Boeing 747-2D3B
Service difficulty reports · 182
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 = '7472D3B' 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 = '7472D3B' 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 UIEA200800335Fairing · damagedLT WING NR 1 CANOE FAIRING AT WBL 743.828 WAS DAMAGE ON CARGO LOADING. CANOE WAS REMOVED PER ATLAS DMI M08-227. AREAS OF CANOE AT FAIRING STA 147.766 LOWER SIDE, STA 124.5 & 135.5 INSIDE OF CANOE, STA 152.766, 159.766, 167.766 ON OUTBOARD SIDE, SMALL HOLES 3SDR UIEA2008002272Skin · chafedLEFT WING INBOARD FLAP, AFT FLAP S/N 000204 UPPER SKIN HAS 4 EACH AREAS OF CHAFING CAUSED BY LONG BOLTS ON MID-FLAP. AREAS ARE WBL 248.0, 297.0, 339.0 AND 425.0. CHAFE IS .500 INCH IN DIAMETER. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG SDR UIEA200800270Wire Harness · damagedNR 2 ENG SHUT DOWN IN FLIGHT DUE TO HIGH EGT INDICATION - EGT WAS READING 1047C FOR 70 SECONDS. FOUND EGT HARNESS DAMAGED. REMOVED AND REPLACED HARNESS AND OPS CHECKED OK PER MM 77-21-01. (S)SDR UIEA200800210Mec · failedAT FL 320 ON DESCENT, NR 1 ENGINE N1, N2 AND EGT ROLLED BACK WITH NO THROTTLE RESPONSE. RESTART NO HELP. SHUT DOWN FOR LANDING. REPLACED NR 1 MEC PER AMM 73-21-01 ACCOMPLISHED VSV RIG PER 75-30-00 CHECKED OK. LEAK CHECKED OK, ACCOMPLISHED ENGINE RUN TEST PESDR UIEA200800183Mec · failedINFLIGHT ENGINE SHUTDOWN. AT TOD, DURING ENGINE THROTTLE BACK NR 1 ENGINE ROLLED BACK DOWN TO 30 PERCENT N1 WITH NO THROTTLE RESPONSE. CREW SHUT DOWN ENGINE AND PERFORMED INFLIGHT RE-START. AFTER SUCCESSFUL RE-START THERE WAS STILL NO THROTTLE RESPONSE ABOVSDR UIEA200800182Fan Blade · bird ingestionBIRD STRIKE AT TAKEOFF TO FUSELAGE AND ENGINE NR 1 FAN BLADES. ACCOMPLISHED BIRD STRIKE INSPECTION FOR FUSELAGE AND NR 1 ENGINE AND OVERWEIGHT LANDING CHECKS AS PER IAW 05-51-14, 05-51-39 AND 72-00-00 FOR FAN BLADES CHANGED AND ENGINE INSPECTION. REPLACED NRSDR UIEA200800161Skin · crackedRT I/B ELEVATOR HAS A 2.0 INCH CRACK AT TRAILING EDGE OF ELEVATOR STA 154.0, CAUSED BY GROUND EQUIPMENT. ACCOMPLISHED INTERIM REPAIR AS PER B747-200 SRM 51-40-09 FIG 8, SHEETS 1 AND 2, AND SRM 51-40-15. REFERENCE EO 4755A062, TO ACCOMPLISH REPEAT INSPECTIONSSDR UIEA200800151Panel · damagedLT WING UPPER SURFACE NR 5 SPOILER CENTER HINGE GAP PANEL DAMAGED, ALSO, INBOARD, OUTBOARD AND CENTER HINGE CUT-OUT AND FORWARD PANEL OF CENTER HINGE DAMAGED, SKIN PULLED AND CRACKED. PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG. 2, SHEETS SDR UIEA200800150Panel · delaminatedRT WING UPPER FIXED TRAILING EDGE PANEL, OUTBOARD OF NR 8 SPOILER HAS AN AREA OF 5.0 INCH BY 2.0 INCH OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 2, SHEETS 1, 2 AND 5. PREPREG LAYUP 250 DEGREES F CURE PER SRM 51-40-12. RESDR UIEA200800149Skin · crackedMAIN ENTRY DOOR L-1 EXTERIOR SKIN, UPPER HINGE CUT-OUT PREVIOUS DOUBLER REPAIR, LOWER RADIUS CORNER IS CRACKED. VERIFIED CRACK WITH HFEC AS PER B747-200 NDT MANUAL PART 6, 51-00-00 FIG 23. STOPPED DRILLED CRACK AND ACCOMPLISHED PERMANENT REPAIRS AS PER B747 SDR UIEA200800110Smoke Detector · malfunctionedDIVERSION TO YJT DUE TO "MAIN DECK CARGO SMOKE DET ZONE 4 LIGHT ILLUMINATED WITH CARGO AND MASTER FIRE ANNUNCIATOR LIGHTS ILLUMINATED. AFTER LANDING RETESTED OKAY (NORMAL). AIRCRAFT ALSO SUSTAINED AN OVERWEIGHT LANDING. SWAPPED ZONE 3 AND 4 SMOKE DETECTORS SDR UIEA200800099Lead · chafedREJECTED TAKEOFF, NR 3 EGT WENT TO OFF SCALE HIGH WITH RED BALL. NR 3 ENGINE EGT SHOWED 1074 DEGREES FOR 1 SEC. FOUND THERMOCOUPLE LEAD WAS DEFECTIVE WHILE PERFORMING FIM PROCEDURE 71-03-00 AS NOTED IN AMM 72-00-00 PAGE 680G. REPLACED LEAD PER AMM 77-21-02 SDR UIEA200800064Fitting · crackedAFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. AFTER DISASSEMBLY (REFERENCE SDR UIEA200800063) FOUND FORWARD POSITION ROTARY LIFT ACTUATOR FRAME REINFORCEMENT FITTING WITH ELONGATED ACTUATOR MOUNT BOLT HOLES. REPLACED FITTING 65B38170-3 PER STANDARDSDR UIEA200800063Fitting · crackedAFT CARGO DOOR FAILED TO CLOSE DURING NORMAL OPERATION. FOUND AFT POSITION ROTARY LIFT ACTUATOR FRAME REINFORCEMENT FITTING CRACKED. REPLACED FITTING 65B38174-3 PER STANDARD PRACTICES IAW SRM 51-30-02 AND LIFT ACTUATOR 60B00305-1 PER AMM 52-34-03. OPS CHECKSDR UIEA200800021Skin · crackedLT WING LEADING EDGE LOWER SURFACE, OUTBOARD FUELING DOOR FRAME CUT-OUT HAS A COMPOSITE CRACK AT OUTBOARD SIDE, FORWARD EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-40-09 FIG 18 SHEETS 3 AND 5 AND SRM 51-40-12, PREPREG 250 DEGREES F CURE. ALSO,SDR UIEA200800020Structure · delaminatedLT MAIN LANDING GEAR OUTBOARD STRUT DOOR HAS AN 18.0 INCH LONG SECTION AT LEADING EDGE OF MATERIAL SEPARATING. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 12 SHEET 1 AND 4 AND SRM 51-40-12, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4752A129.SDR UIEA200800019Panel · delaminatedRT WING NR 10 SPOILER PANEL HAS A 5.0 INCH BY 5.0 INCH AREA OF DELAMINATION AT UPPER SIDE, OUTBOARD, TRAILING EDGE. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-06 FIG. 1 AND 4 AND SRM 51-40-20, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4757A413.SDR UIEA200800018Skin Panel · delaminatedRT WING LOWER FIXED LEADING EDGE HAS A 12.0 INCH LONG BY 10.0 INCH WIDE AREA OF DELAMINATION. PERMANENT REPAIR ACCOMPLISHED AS PER SRM 51-40-09 FIG 18, SHEET 1, 2, AND 5, PREPREG 250 DEGREES F CURE. ALSO REFERENCE EO NR 4757A412.SDR UIEA200800017Smoke Detector · dirtyAIRCRAFT DIVERTED TO SNN DUE TO NR 4 CARGO LIGHT SMOKE DETECTOR LIGHT CAME ON IN CRUISE. NR 4 A/B SMOKE DETECTORS CLEANED AND OPS CHECKED IAW 26-14-00, OPS CHECKED OK.SDR UIEA200700472Panel · delaminatedRT WING LEADING EDGE, INBOARD OF LANDING LIGHTS, INTERIOR AREA OF LEADING EDGE, COMPOSITE SKIN IS DELAMINATED. AREA IS 64.0 INCH BY 20.0 INCH. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 57-30-02, FIG 10 AND SRM 51-40-09, FIG 18, REFERENCE ATLAS AIR SDR UIEA200700467Panel · delaminatedLT WING UPPER L/E FIXED PANEL BETWEEN AISLES 170.0 TO AISLES 630.72 HAS AN AREA DELAMINATION, AREA IS 58.0 INCH LONG BY 50.0 INCH WIDE. INTERIM REPAIR WAS ACCOMPLISHED AS PER B747-200 SRM 51-40-16 AND ATLAS AIR EO NR 4757A402 PART 4. PER FAA FORM 8110-3 REQUSDR UIEA200700465Panel · delaminatedUPPER SURFACE OF LEFT WING INBOARD NR 2 ENGINE FIBERGLASS HAS HOLE AND DENT. REPAIRED PER XEO 57-102607 TRANS TO NON MEL N07-126. REINSPECTED IN ORD AND ACCOMPLISHED XEO 57-102607 PART 3 IAW SRM 51-40-16. REPAIRED AND TO BE INSPECTED EVERY 10 FLIGHT CYCLES SDR UIEA200700432Sensor · failedAIR TURN BACK, AT ROTATION STICK SHAKER CAME ON AND STAYED ON UNTIL LANDING. VR SPEED WAS 129 KNOTS. REMOVED AND REPLACED LEFT AOA SENSOR AND STALL WARNING COMPUTER IAW 27-30-01, OPS CHECKED NORMAL IAW 27-30-00.
SDR UIEA200700427Skin · tornLT INBOARD ELEVATOR, TRAILING EDGE COMPOSITE SKIN TIP AREA HAD GROUND DAMAGE. PERMANENT REPAIR ACCOMPLISHED AS PER B747 SRM 51-40-09, FIG 1A, SHEET 1 AND FIG 8, SHEETS 1 AND 2. REFERENCE ATLAS AIR EO NR 4755A049.SDR UIEA200700425Skin · damagedLOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2613 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCE ATLAS XEOSDR UIEA200700422Skin · damagedFUSELAGE TAIL CONE LOWER AREA FROM FS 2742 TO 2792 SKIN AND FRAMES SCRAPED AND DENTED DUE TO TAIL DRAG. REMOVE AND REPLACED LOWER SECTION OF CONE FROM STA 2742 TO 2792, ASSY P/N 65B02785-1 AND PERMANENT REPAIRS ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3,SDR UIEA200700426Skin · damagedLOWER AFT FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER AT FS 2594 TO 2604.0 PREVIOUS REPAIR DAMAGED WITH HEAVY ABRASION/SCRAPING DUE TO TAIL DRAG. REMOVED AND REPLACED DOUBLER/TRIPLER REPAIR AS PER 747-200 SRM 51-30-02 AND 51-30-03 FIG 1 SHEETS 1 THRU 6. REFERENCESDR UIEA200700424Frame · damagedAFT LOWER FUSELAGE AT FS 2658 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 53-10-04 FIG 75 SHEETS 1 THRU 15. REFERENCE ATLAS AIR XEO 53-093007.SDR UIEA200700423Frame · damagedAFT LOWER FUSELAGE AT FS 2638 FRAME LOWER SURFACE SCRAPED DUE TO TAIL DRAG. PERMANENT REPAIR ACCOMPLISHED AS PER B747-200 SRM 51-20-01 FIG 3, AND SRM 51-30-02. ALSO REFERENCE ATLAS AIR XEO NR 53-093007-1.SDR UIEA200700353Seal · damagedAIR TURN BACK DUE TO NOSE GEAR DOOR OPEN INDICATION AFTER GEAR RETRACTION. FLIGHT CREW ADVISED, ACTUAL DOOR OPEN FAULT AND NOT INDICATION. AFTER ARRIVAL, MX INSPECTED AND FOUND FWD DOOR SEAL PARTIALLY OUT OF RETAINER. UPON MORE DETAILED INSPECTION AND MULTISDR UIEA200700250Pump · leakingNR 2 HYD LEAK STOPPED WITH 1.8 GALLONS REMAINING. EDP TO SUPPLY OFF. REMOVED AND REPLACED HYD PUMP AND CASE DRAIN RETURN FILTER, OPS AND LEAK CHECKED OKAY.SDR UIEA200700233Skin · dentedNR 3 ENGINE RT THRUST REVERSER EXTERIOR SKIN LOWER AREA AT 5 O'CLOCK POSITION HAS 3 EACH DENTS. PERMANENT REPAIR WAS ACCOMPLISHED AS PER GE CF6-50 ENGINE MANUAL 78-32-01 REPAIR 3, FIG 1. ALSO, REFERENCE ATLAS AIR EO NR 4778A098.SDR UIEA200700145Wire · chafedAFTER T/O FROM AMS, WHERE NR 3 ENGINE B LOOP WAS DEFERRED AS INOP. NR 3 ENGINE FIRE BELL AND LIGHT ILLUMINATED, NR 3 ENGINE A LOOP WAS ERRATIC AND WAS AT 10 ON THE SCALE FLUCTUATING. ENGINE SHUT DOWN AS PER ATLAS PROCEDURE USING FIRE CHECK LIST FIRE SWITCH ASDR UIEA200700130Strap · crackedCRACKS FOUND ON BS 800 LT STRAP AND INNER CHORD AT NR 2 MAIN ENTRY DOOR. REPAIRED ACCOMPLISHED IAW SR ID NR 1-289052431 AND FAA FORM 8100-9.SDR UIEA200700125Skin · corrodedM/DECK RT NR 3 MED CUTOUT AFT UPPER CORNER SKIN STA1319, STR 17R-18R FOUND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-289657194-1, 747 SRM 53-30-03 FIG 44 AND FAA FORM 8100-9.SDR UIEA200700128Doubler · separatedNR 3 PYLON FWD FIXED FAIRING LT EXTERIOR SURFACE AFT CORNER SKIN DOUBLER SEPARATED. FAIRING REPLACED BUT NUMEROUS FASTENERS HOLES FOUND MISALIGNED. TIME LIMIT REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-292185930-1 THRU -14, DWG 65B90813-52 AND FAA FORMSDR UIEA200700124Bulkhead · corrodedBS 1250, L WLG W/W CANTED PRESSURE BULKHEAD, NR 2 PACK COOLING DUCT CUTOUT FOUND CORROSION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-289645346-1 THRU -5 AND FAA FORM 8100-9.SDR UIEA200700129Skin · corrodedFOUND M/DECK STA1241 FRAME AND SKIN SPLICE AREA HAS HOLE, CRACKED AND CORRODED. REPAIRED ACCOMPLISHED AS PER BOEING MESSAGE NR 1-29020776-1 AND -6 AND FAA FORM 8100-9.SDR UIEA200700127Stringer · corrodedFWD CARGO COMPARTMENT STA 978, STR 47L FOUND CORRODED. FWD CARGO COMPARTMENT STA978, STR47L REPLACED AS PER SRM 51-10-01.SDR UIEA200700126Intercostal · crackedUPPER DECK FLOOR SUPPORT INTERCOSTAL CRACKED AT BS 420, LBL 50. U/DECK FLOOR SUPPORT INTERCOSTAL AT BS420, LBL 50 REPLACED AS PER SRM 51-30-02.SDR UIEA200700107Stringer · crackedM/DECK ZONE "C" LT SIDEWALL STRUCTURE STA 905, STR-10L FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER SRM 53-10-03, FIG 4.SDR UIEA200700106Keelbeam · bulgedFOUND KEEL BEAM BOTH SIDES WEB BULGE FOUND AT BS 1450. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286690602-1 THRU -10.SDR UIEA200700101Shear Tie · crackedRT STA 840 FWD CHANNEL TENSION TIE AT 12 O'CLOCK FOUND CRACKED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID 1-288425027-1 AND -6, 1-289012875-1, SB747-53-2502 AND FAA FORM 8100-9.SDR UIEA200700100Skin · crackedNR 3 ENGINE LT CORE COWL SKIN BOND DOUBLER CRACKED AT AIR EXHAUST DUCT AFT LOWER PORTION. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-286833874-1 THRU -6, DWG 65B94280 AND FAA FORM 8100-9.SDR UIEA200700099Skin · puncturedNR 20 VC FLAP FOLDING NOSE I/B END SKIN PUNCHED. REPAIRED ACCOMPLISHED AS PER BOEING SR ID NR 1-290202458-1 THRU -3 AND FAA FORM 8100-9.SDR UIEA200700098Stringer · crackedM/DECK LT SIDE STA 875, STR9L FOUND CRACKED. STRINGER REPAIRED AS PER SRM 53-10-03, FIG.4SDR UIEA200700097Crease Beam · crackedM/DECK RTH SIDE STA 940, S-8R CREASE BEAM WEB FOUND CRACKED. CREASE BEAM WEB REPLACED AS PER SRM 51-10-01 AND 51-30-02.SDR UIEA200700096Stringer · corrodedFOUND FWD CARGO COMPT STA 980, STR 43R IS CORRODED. STRINGER REPAIRED AS PER SRM 53-10-03 FIG 1.SDR UIEA200700095Crease Beam · crackedFOUND M/DECK STA960, S-7R CREASE BEAM SUPPORT ANGLE FOUND CRACKED. CREASE BEAM SUPPORT WEB REPLACED AS PER SRM 51-10-01.SDR UIEA200700094Stringer · crackedM/DECK STA 895 STR 7R FOUND CRACKED. STRINGER REPAIRED ACCOMPLISHED AS PER SRM 53-10-03 FIG 4.
Back to Boeing 747-2D3B