Boeing 737-2Q9
Service difficulty reports · 250
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 = '7372Q9' 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 = '7372Q9' 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 DHL2005741504Torque Box · crackedLT LOWER TORQUE BOX CRACKED AT BS 1213 IN AFT STAIR WELL. REMOVED EXISTING FASTENERS IN AREA AND CUT OUT DAMAGED SECTION (1 IN BY 1 IN) IAW B727 SRM 51-40-2 FIG 1. FABRICATED DOUBLER 7075-T6 .032 PO NR 900878 (5 1/2 INCH BY 2 1/2 INCH), FILLER 7075-T6 .025 7SDR DHL2005741503Torque Box · crackedRT LOWER TORQUE BOX CRACKED IN AFT AIR STAIR WELL AT BS 1225. STOP DRILLED CRACK (.250) IAW B727 SRM 51-10-1. FABRICATED DOUBLER 7075-T6, .032 PO NR 209041(5 INCH BY 3 INCH) IAW B727 SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. TREATED AN PRIMED AREA AND PART IAW BSDR DHL2005740542Seat Track · damagedMAIN CABIN SEAT TRACK BS 760 - BS 870 RBL 24.75 DAMAGED. REMOVED AND REPLACED SEAT TRACK BS 760 - 870 RBL 24.75 AND FABRICATED NEW SEAT TRACK P/N BAC1520-841 PO NR 9001690 DIM 4 FT AND P/N BAC1520-841 PO NR 9001474 DIM. 4 FT IAW B727 SRM 53-10-2 FIG 1 AND 53-SDR CA050125010Skin · cracked(CAN) AN OUTER FUSELAGE CRACK WAS DISCOVERED AT STRINGER S-18R, STATION 750, APPROXIMATELY 1.125 INCHES LONG. THE CRACK WAS REPAIRED IAW SRM 53-30-3 FIGURE 48, DETAIL IX AND DETAIL XIX.SDR CA050111001Gusset · cracked(CAN) DURING A ROUTINE PHASE 3 CHECK (137.5 HRS.), A 2.75 INCH CRACK WAS FOUND ON THE NOSE LANDING GEAR GUSSET WHILE CARRYING OUT SERVICE DIFFICULTY ALERT AL-2002-03.RETRACT ACTUATOR SUPPORT FITTING GUSSET REPLACED IAW SRM 51-30-2 FIG II. TIMES. 61981.7 CYCLESSDR CA041203006Skin · cracked(CAN) AN OUTER FUSELAGE CRACK WAS FOUND AT STR 16 LT BETWEEN STA 767 & 787 APPROX 2 INCHES LONG. FUSELAGE CRACK REPAIRED IAW SRM 53-30-1 FIG.48 PROCEDURES I, IV & VII. THIS REPAIR IS TIME LIMITED UNTIL 25 FEB. 04. TIMES- 61761:52 CYCLES- 57769.SDR CA041117005Engine · failedDURING DAILY CHECK, OIL WAS FOUND IN TAILPIPE AND LAST TWO STAGES OF TURBINE SECTION COATED WITH OIL. RT ENGINE SER NR 667210. RT ENGINE REPLACED. ENGINE SER NR ON 667217. TIMES 61700.25 CYCLES 57721.SDR CA041108010Skin · cracked(CAN) FUSELAGE CRACK FOUND ON OUTER SKIN AT STN 767 STR 18L, 0.875 INCHES LONG. CRACK REPAIRED IAW SRM 53-30-3 FIG 48 SHEET 32 DETAIL X REV.90. TIMES 61643.42 CYCLES 57682.SDR CA040419002Control Cable · chafed(CAN) DURING C-CHECK, THE LT ENGINE THRUST LEVER CONTROL CABLE (T1A) WAS FOUND TO BE CHAFED AND HAD BROKEN CABLE STRANDS. DURING INSTALLATION OF NEW CABLE, IT WAS FOUND THAT THE T1A CABLE HAD BEEN ROUTED UNDER THE CABLE GUARD INSTEAD OF OVER, CONTRIBUTING TO SDR CA030918007Skin · cracked(CAN) DURING ROUTINE DAILY CHECKS A CRACK WAS FOUND ON THE EXTERIOR FUSELAGE AT STN 935-937 STRINGER 24L. CRACK WAS REPAIRED IAW SRM 53-30-3 FIG 48 SHEET 29 DETAIL VI. ACFT TIMES 58839.13 ACFT CYCLES 55678.SDR CA030520003Wire · burned(CAN) FIVE WIRES DAMAGED FROM ARCING, AT WIRE CLAMP LOCATED OUTBOARD OF NR 2 SLAT OUTBOARD ATTACH ARM AT LT WING STATION 480. NO EVIDENCE OF RUBBING OR CHAFING.WIRE BUNDLE CLAMPS FOUND TO BE IN COMPLIANCE WI TH AD CF-84-08R2. SUSPECT BRITTLE WIRING DUE AGE OF SDR CA030409018Skin · cracked(CAN) 2.5 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 733 AT STRINGER S-17R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.25. TIMES - 57548:02 CYCLES- 54795SDR CA030409017Skin · cracked(CAN) 1.7500 FT CRACK FOUND ON EXTERIOR FUSELAGE AT FS 767 AT STRINGER S-18R. CRACK REPAIRED I.A.W. SRM 53-30-3 FIG.1 TIMES -57548:02CYCLES -54795SDR TSAA0356043Windshield · crackedTHE CAPTAIN'S FORWARD WINDSHIELD CRACKED WHILE CRUISING AT FL350. AN EMERGENCY WAS DECLARED. THE AIRCRAFT RETURNED TO HNL AND LANDED WITH NO FURTHER INCIDENT. MAINTENANCE REPLACED THE CAPTAINS FORWARD WINDSHIELD. GROUND OPERATIONAL AND PRESSURIZATION CHECKSSDR DHL2003740516Frame · crackedUPPER MAIN DECK CARGO DOOR FUSELAGE FRAME 480 CRACKED FWD SIDE WHERE ATTACHED TO FUSELAGE SKIN. CUT OUT DAMAGED FLANGE AND FABBED REPAIR FROM 7075-T6 AND FILLER FROM 7075-T6 .050 PER SRM 53-10-4 FIG 11. PARTS TREATED AND DRILLED PER SRM 51-10-2. INSTALLED RSDR CA030120008Line · chafed(CAN) NR 1 ENGINE FUEL LINE FROM FUEL CONTROL UNIT TO FUEL FLOW TRANSMITTER CHAFING ON TOP OF MAIN OIL TANK. FUEL LINE AND OIL TANK REPLACED. 57134.39 HOURS. 54518 CYCLES.SDR CA021015007Skin · cracked(CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STATION 727A & 727B AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30-3 FIG 48.SDR CA021015006Skin · cracked(CAN) CRACK FOUND ON OUTER FUSELAGE SKIN BETWEEN STA 747 & STA 767 AT STRINGER 18 LT. REPAIR CARRIED OUT PER SRM 53-30-3 FIG.6 SHEET 4.SDR CA021009024Skin · cracked(CAN) A 4 INCH CRACK,RUNNING FORE & AFT WAS FOUND DIRECTLY ABOVE STRINGER 16L AT STATION 520. CRACK REPAIR ACCOMPLISHED AS PER 737 SRM 53-30-3.SDR CA020819009Dump Valve · leaking(CAN) FORWARD LAVATORY FLUID BYPASSED DUMP VALVE ASSEMBLY INTO DRAIN MAINIFOLD AND LEAKED INTO THE SERVICE PANEL AREA. AIRCRAFT WAS AT 32,000 FT AT A TEMP OF -17C, OAT, WHEN THE ICE SHED FROM THE FWD LAV SERVICING PANEL AND CONTACTED THE RT INBOARD WING AND HOSDR CA020812003Connector · burned(CAN) ON TURNAROUND, WHEN FLT CREW SELECTED APU GENERATOR ON LINE, SEVERAL C/B,S TRIPPED. GENERATOR VOLTAGE LOW UNDER LOAD,BUT DID NOT TRIP OFF BUS. FOUND BTB TERMINAL CONNECTOR BOLT BURNED & LOOSE. BTB REPLACED. CHECKED SERVICEABLE.SDR DHL2002741002Battery · dischargedEMERGENCY LIGHT FAILED TO ILLUMINATE WHEN TURNED ON. REMOVED AND REPLACED BATTERIES IN BOTH EMERGENCY LIGHTS, OPS CHECK GOOD IAW BMM CH 33-50-01.SDR TSAA0133143Light · inoperativeREPLACED AFT SERVICE DOOR EMERGENCY LIGHT ASSEMBLY DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133141Battery Pack · dischargedREPLACED FORWARD SERVICE DOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133140Light · inoperativeREPLACED FORWARD OVERHEAD EMERGENCY AISLE LIGHT ASSEMBLY PACK DUE TO NO TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133108Battery Pack · inoperativeREPLACED NR 6 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133105Battery Pack · inoperativeREPLACED NR 3 EMERGENCY FLOOR BATTERY PACKS DUE TO INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133103Battery Pack · inoperativeREPLACED NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0153090Skin · crackedIDENTIFIED 1.5 INCH FUSELAGE SKIN CRACK AT BS 727, S16R. REMOVED TWO PREVIOUS REPAIRS IN THE IMMEDIATE AREA, TRIM OUT DAMAGED AREA, HFEC INSPECTION COMPLETED AROUND TRIM AREA NO DEFECTS NOTED, .040 INCH INSURANCE CUT COMPLETED, VISUALLY INSPECTED AREA UNDER RSDR TSAA0153063Skin · dentedDENT AT FUSELAGE SKIN AT BS 360-BS400, STRINGER 17L. REMOVED DAMAGED AREA, HFEC INSPECTION COMPLETED NO DEFECTS NOTED AROUND CUTOUT AREA, INSTALLED 7075-T6 CREASE BEAM, INSTALLED .071 INCH FILLER 2024-T3 INSTALLED .032 INCH DOUBLER 2024-T3, INSTALLED .050 INCSDR CA010515004Isolation Valve · leaking(CAN) AIRCRAFT LOST A SYSTEM HYDRAULIC FLUID UPON TAXIING TO THE TERMINAL. CREW HAD TO USE DIFFERENTIAL BRAKING TO GET TO GATE. AFTER INVESTIGATION IT WAS DETERMINED THAT THE MAIN GEAR ISOLATION VALVE P/N 65-44581-6, S/N 0575 WAS LEAKING.SDR TSAA0133026Battery Pack · dischargedREPLACED FORWARD ENTRY IDENT LIGHT ASSEMBLY DUE TO BEING INOPERATIVE. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0133017Battery Pack · dischargedREPLACED FORWARD SERVICE EMERGENCY EXIT IDENT AND RIGHT CENTER EXIT IDENT BATTERY PACKS. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR CA010308011Wire · chafed(CAN) WIRE W200-453-06 CHAFED THROUGH INSULATION AND WIRE. LENGTH & WIDTH OF CHAFE IS 3/8 INCH, DEPTH 1/8 INCH. APPEARS TO HAVE RUBBED AGAINST COWLING AT SOME TIME. HOWEVER, AT TIME OF DISCOVERY, IT WAS NOT APPARENT WHAT THE WIRE HAD CHAFED. THERE HAD BEEN NO SDR TSAA0033240Battery Pack · dischargedREPLACED NR 1, NR 2 AND NR 3 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR USAASB00300Battery Pack · dischargedTPA - FOUND THE R2 AND L2 DOOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE AFT CARGO BATTERY PACK. (M)SDR CA001102014Actuator · cracked(CAN) ON LANDING DURING GROUND SPOILER DEPLOYMENT HYDRAULIC FLUID WAS OBSERVED LEAKING FROM THE NR 5 GROUND SPOILER NR 5 ACTUATOR. OBSERVATION REVEALED THAT UNDER PRESSURE A CRACK WOULD OPEN UP IN THE CASE. SPOILER ACTUATOR WAS REPLACED. CHECKED SERVICEABLE.SDR TSAA0053209Stringer · damagedFABRICATED AND INSTALLED STRIGNER S21R BETWEEN BS 947 TO BS 967 DUE TO RUPTURED PORTABLE WATER TANK, IAW SRM 53-10-3. AIRCRAFT RETURNED TO SERVICE. (M)SDR 20010104AP004Relief Valve · inoperativeFLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUPSDR TSAA0038201Regulator · inoperativeFLT 124 - HNL-KOA - DURING CLIMB-OUT FROM HNL, THE CREW HEARD A LOUD BANG FROM THE AFT SECTION OF THE AIRCRAFT. CREW REPORTED ALL INDICATIONS NORMAL. CAPTAIN DECLARED AN EMERGENCY. RETURNED TO HNL FOR AN UNEVENTFUL LANDING. FOUND THE POTABLE WATER TANK RUPSDR TSAA0033204Battery Pack · inoperativeREPLACED NR 3 AND NR 5 FLOOR PROXIMITY BATTERY PACK DUE TO UNIT FAILS BATTERY TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0053197Frame · corrodedREMOVED CORROSION FROM INNER CHORD AT BS 1088 STRINGER 17 AND INSTALLED REPAIR ANGLES IAW ECO 3178. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0053196Keelbeam · corrodedREPAIRED FUSELAGE SECTION 46, BS 727 KEEL BEAM AREA SKIN AND DOUBLER DUE TO CORROSION. REMOVED CORROSION AND INSTALLED .063 INCH AND .050 INCH FILLER AND .063 INCH DOUBLER IAW ECO 2454. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033193Battery Pack · inoperativeREPLACED NR 6 EMERGENCY FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK AIRCRAFT RETURNED TO SERVICE. (M)SDR USAASB00210Valve · failedBWI - FLT 2633 - ON CLIMB-OUT FROM BWI, THE NR 1 ENGINE BLEED TRIP OFF LIGHT ILLUMINATED (RESET WAS SUCCESSFUL) AND THE EGT WENT TO 645 DEGREES FOR 5 SECONDS. ALL OTHER ENGINE INDICATIONS WERE NORMAL. THIS OCCURRED DURING FLAP RETRACTION AT 1,500 FEET. CREWSDR TSAA0033170Battery Pack · inoperativeREPLACED NR 2 AND NR 5 FLOOR PROXIMITY BATTERY PACK DUE TO UNIT FAILS BATTERY TEST. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033171Light · inoperativeREPLACED FORWARD SERVICE DOOR EXIT IDENTIFIER LIGHT ASSEMBLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0033172Light · inoperativeREPLACED NR 2 FLOOR EMERGENCY LIGHT ASSEMBLY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)SDR TSAA0027136Transmitter · malfunctionedFLT 91 - OGG-HNL - DURING TAKEOFF FROM OGG, THE STALL WARNING STICK SHAKER BEGAN AT ROTATION AND WAS CONTINUOUS THROUGH 1000 FEET AND INTERMITTENT AFTER THAT. RETURNED TO OGG FOR AN UNEVENTFUL LANDING. REPLACED THE RIGHT TRAILING EDGE FLAP POSITION TRANSMITTSDR TSAA0053143Lap Joint · crackedLOWER SKIN LAP JOINT, CRACK REPAIR AND LAP JOINT MODIFICATION COMPLETED AT BS 360-540, STRINGER 14R, STRINGER 10R, STRINGER 10L AND STRINGER 14L, BS 727-908, STRINGER 14R, 10R, STRINGER 10L AND STRINGER 14L, BS 360-908 IAW ECO 3080R1. AIRCRAFT RETURNED TO SER
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