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 EIA2003076Engine · bird ingestionPOST FLIGHT WALKAROUND FOUND BIRD STRIKE NR 1 ENGINE. FOUND 2 EACH N1 FAN BLADES DAMAGED ENGINE INSPECTED IAW MM 72-00-00. REMOVED AND REPLACED NR 1 AND NR 2 BLADES IAW WC F7208 RII ACCOMPLISHED.SDR EIA2003075Engine · malfunctionedNR 4 ENGINE SHUTDOWN DUE TO LOW OIL PRESSURE, AFTER SHUTDOWN ENGINE WINDMILLED FOR 20 MINUTES. REMOVED AND REPLACED NR 4 ENGINE PER WORKCARD F7201, F7202, F7203 AND F7207, OPS CHECK GOOD.SDR EIA2003058Skin · corrodedFRETTING CORROSION AT FWD EDGE OF NR 1 PYLON O/B SAILPLANE DOOR CUTOUT. TRIMMED DAMAGE, NDT AREA, FABRICATED AND INSTALLED REPAIR PER ECRA 486-54-017-2.SDR UIEA200300017Warning Light · illuminatedINFLIGHT ENGINE SHUTDOWN, DURING CRUISE, NR 4 ENGINE SHUTDOWN IN FIGHT DUE TO 'OIL FILTER BYPASS LIGHT. OIL TEMPEARTURE AND PRESSURE NORMAL AT 49 PSI/120 DEGREES AND N2 AT 94 PERCENT. WITH THRUST AT IDEL (75 PERCENT N2) PRESSURE WAS 30 PSI AND TEMPERATURE ROSDR UPS03440414Bulb · burned outINSPECTION TYPE: A 3, EMERGENCY LIGHTS ON UPPER DECK HAS 1 BULB INOP. RELAMPED 3 LIGHTS AS REQUIRED, OPS CHECKED NORMAL.SDR UPS03440288Engine · failedDURING T/O AND CLIMB, TOWER NOTICED AND NOTIFIED FLT 6703 THAT SMOKE WAS TRAILING FROM NR 4 ENGINE. AT 6500 FEET CREW REPORTED A BANG AND ASSOCIATED ROLL BACK OF N1/N2. CREW FOLLOWED SEVERE ENGINE DAMAGE CKLIST. FUEL DUMPED AND AIRCRAFT 526 ON FLT 6703 RETUSDR EIA2003049Line · leakingNR 2 ENG OIL QTY BEGAN DECREASING FROM 5.0 GAL, OIL PRESS/TEMP NORMAL. LATER NR 2 OIL PRESSURE DROPPED BELOW YELLOW BAND AND OIL PRESSURE LIGHT ILLUMINATED. NR 2 ENGINE WAS SHUTDOWN, WINDMILLING OIL PRESSURE MAINTAINED 20 PSI. INSPECTED AND REPLACED MAIN OIL SDR EIA2003046Connector · damagedDURING TAKE-OFF ROLL, BEFORE TAKE-OFF POWER WAS SET NR 1 ENGINE N1 MAX OUT THEN FAIL, 75,000LBS OF FUEL WAS JETTISON TO GET TO LANDING WEIGHT. REMOVED AND REPLACED N1 TACH CANNON PLUG IAW MM 77-12-00SDR EIA2003045Valve · failedNR 3 ENGINE ANTI-ICE VALVE INOPERATIVE. REPLACED NR 3 ENGINE ANTI-ICE VALVE, OPS AND LOCK CHECK, OK. IAW 30-21-03 AND 30-21-00.SDR 0300486642Skin · corrodedDuring "L" check found corrosion under seal plane area on upper forward corner of #3 LH passenger door. Repaired per EA 66-193805.SDR 0300476642Skin · corrodedDuring "L" check found corrosion on #3 door forward upper door surround skin. Repaired per EA 66-193805.SDR 0300356642Skin · crackedDuring "L" check found crack in fuselage skin at aft cargo door cutout upper forward corner BS 1830 STR 26R Repaired per EA 66-193973.SDR 0300226641Wire · misroutedDURING FLIGHT SMOKE EMITTED FROM THE LEFT AFT GALLEY COFFEE MAKER. PULLED CIRCUIT BREAKER AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REROUTED CROSSED WIRES ON COFFEE MAKER TERMINAL STRIP AND REPLACED COFFEE MAKER. OPERATIONAL CHECK GOOSDR UPS03440132Light · inoperativeEMERGENCY LIGHT MAIN DECK CEILING AFT OF STAIRS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ON MAIN DECK, OPS OK.SDR UPS02439966Light · intermittentINSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT IN CEILING JUST INBOARD OF UPPER DECK ESCAPE LATCH, COMES ON THEN GOES OFF AFTER A FEW SECONDS. REMOVED AND REPLACED LIGHT ASSY. OPS CHECK NORMAL IAW BMM 33-51-07.SDR UIEA200200059Skin · corrodedDURING CURRENT "C" CHECK, FOUND CORROSION BETWEEN OUTER SKIN, DOUBLER AND TRIPLER AT BS 1960 STR 42 RT, LOCATED AT THE AFT LOWER CORNER CUTOUT OF THE AFT LOWER LOBE COMPARTMENT DOOR. NO LEVEL DECLARED BUT CORROSION CONSIDERED LOCAL. OUTER SKIN, DOUBLER AND TSDR UIEA200200060Panel · crackedDURING CURRENT C-CHECK, AT HKG FOUND REVEAL PANEL CRACKED AT NR 2 MED STATION 800 BETWEEN STRINGER 17L AND 18L. CRACK LENGTH IS APPROX .5 INCH LONG TERMINATING IN A COMMON FASTENER HOLE. PERFORMED E/C INSPECTION TO ENSURE NO CRACK PROPAGATION FROM HOLE. OVESDR 0203386642Battery Pack · dischargedDURING LINE CHECK, FOUND A-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD.SDR UPS02439437Plug · looseINSPECTION TYPE:N/A AIR TURNBACK ENG FIRE NR 3 ENGINE. FOUND BORESCOPE PLUG AT 2 O'CLOCK POSITION ON DIFFUSER CASE LOOSE. REINSTALLED PLUG AND SAFETIED IAW 72-00-00. RAN NR 3 ENGINE WITH NO RISE IN TEMP. A/C RETURNED TO SERVICE.SDR EIAA2002099Light · inoperativeDURING A-CHECK, FOUND R5 EMERGENCY EXIT SIGN, L5 DOOR EMERGENCY EXIT FLOOD LIGHT, EMERGENCY EXIT CEILING LIGHT INOPERATIVE AT STATION 2125 LT, EMERGENCY EXIT CREW DOOR SILL LIGHTS INOPERATIVE. REMOVED AND REPLACED EMERGENCY LIGHT ASSY`S, OPS CHECKED OK, PER MSDR UPS02439389Panel · crackedINSPECTION TYPE:N/A LT WING OTBD MID T/E FLAP 4 FT CRACK ON TRAILING EDGE. INSTALLED COVE PANEL REF SRM 51-30-02.SDR UPS02439220Bulkhead · corrodedINSPECTION TYPE:C, CORROSION REVEALED ON BS 1480 BULKHEAD WEB LEFT I/B CORNER AREA, AREA INSP AFTER BATHTUB FITTING REMOVED INSIDE KEEL BEAM BOX. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPAIRED IAW HX RS R53-49-3SDR UPS02439071Fitting · crackedINSPECTION TYPE:C RH BS 1480 BULKHEAD EXTENSION FITTING BOLT HOLE #11 FOUND CRACK. RH BS 1480 BULKHEAD #11 HOLE AT EXTENSION FITTING REAMED TO 0.625" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-SDR UPS02439225Stiffener · corrodedINSPECTION TYPE:C, RIGHT WLG BS 1241 BULKHEAD STIFFENER FOUND CORROSION AT WL 150 RBL 4-10. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 57-10-01 FIG 1 LIMITS FOR REPAIR REFER TO HX RS R57-12-34875.SDR UPS02439178Pressure Panel · crackedINSPECTION TYPE:C BS RIGHT 1241 CANTED BULKHEAD OF WEB PNL HAS TWO CRACKS BETWEEN RBL 76 TO 80 AT THE AREA ADJACENT TRIM AIR DUCTS. WEB REPAIRED AS PER SRM 53-10-07 FIG 6.SDR UPS02439098Skin · damagedINSPECTION TYPE:C NR 2 PYLON I/B REAR MOUNT PYLON SKIN LOWER EDGE DOUBLER NONSTANDARD REPAIR IS FOUND AS MARKED. NR 2 PYLON I/B LOWER EDGE SKIN REPAIRED AS PER SRM 54-34-03 FIG 24 AND SRM 54-34-03 FIG 25.SDR UPS02439223Keelbeam · corrodedINSPECTION TYPE:C, FX-KEEL BEAM BOX INTERIOR RIGHT SIDE LOWER CHORD FOUND CORROSION AT STA 1460-1468 RBL 6 TO RBL 8. CORROSION REMOVED IAW SRM 51-10-01 CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPAIRED IAW HX RS R53-49-34878.SDR UPS02439215Splice · crackedINSPECTION TYPE:C, RIGHT BS 1241 BULKHEAD SPLICE STRAP FWD HOLE FOUND CRACK AT 12 O/C POSN WL 190. HOLE REWORKED IAW EO 5310-0323 APP F LIMIT. REF EO 5310-0323 PARA 4D ITEM 3 FOR SPLICE STRAP CRACK FINDING NO FURTHER ACTION IS REQUIRED.SDR UPS02439113Panel · corrodedINSPECTION TYPE:C FX- KEEL BEAM FIXED PANEL UPPER SURFACE FOUND SURFACE CORROSION AT STA 1255 TO STA 1275 RBL 9 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG 8.SDR UPS02439111Web · corrodedINSPECTION TYPE:C FX- AIR CONDITIONING BAY REAR FIXED FAIRING LT SIDE. GROUND PNEUMATIC AIR CONNECTOR SERVICE BOX INTERIOR REAR WEB FOUND SURFACE CORROSION AT STA 1255 LBL 34 TO LBL 36. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-SDR UPS02439110Shim · corrodedINSPECTION TYPE:C FX-KEEL BEAM BOX EXTERIOR LOWER CHORD TO PANEL SUPPORT ATT SHIM FOUND CORROSION AT LT SIDE STA 1308 LBL 6 TO LBL 9. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG SDR UPS02439109Panel · corrodedINSPECTION TYPE:C FX- KEEL BEAM FIXED PANEL UPPER SURFACE FOUND SURFACE CORROSION AT LT SIDE STA 1438 TO STA 1460 LBL 9 TO LBL 16. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 51-10-01.SDR UPS02439107Shim · corrodedINSPECTION TYPE:C FX-KEEL BEAM BOX EXTERIOR LOWER CHORD TO PANEL SUPPORT ATT SHIM FOUND CORROSION AT RT SIDE STA 1328 RBL 6 TO RBL 9. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACED IAW SRM FIG 51-10-01 PG SDR UPS02439216Bulkhead · crackedINSPECTION TYPE:C LEFT BS 1241 BULKHEAD FWD HOLE CRACKED AT BULKHEAD FRAME FORGING SPLICE STRAP & SKIN WL 170 TO 180. REWORKED HOLE AS PER EO 5310-0323 APP F TABLE 1, REWORKED HOLE NDT INSPECTED NIL CRACK FOUND AS PER NTM PART 6 51-00-00 FIG 1.SDR UPS02439108Support · corrodedINSPECTION TYPE:C FX- KEEL BEAM PNL SUPPORT LOWER CHORD FOUND SURFACE CORROSION AT STA 1480 LBL 16 TO RBL 16. CORROSION REMOVED IAW SRM 51-10-01, CORROSION BLEND OUT EXCEEDS SRM 53-10-01 LIMITS, REPLACED IAW SRM FIG 51-10-01.SDR UPS02439099Skin · deformedINSPECTION TYPE:C NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN DEFORMED AS MARK. NR 1 PYLON RT LOWER EDGE AREA FROM NAC STA 180- REAR DRAG FIXED FAIRING INTERIOR METAL SKIN REPLACED AS PER SRM 54-34-03 FIG 25.SDR UPS02439176Stiffener · crackedINSPECTION TYPE:C #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER FOUND 2EA FASTENER HOLE CRACKED REFER ATTACHED SKETCH FOR DETAILS. #1 PYLON REAR ENGINE MOUNT B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8.SDR UPS02439175Stiffener · crackedINSPECTION TYPE:C #2 PYLON REAR ENGINE MOUNT BULKHEAD UPPER STIFFENER 2EA FASTENER HOLES CRACK FOUND AT O/B SIDE OF PYLON THROUG THICKNESS REFER TO ATTACHED DRAWING FOR LOCATION. #2 PYLON REAR ENGINE B/H UPPER STIFFENER REPLACED AS PER SRM 51-10-01 PAGE 8.SDR UPS02439171Web · crackedINSPECTION TYPE:C #3 PYLON REAR MOUNT BULKHEAD FOUND CRACKED AT FWD & AFT WEB AT THREE FASTENER HOLE LOCATIONS AS PER ATTACHED FIGURE.(STA 221.9 TO 222, WL 170 TO 180). #3 PYLON REAR ENG MOUNT BULKHEAD REPAIR CARRIED OUT AS PER HX RS # R-54-53-34870.SDR UPS02439163Skin · crackedINSPECTION TYPE:C RH BS 1480 B/H #12 HOLE CRACK FOUND AT SKIN THROUGH THICKNESS RUNNING FWD & AFT REFER ATTACHED SKETCH. (STR R33 TO R34) RH BS 1480 B/H #12 HOLE AT SKIN REAMED TO 0.710 " DIAMETER AND BUSHING REPAIR CARRIED OUT AS PER RS # R-53-43-34784. NSDR UPS02439162Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H EXTENSION FITTING #9 HOLE CRACK FOUND, APPROX 1/16", RUNNING FWD & AFT REFER ATTACHED SKETCH. ( STR R33 TO R34) RH BS 1480 B/H EXTENSION FITTING #9 HOLE REAMED TO 0.850" DIAMETER AND BUSHING REPAIR CARRIED OUT AS PER RS #RSDR UPS02439101Web · crackedINSPECTION TYPE:C RH BS 320 NOSE W/W VERTICAL BEAM WEB ONE INSULATION BLANKET STANDOFF HOLE CRACK FOUND APPROX 7/8" LONG AS MARKED. (WL 160 TO 170) VERTICAL BEAM WEB REPLACED AS PER DWG 624U0005 SHEET 4 AND SRM 51-10 -01 PG 8.SDR UPS02439100Skin · corrodedINSPECTION TYPE:C RIGHT BS 1480 BULKHEAD NR 6 HOLE CORROSION FOUND AT SKIN AROUND BORE STR 33R TO 34R. HOLE REAMED AND BUSHING INSTALLED AS PER SB 747-53A2390. REWORKED HOLE INSPECTED - SATISFACTORY AS PER NTM PART 6 51-00-00 FIG 1.SDR UPS02439097Web · crackedINSPECTION TYPE:C FWD CARGO - STA 900 (LBL 46", BELOW FLOOR 6") FRAME WEB FOUND CRACK AS MARKED. REPAIRED WEB AT FWD CARGO STA 900 LBL 46" AS PER SRM 51-40-02.SDR UPS02439096Seat Track · corrodedINSPECTION TYPE:C M/D- BS2278 LBL 33 SEAT TRACK CROWN CORR. CORROSION REMOVED IAW SRM 51-10-01. CORROSION BLEND OUT 0.040" X 1" X 2" EXCEED SRM 53-10-01 FIG 1 LIMITS. FOR REPLACEMENT REFER TO SRM FIG 51-10-01.SDR UPS02439081Floor Support · corrodedINSPECTION TYPE:C M/D- BS 2320 - 2340 RBL 2 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXCEEDS SRM 53-10-01 FIG 1 LIMITS, FOR REPLACEMENT REFER SRM FIG 51-10-01.SDR UPS02439080Floor Support · corrodedINSPECTION TYPE:C M/D- BS 2350 - 2360 RBL 16 FLOOR SUPPORT CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXCEEDS SRM 53-10-01 FIG 1, LIMITS REPLACEMENT REFER SRM FIG 51-10-01.SDR UPS02439079Channel · corrodedINSPECTION TYPE:C M/D- BS 2280 - 2300 RBL 11 HAT SECTION CORRODED. CORROSION REMOVED IAW SRM 51-10-01, CORROSION EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACEMENT REFER SRM FIG 51-10-01.SDR UPS02439078Channel · corrodedINSPECTION TYPE:C M/D- BS 2315 - LBL 11 HAT SECTION CORRODED. CORROSION REMOVED IAW SRM 51-10-01. CORROSION EXCEEDS SRM 53-10-01 FIG 1 LIMITS, REPLACEMENT REFER SRM FIG 51-10-01.SDR UPS02439072Fitting · crackedINSPECTION TYPE:C RH BS 1480 B/H #16 HOLE CRACK AT B/H WEB AFT SURFACE RUNNING UP APPROX 0.040" LONG. REFER ATTACHED SKETCH. (STR R34) RH BS 1480 B/H HOLE AT WEB PNL REAMED TO 0.500" AND BUSHING INSTALLED AS PER SB 747-53A2390 REWORKED HOLE INSPECTED. NIL
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