Boeing 747-2D7B
Service difficulty reports · 726
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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 = '7472D7B' 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 = '7472D7B' 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 UIEA200800002Inu · failedAIR TURN BACK, AFTER TAKEOFF THE CAPT'S ADI AND THE NR 1 INS FAILED. PLACING THE PLATFORM SWITCH TO POSITION 3 MADE NO DIFFERENCE. SWAPPED NR 1 AND NR 3 INU DUE TO NR 1 FAILED. OPS CHECKED GOOD ON NR 1 PLACED NR 3 ON DMI.SDR UIEA200800005Selector Panel · failedA/P F/D SYSTEM "A" ROLL DC CIRCUIT BREAKER POPPED, PREVIOUSLY DETECTED ELECTRICAL ODOR MOMENTARILY.SDR UIEA200700493Panel · delaminatedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 8 LEADING EDGE FLAP WS 917) HAS EVIDENCE OF DELAMINATION. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12.SDR UIEA200700492Panel · delaminatedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 6 LEADING EDGE FLAP WS 1028) HAS EVIDENCE OF DELAMINATION. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12.
SDR UIEA200700497Panel · delaminatedLEFT HAND WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION 3 INCHES LONG, 2INCHES AWAY FROM OUTBOARD EDGE AND 5 INCHES FROM THE LEADING EDGE. REPAIRED PANEL IAW SRM 51-40-12 AT 250 DEGREES AND 26" HG VACUUM AND XEO 57-121207.SDR UIEA200700496Panel · gougedLEFT WING UPPER SURFACE PANEL NR 521 HAS A CIRCULAR SHAPED GOUGE ABOUT 12 INCHES OUTBOARD OF THE INBOARD EDGE ( 7.5 INCHES LONG BY 5.5 WIDE). INTERIM REPAIR ACCOMPLISHED IAW SRM 51-40-15 AND XEO 57-121207.SDR UIEA200700494Panel · crackedLT WING UPPER SURFACE LEADING EDGE TO FRONT SPAR PANEL (BEHIND NR 9 LEADING EDGE FLAP WS 862) HAS 2 INCH CRACK. PANEL REPAIRED IAW SRM 51-40-9 AND 51-40-12.SDR UIEA200700495Panel · delaminatedLEFT WING UPPER SURFACE PANEL NR 521 HAS EVIDENCE OF DELAMINATION ABOUT 3 INCHES LONG 6 INCHES FORWARD OF THE TRAILING EDGE AND 18 INCHES INBOARD OF THE OUTBOARD EDGE. ALSO AN AREA 3 INCHES LONG 21 INCHES AWAY FROM THE OUTBOARD EDGE AND 5 INCHES AFT OF THE LESDR UIEA200700484Panel · crackedDURING ROUTINE INSPECTION FOUND LT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE AT WS 577/586 CRACKED LONGITUDINAL AND AT WS 752 PREVIOUS REPAIR DELAMINATED. PERMANENT REPAIRS ACCOMPLISHED IAW 51-40-09 AND 51-40-12, DOCUMENTED ON EO 4757A406.SDR UIEA200700483Panel · crackedDURING ROUTINE INSPECTION FOUND RT WING L/E FIXED FIBERGLASS PANEL UPPER SURFACE CRACKED LATERAL 4" AT WS 1322. PERMANENT REPAIRS ACCOMPLISHED IAW SRM 51-40-09 AND 51-40-12. DOCUMENTED ON EO 4757A407.SDR UIEA200700474Pushrod · brokenAIRCRAFT EXPERIENCED HARD LANDING. PERFORMED HARD LANDING PHASE I INSPECTION. NOTED DEFECTS LISTED ON FOLLOWING LOG PAGES PER AMM 5-51-05, FOUND LEFT INBOARD FLAP NR 4 PUSH ROD BROKEN. REPLACED AND ADJUST PUSH ROD ASSY. ACCOMPLISHED PARTS OF PHASE II INSPESDR UIEA200700471Skin · delaminatedLEFT WING INBOARD T/E FOREFLAP HAS SIGNS OF DELAMINATION 15" FROM OUTBOARD EDGE. PERFORMED WING TRAILING EDGE REPAIR AS PER SRM 51-40-09 AND 51-40-06 AND XEO 57-110707.SDR UIEA200700464Drive System · brokenNR 3 REVERSER DID NOT DEPLOY DURING LANDING. NO AMBER THRUST REVERSER LIGHT. REVERSER WOULD NOT GO PAST INTERLOCK. INSPECTED AND FOUND BROKEN DRIVE CABLE ON THE OUTBOARD SIDE OF NR 3 ENGINE. ITEM TRANSFERRED TO DMI M07-241 PER MEL 78-1-5 CAT C LOCKED OUT PSDR UIEA200700463Skin · crackedNR 4 PYLON LT SKIN WAS FOUND A CRACK AT THE 483 AL ACCESS PANEL CUTOUT LOWER AFT CORNER. DEFECTIVE CRACK AREA INTERIM REPAIRED AS PER BOEING MESSAGE NR 1-656345659-3 AND ATLAS XEO NR 54-102307.
SDR UIEA200700457Seat Track · damagedSEAT TRACK AT MAIN DECK STA 1880L AND LBL 99 HAS WORN AND TORN CROWN LUGS. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 53-10-05 FIG 1A, SHEETS 1 THRU 4. ALSO, REFERENCE ATLAS AIR EO NR 4753B098.SDR UIEA200700456Panel · delaminatedRT WING UPPER SURFACE L/E FIXED PANEL AT WING STA 526.0 HAS A 3.0 INCH BY 4.0 INCH AREA OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A400.SDR UIEA200700455Skin · delaminatedRT WING NR 11 SPOILER TRAILING EDGE HAS A 1.0 INCH BY 2.0 INCH AREA OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-06 FIG 3 AND 4, SHEET 1 AND SRM 51-40-20. ALSO, REFERENCE ATLAS EO NR 4757A399.SDR UIEA200700421Frame · crackedNR 3 ENGINE RT CORE COWL FORWARD FRAME HAS A HOLE AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 4 AND SRM 51-40-03 FIG 1. ALSO, REFERENCE ATLAS AIR XEO NR 71-092807.SDR UIEA200700420Door · debondedRT WING GEAR INBOARD STRUT DOOR AFT EDGE, CENTER AREA HAS A 10.0 INCH LONG BY 4.0 INCH WIDE OF MATERIAL SEPARATING AT BS 1343.3. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 12, SHEETS 1 THRU 4 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EOSDR UIEA200700418Panel · delaminatedLT WING UPPER L/E FIXED PANEL AT WS 490.00 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393.SDR UIEA200700419Fairing · delaminatedRT WING NR 5 FLAP TRACK FORWARD FIXED FAIRING AT WBL 235.20, OUTBOARD SIDE HAS AN AREA 12.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION AND CRACK. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 6, SHEETS 1 THRU 4 AND SRM 51-40-12. ALSO, REFERESDR UIEA200700417Panel · delaminatedRT WING UPPER L/E FIXED PANEL AT WS 317.32 HAS AN AREA OF 2.0 INCH LONG BY 2.0 INCH WIDE OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1 THRU 5 AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR EO NR 4757A393.SDR UIEA200700385Skin · damagedRT OUTBOARD AILERON HAS A 5.250 INCH SCRATCH/GROOVE AT UPPER LEADING EDGE. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-02 FIG 1, SHEETS 1, 2 AND 3. TOTAL WEIGHT OF MATERIAL USED FOR THIS REPAIR IS 0.15 LBS AND DOES NOT REQUIRE BALANCE ADJUSTMSDR UIEA200700384Panel · delaminatedLT WING, UPPER LEADING EDGE FIXED PANEL AT WING STATION 766 HAS AN AREA OF 12.0 INCH BY 12.0 INCH OF DELAMINATION. PERMANENT REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18, SHEETS 1, 3 AND 5, AND SRM 51-40-12. ALSO, REFERENCE ATLAS AIR XEO NR 57SDR UIEA200700354Link · brokenON LANDING INTO DOV, HEAVY SPARKS REPORTED DOWN RUNWAY. MX FOUND RIGHT BODY GEAR, FWD BRAKE TORSION LINK AT NR 10 BRAKE GAVE WAY, CAUSING DAMAGE (GROOVE) TO RUNWAY. BOTH THE NR 10 AND NR 12 BRAKES WERE REMOVED PER DDPG 32-5, AND THE AIRCRAFT WAS MADE READY FSDR UIEA200700352Web · crackedOLEO 1450 FWD CRACKED JUST FWD OF NR 25 V/C FLAP UPPER FITTING. CARRY OUT REPAIR AS PER SRM 51-40-03.SDR UIEA200700349Nozzle · dentedNR 1 ENGINE EXHAUST NOZZLE DENTED AT 0300. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMITS AMM 78-11-01 PAGE 601.SDR UIEA200700347Web · crackedUPON L/E CAP REMOVAL OLES 1522, NR 26VC FLAP UPPER STOP FTG FWD WEB DOUBLER FOUND CRACKED. DOUBLER REPLACED IAW SRM 51-10-01.SDR UIEA200700346Frame · crackedR1 MED LOWER AFT CORNER FRAME CRACKED AT STA 490 RT S-25R TO S-26R AREA. C/OUT AS PER SRM 52-10-02 FIG 10.SDR UIEA200700345Door Frame · crackedM/D R4 MED FWD UPPER CORNER FRAME CRACKED AT STA 1670 S-16R TO S-17R AREA. CARRY OUT REPAIR AS PER SRM 52-10-02, FIG 10.SDR UIEA200700344Door Frame · crackedR3 DOOR FWD UPPER CORNER FRAME FOUND CRACKED. C/OUT AS PER SRM 52-10-02, FIG 10.SDR UIEA200700343Web · corrodedBULK CARGO BS 1980-2030 DOOR LOWER SILL FLOOR WEB, CORRODED. CORROSION REMOVED AND REPROTECTED AS PER SRM 51-10-01 AND SRM 51-10-02 WITHIN ALLOWABLE LIMIT AS PER SRM 53-10-01.SDR UIEA200700342Panel · contaminatedRT WING I/B T/E PANEL FOUND WATER. REPLACE RHW I/B T/E PANEL AS PER SRM 51-10-01 AND SRM 51-30-02.SDR UIEA200700348Frame · crackedAFT REMOVAL OF L/E NOSE CAP FOUND THAT "D" SECTION CRACKED. CARRY OUT REPAIR AS PER SRM 57-20-03.SDR UIEA200700350Nozzle · dentedNR 3 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR UIEA200700351Nozzle · dentedNR 4 ENGINE EXHAUST NOZZLE EXTERIOR SKIN DENTED AT 0700 TO 0900. NDT CHECKED NIL CRACK DENT AREA WITHIN LIMIT AMM 78-11-01 PAGE 601.SDR UIEA200700336Access Panel · elongatedAIR COND, BAY ACCESS PANEL 192ER EXT SURFACE FOUND SKIN ELONGATION. AIR COND BAY ACCESS PANEL 192ER REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700329Frame · crackedBS 800 S17 LT ONE FASTENER HOLE FOUND CRACK ON FWD INNER CHORD ANGLE. REPLACEMENT PER BOEING CONTROL NO PO24708.SDR UIEA200700337Access Panel · delaminatedAIR COND, BAY ACCESS PANEL 192HR EXT SURFACE FOUND SKIN DELAMINATION. AIR COND BAY ACCESS PANEL 192HR REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700335Access Panel · erodedAIR COND, BAY ACCESS PANEL 191HL EXT SURFACE FOUND ERODED. AIR COND BAY ACCESS PANEL 191HL REPAIRED WITH PRE-PRED FABRIC AS PER MESSAGE NR 1-497468248-2.SDR UIEA200700332Floorbeam · crackedFLOOR STRUCTURE BEAM WEB CRACKED. C/OUT AS PER BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700338Torque Link · chafedNLG LOWER TORSION LINK FOUND CHAFING. BLEND OUT THE CHAFING AREA WITH MIN 20-1 BLEND-RATIO.SDR UIEA200700331Skin · dentedHORIZONTAL STAB RT I/B ELEVATOR L/E UPPER SKIN DENTED. REPAIRED IAW BOEING MESSAGE SR 1-514407012.SDR UIEA200700333Floorbeam · crackedFLOOR STRUCTURE BEAM WEB CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700339Skin · dentedFX EXTERIOR SKIN DENT AS MARKED APPR, 1" SQ IN AT BS 780 S47-R. REINSTALLED A REPAIRED DOUBLER AS PER SRM 53-30-03 DETAILS AS PER SWS SHOWN.SDR UIEA200700334Pan · crackedCOCKPIT 2ND OBSERVER SEAT PAN CRACKED. REPAIRED IAW BOEING MESSAGE NR 1-497681686-1.SDR UIEA200700340Hinge Fitting · crackedBS 2598 H/S RT RBL 40" REAR SPAR UPPER I/B OF HINGE FITTING OPEN HOLE. OVERSIZE TO 0.403", USED BACB30 US6K21Y BOLT. CARRIED OUT NDT TEST OF THE OPEN OVERSIZE HOLE FOUND SATISFACTORY.SDR UIEA200700330Panel · contaminatedLT WING T/E I/B PANEL FOUND WATER. REPLACE LHW T/E I/B FIXED PAL AS PER SRM 51-10-01 AND SRM 51-30-02, AND PANEL REPAIR IAW BOEING MESSAGE 31-516595696-1 TO 1-516595696-4.SDR UIEA200700358Drain Valve · corrodedDURING SCHEDULED TIME REMOVAL OF THE TOILET SERVICE DRAIN VALVE FOUND HEAVY CORROSION ON THE BRACKET ABOVE THE PAN AND SERVICE DOOR INSTALLATION. REMOVED ALL BRACKET THAT HAD CORROSION DAMAGE. REPAIRED INTERNAL STRAPS PER SRM 53-30-03. REPAIRED INTERNAL SECSDR UIEA200700357Flap Track · crackedNR 1 MOVABLE FLAP TRACK FAIRING HAS SMALL CRACK LOWER SURFACE. REPAIRED PER SRM 51-40-09 AND 51-40-12.
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