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.

SDR AMTA200600450Regulator · unserviceableENG DUCT PRESSURE SPLIT. REMOVED AND REPLACED BLEED AIR REGULATOR ON NR 2 ENGINE, OPS CHECKED NORMAL IAW MM. (K)Jul 27, 2006 · N318TZ · Boeing 73783N · Pneumatic Distribution SystemSDR AMTA200600447Coupler · unserviceableRECEPTION ON BOTH HF RADIOS GARBLED AND COMPLETELY UNREADABLE ON ALL FREQ`S. REMOVED AND REPLACED NR 1 HF COUPLER OPS CHECK GOOD IAW MM. NR 2 HF OPS CHECK GOOD ON GROUND. (K)Jul 25, 2006 · N323TZ · Boeing 73783N · Communications System WiringSDR AMTA200600446Shutoff Valve · unserviceableRT DUCT PRESSURE = 20 PSI, LT DUCT PRESSURE= 40 PSI BOTH IN CLIMP AND CRUISE. REMOVED AND REPLACED PRSOV VALVE AND OPS CHECKED NORMAL IAW MM. A/C OK FOR SERVICE. (K)Jul 25, 2006 · N318TZ · Boeing 73783N · Pneumatic Distribution SystemSDR AMTA200600444Warning Light · unknownLT NR 1 REVERSER LIGHT REMAINED ILLUMINATED DURING TAXI IN AND AFTER ENGINE SHUTDOWN. PERFORMED EAU BITE PROCEDURE IAW OF MM REST NO CURRENT FAULT SHOWN OK FOR CONTINUED SERVICE. (K)Jul 24, 2006 · N305TZ · Boeing 73783N · Central WarningSDR AMTA200600427Actuator · unserviceableON CLIMB OUT PASSING 4500 FT 250 KIAS, CAPT AND OF ELECTRIC TRIM DID NOT RESPOND. ALL STAB TRIM SWITCH IN NORMAL. STAB TRIM WHEEL WORKS NORMAL. PERFORMED FIM, NO FAULTS NOTED ALL OPS NORMAL. REMOVED AND REPLACED STAB TRIM MOTOR FOR PRECAUTIONARY REASON IAWJul 8, 2006 · N315TZ · Boeing 73783N · Stabilizer ActuatorSDR AMTA200600426Display · malfunctionedSTANDBY FLIGHT DISPLAY INTERGRATED (ISFD) ATT FLAG SHOWS. PERFORMED FIM, NO DEFECTS NOTED, OK FOR SERVICE. (K)Jul 8, 2006 · N314TZ · Boeing 73783N · Central DisplaySDR AMTA200600425Warning Light · false indicationRT PACK LIGHT CAME ON AFTER TAKEOFF. LIGHT STAYED OUT AFTER RESET. PERFORMED BITE CHECK ON BOTH CONTROLLER NO FAULTS. INSPECT PACK INLET/EXHAUST NO OBSTRUCTIONS. PACK CHECKS NORMAL ON GROUND AT MDW AMM. (K)Jul 8, 2006 · N310TZ · Boeing 73783N · Cabin Temperature Control SystemSDR AMTA200600423Warning System · malfunctionedAFTER LANDING NR 1 ENG (ENGINE CONTROL) LIGHT AND NR 1 ENG (REVERSER) LIGHT ILLUMINATED. T/S IAW FIM. OPS CK OF NR 1 ENG FAULT MSG CLEARED, RAN T/R NO LIGHS OR FAULT MSG, OK FOR SERVICE. (K)Jul 5, 2006 · N315TZ · Boeing 73783N · Engine Thrust ReverserSDR AMTA200600420Warning System · malfunctionedSINGLE FMC OPERATION MESSAGE DISPLAYED ON THE CDU. TROUBLESHOT IAW FIM, RELOADED SOFTWARE IAW MM. SYSTEM OPS CHECK NORMAL, NO MESSAGES OK FOR SERVICE. (K)Jul 1, 2006 · N314TZ · Boeing 73783N · Central WarningSDR AMTA200600419Battery · damagedFLASHLIGHT UNDER FORWARD IB F/A JUMPSEAT, RED LIGHT NOT FLASHING. REMOVED AND REPAIRED BATTERY ON FLASHLIGHT, OPS NORMAL. (K)Jul 1, 2006 · N304TZ · Boeing 73783N · Emergency EquipmentSDR AMTA200600418Fmc · malfunctionedRT FMC FAILED IN FLIGHT. RERACKED FMC COMPUTER. PERFORMED FIM. OPS CHECK NORMAL. (K)Jun 29, 2006 · N315TZ · Boeing 73783N · Flight Management Computing Hardware SystemSDR AMTA200600405Valve · malfunctionedLT AND RT DUCT PRESSURE POINTERS SPLIT WITH ENG BLEED ON, APU BLEED OFF. N1 89.0 EACH SIDE LT 40 PSI, RT 30 PSI FL370 WITH WING A/I ON BOTH LT AND RT = 28 PSI. T/S IAW FIM 361000810804 FOUND HIGH STAGE VALVE IAW MM. (K)Jun 19, 2006 · N318TZ · Boeing 73783N · Pneumatic Distribution SystemSDR AMTA200600404Lens · missing12 DEF LENS MISSING ON EMERGENCY EXIT LIGHT FOR THE OVERWING EXIT. REMOVED AND REPLACED EMERGENCY EXIT SIGN, OPS CHECKED GOOD. (K)Jun 19, 2006 · N304TZ · Boeing 73783N · Emergency LightingSDR AMTA200600403Acm · malfunctionedLT PACK OVER TEMP. REMOVED AND REPLACED LT PACK ACM IAW MM 21-51-04. NO LEAKS NOTED, OK FOR SERVICE. (K)Jun 19, 2006 · N304TZ · Boeing 73783N · Cabin Cooling SystemSDR AMTA200600402Control Valve · malfunctionedLT PACK LIGHT ILLUMINATES ON RECALL GOES OUT WITH RESET. REMOVED AND REPLACED NR 1 TEMP CONTROL VALVE. IAW MM. OPERATIONAL CHECK NORMAL. OK FOR SERVICE. (K)Jun 18, 2006 · N321TZ · Boeing 73783N · Cabin Cooling SystemSDR AMTA200600401Controller · failedLT SIDE WINDOW HEAT (OFF) LIGHT ILLUMINATED DURING DESCENT. PERFORMED BIT TEST, NO FAULT NOTICED AT THIS TIME. SWAPED LT HEAT CONTROLLER WITH RT HEAT CONTROLLER FOR FURTHER T/S. (K)Jun 16, 2006 · N319TZ · Boeing 73783N · Windshield/Door Rain/Ice RemovalSDR AMTA200600399Indication Sys · malfunctionedWITH APU ON SPEED, THE APU GEN OFF BUSS LIGHT DOES NOT ILLUMINATE. T/S IAW FIM, APU GEN OFF BUSS LIGHT OPERATES NORMAL, NO FAULTS NOTED. (K)Jun 14, 2006 · N317TZ · Boeing 73783N · Airborne Auxiliary Power Unit (APU) SystemSDR AMTA200600394Indication Sys · malfunctionedAPU GEN OFF BUSS LIGHT NOT ON, APU SPEED AT 95 PERCENT. PERFORMED RESET IAW FIM. NO DEFECTS NOTED. (K)Jun 12, 2006 · N317TZ · Boeing 73783N · Airborne Auxiliary Power Unit (APU) SystemSDR AMTA200600389Drive Assy · unserviceableON DESCENT INTO MMGL TURNED ON RADAR AND GOT PWS FAIL, WXR FAIL, ANT ON IB FLIGHT DISPLAY. DRIVE UINT WILL NOT SWEEP. REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE UNIT. IAW MM. OPERATIONAL CHECK NORMAL. OK FOR SERVICE. (K)Jun 11, 2006 · N305TZ · Boeing 73783N · Inertial Guidance SystemSDR AMTA200600391Transceiver · failedWX RADAR FAIL AND PWS FAIL AMBER LIGHT AMBER LIGHT REMAINS ILLUMINATED DURING FLT NO WX RADAR. REMOVED AND REPLACED WEATHER RADAR RECEIVER/ TRANSMITTER ALL SYS OPS CKD NORMAL IAW MM. (K)Jun 10, 2006 · N323TZ · Boeing 73783N · Weather Radar SystemSDR AMTA200600390Fmc · malfunctionedBOTH FMC DISPLAYS FROZE UP. RESET BOTH FMC COMPUTERS. BOTH FMC OPERATES NORMAL. (K)Jun 10, 2006 · N315TZ · Boeing 73783N · Flight Management Computing Hardware SystemSDR AMTA200600388Drive Unit · failedGATE RETURN. WEATHER RADAR FAILED. PWS FAIL AND WXR FAIL DISPLAYED. REMOVED AND REPLACED WEATHER RADAR ANTENNA DRIVE UNIT ASSY. IAW AMM 34-41-11-4. INSTALLATION TEST OK. (K)Jun 10, 2006 · N305TZ · Boeing 73783N · Weather Radar SystemSDR AMTA200600379Pin · corrodedDURING ACCOMPLISHMENT OF EO, FOUND THE LT SIDE PINS (5) CORRODED OR WORN AND FOUND THE RT SIDE PINS (4) CORRODED OR WORN. REMOVED AND REPLACED ALL 10 MOUNT PIN IAW EO. (K)Jun 3, 2006 · N315TZ · Boeing 73783N · Fuselage Structure (General)SDR AMTA200600372Floor Panel · corrodedFWD CARGO FLOOR PANEL 120BF BOTTOM SIDE HAS CORROSION (LIGHT) SEVERAL AREAS MAINLY AROUND FASTNER HOLES BS 440-500. REMOVED CORROSION ON BOTTOM SIDE OF FLOOR PANEL 120 BF 13 PLACES LENGTH 2 INCHES X 2 INCHES. ORIGINAL THICK .080 MATERIAL LOSS .006-.010. FOUJun 1, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600371Floor Panel · corrodedFWD CARGO FLOOR PANEL 120BF UPPER SURFACE HAS LIGHT CORROSION AT END FULL WIDTH OF PANEL AND ALONG LT SIDE FULL LENGTH. REMOVED CORROSION UPPER SURFACE OF FLOOR PANEL 120 BF PANEL 75 W 37 AREA REWORKED 756 SQ INCHES MAX ALLOWED 832.5 WITHIN LIMITS. (K)Jun 1, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600370Structure · corrodedLT VERT STAB LOWER STRUCTURE AT BASE OF STAB WHERE PANEL 9501 ATTACHES STA APP 1052-1088-36 INCHES OF BARE METAL AND 2 AREAS OF FRETTING CORROSION IAW MM. REMOVED FRETTING CORROSION LT VERT STAB LOWER BASE STRUCTURE AT PANEL 9501, SRM. ORIG THICK .071 MTL LOJun 1, 2006 · N315TZ · Boeing 73783N · Vertical Stabilizer Miscellaneous StructureSDR AMTA200600369Floor Panel · corrodedFWD PIT METAL FLOOR PANEL 120DF HAS SURFACE CORROSION, NUMEROUS AREAS MARKED ON BOTTOM OF PANEL. BLENDED MARKED AREAS ON BOTTOM OF PANEL, PANEL 120DF L=114 INCHES, W=46 INCHES. AREAS REWORKED 41 SQ INCHES. MAX ALLOWED 1641.6 SQ INCHES WITHIN LIGHTS IAW SRM.Jun 1, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600368Floor Panel · gougedFWD CARGO CENTER FLOOR PANEL HAS GOUGE FULL LENGTH OF PANEL. REMOVED GOUGE FROM FLOOR PANEL SRM, PANEL 120CF L=77 INCHES, W=48 INCHES, MAX ALLOWED REWORK 1108.8. AREA WITHIN LIMITS IAW SRM. (K)Jun 1, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600367Panel · corrodedCORROSION AROUND SEVERAL FASTENER HOLES ON AFT CARGO PANEL 140 AF, BL 21R-21L, BS 727 +4 TO BS 727D. REMOVED CORROSION AROUND FASTENER HOLES ON AFT CARGO PANEL 140AF IAW B737-800, SRM 51-10-02-06, ORIGINAL MATERIAL THICKNESS .070 IAW B737-800, SRM 53-70-53, MMay 31, 2006 · N315TZ · Boeing 73783N · Fuselage Miscellaneous StructureSDR AMTA200600366Floor Panel · corrodedCORROSION AROUND FASTENER HOLES ON AFT SIDE OF FLOOR PANEL NR 140BF, BS727I-767, RBL 21-LBL21 (AFT CARGO). REMOVED CORROSION AROUND FASTENER HOLES ON AFT CARGO PANEL NR 140BF IAW SRM. ORIGINAL MATERIAL THICKNESS .070 MATERIAL LOSS ..004 IN A .5 X .5, AREA FOMay 31, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600365Floor Panel · corrodedFLOOR PANEL NR 140CF, BS 767-887, RBL21, LBL21 AT SIDE OF FLOOR PANEL HAS AREA OF SURFACE CORROSION AROUND FASTENER HOLES (AFT CARGO) REMOVED CORROSION ORIGINAL MATERIAL THICKNESS .071 MATERIAL LOSS .001 FOUND TO BE WITHIN LIMITS IAW SRM. (K)May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600364Floor Support · corrodedCORROSION IN AFT CARGO COMP FLOOR SUPPORT FROM STA 847 TO STA 927, RBL 20. REMOVED CORROSION FROM AFT CARGO COMP FLOOR SUPPORT STA 847 TO STA 927, RBL 20. ORIG THICKNESS .050 WITH MAX MATERIAL LOSS OF .004. BLENDOUTS WITHIN LIMITS IAW SRM, DETAIL A-A. TREAMay 31, 2006 · N315TZ · Boeing 73783N · Fuselage Miscellaneous StructureSDR AMTA200600363Floor Support · corrodedAFT CARGO FLOOR SUPPORT HAS CORROSION FROM STA 767 TO STA 827 AT LBL 20. REMOVED CORROSION FROM MATERIAL ORIGINAL THICKNESS .050 INCH MATERIAL LOSS IS .004 INCH WITHIN LIMITS IAW SRM, TREATED AND PRIMED IAW SRM. (K)May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Miscellaneous StructureSDR AMTA200600362Floor Support · corrodedAFT CARGO FLOOR SUPPORT HAS CORROSION AT STA 727D TO STA 790, RBL-20. REMOVED CORROSION IAW SRM, STA 727D TO STA 790, RBL 20. MATERIAL THICKNESS.055 MATERIAL LOSS, .003 FOUND TO BE WITHIN LIMITS. (K)May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Miscellaneous StructureSDR AMTA200600361Floorbeam · corrodedSURFACE CORROSION ON FLOORBEAM AT STA 767, RBL-3, AFT CARGO COMP. REMOVED CORROSION IAW SRM AT STA 767, RBL-3 OR ORIGINAL MATERIAL THICKNESS .071 MATERIAL REMOVE .002 MATERIAL REMAINING .069. FOUND TO BE WITHIN LIMITS IAW SRM DETAIL D. (K)May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Main, Floor BeamSDR AMTA200600360Floor Panel · chafedCHAFING APPROX 80 X 36 AREA ON AFT SIDE OF AFT CARGO FLOOR PANEL NR 140CF. BLENDED CHAFED AREA ON AFT CARGO FLOOR PANEL NR 140CF ORIGINAL MATERIAL THICKNESS .071 MATERIAL LOSS .001 IAW SR 53-00-53-1A FOUND TO BE WITHIN LIMITS. (K)May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600359Panel · chafedCHAFFING APPROX 60 X 24 AREA ON AFT SIDE OF AFT CARGO PANEL 14 OBF BS 727I-767. REMOVED CHAFING ON AFT SIDE OF PANEL NR 140 BF IAW B737, SRM 51-10-02-06, ORIGINAL MATERIAL THICKNESS .070 MATERIAL REMOVED .002-.004. FOUND TO BE WITHIN LIMITS, MAX ALLOWED 774 May 31, 2006 · N315TZ · Boeing 73783N · Fuselage Miscellaneous StructureSDR AMTA200600358Floor Panel · corrodedAFT CARGO FLOOR PNL NR 140DF HAS CORROSION ON TOP SURFACE AROUND FASTENER HOLES. REMOVED CORROSION AFT CARGO COMP FLOOR PNL NR 140DF ON TOP SURFACE AROUND FASTENER HOLES 61 INCH L X 1.0 INCH W ORIGINAL MATERIAL THICKNESS .080 MATERIAL LOSS .003 FOUND TO BE WIMay 31, 2006 · N315TZ · Boeing 73783N · Fuselage Floor PanelSDR AMTA200600353Radio · inoperativeHF NR1 RADIO WILL NOT TUNE AND TRANSMIT. NO FAULTS ON TRANSCEIVER. OPS CHECKED NR 1 HF. CHECKS GOOD. (K)May 25, 2006 · N323TZ · Boeing 73783N · HF Communications SystemSDR AMTA200600352A/C Pack · trippedRT PACK TRIP ON T/O. RESET OK IAW QRH. OP CHECK OK IAW MM. (K)May 25, 2006 · N310TZ · Boeing 73783N · Cabin Cooling SystemSDR AMTA200600351Warning Light · illuminatedDURING CLIMB LT BLEED TRIP OFF LIGHT ILLUMINATED. IAW FIM 36-10-00-810-801, STEP I, PERFORMED REPAIR CONFIRMATION, ALL INDICATIONS WERE SATISFACTORY, OK FOR SVC. (K)May 25, 2006 · N308TZ · Boeing 73783N · Pneumatic Distribution SystemSDR AMTA200600356Warning Light · illuminatedDURING CLIMB OUT LT PACK BLEED TRIP OFF LIGHT ILLUMINATED. IAW FIM 36-10-00-810-801 PERFORMED REPAIR CONFIRMATION. ALL INDICATIONS NORMAL, (BLEED TRIP OFF), LIGHT DID NOT ILLUMINATE, OK FOR SERVICE. (K)May 24, 2006 · N308TZ · Boeing 73783N · Cabin Cooling SystemSDR AMTA200600350Regulator · unserviceableDURING CLIMB LT BLEED TRIP OFF LIGHT ILLUMINATED. REMOVED AND REPLACED HIGH STAGE REGULATOR IAW. OPS AND LEAK CHECK GOOD. (K)May 24, 2006 · N308TZ · Boeing 73783N · Pneumatic Distribution SystemSDR AMTA200600346Warning Light · activatedNR 2 ENGINE CONTROL LIGHT CAME ON DURING ENGINE START. NO OTHER LIGHTS ASSOCIATED CAME ON. EEC BITE SHOWED MSG 75-20582. PERFORMED INIT EVAL IN FIM AND NO CURRENT OR RECENT FAULTS AFTER ACTUATORS TEST. CKD CONNECTORS AT EEC AND HMU AND RAN ENGINE TWICE, NOMay 20, 2006 · N319TZ · Boeing 73783N · Engine Indicating SystemSDR AMTA200600345Warning Message · activatedELEC LIGHT REMAINS ON AFTER POWERING BUSES. PERFORMED BITE TEST, FOUND MSG STAT INV INOP1, SPCU1 INOP BAT CHRG INOP 1, AUX BAT CHGR, CLEARED ALL OF THE MSGS IAW FIM, DID NOT DUPLICATE, OK FOR SERVICE. (K)May 19, 2006 · N319TZ · Boeing 73783N · Central WarningSDR AMTA200600341Hydraulic System · underservicedFLAPS WOULD NOT MOVE BEYOND 25 DEG WHEN SELECTED TO 30 DEG NOTE (B) SYSTEM QUANTITY INDICATES 70 PERCENT RF. SERVICED (B) SYS HYD, PERFORMED OPS CHECK OF THE TE. OPS CHECK NORMAL, REF MM. (K)May 18, 2006 · N308TZ · Boeing 73783N · Hydraulic System, AuxiliarySDR AMTA200600338Fire Loop · contaminatedFIRE/OVERHEAT DETECTION TEST ENGINE NR 2 FAILED IN LOOP A. PERFORMED BITE TEST ON ENG/APU FIRE DETECTION CONTROL MODULE. CLEANED FIRE LOOP A CONTACT POINTS OPS GO OD, IAW 26-10-00-810-801 OK FOR CONT SERVICE. (K)May 15, 2006 · N308TZ · Boeing 73783N · Fire DetectionSDR AMTA200600336Wire · brokenDURING TEST OF WINDOW O-HEAT SYS FOUND L2 WINDOW SHOWS (OVERHEAT) LIGHT ILLUMINATED AND (OFF) LIGHT ILLUMINATED AND WITH SW (ON). FOUND BROKEN WIRE AT D10572 PIN NR 3, IAW AMM 20 AND WDM 30-41-12 AND FIM 30-41-00-810-813. REPLACED PIN- WINDOW NR L2 TEST OK. May 15, 2006 · N314TZ · Boeing 73783N · Windshield/Door Rain/Ice RemovalSDR AMTA200600340Switch · out of adjustLDG GEAR WARNING HORN SOUNDS AFTER T/O WHILE GEAR IS IN TRANSIT AND FLAP RETRACTING FROM 1-0. HORN COULD NOT BE CANCELLED. ADJUSTED FLAP LANDING WARNING SWITCH IAW MM. CHECKS GOOD. (K)May 14, 2006 · N314TZ · Boeing 73783N · Landing Gear Retraction/Extension SystemSDR AMTA200600339Wire · brokenLT SIDE NR 3 WINDOW OVHT LT ON. SHOULD HAVE BEEN IDENTIFIED AS L2 WINDOW. FOUND BROKEN WIRE AT D10572 PIN NR 3, IAW AMM 20 AND WDM 30-41-12 AND FIM 30-41-00-810-813. REPLACED PIN. L2 TEST, OK. (K)May 14, 2006 · N314TZ · Boeing 73783N · Flight Compartment Lighting
Back to Boeing 737-83N