# Service difficulty reports: N120DL, cancelled Feb 28, 2018

A list on [N120DL, cancelled Feb 28, 2018](https://openairdocs.org/deregistered/N120DL-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 DALAFAR145SDR103](https://openairdocs.org/sdr/DALAFAR145SDR103.md): Floorbeam · corroded · Nov 5, 2010 · N120DL · Boeing 767332 · Fuselage Main, Floor Beam
  > FOUND CORROSION ON FLOORBEAM UPPER CAP AT FS 325 RBL 30 TO RBL 51. CONDITION FOUND DURING FLOOR COVERING REPLACEMENT. REF DAL NON-ROUTINE CARD 336. REPAIRED PER SRM 53-00-51 FIG 201. CLASSIFIED AS LEVEL 2 CORROSION.
- [SDR RYNA2010001020035](https://openairdocs.org/sdr/RYNA2010001020035.md): Oil System · low · Oct 7, 2010 · N120DL · Boeing 767332 · APU Oil System
  > THE RIGHT ENGINE IDG WAS PLACED ON MEL, DURING THE FLIGHT HAD TO RUN THE APU DUE TO MEL. DURING THE FLIGHT THE APU LOW OIL QTY MESSAGE CAME ON. THE CREW HAD TO DIVERT THE AIRCRAFT TO PIK. MX REPAIRED THE RIGHT ENGINE IDG BY CLEANING THE CONNECTOR TO THE ID
- [SDR RYNA2010008020026](https://openairdocs.org/sdr/RYNA2010008020026.md): Fmc · malfunctioned · Aug 20, 2010 · N120DL · Boeing 767332 · Flight Management Computing Hardware System
  > ON CLIMBOUT RECEIVED EICAS MESSAGE "L" FAILED. SELECTED ALTERNATE OF FMC INST SIYRCE SEKECTIR & R. AUTOPILOT CMO. PERFORMED FIM 34-61-00 F16180A 1-3423. PERFORMED FIM 34-61-00 F16 111 STEPS 1, 50, 6 & 110. REMOVED AND REPLACED LT. ROBBED FMC FROM AC N123
- [SDR RYNA2010007020023](https://openairdocs.org/sdr/RYNA2010007020023.md): Indication Sys · malfunctioned · Jul 22, 2010 · N120DL · Boeing 767332 · Aileron Control System
  > WHILE PERFORMING CONTROL WHEEL SURFACE CHECKS, LEFT O/B AILERON SHOWED NO MOVEMENT ON LOWER EICAS SCREEN. SWAPPED RT & LT STAB TRIM/AILERON LOCKOUT MODULES FOR TROUBLESHOOTING. CHECKS GOOD PER FIM 27-09-00, NO HELP. SWAPPED BACK, BOTH CHECK GOOD. TRANSFERR
- [SDR RYNA200912080025](https://openairdocs.org/sdr/RYNA200912080025.md): Fmc · failed · Dec 6, 2009 · N120DL · Boeing 767322 · Flight Management Computing Hardware System
  > DURING CRUISE EICAS STATUS MESSAGE R FMC FAIL APPEARED WITH CORRESPONDING LOSS OF FIRST OFFICERS, FMC DISPLAY ALONG WITH THE FIRST OFFICERS LOSS OF MAP AND NAVIGATION DATA. REMOVED AND REPLACED THE FIRST OFFICERS FMC IAW AMM 34-61-01, OPS CHECK GOOD NO DEFECT
- [SDR RYNA200912070024](https://openairdocs.org/sdr/RYNA200912070024.md): Battery Pack · discharged · Dec 5, 2009 · N120DL · Boeing 767332 · Emergency Lighting
  > ON 12/05/2009, ON AIRCRAFT 120DL, INSPECTION OF THE CABIN REVEALED THE EMERGENCY LIGHTS AT SEAT ROWS 17-28 WILL NOT STAY ILLUMINATED FOR VERY LONG DURING THE REQUIRED EMERGENCY LIGHT TEST. REMOVED AND REPLACED THE M732 EMERGENCY LIGHT BATTERY PACK PER AMM 31-
- [SDR RYNA200908170015](https://openairdocs.org/sdr/RYNA200908170015.md): Selector Valve · leaking · Aug 15, 2009 · N120DL · Boeing 767332 · Landing Gear Brake System
  > DURING CRUISE HYDRAULIC FLUID APPEARED TO BE MIGRATING FROM THE RT SYSTEM TO THE CENTER DIVERTED TO SUITABLE AIRPORT READINGS UPON LANDING INDICATED.45 CENTER AND 1.38 IN RT SYSTEM. REMOVED AND REPLACED THE ALTERNATE BRAKE SELECTOR VALVE IAW AMM 32-41-04 LEA
- [SDR RYNA200908110013](https://openairdocs.org/sdr/RYNA200908110013.md): Door Frame · cracked · Aug 4, 2009 · N120DL · Boeing 767332 · Fuselage Main, Structure
  > WHILE PERFORMING MAINTENANCE ON AIRCRAFT 120DL DURING THE INSPECTION PROCESS A DENT AND CRACK ON THE C2 CARGO DOOR OPENING FRAME WEB AT FS 1270 WL 162.5. THE CRACKS MEASURE APPROXIMATELY 1 INCH UP/DOWN BY 1.4 IB/OB. REPAIRED WEB AND OUTER CORD, C-2 DOOR OPEN
- [SDR RYNA20090811014](https://openairdocs.org/sdr/RYNA20090811014.md): Structure · corroded · Jul 31, 2009 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > WHILE PERFORMING MAINTENANCE ON AIRCRAFT 120DL DURING THE INSPECTION PROCESS CORROSION DAMAGE WAS DISCOVERED BETWEEN FS 632 TO FS 654 ALONG STRINGERS 35L TO 36L. THE DAMAGE IS LOCATED AT THE MID-GALLEY DRAIN MAST ATTACH POINT. REMOVED A 3 INCH SECTION STRING
- [SDR RYNA200908040010](https://openairdocs.org/sdr/RYNA200908040010.md): Battery Pack · discharged · Jul 24, 2009 · N120DL · Boeing 767332 · Emergency Lighting
  > DURING ACCOMPLISHMENT OF TASK-CARD 767-33-033-01 EMERGENCY LIGHT POWER SUPPLIES ON C-CHECK 1C/2C/S1C/S2C ALL BATTERY PACKS FAILED THE CAPACITY CHECK AND RT EXTERIOR LIGHTS ABOVE THE R-4 DOOR AND BOTH AFT WING SLIDE LIGHT FAILED TO ILLUMINATE. REMOVED AND REPL
- [SDR RYNA200908040011](https://openairdocs.org/sdr/RYNA200908040011.md): Cable Assy · out of rig · Jul 16, 2009 · N120DL · Boeing 767332 · Escape Slide
  > DURING INSPECTION OF EMERGENCY ESCAPE SYSTEM ON C-CHECK 1C/2C/S1C/S2C BOTH THE LT AND RT OFF-WING SLIDE BOTTLE INFLATION CABLES WERE FOUND OUT OF RIG. INSTALLED CABLES IN CORRECT POSITIONS PER CMM 25-61-24, OPS CHECK GOOD.
- [SDR RYN2008F00003](https://openairdocs.org/sdr/RYN2008F00003.md): Slide · unwanted deploy · Jun 30, 2008 · N120DL · Boeing 767332 · Escape Slide
  > FLIGHT ATTENDANT DEPLOYED L2 PASSENGER ENTRY DOOR SLIDE. ACFT MADE A FERRY FLIGHT KWI TO BAH FOR DOOR SLIDE REPLACEMENT. INSTALLED SERVICEABLE L2 DOOR SLIDE IAW AMM 28-66-08. (A)
- [SDR DL76S060889](https://openairdocs.org/sdr/DL76S060889.md): Bulkhead · cracked · Oct 16, 2006 · N120DL · Boeing 767332 · Fuselage Main, Bulkhead
  > THE NLG BULKHEAD AFT WEB AND CHORD AT STA. 287, RBL 25 HAS DRILL DAMAGE TO THE WEB AND CHORD AND THE CHORD WAS STOP DRILLED INSTEAD OF CUT OUT AS REQUIRED PER THE SRM. THE EXISTING REPAIR ANGLE WAS REMOVED AND THE CRACKED CHORD WAS CUT OUT. THE DRILL DAMAGED
- [SDR DL76S060839](https://openairdocs.org/sdr/DL76S060839.md): Spar · cracked · Oct 11, 2006 · N120DL · Boeing 767332 · Wing Spar
  > CRACK WAS FOUND IN LOWER OB FASTENER HOLE IN REAR SPAR. THE CRACK WAS REMOVED BY OVERSIZING HOLE AND INSTALLATION OF A FLANGED BUSHING IAW MFG INSTRUCTIONS. REPAIR ERA 455471-14.
- [SDR DL76S060838](https://openairdocs.org/sdr/DL76S060838.md): Web · damaged · Oct 11, 2006 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > WEB AT STA 654+121, LBL 40 WAS FOUND DAMAGED, CARGO COMPARTMENT JUST BELOW INNER CHORD. REPAIR WILL INVOLVE CUTTING THE WEB, SPLICING IAW INSTRUCTIONS. REPAIRED IAW ERA 455777-14.
- [SDR DL76S060834](https://openairdocs.org/sdr/DL76S060834.md): Skin · corroded · Oct 10, 2006 · N120DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > DURING ROUTINE MTC CORROSION AND MINOR CRACKS WERE FOUND IN FUSELAGE SKIN AT 789.5 AND S-38L. SKIN WAS TRIMMED, DOUBLER AND TRIPLER INSTALLED IAW 455466-14 IAW MFG INSTRUCTIONS.
- [SDR DL76S060716](https://openairdocs.org/sdr/DL76S060716.md): Fitting · corroded · Aug 29, 2006 · N120DL · Boeing 767332 · Wing, Landing Gear Attach Fittings
  > THE LT MLG ATTACH FITTING DRAG BRACE BORE IS CORRODED. THE BORE WAS OVERSIZED TO REMOVE THE CORROSION.
- [SDR DL76S060715](https://openairdocs.org/sdr/DL76S060715.md): Fitting · corroded · Aug 29, 2006 · N120DL · Boeing 767332 · Wing, Landing Gear Attach Fittings
  > THE RT MLG DRAG BRACE FITTING HAD CORROSION IN THE BORE. THE CORROSION WAS REMOVED BY OVERSIZING THE BORE.
- [SDR DL76S060423](https://openairdocs.org/sdr/DL76S060423.md): Frame · cracked · May 24, 2006 · N120DL · Boeing 767332 · Fuselage Main, Frame
  > CRACKS WERE FOUND IN THE INNER CHORD OF THE BS 903.5 LT AND RT FRAMES. THE CRACK WAS TRIMMED OUT AND A REPAIR ANGLE WAS INSTALLED REF AD 2003-18-10.
- [SDR DL76S050474](https://openairdocs.org/sdr/DL76S050474.md): Battery · inoperative · Aug 22, 2005 · N120DL · Boeing 767332 · Emergency Equipment
  > 1L DOOR FLASHLIGHT WON`T TEST. REPLACED BATTERY.
- [SDR DL76S050473](https://openairdocs.org/sdr/DL76S050473.md): Smoke Detector · inoperative · Aug 22, 2005 · N120DL · Boeing 767332 · Smoke Detection
  > MID LEFT SMOKE DETECTOR WOULD NOT SILENCE. REPLACED SMOKE DETECTOR.
- [SDR DL76S040581](https://openairdocs.org/sdr/DL76S040581.md): Rod · broken · Jun 20, 2004 · N120DL · Boeing 767332 · Landing Gear Actuator
  > ON TAKEOFF HAD GEAR DISAGREE LIGHT ON EICAS WITH WARNING, GEAR HANDLE UP. LEFT MAIN GEAR INDICATED DOWN WITH DOORS LIGHT ON AND GEAR LIGHT ON. PUT GEAR DOWN AND ALL GEAR INDICATED SAFE. RETURNED TO ATLANTA. FOUND SIDE BRACE ACTUATOR RETRACT ROD BROKEN. RE
- [SDR DL76S040185](https://openairdocs.org/sdr/DL76S040185.md): Filter · dirty · Feb 20, 2004 · N120DL · Boeing 767332 · Buffet/Galleys
  > FLIGHT ATT REPORTS THAT FIRST CLASS GALLEY CHILLER HAS OVERHEATED. ALSO REPORTED AN ELECTIRICAL ODOR THAT APPEARED TO ORIGINATE NEAR THE TRASH BIN. INSPECTED FREEZER ASSY, COULD NOT SMELL ANY ELECTRIC ODOR, FOUND FREEZER FILTER EXTREMELY CLOGGED. CLEANED FI
- [SDR DL76S030132](https://openairdocs.org/sdr/DL76S030132.md): Frame · cracked · Feb 6, 2003 · N120DL · Boeing 767332 · Fuselage Main, Frame
  > INSPECTION OF THE FS 1809.5 BULKHEAD OUTER FRAMES PER BAC S/B 767-53-0078 AND AD 2001-09-13 REVEALED A CRACK IN THE FWD FRAME AND THE AFT FRAME ON THE RT SIDE NEAR STRINGER 12. THE FWD FRAME WAS REPLACED PER THE S/B. THE AFT FRAME WAS REMOVED AND REPLACED WI
- [SDR DL76S011656](https://openairdocs.org/sdr/DL76S011656.md): Skin · worn · Oct 11, 2001 · N120DL · Boeing 767332 · Wing, Plate/Skin
  > DURING ACCOMPLISHMENT OF SIP MOD ON THE NR 2 PYLON WEAR DAMAGE FROM A HYDRAULIC LINE CLAMP SCREW WAS FOUND ON THE LOWER WING SKIN. THE DAMAGE IS LOCATED AT APPROX WS 420 AND IS BETWEEN WING STRINGERS L7 AND L8. THE WORN AREA WAS APPROXIMATELY.11 INCH IN DEP
- [SDR DL76S011650](https://openairdocs.org/sdr/DL76S011650.md): Bulkhead · cracked · Oct 11, 2001 · N120DL · Boeing 767332 · Nacelle/Pylon, Bulkhead/Firewall
  > DURING ACCOMPLISHMENT OF PYLON SIP MOD, CRACK INDICATIONS WERE FOUND IN THE MID STRUT BULKHEAD LAYER. REPAIR ER/A 398051-14AD.
- [SDR DL76S010953](https://openairdocs.org/sdr/DL76S010953.md): Unknown · odor · Jun 12, 2001 · N120DL · Boeing 767332 · Air Distribution System
  > AT FL 410 TERRAIN SYSTEM STARTED WARNING OF TERRAIN, NOTICED ODOR OF MELTING PLASTIC. CK UNDER O-CARE SHIELD WIRING OR ODOR FOUND FIBERGLASS ON F/O ALT. REPOSITION, OK. DROPPED O/H PNL, ALL NORMAL. DROPPED C/B BOS NORMAL. CK E/E BUNDLES P51 PNL AREA NORMA
- [SDR DL76S002287](https://openairdocs.org/sdr/DL76S002287.md): Skin · punctured · Nov 19, 2000 · N120DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > FUSELAGE / SKIN / FS 390-412 / STRG. 33R-34R: PUNCTURE REPAIR. THE FUSELAGE SKIN WAS PUNCTURED BY GROUND EQUIPMENT BETWENN FS 390 & 412 AND BETWEEN STRINGERS 33R & 34R. THE DAMAGE WAS REMOVED WITH A 12 INCH X 7 INCH SKIN CUTOUT. THE CUTOUT WAS REPAIRE
- [SDR DL76S992807](https://openairdocs.org/sdr/DL76S992807.md): Frame · dented · Dec 16, 1999 · N120DL · Boeing 767332 · Fuselage Main, Frame
  > EXISTING REPAIR REMOVED AT C-1 DOORWAY AFT EDGE. REVEALING DAMAGE TO SKIN BEARSTRAP AND FRAME OUTER CHORD. DAMAGE LOCATED BETWEEN STR-31R AND 32R AT STA 615. SKIN AND BEARSTRAP WERE GOUGED, CUTOUT AND THE FRAME WAS DENTED. ER/A 333883-14 REV A.
- [SDR DL76S992775](https://openairdocs.org/sdr/DL76S992775.md): Frame · corroded · Dec 6, 1999 · N120DL · Boeing 767332 · Fuselage Main, Frame
  > FS 1562 FRAME FAIL-SAFE CHORD WAS FOUND CORRODED BETWEEN STR 38L AND STR 38R. THE (P/N 146T1223-30) CHORD WAS REPLACED PER DWG 146T1223.
- [SDR DL76S992777](https://openairdocs.org/sdr/DL76S992777.md): Shear Tie · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > THE FUSELAGE TO FRAME SHEAR TIE AT STA 1562 LOCATED ON THE FWD SIDE OF THE FRAME BETWEEN STR 38L AND 38R WAS FOUND CORRODED. THE (P/N 150T2102-656) SHEAR TIE WAS REPLACED PER DWG 146T1223.
- [SDR DL76S992776](https://openairdocs.org/sdr/DL76S992776.md): Shear Tie · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > THE FUSELAGE SKIN TO FRAME SHEAR TIE LOCATED ON THE AFT SIDE OF FRAME STA 1562 WAS FOUND CORRODED. THE (P/N 140T2102-23) SHEAR TIE WAS REPLACED PER DWG 146T1223. THE SHEAR TIE IS LOCATED BETWEEN STR 38L AND STR 38R.
- [SDR DL76S992774](https://openairdocs.org/sdr/DL76S992774.md): Splice · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > STRINGER 37R SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992773](https://openairdocs.org/sdr/DL76S992773.md): Splice · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > STRINGER 34L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992772](https://openairdocs.org/sdr/DL76S992772.md): Splice · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > STRINGER 37L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992771](https://openairdocs.org/sdr/DL76S992771.md): Splice · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > STRINGER 38L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE TO THE STRINGER WAS FOUND.
- [SDR DL76S992770](https://openairdocs.org/sdr/DL76S992770.md): Splice · corroded · Dec 1, 1999 · N120DL · Boeing 767332 · Fuselage Miscellaneous Structure
  > STRINGER 39L SPLICE WAS FOUND CORRODED AT FS 434. THE (P/N 140T0115-16) SPLICE WAS REPLACED PER SRM 51-10-00. NO DAMAGE WAS FOUND ON THE STRINGER.
- [SDR DL76S980522](https://openairdocs.org/sdr/DL76S980522.md): Bulb · failed · Feb 13, 1998 · N120DL · Boeing 767332 · Exterior Lighting
  > EXTERIOR EMERG LIGHT AFT OF WING INOP, LEFT SIDE. RELAMPED, CK GOOD.
- [SDR DL76S972111](https://openairdocs.org/sdr/DL76S972111.md): Skin · corrosion · Oct 10, 1997 · N120DL · Boeing 767332 · Fuselage Main, Plate/Skin
  > DURING ACCOMPLISHMENT OF EO 1-60000-3, CORROSION WAS FOUND DIRECTLY UNDER THE DRAIN SCREEN LOCATED AT APPROXIMATELY LBL 70. THE RESULTING BLENDS, WITH A MAXIMUM DEPTH OF.155, ARE SHOWN ON FIGURE 1. TO FACILITATE INSTALLATION OF A REPAIR DOUBLER UNDER THE LB
- [SDR DL76S971922](https://openairdocs.org/sdr/DL76S971922.md): Floorbeam · cracked · Sep 18, 1997 · N120DL · Boeing 767332 · Fuselage Main, Floor Beam
  > THE FUSELAGE SEAT TRACKS LOCATED AT RBL 33, LBL 54, AND RBL 54 WERE FOUND CRACKED IN THE VERTICAL WEB OF THE UPPER CHORD AT APPROXIMATELY FS 786 AS DESCRIBED IN BOEING SB 767-57-0029. THE VERTICAL WEB IS M/F FROM.063 THK 2024-T3 AL MATERIAL. IN ADDITION, TO
- [SDR DL76S971264](https://openairdocs.org/sdr/DL76S971264.md): Bulb · shorted · Jun 29, 1997 · N120DL · Boeing 767332 · Passenger Compartment Lighting
  > DURING CRUISE 37000 FT 1 HR INTO FLT, SMELLED ELECTRICAL SMELL. SHUT OFF UTILITY BUSSES PULLED C/BS U6 U33. F/A REPORTED, WORSE IN LT HAND F/C TURNED OFF LT PACK WHEN PAX IN 14A. REPORTED PUFF OF SMOKE FROM LT FLOOR BOARD GRAY IN COLOR. RECEIVED PRIORITY H
- [SDR DL76S971108](https://openairdocs.org/sdr/DL76S971108.md): Valve · inoperative · Jun 9, 1997 · N120DL · Boeing 767332 · Hydraulic System, Main
  > NOSE GEAR DID NOT RETRACT ON T/O, DURING GEAR RETRACTION A/C SHUDDERED, CENTER HYD SYS EICAS MSG CAME ON, CENTER HYD PUMP LOW PRESS LTS CAME ON. DEMAND PUMP LOW PRESS LTS CAME ON WHEN GEAR HANDLE WAS PLACED IN DOWN POSITION. CENTER HYD SYS RETURNED TO NORMAL
- [SDR DL76S961254](https://openairdocs.org/sdr/DL76S961254.md): Engine · malfunctioned · May 22, 1996 · N120DL · Boeing 767332 · Engine (Turbine/Turboprop)
  > RT ENG FLAME-OUT JUST AFTER ROTATION. ALL INDICATIONS NORMAL AT LIFTOFF, THEN FLAME-OUT OCCURRED. REPLACED LEAKING FUEL MANIFOLD LINE AND LEAKING FUEL NOZZLE, LEAK CHECK AND ENGINE RUN OK.
- [SDR DL76S960908](https://openairdocs.org/sdr/DL76S960908.md): Te Wedge · delamination · Apr 2, 1996 · N120DL · Boeing 767332 · Leading Edge Devices
  > THE NR 5 LEADING EDGE SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROX 3 INCH BY 3 INCH AND IS LOCATED AT THE INBOARD AFT END OF THE TRAILING EDGE. ACCOMPLISHED REPAIRS PER DL ERA 273577-14AD.
- [SDR DL76S960106](https://openairdocs.org/sdr/DL76S960106.md): Line · cracked · Jan 15, 1996 · N120DL · Boeing 767332 · Hydraulic System, Main
  > ON APPROACH TO ATL, HAD SMOKE OR BURNING ODOR IN AFT AND MID CABIN. FOUND SLAT PRESSURE HYD LINE CRACKED AT WING ROOT FUSELAGE FITTING. REPLACED HYD LINE, NO LEAKS NOTED. REPLACED PRECOOLER FILTERS DUE TO SKYDROL CONTAMINATION.
- [SDR DL76S954237](https://openairdocs.org/sdr/DL76S954237.md): Eel · inoperative · Nov 3, 1995 · N120DL · Boeing 767332 · Emergency Lighting
  > LEFT WING LWR AFT EMERGENCY LIGHT INOP. RELAMPED, CKS OK.
- [SDR DL76S953919](https://openairdocs.org/sdr/DL76S953919.md): Eel Lamp · failed · Oct 3, 1995 · N120DL · Boeing 767332 · Emergency Lighting
  > RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. LOCATED AFT OF R2 ENTRANCE DOOR. RELAMPED, CHECKS GOOD.
- [SDR DL76S952463](https://openairdocs.org/sdr/DL76S952463.md): Pneumatic Sys · contaminated · Jun 3, 1995 · N120DL · Boeing 767332 · Pneumatic Distribution System
  > ON TAKEOFF AND CLIMB, HAD SMOKE ODOR AND FUMES IN MID GALLEY LAV AREA, RETURNED FLT TO ATL. FOUND COMPRESSOR WASH FLUID CONTAMINATION IN NR 2 ENGINE INLET. RAN ENGINE UNTIL ODOR WAS GONE, RETURNED TO SERVICE.
- [SDR DL76S952238](https://openairdocs.org/sdr/DL76S952238.md): Hose · leaking · May 19, 1995 · N120DL · Boeing 767332 · Landing Gear Retraction/Extension System
  > AFTER TAKEOFF, RT MAIN LANDING GEAR WOULD NOT RETRACT, RETURNED MCO. FOUND RT MLG TRUCK TILT PRESSURE LINE BROKEN. REPLACED LINE OPERATION NORMAL.

## 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 = 'N120DL' AND deregistration_id = 'N120DL-2018-02-28'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N120DL-2018-02-28/reports

---
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