Boeing 747-2D7B
Service difficulty reports · 726
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 = '7472D7B' 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 = '7472D7B' 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 UIEA200700116Bear Strap · crackedFOUND CRACK IN BEARSTRAP HOLE FORWARD CARGO DOOR FORWARD UPPER CORNER. REAMED HOLE COMMON TO SKIN AND BEARSTRAP TO REMOVE CRACK INDICATION AND INSTALLING FREEZE PLUG AND OVERSIZED FASTENER AS PER BOEING MESSAGE 1-285675404-1 AND 8100-9.SDR UIEA200700115Skin · corrodedFOUND BS 1240 LBL 99 WING CENTER SECTION SKIN CORRODED. CORROSION REMOVED PER SRM 51-10-01. AREA HFEC INSPECTED AND FLAT PEENED. REPAIR DOUBLER WERE FABRICATED AND INSTALLED PER 8100-9.SDR UIEA200700105Shear Tie · crackedBS 860L TENSION TIE ATTACHMENT FOUND ONE HOLE CRACKED. TENSION TIE REPAIRED AS PER BOEING MESSAGE DRAWING 1-283852979-4.SDR UIEA200700112Frame · crackedFOUND BS 840 FRAME TO TENSION TIE CONNECTION FOUND 1 HOLE CRACKED. REPAIR ACCOMPLISHED PER BOEING DRAWING ON MESSAGE 1-283852403-4.SDR UIEA200700104Doubler · crackedBS 800 STR 19R DOOR CUTOUT DOUBLER FOUND CRACKED. REPAIRED PER BOEING MESSAGE 1-285788451-4. TRIMMED AND REMOVED DAMAGED FRAME STRAP NDT AREA. FABRICATED REPAIR STRAP AND DOUBLER. ALODINED AND COATED WITH BMS 5-95 BETWEEN MATING SURFACE. INSTALLED HI LOCKSDR UIEA200700103Floorbeam · crackedFOUND UPPER DECK FLOORBEAM AT BS 420R ONE FASTENER HOLE CRACK AT FRAME WEB. THE CRACK WAS TRIMMED OUT AND REPAIRED PER BOEING MESSAGE AND SRM 53-10-04 FIG 107.SDR UIEA200700102Floorbeam · crackedUPPER DECK FLOORBEAM AT BS 340L ONE FASTENER HOLE CRACK AT FRAME WEB. THE CRACK WAS TRIMMED OUT AND REPAIRED PER BOEING MESSAGE AND SRM 53-10-04 FIG 102.SDR UIEA200700091Csd · leakingDIVERSION TO JFK WHILE AIRCRAFT WAS EN ROUTE TO PIK FROM CHS. AT LEVEL OFF AT FL 33.0 #3 ENGINE OIL QTY DROPPED TO 2 GALLONS. 15 MIN LATER DROPPED TO 0.5 GALLONS. ENGINE POWER REDUCED TO IDLE. REINSTALLED PREVIOUSLY DEFERRED GENERATOR AND REPLACED THE CSD.SDR UIEA200700092Relief Valve · failedDURING PASSING 3000' WHEN PACKS WERE TURNED ON DUCT PRESS LOW LIGHT ILLUMINATED. DUCT PRESS 9 PSI. ENGINE BLEED VALVES 2, 3 AND 4 OPEN. REMOVED AND REPLACED NR 4 PRESS RELIEF VALVE. LEAK CHECKED COMPLIED WITH, NO DEFECTS AT THIS TIME REF AMM 71-00-00.SDR UIEA200700073Duct · damagedNUMBER ONE POSITION ENGINE SERIAL NUMBER 517598 WAS FOUND WITH A 4 INCH BLOWN HOLE ON 8TH STAGE "Y" DUCT. DUCT WAS REMOVED AND REPLACED AS PER 747 MM 75-25-00.SDR UIEA200700068Altimeter · faultyCAPT ALT UNRESPONSIVE TO ALL CHANGE BOTH CADC/STBY MODES, PERFORMED CHECK DIFFERENCE BETWEEN ALT INDICATORS (3,34,7), CHANGE ALT LAGS IN DESCENT BY OVER 300' AND DIFFERS BY OVER 180' AT EL 290-310-MACH .84. T/S AND FOUND PIN NR 22 AT PLUG DN 101. CAPT ALT INSDR UIEA200700066Cadc · stickingDURING CLIMB CAPT ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNINGS, DON’T SINK WARNING AUDIBLES, ALTIMETER READ 37.0, ATC 36.8. PERFORMED STATIC SYSTEM LEAK CHECK NORMAL AS PER MM 34-11-00. FOUND NR 1 CADC DEFECTIVE. REMOVED AND REPSDR UIEA200700065Altimeter · stickingDURING CLIMB CAPT'S ALTIMETER NEEDLE WOULD STICK IN POSITION CAUSING PULL-UP TERRAIN WARNING, DON'T SINK WARNING AUDIBLES. CAPT'S ALTIMETER REMOVED AND REPLACED, INDICATION AND LEAK CHECK CARRIED OUT, OK IAW MM 34-13-04.SDR UIEA200700061Beam · crackedDURING NDT INSPECTION OF THE RT WING GEAR DOOR ACTUATOR BEAM IAW NDT MANUAL D6-7170, PART 4, 32-10-01. FOUND ACTUATOR BEAM BEARING BORE HOLE CRACKED. CRACK LOCATED WITHIN THE REQUIRED INSPECTION AREA. REPLACED ACTUATOR BEAM IAW AMM 32-32-28.SDR UIEA200700050Floorbeam · crackedM/DECK STA 260 RBL90 FLOORBEAM UPPER CHORD FOUND CRACKED. REPAIRED ACCOMPLISHEED AS PER BOEING SR ID NR 1-273725179 AND FAA FORM 8100-9.SDR UIEA200700054Stringer · corrodedAFT CARGO BS 1700 STRINGER S-46L FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272065605 AND FAA FORM 8100-9.SDR UIEA200700051Skin · damagedFUSELAGE BS 2300 S-23 EXISTING DOUBLER FOUND DAMAGED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-274437619.SDR UIEA200700052Floorbeam · crackedBS 400 RT UPPER DECK FLOORBEAM UPPER CHORD FOUND HOLES AND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271227292 AND FAA FORM 8100-9.SDR UIEA200700044Shear Web · crackedM/DECK STA 840 RT TENSION TIE ATT SLOPING WEB AT FWD CORNER FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-30-02.SDR UIEA200700041Bearing · migratedLT WING NR 3 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATION. REPAIRED ACCOMPLISHED AS PER SB747-57-2325.SDR UIEA200700043Shear Web · crackedM/DECK STA 840 LT TENSION TIE ATT SLOPING WEB FWD CORNER FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-30-02.SDR UIEA200700042Bearing · migratedRT WING NR 6 FLAP TRACK FWD ATTACH FITTING BEARING FOUND MIGRATED. REPAIRED ACCOMPLISHED AS PER SB747-57-2325.SDR UIEA200700040Floorbeam · crackedUPPER DECK FLOOR BEAM UPPER CHORD LT STA 380 FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271217089 AND FAA FORM 8110-9.SDR UIEA200700032Frame · crackedRT NR 2 MED FWD CUTOUT MIDDLE AREA FOUND CRACKED AT TWO LOCATIONS. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272479981 AND FAA FORM 8110-9.SDR UIEA200700033Access Panel · wornNR 2 PYLON RT ACCESS PANEL 463AR CUTOUT FOUND WORN AT TWO POSITIONS. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272049267 AND FAA FORM 8110-9.SDR UIEA200700037Shear Tie · corrodedAFT CARGO STA 1800 FRAME SHEAR TIE S-50R TO S-51L FOUND CORRODED. AFT CARGO STA 1800 FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.SDR UIEA200700036Shear Tie · corrodedAFT CARGO STA 1760 FRAME SHEARTIE S-50L TO S-51L FOUND CORRODED. AFT CARGO STA 1760 FRAME SHEAR TIE REPAIRED AS PER SRM 53-10-04 FIG 3A.SDR UIEA200700035Bulkhead · crackedFUSELAGE STA 260 BULKHEAD LT LBL60 CANTED BULKHEAD WEB FOUND CRACKED. BULKHEAD STA 260 WEB REPAIRED AS PER SRM 53-10-04 FIG 47.SDR UIEA200700031Stringer · corrodedBULK CARGO STA 2200-2220 STR 49L FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271194583 AND FAA FORM 8110-9.SDR UIEA200700034Skin · chafedNR 3 PYLON RT ACCESS PANEL 473AR CUTOUT AT NAC STA 286 TO STA 300 FOUND CHAFING. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-272049267 AND FAA FORM 8110-9.SDR UIEA200700026Panel · crackedLT WING PYLON GAP PANEL AT ILES 640.47 HAS A 3.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 18 SHEET 5 AND SRM 51-40-12, ALSO REFERENCE ATLAS AIR EO 4757A342.SDR UIEA200700027Panel · crackedLT WING UPPER FIXED PANEL, 12 INCHES FROM FORWARD EDGE OF NR 5 SPOILER, WBL 421.00 HAS A 6.0 INCH CRACK. ACCOMPLISHED PERMANENT REPAIR AS PER 747 SRM 51-40-09 FIG 2 SHEET 5 AND SRM 51-40-12 AND ATLAS AIR EO 4757A342.SDR UIEA200700038Start Valve · faultyNR 3 ENGINE START VALVE OPEN LIGHT CAME ON DURING CRUISE, FOLLOWED FHB PROCEDURES AND SHUT DOWN THE ENGINE. TRANSFERRED TO DEFERRED ITEM M07-010, MEL 80-1-1. AS PER MCC REQUEST REMOVED AND REPLACED START VALVE. REMOVED AND REPLACED START VALVE AS REQUIRED.SDR UIEA200700022Angle · damagedNR 2, NR 3 AND NR 4 LT FAN T/REV ACCESS DOOR CLOSEOUT ASSY ANGLE FOUND DAMAGED. REPAIR ACCOMPLISHED AS PER EO NR 4778A091 AND FAA FORM 8110-3.SDR UIEA200700029Mec · unserviceableNR 3 ENGINE ROLLED BACK IN CLIMB TO 42.6 PERCENT N1, 663KGS/HR FUEL FLOW WOULD NOT RESPOND TO THROTTLE MOVEMENT TO ADD POWER. LOW THRUST CONFIRMED BY HIGH STAGE LIGHT ON, BLEED VALVE CLOSED LIGHT ON. REPLACED NR 3 MEC ,FUEL PUMP,AND CIT SENSOR. ACCOMPLISHEDSDR UIEA200700021Ring · damagedNR 3 ENGINE RT T/REV OUTER SUPPORT RING AFT I/B EDGE DAMAGED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A090 AND FAA FORM 8110-3.SDR UIEA200700019Transfer Tube · wornRT WING NR 3 RESERVE TANK AT WS 1454 TRANSFER TUBE ASSY 2 COTTER PINS HOLES FOUND WORN. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-276113094 AND EO NR 4728A027.SDR UIEA200700020Skin · debondedNR 1 ENGINE RT T/REV TRANSLATING COWL UPPER EDGE SKIN FOUND DEBOND. REPAIR ACCOMPLISHED AS PER EO NR 4778A088 AND FAA FORM 8110-3.SDR UIEA200700017Fitting · crackedCRACKS FOUND ON RT HORIZ STAB AT HOLE 15 IN THE SPLICE PLATE AND HOLE 28 IN THE HINGE FITTING. REPAIRED ACCOMPLISHED AS PER BOEING SRM ID NR 1-273714301 AND FAA FORM 8110-9.SDR UIEA200700016Rib · crackedLT WING INBOARD FIXED LEADING EDGE RIB AT ILES 1024.45 FOUND CRACKED IN THE INTEGRAL STIFFENER ATTACHING THE UPSTOP FITTING INTERCOSTAL. INTERIM REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-271219411 AND FAA FORM 8100-9.SDR UIEA200700015Crease Beam · crackedM/DECK STA 940-960 S-7R TO S-8R CREASE BEAM WEB FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 51-10-01.SDR UIEA200700014Cowling · crackedAS PER N/R 746, NR 3 ENG RT T/REV TRANSLATING COWL UPPER FAIRING (BEAVER TAIL) INTERIOR SKIN FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER EO NR 4778A089 AND FAA FORM 8110-3 DATED 12 JAN, 2007.SDR UIEA200700013Seat · crackedCRACK AND GOUGES WERE FOUND ON 2ND OBSERVER SEAT. REPAIR ACCOMPLISHED AS PER EO NR 4725A223 AND FAA FORM 8110-3 DATED 17 JAN 2007.SDR UIEA200700012Panel · dentedRT WING INBOARD LEADING EDGE PANEL AT WBL 158.0 HAS A 2.0 INCH LONG BY 1.5 INCH WIDE BY .073 INCH DEEP DENT. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 18 SHEET 1 THRU 5. ALSO, REFERENCE ATLAS AIR EO NO. 4757A314.SDR UIEA200700011Skin · crackedLT WING, UPPER SURFACE, TRAILING EDGE PANEL, AFT OF REAR SPAR, WBL 445 IS CRACKED AROUND FASTENER HOLE. ACCOMPLISHED PERMANENT REPAIR AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1 THRU 5. REPAIR AREA IS 4.0 INCH BY 4.0 INCH ALSO, REFERENCE ATLAS AIR EO NR 475SDR UIEA200700010Frame · crackedCABIN BS 2231 RT FRAME INNER CHORD S-25R FOUND CRACK ON FASTENER HOLE AT STRAP. REPAIR ACCOMPLISHED AS PER SRM 53-10-04 FIG 115.SDR UIEA200700008Frame · crackedCABIN BS 2231 LT FRAME UPPER STRAP AND INNER CHORD FOUND CRACKED. CABIN BS 2231 LT FRAME UPPER STRAP AND INNER CHORD REPAIRED AS PER SRM 53-10-04 FIG 115.SDR UIEA200700009Frame · crackedNR 1R BS 488 CUTOUT FRAME WEB AT STOP NR 1 FOUND CRACKED. NR 1R BS 488 FRAME REPAIRED PER SRM 53-10-04 FIG 92.SDR UIEA200700005Frame · crackedDURING PERFORMANCE OF EO NR 4753A531 AS PER AD 2005-22-06, AS PER NON ROUTINE CARD NR 212 CRACK FOUND DURING HFEC AT BS 488 MAIN ENTRY DOOR 1R CUT OUT FRAME WEB AT STOP 9. BS 488 MED FRAME REPAIRED AS PER SRM 53-10-04 FIG 121.SDR UIEA200700004Door Frame · crackedAT XMN UNDER C-1 CHECK, DURING PERFORMING EO NR 4753A531 AS PER AD 2005-22-06.AS PER NR NR 215, CRACK FOUND DURING HFEC AT BS488 ME DOOR 1L CUT OUT FRAME WEB AT STOP 9. RECTIFICATION, BS 488 MED 1L DOOR FRAME WEB REPAIRED AS PER SRM 53-10-04 FIG 121.
Back to Boeing 747-2D7B