# Service difficulty reports: N15017, cancelled May 14, 1998

A list on [N15017, cancelled May 14, 1998](https://openairdocs.org/deregistered/N15017-1998-05-14.md).

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

- [SDR TWAA9781001](https://openairdocs.org/sdr/TWAA9781001.md): Oil Filter · dirty · Jul 19, 1997 · N15017 · Lkheed 10113851 · Turbine Engine Oil System
  > LAX - FLT 442 - DURING CLIMB, NR 2 ENGINE, SN 4816, LOST OIL INDICATION. DRAINED GEARBOX, CHANGED MAIN OIL SCREEN AND SCAVENGE SCREEN. SERVICED GEARBOX AND RAN ENGINE. RE-CHECKED MAIN OIL SCREEN AND SCAVENGE SCREEN, NO DEFECTS NOTED. ENGINE RUN NORMAL. EN
- [SDR TWAA9752010](https://openairdocs.org/sdr/TWAA9752010.md): Skin · corroded · Mar 20, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION WITH HI-LOK HEADS PULLED AT STR 38, FS 1615. REMOVED CORROSION PER SRM 51-21-01 AND REPAIRED STRINGER PER SRM 53-13-00. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752009](https://openairdocs.org/sdr/TWAA9752009.md): Frame · corroded · Mar 20, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Frame
  > LAX - DURING CHECK 'C', FOUND CORROSION, 3 INCH BY 3 INCH CORROSION HOLE BETWEEN STRINGERS 40 AND 41, FS 1625 FRAME. INSTALLED FRAME REPAIR PER SRM 53-12-00, FIGURE 805, PAGES 806 AND 807. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752008](https://openairdocs.org/sdr/TWAA9752008.md): Intercostal · cracked · Mar 19, 1997 · N15017 · Lkheed 10113851 · Fuselage Miscellaneous Structure
  > LAX - DURING CHECK 'C', FOUND STR 42 INTERCOSTAL CRACKED, FS 1705. STOP DRILLED CRACK AND INSTALLED DOUBLER WITH SEALANT PER SRM 51-50-02, PAGE 4, FIGURE 2. AIRCRAFT TOTAL TIME: 62,400 HOURS, 23,718 CYCLES. (X)
- [SDR TWAA9752007](https://openairdocs.org/sdr/TWAA9752007.md): Skin · corroded · Mar 19, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION WHICH POPPED TWO BLIND FASTENERS AND CRACKED RIVET HEAD, STRINGER 37, FS 1615. REPAIRED BY REMOVAL OF CORROSION AND INSTALLATION OF DOUBLER PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYC
- [SDR TWAA9752006](https://openairdocs.org/sdr/TWAA9752006.md): Skin · corroded · Mar 18, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHCK 'C', FOUND FUSELAGE SKIN CORROSION AT FOUR BLIND FASTENERS, STR 29, FS 1732. REMOVED CORROSION AND REPAIRED PER SRM 53-30-07, PAE 20. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752004](https://openairdocs.org/sdr/TWAA9752004.md): Stringer · corroded · Mar 17, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Longeron/Stringer
  > LAX - DURING CHECK 'C', FOUND CORROSION AT STRINGERS 37 AND 40, FS 1715. REMOVED CORROSION AND REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752003](https://openairdocs.org/sdr/TWAA9752003.md): Skin · corroded · Mar 17, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION BELOW STR 30, FS 839.5. REPAIRED PER SRM 53-03-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752002](https://openairdocs.org/sdr/TWAA9752002.md): Skin · corroded · Mar 17, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION ABOVE STR 30, FS 816.5. REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9752005](https://openairdocs.org/sdr/TWAA9752005.md): Skin · corroded · Mar 1, 1997 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > LAX - DURING CHECK 'C', FOUND FUSELAGE SKIN CORROSION BETWEEN STRINGERS 29 AND 30, FS 822. REPAIRED PER SRM 53-30-02. AIRCRAFT TOTAL TIME: 62,400 HOURS; 23,718 CYCLES. (X)
- [SDR TWAA9720001](https://openairdocs.org/sdr/TWAA9720001.md): Bracket · failed · Feb 10, 1997 · N15017 · Lkheed 10113851 · Elevator Structure
  > MCO - FLT 264 - DURING LANDING, RIGHT INBOARD ELEVATOR GAP FAIRING SEPARATED FROM THE AIRCRAFT DUE TO BRACKET FAILURE. REPLACED FAIRING, MFG P/N 1554958-104. VISUAL CHECK NORMAL. (M)
- [SDR TWAA9703002](https://openairdocs.org/sdr/TWAA9703002.md): Food Cart · failed · Jan 3, 1997 · N15017 · Lkheed 10113851 · Buffet/Galleys
  > LAX - FLT 443 - DURING CRUISE SINGLE SERVE FOOD CART NR 1479, P/N 88801-1 SMOKED WHEN TURNED ON. REMOVED AND REPLACED CART NR 1479, WITH A SERVICEABLE CART. (M)
- [SDR TWAA9616002](https://openairdocs.org/sdr/TWAA9616002.md): Engine · malfunctioned · Aug 4, 1996 · N15017 · Lkheed 10113851 · Engine (Turbine/Turboprop)
  > LAX - DURING CLIMB, NR 3 ENGINE, S/N 4456 EXPERIENCED HIGH AVM. ENGINE WAS SHUT DOWN. INLET AND EXHAUST WERE CHECKED, CHIP DETECTORS CHECKED, AND GEARBOX WAS DRAINED AND SERVICED. NO DEFECTS WERE NOTED. ACCOMPLISHED TRIM BALANCED. (M)
- [SDR 96ZZZX3031](https://openairdocs.org/sdr/96ZZZX3031.md): Rib · cracked · May 10, 1996 · N15017 · Lkheed 10113851 · Wing, Rib/Bulkhead
  > MCI - DURING SPECIAL CHECK FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 9, BOTTOM IWS 555. REPAIRED PER SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.
- [SDR 96ZZZX3030](https://openairdocs.org/sdr/96ZZZX3030.md): Rib · cracked · May 10, 1996 · N15017 · Lkheed 10113851 · Wing, Rib/Bulkhead
  > MCI - DURING SPECIAL CHECK FOUND CRACKS IN TOP WING RIB CASTELLATION OF RT WING, IWS 503, STRINGERS 18, 19, AND 21. REPAIRED PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 3. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.
- [SDR 96ZZZX3029](https://openairdocs.org/sdr/96ZZZX3029.md): Rib · cracked · May 10, 1996 · N15017 · Lkheed 10113851 · Wing, Rib/Bulkhead
  > MCI - DURING SPECIAL CHECK, FOUND CRACK IN RIB CASTELLATION AT FORWARD SIDE OF STR 13 AND STR 19, TOP IWS 555. REPAIRED PER SB 093-57-207 AND SRM 51-10-01. AIRCRAFT TOTAL TIME: 60,229 HOURS; 22,908 CYCLES.
- [SDR 96ZZZX3027](https://openairdocs.org/sdr/96ZZZX3027.md): Angle · cracked · May 10, 1996 · N15017 · Lkheed 10113851 · Wing Miscellaneous Structure
  > MCI - DURING SPECIAL CHECK, FOUND A 2 INCH CRACK AT TOP OF CLOSURE RIB ATTACH ANGLE IN RIGHT WING, IWS 503. REPAIRED BY INSTALLING NEW ATTACHED ANGLE PER SB 093-57-207 AND LOCKHEED DWG NR 1647070, SHEET 2. AIRCRAFT TT: 60,229 HOURS; 22,908 CYCLES.
- [SDR 96ZZZM892](https://openairdocs.org/sdr/96ZZZM892.md): Engine · vibration · Apr 24, 1996 · N15017 · Lkheed 10113851 · Engine (Turbine/Turboprop)
  > MCI - FLT 5034 - DURING CRUISE, SHUT DOWN NR 2 ENGINE DUE TO INCREASE OF VIBRATION ON BOTH A AND B CHANNELS. FOUND FAN OUT OF TRIM BALANCE. PERFORMED ENGINE TRIM BALANCE. ENGINE OPERATION AND INDICATION THEN CHECKED NORMAL.
- [SDR 96ZZZM896](https://openairdocs.org/sdr/96ZZZM896.md): Rib · cracked · Apr 18, 1996 · N15017 · Lkheed 10113851 · Wing, Rib/Bulkhead
  > MCI - DURING SPECIAL CHECK, FOUND SEVEN CRACKS IN LEFT WING TOP RIB CASTELLATION, STATION 555. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B. (M)
- [SDR 96ZZZM895](https://openairdocs.org/sdr/96ZZZM895.md): Rib · cracked · Apr 18, 1996 · N15017 · Lkheed 10113851 · Wing, Rib/Bulkhead
  > MCI - DURING SPECIAL CHECK, FOUND 1.25 INCH CRACK IN LEFT WING RIB CASTELLATION FORWARD SIDE OF STRINGER 19, TOP CHORD, WS 503. REPAIRED PER SERVICE BULLETIN 093-57-207, PARA 2B.
- [SDR 95ZZZM293](https://openairdocs.org/sdr/95ZZZM293.md): Oil Filter · dirty · Jul 21, 1995 · N15017 · Lkheed 10113851 · Turbine Engine Oil System
  > DURING DESCENT SHUT DOWN NR 2 ENGINE, S/N 4806, DUE TO OIL FILTER DIFFERENTIAL PRESSURE LIGHT ILLUMINATION. FOUND CARBON IN OIL FILTER. REPLACED OIL FILTER, DRAINED AND REPLENISHED ENGINE OIL. ENGINE OIL FILTER DIFFERENTIAL PRESSURE SYSTEM CHECKED NORMAL.
- [SDR 95ZZZW441](https://openairdocs.org/sdr/95ZZZW441.md): Control Valve · malfunctioned · Mar 31, 1995 · N15017 · Lkheed 10113851 · Landing Gear Retraction/Extension System
  > JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6. LANDING GEAR SYSTEM OPERATION CHECKED NO
- [SDR 95ZZZW440](https://openairdocs.org/sdr/95ZZZW440.md): Control Switch · malfunctioned · Mar 31, 1995 · N15017 · Lkheed 10113851 · Landing Gear Retraction/Extension System
  > JFK - DURING APPROACH LANDING GEAR WOULD NOT EXTEND WHEN SELECTED. USED MECHANICAL LANDING GEAR EXTENSION. REPLACED LANDING GEAR CONTROL SWITCH, MFG P/N 450-100-109, AND LANDING GEAR CONTROL VALVE, MFG P/N 2680262M6. LANDING GEAR SYSTEM OPERATION CHECKED NO
- [SDR 95ZZZW224](https://openairdocs.org/sdr/95ZZZW224.md): Skin · cracked · Feb 13, 1995 · N15017 · Lkheed 10113851 · Fuselage Main, Plate/Skin
  > MCI - DURING CHECK C-6C, FOUND 1.5 INCH CRACK IN FUSELAGE SKIN, WITH AREA BULGED OUTWARD AND WITH RIVET HEAD MISSING, STATION 649, STRINGER 36-37. REPAIRED PER SRM 53-31-00, FIGURE 815. TOTAL CYCLES 22,020.

## 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 = 'N15017' AND deregistration_id = 'N15017-1998-05-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N15017-1998-05-14/reports

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