Boeing 737-490
Service difficulty reports · 3,288
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 = '737490' 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 = '737490' 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 ASAA2015110413641Acm · damagedLEFT ACM DAMAGED, DISCOVRED DURING PACK FLOW CONTROL VALVE CHANGE. ACFT GROUNDED. R & R LT ACM IAW AMM TASK 21-51-04-400-802-002 THROUGH STEP 31H, 7, I, 39071. COMPLETED STEPS I, J. LT ACM. OPS CK GOOD.SDR ASAA2015110313884Shear Tie · corrodedFWD CARGO BAY, BS 500 BETWEEN STRINGERS 27 - 28R AFT SIDE OF FRAME HAS CORROSION. ACFT GROUNDED. R & R FRAME ANGLE IAW SRM 51-40-02-0G-0.SDR ASAA2015103013870Web · crackedFWD CABIN AT BS 303 ON WEB ON 4L AREA IS CRACKED. ACFT GROUNDED. R & R WEB IAW SRMSDR ASAA2015103013819Stringer · crackedAFTER REMOVING STRINGER CLIP AT BS 380 S-8R STR WAS FOUND TO BE CRACKED. ACFT GROUNDED. REPAIRED STRINGER IAW ASA EA 400 53EA 16105, THIS IS A CATEGORY B REPAIR DTE FOR FIRST AND SECOND STAGE HAS BEEN GRANTED. THIRD STAGE APPROVAL IS REQUIRED PRIOR TO THE INSDR ASAA2015102813577Strap · crackedINTERCOSTAL STRAP AT BS 294, STRINGER 4L IS CRACKED. ACFT GROUNDED. FAB, LOCATED AND DRILLED NEW STRAP IAW SRM 51-40-05-0G-0.SDR ASAA2015102813576Skin · damagedRIGHT NOSE GEAR DOOR AND ADJACENT STRUCTURE DAMAGED. ACFT GROUNDED. INSTALLED REPAIR DOUBLER TO DAMAGED FUSELAGE SKIN AND REPLACED GEAR DOOR.SDR ASAA2015102713868Intercostal · crackedFWD WET AREA INTERCOSTAL CRACKED AROUND 2 FASTENER HOLES ON UPPER FLANGE BETWEEN BS 312-328 AT LBL44. ACFT GROUNDED. R & R INTERCOSTAL IAW SRM 51-40-02-0G-0.SDR ASAA2015102213832Fitting · crackedLEFT AFT LOWER HORIZONTAL THRUST BEAM FITTING IS CRACKED, REF TASK SB737-55-1091-400-1 STEP 17, REQUIRES ISSUANCE OF EC SB737-55-1091-400-2. ACFT GROUNDED. R & R HORIZONTAL STABILIZER UPPER AND LOWER LT CORNER FITTINGS IAW EA 400 55EA-16060.SDR ASAA2015102213598Angle · crackedPASSENGER CABIN FUSELAGE STIFFENER ANGLE CRACKED FWD OF R1 DOOR AT WL 240. ACFT GROUNDED. R & R ANGLE BETWEEN 12R AND 13R IAW SRM 51-40-02-0G-0.SDR ASAA2015102113837Frame · crackedFRAME AT BS IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15.SDR ASAA2015102113834Frame · crackedFRAME AT BS 907 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 400-53-107, REV 00, DATED 11SEP15, FIG 2.SDR ASAA2015102113831Frame · crackedFRAME AT BS 907 IS CRACKED BETWEEN S-8L AND S-9L. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400-53-107, REV 00, DATED 11SEP15.SDR ASAA2015102113830Frame · crackedFRAME AT BS 380 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609 S400-53-107, REV 00, DATED 11SEP15, FIG 2.SDR ASAA2015102113829Frame · crackedFRAME AT BS 480 IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20061609-400-53-107, REV 00, DATED 11SEP15, FIG 2.SDR ASAA2015102113828Frame · crackedFRAME AT BS 727F IS CRACKED BETWEEN S-8R AND S-9R. ACFT GROUNDED. REPAIRED FRAME IAW T/C AD20062609-400 -3-107, REV 00, DATED 11SEP15, FIG 2.SDR ASAA2015101713867Skin · delaminatedRT WING NR 4 L/E SLAT INBD T/E WEDGE HAS POSSIBLE AREA OF DELAMINATION AT EDGE, MARKED. ACFT GROUNDED. REPAIRED RT WING NR 4 SLAT L/E IB T/E WEDGE AT EDGE IAW SRM 51-70-10-2R-4 REPAIR 4.SDR ASAA2015100613345Fuel Nozzle · faultedNR 2 ENGINE LOGGED ECONOMIC FAULT 73-31372. ACFT GROUNDED. REPLACED UPPER 11 FUEL NOZZLES MONITORED IN THE UPPER SEGMENT, REF T/C PWRPL-73CMPT-07267-2.SDR ASAA2015100513347Lamp · failedEMERGENCY LIGHT EXIT LOCATOR SIGNS AT LT FORWARD, LT AFT, AND RT AFT OVERWING EXITS HAVE MULTIPLE LAMPS INOPERATIVE. ACFT GROUNDED. RELAMPED AND TESTED IAW MM 33-51-81-962-011. OPS NORMAL.SDR ASAA2015100113552Doubler · crackedL2 DOOR CUTOUT BEARSTRAP IS CRACKED AT THE FWD LOWER RADIUS. ACFT GROUNDED. REPAIRED L2 DOORWAY CUTOUT FWD, LOWER BEAR STRAP IAW SRM 53-00-01-2R-32, DETAIL IV. THIS IS A CAT B REPAIR WITH AN INSPECTION THRESHOLD OF 66,000 FLT. CYCLES AFTER AIRPLANE DELIVERYSDR ASAA2015100113536Stiffener · corrodedAPU TORQUE BOX CUTOUT AT 10888 BULKHEAD INBD STIFFENER FLANGE CORRODED. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-80-08-1A-1, FIG 11. NOTED G DETAIL VI R & R STIFFENER IAW SRM 51-40-02-0G-0, PARA 4, W .75", OSDR ASAA2015100113438Intercostal · corrodedFLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G2 INBD GALLEY MOUNT IS CORRODED. ACFT GROUNDED. REAMED HOLE FOR NUTPLATE ON FLOOR SUPPORT STRUCTURE AT APPROXIMATELY BS 360 JUST AFT OF G-2 INBD GALLEY MOUNT TO .261, CORROSION STIL EXISTS, OUT OF LSDR ASAA2015100113525Door Sill · corrodedL1 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. BLENDED CORRODED AREAS ON L1 MOPSILL, INNER CHORD OUT OF LIMITS, REMOVED AND INSTALLED NEW MOPSILL, INNER CHORD IAW SRM 53-10-15-1A-1, FIG 101, DETAIL IX, 51-40-02-0G-0, W 1.0, O .090, R .076SDR ASAA2015100113439Attach Angle · crackedINTERCOSTAL ATTACH ANGLE AT BS 348.2 STR 15L IS CRACKED. ACFT GROUNDED. REPAIRED IAW AD20121205-400-53-2.SDR ASAA2015093013594Floorbeam · corrodedBS 986 FLOORBEAM UPPER HORIZONTAL FLANGE HAS AREAS OF CORROSION. ACFT GROUNDED. REPAIRED FLOORBEAM IAW EA 400, 53EA 15973.SDR ASAA2015093013593Stringer · corrodedSTRINGER 21R AT BS 986 HAS LARGE AREA OF CORROSION. ACFT GROUNDED. REMOVED CORROSION AND CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-A-1. REMOVED, FABRICATED NEW AND INSTALLED NEW STIFFENER IAW SRM 51-40-02-0G-0, PARA 4 AND 7D SRM
51-40-05-0SDR ASAA2015093013533Frame · corrodedFRAME AT BS 992 HAS AREAS OF CORRODED JUST ABOVE L2 MOPSILL. ACFT GROUNDED. REPAIRED FRAME IAW EA 400 53EA, 15969. THIS IS A CAT B REPAIR WITH TRACKING IAW 400, 53DTI, 15970. INSPECTION THRESHOLD OF 66,000 FLT CYCLES, CURRENT FLT CYCLES AT TIME OF REPAIR ISSDR ASAA2015093013493Door Sill · corrodedL2 MOPSILL HAS AREAS OF CORROSION ON UPPER SURFACE. ACFT GROUNDED. R & R MOPSILL IAW SRM 51-40-02-0G-0 AND DWG NR 65-52878, W 5", O .071", R .060, L 1", D .011".SDR ASAA2015093013439Stringer Clip · crackedSTRINGER CLIP AT BS 947 AT 25R IS CRACKED. ACFT GROUNDED. REMOVED, LOCATED AND DRILLED NEW CLIP AND INSTALLED IAW SRM 51-40-02-0G-0, 51-40-05-0G-0.SDR ASAA2015093013453Frame · crackedFRAME AT BS 400 BETWEEN STRINGERS 8-9L IS CRACKED. ACFT GROUNDED. REPAIRED THE FRAME IAW TC QAD20062609 400-53-107, FIG 2.SDR ASAA2015093013451Angle · crackedINTERCOSTAL AT BS 727A AT 25R HAS A CRACKED ATTACH ANGLE. ACFT GROUNDED. REMOVED ANGLE IAW SRM 51-40-02-0G-0, FIG 8 INSTALLED NEW ANGLE IAW SRM 51-40-02-0G-0, PARA 4.SDR ASAA2015092913578Spar · corrodedRIGHT HORIZONTAL STABILIZER AFT UPPER ATTACH LUG, STABILIZER SIDE, HAS CORROSION ON AFT FACE. ACFT GROUNDED. REPAIRED RT HORIZONTAL STABILIZER AFT UPPER ATTACH LOG CORROSION IAW EA COMPARTMENT 55 EA 15987.SDR ASAA2015092913472Stringer · corrodedSTRINGER AT BS 500G AT 27R IS CORRODED AROUND DOMENUT. ACFT GROUNDED. REMOVED CORRODED FROM STR 27R AT BS 500G FOUND TO BE OUT OF LIMITS IAW SRM 53-00-03-1A-1, FIG 101, DETAIL II, REPAIRED STR 27R AT BS 500G IAW SRM 53-30-03-2R-1, REPAIR 1, W 1.00, O .063, RSDR ASAA2015092913454Attach Angle · crackedINTERCOSTAL AT BS 500E AT 26R HAS A CRACKED ATTACHED ANGLE. ACFT GROUNDED. R & R ATTACH ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.SDR ASAA2015092913452Angle · crackedINTERCOSTAL AT BS 500E AT 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.SDR ASAA2015092913438Beam · crackedAFT CARGO DOOR FWD END E BEAM OUTER ANGLE IS CRACKED AT 3RD FASTENER AFT VERTICAL LEG. ACFT GROUNDED. REPAIRED AFT CARGO DOOR FWD END E BEAM OUTER ANGLE IAW T/C AD20131312-400-52-15, REV 00, DATED 18AUG14 AND DWG 65C37547.SDR ASAA2015092913362Angle · crackedINTERCOSTAL AT BS 500F 26L HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PARA 4 AND 7D.SDR ASAA2015092913361Angle · crackedINTERCOSTAL AT BS 500F AT 26R HAS A CRACKED ANGLE. ACFT GROUNDED. R & R ANGLE IAW SRM 51-40-02-0G-0, PAR 4 AND 7D.SDR ASAA2015092213173Blade · wornNR 1 ENGINE FAN BLADE PLATFORM SEALS MISSING OVER 42", EXCEEDS MM 72-21-02 ALLOWABLE LIMITS OF 39.37. ACFT GROUNDED. REPLACED ALL 24 PLATFORMS ON NR 1 ENGINE REF TASK CARD NR 78472002.SDR ASAA2015092213172Spinner · wornNR 1 ENGINE SPINNER CONE WHITE PAINT WORN IN SEVERAL SPOTS. ACFT GROUNDED. R & R NR 1 ENGINE SPINNER CONE REF MM 72-21-01.SDR ASAA2015091515288Bear Strap · crackedFOUND GOUGE/DENT ON INTERIOR FUSELAGE SKIN NEAR UPPER FUSELAGE ASSIST SPRING HINGE SPIGOT. L1 DOOR MIG 2C 317241 INITIATED. ACFT GROUNDED. RESOLVED ON W/O: 321296 TASKCARD: N/R-00011. REPAIRED FUSELAGE SKIN AND BEAR STRAP AT L1 DOOR UPPER HINGE CUTOUT IAW SDR ASAA2015091013144Structure · crackedLIGHTNING HOLE AT AFT TAIL COMPARTMENT ENTRANCE BELOW LEFT CABLE PULLEY BRACKET IS CRACKED. ACFT GROUNDED. REPAIRED LIGHTNING HOLE IN WEB SUPPORT ASSY AT BS 1040 IN AFT TAIL COMPARTMENT IAW EA 400-53EA-15819.SDR ASAA2015090312922Satcom · lockedSATCOM LOCKUP, ACFT GROUNDED. RESET, NORMAL OPS, PERFORMED SAT SYS, TEST REF 23-15-00. SYS CKS NORMAL.SDR ASAA2015082012954Floor Support · bentAFT CARGO COMPARTMENT, LT FLOOR SUPPORT INTERCOSTAL BS 727A-727B IS BENT. ACFT GROUNDED. R & R FLOOR SUPPORT INTERCOSTAL AT BS 727A-727B IAW SRM 51-10-02, PARA NR 8 SRM 51-40-05 , DWG 69-16500 REV:D AND REAPPLIED CIC IAW AMM 51-21-91.SDR ASAA2015081212898Light · failedF/A REPORTS FWD LT OVERWING EMERGENCY EXIT TRACK LIGHTING LENS WILL NOT STAY ON. ACFT GROUNDED. REPLACED FWD LT OVERWING EMERGENCY EXIT TRACK LIGHTING ASSY. OPS CHECK SAME GOOD.SDR ASAA2015080712785Guide Arm · lack of lubeL1 DOOR WOULD NOT OPEN AFTER MULTIPLE ATTEMPS. HANDLE LOCKED IN INTERMEDIATE POSITION AND COULD NOT BE FULLY ROTATE. ACFT GROUNDED. REMOVED DEBRIS AND LUBRICATED GUIDE ARM ECCENTRIC TRACK. DOOR OPERATES NORMALLY.SDR ASAA2015080712790Hmu · faultedENGINEERING REQUESTS NR 2 ENGINE HMU REPLACEMENT FOR CONTINUING HPT ACCV FAULTS. ACFT GROUNDED. REPLACED NR 2 ENGINE HMU IAW TASK CARDS N8473000, N8473001. NO RECENT OR FAULT HISTORY NOTED PRIOR TO HMU INSTALLATION TESTS.SDR ASAA2015080712767Light · inoperativeMODE CONTROL PANEL DISENGAGE LIGHTS INOPERATIVE. ACFT GROUNDED. REPLACED MCP IAW AMM 22-11-34-000-801. ACCOMPLISHED OPS CHECKS TO AMM 22-11-34-740-801 AND ADDITIONAL TESTS BITE GROUP NR 32, NR 49. DFCS LRU INTERFACE TEST FOR MCP, LAND VERIFY TEST AND HOUSISDR ASAA2015080512744Gcu · failedWITH APU RUNNING, NO VOLTS OR FREQUENCIES, APU WILL NOT GO ONLINE. ACFT GROUNDED. REMOVED AND RE-INSTALLED APU GCU IAW MM 24-21-81-400-801. FOUND S16 BAD, R & R APU REMOTE CONTROL PANEL IAW MM 26-22-03-400-801. ACCOMPLISHED APU FIRE EXTINGUISHING BOTTLE SQSDR ASAA2015080312704Generator · malfunctionedAFTER LANDING APU STARTED NORMALLY BUT APU GEN SHOWED NO VOLTS, NO FREQ'S WITH BLUE APU OFF, BUS LIGHT ILLUMINATED. ALL C/B'S CHECKED IN. APU GENERATOR WOULD NOT SWITCH ON & TAKE POWER. ACFT ACCEPTED GROUND POWER OK. ACFT GROUNDED. ACCOMPLISHED APU OPS TESSDR ASAA2015073112662Fmc · malfunctionedSINGLE FMC FAIL, CAPTAIN SIDE. ACFT GROUNDED. ACCOMPLISHED FMC BITE, IAW FIM 34-61, TASK 801. NO FAULTS. GROUND VERIFICATION ACCOMPLISHED.
Back to Boeing 737-490