# Service difficulty reports: N229WN A list on [N229WN](https://openairdocs.org/aircraft/N229WN.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 · 293 reports - [SDR SWAA2026040785717](https://openairdocs.org/sdr/SWAA2026040785717.md): Hmu · faulted · Apr 2, 2026 · N229WN · Boeing 7377H4 · Fuel Controlling System > NR 1 ENGINE N1 ROLLED BACK 10% AT CLIMB OUT. REF TTG8Q01BFMVQ FOR REPLACEMENT OF HMU AND FUEL PUMP PACKAGE. PERFORMED TESTS 8; 12 AND 13 PER POWER PLANT TEST REFERENCE TABLE AMM 71-00-00. TESTS PASSED. A/C STILL NEEDS TEST 15 (85% N1 LEAK CHECK).;[02] PERFOR - [SDR SWAA2026040787175](https://openairdocs.org/sdr/SWAA2026040787175.md): Pump · weak · Apr 2, 2026 · N229WN · Boeing 7377H4 · Engine Fuel Pump > NR 1 ENGINE, N1 ROLLED BACK 10% AT CLIMB OUT. REF TTG8Q01BFMVQ FOR REPLACEMENT OF HMU AND FUEL PUMP PACKAGE. PERFORMED TESTS 8; 12 AND 13 PER POWER PLANT TEST REFERENCE TABLE AMM 71-00-00. TESTS PASSED. PERFORMED TASK 71-00-00-SWA-823-F00, LEAK CHECK AFT - [SDR SWAA2026032783823](https://openairdocs.org/sdr/SWAA2026032783823.md): Slide · unpacked · Mar 26, 2026 · N229WN · Boeing 7377H4 · Escape Slide > AFT ENTRY DOOR SLIDE CAME OUT OF CONTAINER. REPACKED AFT ENRY DOOR SLIDE REF MT 725-61-06. AC OK FOR SERVICE - [SDR SWAA2025122955602](https://openairdocs.org/sdr/SWAA2025122955602.md): Power Supply · smoke · Dec 25, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT POWER SUPPLY IN FWD GALLEY (M01674) SMOKING. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY ASSY AND BATTERY PACK IAW AMM 33-51-06. REMOVED & REPLACED FWD GALLEY LIGHT ASSY IAW AMM 33-26-02. OPS CHECKED GOOD. - [SDR SWAA2025122956408](https://openairdocs.org/sdr/SWAA2025122956408.md): Battery Pack · smoke · Dec 25, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT POWER SUPPLY IN FWD GALLEY (M01674) SMOKING. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY ASSY AND BATTERY PACK IAW AMM 33-51-06. AND REMOVED AND REPLACED FWD GALLEY LIGHT ASSY IAW AMM 33-26-02. OPS CHECK GOOD. - [SDR SWAA2025122956409](https://openairdocs.org/sdr/SWAA2025122956409.md): Light · smoke · Dec 25, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY LIGHT POWER SUPPLY IN FWD GALLEY (M01674) SMOKING. R & R EMERGENCY LIGHT POWER SUPPLY ASSY AND BATTERY PACK IAW AMM 33-51-06. AND R & R FWD GALLEY LIGHT ASSY IAW AMM 33-26-02. OPS CHECKED GOOD. - [SDR SWAA2025081504621](https://openairdocs.org/sdr/SWAA2025081504621.md): Light · out of adjust · Aug 15, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > STORAGE BIN LOWER TRIM, EMERGENCY LIGHT IS LOOSE AT ROWS 7, 8, & 9 FED. ADJUSTED STORAGE BIN LOWER TRIM WITH EMERGENCY LIGHT IAW CMM 25-24-02. - [SDR SWAA2025081498886](https://openairdocs.org/sdr/SWAA2025081498886.md): Scuff Plate · cracked · Aug 6, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FWD ENTRY DOOR FWD CORNER SCUFF PLATE IS CRACKED. REPAIRED PER EA 25-153-02123. - [SDR SWAA2025081598171](https://openairdocs.org/sdr/SWAA2025081598171.md): Scuff Plate · cracked · Aug 4, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO FWD CORNER SCUFF PLATE CRACKED. WILL BE REPLACED ON CARD TTG8Q006MC7E. - [SDR SWAA2025081596516](https://openairdocs.org/sdr/SWAA2025081596516.md): Nut Plate · corroded · Jul 29, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CORROSION AT NUT-PLATE STRAP COMMON TO ACB LOWER MAIN SILL VERTICAL WEB STA-787+10'' RBL-20.5<[01] REMOVED AND REPLACED STRAP ON ACB LOWER MAIN SILL BS787+10 RBL 20.5 IAW SRM 51-40-02-0G-0 AND DWG 146A8340 REV -. - [SDR SWAA2025081596517](https://openairdocs.org/sdr/SWAA2025081596517.md): Support Fitting · cracked · Jul 29, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > FUSELAGE PANEL 192E FWD RT SUPPORT FITTING IS CRACKED BS 551, RBL 5. REMOVED AND REPLACED SUPPORT BRACKET IAW SRM 51-40-02-0G-0 AND DWG#149A7701 REV-A. - [SDR SWAA2025081595102](https://openairdocs.org/sdr/SWAA2025081595102.md): Web · corroded · Jul 24, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON AFT CARGO BAY LOWER MAIN SILL WEB AT BS 787+10, RBL 20.5, WL 156. REMOVED AND REPLACED WEB ON ACB LOWER MAIN SILL BS 794 - BS 847, RBL 20.5, WL156 IAW SRM 51-40-02-0G-0 AND DWG 146A8120 REV -. - [SDR SWAA2025081594505](https://openairdocs.org/sdr/SWAA2025081594505.md): Web · corroded · Jul 23, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION IN AFT CARGO DOOR CUTOUT LOWER MAIN SILL WEB BS 794+4, WL 156, RBL 18. LOWER MAIN SILL WEB BS 794 TO BS 847, RBL 18 WAS REPLACED ON CARD TTG8Q0146N47. - [SDR SWAA2025081994261](https://openairdocs.org/sdr/SWAA2025081994261.md): Attach Angle · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACK ON FCB BAFFLE ASSEMBLY ATTACH ANGLE AT BS500C RBL26 WL156. REMOVED AND REPLACED FCB BAFFLE ASSEMBLY ATTACH ANGLE AT BS500C RBL26 WL156 IAW SRM 51-40-02-0G-0.AND DWG 143A7505. - [SDR SWAA2025081594246](https://openairdocs.org/sdr/SWAA2025081594246.md): Floorbeam · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; LBL 2; WL 208; REMOVED AND REPLACED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; LBL 2; WL 208 IAW SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] CORRECTIVE ACTION COMPLETED. - [SDR SWAA2025081594247](https://openairdocs.org/sdr/SWAA2025081594247.md): Floorbeam · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208; REMOVED AND REPLACED NEW PANEL BREAK AT PASSENGER COMPARTMENT BS 540; RBL 2; WL 208 I.A.W SRM 51-40-02-0G-0 AND DWG 143A5240.;[02] VERIFIED CORRECTIVE ACTION 1 AND MEASUREMENT TABLE. - [SDR SWAA2025081594249](https://openairdocs.org/sdr/SWAA2025081594249.md): Floorbeam · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Floor Beam > CRACKED FLOOR BEAM ATTACH ANGLE AT PASSENGER COMPARTMENT BS 695; LBL 1; WL 208; REMOVED AND REPLACED ANGLE AT BS 695 LBL 1; WL 208 IAW SRM 51-40-02 AND DWG 273A9110 ID:005 REV: A. - [SDR SWAA2025081595592](https://openairdocs.org/sdr/SWAA2025081595592.md): Intercostal · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > INTERCOSTAL FROM BS294.5-BS303.9 STR 16L WL216 IS CRACED. REMOVED AND REPLACED INTERCOSTAL FROM BS 294.5 TO BS 303.9 STR 16L IAW SRM 51-40-02 AND DWG 141A8180 ID: 0027 REV:C. - [SDR SWAA2025081494257](https://openairdocs.org/sdr/SWAA2025081494257.md): Strap · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON STRAP ACB STA-847 RBL-19 FLOOR AREA. REMOVED AND REPLACED STRAP ON ACB BS847 RBL19 IAW SRM 51-40-02 AND DWG 146A8340 REV -. - [SDR SWAA2025081494258](https://openairdocs.org/sdr/SWAA2025081494258.md): Sidewall Support · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB RH FLOOR TO SIDEWALL SUPPORT, RBL 21, BS 727A TO 767. REMOVED AND REPLACED ACB RH FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146A7500. - [SDR SWAA2025081494259](https://openairdocs.org/sdr/SWAA2025081494259.md): Sidewall Support · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON ACB LH FLOOR TO SIDEWALL SUPPORT, LBL 21, BS 727A TO 847. REMOVED AND REPLACED ACB LT FLOOR TO SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 146A7500. - [SDR SWAA2025081494268](https://openairdocs.org/sdr/SWAA2025081494268.md): Sidewall Support · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS WITH CORROSION ON FCB SIDEWALL TO FLOOR SUPPORT NUTPLATE HOLES AT BS 460+2 TO 500B+2, LBL 22, WL156. REMOVED AND REPLACED FCB AT FLOOR SIDEWALL SUPPORT IAW SRM 51-40-02-0G-0, AND DWG 143A7500, REV-. - [SDR SWAA2025081494806](https://openairdocs.org/sdr/SWAA2025081494806.md): Shield · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON FCB AFT SHIELD FROM BS492 TO 500+7, RBL 22, WL156. REMOVED AND REPLACED FCB AFT SHIELD IAW SRM 51-40-02, AND DWG 143A0080, REV-. - [SDR SWAA2025081494262](https://openairdocs.org/sdr/SWAA2025081494262.md): Angle · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON ANGLE ACB STA-867 LBL-13'' FLOOR AREA. REMOVED AND REPLACED ANGLE ACB STA 867 LBL 13
IAW SRM 51-40-02-0G-0; IAW SRM 51-40-05 AND DWG#149A8102 REV:-. - [SDR SWAA2025081494263](https://openairdocs.org/sdr/SWAA2025081494263.md): Support Fitting · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK ON ACB WATER TANK SUPPORT FITTING STA-947 LBL-10''. REMOVED AND REPLACED SUPPORT FITTING STA-947 LBL-10 IAW SRM 51-40-02 AND DWG 149A8103 ID:0007 REV: A. - [SDR SWAA2025081494267](https://openairdocs.org/sdr/SWAA2025081494267.md): Attach Angle · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CRACK ON FCB BAFFLE ASSEMBLY ATTACH ANGLE AT BS400 LBL26 WL156. REMOVED AND REPLACED ATTACH ANGLE AT FCB BS400 LBL26 WL156 IAW SRM 51-40-02 AND DWG 143A7505 ID:0002 REV: B. - [SDR SWAA2025081494243](https://openairdocs.org/sdr/SWAA2025081494243.md): Stub Frame · cracked · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Frame > FSD LOWER STUB FRAME IS CRACKED AT BS294.5 WL208. REPAIRED FSD LOWER STUB FRAME IAW SRM 53-10-15-2R-7 REPAIR-7 AND DWG 141A8310 REV-B. - [SDR SWAA2025081494254](https://openairdocs.org/sdr/SWAA2025081494254.md): Stringer Clip · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CORROSION ON STRINGER CLIP ACB STA-787 RBL-5'' FLOOR AREA. REMOVED AND REPLACED STRINGER CLIP ACB BS787 RBL5 IAW SRM 51-40-02-0G-0 AND DWG 146A8130 REV: C. - [SDR SWAA2025081494256](https://openairdocs.org/sdr/SWAA2025081494256.md): Stringer Clip · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Attach Fittings > CORROSION ON STRINGER CLIP ACB STA-807 RBL-13'' FLOOR AREA. REMOVED AND REPLACED STRINGER CLIP ACB STA 807 RBL 13 IAW SRM 51-40-02-0G-0; IAW SRM 51-40-05 AND DWG 146A1263 REV:C. - [SDR SWAA2025081494260](https://openairdocs.org/sdr/SWAA2025081494260.md): Web · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION ON SUB THRESHOLD WEB ACB BS 787 TO 847 RBL-33. REMOVED AND REPLACED ACB SUBTHRESHOLD WEB IAW SRM 51-40-02 AND DWG 146A8340 ID:0012 REV: C. - [SDR SWAA2025081494266](https://openairdocs.org/sdr/SWAA2025081494266.md): Web · corroded · Jul 22, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > MULTIPLE SPOTS WITH CORROSION ON FCB DOOR CUTOUT SURROUND THRESHOLD BS440+14; BS460;460+9 RBL30;WL156. REMOVED AND REPLACED SUBTHRESHOLD WEB AT FCB; BETWEEN BS 440 TO BS 492 RBL 30 WL 156 IAW SRM 51-40-02 AND DWG 143A8330 REV -. - [SDR SWAA2025081593551](https://openairdocs.org/sdr/SWAA2025081593551.md): Seal · cracked · Jul 21, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer Structure > LEFT HORIZONTAL STAB FWD UPPER SLIDE SEAL CRACKED. REMOVED AND REPLACED LT HORIZONTAL STAB FWD UPPER SLIDE SEAL IAW AMM 53-31-31-000-802; AMM 53-31-31-400-802 AND AMM 20-50-11-910-801 STEP 2.C.(1); D. TABLE 210. - [SDR SWAA2025081493778](https://openairdocs.org/sdr/SWAA2025081493778.md): Bear Strap · cracked · Jul 21, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK FOUND ON FSD BEAR STRAP AT BS294.5; WL 266.1; 2' IN LENGTH (MARKED)<[01] 'REPAIRED BY 737 SRM 53-10-01-2R-6 AND EA M-25-153-01539';[02] VERIFIED CORRECTIVE ACTION - [SDR SWAA2025081493777](https://openairdocs.org/sdr/SWAA2025081493777.md): Stub Frame · cracked · Jul 21, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK FOUND ON FSD STUB FRAME AT BS291.5+7.5;.6' ABOVE SEAL DEPRESSOR; 1.8' IN LENGTH. REMOVED AND REPLACED FSD STUB FRAME UPPER FWD CORNER IAW SRM 51-40-02 AND DWG 141A8370 REV D. - [SDR SWAA2025081893064](https://openairdocs.org/sdr/SWAA2025081893064.md): Fan Cowl · cracked · Jul 19, 2025 · N229WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame > NUMBER 1 ENGINE IB FAN COWL OIL DOOR SHIELD CRACKED. REMOVED AND INSTALLED A NEW FAN COWL ON CARD #TTG8Q00S5G98 STEP 4. - [SDR SWAA2025081592918](https://openairdocs.org/sdr/SWAA2025081592918.md): Seat Track · corroded · Jul 18, 2025 · N229WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CORROSION ON SEAT TRACK LBL 25 AT BS 500A+11, & BS 500C+5. PART WAS FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02. AND PART WILL BE REPACED IN CUSTOMER CARD ID: TTG8Q0144PBW. - [SDR SWAA2025081592727](https://openairdocs.org/sdr/SWAA2025081592727.md): Rib · cracked · Jul 18, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > LEFT HORIZONTAL STAB LEADING EDGE NR 5 RIB; AT LE HSS 114.55 CRACKED. REMOVED AND REPLACED NEW #5 RIB AT LE HSS 114.55 IAW SRM 51-40-02 & DWG 186A1001 REV A. - [SDR SWAA2025081492901](https://openairdocs.org/sdr/SWAA2025081492901.md): Scuff Plate · cracked · Jul 18, 2025 · N229WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ACB AFT CORNER SCUFF PLATE IS CRACKED. WELDED THE CORNER SCUFF PLATE IAW SRM 53-60-15-2R-1 STEP 4.B.(4). - [SDR SWAA2025081492311](https://openairdocs.org/sdr/SWAA2025081492311.md): Structure · cracked · Jul 17, 2025 · N229WN · Boeing 7377H4 · Leading Edge Devices > CRACK ON RT WING NR 7 SLAT AT SLAT STATION 322.71. REPAIRED IAW SRM 57-42-01-2R-8. - [SDR SWAA2025081592148](https://openairdocs.org/sdr/SWAA2025081592148.md): Rib · cracked · Jul 16, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > LEFT HAND HORIZONTAL STABILIZER INSPAR RIB 6, AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. REPAIRED IAW SRM 55-10-09-2R-4. - [SDR SWAA2025081592145](https://openairdocs.org/sdr/SWAA2025081592145.md): Rib · no discrepancy · Jul 16, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB 6; AT STABILIZER STATION 138.70; 3RD VERTICAL STIFFENER IS CRACKED. HFEC INSPECTED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB 6 IAW 6;51-00-00 PROCEDURE 23, NO CRACK NOTED. - [SDR SWAA2025081592147](https://openairdocs.org/sdr/SWAA2025081592147.md): Rib · cracked · Jul 16, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > RIGHT HORIZONTAL STABILIZER INSPAR RIB 9; AT STABILIZER STATION 166.30; 1ST VERTICAL STIFFENER IS CRACKED.<[01] HFEC INSPECTED RIGHT HAND HORIZONTAL STABILIZER INSPAR RIB 9; AT STABILIZER STATION 166.30; 1ST VERTICAL STIFFENER IAW 737 PART 6; 51-00-00 PROCEDUR - [SDR SWAA2025081592146](https://openairdocs.org/sdr/SWAA2025081592146.md): Rib · cracked · Jul 16, 2025 · N229WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > RIGHT HORIZONTAL STABILIZER INSPAR RIB 6; AT HSS 138.70; 2ND VERTICAL STIFFENER IS CRACKED. HFEC INSPECTED RIGHT HORIZONTAL STABILIZER INSPAR RIB 6 IAW 6;51-00-00 PROCEDURE 23. NO CRACK NOTED. - [SDR SWAA2025081492149](https://openairdocs.org/sdr/SWAA2025081492149.md): Seat Track · cracked · Jul 16, 2025 · N229WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CAPTAIN'S FWD INBD SEAT TRACK CRACKED. RECEIVED NEW CAPTAIN'S FWD INBD SEAT TRACK IAW AMM 25-11-11-400-801. THE INSTALLATION WILL BE PERFORM ON TASK CARD NR TTG8Q003NM2R STEP 12. - [SDR SWAA2025081492150](https://openairdocs.org/sdr/SWAA2025081492150.md): Seat Track · cracked · Jul 16, 2025 · N229WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > FIRST OFFICER I/B FWD SEAT TRACK CRACKED. RECEIVED NEW FIRST OFFICER INBD FWD SEAT TRACK IAW AMM 25-11-11-400-801. THE INSTALLATION WILL BE PERFORM ON TASK CARD TTG8Q003NM2R, STEP 12. - [SDR SWAA2025081491822](https://openairdocs.org/sdr/SWAA2025081491822.md): Floor Panel · pulled · Jul 16, 2025 · N229WN · Boeing 7377H4 · Fuselage Floor Panel > FLOOR PANEL 241CF UPPER SKIN HAS AREAS OF PULLED STRANDS. DUE TO EXTENSIVE DAMAGE, FLOOR PANEL 241CF WAS FABRICATED IAW SRM 53-00-50-2R-0. - [SDR SWAA2025081891425](https://openairdocs.org/sdr/SWAA2025081891425.md): Skin · delaminated · Jul 15, 2025 · N229WN · Boeing 7377H4 · Trailing Edge Flaps > RIGHT INBD MAIN FLAP T/E WEDGE LOWER SKIN T/E IS DELAMINATED 10' FROM O/B EDGE. REMOVED AND REPLACED RT INBD MAIN FLAP T/E WEDGE IAW AMM 20-50-11-910-801; SRM 51-40-05 AND DWG 113A2550 REV -; AIPC 27-51-11-01B AND SRM 51-40-02. - [SDR SWAA2025081491794](https://openairdocs.org/sdr/SWAA2025081491794.md): Pressure Deck · cracked · Jul 15, 2025 · N229WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK ON RH HORIZONTAL PRESSURE DECK WEB BS 663+9.5; RBL 42. L: 0.6'. PERFORMED REPAIR #2 ON PRESSURE DECK WEB BS 663+9.5' RBL 42 L:0.6' IAW SRM 53-40-51-2R-2 AND SRM 51-40-02-0G-0. - [SDR SWAA2025081490977](https://openairdocs.org/sdr/SWAA2025081490977.md): Battery Pack · no test · Jul 13, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY BATTERY PACK M1669 FAIL CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1669 PER AMM 33-51-06-960-805. FUNCTIONAL TEST WILL BE PERFORMED ON CCN: TTG8Q013Q3XC. - [SDR SWAA2025081490978](https://openairdocs.org/sdr/SWAA2025081490978.md): Battery Pack · no test · Jul 13, 2025 · N229WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY BATTERY PACK M1675 FAIL CAPACITY CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1675 AND PERFORMED GOOD OPERATIONAL TEST PER AMM 33-51-06-960-805. Next page: https://openairdocs.org/aircraft/N229WN/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 = 'N229WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N229WN/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.