# Service difficulty reports: N568WN, cancelled Oct 30, 2024

A list on [N568WN, cancelled Oct 30, 2024](https://openairdocs.org/deregistered/N568WN-2024-10-30.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 2 · 96 reports

- [SDR SWAA2019112739180](https://openairdocs.org/sdr/SWAA2019112739180.md): Battery Pack · discharged · Nov 25, 2019 · N568WN · Boeing 73776N · Emergency Lighting
  > SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 14. R&R BATTERY PACK PER AMM.
- [SDR SWAA2019112739179](https://openairdocs.org/sdr/SWAA2019112739179.md): Battery Pack · discharged · Nov 25, 2019 · N568WN · Boeing 73776N · Emergency Lighting
  > SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 9. R&R BATTERY PACK PER AMM.
- [SDR SWAA2019112739178](https://openairdocs.org/sdr/SWAA2019112739178.md): Battery Pack · discharged · Nov 25, 2019 · N568WN · Boeing 73776N · Emergency Lighting
  > SUPPLEMENTAL INFORMATION, LT EMERGENCY LIGHTING ON OVERHEAD BIN BULLNOSE INOP AT ROW 7. R&R BATTERY PACK PER AMM.
- [SDR SWAA2022031467432](https://openairdocs.org/sdr/SWAA2022031467432.md): Retainer · cracked · Aug 11, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > RIGHT WING FIXED T/E I/B BULKHEAD ASSY. SEAL RETAINER IS CRACKED / R/H WING; FIXED T/E I/B BULKHEAD. REMOVED AND REPLACED SEAL RETAINER IAW B737 SRM 51-40-02-0G-0
- [SDR SWAA2019081936006](https://openairdocs.org/sdr/SWAA2019081936006.md): Wire · broken · Aug 7, 2019 · N568WN · Boeing 73776N · Light System Wiring
  > EMERGENCY EXIT LIGHT LOCATED ON THE G1 GALLEY BROKEN. / R&R CONTACT SPLICE IAW SWPM & AMM.
- [SDR SWAA2022031467392](https://openairdocs.org/sdr/SWAA2022031467392.md): Rail · incorrect · Jul 23, 2019 · N568WN · Boeing 73776N · Fuselage Main, Structure
  > DTIP - PREVIOUS OPERATOR INSTALLED REPAIR ON AFT CARGO RAIL AT BS 767; RBL 3.0 IS NON-CONFORMING & REQUIRES REMOVAL & INSTALLATION OF NEW REPAIR PER CUSTOMER REQUEST. / REMOVED OLD REPAIR OF AFT CARGO RAIL BS 767 RBL 3 IAW B737-700 SRM 51-40-02-0G-0. INSTALLED
- [SDR SWAA2019080735697](https://openairdocs.org/sdr/SWAA2019080735697.md): Support · cracked · Jul 18, 2019 · N568WN · Boeing 73776N · Vertical Stabilizer, Spar/Rib
  > VERTICAL STABILIZER RIB LATERAL SUPPORT CRACKED AT BS. 1018, BETWEEN LBL 10 TO RBL 10. / R&R SUPPORT IAW DWG & SRM.
- [SDR SWAA2019073135452](https://openairdocs.org/sdr/SWAA2019073135452.md): Flap · delaminated · Jul 16, 2019 · N568WN · Boeing 73776N · Trailing Edge Flaps
  > LT OUTBOARD AFT FLAP, AFT INBOARD CORNER DELAMINATED. REPAIRED AFT FLAP IAW SRM.
- [SDR SWAA2019081335757](https://openairdocs.org/sdr/SWAA2019081335757.md): Angle · cracked · Jul 15, 2019 · N568WN · Boeing 73776N · Fuselage Main, Bulkhead
  > REAR SPAR VERTICAL PRESSURE DECK CRACKED AT BS. 663, BETWEEN RBL 25 TO RBL 45. REPAIRED ANGLE IAW EA.
- [SDR SWAA2022031267347](https://openairdocs.org/sdr/SWAA2022031267347.md): Floor Panel · delaminated · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > RH MAIN CABIN FLOOR ACCESS PANEL #222AF TOP LAYER IS MISSING IN SEVERAL AREAS. / EVALUATED; PREPPED; CLEANED AND REPAIRED UPPER SURFACE DAMAGE TO SKIN PLY ON FLOORBAORD 222AF IAW B737 SRM 53-00-50-2R-1; PAR 3 9A;C;E-F; K1;L1;M1) REV 68/
- [SDR SWAA2022031267344](https://openairdocs.org/sdr/SWAA2022031267344.md): Floor Panel · delaminated · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > LH MAIN CABIN FLOOR ACCESS PANEL #221CF TOP LAYER IS COMING OFF. / REPAIRED CABIN FLOOR PANEL #221CF I.A.W B737-700 SRM'S 53-00-50-2R-0 REV. 68 & 53-00-50-2R-1
- [SDR SWAA2022031267340](https://openairdocs.org/sdr/SWAA2022031267340.md): Floor Panel · pulled · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > CABIN FLOORBOARD 231XF UPPER SURFACE HAS PULLED FIBE / REPLACED CABIN FLOORBOARD 231 X F BY FABRICATION I.A.W. B737-700 SRM 53-00-50-2R-0 TABLE 204 REV. 68 AND BAC 3085 REV. E AND BOEING DWG # 144A5810-126 REV A (MP1345) (A40400) (A71226)
- [SDR SWAA2022031267338](https://openairdocs.org/sdr/SWAA2022031267338.md): Floor Panel · delaminated · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > PASSENGER CABIN FLOOR BOARD 232SF HAS A PUNCTURE WITH DELAM ON UPPER SURFACE 1.5' FROM FORWARD EDGE AND 5' FROM INBOARD EDGE / REPAIRED PUNCTURE W/ DELAM ON UPPER SURFACE 1.5' FROM FWD EDGE & 5' FROM INBOARD EDGE ON PASSENGER CABIN FLOOR BOARD 232 SF IAW B 737
- [SDR SWAA2022031267331](https://openairdocs.org/sdr/SWAA2022031267331.md): Floor Panel · delaminated · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > AFT CABIN FLOORBOARD 242UF HAS MISSING FIBERS ON TOP SIDE. / REPAIRED AFT CABIN FLOOR BOARD 242UF ON TOP SIDE IAW B737-700 SRM 53-00-50-2R-1 AND 51-00-05 NDT P4; BOND CHECKED (A09236) (A36551) C
- [SDR SWAA2019080135483](https://openairdocs.org/sdr/SWAA2019080135483.md): Crease Beam · corroded · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Main, Structure
  > R2 CREASE BEAM INNER CHORD UPPER FLANGE CORRODED BETWEEN BS. 958 TO BS. 985, RBL 51, AROUND NUT PLATES. R&R CREASE BEAMS IAW DWG AND SRM.
- [SDR SWAA2019072435243](https://openairdocs.org/sdr/SWAA2019072435243.md): Crease Beam · corroded · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Main, Structure
  > L2 CREASE BEAM INNER CHORD UPPER FLANGE CORRODED AROUND NUT PLATES BETWEEN BS. 958 TO BS. 985, LBL 51.8. R&R INNER CHORD IAW SRM & DWG.
- [SDR SWAA2019072435242](https://openairdocs.org/sdr/SWAA2019072435242.md): Floorboard · damaged · Jul 14, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > PASSENGER CABIN FLOORBOARD 241AF HAD A FIBER DAMAGE ON UPPER SURFACE ALONG LENGTH OF PANEL. R&R FLOORBOARD 241AF IAW SRM & DWG.
- [SDR SWAA2022031267325](https://openairdocs.org/sdr/SWAA2022031267325.md): Shear Web · corroded · Jul 13, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > CABIN FLOOR WEB AT STA 1006+11' LBL 19 WL 208 CORRODED ON TOP SURFACE / ACCOMPLISHED BLEND REPAIR ON FLOOR SUPPORT STRUCTURE SHEAR WEB AT STA 1020 LBL 19 TO 27 I..A.W E.A 190593 IR AND SEA 1-753-35278 REV IR.
- [SDR SWAA2022031267327](https://openairdocs.org/sdr/SWAA2022031267327.md): Baffle · corroded · Jul 13, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FWD CARGO COMPARTMENT BAFFLE AT STA 500C TO 500D LBL 21 CORRODED. / REMOVED CORROSION IAW SRM 51-10-02-0G0 VISUAL INSPECTON WITH A 10X MAG G LOSS NO DEFECTS ORIGINA.032 REMAININ.025 LOSS.007 FOUND TO BE OUT LOF LIMITS IAW SRM 53-00-53-1A-2 FIG 103. REMVOED
- [SDR SWAA2019081335859](https://openairdocs.org/sdr/SWAA2019081335859.md): Floorbeam · corroded · Jul 13, 2019 · N568WN · Boeing 73776N · Fuselage Main, Floor Beam
  > CABIN FLOOR STRUCTURE "T" CAP UPPER AND LOWER SURFACE CORRODED AT NUTPLATE HOLES BS. 986, RBL 43. / REPAIRED FLOOR BEAM UPPER T-CAP IAW EA.
- [SDR SWAA2019081335756](https://openairdocs.org/sdr/SWAA2019081335756.md): Intercostal · corroded · Jul 13, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > AFT CARGO COMPARTMENT INTERCOSTAL CORRODED BETWEEN BS. 767 TO BS. 787, RBL 20. REPAIRED INTERCOSTAL IAW DWG & SRM.
- [SDR SWAA2019071834965](https://openairdocs.org/sdr/SWAA2019071834965.md): Angle · corroded · Jul 12, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FORWARD WET AREA, FLOOR STRUCTURE R1 DOOR Z ANGLE CORRODED AT BS. 291+5. R&R R1 DOOR LOWER SILL CREASE BEAM ANGLE IAW SRM AND DWG.
- [SDR SWAA2022031167291](https://openairdocs.org/sdr/SWAA2022031167291.md): Attach Bracket · cracked · Jul 11, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > LT WING; I/B FIXED T/E PANEL 551FB; MOUNT ANGLE IS BROKEN. (STREAMER) / REMOVED ATTACH BRACKET P/N 287A9152-23 @ L/H WING; I/B FIXED; T/E PANEL 551FB. LOCATED & DRILLED NEW BRACKET. INSTALLED NEW BRACKET. ALL ACTIONS ARE IAW B737 SRM'S 51-40-02-0G-0; 51-40-05
- [SDR SWAA2022031167234](https://openairdocs.org/sdr/SWAA2022031167234.md): Support · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > RIGHT WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT ATTACH CLIP; CRACKED THROUGH. / REMOVED & REPLACED CRACKED ATTACH CLIP R/H WING AFT SPAR; 7' OTBD OF FUSELAGE SIDE OF BODY; UPPER WING PANEL SUPPORT IAW BOEING DWG # 115A2000 REV.
- [SDR SWAA2022031167239](https://openairdocs.org/sdr/SWAA2022031167239.md): Scuff Plate · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Main, Plate/Skin
  > FWD CARGO FWD CORNER SCUFF PLATE IS CRACKED / REPAIRED FORWARD CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11
- [SDR SWAA2022031167240](https://openairdocs.org/sdr/SWAA2022031167240.md): Scuff Plate · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Main, Plate/Skin
  > FWD CARGO AFT CORNER SCUFF PLATE CRACKED / REPAIRED AFT CORNER SCUFF PLATE IAW E.A. 1-A53-2076 REV 11
- [SDR SWAA2022031167244](https://openairdocs.org/sdr/SWAA2022031167244.md): Finger Doubler · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Wing, Plate/Skin
  > (NO DOT-18) LEFT WING AFT SPAR; LOCATED JUST INBOARD OF #1 ENGINE LINES. FINGER PLATE LOOSE AND CRACKED. / REMOVED LEFT WING AFT SPAR FINGER PLATE IAW SRM 51-40-02-0G-0. VERIFIED NEW PT 115A2781-13 IAW BOEING DRAWING 115A2714 REV A FRAME 2 AND BOEING ENGINEERI
- [SDR SWAA2022031167266](https://openairdocs.org/sdr/SWAA2022031167266.md): Attach Bracket · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > AFT CARGO PIT ATTACH BRACKET STA 867-2' ON WASTE TANK VERTICAL SUPPORT LBL 10 AT FLOOR LEVEL CRACKED / INSTALLED NEW AFT CARGO PIT ATTACHE BRACKET STA 867-2' ON WASTE TANK VERTICAL SUPPORT LBL 10 AT FLOOR LEVEL IAW SRM B737NG SRM 51-40-02-0G-0; DWG 149A8102 RE
- [SDR SWAA2022031167253](https://openairdocs.org/sdr/SWAA2022031167253.md): Angle · corroded · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > AFT CARGO PIT R/H Z ANGLE BETWEEN STA 727E+6' TO 767 RBL 21 HAS CORROSION UPPER SURFACE / REMOVED CORROSION ON R/H Z ANGLE STA 727E TO 767 RBC 21. IAW SRM 51-10-02-0G-0. MEASURED 100% MATERIAL LOSS FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2. REMOVED AND REPLA
- [SDR SWAA2019081335858](https://openairdocs.org/sdr/SWAA2019081335858.md): Angle · corroded · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > AFT CARGO PIT LEFT ZEE ANGLE CORRODED UPPER SURFACE BETWEEN BS. 747 TO BS. 847, LBL 21. / REPAIRED Z ANGLE IAW SRM & DWG.
- [SDR SWAA2019072935317](https://openairdocs.org/sdr/SWAA2019072935317.md): Door Sill · corroded · Jul 10, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > AFT CARGO PIT LOWER SILL WEB CORRODED UPPER SURFACE BETWEEN BS. 787+18 TO BS. 847, RBL 27. R&R WEB IAW SRM & DWG.
- [SDR SWAA2019072535295](https://openairdocs.org/sdr/SWAA2019072535295.md): Support Angle · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > LT WING AFT SPAR FIXED PANEL BETWEEN #5 SPOILER AND GROUND SPOILER SUPPORT ANGLE CRACKED ON FORWARD SIDE. R&R SUPPORT ANGLE IAW DWG.
- [SDR SWAA2019072535277](https://openairdocs.org/sdr/SWAA2019072535277.md): Support Rib · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Wing, Rib/Bulkhead
  > LT WING AFT SPAR FIXED PANEL BETWEEN #5 SPOILER AND GROUND SPOILER SUPPORT RIB CRACKED IN RADIUS. R&R SUPPORT RIB IAW DWG & SRM.
- [SDR SWAA2019071634856](https://openairdocs.org/sdr/SWAA2019071634856.md): Support Fitting · cracked · Jul 10, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > RT WING UPPER FIXED TRAILING EDGE 10" INBOARD OF DEFLECTION CONTROL RIB, UPPER PANEL SUPPORT CLIP CRACKED. R&R SUPPORT CLIP IAW SRM & DWG.
- [SDR SWAA2022031167211](https://openairdocs.org/sdr/SWAA2022031167211.md): Panel · delaminated · Jul 9, 2019 · N568WN · Boeing 73776N · Wing, Plate/Skin
  > L/H WING LWR L/E PANEL 521WB INNER SURFACE FWD OUTBD CORNER MISSING PIECE OF COMPOSITE AND DELAMINATING / REPAIRED DAMAGE ON PANEL 521WB; APPLIED RESIN SWEEP TO REPAIR AREA AND CURED. RESTORED DECORATIVE FINISH. IAW B737-700 SRM 51-70-04-2R-13 REV 68; B737 AMM
- [SDR SWAA2022031167214](https://openairdocs.org/sdr/SWAA2022031167214.md): Vapor Barrier · cracked · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > LH MAIN WHEEL VAPOR BARRIER BULKHEAD EXISTING REPAIR DELAMED. / ACCOMPLISHED COMPOSITE BOND REPAIR ON LH STA 663 VAPOR BARRIER BULKHEAD I.A.W. SRM 51-70-04-2R-10 REV 68
- [SDR SWAA2022031167213](https://openairdocs.org/sdr/SWAA2022031167213.md): Shield · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FWD CARGO COMP.RH FLOOR SHIELD CORROSION AROUND FASTNER HOLES STA.490-500A / REMOVED CORROSION IAW SRM 51-10-02-0G-0 100% LOSS OF MATERIAL. REMOVED AND REPLACED FWD CARGO FLOOR SHIELD @ STA 490 TO 500A IAW SRM 51-40-02-0G-0 AND BOE8ING DWG 143A0080 SHT 11 REV:
- [SDR SWAA2022031067217](https://openairdocs.org/sdr/SWAA2022031067217.md): Floor Panel · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > AFT CARGO PIT COVER PLATE FOR FLOOR PANEL 140CF CORRODED LOWER SURFACE / VERIFY LIMITS FOR AFT CARGO PIT COVER PLATE FOR FLOOR PANEL 140CF NO LIMITS GIVEN IN THE SRM REPAIR BY REPLACEMENT IAW SRM 51-10-02-0G-0. P;C. VERIFIED NEW PART IAW IPC 25-52-10-02 PART #
- [SDR SWAA2022031067218](https://openairdocs.org/sdr/SWAA2022031067218.md): Floor Panel · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > AFT CARGO PIT FLOOR PANEL 140BF HAS CORROSION ON EDGES ON UPPER SURFACE / VERIFIED NEW FLOOR PNL 140 BF IAW IPC 25-52-10-02 PART# 453A2610-32 ATAG WN9914. FLOOR PNL WILL BE INSTALLED ON SOUTHWEST CARD 39747/1600/0012; JPANEL-141-CLOSE. REMOVED AND REPLACED PNL
- [SDR SWAA2022031067223](https://openairdocs.org/sdr/SWAA2022031067223.md): Floor Panel · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > FWD CARGO PIT FLOOR PANEL 120AF HAS CORROSION UPPER SURFACE AT NET TIE DOWN PLATE & FWD EDGE / REMOVED CORROSION ON FWD CARGO FLOORPANEL 120AF UPPER SURFACE @ NET TIEDOWN IAW SRM 51-10-02-0G. VISUAL INSPECTION WITH A 10X MAG GLASS; NO DEFECTS- ORIGINAL.071' R
- [SDR SWAA2022031067224](https://openairdocs.org/sdr/SWAA2022031067224.md): Floor Panel · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Floor Panel
  > FWD CARGO PIT FLOOR PANEL 120CF HAS CORROSION UPPER SURFACE AFT EDGE / REMOVED CORROSION FROM FWD CARGO FLOOR PANEL 120CF ON AFT EDGE BELOW SRM 51-10-02-0G-0 PAR 15. ORIG 'T'.071';.067'.004' LOSS 48' LONG FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-1 FIG 103 TO
- [SDR SWAA2019080535626](https://openairdocs.org/sdr/SWAA2019080535626.md): Angle · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT LEFT Z-ANGLE CORRODED AROUND FASTENER HOLES BETWEEN BS 500A TO 500D. R & R THE LT Z-ANGLE IAW SRM AND DWG.
- [SDR SWAA2019072535294](https://openairdocs.org/sdr/SWAA2019072535294.md): Gusset · cracked · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT GUSSET CRACKED AT BS. 500D, STR. 19L. R&R GUSSET IAW DWG & SRM.
- [SDR SWAA2019071634855](https://openairdocs.org/sdr/SWAA2019071634855.md): Shield · corroded · Jul 9, 2019 · N568WN · Boeing 73776N · Fuselage Miscellaneous Structure
  > FORWARD CARGO COMPARTMENT R/H FLOOR SHIELD CORRODED AROUND FASTENER HOLES BETWEEN BS. 420 TO BS. 440. R&R SHIELD IAW SRM & DWG.
- [SDR SWAA2022031167204](https://openairdocs.org/sdr/SWAA2022031167204.md): Panel · delaminated · Jul 8, 2019 · N568WN · Boeing 73776N · Wing, Plate/Skin
  > R/H WING LWR L/E PANEL 621VB FWD INDB CORNER DELAMINATED AT EROSION STRIP / EVALUATED PREPPED CLEANED AND REPAIRED DELAM DAMAGE AT FWD IND CORNER ON PANEL 621 VB IAW B 737 SRM 51-70-04 PAR 4 (A-E) REV 68
- [SDR SWAA2022031167205](https://openairdocs.org/sdr/SWAA2022031167205.md): Retainer · corroded · Jul 8, 2019 · N568WN · Boeing 73776N · Wing Miscellaneous Structure
  > R/H WING REFUEL PANEL 621GB SEAL RETAINER HAS MINOR CORROSION / RETAINER FOUND WITH 100% MATERIAL LOSS. FABRICATED NEW P/N 116A8504-8 RETAINER FROM 7075-T6 X. 040' MATERIAL IAW DRAWING 116A8504 REV B. INSTALLED NEW RETAINER IAW 737 AMM 20-50-11-910-801 TABLE 2
- [SDR SWAA2019071935130](https://openairdocs.org/sdr/SWAA2019071935130.md): Stiffener · cracked · Jul 8, 2019 · N568WN · Boeing 73776N · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STABILIZER INSPAR RIB, STAB. STA. 120.30, VERTICAL STIFFENERS #3 CRACKED APPROXIMATELY 1" ABOVE RIB LOWER FLANGE. REPAIRED STIFFENER IAW SRM.
- [SDR SWAA2019071935129](https://openairdocs.org/sdr/SWAA2019071935129.md): Stiffener · cracked · Jul 8, 2019 · N568WN · Boeing 73776N · Horizontal Stabilizer Miscellaneous Structure
  > RT HORIZONTAL STABILIZER INSPAR RIB, STAB. STA. 120.30, VERTICAL STIFFENER #2 CRACKED. REPAIRED STIFFENER IAW SRM.
- [SDR SWAA2019071935128](https://openairdocs.org/sdr/SWAA2019071935128.md): Bonding Jumper · frayed · Jul 8, 2019 · N568WN · Boeing 73776N · Emergency Exits
  > RT EMERGENCY EXIT HATCH BONDING JUMPER FRAYED. R&R BONDING JUMPER IAW AMM.
- [SDR SWAA2022031167181](https://openairdocs.org/sdr/SWAA2022031167181.md): Skin · cracked · Jul 6, 2019 · N568WN · Boeing 73776N · Leading Edge Devices
  > LEFT WING #1 SLAT L/E NOSE SKIN @ ACTUATOR FTG ATTACH FASTENER HOLE; CRACK; MRK'D. / REPAIRD L/H WING #1 SEAT LEADING EDGE SKIN IAW B 737-700 SRM S7-42-01-2R-8

Next page: https://openairdocs.org/deregistered/N568WN-2024-10-30/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 = 'N568WN' AND deregistration_id = 'N568WN-2024-10-30'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N568WN-2024-10-30/reports

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