Boeing 737-800
Service difficulty reports · 843
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 = '737800' 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 = '737800' 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 CA120528008Bearing · damaged(CAN) AFTER LANDING, PILOT REPORTED THAT ACFT REQUIRED MORE POWER THAN NORMAL DURING TAXI TO GATE. ACA INSPECTED WHEELS & BRAKES AND FOUND NR 4 BRAKE AND MAIN WHEEL ASSY WERE DAMAGED BEYOND REPAIR. TIRE PRESSURE FOUND NORMAL, FUSE PLUGS DID NOT MELT. THE DASDR SAJF201206141018Strap · corroded(B18605) LEFT WING L/E FRONT SPAR LOWER ATTACH STRAP HAS A 3.5 X 1.3 INCH AREA CORROSION. CORRODED AREA R & R IAW EO 738-57-00-0152.SDR ASMF201204008Blade · damagedDURING A BORESCOPE INSPECTION OF THE HPT 1ST STAGE BLADES OF THE LT ENGINE WAS DETECTED 1 BLADE OF THE HPT 1ST STAGE WITH A CRACK OUT OF LIMITS IAW MM 72-00-00 PARAGRAPH G 1(A), WITH DIMENSIONS OF 0.125" LONG IN THE T/E AREA. MX PERSONNEL REPLACED AND TESTED SDR ASMF20120420007Probe · damagedCAPTAIN REPORTED THAT DURING TAKEOFF, THE LT ENGINE WAS REACHED 969 C FOR AROUND 12 SECONDS; SO FLIGHT CREW IMMEDIATELY REDUCING THRUST AND AFTER THE REDUCTION, THE LT ENGINE INDICATION WAS SHOWED NORMAL AND IT WAS ACCOMPLISHED THE QRH 8.5 PROCEDURE AND CONTINSDR SWAA2012032902693Light · inoperativeRT FWD EXTERNAL OVERWING EMERGENCY EXIT LIGHT INOP. RELAMPED LIGHT PER MM.SDR CA120305001Pin · sheared(CAN) DURING WALKAROUND, THE PILOT REPORTED RT MAIN GEAR HAD A LOOSE SPRING HANGING. UPON FURTHER INVESTIGATION IT WAS NOTED THE RT DOWNLOCK SPRING PIN HAD SHEARED. THE PIN WAS REPLACED AND THE ACFT RETURNED TO SERVICE.SDR FOTR2012021436495Stiffener · crackedLEFT WING INBD K-FLAP CRACKED AT OTBD SIDE VERTICAL STIFFENER. REPAIRED ON FASI WO 21143, NR 36495.SDR FOTR2012021436334Skin · crackedCRACKED L/E BOTTOM NR 1 SLAT EXTERIOR SKIN. REPAIRED ON FAS WO 21143, NR 36334.SDR FOTR201202016401Skin · crackedLT WING L/E WS204 SKIN AT UPPER FASTENER ROW IS LOOSE AND CRACKED IN 2 PLACES. REPAIRED FAS WO 21143, NR 36401.SDR FOTR201201282013Skin · debondedLWR INBD T/E OF RT WING OTBD AFT FLAP DISBONDED. REPAIRED ON FAS WO 21143, NR 36435.SDR FOTR0209201236446Skin · delaminatedLEFT WING INBD FLAP OTBD T/E DELAMINATED. REPAIRED ON FAS WO21143, NR 36446.SDR FOTR0201201276387Skin · debondedLEFT WING T/E INBD FLAP ON THE UPPER SURFACE HAS 1 EA. REPAIR, REQUIRES EVALUATION. REPAIRED ON FAS WO 21143, NR 36387.SDR FOTR2011011145336Skin · damagedR & R AFT CARGO DOOR SKIN. REPAIRED ON FAS WO 21143, NR 05336.SDR FOTR2011111405335Skin · damagedR & R FWD CARGO DOOR SKIN. REPAIRED ON FAS WO21143, NR05335.SDR ASMF201111008Regulator · failedACFT PERFORMED AN UNSCHEDULED LANDING, DURING CLIMB THE LT ENGINE PURGE INDICATED 5 PSI, SO THE FLIGHT CREW ACCOMPLISHED THE QRH 2.6 PROCEDURE. MX PERFORMED THE FIM 36-10, TASK 804 DETECTING VALUES WITHIN LIMITS, NO FAILURE WAS FOUND; REFUEL WAS PERFORMED. ASDR FOTR201111045347Skin · crackedFWD CARGO DOOR INTERNAL SKIN LIGHTNING HOLE HAS CRACK. REPAIRED ON FAS WO 21143, NR 05347.SDR ASMF201109008Valve · damagedCAPTAIN REPORTED MAIN TANKS FUEL IMBALANCE FROM 300 KGS TO 400 KGS. MX PERFORMED CROSS FEED VALVE OPS TEST IAW MM 28-22-00, DETECTING THE RESULTS WERE OPS OUT OF LIMITS, BEING THE FUEL TRANSFERENCE OF 500 KGS IN TWO MINUTES. THE FUEL CROSSFEED VALVE WAS REPLASDR ASMF201108009Valve · leakingDURING TRANSIT CHECK IT WAS DETECTED A FUEL LEAK IN THE RT ENGINE WITH MORE THAN 180 DROPS PER MINUTE. MX PERFORMED REVISION DETECTING THE HPTACC VALVE WITH LEAK OUT OF OPERATION LIMIT, SO THE HPTACC VALVE WAS REPLACED IAW MM 75-21-01, TESTED CORRECT.SDR FOTR2111311130Skin · dentedRT WING NR12 SPOILER UPPER SURFACE HAS 2 EACH DENTS BEYOND ALLOWABLE LIMITS. REPAIRED ON FASI WORK ORDER 21113 NR11130.SDR FOTR2111311126Skin · dentedLEFT WING NR6 SPOILER UPPER SURFACE HAS 1 DENT BEYOND ALLOWABLE LIMITS. REPAIRED ON FASI WORK ORDER 21113 NR 11126.SDR FOTR2111311125Skin · dentedLT WING NR 5 SPOILER UPPER SURFACE HAS ONE DENT BEYOND ALLOWABLE LIMITS. REPAIRED ON FASI WORK ORDER 21113, NR 11125.SDR FOTR2111311101Flap · delaminatedLT WING INBD FLAP LOWER SKIN STATION 253 IS DELAMINATED. REPAIRED ON FASI WORK ORDER 21113 NR 11101.SDR FOTR2111311100Skin · dentedLT WING INBD AFT FLAP LOWER SKIN HAS DENT WITH A CRACK. REPAIRED ON FASI WORK ORDER 21113 NR 11100.SDR SAJFCALS100022Bearing · cracked(AIRCRAFT B18606) HORIZONTAL STABILIZER CENTER SECTION HINGE FITTING BEARINGS FOUND DAMAGED (CRACK). OTHER ACFT HAVE REPORTED SIMILAR CRACK DAMAGED BEARING AT THE HINGE FITTING BEARING. THE REPLACEMET FOR THE DAMAGED BEARINGS IS IN PROGRESS.SDR 2011FA0000360Wheel · failedWHEEL SUSTAINED HUB FAILURE.SDR SAJFCALS100014Actuator · malfunctioned(B-18609) "SPEED BRAKE DO NOT ARM" LT ILLUMINATED WHEN ACFT ROLLING AT SPD 90 KTS. ACFT ABORTED TAKEOFF AT SPD 100 KTS AND THEN RETURNED TO GATE. AUTOSTOW ACTUATOR REPLACED IAW AMM 27-62-33 AND TEST NML. PERFORM AMM 05-51-07 HIGH ENERGY STOP/HEAT DAMAGE CONDISDR SAJFCALS100010Computer · malfunctioned(B-18617) DURING DESCENT, WHEEL WELL FIRE WARNING CAME AT SPEED OF 235 KNOTS, THE LANDING GEARS WERE DOWN. THE COMPARTMENT OVERHEAT DETECTION COMPUTER SHOWED "CODE 84 - WHEEL WELL FIRE ALARM". TRIED THE WW DETECTOR REPLACEMENT IN VAIN. WITH THE DETECTOR DISCSDR CA110310008Antenna · broken(CAN) THE CABIN CREW REPORTED HEARING A BANGING NOISE FOR A FEW SECONDS IN THE CEILING DURING CRUISE. AFTER LANDING, MAINTENANCE INPSECTED THE AIRCRAFT AND FOUND THE ELT ANTENNA TO BE BROKEN IN HALF. THE ANTENNA WAS REPLACED AND THE SURROUNDING AREA INSPECTED SDR XV6A2011021600001Light · inoperativeONE EACH FLOOR MOUNTED EMERGENCY LIGHT INOP AT ROW 4.SDR CA110125022Wire · chafed(CAN) DURING APPROACH AND AFTER SELECTION OF FLAP 15 FOR LANDING, THE FLAP INDICATOR SHOWED ASSYMETRY AND THE FLAPS REMAINED AT FLAP SETTING 5. AN EMERGECNY LANDING OCCURED WITHOUT ANY FURTHER INCIDENT. THE PSEU LIGHT ILLUMINATED AFTER LANDING. MAINTENANCE WASSDR SAJFCALS100003Flap System · malfunctioned(B-18612) T/E FLAP, ASSYMETRY AT L/24 R/17 ON FINAL APPROACH. ON ARRIVAL CHECK BOTH FLAP POSITION CHECKED NORMAL. IAW FIM 2725 TASK 802 CARRY OUT FLAP INSP AND CK NML. FSEU BITE TEST CARRY OUT NO EXISTING FAULT FOUND. PSEU R & R AFTER ACFT BACK TO TPE (MAINSDR CA110125019Pitot Tube · blocked(CAN) AFTER TAKE-OFF, THE AIRCRAFT DISPLAYED A IAS DISAGREE CAUTION LIGHT AS THE CAPTAIN`S ASI DID NOT MATCH THE CO-PILOT OR STANDBY. MAINTENANCE CARRIED OUT TROUBLESHOOTING AND FOUND A PARTIALLY BLOCKED PITOT TUBE TO BE THE CAUSE. THE PITOT TUBE WAS REPLACED SDR 2010F00208Tie Bolt · brokenWHEEL HAD MULTIPLE BROKEN TIE BOLTS ON POSITION 1 OF AIRCRAFT.SDR 2010F00207Tie Bolt · brokenMULTIPLE BROKEN TIE BOLTS FOUND DURING THE INSPECTION OF WHEEL. WHEEL INSPECTED UPON RECEIPT.SDR CA100714001Skin · debonded(CAN) TOP AND BOTTOM SKINS DISBONDED. 21 INCH BY 6.5 INCH. 21 INCHES INBOARD OF OUTBOARD EDGE DUE TO WATER INGRESS THROUGH THE BOND LINE BETWEEN THE TRAILING EDGE SKINS AND THE SPAR. UNIT REPAIRED WITH STANDARD HOT BOND TECHNIQUES PER MANUFACTURER RECOMMENDASDR ASMF201006003Pseu · malfunctionedACFT REJECTED TAKEOFF AT 60 KNOTS DUE TO RT FWD AND AFT OVERWING LIGHTS TURNED ON. MX PERSONNEL RESEATED THE PRIMARY PSEU IAW FIM 52-20 TASK 806 AND ALL LIGHTS EXTINGUISHED, DELIVERING ACFT TO SERVICE, ALL CORRECT. THE HIGH ENERGY STOP INSP WAS NOT NECESSARY DSDR SAJFCALS099008Flap System · malfunctioned(B-18609) AIR TURN BACK DUE TO "L/E FLAPS TRANSIT" LIGHT ILLUMINATED AT FL 110, THE FOLLOWING TASKS WERE PERFORMED: A) FSEU BITE TEST NO FAULT WAS FOUND. QAR READING RESULT SHOWN "T/E FLAP IND" ERROR (HANDLE: UP VS. QAR READ OUT DATA: 14.9 DEGREES) CAUSED "L/SDR SCNA10003Light · looseROW 11ABC FLOOR EMERGENCY LIGHTING COMING UP OFF FLOOR. MAINTENANCE REMOVED & REPLACED SECTION OF LUMINESCENT FLOOR LIGHTING. OPERATIONAL CHECK GOOD.SDR SCNA10001Sign · damagedINSPECTION FOUND EMERGENCY EXIT SIGN MOUNT BROKE AT AFT LWR CORNER OF LT AFT OVERWING DOOR. EXIT SIGN WON'T STAY ON. MAINTENANCE REPLACED EXIT SIGN.SDR CA100216012Bolt · missing(CAN) DURING A BI-WEEKLY INSP, AN AME NOTICED THAT THE RT INBD KRUEGER FLAP DID NOT SEEM TO BE DEPLOYED FULLY, AS COMPARED WITH THE OTHERS. ON INSP IT WAS NOTED THAT THE 3 BULLNOSE WAS DISCONNECTED AND THE HARDWARE WAS MISSING. THE AREA WAS INSPECTED FOR FURTHSDR SCNA10002Lens · looseMAINTENANCE FOUND EXIT ROW STRIP LIGHT IS OFF AT 14DEF SEAT POSITION. SECURED LENS. EMERGENCY LIGHT IS READABLE & OPERATIONALLY CHECKS GOOD.SDR SCNA09018Light · inoperativeRIGHT FWD EMERGENCY OVERWING EXIT DOOR EXT LIGHT INOP. RELAMPED PER AMM 35-51-04-960-801.SDR 2009F00138Lamp · inoperativeRT FWD EMERGENCY OVER WING EXIT DOOR EXTERNAL LIGHT INOP. RELAMPED RT FWD EMER O/W EXIT DOOR LIGHT OPS CKS GOOD IAW AMM 35-51-04-960-801.SDR CA091202016Scuff Plate · damaged(CAN) AFTER DEPARTURE FROM YEG, CREW REPORTED DIFFICULTY PRESSURIZING THE AIRCRAFT AND THE LT SLIDING WINDOW APPEAR TO BE NOT CLOSED PROPERLY. AIRCRAFT RETURNED TURNED BACK FROM FLIGHT AND LANDED SAFELY IN YEG. ON INVESTIGATION, FOUND THE SCUFF PLATE ON LT CDSDR MYWA09061Warning System · intermittentETOPS SIGNIFICANT SYSTEM - REFERENCE DMI 6894 LP 228056 RIGHT SIDE WINDOW OVERHEAT LIGHT ON IN FLT. FOLLOWED PROCEDURES, LIGHT REMAINED ON. WINDOW WENT OFF PER QHQ REMAINDER FLIGHT. PERFORMED FIM TASK 30-41 TASK 811. FAULT FOUND TO BE INTERMITTENT. OPS CHSDR SAJFCALS098034Drain · unsecureAIR TURN BACK, DUE TO LOUD NOISE IN THE COCKPIT WHEN PASSING 5000 FT. INSP FOUND F/O SIDE FLIGHT DECK DRIPSHIELD DRAIN TUBE BEING TRAPPED IN THE L/E OF THE RT NR 2 SLIDE WINDOW. (THE WINDOW IS CLOSED AND LOCKED) FURTHER EXAM FOUND THE ADHESIVE DETERIORATED ANSDR SAJFCALS098027Warning Light · false activationAIRCRAFT B-18610 LT AFT ENTRY DOOR WARING LIGHT ILLUMINATED DURING TAKEOFF. AIRCRAFT ABORTED TAKEOFF. GROUND OPERATION CHECK FOUND LT AFT ENTRY DOOR CONDITION NORMAL. IAW AMM 52-13-00 AFT ENTRY DOOR (SOFT UNLATCHING) MAKE SURE THAT RIG PIN EASILY THROUGH THESDR CA090708006Connector · burned(CAN) FOLLOWING A PROBLEM WITH INFLIGHT ENTERTAINMENT SYSTEM (IFE) SCREENS BEING INOPERATIVE, TROUBLESHOOTING FOUND A CONNECTOR PN: SJS816220 OR APCD0650(MALE) AND SJS816120 OR APCD0641 (FEMALE), DISCONNECTED/PINS BURNED. BOTH MALE AND FEMALE CONNECTORS WERE SDR CA090715003Wire Harness · damaged(CAN) ON ARRIVAL, CREW REPORTED NO SMOKING/FASTEN SEAT BELT SIGN CIRCUIT BREAKER TRIPPED DURING FLIGHT. UPON INVESTIGATION, MX TECH FOUND NO SMOKING/FASTEN SEAT BELT SIGN HARNESS DAMAGED ABOVE SEAT 11DEF. HARNESS HAD CAUGHT IN THE INFLIGHT ENTERTAINMENT SYSTESDR 2009F00035Floorbeam · corrodedDURING AV11 CHECK B18601, CORROSION WAS FOUND ON FLOORBEAM AT STA 986.5 LBL 22.5 AND RBL 23 ABOUT 0.4 INCH X 0.4 INCH X 0.050 INCH. THIS IS A CPCP LEVEL 2 ITEM. REPAIRED THE CORRODED AREAS IAW SRM 53-00-51.
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