Boeing 737-300

Service difficulty reports · 184

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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 = '737300'
  ORDER BY difficulty_date DESC"

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SDR AWXA0002187Web · crackedD: Lt wheel well pressure web cracked B.S. 664 LBL 32.C: Repaired Lt wheel well pressure web at B.S. LBL 32 IAW AWA ER #03-5712-01226-DL1Jul 29, 2001 · N332AW · Boeing 737300 · Fuselage Main, FrameSDR AWXA0001985Panel · damagedLEFT INBOARD MID FLAP T/E PANEL 7220L APPROX 15 INCHES OUTBOARD END, HOT BOND REPAIR WAS NOT ACCOMPLISHED PER SRM 51-70-10. REPAIRED LEFT INBOARD MID FLAP T/E PANEL 7220L WITH HOT BOND PER SRM 57-53-02 & 51-70-10.Jul 16, 2001 · N327AW · Boeing 737300 · Trailing Edge FlapsSDR AWXA0001984Panel · damagedLEFT I/B MIDFLAP T/E PANEL 722OL APPROX 18 INCHES I/B OF O/B END HOT BOND REPAIR NOT ACCOMPLISHED PER SRM 51-70-10. REPAIRED LEFT I/B MID FLAP T/E PANEL 7220L WITH A HOT BOND RCF SRM 57-53-02 & SRM 51-70-10.Jul 16, 2001 · N327AW · Boeing 737300 · Trailing Edge FlapsSDR DL733010182Bulkhead · crackedTHE CENTER WEB OF THE FS 178 BULKHEAD WAS FOUND CRACKED AT WL 195 AT BOTH LBL 5 AND RBL 5. THE CRACKS WERE REPAIRED PER S/B 737-53A1173, REV 3.Feb 1, 2001 · N241DL · Boeing 737300 · Fuselage Main, BulkheadSDR DL733010166Unknown · odorAFTER PUSHBACK BOTH ENGINES RUNNING, TWO F/A NOTICED ELECTRICAL ODOR AFT OF EMERGENCY EXITS, FWD OF AFT GALLEY. F/O CONFIRMS ELECTRICAL ODOR AROUND ROW 24 THE STRONGEST ODOR SEEMS TO DISSIPATE AFTER 3 - 4 MINUTES. RAN BOTH ENGINES, NTF.Jan 29, 2001 · N242DL · Boeing 737300 · Air Distribution SystemSDR AWXA0001072Intercostal · corrodedCABIN FLOORBEAM STA 294-312 RBL 12 INTERCOSTAL HAS CORROSION EMINATING FROM UNDER FILLER. REMOVED FILLER IAW SRM 51-40-02; REMOVED CORROSION FROM UPPER FLANGE IAW 51-10-02; MATERIAL LOSS MORE THAN 10 PERCENT OG THICKNESS; .100 INCH AFTER REMOVED CORROSION .088Dec 15, 2000 · N334AW · Boeing 737300 · Fuselage Miscellaneous StructureSDR AWXA0001074Angle · corrodedSUPPORT ANGLES 2 EA. UNDER PIE PANEL 8405 HAVE CORROSION ON UPPER SURFACES, ANGLES SUPPORT 2 EA PLUMBING LINES. REMOVED CORROSION PAIR THICKNESS .140 MATERIAL LOSS .050 FOUND TO BE OUT OF LIMITS IAW SRM 51-10-02; INSTALLED FABED SUPPORT ANGLES UNDER PIE PANEL Dec 15, 2000 · N334AW · Boeing 737300 · Fuselage Miscellaneous StructureSDR AWXA0001103Floorbeam · corrodedCABIN FLOORBEAM STA 328 LBL 12 TOP OF BEAM HAS CORROSION. REMOVED 2 EA. HILOCKS IAW SRM 51-40-00; REMOVED CORROSION IAW 51-10-2; FOUND OUT OF LIMITS IAW 53-10-13 FIG 102; FABED UPPER CHORD DOUBLER TWO EACH ANGLE DOUBLER TO REPAIR AREA IAW 53-10-51 FIG 205; INDec 15, 2000 · N334AW · Boeing 737300 · Fuselage Main, Floor BeamSDR AWXA0001025Skin · damagedSTA 370 STR 20R HAS A CREASE IN IT ITS SKIN. (APPROX 9 INCHES X 5 INCHES) REMOVED DAMAGED SECTION OF SKIN; FABED DOUBLER; INSTALLED CONICAL WASHERS AND INSTALLED DOUBLER IAW SRM 53-00-01 FIG 202Dec 6, 2000 · N334AW · Boeing 737300 · Fuselage Main, Plate/SkinSDR AWXA0001026Intercostal · crackedINTERCOSTAL CRACKED FS 178 WL 195 LBL 24. REMOVED DAMAGED INTERCOSTAL IAW SRM 57-40-02; INSTALLED NEW INTERCOSTAL IAW 53-10-08 FIG 207 AND 51-40-02Dec 6, 2000 · N334AW · Boeing 737300 · Fuselage Main, BulkheadSDR 20001218SH013Wheel · failedINBOARD AND OUTBOARD WHEEL HALVES DAMAGED. INBOARD WHEEL HUB FAILURE. WHEEL SENT FOR ANALYSIS. DYE PENETRANT INSPECTION OF ALL WHEELS MFG PRIOR TO 1/1/94 NEXT SHOP VISIT. WHEEL MFG 12/31/93 OR LATER DPI TO TAKE PLACE NEXT OVERHAUL. (X)Dec 4, 2000 · Boeing 737300 · Wheel/Ski/FloatSDR AWXA0001009Flap Track · damagedRT O/B FOREFLAP O/B TRACK CHAFED ON BOTTOM SIDE. GENERATED NEW N/R FOR R/R; MATERIAL LOSS RANGE .941 TO .978 OUT OF LIMITS IAW CMM 57-53-18; REMOVED AND REPLACED R/H O/B FOREFLAP O/B TRACK IAW MM 57-53-18Dec 4, 2000 · N334AW · Boeing 737300 · Trailing Edge FlapsSDR AWXA0001015Floorbeam · corrodedCABIN FLOOR BEAM FS 312 RBL 12 LBL 12 TOP OF FLOORBEAM HAS CORROSION. REMOVED CORROSION IAW SRM 53-10-13 FIG 102 FOUND TO BE OUT OF LIMITS; REMOVED FLOORBEAM UPPER T CAP AND REMOVED A STIFFENER; FABED CHORD AND INSTALLED CHORD IAW SRM 53-10-51 FIG 205 AND REINDec 4, 2000 · N334AW · Boeing 737300 · Fuselage Main, Floor BeamSDR AWXA000109Flap Track · chafedRT OB FOREFLAP OB TRACK CHAFED ON BOTTOM SIDE. GENERATED NEW N/R FOR R/R; MATERIAL LOSS RANGE .941 TO .978 OUT OF LIMITS IAW CMM 57-53-18; REPLACED FLIGHT RECORDER MODULE PART NUMBER 69-37325-52 WITH 69-37325-168 OP CHECK WILL BE COMPLIED WITH ON EO 31-31-73 ADec 4, 2000 · N334AW · Boeing 737300 · Leading Edge DevicesSDR AWXA0001010Angle · crackedSUPPORT ANGLE CRACKED BETWEEN FLOORBEAM STA 500D TO 520 LBL 45. REMOVED CRACKED SUPPORT ANGLE IAW SRM 51-40-02; FABED REPLACEMENT PART IAW 51-40-02; INSTALLED SUPPORT ANGLE IAW 51-40-02Dec 4, 2000 · N334AW · Boeing 737300 · Fuselage Miscellaneous StructureSDR AWXA0001005Web · chafedKEELBEAM WEB CHAFED FS 590 LBL 8 WL 160.REMOVED DMGD AREA; FABED REPAIR DOUBLER AND INSTALLED IAW ER 03-5300-00328-JS1 AND SRM 53-00-01 FIG 208Dec 4, 2000 · N334AW · Boeing 737300 · Fuselage Main, KeelSDR AWXA0001016Skin · dentedFWD CARGO DOOR EXTERNAL SKIN 16 EACH NOTICEABLE DENTS. REMOVED SKIN IAW 737 SRM 51-40-02; FABED SKIN, DRILLED, AND COUNTER SUNK IAW 51-40-02 AND 52-30-01; INSTALLED IAW 51-40-02; APPLY TOPCOAT IAW MN 51-21-99Dec 4, 2000 · N334AW · Boeing 737300 · Cargo/Baggage DoorsSDR AWXA0001011Seat Track · damagedD: CABIN SEAT TRACK LBL 45 HAS NUMEROUS BLEND OUTS THAT WENT OUT OF LIMITS FROM STA 723 TO STA 800C: REMOVED DAMAGED SEAT TRACK STA 727B TO 807; FABED SEAT TRACK, SPLICES, AND RADIUS BLOCK IAW 53-00-52; INSTALLED IAW 51-00-52Dec 4, 2000 · N334AW · Boeing 737300 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001008Duct · damagedRIVETS PULLED THROUGH ON APU RAM AIR INTAKE DUCT; ANGLE BROKEN OFF ON END. REMOVED Z ANGLE, CUTOUT THE DAMAGED AREA; FABED Z ANGLE AND REPAIR PARTS; INSTALLED Z ANGLE AND REPAIR PARTS ON APU RAM AIR INTAKE DUCT IAW SRM 51-40-02, 51-70-13 FIG 1 DWG 65-50938Dec 4, 2000 · N334AW · Boeing 737300 · APU Cowling/ContainmentSDR AWXA0001007Fitting · gougedLEFT PYLON I/B AT FRAME TOP SURFACE AT PANEL 5735L GOUGED BEYOND LIMITS AT I/B FASTNER. BLENDED GOUGE IAW 57-20-01 AND EO 03-1754-00355; ALL FABED SHIM AND FLAP PEENED IAW SOPM 20-10-03 AWA ER 03-5754-00333-001; HFC NO CRACKS NOTED ; INSTALLED SHIM IAW 51-40-0Dec 4, 2000 · N334AW · Boeing 737300 · Nacelle/Pylon, Attach FittingsSDR AWXA0001006Seat Track · damagedCABIN SEAT TRACK LBL 45 AREAS BLENDED OUT OF LIMITS FROM STA 862 TO 873. REMOVED SEAT TRACK LBL 45 STA 807 TO 947; FABED SEAT TRACK IAW SRM 53-60-52 FIG 1; TREATED, PRIMED, AND TOP COATED IAW 51-20-01 DWG 51-21-21; INSTALLED SEAT TRACK IAW 51-40-02 AND 53-60-5Dec 4, 2000 · N334AW · Boeing 737300 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA0001004Floorbeam · damagedCABIN FLOORBEAM WEB AT STA 328, LBL 46 WAS DAMAGED DURING MAINT. CUTOUT DMGD WEB, FABED FILLER AND DOUBLER IAW ER 03-5310-00327-JS2, SRM 51-20-1; INSTALLED REPAIR PARTS IAW ER 03-5310-00327JS2 AND SRM 51-40-02Dec 4, 2000 · N334AW · Boeing 737300 · Fuselage Main, Floor BeamSDR AWXA0001014Floorbeam · corrodedCABIN FLOOR BEAM STA 312 RBL 12 - LBL 12 TOP OF FLOOR BEAM WENT OUT OF LIMITS AFTER CORROSION REMOVAL. REMOVED UPPER TEE AT STA 312 LBL 18 TO RBL 22 AND A STIFFENER AT BETWEEN STA 312 AND 328 LBL 12 IAW SRM 51-40-02; FABED AND INSTALLED CHORD IAW 53-10-51 FIG Dec 1, 2000 · N334AW · Boeing 737300 · Fuselage Main, Floor BeamSDR AWXA0001013Stringer · crackedCABIN STA 500C + 6 LONGERON 16L HAS CRACK. REMOVED DMGD STRINGER IAW BSB 737-53-1145; NDT VERIFIED NO CRACKS; FABED AND INSTALLED REPAIR PARTS IAW BSB 737-53-1145 AND AWA ER 03-5314-00320-DL1Dec 1, 2000 · N334AW · Boeing 737300 · Fuselage Main, Longeron/StringerSDR AWXA0001003Frame · corrodedCABIN FS 318 STR 4L REINFORCING STRAP AND FRAME CRACKED. REMOVED STRAP AND FRAME IAW SRM 51-40-02; FABED STRAP AND INTERCOSTAL IAW 53-10-0 FIG 1; TREATED AND PRIMED IAW 51-10-2; INSTALLED PARTS IAW 51-40-02Dec 1, 2000 · N334AW · Boeing 737300 · Fuselage Main, FrameSDR AWXA0001002Intercostal · crackedINTERCOSTAL CRACKED @ FS 178 WL 195 RBL 24. REMOVED INTERCOSTAL IAW SRM 51-40-02; REMOVED DMGD AREA IAW 53-10-08 FIG 101, NDT TO VERIFY CRACK REMOVAL - NO CRACKS NOTED AROUND CUTOUT; REINSTALLED INTERCOSTAL IAW 51-40-02Dec 1, 2000 · N334AW · Boeing 737300 · Fuselage Main, BulkheadSDR 20001031SH012Spar · cracked737300/737400/737500 WERE FOUND WITH A CRACK IN THE UPPER AFT SPAR T-CAP OF THE OUTBOARD MIDFLAP. CRACK IS LOCATED ON THE VERTICAL LEG OF THE SPAR NEAR THE EXHAUST GATE HINGE. EACH OF THE LAST FOUR 737 OTBD MIDFLAPS EVALUATED WERE CRACKED IN THE DESCRIBED LOOct 31, 2000 · Boeing 737300 · Trailing Edge FlapsSDR 20000501SH042Housing · crackedHOUSING HAS A HAIRLINE CRACK ALONG SEAM OF CASTING. LEAKAGE IS VISIBLE AT MOUNTING HOLES DURING NORMAL OPERATION. POSSIBLE CAUSE: WEAK POINT IN CASTING OF HOUSING. NOTED TO BE A RECURRING PROBLEM/DEFECT IN THE CASTING SEAM OF THESE HOUSINGS. SUBMITTER SUFeb 18, 2000 · Boeing 737300 · Hydraulic System, MainSDR 99ZZZX4064Housing · crackedINNER BORE OF HOUSING IS CRACKED IN TWO LOCATIONS POSSIBLY DUE TO FATIGUE.Sep 30, 1999 · Boeing 737300 · Drag Control ActuatorSDR 99ZZZX2366Housing · crackedHOUSING ASSY CRACKED AT PRESSURE PORT.May 27, 1999 · Boeing 737300 · Hydraulic Pump, AuxiliarySDR 99ZZZX1823Fitting · gougedTHE AUXILIARY ACTUATOR FITTING IS CONSTANTLY BEING RECEIVED INTO FACILITY WITH GOUGES ON THE INNER FACE OF THE LOWER ARM. THIS IS A WEAR AREA CIRCULAR IN SHAPE CAUSED BY THE ACTUATOR. AVERAGE GOUGE DEPTH IS .020 INCH - .025 INCH. THIS IS A COMMON PROBLEM REDec 15, 1998 · Boeing 737300 · Rudder StructureSDR A3L398031Bolt · brokenINSPECTION FOUND BROKEN WHEEL BOLT. (X)Mar 18, 1998 · Boeing 737300 · Wheel/Ski/FloatSDR 96ZZZX4609Housing · crackedHOUSING IS CRACKED IN THE BEARING RECESS AREA EXTENDING LATERALLY FROM THE RETRACT PRESSURE PORT. THIS MAY BE CAUSED BY A LACK OF PISTON SNUBBING ACTION DURING GROUND NO-LOAD CONDITIONS. SUBMITTER RECOMMENDS A RE-DESIGN OF THE HOUSING ASSEMBLY BY STRENGTHENIJul 19, 1996 · Boeing 737300 · Drag Control ActuatorSDR F3LA95017Target · out of adjustFLT NR 441 - DEN - UPON ARRIVAL, FLIGHT CREW REPORTED THE RIGHT MAIN LANDING GEAR UNSAFE LIGHT ILLUMINATED. MAINTENANCE ADJUSTED TARGET ON THE PROXIMITY SWITCH AND SYSTEM CHECKED OK. (M)Nov 21, 1995 · N2FOR · Boeing 737300 · Landing Gear Position and Warning
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