Boeing 737-2B7

Service difficulty reports · 1,360

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 = '7372B7'
  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 USAA990135Gusset · crackedCLT - DURING DROP IN VISUAL INSPECTION, FOUND A 1 INCH CRACK IN UPPER RADIUS OF GUSSET AT TOP OF N/G WELL. REPAIRED PER SRM 51-10-1. (M)Feb 18, 1999 · N272AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA990064Skin · crackedCLT - DURING CHECK VISUAL INSPECTION, FOUND A .1 INCH CRACK STATION 727B PLUS 3 INCH STRINGER 18R ON SKIN. INSTALLED DOUBLER PER SRM 53-30-3 FIG 1. (M)Feb 9, 1999 · N281AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990083Skin · crackedPIT - DURING A CHECK, FOUND 3 INCH CRACK IN SKIN ALSO INTERNAL ANTENNA CHANNEL CRACKED 8 INCH - 10 INCH LONG BETWEEN STATION 767 AND 787 BL0. INSTALLED EXTERNAL DOUBLER AND REPLACED INNER ANTENNA CHANNEL PER SRM 53-30-3 FIG 1, FOR REPAIR DOUBLER. (M)Feb 7, 1999 · N271AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA990069Skin · crackedTPA - DURING METRO JET CONVERSION VISUAL INSPECTION, FOUND 3 SMALL CRACKS .125 INCH, .25 INCH AND .5 INCH FROM RIVET HOLES NEAR APU FIRE EXT INDICATOR CUTOUT STATION 1070 STRINGER 23R SKIN. INSTALLED DOUBLERS PER SRM 53-30-3 FIG 1. (M)Feb 2, 1999 · N270AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB99025Connector · shortedBOS - FLT 1241 - DURING CLIMB-OUT FROM BOS AT FL 200, THE CREW RECEIVED A NR 2 ENGINE FIRE WARNING LIGHT AND HORN. CREW ACCOMPLISHED QUICK REFERENCE HANDBOOK PROCEDURES AND IMMEDIATELY SHUT DOWN THE NR 2 ENGINE AND FIRE BOTH FIRE EXTINGUISHING BOTTLES. AN EMJan 31, 1999 · N272AU · Boeing 7372B7 · Fire DetectionSDR USAASB99018Fire Light · illuminatedILM - FLT 439 - ON DESCENT INTO ILM, THE CREW REPORTED THAT THE APU FIRE WARNIG LIGHT ILLUMINATD WITH THE APU ON MEL AND SHUTDOWN. THE APU IS SCHEDULED FOR REPLACEMENT DUE TO PERFORMANCE. CAPTAIN STATED THAT THE FLIGHT WAS AT 12,000 FEET WHEN THE FIRE WARNINJan 23, 1999 · N269AU · Boeing 7372B7 · Fire DetectionSDR USAASB99014Coalescer · dirtyFWA - FLT 1177 - EN ROUTE FROM BWI TO ORD AT FL310, ONE OF THE FLIGHT ATTENDANTS ADVISED THE COCKPIT CREW THAT THERE WERE FUMES IN THE CABIN AND THE FUMES WERE IRRITATING THE PASSENGERS. AN EMERGENCY DECLARED AND FLT DIVERT TO FWA. THE FUMES DISSIPATED ON DEJan 15, 1999 · N274US · Boeing 7372B7 · Humidity Control SystemSDR USAASB99002Duct · leakingMCO - FLT 2740 - CLIMBING THROUGH FL110, THE NR 2 ENG OVERHEAT LIGHT ILLUMINATED. ALL OTHER ENGINE INDICATIONS WERE NORMAL. CREW LEVELED FLIGHT OFF AT FL120, THEN ADVISED ATC, RETURNING TO MCO. CAPT PULLED THE NR 1 ENGINE THROTTLE BACK TO IDLE, DECLARED AN Jan 2, 1999 · N271AU · Boeing 7372B7 · Air Intake Anti/De-Ice SystemSDR USAASB00002Charger · failedSYR - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN IN THE FORWARD CABIN CEILING INOPERTIVE. MAINTENANCE REMOVED AND REPLACED THE CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Jan 2, 1999 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAASB99001Switch · failedBWI - FLT2679 - CLIMB THROUGH FL190, THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED. CREW LEVELED THE AIRCRAFT AT FL230 AND WERE UNSUCCESSFUL AT CORRECTING THE PROBLEM. QUICK REFERENCE HANDBOOK PROCEDURES WERE FOLLOWED AND THE NR 1 ENGINE WAS SHUT DOWN. Jan 1, 1999 · N271AU · Boeing 7372B7 · Engine Start Valves/ControlsSDR USAASB98343Valve · failedMCO - FL2695 - EN ROUTE FROBWI TO MCO, SOUTHEAST OF SAV, FLIGHT LOST 'A' SYSTEM HYDRAULICS. CREW WENT TO ALTERNATE FLAP EXTENSION PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT LANDED AT MCO WITHOUT INCIDENT AND WAS TOWED OFF THE RUNWAY AND THEN TO THE GATE. Dec 31, 1998 · N284AU · Boeing 7372B7 · Hydraulic Pressure Relief Valve, MainSDR USAASB98341Start Valve · inoperativeBWI - FL2696 - CAPT REPORTED THAT THE NR 1 ENGINE START VALVE OPEN LIGHT ILLUMINATED IN FLIGHT AT APPROX FL250. CAPT STARTED DESCENT AND RETURN TO BWI. THE NR 1 ENGINE WAS SHUT DOWN AT FL100. FLIGHT LANDED AT BWI WITHOUT INCIDENT AND TAXIED TO THE GATE. ANDec 31, 1998 · N271AU · Boeing 7372B7 · Engine Start Valves/ControlsSDR 99ZZZM42Regulator · failedMCO - FL2695 - EN ROUTE FROBWI TO MCO, SOUTHEAST OF SAV, FLIGHT LOST 'A' SYSTEM HYDRAULICS. CREW WENT TO ALTERNATE FLAP EXTENSION PROCEDURES AND DECLARED AN EMERGENCY. FLIGHT LANDED AT MCO WITHOUT INCIDENT AND WAS TOWED OFF THE RUNWAY AND THEN TO THE GATE. Dec 31, 1998 · N284AU · Boeing 7372B7 · Hydraulic System, MainSDR USAASB98340Wire · brokenPIT - MAINTENANCE FOUND THE LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. MAINTENANCE TROUBLESHOT FAULT TO THE M192 BATTERY PACK CANNON PLUG D1494, PIN 5. REPAIRED GROUND WIRE FROM PIN NR 5 ON CANNON PLUG D1494. OPERATIONAL CHECK GOOD. (M)Dec 29, 1998 · N269AU · Boeing 7372B7 · Light System WiringSDR USAA980661Skin · crackedTPA - DURING A CX-5 CHECK EDDY CURRENT, FOUND A .25 INCH CRACK IN FORWARD SERVICE DOOR UPPER HINGE CUTOUT AFT UPPER CORNER DOOR SKIN. INSTALLED DOUBLER PER TR 52-40-03A. (M)Dec 29, 1998 · N286AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAASB98336Light · inoperativeBWI - MAINTENANCE FOUND THE EMERGENCY EXIT LIGHT AT SEAT ROW 13 INOPERATIVE. MAINTENANCE REPAIRED WIRING BENEATH SEAT ASSEMBLY AT ROW 13. OPERATIONAL CHECK GOOD. (M)Dec 20, 1998 · N287AU · Boeing 7372B7 · Emergency LightingSDR USAASB98313Battery · dischargedROC - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN AT THE FORWARD RIGHT SERVICE DOOR, WON'T REMAIN ILLUMINATED. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Nov 25, 1998 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAASB98310Battery Pack · dischargedCLE - MAINTENANCE FOUND THE AFT AISLE EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPERATIONAL CHECK GOOD. (M)Nov 23, 1998 · N279AU · Boeing 7372B7 · Emergency LightingSDR USAASB98309Mechanism · out of adjustBWI - FLT 2608 - FLIGHT WAS CLEARED FOR APPROACH AT BWI FOR RUNWAY 28. AS CAPTAIN SELECTED FLAPS 1, THE LEADING EDGE TRANSIT LIGHT AND THE NR 4 SLAT TRANSIT LIGHT ON THE OVERHEAD PANEL ILLUMINATED. CREW RECYCLED THE FLAPS AND DISCONTINUED THE APPROACH. CREWNov 22, 1998 · N282AU · Boeing 7372B7 · Leading Edge Slat Control SystemSDR USAASB98300Link · brokenCLE - FLT 957 - DURING CLIMB AND GEAR RETRACTION, CREW HEARD A LOUD BANG FROM THE NOSE WHEEL WELL FOLLOWED BY A CONTINUOUS VIBRATION IN THE COCKPIT. CAPTAIN DECIDED TO RETURN TO FIELD AT CLE AND DECLARE AN EMERGENCY. FLIGHT LANDED WITHOUT FURTHER INCIDENT. Nov 15, 1998 · N270AU · Boeing 7372B7 · Landing Gear Door Retract SectionSDR USAASB98304Battery Pack · dischargedPHL - MAINTENANCE FOUND THE AFT CENTER AISLE OVERHEAD EMERGENCY EXIT SIGN INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERY PACK. OPS CHECK GOOD. (M)Nov 13, 1998 · N268AU · Boeing 7372B7 · Emergency LightingSDR USAASB98294Light · inoperativeROC - DURING OVERNIGHT CHECK WHILE PERFORMING OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM. MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE AFT RIGHT SERVICED DOOR WOULD NOT ILLUMINATE. MAINTENANCE CHECKED BATTERIES AND LAMPS. CHECKED GOOD. REPLACED LNov 10, 1998 · N284AU · Boeing 7372B7 · Emergency LightingSDR USAASB98290Pack Valve · malfunctionedPHL - FLT 1264 - AT APPROXIMATELY 400 FT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CREW SWITCHED OVER TO STANDBY MODE AND COULD NOT CONTROL RATE OF CLIMB IN CABIN. CREW THEN TRIED MANUAL MODE AND AIRCRAFT STILL WOULD NOT PRESSURIZE. FLIGHT RETURNED TOct 30, 1998 · N266AU · Boeing 7372B7 · Cabin Pressure Control SystemSDR 98ZZZM907Valve · malfunctionedPHL - FLT 1264 - AT APPROXIMATELY 400 FT, THE PRESSURIZATION AUTO FAIL LIGHT ILLUMINATED. CREW SWITCHED OVER TO STANDBY MODE AND COULD NOT CONTROL RATE OF CLIMB IN CABIN. CREW THEN TRIED MANUAL MODE AND AIRCRAFT STILL WOULD NOT PRESSURIZE. FLIGHT RETURNED TOct 30, 1998 · N266AU · Boeing 7372B7 · Cabin Pressure Control SystemSDR USAASB98286Battery · dischargedROC - MAINTENANCE FOUND THE EMERGENCY EXIT SIGN OVER THE FORWARD SERVICE DOOR INOP. MAINTENANCE REMOVED AND REPLACED THE BATTERIES IN THE LIGHT ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Oct 29, 1998 · N273AU · Boeing 7372B7 · Emergency LightingSDR USAA980554Skin · creasedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH CREASE APU DOOR AFT LATCH CUTOUT AT STATION 1146 ON SKIN. INSTALLED DOUBLER PER EA 62761. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980553Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .5 INCH CRACK AFT ENTRY DOORWAY AT LOWER HINGE CUTOUT ON FUSELAGE SKIN. INSTALLED REPAIR DOUBLER AND TRIPLER PER SRM 53-30-3 FIG 34 AND TR 53-30-11. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980552Stringer · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 6 INCH CORRODED AREA STATION 907, STRINGER 26L. CORROSION TASK NR C53-208-01. INSTALLED NEW STRINGER AND STRINGER SPLICES PER SRM 53-10-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA980551Angle · crackedDURING Q-5 CHECK VISUAL INSPECTION, FOUND A 2 INCH STATION 727 WL 200 LBL 45 CHORD ANGLE. INSTALLED REPAIR ANGLE PER TR 53-10-03A. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980550Sill · corrodedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH BY 6 INCH AREA OF CORROSION BS 300-306 WL 208.10, RBBL 54 FORWARD SERVICE DOOR INNER CHORD. CORROSION TASK NR C53-107-01. INSTALLED NEW 'Z' ANGLE PER SRM 51-10-1 AND SRM 51-30-2. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980546Skin · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION, FOUND A .03125 INCH CRACK AT LOWER AFT CORNERS FORWARD ENTRY DOOR STATION 342 WL 208.1 SKIN FUSELAGE. CUT OUT CRACKED AREA FABRICATED AND INSTALLED REPAIR FILLER, DOUBLER AND TRIPLER PER BOEING DRAWING 65C27257 AND EAOct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980545Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 727B STRINGER 7R TIE CLIP. INSTALLED NEW STRINGER TIE CLIP PER PCI 1093, EO 5393G227. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980544Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION FOUND A .25 INCH CRACK BS 727A STRINGER 7R TIE CLIP. INSTALLED NEW TIE CLIP PER PCI 1093, EO 5393G227. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980543Web · crackedCLT - DURING Q-2 CHECK VISUAL INSPECTION VERIFIED BY EDDY CURRENT, FOUND A CRACK BL 0 BS 706, .6 INCH CRACK BS 708 .25 INCH CRACK BS 709 .6 INCH CRACK BS 710 .2 INCH CRACK BS 712 .15 INCH CRACK ON WEB. INSTALLED DOUBELR PER EA 62724A. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980534Skin · crackedCLT - DURING Q-CHECK VISUAL INSPECTION, FOUND A .20 INCH CRACK LEFT AFT ENTRY DOORWAY FORWARD LOWER CORNER BS 961, 2 INCHES ABOVE STRINGER 17L OF SKIN. INSTALLED TRIPLER PER REPAIR DOCUMENT 53-30-3 FIG 24. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980524Floorbeam · corrodedCLT - DURING Q-3 CHECK VISUAL INSPECTION, FOUND 11 CORRODED AREAS BS 986.5 LBL 18 TO RBL 43 WL 208.1 OF FLOORBEAM. CORROSION TASK NR C53-107-02. INSTALLED REPAIR T-CAP PER SRM 53-10-9 FIG 2. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Floor BeamSDR USAA980518Stringer · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 927 STRINGER 25L. REPAIRED AREA PER SRM 53-10-1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Longeron/StringerSDR USAA980517Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 1R TIE CLIP. REMOVED AND REPLACED PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980516Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 807 STRINGER 9R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980515Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 2R TIE CLIP. INSTALLED IDENTICAL PART PER EO 5393G227 REV 'A'. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980513Sill · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1 INCH CRACK BS 294.5 WL 208.10 RBBL 53 FORWARD SERVICE ENTRY DOOR LOWER SILL INBOARD CHORD DOUBLER ANGLE. REPLACED WITH IDENTICAL PART PER SRM 51-10-02. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980512Skin · dentedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 3 INCH BY 1.5 INCH BY .062 INCH DENT 11 INCH AFT OF REAR ENTRY AND 18 INCH ABOVE LOWER DOOR SILL OF SKIN. INSTALLED DOUBLER PER SERM 53-30-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980511Skin · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A 1.5 INCH CRACK STATION 767 STRINGER 19R OF SKIN. INSTALLED DOUBLER PER SRM 53-30-3. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Main, Plate/SkinSDR USAA980510Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 597 STRINGER 9R. INSTALLED MODIFIED PART PAR EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980509Clip · crackedCLT - DURIGN Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK STATION 727B STRINGER 8R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980508Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 616 STRINGER 5R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980507Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 685 STRINGER 4R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980506Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 747 STRINGER 9L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980505Clip · crackedCLT - DURING Q-5 CHECK VISUAL INSPECTION, FOUND A .25 INCH CRACK BS 639 STRINGER 4L TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous StructureSDR USAA980504Clip · crackedCLT - DURING Q-5 CHECK VIAUL INSPECTION, FOUND A .25 INCH CRACK STATION 616 STRINGER 2R TIE CLIP. INSTALLED MODIFIED PART PER EO 5393G227 AD 93-08-04 SB 737-53-1085 R1. (M)Oct 29, 1998 · N268AU · Boeing 7372B7 · Fuselage Miscellaneous Structure
Back to Boeing 737-2B7