# Service difficulty reports: N907WN A list on [N907WN](https://openairdocs.org/aircraft/N907WN.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 5 · 223 reports - [SDR SWAA2026042993596](https://openairdocs.org/sdr/SWAA2026042993596.md): Insulation · odor · Apr 28, 2026 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > DUE TO FLIGHT CREW REPORT OF FISH ODOR IN AIRCRAFT CABIN AND FWD CARGO PIT. ISOLATE NEUTRALIZE ODOR CAUSING AREA AS REQUIRED. R & R TWO INSULATION BLANKETS, ONE UNDER THE MIX CHAMBER AND ONE IN FRONT OF AND TO THE RT OF THE AFT CARGO BULKHEAD IAW AMM 25-8 - [SDR SWAA2026040185229](https://openairdocs.org/sdr/SWAA2026040185229.md): Battery Pack · no test · Apr 1, 2026 · N907WN · Boeing 7377H4 · Emergency Lighting > EMERGENCY BATTERY PACK, FWD ENTRY M1675 FAILED A CAPACITY CHECK. R & R CABIN EMERGENCY BATTERY PACK IAW AMM 33-51-06. - [SDR SWAA2026020667929](https://openairdocs.org/sdr/SWAA2026020667929.md): Battery Pack · inoperative · Feb 5, 2026 · N907WN · Boeing 7377H4 · Emergency Lighting > AFT EMERGENCY LIGHT BY L2 DOOR INOPERATIVE. REMOVED AND REPLACED AFT LT EMERGENCY LIGHT BATTERY PACK IAW AMM 33-51-06. OPS CHECKED GOOD. - [SDR SWAA2025103029481](https://openairdocs.org/sdr/SWAA2025103029481.md): Strap · debonded · Oct 28, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > PAX CABIN RIGHT FWD BULKHEAD LOWER STRAP DISBANDED. BONDED PAX CABIN RIGHT FWD BULKHEAD LOWER STRAP IAW SOPM 20-50-12 REV 58. - [SDR SWAA2025103124954](https://openairdocs.org/sdr/SWAA2025103124954.md): Fitting · cracked · Oct 16, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FITTING, BS 727B, RBL 24.75, FLOOR STRUCTURE. REPLACED THE FITTING IAW SRM 51-40-02-0G-0 AND DWG 146A5502 SHEET 9 REV A. - [SDR SWAA2025110324116](https://openairdocs.org/sdr/SWAA2025110324116.md): Access Panel · damaged · Oct 13, 2025 · N907WN · Boeing 7377H4 · Wing, Plate/Skin > ELONGATED HOLE ON ANGLE LOCATED ACCESS PANEL 651GB RT WING. REPLACED SUPPORT ANGLE LOCATED ON T/E ACCESS PANEL IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02. - [SDR SWAA2025110320698](https://openairdocs.org/sdr/SWAA2025110320698.md): Bracket · damaged · Oct 2, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATE HOLES ON BRACKET, HORIZONTAL PRESSURE DECK BTW BS 663 - 675, LBL 45 - 54. FABRICATED NEW BRACKET IAW SRM 51-10-02, ITEM 9, AND DWG 144A7715, SHEET 2, REV -. - [SDR SWAA2025103119889](https://openairdocs.org/sdr/SWAA2025103119889.md): Floorbeam · cracked · Sep 30, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Floor Beam > MAIN CABIN FLOORBEAM CRACKED AT BS 540, BL 0 - RBL 24.75. REPLACED THE FLOORBEAM IAW SRM 51-40-02 AND DWG 143A0060 SHEET 46 REV-. - [SDR SWAA2025103019891](https://openairdocs.org/sdr/SWAA2025103019891.md): Support Angle · elongated · Sep 30, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > AFT CARGO COMPARTMENT BULKHEAD; SUPPORT ANGLE HAS SEVERAL FASTENERS HOLES ELONGATED; BTW STA 867 AND STA 947. REPLACED SUPPORT ANGLE LOC. AFT CARGO COMPARTMENT BULKHEAD; ON BTW STA 867 AND STA 947 IAW SRM 51-40-02. - [SDR SWAA2025103019286](https://openairdocs.org/sdr/SWAA2025103019286.md): Rib · cracked · Sep 29, 2025 · N907WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACK LEADING EDGE RIB LE STA 95.96 RT HORIZONTAL STAB. REPLACED RIB IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 186A1001, SHEET 19, REV -. - [SDR SWAA2025103019287](https://openairdocs.org/sdr/SWAA2025103019287.md): Rib · cracked · Sep 29, 2025 · N907WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib > CRACK LEADING EDGE RIB LE STA 105.26 RT HORIZONTAL STAB. REPLACED LEADING EDGE RIB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, AND DWG 186A1001, SHEET 19 REV -. - [SDR SWAA2025110319070](https://openairdocs.org/sdr/SWAA2025110319070.md): Fastener · cracked · Sep 28, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Structure > EVIDENCE OF CRACK ON FASTENER ITEM A IDENTIFIED ON FIGURE 1 MT 5340-I-1520-NG COMMON TO BS 727B LBL 24.75. REFER TO FAULT TTG8Q015EFW5 WHERE 25-153-02708 WAS ADDED AS A SUBTASK. - [SDR SWAA2025110319073](https://openairdocs.org/sdr/SWAA2025110319073.md): Fastener · cracked · Sep 28, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Structure > EVIDENCE OF A CRACK ON FASTENER, ITEMS A & B IDENTIFIED ON FIGURE 1 MT 5340-I-1520-NG COMMON TO BS 727B, RBL 24.75. REPLACED FASTENERS IAW EA 25-153-02708. REFER TO FAULT TTG8Q015NQJQ. - [SDR SWAA2025103018644](https://openairdocs.org/sdr/SWAA2025103018644.md): Web · corroded · Sep 26, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SHIELD WEB LOCATED BETWEEN STA492.4 TO STA500A AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB LOC. BTW STA 492.5 TO STA 500A AND RBL21 WL156 IAW SRM 51-40-02-0G-0; SRM 51-10-02-0G-0 ITEM 9 AND DWG 143A0080 SHEET 23 REV -. - [SDR SWAA2025103018646](https://openairdocs.org/sdr/SWAA2025103018646.md): Shield · corroded · Sep 26, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SHIELD WEB LOCATED BETWEEN STA420 TO STA440 AND RBL21 WL156 AT FWD CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN STA420 TO STA440 AND RBL21 WL156 AT FWD CARGO COMPARTMENT I.A.W B737-700 SRM 51-40-02-AND DWG# 143A0080; SHEET 2 - [SDR SWAA2025103018641](https://openairdocs.org/sdr/SWAA2025103018641.md): Angle · cracked · Sep 26, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE, BS 400, S26L. REPLACED THE ANGLE AND FASTENERS IAW SRM 51-10-02-0G-0, ITEM 9, SRM 51-40-02-0G-0, AND DWG143A7505, SHEET 81, REV-. - [SDR SWAA2025103018639](https://openairdocs.org/sdr/SWAA2025103018639.md): Nut Plate · corroded · Sep 26, 2025 · N907WN · Boeing 7377H4 · Wing Miscellaneous Structure > CORROSION ON RAIL NUT-PLATE LOCATED ORSS 355 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING. REPLACED RAIL NUT-PLATE LOCATED ORSS 355 INTERNAL CAVITY UPPER AREA TRAILING EDGE AT RT WING IAW SRM 51-40-02 AND 51-10-02 ITEM 9. - [SDR SWAA2025103118223](https://openairdocs.org/sdr/SWAA2025103118223.md): Floor Support · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS277 TO BS 294.5 AND BL 0 FWD GALLEY AND LAV. REPLACED FLOOR SUPPORT IAW SRM 51-40-02-0G AND DWG 141A5400 SHEET 20 REV -. - [SDR SWAA2025103118230](https://openairdocs.org/sdr/SWAA2025103118230.md): Floor Support · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB - INTERCOSTAL FLOOR STRUCTURE LOCATED BS 344 TO BS 360 AND LBL 12 FWD GALLEY AND LAV. REPLACED THE FLOOR SUPPORT IAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG: 141A5400 SHEET: 46 REV A. - [SDR SWAA2025103118233](https://openairdocs.org/sdr/SWAA2025103118233.md): Support Angle · corroded · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORRODED SUPPORT ANGLE, BS 947.5, S25L TO S25R, WL 156. REPLACED SUPPORT ANGLE AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, DWG 149A8117, SHEET 6, REV - & DWG 149A8110, SHEET 13, REV B. - [SDR SWAA2025103118234](https://openairdocs.org/sdr/SWAA2025103118234.md): Support Bracket · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SUPPORT BRACKET, BS 947.5, STR25L. REPLACED SUPPORT BRACKET, BS 947.5, STR25L IAW SRM 51-10-02-0G-0 ITEM 9, SRM 51-40-02-0G-0, AND DWG 149A8103 SHEET: 7 REV A. - [SDR SWAA2025103118368](https://openairdocs.org/sdr/SWAA2025103118368.md): Tie Clip · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED TIE CLIP, BS 277 AND S-10R. REPLACED THE TIE CLIP IAW SRM 51-40-02 AND DWG 141A8380 SHEET 21 REV- AND 141A1110 SHEET 18 REV-. - [SDR SWAA2025103118366](https://openairdocs.org/sdr/SWAA2025103118366.md): Angle · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED ANGLE LOCATED BS 294.5 AND S-13L. REPLACED THE ANGLE LOCATED BS 294.5 AND S-13L IAW SRM 51-10-02 ITEM 9, AND DWG 141A1311 SHEET 1, REV C. - [SDR SWAA2025103118371](https://openairdocs.org/sdr/SWAA2025103118371.md): Beam · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Wing Main, Frame Structure > CRACKED BEAM ORSS 297 TRAILING EDGE AT LT WING. REPLACED THE BEAM ORSS 297 TRAILING EDGE AT LT WING IAW SRM 51-10-01 ITEM 9; SRM 51-40-02 AND DWG: 115A3700, SHEET 30, REV -.MEASUREMENT OF CRACK: 0.9390 IN. - [SDR SWAA2025103118225](https://openairdocs.org/sdr/SWAA2025103118225.md): Cargo Track · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings > CRACKED TRACK RBL 13.84 BS 747 AFT CARGO COMPARTMENT. PERFORMED REPAIR ON TRACK LOC. RBBL 13.84 BS 727D TO BS 767 AFT CARGO COMPARTMENT IAW SRM 53-00-53-2R-3 REPAIR 3; ALTERNATIVE 1 FIGURE 203. - [SDR SWAA2025103118227](https://openairdocs.org/sdr/SWAA2025103118227.md): Frame · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK FRAME ON BS 947.5 BETWEEN STRINGER 25L TO STRINGER 26L AFT CARGO COMPARTMENT. PERFORMED HFEC AND ROTOTEST INSPECTION ON HOLE LOCATED ON LBL 8.10 STA 947.5 AND NOT FOUND CRACK INDICATION AS PER 737 NDT MANUAL; PART 6; 51-00-00 PROCEDURE 23 AND AS PER NDT - [SDR SWAA2025103018367](https://openairdocs.org/sdr/SWAA2025103018367.md): Stub Frame · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Frame > CRACKED STUB FRAME LOCATED BS 294.5, S17R. REPLACED STUB FRAME AND FASTENERS IAW SRM 51-10-02 ITEM 9, SRM 51-40-02, AND DWG 141A8370, SHEET 16, SHEET 19, & 20, REV-, DWG 141A8430, SHEET 5, REV -. - [SDR SWAA2025103018372](https://openairdocs.org/sdr/SWAA2025103018372.md): Support Angle · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE BS 663.75 AND LBL 8. REPLACED ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5, STEP 4.L (1) UP TO (7); DWG 111A1000 SHEET 259 REV. - [SDR SWAA2025103018228](https://openairdocs.org/sdr/SWAA2025103018228.md): Floor Support · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED FLOOR SUPPORT BS 312 - 328, LBL 46. REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5400 SHEET 26 REV -. - [SDR SWAA2025103018226](https://openairdocs.org/sdr/SWAA2025103018226.md): Web · corroded · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CORROSION SHIELD WEB BETWEEN BS 767 TO BS 794 AND RBL 22 WL 156 AFT CARGO COMPARTMENT. REPLACED SHIELD WEB AND FASTENERS LOCATED BETWEEN BS 767 TO BS 794 AND RBL 22 WL 156 IAW SRM 51-10-02 ITEM 9; SRM 51-40-02 AND DWG: 146A0081 SHEET: 37 REV: -. - [SDR SWAA2025103018004](https://openairdocs.org/sdr/SWAA2025103018004.md): Scuff Plate · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED SCUFF PLATE AFT CORNER, IN AFT CARGO BAY. REPAIRED THE SCUFF PLATE IAW SRM 53-60-15-2R-1, REPAIR 1, AND 5975. - [SDR SWAA2025103018224](https://openairdocs.org/sdr/SWAA2025103018224.md): Web · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK WEB BS 947.5, S25R. REPLACED THE WEB IAW SRM 51-10-02, ITEM 9, SRM 51-40-02, DWG: 147A7500, SHEET 28 REV -& DWG 147A7500, SHEET 29 REV -. - [SDR SWAA2025103018365](https://openairdocs.org/sdr/SWAA2025103018365.md): Web · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACKED WEB, BS 294.5 - 303.9, S16L. REPLACED WEB IAW SRM 51-40-02-0G-0, AND DWG 141A8180, SHEET 27, SHEET 28 REV C, & SHEET 30, REV C. - [SDR SWAA2025103018376](https://openairdocs.org/sdr/SWAA2025103018376.md): Support Angle · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE, BS 663.75, RBL 8, WL 168. REPAIRED THE ANGLE IAW SRM 57-10-10-2R-5, REPAIR 5, STEP 4L 1 UP TO 7, DWG 111A1000, SHEET 259, REV A, & DWG 144A7100, SHEET 76, REV-. - [SDR SWAA2025103018375](https://openairdocs.org/sdr/SWAA2025103018375.md): Skin · cracked · Sep 25, 2025 · N907WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin > CRACK FOUND ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN AT HSS 193.90, RIB 17.5 INCHES FROM FRONT SPAR. INBD SIDE OF RIB LENGTH APPROX= 1.130 INCHES. PERFORMED REPAIR ON RT HORIZONTAL STABILIZER LOWER IN-SPAR SKIN IAW SRM 55-10-01-2R-11, REPAIR 11. - [SDR SWAA2025110317981](https://openairdocs.org/sdr/SWAA2025110317981.md): Threshold · damaged · Sep 24, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > ELONGATED HOLE ON THRESHOLD PANEL. REPLACED THRESHOLD PANEL IAW SRM 51-40-02, AND DWG 146A8340, SHEET 26, REV -. - [SDR SWAA2025103017807](https://openairdocs.org/sdr/SWAA2025103017807.md): Stub Frame · cracked · Sep 24, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK INDICATIONS, 2 EA ON STUB FRAME BETWEEN BS 294.5 - 296.5 S8 - 9R. CRACK LENGTH 1.312 IN. AND 1.125 IN. REPLACED THE STUB FRAME IAW SRM 51-40-02. - [SDR SWAA2025103017806](https://openairdocs.org/sdr/SWAA2025103017806.md): Bear Strap · cracked · Sep 24, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Plate/Skin > CRACK INDICATION ON BEAR STRAP FWD GALLEY DOOR AREA, BS 291-294.5, S8 - 9R.CRACK LENGTH 0.187 IN. REPAIRED IAW SRM 53-10-01-2R-6 AND EA M-25-153-01539. - [SDR SWAA2025103017977](https://openairdocs.org/sdr/SWAA2025103017977.md): Pressure Deck · cracked · Sep 24, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Structure > CRACK INDICATION ON HORIZONTAL PRESSURE DECK WEB LBL 31 STA 663. CRACK LENGTH: 0.200 IN. PERFORMED REPAIR ON THE PRESSURE DECK IAW SRM 53-40-51-2R-2, REPAIR 2. - [SDR SWAA2025103117544](https://openairdocs.org/sdr/SWAA2025103117544.md): Support Angle · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Fuselage Miscellaneous Structure > CRACK SUPPORT ANGLE LOCATED BS 695 BL 0. REPLACED SUPPORT ANGLE LOCATED BS 695 BL 0 IAW SRM 51-40-02 AND DWG 273A9110 SHEET 6 REV A. - [SDR SWAA2025103117343](https://openairdocs.org/sdr/SWAA2025103117343.md): Nut Plate · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Wing, Attach Fittings > CRACK ON RAIL NUT PLATE, OFSS 491 INTERNAL CAVITY LEADING EDGE, RT WING. REPLACED THE NUT PLATEIAW SRM 51-10-02-0G-0 ITEM 9; SRM 51-40-02-0G-0 AND DWG:112A4402; SHEET:13; REV -. - [SDR SWAA2025103117349](https://openairdocs.org/sdr/SWAA2025103117349.md): Nut Plate · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Wing, Attach Fittings > CRACK ON RAIL NUT PLATE, OFSS 410, INTERNAL CAVITY LEADING EDGE LT WING. REPLACED THE RAIL NUT PLATE IAW SRM 51-40-02 AND DWG 112A4402 SHEET 13 REV -. - [SDR SWAA2025103117342](https://openairdocs.org/sdr/SWAA2025103117342.md): Light · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Emergency Lighting > CRACK ON PHOTOLUMINESCENT STRIP RIGHT SIDE AT PASSENGER CABIN 6 EA. REPLACED PHOTOLUMINESCENT STRIP IAW AMM-33-51-15-400-802. - [SDR SWAA2025103117354](https://openairdocs.org/sdr/SWAA2025103117354.md): Light · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Emergency Lighting > CRACK ON PHOTOLUMINESCENT STR LEFT SIDE AT PASSENGER CABIN 6 EA. REPLACED PHOTOLUMINESCENT LIGHT IAW AMM-33-51-15-400-802. - [SDR SWAA2025103117348](https://openairdocs.org/sdr/SWAA2025103117348.md): Nut Plate · corroded · Sep 23, 2025 · N907WN · Boeing 7377H4 · Wing, Attach Fittings > CORROSION ON RAIL NUT-PLATE LOCATED OFSS 330 INTERNAL CAVITY LEADING EDGE AT LT WING. REPLACED RAIL NUT-PLATE LOCATED OFSS 330 INTERNAL
CAVITY LEADING EDGE AT LT WING IAW SRM 51-40, AND DWG 112A4402 SHEET 13 REV-. - [SDR SWAA2025103017345](https://openairdocs.org/sdr/SWAA2025103017345.md): Frame · cracked · Sep 23, 2025 · N907WN · Boeing 7377H4 · Fuselage Main, Frame > CRACK FRAME BS 727D, STRINGER 25L AFT CARGO, PERFORMED REPAIR ON FRAME IAW SRM 53-60-07-2R-2, REPAIR 2, ALTERNATIVE 2, FIGURE 205. REPAIR IS CATEGORY B. - [SDR SWAA2025103116926](https://openairdocs.org/sdr/SWAA2025103116926.md): Light · burned · Sep 22, 2025 · N907WN · Boeing 7377H4 · Emergency Lighting > BURNED EMERGENCY LIGHT ON OVERHEAD STOWAGE BIN 1 LH SIDE AT PASSENGER CABIN. REPLACED EMERGENCY LIGHT ON OVERHEAD STOWAGE BIN 1 LH SIDE AT PASSENGER CABIN IAW AMM 33-51-03-960-801 AND PERFORMED OPERATIONAL TEST IS OK. - [SDR SWAA2025103116726](https://openairdocs.org/sdr/SWAA2025103116726.md): Skin · cracked · Sep 20, 2025 · N907WN · Boeing 7377H4 · Leading Edge Devices > CRACK LOWER SURFACE OF LEADING EDGE SLAT NR 4, NOSE SKIN AT ACTUATOR, AROUND FASTENER AT LT WING. PERFORMED HFEC AND ROTOTEST INSPECTION ON HOLES LOC. LOWER SURFACE OF LEADING EDGE NR 4 SLAT NOSE SKIN AT ACTUATOR & CRACK INDICATION NOT FOUND IAW NDT MANUAL P - [SDR SWAA2025072893676](https://openairdocs.org/sdr/SWAA2025072893676.md): Acoustic Liner · delaminated · Jul 22, 2025 · N907WN · Boeing 7377H4 · Nacelle/Pylon, Main Frame > NUMBER 2 ENGINE, RT ACOUSTICAL PANEL IN 4TH POSITION DELAMINATED. REMOVED AND REPLACED PER AMM 72-23-02-401-NG AFT ACOUSTICAL PANELS. - [SDR SWAA2025051971760](https://openairdocs.org/sdr/SWAA2025051971760.md): Slide · detached · May 16, 2025 · N907WN · Boeing 7377H4 · Escape Slide > R1 DOOR EMER SLIDE FELL OUT OF COVER AND DEPLOYED<[01] REMOVED AND REPLACED FWD SERVICE DOOR EMERGENCY SLIDE PER MT 725-61-06-FS Next page: https://openairdocs.org/aircraft/N907WN/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 = 'N907WN' AND registry_match = 'registration' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/aircraft/N907WN/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.