Boeing 737-83N
Service difficulty reports · 1,087
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 = '73783N' 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 = '73783N' 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 ASMF201203001Switch · out of adjustACFT RETURNED TO DEPARTURE, DURING CLIMB, THE MLG DID NOT RETRACT; SO FLIGHT CREW ACCOMPLISHED THE QRH 14.16 PROCEDURE, CONFIRMING THE FAILURE. ACFT WAS SENT TO THE HANGAR AND MX PERSONNEL PERFORMED A REVISION DETECTING THE MANUAL EXTENSION ACCESS DOOR SWITCHSDR ASMF201202005Bellcrank · brokenCAPTAIN REPORTED THAT DURING TAKEOFF, THE ACFT REQUIRED 3 UNITS TO THE LEFT OF RUDDER TRIM. DURING MX REVIEW, THE RT OTBD FLAP, INBD BELLCRANK WAS FOUND BROKEN. THE RT OTBD FLAP, INBD BELLCRANK WAS REPLACED IAW MM 27-51-24, TESTED CORRECT.SDR ASMF201202004Fseu · damagedCAPTAIN REPORTED THAT DURING APPROACH, FLAPS DID NOT EXTEND, FLIGHT CREW ACCOMPLISHED QRH 9.4 PROCEDURE, CONFIRMING THE FAILURE. MX REPLACED THE FLAP SLAT ELECTRONIC UNIT IAW MM 27-51-01, TESTED CORRECT.SDR MYWA110134Engine · vibrationETOPS SIGNIFICANT SYSTEM: NR 1 ENG VIBRATION ERRATIC FROM OFF BACK LOW TO OFF SCALE HIGH. NO VIBRATION NOTED BY CREW.SDR ASMF201109006Pump · damagedCAPTAIN REPORTED THAT DURING APPROACH LANDING GEAR HANDLE HAD NOT MOVED EVEN THROUGH LOCK OVERRIDE HANDLE WAS MOVED; FLIGHT CREW ACCOMPLISHED THE QRH 14.10 PROCEDURE AND MANUAL GEAR EXTENSION WAS PERFORMED. MX REPLACED THE EMDP SYS A IAW M 29-11-21 AND EXTENSSDR ASMF201109003Actuator · leakingDURING OVERNIGHT CHECK, A HYD LEAK WAS DETECTED IN THE LT ELEVATOR TAB LOCK ACTUATOR. THE LT ELEVATOR TAB LOCK ACTUATOR WAS REPLACED IAW MM 27-31-34 AND OPS TEST WAS PERFORMED IAW MM 27-31-00-700-815, ALL CORRECT.SDR ASMF201109001Skin · dentedDURING TRANSIT CHECK, MX DETECTED 2 DENTS IN THE LT HORIZ STABILIZER L/E AT STATION 59.5 OF 5.5" LONG, 2.125" WIDE AND 0.135" DEPTH; OTHER OF 4.5" LONG, 2.0" WIDE AND 0.120" DEPTH. MX CONFIRMED THAT THE DENTS WERE WITHIN LIMITS IAW SRM 55-10-01 PARAGRAPH 4.D,SDR ASMF201107011Structure · damagedDURING TRANSIT CHECK, THE LT AFT CABIN DOOR WAS DAMAGED. MX PERFORMED VISUAL INSPECTION TO LT AFT ENTRY STRUCTURE DOOR IAW MM 52-13-00 DETECTING DAMAGES OUT OF LIMIT IN THE DOOR COVER AND THE LATERAL STRIPS OF THE COVER DOOR WERE BENT. TECH REPAIRED THE DOORSDR ASMF201107009Pump · damagedACFT REJECTED TAKEOFF AT LESS THAN 70 KNOTS WITH GROSS WEIGHT OF 58764 KG DUE TO LEFT ENGINE NOT REACHING THRUST, 101PERCENT REQUIRED, ONLY IT REACHED 90 PERCENT THRUST WITH ATS SET AND OFF. MX PERFORMED BITE IN EEC IAW MM 73-21-00 AND BITE TO THE ATS WAS PERFSDR ASMF201107008Engine · malfunctionedACFT REJECTED TAKEOFF AT 80 KNOTS AND GROSS WEIGHT OF 67 870 KG DUE TO THRUST ASYMMETRY OF 97 PERCENT N2 ON LT ENGINE AND 103 PERCENT N2 ON RT ENGINE AND LT THRUST LEVEL CUT BACK AUTOMATICALLY AFTER TRYING TO EQUAL POWER. MX PERFORMED BITE IN EEC IAW MM 73-21SDR MYWA090101Trim Motor · inoperativeSTAB TRIM FAIL AFTER TAKEOFF. ACFT RETURNED TO BLOCK. MX CLEANED AND INSPECTED CONNECTOR PLUG TO STAB TRIM MOTOR. OPS CHECK GOOD, RETURN TO SERVICE. ACFT ARRIVED, UPON TAXI, STAB TRIM FAILED. MX REMOVED AND REPLACED STAB TRIM MOTOR. ACFT HAS FLOWN WITH NO MOSDR 2008FA0000465Floorbeam · corrodedDURING SCHEDULED INS, FUND FWD CABIN BS 344, LBL10, FLOORBEAM CORRODED. (K) SO 245010, NR27110SDR 2008FA0000464Floorbeam · chafedDURING SCHEDULED INSP, FOUND CLIP NUTS CHAFING FLOORBEAM IN FWD CABIN BS 344, LBL 0 TO LBL 55. (K)SDR 2008FA0000462Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AT BS 328, RBL 26 AFT SIDE OF BEAM FOUND TO BE BEYOND LIMITS. (K)SDR 2008FA0000463Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AT BS 328 FROM RBL 13 TO RBL 50. (K)SDR 2008FA0000461Floorbeam · corrodedDURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN FWD WET AREA ON FLOORBEAM AROUND FASTENERS AT BS 294 FROM RBL-2 TO RBL 43. SO NR 245010 NR 27077. (K)SDR 2008FA0000402Floorbeam · corrodedDURING SCHEDULED INSPECTION, FOUND CORROSION ON AFT CABIN FLOORBEAM, BS947, RBL 5 TO LBL5. S/O 245009, N/R 26378 (K)SDR 2008FA0000401Skin · dentedDURING SCHEDULED INSPECTION, FOUND DENT IN LT L/E OF HORIZ STAB STA 105. S/O 245008, N/R 21591. S/O 245008, N/R 21591. (K)SDR 2008FA0000400Skin · dented(REF DU4R2008227) DURING SCHEDULED INSPECTION, FOUND OUT OF LIMITS DENT IN LT HORIZ STAB L/E STA 280. S/O 245008, N/R 21578 (K)SDR 2008FA0000399Floorbeam · corroded(DU4R2008226) DURING SCHEDULED INSP, FOUND CORROSION IN PAX CABIN WET AREA ON FLOORBEAM FASTENERS AND FASTENER HOLES AT BS 986 FORM RBL45 TO LBL 45. S/O 245010 , N/R 27072 (K)SDR 2008FA0000398Nut Clip · chafed(DU4R2008225) DURING SCHEDULED INSP, FOUND AFT CABIN BS 967, RBL 24, TO LBL 49 FLOORBOARD ATTACH POINTS, CLIP NUTS HAVE WORN GROOVES/CHAFE MARKS. S/O NR 245010, N/R NR27070 (K)SDR 2008FA0000397Skin · dented(DU4R2008223) DURING SCHEDULED INSPECTION, FOUND DENT IN AFT CARGO DOOR (C-2) EXT. SKIN. S/O NR 245010, N/R 26678. (K)SDR 2008FA0000396Skin · dented(REDF DU4R2008222) DURING SCHEDULED INSPECTION FOUND DENT IN EXT SKIN OF C-1 DOOR 25 INCH DOWN FROM TOP EDGE OF DOOR AND 22 INCHES AFT FROM FWD EDGE OF DOOR. (K)SDR 2008FA0000395Skin · dented(DU4R2008221) DURING SCHEDULED INSPECTION, FOUND AFT CARGO DOOR EXT SKIN HAS DENT 11 INCHES AFT FROM FWD EDGE 5 INCHS UP FROM BOTTOM EDGE WIDTH OF DENT 1.25 INCHES OF DENT .070 INCH W/Y=17 DENT MEASURES WITH DEPTH GUAGE A-1979. S/O NR 245010, OPS NR 26681. (SDR 2008FA0000394Floor Support · corroded(REF DU4R2008220) DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT CABIN. STA 340, LBL 11. (K)SDR 2008FA0000391Floor Support · corroded(REF DU4R2008219) DURING SCHEDULED INSPECTION, FOUND CORROSION ON FLOOR SUPPORT CABIN STA 344, BL-0 TO BL-12L. (K)SDR AMTA200800246Fmc · unserviceableSINGLE FMC FAILURE. REMOVED AND REPLACED FMCS COMPUTER IAW 34-61-02-4. OPS NORMAL. (K)SDR AMTA200800245Battery · dischargedFWD EMERGENCY FLASH LIGHT BATTERY NEEDS REPLACING. REMOVED AND REPLACED FWD EMERGENCY FLASH LIGHT BATTERY IAW AMM 25-64-00-900-806, OPS CHECK GOOD. (K)SDR AMTA200800244Battery Pack · inoperativeEMERGENCY FLASH LIGHT AT L2 DOOR IB RED LIGHT IS NOT FLASHING. REMOVED AND REPLACED POWER SUPPLY PACK, SECURED AND OPS CHECK OK. (K)SDR AMTA200800240Apu · damagedDURING TAXI OUT, APU MAINT LIGHT ILLUMINATED, RETURNED TO GATE. INSTALLED MISSING HARDWARE AND REPLACED BENT WASHERS. REINSTALLED ACTUATOR ARMS IAW AMM 49-15-31-4. OPS CHECK APU NO MANT MSG NOTICE ON OVERHEAD. CURRENT STATUS SHOWED NO FLIGHT DECK LIGHT WITSDR AMTA200800241Transceiver · unserviceableON HFI, NO LIGHT, NO CHIME ON SELCAL CONTROL PANEL SIGNAL WEAK. REMOVED AND REPLACED NR 1 HF TRANSCEIVER IAW AMM 23-11-21-4. CALLED SFO RADIO AND RECEIVED SELCAL FROM THE M. GOT LIGHT AND CHIME. (K)SDR AMTA200800238Fmc · unserviceableSINGLE FMC FAILURE. REMOVED AND REPLACED NEW RT FMC IAW AMM 34-61-02-4. OPS CHECK NORMAL. (K)SDR AMTA200800237Converter · unserviceableDURING ETOPS PREDEPARTURE CHECK, FOUND MSG NR 49-41-244 FOR APU BITE TEST. START CONVERTER SHOWS FAILED GENERATOR DIODE. T/S IAW FIM 49-40-00-810-806. FOUND START CONVERTER UNIT FAILED. REMOVED AND REPLACED START CONVERTER UIT IAW MM 49-41-61. OPS CHECK GSDR AMTA200800239Switch · malfunctionedAPU MAINT LIGHTS ON. REMOVED AND REPLACED APU AIR INLET DOOR SWITCH REF A MM 49-15-41-4. OPS NORMAL. REMOVED PLACARD. (K)SDR AMTA200800233Bleed Air Sys · malfunctionedAFTER DEPARTURE LT BLEED TRIP WOULD NOT RESET. RE-ACTIVATED HIGH STAGE VALVE, ACTURATED VALVE SEVERAL TIMES, NO FAULTS NOTED. PERFORMED NR1 ENG BLEED SYSTEM HEALTH CHECK IAW 36-11-00-5, NO FAULTS. (K)SDR AMTA200800230Charger · faultyISFD BATTERY FAULT LIGHT ON. REMOVED AND REPLACED ISFD BATTERY CHARGER OPS CHECK GOOD NO FAULT LIGHT. (K)SDR AMTA200800229Battery · unsecureISFD WENT BLANK WITH NOSE WHEEL TOUCHDOWN. FOUND ISFD BATTERY NOT SEATED IN RACK. SECURED ISFD BATTERY. OPS TEST IAW FIM 34-24-00-810-804. OK FOR SERVICE. (K)SDR AMTA200800228Battery · unsecureISFD WENT BLACK WITH NOSE WHEEL TOUCHDOWN. FOUND ISFD BATTERY NOT SEATED IN RACK. SECURED ISFD BATTERY. OPS TEST IAW FIM 34-24-00-810-804. OK FOR SERVICE. (K)SDR AMTA200800227Indicator · unserviceableSTANDBY ATTITUDE INDICATOR GYRO FLAG SHOWS AND WILL NOT ALINE. REMOVED AND REPLACED STANDBY ATTITUDE INDICATOR REF AMM 34-24-01-4 AND TESTED REF AMM 34-24-00-5. OPS CHECK GOOD. (K)SDR AMTA200800231Vane · inoperativeNR 1 ENGINE ONLY WENT UP TO 75 PERCENT ON TAKEOFF AND KICKED OFF AUTO THROTTLES MX POWER 101.8 PERCENT, NR 2 ENG GOOD. DURING MANUAL ACTUATION TEST, FOUND RT VSV NOT OPENING, ON NR 1 ENG, BLED THE SYSTEM, PERFORMED MANUAL ACTUATION, RT VSV, OPS NORMAL IAW 75-SDR AMTA200800222Lens · distortedLT AFT ENTRY DOOR EGRESS LENS UNREADABLE. REMOVED AND REPLACED LENS ASSY. REQ`D OPS CK NORMAL. (K)SDR AMTA200800202Unknown · unknownAC DID NOT PRESSURIZE AFTER TAKEOFF, NON NORMAL CHECKLIST NO HELP. LOUD NOISE IN FWD CABIN NEAR L1 NO DOOR LIGHTS. NO WARNING LIGHTS. PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CK IAW AMM 05-51-91-2. AC PRESSURIZED NORMAL, NO EXCESSIVE LEAKS NOTED, PERFOMESDR AMTA200800200Cargo Track · corrodedRAIL ASSY RBL 8.1 STA, 767 HAVE A UNIFORM CORROSION AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL ASSY, ORG MAT .071, MAT LOSS .030, REM MAT .041, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1510-1355 IAW EA 737-SDR AMTA200800199Rail · corrodedRAIL ASSY LBL 3.0, STA 767, HAVE A LIGHT CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL ASSY, ORG MAT .071, MAT LOSS .025, REM MAT .046, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1510-1355 IAW EA 737-SDR AMTA200800198Rail · corrodedRAIL ASSY LBL 8.1, STA 767, HAVE A UNIFORM CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL, ORG MAT .071, MAT LOSS .030, REM MAT .041, FOUND TO OUT OF LIMITS IAW SRM 53-00-53-1A. DETAIL D, FABRICATED REPAIR PART FROM BAC 1510-1355 IAW EA 737-5300SDR AMTA200800197Rail · corrodedRAIL ASSY LBL 17.24, STA 767 HAVE A LIGHT CORROSION, AFT CARGO COMPARTMENT AREA. REMOVED CORROSION ON RAIL, ORG MAT .071, MAT LOSS .017, REM MAT.054, FOUND TO BE OUT LIMITS IAW SRM 53-00-53-1A DETAILED FABRICATED REPAIR PART FROM BAC 1509-100688 IAW EA 737-53SDR AMTA200800196Rail · corrodedRAIL ASSY LBL 12.5, STA 767 HAVE A UNIFORM CORROSION, AFT CARGO COMPARTMENT. REMOVED CORROSION ON RAIL, ORG MAT .071, MAT LOSS .014, REM MAT .057, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A DETAIL D, FABRICATED REPAIR PART FROM BAC 1510-1355 IAW EA 737-530SDR AMTA200800195Floor Support · corrodedNUTPLATE AREA BETWEEN STA 827 AND 807, RBL 13.84. HAS LIGHT CORROSION. REMOVED LIGHT CORROSION, ORG MAT .071, MAT LOSS .025, REM MAT .046, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2, FABRICATED REPAIR STRAP FROM 7075-T6, .071 IAW EA 737-5300-08-A0038. SDR AMTA200800194Rail · corrodedRAIL ASSY LBL 8.1, STA 727I (T-UNION) AREA HAS LIGHT CORROSION. REMOVED CORROSION ON RAIL, OR MAT .071, MAT LOSS .012, REM MAT .059, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A, FIG 103, DETAIL D, FABRICATED REPAIR IAW SRM 53-00-53-2R2, TABLE 201 AND EA 737SDR AMTA200800190Rail · out of limitsRAIL ASSY RBL 13.84, STA 727I (T-UNION) AREA, ORG MAT .071, MAT LOSS .034, REM MAT .037, FOUND TO BE OUT OF LIMITS, IAW SRM 53-00-53-1A, FIG 103, DETAIL D, FABRICATED REPAIR PART FROM BAC 1509-100688 IAW EA 737-08-A0037. (K)
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