# Service difficulty reports: N17025, cancelled Jul 11, 2003

A list on [N17025, cancelled Jul 11, 2003](https://openairdocs.org/deregistered/N17025-2003-07-11.md).

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

- [SDR CALA9802066](https://openairdocs.org/sdr/CALA9802066.md): Skin · damaged · Nov 14, 1998 · N17025 · Boeing 747238B · Fuselage Main, Plate/Skin
  > THE LOWER FUSELAGE BELLY SKIN WAS FOUND TO BE PUNCTURED BY GROUND EQUIPMENT AT STA 1997. THE PUNCTURED AREA WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED IAW SRM 53-30-3, FIGURE 19, 53-10-3, FIGURE 1 AND 51-40-4, FIGURE 2.
- [SDR CALA9700753](https://openairdocs.org/sdr/CALA9700753.md): Power Supply · inoperative · May 18, 1997 · N17025 · Boeing 747238B · Emergency Lighting
  > INSPECTION FOUND AIRCRAFT LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. THE POWER SUPPLY AT L-3 DOOR WAS REMOVED AND REPLACED.
- [SDR CALA9700040](https://openairdocs.org/sdr/CALA9700040.md): Channel · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Leading Edge Devices
  > INSPECTION FOUND A.125 INCH CRACK IN AFT SUPPORT CHANNEL AT LT WING NR 4 LEADING EDGE FLAP. THE CHANNEL WAS REPAIRED IAW SRM 51-40-03, FIGURE 2.
- [SDR CALA9700038](https://openairdocs.org/sdr/CALA9700038.md): Rib · corroded · Dec 22, 1996 · N17025 · Boeing 747238B · Wing, Rib/Bulkhead
  > INSPECTION FOUND TOP RIB CHORD CORRODED AT LT WING LEADING EDGE, WS 614. THE RIB CHORD WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.
- [SDR CALA9700033](https://openairdocs.org/sdr/CALA9700033.md): Angle · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Wing Miscellaneous Structure
  > INSPECTION FOUND A.5 INCH CRACK IN VERTICAL SUPPORT ANGLE OF RT WING LEADING EDGE NOSE STRUCTURE BACKING WEB AT INBOARD LEADING EDGE STA 631. THE ANGLE WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9700032](https://openairdocs.org/sdr/CALA9700032.md): Chord · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND A 6 INCH CRACK IN UPPER CHORD OF RT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA9700031](https://openairdocs.org/sdr/CALA9700031.md): Web · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Wing Spar
  > INSPECTION FOUND A 2 INCH CRACK IN FORWARD SPAR WEB OF LT WING AT WS 780. THE WEB WAS REPAIRED IAW SRM 51-40-02, FIGURE 1.
- [SDR CALA9700030](https://openairdocs.org/sdr/CALA9700030.md): Web · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND A.5 INCH CRACK IN THREE LOCATIONS OF MOST INBOARD WEB OF RT WING INBOARD FOREFLAP. THE WEB WAS REPLACED IAW SRM 51-10-01, PAGE 18.
- [SDR CALA9700028](https://openairdocs.org/sdr/CALA9700028.md): Stiffener · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Wing Miscellaneous Structure
  > INSPECTION FOUND A 1.5 INCH CRACK IN FORWARD VERTICAL STIFFENER AT LT WING LEADING EDGE RIB, INBOARD LEADING EDGE STA 636.72. THE STIFFENER WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9700027](https://openairdocs.org/sdr/CALA9700027.md): Chord · cracked · Dec 22, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND AN 8 INCH CRACK IN UPPER CHORD OF LT WING OUTBOARD MID FLAP OUTBOARD REAR SPAR. THE CHORD WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA9700034](https://openairdocs.org/sdr/CALA9700034.md): Door Frame · cracked · Dec 19, 1996 · N17025 · Boeing 747238B · Passenger/Crew Doors
  > INSPECTION FOUND A 1 INCH CRACK IN DOOR FRAME AT BS 440, STRINGER 26R. THE DOOR FRAME WAS REPAIRED IAW SRM 52-10-02, FIGURE 2.
- [SDR CALA9700037](https://openairdocs.org/sdr/CALA9700037.md): Rib · cracked · Dec 16, 1996 · N17025 · Boeing 747238B · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1.5 INCH CRACK IN RIB CHORD AT RT WING NR 3 MAIN TANK, WS 670. THE RIB CHORD WAS REPAIRED IAW SB 57-2273.
- [SDR CALA9700036](https://openairdocs.org/sdr/CALA9700036.md): Frame · cracked · Dec 16, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN FRAME WEB AT STRINGER 24R AND A.75 INCH CRACK WAS FOUND IN FRAME WEB AT STRINGER 24L, BS 800. THE WEBS WERE REPAIRED IAW SRM 53-10-04, FIGURE 84.
- [SDR CALA9700035](https://openairdocs.org/sdr/CALA9700035.md): Web · cracked · Dec 16, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.75 INCH CRACK IN WEB AT BS 1650, STRINGER 24L. THE WEB WAS REPAIRED IAW SRM 53-10-04, FIGURE 84.
- [SDR CALA9700029](https://openairdocs.org/sdr/CALA9700029.md): Rib · cracked · Dec 12, 1996 · N17025 · Boeing 747238B · Wing, Rib/Bulkhead
  > INSPECTION FOUND A.5 INCH CRACK IN RIB TOP AREA OF LT WING INBOARD LEADING EDGE STA 628. THE RIB WAS REPAIRED IAW SRM 51-40-02.
- [SDR CALA9700039](https://openairdocs.org/sdr/CALA9700039.md): Doubler · cracked · Dec 11, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A.25 INCH CRACK IN DOUBLER AT BS 400 BULKHEAD AFT FACE, WL 120, RBL 40. A REPAIR WAS ACCOMPLISHED IAW SRM 53-10-04, FIGURE 37.
- [SDR CALA9601841](https://openairdocs.org/sdr/CALA9601841.md): Web · cracked · Dec 5, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND A 3.5 INCH CRACK IN BEAM WEB AT BS 980, STRINGER 5R. THE WEB WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601840](https://openairdocs.org/sdr/CALA9601840.md): Support · corroded · Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1367, RBL 11 TO RBL 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601839](https://openairdocs.org/sdr/CALA9601839.md): Support · corroded · Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 1280, LBL 11 TO RBL 11. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601838](https://openairdocs.org/sdr/CALA9601838.md): Angle · corroded · Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND ANGLE CORRODED AT BS 480, LBL 89. THE ANGLE WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601837](https://openairdocs.org/sdr/CALA9601837.md): Support · corroded · Dec 4, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND LATERAL FLOOR SUPPORT CORRODED AT BS 1300, RBL 11 TO 33. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601833](https://openairdocs.org/sdr/CALA9601833.md): Fittings · corroded · Dec 3, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRINGER END FITTINGS CORRODED AT BS 2360, S49L, S50L, S51L, S48R AND S51R. THE STRINGER END FITTINGS WERE REPLACED IAW SRM 51-10-01.
- [SDR CALA9601836](https://openairdocs.org/sdr/CALA9601836.md): Support Plate · corroded · Nov 29, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT PLATE CORRODED AT BS 1259, RBL 11 TO 33. THE FLOOR SUPPORT PLATE WAS REPLACED IAW SRM 51-10-01.
- [SDR CALA9601835](https://openairdocs.org/sdr/CALA9601835.md): Support · corroded · Nov 29, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 1259, LBL 33 TO RBL 11. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-01.
- [SDR CALA9601834](https://openairdocs.org/sdr/CALA9601834.md): Support · corroded · Nov 22, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND TWO FLOOR SUPPORTS CORRODED AT BS 765 TO 880, LBL 36. THE CORROSION WAS REMOVED AND TREATED, THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-10-01 AND 51-10-02.
- [SDR CALA9700006](https://openairdocs.org/sdr/CALA9700006.md): Stringer · cracked · Nov 9, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND CRACKS IN STRINGER 2R AND 2AR AT BS 741. THERE WERE A TOTAL OF FOUR CRACKS MEASURING 2.5, 1.18, 1.38, AND 0.62 LONG. THE STRINGERS WERE REPAIRED IAW ECRA 5310-03383.
- [SDR CALA9700007](https://openairdocs.org/sdr/CALA9700007.md): Skin · corroded · Nov 8, 1996 · N17025 · Boeing 747238B · Fuselage Main, Plate/Skin
  > INSPECTION FOUND CORROSION IN SKIN LAP SPLICE AT SEVERAL LOCATIONS FROM BS 520 TO 741, STRINGER 6L. THE SKIN WAS REPAIRED IAW ECRA 5330-02472.
- [SDR CALA9700015](https://openairdocs.org/sdr/CALA9700015.md): Fitting · cracked · Nov 7, 1996 · N17025 · Boeing 747238B · Wing Spar
  > INSPECTION FOUND SPLICE FITTING AND UPPER SPLICE PLATE CRACKED AT LT WING REAR SPAR. THE CRACKS WERE 0.040 AND.25 INCH LONG. THE SPLICE PLATE AND SPLICE FITTING WERE REPLACED IAW EA 5710-01199 AND BOEING SB 57-2110.
- [SDR CALA9700003](https://openairdocs.org/sdr/CALA9700003.md): Doubler · corroded · Nov 7, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND CORROSION ON LT WING OUTBOARD TRAILING EDGE MID FLAP OUTBOARD DOUBLER. THE DOUBLER WAS REPAIRED IAW ECRA 5750-02581.
- [SDR CALA9700002](https://openairdocs.org/sdr/CALA9700002.md): Lug · worn · Nov 7, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND LT WING NR 4 MOVEABLE FLAP TRACK FAIRING DRIVE ARM LOWER OUTBOARD HINGE OUTBOARD LUG WORN. THE WORN AREA WAS REPAIRED IAW ECRA 5750-02580.
- [SDR CALA9700001](https://openairdocs.org/sdr/CALA9700001.md): Frame · cracked · Nov 7, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A 1.75 INCH CRACK IN RT FRAME AT BS 220, STRINGER 32A. THE FRAME WAS REPAIRED IAW ECRA 5310-03374.
- [SDR CALA9700022](https://openairdocs.org/sdr/CALA9700022.md): Stringer · cracked · Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A.125 INCH CRACK IN STRINGER 3R AT MAIN DECK BS 2180 TO 2190. THE STRINGER WAS REPAIRED IAW SRM 53-10-03, FIGURE 6.
- [SDR CALA9700017](https://openairdocs.org/sdr/CALA9700017.md): Stringer · cracked · Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 1 INCH CRACK IN STRINGER 9R AT BS 990 MANUFACTURING SPLICE LOCATION. THE STRINGER WAS REPAIRED IAW ECRA 5310-03384.
- [SDR CALA9700016](https://openairdocs.org/sdr/CALA9700016.md): Skin · cracked · Nov 6, 1996 · N17025 · Boeing 747238B · Wing, Plate/Skin
  > INSPECTION FOUND A 0.040 CRACK AT THE RT WING EXTERNAL SPLICE FITTING AND A.1875 INCH CRACK AT THE MATING STRUCTURE WING CENTER SECTION UPPER SKIN PANEL. THE SPLICE FITTING WAS REPLACED IAW EA 5710-01199. THE SKIN PANEL WAS REPAIRED IAW ECRA 5710-01769.
- [SDR CALA9700005](https://openairdocs.org/sdr/CALA9700005.md): Stringer · cracked · Nov 6, 1996 · N17025 · Boeing 747238B · Fuselage Main, Longeron/Stringer
  > INSPECTION FOUND A 0.87 INCH CRACK AT INBOARD VERTICAL FLANGE FASTENER HOLE OF STRINGER 9R AT THE MANUFACTURING SPLICE LOCATION, BS 1740. THE STRINGER WAS REPAIRED IAW ECRA 5310-03373.
- [SDR CALA9700024](https://openairdocs.org/sdr/CALA9700024.md): Skin · delaminated · Nov 5, 1996 · N17025 · Boeing 747238B · Trailing Edge Flaps
  > INSPECTION FOUND LT WING INBOARD MID FLAP PANEL NR 577KT SKIN DELAMINATED. A HOT BOND REPAIR WAS ACCOMPLISHED IAW SRM 51-40-06, FIGURE 15.
- [SDR CALA9700014](https://openairdocs.org/sdr/CALA9700014.md): Frame · cracked · Nov 4, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A.5 INCH CRACK IN FRAME AT MAIN DECK BS 360, LT SIDE, BETWEEN STRINGER 15 AND 16. THE FRAME WAS REPAIRED IAW ECRA 5310-03376.
- [SDR CALA9700012](https://openairdocs.org/sdr/CALA9700012.md): Frame · cracked · Nov 4, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN FRAME AT BS 360 ON RT SIDE, STRINGER 14E. THE FRAME WAS REPAIRED IAW ECRA 5310-03375.
- [SDR CALA9700025](https://openairdocs.org/sdr/CALA9700025.md): Fitting · corroded · Nov 1, 1996 · N17025 · Boeing 747238B · Wing, Fuselage Attach Fittings
  > INSPECTION FOUND LT AND RT WING TO BODY KICK FITTINGS CORRODED. THE BODY KICK FITTINGS WERE REPAIRED IAW ECRA 5340-01283.
- [SDR CALA9700021](https://openairdocs.org/sdr/CALA9700021.md): Spar Web · cracked · Nov 1, 1996 · N17025 · Boeing 747238B · Wing Spar
  > INSPECTION FOUND A.1875 INCH CRACK AT FASTENER HOLE OF NR 2 PYLON WING FRONT SPAR VERTICAL WEB AT INBOARD NACELLE RIB POST ATTACH AREA, WS 688. THE FRONT SPAR VERTICAL WEB WAS REPAIRED PER BOEING DRAWING 112U8040, FCD 5710-01758 AND SRM 51-10-01.
- [SDR CALA9700004](https://openairdocs.org/sdr/CALA9700004.md): Splice · cracked · Nov 1, 1996 · N17025 · Boeing 747238B · Fuselage Miscellaneous Structure
  > INSPECTION FOUND STRINGER SPLICE CORRODED WITH A 1.8 INCH CRACK ALONG FLANGE AT BS 1480, STRINGER 1L. THE STRINGER SPLICE WAS REPLACED IAW ECRA 5310-03380.
- [SDR CALA9700026](https://openairdocs.org/sdr/CALA9700026.md): Skin · corroded · Oct 31, 1996 · N17025 · Boeing 747238B · Wing, Plate/Skin
  > INSPECTION FOUND CORROSION AT RT WING LOWER SKIN FORWARD OF FRONT SPAR LOWER CHORD AND EXTENDING AFT OF FRONT SPAR BETWEEN WS 1454 AND WS 1548. THE AREA WAS REPAIRED IAW ECRA 5710-01766.
- [SDR CALA9700018](https://openairdocs.org/sdr/CALA9700018.md): Rib · cracked · Oct 28, 1996 · N17025 · Boeing 747238B · Wing, Rib/Bulkhead
  > INSPECTION FOUND A 1 INCH CRACK IN FORWARD SHEAR TIE AT LT WING NR 2 MAIN TANK WS 670, UPPER STRINGER 27 AND A.5 INCH CRACK WAS FOUND AT SHEAR TIE OF RIB CHORD, LOWER STRINGER 19. THE RIB CHORD AT UPPER STRINGER 27 WAS REPAIRED IAW SB 57-2273. THE RIB CHORD
- [SDR CALA9700013](https://openairdocs.org/sdr/CALA9700013.md): Frame · cracked · Oct 28, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A 2 INCH CRACK IN FRAME AT THE OUTBOARD FRAME WEB BETWEEN STRINGER 26R AND 27AR, BS 280. THE FRAME WAS REPAIRED IAW ECRA 5310-03370.
- [SDR CALA9700011](https://openairdocs.org/sdr/CALA9700011.md): Frame · cracked · Oct 28, 1996 · N17025 · Boeing 747238B · Fuselage Main, Frame
  > INSPECTION FOUND A.75 INCH CRACK IN FRAME AT BS 380, STRINGER 23R. THE FRAME WAS REPAIRED IAW ECRA 5310-03367.
- [SDR CALA9700023](https://openairdocs.org/sdr/CALA9700023.md): Bulkhead Chord · cracked · Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION FOUND A.125 INCH CRACK AT FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING OF NR 2 PYLON. THE CHORD ASSEMBLY WAS REPLACED IAW BOEING DRAWING 65B90413 AND SRM 51-10-01.
- [SDR CALA9700020](https://openairdocs.org/sdr/CALA9700020.md): Bulkhead · cracked · Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION FOUND A.125 INCH CRACK AT NR 3 PYLON FASTENER HOLE COMMON TO THE AFT BULKHEAD VERTICAL CHORD LT FITTING. THE NR 3 PYLON LT BULKHEAD ASSEMBLY WAS REPLACED IAW SRM 51-10-01 AND BOEING DRAWING 65B90413.
- [SDR CALA9700019](https://openairdocs.org/sdr/CALA9700019.md): Bulkhead · cracked · Oct 26, 1996 · N17025 · Boeing 747238B · Nacelle/Pylon, Bulkhead/Firewall
  > INSPECTION FOUND A 2 INCH CRACK AT UPPER POSITION OF NR 4 PYLON AFT BULKHEAD INBOARD CHORD. THE CHORD AND AFT BULKHEAD ASSEMBLY WERE REPLACED IAW SRM 57-10-01 AND SB 747-54A2159.

## 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 = 'N17025' AND deregistration_id = 'N17025-2003-07-11'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N17025-2003-07-11/reports

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