# Service difficulty reports: N379CX, cancelled Oct 9, 2025

A list on [N379CX, cancelled Oct 9, 2025](https://openairdocs.org/deregistered/N379CX-2025-10-09.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 6 · 277 reports

- [SDR NACA2025071600001](https://openairdocs.org/sdr/NACA2025071600001.md): Apu · faulted · Jul 25, 2025 · N379CX · Boeing 767323 · APU Start/Ignition System
  > APU WILL NOT START, AUTO ABORTS AT 45%
- [SDR NACA2025071300001](https://openairdocs.org/sdr/NACA2025071300001.md): Acm · seized · Jul 13, 2025 · N379CX · Boeing 767323 · Cabin Cooling System
  > RH AIR CYCLE MACHINE SEIZED. REMOVED AND REPLACED RH AIR CYCLE MACHINE B767-300 AMM 21-51-03 OPS CHECK GOOD.
- [SDR NACA20250717008](https://openairdocs.org/sdr/NACA20250717008.md): A/C Pack · inoperative · Jul 13, 2025 · N379CX · Boeing 767323 · Cabin Cooling System
  > DURING OPE RATIONAL PRESSURE TEST, INOP RH AIR CONDITION PACK, WITH MESSAGE ON EICAS RH PACK BITE.
- [SDR NACA20250717003](https://openairdocs.org/sdr/NACA20250717003.md): Floorbeam · damaged · May 20, 2025 · N379CX · Boeing 767323 · Fuselage Main, Floor Beam
  > AFTER REMOVAL OF BALLMAT FOUND AFT CARGO DOOR FLOOR FRAME UPPERFLANGE EXFOLIATED/ BLOWN OUT STA 1380 RBL 14. ACCOMPLISHED EA NO. 767-5360-73-B0524 REV IR ON AFT CARGO FLOOR FRAME UPPER FLANGE STA 1395 RBL 5 AND RBL 25.
- [SDR NACA20250717002](https://openairdocs.org/sdr/NACA20250717002.md): Skin · damaged · May 1, 2025 · N379CX · Boeing 767323 · Trailing Edge Flaps
  > LH INBD AFT FLAP HAS 2 DENTS ON LOWERSURFACE JUST BEHIND AND OTBD OF #5 TIRE. EVALUATED L/H I/B AFT FLAP AT LOWER SURFACE AT 2EA DENTS, FOUND DENTSTO BE NEAR EACH OTHER APPROX..50", MINIMUM IS 3" TO OTHER DENT, AREASIS NOT WITHING ALLOWABLE LIMITS, DENTS ARE
- [SDR NACA2025071701](https://openairdocs.org/sdr/NACA2025071701.md): Skin · corroded · Apr 29, 2025 · N379CX · Boeing 767323 · Fuselage Main, Plate/Skin
  > LH FUSELAG E SKIN HAS NUMEROUS AREAS OF CORROSION AT LAP SEAM STA 883 TO STA 965, ACCOMPLISHED EA 767-53-50-73 - B0479 REV.IR AT L/H FUSELAGE SKIN LAP SEAM STA 883 TO STA 965 S-17L
- [SDR NACA2025042200003](https://openairdocs.org/sdr/NACA2025042200003.md): Seat Track · cracked · Apr 22, 2025 · N379CX · Boeing 767323 · Fuselage, Seat/Cargo Attach Fittings
  > MOST OUTBOARD L/H SEAT TRACK STA 1060 TO STA 1070 FOUND TO BE CRACKED AT 2EA AREAS OF VERTICAL FLANGE RADIUS. ACCOMPLISHED NAC 767 E.O. 767-53-0076 REV. IR PERMANENT REPAIR OF SEAT TRACK LOCATED BETWEEN L/H STA 925 TO STA 1100, LBL 88.5.
- [SDR NACA20250717007](https://openairdocs.org/sdr/NACA20250717007.md): Connector · chafed · Mar 29, 2025 · N379CX · Boeing 767323 · Air Conditioning System Wiring
  > AFTER REMOVAL OF PANEL 193FL FOUND LT LOWER TRIM AIR SUPPLY VALVE POSITIONED INCORRECTLY CONNECTOR PLUG HARD CHAFING ON ACCESS PANEL SUPORT FRAME. REMOVED LT LOWER TRIM AIR SUPPLY VALVE IAW AMM 21-61-11-004-023. AFTER REPAIRED THE DAMAGE ON SUPORT FRAME AT N
- [SDR NACA2025032800003](https://openairdocs.org/sdr/NACA2025032800003.md): Plate · corroded · Mar 28, 2025 · N379CX · Boeing 767323 · Fuselage, Landing Gear Attach Fittings
  > L/H MLG ST A 955 BEARING PLATE P/N 111T1008-1 HAS CORROSION. ACCOMPLISHED EA 767-5300-73-B0473 REV IR ON LH STA 955 BEARING PLATE PN 111T1008-3. SDR SUBMITTED 00351 SAA118 07/01/25
- [SDR NACA202507170015](https://openairdocs.org/sdr/NACA202507170015.md): Fitting · corroded · Mar 20, 2025 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > FITTING AT L/H STA 955, LBL 98 (APPROX) HAS CORROSION ON MATING SURFACE. REMOVED CORROSION AND ACCOMPLISHED REPAIR ON UPPER KICK FITTING AT LH STA 955 LBL 98 IAW B767-3 SRM 57-10-10 REPAIR 3.
- [SDR NACA202507170014](https://openairdocs.org/sdr/NACA202507170014.md): Deck Plate · corroded · Mar 12, 2025 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > UPON REMOVAL OF DOUBLER ON SB 767-53-0016 FIG 47 STEP 6 STA 955 TO 977 FROM THE DECK PANEL FOUND CORROSION ON THE DOUBLER SKIN. REPLACED DOUBLER P/N:145T8754-33 B/N:0004379159 AT PRESSURE DECK, BETWEEN STA 955 TO STA 977 IAW SB767-53-0016 AND SRM 51-40-02-0G
- [SDR NACA20250717010](https://openairdocs.org/sdr/NACA20250717010.md): Deck Plate · corroded · Mar 10, 2025 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > UPON REMOVAL OF DECK PANEL AT L/H STA 955 - 977, LBL50 TO LBL 98 FOUND AREA OF CORROSION. ACCOMPLISHED EA #767-5700-73-B00461 IR AT L/H STA. 955 TO STA. 977 LBL 50 TO LBL 98 DECK PANEL
- [SDR NACA20250717009](https://openairdocs.org/sdr/NACA20250717009.md): Failsafe · corroded · Mar 10, 2025 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > UPON REMOV AL OF FAIL-SAFE STRAP FROM L/H STA 955 STGR12 TO LWR O/B SIDE FITTING LEG FOUND CORROSION ON MATING SURFACE OF STRAP. CLEAN, REMOVE CORR, MAP, SUBMIT TO ENGINEERING. ACCOMPLISHED EA #767-5300-73-B0453, REV I/R OF 400 L/H SIDE FAIL SAFE STRAP.
- [SDR NACA202507170013](https://openairdocs.org/sdr/NACA202507170013.md): Stiffener · damaged · Mar 7, 2025 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > STIFFENER AT L/H STA 933 TO STA 955 STGR 22 HAS 2EA DAMAGED HOLES. ACCOMPLISHED MAJOR CATEGORY A REPAIR ON 1EA. STIFFENER AT STA. 933 TO STA. 955 AND STGR 22L IAW E.A. #767-5300-73-B0447 REV. I/R
- [SDR NACA202507170012](https://openairdocs.org/sdr/NACA202507170012.md): Tee Fitting · damaged · Mar 7, 2025 · N379CX · Boeing 767323 · Fuselage Main, Attach Fittings
  > UPON HFEC OPEN HOLE INSP. OF "T" FITTING PER SB 767-53-0116 LOCATED BTWN L/H STA 960 TO STA 975, STGR 22 FOUND 1EA HOLE WITH A CRACK INDICATION. ACCOMPLISHED EA#767-5300-73-B0458 I/R ON THE AFT SIDE OF THE FWD WEB P/N 111T1003 AT STA 955 JUST OUT BOARD OF LBB
- [SDR NACA2025071700001](https://openairdocs.org/sdr/NACA2025071700001.md): Longeron Splice · damaged · Mar 6, 2025 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > LH FUSELAGE, LONGERON SPLICE PLATE, REMOVED FROM STA 933 TO 977 AND BELOW STR 22L HAS SEVERAL NICKS AND GOUGES IDENTIFIED WITH ORANGE STICKER 118-001. 1)ACCOMPLISHED EA 767-5700-73-B0451, IR (REV) AT L/H FUSELAGE LONGERON SPLICE PLATE BTWN. STA 916 TO STA 977
- [SDR NACA20250717011](https://openairdocs.org/sdr/NACA20250717011.md): Pressure Deck · corroded · Mar 5, 2025 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > AFTER REMO VAL OF GUSSET FROM L/H WW PRESS.DECK AREA STA 955 LBL 85 (APPROX) FOUND CORROSION ON MATING SURFACE OF GUSSET. REMOVED CORROSION ON GUSSET FROM L/H WW PRESS. DECK AREA STA 955 LBL 85, DIMENSIONS L=3.050" W=2.500 IAW SRM 51-10-02 STEP 15A3. EVALUAT
- [SDR NACA202507160001](https://openairdocs.org/sdr/NACA202507160001.md): Fitting · corroded · Feb 10, 2025 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > UPON REMOV AL OF SIDE FRAME FITTING (PICKLE FORK) FROM L/H STA 955 STGR 12 TO LWR W/W CENTER TANK WALL FOUND SEVERAL AREAS OF CORROSION ON FRAME FITTING. 1) RECEIVED 1EA FRAME FITTING (PICKLE FORK) P/N: 145T2523U9, BATCH: 0004378721 AND LOCATED AND DRILLED AT
- [SDR NACA20250717006](https://openairdocs.org/sdr/NACA20250717006.md): Connector · damaged · Feb 5, 2025 · N379CX · Boeing 767323 · Communications System Wiring
  > HF RIGHT AUDIO IS WEAK. PER TS PURPOSES A SELF-TEST WAS PERFORMED ON THE LT & RT HF XCVR,DURING THE SELF-TEST THE STATUS LIGHTS ON RT XCVR DID NOT COME ON.AFTER THAT SWAPPED THE XCVR LT FOR RT SIDE AND PERFORMED THE SELF-TESTAND FOUND SAME RESULT. REMOVED THE
- [SDR NACA20250717005](https://openairdocs.org/sdr/NACA20250717005.md): Valve · binding · Feb 4, 2025 · N379CX · Boeing 767323 · Pneumatic Distribution System
  > LEFT BLEED AIR INTERMITTENTFAULT. PERFORMED BITE TEST TO GET THE RECORD OF ALL THE FAULTS AT THE AIR SUPPLY BITE MODULE, FOUND PRSOV, PRV, PRC, PRESS SENSOR AND WIRE FAULT LH SIDE LIGHTS ON. THEN PER TS PURPOSES PERFORMED CONTINUITY CHECK FROM PRSOV CONNECTOR
- [SDR NACA2025071704](https://openairdocs.org/sdr/NACA2025071704.md): Apu · faulted · Feb 4, 2025 · N379CX · Boeing 767323 · APU Core Engine
  > APU DID NOT START AFTER LANDING. PERFORM TROUBLESHOOTING AS REQ OR83208 02/06/25 1. OPENED APU DOOR ACCESS PANELS 315AL & 316AR IAW AMM 12-13-04-200-801 STEP D. PERFORMED APU OIL CHECK IAW AMM 12-13-04-200-801 FOUND LWR OIL LEVEL. PERFORMED APU OIL FILL IA
- [SDR NACA2025012900001](https://openairdocs.org/sdr/NACA2025012900001.md): Web · corroded · Jan 29, 2025 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > DURING WALK AROUND OF AIRCRAFT A LARGE AREA OF CORROSION WAS FOUND LOCATED ON AFT SIDE OF WEB AT FWD STA 955 OUTBD OF LBL 74.69 APPROX WL 198. BLENDING OF CORROSION ACCOMPLISHED ON AMES WO -0006 AND NAC EO 767-53-0069. CORROSION STILL PRESENT. PERFORMED CUSTOM
- [SDR NACA2025011000002](https://openairdocs.org/sdr/NACA2025011000002.md): Control Unit · failed · Jan 10, 2025 · N379CX · Boeing 767323 · APU Start/Ignition System
  > APU WILL NOT START. DEFERRED PER MEL 49-11-01A CAT C @ 1807Z 1/10/25. REMOVED AND REPLACED APU CONTROL UNIT.
- [SDR NACA2024120300014](https://openairdocs.org/sdr/NACA2024120300014.md): Intercostal · corroded · Dec 14, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1285~1307 RBL82. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024121200002](https://openairdocs.org/sdr/NACA2024121200002.md): Tee Angle · corroded · Dec 12, 2024 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > CORROSION- FOUND MAIN DECK DOOR SILL FLOOR SUPPORT TEE CORROSION STA 1505 LBL 83. REMOVED AND REPLACED DAMAGED TEE IAW SRM 51-40-02-0G-0
- [SDR NACA2024120300016](https://openairdocs.org/sdr/NACA2024120300016.md): Floor Support · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > CORROSION - FOUND MAIN DECK FLOOR STRUCTURE DRAIN SUPPORT CORROSION STA 1601 LBL 43. REMOVED AND REPLACED DAMAGED DRAIN SUPPORT IAW 51-40-03-0G-0.
- [SDR NACA2024120300015](https://openairdocs.org/sdr/NACA2024120300015.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1329 RBL 82. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300013](https://openairdocs.org/sdr/NACA2024120300013.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1329-1351 RBL 82. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300012](https://openairdocs.org/sdr/NACA2024120300012.md): Bracket · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT UPPER CEILING PANEL SUPPORT BRACKET CORROSION STA 1307 RBL 82-92. REMOVED AND REPLACED BRACKET IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300011](https://openairdocs.org/sdr/NACA2024120300011.md): Bracket · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT MEMBERS CORROSION STA 1293 RBL 82-92. REMOVED AND REPLACED DAMAGED BRACKET IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300010](https://openairdocs.org/sdr/NACA2024120300010.md): Channel · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL CHANNEL CORROSION STA 1307-1329 RBL 62. REMOVED AND REPLACED DAMAGED CHANNEL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300009](https://openairdocs.org/sdr/NACA2024120300009.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1285 RBL 82. REMOVED AND REPLACED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA202501090000](https://openairdocs.org/sdr/NACA202501090000.md): Floorbeam · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Main, Floor Beam
  > FOUND MAIN DECK FLOOR CHORD CORROSION STA 1311, RBL 64. ACCOMPLISHED EO# 767-53-0068.
- [SDR NACA2024120300008](https://openairdocs.org/sdr/NACA2024120300008.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1307-1329 RBL 82. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300007](https://openairdocs.org/sdr/NACA2024120300007.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CARGO COMPT UPPER CEILING PANEL SUPPORT INTERCOSTAL CORROSION STA 1270-1285 RBL 82. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300006](https://openairdocs.org/sdr/NACA2024120300006.md): Support · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL INTERCOSTAL SUPPORT CORROSION STA 1270 RBL 62-82. REMOVED AND REPLACED DAMAGED INTERCOSTAL IAW SRM 51-40-0G-0.
- [SDR NACA2024120300005](https://openairdocs.org/sdr/NACA2024120300005.md): Support · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT MEMBERS CORROSION STA 1320 RBL 82-92. REMOVED AND REPLACED DAMAGED SUPPORT MEMBER IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300004](https://openairdocs.org/sdr/NACA2024120300004.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT ZEE CORROSION STA 1351 RBL 41-90. REMOVED AND REPLACED DAMAGE SUPPORT ZEE IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300003](https://openairdocs.org/sdr/NACA2024120300003.md): Intercostal · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL SUPPORT MEMBERS CORROSION STA 1309 RBL 65-82. REMOVED AND REPLACED SUPPORT MEMBERS IAW SRM 51-40-02-0G-0.
- [SDR NACA2024120300002](https://openairdocs.org/sdr/NACA2024120300002.md): Channel · corroded · Dec 3, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > AFT CGO COMPT UPPER CEILING PANEL CHANNEL CORROSION STA 1285 - 1307, RBL 62. REMOVED AND REPLACED DAMAGED CHANNEL IAW SRM 51-40-42-0G-0.
- [SDR NACA2024120200006](https://openairdocs.org/sdr/NACA2024120200006.md): Skin · corroded · Dec 2, 2024 · N379CX · Boeing 767323 · Fuselage Main, Plate/Skin
  > FOUND M/D INNER SKIN CORROSION AT BS 1197+132 TO 1219 S-13R TO S-14R. ACCOMPLISH EO 767-53-0065
- [SDR NACA2024120200005](https://openairdocs.org/sdr/NACA2024120200005.md): Skin · cracked · Dec 2, 2024 · N379CX · Boeing 767323 · Fuselage Main, Plate/Skin
  > FORWARD R/H SERVICE DOOR CUTOUT AFT LOWER CORNER FASTENER HOLE CRACK. ACCOMPLISHED EO 767-53-0064.
- [SDR NACA2024120200004](https://openairdocs.org/sdr/NACA2024120200004.md): Angle · corroded · Dec 2, 2024 · N379CX · Boeing 767323 · Fuselage Miscellaneous Structure
  > ANGLE, FOUND BULK CARGO COMPARTMENT FLOOR STRUCTURE SIDE ANGLE CORROSION ON STA 1461 & LBL 43. REMOVED AND REPLACED NEW ANGLE IAW SRM 51-40-02-0G-0 "
- [SDR NACA2024120200003](https://openairdocs.org/sdr/NACA2024120200003.md): Structure · cracked · Dec 2, 2024 · N379CX · Boeing 767323 · Fuselage Main, Structure
  > FOUND CRACK ON FASTENER HOLE, STA 1805, S-12A RH SIDE, TTL: 1EA. ACCOMPLISHED EO 767-53-0066.
- [SDR NACA2024120200002](https://openairdocs.org/sdr/NACA2024120200002.md): Skin · corroded · Dec 2, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > RIGHT WING LOWER INSPAR SKIN CORROSION REAR SPAR, WS 694~720. ACCOMPLISHED EO 767-57-0038.
- [SDR NACA2024112800003](https://openairdocs.org/sdr/NACA2024112800003.md): Skin · corroded · Nov 28, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > LEFT WING INSPAR LOWER SKIN LOWER SURFACE CORRODED, WS 852-879, L-10. ACCOMPLISHED JOB IAW EO 767-57-0037.
- [SDR NACA2024112800002](https://openairdocs.org/sdr/NACA2024112800002.md): Skin · corroded · Nov 28, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > LEFT WING INSPAR LOWER SKIN LOWER SURFACE CORRODED, NEAR WS 262, NEAR L-6. ACCOMPLISHED JOB IAW EO 767-57-0031.
- [SDR NACA2024112800001](https://openairdocs.org/sdr/NACA2024112800001.md): Skin · corroded · Nov 28, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > LEFT INSPAR LOWER SKIN AU FUEL CUTOUT AREA CORRODED. WBL 125. ACCOMPLISHED JOB IAW EO 767-57-0032.
- [SDR NACA2024112700002](https://openairdocs.org/sdr/NACA2024112700002.md): Skin · corroded · Nov 27, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > LEFT WING INSPAR LOWER SKIN LOWER SURFACE CORRODED WS 720~WS 746 NEAR REAR SPAR. ACCOMPLISHED EO 767-57-0035.
- [SDR NACA2024112700001](https://openairdocs.org/sdr/NACA2024112700001.md): Skin · corroded · Nov 27, 2024 · N379CX · Boeing 767323 · Wing, Plate/Skin
  > LEFT WING LOWER SKIN LOWER SURFACE CORRODED, NEAR WS 746, STRG 6. ACCOMPLISHED JOB IAW EO 767-57-0036 "

Next page: https://openairdocs.org/deregistered/N379CX-2025-10-09/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 = 'N379CX' AND deregistration_id = 'N379CX-2025-10-09'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N379CX-2025-10-09/reports

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