Boeing 737-247

Service difficulty reports · 1,009

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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 = '737247'
  ORDER BY difficulty_date DESC"

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SDR P2EA98147Fitting · crackedSJO - C-CHECK ITEM - OUTBOARD SUPPORT FITTING RT WING SPOILER NR 5 CRACKED. DEFECT SIZE L = 2.5 INCHES. REPLACED NR 5 GROUND SPOILER OUTBOARD HINGE PER SRM 51-10-1 PAGE 5. FABRICATED FITTING PER COOPESA E.O. COO3-57-377-98 DATED DOCUMENTED ON FAA FORM 8110-Aug 2, 1998 · N204AU · Boeing 737247 · Wing, Control Surface Attach FittingsSDR P2EA98132Frame · crackedC-CHECK ITEM. FUSELAGE FRAME CRACKED AT BS 420 BETWEEN STR 20R AND STR 21R. REPAIRED FUSELAGE FRAME SECTION AT BS 420 BETWEEN STR 19R AND 21R PER SRM 53-40-3 FIG 1. SEE COOPESA W.O. L1-0616-1-86, VAM 100 NR 486. (X)Jul 29, 1998 · N204AU · Boeing 737247 · Fuselage Main, FrameSDR P2EA98128Frame · crackedSJO - FORWARD CARGO DOOR BEAM NR 5 CRACKED IN AFT SECTION DEFECT SIZE L=1.375 INCH. REPAIRED FORWARD CARGO DOOR BEAM NR 5 PER BOEING SERVICE BULLETIN 737-52-1100 REV 2 DATED MARCH 31, 1994, SECTION 111, PAR 'C' FIG 6, DETAIL II. (M)Jul 24, 1998 · N204AU · Boeing 737247 · Cargo/Baggage DoorsSDR DL73E981539Battery Pack · dischargedOVERHEAD EMERGENCY LIGHT SIGN INOP IN MID CABIN OVERWING EXITS. REPLACED BATT PACK PER M/M.Jul 23, 1998 · N378DL · Boeing 737247 · Emergency LightingSDR P2EA98142Skin · damagedSJO - C-CHECK ITEM. REF: VAM 54 NR 050, REPLACED TIME LIMITED SKIN REPAIR AT BS 294, STR 23R. INSTALLED PERMANENT REPAIR AT BS 281 THROUGH BS 298 BETWEEN STR 21R AND STR 24R PER SRM 53-30-3 FIG 1. SEE COOPESA W.O. L1-0616-9-9, VAM 54 NR 50. (X)Jul 21, 1998 · N204AU · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981503Compressor · bird strikeAFTER TAKEOFF, BIRDSTRIKES FOLLOWED BY COMPRESSOR STALLS ON THE NUMBER 1 ENGINE. CHANGED FAN.Jul 19, 1998 · N245WA · Boeing 737247 · Turbine Engine Compressor SectionSDR DL73E981510Skin · damagedFUSELAGE SKIN C1 DOOR SURROUND, LOWER AFT CORNER. REPAIR FOR SKIN GOUGE. THE LOWER AFT CORNER OF THE C1 DOOR CUTOUT WAS DAMAGED BY GROUND EQUIPMENT. THE SKIN ASSY AND UNDERLYING BEAR STRAP WAS DENTED AND TORN. THE DAMAGE WAS TRIMMED AWAY AND HFEC INSPECTJul 17, 1998 · N377DL · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98138Stringer · crackedSJO - C-CHECK ITEM - FUSELAGE STRINGER 10L CRACKED AT BS 529.5. DEFECT SIZE L - 0.095 INCH. REPAIRED STRINGER 10L BETWEEN BS 278 AND BS 302 PER SRM 53-10-3 FIG 3 SHEET 4. SEE COOPESA W.O. L1-0616-2-204, VAM 100 NR 555. (X)Jul 14, 1998 · N204AU · Boeing 737247 · Fuselage Main, Longeron/StringerSDR P2EA98136Bulkhead · crackedSJO - FUSELAGE BULKHEAD WEB CRACKED AT BS 294.5, LBL 16 INCHES, WL 165 (E/E COMPT). REPAIRED WEB AT BS 294.5, LBL 13 TO LBL 18, BETWEEN WL 170 AND WL 160 PER BOEING FAX COO-SJO-98-0491RR DATED JULY 21, 1998. DOCUMENTED ON FAA FORM 8110-3. (M)Jul 14, 1998 · N204AU · Boeing 737247 · Fuselage Main, BulkheadSDR P2EA98137Skin · dentedSJO - FUSELAGE SKIN DENTED AT BS 380 BETWEEN STRINGER 17 LT AND STRINGER 18 LT. DEFECT SIZE LENGTH 4 INCHES WIDTH 2 INCHES. REPAIRED FUSELAGE SKIN SECTION BS 376 AND BS 387, BETWEEN STRINGER 17 LT AND 19 LT PER SRM 53-30-3 FIG 17 DETAIL V. (M)Jul 13, 1998 · N204AU · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98131Frame · crackedC-CHECK ITEM. FUSELAGE FRAME CRACKED AT BS 360, STR 20R. REPAIRED FUSELAGE FRAME SECTION AT BS 360 BETWEEN STR 19R AND 21R PER SRM 51-40-3 FIG 1. SEE COOPESA W.O. L1-0616-1-89, VAM 100 NR 499. (X)Jul 13, 1998 · N204AU · Boeing 737247 · Fuselage Main, FrameSDR P2EA98141Stiffener · crackedSJO - C-CHECK ITEM - RIGHT WING L/E CAVITY WBL 321. FSS 395, STIFFENER CRACKED. DEFECT SIZE L=0.950 INCH. REPLACED CRACKED ANGLE AT FRONT SPAR, BS 395 PER SRM 51-10-1 PAGE 5, AND SRM 51-30-2. SEE COOPESA W.O. L1-0616-6-40, VAM 100 NR 289. (X)Jul 12, 1998 · N204AU · Boeing 737247 · Wing Miscellaneous StructureSDR P2EA98139Skin · crackedSJO - C-CHECK ITEM. FUSELAGE SKIN CRACKED AT AFT ENTRY DOOR (L2) CUT OUT BETWEEN BS 977 AND BS 998, STR 15L THROUGH STR 18L. REPAIRED SKIN SECTION BETWEEN BS 977 AND BS 998, STR 15L THROUGH STR 18L PER BOEING FAX COO-SJO-98-0494RR. DOCUMENTED ON FAA FORM 81Jul 12, 1998 · N204AU · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98130Skin · crrackedC-CHECK ITEM. R2 DOOR CUT-OUT LOWER FORWARD OUTER FUSELAGE SKIN CRACKED. DEFECT SIZE - 2.000 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 943 AND BS 975, STR 16R AND STR 19R PER SRM 53-30-3 FIG 24. SEE COOPESA W.O. L1-0616-2-171, VAM 100 NR 448. (X)Jul 12, 1998 · N204AU · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98146Pressure Web · crackedSJO - C-CHECK ITEM - NOSE LANDING GEAR WHEEL WELL CRACKED AT BS 278, WL 200, RBL 7. DEFECT SIZE L- 2.5 INCHES. REPAIRED NOSE WHEEL WELL UPPER WEB SECTION AT BS 274 THROUGH BS 281, RBL 6 INCHES AND RBL 14 INCHES PER COOPSEA E.O. COO3-53-36998 DATED JULY 21, 1Jul 11, 1998 · N204AU · Boeing 737247 · Fuselage Miscellaneous StructureSDR P2EA98140Doubler · damagedSJO - C-CHECK ITEM. FUSELAGE SKIN REPAIR DOUBLER MISSING MATERIAL AT BS 178. ACCOMPLISHED PREVENTATIVE MODIFICATION ON FUSELAGE CONTROL CABIN SKIN AT WINDSHIELD CENTER POST PER SB 737-53-1059 SECT 3, FIG 2, DATED ON 11-17-80, REV 1 DATED 5-17-90. SEE COOPESJul 11, 1998 · N204AU · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98135Skin · damagedSJO - MAIN ENTRY DOOR (L1) OUTER SKIN BETWEEN BEAM 4 AND BEAM 5 OIL CANNED. REPAIRED MAIN ENTRY DOOR SKIN SECTION BETWEEN BEAM 4 AND BEAM 5 PER SRM 52-00-3 FIG 6 SHEET 1 OF 2. (M)Jul 11, 1998 · N204AU · Boeing 737247 · Passenger/Crew DoorsSDR P2EA98134Splice · corrodedSJO - FUSELAGE FRAME SPLICE SECTION CORRODED BEYOND LIMITS AT BS 1016, BETWEEN STRINGER 25RT AND STRINGER 25LT. REPAIRED FUSELAGE FRAME SPLICE SECTION AT BS 1016, BETWEEN STRINGER 25 RT AND 25 LT PER SRM 51-10-5, PAGE 5 AND SRM 51-30-2. (M)Jul 11, 1998 · N204AU · Boeing 737247 · Fuselage Miscellaneous StructureSDR P2EA98129Slat · dentedSJO - LEFT WING NR 1 SLAT LEADING EDGE DENTED AT SS 373. REPAIRED NR 1 SLAT SKIN SECTION BETWEEN SS 373 AND SS 382 PER SRM 57-50-3 FIG 1. (M)Jul 11, 1998 · N204AU · Boeing 737247 · Leading Edge DevicesSDR P2EA98133Bulkhead · crackedC-CHECK ITEM. BS 727 BULKHEAD SKIN CRACKED RBL 32, WL 200.5. DEFECT SIZE - 1.375 INCH. REPAIRED FUSELAGE BULKHEAD WEB AT BS 727, WL 194.25 AND WL 202 BETWEEN RBL 26.5 AND RBL 39.25 PER BOEING FAX COO-SJO-98-0486RR DATED 7-16-98. DOCUMENTED ON FAA FORM 8110Jul 10, 1998 · N204AU · Boeing 737247 · Fuselage Main, BulkheadSDR DL73E981375Line · chaffedA/C RETURN ATL, DUE TO RT HYD PUMP LOW PRESS LIGHT AND HYD QTY ZERO ON CLIMB-OUT. FOUND HYD RTN LINE CHAFFED. REPLACED LINE AND FILTER AND EDP PER M/M. LEAK CK GOOD AND SYS OPS NML PER M/M.Jun 30, 1998 · N236WA · Boeing 737247 · Hydraulic System, MainSDR DL73E981369Bulb · failedLT WING EMERGENCY LIGHT INOP. REPLAMPED.Jun 30, 1998 · N375DL · Boeing 737247 · Emergency LightingSDR DL73E981310Circuit Breaker · trippedAFTER T/O, LND GEAR HANDLE WOULD NOT COME UP. C/W POM, PULLED RED LOCK OVERRIDE TRIGGER, RAISED GEAR, CONTINUED NML. AT GATE, MECH FOUND LVR LATCH C/B POPPED. TESTED LEV LATCH LOCK SOLENOID PER MM 32-31-31 PG 402 SEVERAL TIMES OPN TEST NML. C/B CKS NML. LJun 21, 1998 · N245WA · Boeing 737247 · Landing Gear Retraction/Extension SystemSDR DL73E981270Duct · crackedWITH APU BLEED OPEN POWERING RIGHT PACK LEFT WING BODY OVERHEAT LIGHT ILLUMINATED APU BLEED PLACED OFF AFTER DELAY LIGHT WENT OUT LATER F/A NOTICED BURNING SMELL IN MID CABIN AREA. FOUND APU BLEED LINE CRACKED JUST AFT OF APU BLEED VALVE. REPLACED BLEED DUCTJun 16, 1998 · N236WA · Boeing 737247 · Pneumatic Distribution SystemSDR DL73E981192Battery · dischargedDURING SVC CK, NR 3 FOUND F/C EMER FLASH LIGHT RED LED DOES NOT FLASH. REPLACED BATT PER M/M LIGHT NOW OPS TEST OK PER M/M.Jun 4, 1998 · N374DL · Boeing 737247 · Emergency LightingSDR DL73E981167Battery Pack · dischargedL2 DOOR EXTERIOR EMER LIGHT INOP AND 3 AFT LEFT CABIN LIGHTS INOP. REPLACED BATTERY PACK.Jun 1, 1998 · N244WA · Boeing 737247 · Emergency LightingSDR DL73E981052Floorbeam · crackedWING/CENTER WING BOX/FLOORBEAM, STA 665, BL 0.07, REPAIR FOR UPPER CAP AND WEB CRACKS. CRACKS WERE FOUND IN THE WING CENTER SECTION BL 0.07 FLOORBEAM AT STA 665. THE UPPER CAP OF THE BEAM WAS COMPLETELY SEVERED AND THE WEB AND WEB DOUBLER WERE FOUND WITH A 4May 13, 1998 · N378DL · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73E981013Floorbeam · crackedTHE UPPER CAP OF THE BL 0.07 CENTER WING BOX FLOORBEAM WAS FOUND SEVERED AT STA 665. THE WEB AND WEB DOULBER WERE ALSO FOUND CRACKED AT THIS LOCATION. THE BEAM WAS REPAIRED PER BAC S/B 737-57-1210 AND DOCUMENTED PER ER/A 364760-14, REV A.May 12, 1998 · N378DL · Boeing 737247 · Fuselage Main, Floor BeamSDR DL73E980999Skin · crackedTHE UPPER OUTBD CORNER OF THE COCKPIT L1 WINDOW SURROUND SKIN WAS FOUND WITH A TYPICAL CRACK. WHILE STOP DRILLING THE CRACK PER SRM, THE DRILL HOLE WAS MISTAKENLY DRILLED THROUGH THE WINDOW POST. THE DRILL HOLE WAS ROUTED OUT OF THE POST AND POST STRAP. AN May 6, 1998 · N244WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E980933Skin · crackedTHE R2 DOOR OPENING SURROUND SKIN WAS FOUND WITH A .75 INCH LONG CRACK AT THE CUTOUT FOR THE LOWER HINGE. THE SKIN AND BONDED DOUBLERS WERE CUTOUT TO REMOVE THE CRACK. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER AND TRIPLER PER ER/A 36464Apr 28, 1998 · N236WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98081Door · damagedFLT 106 - MSP - FORWARD ENTRANCE DOOR WAS DAMAGED BY THE JETWAY AT GATE 36 AT MSP. EVALUATED DAMAGE, DETERMINED TO BE DAMAGE TO DOOR LINER ONLY, TRANSFERRED TO C1 NR P204009 DOOR OK FOR SERVICE. (M)Apr 20, 1998 · N204AU · Boeing 737247 · Passenger/Crew DoorsSDR P2EA98080Connector · looseFLT 712 - MCI - REJECTED TAKEOFF AT 85 KTS, ZERO AIRSPEED INDICATION ON F/O'S SIDE. FOUND PITOT CONNECTION ON F/O AIRSPEED INDICATOR LOOSE, RESECURED AND LEAK CHECKED PER MM 34-12-0. (M)Apr 19, 1998 · N204AU · Boeing 737247 · Airspeed/Mach IndicatorSDR DL73E980842Spindle · brokenWITH A/C FULLY CONFIGURED FOR LANDING, 30 DEGREES FLAPS, GEAR DOWN, THE AILERONS REQUIRED 12 DEGREES LEFT TRIM FOR LEVEL FLIGHT. NO CROSSWIND. EACH PROGRESSIVE FLAP SETTING REQUIRED MORE AILERON INPUT. FOUND RT O/B FLAP CARRIAGE SPINDLE BROKEN, REPLACED.Apr 18, 1998 · N238WA · Boeing 737247 · Trailing Edge FlapsSDR DL73E980648Generator · trippedON CLIMB-OUT OF 23,000 FEET, CTR FUEL PUMPS WERE TURNED ON AND WE LOST THE NR 1 GEN IN ABOUT 2-3 SECONDS, THE NR 1 BUS OFF AND GEN OFF BUS LIGHTS ILLUM FOLLOWING POM PROCEDURES WE WERE UNABLE TO POWER NR 1 BUS BY LT GEN OR APU. GEN NR 1 VOLTS AND FREQS PEGGEDMar 24, 1998 · N239WA · Boeing 737247 · AC Generator-AlternatorSDR 98ZZZM403Pin · bentRIGHT EXTERIOR EMERGENCY EXIT LIGHT INOP. FOUND ON AMPLIFIED PREFLIGHT. STRAIGHTENED PINS ON RT BATTERY PACK CHARGER. (M)Feb 22, 1998 · N487GS · Boeing 737247 · Emergency LightingSDR 98ZZZM402Lamp · failedRIGHT EXTERIOR EMERGENCY EXIT LIGHTS INOP. FOUND ON AMPLIFIED PREFLIGHT. RELAMPED EMERGENCY LIGHT IAW BOEING MM 33-51-22. (M)Feb 22, 1998 · N487GS · Boeing 737247 · Emergency LightingSDR DL73E980260Bulkhead Web · crackedSTA 178 BULKHEAD WEB WAS FOUND WITH CRACKS IN THE TYP LOCATIONS AT LBL 5.7 AND RBL 5.7. THE CRACKS WERE TRIMMED OUT WITH 1 X 4 CUTOUTS. THE DAMAGED AREAS WERE REPAIRED WITH SINGLE ALUMINUM REPAIR DOUBLER PER ER/A 363850-12, REV A.Jan 28, 1998 · N243WA · Boeing 737247 · Fuselage Main, BulkheadSDR DL73E980256Gearbox · failedAT 2000 FT MSL AND 190 KTS NR 2 ENGINE HAD A COMPRESSOR STALL AND ENGINE POWER WAS REDUCED TO IDLE. ENGINE WAS SHUTDOWN WHEN F/A NOTICED METAL STICKING OUT OF INLET. MTC FOUND NOSE BULLET HAD BROKE OFF AND LODGED ITSELF IN THE INLET GUIDE. REPLACED GEARBOX Jan 28, 1998 · N381DL · Boeing 737247 · Turbine Engine Accessory DriveSDR DL73E980226Seal · tornCLIMBING THROUGH FL242 CABIN ALT WARN HORN. CABIN ALT OBSERV CLIMB THROUGH 10000 AND AIRCRAFT LEVELED. DESCENT BEGAN AND CABIN ALT CLIMBED TO 13500, NO HELP IN STBY OR MAN, PRESS MODE OUTFLW VLV FULLY CLOSED AND FWD VALVE CLOSED LIGHT ON ENTIRE TIME. CHECKEJan 26, 1998 · N239WA · Boeing 737247 · Cargo/Baggage DoorsSDR P2EA98002Pt7 Line · brokenATL - FLT 119 - NO EMERGENCY DECLARED. TAKEOFF ABORTED, ROLL OUT AND RETURN TO GATE NORMAL. ON TAKEOFF, THE RIGHT ENGINE EPR FAILED TO GO ABOVE APPROX 1.6 EPR. BOTH ENGINE INDICATIONS WERE N1 - 98 PERCENT, N2 - 100 PERCENT EGT AT 500 DEGREES, TAKEOFF ABORTEJan 2, 1998 · N912MP · Boeing 737247 · Engine Pressure Ratio (EPR)SDR CALA9701754Actuator · leakingTHE SYSTEM B HYDRAULIC LOW QUANTITY LIGHT ILLUMINATED WITH GAUGE READING 1 GALLON WHILE ON APPROACH TO EWR. THE AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND THE NR 2 FLIGHT SPOILER ACTUATOR LEAKING. THE NR 2 FLIGHT SPOILER ACTUATOR WAS REMOVED AND REDec 14, 1997 · N14246 · Boeing 737247 · Drag Control ActuatorSDR DL73E972554Transformer · intermittentDURING CLIMB, NR 1 GEN BUSS TRIPPED AND WOULD NOT RESET/APU WOULD NOT PICK UP BUSS EITHER. REPLACED NUMBER 1 ENG CURRENT TRANSFORMER, CHECKS GOOD.Dec 5, 1997 · N243WA · Boeing 737247 · AC Generation SystemSDR DL73E972553Relay · stuckDURING CLIMBOUT, LT GEN BUSS TRIPPED OFF AND APU WOULD NOT PWR THE BUSS. REPLACED NR 1 GEN CONTROL RELAY. INSP ENG GEN LEADS AND DIFFERENTIAL LOOPS. ALL OK, RAN ENG AT T/O PWR.Dec 5, 1997 · N243WA · Boeing 737247 · AC Generation SystemSDR DL73E972552Gen Contl Pnl · failedDURING CLIMBOUT, LEFT GEN BUSS TRIPPED (NO VOLTS OR FREQS) AND APU WOULD NOT PWR THE BUSS. REPLACED LEFT GEN CONT PANEL, OPERATION OF GEN AND XFR SYS OP CKS GOOD.Dec 5, 1997 · N243WA · Boeing 737247 · AC Generation SystemSDR DL73E972501Battery Pack · dischargedFLT DECK EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK.Nov 30, 1997 · N381DL · Boeing 737247 · Emergency LightingSDR DL73E972422Oil Press Sw · failedCLIMBING THRU 13,000 FT, APU SHUT DOWN WITH LOW OIL PRESSURE LIGHT, (RT GENERATOR ALREADY ON MCO.) REPLACED LOW OIL PRESSURE SW AND LOW SEQ SW APU, CKS NORMAL.Nov 20, 1997 · N379DL · Boeing 737247 · APU Indicating SystemSDR DL73E971863Floorbeam · crackedTHE FS 246 FLOORBEAM WEB WAS FOUND WITH A CRACK APPROXIMATELY 3.75 LONG AT RBL 20. THE RESULTING CUTOUT IS 1.0 BY 3.75. THE SUBJECT WEB IS MANUFACTURED FROM .025 CLAD 7075-T6. THE STIFFENER AT RBL 20 WAS CRACKED AS WELL. THE STIFFENER (P/N 141T5814-88) IS Sep 15, 1997 · N237WA · Boeing 737247 · Fuselage Main, Floor BeamSDR CALA9701225Starter · inoperativeWHILE OPERATING THE APU WITH THE NR 2 GENERATOR PLACARDED INOPERATIVE, THE APU SHUTDOWN CLIMBING THROUGH 3,000 FEET. RESTART ATTEMPT WAS UNSUCCESSFUL. THE AIRCRAFT WAS DIVERTED TO IAH WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE TROUBLESHOT TO A FAILED STAAug 16, 1997 · N14246 · Boeing 737247 · APU Start/Ignition SystemSDR DL73E971675Skin · corrosionA BULGE WAS FOUND IN THE FUSELAGE SKIN AT STA 927 BETWEEN STR 14R AND 15R. MX REMOVED THE AFFECTED AREA OF THE CHEM-MILLED LOWER SKIN (65-45778-82), JUST BELOW THE STR 14R LAP JOINT. THE CUTOUT MEASURED 2.5 BY 8. A TIME LIMITED REPAIR USING BLIND FASTENERS Aug 9, 1997 · N236WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E971538Reading Light · failedPAX REPORTED A BURNING SMELL IN FWD COACH CLASS AT APPROX ROW 12. FOUND READING LIGHT SW AT SEAT 13A DEFECTIVE AND ARCING. DISCONNECTED SW AT OVERHEAD LIGHT ASSY FWD TO MCO AND PLA PER MEL 25-00-10.Aug 6, 1997 · N374DL · Boeing 737247 · Passenger Compartment Lighting
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