Boeing 747-2U3B

Service difficulty reports · 125

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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 aircraft_model_key = '7472U3B'
  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 P5CA0300883Bulkhead · crackedCRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H.May 28, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Bulkhead/FirewallSDR P5CA0300882Bulkhead · crackedCRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390.May 28, 2003 · N922FT · Boeing 7472U3B · Fuselage Main, BulkheadSDR P5CA0300875Warning Light · illuminatedNR 1 HYD SYS HEAT LIGHT ON. RAN AND CHECKED ENG & ADP'S OPERATING FLAPS TEMPS WERE SIMILAR & BELOW 100 C PER TEMP IND. DEFERRED O/TEMP LIGHT PER MEL 29-10.May 4, 2003 · N923FT · Boeing 7472U3B · Hydraulic System, MainSDR P5CA0300871Blade · brokenCAPT'S WIPER BLADE BROKE OFF DURING TAXI. INSP ARM AND DEFERRED ITEM PER DDPG - WAS LATER REPLACED IN PIK. BLADE SHEARED OFF ARM.Apr 25, 2003 · N923FT · Boeing 7472U3B · Windshield/Door Rain/Ice RemovalSDR P5CA0300872Nozzle · leakingDURING FUELING LEAK WAS OBSERVED FROM LT WING FUEL JETTISON NOZZLE VALVE. REPLACED LT FUEL JETTISON NOZZLE VALVE.Apr 24, 2003 · N922FT · Boeing 7472U3B · Fuel Dump SystemSDR P5CA0300781Flap · failedOUTBOUND FLAPS FAILED TO EXTEND PRIOR TO TAXI. FLAPS WERE CYCLED ELECTRICALLY & THEN WITH HYDRAULICS. OPS CHECK WAS SATISFACTORY. UNABLE TO DETERMINE THE CAUSE AT THE TIME.Mar 16, 2003 · N923FT · Boeing 7472U3B · Trailing Flap Position Indicating SystemSDR P5CA0300780Connector · damagedOUTBOUND FLAPS WOULD NOT EXTEND NORMALLY, HAD TO BE EXTENDED ELECTRICALLY. FOUND LOOSE PIN ON OUTBOARD RT POS TRANSMITTER CONNECTOR. REPINNED CONNECTOR & OPERATED FLAPS PER 27-51-00.Mar 16, 2003 · N923FT · Boeing 7472U3B · Trailing Flap Position Indicating SystemSDR P5CA0300769Skin · dentedDENT PUSHED INBD AT EXT FUSELAGE SKIN STA 400 LH - STR 27. DAMAGE AREA TRIMMED OUT. REINFORCED AREA W/ DOUBLER PER SRM 53-30-03, FIG. 1.Feb 24, 2003 · N923FT · Boeing 7472U3B · Fuselage Main, Plate/SkinSDR P5CA0300768Seat Track · corrodedLEVEL 1 CORROSION FOUND UPPER LOBE MAIN DECK SEAT TRACK LBL 1133, RT STA 1480-1660. DAMAGE SEAT TRACK PORTION REMOVED. NEW FABRICATE M/F 7075T6SM EXTRU BAC 1520-1889 PER DWG 866-17-19743-SH-2.Feb 24, 2003 · N923FT · Boeing 7472U3B · Fuselage Miscellaneous StructureSDR P5CA0300738Frame · crackedCRACK, APPROX. 1", FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FRAME ON HORIZONTAL FLANGE, STARTING FROM TOP EDGE. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/RibSDR P5CA0300737Frame · crackedCRACK 1-1/2" FOUND #3 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST L/H FWD FRAME REAPIR ANGLE, STARTING FROM TOP EDGE RADIUS. FRAME REPAIR ANGLE REPLACED PER SRM 54-10-03 & FAA FORM 8110-3.Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/RibSDR P5CA0300736Frame · cracked5 CRACKS TOTAL FOUND #2 PYLON REAR ENG. MOUNT BULKHEAD TOP MOST FWD FRAME. L/H: (1) 2" CRACK ON L/H SIDE FRAME, STARTING FROM TOP EDGE ON VERTICAL FLANGE. R/H: (3) 1/2" EA. CRACKS ON R/H SIDE, STARTING ON 1ST AFT FASTENER HOLE FROM TOP ON HORIZONTAL FLANGEJan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/RibSDR P5CA0300735Frame · crackedCRACK FOUND #1 PYLON REAR ENG. MOUNT BULKHEAD L/H FWD FRAME APPROX. 1/2" FROM TOP RADIUS. FRAME REPAIR CARRIED OUT PER SRM 54-10-03 & FAA FORM 8110-3.Jan 23, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/RibSDR P5CA0300734Skin · crackedEVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 L/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO THE VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9.Jan 22, 2003 · N922FT · Boeing 7472U3B · Passenger/Crew DoorsSDR P5CA0300733Skin · crackedEVIDENCE OF CRACK ON MAIN ENTRY DOOR 1 R/H, AFT LWR OUTER SKIN EMANATING FROM A FASTENER HEAD COMMON TO VERT. INTERCOSTAL. CRACKED SKIN CUT OUT. DOOR SKIN REPAIR CARRIED OUT IAW SRM 52-10-02, FIG. 9.Jan 22, 2003 · N922FT · Boeing 7472U3B · Passenger/Crew DoorsSDR P5CA0300732Fitting · corrodedCORROSION LEVEL 1 FOUND ON LINE SHROUD FITTING DURING REMOVAL OF APU FUEL LINE SHROUD FIBERGLASS CLOSE OUT PANEL. NEW SHROUD LINE FITTING INSTALLED & LEAK CHECK CARRIED OUT PER MM 28-25-04. FOUND SATISFACTORY AND NO LEAKS OBSERVED.Jan 22, 2003 · N922FT · Boeing 7472U3B · APU Engine Fuel and ControlSDR P5CA0300731Panel · delaminatedDELAMINATION FOUND L/H WING LEADING EDGE TOP PANEL AT FSSD 1550 (O/B MOST). PANEL REPAIR CARRIED OUT PER SRM 51-40-12 & SRM 51-30-20.Jan 20, 2003 · N922FT · Boeing 7472U3B · Wing, Plate/SkinSDR P5CA0300730Support Angle · crackedCRACK APPROX. 2-3/4" FOUND #4 PYLON AFT ENG. BULKHEAD FRAME AT NAC STA 221.90 MID SPARE WEB LWR LATERAL SUPPORT ANGLE AT MID SECTION & JOINTING 3 FASTENERS. REPLACEMENT OF CRACKED LATERAL SUPPORT ANGLE CARRIED OUT PER SRM 51-10-01.Jan 20, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Bulkhead/FirewallSDR P5CA0300729Frame · crackedCRACK FOUND #4 PYLON REAR ENG. MOUNT BULKHEAD FRAME ASSY BELOW NAC WL 167.0 ON L/H FWD, R/H FWD & AFT AT FASTENER HOLE. REPLACEMENT OF CRACKED FRAME ASSY CARRIED OUT AS PER SRM 51-10-01Jan 19, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Frame/Spar/RibSDR P5CA0300725Brace · gougedNICK/GOUGE FOUND AT SAILBOAT AREA OF PYLON #1 DIAGONAL BRACE - LOCATED APPROX 10:00 O'CLOCK POSITION, 29" FROM FWD END AT ZONE 5. DAMAGED AREA BLEND-OUT CARRIED OUT - FINAL DIMENSION LENGTH 2.0, WIDTH 1.525, DEPTH 0.100. THESE FIGURES ARE WITHIN LIMITS PER BOEJan 14, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach FittingsSDR P5CA0300724Stiffener · corrodedCORROSION LEVEL 1 FOUND R/H WING LEADING EDGE FRONT SPAR "L" STIFFENER AT FSSI 1435 LOWER PORTION. REPAIR CARRIED OUT IAW SRM 51-30-02.Jan 12, 2003 · N922FT · Boeing 7472U3B · Wing Miscellaneous StructureSDR P5CA0300723Stiffener · corrodedCORROSION LEVEL 1 FOUND LEADING EDGE TOP PANEL SUPPORT RIB AT STA. FSS 1336.00, "L" ANGLE STIFFENER TO FRONT SPAR. "L" ANGLE REPAIR CARRIED OUT AS PER SRM 51-30-02.Jan 12, 2003 · N922FT · Boeing 7472U3B · Wing Miscellaneous StructureSDR P5CA0300722Fitting · crackedSIX CRACKS TOTAL FOUND NR 4 REAR ENG MOUNT BATHTUB FITTING: I/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .1875 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) .125 INCH, (1) .5 INCH & (1) .75 INCH RADIALLY. CRACKED BATHTUB FITTING Jan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach FittingsSDR P5CA0300721Fitting · crackedFIVE CRACKS TOTAL FOUND NR 3 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1.5 INCH & (1) .75 INCH RADIALLY. O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .5 INCH & (2) .125 INCH EA RADIALLY. CRACKED BATHTUB FITTINGJan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach FittingsSDR P5CA0300720Fitting · crackedFIVE CRACKS TOTAL FOUND NR 2 PYLON REAR ENG MOUNT BULKHEAD BATHTUB FITTING: I/B FASTENER HOLE HAS 2 CRACKS - (1) APPROX 1 INCH & (1) .875 INCH RADIALLY/ O/B FASTENER HOLE HAS 3 CRACKS - (1) APPROX .75 INCH & (2) 1 INCH EA RADIALLY. CRACKED BATHTUB FITTING REPJan 12, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach FittingsSDR P5CA0300718Fitting · crackedTWO CRACKS FOUND AROUND INBOARD AND OUTBOARD FASTENER HOLES NR 1 PYLON REAR ENGINE MOUNT BULKHEAD BATHTUB FITTING. - I/B: (1) .75 INCH, (1) .125 INCH RADIALLY. O/B: (1) .75 INCH, (1) .5 INCH RADIALLY. CRACKED BATHTUB FITTING REPLACED AS PER S/B 747-54-2113 R2Jan 9, 2003 · N922FT · Boeing 7472U3B · Nacelle/Pylon, Attach FittingsSDR P5CA0300728Rod · corrodedCORROSION LEVEL 1 FOUND ON L/H INBD ELEVATOR POWER CONTROL PACKAGE ROD END, WITH TEFLON SEAL ADRIFT. POWER CONTROL PACKAGE REPLACED IAW MM 27-31-07.Dec 31, 2002 · N922FT · Boeing 7472U3B · Elevator Control SystemSDR P5CA0200705Tire · out of balanceON TAKEOFF ROLL FROM RWY 24L-ANC, A VIBRATION BEGAN & INCREASED IN INTENSITY. AT 100 KTS IT BECAME VERY SEVERE. T/O WAS REJECTED AT 110 KTS. VIBRATION SEEMED MOST SEVERE IN NOSE GEAR REGION OR MAIN GEAR. DURING DECELERATION, A/C PULLED TO THE RIGHT. PERFOOct 26, 2002 · N923FT · Boeing 7472U3B · TireSDR P5CA0200674Indicator · faultyNR 3 ENG START VALVE OPEN LIGHT CAME ON AFTER TAKEOFF AT 8,000 FT. SHUT DOWN NR 3 ENG, LIGHT WENT OUT AFTER SHUT DOWN AT APPROX 3,000 FT. TROUBLESHOT SYSTEM AND FOUND LIGHT INDICATION SYSTEM AT FAULT.May 13, 2002 · N923FT · Boeing 7472U3B · Engine Start Valves/ControlsSDR P5CA0200671Seal · burnedNR 4 ENGINE 1ST STAGE TURBINE OUTER AIR SEAL HAS 2 INCH BURN THROUGH. ENGINE TO BE REMOVED FROM SERVICE IN 60 HRS PER MM 72-00-00, PAGE 680N, TABLE 6.Apr 10, 2002 · N923FT · Boeing 7472U3B · Turbine SectionSDR P5CA0200658Screw · missingL/H INBD L/E FLAPS ARE DEPLOYED BUT IND UP AT F/E'S PANEL & FWD IND. ON INSPECTION FOUND PDU DRIVE SHAFT DISCONNECTED, LOCKING SCREW MISSING & LOCKING SLEEVE MIGRATED FROM CONNECTION. RE-RIGGED & RE-ATTACHED DRIVE SHAFT IAW MM 27-81-02. OPS CHECK NORMAL.Mar 6, 2002 · N923FT · Boeing 7472U3B · Leading Edge Slat Control SystemSDR P5CA0200655Plug · missingPDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK.Feb 26, 2002 · N922FT · Boeing 7472U3B · Flight Control SystemSDR P5CA0200653Panel · crackedCRACK LT WING REAR SPAR TO INBOARD AILERON TRAILING EDGE UPPER PANEL (573ST). PANEL ASSY REPLACED REF SRM 51-10-01.Feb 26, 2002 · N922FT · Boeing 7472U3B · Wing, Plate/SkinSDR P5CA0200654Panel · damagedDAMAGE LT WING UPPER PANEL STATION WS 440.62, ABOVE KRUEGER FLAPS 11/13. NO CRACK FOUND. REPAIR CARRIED OUT WITH REF TO SRM 51-40-09 & 51-40-15.Feb 25, 2002 · N922FT · Boeing 7472U3B · Wing, Plate/SkinSDR P5CA0200639Latch · unlockedAFTER TAKEOFF, MAIN DECK SIDE CARGO DOOR LIGHT ILLUMINATED. EMERGENCY DECLARED. 180,000 LBS OF FUEL WAS JETTISONED AND PRECAUTIONARY RETURN TO ICN WAS COMPLETED. WARNING LIGHTS REMAINED ILLUMINATED AT BLOCK IN. UPON INSPECTION, FOUND LATCH IN THE UNLOCKED Feb 3, 2002 · N923FT · Boeing 7472U3B · Cargo/Baggage DoorsSDR P5CA0200626Reducer · crackedLOST ALL HYD ON NR 1 HYD SYS AFTER LANDING. FOUND RT TRUCK POSITIONER BYPASS REDUCER FLANGE CRACKED. REMOVED AND REPLACED ASSY PER MM 32-13-16, IPC 32-13-05-02 NR 40. BLED SYSTEM UNTIL NO AIR NOTED.Jan 12, 2002 · N923FT · Boeing 7472U3B · Hydraulic System, MainSDR P5CA0100611Web · cracked1-1/2" CRACK BETWEEN STA 280 & 300 LH OB INTERCOSTAL ON NOSE WHEEL WELL ROOF RUNNING ACROSS UPPER FLANGE & DOWN THE WEB OF THE "Z" SECTION. NO ADJACENT FASTENERS ARE MISSING, LOOSE OR SHEARED. REPAIRED AS PER SRM 51-40-04, FIG 2, DETAIL 2.Nov 13, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, StructureSDR P5CA0100612Web · cracked6" CRACK AT STA 300 RH NOSE WHEEL WELL BEAM RUNNING ACROSS WEB, EMINATING FROM INSULATION BLANKET STANDOFF HOLE. NO ADJACENT FASTENERS LOOSE, SHEARED OR MISSING. REPAIR CARRIED OUT IAW SRM 51-40-02, FIG 1, SHT 5, DETAIL 3. PARTS TREATED W/ ALODINE 1200 & REPAINov 13, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, StructureSDR P5CA0100603Light · inoperativeUPPER DECK CENTER EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER MM 33-51-00.Oct 21, 2001 · N923FT · Boeing 7472U3B · Emergency LightingSDR P5CA0100594Engine · malfunctionedWHEN THROTTLES WERE RETARDED FOR DESCENT, NR 2 ENG HAD EXCESSIVE VIBRATION FOLLOWED BY UNCLEARABLE STALL CONDITION. ENG SHUTDOWN WAS ACCOMPLISHED NORMALLY. LUBRICATED BLEED FEEDBACK PUSH PULL CABLE SYSTEM. INSPECTED ENG INLET EXHAUST BLEEDS. OPS CHECKED OKSep 20, 2001 · N922FT · Boeing 7472U3B · Engine (Turbine/Turboprop)SDR P5CA0100591Warning System · malfunctionedMAIN DECK SIDE CARGO DOOR WARNING LIGHT ILLUMINATED DURING ROTATION AT TAKEOFF. AIRCRAFT RETURNED TO AIRPORT. CYCLED DOOR OPEN AND INSPECTED LATCHES. DOOR CLOSED OK AND LOCKING LEVER CLOSED DOWN. OK FOR SERVICE PER MM 52-32-00.Sep 14, 2001 · N923FT · Boeing 7472U3B · Door Warning SystemSDR P5CA0100514Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT SEVEN ON UPPER RUDDER. REPAIRED PER S/L 747-55-07.Mar 28, 2001 · N923FT · Boeing 7472U3B · Rudder StructureSDR P5CA0100523Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE UPPER RUDDER. REPAIRED PER S/L 747-55-07.Mar 26, 2001 · N923FT · Boeing 7472U3B · Rudder StructureSDR P5CA0100522Skin · corrodedLEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 1319 WL 214 AND WL 227. REPAIRED PER SRM 51010-01.Mar 26, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Plate/SkinSDR P5CA0100521Stringer · corrodedLEVEL 1 CORROSION FOUND ON BS 1700-STR 44 RIGHT, BS 1775- STR 48 RIGHT. SECTION REPLACED PER SRM 53-30-03.Mar 26, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Longeron/StringerSDR P5CA0100520Intercostal · crackedCRACK FOUND ON INTERCOSTAL BULK CARGO BS 2040 LBL-30. REPAIRED PER SRM 53-10-07.Mar 26, 2001 · N923FT · Boeing 7472U3B · Fuselage Miscellaneous StructureSDR P5CA0100519Skin · corrodedLEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2060-STRINGER 46R. REPAIRED PER SRM 51-10-01.Mar 26, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Plate/SkinSDR P5CA0100518Stringer · corrodedLEVEL 1 CORROSION FOUND ON BS 1765-STRINGER 49R, BS 1640-STRINGER 48L, BS 1920-STRINGER 49L. REPAIRED PER SRM 51-10-01.Mar 26, 2001 · N923FT · Boeing 7472U3B · Fuselage Main, Longeron/StringerSDR P5CA0100517Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE LEFT OUTBOARD AILERON NR 3 POSITION. REPAIRED PER S/L 747-55-07.Mar 26, 2001 · N923FT · Boeing 7472U3B · AileronsSDR P5CA0100516Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT THREE LEFT OUTBOARD ELEVATOR. REPAIRED PER S/L 747-55-07.Mar 26, 2001 · N923FT · Boeing 7472U3B · Elevator Structure
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