# Service difficulty reports: N708SA, cancelled May 31, 2013

A list on [N708SA, cancelled May 31, 2013](https://openairdocs.org/deregistered/N708SA-2013-05-31.md).

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

- [SDR TX9Y20110928006](https://openairdocs.org/sdr/TX9Y20110928006.md): Valve · malfunctioned · Sep 27, 2011 · N708SA · Boeing 7472B5F · Engine (Turbine/Turboprop)
  > AIRCRAFT DEPARTED AIRPORT TO PERFORM A FUNCTIONAL TEST FLT, AFTER HEAVY CHECK. ON CLIMBOUT, ACFT DEVELOPED PROBLEMS WITH THE NR 1 ENGINE NACELLE OVERHEAT RUNNING HIGH WHICH INDICATED ON BOTH A AND B DETECTION SYSTEM INDICATORS, ALSO AT THIS TIME A "BURNING OD
- [SDR TX9Y20110924002](https://openairdocs.org/sdr/TX9Y20110924002.md): Structure · damaged · Sep 21, 2011 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main Frame
  > DURING ACCOMPLISHMENT OF SB 747-54-2230 R0, FIGURE 14 ON THE STRUT STRUCTURE ASSEMBLY AT NR 3 PYLON, CRACK DAMAGE AT NUMEROUS HOLES WAS FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND THE FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND IN THE BULKHEAD FRAMES A
- [SDR TX9Y20110924001](https://openairdocs.org/sdr/TX9Y20110924001.md): Structure · damaged · Sep 21, 2011 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main Frame
  > DURING ACCOMPLISHMENT OF SB 747-54-2230 R0, FIGURE 14 ON THE STRUT STRUCTURE ASSEMBLY AT NR 2 PYLON, CRACK DAMAGE AT NUMEROUS FASTENER HOLES WAS FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND THE FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND IN THE BULKHEAD
- [SDR TX9Y20110921002](https://openairdocs.org/sdr/TX9Y20110921002.md): Stiffener · cracked · Sep 18, 2011 · N708SA · Boeing 747200F · Nacelle/Pylon Miscellaneous Structure
  > DURING INSPECTION, CRACKS WERE FOUND ON THE VERTICAL AND HORIZONTAL FLANGES OF NR 2 PYLON RT STIFFENERS (P/N:65B90415-6/-8) NEAR NAC STA 228. FOLLOWING REMOVAL OF THE DAMAGED STIFFENER SECTION, THE BULKHEAD STRAP (P/N:65B90412-38) WAS FOUND CRACKED AT A STIFF
- [SDR TX9Y20110921001](https://openairdocs.org/sdr/TX9Y20110921001.md): Frame · damaged · Sep 18, 2011 · N708SA · Boeing 7472B5F · Fuselage Main, Frame
  > DURING INSPECTION, A DAMAGE WAS FOUND COMMONT TO A TOOL HOLE OF BULKHEAD AT STA1140, S-18R TO S-19R. AND NO ALLOWANCE DAMAGE LIMIT WAS PROVIDED IN SRM. A REPAIR THAT BLENDED OUT THE DAMAGED FRAME WEB AT A TOOLING HOLE AND REFINISHED THE SURFACE PER BOEING ME
- [SDR TX9Y20110920001](https://openairdocs.org/sdr/TX9Y20110920001.md): Frame · none · Sep 17, 2011 · N708SA · Boeing 747200F · Fuselage Main, Frame
  > DURING PERFORMING THE INSP OF FUSLAGE-TAIL SECTION BS 2598 BULKHEAD FWD & AFT INNER CHORD IAW SB 747-53A2427, R5, AN EXISTING REPAIR ANGLE SIMILAR WITH SRM 53-10-04, FIGURE 72 COMMON TO AFT INNER CHORD LT SIDE ONLY AT WL 320 WAS FOUND INTERFERE THE INSP PERFOR
- [SDR TX9Y20110915001](https://openairdocs.org/sdr/TX9Y20110915001.md): Shear Web · cracked · Sep 12, 2011 · N708SA · Boeing 747200F · Fuselage Miscellaneous Structure
  > CRACKS WERE FOUND ON STA 820 LT AND RT SLOPING SHEAR WEB RESPECTIVELY. REPAIR THAT REPLACES THE SLOPING SHEAR WEBS WAS PERFORMED PER BOEING MESSAGE NUMBER TEC-SOF-11-0023 AND SRM 51-00-06. THE DEVIATION WAS APPROVED UNDER BOEING SERVICE REQUEST 1-1969006948 O
- [SDR TX9Y20110914001](https://openairdocs.org/sdr/TX9Y20110914001.md): Intercostal · cracked · Sep 11, 2011 · N708SA · Boeing 747200F · Fuselage Miscellaneous Structure
  > RT SIDE STATION 1220 OVERWING INTERCOSTAL WEB WAS FOUND HAVING CRACKS AND NEED TO BE REPLACED IN ACCORDANCE WITH PARAGRAPH 3B, WORK INSTRUCTIONS OF SB-747-53A2750. FOUND 2EA CRACKS ON STA 1220 INTERCOSTAL LOWER CHORD. THE INTERCOSTAL LOWER CHORD WAS REPLACED
- [SDR TX9Y20110913001](https://openairdocs.org/sdr/TX9Y20110913001.md): Stringer · corroded · Sep 10, 2011 · N708SA · Boeing 747200F · Fuselage Main, Longeron/Stringer
  > BULK CARGO BILGE AREA STA 1960 - STA 1980 S-51R STRINGER FOUND CORROSION. THE CORROSION PART OF THE STRINGER WAS CUT AND REMOVED PER SRM 53-10-03, REV 120. A REPAIR PART WAS MADE LOCALLY AND INSTALLED PER SRM 53-10-03, REV 120. AFTER REPAIR, CAT B REPAIR SU
- [SDR TX9Y20110901001](https://openairdocs.org/sdr/TX9Y20110901001.md): Skin · misrepaired · Aug 29, 2011 · N708SA · Boeing 747200F · Fuselage Main, Plate/Skin
  > THERE ARE 2 EXISTING SKIN REPAIRS FOUND ON 65B14221-37 SKIN ASSY AT STA 140 TO 160. FOUND SIX DEVIATIONS ON THESE 2 SKIN REPAIRS REF TO 747-200 SRM 53-30-03. THE EXISTING REPAIRS WERE REMOVED. PER BOEING MESSAGE NUMBER TEC-SOF-11-0022, NEW INTERNAL DOUBLERS
- [SDR Q2SA708003](https://openairdocs.org/sdr/Q2SA708003.md): Hydraulic Line · ruptured · Aug 25, 2010 · N708SA · Boeing 7472B5F · Hydraulic System, Main
  > SHORTLY AFTER TAKEOFF THE CREW CALLED IN TO NOTIFY, HAD LEFT BODY GEAR PRIMARY/ALT LIGHT ON PER QRH AND ARE RETURNING TO ORD, 110 THOUSAND POUNDS OF FUEL WAS DUMPED AS A PRECAUTION BEFORE LANDING. DURING GROUND INSPECTION, MAINTENANCE WAS UNABLE TO IDENTIFY A
- [SDR 2010FA0000437](https://openairdocs.org/sdr/2010FA0000437.md): Skin · cracked · Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > NR 3 ENG PYLON AFT LWR SPAR FIREWALL SKIN 1.5 INCH CRACK.
- [SDR 2010FA0000436](https://openairdocs.org/sdr/2010FA0000436.md): Skin · cracked · Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > NR 3 ENG LT PYLON ACCESS PANEL CRACKED.
- [SDR 2010FA0000435](https://openairdocs.org/sdr/2010FA0000435.md): Door · cracked · Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main Frame
  > NR 2 PYLON LT SIDE PRESSURE RELIEF DOOR CRACK (0.35 INCH).
- [SDR 2010FA0000438](https://openairdocs.org/sdr/2010FA0000438.md): Skin · dented · Apr 5, 2010 · N708SA · Boeing 7472B5F · Auxiliary Power Unit (APU) Doors
  > APU LT ACCESS DOOR SKIN DENT. INSTALL EXTERNAL REPAIR DOUBLER.
- [SDR 2010FA0000434](https://openairdocs.org/sdr/2010FA0000434.md): Skin · cracked · Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > NR 3 ENG LT SIDE COWL SKIN CRACK. INSTALL EXTERNAL REPAIR DOUBLER.
- [SDR 2010FA0000433](https://openairdocs.org/sdr/2010FA0000433.md): Stiffener · cracked · Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon Miscellaneous Structure
  > CRACK WAS FOUND ON THE STIFFENER OF THE NR 3 PYLON. INSTALLATION SPLICE REPAIR ANGLES.
- [SDR 2010FA0000432](https://openairdocs.org/sdr/2010FA0000432.md): Skin · cracked · Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > NR 4 PYLON AFT FAIRING DOOR LT SIDE CRACKED. BONDING EXTERNAL REPAIR DOUBLER.
- [SDR 2010FA0000431](https://openairdocs.org/sdr/2010FA0000431.md): Longeron · cracked · Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Longeron/Stringer
  > NR 3 ENG LT SIDE COWL UPPER LONGERON CRACK. INSTALL REPAIR DOUBLER.
- [SDR 2010FA0000360](https://openairdocs.org/sdr/2010FA0000360.md): Skin · worn · Aug 8, 2008 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > (KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 4 PYLON AT NAC STA 210.00-221.90 NAC WL 187.63-190.68.
- [SDR 2010FA0000359](https://openairdocs.org/sdr/2010FA0000359.md): Skin · worn · Aug 8, 2008 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/Skin
  > (KADY) WEAR DAMAGE WAS FOUND ON THE CAP SKIN OF THE NR 1 PYLON AT NAC STA 210.00-221.90 WL 187.63-190.60.
- [SDR 2010FA0000358](https://openairdocs.org/sdr/2010FA0000358.md): Frame · cracked · Aug 5, 2008 · N708SA · Boeing 7472B5F · Fuselage Main, Frame
  > (KADY) A CRACK WAS FOUND ON THE FRAME AT STA 1680, S13R-S14R.
- [SDR 2010FA0000357](https://openairdocs.org/sdr/2010FA0000357.md): Floorbeam · damaged · Aug 5, 2008 · N708SA · Boeing 7472B5F · Fuselage Main, Floor Beam
  > (KADY) AN ELONGATED FASTENER HOLE WAS FOUND ON THE UPPER DECK FLOORBEAM UPPER CHORD AT STA 380, LBL 22/12.
- [SDR Q2SA708001](https://openairdocs.org/sdr/Q2SA708001.md): Fuel Control · malfunctioned · Apr 7, 2008 · N708SA · Boeing 7472B5F · Fuel Control/Reciprocating Engines
  > ATB AT ANC DUE TO ENGINE PROBLEM. NR 4 ENGINE STALLED DURING CLIMB AT 33,600 FT. REDUCED THRUST TO IDLE. IDLE PARAMETERS N1 37 PERCENT, N2 61 PERCENT, EPR ERRATIC, EGT 483, FF 800. ALL BLEEDS ON, 2 AIR CONDITIONING PACKS ON. 2 AIR CONDITIONING PACKS ON. R

## 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 = 'N708SA' AND deregistration_id = 'N708SA-2013-05-31'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N708SA-2013-05-31/reports

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