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 P2EA99048Beam · crackedSJO - Q-CHECK ITEM. BEAM LOWER CHORD CRACKED AT BS 685, BL ZERO INCH. DEFECT SIZE: LENGTH 2.00 INCHES. REPLACED FUSELAGE LONGITUDINAL BEAM LOWER CHORD BL ZERO INCH BETWEEN BS 645 AND BS 727B PER 51-10-1, PAGE 5 AND SRM 51-30-2, PAGE 1. SEE COOPESA W.O. M1Jan 12, 1999 · N912MP · Boeing 737247 · Fuselage Miscellaneous StructureSDR P2EA99019Skin · crackedSJO - FUSELAGE SKIN CRACKED AT BS 239, WL 222 AND WL 227. DEFECT SIZE 1 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 228 AND BS 255, FROM WL 204 TO WL 229.5 PER SERVICE BULLETIN 737-53-1111, SEC III, PART II, REV 1 DATED APRIL 15, 1993. ALSO, PER BOEING Jan 12, 1999 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA99017Skin · crackedSJO - FORWARD SERVICE DOORWAY UPPER HINGE CUTOUT SKIN CRACKED. DEFECT SIZE, LENGTH .050 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 291 AND BS 286, FROM STRINGER 9 RT TO STRINGER 12 RT PER 53-30-3, FIG 20. (M)Jan 12, 1999 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA99013Skin · crackedSJO - FORWARD SERVICE DOORWAY LOWER HINGE CUTOUT CRACKED. DEFECT SIZE, LENGTH 1 INCH. REPAIRED FORWARD SERVICE DOORWAY LOWER HINGE CUTOUT BETWEEN BS 293 AND BS 286 FROM STRINGER 13 RT TO STRINGER 14 RT PER SRM 53-30-3, FIG 32. (M)Jan 12, 1999 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA99038Skin · crackedSJO - Q-CHECK ITEM. SKIN CRACKED AT FORWARD CARGO DOORWAY AFT LOWER CORNER. DEFECT SIZE: 0.500 INCH. REPAIRED FORWARD CARGO DOOR CUT-OUT SKIN BETWEEN BS 480 AND BS 497 FROM STR 22R TO STR 26R PER COOPESSA B.O. COO-SJO-3-53-008-99 DATED 1-19-99 AND BOEING FJan 11, 1999 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA99065Fairing · wornSJO - NR 1 ENGINE LEADING EDGE WORN. REPAIRED NR 1 ENGINE PYLON LEADING EDGE FAIRING PER COOPESA EO C00-3-54-031-99 DATED 1-23-99, BOEING FAXES COO-SJO-99-0075RR DATED JAN 1-22-99 AND COO-SJO-99-0083RR DATED 1-2-99. (M)Jan 10, 1999 · N912MP · Boeing 737247 · Nacelle/Pylon, Plate/SkinSDR P2EA99057Skin · crackedSJO - Q-CHECK ITEM - LEFT WING LEADING EDGE SKIN CRACKED AT 3 PLACES AT SS 196. DEFECT SIZE: AVERAGE LENGTH: 1.00 INCH. REPAIRED LEFT WING LEADING EDGE SKIN BETWEEN SS 182 AND SS 207.875 PER COOPESA E.O. COO-3-57-022-99 DATED JANUARY 21, 1999, AND BOEING FJan 10, 1999 · N912MP · Boeing 737247 · Wing, Plate/SkinSDR P2EA99064Web · crackedSJO - RIGHT WHEEL WELL SKIN CRACKED AT BS 663, RBL 42, WL 195. DEFECT SIZE, AVERAGE LENGTH 2 INCHES. REPAIRED CENTER WING SECTION SPAR VERTICAL PRESSURE WEB BETWEEN RBL 37 AND RBL 52, BS 663 FROM WL 190 TO WL 202 PER BOEING FAX COO-SJO-990036RR DATED 1-12-99Jan 9, 1999 · N912MP · Boeing 737247 · Wing Miscellaneous StructureSDR P2EA99015Angle · crackedSJO - ANGLE CRACKED AT BS 664, LBL 64, WL 194. DEFECT SIZE, LENGTH 3 INCH. PERFORMED STRINGER 18A SHEAR BEAM TO BS 664 FRAME ATTACHMENT MODIFICATION LEFT SIDE ONLY PER SERVICE BULLETIN 737-53-1056, SEC III, FIG 1 DATED 12-15-78. (M)Jan 9, 1999 · N912MP · Boeing 737247 · Fuselage Miscellaneous StructureSDR P2EA99014Skin · damagedSJO - RIGHT HORIZONTAL STAB STATION 88.5 LOWER SURFACE WITH A PROVISIONAL REPAIR. REPAIRED HORIZONTAL STAB LOWER SKIN SECTION BETWEEN STAB STATION 81.5 AND STAB STATION 95.5 PER 55-10-3 FIG 3. (M)Jan 9, 1999 · N912MP · Boeing 737247 · Horizontal Stabilizer, Plate/SkinSDR P2EA99068Skin · cannedSJO - SKIN OIL CANNED BETWEEN BS 243.7 AND BS 259.5, WL 173 RIGHT SIDE. DEFECT SIZE, LENGTH 17 INCH, WIDTH 12 INCH. REPAIRED FUSELAGE SKIN FROM BS 236 TO BS 270, BETWEEN WL 161 AND WL 181 PER COOPESA EO COO-3-53-033-99 DATED JAN 26, 1999 AND BOEING INSTRUCTIJan 8, 1999 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA99063Angle · crackedSJO - RIGHT WING SPAR VERTICAL ANGLE CRACKED AT FSS 268. DEFECT SIZE, LENGTH .5 INCH. REPLACED FRONT SPAR VERTICAL ANGLE AT FSS 268 PER SRM 51-10-1, PAGE 5 AND SRM 51-30-2, PAGE 5. (M)Jan 8, 1999 · N912MP · Boeing 737247 · Wing Miscellaneous StructureSDR P2EA99039Skin · delaminatedSJO - Q-CHECK ITEM. NR 5 SPOILER DELAMINATED. DEFECT SIZE: LENGTH 4.0 INCHES WIDTH 3.0 INCHES. REPAIRED NR 5 SPOILER PER SRM 57-50-5, FIG 2, SHEET 9. SEE COOPESA W.O. M1-0005-6-21, VAM 100 NR 189 FOR TECHNICAL INFORMATION. (X)Jan 8, 1999 · N912MP · Boeing 737247 · SpoilersSDR DL73E990019Skin · dentedTHE FUSELAGE SKIN AT FS 927 AND STRINGER 21L WAS BADLY DENTED. THE SKIN WAS CUT OUT TO REMOVE THE DENT AND AN UNDERLYING SECTION OF STRINGER AND TEAR STRAP WERE CUT. THE STRINGER WAS REPAIRED PER THE B727 SRM. THE TEAR STRAP WAS REPAIRED WITH AN INTERNAL ALJan 4, 1999 · N378DL · Boeing 737247 · Fuselage Main, Plate/SkinSDR 99ZZZM169Link · crackedRIGHT MAIN LANDING GEAR SWING LINK ASSY FOUND CRACKED DURING MAIN LANDING CHANGE, P/N 65-80737-9. REPLACED LINK ASSY WITH NEW LINK ASSY P/N 65-90737-1391, INSTALLED IAW B737MM 57-13-0 AND DRAWING 65C22640. (M)Dec 30, 1998 · N487GS · Boeing 737247 · Landing Gear Retraction/Extension SystemSDR DL73K982635Tire · failedAFTER TAKEOFF FROM BDL, TOWER NOTIFIED US OF RUBBER DEBRIS ON THE RUNWAY. ON APPROACH TO MCO, AT GEAR EXTENTION HAD A RIGHT MAIN GEAR UNSAFE LIGHT ON AND GREEN LIGHT OFF. FOLLOWED ABNORMAL PROCEDURE. FOUND NR 3 MAIN TIRE LOST CAP AND DAMAGED INBD BRAKE LINEDec 26, 1998 · N239WA · Boeing 737247 · TireSDR DL73K982628Sign · inopEXIT SIGN AT DOOR 2L WILL NOT TEST.Dec 25, 1998 · N239WA · Boeing 737247 · Emergency LightingSDR P2EA99016Skin · dentedSJO - FUSELAGE SKIN DENTED AT BS 462, WL 199. DEFECT SIZE, LENGTH 1 INCH, WIDTH 1 INCH, DIAMETER .050 INCH. REPAIRED FUSELAGE SKIN SECTION BETWEEN BS 458 AND BS 467, FROM STRINGER 17 LEFT TO STRINGER 19 LEFT PER SRM 53-30-3 FIG 7. (M)Dec 7, 1998 · N912MP · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E982414Indicator · malfunctionedON CLIMBOUT, SPLIT FLAP AT 2 DEG. REPLACED FLAP INDICATOR, CKD ALL FLAP TRANSMISSIONS, ALL CK OK. LUBED FLAPS, RAN FLAPS SEVERAL TIMES, CKS OK.Nov 22, 1998 · N374DL · Boeing 737247 · Trailing Flap Position Indicating SystemSDR DL73E982397Valve · wornON INITIAL DESCENT THRU FL31, GOT LOW PRESSURE LIGHT ON A-HYD SYSTEM AND ELEV FEEL LIGHT. SYS-A HYD PRESSURE WAS ZERO AND HYD QTY WAS LOW. FOLLOWED POM PROCEDURES. ON GROUND HYD QTY APPEARED NORMAL. SERVICED HEAD PRESSURE AND CHANGED FILTERS AND CHECKED VANov 19, 1998 · N381DL · Boeing 737247 · Hydraulic System, MainSDR DL73E982388Indication · malfunctionedTRAILING EDGE FLAP STOPPED AT 2 DEG ON RETRACTION DUE TO SPLIT IN INDICATOR BETWEEN LEFT AND RIGHT NEEDLES. EXTENDED USING ALT FLAPS SWITCH AND LANDED AS PER POM. REPLACED FLAP RELAY UNIT AND TRAILING EDGE FLAPS POSITION IND. CLEANED CANNON PLUGS ON LT AND Nov 18, 1998 · N374DL · Boeing 737247 · Trailing Flap Position Indicating SystemSDR P2EA98254Window · crackedMDW - FLT 414 - NO EMERGENCY DECLARED, LANDING UNEVENTFUL. RIGHT FORWARD OUTER PANE CRACKED IN FLIGHT AT APPROX 20,000 FT, 300 KTS. REPLACED R-1 WINDOW PER VANGUARD JOB CARD J256-11-01. REPLACED WINDOW HEAT CONTROLLER PER MM 30-40, PRECAUTIONARY. (M)Nov 12, 1998 · N204AU · Boeing 737247 · Flight Compartment WindowsSDR DL73E982284Line · leakingAFTER TAKEOFF, THE NOSE GEAR INDICATED UNSAFE. BOTH RED AND GREEN LIGHT WITH THE GEAR HANDLE IN UP POSITION. FURTHER INSPECTION REVEALED THE A SYSTEM HYD RAULIC DECREASING RAPIDLY TO ZERO. THE POM C/W AND LANDING MADE. ALL GEAR AND FLAP INDICATION WERE NORNov 6, 1998 · N244WA · Boeing 737247 · Landing Gear Retraction/Extension SystemSDR PE2A98224Seal · wornMDW - FLT 815 - AIR RETURN, NO EMERGENCY DECLARED LANDING UNEVENTFUL. AIRCRAFT ON DEPARTURE FROM MDW WOULD NOT PRESSURIZE IN AUTO, STANDBY, OR MANAUL. DEFERRED PER MEL 21-14-2, CI NR M912306. REF CI M912306. REPLACED LEAKING FLEX LINE AT 450 TEMP SENSOR PENov 1, 1998 · N912MP · Boeing 737247 · Cargo/Baggage DoorsSDR P2EA98224Pressurization · malfunctionedMDW - FLT 815 - AIR RETURN, NO EMERGENCY DECLARED LANDING UNEVENTFUL. AIRCRAFT ON DEPARTURE FROM MDW WOULD NOT PRESSURIZE IN AUTO, STANDBY, OR MANUAL. (M)Nov 1, 1998 · N912MP · Boeing 737247 · Cabin Pressure Control SystemSDR DL73E982133Power Supply · inopON LAYOVER CHECK, FOUND F/C EMERGENCY LIGHTS- TRACK LIGHTING INOP. REPLACED POWER SUPPLY.Oct 13, 1998 · N378DL · Boeing 737247 · Emergency LightingSDR DL73E982039Fan · failedGASPER FAN C/B FOUND OPEN, WHEN CLOSED IT RETRIPPED ACCOMPANIED BY A LOUD POP HEARD UNDER FLOOR IN MID CABIN AND STRONG ELECTRICAL SMELL. INSP GASPER FAN NO PROBLEMS. REPLACED FAN.Oct 3, 1998 · N236WA · Boeing 737247 · Air Distribution FanSDR P2EA98313Wall · dentedMCI - NOSE WHEEL WELL WALL DENTED AT BS 251, DEFECT SIZE 1.5 INCH BY 2 INCH BY .250 INCH. REPAIRED NOSE WHEEL WELL SECTION AT BS 251 PER BOEING TELEX VAG-MCI-98-0086RR DATED SEPT 27, 1998. (M)Sep 27, 1998 · N912MP · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73E981988Frame · crackedA CRACK WAS FOUND DURING ACCOMPLISHMENT OF DAL EO 3-60725-3 AND WAS NOT TYPICAL. THE CRACK WAS IN THE WEB OF THE FRAME. REPAIRED PER ERA 332245-14.Sep 21, 1998 · N237WA · Boeing 737247 · Fuselage Main, FrameSDR W7NA9800003Fuel Manifold · chafedACY - RT FUEL MANIFOLD P/N 581033 FND WITH CHAFE THRU HOLE BETWEEN NR'S 2 AND 3 FUEL NOZZLE. CHAFE CAUSED BY BRACKET P/N 487659 CRACKING AND PARTING NR 2 NOZZLE AND LOGGING ITSELF BTWN MANIFOLD AND CCOC FWD FLANGE. REMOVED AND REPLACED RT FUEL MANIFOLD IAW PSep 17, 1998 · N902WC · Boeing 737247 · Aircraft Fuel Distribution SystemSDR DL73E981860Seat Track · gougedSEVERAL LIGHTENING HOLES IN THE UPPER SHORD OF THE RBL 25 OVERWING SEAT TRACK WERE DAMAGED DURING REPLACEMENT OF THE PART. THE DAMAGED HOLES ARE LOCATED BETWEEN BS 543 TO 769. REPAIRED PER ER/A 332203-14.Sep 5, 1998 · N238WA · Boeing 737247 · Fuselage, Seat/Cargo Attach FittingsSDR DL73E981859Skin · damagedTOOLING DAMAGE WAS INCURRED TO THE FUSELAGE SKIN AT A FASTENER LOCATION UNDER THE FWD CORNER OF THE R1 DOOR CUTOUT. THE SUBJECT FASTENER WAS LOCATED UNDER THE DOOR LOWER THRESHOLD PLATE. REPAIR PER ER/A 332212-14.Sep 5, 1998 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981835Skin · wornTHE FUSELAGE SKIN AND BEAR STRAP WAS FOUND WITH WEAR ON THE C1 DOOR CUTOUT FORWARD EDGE JUST ABOVE STRINGER 22R. THE DAMAGE WAS REPAIRED BY ER/A 332204-14.Sep 2, 1998 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981834Skin · wornDURING INSPECTION OF CARGO DOOR CUTOUT, FUSELAGE SKIN DAMAGE WAS FOUND TO THE C1 DOOR CUTOUT AFT EDGE SKIN BETWEEN STRINGERS 22-23R. THE DAMAGE WAS REPAIRED BY ER/A 332205-14.Sep 2, 1998 · N238WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981814Hinge · failedRT I/B LEADING EDGE FLAP SKIN BENT/CRACKED AT UPPER I/B EDGE DUE TO FAILURE OF I/B HINGE.Sep 2, 1998 · N373DL · Boeing 737247 · Leading Edge DevicesSDR DL73E981791Battery Pack · dischargedMID AISLE EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK.Aug 29, 1998 · N375DL · Boeing 737247 · Emergency LightingSDR DL73E981831Intercostal · crackedTHE R1 DOOR FRAME INTERCOSTAL AT STR 8A WAS FOUND CRACKED. THE REPAIR WAS ACCOMPLISHED PER BOEING S/B 737-53A1108 WITH A MINOR DEVIATION ON THE FINISH.Aug 28, 1998 · N238WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73E981768Skin · gougedTHE UPPER AFT PORTION OF THE C1 DOOR CUTOUT WAS FOUND TO HAVE A GOUGE APPROX 10.5 BY 2.5. REPAIRED PER ERA 332098-14.Aug 26, 1998 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981767Skin · damagedDURING INSP OF THE C1 DOOR CUTOUT PER RTN OPN 8706, AN EXISTING DOUBLER WAS REMOVED TO ACCOMMODATE THE INSPECTION. UPON REMOVING THE DOUBLER, ADDITIONAL SKIN DAMAGE WAS FOUND. REPAIRED PER ERA 332066-14.Aug 26, 1998 · N239WA · Boeing 737247 · Fuselage Main, Plate/SkinSDR DL73E981758Doubler · crackedDURING RTN INSP PER SI3-56673-12 OF THE LH AND RH LONGITUDINAL OVERWING FLOORBEAMS, CRACKS WERE FOUND IN THE WEB DOUBLERS. THE CRACKS ARE LOCATED IN THE DOUBLERS IN THE UPPER AFT CORNER OF THE AILERON CONTROL QUADRANT CUTOUTS AT THE LBL/RBL 24.82 AND APPROX SAug 25, 1998 · N239WA · Boeing 737247 · Fuselage Miscellaneous StructureSDR DL73E981744Bearing · wornRUDDER TRIM AND CENTERING UNIT, (P/N 65-70973-6) FOUND WORN BEARING, (P/N BACB10B257R) ITEM 220, FIG 1, 27-20-4-1. ALSO, FOUND ARM ASSY (P/N 69-51251-6) HAD SEPARATION OF SIDE PLATE ON END WITH BRG (P/N B538DDFS464). REPAIRED SAME.Aug 22, 1998 · N377DL · Boeing 737247 · Rudder Tab Control SystemSDR DL73E981719Battery Pack · dischargedEMERGENCY LIGHT ABOVE 23 DEF INOP. REPLACED BATTERY PACK.Aug 20, 1998 · N243WA · Boeing 737247 · Emergency LightingSDR P2EA98160Warning System · activatedFLT 8189 - MCI - NO EMERGENCY DECLARED LANDING UNEVENTFUL. NOSE GEAR RED LIGHT WAS ILLUMINATED IN FLIGHT. GEAR EXTENSION NORMAL. UNABLE TO BURN FUEL OUT OF CENT TANK WITH LEFT BOOST PUMPS ON. (M)Aug 19, 1998 · N912MP · Boeing 737247 · Landing Gear Position and WarningSDR 98ZZZX3701Check Valve · wrong partMCI - FLT 8189 - NOSE GEAR RED LIGHT WAS ILLUMINATED IN-FLIGHT. GEAR EXTENSION NORMAL. FOUND UPLOCK TARGET MISSING. INSTALLED TARGET AND ADJUSTED SENSOR, PERFORMED GEAR SWING, OPS CHECK NORMAL PER MM 32-61-41. UNABLE TO BURN FUEL OUT OF CENTER TANK WITH LEAug 19, 1998 · N912MP · Boeing 737247 · Fuel Boost PumpSDR P2EA98159Valve · inopFLT 701 - MDW - AIR RETURN, NO EMERGENCY DECLARED. LANDING UNEVENTFUL. AUTO AND STANDBY PRESSURIZATION FAILED IN FIGHT AT 5000FT. ONLY DC MANUAL OPERATIONAL. REPLACED OUTFLOW VALVE. OPS CHECK NORMAL PER MM 21-31-11. (M)Aug 17, 1998 · N204AU · Boeing 737247 · Pressure Regulator/Outflow ValveSDR P2EA98157Wire · brokenFLT 584 - MCI - EMERGENCY DECLARED, LANDING UNEVENTFUL. APU FIRE WARNING BELL AND LIGHT CAME ON IN FLIGHT. APU REPORTED TO BE SHUT DOWN WHEN FIRE WARNING SOUNDED. CREW DISCHARGED APU EXTINGUISHER BOTTLE PERFORMED DETAILED VISUAL INSPECTION OF APU, SHROUD, SAug 16, 1998 · N204AU · Boeing 737247 · Fire DetectionSDR P2EA98158Light · inoperativeMCI - FLT 303 - L-1 DOOR EMERGENCY LIGHT INOP REPLACED BAD SPLICE ON WIRE TO L-1 DOOR LIGHT PER STANDARD PRACTICES. OPS NORMAL CLEARED DEFERRAL M912765. (M)Aug 14, 1998 · N912MP · Boeing 737247 · Emergency LightingSDR DL73E981677Skin · crackedTHE UPPER OUTBD CORNER OF THE L1 COCKPIT WINDOW WAS FOUND WITH A .75 INCH LONG CRACK IN THE SKIN AND UNDERLYING GUSSET ALONG THE C-D WINDOW POST. THE GUSSET CRACK WAS STOP DRILLED AND THE SKIN CRACK TRIMMED OUT. AN EXTERNAL STEEL DOUBLER AND ALUMINUM TRIAug 11, 1998 · N373DL · Boeing 737247 · Fuselage Main, Plate/SkinSDR P2EA98155Brake · damagedMCI - FLT 815 - THE FOLLOWING WAS NOTED DURING POST FLIGHT WALKAROUND, NR 2 BRAKE LINE QUICK DISCONNECT, METERING VALVE, IS BROKEN OFF OF THE BRAKE ASSY. MAINTENANCE ENTRY REPLACED LEFT MLG DUE TO DAMAGE AT NR 2 BRAKE. REPLACED BRAKE LINE AND QUICK DISCONNECAug 8, 1998 · N912MP · Boeing 737247 · BrakeSDR DL73E981649Skin · dentedTHE FUSELAGE SKIN AT FS 380 WAS DAMAGED BY GROUND EQUIPMENT BETWEEN STRINGERS 17L AND 18L. THE DAMAGED AREA WAS CUTOUT AND AN EXTERNAL ALUMINUM REPAIR DOUBLER WAS INSTALLED PER ER/A 365386-14.Aug 7, 1998 · N374DL · Boeing 737247 · Fuselage Main, Plate/Skin
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