# Service difficulty reports: N122DL, cancelled Dec 3, 2009 A list on [N122DL, cancelled Dec 3, 2009](https://openairdocs.org/deregistered/N122DL-2009-12-03.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR DL76S071307](https://openairdocs.org/sdr/DL76S071307.md): Warning Light · illuminated · Oct 7, 2007 · N122DL · Boeing 767332 · Central Warning > DURING T/O ROLL, RT ENG FUEL FILTER ADVISORY STATUS MSG INDICATED. OCCURRED APPROX 100-110 KNTS T/S PER FIM. REMOVED FUEL FILTER ELEMENT INSP FOR DEBRIS, NONE FOUND. INSTALLED NEW FILTER ELEMENT PER MM. RAN ENG, OPS CHECK AND LEAK CHECK OK. - [SDR DL76S060844](https://openairdocs.org/sdr/DL76S060844.md): Skin · corroded · Oct 13, 2006 · N122DL · Boeing 767332 · Fuselage Main, Plate/Skin > CORROSION WAS FOUND IN THE SKIN AROUND THE RHS DME ANTENNA CABLE. CORROSION WAS BLENDED AND A BOEING APPROVED REPAIR INSTALLED PER ERA 456420-14. - [SDR DL76S060843](https://openairdocs.org/sdr/DL76S060843.md): Floorbeam · cracked · Oct 13, 2006 · N122DL · Boeing 767332 · Fuselage Main, Floor Beam > UPPER CHORD OF THE STA 999 AT LBL 33 FLOORBEAM WAS FOUND CRACKED IN THE VERTICAL FLANGE FROM THE AFT SLOTTED CUTOUT TO THE END OF THE CHORD. THE CRACK WAS REMOVED BY EXTENDING THE SLOT CUTOUT TO THE END OF THE CHORD AND WAS REPAIRED WITH A REPAIR ANGLE APPRO - [SDR DL76S060846](https://openairdocs.org/sdr/DL76S060846.md): Skin · gouged · Oct 10, 2006 · N122DL · Boeing 767332 · Fuselage Main, Plate/Skin > GOUGES WERE FOUND IN THE FUSELAGE SKIN PANEL IN THE VICINITY OF AN EXISTING REPAIR. EXISTING REPAIR REMOVED AND ONE LARGE EXTERNAL REPAIR DOUBLER INSTALLED PER BOEING INSTRUCTIONS ERA 456554-14. - [SDR DL76S060633](https://openairdocs.org/sdr/DL76S060633.md): Coffeemaker · odor · Aug 6, 2006 · N122DL · Boeing 767332 · Buffet/Galleys > FLT ATTENDANT SMELLED BURNT PLASTIC IN AFT GALLEY FROM A CEILING PANEL IN PROX OF COFFEEMAKERS. NO HEAT FELT ON PANEL, F/A TURNED OFF ALL COFFEEMAKERS AND PULLED A FEW C/BS AND SMELL DISSIPATED. OPERATED ALL APPLIANCES AND LIGHTS. NO IRREG NOTED. - [SDR DL76S060603](https://openairdocs.org/sdr/DL76S060603.md): Fitting · cracked · Jul 21, 2006 · N122DL · Boeing 767332 · Nacelle/Pylon, Attach Fittings > THE NR 2 PYLON OUTBOARD PITCH LOAD FITTING WAS FOUND CRACKED. THE CRACKED HOLE WAS OVERSIZED TO REMOVE THE DAMAGE AND AN OVERSIZED FASTENER WAS INSTALLED REF AD 2004-16-12. - [SDR DL76S060601](https://openairdocs.org/sdr/DL76S060601.md): Fitting · damaged · Jul 18, 2006 · N122DL · Boeing 767332 · Nacelle/Pylon, Main Frame > DURING MODIFICATION OF THE PYLON MIDSPAR FITTING, TWO HOLES WERE DAMAGED DURING FASTENER REMOVAL. THE HOLES WERE OVERSIZED TO REMOVE THE DAMAGE AND OVERSIZED FASTENERS WERE INSTALLED. REF AD2004-16-12. - [SDR DL76S060586](https://openairdocs.org/sdr/DL76S060586.md): Fitting · damaged · Jul 13, 2006 · N122DL · Boeing 767332 · Nacelle/Pylon, Attach Fittings > DURING ACCOMPLISHMENT OF S/B 767-54-0081, THE SIDE LINK FITTING WAS SPOTFACED IN THE WRONG LOCATION. A FILLER WAS INSTALLED IN THE SPOTFACED AREA. - [SDR DL76S060585](https://openairdocs.org/sdr/DL76S060585.md): Frame · cracked · Jul 13, 2006 · N122DL · Boeing 767332 · Fuselage Main, Frame > THE LT BS 903.5 FRAME HAS A CRACK IN THE LOWER END BETWEEN CHORD FLANGES. THE CRACKED AREA WAS REMOVED AND A REPAIR ANGLE WAS INSTALLED. - [SDR DL76S060584](https://openairdocs.org/sdr/DL76S060584.md): Fitting · cracked · Jul 13, 2006 · N122DL · Boeing 767332 · Nacelle/Pylon, Plate/Skin > THE FORWARD UPPER SPAR FITTINGS ARE CRACKED AT A FASTENER HOLE. THE HOLES WERE OVERSIZED TO REMOVE THE CRACK AND BUSHINGS WERE INSTALLED. - [SDR DL76S050543](https://openairdocs.org/sdr/DL76S050543.md): Engine · leaking · Sep 13, 2005 · N122DL · Boeing 767332 · Turbine Engine Oil System > ODOR DETECTED AND SEVERAL SMOKE DETECTORS WENT OFF. ODOR DISSIPATED WITH UTILITY BUSSES OFF, BUT RETURNED WHEN POWER LEVERS ADVANCED. OIL LEAK NR 1 ENGINE. REPLACED NR 1 BEARING MANIFOLD PKNGS, PERF SAME INSPECTION ON NR 2 ENGINE CKS OK. RAN AT HIGH PWR WI - [SDR DL76S040472](https://openairdocs.org/sdr/DL76S040472.md): Ecu · malfunctioned · May 27, 2004 · N122DL · Boeing 767332 · APU Start/Ignition System > MCO - APU STARTER CONTINUOUSLY POWERED CAUSING OVERHEATING AND SMELL IN APU AIR. REPLACED ECU AND K117 CONTACTOR. - [SDR DL76S040301](https://openairdocs.org/sdr/DL76S040301.md): Odor · detected · Apr 3, 2004 · N122DL · Boeing 767332 · Entertainment System > ELECTRICAL SMOKE ODOR FROM VIDEO EQUIP RACK, WHEN SHUT OFF SMOKE DISSIPATED. RAN VCP 1 AND VCP 2 FOR 15 MINUTES EACH, NO SMOKE ODOR NOTICED. REMOVED VCP 1 AND VCP 2 AND FOUND NO EVIDENCE OF SMOKE. REINSTALLED VCP 1 AND VCP 2, RAN GASPER AND RECIRC FANS. NO - [SDR DL76S030756](https://openairdocs.org/sdr/DL76S030756.md): Support Beam · corroded · Aug 13, 2003 · N122DL · Boeing 767332 · Trailing Edge Flaps > CORROSION WAS FOUND IN THE HOLE BORES OF 4 ATTACH FASTENERS ON THE 9-10 BEAM ASSEMBLY FOR THE OUTBOARD SUPPORT OF THE INBD FLAP ATTACH ASSEMBLY. THE HOLES WERE OVERSIZED TO REMOVE CORROSION, HFEC INSPECTED, AND REPAIR BUSHINGS INSTALLED TO RESTORE THE HOLE SI - [SDR DL76S030547](https://openairdocs.org/sdr/DL76S030547.md): Lens · broken · Jun 13, 2003 · N122DL · Boeing 767332 · Emergency Lighting > ONE WHITE EMERGENCY LIGHT IS BROKEN ON SEAT 2B. REPLACED LENS AND SHROUD. - [SDR DL76S020783](https://openairdocs.org/sdr/DL76S020783.md): Fan · damaged · Jul 7, 2002 · N122DL · Boeing 767332 · Air Distribution Fan > ON APPROACH, BURNING SMELL IN COCKPIT ALL THE WAY BACK TO ROW 4. SMELL DISSIPATED WITHIN 2 MINUTES. ISOLATED PROBLEM TO LEFT RECIRC FAN. FOUND FAN DAMAGED BY DEBRIS. REMOVED AND REPLACED LT RECIRC FAN. - [SDR DL76S011789](https://openairdocs.org/sdr/DL76S011789.md): Engine · damaged · Nov 12, 2001 · N122DL · Boeing 767332 · Turbine Engine Compressor Section > CLIMBING THRU 19000FT, LOUD BANG ON THE RIGHT SIDE. TEMP ONNO 2 ENG WENT TO 959 DEG. PULLED ENG TO IDLE. SUBSEQUENT ENG OIL EICAS MSG. SHUT DOWN ENG. ON ARRIVAL AT GATE, MTC FOUND OIL DRAINING FROM COWL, METAL IN TAIL PIPE AND FAN DIFFICULT TO TURN. - [SDR DL76S010414](https://openairdocs.org/sdr/DL76S010414.md): Skin · cracked · Mar 12, 2001 · N122DL · Boeing 767332 · Fuselage Main, Plate/Skin > THE FUSELAGE SKIN WAS FOUND WITH A 9.5 INCH CRACK ADJACENT TO THE LOWER AFT VHF ANTENNA AT FS 1197+95 BETWEEN STRINGERS 39L & 39R. THE CRACK WAS REMOVED WITH A CUTOUT AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380276-14, REV A. - [SDR DL76S000210](https://openairdocs.org/sdr/DL76S000210.md): Skin · punctured · Jan 25, 2000 · N122DL · Boeing 767332 · Fuselage Main, Plate/Skin > FUSELAGE SKIN PUNCTURE DISCOVERED AT STA 1443 (GROUND DAMAGE DURING HMV) AND STR 37R. ADDITIONALLY THE STRINGER WAS DENTED. ER/A 334052-14 REV A. - [SDR DL76S990604](https://openairdocs.org/sdr/DL76S990604.md): Light · inoperative · Mar 21, 1999 · N122DL · Boeing 767332 · Emergency Lighting > ON L/O, FOUND SEAT 41F EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED LIGHT ASSY. - [SDR DL76S982582](https://openairdocs.org/sdr/DL76S982582.md): Hose · ruptured · Dec 17, 1998 · N122DL · Boeing 767332 · Stabilizer Control System > CENTER HYD QUANITY LIGHT CAME ON. QTY INDICATED.47 ON DOWN WIND WHEN LIGHT CAME ON. FOUND HYD LINE PN AS115-04K0146 RUPTURED ON STAB TRIM CONTROL MODULE. IPC LOCATION 27-41-65-01 ITEM 220. INSTALLED TEMP REPAIR HYD LINE. - [SDR DL76S982184](https://openairdocs.org/sdr/DL76S982184.md): Skin · torn · Oct 20, 1998 · N122DL · Boeing 767332 · Fuselage Main, Plate/Skin > FUSELAGE SKIN, FS 1439 STRG 36L-39L: GROUND DAMAGE REPAIR. THE FUSELAGE SKIN AT FS 1439 BETWEEN STRINGERS 36L AND 39L WAS DENTED OR TORN DUE TO CONTACT WITH GROUND EQUIPMENT. THE DAMAGED SKIN WAS CUTOUT OVER A 17 BY 7 AREA. THE CUTOUT WAS REPAIRED WITH - [SDR DL76S962187](https://openairdocs.org/sdr/DL76S962187.md): Hose · leaking · Sep 27, 1996 · N122DL · Boeing 767332 · Hydraulic System, Main > AFTER T/O UPON GEAR RETRACTION, GOT GEAR DOOR MSG AND GEAR DISAGREE MSG ON EICAS. LT MAIN GEAR GREEN LIGHT REMAINED ILLUMINATED. FOUND UP PRESSURE LINE TO LT GEAR TRUCK POSITIONER ACTUATOR LEAKING. REPLACED SAME. - [SDR DL76S962146](https://openairdocs.org/sdr/DL76S962146.md): Bulb · failed · Sep 20, 1996 · N122DL · Boeing 767332 · Emergency Lighting > ON FAA INSP FOUND EMERGENCY FLOOR TRACK WHITE LIGHT OUT, SEAT 45FG. - [SDR DL76S953488](https://openairdocs.org/sdr/DL76S953488.md): Eel Bulb · failed · Aug 24, 1995 · N122DL · Boeing 767332 · Emergency Lighting > FOUND RT OVERWING EMERGENCY ESCAPE LIGHT INOP. RELAMPED, OPERATION NORMAL. - [SDR DL76S951575](https://openairdocs.org/sdr/DL76S951575.md): Te Wedge · delamination · Apr 7, 1995 · N122DL · Boeing 767332 · Leading Edge Devices > DURING LTR CHECK, THE NR 1 L/E SLAT TRAILING EDGE WEDGE WAS FOUND TO HAVE THE UPPER SKIN DELAMINATED. THE DELAMINATED AREA IS APPROXIMATELY 5 INCHES IN DIAMETER AND IS LOCATED 75 INCHES FROM THE INBOARD END AND 2 INCHES FROM THE TRAILING EDGE. REPAIRED PER D - [SDR DL76S951429](https://openairdocs.org/sdr/DL76S951429.md): Skin · puncture · Apr 6, 1995 · N122DL · Boeing 767332 · Trailing Edge Flaps > FOUND DURING LETTER CHECK INSP, DENT AND PUNCTURE ON UNDERSIDE OF OUTBOARD AFT FLAP BEHIND NR 11 SPOILER R5T WING. REPAIRED PER SRM 57-53-01, PAINTED AREA. - [SDR DL76S951428](https://openairdocs.org/sdr/DL76S951428.md): Skin · dented · Apr 6, 1995 · N122DL · Boeing 767332 · Trailing Edge Flaps > FOUND DURING LETTER CHECK INSP, DENT ON UNDERSIDE OF OUTBOARD FLAP OUTBOARD END RT WING. REMOVED DAMAGED AREA AND STARTED REPAIR PER SRM 57-53-01, OK TO PAINT FINISHED REPAIR PER SRM 57-53-01 AND PAINTED AREA. ## 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 = 'N122DL' AND deregistration_id = 'N122DL-2009-12-03' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N122DL-2009-12-03/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.