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 UPS06448216Battery · inoperativeFOUND EMERG LT AT MAIN CARGO DECK ENTRANCE INOP, LT ASSY ON REQ A863705. REMOVED AND REPLACED BATTERY ASSY IAW MM 33-51-00. OPS CK OK.Oct 9, 2006 · N521UP · Boeing 747283B · Emergency LightingSDR UPS06448249Skin · corrodedINSPECTION TYPE: C FX BS 2180-2186 S46-47R EXISTING REPAIR REMOVE REQUIRE FOR CUTOUT EVALUATION. CORROSION BLEND OUT 0.048 INCH X 1INCH X .7500 INCH, FX BS 2180 TO BS 2193 STR 44R TO STR 48R AREA LAP AND BUTT JOINT SKIN REPAIRED IAW RS R53-61-35631 REPEAT INOct 3, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448211Vertical Beam · crackedINSPECTION TYPE-C NR 4L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1 INCH LONG. NR 4L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Service DoorsSDR UPS06448207Vertical Beam · crackedINSPECTION TYPE-C NR 1R MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX 1.5 INCH LONG. NR 1R MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448206Vertical Beam · crackedINSPECTION TYPE-C NR 2L MED FWD LOWER CORNER VERTICAL BEAM FOUND CRACK APPROX .7500 INCH LONG. NR 2L MED FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 52-10-02 FIG 10.Sep 26, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448212Attach Fitting · corrodedINSPECTION TYPE-C CORROSION FOUND AT 1 FASTENER HOLE AT FRAME WEB ATTACH FITTING LOCATED AT BS 979 S38L. FWD CARGO COMPT BS979 S38L FRAME ATTACHED FTG REPLACED AND INSTALLED IAW SRM 51-10-01 PG 9 AND 51-30-02.Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Main, Attach FittingsSDR UPS06448208Fitting · corrodedINSPECTION TYPE-C FX LT BS 980 STR 38L UPPER AND LOWER DRAG SPLICE FITTINGS ATT BOLT HOLE AREA FOUND CORROSION. CORROSION BLEND OUT 0.092 INCH BY 1.5 INCH BY 3 INCH. FX LT BS 980 STR 38L UPPER AND LWR DRAG SPLICE FTGS REPLACED AND INSTALLED IAW SRM 51-10-01 Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR UPS06448182Stringer · crackedCRACK FOUND AT 1 FASTENER HOLE LOCATED AT BS 983 STR 38L APPROX 1" LONG RUNNING FORWARD AS MARKED. FX BS 970 TO BS 990 STR 38L STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.Sep 23, 2006 · N523UP · Boeing 747283B · Fuselage Main, Longeron/StringerSDR UPS06448209Vertical Beam · crackedINSPECTION TYPE-C M/D RT NR 5 DOOR INTERIOR FWD LWR CORNER VERTICAL BEAM FOUND CRACK, CRACK LENGTH 4.7500 INCH APPROX. M/D RT NR 5 DOOR INTERIOR FWD LOWER CORNER VERTICAL BEAM REPAIRED IAW SRM 51-10-02 FIG 10.Sep 22, 2006 · N523UP · Boeing 747283B · Passenger/Crew DoorsSDR UPS06448231Skin · crackedINSPECTION TYPE:C AFT CARGO DOOR CUTOUT FWD UPPER CORNER HINGE FAIRING COVERED AREA FOUND 1 CRACK AT SKIN AT THE MOST AFT HOLE APPROX 0.040" (CRACK LENGTH 0.040"). AFT CARGO DOOR CUTOUT FWD UPPER CORNER SKIN REPAIRED AS PER SRM 53-30-03 FIG 62. SUBSEQUENT INSep 21, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448210Door Frame · crackedINSPECTION TYPE-C M/D RT DOOR FRAME INTERIOR FACE AFT LWR CORNER AREA FOUND CRACKED, CRACK LENGTH 2.5 INCH APPROX. M/D R4 DOOR FRAME AFT LOWER CORNER AREA REPAIRED IAW SRM 52-10-02 FIG 10.Sep 21, 2006 · N523UP · Boeing 747283B · Fuselage Main, StructureSDR UPS06448239Frame · crackedINSPECTION TYPE:C NR 3 PYLON REAR UPPER ENG MT BULKHEAD O/B FWD FRAME FOUND CRACK AT UPPER PORTION, CRACK LENGTH 1.5". NR 3 PYLON REAR BULKHEAD O/B FWD FRAME REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.Sep 20, 2006 · N523UP · Boeing 747283B · Nacelle/Pylon, Plate/SkinSDR UPS06448233Skin · crackedINSPECTION TYPE:C FWD CARGO DOOR, DOOR EXTERNAL SKIN SURFACE FOUND DENT MARK AT STA 582, 6" TO LOWER EDGE, CRACK LENGTH 1/8". FWD CARGO DOOR EXTERNAL SKIN REPAIRED AT BS 582 6" ABOVE LOWER EDGE AREA AS PER SRM 52-00-03 FIG 4. SUBSEQUENT INSPECTION IS REQUIRESep 20, 2006 · N523UP · Boeing 747283B · Cargo/Baggage DoorsSDR UPS06448181Frame · crackedAPU COMPT BS 2675 LT WL325 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .500 INCH. APU COMPT BS 2675 LT WL 325 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.Sep 20, 2006 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS06448180Frame · crackedEMP APU COMPT LT BS 2701 WL 315 FRAME FOUND CRACK AS MARKED, CRACK LENGTH .7500. APU COMPT LT BS 2701 WL 315 FRAME REPAIRED AS PER SRM 51-40-03 FIG 1.Sep 20, 2006 · N523UP · Boeing 747283B · Fuselage Main, FrameSDR UPS06448232Skin · crackedINSPECTION TYPE:C LT BS 980 STR 38L DRAG SLICE FTG AREA FOUND 1 FASTENER HOLE CRACKED AT FUSELAGE HOLE CRACKED AT FUSELAGE APPROX 1/8". FX BS 950 - BS 990 STR 37L - 39L SKIN. REPAIRED AS PER SRM 53-30-03 FIG 60. REPEAT INSPECTION IS REQUIRED AS PER SRM 53-3Sep 19, 2006 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS06448226Floorbeam · corrodedINSPECTION TYPE:C, RT B/G W/W UPPER PRESSURE FLOOR PANEL ATTACH ANGLE SOME AREA FOUND CORROSION AS MARK AT STA 1403, RBL 34 TO RBL 104. CORROSION BLEND OUT 0.030" BY 1/2" BY 4" EXCEED SRM 53-10-01 FIG 1 LIMITS, RBL 34-63 AND RBL 67-104 CORROSION. REMOVED ANSep 19, 2006 · N523UP · Boeing 747283B · Fuselage Main, Floor BeamSDR UPS06448179Intercostal · crackedN/G W/W TOP PANEL INTERNAL SIDE INTERCOSTAL AT BRAKE SNUBBER FOUND CRACK AS MARK AT STA 290 RBL 21, CRACK LENGTH 1/4". N/G W/W TOP PANEL INTERNAL SIDE INTERCOSTAL REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02Sep 19, 2006 · N523UP · Boeing 747283B · Fuselage Miscellaneous StructureSDR P5CA0601471Skin · corrodedCORROSION BS 1241 BL 0 TO LBL 11. REPAIRED IAW SRM 51-10-01 PAGE 13, 14.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, Plate/SkinSDR P5CA0601470Skin · damagedAFT CARGO DOOR CUTOUT HAS 1 INCH HALF CIRCLE BLEND 8 INCHES FROM BOTTOM OF CUTOUT. REPAIRED PER BOEING 8100-9 PER ECRA 921FT-57-747-017, SRM 51-30-02.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, Plate/SkinSDR P5CA0601469Structure · corrodedRIGHT WING TRAILING EDGE STA 710.0 - 718.0 CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-014.Mar 31, 2006 · N921FT · Boeing 747283B · Wing Main, Frame StructureSDR P5CA0601468Spar · corrodedWS 1010-1038 RT FRONT SPAR WEB CORROSION. REPAIRED PER BOEING 8100-9, PER ECRA 921FT-57-747-013.Mar 31, 2006 · N921FT · Boeing 747283B · Wing SparSDR P5CA0601467Spar · corrodedCORROSION ON LEFT WING LEADING EDGE CAVITY - SPAR WEB - LOWER CHORD LES 1322. REPAIRED PER BOEING 8100-9. REPLACED LEFT WING L/E SPAR WEB LWR CHORD PER ECRA 921-57-747-011.Mar 31, 2006 · N921FT · Boeing 747283B · Wing SparSDR P5CA0601466Bulkhead · corrodedTHE 1241 BULKHEAD CORRODED AT LBL 10 TO RBL 98 (BELOW UPPER CHORD). REPAIRED PER BOEING 8100-9. REMOVED CORROSION AT BS 1241 LBL 10 TO RBL 98. WORK ACCOMPLISHED ON ECRA 921FT-57-474-010 REV NEW.Mar 31, 2006 · N921FT · Boeing 747283B · Fuselage Main, BulkheadSDR P5CA0601465Skin · corrodedEXFOLIATION CORROSION ON LEFT WING LOWER SKIN AT AFT SPAR AREA WS 1376. REPAIRED PER BOEING 8100-9. FABRICATED AND INSTALLED 1-2-3-4 PLATES FILLER PER ECRA 921FT-57-747-004.Mar 31, 2006 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0601464Skin · crackedLEFT WING LOWER SKIN BETWEEN DRY BAY PANELS AT WS 1516 HAS SKIN CRACKED. REPAIRED PER BOEING 8100-9. REPAIRED CRACKED LEFT WING LOWER SKIN PER ECRA 921FT-57-747-001.Mar 31, 2006 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0501419Transmitter · failedON TAKEOFF ROLL, CREW REPORTED NR 3 ENGINE EPR WOULD NOT ADVANCE ABOVE 1.2 EPR, FULL TRAVEL OF THROTTLE HAD NO EFFECT. TAKEOFF ABORTED AT 80 KTS IAS EPR ON NR 3 STAYED AT 1.2 UNTIL ENGINE SHUTDOWN. REPLACED EPR TRANSMITTER, PERFORMED LEAK CHECK AND RAN ENGINDec 15, 2005 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR PDCA0501420Transmitter · failedON CLIMB, NR 3 ENGINE EPR STARTED DECREASING AT FL310 EPR IND., ON DESCENT IT READ HIGH (1.24 AT 150 WITH THRUST LEVERS IDLE) (CORRECTIVE ACTION) REPLACED EPR TRANSMITTER IAW MM 77-11-00 AND DEFERRED OPS CHECK IAW DDPG 77-4.Dec 12, 2005 · N921FT · Boeing 747283B · Engine Pressure Ratio (EPR)SDR UPS05445857Link · crackedNR 4 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE LOWER AREA WITH CRACK INDICATION ( > 126 PERCENT FSH ) WHICH EXCEED LIMIT. NR 4 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03, REF EO NR B747-7120-22596-C APPENDIX I.Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445856Link · crackedNR 3 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AREA WITH CRACK INDICATION (90 PERCENT FSH ); AND AFT END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 110 PERCENT FSH RESPECTIVELY. ALL EXCEED LIMIT. NR 3 ENGINE REAR MOUNT Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445855Link · crackedNR 2 ENGINE REAR MOUNT THRUST LINK AFT END LUG BORE LOWER AREA WITH CRACK INDICATION 70 PERCEMT FSH WHICH EXCEED LIMIT. NR 2 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDIX G.Dec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR UPS05445854Link · crackedNR 1 ENGINE REAR MOUNT THRUST LINK FWD END LUG BORE UPPER AND LOWER AREA WITH CRACK INDICATION 60 PERCENT FSH AND 80 PERCENT FSH RESPECTIVELY. WHICH EXCEED LIMIT. NR 1 ENGINE REAR MOUNT THRUST LINK REPLACED PER 747 MM 71-21-03 REF EO NR B747-7120-22596 APPENDec 6, 2005 · N523UP · Boeing 747283B · Engine Mount SectionSDR P5CA0501407Skin · corrodedCORROSION ON RT UPPER SKIN AFT OF REAR SPAR WS 560 TO 575. REMOVED CORROSION & REPAIRED IAW BOEING REPAIR PROCEDURE 1-129539127-5 AND 8100-9.Oct 19, 2005 · N921FT · Boeing 747283B · Wing, Plate/SkinSDR P5CA0501402Panel · crackedLEFT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REMOVED AND REPLACED NR 3 SPOILER PER MM 27-61-02.Sep 22, 2005 · N921FT · Boeing 747283B · SpoilersSDR P5CA0501401Support Beam · crackedLEFT WING TRAILING EDGE SUPPORT BEAM UPPER CHORD CRACKED (APPROX 2 INCHES) AT WS 528.20, WBL 235.20.Sep 22, 2005 · N921FT · Boeing 747283B · Wing Miscellaneous StructureSDR P5CA0501400Fitting · corrodedLEFT WING AT UPPER CHORD OF SPLICE FITTING OF WING REAR SPAR HAS CORROSION BETWEEN WS 553 AND WS 558. CORROSION BLENDED OUT IAW SRM 57-30-01. HFEC & ULTRASONIC INSPECTION OF AREA CONFIRMED REMOVAL OF CORROSION IAW NDT 06-7170 PT 6, 51-00-00 FIG 23, 12. D6-71Sep 22, 2005 · N921FT · Boeing 747283B · Wing, Attach FittingsSDR P5CA0501404Panel · crackedLT WING NR 3 O/B SPOILER HAS A CRACK AT UPPER SURFACE (NEAR HINGE FITTING SUPPORT). REPLACED NR 3 SPOILER ASSEMBLY IAW AMM 27-61-02.Sep 21, 2005 · N921FT · Boeing 747283B · SpoilersSDR P5CA0501389Switch · out of adjustNR 2 ENGINE REVERSER UNSTOW. ADJUSTED NR 2 REVERSER STOW SWITCH PER MM 78-31-00.Aug 26, 2005 · N921FT · Boeing 747283B · Engine Thrust ReverserSDR P5CA0501387Module · failedDURING CRUISE, LEADING EDGE FLAP GROUP 1, 2, 3, 4 LEFT AND 1 RIGHT DISPLAY AMBER, GROUPS 1 & 2 LEFT ALSO DISPLAY GREEN. REPLACED MODULE OPS CHECK OK PER MM 27-88-00.Aug 26, 2005 · N921FT · Boeing 747283B · Trailing Edge Flap Control SystemSDR P5CA0501388Actuator · failedSIDE CARGO DOOR HOOK ACTUATOR FAILED IN ELECTRICAL MODE. DEFERRED PER MEL 52-20.Aug 24, 2005 · N921FT · Boeing 747283B · Cargo/Baggage DoorsSDR P5CA0501383Door · missingON POSTFLIGHT WALKAROUND, FOUND LEFT BODY GEAR O/B SHOCK STRUT DOOR MISSING. REPLACED DOOR PER MM 32-14-06.Jul 24, 2005 · N921FT · Boeing 747283B · Landing Gear DoorsSDR P5CA0501377Clamp · failedCREW REPORTED NR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE, MM 36-13-00. OPS AND LEAK CHECK OK MM 71-00-00.Jun 10, 2005 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR P5CA0501362Clamp · failedNR 1 ENGINE FIRE WARNING SOUNDED ON DESCENT. CLOSED THRUST AND START LEVER, LIGHT WENT OUT. FIRE HANDLE WAS NOT PULLED. REPLACED CLAMP TO HIGH STAGE VALVE. OPS AND LEAK CHECK OK PER MM 36-13-00 AND 71-00-00.Jun 10, 2005 · N921FT · Boeing 747283B · Pneumatic Distribution SystemSDR UPS05444404Skin · chafedEXTERIOR SKIN CHAFING MARK FOUND ABOVE STR 12L BS 2230. CHAFED AREA 0.016 INCH BY 3 INCH BY 1 INCH. SKIN REPAIRED AT BS 2220 TO BS 2240 BETWEEN S11L TO S12L AREA AS PER SRM 53-30-03 FIG 17 WITH ZERO TIMING AT CRITICAL ROW FASTENER CAT B REPAIR REPEAT INSP ATApr 23, 2005 · N523UP · Boeing 747283B · Fuselage Main, Plate/SkinSDR UPS05444426Frame · crackedNR 1 PYLON AFT BULKHEAD I/B FRAME ADJ TO UPPER SPAR FTG CRACKED APPROX .1875 RUNNING I/B AND O/B, CRACK LENGTH .1875. NR 1 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.Apr 14, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444422Frame · crackedNR 1 PYLON AFT BULKHEAD O/B FRAME ADJ TO UPPER SPAR FITTING FOUND CRACKED RUNNING I/B TO EDGE AND RUNNING O/B .9375 INCH LONG, (CRACK LENGTH .9375 ). NR 1 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINEERING FILE NR 747-54-20Apr 14, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444334Splice · crackedINSPECTION TYPE:C RH BS 1480 B/H #18 HOLE FOUND CRACK AT WEB SPLICE PLATE RUNNING UP APPROX 0.080" LONG ( CRACK LENGTH 0.080" ) NR 18 BOLT HOLE OVERSIZED TO 0.532" AT SPLICE PLATE HFEC INSP C/OUT FOUND CRACK FREE BUSHING REPAIRED AS PER EO B747-5310-10732.Apr 14, 2005 · N523UP · Boeing 747283B · Fuselage Main, BulkheadSDR UPS05444333Bulkhead · crackedINSPECTION TYPE: C, RT BS 1480 B/H NR 7 HOLE FOUND CRACK AT FX, SKIN RUNNING AFT APPROX .0625 INCH LONG, CRACK LENGTH .0625. HOLE OVERSIZED TO 0.687" AS PER EO B747-5310-10732 AND BUSHING INSTALLED.Apr 14, 2005 · N523UP · Boeing 747283B · Fuselage Main, BulkheadSDR UPS05444425Frame · crackedNR 2 PYLON AFT BULKHEAD I/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, CRACK LENGTH .375 AND .250. NR 2 PYLON AFT BULKHEAD I/B FRAME REPAIRED AS PER HX RS R54-53-35295 AND UPS EA ENGINEERING FILE NR 747-54-20051.Apr 13, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/RibSDR UPS05444421Frame · crackedNR 2 PYLON AFT BULKHEAD O/B FRAME ADJACENT TO UPPER SPAR FITTING FOUND CRACKED, (CRACK LENGTH .25 INCH AND .9375 INCH ). NR 2 PYLON AFT BULKHEAD O/B FRAME REPAIRED AS PER HX RS NR R54-53-35295 AND UPS ENGINERING FILE NUMBER 747-54-20051.Apr 13, 2005 · N523UP · Boeing 747283B · Nacelle/Pylon, Frame/Spar/Rib
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