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 USAA040560Skin · crackedCLT - FOUND SKIN CRACKED 4.3125, LT SIDE FUSELAGE STATION 18 AT STATION 75. INSTALLED DOUBLER PER SRM 53-00-01 FIG 229 DETAIL XI. (M)Sep 6, 2004 · N374US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040796Floor Support · corrodedPIT, Q5, FLOOR SUPPORT 1 INCH 10 INCH AREA. CORROSION; LEVEL 1; TASK NR C53-107-02 LOCATED AT STA 986.5 TO 1016, RBL 3.54 TO RBL 18.25. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Sep 5, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040809Skin · delaminatedPIT, Q5, TOP SKIN - CORE BOND, 2 INCH AREA AT NR 5 SLAT T/E; 1 AT IB END AND 1 AT OB END. REMOVED DELAMINATED AREA, INSTALLED NEW TOP SKIN IAW SRM 51-70-10.Sep 3, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040704Angle · crackedANGLE, 1.5 INCH LONG CRACK, RT WING ROOT, BS 540 AT S22R, AFT END. INSTALLED REPAIR ANGLE DOUBLER IAW T/R 53-50-03.Sep 3, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040675Hinge Fitting · wornHINGE FITTING WORN .0625 INCH AT PIVOT POINT NR 5 GROUND SPOILER OB AND WBL 169.25. FABRICATED NEW PART IAW MFG DRG 69-39228.Sep 3, 2004 · N514AU · Boeing 7373B7 · Wing, Attach FittingsSDR USAA040663Angle · crackedPIT - FOUND ANGLE CRACKED 2 INCHES, RT WING ROOT, BS 540 AT S22R. REPLACED CREASE BEAM SECTION PER SRM 51-40-00. (M)Sep 3, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040703Floor Support · crackedFLOOR SUPPORT, .5 INCH CRACK, DAMAGE AREA FLOORBEAM, STA727B, LBBL 8-10. MODIFIED REPAIR ANGLE IAW TR 53-10-06B, INSTALLED DOUBLER.Sep 2, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAASB04117Indicator · malfunctionedBOS - FLT 2022 - ON APPROACH TO BOS, FROM DCA, THE RIGHT FLAP LAGGED BEHIND THE LEFT FLAP TO THE POINT WHERE SELECTING FLAPS TO 25 UNITS, FLAPS ASSYMETRY PROTECTION TOOK PLACE. CREW ACCOMPLISHED A GO AROUND AND LANDED WITHOUT FURTHER INCIDENT. MAINTENANCE RESep 2, 2004 · N376US · Boeing 7373B7 · Trailing Flap Position Indicating SystemSDR USAA040815Clip · crackedPIT, Q5, CLIP 1 INCH CRACK, STR 19 AND STA 986 BULKHEAD. INSTALLED CLIP IAW SRM 5-40-02.Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040820Crease Beam · crackedPIT, Q5, CREASE BEAM WEB 1 INCH CRACK. LT CREASE BEAM BS 616-639. DEFECTIVE PART REPLACED WITH IDENT PART IAW SRM 51-10-02.Sep 1, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA050822Skin · wornMID FLAP L/E, 24 INCHES WORN. IB 24 INCHES ON THE LT OB MID FLAP L/E AT IB END. INSTALLED DOUBLER IAW SRM 57-53-01, FIG 208.Sep 1, 2004 · N383US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040708Floorbeam · corrodedT-CAP, 1 INCH BY 1 INCH AREA, CORROSION; LEVEL 1; TASK NR C53-107-02, STA 328 BL 0, RBL 59 INCH, 3 AREAS. INSTALLED NEW T CAP PER SRM 53-10-51.Sep 1, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Floor BeamSDR USAA040522Skin · crackedPIT - FOUND SKIN CRACKED 1.125 INCH LONG, STATION 727D PLUS 18 INCHES STRINGER 22L FUSELAGE SKIN. INSTALLED DOUBLER AND TRIPLER PER SRM 53-00-01 FIG 229. (M)Sep 1, 2004 · N520AU · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR DL733040830Oven · odorACRID SMOKE COMING FROM ELECTRICAL CONTROL PANEL ABOVE OVENS IN AFT GALLEY. FOUND L2 DOOR GALLEY OVEN AND CONTROLLER SMELLING OF SMOKE. CHECKED GALLEY AREA FOUND NO ELECT DAMAGE. RE-INSTALLED OVENS AND CONTROLLERS. REPLACED OVEN AND CONTROLLER.Sep 1, 2004 · N947WP · Boeing 7373B7 · Buffet/GalleysSDR USAA040637Skin · chafedPIT - FOUND RUDDER CHAFED 1 INCH BY .125 INCH, LOWER LT EDGE 9.5 INCH FROM TRAILING EDGE. REMOVED DAMAGED MATERIAL, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17. (M)Aug 31, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040643Stiffener · corrodedPIT - FOUND STIFFENER CORRODED 1 INCH BY 1 INCH AREA, FLOOR SUPPORT BETWEEN STATION 312-328 RBL 11. REPLACED STIFFENER PER SRM 51-40-02. CORROSION LEVEL 1, TASK NR C53-107-02. (M)Aug 31, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040639Skin · crackedPIT - FOUND RUDDER CRACKED WITH DELAMINATION AND PEELING, RUDDER LOWER LEFT LEADING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 31, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAASB04116Reflector · inoperativeMAINTENANCE REPORTED THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REMOVED AND REPLACED THE FORWARD SERVICE DOOR EXTERIOR EMERGENCY LIGHT REFLECTOR ASSEMBLY. OPERATIONAL CHECK GOOD. (M)Aug 31, 2004 · N391US · Boeing 7373B7 · Emergency LightingSDR USAA040669Bushing · corrodedPIT - FOUND BUSHING CORRODED .25 INCH BY .125 INCH AREA, LEFT HORIZONTAL NR 12 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040668Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, LEFT HORIZ STABILIZER STAB NR 9 LUG. MADE NEW BUSHING PER SRM 55-10-10. (M)Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040666Bushing · corrodedPIT - FOUND BUSHING CORRODED .25 INCH BY .25 INCH AREA, RIGHT HORIZ STAB R10 LUG. MADE NEW BUSHING AMS 4640 PER SRM 55-10-10. (M)Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040665Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH, RIGHT HORIZ STAB, R-8 CLEVIS BUSHING. MADE NEW BUSHINGS WITH AMS 4640 PER SRM 55-10-10. (M)Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAA040664Bushing · corrodedPIT - FOUND BUSHING CORRODED .125 INCH BY .125 INCH AREA, RT HORIZ STAB R-10 LUG. NEW BUSHING INSTALLED PER SRM 55-10-10. (M)Aug 30, 2004 · N514AU · Boeing 7373B7 · Horizontal Stabilizer StructureSDR USAASB04115Socket · shortedPIT - MAINTENANCE REPORTED THE OVERHEAD MOUNTED AISLE ILLUMINATION EMERGENCY LIGHTS AT SEAT ROWS 5 AND 9, LEFT SIDE, INOPERATIVE. MAINTENANCE FOUND SEAT ROW 5 LIGHT SOCKET SHORTED AND THE BATTERY CHARGER FUSE BLOWN. REPLACED SEAT ROW 5 LIGHT/SOCKET ASSEMBLY,Aug 30, 2004 · N391US · Boeing 7373B7 · Emergency LightingSDR USAA040783Stringer Clip · crackedPIT - Q5, TIE- .1250 INCH CRACK, RIVET, STR TO FRAME CLIP, STA 663.75-S10R. REMOVED AND REPLACED STRINGER CLIP (TIE) IAW 53-00-03.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040812Clip · crackedPIT, Q5, CLIP EST. .125 INCH STA 500D S 8L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040813Clip · crackedPIT, Q5, CLIP EST. .125 INCH CRACK, STA 500B S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040814Clip · crackedPIT, Q5, CLIP EST. .125 INCH CRACK, STA 440S 10L. REPLACED CLIP IAW SRM 51-10-02 AND 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040823Clip · crackedCLIP, EST. .125 INCH CRACK, STA 500D SGL. REMOVED AND REPLACED CLIP IAW SRM 51-10-02, 51-40.Aug 29, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040810Stringer Clip · crackedPIT, Q5, STRINGER CLIPS, .5000 INCH AND .1250 INCH CRACKS, STA 578, STR S9R. CLIP REPLACED IAW SRM 51-40-02.Aug 28, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040819Skin · crackedPIT, Q5, SKIN WITH 1.2500 INCH CRACKS (3 EA). NR 1 SLAT, LOWER SURFACE AT ROW IB END 4TH RIVET. INSTALLED DOUBLER IAW SRM 57-43-01, FIG 206.Aug 28, 2004 · N383US · Boeing 7373B7 · Leading Edge DevicesSDR USAA040634Structure · crackedPIT - FOUND FORWARD ENTRY DOOR CRACKED 1 INCH, LOWER FORWARD FRAME CORNER. REMOVED DAMAGE, REPAIRED WITH ANGLES PER SRM 51-70-13. (M)Aug 28, 2004 · N514AU · Boeing 7373B7 · Passenger/Crew DoorsSDR USAA040633Web · crackedPIT - FOUND AFT CARGO INNER WEB CRACKED .25 INCH, LIGHTENING HOLE AFT OF SPRING MOUNT. REMOVED DAMAGE, INSTALLED DOUBLER PER EA 78996. (M)Aug 28, 2004 · N514AU · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA040811Floor Support · crackedPIT, Q5, FLOOR SUPPORT, 3 INCH CRACK (BROKEN) AT STA 540 RBL 2. REPLACED FLOOR SUPPORT IAW SRM 51-40-02.Aug 27, 2004 · N383US · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040818Skin · crackedPIT, Q5, SKIN .300 INCH LONG CRACK, LOWER RADIUS OF LOWER HINGE CUTOUT. INSTALLED DOUBLER IAW TYP REP 52-10-13.Aug 27, 2004 · N383US · Boeing 7373B7 · Fuselage Main, Plate/SkinSDR USAA040636Channel · crackedPIT - FOUND FLOOR CHANNEL CRACKED .125 INCH, STATION 867 RBBI 3.00 FLOOR CHANNEL AFT CARGO NUTPLATE HOLE. CRACK REMOVED AND FILLER AND DOUBLER INSTALLED PER SRM 51-70-11. (M)Aug 27, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040676Anchor Fitting · corrodedANCHOR FITTINGS, .1250 INCH BY .1250 INCH AREA, CORROSION: LEVEL 1; TASK NR C53-107-02 ANCHOR FITTINGS (2) STA 993L. REPLACED FITTINGS IAW SRM 51-10-2.Aug 26, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Attach FittingsSDR USAA040678Frame · crackedPIT - FOUND BELL FRAME CRACKED .125 INCH, SIDE AIR SUPPORT RIVET STATION 908 AND S-9. DOUBLER INSTALLED PER SRM 53-60-07, FIG 201, SRM 53-00-07, FIG 201. (M)Aug 26, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040609Stringer · crackedPIT - FOUND STRINGER CRACKED .5 INCH, STRINGER 5A, BS 1138. INSTALLED NEW PART, ANGLES, FILLER SPER TYPICAL REPAIR 53-80-04. (M)Aug 26, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, Longeron/StringerSDR USAA040642Skin · wornPIT - FOUND COMPOSITE RUDDER SKIN WITH WEAR AND KNIFE EDGING, RUDDER RIGHT LOWER EDGE. REMOVE DAMAGE, INSTALLED REPAIR PLYS, SEAL AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 26, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040641Skin · damagedPIT - FOUND RUDDER COMPOSITE SKIN DAMAGE 5.25 INCH BY 1.5 INCH SINGLE LAYER, RUDDER RIGHT SIDE AT FS 180 10 INCHES FROM TRAILING EDGE. INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 26, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040518Housing · wornPIT - FOUND HOUSING WITH EXCESSIVE WEAR CAUSING GOUGES, LATCH HANDLE SHAFT HOUSING, AFT CARGO DOOR. BLENDED OUT GOUGES AND REPLACED WORK HOUSING ASSEMBLY PER SRM 52-30-01, FIG 101, DETAIL V. (M)Aug 26, 2004 · N514AU · Boeing 7373B7 · Cargo/Baggage DoorsSDR USAA040817Structure · wornPIT, Q5, MIDFLAP 1 INCH X 1 INCH, WORN. LT OB MIDFLAP LOWER SIDE AFT OF OB JACKSCREW ATTACH BRACKET. INSTALLED DOUBLER IAW TR 57-50-17.Aug 25, 2004 · N383US · Boeing 7373B7 · Trailing Edge FlapsSDR USAA040640Skin · chafedPIT - FOUND RUDDER COMPOSITE SKIN CHAFED .25 INCH BY .125 INCH SINGLE LAYER CHAFE MARKS, RUDDER LEFT LEADING EDGE AT STATION 174. REMOVED DAMAGE, INSTALLED REPAIR PLYS, SEAL REPAIR AND REFINISH PER SRM 51-70-17 AND EA 79025. (M)Aug 25, 2004 · N514AU · Boeing 7373B7 · Rudder, Plate/SkinSDR USAA040506Beam · crackedPIT - FOUND VERTICAL BEAM CRACKED, VERT CHORD 5.7 LEFT WL 184 STATION 178 FPBH. REMOVED DEFECTIVE PARTS, INSTALLED REPAIR ANGLE PER EO 5300V155. (M)Aug 24, 2004 · N385US · Boeing 7373B7 · Fuselage Main, StructureSDR USAA040632Duct · crackedPIT - AIRCO PAC INLET DUCT CRACKED 1 INCH, BS 538 S22 PACK RAM AIR INLET LEFT SIDE. INSTALLED DOUBLER PER TYPICAL REPAIR 53-50-03. (M)Aug 22, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040670Support · damagedPIT - FOUND SUPPORT HAS 15 OVERSIZED HOLES, BS 540 BETWEEN RIGHT INBOARD AND OUTBOARD SEAT TRACKS. REMOVED AND REPLACED FLOOR SUPPORT PER SRM 53-00-52. (M)Aug 20, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040516Beltframe · crackedPIT - FOUND BELTFRAME CRACKED .125 INCH, FS 787 LEFT OVERHEAD BIND LOWER ATTACH POINT. REMOVED CRACK AND INSTALLED REPAIR ANGLES PER TYP REPAIR 53-10-20A. (M)Aug 20, 2004 · N514AU · Boeing 7373B7 · Fuselage Main, FrameSDR USAA040508Web · crackedPIT - FOUND WEB CRACKED .25 INCH LONG, STATION 1040 BL 0 JUST ABOVE CENTER PLUG OF PRESSURE WEB. MANUFACTURED REPAIR DOUBLER AND FILLER, PLATE/DOUBLER PER SRM 53-80-08 FIG 201. (M)Aug 19, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous StructureSDR USAA040517Intercostal · crackedPIT - FOUND FLOOR SUPPORT INTERCOSTAL CRACKED THREE PLACES, 3 INCH EACH, BETWEEN 927 AND 947 AT 0 INCH LBL. REMOVED AND REPLACED PER SRM 53-60-51. (M)Aug 19, 2004 · N514AU · Boeing 7373B7 · Fuselage Miscellaneous Structure
Back to Boeing 737-3B7