GOOD TEST PER AMM 33-51-01-960-801.;[02] VERIFIED CORRECTIVE ACTION ITEM 1; CARD COMPLETE.
- [SDR SWAA2025012888496](https://openairdocs.org/sdr/SWAA2025012888496.md): Fuse · burned · Jan 22, 2025 · N276WN · Boeing 7377H4 · Emergency Lighting
  > L732 AFT LEFT ESCAPE SLIDE LIGHT DOES NOT TURN ON.<[01] RELAMPED AFT L/H ESCAPE SLIDE LIGHT AND PERFORME3D INSTALLATION TEST PER AMM 33-51-04-960-801; LIGHT STILL INOP; PERFORMED GOOD CONTINUITY CHECK OF WIRING FOR AFT L/H ESCAPE SLIDE LIGHT PER WDM 33-51-14;
- [SDR SWAA2025012888497](https://openairdocs.org/sdr/SWAA2025012888497.md): Battery Pack · inoperative · Jan 22, 2025 · N276WN · Boeing 7377H4 · Emergency Lighting
  > ASSOCIATED EMERGENCY LIGHTS WITH BATTERY PACK M1674 DO NOT TURN ON<[01] REMOVED; REPLACED AND PERFORMED GOOD OPS CHECK OF M1673 EMERGENCY BATTERY PACK PER AMM 33-51-06-960-805<BR><BR>CARD COMPLETE;[02] UPDATED PART REQUIREMENTS;[03] ALL STEPS COMPLETED FOR CC#
- [SDR SWAA2025012887074](https://openairdocs.org/sdr/SWAA2025012887074.md): Scuff Plate · cracked · Jan 17, 2025 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > FCB FWD CORNER SCUFF PLATE CRACKED<[01] ALL STEPS COMPLETED
- [SDR SWAA2025012883432](https://openairdocs.org/sdr/SWAA2025012883432.md): Baffle · damaged · Jan 6, 2025 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED FASTENER HOLE ON BUFFLE AT BS500 TO BS500A LBL25 WL156<[01] REMOVED AND REPLACED BAFFLE AT BS 500 TO BS 500A<BR>IAW SRM 51-40-02 & DWG# 143A7505 REV: -<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025012883434](https://openairdocs.org/sdr/SWAA2025012883434.md): Baffle · cracked · Jan 6, 2025 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED BUFFLE AT BS500A TO BS500B LBL25 WL156 CORRECT LOCATION IS BS500B TO BS500C<[01] REMOVED AND REPLACED BAFFLE ASSY P/N 143A7510-11 BETWEEN BS500B AND BS500C; LBL25 IAW SRM 51-40-02 AND DWG 143A7505 REV B.;[02] REJECT - CRACK FOUND @ BRACKET AFT OF FRAME
- [SDR SWAA2025012883082](https://openairdocs.org/sdr/SWAA2025012883082.md): Floor Support · elongated · Jan 5, 2025 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED FASTENER HOLE ON INTERCOSTAL AT BS440 TO BS460; LBL25; WL156<[01] REMOVED AND REPLACED INTERCOSTAL AT BS 440 TO BS 460 LBL 25 WL 156 IAW SRM 51-40-02 AND DGW# 143A7505 REV:-<BR>CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025012882811](https://openairdocs.org/sdr/SWAA2025012882811.md): Stub Frame · cracked · Jan 3, 2025 · N276WN · Boeing 7377H4 · Fuselage Main, Frame
  > DURING HFEC INSPECTION OF STUB FRAME FOUND CRACK ABOVE SEAL DEPRESSOR BS 291.5 + 8 WL266 L: 1.7' MARKED.<[01] REJECTED: DURING OK TO INSTALL NEW STUB FRAME; FOUND FASTENER HOLE DAMAGE OUT OF TOLERENCE AND NOT TRUE AND ROUND. LOCATED AT FSD FWD FRAME UPPER FITT
- [SDR SWAA2025012882022](https://openairdocs.org/sdr/SWAA2025012882022.md): Stringer Clip · cracked · Dec 31, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727E S-5L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727E S-5L IAW SRM 51-40-02 AND DWG#146A1112 ID: 0001 REV:C;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2025012882020](https://openairdocs.org/sdr/SWAA2025012882020.md): Stringer Clip · cracked · Dec 31, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS727B S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS727B S-6L IAW SRM 51-40-02 AND DWG#146A1102 ID: 0001 REV:D;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2025012882019](https://openairdocs.org/sdr/SWAA2025012882019.md): Stringer Clip · cracked · Dec 31, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED STR CLIP AT PAX CABIN BS767 S-6L. MARKED<[01] REMOVED AND REPLACED STR CLIP AT PAX CABIN BS767 S-6L IAW SRM 51-40-02 AND DWG#143A1010 ID: 0001 REV:C;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.
- [SDR SWAA2025012882021](https://openairdocs.org/sdr/SWAA2025012882021.md): Stringer · cracked · Dec 31, 2024 · N276WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER S-11L AT FWD CABIN BS294 WL251.<[01] REMOVED AND REPLACED STRINGER 11L AT FWD CABIN BS294 TO 259.5 1AW B737-7 SRM 51-40-02-0G-01 AND DWG# 141A3120 SHEET 7 REV-B.;[02] VERIFIED CORRECTIVE ACTION ITEMS; CARD COMPLETE.
- [SDR SWAA2025013087166](https://openairdocs.org/sdr/SWAA2025013087166.md): Skin · out of limits · Dec 24, 2024 · N276WN · Boeing 7377H4 · Fuselage Main, Plate/Skin
  > SECTION 46 FUSELAGE SKIN HAS A BLEND AT BS 787+4 AND 5' BELOW STR 24R WITHIN 10 INCHES OF AFT CARGO DOOR CUTOUT<[01] REPAIRED PER EA 24-153-03589;[02] VERIFIED CORRECTIVE ACTION COMPLETED.
- [SDR SWAA2025013179869](https://openairdocs.org/sdr/SWAA2025013179869.md): Shield · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON AFT SHIELD AT FCB BS500 - BS500A RBL23 WL156.<[01] REMOVED AND REPLACED SHIELD IAW SRM 51-40-05 & DWG# 143A0080 REV: CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION 1.
- [SDR SWAA2025012979883](https://openairdocs.org/sdr/SWAA2025012979883.md): Web · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Cargo Compartments
  > AFT CARGO ENTRY THRESHOLD BS 807 TO 847 RBL26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED ACB THRESHOLD WEB AT BS 794.25 TO BS847 IAW SRM 51-40-02 AND DWG 146A8340 ID:0024 REV: A.; [02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2025012879885](https://openairdocs.org/sdr/SWAA2025012879885.md): Sidewall Support · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; ZEE SIDE PLATE BS 727 TO 767 RBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT BS 727 TO BS 767 RBL 26 IAW SRM 51-40-02 AND DWG 146A7500 ID 85; AND INTERCOSTAL BS 747 TO BS 767 RBL 26 IAW SRM 51-40
- [SDR SWAA2025012879870](https://openairdocs.org/sdr/SWAA2025012879870.md): Sidewall Support · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION ON FLOOR TO SIDEWALL SUPPORT AT FCB BS500 - BS500D LBL23 WL156.<[01] REMOVED AND REPLACED FCB FLOOR TO SIDEWALL SUPPORT; P/N 143A7501U183; BS400 TO BS500D LBL23 WL156 IAW SRM 51-40-02 AND DWG 143A7500 REV. B.;[02] VERIFIED CORRECTIVE ACTION ENTRY 1.;
- [SDR SWAA2025012882248](https://openairdocs.org/sdr/SWAA2025012882248.md): Shield · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Cargo Compartments
  > CORROSION ON FWD SHIELD AT FCB BS420 - BS440 RBL23 WL156. MARKED<[01] REMOVED AND REPLACED SHIELD FCB BS 420 - BS 440. IAW SRM 51-40-02 AND DWG # 143A0080 REV: CARD COMPLETED;[02] VERIFIED CORRECTIVE ACTION COMPLETE.
- [SDR SWAA2025012879881](https://openairdocs.org/sdr/SWAA2025012879881.md): Shield · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; AFT SHIELD BS 847 TO 867 RBL 26 HAS CORROSION. (MARKED)<[01] STEP 4 OK TO APPLY CIC.;[02] OK TO APPLY CIC;[03] REMOVED AND REPLACED ACB AFT SHIELD; P/N 146A8127-10; BS847 TO BS867 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 REV A;[04] REJECTED STEP 2 IT
- [SDR SWAA2025012879882](https://openairdocs.org/sdr/SWAA2025012879882.md): Shield · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; FWD SHIELD BS 767 TO 794 RBL 26 HAS CORROSION. (MARKED)<[01] REMOVED AND REPLACED AFT CARGO FWD SHIELD BS767 TO BS794 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV: A;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025012879884](https://openairdocs.org/sdr/SWAA2025012879884.md): Shield · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; FWD SHIELD CLIP AT BS 767 RBL 26 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT CARGO FWD SHIELD CLIP AT BS767 RBL26 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV:A;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025012879887](https://openairdocs.org/sdr/SWAA2025012879887.md): Support Angle · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; ZEE SIDEPLATE BS 727 TO 847 LBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED AFT CARGO BAY L/H FLOOR TO SIDEWALL SUPPORT ANGLE BS 727 TO BS 847; LBL 26; IAW SRM 51-40-02-0G-0 AND DWG# 146A7500;[02] VERIFIED CORRECTIVE ACTI
- [SDR SWAA2025012879888](https://openairdocs.org/sdr/SWAA2025012879888.md): Intercostal · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; SIDEPLATE INTERCOSTAL BS 767 TO 787 HAS CORROSION (MARKED). RBL 23<[01] REMOVED AND REPLACED NEW AFT CARGO; WEB BS 767 TO BS 787 RBL21 IAW SRM 51-40-02 AND DWG 146A0081 ID:0028 REV:A;[02] VERIFIED CORRECTIVE ACTION 1
- [SDR SWAA2025012879894](https://openairdocs.org/sdr/SWAA2025012879894.md): Sidewall Support · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO; ZEE SIDEPLATE BS 867 TO 947 RBL 26 HAS SEVERAL SPOTS WITH CORROSION (MARKED).<[01] REMOVED AND REPLACED FLOOR TO SIDEWALL SUPPORT AT BS887 TO BS947 RBL26 IAW SRM 51-40-02 AND DWG 147A7500 ID:0029 REV: -;[02] VERIFIED CORRECTIVE ACTION COMPLETE
- [SDR SWAA2025012879892](https://openairdocs.org/sdr/SWAA2025012879892.md): Crossbeam · corroded · Dec 20, 2024 · N276WN · Boeing 7377H4 · Fuselage Main, Structure
  > AFT CARGO; CROSS BEAM FRAME AT BS 947.5 RBL 20 HAS CORROSION (MARKED).<[01] REMOVED AND REPLACED ACB FRAME BS 947 BETWEEN STR 23L AND STR 23R IAW SRM 51-40-02-0G-0 AND DWG # 147A1047 REV:D;[02] VERIFIED CORRECTIVE ACTION
- [SDR SWAA2025013179516](https://openairdocs.org/sdr/SWAA2025013179516.md): Panel · cracked · Dec 19, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PANEL BREAK CRACKED BS 540 BL 0 - RBL 25 WL 207<[01]. REMOVED AND REPLACED PANEL BREAK BS 540 BL 0 - RBL 25 WL 207 IAW SRM 51-40-2 AND IAW DWG# 143A5240 REV: -;[02] VERIFIED CORRECTIVE ACTION.
- [SDR SWAA2025012079063](https://openairdocs.org/sdr/SWAA2025012079063.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 231XF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 231XF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0126;[02] VERIFIED TASK COMPLETE
- [SDR SWAA2025012079064](https://openairdocs.org/sdr/SWAA2025012079064.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 232RF UPPER SURFACE DELAMINATED<[01] 01 - REMOVED AND REPLACED FLOOR PANEL 232RF DUE TO EXCESSIVE DELAMINATION PER [SRM 51-10-02-0G-0-A00248 (GENERAL - INSPECTION AND REMOVAL OF DAMAGE - AIRFRAME - PERMANENT)];[02] VERIFIED CORRECTI
- [SDR SWAA2025012079065](https://openairdocs.org/sdr/SWAA2025012079065.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241AF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 241AF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0127;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025012079068](https://openairdocs.org/sdr/SWAA2025012079068.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241BF UPPER SURFACE DELAMINATED<[01] REPLACED PASSENGER CABIN FLOOR PANEL 241BF WITH SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PARA 9 AND AIPC 53-21-00-42A ITEM #65.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025012079069](https://openairdocs.org/sdr/SWAA2025012079069.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241DF UPPER SURFACE DELAMINATED<[01] FLOOR PANEL 241DF WITH UPPER SURFACE DELAMINATION WAS REPLACED BY FABRICATING A NEW PANEL IAW SRM 53-00-50-2R-0 AND DWG 144A5810 ID:0128;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025012079070](https://openairdocs.org/sdr/SWAA2025012079070.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241EF UPPER SURFACE DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 241EF WAS REPLACED DUE TO EXCESSIVE UPPER SURFACE DELAMINATION IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM #105.;[02] VERIFIED JOB COMPLETE
- [SDR SWAA2025012079071](https://openairdocs.org/sdr/SWAA2025012079071.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANEL 241FF UPPER SURFACE DELAMINATED<[01] REPLACED PASSENGER CABIN FLOOR PANEL 241FF WITH SERVICEABLE PART IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025012079076](https://openairdocs.org/sdr/SWAA2025012079076.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABN FLOOR PANEL 242AF UPPER SURFACE DELAMINATED.<[01] REPLACED PASSENGER CABIN FLOOR PANEL 242AF WITH SERVICEABLE PANEL IAW SRM 51-10-02-0G-0 PARA 9.;[02] VERIFIED CORRECTIVE ACTION ITEM 1.
- [SDR SWAA2025012079072](https://openairdocs.org/sdr/SWAA2025012079072.md): Floor Panel · delaminated · Dec 18, 2024 · N276WN · Boeing 7377H4 · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR PANE 242DF UPPER SURFACE DELAMINATED<[01] PASSENGER CABIN FLOOR PANEL 242DF WAS REPLACED WITH A NEW PANEL DUE TO EXCESSIVE UPPER SURFACE DELAMINATED PLIES IAW SRM 51-10-02-0G-0 PARAGRAPH 9 AND AIPC 53-21-00-42A ITEM 135.;[02] VERIFIED COR

Next page: https://openairdocs.org/aircraft/N276WN/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 = 'N276WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N276WN/reports

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