Boeing 747-2U3B
Service difficulty reports · 125
Newest first. General aviation reporting is voluntary.
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.
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
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR P5CA0300883Bulkhead · crackedCRACKS FOUND ON AFT TORQUE BULKHEAD ON NR 1 & 4 PYLONS. REPAIRED PER SB 54-2201 BOEING PAO R11-03-00004H.SDR P5CA0300882Bulkhead · crackedCRACK FOUND ON 1480 LWR BULKHEAD RT SIDE. REPAIRED PER S/B 53-2390.SDR 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.SDR 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.SDR P5CA0300872Nozzle · leakingDURING FUELING LEAK WAS OBSERVED FROM LT WING FUEL JETTISON NOZZLE VALVE. REPLACED LT FUEL JETTISON NOZZLE VALVE.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 FLANGESDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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.SDR 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 51-10-01SDR 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 BOESDR 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.SDR 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.SDR 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 SDR 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 FITTINGSDR 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 REPSDR 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 R2SDR 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.SDR 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. PERFOSDR 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.SDR 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.SDR 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.SDR P5CA0200655Plug · missingPDU NR 4 DRAIN PLUG MISSING. INSTALLED PLUG AND FILLED PDU IAW 12-13-12. PDU RAN OK.SDR P5CA0200653Panel · crackedCRACK LT WING REAR SPAR TO INBOARD AILERON TRAILING EDGE UPPER PANEL (573ST). PANEL ASSY REPLACED REF SRM 51-10-01.SDR 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.SDR 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 SDR 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.SDR 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.SDR 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 & REPAISDR P5CA0100603Light · inoperativeUPPER DECK CENTER EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER MM 33-51-00.SDR 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 OKSDR 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.SDR P5CA0100514Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT SEVEN ON UPPER RUDDER. REPAIRED PER S/L 747-55-07.SDR P5CA0100523Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE UPPER RUDDER. REPAIRED PER S/L 747-55-07.SDR P5CA0100522Skin · corrodedLEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 1319 WL 214 AND WL 227. REPAIRED PER SRM 51010-01.SDR P5CA0100521Stringer · corrodedLEVEL 1 CORROSION FOUND ON BS 1700-STR 44 RIGHT, BS 1775- STR 48 RIGHT. SECTION REPLACED PER SRM 53-30-03.SDR P5CA0100520Intercostal · crackedCRACK FOUND ON INTERCOSTAL BULK CARGO BS 2040 LBL-30. REPAIRED PER SRM 53-10-07.SDR P5CA0100519Skin · corrodedLEVEL 1 CORROSION FOUND ON FUSELAGE SKIN BS 2060-STRINGER 46R. REPAIRED PER SRM 51-10-01.SDR P5CA0100518Stringer · corrodedLEVEL 1 CORROSION FOUND ON BS 1765-STRINGER 49R, BS 1640-STRINGER 48L, BS 1920-STRINGER 49L. REPAIRED PER SRM 51-10-01.SDR P5CA0100517Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT ONE LEFT OUTBOARD AILERON NR 3 POSITION. REPAIRED PER S/L 747-55-07.SDR P5CA0100516Balance Weight · corrodedLEVEL 1 CORROSION FOUND ON BALANCE WEIGHT THREE LEFT OUTBOARD ELEVATOR. REPAIRED PER S/L 747-55-07.
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