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 9717546642Skin · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON SKIN AT BS 550, STR 46R. REPAIRED PER EA 66-150239.SDR TWRA97167Compressor · stalledDURING CLIMB THROUGH APPROXIMATELY 1,500 FEET, NR 1 ENGINE COMPRESSOR STALLED. EPR 1.49, EGT 1100 DEGREES CELSIUS FOR APPROXIMATELY 2 SECONDS. ENGINE WAS SHUT DOWN (ACFT RETURN TO JFK). REMOVED AND REPLACED NR 1 ENGINE PER WIC 71-002. ENGINE RUN-UP, LEAK CSDR TWRA97166Light · inoperativeDURING DAILY SERVICE, FOUND CEILING LIGHT INOP ABOVE SEAT 18ABC. REPLACED CEILING LIGHT. OPS CHECK OK PER MM 33-51-00. (M)SDR TWRA97164Fitting · failedDURING CRUISE, NR 1 ENGINE OIL PRESSURE FLUCTUATED AND DROPPED BELOW YELLOW BAND. OIL PRESSURE LIGHT ON AT PILOT'S PANEL. ENGINE FAILURE CHECK LIST ACCOMPLISHED. ENGINE SHUT DOWN ON FINAL APPROACH. ENGINE OIL PRESSURE 7 PSI. FLIGHT DIVERTED TO JFK. MAINTSDR 9717536642Frame · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON TOP SIDE OF BEAM LOWER FLANGE AT OVERHEAD PRESSURE DECK FS 1268, RBL 58 TO 120. REPAIRED PER EA 66-150404.SDR SRAA970708Cable Drum · lack of lubeON TAXI OUT DURING FLIGHT CONTROL CHECK, FOUND LEFT SPOILER DID NOT EXTEND AND A GRINDING NOISE CAME FROM UNDER COCKPIT. AIRCRAFT RETURNED TO BLOCK. RESET SPOILER INDICATOR C/B, LUBRICATED CAPTAIN'S AND CO-PILOT'S CABLE DRUMS, PERFORMED FLIGHT CONTROL FUNCTISDR 9717486642Floorbeam · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM WEB AT FS 580, LBL 115, WL 189. REPAIRED PER EA 66-150706.SDR 9717476642Floorbeam · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM CHORD AT FS 760, LBL 99 TO 120, WL 189 TO 199. REPAIRED PER EA 66-151330.SDR UIEA9706Pdu · defectiveATB - FLT MIA-BOG - ON FLAP RETRACTION AFTER TAKEOFF, NR 4 LE ON LEFT DID NOT INDICATE UP. USED ALTERNATE SYSTEM, BUT STILL DID NOT INDICATE UP. SCANNED LED'S VISUALLY WITH FLAPS SELECTED TO 0 AND 1 DEGREE POSITIONS. LEFT INBOARD LED SECTION DID NOT APPEARSDR TWRA97163Light · inoperativeDURING DAILY SERVICE, FOUND SEAT 64H FLOOR EVAC LIGHT INOPERATIVE, FLOOR LIGHT STRIP TORN. REPLACED FLOOR EVAC LIGHT AND FLOOR STRIP PER MM 33-51-00. OPS CHECKED NORMAL. (X)SDR TWRA97162Light · inoperativeDURING DAILY SERVICE, FOUND CEILING EVAC LIGHT INOPERATIVE AT SEAT 6AC AND 5KH. REPLACED CEILING LIGHT PER MM 33-51-00. OPS CHECKED NORMAL. (X)SDR TWRA97160Light · inoperativeFOUND ON DAILY SERVICE, NON-ROUTINE, EVAC CEILING LIGHT ABOVE 25/26 HJK INOP. REMOVED AND REPLACED CEILING LIGHT ASSEMBLY. OPS CHECK OK PER 33-51-00. (M)SDR TWRA97156Light · inoperativeDURING DAILY SERVICE, FOUND L1 BUSTLE LIGHT INOPERATIVE. REMOVED AND REPLACED L1 BUSTLE LIGHT. OPS CHECKED NORMAL PER MM 33-51-00, PAGE 501. (X)SDR 9716956642Web · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION AROUND FASTENER HOLES ON THE LOWER BEAM WEB AT THE FORWARD CARGO DOOR. REPAIRED PER EA 66-123887.SDR 9712416642Fitting · crackedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CRACK IN FORWARD ACTUATOR LIFT ARM ATTACH FITTING ON FORWARD CARGO DOOR. REPLACED FITTING PER SRM 51-30-02.SDR TWRA97155Light · inoperativeDURING DAILY SERVICE, FOUND 4L DOOR BUSTLE LIGHT INOPERABLE. REPLACED BUSTLE LIGHT. OPS CHECKED OK PER MM 33-51-00. (X)SDR SRAA970609Engine · oil lossDURING FLIGHT, NR 1 ENGINE OIL QUANTITY DROPPED TO 1.2 GAL, OIL PRESSURE TO 47 PSI, AND OIL TEMP AT 101 DEG. SHUT DOWN ENGINE AS PRECAUTIONARY AND LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 1 ENGINE, OPS CHECKED GOOD PER MM CH 71-00-00.SDR 9717626642Floorbeam · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON MAIN DECK FLOORBEAM T-CHORD FS 920, RBL 29 TO 64. REPAIRED PER EA 66-150064.SDR 9717616642Frame · crackedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CRACKED FRAME WEB FS 560, STR 24L. REPAIRED PER EA 66-150619 AND 66-150047.SDR TWRA97145Wire · brokenDURING 'B' SERVICE, FOUND L2 JUMPSEAT EVAC LIGHT INOP. REPAIRED BROKEN WIRE. OPS CHECKED OK PER MM 33-51-00. (M)SDR TWRA97144Light · inoperativeDURING 'B' SERVICE, FOUND R4 DOOR OVERHEAD EVAC LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY. OPS CHECKED OK PER MM 33-51-00. (M)SDR TWRA97143Light · brokenDURING 'B' SERVICE, FOUND L4 JUMPSEAT EVAC LIGHT BROKEN. INSTALLED NEW LIGHT ASSEMBLY. OPS CHECKED OK PER MM 33-51-00. (M)SDR TWRA97142Light · missingDURING 'B' SERVICE, FOUND R2 JUMPSEAT EVAC LIGHT MISSING. INSTALLED LIGHT ASSEMBLY. OPS CHECKED NORMAL PER MM 33-51-00. (M)SDR TWRA97136Power Supply · inoperativeDURING DAILY SERVICE, FOUND 'E' ZONE EVAC SEAT LIGHTS INOP. REPLACED BATTERY POWER SUPPLY. OPS CHECKED OK PER MM 33-51-00. (M)SDR EIAA970174Engine · failedJFK - LOG PAGE: E06131 - SHORTLY AFTER STARTING DESCENT, THE FLIGHT ENGINEER REPORTED THE NR 2 ENGINE OIL QUANTITY INDICATED ONE GALLON. APPROXIMATELY ONE MINUTE LATER, THE OIL PRESSURE LIGHT ON THE ANNUNCIATOR PANEL STARTED BLINKING AND THE OIL PRESSURE DRSDR 97ZZZM725Skin · corrosionDURING C-CHECK INSPECTION DISCOVERED CORROSION ON THE LEFT WING LOWER SKIN FORWARD OF THE FRONT SPAR LOWER CHORD AT APPROX WING STATION 564. REPAIRED BY SPLICING IN A NEW SECTION OF REINFORCEMENT STRAP AND INSTALLING A REPAIR DOUBLER AT THE THE LOCATION OF THSDR 97ZZZM724T-Chord · crackedDURING C-CHECK INSPECTION DISCOVERED CRACKED AND BROKEN UPPER 'T' CHORDS OF BOTH THE LEFT AND RIGHT WINGS AT THE TRAILING EDGE BEAM AT WBL 235.2. RIGHT WING HAD AN 2 INCH CRACK AND THE LEFT WING HAD A BROKEN FORWARD EDGE OF THE FORWARD HORIZONTAL FLANGE OF THSDR 97ZZZM723Bulkhead · corrodedDURING C-CHECK INSPECTION, DISCOVERED CORROSION BETWEEN THE FUSELAGE SKIN AND THE AFT FLANGE FO THE STA 2360 PRESSURE BULKHEAD AFT OUTER CHORD. THE CORROSION EXTENDED ALONG THE ENTIRE WIDTH OF THE AFT CHORD FROM STRINGER 46R TO 51R. REPAIRED BY TRIMMING AWAYSDR 9717606642Seat Track · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON SEAT TRACK CROWN FS 1000 TO 1265, RBL 78. REPAIRED PER EA 66-150065.SDR 9717596642Floorbeam · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM UPPER CHORD FS 640, RBL 50 TO 84. REPAIRED PER EA 66-150438.SDR 9717586642Floorbeam · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON FLOORBEAM UPPER CHORD FS 1720, RBL 84 TO 115. REPAIRED PER EA 66-151404.SDR 9714346641Floorbeam · corrodedDURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON AFT CARGO FLOORBEAM UPPER AND LOWER CHORD FS 1860, RBL 33 TO LBL 79. REPAIRED PER EA 66-150699.SDR 9714356641Keel Beam Web · corrodedDURING M CHECK AND PRIOR TO SERVICE, FOUND CORROSION ON KEEL BEAM WEB, RIGHT SIDE FS 1450. REPAIRED PER EA 66-150690.SDR 9716966642Skin · corrodedDURING M-CHECK AND PRIOR TO SERVICE, FOUND CORROSION ALONG LOWER EDGE OF LOWER BODY LONGITUDINAL SKIN JOINT AT FS 1961 TO 2181, STR 34R TO 46R. REPAIRED PER EA 66-150448.SDR TWRA97132Light · inoperativeDURING SERVICE, FOUND L4 DOOR BUSTLE LIGHT INOPERATIVE. REMOVED AND REPLACED BUSTLE LIGHT ASSY. OPS CHECKED OK PER M 33-51-00. (X)SDR TWRA97131Fuse · failedDURING DAILY SERVICE, FOUND RIGHT OVERWING FORWARD EVAC LIGHT INOP. REPLACED FUSE AND LIGHT ASSEMBLY. OPS CHECKED OK PER MM 33-51-00. (M)SDR EIAA970172Skin · crackedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 2 PYLON SKIN DEFORMED AND CRACKED ON EACH SIDE OF FORWARD UPPER LINK FITTING, NAC STATION 221-222 WBL 470. REPAIRS ACCOMPLISHED IAW SRM 54-40-03 FIGURE 19. (M)SDR EIAA970171Web · crackedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NOSE LANDING GEAR WHEEL WELL TUNNEL BS 260 RBL 70 BULKHEAD WEB RADIUS PORTION CRACKED. REPAIRS ACCOMPLISHED IAW SRM 53-10-04 FIGURE 6, WEB REAR. (M)SDR EIAA970170Skin · crackedHKG - DURNG C5/D-CHECK INSPECTION, DISCOVERED RIGHT WING REAR SPAR TO WING CENTER SECTION REAR SPAR CHORD HAS A CRACK IN SKIN. REPAIRS ACCOMPLISHED IAW SB 747-57-2110, REPAIR BUSHING FABRICATED AND INSTALLED. (M)SDR EIAA970169Pressure Deck · holeHKG - DURING C5/D CHECK INSPECTION, DISCOVERED NOSE LANDING GEAR WHEEL WELL PRESSURE DECK AT RIGHT BS 320, FOUND EXISTING .375 INCH DIAMETER HOLE. REPAIRS ACCOMPLISHED IAW RS 53-18-33351. (M)SDR EIAA970168Light · inoperativeHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED MID BS 2200 LEFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPAIRED ON SHOP TAG NR 017233 AND REINSTALLED IAW MM 33-51-00. (M)SDR EIAA970167Light · inoperativeHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED MID BS 400 LEFT CEILING EMERGENCY LIGHT WAS INOPERATIVE. REPAIRED ON SHOP TAG NR 017231 AND REINSTALLED IAW MM 33-51-00. (M)SDR EIAA970166Frame · crackedHKG - DURNG C5/D CHECK INSPECTION, DISCOVERED MID FRAME CRACKED AT BS 960 STRINGER 5L. REPAIRS ACCOMPLISHED IAW SRM 53-10-04 FIGURE 357-57-2224, REPAIRED. (M)SDR EIAA970165Beam · misrepairedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED LEFT WING AUXILLARY BEAM UPPER CHORD FOUND A NON-STANDARD REPAIR. REPAIRS ACCOMPLISHED IAW SRM 51-40-03 AND SB 747-57-2224, REPAIRED. (M)SDR EIAA970164Fitting · gougedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 3 PYLON UPPER LINK WING ATTACH FITTING OUTBOARD HALF WAS GOUGED AND CORRODED. REPAIRS ACCOMPLISHED IAW RS 57-04-33335 AND BOEING TELEX EVR-HKG-97-0096RE, REWORKED. (M)SDR EIAA970163Bulkhead · corrodedHKG - DUIRNG C5/D-CHECK INSPECTION, DISCOVERED NR 4 PYLON FRONT BULKHEAD AT NAC STATION 128 HAS CHAFING AND CORROSION. REPAIRS ACCOMPLISHED IAW RS 54-53-33350 AND BOEING TELEX EVR-HKG-97-0123RE, REWORKED. (M)SDR EIAA970162Fitting · damagedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 2 PYLON FRONT SPAR UPPER LINK INBOARD FITTING HAS TOOL MARKS. REPAIRS ACCOMPLISHED IAW RS 57-04-33343 AND BOEING TELEX EVR-HKG-97-0114RE, REWORKED. (M)SDR EIAA970161Fitting · damagedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 1 PYLON FRONT SPAR UPPER LINK OUTBOARD FITTING HAS TOOL MARKS. REPAIRS ACCOMPLISHED IAW RS 57-04-33352 AND BOEING TELEX EVR-HKG-97-0103RE, REWORKED. (M)SDR EIAA970160Skin · chafedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED NR 2 PYLON ACCESS DOOR CUTOUTS HAVE WORN LOWER EDGES AT 462BL, 463CL, 462DL, 463EL AND 463GL. REPAIRS ACCOMPLISHED IAW RS 54-40-33355 AND BOEING TELEX EVR-HKG-97-0107TE AND EVR-HKG-97-0125RE. (M)SDR EIAA970159Stop Fitting · crackedHKG - DURING C5/D-CHECK INSPECTION, DISCOVERED MID R-3 DOOR CUTOUT FORWARD FRAME NR 4 STOP FITTING CRACKED. REPAIRS ACCOMPLISHED IAW SRM 51-10-01, REPLACED NR 4 STOP FITTING. (M)
Back to Boeing 747 212B