Boeing 747-283B

Service difficulty reports · 267

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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 = '747283B'
  ORDER BY difficulty_date DESC"

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SDR UPS05444399Shear Tie · crackedCOCKPIT BS 360 STR 1R FRAME SHEAR TIE CRACKED, CRACK LENGTH 1/2 INCH. COCKPIT BS 360 FRAME WEB REPAIRED AT BTN STR 1R AND STR 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086-A.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Internal Mounting StructureSDR UPS05444398Frame · crackedCOCKPIT BS 360 FRAME STR 2R WEB CRACKED, CRACK LENGTH 9/16". COCKPIT BS 360 FRAME WEB REPAIRED AT BETWEEN STR 1R AND 2R AREA AS PER HX RS R53-12-35290 AND UPS EO NR B747-5310-22086A, REFER NRC 6590 FOR WORK DETAIL.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444335Stringer Clip · crackedINSPECTION TYPE:C COCKPIT - BS 360 S-8L FRAME/STR TIE CLIP CRACKED. ( CRACK LENGTH 0.5" ). COCKPIT BS 360 STR -8L TIE CLIP REPLACED AS PER SRM 51-10-01 P.9.Apr 12, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444428Fitting · corrodedU/D - STA 496 RBL 70 TOILET TANK TIE DOWN FTG CORROSION FOUND. CORROSION BLEND OUT 0.020" BY 1" BY 1". TIE DOWN FTG REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444408Frame · crackedBS 480 FRAME S10AL STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. BS 480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22 REFER NRC 6374 FOR WORKING DETAIL.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444407Frame · crackedU/DECK BS480 STR 12L STR CUTOUT CRACKED. CRACK LENGTH 3/4 INCH. U/DECK BS480 STR 10AL TO STR 12L FRAME REPAIRED AS PER SRM 53-10-04 FIG 22.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444406Frame · crackedSTA 440 STR 10R FRAME CRACKED. U/DECK BS440 STR 10R FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444405Frame · crackedBS440 LT FRAME, JUST BELOW U/D FLOORBEAM LWR CHORD, WEB CRACKED WL290, CRACK LENGTH 3/8 INCH. BS 440 LT FRAME WEB REPLACED BETWEEN STR 13L TO 16L AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444402Stringer · crackedBS 1485 LT STR 6L STRINGER END FOUND CRACKED. CRACK LENGTH 0.5 INCH. M/DECK BS 1485 STR 6L REPAIRED AS PER HX RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444401Stringer · crackedBS 1478-1480 STR 6R STRINGER END FOUND CRACK. CRACK LENGTH 1.5 INCH. M/DECK BS 1478-1480 STR 6R STRINGER END REPAIRED AS PER RS R-53-41-35294 AND UPS EA ENGINEERING FILE NR 747-53-20244.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444396Frame · crackedBS 460 FRAME STR -11L STR CUTOUT CRACKED, CRACK LENGTH 1.38 INCH. FRAME WEB REPAIRED AS PER HX RS NR R53-12-35293 AND UPS EO NR B747-5310-22102-AApr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444393Stringer · crackedBS 1238-1241 STR 7R STRINGER END FOUND CRACK (CRACK LENGTH 1 INCH ). M/DECK BS 1238 STR 7R STR REPAIRED AS PER HX RS R-53-41-35297 AND UPS ENGINEERING FILE NR 747-53-20245.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444392Frame · crackedBS 520 FRAME S11L STR CUTOUT CRACKED, CRACK LENGTH ON FRAME CHORD 1.12 INCH, ON FRAME AND DOUBLER 0.43 INCH, DOUBLER 0.56 INCH ). U/DECK BS 520 FRAME REPAIRED AT BETWEEN STR 10L/10AL TO STR 12L AREA AS PER RS R-53-12-35296 AND UPS EO B747-5310-22103-A.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444388Frame · crackedBS 460 LT FRAME, JUST BELOW U/D FLOORBEAM LOWER CHORD. WEB CRACKED, CRACK LENGTH 1 INCH. BS 460 LT FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444386Skin · corrodedLOWER FX EXTERNAL SKIN SURFACE RT POTABLE WATER TANK SERVICE CONNECTOR ATT DOUBLER FOUND SURFACE CORROSION AT STA 975 TO STA 980. CORROSION BLEND OUT 0.040 INCH BY 1 INCH BY 3 INCH EXCEED SRM 53-30-01 FIG 1 LIMITS, DOUBLER REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS05444385Seat Track · corrodedBS 480-485, RBL 47 SEAT TRACK CROWN CORROSION FOUND. CORROSION BLEND OUT 0.030 INCH BY 1 INCH BY 1 INCH EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 480-530 RBL 47 INCH SEAT TRACK REPAIRED AS PER SRM 53-10-05 FIG 1A.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage, Seat/Cargo Attach FittingsSDR UPS05444384Frame · crackedRT BS 460 FRAME (JUST BELOW U/D FLOORBEAM LWR CHORD) WEB CRACKED, CRACK LENGTH 1.875. FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, StructureSDR UPS05444383Frame · crackedRT BS 440 FRAME (JUST BELOW U/D FLR BEAM LWR CHORD ) WEB CRACKED. (CRACK LENGTH 2.5" ). BS 440 RT FRAME WEB REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444382Frame · crackedBS 440 FRAME INNER FLANGE AND WEB CRACKED BTN S-14R AND S-14ER (CRACK LENGTH 4" ). BS 440 FRAME INNER FLANGE ANGLE AND WEB REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444344Stringer Clip · crackedINSPECTION TYPE: C, M/D - BS 1640 STR 1R FRAME ATT TIE-CLIP FOUND CRACKED. (CRACK LENGTH .0625"), M/D- BS 1640 STR 1R FRAME ATT TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444343Stringer Clip · crackedINSPECTION TYPE: C, M/D- BS 1640 LT STR -1L TIE-CLIP FOUND CRACKED. (CRACK LENGTH .125" ), M/D BS1640 STR -1L TIE-CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 11, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444412Stringer Clip · crackedBS 1940 STR 19R STRINGER TIE CLIP FOUND CRACKED (CRACK LENGTH 1/4 INCH) . BS1940 STR 19R STR TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9.Apr 10, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444337Stringer · crackedINSPECTION TYPE:C M/D BS 1956 STR 10R FOUND CRACKED. ( CRACK LENGTH .375" ) STRINGER REPAIRED AS PER SRM 53-10-03 FIG 4 AT BS 1930-1960 STR 10R AREA.Apr 10, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444336Stringer Clip · crackedINSPECTION TYPE:C M/D -BS 1940 STR 18R STRINGER TIE CLIP FOUND CRACKED. (CRACK LENGTH 3/8" ) TIE CLIP REPLACED AS PER SRM 51-10-01 PG 9 AT BS 1940 STR 18R AREA.Apr 10, 2005 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS05444395Frame · crackedBS 160 S14BL - 14CL FRAME INNER FLANGE FOUND CRACKED, CRACK LENGTH .25 INCH. BS 160 STR 14BL TO STR 14CL FRAME INNER FLANGE REPAIRED AS PER HX RS R-53-12-35288 AND UPS EO NR B747-5310-22088-A.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444394Frame · crackedBS 200 S13AL TO S14L FRAME FOUND CRACKED, CRACK LENGTH .750 INCH. M/DECK BS 200 BETWEEN STR 13AL TO STR 14AL FRAME REPAIRED AS PER HX RS R-53-12-35289 AND UPS EO NR B747-5310-22089-A.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444387Frame · crackedBS 320 S24 L - S26L, FRAME FOUND CRACKED, CRACK LENGTH 2.5 INCH. FRAME REPAIRED AS PER HX RS R53-12-35287 AND UPS EO NR B747-5310-22087-A.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444342Stringer · crackedINSPECTION TYPE: C, M/D - BS 180 - 200 S-16R STRINGER FWD FOUND CRACKED. (CRACK LENGTH .250"), M/D BS 180-200 S-16R STRINGER REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444341Splice · crackedINSPECTION TYPE: C, BS 280 S-22L TO S-23L FRAME SPLICE FOUND CRACKED. (CRACK LENGTH .250" ) BS 280 S-22L TO S-23L FRAME SPLICE REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR UPS05444340Stringer · crackedINSPECTION TYPE: C, M/D - BS 240-260 STR 11L STRINGER FOUND CRACKED. (CRACK LENGTH .250" ), M/D BS 240-260 STR -11L STRINGER REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS05444339Stiffener · crackedINSPECTION TYPE:C M/D BS 400 STR 14EL STRINGER ATTACH FOUND CRACKED STIFFENER ( CRACK LENGTH .1875" ). M/D BS 400 STR 14EL STRINGER ATTACH STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR UPS05444338Frame · crackedINSPECTION TYPE: C, M/D BS 240 STR 14L TO STR 14CL FRAME FOUND CRACKED. ( CRACK LENGTH 1.5" ) M/D BS 240 STR 14L TO STR 14CL FRAME REPAIRED AS PER SRM 53-10-04 FIG 11.Apr 9, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444397Frame · crackedNR 1 LT MED CUTOUT BS 488 FRAME AT STR 25L INNER CHORD TWO FASTENER HOLES FOUND CRACKED AND AS MARKED, CRACK LENGTH 1/8 INCH. NR 1 MED LT BS 488 INNER CHORD REPLACED AS PER SB 747-53-2272 AND DWG 624U0003 SHT 40A.Apr 8, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444424Floorbeam · crackedRT BS 340 U/D FLOORBEAM FOUND 2EA FASTENER HOLES CRACKED AT STR 12 RT REFER TO ATTACH SKETCH FOR DETAILS, CRACK LENGTH FS WEB 1/4", 1/8" AND THROUGH THICKNESS FLOORBEAM CHORD 0.060". BS 340 RT U/D FLOORBEAM CHORD REPAIRED AT RBL 48" TO RT MOST O/B END AS PER Apr 7, 2005 · N523UP · Boeing 747283B · Fuselage Main, Floor BeamSDR UPS05444423Floorbeam · crackedLH BS 340 U/D FLOORBEAM FOUND 2EA FASTENER HOLES CRACKED AT STR 12L REFER TO ATTACH SKETCH FOR DETAILS. CRACK LENGTH CHORD 0.060", FRAME WEB 1/8" AND THROUGH THICKNESS FLOORBEAM WEB CRK THROUGH THICKNESS. BS 340 LT U/D FLOORBEAM CHORD REPAIRED AT LBL 36 TO LApr 7, 2005 · N523UP · Boeing 747283B · Fuselage Main, Floor BeamSDR UPS05444427Frame · crackedNR 1 L MED CUTOUT BS 488 FRAME WEB FOUND CRACK AT DOOR STOP NR 1 AREA APPROX 0.5" LONG EXTEND BEYOND DOOR STOP SUPPORT FTG. CRACK LENGTH 1/2 INCH. M/D NR 1L MED CUTOUT BS 488 FRAME WEB REPAIRED BETWEEN STR 23 TO STR 30 AS PER SRM 53-10-04 FIG 92.Apr 6, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444403Frame · crackedNR 1R MED CUTOUT BS 488 FRAME AT DOOR STOP NR 1 AREA FOUND CRACK AT FRAME FWD DOUBLER 1/2 INCH LONG EXTEND BEYOND DOOR STOP FTG AND CRACK AT WEB 1 EA HOLE APPROX 1/16 INCH LONG. CRACK LENGTH 1/4 INCH AT DOUBLER, 1/16 INCH AT WEB. M/DECK NR 1R MED CUTOUT BS48Apr 6, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444414Frame · crackedBS 1265 STR -26R FRAME BELOW DOOR LOWER SILL FASTENER HOLE FOUND CRACKED AT FRAME WEB RUNNING I/B AND O/B (CRACK LENGTH 1/16 INCH), BS 1265 RT FRAME WEB INTERIM REPAIRED AS PER DWG 624U0060.Apr 5, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS05444413Frame · crackedBS 1265 STR -26L FRAME BELOW DOOR LOWER SILL FASTENER HOLE FOUND CRACKED AT FRAME WEB RUNNING I/B AND O/B AND FOUND FRAME WEB EDGE CRACKED (CRACK LENGTH 1/16 INCH) BS 1265 LT FRAME WEB INTERIM REPAIRED AS PER DWG 624U0060.Apr 5, 2005 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR P5CA0501335Data Card · failedGPS DATA CARD FAILED. TRANSFERRED TO DMI 34058 PER MEL 34-27-2S.Apr 3, 2005 · N921FT · Boeing 747283B · Global Positioning SystemSDR P5CA0501331Door · missingON POST FLIGHT NR 3 ENGINE REVERSER PANEL MISSING. ACCOMPLISHED INTERIM REPAIR PER SRM 51-00-04 AND SRM 51-40-16, ALSO GMM 3-17-1. TRANSFERRED TO C/O ITEM 921-179.Mar 20, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501325Warning Light · illuminatedNR 2 ENGINE THRUST REVERSER LIGHT CAME ON FLASHING AS ENGINE APPROACHED TAKE OFF EPR. DEFERRED T/R PER MEL NR 78-3-1B.Mar 3, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501324Engine · malfunctionedCREW REPORTED NR 1 ENGINE WOULD NOT MAKE TAKEOFF EPR. INSPECTED NR 1 ENGINE PER MM 71-00-00, OPENED MEL 77-4-1 FOR EPR UNRELIABLE.Feb 22, 2005 · N921FT · Boeing 747283B · Engine (Turbine/Turboprop)SDR P5CA0501310Seat Track · brokenON PREFLIGHT FOUND BOTH SEAT TRACKS BROKEN ON THE F/O'S SEAT (AFT SEAT TRACK). REMOVED & REPLACED BOTH LT & RT AFT SEAT TRACKS PER AMM 25-11-00.Jan 29, 2005 · N921FT · Boeing 747283B · Fuselage, Seat/Cargo Attach FittingsSDR P5CA0501308Thrust Reverser · inoperativeNR 4 ENGINE THRUST REVERSER WOULD NOT DEPLOY AFTER LANDING. NR 4 ENGINE THRUST REVERSER DEACTIVATED PER MEL 78-01-2A. REF MM 78-31-00.Jan 21, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501307Pump · leakingDURING CLIMB NR 2 ENGINE OIL QTY DROPPED TO ZERO. AFTER 5 MINUTES OIL PRESSURE 40 PSI AND FLUCTUATING. OIL TEMPERATURE NORMAL. ENGINE SHUTDOWN. REPLACED EDP PER MM 29-141-05. LEAK AND OPS CHECK OK PER MM 29-11-05.Jan 21, 2005 · N921FT · Boeing 747283B · Hydraulic Pump (Electric/Engine), MainSDR P5CA0501306Pump · leakingLOSS OF NR 2 HYDRAULIC SYSTEM. HYDRAULIC QUANTITY WENT FROM 6.5 GALLONS TO ZERO IN LESS THAN 5 SECONDS. FOUND NR 2 ENG EDP CASING CRACKED. REMOVED NR 2 EDP PER MM 29-11-05 AND DEFERRED PER MEL 29-1A.Jan 20, 2005 · N921FT · Boeing 747283B · Hydraulic Pump (Electric/Engine), MainSDR P5CA0501297Pulley · wornON TAXI OUT, FLIGHT CONTROL CHECK REVEALED WHEN CONTROL WHEEL TURNED TO LEFT, NORMAL MOVEMENT OBSERVED. WHEN CONTROL WHEEL TURNED TO RIGHT IT STOPPED AT 10 DEGREES FOR 4-6 SECONDS THEN RETURNS SLOWLY TO NEUTRAL. FOUND CABLE PULLEY IN LT WHEEL WELL WORN. REPDec 29, 2004 · N921FT · Boeing 747283B · Aileron Tab Control SystemSDR P5CA0401296Switch · malfunctionedAT APPROXIMATELY 80 KNOTS TAKEOFF WARNING HORN SOUNDED. ABORTED TAKEOFF AT OKO. STAB TRIM WAS AT THE EDGE OF THE GREEN BAN. CAPTAINS TRIM INDICATOR HAS NO CENTER INDEX. MAX THRUST WAS SET PRIOR TO BRAKE RELEASE AT TAKEOFF OKO. RESET GREEN BAND SWITCH PER Dec 29, 2004 · N921FT · Boeing 747283B · Stabilizer Position IndicatingSDR P5CA0401293Hydraulic Line · leakingNR 3 HYD SYS LOST 2 GALS IN THIS FLIGHT FROM UAM-HIK. FOUND LINE LEAKING FROM CASE DRAIN FOR NR 3 EDP. REMOVED EDP DUE TO LEAK. ITEM TRANSFERRED TO DMI 33554 PER MEL 29-1A.Dec 24, 2004 · N921FT · Boeing 747283B · Hydraulic System, Main
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