N708SA, cancelled May 31, 2013

Service difficulty reports · 24

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

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR TX9Y20110928006Valve · malfunctionedAIRCRAFT 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 ODSep 27, 2011 · N708SA · Boeing 7472B5F · Engine (Turbine/Turboprop)SDR TX9Y20110924002Structure · damagedDURING 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 ASep 21, 2011 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main FrameSDR TX9Y20110924001Structure · damagedDURING 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 BULKHEADSep 21, 2011 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main FrameSDR TX9Y20110921002Stiffener · crackedDURING 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 STIFFSep 18, 2011 · N708SA · Boeing 747200F · Nacelle/Pylon Miscellaneous StructureSDR TX9Y20110921001Frame · damagedDURING 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 MESep 18, 2011 · N708SA · Boeing 7472B5F · Fuselage Main, FrameSDR TX9Y20110920001Frame · noneDURING 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 PERFORSep 17, 2011 · N708SA · Boeing 747200F · Fuselage Main, FrameSDR TX9Y20110915001Shear Web · crackedCRACKS 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 OSep 12, 2011 · N708SA · Boeing 747200F · Fuselage Miscellaneous StructureSDR TX9Y20110914001Intercostal · crackedRT 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 REPLACEDSep 11, 2011 · N708SA · Boeing 747200F · Fuselage Miscellaneous StructureSDR TX9Y20110913001Stringer · corrodedBULK 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 SUSep 10, 2011 · N708SA · Boeing 747200F · Fuselage Main, Longeron/StringerSDR TX9Y20110901001Skin · misrepairedTHERE 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 DOUBLERSAug 29, 2011 · N708SA · Boeing 747200F · Fuselage Main, Plate/SkinSDR Q2SA708003Hydraulic Line · rupturedSHORTLY 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 AAug 25, 2010 · N708SA · Boeing 7472B5F · Hydraulic System, MainSDR 2010FA0000437Skin · crackedNR 3 ENG PYLON AFT LWR SPAR FIREWALL SKIN 1.5 INCH CRACK.Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000436Skin · crackedNR 3 ENG LT PYLON ACCESS PANEL CRACKED.Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000435Door · crackedNR 2 PYLON LT SIDE PRESSURE RELIEF DOOR CRACK (0.35 INCH).Apr 6, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Main FrameSDR 2010FA0000438Skin · dentedAPU LT ACCESS DOOR SKIN DENT. INSTALL EXTERNAL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5F · Auxiliary Power Unit (APU) DoorsSDR 2010FA0000434Skin · crackedNR 3 ENG LT SIDE COWL SKIN CRACK. INSTALL EXTERNAL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000433Stiffener · crackedCRACK WAS FOUND ON THE STIFFENER OF THE NR 3 PYLON. INSTALLATION SPLICE REPAIR ANGLES.Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon Miscellaneous StructureSDR 2010FA0000432Skin · crackedNR 4 PYLON AFT FAIRING DOOR LT SIDE CRACKED. BONDING EXTERNAL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000431Longeron · crackedNR 3 ENG LT SIDE COWL UPPER LONGERON CRACK. INSTALL REPAIR DOUBLER.Apr 5, 2010 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Longeron/StringerSDR 2010FA0000360Skin · worn(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.Aug 8, 2008 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000359Skin · worn(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.Aug 8, 2008 · N708SA · Boeing 7472B5F · Nacelle/Pylon, Plate/SkinSDR 2010FA0000358Frame · cracked(KADY) A CRACK WAS FOUND ON THE FRAME AT STA 1680, S13R-S14R.Aug 5, 2008 · N708SA · Boeing 7472B5F · Fuselage Main, FrameSDR 2010FA0000357Floorbeam · damaged(KADY) AN ELONGATED FASTENER HOLE WAS FOUND ON THE UPPER DECK FLOORBEAM UPPER CHORD AT STA 380, LBL 22/12.Aug 5, 2008 · N708SA · Boeing 7472B5F · Fuselage Main, Floor BeamSDR Q2SA708001Fuel Control · malfunctionedATB 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. RApr 7, 2008 · N708SA · Boeing 7472B5F · Fuel Control/Reciprocating Engines
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