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 UPS06446946Stiffener · crackedINSPECTION TYPE:C NWW RT SIDE PANEL BS 300-320 WL160 STIFFENER RADIUS AREA FOUND INTERMITTENT CRACKS, CRACK LENGTH 1/4" - 1/2". NWW RT SIDE PANEL BS 300-320 WL160 STIFFENER REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06446945Stiffener · crackedINSPECTION TYPE:C NWW RT SIDE PANEL BS 280-300 WL160 STIFFENER RADIUS AREA FOUND INTERMITTENT CRACKS CRACK LENGTH 1/4" TO 3/8". RT STIFFENER REPLACED AT BS 280-300 WL160 AREA AS PSR SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06446944Fitting · crackedINSPECTION TYPE:C M/D LT NR 3 DOOR FWD LOWER CORNER REVEAL FITTING FOUND CRACKED AS MARKED CRACK LENGTH 1/2". REVEAL FTG REPLACED AND INSTALLED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR 061161Rib · crackedNR 4 PYLON INTERNAL UPPER RIB FRAME IS CRACKED AT NAC STA 221.SDR 061160Rib · crackedNR 2 PYLON INTERNAL UPPER RIB FRAME IS CRACKED AT NAC STA 221.SDR UPS06446807Angle · corrodedAFT LWR CARGO PIT DOOR OPENING AND FWD LWR CORNER HAS CORRODED ANGLE REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE IAW BOEING DRAWING 65B04642. OK TO INSTALL. INSTALLED ANGLE AND FASTENERS IAW 51-10-01.SDR UPS06446953Attach Bracket · crackedINSPECTION TYPE:C M/D BS 434 FRAME ATT BRACKET AT 26L FWD FOUND CRACK. CRACK LENGTH 3/8". M/D BS 434 FRAME ATT BRACKET AT STR 26L AREA REPLACED AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06446947Clip · crackedINSPECTION TYPE:C N/G WHEEL WELL LT SIDEWALL PANEL VERTICAL BEAM TYPICAL CLIP FOUND CRACK AS MARK AT STA340 WL180 LBL30, CRACK LENGTH 1/4". CLIP REPLACED AT BS340 WL180 LBL30 AREA AS PER SRM 51-10-01 PG 9 AND INSTALLED AS PSR SRM 51-30-02.SDR EIA2006064Module · leakingON NR 3 ENGINE START, MAINTENANCE SAW HYDRAULIC FLUID LEAKING FROM ENGINE. BLOCK TURN BACK, FOUND EDP WOULD LEAK IF PRESSURIZED. DEFERRED PER MEL 29-1. INSTALLED NEW ADAPTER RING, NUT, AND 2 PACKINGS ON EDP PRESSURE MODULE. OPS CHK GOOD PER MM 29-11-23.SDR EIA2006063Circuit Card · odorWHILE TROUBLESHOOTING NR 2 COMPASS HAD A STRONG ODOR OF ELECTRICAL BURNING COMING FROM FLIGHT DECK. FOUND MASTER DIM AND TEST CARD NR 7 AT FAULT REPLACED PER 33-11-01, OPS CHK OK.SDR EIAA2006051Pressure Panel · crackedDURING CHECK, NOSE WHEEL WELL TOP PANEL FOUND WEB CRACKED APPROX 2 INCHES. CRACK REPAIRED PER SRM 53-10-04, FIG 119.SDR EIA2006048Logic Card · malfunctionedMLG WOULD NOT EXTEND ON APPROACH INTO ORD, ALT EXTENTION REQUIRED. DMI 067 WAS GENERATED PER MEL 32-26, CAT C, DUE APRIL 19, 2006. 486EV CONTINUED TO JFK WITH MLG IN DOWN POSITION PER 32-26. REPLACED CARD FILE ASSY FOR PRIMARY GEAR SYSTEM LOGIC BUSS PER MM SDR EIA2006046Indicator · inoperativePRIOR TO TAKEOFF, AIRCRAFT RECEIVED A WARNING INDICATION FOR LT ELEV, VERIFIED OPERATION AND INDICATOR INOP. REPLACED SPI INDICATOR, OPS CHK GOOD PER MM 27-48-00.SDR 061018Floorbeam · damagedAFT LOWER CARGO COMPARTMENT FLOORBEAM AT BS 1520 UPPER CHORD DAMAGED/BENT AT RBL 24.SDR EIA2006049Bulb · inoperativeFWD LOWER CARGO SMOKE DETECTOR NR 2 TEST INOP. RELAMPED TEST BULB. OPS CHK GOOD PER MM CH 26-15-00.SDR EIA200637Control Valve · out of adjustWHEN PACKS TURNED ON AFTER T/O, COCKPIT FILLED WITH ACIDIC, SWEET FUMES. ISOLATED PACKS AND BLEED AIR VALVES, WAS UNABLE TO ISOLATE SOURCE. RETURNED TO FIELD. FOUND ENGINE EVC OUT OF TRIM. TRIMMED PER 747MM 71-00-00 TEST 8, PG 580C GROUND RAN FOR 1.5 HOURSSDR EIA200636Warning Light · false activationAFTER GEAR DOWN RED GEAR LIGHT ON WITH GREEN DOWN, GEAR LIGHT WITH AURAL WARNING, RECYCLE GEAR ALL NORMAL. INSPECTED WING, BODY, NOSE ACTUATORS AND PRIMARY DOWNLOCK SWITCHES AND CONNECTORS, NO DEFECT NOTED. INSP PRIM ACT LANDING GEAR LOGIC FILE, NO DEFECT. SDR EIA2006030Sequence Valve · malfunctionedIN CRUISE EN ROUTE FROM CHS TO PIK, FELT BUFFETING FROM NLG DOOR. DOORS WERE CYCLING OPEN AND CLOSED. PLACED HANDLE IN OFF POSITION AND DIVERTED TO JFK. REPLACED NLG SEQUENCE VALVE MECHANISM AND NLG DOOR ACTUATOR PER MM 32-34-08, 32-34-14. OPS CHK GOOD ON SDR EIA2006082Indicator · reads lowPRIOR TO TAKEOFF CAPTAINS AIRSPEED INDICATOR READING 80KT AND F/O READING 120KT, ABORTED TAKEOFF. REMOVED AND REPLACED F/O AIRSPEED INDICATOR PER MM 34-13-04, PITOT STATIC CHECK GOOD PER MM 34-11-00.SDR EIA2006026Light · inoperativeUPPER DECK RIGHT SIDE EMERGENCY LIGHT FOUND INOP. REPLACED LIGHT ASSY PER MM 33-57-00, OPS CHECK GOOD.SDR EIA2006017Circuit Breaker · malfunctionedDURING FLIGHT, CREW SMELLED SMOKE IN COCKPIT AND NOTED THE NAV TAIL LIGHT AND BEACON STROBE C/B`S HAD POPPED. UPON ARVL AT LICZ, REMOVED AND REPLACED BOTH C/B`S IAW MM33-44-01, 33-44-03 AND MM33-43-01, OP TEST GOOD PER THE ABOVE MM.SDR KCSA06006Battery Pack · inoperativeEXT SLIDE EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK MODULE IAW MM 20-51-00. OPS CHECK GOOD IAW MM 33-51-00.SDR KCSA06005Battery Pack · dischargedEMERGENCY LIGHT INOP AT THE TOP OF THE STAIRS. REMOVED & REPLACED BATTERY PACK & MODULE ASSEMBLY IAW B747 MM 20-51-00, OPS CHECK GOOD IAW B747 MM 33-51-00.SDR EIA2006015Spar · corrodedLT WING FRONT SPAR LOWER SKIN EXTENSION FOUND CORRODED AT OLES 1354. BLEND OUT CORROSION, REPAIR FITTING AND PLUG INSTALLED PER SRM 57-30-03, FIG 4.SDR EIA2006014Panel · crackedNOSE LANDING GEAR WHEEL WELL TOP PANEL FOUND CRACKED AT BS 320, RBL 20 AND BS 270, LBL 20. REPAIR DOUBLERS INSTALLED PER HAECO REPAIR SCHEME, R-53-00-35423, AND EIA ECRA 485-53-179-1.SDR EIA2006013Shear Tie · crackedFORWARD CARGO COMPARTMENT, BS 980, S-46L TO S-47L, SHEAR TIE FOUND CORROSION CRACKED. TRIMMED OUT DAMAGE, SHEAR TIE REPAIRED PER SRM 53-10-04, FIG 4.SDR EIA2006011Switch · failedDEPARTING JFK FOR DOV, DURING TAKEOFF THROUGH 400 FT, ELECTRICAL BURNING/SMOKE ODOR IN COCKPIT. STRONG ODOR FOR 2 TO 5 MINUTES. FOUND DEFECTIVE WING ILLUMINATION LIGHT SWITCH, DFRL DMI 607 PER MEL 33-10 REMAINS OPEN PENDING CORRECTIVE ACTION.SDR UPS06445989Odor · detectedSTRONG ODOR ON APP AFTER LDG WITH SMOKE CAME FROM EYE BALL OUTLETS. LOCKED OUT NR 1 PACK PER DMP 21-1-2-1-1, DUE TO DUCT BLOWN -NOTE PREVIOUSLY DEF M313988. RAN ALL ENG PER MM 71-00-00, ALL PACKS (EXPT NR 1), APU-NO SMOKE OR ODOR SMELL OR VISUAL FOUND (NOTE:PSDR EIA2006009Skin · ground damageDAMAGE FROM IMPACT BY GROUND EQUIPMENT AT BS 160-220, STR 23L-34L. DAMAGE REMOVED, COMPONENTS FABRICATED AND INSTALLED TO REPAIR PER ECRA 482-53-213-2, RVSM INSPECTION COMPLIED WITH PER EO 53=747-1453-96, REV A.SDR EIA2006008Skin · misdrilledMISDRILLED FASTENER HOLE IN EXTERNAL FUSELAGE SKIN AT STR 36L, BS 180. REMOVED DAMAGE, FABRICATED AND INSTALLED REPAIR PER ECRA 482-53-213-2.SDR UPS06445970Stiffener · crackedINSPECTION TYPE:C NWW, RT SIDEWALL PANEL BS 280-300 1ST STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06445969Stiffener · crackedINSPECTION TYPE:C NOSE W/W RT SIDEWALL PANEL BS 280-300 4TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. NOSE W/W RT SIDEWALL PANEL BS 280-300 4TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.SDR UPS06445968Stiffener · crackedINSPECTION TYPE:C NWW, RT SIDEWALL PANEL BS 300-320 4TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 1/4" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06445967Stiffener · crackedINSPECTION TYPE:C NOSE W/W RT SIDEWALL PANEL BS 300-320 5TH STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 3/16" LONG. NOSE W/W RT SIDE WALL PANEL BS 300-320 5TH STIFFENER REPLACED IAW SRM 51-10-01 PG 9.SDR UPS06445966Stiffener · crackedINSPECTION TYPE:C NWW, LT SIDEWALL PANEL BS 300-320 3RD STIFFENER (COUNT FROM TOP) FOUND CRACKS AT RADIUS APPROX 1/2" AND 1/8" LONG. STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06445965Stiffener · crackedINSPECTION TYPE:C NOSE W/W LT SIDEWALL PANEL BS 280-300 2ND STIFFENER (COUNT FROM TOP) FOUND CRACK AT RADIUS APPROX 9" LONG (CRACK LENGTH 9"). NOSE W/W LT SIDEWALL PANEL BS 280-300 2ND STIFFENER REPLACED IAW SRM 51-10-01 PG 9.SDR UPS06445964Stiffener · crackedINSPECTION TYPE:C NWW, LT SIDEWALL PANEL BS 300-320 4TH STIFFENER (COUNT FROM TOP) FOUND 9 INTERMITTENT CRACKS AT RADIUS (CRACK LENGTH 3/8" AND 1/2" 9 LOCATIONS) STIFFENER REPLACED AS PER SRM 51-10-01 PG 9.SDR UPS06445946Floorbeam · crackedINSPECTION TYPE:C U/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 6 FLOOR PNL ATTACH HOLES FOUND CRACKED BETWEEN RBL 10" - RBL 45" (CRACK LENGTH 0.060" ). U/D BS 340 RBL 3" TO RBL 50" FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE CRACK HOLES REPAIRED AS SDR UPS06445945Floorbeam · crackedU/D BS 340 FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE 1 FLOOR PANEL ATTACHED HOLE FOUND CRACKED AT LBL 48". U/D BS 340 LBL 41" TO LBL 53" FLOORBEAM UPPER CHORD HORIZONTAL AFT FLANGE CRACK HOLE REPAIRED AS PER EO NR B747-5320-12407 FIG 3 PLAN 'C'.SDR UPS06445938Floorbeam · crackedINSPECTION TYPE:C U/D BS 380 FLOORBEAM UPPER CHORD FWD HORIZONATAL FLANGE 1EA FLOOR PANEL ATT HOLE FOUND CRACKED, CRACK LENGTH 0.060". U/D BS 380 RBL 61" TO RBL 71" FLOORBEAM UPPER CHORD FWD HORIZONATAL FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 3 PLAN SDR UPS06445935Floorbeam · damagedINSPECTION TYPE:C COCKPIT BS 340 LBL 49" LBL 55" AND LBL 61" FLOORBEAM UPPER CHORD AFT FLANGE ANCHOR NUT SHORT EDGE MARGIN. COCKPIT BS 340 LBL 41" TO LBL 64" FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.SDR UPS06445933Floorbeam · damagedINSPECTION TYPE:C COCKPIT BS 340 RBL 61" FLOORBEAM UPPER CHORD AFT FLANGE ANCHOR NUT HOLE FOUND SHORT EDGE MARGIN. COCKPIT BS 340 RBL 56 TO RBL 64 FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.SDR UPS06445932Floorbeam · damagedINSPECTION TYPE:C COCKPIT BS 380 LBL 66" LBL 72" FLOORBEAM UPPER CHORD AFT FLANGE FOUND SHORT EDGE MARGIN, ANCHOR NUT HOLES. COCKPIT BS 380 LBL 61" - LBL 75" FLOORBEAM UPPER CHORD AFT FLANGE REPAIRED AS PER EO NR B747-5320-12407 FIG 2 PLAN B.SDR UPS06445944Floor Support · crackedINSPECTION TYPE:C COCKPIT BS 340-360 BL 0 FLOOR SUPPORT 'L' ANGLE FOUND CRACK, CRACK LENGTH 4". COCKPIT BS 340-360 BL 0 FLOOR SUPPORT 'L' ANGLE REPLACED AS PER SRM 51-10-01 PAGE 9.SDR UPS06445937Floorbeam · corrodedINSPECTION TYPE:C U/D BS 400 RBL 40" - RBL 68" FLOORBEAM UPPER CHORD ANCHOR NUTS AREA FOUND CORROSION. CORROSION BLEND OUT 0.055" BY 2" BY 2" EXCEED SRM 53-10-01 FIG 1 LIMITS, U/D BS 400 RBL 33 TO MOST RT O/B FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FISDR UPS06445936Floorbeam · corrodedINSPECTION TYPE:C COCKPIT BS 360 LBL 12" - LBL 34" FLOORBEAM UPPER CHORD FOUND CORROSION. CORROSION BLEND OUT 0.065" BY 2" BY 3" EXCEED SRM 53-10-01 FIG 1 LIMITS, COCKPIT BS 360 LBL 4" TO LBL 42" FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG 23.SDR UPS06445934Floorbeam · scoredINSPECTION TYPE:C COCKPIT BS 360 RBL 50" - RBL 54" FLOORBEAM UPPER CHORD SEVERAL SCORE MARK. COCKPIT BS 360 RBL 42" TO RBL 62" FLOORBEAM UPPER CHORD REPAIRED IAW SRM 53-10-07 FIG 23.SDR UPS06445985Fitting · crackedINSPECTION TYPE:C RT WING, NR 8 SPOILER SUPPORT 'H' FTG I/B LOWER FLANGE CRACK 1" LONG. RHW NR 8 SPOILER SUPPORT 'H' FTG REPLACED AS PER SRM 51-10-01 PG 9 AND 51-30-02.SDR UPS06445988Frame · crackedINSPECTION TYPE:C NR 4 PYLON I/B SIDE OF NAC STA 236 VERTICAL FRAME CRACKED, JUST FWD OF PYLON VALVE, CRACK LENGTH : 2.5". VERTICAL FRAME REPLACED AS PER SRM 51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.SDR UPS06445987Frame · crackedINSPECTION TYPE:C NR 1 PYLON NAC STA236 I/B VERTICAL FRAME BOTTOM CRACKED, CRACK LENGTH 2.75". VERTICAL FRAME REPLACED AS PER SRM51-10-01 P.9 AND INSTALLED AS PER SRM 51-30-02.
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