# Service difficulty reports: N8059A

A list on [N8059A](https://openairdocs.org/aircraft/N8059A.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR SCNA20260917403](https://openairdocs.org/sdr/SCNA20260917403.md): Speed Brake · faulted · Sep 16, 2026 · N8059A · Boeing 73786J · Drag Control System
  > SPEED BRAKE DID NOT DEPLOY ON LANDING. PERFORMED FIM 27-62 804 SPEED BRAKES AUTO DEPLOY IS OPERATIVE. FAULT WAS INTERMEDIATE. ACFT OK FOR SERVICE.
- [SDR SCNA20260623257](https://openairdocs.org/sdr/SCNA20260623257.md): Shade · sparks · Jun 22, 2026 · N8059A · Boeing 73786J · Emergency Equipment
  > DURING FLIGHT FO REMOVED WINDOW SHADE FROM R1 AND IT CREATED SPARKS AND A LITTLE BIT OF SMOKE. RAN QRH, LEFT THE HEAT OFF FOR THAT WINDOW. CB DID NOT POP. INSPECTED FO WINDOW IAW AMM 56-11-00. NO DEFECTS NOTED AND PERFORMED WINDOW HEAT SYSTEM OPS TEST IAW AMM
- [SDR SCNA20260612246](https://openairdocs.org/sdr/SCNA20260612246.md): Window · sparks · Jun 11, 2026 · N8059A · Boeing 73786J · Windshield/Door Rain/Ice Removal
  > DURING FLIGHT FO REMOVED WINDOWSHADE FROM R1. THE R1 WINDOW THREW SPARKS AND TRIPPED CB. FOLLOWED QRH, DID NOT RESET CB. MX NOTIFIED. INSPECTED R1 WINDOW PER AMM 56-11-00-200-803, NO DEFECTS NOTED. RESET CB ON P6-12 B25 ACCCOMPLISHED WINDOW HEAT CONTROL UNI
- [SDR SCNA20260120038](https://openairdocs.org/sdr/SCNA20260120038.md): Strut · leaking · Jan 7, 2026 · N8059A · Boeing 73786J · Main Landing Gear Strut/Axle/Truck
  > DUE TO HISTORY OF LEFT MAIN LANDING GEAR STRUT LEAK- PERFORM REPLACEMENT OF THE ACTIVE AND SPARE SEALS IAW AMM 32-11-21-960-802. REMOVED AND REPLACED LT MAIN MANDING GEAR IAW CC 320400100.
- [SDR SCNA20251117438](https://openairdocs.org/sdr/SCNA20251117438.md): Girt Bar · unpacked · Nov 14, 2025 · N8059A · Boeing 73786J · Emergency Equipment
  > L1 DOOR ESCAPE SLIDE GIRT BAR PROTRUDING ON AFT SIDE. PERFOREMED ESCAPE SLIDE PACK CHECK IAW AMM 25-66-01-200-802. NO DEFECTS NOTED.
- [SDR SCNA20250407103](https://openairdocs.org/sdr/SCNA20250407103.md): Light · intermittent · Apr 4, 2025 · N8059A · Boeing 73786J · Emergency Lighting
  > WORK ORDER 866652, NR0514: EMERGENCY LIGHTS AT R1 DOOR ARE INTERMITTENT. - RESOLUTION (INPROGRESS)
- [SDR SCNA20250404095](https://openairdocs.org/sdr/SCNA20250404095.md): Battery Pack · inoperative · Apr 3, 2025 · N8059A · Boeing 73786J · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHTS ARE INOP. REMOVED AND REPLACED ABTTERY PACK M1675 PER B737 AM 33-51-06-960-801, OPS CHECK GOOD.
- [SDR SCNA20250415119](https://openairdocs.org/sdr/SCNA20250415119.md): Bushing · cracked · Feb 25, 2025 · N8059A · Boeing 73786J · Fuselage, Stabilizer Attach Fittings
  > RIGHT HOR. STAB AFT BOTTOM ATTACHMENT BUSHING CRACKED. UNABLE TO CONFIRM WHETHER IF BUSHING IS A SHRINKFIT OR FORCEMENT & P/N IS UNAVAILABLE PER EAR #12 RESPONSE STEP 1. PERFORMED A DVI IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE (POSSIBLE) CRACK NOTED AT
- [SDR SCNA20250505161](https://openairdocs.org/sdr/SCNA20250505161.md): Bushing · migrated · Feb 24, 2025 · N8059A · Boeing 73783N · Fuselage, Stabilizer Attach Fittings
  > LEFT AFT HORIZONTAL STAB UPPER AFT BUSHING MIGRATING. SAA034 027 - RESOLUTION: SUBMIT TO ENG. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRC
- [SDR SCNA20250415120](https://openairdocs.org/sdr/SCNA20250415120.md): Bushing · cracked · Feb 24, 2025 · N8059A · Boeing 73786J · Fuselage, Stabilizer Attach Fittings
  > ON CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23 10MAR2025, GOUGE & CRAVK NOTED AT DEFE
- [SDR SCNA20250415116](https://openairdocs.org/sdr/SCNA20250415116.md): Bushing · cracked · Feb 24, 2025 · N8059A · Boeing 73786J · Horizontal Stabilizer Structure
  > CENTER BOX LEFT AFT LOWER HOR. STAB HAS BUSHING CRACKED. UNABLE TO CONFIRM WHETHE IF BUSHING IS SHRINKFIT OR FORCEMENT & P/N IS UNAVALIABKE, PER EAR #5 RESPONSE STEP 1. PERFORMED A DVI, IAW SRM 51-10-04-0G-0 REV 23, GOUGE & CRAVK NOTED AT DEFECT AREA. PER
- [SDR SCNA20250415113](https://openairdocs.org/sdr/SCNA20250415113.md): Bushing · migrated · Feb 24, 2025 · N8059A · Boeing 73786J · Horizontal Stabilizer Structure
  > LEFT AFT HOR. STAB. MIDDLE BUSHING OUTER COATING DETERIORATED. UNABLE TO CONFIRM IF BUSHING IS SHRRINK FIT OR FORCEMATE P/N CANNOT BEE CONFIRMED PER ENG RESPOSE STEP 1. BUSHING MIGRATED SEALANT WAS BROKEN AROUND ENTIRE CIRCUMFRANCE. NO OTHRER DAMAGE FOUND D
- [SDR SCNA20250415117](https://openairdocs.org/sdr/SCNA20250415117.md): Bushing · gouged · Jan 23, 2025 · N8059A · Boeing 73786J · Horizontal Stabilizer Structure
  > AIRCRAFT TAIL SECTION, RIGHT HAND HORIZONTAL STABILIZER, THE FORWARD LOWER MOUNT FORWARD BUSHING HAS A GOUGEON THE AFT SIDE AT THE THREE O CLOCK POSITION. (120-110) RESOLUTION: SUBMIT TO ENG. REMOVED THE RH FRONT FWD LWR BUSHING, IAW EAR#08 RESPONSE STEP 1,
- [SDR SCNA20250114013](https://openairdocs.org/sdr/SCNA20250114013.md): Slide · dislodged · Jan 13, 2025 · N8059A · Boeing 73786J · Escape Slide
  > DEFECT 794687: ESCAPE SLIDE FELL OUT OF L1 DOOR WHILE CLOSING DOOR. RESOLUTION: REINSTALLED L1 SLIDE IAW AMM 25-66-01 ESCAPE SLIDE.
- [SDR SCNA20241014328](https://openairdocs.org/sdr/SCNA20241014328.md): Switch · not seated · Oct 13, 2024 · N8059A · Boeing 73786J · Flight Compartment Windows
  > DEFECT 723485: 3R WINDOW SPARKS AND ARCHING OBSERVED ON THERMAL SWITCH. - - RESOLUTION: FOUND EVIDENCE OF R3 THERMAL SWITCH IMPROPERLY SEATED INTO CLIP AND CAUSED ARCHING RESEATED THERMAL SWITCH REF AMM 30-41-31 AND OPS CHECK GOOD THIS CLEARS MEL 30-11-4 MDDR
- [SDR SCNA20240826307](https://openairdocs.org/sdr/SCNA20240826307.md): Hook · inoperative · Aug 26, 2024 · N8059A · Boeing 73786J · Emergency Equipment
  > DEFECT 777757: DOOR L1 GIRT BAR RETENTION HOOK WONT HOLD. - - RESOLUTION: ALIGNED STOP ASSEMBLY IAW AMM 25-66-01. OPS CHECK GOOD.
- [SDR SCNA20240208030](https://openairdocs.org/sdr/SCNA20240208030.md): Flap System · locked · Feb 8, 2024 · N8059A · Boeing 7378 · Trailing Edge Flap Control System
  > ON DECENT FLAPS LOCKED OUT NEAR ZERO WITH SLIGHT ASYMETRY OF 1/8" ON FLAP INDICATOR. USED ALERNATE FLAP EXTENTION AND LE FLAPS EXTENDED. (EMERGENCY DECLARED) - RESOLUTION: FOUND FAULT CODE 27-53254. REPLACED #5 & #6 SKEW SENSO ON RIGHTHAND WING. CHECK WIRE
- [SDR SCNA20231024238](https://openairdocs.org/sdr/SCNA20231024238.md): Unknown · unknown · Oct 9, 2023 · N8059A · Boeing 7378 · Passenger/Crew Doors
  > DEFECT 767080 - - - AIRCRAFT DID NOT PRESSUREIZE AFTER TAKEOFF. - - - RESOLUTION - FOUND L1 DOOR NOT COMPLETLY SEALED WHEN CLOSED PERFORMED L1 DOOR SYSTEM TEST IAW 52-11-00-700-804 OPS CHECK GOOD.
- [SDR SCNA20230208077](https://openairdocs.org/sdr/SCNA20230208077.md): Shield · corroded · Feb 7, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203750000 NR0004: FWD CARGO BAY, RH AFT AFT SHIELD HAS SEVERAL COORODED FASTENER HOLES RESOLUTION: REMOVED, FABRICATED AND INSTALLED NEW FWD CARGO RH SHIELD AFT CARGO DOOR IAW SRM 51-40-02-0G-0 LOT# 5127013-1 ITEM HFAB53-RP-011.
- [SDR SCNA20230208076](https://openairdocs.org/sdr/SCNA20230208076.md): Web · corroded · Feb 7, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC203750000 NR00120: CORROSION AFT CARGO DOOR SURROUND SUB THRESHOLD WEB. RESOLUTION: REMOVED AND REPLACED AFT CARGO DOOR SURROUND SUB THRESHOLD WEB IAW 51-40-02-0G-0 AND BOEING DWG 146A5120
- [SDR SCNA20230208075](https://openairdocs.org/sdr/SCNA20230208075.md): Not Reported · corroded · Feb 7, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203750000 NR 00117: CORROSION AFT CARGO LH ZEE CHANNEL STA 727 TO STA 867 STR 25L RESOLUTION: CORROSION ON ZEE CHANNEL FROM STA 727 TO STA 867, STR 25L AT AFT CARGO FOUND IT TO BE OUT OF LIMITS, REMOVED AND REPLACED AND APPLIED FINAL REFINISHED PE
- [SDR SCNA20230208074](https://openairdocs.org/sdr/SCNA20230208074.md): Not Reported · corroded · Feb 7, 2023 · N8059A · Boeing 7378 · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00005: FWD CARGO BAY, RH Z CHANNEL HAS SEVERAL CORRODED FASTENER HOLES FROM STA 500A-500I. RESOLUITION: REPAIRED FWD CARGO BAY RH ZEE CHANNEL FROM STA 500A-500I IAW B737 SRM 51-40-02-0G, SRM 53-00-53-2R-5 REPAIR 5 AND DWG 143A7500.
- [SDR SCNA20230206059](https://openairdocs.org/sdr/SCNA20230206059.md): Intercostal · corroded · Jan 28, 2023 · N8059A · Boeing 73783N · Fuselage Miscellaneous Structure
  > DEFECT NR00204: UPON REMOVAL OF AFT CARGO DOOR SURROUND FORWARD SHIELD, FOUND CORROSION ON INTERSCOSTAL STA 787-794 STR 25R RESOLUTION: REMOVED AND REPLACED DAMAGED INTERCOSTAL STA 787-794 STR 25 IAW B737 SRM 51-40-02-0G-0 AND BOEING DWG 146A8320 REV A.
- [SDR SCNA202302062073](https://openairdocs.org/sdr/SCNA202302062073.md): Not Reported · corroded · Jan 26, 2023 · N8059A · Boeing 73783N · Fuselage Miscellaneous Structure
  > DEFECT TC 203750000 NR00170: CORROSION AFT CARGO RH AFT ZEE CHANNEL STA 887 TO STA 947 STR 25R. RESOLUTION: R/R NEW ZEE CHANNEL AT BSTA 887 TO BSTA 947 STR 25R PER B737-800 51-40-02, DWG 147A7500 REV A.
- [SDR SCNA20230206061](https://openairdocs.org/sdr/SCNA20230206061.md): Not Reported · corroded · Jan 26, 2023 · N8059A · Boeing 73783N · Fuselage Miscellaneous Structure
  > DEFECT TC 203750000 NR00169: CORROSION AFT CARGO RH AFT ZEE CHANNEL STA 867 TO STA 887 STR 25R. RESOLUTION: R/R NEW ZEE CHANNEL FROM STA 867 TO STA 887 STR 25R PER B737 SRM 51-40-02 AND DWG # 146A7500 REV A.
- [SDR SCNA20230206056](https://openairdocs.org/sdr/SCNA20230206056.md): Not Reported · corroded · Jan 26, 2023 · N8059A · Boeing 73783N · Fuselage Miscellaneous Structure
  > DEFECT TC 203750000 NR00166: CORROSION AFT CARGO RH ZEE CHANNEL STA 727 TO STA 767 STR 25R. RESOLUTION: REMOVED DAMAGED AFT CARGO RH ZEE FROM STA 737 TO 767 STR 25R PER BOEING 737 51-40-02-0G-0 REV 16 AND INSTALLED A NEW ZEE CHANNEL LOT # 5093502-1 PER BOEIN
- [SDR SCNA202302100001](https://openairdocs.org/sdr/SCNA202302100001.md): Not Reported · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Main, Structure
  > DEFECT TC 206200000 NR00128: EVIDENCE OF CORROSION ON RH WING REAR SPAR AROUND AFT BOOST PUMP #2 RESOLUTION: CORROSION FOUND IN 2 EA AREAS AT AFT BOOST PUMP #2, RH WING REAR SPAR UPPER AREA MEASURES 3.25"L X 2.5" W X 0.046"D, LOWER AREA MEASURES 4.5"L X 3.5"
- [SDR SCNA20230206069](https://openairdocs.org/sdr/SCNA20230206069.md): Baffle · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00144: CORROSION ON FWD CARGO BAFFLE BS 500E TO 500F LBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500E - 500F LBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
- [SDR SCNA20230206064](https://openairdocs.org/sdr/SCNA20230206064.md): Not Reported · cracked · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00157: FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500E LBL25 WL 156 FWD SIDE OF FRAME CRAKCED. RESOLUTION: R/R BAFFLE CLIP AT BS 500E LBL25 WL 156 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206058](https://openairdocs.org/sdr/SCNA20230206058.md): Not Reported · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Main, Structure
  > DEFECT TC 203350000 NR00148: CORROSION ON FWD CARGO BAFFLE CLIP BS 500C FWD SIDE FRAME LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE CLIP BS 500D FWD SIDE OF FRAME LBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206057](https://openairdocs.org/sdr/SCNA20230206057.md): Intercostal · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00142: CORROSION IOON FWD CARGO BAFFLE BS 500C TO 500D LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500C TO 500D LBL 25 WL 156 ON FWD CARGO IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206055](https://openairdocs.org/sdr/SCNA20230206055.md): Intercostal · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00146: CORROSION ON FWD CARGO BAFFLE BS 500G TO 500H LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500G - 500H LBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
- [SDR SCNA20230206054](https://openairdocs.org/sdr/SCNA20230206054.md): Intercostal · corroded · Jan 24, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR 00147: CORROSION ON FWD CARGO BAFFLE BS 500H TO 500I LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500H TO 500I LBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206053](https://openairdocs.org/sdr/SCNA20230206053.md): Intercostal · corroded · Jan 24, 2023 · N8059A · Boeing 73786J · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00143: CORROSION ON FWD CARGO BAFFLE BS 500D TO 500E LBL 25 WL 156. RESOLUTION: REMOVED AND REPLACED BAFFLE BS 500D TO 500E LBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230210078](https://openairdocs.org/sdr/SCNA20230210078.md): Unknown · unknown · Jan 23, 2023 · N8059A · Boeing 73783N · Wing Main, Frame Structure
  > DEFECT TC206200000 NR00128: EVIDENCE OF CORROSION ON RH WING REAR SPAR AROUND AFT BOOST PUMP #2. RESOLUTION: CORROSION FOUND IN 2 EA AREAS AT AFT BOOST PUMP #2, RH WING REAR SPAR UPPER AREA MEASURES 3.25"L X 2.5"W X.046"D, LOWER AREA MEASURES 4.5"L X 3.5"W
- [SDR SCNA20230206072](https://openairdocs.org/sdr/SCNA20230206072.md): Not Reported · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00108: FWD CARGO BAY, LH SIDEPLATE "Z" CHANNEL HAS SEVERAL CORRODED FASTENER HOLES FROM STA 500D - 500I (MARKED). RESOLUTION: CORROSION ON FWD CARGO BAY, LH SIDEPLATE "Z" CHANNEL FOUND OUT OF LIMITS PER SRM 53-00-53-1A-2, #4.A.2.D REMOV
- [SDR SCNA20230206070](https://openairdocs.org/sdr/SCNA20230206070.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00134: CORROSION ON FWD CARGO BAFFLE BS 500G - 500H RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500G - 500H RBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
- [SDR SCNA20230206068](https://openairdocs.org/sdr/SCNA20230206068.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00132: CORROSION ON FWD CARGO BAFFLE BS 500E - 500F RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500E - 500F RBL 25 WL 156 IAW B737 SRM 51-40-02-0G.
- [SDR SCNA20230206067](https://openairdocs.org/sdr/SCNA20230206067.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00136: FWD CARGO BAFFLE BS 500B - 500C RBL 25 WL 156 CRACKED UPPER FLANGE. RESOLUTION: R/R BAFFLE BS 500B - 500C RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206066](https://openairdocs.org/sdr/SCNA20230206066.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT CORROSION ON FWD CARGO BAFFLE BS500D - 500E RBL 25 WL 156. RESOLUTION: R/R FWD CARGO BAFFLE BS500D - 500E RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505.
- [SDR SCNA20230206065](https://openairdocs.org/sdr/SCNA20230206065.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR 00135: CORROSION ON FWD CARGO BAFFLE BS 500H-500I RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500H-500I RBL 25 WL 156 IAW SRM 51-40-02-0G-0 AND DWG 143A7505
- [SDR SCNA20230206063](https://openairdocs.org/sdr/SCNA20230206063.md): Baffle · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00130: CORROSION ON FWD CARGO BAFFLE BS 500C - 500D RBL 25 WL 156. RESOLUTION: R/R BAFFLE BS 500C - 500D RBL 25 WL 156 IAW SRM 51-40-02-0G-0 DWG 143A7505.
- [SDR SCNA20230206062](https://openairdocs.org/sdr/SCNA20230206062.md): Intercostal · corroded · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR 00129: CORROSION ON FWD CARGO BAFFLE BS 500A - 500B RBL 25 WL 156. RESOLUTION. R/R BAFFLE BS 500A - 500B RBL 25 WL 156 IAW B737 SRM 51-40-02-0G-0 DWG 143A7505.
- [SDR SCNA20230206060](https://openairdocs.org/sdr/SCNA20230206060.md): Not Reported · cracked · Jan 23, 2023 · N8059A · Boeing 73783N · Fuselage Structure (General)
  > DEFECT TC 203350000 NR00138: FWD CARGO COMPARTMENT BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME CRAKCED. RESOLUTION: R/R BAFFLE CLIP AT BS 500H LBL 25 WL 156 FWD SIDE OF FRAME IAW SRM 51-40-02-0G-0 AND DWG 143A7505
- [SDR 2021FA0000430](https://openairdocs.org/sdr/2021FA0000430.md): None · none · Dec 29, 2021 · N8059A · Boeing 7378 · Passenger/Crew Doors
  > AIRCRAFT WOULD NOT PRESSURIZE DUE TO L1 DOOR PRESSURE LEAK. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM PER AMM 52-11-00. OPS CHECK AND PRESSURE CHECK NORMAL. AIRCRAFT OK FOR SERVICE
- [SDR SCNA20210907076](https://openairdocs.org/sdr/SCNA20210907076.md): Target · out of position · Sep 4, 2021 · N8059A · Boeing 73786J · Leading Edge Slat Position Indicating System
  > DEFECT: LE FLAPS TRANSIT ILLUMINATED AFTER FULLY CONFIGURED-SHORT FINAL VIS 24 ABE, WENT MISS, RAN "LE FLAPS TRANSIT" LIGHT CHECKLIST WHICH CALLED FOR FLAPS 15 LDG. LIGHT EXTINGUISHED UPON RETRACTION DURING MISS APPR AND ILLUMINATED AGAIN AT FLAPS 15. RESOLUT

## 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 = 'N8059A' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N8059A/reports

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