Boeing 737-130

Service difficulty reports · 287

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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 = '737130'
  ORDER BY difficulty_date DESC"

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SDR CALA9600856Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED IN TWO PLACES AT STA 1016, S29R. THE DENTED AREAS WERE CUT OUT, A REPAIR DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 SRM 51-30-2 AND 51-10-2.May 29, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9600855Stringer · corrodedINSPECTION FOUND STRINGER CHANNEL CORRODED AT STA 351.2 TO 360, S20L. THE STRINGER CHANNEL WAS REMOVED AND A NEW CHANNEL WAS FABRICATED AND INSTALLED IAW SRM 51-10-2, 51-30-2 AND BOEING DRAWING 69-48934.May 29, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/StringerSDR CALA9600854Angle · corrodedINSPECTION FOUND NOSE WHEEL WELL CEILING SUPPORT I BEAM AND ATTACHING ANGLES CORRODED. THE BEAM AND ANGLES WERE REMOVED. A NEW BEAM AND ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-5, 51-30-2 AND 51-10-2.May 29, 1996 · N24213 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9600853Frame · crackedINSPECTION FOUND A 3 INCH CRACK IN UPPER FLANGE OF C-1 DOORWAY AFT FRAME. THE CRACKED FRAME WAS REMOVED AND A NEW FRAME SECTION WAS FABRICATED AND INSTALLED IAW SRM 51-30-2, 51-10-2 AND BOEING DRAWING 65C35242.May 29, 1996 · N24213 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CALA9600850Skin · dentedINSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9600849Skin · dentedINSPECTION FOUND SKIN DENTED BETWEEN STRINGER 23R AND 24R AT BS 394. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A DOUBLER AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3 FIGURE 6.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9600848Stringer · corrodedINSPECTION FOUND A 3 INCH SECTION OF STRINGER 21R CORRODED AT BS 416. THE CORRODED SECTION OF STRINGER WAS REMOVED AND REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/StringerSDR CALA9600847Stringer · corrodedINSPECTION FOUND CORROSION OVER AN 18 INCH SECTION OF STRINGER 22R BETWEEN BS 390 AND 410. THE CORRODED SECTION OF STRINGER WAS REMOVED. REPAIR CHANNEL AND ANGLES WERE INSTALLED IAW SRM 53-10-3 FIGURE 1.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Longeron/StringerSDR CALA9600846Skin · creasedINSPECTION FOUND SKIN CREASED FROM BS 228 TO 360, JUST ABOVE STRINGER 19R. THE DAMAGED SKIN WAS CUT OUT, REPAIR DOUBLERS AND FILLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 16.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9600845Floorbeam · corrodedINSPECTION FOUND CORROSION ON AFT UPPER FLANGE OF FLOORBEAM AT BS 294.5, RBL 20 TO RBL 40. THE CORRODED SECTION OF FLOORBEAM WAS REMOVED, A NEW SECTION OF FLOORBEAM AND SPLICES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4 FIGURE 1.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Floor BeamSDR CALA9600844Skin · corrodedINSPECTION FOUND SKIN CORRODED AT BS 410, STRINGER 18L. THE CORRODED SKIN WAS CUTOUT. A REPAIR DOUBLER AND FILLER WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 6.May 27, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CALA9600852Skin · dentedINSPECTION FOUND FUSELAGE SKIN DENTED AT STA 344 TO 380, STRINGER 20R TO 22R. THE DENTED AREA OF SKIN WAS CUT OUT AND NEW SKIN, FILLER AND DOUBLER WERE FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 1 AND 9, SRM 51-10-2 AND 51-30-2.May 24, 1996 · N24213 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960643Fuel Control · inoperativeFLT NR 324 - EWR - THE NR 1 ENGINE BEGAN TO SURGE SEVERELY AFTER TAKEOFF FROM EWR. ALL ENGINE GAUGES WERE SHOWING SURGE AND IT COULD BE FELT. THE ENGINE WAS NOT SHUTDOWN. THE AIRCRAFT WAS RETURNED TO EWR WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND May 23, 1996 · N14212 · Boeing 737130 · Fuel Control/Turbine EnginesSDR CAL960560Hydraulic Line · chafedEWR - FLT 0674 - THE B-HYDRAULIC SYSTEM LOW QUANTITY ILLUMINATED ON APPROACH TO DWR. THE 'A' AND 'B' SYSTEMS REMAINED AT 3,000 PSI WITH 2 GALLONS QUANTITY. THE GEAR AND FLAPS EXTENDED NORMALLY. THE QUANTITY WENT TO 1 GALLON WITH T/R ACTIVATED AND RETURNED TMay 6, 1996 · N44214 · Boeing 737130 · Hydraulic System, MainSDR CAL960529Skin · crackedGSO - REMOVED DAMAGE AREA AND FABRICATED DOUBLER, INSTALLED DOUBLER AT STRINGER 20R - STATION 192 PER SRM 53-30-3. (M)Apr 25, 1996 · N16201 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960515T1 Blade · brokenTHE NR 1 ENGINE OIL PRESSURE READ 60 PSI, BUT FLUCTUATED PLUS OR MINUS 5 PSI AND WITHIN 30 SECONDS THE OIL TEMPERATURE BEGAN RISING RAPIDLY. THE ENGINE WAS SHUT DOWN AND RETURNED TO GSO. THE NR 1 ENGINE WAS REMOVED AND REPLACED. SHOP TEAR-DOWN FINDINGS REVEApr 21, 1996 · N14206 · Boeing 737130 · Turbine SectionSDR CAL960511Switch · inoperativeFLT NR 234 - EWR - RIGHT MAIN LANDING GEAR RED UNSAFE LIGHT ILLUMINATED, AFTER GEAR LOWERED DURING APPROACH FOR LANDING. CYCLED GEAR, RED AND GREEN LIGHT FLICKERED ALTERNATELY DURING SECOND APPROACH. FOUND RIGHT DOWNLOCK SENSOR AT FAULT, REPLACED SAME PER MXApr 21, 1996 · N16201 · Boeing 737130 · Landing Gear Position and WarningSDR CAL960611Skin · disbondingGSO - INSPECTION FOUND SKIN PANEL DISBONDING FROM BS 360R TO BS 450R, STR 19R - STR 26R. THE SKIN PANEL WAS REMOVED AND A NEW SKIN AND SPLICE STRAP WERE FABRICATED AND INSTALLED IAW SRM 51-10-2, SRM 51-30-2, AND BOEING DRAWING 67-45768-127. (X)Apr 18, 1996 · N14206 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960612Skin · creasedGSO - INSPECTION FOUND SEVERAL CREASES IN LOWER HALF OF C-1 DOOR SKIN PANEL. THE DAMAGED SECTION OF SKIN WAS CUT OUT, A SKIN FILLER AND DOUBLER SPLICE PLATE WERE FABRICATED AND INSTALLED IAW SRM'S 52-30-2, 53-30-3, 51-10-2, AND 51-30-2. (X)Apr 17, 1996 · N14206 · Boeing 737130 · Cargo/Baggage DoorsSDR CAL960499Flap · damagedFLT NR 439 - ORD - WHILE FLAPS WERE BEING MOVED AFTER TAKEOFF, THE AIRCRAFT ROLLED RIGHT. ABNORMAL AMOUNT OF LEFT RUDDER WAS REQUIRED TO MAINTAIN DIRECTIONAL CONTROL OF AIRCRAFT. MAINTENANCE FOUND THE RIGHT INBOARD TRAILING EDGE FOREFLAP DAMAGED AND THE INBOApr 16, 1996 · N14212 · Boeing 737130 · Trailing Edge FlapsSDR CALA960491Battery · dischargedGSO - THE RIGHT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE RIGHT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (XApr 15, 1996 · N77215 · Boeing 737130 · Emergency LightingSDR CAL960492Battery · dischargedGSO - THE LEFT OVERWING EXTERIOR EMERGENCY LIGHTS FAILED CAPACITY CHECK. THE LEFT POWER SUPPLY BATTERY WAS REPLACED IAW MM 33-51-31 AND OPERATION OF THE LIGHTS WAS RESTORED. (X)Apr 15, 1996 · N77215 · Boeing 737130 · Emergency LightingSDR CAL960613Skin · crackedGSO - INSPECTION FOUND AFT EDGE OF C-2 DOOR SKIN BUCKLED AND CRACKED IN TWO PLACES. THE CRACKS WERE .75 INCH LONG. THE DAMAGED AREA WAS CUT OUT. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 52-00-03. (X)Apr 14, 1996 · N14206 · Boeing 737130 · Cargo/Baggage DoorsSDR CAL960485Chord · crackedGSO - INSPECTION FOUND LT OUTBOARD CHORD CRACKED PAST SECOND FASTENER HOLE AT STA 727. THE CHORD SEGMENT WAS REMOVED AND RPELACED IAW BOEING DRAWING 65C33722. (X)Mar 27, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960484Floor Beam · crackedGSO - INSPECTION FOUND A 2 INCH CRACK IN RADIUS OF FLOOR BEAM LOWER T-CHORD AT BBL ZERO, STA 675. THE FLOOR BEAM CHORD WAS REPAIRED IAW ECRA 5710-01462 AND BOEING DRAWINGS 65C19643, 65C17173, ND 65C17103. (X)Mar 25, 1996 · N77215 · Boeing 737130 · Fuselage Main, Floor BeamSDR CAL960483Skin · delaminatedGSO - INSPECTION FOUND RT AILERON UPPER SURFACE DELAMINATED AT OUTBOARD END OF TRIM TAB CUT-OUT. THE DELAMINATED AREA WAS REMOVED. A FILLER AND DOUBLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 51-40-6, SRM 51-10-2, AND SRM 51-20-21. (X)Mar 25, 1996 · N77215 · Boeing 737130 · AileronsSDR CAL960386Hyd Line · leakingBUF - FLT 1420 - AIRCRAFT LOST A-SYSTEM HYDRAULIC QUANTITY WHILE EN ROUTE FROM EWR TO BUF. THE AIRCRAFT LANDED IN BUF WITHOUT INCIDENT. MAINTENANCE FOUND THE HYDRAULIC PRESSURE LINE AT SYSTEM 'A' MODULAR UNIT LEAKING. THE PRESSURE LINE WAS REMOVED AND REPLAMar 24, 1996 · N44214 · Boeing 737130 · Passenger/Crew DoorsSDR CAL960487Skin · corrodedGSO - INSPECTION FOUND FUSELAGE SKIN CORRODED AT STA 259 TO STA 306, STR 24L TO STR 27L. THE CORRODED SECTION OF SKIN WAS CUT OUT. A NEW SECTION OF SKIN AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 51-30-2. (X)Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960486Stringer · corrodedGSO - INSPECTION FOUND STR 21R AND SKIN PANEL CORRODED AT STA 294.5. THE STRINGER AND SKIN PANEL WERE REMOVED. A NEW STRINGER, SKIN SECTION, AND DOUBLERS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 AND SRM 53-10-4. (X)Mar 23, 1996 · N77215 · Boeing 737130 · Fuselage Main, Longeron/StringerSDR CAL960489Skin · delaminatedGSO - INSPECTION FOUND UPPER AFT TRAILING EDGE SECTION OF RUDDER DELAMINATING. THE LENGTH OF DELAMINATION WAS APPROXIMATELY 12 INCHES. THE DELAMINATED SECTION OF RUDDER WAS REMOVED. A NEW CORE SECTION AND SKIN PLIES WERE FABRICATED AND BONDED IAW SRM 51-40-Mar 21, 1996 · N77215 · Boeing 737130 · Rudder, Plate/SkinSDR CAL960488Chord · corrodedGSO - INSPECTION FOUND LOWER CHORD CORRODED AT LEFT AND RIGHT ENDS ON UPPER AND LOWER SURFACES OF HORIZONTAL FLANGE, STA 294.5. THE CORRODED CHORD SEGMENT WAS REMOVED AND A REPLACEMENT WAS INSTALLED IAW SRM 51-30-2, SRM 51-30-5, AND SRM 51-10-2. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960482Skin · crackedGSO - INSPECTION FOUND A 0.3 INCH CRACK IN RT WING LEADING EDGE SKIN ON OUTBOARD EDGE OF OUTBOARD SLAT TRACK CUT-OUT, WBL 304. THE CRACK WAS ROUTED OUT IAW ECRA 5720-01512. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Wing, Plate/SkinSDR CAL960481Angle · crackedGSO - INSPECTION FOUND A .75 INCH CRACK IN AFT UPPER ATTACH ANGLE AND A 1 INCH CRACK IN FORWARD ATTACH ANGLE OF RT PRESSURE PANEL AT BS 663.75. BOTH ANGLES WERE REMOVED. NEW ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-30-2 AND SRM 51-10-2. (X)Mar 21, 1996 · N77215 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960370Light · inoperativeGSO - INSPECTION FOUND LT OVERWING EMERGENCY LIGHT INOPERATIVE. THE LT OVERWING EMERGENCY LIGHT ASSY REMOVED AND REPLACED. (X)Mar 15, 1996 · N14209 · Boeing 737130 · Emergency LightingSDR CAL960368Angle · corrodedGSO - INSPECTION FOUND SUPPORT ANGLE CORRODED AT LT SLIDING WINDOW, STA 248.7. THE CORRODED SECTION OF ANGLE WAS CUT OUT IAW SRM 51-40-4. REPAIR ANGLES WERE FABRICATED AND INSTALLED IAW SRM 51-40-4, AND SRM 51-30-2. (X)Mar 13, 1996 · N14209 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960353Tab Hinge Ftg · crackedGSO - INSPECTION FOUND LT WING NR 3 AILERON HINGE FITTING CRACKED AT TAB ATTACH POINT. THE CRACK LENGTH WAS NOT IDENTIFIED. THE HINGE ASSY WAS REMOVED AND REPLACED IAW SRM 51-30-2. (X)Mar 13, 1996 · N14209 · Boeing 737130 · Aileron TabsSDR CAL960351Skin · buckledGSO - INSPECTION FOUND FUSELAGE SKIN LAP BUCKLED AND A .25 INCH CRACK IN STR 20L, STA 767 TO STA 804. THE EFFECTED SECTION OF SKIN AND STRINGER WERE REMOVED. A SKIN AND STRINGER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3, FIGURE 13, SRM 53-10-3, FIGMar 12, 1996 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960350Slat · delaminatedGSO - INSPECTION FOUND THE OUTBOARD END OF NR 5 SLAT TOP SURFACE DELAMINATED IN AN AREA APPROXIMATELY 10 INCHES SQUARE. THE DELAMINATED SKIN AND CORE WERE REMOVED. THE AREA WAS REPAIRED BY REPLACING CORE AND APPLYING WET FIBERGLASS OVERLAYS IAW SRM 51-40-6. Mar 12, 1996 · N14209 · Boeing 737130 · Leading Edge DevicesSDR CAL960366Skin · corrodedGSO - INSPECTION FOUND SKIN AND CHORD CORROSION AT FORWARD RT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORRODED SECTION OF SKIN AND CHORD WERE REMOVED IAW SRM 51-30-2 AND SRM 53-30-3. NEW SKIN AND TEE SECTIONS WERE FABRICATED AND INSTALLED IAW SRM 53-30-3 Mar 8, 1996 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960359Door Frame · crackedGSO - INSPECTION FOUND A 1.25 INCH CRACK IN UPPER SECTION OF FORWARD R-2 DOORWAY FRAME AT STR 10R. THE FRAME SEGMENT WAS REMOVED AND REPLACED IAW SRM 51-30-2 AND BOEING DRAWING 65-46561. (X)Mar 8, 1996 · N14209 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960358Skin · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN SKIN AT FORWARD LOWER CORNER OF R-2 DOORWAY CUT-OUT. THE CRACK WAS CUT OUT. A DOUBLER, TRIPLER, AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-30-3. (X)Mar 8, 1996 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960356Web · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN WEB SECTION AT FORWARD R-2 TORQUE BOX UPPER HINGE ARM. THE CRACK WAS CUT OUT IAW SRM 51-40-2. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 51-40-2 AND BOEING DRAWING 65-46561. (X)Mar 8, 1996 · N14209 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960342Spoiler · bulgedGSO - INSPECTION FOUND THE NR 3 SPOILER UPPER SURFACE BULGED. THE SPOILER SKIN WAS RETURNED TO ORIGINAL CONTOUR BY FORMING IAW SRM 51-40-1. (X)Mar 8, 1996 · N14209 · Boeing 737130 · SpoilersSDR CAL960339Skin · dentedGSO - THE FORWARD LOWER CORNER OF FORWARD CARGO DOOR SKIN FOUND DENTED AND SCRATCHED. THE DAMAGED SKIN REMOVED OVER AN AREA OF APPROXIMATELY 6 INCHES IN DIAMETER IAW SRM 52-00-3, FIGURE 3. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 52-00-3, FIGURE 3,Mar 8, 1996 · N14209 · Boeing 737130 · Cargo/Baggage DoorsSDR CAL960355Skin · delaminatedGSO - INSPECTION FOUND NR 2 SPOILER SKIN INBOARD LOWER SURFACE DELAMINATED OVER AN AREA OF APPROXIMATELY 10 INCHES BY 8 INCHES. THE DELAMINATED AREA WAS REMOVED AND FIBERGLASS OVERLAYS WERE APPLIED IAW SRM 57-50-5. (X)Mar 6, 1996 · N14209 · Boeing 737130 · SpoilersSDR CAL960354Skin · gougedGSO - INSPECTION FOUND A GOUGE APPROXIMATELY 10 INCHES SQUARE IN TOP SURFACE OF LT WING INBOARD FOREFLAP. REMOVED GOUGED AREA AND POTTED CORE. REPAIRED WITH FIBERGLASS OVERLAYS IAW SRM 51-40-9. (X)Mar 6, 1996 · N14209 · Boeing 737130 · Trailing Edge FlapsSDR CAL960367Skin · corrodedGSO - INSPECTION FOUND SKIN CORROSION AT FORWARD LT CORNER OF E AND E BAY DOORWAY CUT-OUT. THE CORROSION WAS REMOVED AND A T-CHORD SECTION WAS CUT OUT IAW SRM 51-10-6. A REPAIR STRAP AND NEW T-CHORD WERE FABRICATED AND INSTALLED IAW ECRA 5310-01233. (X)Mar 5, 1996 · N14209 · Boeing 737130 · Fuselage Main, Plate/SkinSDR CAL960362Web · gougedGSO - INSPECTION FOUND A 1 INCH LONG GOUGE IN WEB OF E AND E COMPARTMENT AT LT SIDE OF DOORWAY CUT-OUT. THE WEB WAS REMOVED. A NEW WEB WAS FABRICATED AND INSTALLED IAW SRM 53-10-2 AND SRM 51-30-2. (X)Mar 5, 1996 · N14209 · Boeing 737130 · Fuselage Miscellaneous StructureSDR CAL960348Frame · crackedGSO - INSPECTION FOUND A 1 INCH CRACK IN FRAME AT STA 440 ABOVE STR 21L. A NEW FRAME AND CLIP WERE FABRICATED AND INSTALLED IAW BOEING DRAWING 65C25113 AND SRM 51-10-2. (X)Mar 5, 1996 · N14209 · Boeing 737130 · Fuselage Main, FrameSDR CAL960347Shear Tie · crackedGSO - INSPECTION FOUND A .50 INCH CRACK IN SHEAR TIE AT STA 440, BL ZERO. THE CRACKED SECTION SHEAR TIE WAS CUT OFF IAW SRM 53-10-4. AN ANGLE AND FILLER REPAIR WAS FABRICATED AND INSTALLED IAW SRM 53-10-4 AND SRM 51-30-2. (X)Mar 5, 1996 · N14209 · Boeing 737130 · Fuselage Miscellaneous Structure
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