# Service difficulty reports: N718DA, cancelled Jun 13, 2005

A list on [N718DA, cancelled Jun 13, 2005](https://openairdocs.org/deregistered/N718DA-2005-06-13.md).

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

- [SDR DLL10991808](https://openairdocs.org/sdr/DLL10991808.md): Skin · cracked · Aug 11, 1999 · N718DA · Lkheed 10113851 · Wing, Plate/Skin
  > WING LT UPPER SKIN, IWS 395, CRACK REPAIR. AN EXISTING CRACK IN THE LEFT UPPER WING SKIN AT IWS 395 PROGRESSED BEYOND THE ALLOWABLE SRM LIMIT. THE CRACK STARTED AT THE AFT EDGE OF THE SKIN AND PROGRESSED FWD. THE CRACK IS TYPICAL OF THE SRM, BUT IS NOW 2.3
- [SDR DLL10991806](https://openairdocs.org/sdr/DLL10991806.md): Skin · cracked · Aug 11, 1999 · N718DA · Lkheed 10113851 · Wing, Plate/Skin
  > WING RT LOWER AFT SKIN IWS 425.7, STRINGER 3, CRACK REPAIR. THE LOWER AFT SKIN OF THE RT WING WAS FOUND WITH A 4.5 LONG CRACK AT THE STRINGER 3 RUNOUT AT IWS 425.7. THE CRACK WAS CUTOUT OF THE SKIN AND REPAIRED WITH THREE ALUMINUM DOUBLERS PER ER/A 367909-14
- [SDR DLL10991805](https://openairdocs.org/sdr/DLL10991805.md): Frame · cracked · Aug 11, 1999 · N718DA · Lkheed 10113851 · Fuselage Main, Frame
  > FUSELAGE FRAME FS 1183, WL 280.6, CRACK REPAIR. A TYPICAL CRACK WAS FOUND IN THE FS 1183 FUSELAGE FRAME AT WL 280.6. THE CRACK WAS STOP DRILLED AND REPAIRED PER LACO S/B 093-53-A271 AND ER/A 367927-14, REV A.
- [SDR DLL10991804](https://openairdocs.org/sdr/DLL10991804.md): Frame · cracked · Aug 11, 1999 · N718DA · Lkheed 10113851 · Fuselage Main, Frame
  > FUSELAGE FRAME FS 1645, STRINGER 14L, CRACK REPAIR. THE FS 1645 FRAME WAS FOUND WITH A TYPICAL CRACK AT WL 280.6 AND AN ADDITIONAL CRACK AT STRINGER 14L ABOVE THE TYPICAL CRACK. THE NEW CRACK WAS APPROX 1 LONG AND RAN LONGITUDINALLY ACROSS THE FRA
- [SDR DLL10991484](https://openairdocs.org/sdr/DLL10991484.md): Bulkhead Web · cracked · Jun 29, 1999 · N718DA · Lkheed 10113851 · Fuselage Main, Bulkhead
  > WHILE ACCOMPLISHING HFEC INSPECTIONS OF THE UPPER GORE WEB OF THE AFT P-DOME, A 2.5 INCH CRACK WAS FOUND IN THE WEB AT LBL 10. THE CRACK IS TYPICAL OF LAC S/B 093-53-258 (MANDATED PER AD 95-17-03). THE CRACK WAS REPAIRED WITH A DOUBLER AND TRIPLER PER THE S/
- [SDR DLL10991136](https://openairdocs.org/sdr/DLL10991136.md): Panel · cracked · May 21, 1999 · N718DA · Lkheed 10113851 · Wing, Plate/Skin
  > CRACK IN SHEET METAL ON TOP OF LEFT WING SECOND CANOE FITTING OUTBOARD FROM WING ROOT. REPAIRED PER ERA OR SRM AS APPLICABLE.
- [SDR DLL10991100](https://openairdocs.org/sdr/DLL10991100.md): Fire Loop · inoperative · May 18, 1999 · N718DA · Lkheed 10113851 · Fire Detection
  > NR 1 ENG LOOP A ON MCO, LOOP B FLICKERED THEN CAME ON STEADY. CREW SHUTDOWN NR 1 ENG PER POM. REPLACED UPPER GEARBOX LOOP.
- [SDR DLL10990434](https://openairdocs.org/sdr/DLL10990434.md): Battery · discharged · Mar 2, 1999 · N718DA · Lkheed 10113851 · Emergency Lighting
  > F/C EMER LIGHTS INOP. REPLACED BATTERY PACK AND POWER SUPPLY.
- [SDR DLL10982393](https://openairdocs.org/sdr/DLL10982393.md): Power Supply · inop · Nov 18, 1998 · N718DA · Lkheed 10113851 · Emergency Lighting
  > LWR GALLEY EMER LIGHT INOP. REPLACED PWR SUPPLY, OP CK NORMAL.
- [SDR DLL10981430](https://openairdocs.org/sdr/DLL10981430.md): Chip Detector · not installed · Jul 9, 1998 · N718DA · Lkheed 10113851 · Turbine Engine Accessory Drive
  > NR 1 ENG OIL LOSS IN EXCESS OF 4 QTS HR. DIVERTED SLC. ENG WAS NOT SHUTDOWN AND NO LOSS OF OIL PRESS. FOUND NR 1 ENG FINE SCAVAGE CHIP DET NOT IN HOUSING AND LAYING ON TOP OF OIL TANK. DET VISUALLY CKD OK BUT ONE O-RING FELL OFF WHEN HANDLED. REPLACED BOT
- [SDR DLL10981158](https://openairdocs.org/sdr/DLL10981158.md): Light · inoperative · May 31, 1998 · N718DA · Lkheed 10113851 · Emergency Lighting
  > ON LAYOVER, FOUND FLASHLIGHT AT L-2 FLT ATTN SEAT INOP. RED IND NOT FLASHING. RELAMPED INDICATOR LIGHT. CKS OK.
- [SDR DLL10980632](https://openairdocs.org/sdr/DLL10980632.md): Light · inoperative · Mar 22, 1998 · N718DA · Lkheed 10113851 · Emergency Lighting
  > LOWER GALLEY LEFT SIDE EMERGENCY FLASHLIGHT INOP. FOUND MAGNET MISSING FROM HOLDER CAUSING LIGHT TO REMAIN ON WHEN STOWED. REPLACED HOLDER AND BATTERY.
- [SDR DLL10980264](https://openairdocs.org/sdr/DLL10980264.md): Ballast · failed · Jan 30, 1998 · N718DA · Lkheed 10113851 · Passenger Compartment Lighting
  > BURNING ELECTRICAL SMELL 1ST CLASS LAV CAPT'S SIDE. REPLACED BALLAST, CHECK NORMAL.
- [SDR DLL10970636](https://openairdocs.org/sdr/DLL10970636.md): Bulkhead Web · cracked · Apr 6, 1997 · N718DA · Lkheed 10113851 · Fuselage Main, Bulkhead
  > DURING INSPECTION PER DAL EO 7-69959-12AD, THE FS 1363 BULKHEAD WEB SECTION I/B OF OF LBL 42.5 WAS FOUND WITH TWO CRACKS AT APPROX WL 133. THE SUBJECT WEB SECTION IS MADE FROM 0.085 THICK 7075-T6 AL CLAD.
- [SDR DLL10961360](https://openairdocs.org/sdr/DLL10961360.md): Light · inoperative · Jun 4, 1996 · N718DA · Lkheed 10113851 · Emergency Lighting
  > AFT CABIN EMERGENCY TRACK LIGHTS WILL NOT COME ON DURING TEST. FOUND FUSES BLOWN IN AFT RT CONTROL MODULE. REPLACED FUSES, TRACK LIGHTS CKS GOOD.
- [SDR DLL10960786](https://openairdocs.org/sdr/DLL10960786.md): Seal · torn · Apr 7, 1996 · N718DA · Lkheed 10113851 · Cabin Pressure Control System
  > LOUD BEATING NOISE ABOVE FWD CARGO DOOR AND LOUD AIR NOISE IN LOWER GALLEY. FLIGHT RETURNED TO ATL. FOUND SECTION OF C-1 DOOR SEAL BLOWN. REPLACED SECTION OF SEAL, PRESS NORMAL.
- [SDR DLL10960497](https://openairdocs.org/sdr/DLL10960497.md): Chip Detector · leaking · Mar 5, 1996 · N718DA · Lkheed 10113851 · Turbine Engine Accessory Drive
  > NR 1 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED - GAUGE SHOWED LOW OIL QUANTITY. ENGINE NR 1 SHUT DOWN IAW POM AND EMERG PROCEDURES ON FINAL APPROACH. N3 WENT TO ZERO. FOUND EVIDENCE OF LEAKING AT MASTER CHIP DETECTOR HOUSING. REPLACED FINE SCAVANGE FILTER.
- [SDR DLL10960335](https://openairdocs.org/sdr/DLL10960335.md): Bulb · failed · Feb 13, 1996 · N718DA · Lkheed 10113851 · Emergency Lighting
  > FLIGHT ATTENDENT REPORTED IN CDL THAT THE EXIT SIGN BETWEEN FIRST CLASS AND COACH ON RIGHT SIDE OF CABIN INOP. RELAMPED, OPERATION NORMAL.
- [SDR DLL10960197](https://openairdocs.org/sdr/DLL10960197.md): Mach Feel Wire · broken · Jan 25, 1996 · N718DA · Lkheed 10113851 · Speed-Attitude Correction System
  > DURING CLIMB, NR 1 MACH FEEL FAIL LIGHT CAME ON, WOULD NOT RESET. THEN 30 MINS LATER, DURING CRUISE THE NR 2 MACH FEEL FAIL LIGHT CAME ON AND WOULD NOT RESET. REPLACED NR 1 MACH TRIM MOTOR, FOUND BROKEN WIRE ON CONNECTOR TO NR 2 TRIM MOTOR.
- [SDR DLL10954631](https://openairdocs.org/sdr/DLL10954631.md): Eel Power Supply · inoperative · Dec 6, 1995 · N718DA · Lkheed 10113851 · Emergency Lighting
  > L-2 DOOR EMERGENCY EXIT LIGHT POWER SUPPLY INOP. REPLACED SAME, OPERATION NORMAL.
- [SDR DLL10954161](https://openairdocs.org/sdr/DLL10954161.md): Attach Fitting · corrosion · Oct 27, 1995 · N718DA · Lkheed 10113851 · Wing, Landing Gear Attach Fittings
  > RIGHT MLG ATTACH RIB FITTING WAS CORRODED AT THE MLG RETRACT ACTUATOR ATTACH FITTING LOCATION. ATTACH RIB UPPER AND LOWER ACTUATOR ATTACH PAD FASTENER HOLES WERE OVERSIZED. VERTICAL WEB AND FLANGES HAVE BEEN MACHINED/LOCALLY BLENDED PER DL ERA 272017-14.
- [SDR DLL10954500](https://openairdocs.org/sdr/DLL10954500.md): Rib Tabs · cracked · Oct 26, 1995 · N718DA · Lkheed 10113851 · Wing, Rib/Bulkhead
  > THE RT/LT WINGS IWS 503 AND IWS 529 RIB UPPER/LWR CAP ATTACH TABS ARE CRACKED. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD.
- [SDR DLL10961591](https://openairdocs.org/sdr/DLL10961591.md): Stiffener · cracked · Oct 18, 1995 · N718DA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > DURING HMV, THE NLG PRESSURE DECK INTEGRAL STIFFENER ALONG RBL 40 WAS FOUND CRACKED. THE CRACK WAS TRIMMED OUT AND A FILLER/DOUBLER REPAIR WAS INSTALLED.
- [SDR DLL10954174](https://openairdocs.org/sdr/DLL10954174.md): Rib · cracked · Oct 6, 1995 · N718DA · Lkheed 10113851 · Wing, Rib/Bulkhead
  > THE RT WING IWS 503 RIB UPPER CAP ATTACH TAB IS CRACKED IN THE TYPICAL LOCATION BETWEEN STR 18 AND 19. ACCOMPLISHED REPAIRS PER DL ERA 272012-14AD.
- [SDR DLL10954172](https://openairdocs.org/sdr/DLL10954172.md): Rib · cracked · Oct 6, 1995 · N718DA · Lkheed 10113851 · Wing, Rib/Bulkhead
  > THE LT WING IWS 555 RIB UPPER AND LOWER CAP WERE FOUND WITH CRACKS IN THE ATTACH TABS AT TYPICAL LOCATIONS. ACCOMPLISHED REPAIRS PER DL ERA 272011-14AD.
- [SDR DLL10954177](https://openairdocs.org/sdr/DLL10954177.md): Deck · dented · Oct 5, 1995 · N718DA · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > THE PRESSURE DECK WAS FOUND DAMAGED AT FS 409 AND RBL 80 ON BOTH THE HORIZONTAL LEG AND THE LOWER SURFACE. THE DAMAGE WAS BLENDED OUT PER DL ERA 268387-14.
- [SDR DLL10953994](https://openairdocs.org/sdr/DLL10953994.md): Rib · cracked · Sep 29, 1995 · N718DA · Lkheed 10113851 · Leading Edge Devices
  > NR 6 L/E SLAT RIB CRACKED. REPAIRED PER SRM 57-51-00 FIG 812, FOUND AT LETTER CHECK.
- [SDR DLL10953644](https://openairdocs.org/sdr/DLL10953644.md): Fittings · cracked · Aug 31, 1995 · N718DA · Lkheed 10113851 · Fuselage Main, Bulkhead
  > COMPLYING WITH DL INSPECTION SI7-66332-12 AND AD T95-18-52, FOUND STRINGER TO AFT P-DOME SPLICE FITTINGS AT STRINGERS NR 5, 10 AND 61 CRACKED. THE FITTINGS WERE SCHEDULED FOR REPLACEMENT.
- [SDR DLL10952494](https://openairdocs.org/sdr/DLL10952494.md): Gearbox · failed · Jun 6, 1995 · N718DA · Lkheed 10113851 · Turbine Engine Accessory Drive
  > AT FLT LEVEL 330, NR 3 OIL PRESSURE WENT TO ZERO FOLLOWED BY LOSS OF THRUST. NR 3 ENG SHUT DOWN, OIL QTY AND TEMP NORMAL. FOUND NR 3 GEARBOX FAILED. REPLACED GEARBOX, RETURNED TO SERVICE.
- [SDR DLL10960486](https://openairdocs.org/sdr/DLL10960486.md): Blkhd Cap · cracked · May 12, 1995 · N718DA · Lkheed 10113851 · Fuselage Main, Bulkhead
  > TWO CRACKS WERE FOUND IN BLKHD CAP AT LBL 42.5 AND 74.5. THE CRACKS ARE LOCATED IN THE VERTICAL BLKH ATTACH FLANGE AND EMANATES FROM FASTENER HOLES. THE CRACKS HAVE BEEN REMOVED BY OVERSIZING THE SUBJECT FASTENER HOLES. ALSO, THE BLKHD WAS FOUND CRACKED AT
- [SDR DLL10952104](https://openairdocs.org/sdr/DLL10952104.md): Stringer · damaged · May 6, 1995 · N718DA · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > DURING SERVICE CHECK FOUND TOOLING DAMAGE ON STR 14 RT AT STA 1023. REPAIRED PER SRM 53-13-00 PG. 806.
- [SDR DLL10950084](https://openairdocs.org/sdr/DLL10950084.md): Flap Vane · crack · Jan 2, 1995 · N718DA · Lkheed 10113851 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, CRACKING WAS FOUND IN THE LEFT WING NR 3 FLAP VANE TOP SKIN DOUBLER AT 35 INCHES FROM THE INBOARD EDGE. INSTALLED SPLICED SKIN REPAIR PER SRM 57-53-00 FIG 805.

## 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 = 'N718DA' AND deregistration_id = 'N718DA-2005-06-13'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N718DA-2005-06-13/reports

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