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 EIA2003129Floorbeam · crackedBS. 340 RT UPPERDECK FLOORBEAM UPPER CHORD TO FRAME INTERFACE CRACKED AT 2ND IB HOLE. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-160-1.SDR EIA2003133Skin · wornFUSEALAGE SKIN WORN AT INTERFACE OF VERT STAB SEAL LT SIDE BS 2280-2416. REMOVED DAMAGED, NDT AREA, FABBED AND INSTALLED REPAIR IAW ECRA 482-53-181-2SDR EIA2003131Web · crackedNR 1 PYLON LOWER WEB CRACKED AT NAC STA 210 LT SIDE AFT OF STIFFER FOR PNEU. DUCT. STOP DRILLED CRACK AND FABBED AND INSTALLED REPAIR PLATE AND FILLERS IAW B747 SRM 54-10-03 FIG 2SDR EIA2003128Skin · corrodedLT OUTFLOW VALVE STA. 2240 HAS 2 SKIN BULGES AT OPPOSITE CORNERS UPPER AFT AND LWR FWD. REMOVED AND REPLACED DAMAGED SKIN IAW B747 SRM 51-30-02 AND ECRA 482-53-169-2.SDR EIA2003144Lap Joint · damagedUPON REMOVAL OF A/C DUCTS, CHAFFING WAS FOUND ON UPPER AND LOWER SKINS AND ON NUMEROUS FASTENERS AT STA. 980 STRINGER 39 LAP JOINT. REPAIRED DAMAGE ON UPPER AND LOWER SKINS AND FASTENERS AT STA. 980 STRINGER 39L, LAP JOINT IAW B747 SRM 53-30-03 FIG 13 AND B74SDR EIA2003142Floorbeam · crackedUPPER DECK FLOORBEAM WEB AT BS 440 RBL CRACKED, RBL 66 CORROSION, RBL 40 CRACKED, RBL 55 CRACKED. UPPER DECK FLOORBEAM WEB BS 440, RBL 8 TO RBL 72 REPLACED IAW ECRA 482-53-191-2SDR UPS03441455Skin · crackedCRACK JUST AFT OF NLG CUTOUT. CRACK VERIFIED BY EDDY CURRENT READING. REMOVED CRACKED AREA OF SKIN VERIFIED CRACK REMOVED W/T EDDY CURRENT. REPAIRED IAW SRM 53-30-3SDR UPS03441483Attach Fitting · crackedINSPECTION TYPE: C, NR 2 PYLON DIAGONAL BRACE STEEL ATTACH FITTING HORIZONTAL FLANGE ATTACH BOLTS 6EA TORQUE CHECK FOUND LOOSE AS MARKED. THE BOLT HOLE ID MEASURED, NR 5, 7, 9 ARE 0.314 INCH NR 8, 10 ARE 0.313 INCH & NR 15 IS 0.316 INCH NDT HFEC INSP CONFIRMSDR UPS03441523Fastener · crackedINSPECTION TYPE:C RIGHT BS 1480 BULKHEAD ONE EACH FASTENER NR 5 WAS CRACKED AT SPLICE FITTING AREA RUNNING AFT APPROX 0.065 INCH LONG. RIGHT BS 1480 BULKHEAD SPLICE FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & HFEC CONFIRMED NO CRACK. REPAIR BUSHING FABRICATED & SDR UPS03441522Fastener · crackedINSPECTION TYPE: C, RT BS 1480 BULKHEAD - ONE EACH FASTENER NR 5 WAS CRACKED AT EXTENSION FITTING AREA RUNNING AFT APPROX 0.040 INCH LONG. REF RS R53-43-35093 & EO B747-5310-19423A RT BS 1480 BULKHEAD SPLICE EXTENSION FTG NR 5 HOLE OVERSIZED TO 0.625 INCH & SDR UPS03441511Bulkhead · corrodedINSPECTION TYPE: C, LT MLG WW BS 1241 BULKHEAD CORRODED AT WL 143 BETWEEN LBL 1 & 3 AREA AS MARKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.059 X 1 X 1 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO RS R57-12-35092 & UPS AUTH 7SDR UPS03441485Skin · crackedINSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-46-17 BS 1775-1790 AT STR 34R-36R 2EA HOLES SHORT EDGE MARGIN FOUND. BS 1775-1790 S34R-S36R PREVIOUSLY FX SKIN EXTERIOR DOUBLER REMOVED AS PER SRM 51-30-02 AND SKIN CUTOUT ENLARGED AS PER SRM 53-30-03 FIGSDR UPS03441482Skin · crackedINSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-42-03 AT BS 600-620 STR 39R-40R FWD CARGO DOOR LOWER EDGE AREA REPAIR FASTENER ROWS LESS THAN 2 ROWS. REPAIR REQ'D AT BS 600-620 S39R-40R FWD CARGO DOOR LOWER EDGE EXTERIOR PREVIOUSLY DOUBLER REMOVED AS PSDR UPS03441481Skin · crackedINSPECTION TYPE: C, DURING RAP INSPECTION ITEM N525UP-41-02 BS 375-390 STR 26L-27L REPAIR DOUBLER WITH TWO REPAIR FASTENER ROWS ONLY REPAIR REQ'D. BS 375-390 S26L-S27L FX SKIN EXTERIOR PREVIOUSLY DOUBLER REMOVED AS PER SRM 51-30-02 AND SKIN CUTOUT ENLARGED ASDR UPS03441512Bulkhead · corrodedINSPECTION TYPE: C, RT MLG WW BS 1241 BULKHEAD CORRODED AT WL 143 BETWEEN RBL 1 & 3 AREA AS MARKED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT 0.116 X 1 X 1 INCH EXCEED SRM 57-10-01 FIG 1 LIMITS, FOR REPAIR REFER TO HX RS R57-12-35092 & UPS AUTHSDR UPS03441513Bulkhead · crackedINSPECTION TYPE: C, NR 3 PYLON REAR MOUNT BULKHEAD FOUND CRACK AT FWD AND AFT WEB (NAC 221 TO 221). NR 3 PYLON REAR ENG MOUNT BULKHEAD LWR ASSY FRAME WEB INTERIM REPAIR ACCOMPLISHED AS PER RS R54-53-35090 & UPS AUTH 747-54-20043.SDR UPS03441484Fitting · corrodedINSPECTION TYPE: C, CORROSION REVEALED AT LT WING LANDING GEAR SUPPORT BEAM O/B END AFT FITTING FIVE INDICATIONS AT 2, 6, 7, 9, 11 O'CLOCK RESPECTIVELY WERE FOUND EXCEEDED THE 50 PERCENT ACCEPTANCE LIMIT PER NTM PT4. 57-40-03. REMOVAL OF THE FITTING FOR FURTSDR UPS03441521Skin · corrodedINSPECTION TYPE: C, CENTER E&E COMPT DOOR RT SIDE CUTOUT FOUND CORROSION AT BS 800-820 S46R-S47R. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT THROUGH THK, WIDTH 1.5 INCH, LENGTH 4.75 INCH EXCEED SRM 53-30-01 FIG 1 LIMITS FOR REPAIR REF RS R53-21SDR UPS03441381Skin · corrodedDENT AT NOSE ACFT JACK PAD MOUNT PROTRUDING OUTWARD POSSIBLE CORROSION FMS STA 405 STRINGER 38RT. USED LFEC INSP OF AREA. INDICATION OF APPX 20 PERCENT MATERIAL LOSS. QC 10445/ (2) DEMENTIONS OF DENT IS .045 IN DEPTH. 75705/ THE DAMAGE ALLOWED REF EO. B747-5SDR EIA2003123Frame · corrodedLT WING GEAR WHEEL WELL STATION 1241, LBL 88 (APPROX), BELOW LOWER CANTED FRAME HAS EXFOLIATED CORROSION ON TANK SKIN. REPAIR IAW ECRA NR 482-57-170-2.SDR EIA2003121Spar · corrodedCORROSION ON REAR SPAR WEB TO THE INBOARD SIDE AND UNDER THE LT BULKHEAD FITTING AT BS 1241 UPPER PORTION APPROXIMATELY FASTENER NR 32 AREA DOWN. REMOVED CORROSION ON REAR SPAR WEB UNDER THE LT BULKHEAD FITTING AT BS 1241, IAW EO NR 57-747-1544-99 REV ASDR EIA2003122Web · corrodedAFT CARGO COMPT, BS 1480 TO BS 1490 BETWEEN LBL 0 TO LBL 45.5, UPPER SURFACE OF THE WEB IS CORRODED. FABRICATED THE FOLLOWING REPAIR PARTS, (1) EA, WEB P/N 482-53-2-2, (1) EA DOUBLER P/N 482-53-188-2-3, (1) EA DOUBLER P/N 482-53-188-2-4, AND INSTALLED IAW ECRASDR EIA2003118Stringer · corrodedAFT CARGO COMPT. BS 1790 TO 1800 STR. 51R STRINGER HAS LIGHT SURFACE CORROSION. REMOVED CORROSION FOUND OUT OF LIMITS IAW B747 SRM 53--10-01 PG2-3. REMOVED AND REPLACED DAMAGED STRINGER FROM STA. 1740-1810 AND REPAIRED IAW B747 SRM 53-10-03 FIG 8 PGS. 33-40, SDR EIA2003119Bulkhead · corrodedLT WING MLG WELL CORROSION ON BS 1241 BULKHEAD AT CANTED BULKHEAD TO 1241 BULKHEAD HORIZONTAL SPLICE LBL 96, APPROX W.L. 171. REPAIRED IAW ECRA 482-57-170-2.SDR EIA2003112Shear Tie · corrodedSHEAR TIE L-ANGLE AT BS 2220 HAS HEAVY CORROSION ON BOTTOM LOWER FLANGE STR. 37L TO 41L. REMOVED DAMAGED, FABRICATED AND INSTALLED REPAIR IAW B747 SRM 51-40-03 FIG 1, 51-10-01, 51-10-02, 51-30-02 AND BSOPM 20-41-2.SDR UIEA200300053Relief Valve · failedLIM-MIA - DURING CLIMB AT FL250, NR 4 NACELLE TEMP WENT OT 8.0 WITH A FIRE BELL AND LIGHT IN NR 4 FIRE SWITCH. WHEN NR 4 THRUST LEVER WAS RETARDED TO IDLE, THE FIRE LIGHT WENT OUT AND THE NACELLE TEMP RETURNED TO NORMAL 2.0. CLOSED NR 4 BLEED VALVE AND ADVANSDR 0301636642Battery Pack · inoperativeDURING LINE CHECK, FOUND 'B' ZONE LEFT FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK GOOD.SDR UIEA200300045Relief Valve · defectiveMIP/POS-AIR TURNBACK, AFTER T/O AND DURING CLIMB, NR 4 ENGINE FIRE WARNING CAME ON. WHEN NR 4 THROTTLE WAS CLOSED THE TEMP WENT BACK TO NORMAL. THROTTLE WAS ADVANCED AGAIN THE TEMP STARTED TO GO UP. NOTICED HIGH STAGE BLEED VALVE LIGHT, ON AND OFF. CLOSED NR 4SDR UPS03441074Battery · dischargedINSPECTION TYPE:A CK CREW SERVICE DOOR EMERGENCY LIGHTS INOP. FOUND BATTERY DEAD. REPLACED BATTERY PACK ASSY.SDR EIA2003108Engine · vibrationAT 200 MILES FROM ZURICH FL 400 AT 1/2 THROTTLE NOTICED SHUDDER AND STALL. FUEL OFF THEN ON EGT DROP BUT NO RELIGHT SHUTDOWN CHECKLIST C/W. RAN INFLIGHT ENG START CHECK LIST RELIGHT BUT ENG SHAKING INCREASED TOWARD IDLE. SHUT ENG DOWN AND INFLIGHT SECURING SDR EIA2003115Light · malfunctionedDURING GROUND TEST FOLLOWING FLIGHT EVALUATION. EMERGENCY CEILING LIGHT AFT UPPER DECK ILLUMINATES FOR ABOUT 3 SECONDS BEFORE GOING OUT: REMOVED AND REPLACED LIGHT UNIT IAW MM 747-33-51-00SDR EIA2003106Light · inoperativeDURING GROUND TEST FOLLOWING FLIGHT EVALUATION EMERGENCY CEILING LIGHT AFT UPPER DECK ILLUMINATES FOR ABOUT 3 SECONDS BEFORE GOING OUT. (DMI 763)SDR EIA2003105Frame · crackedBS 1000 BULKHEAD FRAME CRACKED AT S-38L. CRACK VERIFIED WITH HFEC S/N J032592, CAL DUE 4-21-04. CRACK LENGTH APPROXIMATELY .75 INCH. REPAIRED PER ECRA 485-53-157-2.SDR EIA2003104Skin · tornNR 4 PYLON I/B SKIN TORN OUT AFT OF AFT ENGINE MOUNT. DAMAGED AREA REPAIRED PER ECRA 485-54-138-2, REV A.SDR EIA2003103Skin · bulgedBODY STATION 780 IN AREA OF STRINGER 46R, SKIN BULGE. REPAIR WORK ACCOMPLISHED ON ECRA 485-53-143-2 & ECRA 485-53-160-2.SDR EIA2003102Frame · crackedFRAME CRACKED, INTERIOR FUSELAGE STA 300L, BELOW S-25L, OUTBOARD NEAR SKIN. REMOVED AND REPLACED FUSELAGE FRAME AT FS 300L, STR 23-41, PER SB 747-53-2272, PER -B-DRAWINGS 141U1021 AND 65B1708 & ECRA 485-53-152-2.SDR EIA2003101Fitting · crackedFWD CARGO PIT AFT PRESSURE BULKHEAD STA 1000, BATH-TUB FITTING BETWEEN STA 38-39L CRACKED. REMOVED AND REPLACED TWO EACH FITTINGS BETWEEN STA 38-39L, STA 1000, P/N 65B16518-1 AND 65B16517Y3 PER B747 SRM 51-32-02, PGS 8 & 9, 51-10-01, PGS 6 & 7, 53-10-03, PG 1SDR EIA2003100Structure · corrodedRT WING GEAR WELL, STA 1307, RBL 115, CORROSION ON AFT SIDE OF WEB STIFFENER. REMOVED AND REPLACED STIFFENER AS PER B747 SRM 51-30-02, PGS 5-9, 38, 57, 58B.SDR EIA2003099Skin · corrodedUPON REMOVAL OF FASTENERS FOR ADJACENT S/M REPAIR, CENTER TANK UPPER AFT SKIN PANEL WAS FOUND CORRODED AT STA 1237, RBL 37 UNDERNEATH LONGITUDINAL FLOORBEAM LOWER CHORD. DAMAGED AREA REPAIRED PER ECRA 485-57-154-2.SDR EIA2003098Doubler · chafedLT LOWER FUSELAGE EXTERNAL CHAFING MARKS ON REPAIR DOUBLER AT STA 980 STR 44L. REMOVED AND REPLACED DOUBLER PER B747 SRM 553-30-03.SDR EIA2003097Skin · damagedFUSELAGE SKIN CRACKED AT BATHTUB FITTING FWD FASTENER HOLE STA 1000 AT STR 38L. REMOVED DAMAGE, NDT AREA AND FABRICATED AND INSTALLED REPAIR PER SRM 53-30-03 FIG 60.SDR EIA2003096Doubler · crackedCRACK ON DOUBLER OF 1241 WEB APPROX LBL 80 ABOVE LOWER CHORD. REMOVED AND REPLACED DOUBLER PER B747 SRM 57-30-2 AND ECRA 485-53-151-2.SDR EIA2003095Floorbeam · damagedUPPER DECK FLOORBEAM HAS MISSING FASTENERS AND WEB IS TORN AND GOUGED AT BS 440 RBL 32. FABRICATED REPAIR PER ECRA 485-53-145-2.SDR EIA2003094Structure · crackedBULK PIT DOOR INTERIOR CRACKED AT 2ND FROM BOTTOM STOP ON LOWER FWD SIDE IN LOWER RADIUS. REMOVED AND REPLACED FRAME SECTION PER B747 SRM 51-30-02.SDR 0301346641Coffeemaker · burnedDURING FLIGHT, A BURNING ODOR EMITTED IN THE AREA OF DOOR 4R. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE CENTER GALLEY FORWARD COFFEEMAKER. OPERATIONAL CHECK GOOD.SDR EIA2003093Engine · stalledAT CRUISE ALTITUDE FL 320 NOTICED NR 1 ENG EPR DROP TO .25 LOWER THAN THE OTHERS. ALL OTHER READINGS AND INDICATIONS WERE NORMAL. WHEN ADJUSTING THRUST LEVER, ENGINE COMPRESSOR STALLED MULTIPLE TIMES, SHUT DOWN ENGINE. AFTER SHUTDOWN OIL PRESS 29 PSI, N1 29SDR UPS03440947Engine · failedNR 3 ENGINE SHUTDOWN 56 MIN. AFTER TAKEOFF, ICE LIGHT CAME ON,FUEL HEAT APPLIED AND ICING LIGHT STAYED ON.OIL TEMP INCREASED TO 140 DEGREES AFTER 5 MINUTES EPR,N1 AND N2 ROLLED BACK AND ENG. DID NOT RESPOND. ENGINE SHUTDOWN . FOUND METAL IN TAILPIPE AND FSDR EIA2003092Light · inoperativeEMERGENCY LIGHT ASSY IN UPPER DECK DOME LIGHT INOP. DMI OPEN.SDR UIEA200300027Warning Light · false indicationTURN BACK, AFTER TAKEOFF THE LOWER CARGO FIRE PROTECTION AFT LIGHT CAME ON AND WENT OUT 2-4 SECONDS AFTER SILENCING THE BELL. ACCOMPLISHED CHECKLIST AND DUMPED FUEL. RETURNED TO GYE AIRPORT. FUEL DUMPED 43,000 KGS. LOWER CARGO FIRE PROTECTION CHECKED PER MSDR EIA2003091Check Valve · bentJETTISON PUMP CHECK VALVE FOUND BENT. INSTALLED NEW VALVE. PART NUMBER 60-703137.
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