# Service difficulty reports: N123DN, cancelled Feb 28, 2018

A list on [N123DN, cancelled Feb 28, 2018](https://openairdocs.org/deregistered/N123DN-2018-02-28.md).

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

- [SDR RYNA201207250031](https://openairdocs.org/sdr/RYNA201207250031.md): Connector · loose · Jul 25, 2012 · N123DN · Boeing 767332 · Light System Wiring
  > FOUND EMERGENCY LIGHTING WIRE HARNESS CONNECTOR LOOSE UNDER SEAT 26B AND 25F. RECONNECTED CONNECTOR AND SECURED WIRE HARNESS UNDER SEAT 26B AND25F AND EMERGENCY LIGHTING OPS CHECK GOOD PER MM 33-51-00.
- [SDR RYNA201206150026](https://openairdocs.org/sdr/RYNA201206150026.md): Battery Pack · discharged · Jun 15, 2012 · N123DN · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHTS INOPERATIVE AT ALL PASSENGER SEATS AND LOWER EXIT SIGNS AT ALL DOORS. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACKS AT SEATS 2A, 29A, AND 45G PER AMM 33-51-09. OPERATIONAL CHECKED NORMAL.
- [SDR RYNA201203200015](https://openairdocs.org/sdr/RYNA201203200015.md): Actuator Valve · inoperative · Mar 20, 2012 · N123DN · Boeing 767322 · Power Lever
  > NR 2 ENGINE WILL NOT START- ENGINE VALVE LIGHT ILLUMINATED ON OVERHEAD PANEL. EICAS MESSAGE "RIGHT ENGINE VALVE-NO START". REMOVED AND REPLACED ENGINE CONDITIONER CONTROL FUEL ACTUATOR PER MM 76-11-01 PG 401, OPS CHECK NORMAL.
- [SDR RYNA2011082000018](https://openairdocs.org/sdr/RYNA2011082000018.md): Battery Pack · inoperative · Aug 20, 2011 · N123DN · Boeing 767332 · Emergency Lighting
  > RIGHT/LEFT AFT, L1 AND R1 EMERGENCY EXIT THRESHOLD LIGHTS INOPERATIVE. REMOVED AND REPLACED BATTERY PACK PER MM 33-51-07. OPERATIONAL CHECKED GOOD.
- [SDR RYNA2010002260005](https://openairdocs.org/sdr/RYNA2010002260005.md): Battery Pack · discharged · Feb 5, 2010 · N123DN · Boeing 767332 · Emergency Lighting
  > THE FOLLOWING ITEMS WERE NOTED REGARDING THE EMERGENCY LIGHTING SYSTEM DURING THE INSPECTION AND TESTING OF THE C-CHECK ON AIRCRAFT N123DN: EMERGENCY LIGHT OUTSIDE R1 DOOR INOPERABLE AND 3 RT OVERWING. EMERGENCY EXIT SIGN INOPERABLE LEFT AND RIGHT SIDE O/H F
- [SDR RYNA201002040003](https://openairdocs.org/sdr/RYNA201002040003.md): Strap · cracked · Jan 30, 2010 · N123DN · Boeing 767332 · Fuselage Main, Bulkhead
  > DURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06-R1.1875 INCH CRACK WAS FOUND ON THE RT REAR BULKHEAD SIDE FITTING FAIL-SAFE STRAP. ACCOMPLISHED REPAIR ON RT SIDE PER EO RN767-53-02 AND BOEING SB 767-53A0100.
- [SDR RYNA2010002040002](https://openairdocs.org/sdr/RYNA2010002040002.md): Strap · cracked · Jan 30, 2010 · N123DN · Boeing 767332 · Fuselage Main, Bulkhead
  > DURING THE ACCOMPLISHMENT OF EO RN767-53-02 RELATED TO BOEING SB 767-53A0100 AND AD 2004-19-06 R1 A.0937 INCH CRACK WAS FOUND ON THE LT REAR BULKHEAD SIDE FITTING FAIL-SAFE STRAP. ACCOMPLISHED REPAIR ON LT SIDE PER EO RN767-53-02 AND BOEING SB 767-53A0100.
- [SDR RYNA200910300021](https://openairdocs.org/sdr/RYNA200910300021.md): Unknown · malfunctioned · Oct 29, 2009 · N123DN · Boeing 767332 · Door Warning System
  > DURING CLIMB EICAS E/E LIGHT ILLUMINATED, CABIN CONTINUED SLIGHT CLIMB. PERFORMED AIR TURNBACK. PLACARD THE LOWER LOBE ELECTRONIC EQUIPMENT ACCESS DOOR ITEM DEFERRED PER MEL 52-71-1 ITEM IS A CATEGORY C. ADDITIONALLY PERFORMED CABIN PRESSURE CONTROL BITE CH
- [SDR RYNA200909180019](https://openairdocs.org/sdr/RYNA200909180019.md): Structure · cracked · Sep 14, 2009 · N123DN · Boeing 767332 · Fuselage Miscellaneous Structure
  > PERFORMING FLEET CAMPAIGN DIRECTIVE (FCD) 53-205 FOUND CRACKING WITHIN STA 287 AT WL 159 WHICH EXTENDS APPROXIMATELY 0.375 INCHES ABOVE WL 159 AND APPROXIMATELY 0.750 INCHES BELOW WL 159. FERRY WAS AGREED TO UNDER THE LIMITATIONS: FLIGHT TO BE CONDUCTED USIN
- [SDR RYNA200908210016](https://openairdocs.org/sdr/RYNA200908210016.md): Proximity Sensor · faulty · Aug 18, 2009 · N123DN · Boeing 767332 · Door Warning System
  > DURING PREFLIGHT INSPECTION THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT CAME ON. PLACARD THE PILOT’S OVERHEAD EMERGENCY ADVISORY LIGHT PER MEL 52-71-1 DMI REFERENCE 60510. REMOVED AND REPLACED SENSOR 192 PER AMM 52-71-01 PAGE 412-414. OPS CHECK GOOD, CLE
- [SDR RYNA200906170007](https://openairdocs.org/sdr/RYNA200906170007.md): B-Nut · loose · Jun 15, 2009 · N123DN · Boeing 767332 · Hydraulic System, Main
  > LEFT HYDRAULIC SYSTEM PRESSURE, RUDDER RATIO, LEFT HYDRAULIC QUANTITY, YAW DAMPER, AND SPOILER EICAS MESSAGES. TIGHTENED B NUT THAT BACKED OFF ON NR 1 ENGINE HYDRAULIC PUMP. REMOVED AND REPLACED PRESSURE, CASE DRAIN AND RETURN FILTERS.
- [SDR RYNA200800044](https://openairdocs.org/sdr/RYNA200800044.md): Fan Blade · out of balance · Nov 28, 2008 · N123DN · Boeing 767332 · Turbine Engine Compressor Section
  > DURING CLIMB AND LEVEL OFF AT F/L 370 RIGHT ENGINE VIBRATION REACHED 3.9 UNITS. THE AIRCRAFT DIVERTED TO ATLANTA FOR MAINTENANCE TO DELTA AIRLINES MAINTENANCE CENTER. ACCOMPLISHED BORESCOPE INSPECTION, FAN BLADE LUBRICATION, RIGGED VSV & VBV SYSTEM AND BALAN
- [SDR RYN2008F00010](https://openairdocs.org/sdr/RYN2008F00010.md): Radio · failed · Aug 6, 2008 · N123DN · Boeing 767332 · HF Communications System
  > ACFT DIVERTED DUE TO LOSS OF THE RT HF COMMUNICATION SYSTEM. THE LT HF IS ALREADY ON DEFERRAL PER MEL 23-11-1-2. TROUBLESHOOTING IN WORK (ISSUED MEL 23-11-1-2OH DMI NR62632). (S)
- [SDR DL76S071016](https://openairdocs.org/sdr/DL76S071016.md): Window · cracked · Aug 4, 2007 · N123DN · Boeing 767332 · Flight Compartment Windows
  > F/O WINDSHIELD CRACKED AND IS ARCHING. REPLACED R1 WINDOW WINDOW HEAT CONTROL UNIT PER AMM. BITE CHECKED CONTROL UNIT IT VERIFIED GOOD.
- [SDR DL76S060877](https://openairdocs.org/sdr/DL76S060877.md): Floorbeam · corroded · Oct 20, 2006 · N123DN · Boeing 767332 · Fuselage Main, Floor Beam
  > CORROSION WAS FOUND AROUND THE NUT PLATES ON THE LOWER TEE OF THE 1502 FLOORBEAM. THE CORROSION WAS REMOVED AND REPAIR PARTS INSTALLED PER BOEING INSTRUCTIONS AS CONTAINED IN 456631-14.
- [SDR DL76S060876](https://openairdocs.org/sdr/DL76S060876.md): Skin · cracked · Oct 20, 2006 · N123DN · Boeing 767332 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS FOUND CRACKED AT THE NR 3 VHF ANTENNA, FS 1197+90, AT STR 39L 39R. REPAIR INVOLVED CUTTING OUT THE DAMAGE AND INSTALLATION OF BOEING APPROVED REPAIR PARTS PER ERA 455968-14.
- [SDR DL76S060875](https://openairdocs.org/sdr/DL76S060875.md): Fitting · corroded · Oct 20, 2006 · N123DN · Boeing 767332 · Fuselage Main, Attach Fittings
  > CORROSION WAS IDENTIFIED ON THE INBOARD FORWARD SURFACE OF THE REAR SPAR BULKHEAD TERMINAL FITTING. THE BOEING APPROVED REPAIR INVOLVED REMOVING BOLTS FOR ACCESS AND LIGHT BLENDING OF THE SURFACE TO REMOVE THE CORROSION PER ERA 456629-14.
- [SDR DL76S060873](https://openairdocs.org/sdr/DL76S060873.md): Spar · cracked · Oct 20, 2006 · N123DN · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib
  > THE NUMBER 1 PYLON UPPER SPAR FITTING, RHS AT ATTACH FITTING HOLE SHOWED A CRACK INDICATION. THE SUBJECT HOLE WAS OVERSIZED, AND THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF A STRAIGHT SHANK FREEZE PLUG PER ERA 456634-14.
- [SDR DL76S060871](https://openairdocs.org/sdr/DL76S060871.md): Bulkhead · damaged · Oct 20, 2006 · N123DN · Boeing 767332 · Nacelle/Pylon, Bulkhead/Firewall
  > DURING ACCOMPLISHMENT OF THE SIP MOD ON THE AIRCRAFT, AN EXISTING FREEZE PLUG REPAIR WAS FOUND ON THE NR 1 PYLON LHS UPPER ATTACH HOLE FOR GSE FITTING. THE PLUG WAS COMMON TO THE BULKHEAD FLANGE AND SIDE LOAD FITTING. THE SIDE LOAD FITTING WAS REPLACED AS PA
- [SDR DL76S060870](https://openairdocs.org/sdr/DL76S060870.md): Spar · damaged · Oct 20, 2006 · N123DN · Boeing 767332 · Nacelle/Pylon, Frame/Spar/Rib
  > DURING ACCOMPLISHMENT OF EO 01-074906-03 THE NUMBER 2 PYLON SPLICE PLATE UPPER OUTBOARD HOLE WAS FOUND TO ALREADY BE OVERSIZED TO BEYOND MAX EO LIMIT. THE BOEING APPROVED REPAIR INVOLVED INSTALLATION OF AN OVERSIZED FASTENER PER ERA 456537-14.
- [SDR DL76S060869](https://openairdocs.org/sdr/DL76S060869.md): Fitting · damaged · Oct 20, 2006 · N123DN · Boeing 767332 · Nacelle/Pylon, Attach Fittings
  > THE NUMBER 2 PYLON UPPER SPAR FITTING WAS FOUND TO HAVE A PREVIOUSLY OVERSIZED HOLE, AT THE AFT OUTER PERIMETER FASTENER. A BOEING APPROVED REPAIR WAS INSTALLED AT THE SUBJECT LOCATION, PER ERA 456536-14.
- [SDR DL76S060868](https://openairdocs.org/sdr/DL76S060868.md): Skin · misrepaired · Oct 20, 2006 · N123DN · Boeing 767332 · Fuselage Main, Plate/Skin
  > A PREVIOUS REPAIR FOUND ON THE FUSELAGE SKIN AT 500 AND S36L DOES NOT CONFORM TO SRM AND NO RECORDS WERE FOUND. REPAIR WAS REMOVED AND A BOEING APPROVED REPAIR WAS INSTALLED PER ERA 456627-14.
- [SDR DL76S060658](https://openairdocs.org/sdr/DL76S060658.md): Frame · cracked · Aug 11, 2006 · N123DN · Boeing 767332 · Fuselage Main, Frame
  > FUSELAGE FRAME FS 883.5 RHS LOWER INNER CHORD CRACK. CRACK WAS LOCATED ON THE LOWER END OF THE.25 RADIUS TRANSITION BETWEEN CHORD FLANGES.
- [SDR DL76S060649](https://openairdocs.org/sdr/DL76S060649.md): Frame · cracked · Aug 11, 2006 · N123DN · Boeing 767332 · Fuselage Main, Frame
  > CRACKS WERE FOUND ON THE INNER CHORD OF THE FS 903 FRAME, RT SIDE. DAMAGE WAS CUT OUT AND A REPAIR ANGLE WAS INSTALLED.
- [SDR DL76S060583](https://openairdocs.org/sdr/DL76S060583.md): Fitting · misaligned · Jul 13, 2006 · N123DN · Boeing 767332 · Wing, Nacelle/Pylon Attach Fittings
  > THE NR 1 PYLON INBOARD PITCH LOAD FITTING UPPER LINK BUSHING HAS MIGRATED 0.004 INCH. THE MIGRATED BUSHING WAS REPLACED. AD 2004-16-12, B767-57-0053.
- [SDR DL76S060701](https://openairdocs.org/sdr/DL76S060701.md): Linkage · misinstalled · Jun 27, 2006 · N123DN · Boeing 767332 · Escape Slide
  > DURING INSPECTION OF THE LT OFF WING ESCAPE SLIDE PER JIC 6075 THE TECHNICIAN FOUND THAT THE INTEGRATOR LOCK HANDLE HAD TO BE FORCED INTO THE SAFETY POSITION. UPON FURTHER INVESTIGATION IT WAS DETERMINED THAT SLIDE DOOR OPENING ACTUATOR LINKAGE LEVER WAS INST
- [SDR DL76S020312](https://openairdocs.org/sdr/DL76S020312.md): Light · inoperative · Mar 15, 2002 · N123DN · Boeing 767332 · Emergency Lighting
  > SVC CHECK FOUND EMERGENCY OVERHEAD LIGHT AT ROW 17 LT SIDE INOP. REPLACED EMERGENCY LIGHT ASSY AT ROW 17 LT SIDE, CHECKS OK.
- [SDR DL76S011436](https://openairdocs.org/sdr/DL76S011436.md): Battery Pack · discharged · Aug 30, 2001 · N123DN · Boeing 767332 · Emergency Equipment
  > RT EMERGENCY ESCAPE SQUIB WILL NOT TEST. REPLACED RT BATTERY PACK TEST OK.
- [SDR DL76S001594](https://openairdocs.org/sdr/DL76S001594.md): Battery · discharged · Aug 18, 2000 · N123DN · Boeing 767332 · Emergency Lighting
  > EMERGENCY LIGHT BATTERY PACK AND POWER SUPPLY INOP. REPLACED BATTERY.
- [SDR DL76S990685](https://openairdocs.org/sdr/DL76S990685.md): Power Supply · inoperative · Mar 29, 1999 · N123DN · Boeing 767332 · Emergency Lighting
  > DURING ROUTINE MAINTENANCE, THE LEFT AND RIGHT EMERGENCY EXIT THRESHOLD LIGHTS FOUND INOP. REPLACED POWER SUPPLY, OPS CK NORMAL.
- [SDR DL76S980655](https://openairdocs.org/sdr/DL76S980655.md): Wedge · delaminated · Mar 24, 1998 · N123DN · Boeing 767332 · Leading Edge Devices
  > WINGS NR 1 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 1 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 4 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364345-14AD.
- [SDR DL76S980654](https://openairdocs.org/sdr/DL76S980654.md): Wedge · delaminated · Mar 24, 1998 · N123DN · Boeing 767332 · Leading Edge Devices
  > WINGS NR 2 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 2 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 7 BY 4.5 AREA OF DELAMINATION ON THE UPPER SKIN. THE DAMAGE WAS REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364346-14AD.
- [SDR DL76S980653](https://openairdocs.org/sdr/DL76S980653.md): Wedge · delaminated · Mar 24, 1998 · N123DN · Boeing 767332 · Leading Edge Devices
  > WINGS NR 8 SLAT TRAILING EDGE WEDGE, REPAIR FOR DELAMINATION. THE NR 8 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 5 BY 9 AREA OF DELAMINATION ON THE UPPER SKIN. THE DELAMINATION WAS REPAIRED PER THE B767 SRM 57-43-02 AND DOCUMENTED PER ER/A 364347-14AD.
- [SDR DL76S980652](https://openairdocs.org/sdr/DL76S980652.md): Skin · delaminated · Mar 24, 1998 · N123DN · Boeing 767332 · Leading Edge Devices
  > WINGS LEADING EDGE SLAT NR 11, TRAILING EDGE WEDGE, SKIN DELAMINATION REPAIR. THE UPPER SKIN OF THE NR 11 SLAT TRAILING EDGE WEDGE WAS FOUND WITH A 3 BY 6 AREA OF DELAMINATION. THE DAMAGE WAS TRIMMED OUT AND REPAIRED PER B767 SRM 57-43-02 AND DOCUMENTED PER
- [SDR DL76S970585](https://openairdocs.org/sdr/DL76S970585.md): Battery Pack · discharged · Mar 30, 1997 · N123DN · Boeing 767332 · Emergency Lighting
  > RIGHT AND LEFT AFT SERVICE DOOR INTERIOR EMERGENCY EXIT LIGHT SIGNS INOP. REPLACED BATTERY PACK, CHECKS GOOD.
- [SDR DL76S970341](https://openairdocs.org/sdr/DL76S970341.md): Skin · delamination · Feb 24, 1997 · N123DN · Boeing 767332 · Leading Edge Devices
  > THE NR 10 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED AT THE INBD CORNER. THE DAMAGE CUTOUT MEASURES 8 FWD-AFT AND 6 INBD-OUTBD. DAMAGE REPAIRED PER ER/A 361270-14AD.
- [SDR DL76S961847](https://openairdocs.org/sdr/DL76S961847.md): Te Wedge · delaminated · Aug 2, 1996 · N123DN · Boeing 767332 · Leading Edge Devices
  > THE NRS 10, 11, 12 LEADING EDGE SLATS' TRAILING EDGE WEDGES WERE FOUND TO HAVE AREAS OF DELAMINATION. THE AREAS MEASURE 4 INCHES BY 6 INCHES, 2 INCHES BY 3 INCHES, AND 10 INCHES BY 6 INCHES, RESPECTIVELY. REPAIRED IN ACCORDANCE WITH B767-300 SRM, 57-43-02, F
- [SDR DL76S960203](https://openairdocs.org/sdr/DL76S960203.md): Check Valve · cracked · Jan 26, 1996 · N123DN · Boeing 767332 · Hydraulic System, Main
  > INFLIGHT GOT EICAS FOR LT SYS HYDRAULIC'S, FOLLOWED IMMEDIATELY BY LEFT HYDRAULIC SYS PRESSURE MESSAGE. STATUS PAGE SHOWS LT QTY AT 0.04. FOUND CHECK VALVE AT GROUND HYD SERV QUICK DISCONNECT LEAKING.
- [SDR DL76S952151](https://openairdocs.org/sdr/DL76S952151.md): Skin · lightning strike · May 16, 1995 · N123DN · Boeing 767332 · Fuselage Main, Plate/Skin
  > FOUND DURING LETTER CHECK, LIGHTNING STRIKES ABOVE COCKPIT SECTION OF FUSELAGE. BURNISHED OUT DAMAGES, FOUND ONE LIGHTING STRIKE OUT OF LIMITS. REPLACED RIVETS STA 355 BETWEEN STR 3 AND 4R STA 400 STR 4R, STA 484 STR 3R. DYE CHECKED AREAS, TREATED AND PAINT
- [SDR DL76S950698](https://openairdocs.org/sdr/DL76S950698.md): Skin · lightning strike · Feb 19, 1995 · N123DN · Boeing 767332 · Fuselage Main, Plate/Skin
  > DURING LETTER CHECK, FOUND SEVERAL LIGHTNING STIKES TO FUSELAGE SKIN. RT SIDE REPAIRED PER SRM 53-00-01 ITEM 3.

## 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 = 'N123DN' AND deregistration_id = 'N123DN-2018-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N123DN-2018-02-28/reports

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