Boeing 737-230

Service difficulty reports · 466

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '737230'
  ORDER BY difficulty_date DESC"

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SDR P2EA00250Bulkhead · crackedSJO - DURING C-CHECK, LEFT SIDE CHORD AT BS 178 CRACKED .5 INCHES, WL 207 AND WL 190. REMOVED SIDE CHORD AND REPLACED CHORD WITH UPGRADED PART IAW SB 737-53A1173, SECTION III PART XI STEP H. (M)Sep 11, 2000 · N124NJ · Boeing 737230 · Fuselage Main, BulkheadSDR P2EA00249Beam · crackedSJO - DURING C-CHECK, VERTICAL BEAM CHORD CRACKED 1 INCH AT BS 178, WL 184 AND LBL 5.7. REPAIRED VERTICAL BEAM FORWARD CHORD AT BS 178 LBL 5.7 BETWEEN WL 177 AND WL 193 IAW SRM 53-10-11 FIG 8. (M)Sep 11, 2000 · N124NJ · Boeing 737230 · Fuselage Main, BulkheadSDR P2EA00241Fitting · corrodedDURING C-CHECK INSPECTION, (SB 737-55-1028) OF THE FIN ATTACHMENT FITTINGS, CORROSION WAS FOUNDON FIVE OF EIGHT ATTACHMENT LUGS. THE CORROSION WAS FOUND ON THE RT OUTBOARD AFT LUG, AFT FACE, RT OUTBOARD FORWARD LUG, FORWARD FACE, RT INBOARD AFT LUG, AFT FACE Aug 22, 2000 · N122NJ · Boeing 737230 · Vertical Stabilizer, Attach FittingsSDR P2EA00244Fitting · misdrilledDURING C-CHECK, LOWER HOLE IN FITTING AT BS 695 BORED SLIGHTLY OFFSET. ENLARGED HOLE TO .9375 DIA AND INSTALLED BUSHING IAW MPP B737-VAG-00-53-010. (M)Aug 17, 2000 · N122NJ · Boeing 737230 · Fuselage Main, Attach FittingsSDR P2EA00239Frame · crackedDURING C-CHECK, VERTICAL CHORD CRACKED .375 INCHES IN LENGTH AT BS 178, LBL 5.7 INCH AND WL 181.57. REPAIRED IAW SB 737-53A-1173 PARA B2 PAGE 70. (M)Aug 8, 2000 · N122NJ · Boeing 737230 · Fuselage Main, FrameSDR P2EA00236Seat Track · corrodedDURING C-CHECK, FOUND CORROSION (LEVEL 2) ON SEAT TRACK FROM BS 340 TO 360, LBL 45 AND WL 208. FABRICATED SEAT TRACK IAW SRM 51-20-1 AND INSTALLED IAW MM 25-52. (M)Aug 8, 2000 · N122NJ · Boeing 737230 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA00242Frame · crackedDURING C-CHECK, LEFT CHORD CRACKED 1.25 INCH AT BS 178 WL 207 AND LBL 23. REPAIRED CRACK IAW SB 737-53A-1173, FIG 61. (M)Aug 7, 2000 · N122NJ · Boeing 737230 · Fuselage Structure (General)SDR P2EA00245Skin · delaminatedDURING C-CHECK, RIGHT OUTBOARD FORE FLAP UPPER SKIN IS DELAMINATED (16 INCHES) AND DENTED. REPAIRED FORE FLAP IAW SRM 51-40-6 PAGE 8 PARA 11 AND SRM 51-40-6 PAGE 45. (M)Aug 4, 2000 · N122NJ · Boeing 737230 · Leading Edge DevicesSDR P2EA00235Frame · crackedDURING C-CHECK, FRAME LOWER LOBE CRACKED LENGTH 4 INCH, AT BS 312 BETWEEN STRINGER 24L AND 25L. REPAIRED FRAME AT BS 312 BETWEEN STRINGER 24L AND 25L IAW SRM 53-10-4 FIG 10. (M)Aug 4, 2000 · N122NJ · Boeing 737230 · Fuselage Main, FrameSDR TSAA0033184Battery Pack · inoperativeREPLACED NR 5 FLOOR EMERGENCY LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Aug 3, 2000 · N821AL · Boeing 737230 · Emergency LightingSDR TSAA0033181Battery Pack · inoperativeREPLACED CENTER EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 2000 · N823AL · Boeing 737230 · Emergency LightingSDR TSAA0033179Light · inoperativeREPAIRED BROKEN WIRE TO LEFT OVERWING EXIT IDENTIFIER LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 2000 · N818AL · Boeing 737230 · Emergency LightingSDR TSAA0033175Battery Pack · inoperativeREPLACED CENTER EMERGENCY EXIT LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 2000 · N823AL · Boeing 737230 · Emergency LightingSDR TSAA0033174Light · inoperativeREPAIRED BROKEN WIRE TO LEFT OVERWING EXIT IDENTIFIER LIGHT. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Jul 25, 2000 · N818AL · Boeing 737230 · Emergency LightingSDR P2EA00227Mount · wornYYC - DURING C-CHECK, WHILE COMPLYING WITH VANGUARD EO NR 963727A065 FRUEGER FLAP FITTING INSPECTION FOUND THREE ACTUATOR MOUNT LUGS WORN DUE TO MISSING RUB STRIPS. NR 1 LEFT FSS 180.36, NR 3 RIGHT FSS 129.80 AND NR 4 RIGHT FSS 180.36. WEAR DEPTH MEASURED NRJul 14, 2000 · N123NJ · Boeing 737230 · Leading Edge DevicesSDR P2EA00222Skin · misdrilledYYC - DURING C-CHECK, WHILE REPAIRING STRINGER 25R AT BS 304.5 SKIN AND STRAP WAS DAMAGED BY DRILLING 1.20 INCH LONG BY .125 INCH WIDE BY .036 INCH DEEP. REPAIRED SKIN AND STRAP AT STRINGER 25R, BS 304.5 IAW SRM 53-30-3 FIG 6. (M)Jul 14, 2000 · N123NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA00219Stringer · corrodedYYC - DURING C-CHECK, FOUND STRINGER 25R FROM BS 284 THROUGH BS 303.5 WITH CORROSION 19.5 INCHES LONG BY 1 INCH WIDE BY .036 DEEP. REPAIRED STRINGER 25R FROM BS 284 THROUGH BS 303.5 IAW SRM 53-10-3 FIG 1 SHEET 8. (M)Jul 13, 2000 · N123NJ · Boeing 737230 · Fuselage Main, Longeron/StringerSDR P2EA00213Channel · crackedYYC - DURING C-CHECK, FOUND THE CHANNEL AT BS 312 UPPER AIRSTAIR FORWARD STOP PAD WITH A CRACK LENGTH 3.5 INCHES. REPAIRED CHANNEL AT BS 312 UPPER AIRSTAIR FORWARD STOP PAD IAW SRM 51-40-3 FIG 1 AND 53-10-9 FIG 7. (M)Jul 13, 2000 · N123NJ · Boeing 737230 · Entrance StairsSDR P2EA00217Skin · delaminatedYYC - DURING C-CHECK, FOUND THE RIGHT OUTBOARD AFT FLAP OUTBOARD AFT CORNER DELAMINATED 1.5 INCHES LONG BY .50 INCHES WIDE. REPAIRED THE RIGHT OUTBOARD AFT FLAP OUTBOARD AFT CORNER DELAMINATION IAW SRM 51-40-06 FIG 2. (M)Jul 11, 2000 · N123NJ · Boeing 737230 · Trailing Edge FlapsSDR P2EA00214Structure · dentedYYC - DURING C-CHECK, FOUND THE APU DOOR WITH DENT .8 INCH LONG BY .8 INCH WIDE BY .080 INCH DEEP, 26 FEET FROM AFT END AND LBL 18. REPAIRED APU DOOR DENT IAW SRM 52-00-3 FIG 1. (M)Jul 10, 2000 · N123NJ · Boeing 737230 · Auxiliary Power Unit (APU) DoorsSDR P2EA00230Skin · delaminatedYYC - DURING C-CHECK, FOUND THE NR 2 SPOILER UPPER SURFACE WITH DELAMINATION 4 INCHES LONG BY 3 INCHES WIDE BY .125 INCHES DEEP. REPLACED THE NR 2 SPOILER WITH SERVICEABLE SPOILER IAW MM 27-61-11 PAGE 401-602. (M)Jul 7, 2000 · N123NJ · Boeing 737230 · SpoilersSDR P2EA00229Attach Fitting · corrodedYYC - DURING C-CHECK, WHILE COMPLYING WITH VANGUARD EO NR 0055A024 VERTICAL STAB ATTACH LUG MOD, FOUND THE AFT FACE OF THE RIGHT AFT LUG AND THE FORWARD FACE OF THE RIGHT SECOND FROM AFT LUGS WTH CORROSION. THE RIGHT SECOND FROM AFT LUG DEFECT SIZE FORWARD FAJul 7, 2000 · N123NJ · Boeing 737230 · Vertical Stabilizer, Attach FittingsSDR P2EA00216Angle · crackedYYC - DURING C-CHECK, FOUND ANGLE JUST AFT OF THE LEFT SIDE OF VERTICAL STAB ATTACH BOLTS BS 1088 WITH A CRACK 1 INCH LONG. REPLACED THE ANGLE JUST AFT OF THE LEFT SIDE OF VERTICAL STAB ATTACH BOLTS BS 1088 WITH ANGLE FABRICATED AND INSTALLED IAW SRM 51-10-2 Jul 7, 2000 · N123NJ · Boeing 737230 · Fuselage Miscellaneous StructureSDR P2EA00228Skin · crackedYYC - DURING C-CHECK, FOUND THE LEFT WING LEADING EDGE SKIN AT THE NR 2 SLAT OUTBOARD CUTOUT WITH A CRACK .65 INCH. REPAIRED THE LEFT WING LEADING EDGE SKIN AT THE NR 2 SLAT OUTBOARD CUTOUT IAW SRM 57-20-1 FIG 1. (M)Jul 5, 2000 · N123NJ · Boeing 737230 · Wing, Plate/SkinSDR P2EA00215Latch · crackedYYC - DURNG C-CHECK, FOUND THE APU DOOR WITH A CRACK .50 INCH AT THE LEFT AFT DOOR LATCH. REPAIRED THE APU DOOR CRACK .50 LENGTH AT THE LEFT AFT DOOR LATCH IAW SRM 51-40-3. (M)Jul 5, 2000 · N123NJ · Boeing 737230 · Auxiliary Power Unit (APU) DoorsSDR TSAA0079163Transmitter · defectiveFLT 43 - ITO-HNL - NR 2 ENGINE OIL QTY GAUGE DROPPED TO ''0'' INDICATION INFLIGHT. RETURNED TO ITO, UNEVENTFUL LANDING. INSPECTED NR 2 ENGINE OIL QTY, OIL LEVEL GOOD. REMOVED AND REPLACED THE NR 2 ENGINE OIL QTY TRANSMITTER PER MM 79-31-00. OPS AND LEAK CHJul 3, 2000 · N823AL · Boeing 737230 · Engine Oil QuantitySDR P2EA00218Rib · dentedYYC - DURING C-CHECK, WHILE REMOVING THE VERTICAL STAB, THE VERTICAL STAB WAS DAMAGED AT THE FORWARD RIB WEB BS 1007 UPPER END RESULTING IN A DENT 3 INCHES LONG, 4 INCHES WIDE, .250 INCHES DEEP. REPAIRED THE VERTICAL STAB FORWARD RIB WEB BS 1007 UPPER END IAWJun 30, 2000 · N123NJ · Boeing 737230 · Vertical Stabilizer, Spar/RibSDR P2EA00231Skin · gougedYYC - DURING C-CHECK, THE LEFT ELEVATOR LOWER SKIN AT ELEVATOR STATION 80 WAS DAMAGED BY MAN LIFT, 6 INCHES LONG BY 6 INCHES WIDE, 1 INCHE DEEP. REPAIRED THE LEFT ELEVATOR LOWER SKIN AT ELEVATOR STATION 80 IAW SRM 51-40-9 FIG 1 AND 2. (M)Jun 26, 2000 · N123NJ · Boeing 737230 · Elevator StructureSDR P2EA00232Structure · corrodedYYC - DURING C-CHECK, FOUND THE LEFT MAIN LANDING GEAR INNER DOOR EDGE FRAME CASTING CORRODED, 16 INCHES LONG, 1 INCH LONG, .20 INCH DEEP. REPLACED THE LEFT MAIN LANDING GEAR INNER DOOR WITH SERVICEABLE GEAR DOOR IAW BMM 32-13-11. (M)Jun 25, 2000 · N123NJ · Boeing 737230 · Landing Gear DoorsSDR P2EA00199Fan · seizedDEN - FLT 301 - AFTER LANDING, LIGHT SMOKE AND FUMES WERE NOTED IN COCKPIT. DEFERRED CONTROL CABIN AIR FLOW FAN PER MEL 21-30 CONTROL ITEM NR M124377. REFERENCE MEL 21-30 CONTROL ITEM NR M124377 CONTROL CABIN AIR FLOW FAN INOPERATIVE. REMOVED AND REPLACED CJun 6, 2000 · N124NJ · Boeing 737230 · Air Distribution FanSDR TSAA0056137Seal · leakingFLT 88 - HNL-KOA - UNABLE TO PRESSURIZE AIRCRAFT, OUTFLOW VALVE FULLY CLOSED. FIRST OFFICERS SLIDING WINDOW VERY LOUD WIND NOISE. ABORTED TAKEOFF AND RETURNED TO GATE. REPLACED FIRST OFFICERS SLIDING WINDOW SEAL DUE TO WORN. CLEANED FORWARD ENTRY DOOR UPPEMay 18, 2000 · N823AL · Boeing 737230 · Flight Compartment WindowsSDR TSAA0033125Battery Pack · inoperativeREPLACED AFT SERVICE DOOR EMERGENCY EXIT IDENTIFIER BATTERY PACK. OPS CHECK GOOD. AIRCRAFT RETURNED TO SERVICE. (M)Apr 24, 2000 · N818AL · Boeing 737230 · Emergency LightingSDR EE4Y2000002Skin · debondedDURING HEAVY MAINTENANCE INSPECTION, LEFT WING INBOARD FLAP TRAILING EDGE SKIN WAS FOUND DISBONDED AT THREE DIFFERENT LOCATIONS. TOTAL AREA DAMAGED WAS 89 SQUARE INCHES. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 19, 2000 · N621AC · Boeing 737230 · Trailing Edge FlapsSDR EE4Y2000005Intercostal · crackedDURING HEAVY MAINTENANCE INSPECTION, FOUND FORWARD CARGO COMPARTMENT INTERCOSTAL CRACKED AT BS 500 AND BS 460, AND STR 2L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 19, 2000 · N621AC · Boeing 737230 · Fuselage Miscellaneous StructureSDR EE4Y2000003Skin · delaminatedDURING HEAVY MAINTENANCE INSPECTION FOUND RIGHT WING OUTBOARD FLAP LOWER KSI MID-SECTION DELAMINATED BETWEEN WBL 390 AND WBL 397. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 19, 2000 · N621AC · Boeing 737230 · Trailing Edge FlapsSDR EE4Y2000001Skin · canningDURING HEAVY MAINTENANCE INSPECTION, FOUND SKIN WITH OIL CAN DAMAGE AT BS 331 BETWEEN STR 24R AND STR 25R. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 19, 2000 · N621AC · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0022120Connector · contaminatedFLT 87-KOA-HNL-AT FL190, A/C STARTED ROLLING AND YAWING INCREASING IN RATE. DISENGAGED AUTOPILOT, ROLL AND YAW INCREASED. YAW DAMPER DISENGAGED, PILOT CONTROLLED ROLL AND A/C STABILIZED. DECLARED EMERG, FOUND YAW DAMPER C/B TRIPPED DUE TO COFFEE SPILLAGE ON YAApr 13, 2000 · N818AL · Boeing 737230 · Auto Flight SystemSDR P2EA00110Engine · vibrationMCI - UNUSUAL VIBRATION NOTED FROM NR 1 ENGINE AT IDLE TO 55 PERCENT N-1 AFTER PUSHBACK. REPLACED NR 1 ENGINE PER VANGUARD TASK CARD J271-00-01-C. LEAK AND OPERATIONAL CHECKS OK. (X)Apr 7, 2000 · N124NJ · Boeing 737230 · Engine (Turbine/Turboprop)SDR TSAA0033119Light · inoperativeREPLACED FORWARD ENTRY DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Apr 7, 2000 · N821AL · Boeing 737230 · Emergency LightingSDR TSAA0033118Light · inoperativeREPLACED FORWARD SERVICE DOOR EXIT LIGHT ASSY. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Apr 7, 2000 · N821AL · Boeing 737230 · Emergency LightingSDR EE4Y2000006Frame · dentedDURING HEAVY MAINTENANCE INSPECTION, FOUND FORWARD CARGO COMPARTMENT BS 550B FRAME DENTED BETWEEN STR 23L AND STR 24L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 1, 2000 · N621AC · Boeing 737230 · Fuselage Main, FrameSDR EE4Y2000004Cargo Track · corrodedDURING HEAVY MAINTENANCE INSPECTION, FOUND TIE DOWN SUPPORT BASE AND STRAP CORRODED IN FORWARD CARGO COMPARTMENT AT BS 440 AND BS 460, BETWEEN STR 20L AND STR 25L.. REASON FOR THIS DAMAGE WAS UNKNOWN. (X)Apr 1, 2000 · N621AC · Boeing 737230 · Fuselage, Seat/Cargo Attach FittingsSDR P2EA00069Skin · crackedMDW - FUSELAGE DAMAGED AT BS 794 BETWEEN S21R AND S22R BY BELT LOADER DURING THROUGH FLIGHT SERVICE. REPAIRED FUSELAGE SKIN AT BS 794, S21R AND S22R PER FEC DRAWING NR 005301 AND 005302, FAA FORM 8110-3. (M)Mar 19, 2000 · N124NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR TSAA0033087Battery Pack · inoperativeREPLACED NR 1 FLOOR LIGHT EMERGENCY BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 11, 2000 · N823AL · Boeing 737230 · Emergency LightingSDR TSAA0033086Light · inoperativeREPLACED THE FORWARD AND AFT SERVICE DOOR EXIT LIGHT ASSY DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 10, 2000 · N821AL · Boeing 737230 · Emergency LightingSDR TSAA0033075Battery Pack · inoperativeREPLACED NR 3 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 5, 2000 · N818AL · Boeing 737230 · Emergency LightingSDR TSAA0033076Battery Pack · inoperativeREPLACED NR 1 FLOOR LIGHT BATTERY PACK DUE TO INOPERATIVE. OPS CHECK OK. AIRCRAFT RETURNED TO SERVICE. (M)Mar 3, 2000 · N818AL · Boeing 737230 · Emergency LightingSDR TSAA0032078Control Valve · inoperativeFLT 282 - HNL-KOA - AFTER TAKEOFF, THE LANDING GEAR HANDLE FAILURE TO CYCLE UP. LOCKED OUT IN OFF DETEND. WOULD NOT GO UP. ENGAGED MANUAL OVERRIDE AND RETRACTED GEAR AND CONTINUED TO HNL FOR UNEVENTFUL LANDING. REMOVED AND REPLACED THE GROUND SPOILER VALVEFeb 29, 2000 · N823AL · Boeing 737230 · Landing Gear Retraction/Extension SystemSDR P2EA00019Skin · lightning strikeMCI - FLT 410 - LIGHTNING STRIKE IN FLIGHT. INSPECTED A/C PER MM 5-51-151. FOUND ONLY SMALL LIGHTNING BURNS ON BOTTOM RIGHT SIDE OF FUSELAGE. REPAIRED PER SRM 53-30-03. (M)Feb 17, 2000 · N123NJ · Boeing 737230 · Fuselage Main, Plate/SkinSDR P2EA00018Skin · lightning strikeMCI - FLT 410 - LIGHTNING STRIKE IN FLIGHT. ACCOMPLISHED LIGHTNING STRIKE INSPECTION, FOUND VERY MINOR BURNS AT STATION 178-227, 6 O''CLOCK POSITION. REPAIRED PER SRM 53-30-3. (M)Feb 17, 2000 · N123NJ · Boeing 737230 · Fuselage Main, Plate/Skin
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