N433AS
Service difficulty reports · 333
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.
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 n_number = 'N433AS' AND registry_match = 'registration' 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 n_number = 'N433AS' AND registry_match = 'registration' 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 ASAA2019103181181Warning Light · false activationAFTER PUSH LEFT PACK LIGHT ILLUMINATED EXTINGUISHED UPON RECALL. GROUNDED - YES. PERFORMED BITE B737-900 FIM 21-62 TASK 801 NO FAULTS OPS NRML, CLEARED MEL 21-32BSDR ASAA2019102853122Wire Harness · damagedDURING TC N8420001 INSPECTION FOUND MW0326 HARNESS WITH DAMAGED BRAIDING. GROUNDED - YES. REMOVED AND REPLACED MW0326 HARNESS PER B737-900 AMM 26-11-02. PERFORMED GOOD OPS TEST OF R/H ENGINE FIRE DETECTION SYSTEM PER AMM 26-11-02-400-802.SDR ASAA2019102843128Door · bindingL1 DOOR IS HARD TO OPEN. GROUNDED - YES. FOLLOWING B737-900 FIM 52-10-00-810-807 PERFORMED FWD ENTRY DOOR INSPECTION, NO DEFECTS NOTED. PERFORMED FWD ENTRY DOOR SYSTEM TEST, TORQUES ARE WITHIN B737-900 AMM 52-11-00 LIMITS. CLEANED AND LUBRICATED UPPER AND LOWESDR ASAA201910231078Autopilot Sys · malfunctionedAT FL 340 DURING CRUISE, A SINGLE AUTOPILOT DISCONNECT HAPPENED ON CMD "A". AUTOPILOT WAS RE-EMGAGED PM "A" SIDE AND DID NOT OCCUR AGAIN. GROUNDED - YES. ACCOMPLISHED B737-900 FIM 22-11 TASK 801. DFCS BITE FOUND MSG 22-11208 AND 22-11607 IN LEG 1 HISTORY. COMPSDR ASAA2019102173046Autopilot Sys · faultedAUTO PILOT DISENGAGED AT 34000 FT WITH NO PILOT INPUTS. ON DESCENT THE AUTO PILOT KICKED OFF AGAIN WITH OUT ANY PILOT INPUT. GROUNDED - YES. DEFECT DID NOT INDICATE WHICH A/P ENGAGED. USING DFCS FAULT REVIEW DETERMINED B A/P ENGAGED. FAULT MSG 22-11607 ASSOCIASDR ASAA2019102173045Warning Light · false activationLEFT PACK CAUTION LIGHT ILLUM ON RECALL. EXTINGUISH ON RESET. GROUNDED - YES. REF B737-900 FIM 21-53 TASK 809, #1 PZTC BITE PREV FLT LOGGED SRADA INLET FAULT, RESET FAULT, PZTC BITE VERIFY GOOD W/O FAULT. VERIFIED LEFT PACK OPS CHECKED NORMAL ON GND W/O FAULT SDR ASAA2019101433994Warning Light · false activationLEFT PACK LIGHT ILLUM IN FLT. RESET PER QRH, CAME BACK ON. REMAINED ON DURATION OF FLIGHT. RIGHT PACK NORMAL, PRESSURIZATION NORMAL, CONTINUE WITH LEFT PACK OFF. GROUNDED - YES. PERFORMED BITE TEST REF B737-900 FIM 21-62 TASK 801 FAULT TCV FOUND ON THIS PACK, SDR ASAA2019100310891Cover · damagedL-1 DOOR DIFFICULT TO OPEN & CLOSE. GROUNDED - YES. REMOVED JAGGED TEFLON MATERIAL FROM HINGE COVERS (CAUSING A RATCHETING SOUND ). DOOR BRAKE-OVER IS NORMAL. OK FOR SERVICE. IAW CMM 25-00-66 & AMM 52-11-00.SDR ASAA2019100293868Warning Light · false activationLH PACK LIGHT ILLUMINATES ON RECALL AND EXTINGUISHES WHEN MASTER CAUTION SYSTEM IS RESET. GROUNDED - YES. FOLLOWED B737-900 FIM 21-53 TASK 803. REF W.O 1003123 FOR L/H/R/H HEAT EXCHANGER CLEANING. NO FAULTS FOUND. LH PACK OP CHECK GOOD.SDR ASAA2019092630844Unknown · malfunctionedDURING DESCENT APPROACHING 12000', THE RIGHT FUEL QUANTITY RAPIDLY DECREASED TO 1500# IMBALANCE. THE YELLOW IMBALANCE LIGHT REMAINED ILLUMINATED UNTIL WE MADE OUR FIRST RIGHT TURN TAXIING OFF OF THE RUNWAY THEN THE RIGHT FUEL QUANTITY RESUMED READING CORRECTLYSDR ASAA2019092430803Unknown · malfunctionedSATCOMM SHOWS IN PROGRESS CONTINUOSLY. GROUNDED - YES. CYCLED POWER TO SATCOM SYSTEM & PEFORMED FIM 23-15 TASK 801 & FAULT CLEARED SATCOM OPS NORMAL.SDR ASAA2019082983524Warning Light · false activationRIGHT PACK LIGHT ON DURING RECALL EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED CONTROLLER BITE LOGGED SRADA INLET FAULT. PERFORMED B737-900 FIM 21-62 TASK 852 FAULT LIGHT RESET, RT PACK RUNS NORMAL. OK FOR SERVICE GROUND VERIFICATION SUCCESDR ASAA2019082633480Radar · malfunctionedFO RADAR NOT WORKING PROPERLY. GROUNDED - YES. NOTE: CREW REPORTS F/O RADAR INDICATION RETUIRNED TO NORMAL. PERFORMED B737-900 FIM 34-43 TASK 801 WEATHER RADAR SYSTEM BITE. NO FAULTS NOTED.SDR ASAA2019080523304Start Valve · stuck#1 ENGINE START VALVE FAILED TO CLOSE AFTER ENGINE START. RAN QRH AND STILL DIDNT CLOSE. GROUNDED - YES. REPLACED #1 ENG START VALVE REF B737-900 AMM 80-11-03. OPS NORMAL.SDR ASAA2019080523295Lamp · inoperativeWHILE PERFORMING T/C 78233008, L1 DOOR EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED AND REPLACED SLIDE/OVERWING LAMP AT L1 DOOR. REF B737-900 AMM 33-51-04-960-801. OPS CHECKS GOOD.SDR ASAA2019080513299Control Panel · failedWEATHER RADAR MULTI-SCAN FUNCTION INOP, NOTHING SEEMS TO HAPPEN WHEN "AUTO BUTTON PRESSED. MANUAL TILT OPERATES NORMALLY. GROUNDED - YES. PERFORMED WXR SYSTEM - OPERATIONAL TEST REF B737-900 AMM 34-43-00-710-802-001, TEST FAILS AT STEP D.(8). REMOVED AND REPLASDR ASAA2019080133260Radar · malfunctionedAUTO TILT FUNCTION OF RADAR IS INOP. GROUNDED - YES. PERFORMED WEATHER RADAR SYSTEM BITE TEST REF B737-900 FIM 34-43 TASK 801 NO FAULTS FOUND. WXR RADAR SYSTEM OK FOR SERVICE.SDR ASAA2019072330185Control Panel · damagedFO SIDE COURSE SELECTOR WINDOW DISPLAY IS CHIPPED AND DAMAGED. GROUNDED - YES. REMOVED & REPLACED MCP IAW AMM 22-11-34. OPS CHECK NORMAL.SDR ASAA2019072230141Lens · missingFOUND LOWER EMERGENCY EXIT SIGN NEAR L1 DOOR MISSING COVER. GROUNDED - YES. INSTALLED NEW COVER ON EMERGENCY EXIT SIGN NEAR L1 DOOR REF AMM 33-51-01. PERFORMED EMERGENCY LIGHTS TEST, NO DEFECTS NOTED.SDR ASAA2019071029992Start Valve · failed#2 START VALVE DID NOT CUT OUT. GROUNDED - YES. REMOVED AND REPLACED #2 ENGINE START VALVE REF AMM 80-11-03. ETOPS SIGNIFICANT ITEM VERIFIED.SDR ASAA2019061752979Fault Light · false activationAPU FAULT LIGHT ILLUMINATED AFTER ATTEMPT TO START. GROUNDED - YES. COMPLIED WITH BITE CHECK ON APU SYSTEM. NO CURRENT FAULTS NOTED. FAULT HISTORY SHOWS FAULT CODE 49-21015 OVERTEMPERATURE SHUTDOWN. FAULT CODE IS NO LONGER ACTIVE. APU OPERATES NORMALLY. APU FASDR ASAA2019051729389Paint · peelingSPINNER FRONT CONE PAINT WORN AND PEELED. GROUNDED - YES. REMOVED AND REPLACED SPINNER FRONT CONE IAW T/C#78472010.SDR ASAA2019051629378Retainer · separatedR1 DOOR SLIDE PACK SEEMS CROOKED/EXTREMELY DIFFICULT TO ARM/DISARM BAR. GROUNDED - YES. FOUND GIRT BAR RETAINER SEPARATED MAKING GIRT BAR DIFFICULT TO ARM/DISARM AND APPEARS TO LOOK CROOKED WHEN IN RETAINER CLIPS. REMOVED AND REPLACED R-1 GIRT BAR RETAINER FORSDR ASAA2019051629362Glowstrip · missingFLOOR PHOTO LUMINESCENT STRIP AT ROW 21 ABC MISSING. GROUNDED - YES. REPLACED FLOOR PHOTO LUMINESCENT STRIP AT ROW 21 ABC PER AMM 33-51-15.SDR ASAA2019042342997Angle · crackedFWD CARGO PIT STA 500K R/H AFT BAFFLE CLIP IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT R/H STA 500K FWD BAFFLE CLIP IAW B737 900 ER SRM 51 40 02 0G 0 AND STEP 7.D.SDR ASAA2019042342996Angle · crackedFWD CARGO PIT STA 500K R/H FWD BAFFLE CLIP IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT STA 500K R/H FWD BAFFLE CLIP IAW B737 900 ER SRM 51 40 02 0G 0 AND STEP 7.D.SDR ASAA2019042342995Baffle · crackedFWD CARGO PIT L/H BAFFLE BETWEEN STA 500I AND 500J IS CRACKED AT NUTPLATE HOLE. GROUNDED - YES. REMOVED AND REPLACED WITH NEW BAFFLE IN FWD CARGO PIT AT LH BETWEEN STA 500I AND 500J IAW B737 900 ER SRM 51 40 02 0G 0.SDR ASAA2019042342994Angle · crackedFWD CARGO PIT R/H STA 500H FWD BAFFLE CLIP IS CRACKED. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT R/H STA 500H FWD BAFFLE CLIP IAW B737 900 ER SRM 51 40 02 0G 0 FIG 8 AND STEP 7.D.SDR ASAA2019042342992Support · corrodedAFT WET AREA LAV SUPPORT HAS CORR AT BS 948 LBL 51. GROUNDED - YES. REMOVED AND REPLACED LAV SUPPORT INTERCOSTAL IAW 737 900 ER 51 40 02 0G 0 W .5" O .190 R .166 L 1" D .024".SDR ASAA20190429149Transition Panel · corrodedFWD CARGO PIT L/H TRANSITION PANEL HAS MULTIPLE AREAS OF CORR FROM STA 500C+14 TO 500L. GROUNDED - YES. BLENDED MULTIPLE AREAS OF CORR ON FWD CARGO PIT L/H TRANSITION PANEL AND WAS FOUND TO BE OUT OF LIMITS IAW B737 900 ER SRM 53 00 53 1A 2 FIG 103 DETAIL D, FSDR ASAA2019041329127Channel · corrodedFWD CARGO PIT R/H TRANSITION PANEL HAS MULTIPLE AREAS OF CORR FROM STA 500A TO 500L. GROUNDED - YES. REMOVED CORR FROM FWD CARGO PIT R/H TRANSITION PANEL FROM STA 500A TO 500L FOUND TO BE OUT OF LIMITS IAW B737 900 ER SRM 53 00 53 1A 2, REPAIRED IAW B737 900 ESDR ASAA2019042329105Web · corrodedAFT CARGO COMPARTMENT LWR DOOR SILL WEB HAS CORR. GROUNDED - YES. REMOVED CORR AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW B737 900 ER SRM 53 60 15 1A 1 REMOVED AND REPLACED AFT PIT LWR SILL WEB IAW B737 900 ER SRM 51 40 02 0G 0 W 1 O .050 R .044 L 30 D .SDR ASAA2019040988942Warning Light · false activationAFTER GETTING APU GEN ONLINE THE OVERSPEED LIGHT ILLUMINATED AND APU GEN KICKED OFF LINE RE-ESTABLISHED GEN 1 AND 2 RAN QRH AND AFTER 5 MIN OVERSPEED LIGHT EXTINGUISHED. GROUNDED - YES. RAN APU BITE REF B737-900 FIM 49-61 TASK 801 NO CURRENT FAULTS FOUND. SPEESDR ASAA201904028848Autopilot Sys · malfunctionedAP #1 (AUTOPILOT A) DISENGAGED TWICE WHILE AT CRUISE (FL350) WITHOUT ANY PILOT INPUT OF ANY KIND. THERE WAS NO TURBULENCE WHEN THE DISCONNECT OCCURRED. GROUNDED - YES. PERFORMED DFCS BITE AND FOUND NO CURRENT FAULTS PER B737-900 FIM 22-11 TASK 801. FOUND DIFFESDR ASAA2019033028816Warning Light · false activationLEFT HAND PACK LIGHT ILLUMINATED ON RECALL AND EXTINGUISHED WITH MASTER CAUTION RESET. GROUNDED - YES. PERFORMED AMM TASK 21--61-00-700-806-002 PZTC BITE PROC. RESET & GREEN LIGHT SHOWN ON TEST. CHECKED GOOD. OPS NORMAL. CLEARED MEL 21-32B.SDR ASAA2019032228754Ignition Unit · inoperativeAPU FAULT ON START ILLUMINATED AFTER 5 MIN, FAULT LITE EXTINGUISHED. UPON RESTART APU LOW OIL PRESSURE ILLUMINATED. GROUNDED - YES. VERIFIED DISCREPANCY. ACCOMPLISHED FIM 49-40 TASK 805. FOUND IGNITION UNIT INOP. REMOVED AND REPLACED IGNITION UNIT REF AMM 49-4SDR ASAA2019021528215Starter · failedNO LIGHT OFF ON ENG START NR 2. ABORTED ENGINE START. GROUNDED - YES. REMOVED & REPLACED NR 2 ENG STARTER. OP CK & LEAK CK NORMAL. ACCOMPLISHED TWO STARTS. REF AMM 80-11-01-000-801-F00, 80-11-01-400-801-F00 & 71-00-00-800-811-F00.SDR ASAA2019021528189Warning System · false activationLEFT PACK ILLUMINATED DURING RECALL AFTER ENGINE START. PACK LIGHT EXTINGUISHED W/MASTER CAUTION RESET. GROUNDED - YES. TESTED THE PACK/ZONE TEMP CONTROLLER BITE TEST PER AMM 21-61-00-700-806-002. SRADA INLET SENSOR SHOWED A FAULT BUT CLEARED DURING VERIFY. THSDR ASAA2019021228160Probe · failedON PUSHBACK RT AUX PITOT LIGHT ILLUMINATED. GROUNDED - YES. REMOVED & REPLACED ALT PITOT PROBE REF AMM 34-11-01-000-801 & 400-801. ALT PITOT SYSTEM LK CK REF AMM 34-11-00-790-812. CKS GD.SDR ASAA201902128148Filter · trippedWHILE INVESTIGATING SUSPECTED APU OIL LEAKS APU FILTER (UNREADABLE), BYPASS BUTTON FOUND EXTENDED. GROUNDED - YES. DETERMINED FLUID ON THE APU EXHAUST CONE TO BE DEICE FLUID NO OIL LEAKS APU. REPLACED APU LUBE FILTER ELEMENT REF B737-900 AMM 49-91-12 INDICATORSDR ASAA2019011627835Autopilot Sys · malfunctionedIN APPROACH MODE AT 700' AGL, AUTOPILOT DIVERGED RIGHT ON LOCALIZER AND DISCONNECTED. GROUNDED - YES. ON DEFERRAL.SDR ASAA2019011627811Warning System · false activationLT PACK LIGHT ILLUMINATES WITH RECALL EXTINGUISHES WITH MASTER CAUTION RESET. GROUNDED - YES. BITE CHECKED NR 1 ZONE TEMP CONTROLLER REF FIM 21-62 TASK 801. PREV FLT FAULTS LT RAM AIR INLET ACT. PERF FIM 21-62 TASK 851. FAULT CLEARS & RAN MULTIPLE VERIFY TESTSSDR ASAA2019011227745Warning System · false activationAFTER START ON RECALL THE AFT CAB ZONE TEMP LIGHT ILLUMINATED. GROUNDED - YES. ACCOMPLISHED TEMP CONTROLLER BITE CHECK REF FIM TASK 21-61-00-810-801 NO FAULTS FOUND. NO HISTORY PAST 30 DAYS FOR AFT CABIN ZONE TEMP. GROUND VERIFICATION CHECKS NORMAL.SDR ASAA2019011227761Unknown · malfunctionedVTK DISPLAYED ON CAPTAINS ND FOLLOWED BY MAP FAILURE FLAGS. NO FMC DATA ON BOTH CDU'S. QRH CHECKLIST COMPLETED. FMC BOTH ON RIGHT FOR REMAINDER OF FLIGHT. GROUNDED - YES. LEFT FMC OPS CHECK GOOD. NO HISTORY 30 DAYS. REF AMM 34-61 TASK 801.SDR ASAA2019010527673Control Valve · failedRT PACK WONT COOL CABIN - PACK TEMP 96C AND CLIMBING. GROUNDED - YES. PERFORMED BITE TEST REF AMM 21-61-00 FAULTED BOTH TCV AND ZONE TRIM VALVE. REMOVED AND REPLACED TCV REF AMM 21-51-10 AND REMOVED AND REPLACED FWD CABIN TRIM VALVE REF AMM 21-51-04 OPS CHECK SDR ASAA2018123167576Acm · failedAS PER MEL 21-32B- WE TRIED TO RESET THE SYSTEM AND THE PACK LIGHT REMAINED ON. GROUNDED - YES. REPLACED R/H ACM PER B737-900 AMM 21-51-04 AND EA 900ER-2EA-21116. ACCOMPLISHED ICE PROTECTION SYSTEM INSP PER AMM 21-51-04-400-802-002 STEP G. 3 AND 5. NO DEFECTS.SDR ASAA2018122867590Duct · closedAFTER TAKEOFF THE "FWD CAB" ZONE TEMP LIGHT ILLUMINATED. AFTER RUNNING THE QRH, THE ZONE TEMP DID NOT GO OUT. THE FORWARD CABIN'S TEMP IS O/K AS PER THE FLIGHT ATTENDANT. GROUNDED - YES. CHECKED AND RELEASED PER MEL 21-1G, ONE PACK INOP RIGHT HAND, COMPLIED WISDR ASAA201812287549Actuator · faultedRIGHT PACK TRIP OFF LIGHT ON RECALL. GROUNDED - YES. PERFORMED BITE CHECK OF RH PACK/ZONE TEMP CONTROLLER PER B737-900 AMM 21-51-00/501. FOUND SRADA EXIT FAULT ILLUMINATED DURING PREV FLT. REPLACED R/H RAM AIR ACTUATOR (EXIT ACTUATOR) PER AMM 21-51-27 LINKAGE SDR ASAA2018122647547Acm · seizedRIGHT PACK LIGHT STAYS ILLUMINATED UPON ATTEMPT TO RESET PER MEL - 21-32B. GROUNDED - YES. BITE OF RH PACK ZONE TEMP CONTROL LOGGED - TCV, WILL NOT RESET. ON P5 PNL RH PACK LIGHT ONLY RESET WITH "TRIP" RESET BUTTON. DEACTIVATED RH PACK "TCV" TO CLOSED POSITIONSDR ASAA20181227564Fault Code · false indicationWHILE ACCOMPLISHING TC 78273000 FOUND FAULT 73-20021 ON #1 ENGINE. SHORT TIME FAULT INTERNAL EEC FAULT. DEFERRED PER TC 78273000. GROUNDED - YES. ACCOMPLISHED T/C 787273000 #1 ENGINE HAS NO RECENT FAULTS AND NOTHING IN FAULT HISTORY. ACCOMPLISHED EEC BITE PER
Back to N433AS