N760SA, cancelled Oct 30, 2017

Service difficulty reports · 41

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 = 'N760SA' AND deregistration_id = 'N760SA-2017-10-30'
  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 Q2SA2012042876002Engine · damagedNUMBER FOUR ENGINE STALLED DURING CLIMB AND FLAP CLEAN UP. AT APPROXIMATELY 3000 FEET THE CREW PULLED THE THRUST LEVER BACK TO BREAK THE ENGINE STALL. THEY THEN CONTINUED TO CLEAN UP AND ACCELERATE TO VZ + 100 TILL 10,000 FEET. AFTER PASSING 10,000 FEET THEApr 28, 2012 · N760SA · Boeing 747230B · Engine (Turbine/Turboprop)SDR TX9Y20111021001Post · crackedA CRACK WAS FOUND COMMON TO FWD CARGO SUPPORT POST AT MAIN DECK BS 560 FLOORBEAM DURING INSPECTION. SECTION OF POST ENCOMPASSING THE CRACK WAS TRIMMED AWAY, AND REPAIRED IAW SRM D6-13592 REV 120 SUBJECT 53-10-07 FIGURE 7 WAS INSTALLED.Oct 21, 2011 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR TX9Y20110928005Skin · crackedDURING MAINTENANCE, NR 1 NACELLE SKIN WAS FOUND CRACKED AT LATCH AREA. THE CRACK IS ABOUT 0.8 IN LENGTH. REMOVED THE DAMAGE BY TRIMMING THE SKIN ASSEMBLY PER SRM 51-10-01. NDT INSPECTED TRIMMED AREA, NO CRACKS FOUND. FABRICATED AND INSTALLED NEW REPAIR FILSep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR TX9Y20110928004Strut · crackedDURING PERFORMING NR 3 PYLON STRUT CAP SKIN INSPECTION AND MODIFICATION AS PER SB 747-54A2230 R0, CRACK DAMAGE AT NUMEROUS HOLES WERE FOUND IN THE CAP SKIN ASSEMBLY, THE BULKHEAD STRAP AND FRONT SPAR CHORD. DAMAGE WAS ALSO FOUND AT THE BULKHEAD FORWARD FRAMES Sep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Main FrameSDR TX9Y20110928003Bulkhead · crackedDURING INSPECTION OF THE NR 4 PYLON STA 286 BULKHEAD PER SB 747-54A2202 REV 01, 1EA 0.50 INCHES LONG CRACK WAS FOUND COMMON TO THE FRAME. REPAIRED PER SR 1-1535936828.Sep 28, 2011 · N760SA · Boeing 747230B · Nacelle/Pylon, Bulkhead/FirewallSDR TX9Y20110928002Structure · corrodedLEFT WING I/B T/E AFT FLAP CONER FOUND HEAVY CORROSION. REPLACE THE LT WING I/B T/E AFT FLAP AS PER AMM 27-51-03.Sep 26, 2011 · N760SA · Boeing 747230B · Trailing Edge FlapsSDR TX9Y20110928001Bear Strap · corrodedFWD CARGO BS 550-570, STRINGER 46R BEAR STRAP FOUND CORRODED. BEAR STRAP WAS TRIMMED OUT AND INSTALLED REPAIR DOUBLERS AND FILLER, AND SPLICED A NEW SEGMENT OF STRINGER AT S46R. THIS REPAIR WAS ACCOMPLISHED IAW BSR 1-1990327420.Sep 26, 2011 · N760SA · Boeing 747230B · Fuselage Main, Plate/SkinSDR TX9Y20110922005Doubler · corrodedFUSELAGE BS 980-1000 WATER SERVICE PORT AREA DOUBLER FOUND CORROSION. FABRICATE AND INSTALL THE NEW DOUBLER (P/N:65B09637-1) AS PER BOEING DRAWING 65B09637.Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR TX9Y20110922004Bear Strap · corrodedFUSELAGE BS 540-560 FWD LAV SERVICE PANEL CUT OUT SKIN FOUND CORROSION. DURING INSPECTION OF THIS DATUM AIRPLANE, CORROSION WAS FOUND ON THE BEAR STRAP (P/N: 65B07201-2) AT FWD LAVATORY SERVICE PANEL CUTOUT AT STA560, STRINGER 46R. THE DAMAGED BEAR STRAP WASSep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Plate/SkinSDR TX9Y20110922003Floorbeam · corrodedAFT CARGO BS 1800 RBL 58 FLOORBEAM FOUND CORROSION. FABRICATE AND INSTALL THE FLOORBEAM CHORD (P/N:65B04327-71) AS PER BOEING DRAWING 65B04327.Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Floor BeamSDR TX9Y20110922002Frame · corrodedAFT CARGO BS 1920 RT FRAME INNER CHORD FOUND CORROSION. REMOVE THE CORROSION AS PER SRM 51-10-01. CHECK THE ALLOWABLE WITHIN SRM LIMIT AS PER SRM 53-10-01.Sep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR TX9Y20110922001Stringer · corrodedDURING INSPECTION OF THIS DATUM AIRPLANE, THE STRINGER 51R (P/N: 65B04483-13) IS FOUND HEAVILY CORRODED ON THE INBOARD SIDE WEB FLANGE AT STA 1958. THE STRINGER AFT END WAS TRIMMED AND A REPAIR SPLICE CHANNEL SIMILAR WITH THE ORIGINAL ONE, BUT WITH EXTENDED CSep 20, 2011 · N760SA · Boeing 747230B · Fuselage Main, Longeron/StringerSDR Q2S2010F00034Floor Support · crackedWS NR 0978, WC NR 53-520-01-01- FWD CARGO COMPARTMENT AT STA 570, RBL 44 FOUND FLOOR SUPPORT FRAME WEB CRACKED. CRACKED FLOOR SUPPORT WEB REMOVED IAW SRM 51-30-02, REV 116. NEW FLOOR SUPPORT WEB FASTENER HOLES TRANSFERRED AND INSTALLED IAW SRM 51-30-05 AND 5Mar 4, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00042Spar · corrodedWS NR 0912, WC NR 57-910-01-01. RT WING L/E FRONT SPAR LOWER CHORD AT OLES 1356 FOUND CORROSION. RT WING LOWER SKIN CORROSION AREA CUT AND REMOVED IAW SRM 57-30-03, FIG 9 REV 116 AT FRONT SPAR OLES 1356 TO 1362. HFEC CARRIED OUT AND FUND NO CRACK EVIDENT. Mar 3, 2010 · N760SA · Boeing 747230B · Wing SparSDR Q2S2010F00033Frame · crackedWS NR 0924, WC-SAI EAO NR 4754020R1. NR 4 PLYON INBD REAR EANGINE MOUNT BULKHEAD INBD LOWER CHORD FWD CRACKED. REPAIR CARRIED OUT IAW EN:1014-10, FORM 8100-9, DATED 19 MARCH 2009 ISSUED FOR THE REPAIRED.Mar 3, 2010 · N760SA · Boeing 747230B · Nacelle/Pylon, Frame/Spar/RibSDR Q2S2010F00039Hinge · crackedWS NR 0896, WC NR 57-940-01-01. RT WING T/E NR 8 SPOILER CTR HINGE AREA FOUND CRACKED BETWEEN FASTENERS. RT WING T/E NR 8 SPOILER REPLACED IAW AMM 27-61-01, REV 142. PN 65B02300-1, SN 000074.Mar 2, 2010 · N760SA · Boeing 747230B · SpoilersSDR Q2S2010F00036Intercostal · crackedWS 0907, WC SAI EAO NR 4753028-R2. NLG TORQUE BOX TOP SIDE (PRESSURIZED COMPARTMENT) FOUND INTERCOSTAL CRACKED AT RBL 12, BS 320. CRACKED INTERCOASTAL REMOVED IAW SRM 51-30-02, REV 116. NEW INTERCOSTAL FABRICATED IAW DWG 65B13792 AND FPI CARRIED OUT. NEW FMar 2, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00045Floorbeam · damagedWS 0784, WC SAI NR 4753119, HFEC OPEN HOLE FOUND 07 HOLES ELONGATED ON UPPER DECK FLOORBEAM AT BS 520, FROM RBL 0 TO RBL 35 FWD CHORD. DAMAGED UPPER CHORD TRIMMED OUT FORM LBL 54 TO RBL 54 IAW SRM 53-10-07, FIG 13, REV 116. HFEC INSP CARRIED OUT ON TRIMMED OMar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, Floor BeamSDR Q2S2010F00044Mount · crackedWS NR 0844, WC SAI NR 4754020R1. NR 1 PYLON AFT ENGINE MOUNT INBD UPPER CHORD FOUND CRACKED. REPAIR CARRIED OUT IAW EN 1013-10. FORM 8100-9, DATED 19 MARCH 2010 ISSUED FOR THE REPAIRED.Mar 1, 2010 · N760SA · Boeing 747230B · Engine Mount SectionSDR Q2S2010F00043Skin · corrodedWS NR 0827, WC NR 53-176-02-01. LOWER FUSELAGE SKIN AT STA 1504, STRINGER 26L FOUND SKIN CORROSION. REPAIR CARRIED OUT IAW EN NR 1010-10. FORM 8100-9, DATED 22, MARCH 2010 ISSUED FOR THE REPAIRED.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, Plate/SkinSDR Q2S2010F00041Bear Strap · corrodedWS NR 0809, WC NR SAI EAO NR 4753028R2. MAIN ENTRY DOOR NR 3 RIGHT CUT OUT AFT TOP SIDE FOUND CORROSION. REPAIR CARRIED OUT IAW EN NR 1019-10. FORM 8100-9, DATED 29, MARCH 2010 ISSUED FOR THE REPAIRED.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, Plate/SkinSDR Q2S2010F00029Frame · corrodedWORKSHEET NR 0823, WORKCARD NR 53-176-02-01. LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00028Frame · corrodedWORKSHEET NR 0824, WORKCARD NR 53-176-02-01. LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 920 FOUND CORROSION. REPALCED FRAME ASSY IAW SRM 51-30-02, REV 116.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00024Frame · corrodedWOKSHEET NR 0821, WORKCARD NR 53-176-02-01, LOWER FUSELAGE RT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00023Plate · crackedWORKSHEET NR 0810, WORKCARD NR 4753028R2. MAIN DECK, FWD OF MAIN ENTRY DOOR L1 CUT OUT FOUND DOUBLER PLATE CRACKED AT STA 430, STR 23L. REPLACED NEW STRAP IAW SRM 51-30-02, REV 116. PN ON : 141U1050-193.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00022Frame · corrodedWORKSHEET NR 0819, WORKCARD NR 53-176-02-01, LOWER FUSELAGE LT BODY FAIRING SUPPORT AT STA 880 FOUND CORROSION. REPLACED FRAME ASSY IAW SRM 51-30-02, REV 116.Mar 1, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00026Floor Support · crackedWORKSHEET NR 0743. WORKCARD NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 23 FOUND FLOOR SUPPORT FRAME WEB CRACKED. DAMAGED AREA TRIMMED IAW SRM 51-40-03 FIGURE 1 REVISION 116. FABRICATED REPAIR CHANNEL AND FILLER IAW SRM 51-40-03, FIG 1 REVISION 1Feb 28, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00025Floor Support · crackedWORKSHEET NR 0745, WORKCARD REF NR 53-520-01-01. FWD CARGO COMPARTMENT AT STA 570, LBL 44 FOUND FLOOR SUPPORT FRAME WEB CRACKED. CRACKED FLOOR SUPPORT WEB REMOVED IAW SRM 51-30-02 REV 116. NEW FLOOR SUPPORT WEB FASTENER HOLES TRANSFERRED AND INSTALLED IAW SFeb 28, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00030Frame · crackedWORKSHEET NR 0654, WORKCARD NR 54-410-01-01. PRESSURE BULKHEAD FWD FACE/TOP LT RING FRAME (FACING THE FWD FACE) AT BS 134 FOUND CRACKED AT TOP MOST CORNER. CRCKED RING FRAME REMOVED IAW SRM 51-30-02, REV 116. NEW RING FRAME FABRICATED IAW DWG 65B01700, HEATFeb 27, 2010 · N760SA · Boeing 747230B · Fuselage Main, FrameSDR Q2S2010F00038Spar · corrodedWS NR 0630, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD EXTENSION AT APPROX OLES 1361 FOUND CORROSION. REPAIR CARRIED OUT IAW EN 1020-10. FORM 8100-9, DATED 22 MARCH 2010 ISSUED FOR THE REPAIRED.Feb 26, 2010 · N760SA · Boeing 747230B · Wing SparSDR Q2S2010F00035Spar · corrodedWS NR 0631, WC NR 57-830-01-01. LT WING L/E FRONT SPAR LOWER CHORD AT APPROX OLES 1305 FOUND EXFOLIATION. REPAIR CARRIED OUT IAW EN NR 1020-10. FORM 8100-9 DATED 22, MARCH 2010 ISSUED FOR THE REPAIRED.Feb 26, 2010 · N760SA · Boeing 747230B · Wing SparSDR Q2S2010F00027Web · crackedWORKSHEET NR 0620, WORKCARD NR 53-850-01-01. AFT CARGO COMPARTMENT AT STA 1850, RBL 28 FOUND LATERAL GUIDE SUPPORT WEB CRACKED. CRACKED SUPPORT WEB REMOVED IAW SRM 51-30-02 REV 116. NEW SUPPORT WEB FABRICATED IAW DWD 69B03257. NEW FABRICATED SUPPORT WEB HEFeb 26, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00020Strap · corrodedWORKSHEET NR 0628, WORKCARD 57-830-01-01. LT WING L/E FRONT SPAR UPPER CHORD STRAP AT APPROX OLES 1481 FOUND CORROSION. CORRODED STRAP REPLACED IAW SRM 51-30-02 REV 116. PN ON: 65B016877.Feb 26, 2010 · N760SA · Boeing 747230B · Wing SparSDR Q2S2010F00040Pressure Panel · crackedWS NR 0437, WC NR 53-842-01-01. LT BODY LANDING GEAR WHEEL WELL AT ABOUT STA 1480 ABOVE ANTI-SKID VALVE MODULE FOUND PRESSURE DECK WEB CRACKED. REPAIR CARRIED OUT IAW EN NR 1011-10, FORM 8100-9, DATED 22 MARCH 2010 ISSUED FOR THE REPAIRED.Feb 25, 2010 · N760SA · Boeing 747230B · Fuselage Floor PanelSDR Q2S2010F00021Mount · corrodedWORKSHEET NR 0435, WORKCARD NR 71-012-01-03, ENGINE NR 3 AFT UPPER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT UPPER MOUNT IAW AMM 71-21-03, REV 142. PN ON: 65B94349-1, SN ON: SA-982.Feb 25, 2010 · N760SA · Boeing 747230B · Engine Mount SectionSDR Q2S2010F00019Mount · corrodedENGINE NR 3 AFT LOWER MOUNT FOUND WITH CORROSION. REPLACED ENGINE NR 3 AFT LOWER MOUNT IAW AMM 71-21-04, REV 142. PN ON: 65B94350-5, SN ON: P181R.Feb 25, 2010 · N760SA · Boeing 747230B · Engine Mount SectionSDR Q2S2010F00032Floor Support · crackedWORKSHEET NR 0292, WORKCARD NR 53-550-02-01. AFT CARGO COMPARTMENT, LT NR 3 PDU SUPPORT WEB AT STATION 1600 TO 1620, LBL 44 FOUND CRACKED. CRACKED FLOOR SUPPORT WEB, REMOVED IAW SRM 51-30-02 REV 116. NEW FLOOR SUPPORT WEB FASTENER HOLES TRANSFERRED AND INSTFeb 24, 2010 · N760SA · Boeing 747230B · Fuselage Miscellaneous StructureSDR Q2S2010F00031Skin · damagedWORKSHEET NR 0127, WORKCARD NR SAI RNR 4753078. FUSELAGE-CURRENTLY 02 EXISTING DOUBLERS FOUND SIDE BY SIDE AT BS 520 TO 550, STRINGER 34R TO 36R. REPAIR CARRIED OUT IAW SASCO EN 1012-10. FORM 8100-9, DATED 18 MARCH 2010.Feb 24, 2010 · N760SA · Boeing 747230B · Fuselage Main, Plate/SkinSDR Q2S2010F00037Hinge · crackedWS NR 0066, WC NR 57-530-01-01. LT WING NR 6 GROUND SPOILER LOWER SURFACE FOUND CRACKED AT INBD OF ACTUATOR LUG HINGE ALONG FASTENERS. LT WING NR 6 GROUND SPOILER REPLACED IAW AMM 27-61-01, REV 142. PN 65B023101. SN 001395.Feb 23, 2010 · N760SA · Boeing 747230B · SpoilersSDR Q2SA760001Flex Duct · crackedON TAKEOFF CLIMBOUT OF EBLG ENGINE FIRE WARNING CAME ON FOR ENGINE NR 2, CREW ELECTED TO SHUTDOWN ENGINE NR 2, DUMPED 77,000 LBS OF FUEL, RETURNED TO AND LANDED SAFELY AT EBLG. AFTER LANDING MAINTENANCE CREW IN EBLG INSPECTED ENGINE NR 2 AND FOUND A CRACKED POct 30, 2009 · N760SA · Boeing 747230B · Pneumatic Distribution SystemSDR 2007FA0000228Sensor · malfunctionedDURING TAKEOFF, THE LANDING GEAR HANDLE WILL NOT GO TO UP OR RETRACT POSITION. AIRCRAFT RETURNED TO BASE. PERFORMED TROUBLESHOOTING ON THE LANDING GEAR SYSTEM AND FOUND THAT LT WING GEAR TRUCK ROTATION SENSOR AT FAULT. ADJUSTED THE LT WING GEAR TRUCK ROTATIMar 6, 2007 · N760SA · Boeing 747230B · Landing Gear Position and Warning
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