Boeing 747-446
Service difficulty reports · 932
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 = '747446' 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 = '747446' 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 KCSA201801031002Reveal · crackedSTA 2231 R/H SIDE REVEAL HAS 4 INCH CRACK BETWEEN STR 21R & 22R.SDR KCSA201801031001Bulkhead · crackedBS2598 LT BULKHEAD LWR INNER CHORD AND WEB HAS CRACK INDICATIONS AT 2 EA FASTENER HOLES. CRACK INDICATION IN CHORD AND CRACK INDICATION IN WEB LBL 40 WL 265 APPROX. .100" IN LENGTH.SDR UIEA2018022500279Landing Gear · fodFOUND FIRE EXTINGUISHER WEDGED IN THE RIGHT INBOARD LANDING GEAR TRUCK BETWEEN THE NR 9 AND 10 MAIN LANDING TIRES. THIS CAUSED THE EICAS WARNING CONFIG STAB ON TAKE OFF. THE FIRE EXTINGUISHER RUBBED THE INBOARD SIDE LINER OF EACH NR 9 AND 10 MLG TIRES. REMSDR UIEA2017122602437Light · missingSEAT 34C EMERGENCY LIGHT MISSING.SDR UIEA2017122002420Panel · out of adjustFIXED CLOSE OUT PANEL ON UPPER TRAILING EDGE OF THE LEFT WING OUTBOARD OF THE NR 5 SPOILER, BECAME SEPERATED DURING FLIGHT. NO DAMAGE TO PANEL NOTED. FOUND TO BE OUT OF ADJUSTMENT. ADJUSTED THE PANEL.SDR UIEA2017120802376Light · looseU/D FLOOR MOUNT EMERGENCY LIGHT AT L & R DOOR PADS LOOSE(<P>LOCATED AND RE SECURED LOOSE PADS AT U/D FLOOR MOUNTED EMERGENCY LIGHT AT EMERGENCY DOOR. PER AMM 20-30-01-802-001</P>)SDR UIEA2017120702372Pad · looseU/D FLOOR MOUNT EMERGENCY LIGHT AT L & R DOOR PADS LOOSE.(<P>LOCATED AND RE SECURED LOOSE PADS AT U/D FLOOR MOUNTED EMERGENCY LIGHT AT EMERGENCY DOOR. PER AMM 20-30-01-802-001.</P>)SDR UIEA2017112702301Floorbeam · corrodedCORROSION ON THE FLOORBEAM UPPER TEE AT BS 460, BETWEEN LBL 39 TO LBL 51. BLENDED AND REPAIRED THE AREA IAW EI T2017A53M-2357, REV 2.SDR UIEA2017112702304Structure · crackedCRACK ON RT WHEEL WELL HINGE BOX AT BS 1480. ACCOMPLISHED EI T2017A53M-2275, REV 1.SDR UIEA2017112702305Rivet · corrodedRT HORIZONTAL STAB FIXED T/E RBL 372 - RBL 392 RIVET CORRODED. REMOVED THE RIVET IAW SRM 51-40-02, REV.1. INSTALLED A NEW RIVET IAW DWG 65B03710 SH2, REV J, AND SRM 51-40-02, REV 1. CHECKED NORMAL.SDR UIEA2017112702306Skin · corrodedSKIN CORRODED AT BS 2090, BETWEEN STRINGERS 35L AND 36L. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-1, TABLE I, FIGURE 101, DETAIL II, REV 101. PERFORMED PROTECTIVE TREATMENT ON REWORKED AREA IAW SRM 51-20-01 REV 101.SDR UIEA2017112702307Skin · corrodedBULGE DAMAGE ON THE LT WING LEADING EDGE LOWER SKIN NEAR ILES 500. REPAIRED THE AREA IAW EI T2017A57M-2423, REV 3. CHECKED NORMAL.SDR UIEA2017112702308Skin · corrodedSKIN CORRODED, BS 2090 BETWEEN STRINGERS 35R AND 36R. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 53-00-01-1A-1, TABLE I, FIGURE 101, DETAIL II, REV 101.SDR UIEA2017112802316Stiffener · corrodedSTIFFENER CORRODED, STAB T/E INNER UPPER SURFACE, HSS 118.9 . REWORKED THE FITTING AREA AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 55-20-09-1A-1, DETAIL III, REV 101. OPS CHECKED GOOD.SDR UIEA2017112802317Bulkhead · corrodedMLG WW. FWD BULKHEAD, BS 1253, LBL91 CORRODED. CORROSION REMOVED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2, DETAIL V, REV 101. PERFORMED SURFACE NDT INSPECTION AND BONDING TEST AT REWORKED AREA. CHECKED GOOD.SDR UIEA2017112802318Bulkhead Web · corrodedSKIN BS 1241, RBL 93, WW BULKHEAD AFT FACE CORRODED. CORROSION REMOVED AND FOUND WITHIN ALLOWABLE LIMITS IAW SRM 57-10-10-1A-2, DETAIL V, REV 101, PERFORMED SURFACE NDT INSPECTION AND BONDING TEST AT REWORKED AREA IAW JOB CARD. REWORK AREA IAW SRM 51-20-01 RSDR UIEA2017112802319Skin · corrodedRT WING INSPAR UPPER SKIN UPPER SURFACE ACCESS REAR SPAR CORRODED, WS 528.2. REMOVED CORROSION IAW SRM 51-10-02 REV101. WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1, FIG 101, DETAIL II, REV 101.SDR UIEA2017112802320Angle · corrodedDUCT ASSY AT AIR CONDITIONING NR 2 RAM AIR INLET DUCT AREA CORRODED. REMOVED AND REPLACED THE CORRODED ANGLE IAW SRM 51-40-02, REV 101, AND DWG 65809716, SHEET 3, REV F. OPS CHECKED NORMAL.SDR UIEA2017112802321Duct · corrodedDUCT ASSY AT AIR CONDITIONING NT 3 RAM AIR INLET DUCT AREA CORRODED. REMOVED AND REPLACED THE DAMAGED PARTS IAW SRM 51-40-02-0G-0, REV 101, AND DWG NO 65B09715, SHEET 3, REV G. OPS CHECKED NORMAL.SDR UIEA2017112802322Strap · corrodedTHE UPPER STRAP OF THE LT WING LEADING EDGE NEAR OLES 1525 CORRODED. REPAIRED THE AREA IAW EI T2017A57M-2362 REV 1. OPS CHECK NORMAL</P>)SDR UIEA2017112802323Skin · corrodedLEFT WING INSPAR UPPER SKIN UPPER SURFACE CORRODED. WBL 183 - WBL 210 FRONT SPAR - S27. REMOVED CORROSION IAW SRM 51-10-02, REV 101. WITHIN ALLOWABLE LIMITS IAW SRM 57-20-01-1A-1, FIG 1-1, DETAIL II, REV101.SDR UIEA2017112802324Light · inoperativeFWD CABIN EMERGENCY LIGHT CRACKED AT THE LAVATORY, REPLACED CABIN EMERGENCY LIGHT IAW SWPM 20-30-12, REV 66, CMM 25-33-41, 25-42-69, REV 2. AND CONDITION CHECK NORMAL. IAW AMM 33-51-12-962-162 REV90 STEP 6.C PERFORMED LAMP TEST AND THE RESULT WAS SATISFACTORSDR UIEA2017112802325Battery Pack · inoperativeFOUND MANY MAIN DECK AND UPPER DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED POWER SUPPLY BATTERIES IAW AMM 33-51-06-000-801 AND 33-51-06-400-801, REV 91. REPLACED SLIDE LIGHT BATTERIES IAW AMM 33-51-06-400-801, REV 91. PERFORMED EMERGENCY LIGHT OPS TEST AND SDR UIEA2017112802327Doubler · corrodedSKIN DOUBLER AT FUSELAGE SEX 42 POTABLE WATER SERVICE PANEL 192FFR CORRODED. INTERNAL SKIN DOUBLER SURFACE AREA. REPLACED THE DOUBLER IAW SRM 51-40-02-0G-0, REV 101, DWG 65B04118, S42, REV P AND S44 REV H.SDR KCSA201710161070Doubler · corrodedPOTABLE WATER SERVICE DOUBLER HAS EVIDENCE OF CORROSION.SDR KCSA201710041064Power Supply · no testEMERGENCY LIGHT POWER SUPPLY M5932 WILL NOT TEST.SDR UIEA2017100101911Vent · crackedDURING POST FLIGHT INSPECTION , FOUND A .750 INCH CRACK AT THE RT BS 2090 WASTE SYSTEM OVERBOARD VENT. REPAIRED IAW EO 4453B398.SDR KCSA201709081060Skin · crackedR5 MAIN DECK DOOR FWD SURROUND SKIN STRUCTURE BETWEEN STR 21 & 22 HAS POSSIBLE CRACKSDR KCSA201709081059Skin · crackedL5 MAIN DECK DOOR FWD SURROUND SKIN STRUCTURE BETWEEN STRINGERS 21 & 22 HAS A POSSIBLE CRACK.SDR KCSA201708301057Doubler · corrodedPOTABLE WATER SERVICE DOUBLER HAS EVIDENCE OF CORROSION.SDR UIEA2017083001583Light · missingFLOOR EMERGENCY LIGHT MISSING ON UPPER DECK. REMOVED AND REPLACED THE LIGHT ASSY IAW 33-51-12, OPS CHECKED GOOD.SDR UIEA2017082601549Sensor · out of adjustREJECTED TAKE OFF AT LOW SPEED DUE TO NO N1 ADVANCE ON NR 3 ENGINE. ADJUSTED THE FEEDBACK SENSOR FOR THE NR 3 ENGINE THRUST REVERSER, OPS CHECKED NORMAL IAW AMM 78-34-10-404.SDR KCSA2017082011Bottle · low pressureLEFT FORWARD SLIDE BOTTLE PRESSURE LOW. REMOVED AND REPLACED THE SLIDE BOTTLE IAW 25-68-02.SDR UIEA2017081101466Fuel Filter · malfunctionedAN IN-FLIGHT DIVERSION HAPPENED DUE TO BOTH AN ENGINE 3 FUEL FILTER EICAS STATUS MESSAGE, AND AN ENGINE 4 FUEL FILTER EICAS STATUS MESSAGE. THE FUEL FILTER ELEMENTS WERE REPLACED.SDR UIEA2017060500941Panel · missingPANEL 461AL ON THE NR 2 PYLON OTBD DISCOVERED MISSING DURING WALK AROUND INSPECTION. INSTALLED A TEMPORARY PANEL IAW EO 4454A089.SDR UIEA2017053000878Warning Message · illuminatedUPPER DECK DOOR LEAKK MESSAGE AFTER DEPARTURE. RETURNED TO DEPARTURE. VERIFIED LEFT DOOR WAS THE ISSUE.SDR UIEA2017030200257Battery Pack · no testL3 DOOR EMERGENCY LIGHT FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 33-51-04, NO DEFECTS NOTED.SDR UIEA2017030200258Battery Pack · no testR1 DOOR EMERGENCY LIGHT FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 33-51-04, NO DEFECT NOTED.SDR UIEA2017030200259Battery Pack · no testEMERGENCY EXIT SIGN AFT OF R3 DOOR FAILED A 15 MINUTE TEST. REPLACED THE BATTERY PACK AND PERFORMED A POWER SUPPLY TEST IAW AMM 31-51-04. NO DEFECTS NOTED.SDR UIEA2017040600524Fitting · corrodedON ACCESSING FOR FRONT SPAR CORROSION, FOUND FITTING ON L/E RIB ATTACHMENT AT WS 1462 CORRODED AT BUSHING HOLE. FITTING REPLACED.SDR UIEA2017042600640Spar · corrodedCORROSION ON LT WING FRONT SPAR ON FSS 1440. REMOVED CORROSION.SDR UIEA2017042600641Skin · damagedLEFT WING, INBOARD, TRAILING EDGE FLAP, AFT FLAP, OUTBOARD, NEAR TIP, HAS NICK AT FASTENER HOLD ON LEADING EDGE. APPLIED REPAIR TO LEFT WING, INBOARD TRAILING EDGE FLAP AFT FLAP OUTBOARD NEAR TIP IAW SRM 51-70-06 PARA 5.L. INSTALLED FASTENER IAW SRM 51-40-02 SDR UIEA2017042600642Structure · damagedMULTIPLE DENTS IN APU DOORS AND EDGES AROUND DOORS ARE DAMAGED, FOUND OUT OF LIMITS IAW SRM 52-40-01-1A-5. DETAIL 111 FIG 101. FABRICATED A REPAIR IAW SRM 52-00-01-2R7. INSTALLED THE REPAIR IAW SRM 51-40-02.SDR UIEA2017042600643Bearing · corrodedRIGHT MLG TRUNNION AFT BEARING SLEEVE CORRODED. REMOVED & REPLACED THE BEARING SLEEVE IAW AMM 32-11-01, & AMM 32-11-01-404-205.SDR UIEA2017042600645Splice · crackedWHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT FWD INNER CHORD AND SPLICE FITTING, FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY.SDR UIEA2017042600646Splice · crackedWHILE PERFORMING NDT OPEN HOLE INSPECTION ON THE BS 2598 BULKHEAD, RIGHT SPLICE FITTING AND FRAME SUPPORT FOUND UPPER HOLE CRACKED IN SPLICE FITTING ONLY . REMOVED AND REPLACED THE RT SPLICE FITTING IAW SRM 51-40-02.SDR UIEA2017042600647Angle · corrodedON REMOVAL OF APU FIRE CONTROL MODULE IN RT BODY GEAR WHEEL WELL FOR ROUTINE TASK CARD REPLACEMENT, LOWER AFT MOUNT FOUND TO HAVE EXFOLIATED CORROSION. REMOVED CORRODED ZEE ANGLE IAW SRM 51-40-02, FABRICATED A NEW ZEE ANGLE, FABRICATED A FILLER IAW SRM 53-40SDR UIEA2017042600648Keelbeam · corrodedFOUND CORROSION BETWEEN FASTENERS ON KEEL BEAM LOWER FLANGE. BS 1460, RBL 9. REMOVED FASTENERS AT LWR KEEL BEAM CHORD TO REMOVE CORROSION BETWEEN FASTENERS HOLES IAW SRM 53-40-12-1A-1, PARA 3, STEP B. FOUND WITHIN LIMITS IAW 53-40-12, AND SRM 51-40-02.SDR UIEA2017042600649Bracket · crackedRIGHT WING OTBD SIDE OF THE NR 7 FLAP TRACK REAR SPAR AREA BRACKET IS CRACKED. REMOVED AND REPLACED THE BRACKET IAW SRM 51-40-02.SDR UIEA2017042600650Structure · crackedJ8 JUNCTION BOX ON LT WING LANDING GEAR CRACKED. CLEANED, PREPPED, REPAIRED, & REFINISHED J8 JUNCTION BOX IAW SRM 51-20-06, 51-70-06, AND AMM 51-24-22.
Back to Boeing 747-446