Boeing 747-230B

Service difficulty reports · 618

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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 aircraft_model_key = '747230B'
  ORDER BY difficulty_date DESC"

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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 EIAA20120404037Battery Pack · dirtyEMERGENCY EXIT SLIDE LIGHTS UPPER DECK LEFT DOOR SILL INOPERATIVE. REMOVED BATTERY CLEANED BATTERY PACK X631 CONTACTS AND RE-INSTALLED PER B747 MM 33-51-04 PG 204-205, OPS CHECK GOOD.Apr 4, 2012 · N489EV · Boeing 747230B · Emergency LightingSDR EIAA20120404036Floorbeam · crackedUPPER DECK FLOORBEAM VERTICAL WEB CRACKED AT UPPER AND LOWER END BS 420 RBL 80. REMOVED DAMAGE FABRICATED AND INSTALLED REPAIR PER SRM 53-10-07 PG. 47-50A.Apr 4, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120403035Access Panel · gougedNR 3 PYLON RT SIDE INSIDE ACCESS PANEL 473AR DEEP GOUGE JUST UNDER CUT OUT. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-020-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Main FrameSDR EIAA20120403034Skin · damagedNR 2 PYLON RT FRAMES STA 259 AND 234, RT SKIN BELOW LOUVER CUTOUT ARE HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120403033Skin · damagedNR 4 PYLON RT BETWEEN FRAMES STA 248 AND 259, RT INTERNAL SKIN AT STIFFENER 2 TO 4 AND FRAMES HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120403032Skin · damagedNR 2 PYLON RT BETWEEN FRAMES STA 259 AND 270, RT SKIN BETWEEN STIFFENERS 2 AND 3 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120403031Skin · damagedNR 1 PYLON RT BETWEEN FRAMES STA 234 AND 270, RT INTERNAL SKIN BETWEEN STIFFENERS 2 AND 4 HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120403030Skin · damagedNR 3 PYLON RT BETWEEN FRAMES STA 234 AND 248, RT INTERNAL SKIN AT STIFFENER 3 AND STIFFENER HEAT DAMAGED. REMOVED DAMAGE, FABBED REPAIR PARTS AND INSTALLED PER ECRA 489-54-025-2.Apr 3, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120402029Battery · dischargedTWO EA UPPER DECK EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERIES WITH SERVICEABLE.Apr 2, 2012 · N489EV · Boeing 747230B · Emergency LightingSDR EIAA20120402028Skin · damagedNR 3 PYLON SKIN CAP DOUBLER MOST AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-023-2.Apr 2, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120330027Skin · damagedNR 2 PYLON SKIN CAP DOUBLER AFT I/B FASTENER HOLE HAS DEFECT. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-024-2.Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120330026Structure · crackedNR 4 PYLON O/B SIDE FWD ACCESS CUT OUT HAS CRACK IN UPPER FWD SIDE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2Mar 30, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon Miscellaneous StructureSDR EIAA20120327025Angle · damagedLT BS 800 FRAME STR 17L UPPER AFT HOLE IS MISMATCHED COMMON TO STRAP FRAME INNER CHORD AND DOOR STOP FITTING. REMOVED DAMAGE INNER CHORD ANGLE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-021-2.Mar 27, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous StructureSDR EIAA20120327024Skin · crackedNR 4 PYLON I/B SIDE CRACK IN SKIN OF ACCESS CUT OUT, FWD UPPER CORNER NAC273. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-54-019-2.Mar 27, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120326022Floorbeam · damagedELONGATED HOLE IN UPPER CHORD OF UPPER DECK FLOORBEAM BS 780 LBL 27. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120326020Strap · damagedRIGHT BS 800 FRAME STRAP AND STR 17R STRAP HAS 2 EACH HOLES WITH TOOL MARKS. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ERCA 489-53-021-2.Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, FrameSDR EIAA20120326019Structure · damagedBS 2231 O/B CHORD ABOVE STR 19L HAS TOOL MARKS INSIDE HOLE AND HOLE ELONGATED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2.Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous StructureSDR EIAA20120326018Floorbeam · chafedLOWER CHORD OF UPPER DECK FLOORBEAM BS 560 LBL 87 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120326017Floorbeam · chafedLOWER CHORD OF UPPER DECK FLOORBEAM BS 560 RBL 87.50 IS CHAFED. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 51-40-04 FIG 1.Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120326016Skin · chafedNR 4 PYLON CAP SKIN O/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION 17.Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120326015Skin · chafedNR 4 PYLON CAP SKIN I/B SIDE NAC STA 258 HAS CHAFE. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER B747 SRM 54-31-03 FIG 2 SHEET 1-4 AND ENG DISPOSITION NR 16.Mar 26, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120326014Structure · damagedBS 2231 I/B CHORD BELOW STR 19L HAS DRILL START. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 489-53-022-2Mar 26, 2012 · N489EV · Boeing 747230B · Fuselage Miscellaneous StructureSDR EIAA20120306012Skin · chafedNR 4 PLYON CAP SKIN I/B SIDE AT NAC 258 HAS CHAFING. REMOVED DAMAGED SECTION OF CAP SKIN, FABBED REPAIR PARTS AND INSTALLED PER EMC ENGINEERING DISPOSITION 3823 AND B747 SRM 54-31-03 PG 2 SHEET 1-4.Mar 6, 2012 · N489EV · Boeing 747230B · Nacelle/Pylon, Plate/SkinSDR EIAA20120201009Floorbeam · crackedBS 360 FLOORBEAM LBL 54.50 FWD SIDE HAS CRACK. REMOVED DAMAGE FABBED AND INSTALLED REPAIR PER SB 747-53A2431 PART 3 FIG 9.Feb 1, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120131008Floorbeam · crackedBS 340 FLOORBEAM LBL 13.25 AFT SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 TABLE 1 FIG 9.Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120131007Floorbeam · crackedBS 360 FLOORBEAM LBL 13.12 AND 14.65 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J SB 747-53A2431 REV 2 PART 3 FIG 9.Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120131006Floorbeam · crackedBS 340 FLOORBEAM LBL 29.50 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-7471587-00 REV J, SB 747-53A2431 REV 2 TABLE 1 FIG 8.Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120131005Floorbeam · crackedBS 360 FLOORBEAM LBL 36.70 FWD SIDE HAS CRACK. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR PER EO 53-747-1587-00 REV J PART 3 FIG 9.Jan 31, 2012 · N489EV · Boeing 747230B · Fuselage Main, Floor BeamSDR EIAA20120126004Reveal · crackedBS 2231 RT DOOR FRAME REVEAL HAS CRACK BETWEEN STR 16R AND 17R. REMOVED DAMAGE, FABBED AND INSTALLED REPAIR DOUBLERS PER B747 SRM 53-10-04 FIG 91.Jan 26, 2012 · N489EV · Boeing 747230B · Fuselage Main, StructureSDR EIAA20120119003Battery Pack · dischargedUPPER DECK RT "EXIT" DOOR EMERGENCY LIGHT IS INOP. REMOVED AND REPLACED BATTERY CARTRIDGE FOR RT EXIT DOOR LIGHT SYSTEM OP'S CHECK NORMAL REF: 33-51-00.Jan 19, 2012 · N487EV · Boeing 747230B · Emergency LightingSDR EIAA20120101001Control Quadrant · lack of lubeON DESCENT THROUGH 8000 FT NR 2 THRUST LEVER SEIZED JUST FORWARD OF IDLE POSITION. CONFIRMED NR 2 THROTTLE SEIZED JUST FORWARD OF IDLE INSPECTED THROTTLE RUN FROM WING ROOT TO MEC NO OBVIOUS DEFECTS NOTED LUBRICATED QUADRANT AND INTERTOCK MECHANISM PER AMM 76Jan 1, 2012 · N489EV · Boeing 747230B · Power LeverSDR EIAA20111229265Battery · dischargedUPPER DECK RT EXIT EMERGENCY LIGHT OP. RECHARGED BATTERY, OP CHECK OK REF 33-51-00/501.Dec 29, 2011 · N487EV · Boeing 747230B · Emergency LightingSDR EIAA20111204258Pin · shearedO/B WING GEAR BEAM PIN RETAINER NUT AND SHAFT SHEARED OFF LT WING. REMOVED AND REPLACED LT WING GEAR SUPPORT BEAM O/B BEARING PIN PER MM 57-15-01 PG 401-410.Dec 4, 2011 · N488EV · Boeing 747230B · Wing, Landing Gear Attach FittingsSDR EIAA20111204257Skin · crackedL1 DOOR SKIN CRACKED AT FASTENER ROW 6.5" UP FROM LOWER GATE HINGE AND 10" FWD OF DOOR TRAILING EDGE. CUT OUT CRACK, FABRICATED AND INSTALLED REPAIR PARTS PER SRM 52-10-02 FIG. 9 AND ENGINEERING DISPOSITION 3786 ITEM 001.Dec 4, 2011 · N488EV · Boeing 747230B · Passenger/Crew DoorsSDR EIAA20111120256Battery · dischargedFWD LAVATORY SMOKE DETECTOR CHIRPS ONCE EVERY FEW MINUTES, SUSPECT WEAK BATTERY. REMOVED AND REPLACED 9 VOLT BATTERY OP'S CHECKED OK PER SMM 26-13-01 PAGE 401.Nov 20, 2011 · N487EV · Boeing 747230B · Smoke DetectionSDR EIAA20111106247Duct · separatedNR 4 ENGINE FIRE FAULT WARNING AND BOTH NACELLE TEMPS READING 8 UNITS. SELECTED "A" LOOP HAD FIRE WARNING BELL AND HANDLE CAUTION LIGHT. PULLED FIRE TEE HANDLE LIGHT AND AURAL WARNING LIGHT EXTINGUISHED/SILENCED. SUSPECT PNEUMATIC LEAK. FIRE BOTTLE WAS NOT Nov 6, 2011 · N488EV · Boeing 747230B · Pneumatic Distribution SystemSDR 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 EIAA2011235Squib · no testDURING PREFLIGHT FLIGHT, ENGINEER DISCOVERED FIRE BOTTLE SQUIB 3B WOULD NOT TEST. REMOVED AND REPLACED 3B FIRE BOTTLE SQUIB.Oct 4, 2011 · N489EV · Boeing 747230B · Fire Bottle, FixedSDR 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 EIAA2011230Circuit Card · faultedNUMBER 1 ENGINE FIRE DETECTOR A LOOP FAULTED. RESET FIRE DETECTOR CARD PER AMM 26-11-00. OPS CHECKED NORMAL.Sep 28, 2011 · N487EV · Boeing 747230B · Fire DetectionSDR 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/Stringer
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