# Service difficulty reports: N950WN

A list on [N950WN](https://openairdocs.org/aircraft/N950WN.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 · 219 reports

- [SDR SWAA2026080318656](https://openairdocs.org/sdr/SWAA2026080318656.md): Bracket · loose · Jul 29, 2026 · N950WN · Boeing 7377H4 · Emergency Equipment
  > AFT SERVICE DOOR SLIDE BRACKET LOOSE. GIRT BAR DROPS OUT SECURED BRACKET PER 25-66-02 AMM
- [SDR SWAA2026072014532](https://openairdocs.org/sdr/SWAA2026072014532.md): Fuse · inoperative · Jul 13, 2026 · N950WN · Boeing 7377H4 · Emergency Lighting
  > INOPERATIVE EMERGENCY LIGHT ON BULL NOSE BINS 4, 5, 6, 7, & 8 RT SIDE. R & R FUSES OF THE EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-06-960-804. PERFORMED TEST OF THE NEW FUSE IAW AMM 33-51-06-960-804, TESTED OK.
- [SDR SWAA2026072025994](https://openairdocs.org/sdr/SWAA2026072025994.md): Baffle · damaged · Jul 11, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON SUPPORT ZEE BAFFLE WEB FROM BS 500A - 500B, IN THE FWD CARGO BAY. REPLACED BAFFLE WEB IAW SRM 51-10-02-0G-0, AND PERFORMED REPAIR ON WEB IAW SRM 53-30-53 2R-1.
- [SDR SWAA2026072027312](https://openairdocs.org/sdr/SWAA2026072027312.md): Web · damaged · Jul 11, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > ELONGATED HOLES ON SUPPORT ZEE BAFFLE WEB FROM BS 500 - 500A, LT SIDE AT FWD CARGO BAY. REPLACED BAFFLE WEB AND FASTENERS BS 500 - 500A IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, AND DWG 146A7505, SHEET 118, AND 119 REV -.
- [SDR SWAA2026072081283](https://openairdocs.org/sdr/SWAA2026072081283.md): Fitting · deteriorated · Jul 1, 2026 · N950WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON AFT ENTRY DOOR. REPLACED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON AFT ENTRY DOOR IAW AMM 25-66-02-400-801, STEP 3.D. (1) (A) (B) THE INSTALLATION WILL BE ACCOMPLISHED ON TTG8Q01CYSUH.
- [SDR SWAA2026072081007](https://openairdocs.org/sdr/SWAA2026072081007.md): Access Panel · cracked · Jul 1, 2026 · N950WN · Boeing 7377H4 · Wing, Plate/Skin
  > CRACKED PLATE ON ACCESS PANEL 651EB AT RT WING. REMOVED & REPLACED PLATE ON ACESS PANEL 651EB AT RT WING IAW SRM 51-40-02-0G-0.
- [SDR SWAA2026072086627](https://openairdocs.org/sdr/SWAA2026072086627.md): Fitting · deteriorated · Jul 1, 2026 · N950WN · Boeing 7377H4 · Emergency Equipment
  > DETERIORATED GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA. REPLACED THE GIRT BAR FITTING HARDWARE AND ADAPTER PLATE ON FWD ENTRY AND SERVICE DOOR AT FWD GALLEY AREA IAW AMM 25-66-02-400-801.
- [SDR SWAA2026072046075](https://openairdocs.org/sdr/SWAA2026072046075.md): Rib · cracked · Jun 29, 2026 · N950WN · Boeing 7377H4 · Vertical Stabilizer, Spar/Rib
  > CRACKED ACCESS PANEL 321A RIB 8 AT VERTICAL STAB. REPLACED RIB 8 LOC ACCESS PANEL 321A VERTICAL STAB IAW SRM 51-40-02, DWG 174A1108, SHEET 2, REV C, AND DWG 174A0103, SHEET 11, REV -.
- [SDR SWAA2026072097235](https://openairdocs.org/sdr/SWAA2026072097235.md): Panel · cracked · Jun 27, 2026 · N950WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED BLADE ACCESS PANEL 343AB AT RT HORIZONTAL STAB. REPLACED BLADE ON ACCESS PANEL 343AB AT RT HORIZONTAL STAB IAW SRM 51-40-02-0G.
- [SDR SWAA2026072083445](https://openairdocs.org/sdr/SWAA2026072083445.md): Support · corroded · Jun 27, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SUPPORT ZEE BTW BS 500A TO BS 500D RBL 22 WL 156 FWD CARGO BAY. REPLACED SUPPORT ZEE AND FASTENERS LOCATED BTW BS 500A TO BS 500D, RBL 22, WL 156, IAW SRM 51-40-02-0G-0, AND DWG 143A7500, SHEET 71, REV-, DWG 143A7505, SHEET 119, REV-.
- [SDR SWAA2026072092325](https://openairdocs.org/sdr/SWAA2026072092325.md): Support Angle · cracked · Jun 27, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT ANGLE, BS 867, BTW S2R - 3R IN THE PAX CABIN. REPLACED THE SUPPORT ANGLE IAW SRM 51-40-02-0G-0, SRM 51-10-02-0G-0, ITEM 9, AND DWG 146A7901, SHEET 66, REV A.
- [SDR SWAA2026072016707](https://openairdocs.org/sdr/SWAA2026072016707.md): Web · corroded · Jun 27, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION SHIELD WEB BTW BS 492.4 TO BS 500A RBL 23 WL 156 FWD CARGO BAY. REPLACED SHIELD WEB AND FASTENERS LOCATED BTW BS 492.4 TO BS 500A RBL23 WL156 AT FWD CARGO BAY IAW SRM 51-10-02-0G-0 I?TEM 9, SRM 51-40-02-0G-0, AND DWG 143A0080, SHEET 37, REV-.
- [SDR SWAA2026072021635](https://openairdocs.org/sdr/SWAA2026072021635.md): Support Bracket · cracked · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED SUPPORT BRACKET BS 947.5, S25L AT AFT CARGO BAY. REPLACED THE SUPPORT BRACKET BS 947.5, S25L IN THE AFT CARGO BAY IAW SRM 51-10-02-0G-0, PARAGRAPH 9, SRM 51-40-02-0G-0, AND DWG 149A8103, SHEET 8, REV -.
- [SDR SWAA2026072006631](https://openairdocs.org/sdr/SWAA2026072006631.md): Stringer · cracked · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 23L, BS 540 IN THE FWD CARGO BAY. PERFORMED PERMANENT REPAIR ON STRINGER 23L, BETWEEN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1. MAJOR REPAIR IAW MPM 18.2.
- [SDR SWAA2026072022642](https://openairdocs.org/sdr/SWAA2026072022642.md): Support Angle · corroded · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CORROSION INTERNAL STRUCTURE SUPPORT ANGLE BTW BS 767 TO BS 787 AND RBL 22 WL 156 AT AFT CARGO BAY. REPLACED THE SUPPORT ANGLE BTW BS 767 - 787, RBL 22, WL 156 IN THE AFT CARGO BAY IAW SRM 51-40-020G-0, SRM 51-10-02-0G-0, PARAGRAPH 9, AND DWG 146A8123, SHEET
- [SDR SWAA2026072095431](https://openairdocs.org/sdr/SWAA2026072095431.md): Stringer · cracked · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage Main, Longeron/Stringer
  > CRACKED STRINGER 23R. BS 540. PERFORMED BEND OF REPLACEMENT STRINGER 23R SECTION BTWN BS 500D - 540 IAW SRM 53-00-03-2R-1, REPAIR 1, PARAGRAPH 4.D, FIGURE 206, SHEET 2, TABLE 202, AND SRM 51-30-01.
- [SDR SWAA2026072036332](https://openairdocs.org/sdr/SWAA2026072036332.md): Cargo Track · cracked · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage, Seat/Cargo Attach Fittings
  > CRACK CARGO TRACK RBL 13.84 AND BS 767 IN THE AFT CARGO BAY. PERFORMED A REPAIR ON CARGO TRACK LOCATED BTW BS 747 TO BS 787 RBL 13.84 AFT CARGO BAY IAW SRM 53-00-53-2R-3, REPAIR 3, FIGURE 203, SHEET 2 AND 6 PARAGRAPH 4.
- [SDR SWAA2026072056757](https://openairdocs.org/sdr/SWAA2026072056757.md): Support Bracket · cracked · Jun 26, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK SUPPORT BRACKET ON PRESSURE BULKHEAD BS 727, STR 27R IN THE AFT CARGO BAY. EVALUATED SUPPORT BRACKET AND NOT FOUND ALLOWABLE DAMAGE LIMIT IAW SRM 53-40-08-1A-3. REPLACED LOCATED ON PRESSURE BULKHEAD BS 727, STR 27R AT AFT CARGO BAY IAW SRM 51-40-02-0G
- [SDR SWAA2026072060995](https://openairdocs.org/sdr/SWAA2026072060995.md): Angle · cracked · Jun 25, 2026 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACKED ANGLE, BS 400, S25L IN FWD CARGO BAY. REPLACED NEW ANGLE IAW SRM 51-10-02-0G-0, SRM 51-40-02-0G-0, & DWG 143A7505, SHEET 107, REV-.
- [SDR SWAA2026072002975](https://openairdocs.org/sdr/SWAA2026072002975.md): Strap · cracked · Jun 25, 2026 · N950WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED DOOR CUTOUT LOWER STRAP BS 440, S25R AT FWD CARGO BAY. REPLACED CARRIER STRIP DOOR CUTOUT BS 440, S25R IAW SRM 51-40-02-0G-0, AND DWG 143A8200, SHEET 1, REV H.
- [SDR SWAA2026072048583](https://openairdocs.org/sdr/SWAA2026072048583.md): Light · deteriorated · Jun 25, 2026 · N950WN · Boeing 7377H4 · Emergency Lighting
  > DETERIORATED PHOTOLUMINESCENT STRIP (5EA) LT SIDE AND (5EA) RT SIDE ALONG PAX CABIN. REPLACED PHOTOLUMINESCENT STRIP (5EA) LT SIDE AND (5EA) RT SIDE ALONG PAX CABIN IAW AMM 33-51-15-400-802.
- [SDR SWAA2026072083840](https://openairdocs.org/sdr/SWAA2026072083840.md): Access Panel · cracked · Jun 23, 2026 · N950WN · Boeing 7377H4 · Horizontal Stabilizer, Plate/Skin
  > CRACKED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB. REPLACED BLADE ACCESS PANEL 333AB AT LT HORIZONTAL STAB IAW SRM 51-10-02, ITEM 9, AND SRM 51-40-02-0G.
- [SDR SWAA2026072023905](https://openairdocs.org/sdr/SWAA2026072023905.md): Crossbeam · cracked · Jun 23, 2026 · N950WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACK FLOOR STRUCTURE SUPPORT LOCATED BS 540 BTW LBL 0.07 TO RBL 24.82 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE SUPPORT [BRAKE PANEL] AND FASTENERS LOCATED BS 540 BTW LBL 0.07 TO RBL 24.82 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 143A0060, SHEET 5
- [SDR SWAA2026072047118](https://openairdocs.org/sdr/SWAA2026072047118.md): Crossbeam · cracked · Jun 23, 2026 · N950WN · Boeing 7377H4 · Fuselage Main, Structure
  > CRACKED FLOOR STRUCTURE SUPPORT LOCATED BS 540 BTW LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN. REPLACED FLOOR STRUCTURE SUPPORT [BRAKE PANEL] AND FASTENERS LOCATED BS 540 BTW LBL 0.07 TO LBL 24.82 AT PASSENGER CABIN IAW SRM 51-40-02-0G-0 AND DWG 143A0060, SHEE
- [SDR SWAA2026072029726](https://openairdocs.org/sdr/SWAA2026072029726.md): Access Panel · damaged · Jun 22, 2026 · N950WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 661BB AT RT WING. REPAIRED ACCESS PANEL 661BB AT RT WING IAW SRM 51-70-04-2R-10, REPAIR 10.
- [SDR SWAA2026072053379](https://openairdocs.org/sdr/SWAA2026072053379.md): Access Panel · damaged · Jun 22, 2026 · N950WN · Boeing 7377H4 · Wing, Plate/Skin
  > ELONGATED HOLES ON ACCESS PANEL 561BB AT LT WING. REPAIRED THE ACCESS PANEL 561BB AT LT WING IAW SRM 51-70-04-2R-9, REPAIR 9.
- [SDR SWAA2026052104797](https://openairdocs.org/sdr/SWAA2026052104797.md): Girt Bar · out of adjust · May 20, 2026 · N950WN · Boeing 7377H4 · Emergency Equipment
  > AFT ENTRY DOOR (L2) EMERGENCY ESCAPE SLIDE GIRT IS HANGING TOO LOW AND STRIKING THE AFT ENTRY SCUFF PLATE. SLIDE REPACKED PER MT 725-61-06. GIRT SWINGS CLEAR OF SCUFF PLATE.
- [SDR SWAA2025091512742](https://openairdocs.org/sdr/SWAA2025091512742.md): Seal · cracked · Sep 9, 2025 · N950WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > LEFT HORIZONTAL STAB UPPER FWD SLIDING SEAL FOUND CRACKED. REMOVED AND REPLACED THE UPPER FWD HORIZONTAL STAB SLIDING SEAL ON LT SIDE AND REPLACED WITH NEW IAW AMM 53-31-31. INSPECTED IAW AMM 53-31-31-401, CONFIG 1-NG.
- [SDR SWAA2025091512747](https://openairdocs.org/sdr/SWAA2025091512747.md): Seal · cracked · Sep 9, 2025 · N950WN · Boeing 7377H4 · Horizontal Stabilizer Miscellaneous Structure
  > RIGHT HORIZONTAL STAB UPPER FWD SLIDING SEAL FOUND CRACKED. R & R RT HORIZONTAL STAB UPPER FWD SLIDING SEAL IAW AMM 53-31-31. INSPECTED IAW AMM 53-31-31-401, CONFIG 1.
- [SDR SWAA2025090208481](https://openairdocs.org/sdr/SWAA2025090208481.md): Transmitter · stuck · Aug 26, 2025 · N950WN · Boeing 7377H4 · Trailing Flap Position Indicating System
  > TRAILING EDGE FLAP DISAGREE COMMANDED POSITION WAS 30 FLAPS STUCK BETWEEN25-30<[01] 01 - REMOVED AND REPLACED PER [AMM 27-58-01-401-NG (FLAP POSITION TRANSMITTER - REMOVAL/INSTALLATION - PERMANENT)] OPS CHECK NORMAL. NO FAULTS AT THIS TIME.
- [SDR SWAA2024082727703](https://openairdocs.org/sdr/SWAA2024082727703.md): Battery Pack · inoperative · Aug 19, 2024 · N950WN · Boeing 7377H4 · Emergency Lighting
  > SEVERAL EXTERIOR AND INTERIOR EMERGENCY LIGHTS INOPERATIVE.<[01] PERFORMED TROUBLESHOOTING AND FOUND BATTERY PACKS DEFECTIVE AT POS. M1670 AND M1672 AS PER B737 SSM 33-51-14 & 33-51-13; REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT POS. M1670 AND M1672
- [SDR SWAA2024082722576](https://openairdocs.org/sdr/SWAA2024082722576.md): Intercostal · corroded · Aug 5, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT INTERCOASTAL FROM STA 747 TO 767 HAS CORROSION AROUND FASTENER HOLES<[01] STARTED REMOVING CORROSION PER SRM 51-40-02-0G-0 AND FOUND THAT THE CORROSION WAS ALL THE WAY THROUGH THE PART MAKING IT OUT OF LIMITS PER SRM 53-00-53-1A-2. REMOVED AFT
- [SDR SWAA2024082722337](https://openairdocs.org/sdr/SWAA2024082722337.md): Shield · cracked · Aug 3, 2024 · N950WN · Boeing 7377H4 · Nacelle/Pylon Miscellaneous Structure
  > #2 ENGINE IB FAN COWL SHIELD 314-2259-X CRACKED. CORRECTION...#1 ENGINE IB FAN COWL...<[01] REMOVED AND INSTALLED NEW SHIELD AT #1 ENGINE I/B FAN COWL AS PER B737-700 SRM 51-40-02-0G-0 PARA 4 AND 5.;[02] FINAL INSPECTION; VERIFIED STEP #1.
- [SDR SWAA2024082722049](https://openairdocs.org/sdr/SWAA2024082722049.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 727E TO 747<[01] REMOVED CORROSION ON AFT CARGO RIGHT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 727E TO 747 PER REF AMM 51-10-02-0G-0. ACCOMPLISHED NDT AND CHECKED LIMITS OF REWORKED AREA. OR
- [SDR SWAA2024082722054](https://openairdocs.org/sdr/SWAA2024082722054.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 727D TO 727E<[01] REMOVED CORROSION ON AFT CARGO LEFT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 727D TO 727E PER REF AMM 51-10-02-0G-0. ACCOMPLISHED NDT AND CHECKED LIMITS OF REWORKED AREA. O
- [SDR SWAA2024082722051](https://openairdocs.org/sdr/SWAA2024082722051.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 727E TO 747<[01] REMOVED CORROSION TO AFT CARGO RIGHT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 727E TO 747 PER REF SRM 51-10-02-0G-0 AND CHECKED LIMITS OF REWORKED AREA ORIGINAL THICKNESS:
- [SDR SWAA2024082722052](https://openairdocs.org/sdr/SWAA2024082722052.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 727D TO 727E<[01] REMOVED CORROSION AFT CARGO RIGHT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 727D TO 727E PER REF AMM 51-10-02-0G-0. CHECKED LIMITS OF REWORKED AREA. ORIGINAL THICKNESS:.040
- [SDR SWAA2024082722053](https://openairdocs.org/sdr/SWAA2024082722053.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 747 TO 767 CORRECTION TO FAULT DESCRIPTION: AFT CARGO RIGHT FWD 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 747 TO 767<[01] REMOVED CORROSION ON AFT CARGO FWD RIGHT Z CHANNEL; FO
- [SDR SWAA2024082722058](https://openairdocs.org/sdr/SWAA2024082722058.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO RIGHT 'Z' CHANNEL HAS CORROSION ON FASTENER HOLES ON STA 727B TO 727C<[01] REMOVED CORROSION AFT CARGO RIGHT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 727B TO 727C PER REF AMM 51-10-02-0G-0. CHECKED LIMITS OF REWORKED AREA. ORIGINAL THICKNESS:.040'; M
- [SDR SWAA2024082722056](https://openairdocs.org/sdr/SWAA2024082722056.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT 'Z' CHANNEL HAS CORROSION ON FASTENER HOLES ON STA 767 TO 787<[01] REMOVED CORROSION AFT CARGO LEFT 'Z' CHANNEL AROUND FASTENER HOLES ON STA 767 TO 787 PER REF AMM 51-10-02-0G-0. ACCOMPLISHED NDT AND CHECKED LIMITS OF REWORKED AREA. ORIGINAL THI
- [SDR SWAA2024082722050](https://openairdocs.org/sdr/SWAA2024082722050.md): Channel · corroded · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > AFT CARGO LEFT 'Z' CHANNEL HAS CORROSION AROUND FASTENER HOLES ON STA 747 TO 767<[01] REMOVED CORROSION ON AFT CARGO LEFT Z CHANNEL; FOUND OUT OF LIMITS AND REMOVED; FABRICATED MATERIAL USED: BAC1496-377 7075T6 AND INSTALLED NEW LEFT Z CHANNEL. PER SRM 51-10-0
- [SDR SWAA2024082722048](https://openairdocs.org/sdr/SWAA2024082722048.md): Vapor Barrier · cracked · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CRACK FOUND AT FASTENER HOLE LBL 9 EXTERNAL VAPOR BARRIER UPPER ATTACHMENT ANGLE ADJACENT TO CENTER BOX REAR SPAR STA 663<[01] REMOVED; REPAIRED AND RE-INSTALLED LH VAPOR BARRIER UPPER ATTACHMENT ANGLE STA 663 PER SRM 51-40-02-0G-0 AND SRM 57-10-10-2R-5.;[02]
- [SDR SWAA2024082722047](https://openairdocs.org/sdr/SWAA2024082722047.md): Angle · cracked · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT FASTENER HOLE RBL 9 EXTERNAL VAPOR BARRIER UPPER ATTACHMENT ANGLE ADJACENT TO CENTER BOX REAR SPAR STA 663<[01] REMOVED AND REPLACED VAPOR BARRIER UPPER ATTACH FUEL TANK ANGLE STA 663 PER SRM 51-40-02-0G-0 AND DWG#111A1000;[02] (RII) FINAL INSPE
- [SDR SWAA2024082722046](https://openairdocs.org/sdr/SWAA2024082722046.md): Angle · cracked · Aug 2, 2024 · N950WN · Boeing 7377H4 · Fuselage Miscellaneous Structure
  > CRACK FOUND AT FASTENER HOLE RBL 53 EXTERNAL VAPOR BARRIER UPPER ATTACHMENT ANGLE ADJACENT TO CENTER BOX REAR SPAR STA 663<[01] REPLACEMENT OF ANGLE ACCOMPLISHED ON TASKCARD #TTG8Q00UZFNR;[02] FINAL INSPECTION; VERIFIED STEP #1.
- [SDR SWAA2024082721355](https://openairdocs.org/sdr/SWAA2024082721355.md): Girt Bar · torn · Aug 1, 2024 · N950WN · Boeing 7377H4 · Emergency Equipment
  > L1 SLIDE DOOR AT LOWER POSITION ATTACH GIRT BAR;LOWER SEAL WEAR AND TORN NOTED.<[01] L-1 DOOR SLIDE WAS REPLACED ON MT CARD # 725-61-06 CUSTOMER BARCODE: TTG8Q00V33GK;[02] FINAL INSPECTION; VERIFIED STEP #1.
- [SDR SWAA2024082721626](https://openairdocs.org/sdr/SWAA2024082721626.md): Floor Panel · delaminated · Aug 1, 2024 · N950WN · Boeing 7377H4 · Fuselage Floor Panel
  > CABIN FLOOR PANEL 241AF UPPER SKIN DELAMINATED TORN.<[01] RECEIVED LOCETED MATERIAL PN. 4417A4400001CC-10 AD FABRICATED NEW FLOR PANEL 241AF REF. DWG. 144A5810;[02] VERIFIED RECEIVED MATERIAL AND FABRICATED FLOOR PANEL
- [SDR SWAA2024082724442](https://openairdocs.org/sdr/SWAA2024082724442.md): Duct · corroded · Jul 31, 2024 · N950WN · Boeing 7377H4 · Engine Thrust Reverser
  > #1 ENGINE OB TR C-DUCT AFT EXHAUST INNER SURFACE WITH PITTING CORROSION SPOTS.<[01] #1 ENGINE O/B T/R IS BEING REPLACED ON TTG8Q00UYKAX;[02] VERIFIED STEP 1
- [SDR SWAA2024082721048](https://openairdocs.org/sdr/SWAA2024082721048.md): Vapor Barrier · cracked · Jul 31, 2024 · N950WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > ACCOMPLISH REPAIR OF L/H VAPOR BARRIER AS REQUIRED<[01] LATE ENTRY; WORK ACCOMPLISHED ON 08-04-24; APPLIED REPAIR AT L/H VAPOR BARRIER STA 663 ON FWD AND AFT SIDE AS PER B737 SRM 51-70 -04-2R-10 PARAG 4F AND 737 SRM57-10-10-2R-2 AND SRM 51-70-04-2R-0 PARAG4-N
- [SDR SWAA2024082721049](https://openairdocs.org/sdr/SWAA2024082721049.md): Vapor Barrier · cracked · Jul 31, 2024 · N950WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > ACCOMPLISH REPAIR OF R/H VAPOR BARRIER AS REQUIRED<[01] LATE ENTRY;WORK ACCOMPLISHED ON 08-04-2024; APPLIED REPAIR AT R/H VAPOR BARRIER STA 663 ON FWD AND AFT SIDE AS PER B737 SRM 51-70-04-2R-10 PARG 4F AND B737 SRM 57-10-10-2R-2 AND SRM 51-70-04-2R-0 PARAG 4
- [SDR SWAA2024082721045](https://openairdocs.org/sdr/SWAA2024082721045.md): Bulkhead Web · cracked · Jul 31, 2024 · N950WN · Boeing 7377H4 · Fuselage Main, Bulkhead
  > CENTER WING REAR VAPOR WEB STA 663.75;LBL 10 HAS CRACK EVIDENCE NOTED(LOWER # 1 ELECTRIC HYDRAULIC PUMP).<[01] REPAIR OF L/H VAPOR BARRIER WAS ACCOMPLISHED ON BARCODE TTG8Q00UXQ95;[02] FINAL INSPECTION; VERIFIED STEP #1.

Next page: https://openairdocs.org/aircraft/N950WN/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 = 'N950WN' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N950WN/reports

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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.