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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
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 ODSDR 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 ASDR 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 BULKHEADSDR 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 STIFFSDR 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 MESDR 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 PERFORSDR 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 OSDR 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 REPLACEDSDR 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 SUSDR 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 DOUBLERSSDR 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 ASDR 2010FA0000437Skin · crackedNR 3 ENG PYLON AFT LWR SPAR FIREWALL SKIN 1.5 INCH CRACK.SDR 2010FA0000436Skin · crackedNR 3 ENG LT PYLON ACCESS PANEL CRACKED.SDR 2010FA0000435Door · crackedNR 2 PYLON LT SIDE PRESSURE RELIEF DOOR CRACK (0.35 INCH).SDR 2010FA0000438Skin · dentedAPU LT ACCESS DOOR SKIN DENT. INSTALL EXTERNAL REPAIR DOUBLER.SDR 2010FA0000434Skin · crackedNR 3 ENG LT SIDE COWL SKIN CRACK. INSTALL EXTERNAL REPAIR DOUBLER.SDR 2010FA0000433Stiffener · crackedCRACK WAS FOUND ON THE STIFFENER OF THE NR 3 PYLON. INSTALLATION SPLICE REPAIR ANGLES.SDR 2010FA0000432Skin · crackedNR 4 PYLON AFT FAIRING DOOR LT SIDE CRACKED. BONDING EXTERNAL REPAIR DOUBLER.SDR 2010FA0000431Longeron · crackedNR 3 ENG LT SIDE COWL UPPER LONGERON CRACK. INSTALL REPAIR DOUBLER.SDR 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.SDR 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.SDR 2010FA0000358Frame · cracked(KADY) A CRACK WAS FOUND ON THE FRAME AT STA 1680, S13R-S14R.SDR 2010FA0000357Floorbeam · damaged(KADY) AN ELONGATED FASTENER HOLE WAS FOUND ON THE UPPER DECK FLOORBEAM UPPER CHORD AT STA 380, LBL 22/12.SDR 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. R
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