# Service difficulty reports: N482WN

A list on [N482WN](https://openairdocs.org/aircraft/N482WN.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 7 · 301 reports

- [SDR SWAA2026100741317](https://openairdocs.org/sdr/SWAA2026100741317.md): Pump · low pressure · Oct 3, 2026 · N482WN · Boeing 7377H4 · Hydraulic Pump (Electric/Engine), Main
  > ENG 1 HYD PUMP LOW PRESSURE LIGHT CAME ON IN FLIGHT. HYDRAULIC SYSTEM A QTY: 13% PRESS: 3080.
- [SDR SWAA2026071420114](https://openairdocs.org/sdr/SWAA2026071420114.md): Attach Bracket · cracked · Jul 10, 2026 · N482WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET IS CRACKED. REMOVED AND REPLACED AFT ENTRY (L2) DOOR LOWER DOOR LINER ATTACHMENT PANEL BRACKET USING SRM 51-40-02
- [SDR SWAA2026071320213](https://openairdocs.org/sdr/SWAA2026071320213.md): Battery Pack · failed · Jul 10, 2026 · N482WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.
- [SDR SWAA2026071320978](https://openairdocs.org/sdr/SWAA2026071320978.md): Battery Pack · no test · Jul 10, 2026 · N482WN · Boeing 7377H4 · Emergency Lighting
  > FLIGHT DECK, BATTERY PACKS M1668 & M1675 EACH FAILED RESPECTIVE CAPACITY TESTS. R & R BATTERY PACKS M1668 & M1675 IAW AMM 33-51-06.
- [SDR SWAA2026071019308](https://openairdocs.org/sdr/SWAA2026071019308.md): Sign · broken · Jul 7, 2026 · N482WN · Boeing 7377H4 · Emergency Lighting
  > CENTER CABIN CEILING OVER WING EMERGENCY EXIT SIGN BROKEN. REMOVED AND REPLACED IAW AMM 33-51-01-960-802-NG.
- [SDR SWAA2026061807884](https://openairdocs.org/sdr/SWAA2026061807884.md): Strap · corroded · May 30, 2026 · N482WN · Boeing 7377H4 · Spoilers
  > CORROSION ON RETAINER STRAP SEAL, SPOILER 1, LT WING. REPLACED RETAINER STRAP SEAL SPOILER 1 AT LT WING IAW SRM 51-40-02, DWG 115A3500, SHEET 22, REV A.
- [SDR SWAA2026061707972](https://openairdocs.org/sdr/SWAA2026061707972.md): Plate · cracked · May 30, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED OTBD TRAILING EDGE CORRUGATED PLATE ON ORSS 314, RT WING. REPLACED CORRUGATED PLATE LOCATED OTBD TRAILING EDGE ON ORSS 314 AT RT WING. IAW SRM 51-40-02-0G-0 AND DWG 115A3700, SHEET 32 REV-.
- [SDR SWAA2026061707883](https://openairdocs.org/sdr/SWAA2026061707883.md): Plate · cracked · May 30, 2026 · N482WN · Boeing 7377H4 · Trailing Edge Flaps
  > CRACKED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING. REPLACED CORRUGATED PLATE TRAILING EDGE LOCATED ON IRSS 261 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001 SHEET 26 REV-.
- [SDR SWAA2026061707881](https://openairdocs.org/sdr/SWAA2026061707881.md): Support Angle · cracked · May 30, 2026 · N482WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED OTBD TRAILING EDGE SUPPORT ANGLE ON ORSS 287 AT LT WING. REPLACED OTBD TE SUPPORT ANGLE AT ORSS 287, LT WING IAW SRM 51-40-02-0G-0, DWG 115A3700, SHEET 31, REV-, & DWG 115A3712, SHEET 12, REV-.
- [SDR SWAA2026061707882](https://openairdocs.org/sdr/SWAA2026061707882.md): Support Bracket · cracked · May 30, 2026 · N482WN · Boeing 7377H4 · Wing Miscellaneous Structure
  > CRACKED TRAILING EDGE SUPPORT BRACKET LOCATED ON IRSS 268 AT LT WING. REPLACED SUPPORT BRACKET LOCATED TRAILING EDGE IRSS 268 AT LT WING IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 115A2930, SHEET 7, REV -.
- [SDR SWAA2026061707886](https://openairdocs.org/sdr/SWAA2026061707886.md): Plate · cracked · May 30, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED INBD TRAILING EDGE CORRUGATED PLATE LOCATED ON IRSS 242 AT LT WING. REPLACED CORRUGATED PLATE LOCATED ON INBD TRAILING EDGE IRSS 242 AT LT WING IAW SRM 51-40-02-0G-0 AND DWG 115A2001, SHEET 30, REV A.
- [SDR SWAA2026061807351](https://openairdocs.org/sdr/SWAA2026061807351.md): Fitting · cracked · May 28, 2026 · N482WN · Boeing 7377H4 · Leading Edge Devices
  > REMOVE AND REPLACE SLAT 1 LT WING DUE TO SECONDARY FINDING: CRACK ON FITTING SLAT 1. REPLACED LEADING EDGE SLAT 1 IAW AMM 27-81-21-401. TESTED OK.
- [SDR SWAA2026061707339](https://openairdocs.org/sdr/SWAA2026061707339.md): Rib · cracked · May 27, 2026 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACKED INSPAR RIB LOCATED STAB BS 129.50 AND 18 INCH FROM FRONT SPAR RT HORIZONTAL STAB. PERFORMED PERMANENT REPAIR ON INSPAR RIB STA 129.50 AND 18 INCHS OF FRONT SPAR RT HORIZONTAL STABILIZER IAW SRM 55-10-09-2R-4 REPAIR 4.
- [SDR SWAA2026061707340](https://openairdocs.org/sdr/SWAA2026061707340.md): Support Angle · elongated · May 27, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame Structure
  > ELONGATED HOLE ON SUPPORT ANGLE FOR ACCESS PANEL 551FB TRAILING EDGE AT LT WING. REPLACED SUPPORT ANGLE AND RE-INSTALLED BRACKET(2E/A) ACCESS PANEL 551FB TRAILING EDGE AT LT WING IAW SRM 51-10-02-OG-0, ITEM 9, SRM 51-40-02-OG-0, SRM 51-20-01-0G-0, AND DWG 11
- [SDR SWAA2026061707341](https://openairdocs.org/sdr/SWAA2026061707341.md): Support Angle · cracked · May 27, 2026 · N482WN · Boeing 7377H4 · Wing Main, Frame Structure
  > CRACKED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING. REPLACED SUPPORT ANGLE, ACCESS PANEL 651GB AT RT WING IAW SRM 51-40-02-0G-0 AND SRM 51-10-02 ITEM 9.
- [SDR SWAA2026061706551](https://openairdocs.org/sdr/SWAA2026061706551.md): Access Panel · damaged · May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 661BB AT RT WING. REPAIRED THE ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706765](https://openairdocs.org/sdr/SWAA2026061706765.md): Scuff Plate · cracked · May 26, 2026 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED AFT CORNER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED AFT CORNER SCUFF PLATE AT AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026061706766](https://openairdocs.org/sdr/SWAA2026061706766.md): Scuff Plate · cracked · May 26, 2026 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT. REPAIRED CENTER SCUFF PLATE LOCATED AFT CARGO COMPARTMENT IAW SRM 53-60-15-2R-1, REPAIR 1, AND BAC 5975.
- [SDR SWAA2026061706552](https://openairdocs.org/sdr/SWAA2026061706552.md): Access Panel · damaged · May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ON ACCESS PANEL 661CB TRAILING EDGE AT RT WING. REPAIRED ACCESS PANEL 661CB TRAILING EDGE AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706548](https://openairdocs.org/sdr/SWAA2026061706548.md): Access Panel · damaged · May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 561AB AT LT WING. REPAIRED THE ACCESS PANEL 561AB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706550](https://openairdocs.org/sdr/SWAA2026061706550.md): Access Panel · damaged · May 26, 2026 · N482WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLE ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026061706219](https://openairdocs.org/sdr/SWAA2026061706219.md): Skin · cracked · May 24, 2026 · N482WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK AROUND FASTENER LOWER SURFACE LEADING EDGE SLAT NOSE SKIN AT THE ACTUATOR FITTING SLAT 7 AT RT WING. REPLACED SLAT NR 7 DUE TO SEVERAL CRACKS DAMAGE AT LOWER SKIN AND FITTING. REPLACED WITH FAULT TTG8Q01CFMD6.
- [SDR SWAA2026061706218](https://openairdocs.org/sdr/SWAA2026061706218.md): Skin · cracked · May 24, 2026 · N482WN · Boeing 7377H4 · Leading Edge Devices
  > CRACK LOWER SURFACE OF LEADING EDGE SLAT 1 NOSE SKIN AT ACTUATOR LOC. AROUND FASTENER AT LT WING. REPLACED SLAT NR 1 DUE TO WAS FOUND SEVERAL CRACKS DAMAGE. FOR REPLACE SEE FAULT TTG8Q01CF1A3.
- [SDR SWAA2025121242831](https://openairdocs.org/sdr/SWAA2025121242831.md): Tail Cone · delaminated · Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic Fairings
  > THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4' LEFT OF TOP. CRACK LENGTH, L=4' W=2.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NE
- [SDR SWAA2025121242832](https://openairdocs.org/sdr/SWAA2025121242832.md): Tail Cone · delaminated · Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic Fairings
  > THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. BS 1193.5; 24.5' RIGHT OF TOP. CRACK LENGTH, L=3' W=1.5'. THE TAIL CONE WAS REMOVED AND REPLACED WITH A NEW
- [SDR SWAA2025121246031](https://openairdocs.org/sdr/SWAA2025121246031.md): Tail Cone · delaminated · Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic Fairings
  > THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID. LOCATED BS 1192; 4 INCHES LT OF TOP. CRACK LENGTH, L=4' W=2.5'. TAIL CONE R & R WITH A NEW ONE.
- [SDR SWAA2025121246032](https://openairdocs.org/sdr/SWAA2025121246032.md): Tail Cone · delaminated · Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic Fairings
  > THE FORWARD TAIL CONE FAIRING IS DELAMINATED WITH DAMAGE TO THE FACE SHEETS WITH FIBERS AND HONEYCOMB EXPOSED AND CONTAMINATED WITH HYDRAULIC FLUID, BS 1193.5; 24.5' RT OF TOP. CRACK LENGTH, L=3' W=1.5'. TAIL CONE R & R WITH A NEW ONE.
- [SDR SWAA2025121242833](https://openairdocs.org/sdr/SWAA2025121242833.md): Tail Cone · delaminated · Dec 5, 2025 · N482WN · Boeing 7377H4 · Aerodynamic Fairings
  > THE FORWARD TAIL CONE FAIRING IS DELAMINATED, BS 1190 21 INCHES RIGHT OF TOP. CRACK LENGTH: L=2.3' W=2.2'. LOCATED & DRILLED INITIAL TAIL CONE SCREW HOLES WITH EXCEPTION OF HOLES AROUND ELEVATOR PUSH ROD CUT OUTS IAW MM 51-40-02 & SIP. TAIL CONE WAS R & R
- [SDR SWAA2025091213803](https://openairdocs.org/sdr/SWAA2025091213803.md): Lens · loose · Sep 11, 2025 · N482WN · Boeing 7377H4 · Emergency Lighting
  > OVERHEAD EMERGENCY EXIT SIGN LENS LOOSE. SECURED LENS PER AMM 33-51-01.
- [SDR SWAA2025042125797](https://openairdocs.org/sdr/SWAA2025042125797.md): Sign · detached · Apr 16, 2025 · N482WN · Boeing 7377H4 · Emergency Lighting
  > MID CABIN OVERHEAD EXIT SIGN FELL OFF. SECURED SIGN AS PER SIP
- [SDR SWAA2025030601774](https://openairdocs.org/sdr/SWAA2025030601774.md): Seal · cracked · Mar 4, 2025 · N482WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > R/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.
- [SDR SWAA2025030601773](https://openairdocs.org/sdr/SWAA2025030601773.md): Seal · cracked · Mar 4, 2025 · N482WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > L/H HORIZONTAL UPPER SLIDER CRACKED<[01] REF ADDED;[02] REMOVED AND REPLACED PER 53-31-31.
- [SDR SWAA2025012489193](https://openairdocs.org/sdr/SWAA2025012489193.md): Handle · broken · Jan 23, 2025 · N482WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM FWD LAV AND INSTALLED ON AFT LEFT ENTRY DOOR IAW AMM 52-13-31. FWD LAV ASSIST HANDLE INOP. OK TO CONTINUE PER MEL 25-10-01 SP 1B;[02] REPLACED MISSING FWD LAV ASSIST HANDLE PER CMM 25-42-59.
- [SDR SWAA2025012288475](https://openairdocs.org/sdr/SWAA2025012288475.md): Handle · broken · Jan 22, 2025 · N482WN · Boeing 7377H4 · Passenger/Crew Doors
  > AFT ENTRY DOOR ASSIST HANDLE BROKEN<[01] ROBBED ASSIST HANDLE FROM AFT LAV AND INSTALLED ON AFT ENTRY DOOR IAW AMM 52-13-31. AFT LAV ASSIST HANDLE INOP. OK TO CONTINUE PER MEL 25-10-01 SP 1B. REPLACED MISSING AFT LAV ASSIST HANDLE PER CMM 25-42-60.
- [SDR SWAA2024080713755](https://openairdocs.org/sdr/SWAA2024080713755.md): Seat Track · cracked · Jul 18, 2024 · N482WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727 AND AT LBL 45.5 HOLE POSITION B 2024-405210 CRACK INDICATION ON FLOOR STRUCTURE SEAT TRACK AT BS 727B AND AT LBL 45.5 HOLE POSITION B<[01] PERFORMED REPAIR CATEGORY A LOC ON FLOOR STRUCTURE SEAT TRACK BT
- [SDR SWAA2024080709054](https://openairdocs.org/sdr/SWAA2024080709054.md): Access Panel · cracked · Jul 4, 2024 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA198.23 LT HORIZONTAL STAB 2024-405175<[01] REPLACED RIB LOC ON LEADING EDGE STA198.23 ACCESS PANEL 331B HORIZONTAL STABILIZER LH IAW B737-700 SRM 51-40-02 AND SRM 51-10-02 ITEM 9. DWG 186A1001; SHEET 11; R
- [SDR SWAA2024080709053](https://openairdocs.org/sdr/SWAA2024080709053.md): Rib · cracked · Jul 4, 2024 · N482WN · Boeing 7377H4 · Horizontal Stabilizer, Spar/Rib
  > CRACK LEADING EDGE RIB ACCESS PANEL 331B LOCATED LE STA188.94 LT HORIZONTAL STAB 2024-405174<[01] REPLACED NEW RIB 188.94 AND FASTENERS LOCATED ON LEADING EDGE HORIZONTAL STABILIZER ACCESS PANEL 331B LH IAW B737-700 SRM 51-40-02 AND DWG 186A1001 SHEET 11 REV:
- [SDR SWAA2024080821406](https://openairdocs.org/sdr/SWAA2024080821406.md): Unknown · unknown · Jul 2, 2024 · N482WN · Boeing 7377H4 · Standard Practices/Structures
  > THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 RIGHT SIDE IS 0.024 INCH 2024-405139<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC80; RII
- [SDR SWAA2024080821405](https://openairdocs.org/sdr/SWAA2024080821405.md): Unknown · unknown · Jul 2, 2024 · N482WN · Boeing 7377H4 · Standard Practices/Structures
  > THICKNESS MEASUREMENT OF GAP BETWEEN INNER CHORD AND WEB S-18A BS 727 LEFT SIDE IS 0.037 INCH 2024-405138<[01] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V;[02] FAULT RESOLVED ON OTHER FAULT TTG8Q00UBC7V; RII
- [SDR SWAA2024080707754](https://openairdocs.org/sdr/SWAA2024080707754.md): Frame · cracked · Jul 1, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN 2024-405134<[01] EQUIPMENT USED P/N: NORTEC 600D; S/N: 220272512; DUE DATE: 08-JAN-25;[02] PERFORMED REPAIR ON FRAME WEB LOCATED BS259.5 BTW STR8L AND STR9L AT PASSENGER CABIN IAW EA 24-
- [SDR SWAA2024080719012](https://openairdocs.org/sdr/SWAA2024080719012.md): Stringer · cracked · Jun 29, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 8 INTERNAL AREA FUEL TANK UPPER POSITION LOC. BTW RIB 19 AND RIB 20 AT LT WING 2024-405124<[01] PERFORMED REPAIR CATEGORY A ON STRINGER 8 INTERNAL AREA FUEL TANK UPPER POSITION LOC. BTW RIB 19 AND RIB 20 AT LT WING IAW 24-157-01864. SEE INDIVIDU
- [SDR SWAA2024080706185](https://openairdocs.org/sdr/SWAA2024080706185.md): Bolt · worn · Jun 27, 2024 · N482WN · Boeing 7377H4 · Emergency Equipment
  > WEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405056<[01] REPLACED GIRT BAR FITTING BOLT FWD POSITION ENTRY DOOR AT AFT GALLEY AREA (2 EA) IAW B737-700 AMM 25-66-02-400-801.;[02] CORRECTED STEP 1 <BR>REPLACED GIRT BAR FITTING BOLT F
- [SDR SWAA2024080706183](https://openairdocs.org/sdr/SWAA2024080706183.md): Bolt · worn · Jun 27, 2024 · N482WN · Boeing 7377H4 · Emergency Equipment
  > WEAR ON GIRT BAR FITTING BOLT FWD POSITION AT AFT GALLEY AREA (2 EA) 2024-405217<[01] FAULT WILL RESOLVED ON ANOTHER FAULT DUE TO DUPLICATED DISCREPANCY REPORT. <BR>TTG8Q00U7VJ1;[02] CORRECTED STEP 1 <BR>FAULT WILL RESOLVED ON ANOTHER FAULT DUE TO DUPLICATED D
- [SDR SWAA2024080705917](https://openairdocs.org/sdr/SWAA2024080705917.md): Stringer · cracked · Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 26L LOCATED BS540 AT FWD CARGO COMPARTMENT 2024-405036<[01] TOOL USED ULTRASONIC THICKNESS EQUIPMENT PN:45MG; SN:430063701; DUE DATE:24-JUL-24.;[02] TOOL USED ON STEP 5: EDDY CURRENT EQUIPMENT P/N: NORTEC 600D; S/N: 210138003; DUE DATE: 11-JUN-2
- [SDR SWAA2024080705918](https://openairdocs.org/sdr/SWAA2024080705918.md): Stringer · cracked · Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT 2024-405037 CRACK STRINGER 24L LOCATED BS540 FWD CARGO COMPARTMENT<[01] STEP 2. ULTRASONIC EQUIPMENT USED P/N: 45MG; S/N: 2218618T11 AND DUE DATE: 30-NOV-24.;[02] CORRECTED STEP 1. <BR>STEP 2. ULTRASONIC
- [SDR SWAA2024080705916](https://openairdocs.org/sdr/SWAA2024080705916.md): Intercostal · cracked · Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS500D TO BS520 AND S-28R FWD CARGO COMPARTMENT 2024-405034<[01] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811020; DUE DATE: 23-JAN-25 AND TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; DUE DATE
- [SDR SWAA2024080705915](https://openairdocs.org/sdr/SWAA2024080705915.md): Intercostal · cracked · Jun 26, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO COMPARTMENT 2024-405035<[01] REPLACED WEB - INTERCOSTAL LOCATED BS 500D TO BS 520 AND S-28L FWD CARGO COMPARTMENT IAW B737-700 SRM 51-10-02 Ï¿½TEM 9 AND SRM 51-40-02. AND DWG 143A7902 REV A
- [SDR SWAA2024080705556](https://openairdocs.org/sdr/SWAA2024080705556.md): Frame · cracked · Jun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Frame
  > CRACK FRAME WEB LOCATED STA259.5 AND BETWEEN STR8R TO STR9R AT FWD GALLEY AREA 2024-405014<[01] TOOL USED STEP 5 EDDY CURRENT EQUIPMENT. PN: NORTEC 600D; SN:210138003; DUE DATE: 11-JUN-25;[02] PERFORMED REPAIR ON FRAME WEB LOCATED STA259.5 AND BETWEEN STR 8R T
- [SDR SWAA2024080705558](https://openairdocs.org/sdr/SWAA2024080705558.md): Stringer · cracked · Jun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACK STRINGER 7L LOCATED BETWEEN STA303.9 TO STA294.5 AT PASSENGER CABIN 2024-405020<[01] STEP 7 TOOL USED EDDY CURRENT EQUIPMENT PN: NORTEC 600D; SN: 200053402; DUE DATE: 24-AUG-24;[02] TOOL USED: TEMPERATURE CONTROLLER P/N: P3015GOES00000; S/N: 142811019; D
- [SDR SWAA2024080705555](https://openairdocs.org/sdr/SWAA2024080705555.md): Support · elongated · Jun 25, 2024 · N482WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLE SUPPORT ZEE LOCATED BS 887 TO BS 907 AND S-25R AT AFT CARGO COMPARTMENT 2024-405009<[01] REJECTION MISSING FASTENERS SUPPORT ZEE AND RIVET BTW STA 887 TO STA 947.5 STR 25R AT AFT CARGO COMPARTMENT (4 EA) SEE TTG8Q00UW75F;[02] REPLACED SUPPORT ZE

Next page: https://openairdocs.org/aircraft/N482WN/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 = 'N482WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N482WN/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.