# Service difficulty reports: N67158, cancelled Aug 23, 2012

A list on [N67158, cancelled Aug 23, 2012](https://openairdocs.org/deregistered/N67158-2012-08-23.md).

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

- [SDR UALA2012F00145](https://openairdocs.org/sdr/UALA2012F00145.md): Skin · damaged · Aug 1, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN REPAIR PERFORMED IAW REO-G15199, REV A, AT FUSELAGE BS 368, AT STRINGER 31 LEFT.
- [SDR 2012FA0000521](https://openairdocs.org/sdr/2012FA0000521.md): Skin · dented · Aug 1, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1714 BETWEEN STRINGER 36 AND 37 RT. PERFORMED REPAIR IAW REO-G15177 REVB. REPAIR IS A CATEGORY A REPAIR AS DEFINED IN SRM 51-00-06.
- [SDR 2012FA0000518](https://openairdocs.org/sdr/2012FA0000518.md): Skin · dented · Jul 30, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DENTED AT BS 1898.45 ON UPPER LEFT SURFACE. REPAIRED IAW SRM 53-00-01 FIG 201.
- [SDR 2012FA0000498](https://openairdocs.org/sdr/2012FA0000498.md): Skin · misrepaired · Jul 20, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > SKIN AT BS 325 AT STRINGER 31 LT, MISREPAIRED. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.
- [SDR 2012FA0000493](https://openairdocs.org/sdr/2012FA0000493.md): Skin · misrepaired · Jul 20, 2012 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > DURING REPAIR ASSESSMENT IT WAS DETERMINED THAT SKIN AT BS 1793 BETWEEN STRINGERS 34 AND 35 LT WAS MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201.
- [SDR CALA2011052700396](https://openairdocs.org/sdr/CALA2011052700396.md): Spring · wrong part · May 26, 2011 · N67158 · Boeing 767224 · Escape Slide
  > SUPPORT TASK CABIN - R1 DOOR SLIDE DEPLOYMENT BAR AFTER POSITION SEPARATION LINK ATTACH SPRING FOUND INCORRECT PARTS. CABIN R1 DOOR SLIDE DEPLOYMENT BAR AFTER POSITION SEPARATION LINK ATTACH SPRING REPLACED AS EPR EA 2566-01036 REV A AND CMM 25-66-30.
- [SDR CALA2011051700369](https://openairdocs.org/sdr/CALA2011051700369.md): Seat Track · cracked · May 16, 2011 · N67158 · Boeing 767224 · Fuselage, Seat/Cargo Attach Fittings
  > 767-53-3-0164U CABIN - RT STA 412 RBL 20 SEAT TRACK FLANGE FOUND CRACKED. CABIN RT STA 344 TO STA 412 RBL 20 SEAT TRACK REPLACED AS PER SRM 51-10-02 AND INSTALLED AS PER SRM 51-40-02 NEW TRACK FABRICATED DETAIL REF NRC 5754156 (200-0920) ATT MAINTENANCE WORKS
- [SDR CALA2011051600366](https://openairdocs.org/sdr/CALA2011051600366.md): Floorbeam · corroded · May 15, 2011 · N67158 · Boeing 767224 · Fuselage Main, Floor Beam
  > BS 325 LBL 26 TO 55 FLOORBEAM CORRODED. REPAIRED AS PER SRM 53-00-51 REPAIR 1 FIG 201. HFEC NO CRACK FOUND.
- [SDR CALA2009080400414](https://openairdocs.org/sdr/CALA2009080400414.md): Light · inoperative · Aug 4, 2009 · N67158 · Boeing 767224 · Emergency Lighting
  > L2 DOOR THRESHOLD EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD.
- [SDR CALA2009080400413](https://openairdocs.org/sdr/CALA2009080400413.md): Light · inoperative · Aug 4, 2009 · N67158 · Boeing 767224 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FWD OF CARGO DOOR IS INOPERATIVE. RELAMPED LIGHT, OPS CHECKS GOOD.
- [SDR CALA2009051400250](https://openairdocs.org/sdr/CALA2009051400250.md): Light · inoperative · May 7, 2009 · N67158 · Boeing 767224 · Emergency Lighting
  > LEFT WING SLIDE GROUND ILLUMINATION LIGHT INOP, EXTERIOR EMERGENCY LIGHT AT STATION 1230. REPLACED EMERGENCY LIGHT ASSY, OP CHECKED GOOD PER MM 33-51-06.
- [SDR CALA2008112401097](https://openairdocs.org/sdr/CALA2008112401097.md): Skin · gouged · Nov 23, 2008 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > LIGHTNING STRIKE DAMAGE AT 4 LOCATIONS SEE L/P 8072815 STA 111, 129, 412 STA 111 S-30 DMG DIAM 0.184 IN RIVET HEAD DMG 0.066 IN. STA 129 S-30 DMG DIAM 0.170 IN RIVET HEAD DMG 0.056 IN. STA 412 S-30 DMG DIAM 0.147 IN RIVET HEAD DMG 0.071IN. WITHIN LIMITS PER
- [SDR CALA2008112401096](https://openairdocs.org/sdr/CALA2008112401096.md): Skin · gouged · Nov 23, 2008 · N67158 · Boeing 767224 · Fuselage Main, Plate/Skin
  > FOUND FASTENER AT STA 368 AROUND S-30 DAMAGED BY LIGHTNING STRIKE. TOTAL DAMAGE 0,250 IN RIVET HEAD DAMAGE 0,091 IN. PER SRM 53-00-01 P103 TABLE III DETAIL IV NEEDS FASTENER REPLACEMENT WITHIN 50 FLIGHT CYCLES. PERFORMED INTERIM REPAIR PER PART 1-2. PERFORM
- [SDR CALA2008112401095](https://openairdocs.org/sdr/CALA2008112401095.md): Support · corroded · Nov 23, 2008 · N67158 · Boeing 767224 · Fuselage Main, Floor Beam
  > CABIN - BS 325 LBL 27- LBL 60 FLOOR SUPPORT FOUND CORRODED. CABIN BS 325 LBL 16- LBL 62 FLOORBEAM SUPPORT REPAIRED PER SRM 53-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND.
- [SDR CALA2008112401089](https://openairdocs.org/sdr/CALA2008112401089.md): Floorbeam · corroded · Nov 21, 2008 · N67158 · Boeing 767224 · Fuselage Main, Floor Beam
  > CABIN - BS 303 LBL 26-44 FLOOR SUPPORT FOUND CORRODED. CABIN - BS 303 LBL 7 TO LBL 62 FLOOR SUPPORT BEAM UPPER FLANGE REPAIRED PER SRM 33-00-51 REPAIR 1, FIG 201. HFEC NO CRACK FOUND.
- [SDR CALA0600286](https://openairdocs.org/sdr/CALA0600286.md): Floorbeam · corroded · Jul 31, 2006 · N67158 · Boeing 767224 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT BS 325, LBL 30-60. THE FLOORBEAM WAS REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.
- [SDR CALA0600284](https://openairdocs.org/sdr/CALA0600284.md): Stiffener · cracked · Jul 31, 2006 · N67158 · Boeing 767224 · Nacelle/Pylon, Main Frame
  > INSPECTION FOUND NR 2 PYLON I/B CLIP, FRAME, AND STIFFENER CRACKED AT STA 275. THE CLIP, FRAME, AND STIFFENER WERE REPLACED IAW SRM 51-10-02.
- [SDR CALA0600285](https://openairdocs.org/sdr/CALA0600285.md): Floorbeam · corroded · Jul 21, 2006 · N67158 · Boeing 767224 · Fuselage Main, Floor Beam
  > INSPECTION FOUND FLOORBEAM CORRODED AT BS 303, LBL 25-60. REPAIRED IAW SRM 53-00-51, FIGURE 201, REPAIR 1.
- [SDR CALA0600262](https://openairdocs.org/sdr/CALA0600262.md): Floor Support · corroded · Jul 20, 2006 · N67158 · Boeing 767224 · Fuselage Miscellaneous Structure
  > INSPECTION FOUND FLOOR SUPPORT CORRODED AT BS 303-325, LBL 32. THE FLOOR SUPPORT WAS REPLACED IAW SRM 51-10-02 AND 51-40-02.
- [SDR CALA0600283](https://openairdocs.org/sdr/CALA0600283.md): Skin · cracked · Jul 6, 2006 · N67158 · Boeing 767224 · Nacelle/Pylon, Plate/Skin
  > INSPECTION FOUND NR 2 PYLON I/B MID-SPAR AREA ONE EACH FASTENER HOLE HAD A 0.06" CRACK IN SKIN AT STA 285. THE SKIN WAS REPAIRED IAW ECRA 5430-01784.
- [SDR CALA050110](https://openairdocs.org/sdr/CALA050110.md): Engine · failed · Apr 18, 2005 · N67158 · Boeing 767224 · Engine (Turbine/Turboprop)
  > ON TAKEOFF, AT APPROXIMATELY 90 KNOTS, RT ENGINE FAILED. REPLACED ENGINE.

## 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 = 'N67158' AND deregistration_id = 'N67158-2012-08-23'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N67158-2012-08-23/reports

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