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 EIA2008035Angle · crackedNR 1 PYLON AT A7 NAL STATION 22/LOWER SURFACE OF MID SPAR WEB LT 1 EA ANGLE CRACKED. FAB NEW ANGLE PER DRW 65B90387. HEAT TREAT AND NDT. INSTALLED PER SRM 51-30-02.SDR EIA2008033Structure · crackedRT WING L/E DEVICE FAIRING AFT WEB ADJACENT UPPER CHORD AND LOWER CHORD CRACK AT 1 LES 1127. REPLACED PER SRM 57-20-03.SDR EIA2008034Light · inoperativeDURING EMG LT OPS TEST, FOUND V/D AFT CEILING EMERG. LT. INOP. REPLACED PER MM 33-51-00.SDR EIA2008036Skin · crackedFUSELAGE BS 740 TOP AFT OF VHF BL 0 SURFACE SKIN CRACKED. REPAIRED PER SRM 53-30-03 FIG 48.SDR EIA2008037Floor Support · crackedMAIN DECK STATION 940 RBL 120 FLOOR PANEL SUPPORT CRACK. FABRICATED AND REPLACED IAW SRM 51-30-02.SDR EIA2008038Stringer · crackedSTATION 750 TO 760 STRINGER R-23 CRACKED. SPLICED AND REPAIRED PER 51-30-02.SDR EIA2008039Skin · crackedFUSELAGE BOTTOM SKIN AT BS 2061 5-45R CRACKED APPROX 2 INCHES. REPAIRED PER SRM 53-30-03 FIG 1.SDR EIA2008040Sign · defectiveEXIT SIGN OVER CREW STAIR FOUND BELOW 100 M/L. REPLACED PER AMM 20-51-01.SDR EIA2008041Skin · damagedFUSELAGE AT BS 460-480 TOP BL O TO 5-IL, ANTENNA LOCATION SURFACE SKIN SUNK. REPAIRED PER SRM 51-30-02.SDR EIA2008042Engine · malfunctionedIN FLIGHT SHUT DOWN NR 2 ENGINE. C CRUISE RAIN, FL 4.0 WITH MODERATE TURB. NO THROTTLE MOVEMENT AND NOTED COMPRESSOR STALL.SDR KCS2008F00004Battery · fumesSMOKE AND FUMES IN COCKPIT. FOUND SHIP’S MAIN BATTERY EMITTING FUMES. REMOVE AND REPLACE MAIN BATTERY AND CHARGER WITH APU BATTERY AND CHARGER PER GMM 3-5-8. APU BATTERY P/N 40176-7, S/N 076021 INSTALLED IN MAIN POSITION PER AMM 24-31-01. APU BATTERY CHARGSDR KCSA081332Light · inoperativeUPPER DECK EMERGENCY LIGHT FWD OF LAV INOP. (A)SDR KCSA081305Light · inoperativeEMERGENCY LIGHTS ARE OUT AT FORWARD AND AFT OF L1 DOOR (B)SDR KCSA081291Skin · corrodedCORROSION ON RT. WING LOWER SKIN AT BOOST PUMP CUTOUT WS 538 (B)SDR KCSA081281Frame · crackedNR 2 PYLON REAR ENG. MOUNT BULKHEAD FWD. O/B FRAME IS CRACKED AT NAC STA 221.9 (B)SDR KCSA081271Frame · crackedNR 1 PYLON REAR ENG MOUNT BULKHEAD AFT I/B FRAME EDGE CRACKED AT NAC STA 221.9.SDR KCSA081270Skin · crackedNR 4 PYLON I/B SKIN CRACKED AT FWD LOWER ACCESS PANEL CUTOUT.SDR KCSA081267Stringer · crackedSTA-495 STR-39L STRINGER CRACKED .5 INCH.SDR KCSA081265Skin · damagedSTA-1700 BETWEEN STR-43L AND STR-44L SKIN DAMAGED .5 INCH.SDR KCSA081264Cargo Track · crackedFWD PIT CARGO PALLET RESTRAINT BRACKET CRACKED AT FWD LOWER CORNER OF THE FWD PIT DOOR BS 560, RBL-67.SDR KCSA081258Seat Track · crackedFIRST OFFICERS FWD O/B SEAT TRACK CRACKED AT FWD STOP BS 320, RBL-36.SDR KCSA081257Stiffener · damagedFUSELAGE FRAME STIFFENERS (2EA) AND STRINGER CLIP DAMAGED AT BS 2280, STR-12R.SDR KCSA081253Frame · damagedFUSELAGE FRAME DAMAGED AT BS 1120, STR 13L.SDR KCSA081249Shear Tie · crackedFUSELAGE FRAME SHEAR TIE CRACKED AT BS 2100 BETWEEN STR-24L AND 25L.SDR KCSA081248Web · damagedL-4 MAIN ENTRY DOOR LOWER WEB ACCESS AREA DAMAGED AT BS 1700, STR 24L.SDR KCSA081247Strap · crackedFUSELAGE FRAME STABILIZATION STRAP CRACKED AT B.S.2230 ABOVE STR-42LSDR KCSA081246Stringer Clip · corrodedSTRINGER CLIP CORRODED AT BS 1680, STR-2R.SDR EIA2008021Boot · tornDURING CLIMB-OUT, APU FIRE WARNING LIGHT AND BELL CAME ON. FIRE SWITCH PULLED AND BOTTLE DISCHARGED. FIRE WARNING INDICATIONS CONTINUED AFTER APU SHUTDOWN AND EMERGENCY ACTION ITEMS COMPLETED. REPLACED SURGE BLEED VALVE BOOT PER B747 MM 49-53-01. OPS CHECKSDR EIA2008020Module · no testUPPER DECK CEILING EMERGENCY LIGHT DOES NOT TEST. REPLACED U/D AFT CEILING EMERGENCY LIGHT MODULE PER B747 MM 33-51-00. SYSTEM OPS CHECKED NORMAL PER B747 MM 33-51-00 PAGE 501.SDR KCSA081241Stiffener · damagedFUSELAGE FRAME STIFFENER IS DAMAGED AT STA 880, STR 39R.SDR KCSA081240Stiffener · damagedFORWARD BILGE SEAT TRACK STIFFENER IS DAMAGED AT STA 585, LBL 25.SDR KCSA081239Strap · crackedAFT BILGE FUSELAGE FRAME STABILIZER STRAP IS CRACKED AT STA 2050, RBL 66.SDR UPS08452200Wing · damagedLT WING DAMAGE ON CONTACT WITH POLE ON TAXI IN.SDR KCSA081234Door Frame · crackedR5 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS, BS 2241, WL-207.SDR KCSA081233Door Frame · crackedL1 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS ADJACENT TO DOOR STOP FITTING, BS 441, WL-209.SDR KCSA081232Door Frame · crackedL5 MAIN ENTRY DOOR FWD LOWER CORNER VERTICAL FRAME CRACKED IN RADIUS ADJACENT TO DOOR STOP, BS 2241, WL-207.SDR UPS08452165Light · inoperativeAFT L1 DOOR EMERGENCY LIGHT INOP. RELAMPED, OPS CHECK GOOD PER B747 MM 33-51-05.SDR EIA2008017Light · inoperativeEMERGENCY LIGHT AT AFT UPPER DECK DOOR INOP. AFT U/D EMERGENCY EXIT LIGHT ASSEMBLY REPLACED AS PER B747MM 33-51-00 PAGE 10. OPS CHECKED NORMAL.SDR UPS08452007Coalescer Bag · odorCLIMBING THROUGH FL 220 A VIBRATION WAS FELT ACCOMPANIED BY A BURNING ODOR. SECURED NR 3 PACK AND VIBRATION AND ODOR WENT AWAY. ON NR 3 PACK REPLACED COALESCER BAG AND RETAINING RING MM 21-51-05 LP 935157/1. REPLACED COMP DISCH TEMP BULB MM 21-51-02 LP 93515SDR EIA2008014Light · looseDURING DESCENT, ABOUT 30 MILES OUT, 2 VISIBLE PUFFS OF SMOKE WITH ASSOCIATED ELECTRICAL ODOR UNDER F/OS GLARESHIELD. HAPPENED 2 TIMES WITHIN A 3 MINUTE PERIOD. AIRCRAFT OPERATED 15 ADDITIONAL MINUTES UNTIL LANDING WITHOUT FURTHER OCCURRENCE. ALL SYSTEMS OPESDR EIA2008013Battery Pack · dischargedUPPER DECK EXIT DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED UPPER EXIT DOOR EMERGENCY LIGHT BATTERY PACK IAW B747 MM 33-51-00, OPS CHECK NORMAL.SDR EIA2008012Skin · crackedBS 340 LEFT BELOW STRINGER 5 CRACK FROM FASTENER HOLE. STOP DRILLED CRACK INSTALLED PREFABBED DOUBLERS PER ECRA 485-53-188-2.SDR UPS08452145Intercostal · crackedINSPECTION TYPE:C CABIN LT NR 1 DOOR BEAM INSTL FOUND CRACKED AS MARKED. NEW BEAM INTERCOSTAL FABRICATED USING MATL 7075-0.050" PER DWGABA7096. INTERCOSTAL HEAT TREATED TO T62 PER DPS7.00-1 HARDNESS HRB 78.4 IS ACCEPTABLE PER DPS1.05-3. HOLES PICKED UP ON NSDR UPS08451597Door · out of rigL1 ENTRY DOOR OUT OF RIG. FOUND LOWER HINGE BOLTS LOOSE, REPLACED BOLTS. GROUND OPS CHECKS GOOD PER MM 52-11-02. OK FOR SERVICE.SDR UPS08451576Fan Blade · damagedAFTER LANDING IN MEM, MX REPORTED DAMAGE TO MULTIPLE FAN BLADES AND INSIDE OF COWLING ON NR 2 ENGINE. THERE WERE NO IN FLIGHT INDICATIONS. REMOVED AND REPLACED 6 PAIRS OF FAN BLADES IAW MM 72-31-02. REMOVED AND REPLACED NR 2 ENG NOSE COWL IAW T C 5027. REPSDR EIA2008010Bulb · no testR5 DOOR EMERGENCY EXIT AFT SILL LIGHT INOP. RELAMPED R5 EMERGENCY EXIT AFT SILL LIGHT PER 33-51-00. OPS CHECKED NORMAL.SDR EIA2008016Guide Vane · separatedON WALK AROUND, FOUND NR 2 ENG FAN EXIT GUIDE VANE EXITED ENGINE AND DAMAGED LT INBOARD MID TRAILING EDGE FLAP. REMOVED DAMAGED GUIDE VANE AND PLACED ENGINE ON COI NR 114, AND REPLACED MID FLAP, OPS CHECKED GOOD.SDR EIA2008008Battery Pack · dischargedRIGHT UPPER DECK SERVICE DOOR SEAL EMERGENCY LIGHT INOP. REMOVED AND REPLACED SERVICE DOOR EMERGENCY LIGHT BATTERY PACK, OPS CHECKED NORMAL PER B747 MM 33-51-00.SDR WRNA200800002Frame · crackedDURING B-CHECK INSPECTION, RIGHT FRAME AT STATION 2674.85 WAS FOUND CRACKED AT WL 325. REMOVED DAMAGE SECTION OF FRAME, FABRICATED AND INSTALLED REPAIR DOUBLERS IAW 747 SRM 51-40-03 FIG 2.SDR WRNA200800001Bulkhead · chafedDURING B-CHECK WHILE ACCOMPLISHING AD 2007-19-19, NR 1 PYLON STRUT FORWARD ENGINE MOUNT BULKHEAD CORD WAS FOUND WITH CHAFED RADIUS AT LOWER INBOARD END. FABRICATED AND INSTALLED REPAIR ANGLE IAW BOEING SKETCH SR1-733824930-1. THIS REPAIR IS TEMPORARY AND REQ
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