Boeing 737-222

Service difficulty reports · 657

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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 = '737222'
  ORDER BY difficulty_date DESC"

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SDR P2EA99031Frame · crackedSJO - FRAME LOWER FLANGE CRACKED AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT, DEFECT SIZE, LENGTH .50 INCH. REPAIRED FRAME SECTION AT BS 440, BETWEEN STRINGER 28 LEFT AND STRINGER 28 RT PER SRM 53-10-4, FIG 10. (M)Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Main, FrameSDR P2EA99025Rib · crackedSJO - LEADING EDGE FSS 594, NR 1 SLAT OUTBOARD MAIN TRACK, RIB CRACKED. DEFECT SIZE, LENGTH .0125 INCH. REPLACED RIB AT FSS 594 PER SRM 51-10-1 PAGE 5 AND SRM 51-30-2. (M)Jan 6, 1999 · N209US · Boeing 737222 · Leading Edge DevicesSDR P2EA99024Splice · crackedSJO - STRINGER 10 LEFT SPLICE CRACKED AT BS 544, DEFECT SIZE, LENGTH .50 INCH. REPAIRED STRINGER 10 LEFT SPLICE BETWEEN BS 538 TO BS 550 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. (M)Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99023Splice · crackedSJO - STRINGER 27 LEFT SPLICE CRACKED FROM BS 420 TO BS 440, DEFECT SIZE, LENGTH .312. REPAIRED STRINGER 27 LEFT FROM BS 420 TO BS 442 PER SRM 53-10-3, FIG 1. (M)Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99021Cowl · wornSJO - NR 2 ENGINE NOSE COWL REAR MATTING SURFACE AT THE 6 O'CLOCK POSITION WORN. DEFECT SIZE, LENGTH 6 INCHES. NR 2 ENGINE NOSE COWL, REAR MATTING SURFACE FROM 5 O'CLOCK TO 7 O'CLOCK POSITION, STRAP REPAIRED PER SRM 54-10-3, FIG 4, SHEET 1, 2. (M)Jan 6, 1999 · N209US · Boeing 737222 · Engine Cowling SystemSDR P2EA99018Skin · crackedSJO - AFT RT SERVICE DOOR, LOWER FORWARD CORNER CRACKED. DEFECT SIZE, LENGTH .375 INCH. REPAIRED AFT GALLEY SERVICE DOOR FORWARD CUTOUT BETWEEN BS 749 TO BS 979 AND STRINGER 16 TO STRINGER 20 RT PER SRM 53-30-3, FIG 24. (M)Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99009Skin · crackedFUSELAGE MAIN ENTRY DOOR CUTOUT, ANGLE CRACKED BETWEEN STOP FITTING NR 6 AND NR 7, DEFECT SIZE, LENGTH .375. ANGLE REPLACED AT MAIN ENTRY DOOR, FORWARD SECTION PER SRM 51-10-1, PAGE 5, AND SRM 51-30-2. (M)Jan 6, 1999 · N209US · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA99008Skin · damagedSJO - RUDDER TRAILING EDGE ERODED AT RUDDER STATION 233, RIGHT SIDE, DEFECT SIZE, LENGTH 6 INCHES, WIDTH 4 INCHES. REPARIED RUDDER SECTION AT RUDDER STATION 233 PER SRM 51-40-9, PAR 3 AND 4. (M)Jan 6, 1999 · N209US · Boeing 737222 · Rudder, Plate/SkinSDR P2EA99007Skin · damagedSJO - HOLE FOUND AT RUDDER STATION 214, LEFT SIDE, TRAILING EDGE. DEFECT SIZE, DIAMETER .250 INCH. REPAIRED RUDDER PER SRM 51-40-9, PAR 3 AND 4 AT RUDDER STATION 214. (M)Jan 6, 1999 · N209US · Boeing 737222 · Rudder, Plate/SkinSDR P2EA99058Angle · crackedSJO - Q-CHECK ITEM. RIGHT WHEELWELL SUPPORT ANGLES CRACKED AT BS 664, WL 192, RBL 70. DEFECT SIZE: LENGTH 2.0 INCHES. PERFORMED ON STR 18A SHEER BEAM TO BE 664 FRAME ATTACHMENT MODIFICATION PER BOEING SB 737-53-1056, SEC III, FIG 1 DATED DECEMBER 15, 1978 Jan 5, 1999 · N209US · Boeing 737222 · Fuselage Miscellaneous StructureSDR P2EA99043Rib · crackedSJO - Q-CHECK ITEM. RIGHT WING, RIB CRACKED AT FRONT SPAR CAVITY AT FSS 479 (SLAT STA 231.84). DEFECT SIZE: LENGTH 0.0250 INCH. SEE COOPESA W.O. M1-0003-6-3, VAM 100 NR 148. (X)Jan 5, 1999 · N209US · Boeing 737222 · Wing, Rib/BulkheadSDR P2EA99040Rib · crackedSJO - Q-CHECK ITEM. RIGHT WING, FRONT SPAR RIB CRACKED AT FSS 595 (SLAT STA 387) DEFECT SIZE: LENGTH 0.0375 INCH. REPLACED RIB PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2. SEE COOPESA W.O. M1-0003-6-6, VAM 100 NR 151 FOR TECHNICAL AND PART FABRICATION INFORMATJan 5, 1999 · N209US · Boeing 737222 · Wing, Rib/BulkheadSDR P2EA99113Cam · mismanufacturedSJO - DURNIG Q-CHECK, THE RIGHT INBOARD MIDFLAP MAIN CARRIAGE CAM WAS FOUND WITH SHARP EDGES. THE AREA WAS REWORKED IAW COOPESA EO NR COO-3-27-139-99. (M)Jan 2, 1999 · N208AU · Boeing 737222 · Trailing Edge Flap Control SystemSDR P2EA00002Duct · crackedBUF - FLT 374 - NR 1 ENGINE OVERHEAT LIGHT ILLUMINATED IN FLIGHT, AFTER THRUST LEVER IS RETARDED TO FLIGHT IDLE THE OVERHEAT LIGHT EXTINGUISHED. AIRCRAFT RETURNED TO GROUND UNEVENTFUL. DUPLICATED PROBLEM ON GROUND, FOUND 13TH STAGE BLEED AIR DUCT CRACKED. RJan 2, 1999 · N209US · Boeing 737222 · Engine Bleed Air SystemSDR P2EA982283Warning System · activatedFLT 586 - MDW - ON LANDING ROLLOUT, NOSE GEAR UNSAFE LIGHT AND HORN CAME ON INTERMITTENTLY, INDICATIONS NORMAL ON TAXI IN. CHECKED NOSE GEAR DOWN LOCK SENSOR, ACTUATOR, AND ALL SENSOR WIRES. ALL OPS CHECKED NORMAL PER MM 32-61-51. ALSO, PERFORMED GEAR RETRADec 13, 1998 · N603DJ · Boeing 737222 · Landing Gear Position and WarningSDR P2EA98255Engine · failedFLT 408 - MCI - AIR RETURN, NR 2 ENGINE SHUTDOWN INFLIGHT. EMERGENCY DECLARED LANDING UNEVENTFUL. NR 2 ENGINE START VALVE ILLUMINATED INFLIGHT, ENGINE NR 2 SHUTDOWN IAW QRH RETURNED MCI. (M)Nov 22, 1998 · N209US · Boeing 737222 · Engine (Turbine/Turboprop)SDR P2EA98253Engine · overtempFLT 422 - MDW - NO EMERGENCY DECLARED LANDING UNEVENTFUL. ON TAXI IN OVERHEAT DETECTOR, NR 2 ENGINE CAME ON. ENGINE SHUT DOWN. (M)Nov 11, 1998 · N603DJ · Boeing 737222 · Engine (Turbine/Turboprop)SDR P2EA98247Fire Control Box · failedMSP - FLT 418 - EMERGENCY DECLARED NR 2 ENGINE SHUTDOWN INFLIGHT, LANDING UNEVENTFUL. ON CLIMB-OUT, NR 2 ENGINE OVERHEAT LIGHT ILLUMINATED. CHECKLIST COMPLIED WITH. REPLACED FIRE CONTROL BOX (MODULE), ALSO INSPECTED OVERHEAT LOOP. RAN ENGINE WITH BLEEDS ANNov 10, 1998 · N603DJ · Boeing 737222 · Fire DetectionSDR VJ9800617Fitting · corrodedLT MLG OUTER DOOR SUPPORT BEAM ATTACH FITTING, AFT SIDE OF REAR SPAR, HAS FRETTED CORROSION. REPLACED SUPPORT BEAM ATTACH FITTING IAW B737 SRM 57-15-01.Oct 31, 1998 · N468AT · Boeing 737222 · Landing Gear DoorsSDR VJ9800616Shear Tie · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, CORROSION WAS FOUND AT BS 285 LT SIDE BETWEEN W/W AND FUSELAGE SKIN AT THE BOTTOM SKIN. MECHANICALLY REMOVED CORROSION. FUSELAGE SKIN AND BEAM WERE WITH-IN THE SRM LIMITS. THE SHEAR TIE WAS OUT LIOct 29, 1998 · N468AT · Boeing 737222 · Fuselage Miscellaneous StructureSDR VJ9800615Bulkhead · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL. THE 540 BULKHEAD WAS FOUND WITH CORROSION AT THE BOTTOM STRINGERS 26 AND 28R. REMOVED TWO EACH DOUBLERS, CUT OUT CORROSION. FABRICATED AND INSTALLED INNER DOUBLER AND TWO EACH DOUBLERS IAW B737 SOct 29, 1998 · N468AT · Boeing 737222 · Fuselage Main, BulkheadSDR P2EA98207Ballast · failedFLT 418 - EMERGENCY DECLARED LANDING UNEVENTFUL. AT FL 220 SMELL SMOKE, THEN SMOKE ENTERED COCKPIT. MADE EMERGENCY LANDING AT MZV. FOUND BALLAST FOR FORWARD GALLEY LIGHTS INOP. DETERMINED TO BE SOURCE OF SMOKE. PULLED AND COLLARED CIRCUIT BREAKER. DEFERROct 29, 1998 · N603DJ · Boeing 737222 · Flight Compartment LightingSDR VJ9800614Gate · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL. THE L-2 DOOR BOTTOM FRAME WAS FOUND WITH CORROSION. CORROSION WAS OUT OF LIMITS IAW B737 SRM. REMOVED THE GATE AND INSTALLED IAW B737 SRM 51-30-2, 51-30-5 AND 52-00-2.Oct 27, 1998 · N468AT · Boeing 737222 · Passenger/Crew DoorsSDR P2EA98193Valve · leakingMSP - FLT 614 - NO EMERGENCY DECLARED. LOST ALL HYDRAULIC FLUID WHILE TAXIING IN. REPLACED LEFT INBOARD ANTI-SKID CONTROL VALVE, SERVICED HYDRAULIC RESERVOIR. OPS CHECK OK LEAK CHECK OK PER MM 32-42-31A. (M)Oct 26, 1998 · N209US · Boeing 737222 · Brake Anti-Skid SectionSDR P2EA98183Skin · dentATL - FLT 612 - THE FOLLOWING OCCURED WHILE RAMP AGENT WAS CONNECTING TOW BAR TO PUSH TRACTOR. L1 DOOR SKIN DAMAGED BY JETWAY. INSTALLED DOUBLER ON L1 DOOR PER SRM 52-00-3, FIG 5. (M)Oct 17, 1998 · N209US · Boeing 737222 · Passenger/Crew DoorsSDR P2EA98176Sensor · contaminatedMSP - FLT 614 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. RIGHT GEAR RED LIGHT STAYS ON WHEN GEAR RETRACTED UNTIL PRESSURE RELIEVED. LEVER MOVED TO OFF POSITION. FOUND UPLOCK SENSOR VERY DIRTY, CLEANED SENSOR. PERFORMED SENSOR RESISTANCE TEST PER MM 32-61Oct 9, 1998 · N209US · Boeing 737222 · Landing Gear Position and WarningSDR P2EA98174Connector · failedFLT 612 - MCI - EMERGENCY DECLARED, NR 1 ENGINE INFLIGHT SHUTDOWN, LANDING UNEVENTFUL. NR 1 FUEL HEAT VALVE CAME ON IN FLIGHT. NR 1 OIL TEMP EXCEEDED LIMTIS (TIME IN YELLOW BAND) SHUTDOWN NR 1 ENGINE, RETURNED TO MCI. FOUND WIRE BURNED AT 'B' PIN ON NR 1 FUSep 24, 1998 · N208AU · Boeing 737222 · Fuel HeaterSDR P2EA98173Connector · damagedFLT 590 - MCI - EMERGENCY DECLARED, NR 1 ENGINE INFLIGHT SHUTDOWN. LANDING UNEVENTFUL. SHUTDOWN NR 1 ENGINE DUE TO HIGH OIL TEMP. FOUND LOOSE PIN IN FUEL HEAT VALVE CONNECTOR. RESET PIN, CLEANED CONNECTOR. VALVE OPS CHECKED OK. RAN ENGINE, CYCLED FUEL HESep 23, 1998 · N208AU · Boeing 737222 · Fuel HeaterSDR P2EA98172Acm · failedATL - FLT 406 - RIGHT PACK PUTS SMOKE IN THE CABIN. RIGHT PACK DEFERRED PER MEL 21-1, CI NR M208057 ASSIGNED PER MAINTENANCE CONTROLLER. PERFORMED SPECIAL PROCEDURES 21-1 AND 21-2. PLACARDS INSTALLED. REPLACED RT AIR CYCLE MACHINE PER MM 21-51-11, M208057 Sep 22, 1998 · N208AU · Boeing 737222 · Cabin Cooling SystemSDR P2EA98171Circuit Breaker · trippedDEN - FLT 305 - EMERGENCY DECLARED, FLAPS UP LANDING UNEVENTFUL. FLAP GAUGE INDICATED SPLIT FLAPS LOCKED OUT. UPON INSPECTION, FOUND BOTH TRAILING EDGE CIRCUIT BREAKERS TRIPPED. RESET BREAKERS, SYSTEM OPS NORMAL THROUGH FULL RANGE. REF MM 27-58-0A. (X)Sep 21, 1998 · N209US · Boeing 737222 · Trailing Edge Flap Control SystemSDR CALA9801537Solenoid · inoperativeTHE LANDING GEAR HANDLE WOULD NOT MOVE PAST OFF POSITION TO UP UNLESS OVERRIDE TRIGGER WAS PULLED AFTER TAKEOFF. MAINTENANCE FOUND THE LANDING GEAR CONTROL LEVER LOCK SOLENOID AT FAULT. THE LEVER LOCK SOLENOID WAS REMOVED AND REPLACED IAW MM 32-31-31. IN ADAug 26, 1998 · N10236 · Boeing 737222 · Landing Gear SelectorSDR P2EA98162Battery Pack · dischargedPHX - DURING SCHEDULED MAINTENANCE, IT WAS NOTED THAT THE SEAT MOUNTED EMERGENCY EXIT LIGHTS ON ROWS 9 THROUGH 17 WERE INOPERATIVE. REPLACED BATTERY PACK. OPERATIONAL CHECK NORMAL. (M)Aug 24, 1998 · N209US · Boeing 737222 · Emergency LightingSDR P2EA98161Switch · out of adjustFLT 588 - WITH FLAPS AT 5 DEGREES AND GEAR UP THE GEAR HORN CAME ON AS NORMAL, WAS SILENCED, AND CAME ON AGAIN. HORN CONTINUED UNTIL GEAR WAS DOWN AND LOCKED. ADJUSTED FLAP LANDING WARNING SWITCH IN RIGHT WHEEL WELL IAW MM 31-26-12. HORN SOUNDS IN CORRECT PAug 19, 1998 · N208AU · Boeing 737222 · Landing Gear Position and WarningSDR P2EA98148Control Cable · brokenMDW - FLT 821 - NOSE WHEEL STEERING FAILED ON TAXI, PRIOR TO DEPARTURE. MAINTENANCE FOUND NOSE WHEEL STEERING CABLE BROKEN. CABLE WAS REPLACED AND SYSTEM TESTED GOOD IAW MM 32-51-31A AND MM 32-51-0. (X)Jul 31, 1998 · N209US · Boeing 737222 · Landing Gear Steering SystemSDR 98UAL900324Accessory Unit · failedBOTH TRANSPONDERS ARE INOPERATIVE. *S/D* THE CAUSE FOR THE APPARENT FAILURE OF BOTH TRANSPONDERS IS BELIEVED TO HAVE BEEN AN AIR/GROUND SENSING PROBLEM AS IT WAS ALSO REPORTED THAT THE AIRCRAFT WOULD NOT PRESSURIZE. ALSO, NOTED BY ENGINEERING, THE AIRCRAFT Jul 14, 1998 · N9009U · Boeing 737222 · Landing Gear Position and WarningSDR P2EA98126Skin · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-50-5325C, A CRACK WAS FOUND ON THE SKIN AT BS 727B PLUS 2. THE CRACK WAS 1.5 INCH IN LENGTH. DUE TO OTHER REPAIRS IN THE AREA, IT WAS DETERMINED BY BOEING TO REPLACED THE SKIN SECTION FROM BS 727 TJul 2, 1998 · N208AU · Boeing 737222 · Fuselage Main, Plate/SkinSDR P2EA98125Frame · misreamedSJO - AT A/C'S LAST C-CHECK, THE FRAME FITTING AT BS 685 LEFT WAS MISREAMED. BOEING APPROVED RETURN TO SERVICE PENDING REPLACEMENT AT NEXT SCHEDULED C-CHECK. A NON-ROUTINE WORK CARD WAS ISSUED TO ACCOMPLISH REPLACEMENT. FRAME FITTING REPLACEMENT ACCOMPLISHEJul 2, 1998 · N208AU · Boeing 737222 · Fuselage Main, FrameSDR P2EA98124Rib · crackedSJO - DURING C-CHECK, WHILE REMOVING RT WING INBOARD MID-FLAP TO FACILITATE OTHER MAINTENANCE OBSERVED TWO RIBS CRACKED AT WBL 87.7. NEWS RIBS FABRICATED BY COOPESA MACHINE SHOP AS PER COOPESA EO NR C00-3-57-330-98. INSTALLED IAW SRM 51-10-1 PAGE 5 AND 51-30Jul 1, 1998 · N208AU · Boeing 737222 · Wing, Rib/BulkheadSDR P2EA98121Stringer · crackedSJO - DURING C-CHECK, WHILE PERFORMING SKIN REPLACEMENT AT BS 727, A CRACK WAS FOUND ON STRINGER 19L. REPAIRED CRACK IAW SRM 53-10-3 FIG 2. (M)Jul 1, 1998 · N208AU · Boeing 737222 · Fuselage Main, Longeron/StringerSDR P2EA98123Angle · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-50-5325C, A CRACK WAS NOTED ON AN ANGLE LOCATED ON THE WING CENTER SECTION AT LBL 52.5. THE CRACK WAS 1.5 INCH IN LENGTH. REPAIRED ANGLE AT WING CENTER SECTION BETWEEN BS 575 AND 615, LBL 52, IAJun 30, 1998 · N208AU · Boeing 737222 · Wing Miscellaneous StructureSDR P2EA98122Rib · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-10-5726C, A CRACK WAS FOUND ON A RIB OF THE RT WING, INBOARD MID-FLAP. THE CRACK WAS LOCATED AT WBL 83 AND WAS 1 INCH IN LENGTH. THE RIB WAS REPLACED IAW SRM 51-10-1 PAGE 6. RIVETS REPLACED IAWJun 29, 1998 · N208AU · Boeing 737222 · Wing, Rib/BulkheadSDR P2EA98120Stringer · corrodedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD J2C-51-2125, CORROSION WAS FOUND ON STRINGER 28 LEFT BETWEEN BS 520 AND BS 540. THE CORROSION WAS OUT OF LIMITS AS PER SRM, (MORE THAN 10 PERCENT REMOVED). REPAIRED AS PER COOPESA EO NR C00-3-53-328-98Jun 29, 1998 · N208AU · Boeing 737222 · Fuselage Main, Longeron/StringerSDR P2EA98119Beam · crackedSJO - DURING C-CHECK ROUTINE INSPECTION, A CRACK WAS FOUND ON THE NR 5 BEAM OF THE FORWARD CARGO COMPARTMENT DOOR, FORWARD SECTION LENGTH 1.5 INCH. REPAIRED CRACK AS PER BOEING S/B 737-52-1100. (M)Jun 28, 1998 · N208AU · Boeing 737222 · Cargo/Baggage DoorsSDR 98ZZZX2507Light · inoperativeNR 14 INCH EMERGENCY FLOOR TRACK LIGHT STRIP INOPERATIVE. REPLACED NR 14 INCH FLOOR LAMP ASSEMBLY (FLEX) STRIP IAW B737 MM 33-50. (X)Jun 28, 1998 · N737AP · Boeing 737222 · Emergency LightingSDR P2EA98118Spar · crackedSJO - DURING C-CHECK ROUTINE INSPECTION WHILE PERFORMING WORK CARD NR J2C-10-5726C. A CRACK WAS FOUND ON THE VERTICAL ANGLE ON THE FRONT WING SPAR AT FSS 525. THE LENGTH WAS .187 INCH. ANGLE WAS REPLACED AS PER SRM 51-10-1, PAGE 5. FABRICATED ANGLE IAW SRMJun 21, 1998 · N208AU · Boeing 737222 · Wing SparSDR P2EA98117Bulkhead Beam · crackedSJO - DURING C-CHECK ROUTINE INSPECTION AS PER WORK CARD NR J2C-51-2525, A CRACK WAS NOTED ON THE FORWARD CARGO COMPT, AFT PRESSURE BULKHEAD, VERTICAL BEAM, RBL 15, WL 167.5 (FRONT SPAR, WING CENTER SECTION). REPLACED BEAM AS PER SRM 51-10-1, PAGE 5. (M)Jun 21, 1998 · N208AU · Boeing 737222 · Fuselage Main, BulkheadSDR P2EA98116Stringer · crackedDURING C-CHECK WHILE PERFORMING SPECIAL ITEM J253-10-12L, STR 18A LEFT, SHEAR BEAM WAS FOUND CRACKED. THE CRACK WAS 1.25 INCHES LONG. CRACK REPAIRED IAW SB 737-53-1066 REV 3 DATED 9-24-82. SECTION III PART III. REF: COOPESA W.O. NR L1-0630-2-154. VAM100-2Jun 20, 1998 · N208AU · Boeing 737222 · Fuselage Main, Longeron/StringerSDR VJ9800201Battery · dischargedFWD MEGAPHONE WAS INOP. REPLACED THE MEGAPHONE BATTERIES, OPS CHECKED GOOD.Jun 19, 1998 · N468AT · Boeing 737222 · Emergency EquipmentSDR 98UAL900274Pressurization · malfunctionedAIRCRAFT WOULD NOT PRESSURIZE IN AUTO OR STANDBY.Jun 19, 1998 · N9032U · Boeing 737222 · Cabin Pressure Control SystemSDR CALA9801116Light · looseWHEN GEAR WAS EXTENDED ON APPROACH TO EWR, NEITHER A RED OR GREEN INDICATION WAS RECEIVED FOR RT MLG. THE APPROACH WAS ABORTED, AND WHEN GEAR WAS CYCLED, THE GREEN DOWN AND LOCKED LIGHT ILLUMINATED. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THEJun 18, 1998 · N12235 · Boeing 737222 · Landing Gear Position and Warning
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