# Service difficulty reports: N255CM

A list on [N255CM](https://openairdocs.org/aircraft/N255CM.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 · 245 reports

- [SDR IXXA20260826075](https://openairdocs.org/sdr/IXXA20260826075.md): Escape Reel · unwanted deploy · Aug 26, 2026 · N255CM · Boeing 767223 · Emergency Equipment
  > NUMBER 2 EMERGENCY ESCAPE DEVICE DEPLOYED. R & R NR 2 EMERGENCY DESCENT DEVICE IAW AMM 25-61-03.
- [SDR IXXA20260822073](https://openairdocs.org/sdr/IXXA20260822073.md): Battery · inoperative · Aug 22, 2026 · N255CM · Boeing 767223 · Emergency Equipment
  > PORTABLE FLASHLIGHT INDICATOR LIGHT NOT FLASHING. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-02. OPS CHECKED GOOD.
- [SDR IXXA20260422002](https://openairdocs.org/sdr/IXXA20260422002.md): Bracket · cracked · Apr 22, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Plate/Skin
  > CRACK NOTED AT PYLON NR 1 I/B SIDE PYLON STRUCTURE BRACKET NEXT TO ACCESS PANEL 437BR FWD LOWER CORNER REFERENCE XTREME WO 014592 NRC 512
- [SDR IXXA202604211001](https://openairdocs.org/sdr/IXXA202604211001.md): Channel · worn · Apr 21, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NR 2, SHIP FAIRING FWD SECTION FWD LOWER BRACE FRAME FROM INB TO O/B, FOUND OUT OF LIMITS AND WITH ELONGATED HOLES. REFERENCE XTREME WO 014592 NRC 884
- [SDR IXXA20260421001](https://openairdocs.org/sdr/IXXA20260421001.md): Floor Support · corroded · Apr 21, 2026 · N255CM · Boeing 767223 · Fuselage Miscellaneous Structure
  > FOUND INTERCOSTAL SUPPORT APPROX AT STA 1339 AND RBL 33 WITH CORROSION REFERENCE XTREME WO 014592 NRC 939
- [SDR IXXA20260420002](https://openairdocs.org/sdr/IXXA20260420002.md): Skin · cracked · Apr 20, 2026 · N255CM · Boeing 767223 · Fuselage Main, Plate/Skin
  > CRACK FOUND AT FORWARD ENTRY DOOR CUT OUT AFT LOWER CORNER BETWEEN STA 340- STA 332 - 1" ABOVE S-20L
- [SDR IXXA20260419001](https://openairdocs.org/sdr/IXXA20260419001.md): Rib · cracked · Apr 19, 2026 · N255CM · Boeing 767223 · Wing, Rib/Bulkhead
  > FOUND RT WING OTBD L/E RIB AT OSS 464.48 CRACKED. REFER TO XTREME WO 014592 NRC 842
- [SDR IXXA20260422001](https://openairdocs.org/sdr/IXXA20260422001.md): Skin · worn · Apr 18, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Plate/Skin
  > ENGINE NR 2 SHIP FAIRING FWD O/B VERTICAL OVERLAP FRAME BENT AND WORN. REF XTREME AVIATION NRC 889
- [SDR IXX2026F00006](https://openairdocs.org/sdr/IXX2026F00006.md): Frame · corroded · Apr 18, 2026 · N255CM · Boeing 767223 · Auxiliary Power Unit (APU) Doors
  > CORROSION EVIDENCE NOTED AT APU COMPARTMENT DOOR 315AL (L/H SIDE) INTERNAL SIDE FRAME STA 1840.2 CLOSE TO I/B EDGE REFERENCE XTREME WO 014592 NRC 905
- [SDR IXXA20260417003](https://openairdocs.org/sdr/IXXA20260417003.md): Angle · cracked · Apr 17, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Structure
  > CRACK NOTED AY PYLON #1 HYDRAULLIC BAY INTERNAL AREA, I/B SIDE FWD UPPER CORNER, CLOSE TO BOOT-STRAP ENGINE REMOVAL TOOL ATTACHING POINT REFERENCE XTREME WO 014592 NRC 872
- [SDR IXXA20260417002](https://openairdocs.org/sdr/IXXA20260417002.md): Shear Tie · corroded · Apr 17, 2026 · N255CM · Boeing 767223 · Fuselage Internal Mounting Structure
  > BULK CARGO COMPARTMENT STA 1518 BETWEEN STR 34R TO STR 33R WAS FOUND CORROSION ON T-SHIELD REFERENCE XTREME WO 014592 NRC 788
- [SDR IXXA20260417001](https://openairdocs.org/sdr/IXXA20260417001.md): Bracket · worn · Apr 17, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NR 1 SHIP FAIRING FWD SECTION VERTICAL ANGLE BRACKET O/B FOUND ELONGATED HOLES REFERENCE XTREME WO 014592 NRC 943
- [SDR IXXA20260408001](https://openairdocs.org/sdr/IXXA20260408001.md): Skin · dented · Apr 8, 2026 · N255CM · Boeing 767223 · Fuselage Structure (General)
  > DENT NOTED AT FUSELAGE SKIN LOWER SIDE BETWEEN BS 390 TO BS 412. AND BETWEEN STRINGERS S-38R AND S-37R. REF XTREME AVIATION NRC 166
- [SDR IXX2026F00005](https://openairdocs.org/sdr/IXX2026F00005.md): Stiffener · elongated · Mar 18, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NO 2. SHIP FAIRING FWD SECTION VERTICAL ANGLE BRACKETS, I/B AND O/B BRACKETS FOUND ELONGATED HOLES. REF XTREME AVIATION NON ROUTINE 883
- [SDR IXXA20260328002](https://openairdocs.org/sdr/IXXA20260328002.md): Channel · cracked · Mar 11, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NO 1 NACELLE STRUT FAIRING, FWD BRACE FROM I/B TO O/B CRACKED AND HAVE ELONGATED FASTENER HOLES. REF XTREME AVIATION NRC 851
- [SDR IXXA20230327001](https://openairdocs.org/sdr/IXXA20230327001.md): Strut · cracked · Mar 11, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Main Frame
  > NR 1 NACELLE STRUT FAIRING, I/B U FRAME CRACKED. XTREME AVIATION NON ROUTINE 856
- [SDR IXXA20260418002](https://openairdocs.org/sdr/IXXA20260418002.md): Shear Tie · corroded · Mar 4, 2026 · N255CM · Boeing 767223 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, STA 1380 STR 39L WAS FOUND CORROSION. REF XTREME AVIATION NON ROUTINE 809
- [SDR IXX2026F00007](https://openairdocs.org/sdr/IXX2026F00007.md): Bracket · cracked · Mar 3, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > ENGINE NR 2 INBD SJIP FAIRING ACCESS PANEL, LOWER BRACKET TO SIDEWALL MOUNT CRACKED. REF TO XTREME AVIATION NRC 738
- [SDR IXXA202604060011](https://openairdocs.org/sdr/IXXA202604060011.md): Support Bracket · cracked · Mar 3, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon, Main Frame
  > STRUT NR 1, LT AT NAC 295.09 SUPPORT BRACKET WITH CRACK. REF XTREME AVIATION NRC 732
- [SDR IXXA20260328001](https://openairdocs.org/sdr/IXXA20260328001.md): Bracket · cracked · Feb 27, 2026 · N255CM · Boeing 767223 · Nacelle/Pylon Miscellaneous Structure
  > CRACK NOTED AT PYLON NR 1 AFT SECTION MID ANGLE FOR LATERAL SUPPORT OF PYLON PANEL I/B SIDE FWD END BRACKET. (CRACK VISABLE FROM AFT SIDE WITH ACCESS PANEL 437DB REMOVED). REF XTREME AVIATION NRC 522
- [SDR IXXA20260420003](https://openairdocs.org/sdr/IXXA20260420003.md): Skin · cracked · Feb 25, 2026 · N255CM · Boeing 767223 · Fuselage Main, Plate/Skin
  > AD2024-05-03, SB 767-53A0301 REV 2. CRACK FOUND AT FORWARD SERVICE DOOR CUTOUT AFT LOWER CORNER BETWEEN STA 340 - STA 332 1' HOLE ABOVE S-20R. REF XTREME AVIATION NRC 341
- [SDR IXX2026F00004](https://openairdocs.org/sdr/IXX2026F00004.md): Channel · cracked · Feb 24, 2026 · N255CM · Boeing 767223 · Fuselage Miscellaneous Structure
  > NOSE WHEEL WELL LH LOWER CHORD AT STA 276 CRACK NOTED. REF XTREME AVIATION NRC 187
- [SDR IXXA20251106073](https://openairdocs.org/sdr/IXXA20251106073.md): Link · damaged · Nov 6, 2025 · N255CM · Boeing 767223 · Nose/Tail Landing Gear
  > ON APPROACH GEAR NOT DOWN EICAS & NO NLG GREEN LIGHT NOT ILLUMINATED, FOLLOWED BY GEAR DISAGREE CHKLIST. 2 LOW PASSES FROM TOWER INDICATED NLG GEAR APPEARED TO BE DOWN. EICAS CONFIG & DISAGREE CHKLISTS PERFORMED & GEAR COMPLETION OF 14:16 LANDING SUCCESSFUL &
- [SDR IXXA20240628045](https://openairdocs.org/sdr/IXXA20240628045.md): Seal · dirty · Jun 24, 2024 · N255CM · Boeing 767223 · Flight Compartment Windows
  > PREFLIGHT CREW REPORTED R2 WINDOW DIFFICULT TO CLOSE. R2 WINDOW SEAL CLEANED AND LUBRICATED IAW BOEING 767-300 AIRCRAFT MAINTENANCE MANUAL 56-11-02. OPERATIONAL CHECK GOOD.
- [SDR IXXA20240624043](https://openairdocs.org/sdr/IXXA20240624043.md): Escape Reel · unwanted deploy · Jun 22, 2024 · N255CM · Boeing 767223 · Emergency Equipment
  > POST FLIGHT LINE MAINTENANCE REPORTED ESCAPE REEL POSITION 5 DEPLOYED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52790 PER ATI MINIMUM EQUIPMENT LIST 25-61-01-01. ESCAPE DESCENT DEVICE CERTIFIED INOPERATIVE. POSITION 5 ESCAPE DEVICE REMOVED AND REPLACE
- [SDR IXXA20240624042](https://openairdocs.org/sdr/IXXA20240624042.md): Escape Reel · unwanted deploy · Jun 22, 2024 · N255CM · Boeing 767223 · Emergency Equipment
  > POST FLIGHT LINE MAINTENANCE REPORTED ESCAPE REEL POSITION 4 DEPLOYED. FAULT TRANSFERRED TO DEFERRAL MAINTENANCE ITEM 52789 PER ATI MINIMUM EQUIPMENT LIST 25-61-01-01. ESCAPE DESCENT DEVICE CERTIFIED INOPERATIVE. POSITION 4 ESCAPE DEVICE REMOVED AND REPLACE
- [SDR IXXA2024032600002](https://openairdocs.org/sdr/IXXA2024032600002.md): Frame Angle · cracked · Mar 26, 2024 · N255CM · Boeing 767223 · Fuselage Main, Frame
  > REPAIR, MAIN FRAME INNER CHORD TRANSITION RADIUS. STA 883.5 RBL 89
- [SDR IXXA2024032001](https://openairdocs.org/sdr/IXXA2024032001.md): Skin Panel · delaminated · Mar 20, 2024 · N255CM · Boeing 767223 · Vertical Stabilizer, Plate/Skin
  > R/H VERTICAL STAB HAS AREA DELAMINATED ON SKIN PANEL
- [SDR IXXA202308175047](https://openairdocs.org/sdr/IXXA202308175047.md): Battery · inoperative · Aug 15, 2023 · N255CM · Boeing 767223 · Emergency Equipment
  > DURING DAILY CHECK FOUND FLASHLIGHT IN FLIGHT DECK INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IN ACCORDANCE WITH IAI SSM 25-60-00.
- [SDR IXXA20230730042](https://openairdocs.org/sdr/IXXA20230730042.md): Battery · inoperative · Jul 30, 2023 · N255CM · Boeing 767223 · Emergency Equipment
  > DURING SERVICE CHECK FOUND FLASHLIGHT INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PACK PER AMM 25-64-00. OPERATIONAL CHECK GOOD.
- [SDR IXXA20221014140](https://openairdocs.org/sdr/IXXA20221014140.md): Battery · inoperative · Oct 14, 2022 · N255CM · Boeing 767223 · Emergency Equipment
  > DURING ROUTINE MAINTENANCE FLIGHT DECK'S FLASHLIGHT RED BATTERY INDICATOR INOPERATIVE. REMOVED AND REPLACED EMERGENCY FLIGHT DECK FLASHLIGHT BATTERY IN ACCORDANCE WITH B767 IAI 25-60-00. OPERATIONAL CHECK GOOD.
- [SDR IXXA2022061403](https://openairdocs.org/sdr/IXXA2022061403.md): Pad · worn · Jun 14, 2022 · N255CM · Boeing 767200 · Powerplant System
  > REMOVED AND REPLACED # 2 ENGINE LOUVRED DOOR, AFT LATCH STOP PAD SEE PARTIAL 1-4 FOR FAB OF STOP PAD IAW B767 SRM 51-40-02 PARA 4
- [SDR IXXA2022061402](https://openairdocs.org/sdr/IXXA2022061402.md): Web · corroded · Jun 14, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > ALC PRESSURE DECK WEB @ STA 1310 RBL6 CORRODED
- [SDR IXXA2022061401](https://openairdocs.org/sdr/IXXA2022061401.md): Rod · damaged · Jun 14, 2022 · N255CM · Boeing 767200 · Nacelle/Pylon Miscellaneous Structure
  > HOLD OPEN ROD CHAFED AND DAMAGED #1 ENGINE O/B HYDRAULICS' BAY DOOR
- [SDR IXXA2022061304](https://openairdocs.org/sdr/IXXA2022061304.md): Panel · corroded · Jun 13, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > AORROSION FLC STA 522,RBL47 IN POCKET AT CHORD
- [SDR IXXA2022061303](https://openairdocs.org/sdr/IXXA2022061303.md): Bracket · corroded · Jun 13, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > CORROSION WASTE TANK BRACKET P/N 417T1310-23
- [SDR IXXA2022061302](https://openairdocs.org/sdr/IXXA2022061302.md): Pressure Web · corroded · Jun 13, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > CORROSION ON FWD SIDE OF P-DOME
- [SDR IXXA2022061301](https://openairdocs.org/sdr/IXXA2022061301.md): Strap · corroded · Jun 13, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > FAIL SAFE STRAP CORRODED STA 540-610 RBL 44
- [SDR IXXA2022061203](https://openairdocs.org/sdr/IXXA2022061203.md): Skin · damaged · Jun 12, 2022 · N255CM · Boeing 767200 · Wing, Plate/Skin
  > CRACK DAMAGE RIGHT WING FIXED LEADING EDGE SKIN
- [SDR IXXA2022061202](https://openairdocs.org/sdr/IXXA2022061202.md): Bracket · corroded · Jun 12, 2022 · N255CM · Boeing 767200 · Cargo Compartments
  > CANNON PLUG CONNECTOR BRACKET ON PDU PAN AT STA 621 CORRODED
- [SDR IXXA2022061201](https://openairdocs.org/sdr/IXXA2022061201.md): Support Web · corroded · Jun 12, 2022 · N255CM · Boeing 767200 · Fuselage Miscellaneous Structure
  > ALC PDU MOUNT STA 1346 LBL33 CORRODED
- [SDR IXXA20220601104](https://openairdocs.org/sdr/IXXA20220601104.md): Support Frame · corroded · Jun 11, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > FUSELAGE FRAME CORRODED
- [SDR IXXA2022061103](https://openairdocs.org/sdr/IXXA2022061103.md): Floor Support · corroded · Jun 11, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > INNER CHORD CORRODED
- [SDR IXXA2022061102](https://openairdocs.org/sdr/IXXA2022061102.md): Stringer · corroded · Jun 11, 2022 · N255CM · Boeing 767200 · Fuselage Structure (General)
  > STRINGER 39 L CORRODED
- [SDR IXXA2022061101](https://openairdocs.org/sdr/IXXA2022061101.md): Stringer · corroded · Jun 11, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > STRINGER CORRODED
- [SDR IXXA2022061004](https://openairdocs.org/sdr/IXXA2022061004.md): Web · corroded · Jun 10, 2022 · N255CM · Boeing 767200 · Fuselage Structure (General)
  > UPPER CARGO FRAME CORRODED.
- [SDR IXXA2022061002](https://openairdocs.org/sdr/IXXA2022061002.md): Panel · cracked · Jun 10, 2022 · N255CM · Boeing 767200 · Fuselage Structure (General)
  > P-33 PANEL CRACKED
- [SDR IXXA2022061001](https://openairdocs.org/sdr/IXXA2022061001.md): Panel Support · corroded · Jun 10, 2022 · N255CM · Boeing 767200 · Fuselage Structure (General)
  > LPANEL SUPPORT CHORD CHORD
- [SDR IXXA2022060806](https://openairdocs.org/sdr/IXXA2022060806.md): Frame · corroded · Jun 8, 2022 · N255CM · Boeing 767200 · Fuselage Main, Structure
  > CORROSION ON LOWER SURFACE OF UPPER FRAME CHORD, FRAME 1395 AT THE ROLLER RAIL LBL42 TO RBL42
- [SDR IXXA2022061315](https://openairdocs.org/sdr/IXXA2022061315.md): Floor Panel · corroded · Jun 7, 2022 · N255CM · Boeing 767223 · Fuselage Main, Structure
  > CORRODED FLOOR BEAM UPPER CHORD

Next page: https://openairdocs.org/aircraft/N255CM/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 = 'N255CM' AND registry_match = 'registration'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/aircraft/N255CM/reports

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