# Service difficulty reports: N755DL, cancelled Sep 10, 2013

A list on [N755DL, cancelled Sep 10, 2013](https://openairdocs.org/deregistered/N755DL-2013-09-10.md).

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

- [SDR DLL19001775](https://openairdocs.org/sdr/DLL19001775.md): Latch · out of adj · Sep 14, 2000 · N755DL · Lkheed 10113853 · Cargo/Baggage Doors
  > ON LIFT OFF DOOR LIGHT ILLUMINATED, CHECKED S/O''S PANEL AND BOTH FWD AND AFT CARGO DOOR LIGHTS REMAINED ON. FOUND LOCK MECHANISM OUT OF ADJUSTMENT. RIGGED PER MM CHECKS OK.
- [SDR DLL19001220](https://openairdocs.org/sdr/DLL19001220.md): Wire · broken · Jun 27, 2000 · N755DL · Lkheed 10113853 · Light System Wiring
  > FOUND DURING LAYOVER THREE FOOT SECTION OF EMERGENCY TRACK LIGHTING AT LEFT SIDE OF MIDDLE GALLEY INOPERATIVE - REPAIRED BROKEN WIRE IN TRACK
- [SDR DLL19000949](https://openairdocs.org/sdr/DLL19000949.md): Light · malfunctioned · May 12, 2000 · N755DL · Lkheed 10113853 · Emergency Lighting
  > ON L/O, FOUND 2R EXTERIOR EMERGENCY LIGHT ON CONSTANTLY. REPLACED POWER SUPPLY.
- [SDR DLL19992546](https://openairdocs.org/sdr/DLL19992546.md): Unknown · odor · Nov 18, 1999 · N755DL · Lkheed 10113853 · Air Distribution System
  > NUMEROUS COMPLAINTS OF SMOKE ODOR IN CABIN. INSPECTED CABIN AND GALLEYS FOR FAULTS AND FOUND NONE. OPERATED AIR CONDITIONING SYSTEM FOR 30 MINUTES WITH NO FAULTS. UNABLE TO IDENTIFY SOURCE OF ODOR. ALL CHECKS NORMALLY.
- [SDR DLL19992131](https://openairdocs.org/sdr/DLL19992131.md): Control Cable · out of adj · Sep 23, 1999 · N755DL · Lkheed 10113853 · Landing Gear Position and Warning
  > MAIN LT GEAR DOOR LIGHT ON WITH DOOR INTRANS LIGHTS ON GEAR ANNUNICATOR. RAN POM CK LIST, CYCLED GEAR AUTOMATICALLY AND USING MECHANICAL RELEASE HANDLES, NO HELP. RETURN LAX. ADJUSTED LOWER PHASE INPUT CABLE PER MM 32-33-06. PERFORMED GEAR SWING, OPS CHECK
- [SDR DLL19992127](https://openairdocs.org/sdr/DLL19992127.md): Snubber · broken · Sep 22, 1999 · N755DL · Lkheed 10113853 · Main Landing Gear
  > ON ARRIVAL, LEFT MAIN LANDING GEAR DOOR HANGING DOWN. MTC FOUND LEFT MLG DOOR SNUBBER ROD BROKEN. REPLACED LEFT MLG DOOR SNUBBER ROD. DOOR OPS NORMAL.
- [SDR DLL19991434](https://openairdocs.org/sdr/DLL19991434.md): Stiffener · cracked · Jun 23, 1999 · N755DL · Lkheed 10113853 · Wing Spar
  > THE LBL 30 VERTICAL STIFFENER ON THE CENTER WING FRONT SPAR WAS FOUND CRACKED AT A LIGHTENING HOLE 12 FROM THE UPPER END OF THE STIFFENER. THE UPPER END OF THE STIFFENER WAS TRIMMED OFF AND A NEW SECTION SPLICED IN PER ER/A 367639-14, REV A.
- [SDR DLL19990983](https://openairdocs.org/sdr/DLL19990983.md): Regulator · failed · May 5, 1999 · N755DL · Lkheed 10113853 · Crew Oxygen System
  > CAPTS 02 MASK HAS CONTINUOUS FLOW IN ON POSITION ON REGULATOR PANEL. PANEL SWITCH MUST BE TURNED OFF TO CEASE FLOW. CREW 02 PRESSURE NOW AT 800 PSI. REPLACED CAPTS REGULATOR AND SERVICED CREW 02 BOTTLE, BOTH LEAK CHECK OK.
- [SDR DLL19982534](https://openairdocs.org/sdr/DLL19982534.md): Skin · cracked · Dec 9, 1998 · N755DL · Lkheed 10113853 · Wing, Plate/Skin
  > THE LT WING LOWER SKIN WAS FOUND WITH A 1.25 INCH LONG CRACK BETWEEN FASTENER HOLES AT THE END OF STRINGER 16 (OWS 130). THE CRACK WAS ROUTED OUT OF THE SKIN AND REPAIRED WITH AN ALUMINUM DOUBLER AND TRIPLER PER ER/A 366221-14, REV A.
- [SDR DLL19981299](https://openairdocs.org/sdr/DLL19981299.md): Vibration Light · illuminated · Jun 18, 1998 · N755DL · Lkheed 10113853 · Engine Vibration Analyzer
  > NR 3 VIBRATION LIGHT CAME ON. INDICATED APPROX 2.9 BOTH A AND B. ACCOMPANIED BY ENGINE VIBRATION. SHUT DOWN ENGINE VIAPOM. CRUISE AT 350. NO THROTTLE MOVEMENT AT TIME OF FAILURE. LUBED FAN BLADE CLAPPERS. CHECKED CHIP DETECTORS. INSPECTED ENGINE FOR LO
- [SDR DLL15980591](https://openairdocs.org/sdr/DLL15980591.md): Battery Pack · discharged · Mar 16, 1998 · N755DL · Lkheed 10113853 · Emergency Lighting
  > AFT CABIN EMERGENCY FLOOR LIGHTS INOP BOTH SIDES. REPLACED BATTERY PACK.
- [SDR DLL15980590](https://openairdocs.org/sdr/DLL15980590.md): Power Supply · inoperative · Mar 16, 1998 · N755DL · Lkheed 10113853 · Emergency Lighting
  > AFT CABIN FLOOR EMERGENCY LIGHTS ON BOTH SIDES INOP. REPLACED POWER SUPPLY.
- [SDR DLL15980589](https://openairdocs.org/sdr/DLL15980589.md): Battery Pack · discharged · Mar 16, 1998 · N755DL · Lkheed 10113853 · Emergency Lighting
  > BATTERY DISCHARGED RAPIDLY BY DEFECTIVE BATTERY CHARGER/ POWER SUPPLY. REPLACED BATTERY PACK.
- [SDR DLL15980587](https://openairdocs.org/sdr/DLL15980587.md): Power Supply · inoperative · Mar 16, 1998 · N755DL · Lkheed 10113853 · Emergency Lighting
  > BATTERY PACK WOULD NOT LIGHT CABIN OVERHEAD, AFT GALLEY OR OUTSIDE ESCAPE SLIDE LIGHTS DURING TEST.
- [SDR DLL15972698](https://openairdocs.org/sdr/DLL15972698.md): Rear Spar · cracked · Dec 19, 1997 · N755DL · Lkheed 10113853 · Wing Spar
  > THE LT AND RT REAR SPAR UPPER CAP TO WEB ATTACH HOLES WERE OVERSIZED BEYOND REPAIRABLE LIMITS TO REMOVE CRACKS. THE REAR SPARS WERE SUBSEQUENTLY MODIFIED BY REPLACING THE INBD WEB AND UPPER SPAR CAP PER LAC S/B 093-57-215. THE WORK WAS ACCOMPLISHED PER THE
- [SDR DLL15970461](https://openairdocs.org/sdr/DLL15970461.md): Skin · corrosion · Mar 7, 1997 · N755DL · Lkheed 10113853 · Fuselage Main, Plate/Skin
  > DURING INSPECTION, CORROSION WAS FOUND IN THE MATING SURFACE BETWEEN THE L3 DOOR TRIPLER PAD-UP LIP AND THE UPPER EDGE OF THE FUSELAGE SKIN. REMOVAL OF THE CORROSION RESULTED IN TWO TRIM-OUTS IN THE SKIN AND SEVERAL BLEND-OUTS IN THE FAIL SAFE TRIPLER. MAXIM
- [SDR DLL15970448](https://openairdocs.org/sdr/DLL15970448.md): Sill · corrosion · Mar 7, 1997 · N755DL · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > THE L-2 PASSENGER DOOR SURROUND LOWER SILL WAS FOUND WITH CORROSION ON ITS OUTER CAP AT STA 895. THE CORROSION WAS REMOVED FROM THE UPPER AND LOWER SURFACES OF THE INBD HORIZONTAL FLANGE LEAVING 0.097 INCH MINIMUM FLANGE THICKNESS. ER/A 361143-14 WAS ISSUED
- [SDR DLL15970449](https://openairdocs.org/sdr/DLL15970449.md): Rear Spar · cracked · Mar 5, 1997 · N755DL · Lkheed 10113853 · Wing Spar
  > DURING ACCOMPLISHMENT OF E.O. 7-59089-3, SEVERAL HOLES IN THE LT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE UPPER WING SKIN AND SPAR CAP AND TO THE SPAR WEB AND SPAR CAP. THE SUBJEC
- [SDR DLL15970415](https://openairdocs.org/sdr/DLL15970415.md): Pressure Deck · cracked · Mar 4, 1997 · N755DL · Lkheed 10113853 · Fuselage Miscellaneous Structure
  > THE FUSELAGE HORIZONTAL PRESSURE DECK PANEL WAS FOUND WITH A 1.75 INCH LONG CRACK. THE CRACK IS LOCATED AT RBL 102, JUST AFT OF FS 378, AND EXTENDS DIAGONALLY INBOARD AND AFT FROM THE FORWARD EDGE OF THE PANEL AT THE EXISTING FRAME CUTOUT. THE CRACK EXTENDS
- [SDR DLL15970414](https://openairdocs.org/sdr/DLL15970414.md): Spar Cap · cracked · Mar 4, 1997 · N755DL · Lkheed 10113853 · Wing Spar
  > DURING ACCOMPLISHEMENT OF EO 7-59089-3, SEVERAL HOLES IN THE RT WING REAR SPAR WERE FOUND CRACKED IN THE UPPER SPAR CAP BETWEEN IWS 293.58 AND IWS 346.109. THE HOLES ARE COMMON TO THE UPPER WING SKIN AND SPAR CAP AND TO THE SPAR WEB AND SPAR CAP. THE DAMAGE
- [SDR DLL15970413](https://openairdocs.org/sdr/DLL15970413.md): Bulkhead Panel · corrosion · Mar 4, 1997 · N755DL · Lkheed 10113853 · Fuselage Main, Bulkhead
  > THE AFT PRESSURE BULKHEAD LOWER GORE PANEL WAS FOUND CORRODED IN SEVERAL AREAS BETWEEN STRINGERS 31 AND 33. THE BONDED GORE DOUBLER WAS FOUND CORRODED BETWEEN STRINGERS 24 AND 33. THE DAMAGE WILL BE REPAIRED PER ER/A 304834-14 REVISION 'A'.
- [SDR DLL15970412](https://openairdocs.org/sdr/DLL15970412.md): Skin · corrosion · Mar 4, 1997 · N755DL · Lkheed 10113853 · Wing, Plate/Skin
  > DURING ROUTINE FLOOR PANEL OPEN-UP AT HMV, THE UPPER SURFACE OF THE CENTER WING SKIN BETWEEN RBL AND LBL 94.5 AND 115.8 WAS FOUND TO HAVE CORROSION. THE CORROSION WAS MOSTLY ISOLATED TO THE IMMEDIATE AREA AROUND STRINGER TO SKIN FASTENERS AND EXTENDED BETWEEN
- [SDR DLL15970411](https://openairdocs.org/sdr/DLL15970411.md): Bulkhead Frame · corrosion · Mar 4, 1997 · N755DL · Lkheed 10113853 · Fuselage Main, Bulkhead
  > THE AFT P-DOME ZEE FRAME WAS FOUND WITH CRACKS DUE TO CORROSION IN THE ZEE ANGLE AND WEB. THE DAMAGED FRAME SEGMENTS WERE CUT AND REMOVED AND WILL BE SPLICE REPAIRED. THE ZEE FRAME WAS REMOVED BETWEEN THE S-29 FACTORY SPLICE LOCATION AND S-37. THE WEB WAS R
- [SDR DLL15970410](https://openairdocs.org/sdr/DLL15970410.md): Skin · dented · Mar 4, 1997 · N755DL · Lkheed 10113853 · Passenger/Crew Doors
  > THE L-3 DOOR OUTER SKIN AT THE LOWER AFT CORNER WAS FOUND DENTED AND GOUGED 4.25 FWD OF THE AFT DOOR EDGE. THE RESULTING CUTOUT MEASURES 3.0 WIDE BY 8.7 TALL. NO UNDERLYING STRUCTURE WAS DAMAGED. DAMAGE WILL BE REPAIRED PER ER/A 361178-14 REVISION 'A'.
- [SDR DLL15970307](https://openairdocs.org/sdr/DLL15970307.md): Skin · cracked · Feb 11, 1997 · N755DL · Lkheed 10113853 · Wing, Plate/Skin
  > DURING INSPECTION OF THE RT WING LOWER SKIN AT THE OUTBOARD END OF STRINGER 18 PER E.O. 7-70043-3, A CRACK WAS FOUND EMANATING FROM THE STRINGER END, FORWARD FASTENER HOLE. AFTER PERFORMING AN EDDY CURRENT SURFACE SCAN. THE ENDS OF THE CRACK WERE FOUND TO BE
- [SDR DLL15970068](https://openairdocs.org/sdr/DLL15970068.md): Power Supply · malfunctioned · Jan 15, 1997 · N755DL · Lkheed 10113853 · Emergency Lighting
  > DURING TEST OF THE EMERGENCY LIGHTING SYSTEM, IT WAS DISCOVERED THAT THE TRACK LIGHTS IN FIRST CLASS EXTINGUISHED AFTER TOO SHORT A TIME PERIOD. THE POWER SUPPLY AT THE R-1 POSITION WAS REPLACED AND THE EMERGENCY LIGHTS TESTED NORMALLY.
- [SDR DLL15962706](https://openairdocs.org/sdr/DLL15962706.md): Socket · broken · Dec 18, 1996 · N755DL · Lkheed 10113853 · Emergency Lighting
  > EMERGENCY PATH LIGHTS SOCKET BROKEN AT ROW 22G AND 27C. INSTALLED NEW LIGHT SOCKETS, OPS CHECK OK.
- [SDR DLL15962575](https://openairdocs.org/sdr/DLL15962575.md): Vib Monitor · malfunctioned · Nov 23, 1996 · N755DL · Lkheed 10113853 · Engine Vibration Analyzer
  > NR 2 ENGINE WAS SHUTDOWN ON DESCENT APPROX 20K FT. HIGH VIBS BOTH CHANNELS 2.6 VIBS. NO OTHER ABNORMAL ENGINE INDICATIONS, NO ICING PRESENT. REPLACED ENG VIB MONITOR, RAN ENGINES PER PFHB TEST. CK'D CHIP DETECTORS, FILTERS, INLET AND EXHAUST. BORESCOPED H
- [SDR DLL15962155](https://openairdocs.org/sdr/DLL15962155.md): Light · inoperative · Sep 22, 1996 · N755DL · Lkheed 10113853 · Emergency Lighting
  > EMERGENCY LIGHT INOP AT SEAT 32C. REPLACED LIGHT SOCKET, BULB AND LENS.
- [SDR DLL15961558](https://openairdocs.org/sdr/DLL15961558.md): Lights · broken · Jun 29, 1996 · N755DL · Lkheed 10113853 · Emergency Lighting
  > ON L/O, FOUND EMERGENCY FLOOR TRACK LIGHTS 1B, 12E, 24G INOP. REPLACED LAMP HOLDERS ON 1B, 12E, 24G, EMERGENCY LIGHTS CK GOOD.
- [SDR DLL15960633](https://openairdocs.org/sdr/DLL15960633.md): Light · broken · Mar 21, 1996 · N755DL · Lkheed 10113853 · Emergency Lighting
  > EMERGENCY LIGHT CAME APART L1 DOOR EXIT SIGN. REPLACED LIGHT ASSY.
- [SDR DLL15960292](https://openairdocs.org/sdr/DLL15960292.md): Control Cable · jammed · Feb 6, 1996 · N755DL · Lkheed 10113853 · Rudder Control System
  > ON TAXI OUT - RUDDER PEDAL WOULD NOT MOVE LEFT - RIGHT MOVEMENT OK. FOUND CAPTAIN'S FORE/AFT RUDDER POSITION HAND CRANK MECHANISM JAMMED. FREED CABLE. OPERATION NORMAL.
- [SDR DLL15960103](https://openairdocs.org/sdr/DLL15960103.md): Battery Pack · discharged · Jan 16, 1996 · N755DL · Lkheed 10113853 · Emergency Lighting
  > OVERHEAD EMERGENCY LIGHTS AT 20AB INOP. REPLACED DEFECTIVE BATTERY PACK AT 22AB OVERHEAD AND LIGHTS CHECK GOOD.
- [SDR DLL15954392](https://openairdocs.org/sdr/DLL15954392.md): Vane · cracked · Oct 31, 1995 · N755DL · Lkheed 10113853 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, NR 1 RT FLAP VANE WAS FOUND WITH WEAR DAMAGE AT OUTBOARD RUB STRIP 8 INCHES FROM TRAILING EDGE. REPAIRED PER SRM 57-53-00.
- [SDR DLL15954649](https://openairdocs.org/sdr/DLL15954649.md): Skin · worn · Oct 17, 1995 · N755DL · Lkheed 10113853 · Trailing Edge Flaps
  > NR 3 RT FLAP VANE UPPER SKIN HAD A WORN AND SCRATCHED SPOT. REPLACED SKIN SECTION PER SRM 57-53-00.

## 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 = 'N755DL' AND deregistration_id = 'N755DL-2013-09-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N755DL-2013-09-10/reports

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