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 UPS02437980Channel · corrodedINSPECTION TYPE:C FX - KEEL BEAM BOX UNDER FAIRING SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT BS 1438 TO BS 1465 RBL 16 TO LBL 16. CHANNEL REPLACED AS PER SRM 51-10-01 PG 8.SDR UPS02437979Support · corrodedINSPECTION TYPE:C FX - KEEL BEAM BOX UNDER FAIRING SUPPORT LOWER SURFACE FOUND SURFACE CORROSION AT BS 1465 RBL 16 TO LBL 16. FAIRING SUPPORT REPLACED IAW SEM 51-10-01 PG 8.SDR UPS02438025Pressure Panel · crackedINSPECTION TYPE:C PRESSURE PAN AT BS 400 CRACK INDICATION FOUND AT 1 EA FASTENER APPROX .75 INCH LENGTH. CRACKED PRESSURE PAN AT BS 400 REPLACED AS PER DWG 624U0005 SHT 9.SDR UPS02437990Angle · crackedINSPECTION TYPE:C NLG W/W - CRACK SUSPECTED AT PRESSURE DECK RH LONGI. SUPPORT ANGLE STA 307 & STA 320 AS MARKED. NLG W/W CEILING R/H UPPER O/B ANGLE REPLACED AS PER EO B747-5310-0574.SDR UPS02438027Frame · crackedINSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B FWD AREA AS MARKED. REPAIR CARRIED OUT IAW REPAIR SCHEME INSTRUCTIONS REFER R-54-53-34756 FOR MAT HT REFER TO CWPS CONTROL SEQUENCE NO.SQYJ016-090 CLASSIFIED MAJOR REPAIR.SDR UPS02438026Frame · crackedINSPECTION TYPE:C NO.3 PYLON - REAR ENG MOUNT FTG UPPER FRAME FOUND CRACK AT O/B AFT PORTION AS MARKED. REPAIR CARRIED OUT IAW REPAIR SCHEME INSTRUCTION REFER R-54-53-34756 FOR MATERIAL HEAT TREATMENT REFER TO COMPONENT WORK PROCESS CARD CONTROL SEQUENCE NSDR UPS02438004Gate · corrodedINSPECTION TYPE:C M/D - L1 DOOR LOWER GATE FOUND PITTING CORROSION. LOWER GATE ASSY CHANGED AS PER MM 52-11-00.SDR UPS02438002Stringer · crackedINSPECTION TYPE:C M/D - BS 856 S25R STRINGER END FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG.1.SDR UPS02438001Tie Clip · crackedINSPECTION TYPE:C FWD CARGO COMPT BS 560 S-33L STRINGER TIE CLIP CRACKED. TIE CLIP REPLACED AS PER SRM 51-10-01 P.8.SDR UPS02437999Web · crackedINSPECTION TYPE:C M/D - R5 DOOR FWD CUTOUT UPP SPLICE WEB FOUND CRACKED. REPAIR DOUBLER INSTALLED AS PER SRM 53-10-04 FIG.91.SDR UPS02437989Web · crackedINSPECTION TYPE:C M/D - L2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. M/D L2 DOOR FWD CUTOUT REVEAL REPAIRED AS PER RS #R-53-20-34755.SDR UPS02437988Web · crackedINSPECTION TYPE:C M/D - R2 DOOR FWD CUTOUT REVEAL FOUND CRACKED. M/D R2 DOOR FWD CUTOUT REVEAL REPAIRED AS PER HX RS #R-53-20-34755.SDR UPS02437978Frame · crackedINSPECTION TYPE:C M/D - R1 DOOR FWD LOWER CORNER FRAME FOUND CRACKED. FRAME REPAIRED AS PER SRM 52-10-02 FIG 10.SDR UPS02438029Bulkhead · crackedINSPECTION TYPE:C NR 1 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS R-54-53-34764 INSTRUCTION.SDR UPS02438028Bulkhead · crackedINSPECTION TYPE:C NR 4 PYLON AFT TORQUE BULKHEAD FOUND 3 FASTENER HOLES CRACK AT CHORD AREA. REPAIR CARRIED OUT AS PER RS-54-53-34764 INSTRUCTIONS.SDR UPS02438009Fitting · corrodedINSPECTION TYPE:C FX - R/H BS 1241 WING CENTER SECTION REAR SPAR WEB AFT SURFACE BULKHEAD FITTING FOUND COR BETWEEN FASTENER #2 AND #9. R/H BS 1241 WING CENTER SECTION REAR SPARE WEB AFT FACE BULKHEAD FTG BETWEEN FASTENER #2 & #9 CORROSION REMOVED AS PER USDR UPS02438020Skin · crackedINSPECTION TYPE:C FX - FUSELAGE EXTERNAL SKIN IS CRACKED AROUND RIVET HEAD AT BS 400 STR 44R - STR 45R (NLG W/WELL RH AFT CORNER CUTOUT). NLG W/W R/H AFT CORNER CUTOUT FX EXTERNAL SKIN REPAIRED AS PER UPS EO B747-5330-3520E AND SRM 51-30-02 AND DWG 141U109SDR UPS02437991Beam · crackedINSPECTION TYPE:C LEFT MLG INBOARD W/W DOOR INBOARD CHANNEL FWD CORNER AREA CRACKED AS MARKED. LEFT MLG INBOARD W/W DOOR INBOARD BEAM REPLACED AS PER SRM 51-10-01 PG 8.SDR 0200836641Drain Line · dirtyDURING FLIGHT, SMOKE EMITTED FROM BEHIND NR 3 GALLEY COFFEEMAKER. TURNED OFF GALLEY POWER AND PULLED GALLEY CIRCUIT BREAKERS, SMELL DISSIPATED. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. CLEANED COFFEEMAKER DRAIN LINE AND REPLACED THE COSDR UPS02437716Light · inoperativeINSPECTION TYPE:N/A 1 EMERGENCY LT INOP UPPER DECK. REMOVED AND REPLACED BULB, OPS CHECK GOOD.SDR 200200180Web · corrodedCANTED WEB (65B07992-110) CORROSION, BODY STATION 1245, RBL 0.00 - 33.9. THE REPAIR TO THE WEB TO ENSURE CRACK AND CORROSION FREE CONDITIONS WAS DONE BY TRIMMING OUT THE DAMAGED AREAS AND INSTALLING FILLERS AND DOUBLERS PER ECRA 482-53-147-2.SDR 200200179Skin · corrodedLEFT HORIZONTAL STABILIZER UPPER SKIN CORROSION. THE REPAIR IS ACCOMPLISHED BY TRIMMING OUT CORRODED AREA OF SKIN THEN INSTALLING AN EXTERNAL DOUBLER SKIN REPAIR PER ECRA 482-55-148-2.SDR 200200178Frame · crackedFRAME WEB CRACK, STA 1760 - STR 39L. THE CRACK LENGTH EXTENDS JUST BELOW THE FAILSAFE CHORD. THIS EXCEEDS THE 747 SRM REPAIR LIMITS. REPAIR OF THE FRAME IS ACCOMPLISHED BY USING THE 747 53-10-04 FIGURE 69. REPAIR WITH BOEING SPECIFIED CHANGES. THIS REPAIRSDR 200200177Web · corrodedCANTED WEB (P/N 65B07992-109) CORROSION, BODY STATION 1245, LBL 0.00-21.5. THIS REPAIR TO THE WEB WAS DONE BY TRIMMING OUT THE DAMAGED AREA AND INSTALLING FILLERS AND DOUBLERS PER ECRA 482-53-144-2.SDR 200200176Skin · corrodedLEFT HORIZ STAB UPPER SKIN STA 385 HOIST ATTACH POINT. THIS REPAIR IS ACCOMPLISHED USING AN EXTERNAL DOUBLER REPAIR. THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-55-143-2.SDR 200200175Spar · corrodedCENTER WING REAR SPAR WEB CORROSION. THIS REPAIR IS ACCOMPLISHED BY BLENDING OUT CORROSION AREAS. SECTION OF THE SLOPING PRESSURE DECK ANGLE WHICH WAS REMOVED TO GAIN ACCESS TO CORRODED AREAS IS ALSO REPLACED. THIS IS ACCOMPLISHED USING TWO SPLICE ANGLES. SDR 200200174Fitting · wornTHE REINSTALLATION OF THE FITTING REQUIRED THE SUBSTITUTION OF STRAIGHT SHANK FASTENERS IN LIEU OF THE TAPER SHANK FASTENERS, ORIGINALLY USED THIS REPAIR IS APPROVED BY THE BOEING COMPANY PER ECRA 482-57-141-02.SDR 200200173Doubler · crackedMAIN ENTRY DOOR NR 5 REVEAL DOUBLER CRACKING. THE REPAIR IS ACCOMPLISHED BY TRIMMING SECTIONS OF THE DOUBLERS OFF AND INSTALLING REPLACEMENT SECTIONS USING SPLICE DOUBLERS PER ECRA 482-53-140-2.SDR EIA2002007Structure · corrodedMZJ - FOUND EXFOLIATION CORROSION AT STATION 1241 RBL 2, UNDER DOUBLER FOR APU SHROUD LINE. REPAIRED CORROSION AREA PER ECRA 482-53-147-2. (M)SDR EIA2002006Frame · crackedMZJ - FOUND C-CHECK, FOUND 6 INCH CRACK IN FRAME AT STATION 1760 BELOW AND INBOARD OF STRINGER 39L TIE CLIP. FABRICATED AND INSTALLED CLIP, STRAP AND DOUBLER PER ECRA 482-53-146-2. (M)SDR EIA2002016Web · corrodedMZJ-EAC - DURING C-CHECK, FOUND CORROSION ON THE LEFT WHEEL WELL CANTED WEB. REPAIRED PER ECRA 482-53-144-2. (M)SDR EIAA2002015Bulkhead · corrodedMZJ-EAC - DURING C-CHECK, FOUND EXFOLIATION CORROSION AT STATION 1241 BULKHEAD, RBL 46, RBL 60 AND INBOARD OF FORK FITTING ALONG UPPER CHORD WEB IN THE RIGHT WING GEAR WHEEL WELL. REPAIRED PER ECRA 482-57-142-2 AND SRM 57-10-1. (M)SDR EIAA2002017Pressure Panel · corrodedMZJ-EAC - FOUND CORROSION AT STATION 1245, RBL 34 ON CANTED PRESSURE DECK. REPAIRED PER ECRA 482-53-147-2. (M)SDR EIA2002018Structure · corrodedMZJ-EAC - FOUND CORROSION AT STATION 1238, RBL 2, ON CENTER WING TANK SKIN. REPAIRED PER ECRA 482-57-149-2. (M)SDR EIAA2002013Frame · crackedMZJ-EAC - FOUND TWO CRACK DURING HFEC INSPECTION ON FRAME STRAP AT STATION 2231 BETWEEN STRINGERS 24L AND 25L. REPAIRED PER ECRA 482-53-140-2. (M)SDR EIAA2002014Frame · crackedMZJ-EAC - FOUND CRACK DURING HFEC INSPECTION ON FRAME STRAP AT STATION 2231 BETWEEN STRINGERS 24R AND 25R. REPAIRED PER ECRA 482-53-140-2. (M)SDR EIAA2002008Web · corrodedMZJ-EAC - LEFT WHEEL WELL, STATION 1241, LBL 19, HAS AREA OF EXFOLIATION CORROSION ON WEB. REPAIRED PER ECRA 482-57-142-2. (M)SDR EIA2002009Stiffener · corrodedMZJ-EAC - FOUND STATION 1241, BL 0, T-STIFFENER HAS CORRODED FASTENER HOLE ON RIGHT SIDE, SECOND FROM TOP. REPAIRED PER ECRA 482-57-142-2. (M)SDR EIAA2002010Stringer · corrodedMZJ-EAC - FOUND CORROSION ON INSIDE AND OUTSIDE OF OUTBOARD FLANGE OF STRINGER 2L, JUST ABOVE STATION 1560 FRAME,MAIN DECK, UPPER LOBE. REPAIRED STRINGER SECTION WITH FABRICATED PARTS PER SRM 53-10-03, 51-10-02 AND 51-30-02. (M)SDR EIAA2002011Web · corrodedMZJ-EAC - FOUND LEFT WHEEL WELL STATION 1241, LBL 2, WAS FOUND TO HAVE CORROSION ON OUTSIDE OF CENTER TANK WEB AROUND SCAVENGE PUMP OPENING. REPAIRED PER ECRA 482-57-142-2. (M)SDR EIAA2002012Spar · corrodedMZJ-EAC - FOUND STATION 1241 REAR SPAR WEB, LEFT SIDE WAS FOUND TO HAVE 2 LOCATIONS OF CORROSION BEHIND FITTING. CORROSION REMOVED AND REPAIRED PER SB 747-57-2263 R2, EO 57-747-1544-99A AND ECRA 482-57-141-2. (M)SDR EIA2002005Spar · corrodedMZJ - FOUND CORROSION ON REAR SPAR WEB OF WING CENTER SECTION BS 1241 BULKHEAD FITTING. CORROSION REMOVED AND WORK ACCOMPLISHED PER SB 747-57-2263/EO 57--747-1544-99 (A).SDR EIA2002002Floorbeam · damagedMZJ - FOUND FLOORBEAM UPPER RETURN FLANGE AT STATION 571, RBL 25, WAS FOUND BROKEN. REMOVED DAMAGED PORTION OF FLOORBEAM AND REPAIRED PER SRM CHAPTER 51. (M)SDR UPS02437394Light · inoperativeINSPECTION TYPE:PFLT EMERGENCY LIGHT OVER UPPER DECK STAIRS INOP. RELAMPED, CHECKS GOOD.SDR UPS01437379Engine · flamed outINSPECTION TYPE:N/A PILOT REPORT NR 1 AND NR 2 ENGINE FLAME-OUT. INGN FUEL AND OIL SYS CK PER MM AND ENGINEERING OPRN NORMAL.SDR 2002F00031Smoke Detector · malfunctionedDURING CLIMB-OUT FROM MIA AT APPROXIMATELY 21,000 FEET, THE CARGO LOWER AFT FIRE LIGHT ILLUMINATED. CHECKLIST SECTION III WAS COMPLETED. THE CARGO FLOOR FELT WARM AT SL, BOTH FORWARD AND AFT CARGO HEAT TURNED OFF. WHILE DESCENDING AT 1800 FT THE FIRE LIGHTSSDR 0104276642Skin Panel · corrodedDuring "H" check found corrosion on center wing upper skin panel at WS 1050 RBL 125 and S27. Repaired per EA 66-186829.SDR 0104266642Frame · crackedDuring "H" check found crack in frame at BS 2231 at door 5L S24L and S25L. Repaired per EA 66-186830.SDR 0104466642Bulkhead · crackedDuring "H" check found 2 1/4 inch crack in number 3 pylon rear engine mount bulkhead frame assembly. Repaired per EA 66-185922.SDR UIEA01104Fire Warning · false indicationDURING TAKEOFF ROLL FROM SUU AT ABOUT 80 KTS, HAD A CARGO FIRE WARNING LIGHT. REJECTED TAKEOFF PERFORMED. PERFORMED VISUAL INSPECTION OF FORWARD AND AFT CARGO COMPARTMENTS. BOTH COOL, NO EVIDENCE OF HEAT OR OVERHEAT CONDITION EXISTS. INSPECTED AFT CARGO HE
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