Boeing 737-3B7

Service difficulty reports · 4,722

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 = '7373B7'
  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 USAA001638Frame · crackedCLT - Q-4, FRAME HAD .25 INCH CRACK AT STA 400 BETWEEN S9L AND S8L. DOUBLER INSTALLED PER TR NR 53-10-14. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001637Crease Beam · crackedCLT - Q-4, CREASE BEAM HAD 3 INCH CRACK AT FORWARD END OF S17R STA 617. FABRICATED REPAIR ANGLES PER SRM 53-60-13. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA001635Frame · crackedCLT - Q-4, FRAME HAD .25 INCH CRACK AT BS 907 BETWEEN S8L - S9L. FABRICATED REPAIR DOUBLER PER TR 53-10-14. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001634Tie Clip · crackedCLT - Q-4, TIE CLIP HAD .25 INCH CRACK AT S4L STA 907. REPLACED WITH ORIGINAL PART NUMBER PER SRM 51-10-02. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001633Tie Clip · crackedCLT - Q-4, TIE CLIP CRACKED AT STA 597 S10L. DEFECTIVE PART REPLACED WITH IDENTICAL PART NUMBER PER SRM 51-10-02 - SRM 51-40-02. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001632Frame · crackedCLT - Q-4, FRAME CRACKED .25 INCH AT BS 727D BETWEEN S9R - S8R. FABRICATED REPAIR DOUBLER, HEAT TREATED AND INSTALLED WET PER TR 53-10-14. (X)Sep 29, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001612Skin · crackedCLT - Q-4, SKIN HAD 1 INCH CRACK AT LOWER SKIN STABILIZER, STA 134, FORWARD OF REAR SPAR. INSTALLED DOUBLER PER 55-10-07. (X)Sep 28, 2000 · N516AU · Boeing 7373B7 · Horizontal Stabilizer, Plate/SkinSDR USAA001611Stiffener · crackedCLT - Q-4, STRINGER, STIFFENER/WEB CRACKED, .1250 INCH, AT STA 294.5 - 277, STR 14R. FABRICATED NEW WEB PER SRM 53-30-01 AND SRM 51-70-13. (X)Sep 28, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001581Angle · corrodedCLT - FOUND CORROSION AT T-ANGLE AND WEB, 2 INCHES BY 4 FEET, AFT STATION 1088 ABOUT WL 294. REMOVED CORROSION PER RM 51-10-02. (M)Sep 27, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001580Door Frame · crackedCLT - DURING Q-4 INSPECTION, FOUND DOOR FRAME CRACKED .375 INCH AT UPPER STOP PAD SUPPORT R-1 DOOR INBOARD FRAME. REPLACED WITH NEW STUB FRAME PER SRM 51-40-02 AND DWG 65 45807. (X)Sep 27, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAA001579Frame · crackedCLT - DURING Q-4 INSPECTION, FOUND DOOR FRAME CRACKED .500 INCH AT INBOARD UPPER FORWARD CORNER R-1. FABRICATED SPLICE AND INSTALLED PER SRM 51-40-02. (X)Sep 27, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001568Z-Angle · corrosionCLT - FOUND Z-ANGLE CORRODED, STATION 277 TO 360, LBL 58. INSTALLED NEW Z-ANGLE PER SRM 51-10-02. CORROSION LEVEL 1. (M)Sep 26, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, StructureSDR USAASB00276Oven · contaminatedSAV - FLT 1975 - EN ROUTE FROM CLT TO MBJ, A BURNING SMELL AND SMOKE WAS NOTED COMING FROM THE FORWARD GALLEY OVEN. CREW SHUTOFF GALLEY POWER, DECLARED AN EMERGENCY AND DIVERTED TO SAV. SMOKE AND BURNING SMELL HAD DISSIPATED AFTER FIVE MINUTES OF GALLEY POWESep 26, 2000 · N387US · Boeing 7373B7 · Buffet/GalleysSDR USAASB00272Battery Pack · dischargedALB - MAINTENANCE FOUND THE LEFT OVERWING EXIT SIGN, THE CENTER AISLE EXIT SIGN ON CEILING AT ROW 10 AND RIGHT SIDE BULL NOSE LIGHTS AT ROW 16, INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Sep 25, 2000 · N396US · Boeing 7373B7 · Emergency LightingSDR USAA001556Angle · corrodedCLT - FOUND ANGLE CORRODED 2 INCHES BY 6 INCHES, BETWEEN BS 747 AND 767 TRANSITION ANGLE. FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-02. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001555Angle · corrodedCLT - FOUND Z-ANGLE CORRODED 1 INCH BY 20 INCHES, STATION 270 TO 360, RBL 58. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001554Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .250 INCH, STRINGER 10LT STATION 663.75. REPLACED TIE CLIP PER SRM 51-40-02. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001542Floorbeam · corrodedCLT - FOUND 2 INCH BY 1 INCH AREA OF CORROSON, STATION 244, LBL 32 TO RBL 54. CORROSION LEVEL 1. INSTALLED NEW T-CAP PER SRM 53-10-51 FIG 205. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001541Web · corrodedCLT - FOUND WEB CORRODED 20 INCHES, STRINGER 17L CREASE BEAM STATION 616 TO 639. CORROSION LEVEL 1. REMOVED AND REPLACED WEB PER SRM 51-10-02. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001540Angle · corrodedCLT - FOUND SUPPORT ANGLE CORRODED 2 INCHES BY 4 INCHES, STATION 312 TO STATION 344, LBL 60. INSTALLED NEW ANGLE PER RM 51-10-2. (M)Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00274Swivel · brokenBOS - FLT 1090 - EN ROUTE FROM PHL TO BOS, FLT LOST A-SYSTEM HYDRAULIC QUANTITY AND PRESSURE. MX CONTROL ADVISED THAT FLIGHT SHOULD PROCEED TO ORIGIN OR DESTINATION, WHICHEVER WAS CLOSER. FLIGHT WAS CLOSER TO BOS, SO IT CONTINUED ONTO BOS. FLIGHT LANDED WITSep 25, 2000 · N373US · Boeing 7373B7 · Hydraulic System, MainSDR USAA001557Skin · crackedCRACKINSTALLED DOUBLER PER EA68049, TYP REP 53-60-03Sep 25, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001553Tie Clip · crackedTIE CLIP CRACK. REPLACED TIE CLIP PER SRM 51-10-2Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001552Tie Clip · crackedTIE CLIP CRACK. FABRICATED NEW TIE CLIP PER SRM 51-10-02Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001551Bulkhead · crackedBULKHEAD CRACKED. FABRICATED NEW WEB PER SRM 51-10-02Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Main, BulkheadSDR USAA001550Web · crackedWEB CRACKED. FABRICATED NEW WEB PER SRM 51-10-02Sep 25, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB00268Actuator · detachedBDL - FLT 1738 - WHEN FLAPS WERE EXTENDED FOR LANDING AT BDL, FROM PHL, THE AIRCRAFT ROLLED RIGHT. IT REQUIRED OPPOSING AILERON FORCE OF 2 TO 3 DEGREES LEFT AILERON TO STOP ROLL. FLIGHT LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE FOUND THE RIGHT INBOARD AFSep 21, 2000 · N395US · Boeing 7373B7 · Trailing Edge Flap ActuatorSDR AWXA0000711Wire · brokenEMERGENCY LIGHTING WRITE-UP DISCOVERED ON 3 OCT 2000. EMERGENCY EXIT LIGHTS AT 11D FLOOR TRACK 1 LENS BROKEN, TRACK AND WIRES PULLED UP. REPAIRED SPLICED WIRE FOR LIGHTING IAW BOEING MANUAL D6-54446 20-10-13 AND 20-30-12.Sep 20, 2000 · N332AW · Boeing 7373B7 · Light System WiringSDR USAASB00263Uplock Sensor · failedIND - FLT 1598 - AFTER SELECTING GEAR UP AFTER DEPARTURE FROM IND, CREW REPORTED THE RIGHT MLG WARNING LIGHT REMAINED ILLUMINATED. AFTER GEAR WAS VERIFIED DOWN AND LOCKED, CREW ELECTED TO RETURN TO FIELD. FLIGHT LANDED WITHOUT FURTHER INCIDENT. NO EMERGENCYSep 18, 2000 · N519AU · Boeing 7373B7 · Landing Gear Position and WarningSDR USAASB00259Engine · overheatedBHM - FLT 1985 - EN ROUTE FROM DFW-CLT, AT FL370, THE NR 2 ENGINE EGT INDICATED OVER 1,000 DEGREES AND THE RED OVERTEMP LIGHT ILLUMINATED. CAPTAIN BACKED OFF THE POWER TO IDLE AND THE EGT DROPPED TO WITHING NORMAL LIMITS. WHEN THROTTLE WAS ADVANCED, EGT WOULSep 16, 2000 · N526AU · Boeing 7373B7 · Engine (Turbine/Turboprop)SDR USAA002192Frame · crackedPIT - FOUND FRAME CHORD CRACKED APPROX .25 INCH, RT 178 WL 212. SPLICED IN NEW SECTION OF CHORD PER EO 5300V157. (M)Sep 15, 2000 · N390US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA002191Frame · crackedPIT - FOUND CHORD ANGLE CRACKED .5 INCH, LEFT 178 WL 212. SPLICED IN NEW SECTION OF CHORD PER EO 5300V157. (M)Sep 15, 2000 · N390US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001536Attach Fitting · corrodedPIT - FOUND CORROSION 1 INCH BY 10 INCH ON HARDWARE AND ATTACH FITTING, STATION 1088-1104 RUNNING INBOARD OF S-52 SHELF. (M)Sep 13, 2000 · N518AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA001535Attach Fitting · corrodedPIT - FOUND CORROSION 1 INCH BY 10 INCH AT STATION 1088-1104 RUNNING INBOARD OF S-5R SHELF. CORROSION LEVEL 1, TASK NR C53-701-01. (M)Sep 13, 2000 · N518AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA001513Tie Clip · crackedCLT - FOUND TIE CLIP CRACKED .25 INCH, BS 663.75, STRINGER 10R. INSTALLED NEW TIE CLIP PER SRM 51-10-02. (M)Sep 12, 2000 · N516AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR AWXA0000641Wire · exposedNON ROUTINE LINE, FLOOR LIGHT AT SEAT 1C HAS EXPOSED WIRE. REMOVED AND REPLACED LIGHT ASSEMBLY.Sep 12, 2000 · N328AW · Boeing 7373B7 · Light System WiringSDR USAASB00241Hydraulic Line · leakingCLT - FLT 579 - ON APPROACH TO CLT, CREW DECLARED AND EMERGENCY DUE TO LOW PRESSURE ON THE SYSTEM A HYDRAULICS. QUANTITY AND PRESSURE LOSS WAS THROUGH THE ENGINE DRIVEN PUMP. QUANTITY LOSS STOPPAGE WHEN ENGINE DRIVEN PUMP WAS BYPASSED. FLIGHT LANDED WITHOUTSep 2, 2000 · N517AU · Boeing 7373B7 · Hydraulic System, MainSDR USAASB00238Bulb · failedORF - FLT 2299 - ON CLIMB-OUT FROM DCA, EN ROUTE TO MCO AT FL280, CREW REPORTED A HIGH OIL TEMPERATURE READING OF 190 DEGREES CELSIUS ON THE NR 1 ENGINE. AFTER PULLING/RESETTING CIRCUIT BREAKER AND FOLLOWING REQUIRED PROCEDURES, INDICATION WENT BACK TO 190 DESep 1, 2000 · N374US · Boeing 7373B7 · Engine Oil Indicating SystemSDR USAASB00237Drag Brace · crackedPIT - FLT 967 - AFTER TAKEOFF FROM PIT, CREW RAISED LANDING GEAR NORMALLY BUT WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION, THE NOSE GEAR RED LIGHT ILLUMINATED AND GEAR NOISE WAS PRESENT. GEAR HANDLE WAS PLACED TO THE DOWN POSITION AS CREW ACCOMPLISHED QUIAug 31, 2000 · N530AU · Boeing 7373B7 · Landing Gear Retraction/Extension SystemSDR USAASB00246Charger · failedGSO - MAINTENANCE FOUND THE FORWARD SERVICE DOOR EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE EMERGENCY LIGHT BATTERY PACK (P/N AD2013-1A) AND CHARGER ASSEMBLY. OPS CHECK GOOD. (M)Aug 29, 2000 · N507AU · Boeing 7373B7 · Emergency LightingSDR USAA001391Keelbeam · corrodedCLT - FOUND FLANGE CORRODED 30 INCHES, RT KEEL BEAM PANEL ATTACH FLANGE. CORROSION LEVEL 1 C53-100-01. INSTALLED REPAIR STRAP PER EA 67882. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA001390Keelbeam · corrodedCLT - FOUND FLANGE CORRODED 30 INCHES, KEEL BEAM FLANGE BS 727 TO BS 680. CORROSION LEVEL 1 C53-100-01. INSTALLED REPAIR STRAP PER EA 67882. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, KeelSDR USAA001382Floorbeam · corrodedCLT - FOUND FLOORBEAM CORRODED .250 INCH BY 10 INCH, STATION 986 LEFT TO RIGHT. CORROSION LEVEL 1 C53-107-02. INSTALLED NEW T-CAP PER TR 53-10-05A. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA001389Stringer · crackedCLT - FOUND SHELF CRACKED .5 INCH, STRINGER 18A, RT MLG, BS 727 BULKHEAD. REPLACED SHELF PER SRM 51-10-2. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA001388Angle · corrodedCLT - FOUND CREASE BEAM Z-ANGLE CORRODED 1 INCH BY 45 INCHES, LT BS 947-992. CORROSION LEVEL 1. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001387Angle · corrodedCLT - FOUND CREASE BEAM Z-ANGLE CORRODED 1 INCH BY 48 INCHES, BS 947 TO 995. CORROSION LEVEL 1, C53-107-02. INSTALLED NEW Z-ANGLE PER SRM 51-10-2. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA001370Frame · crackedCLT -FOUND 4 INCH CRACK IN FRAME, AT FS 727 AND STRINGER 15R. REMOVED DAMAGED AND INSTALLED TRIPLER PER EA 67776B. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, FrameSDR USAA001369Skin · crackedCLT - FOUND SKIN CRACKED .250 INCH, STATION 380 E/E CASING HOLE CUTOUT. INSTALLED DOUBLER PER TR 53-30-07 AND DWG 65C33930. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA001368Stringer · crackedCLT - FOUND STRINGER CRACKED 5 INCHES, HORIZ STAB CUTOUT STRINGER 5L AND FS 1138 TO 1143. REPLACED ANGLE PER SRM 53-00-01 FIG 221. (M)Aug 29, 2000 · N383US · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAASB00234Pump · leakingMCO - FLT 808 - DURING CLIMB-OUT FROM MCO, EN ROUTE TO PHL, CREW NOTICED A LOSS OF NR 1 ENGINE HYDRAULIC PRESSURE ON THE ENGINE DRIVEN PUMP AND THE SYSTEM A HYDRAULIC QUANTITY INDICATOR READING BELOW ONE-QUARTER GALLON. CREW DECLARED AN EMERGENCY AND RETURNEDAug 27, 2000 · N517AU · Boeing 7373B7 · Hydraulic Pump (Electric/Engine), Main
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