Boeing 747-2L5B
Service difficulty reports · 41
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 = '7472L5B' 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 = '7472L5B' 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 Q2SA815003Support Beam · brokenUPON ACCOMPLISHING A SCHEDULED INSPECTION, MAINTENANCE PERSONNEL DISCOVERED THE INBOARD FLAP, INBOARD TRACK SUPPORT BEAM /BRACKET BROKEN. REMOVED AND REPLACED INBOARD SECTION OF TRAILING EDGE SUPPORT BEAM UPPER TEE TO EXISTING SPLICE AT WBL 276 PER SOF-SOF -1SDR Q2SA815002Cooling Duct · brokenAFTER LEVEL OFF FROM CLIMB, NR 2 ENGINE "B" LOOP BEGAN OSCILLATING TO TOP OF SCALE AND BACK AND ILLUMINATED THE FIRE DETECTION AMBER LIGHT INTERMITTENTLY; THE "A" LOOP WAS SELECTED AND FOUND TO BE NORMAL. THE FLIGHT PROCEEDED NORMALLY FOR APPROX 1 HOUR WHEN TSDR Q2SA815001Cowling · departedON WALK AROUND, FOUND DAMAGE TO THE NR 3 ENGINE FIXED COWL. UPON INSPECTION, FOUND EVIDENCE THAT PORTIONS OF THE FIXED COWL DEPARTED CAUSING DAMAGE TO THE RIGHT INBOARD AFT FLAP.SDR VGQY2010082600123Splice Plate · crackedHFEC INSP FOUND SPLICE PLATE CRACK APPROX 1 INCH ON BS 400 S45R O/B LWR CHORD OF BULKHEAD AREA. CRACKED END STOP DRILLED AS PER SRM 53-30-03 FIGURE 35 REVISION 117. HFEC INSPECTION CARRIED OUT AROUND STOP DRILL HOLE AND FOUND CRACKED CONTAINED. FABRICATED SDR VGQY2010082400122Strap · damagedMAIN DECK - BS 720 RT FOUND FRAME STRAP WITH DEEP CUTTING MARKS BETWEEN STR 22-23. COMPLIED WITH EN1180-10, ALTERNATE FABRICATION OF FRAME STRAP 65B01729-197 AT STA 720, BETWEEN S-22R & S-23R.SDR VGQY2010082300118Spar · crackedRIGHT WING NR 3 TANK INTERIOR MID SPAR UPPER / WEB CRACK. WEB CUTOUT, REPAIR PARTS FABRICATED USING 7075-T6 0.100" AND 2023-T3 0.125" AND INSTALLED AS PER SRM 57-10-06 REV 117, FIGURE 5.SDR VGQY2010082300121Door · damagedREPAIR DOUBLER FOUND AT NR 5L MED UPPER HINGE CUTOUT.SDR VGQY2010082300119Door · damagedREPAIR DOUBLER FOUND AT NR 2R MED, DOOR LOWER AREA. COMPLIED WITH EN 1198-10.SDR VGQY2010082000117Mount · corrodedNR 4 ENGINE LOWER AFT MOUNT CORRODED. MOUNT REMOVED AND REPLACED PER AMM 71-21-0SDR VGQY1900010000117Mount · corrodedNR 4 ENGINE LOWER AFT MOUNT CORRODED.SDR VGQY2010081700115Fitting · crackedUPON REPLACEMENT OF RIGHT WING I/B TRAILING EDGE FLAP O/B DEFLECTION CONTROL ROLLER AS PER NRC NO: 0667, FOUND ROLLER FITTING CRACKED. ROLLER FITTING ASSEMBLY REMOVED AND REPLACED PER B747 SRM 51-30-02 REV 117.SDR VGQY2010081600105Bulkhead · crackedDURING STA 2598 MODIFICATION, STA 2598 LT LWR BULKHEAD FOUND CRACK. COMPLIED WITH EN 1161-10.SDR VGQY2010081500104Skin · crackedNR 2 SPOILER LOWER SURFACE ADJACENT TO INBOARD LUG / SKIN CRACK. LT HAND WING NR 2 SPOILER REMOVED AND REPLACED PER AMM 27-61-02 REV 79. P/N INSTALLED: 65B02250-41, S/N INSTALLED: 006474SDR VGQY2010081200078Channel · crackedLEFT WING T/E REAR SPAR ADJACENT TO NR 6 SPOILER ACTUATOR AFT FACE / UPPER CHANNEL CORRODED. TRAILING EDGE BEAM UPPER CHORD 65B11614-7 FOUND WITH CORROSION CRACKING AT TWO LOCATIONS. CRACK LENGTHS ARE APPROX 3.5" INCH AND 1.75" AT THE RADAII. COMPLIED WITH SDR VGQY2010081200086Structure · corrodedLEFT WING I/B TRAILING EDGE MID FLAP AFT LOWER CHORD FOUND CORRODED. R & R IAW AMM 27-51-03 REV 79.SDR VGQY2010081200085Bear Strap · crackedHFEC OPEN HOLE INSP FOUND CRACK INDICATION ON FWD CARGO DOOR AFT CUTOUT UPPER CORNER DOOR HINGE AREA. COMPLIED WITH EN 1193-10.SDR VGQY2010081200079Skin · corrodedRIGHT WING T/E NR 11 SPOILER LWR SURFACE ACTUATOR CUTOUT AREA FOUND CORROSION AT SUPPORT ANGLE. R & R IAW AMM 27-61-02 REV 79.SDR VGQY2010081200084Bracket · crackedAPU COMPT AFT MOUNT ROD UPPER END, BRACKET FOUND CRACK. REMOVED AND REPLACED PER AMM 51-30-02 REV 117.SDR VGQY2010081200083Beam · crackedRIGHT WING L/E BULLNOSE SKIN ADJACENT TO NR 16 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.SDR VGQY2010081200082Beam · crackedRIGHT WING L/E BULLNOSE SKIN ADJACENT TO NR 14 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.SDR VGQY2010081200081Skin · crackedLEFT WING L/E BULLNOSE SKIN ADJACENT TO NR 13 KRUEGER FLAP O/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10.SDR VGQY2010081200080Beam · crackedLEFT WING L/E BULLNOSE SKIN ADJACENT TO NR 11 KRUEGER FLAP I/B LINKAGE FOUND CRACKED. COMPLIED WITH EN1180-10, REPAIR FOR 05 EA CRACKS ON WING FIXED L/E LWR PANEL SUPPORT BEAM.SDR VGQY2010081000076Frame · crackedNR 3 PYLON INTERIOR AFT SIDE UPPER AFT ENGINE MOUNT BULKHEAD FRAME ATTACHING CHORD FOUND CRACK MARKS AT NAC STA 286 (NEXT TO I-BEAM). NDT METHOD OF EDDY CURRENT INSP REQ'D TO VERIFY AND LOCATE SUBJECT CRACK MARKS FOR STRUCTURE REPAIR. COMPLIED WITH EN 1188-1SDR VGQY2010081000066Frame · crackedNR 4 PYLON INTERIOR - DET FOUND CRACKS ON BOTH I/B AND O/B SIDE OF AFT MOUNT BULKHEAD FWD AREA UPPER CHORD AT NAC STA 270. COMPLIED WITH EN 1185-10.SDR VGQY2010080600065Spar · corrodedLEFT WLG WHEEL WELL STA 1241 LBL 5 CENTER TANK REAR SPAR WEB AFT OF CCA FOUND CORRODED. COMPLIED WITH EN 1192-10, CORROSION REPAIR FOR LT WLG WHEEL WELL STA 1241 WING CENTER SECTION REAR SPAR MACHINE WEB 65B10281-10SDR VGQY2010080600064Keelbeam · corrodedAFT KEEL BEAM ASSY STA 1466.50 RBL 5 FOUND CORROSION. COMPLIED WITH EN 1195-10, REPAIR FOR CORROSION ON LT & RT KEEL BEAM CHORD (65B15074-5 & -6) HORIZONTAL FLANGE UPPER SURFACE AT STA 1469 LBL 7 & RBL 7.SDR VGQY2010080600063Keelbeam · corrodedAFT KEEL BEAM ASSY STA 1466.50 LBL 5 LOWER CHORD FOUND CORROSION. COMPLIED WITH EN 1195-10, REPAIR FOR CORROSION ON LT & RT KEEL BEAM.SDR VGQY2010080500058Floorbeam · damagedHFEC OPEN HOLE INSP FOUND DOUBLE HOLE ON BS 640 RBL 50 UPPER DECK FLOORBEAM UPPER CHORD AFT HORIZONTAL FLANGE AS MARKED. NEW WEB FABRICATED PER DWG 65B14743 DAMAGED UPPER CHORD AND WEB REMOVED AND REPLACED PER SRM 51-30-02 REV 117.SDR VGQY2010080600057Spar · corrodedLEFT WLG WHEEL WELL STA 1241 LBL 10 CENTER TANK REAR SPAR WEB NEAR UPPER CHORD FOUND CORRODED. CORROSION REMOVED AS PER SRM 51-10-01 REV 117. MATERIAL REMOVED= 0.012 INCH, MATERIAL REMAINING= 0.3025 INCH AND FOUND WITHIN LIMITS PER SRM 57-10-01 REV 117. REWSDR VGQY2010080500056Frame · crackedMAIN DECK CARGO COMPARTMENT - RT STA 1900 FRAME FOUND CRACKED. COMPLIED WITH EN 1179-10.SDR VGQY2010080400055Floorbeam · crackedHFEC OPEN HOLE INSP FOUND CRACK ON BS 340 LBL 32 UPPER DECK FLOORBEAM UPPER CHORD AFT HORIZONTAL FLANGE. REPAIR STRAP AND FILLER FABRICATED AND INSTALLED PER SERVICE BULLETIN B747-53A2431 FIGURE 9 REVISION 2.SDR VGQY2010080400054Channel · crackedCABIN STA 940 APPROX RBL 60 TENSION TIE FWD CHANNEL FOUND CRACKED. CRACKED ‘C’ CHANNEL AT BS 940 TRIMMED OUT AS PER SRM 53-10-11 FIGURE 2 REVISION 117. HFEC INSPECTION CARRIED OUT ON THE TRIMMED OUT AREA AND FOUND NO CRACK EVIDENT. FABRICATED REPAIR CHANNELSDR VGQY2010080400053Frame · corrodedCBN/ U/D/ STA 540 RT FRAME FOUND WITH SURFACE CORROSION. SURFACE CORROSION REMOVED AND REPROTECTED PER SRM 51-10-01 AND SRM 51-10-02 REV 117. ORIG THICKNESS: 0.180 INCH; REMOVED: 0.177 INCH; FOUND WITHIN LIMITS AS PER B747-200 SRM 53-10-01 FIGURE 1, REV 117.SDR VGQY2010080400052Bulkhead · corrodedLEFT MLG WHEEL WELL STA 1480 BULKHEAD LOWER CHORD FOUND CORRODED. REMOVED AND REPLACED PER SRM 51-30-02 REV 173.SDR VGQY2010080400051Pressure Panel · corrodedRIGHT MLG WHEEL WELL STA 1480 / LWR T-CHORD FOUND CORRODED. COMPLIED WITH EN 1162-10.SDR VGQY2010080300049Fitting · damagedNR 2 FLAP TRACK FWD FITTING / BEARING MIGRATION. HOLE DIAMETER MEASURED: 2.1985 INCH FOUND EXCEEDED BOEING DRAWING 65B10471 LIMIT. FITTING BORE HOLE MACHINED AND CHAMFERRED IAW SB 747-57-2325, FIG 18, REV 2. FINAL DIAMETER= 2.226 INCH. FLAP-PEENED, CADMIUMSDR VGQY2010080300048Frame · crackedHFEC INSP FOUND CRACK INDICATION ON BS 1000 RADIUS OF BULKHEAD CHORD BETWEEN STR 38R AND STR 39R BELOW BATHTUB FITTING. COMPLIED WITH EN 1190-10,SDR VGQY2010080300047Door Frame · crackedCABIN - DURING HFEC INSPECTION ON R2 MAIN DECK ENTRY DOOR CUTOUT AT BS 800, 02 EA CRACKS FOUND ON LAST 2 RIVETS ON FRAME INNER CHORD ANGLE AT STR 17 AND CRACK LENGTH APPROX .125 INCH AND .75 INCH AS PER MARKED. COMPLIED WITH EN 1164-10, CRACKS FOUND ON AFT FRSDR VGQY2010080300046Web · crackedMAIN DECK - AT BS 1440, LBL 110 FOUND RIB WEB AT FASTENER AREA CRACKED. REPAIR CARRIED OUT AS PER EN NR 1189-10, STA 1438 RT BONDED WEB ASSY 65B15474-3 ALTERNATE FABRICATION.SDR VGQY2010080200045Mount · corrodedCORROSION ON NR 1 ENGINE AFT UPPER MOUNT MATING SURFACE AREA FOUND OUT OF LIMITS PER OHM 71-20-02. ORIGINAL THICKNESS: 0.500 INCH, MATERIAL REMAINING: 0.470 INCH. COMPLIED WITH ENGINEERING NOTE, EN 1165-10, NR 1 PYLON AFT ENGINE MOUNT FITTING 65B94349-2 EXCESDR VGQY2010120300131Frame · corrodedACFT WAS IN FOR A HEAVY 'D' TRANSITION CHECK). CORROSION WAS FOUND ON INBD FLANGE OF LOWER CHORD. PN 65B10538-151, OTBD OF NR1 ACM BETWEEN STA 1020-1030, LBL 60-80/ AIR-CON PANELS NR191AL & NR191BL SUPPORT FRAME. CORROSION REMOVED AS PER SRM 51-10-01 REV 117
Back to Boeing 747-2L5B