Boeing 747 212B
Service difficulty reports · 2,202
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 = '747212B' 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 = '747212B' 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 EIAA2010012Light · inoperativeUPPER DECK DOME LIGHT (EMERG) INOP. RELAMPED DOME LIGHT, OP'S CHECKED OK PER M/M 33-51-07.SDR EIAA2010011Battery Pack · dischargedL1 DOOR FWD THRESHOLD. REPLACED EMERGENCY LIGHT BATTERY PACK, OP'S CHECK OK PER 33-51-07.SDR EIAA2010009Fitting · crackedNR 1 PYLON UNDERWING DIAGONAL FTG FOUND CRACKED. REPLACED PER EO 57-747-1404-95 REV C.SDR EIAA2010008Fitting · crackedNR 3 PYLON UNDERWING DIAGONAL FITTING FOUND CRACKED AT AFT END OUTBOARD RADIUS 3.5 INCHES LONG. REPLACED DIAGONAL BRACE UNDERWING FITTING PER EO 57-747-1404-95 REV C P/N ON IS 65B07795U23.SDR EIAA2010007Skin · corrodedFUSELAGE EXTERIOR CORROSION, POST CLEAN UP EXCEED LIMITS. REPAIRED PER SRM 53-20-03 FIG 1 CAT B REPAIR DUE INSPECTION AT (THRESHOLD) 15,000 CYCLES LFEC.SDR KCSA101015Rib · crackedLEFT WING T/E HAS A LOWER RIB CHORD CRACKED AT WBL 445.SDR EIAA20100005Structure · damagedREPAIRED DAMAGE ON RIGHT SIDE OF AIRCRAFT PER ECRA 485-53-193-1 AND ECRA 485-53-194-1, SRM REF 51-40-03 FIG 4 AND SRM REF 53-10-03 FIG 4.SDR EIAA2010005Skin · damagedAIRCRAFT RT UPPER FUSELAGE CROWN AREA DENTED AND GOUGED.SDR EIAA2010004Structure · damagedWHILE TOWING AIRCRAFT OUT OF HANGAR HIGH DOOR WAS NOT OPENED FULLY, TOP OF VERT FIN DAMAGED APPROX 12 INCHES AND FROM TRAILING EDGE. FOUR (4) INCHES BROKE OFF TOP STATIC WICKS. REPAIRED DAMAGE ON RIGHT SIDE OF AIRCRAFT PER ECRA 485-53-193-1 AND ECRA 485-53-1SDR EIAA2010001Cover · missingLEFT NR 1 DOOR UPPER JAM FWD EMERGENCY LIGHT COVER FOUND MISSING. LEFT NR 1 DOOR UPPER JAM EMERGENCY LIGHT LENS INSTALLED AND CONDITION FOUND SATISFACTORY PER MM 33-51-06.SDR KCSA091142Light · inoperativeEXTERIOR EMERGENCY SLIDE LIGHT INOP.SDR KCSA091141Light · inoperativeAFT UPPER DECK EMERGENCY LIGHT INOP.SDR KCSA091140Sign · inoperativeEMERGENCY EXIT SIGN OVER CREW SERVICE DOOR IS INOP.SDR KCSA091139Skin · corrodedLEFT WING UPPER SKIN CORRODED FWD OF FRONT SPAR AT WS 1485.SDR KCSA091138Light · inoperativeRIGHT SLIDE EXTERIOR EMERGENCY LIGHT IS INOP.SDR EIAA200900138Warning System · activatedAT 2000 FEET AGL CREW FELT A RUMBLE IN THE AIRFRAME AND DISCOVERED L1 DOOR LIGHT ON. ADJUSTED MAIN ENTRY DOOR GUIDE CAM AS PER 52-11-04, DOOR OPS CHECK NORMAL. THIS IS A SECOND OCCURRENCE REFERENCE SDR EIAA200900137.SDR EIAA200900137Unknown · malfunctionedAFTER TAKEOFF WHEN AC PACK WAS SELECTED THE L1 DOOR LIGHT ILLUMINATED, AIRCRAFT WOULD NOT PRESSURIZE. AFTER LANDING THE L1 DOOR LIGHT EXTINGUISHED. INSPECTED L1 DOOR IAW B747 MM 52-11-01 PG 601, NO DEFECTS FOUND.SDR EIAA200900136Oil System · leakingINFLIGHT SHUTDOWN OF ENGINE NR 1 FOR OIL LOSS. SERVICE ENG OIL, RAN AND INSPECTED ENG NR 1. FOUND OIL BEING BLOWN OUT OF RT 3.5 AND LT 3.5 UPPER BLEED VALVES. REPLACED NR 1 ENG EVC AND FILTER PER MM 75-31-09, 75-31-01. OPS CHECK NORMAL.SDR EIAA200900135Battery Pack · inoperativeEMERGENCY AREA LIGHT ASSY DIRECTLY OVER THE L5 DOOR EXIT LIGHT INOP. REMOVED AND REPLACED L5 DOOR EMERGENCY BATTERY PACK PER 747 MM 33-51-00. OPS CHECK GOOD.SDR EIAA200900131Fcu · malfunctionedDURING CRUISE, NR 4 ENGINE INDICATED LOSS OF THRUST. THRUST LEVER MOVEMENT CAUSED ALL ENG INDICATIONS TO FLUCTUATE. ENG NR 4 LEVER WAS REDUCED TO IDLE AN INFLIGHT START IAW COMPANY QRH PROCEDURES DURING DESCENT. S/D ENG NR 4 AS PRECAUTIONARY MEASURE DUE TO SDR EIAA200900130Unknown · malfunctionedEMERGENCY LIGHT UPPER DECK AFT CABIN DOES NOT TEST LONGER THAN 5 SECONDS.SDR EIAA200900133Skin · dentedFAA OFFICER SPOTTED FILLER FILLED AIRCRAFT OUTER SKIN AT LT BS 560 BETWEEN STR 28L-STR 29L. AREA CORRELATE TO DENT LOG N486-021 ENTRY FILLER REPAIRED REMOVED FILLERS FOR THE TWO SPOTS DESCRIBED. FOUND FWD DENT EXIT LIMITS. DENT NR 1 BS 564 STR 28L/29L WITHISDR EIAA200900127Circuit Card · defectiveUPON GEAR EXTENSION ALL PRIMARY SENSORS FOR ALL GEAR INOPERATIVE, ALL ALTERNATE SENSORS OK. WITH THIS THERE WAS NO RED GEAR UNSAFE LIGHT INDICATION TO INDICATE PRIMARY SENSOR FAILURES AND ALTERNATE SENSORS INDICATION DOWN AND LOCKED WHEN GOING BEYOND FLAPS 20SDR EIAA200900122Skin · damagedRT SEC 41 EXTERNAL SKIN BS 320-340 STR 2R - 5R 5 EACH DEFECT HOLES. FABBED REPAIR PARTS AND INSTALLED PER ECRA 486-53-073-2.SDR EIAA200900125Door Frame · corrodedR1 DOOR AFT FRAME CORRODED ON OUTER SURFACE AT LWR END OF FRAME. REMOVE DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 486-52-078-2.SDR EIAA200900124Skin · damagedRT SEC 41 EXTERNAL SKIN BS 320-340 STR 8R-10R 14 EA DEFECT HOLES. FABBED REPAIR PARTS AND INSTALLED PER ECRA 486-53-073-2.SDR EIAA200900123Skin · corrodedFWD PIT SKIN CORRODED AT BOTH PRESSURE RELIEF VALVES LWR CUTOUTS BS 770, STR 28L - 32L. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER B747 SRM 53-30-03 FIG 55.SDR EIAA200900121Door Frame · corrodedL3 DOOR FWD FRAME HAS CORROSION LWR CORNER VERTICAL SIDE. CUT OUT DAMAGE, FABBED AND INSTALLED REPAIR PER ECRA 486-52-076-2.SDR EIAA200900120Floorbeam · damagedAFT PIT FUS BS 1820 LT BUTT LINE 2, 23 AND 26 WL 118 FLOORBEAM UPPER CHORD DING. REMOVED DAMAGE, FABBED REPAIR AND INSTALLED PER B747 SRM 51-40-04 PF 5-9 DETAIL III FIG 2.SDR EIAA200900119Skin · corrodedRT WING LEADING EDGE CAVITY LWR SKIN "PAD UP" AT LES 1291 HAS CORROSION. REMOVED CORROSION, FABBED AND INSTALLED REPAIR PER ECRA 486-57-074-2 REV A.SDR EIAA200900118Skin · crackedL1 DOOR SKIN CRACK IN LOWER AFT CORNER COMMON TO DOOR FRAME. REMOVED DAMAGE, FABBED AND INSTALL REPAIR PER B747 SRM 52-10-02 PG 8-10A.SDR EIAA200900117Lamp · inoperativeUPPER DECK EMERGENCY LIGHT OUT OVER STAIRCASE (INSIDE LIGHT). RELAMPED OPS OK PER MM 33-42-02.SDR EIAA200900116Bracket · brokenEMERGENCY EXIT LIGHT AT BODY STATION 2120 LT SIDE ABOVE L5 DOOR BRACKET BROKEN. LIGHT REMOVED. REMOVED THE BROKEN BRACKET AND INSTALLED NEW BRACKET ASSY 33-4-0045-93-1 AS PER DRWG 33-4-045-93-33-4-046-93 AND SRM 51-40-031.SDR KCSA091106Light · inoperativeUPPER DECK FORWARD EMERGENCY LIGHT IS INOP.SDR KCSA091105Light · inoperativeUPPER DECK RT ESCAPE DOOR EMERGENCY LIGHT IS INOP.SDR EIAA200900112Skin · corrodedCORROSION ON SKIN UPPER DECK BETWEEN BS 620-640 ABOVE STR 6L. REMOVED DAMAGED AREA, FABBED AND INSTALLED REPAIR PARTS PER B747 SRM 53-30-03 FIG 17 SHEET 1.SDR EIAA200900107Door · crackedAFTER ALL GEAR EXTENSIONS, BODY GEAR, LT AND RT, OUTBOARD SECONDARY DOORS STRUCK NR 5 AND NR 10 MWT ASSY WHILE CLOSING CAUSING DENTS AND CRACKS TO CONTACT AREA. CUT OUT OUTER SHIM AND EDGE FRAME PER SRM 52-80-01. FLUSH REPAIR THE EDGE FRAME PER SRM 51-40-03 SDR EIAA200900103AFrame · crackedFRAMES AT LEFT BS 440, STR 10-10A AND BS 460, STR 0-16 CRACKED. ASSOCIATED FRAMES BS 420 AND BS 480 SHOWED NO DAMAGE. FRAMES AT BS 440 AND BS 460 WERE REPLACED PER ECRA 485-53-191-1.SDR EIAA20090906001Frame · crackedSUPPLEMENTAL INFORMATION: FRAMES AT LEFT BS 440, STRINGER 10-10A AND BS 460, STRINGER 0-16 CRACKED. ASSOCIATED FRAMES BS 420 AND BS 480 SHOWED NO DAMAGE. FRAMES AT BS 440 AND BS 460 WERE REPLACED PER ECRA 485-53-191-1.SDR EIAA200900103Fastener · missingMECHANIC FOUND EIGHT (8) MISSING FASTENERS ABOVE DOOR L-1 AT STA 440BS STRINGERS 10-10A. THIS IS A VERTICAL LINE OF FASTENERS.SDR EIAA200900106Battery Pack · dischargedRS DOOR FWD SILL LIGHT INOP 1 EA (P/N S1356B37 MRG 92843 9OVER RS DOOR). REPLACED 1 EA BATTERY PACK ON RS DOOR LIGHT. OPS CHECK OK IAW MM 33-51-04.SDR EIAA200900105Battery · dischargedEMERGENCY EXIT SIGN OVER UPPER DECK CREW DOOR INOP (BEHIND LAV) 1 EA. P/N 9008-3-5A MR G92843. RECYCLING THE EMERGENCY LIGHTS ON TO OFF SEVERAL TIMES CAUSED THIS BATTERY TO CHARGE. IT NOW CHECKS OK IAW MM 33-51-00.SDR EIAA200900104Battery Pack · dischargedLS DOOR BOTH SILL LIGHTS INOP 2 EA P/N S1356B37, MRG92843 (OVERHEAD NEAR CONTROL CABLES). REPLACED 2 EA BATTERY PACKS FOR THE LS DOOR SILL LIGHT, IAW MM 33-51-04.SDR KCSA09034Light · inoperativeEVAC CEILING LIGHT BY ESCAPE SLIDE DOES NOT ILLUMINATE. REPLACED LIGHT ASSEMBLY BY ESCAPE SLIDE CEILING REF MM 33-51-07. OPS CHECKS OK REF MM 33-51-00.SDR EIAA200900084Nut Plate · corrodedAFT CARGO DOOR 822D ACCESS PANEL NUT PLATE, AFT AREA FOUND CORROSION. AFT CARGO DOOR 822D ACCESS PANEL NUT PLATE, AFT AREA CORROSION REMOVED, FOUND BEYOND LIMITS. REPAIRED AS PER TEC-EVR-09-0004-05B AND EA-52-0064. REPAIR APPROVED THROUGH 8100-09 ISSUED BY SDR EIAA200900085Doubler · crackedFUSELAGE INTERNAL STRUCTURE UPPER LOBE DOUBLER AT BS 2517 STR 3R FOUND CRACK. STA 2517 RT SIDE CORROSION CLEARED AND CRACK STOP HOLE DRILLED. REINFORCEMENT DOUBLERS INSTALLED REF TEC-EVR-09-0002-10B STA 2517 LT SIDE, REINFORCEMENT DOUBLERS INSTALLED REF EC-ESDR EIAA200900083Floor Support · crackedBULK CARGO COMPT, BS 1980, LBL 40 FLOOR SUPPORT CRACKED. BULK CARGO COMPT, BS 1980, LBL 40 FLOOR SUPPORT REPAIRED PER SRM 53-10-07 FIG 20.SDR EIAA200900082Frame · crackedBS 2220 STR 24L TO 26L WL 200-210 FRAME CRACKED. MAIN DECK BS 2220 LT STR 24L TO 26L WL 200-210 FRAME REMOVED AND REPLACED AS PER DWG 65B04348 AND SRM 53-10-04 FIG 100.SDR EIAA200900081Floor Support · crackedBULK CARGO COMPT, BS 1960 LBL 40 FLOOR SUPPORT CRACKED. BULK CARGO COMPT, BS 1960 LBL 40 FLOOR SUPPORT REPAIRED AS PER SRM 53-10-07 FIG 20.SDR EIAA200900080Frame · crackedBULK CARGO AREA, BS 2200, STR 42R - 44R FRAME CRACKED. BULK CARGO AREA, BS 2200, STR 42R - 44R FRAME REMOVED AND REPLACED PER DWG 65B04347 AND SRM 51-30-02.
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