Boeing 737-297

Service difficulty reports · 454

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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 = '737297'
  ORDER BY difficulty_date DESC"

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SDR KNNA147071110KACYHydraulic Line · leakingTHE "A" SYSTEM QUANTITY AND PRESSURE DROPPED TO ZERO ON DESCENT TO KACY (ATLANTIC CITY IAP, NJ). COMPLETED CHECKLIST 6.77 OF THE AFM.Jul 11, 2010 · N147AW · Boeing 737297 · Hydraulic System, MainSDR KNNA20090001Seal · failedNR 1 ENGINE OIL QUANTITY DROPPED TO ZERO DURING FLIGHT FOLLOWED BY DROP IN OIL PRESSURE LEADING TO ENGINE SHUT DOWN AND DECLARATION OF AN EMERGENCY. IT WAS DISCOVERED DURING TROUBLE SHOOTING THAT BOTH THE STARTER SEAL AND THE FUEL PUMP SEALS WERE LEAKING. BApr 3, 2009 · N147AW · Boeing 737297 · Turbine Engine Oil SystemSDR PIDR07001Skin · crackedCRACK IN THE FUSELAGE SKIN AT BS 727B+4 AT STR 17 RT WAS REPAIRED BY REPLACING THE DAMAGED SECTION OF SKIN FROM BS 727 TO BS 757 FROM STR 14 RT TO STR 20 RT DUE PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROAug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Plate/SkinSDR PIDR07002Skin · crackedCRACK IN FUSELAGE SKIN AT BS 727A+14.5 AT STR 17 LT WAS REPAIRED BY REPLACING SECTION OF SKIN FROM BS 727A +8 TO BS 767 FROM STR 16 LT TO STR 18 LT DUE TO PROXIMITY OF ADJACENT REPAIRS. REPAIR WAS ACCOMPLISHED IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDUREAug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Plate/SkinSDR PIDR07003Stringer · damagedSTRINGER 16 RT AT BS 727B HAS A DAMAGED FASTENER HOLE. REPAIRED IN ACCORDANCE WITH SRM 53-10-3 FIGURE 2.Aug 24, 2007 · N147AW · Boeing 737297 · Fuselage Main, Longeron/StringerSDR KNNA200700011Frame · misdrilledFOUND MISDRILLED HOLE AT SKIN OF SIDE FRAME, WL 212 LT, STA 179. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF MISDRILLED FASTENER HOLE BS 178 W/L 212.Feb 5, 2007 · N147AW · Boeing 737297 · Fuselage Main, FrameSDR KNNA200700018Frame · crackedFOUND STA 178, LT SIDE FRAME IS CRACKED AT W/L 195. PROVIDE INSTRUCTION ON REPAIR CRACK BY INSTALLING A SPLICE OVER THE (LEFT SIDE) SIDE CHORD AT WL 212.Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, FrameSDR KNNA200700017Vertical Beam · crackedFOUND LBL 5.7 VERTICAL BEAM IS CRACKED BOTH FLANGES AT STA 178 BULKHEAD. PROVIDE INSTRUCTIONS ON REPAIR OF LBL 5.7 VERTICAL CHORD AT STA 178.Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, BulkheadSDR KNNA200700015Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT WL-234, LBL-8 TO LBL-9. PROVIDE INSTRUCTION ON REPAIR OF BULKHEAD AT STA 178 LBL 8 - LBL 9 AND LBL-10-LBL 12.Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, BulkheadSDR KNNA200700014Frame · crackedFOUND STA 178 RT SIDE FRAME IS CRACKED AT WL 207. PROVIDE INSTRUCTION TO REPAIR CRACK BY INSTALLING A SPLICE OVER THE (RIGHT SIDE) SIDE CHORD AT WL 212.Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, FrameSDR KNNA200700012Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT STA 178 W/L 213.5, RBL1, W/L 224, LBL-1-RBL1, W/L 227, RBL 1. PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 W/L 213.5, RBL 1,Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, BulkheadSDR KNNA200700010Bulkhead · crackedFOUND STA 178 BULKHEAD IS CRACKED AT W/L 234,RBL 9-RBL 10. FOUND PROVIDE INSTRUCTIONS ON REPAIR OF BULKHEAD AT STA 178 RBL 9-RBL 10 .Jan 25, 2007 · N147AW · Boeing 737297 · Fuselage Main, BulkheadSDR KNNA200700013Skin · damagedE/E BAY ACCESS DOOR EXTERIOR SURFACE, RT EDGE BEND. PROVIDE INSTRUCTIONS ON REPAIR OF E/E BAY DOOR .Jan 19, 2007 · N147AW · Boeing 737297 · Electrical/Electronic Compartment DoorsSDR KNNA200700016Stringer Splice · activeFOUND CRACKED CHORD OF STRINGER 14L AT BS 663.75. PROVIDE INSTRUCTION ON REPAIR OF S14L AT BS 663.75.Jan 12, 2007 · N147AW · Boeing 737297 · Fuselage Main, Longeron/StringerSDR KNNA200300001Skin · crackedAIRCRAFT AT MAINT. BASE FOR "A3" CHECK COMPLIANCE. IN C/W TASK CARD A-07A A 1.8 INCH CRACK WAS FOUND IN EXTERIOR FUSELAGE SKIN AT LT BS 757 BELOW STR 17. A NON-ROUTINE T030446 AND ACO 035313R00 WAS ISSUED TO DOCUMENT SRM REPAIR CH 53-30-3 FIG 25. CRACK IN SKFeb 24, 2003 · N147AW · Boeing 737297 · Fuselage Main, Plate/SkinSDR CA020528005Duct · ruptured(CAN) SHORTLY AFTER TAKEOFF CREW OBSERVED NR 1 ENGINE OVERHEAT - WHEN POWERLEVER RETARDED, IND. EXTINGUISHED. WHEN POWERLEVER FOR NR 1 ENGINE ADVANCED, OVERHEAT WARNING ILLUMINATED. CREW DECLARED EMERGENCY AND AIRCRAFT LANDED WITHOUT INCIDENT. CFR ON STANDBY.May 16, 2002 · Boeing 737297 · Engine Bleed Air SystemSDR CA020502004Fitting · missing(CAN) ENROUTE PILOT NOTICED THE OIL QUANTITY WAS AT ZERO ON THE NR 1 ENGINE - BOTH OIL PRESSURE AND OIL TEMPERATURE WERE NORMAL. SHORTLY THERE AFTER THE OIL PRESSURE STARTED TO FLUCTUATE AND THE OIL PRESSURE WARNING LIGHT ILLUMINATED.FLIGHT CREW SHUTDOWN NR 1 Apr 27, 2002 · Boeing 737297 · Accessory GearboxesSDR CA020408017Wheel · cracked(CAN) FLIGHT CREW REPORTED ON TAXI THE AIRCRAFT SEEMED TO REQUIRE MORE POWER THAN NORMAL - AIRCRAFT DEPARTED WITHOUT INCIDENT.ON NEXT LANDING THE CREW NOTICED THE SAME AND REPORTED TO YLW MAINTENANCE. INSPECTION FOUND THE MAIN BRAKE ON NR 2 MAIN WHEEL ASSEMBLYApr 5, 2002 · Boeing 737297 · Wheel/Ski/FloatSDR CA020305003Wire · chafed(CAN) DURING FLT A/C EXPERIENCED FLICKERING LT WING BODY OVERHEAT INDICATION WITH INCREASING FREQ. OVERHEAT LIGHT ILLUMINATED OFF & FLICKERED ON & OFF CONTINUOUSLY WHEN LT ENGINE BLEED VALVE & ISOLATION VALVE WERE CLOSED (WITH APU OFF). FLT CREW CONTACTED MCFeb 22, 2002 · Boeing 737297 · Fire Protection System WiringSDR P2EA2002M001Actuator · crackedAfter Landing Lost A System Hydraulics upon exiting taxi way at MCI.Inspected and found the #1 Ground Spoiler actuator with crack. R&R #1 Ground Spoiler actuator IAW Boeing MM 27-62-101 op's check and leak checks good.Jan 10, 2002 · Boeing 737297 · Hydraulic System, MainSDR CA011120004Control Unit · leaking(CAN) RETURNED TO YHM DUE TO LOSS OF 'A' SYS HYDRAULIC FLUID. SHORTLY AFTER TAKEOFF OUT OF YHM CREW NOTICED HYD MASTER CAUTION LIGHT HAD ILLUMIINATED, THE 'A' SYS HYDRAULIC FLUID HAD DEPLETED & THE HYDRAULIC LOW PRESSURE WARNING LIGHTS HAD ILLUMINATED. CREW Nov 16, 2001 · Boeing 737297 · Hydraulic System, MainSDR P2EA2001M0005CouplerMach Trim "fail" light illumimnates intermitently. Corrective action: Defferred Mach Trim system per MEL 22-5, CI#M005089 per MX CNTL Mic. Removed and replaces Mach Trim Coupler IAW MM 22-21-31, operational check normal. This clears MEL CI#M005089. See 005 LogSep 24, 2001 · Boeing 737297 · Speed-Attitude Correction SystemSDR P2EA01193Computer · faultyFLT 451 - MCI - WITH AUTOPILOT IN HGD HOLD AIRCRAFT ROLLS TO APPROXIMATELY WINGS LEVEL FROM AND BANK ANGLE AND TURNS AT ABOUT 1 DEGREE PER MINUTE TO THE LEFT. ALL OTHER AUTO PILOTS FUNCTIONS ARE NORMAL. REMOVED AND REPLACED ROLL COMPUTER AND OPERATIONAL CHECSep 16, 2001 · N120NJ · Boeing 737297 · Autopilot ComputerSDR P2EA01089Hydraulic Line · inoperativeFLT 408 - MCI - WHILE ON APPROACH INTO MCI, AIRCRAFT A SYSTEM HYDRAULIC FAILED. DECLARED AN EMERGENCY. INSPECTED HYDRAULIC SYSTEM A AND FOUND LEAK IN FORWARD LEFT MAIN WHEEL WELL. REMOVED AND REPLACED HYDRAULIC LINE LEAK CHECKED GOOD PER BOEING MM 29-00 PARJun 7, 2001 · N5WM · Boeing 737297 · Hydraulic Power SystemSDR CA010504024Tube · worn(CAN) CREW REPORTED NR 1 ENGINE EPR INDICATION FLUCTUATING TO .20 EPR LOWER THAN NR 1 ENGINE. N1, N2 AND FUEL FLOWS WERE STEADY. INSPECTION FOUND A CHAFED WIRE AT THE R/H ANTI-ICE VALVE HAD ARCHED AND WORN A HOLE THRU THE SIDE OF THE LINE FROM THE PT 7 PROBE. Apr 13, 2001 · Boeing 737297 · Engine Pressure Ratio (EPR)SDR P2EA01025Skin · puncturedFLT 350 - MDW - PUNCTURE THROUGH SKIN AT BS 933 WL 203 BETWEEN STRINGER 20L AND 21L. (M)Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/SkinSDR P2EA01028Skin · puncturedMDW - FLT 350 - PUNCTURE THROUGH SKIN AT BS 933, WL 203 BETWEEN STRINGER 20L AND 21L. REPAIRED IAW SRM 53-30-3. (M)Apr 8, 2001 · N5WM · Boeing 737297 · Fuselage Main, Plate/SkinSDR TSAA0133015Battery Pack · dischargedREPLACED BATTERY FOR THE NR 3 AND NR 4 POSITION FOR THE EMERGENCY FLOOR PROX LIGHT. OPS CHECK OK. AIRCRAFT RETURNED SERVICE. (M)Feb 16, 2001 · N726AL · Boeing 737297 · Emergency LightingSDR 2001F00633Tire · separatedLOSS OF A SYSTEM HYDRAULICS. LEFT INBOARD TIRE LOST TREAD DURING TAKEOFF ROLL. PIECES OF THE TIRE TREAD DAMAGED HYDRAULIC LINES AND CONTROL CABLES LOCATED IN THE LEFT WHEEL WELL. ALSO, DAMAGE FROM FLYING RUBBER TO LEFT FORE FLAP, MID FLAP AND TRAILING EDGE Jan 26, 2001 · N147AW · Boeing 737297 · TireSDR P2EA00460Skin · crackedSJO - DURING Q-CHECK, FOUND THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 WITH CRACK. L = 1.1250 INCHES. W = 0.001 INCH. REPAIRED THE L-2 DOOR SKIN BS 956.5 TO BS 962.5 BETWEEN BEAMS NR 6 AND NR 7 IAW BOEING SRM 52-00-3 FIG 3. (X)Dec 8, 2000 · N5WM · Boeing 737297 · Service DoorsSDR P2EA00451Fitting · crackedSJO - DURING Q-CHECK, FOUND LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO WITH CRACK L = 2.00 INCHES. W = 0.002 INCH. REPLACED THE LEFT ELEVATOR HINGE SUPPORT AT BS 1156 ELEVATOR STA ZERO IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)Dec 2, 2000 · N5WM · Boeing 737297 · Horizontal Stabilizer, Tab StructureSDR P2EA00424Clip · crackedDURING Q CHECK, FOUND THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L WITH CRACK. REPLACE THE FRAME SUPPORT CLIP AT BS 663.75 STR 10L.Nov 23, 2000 · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00414Floor Support · crackedDURING Q CHECK, FOUND THE PASSENGER CABIN AT BS 727 RBL 65 WITH CRACKED ANGLE ON FLOOR SUPPORT. L/0.050 W/0.005 REPAIRED THE PASSENGER CABIN FLOOR SUPPORT ANGLE AT BS 727 RBL 65.Nov 22, 2000 · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00407Bulkhead · crackedSJO - DURING Q-CHECK, FOUND THE BS 178 BULKHEAD AT WL 196 FROM LBL 25 TO RBL 25 WITH CRACK. L = 1.00 INCH. W = 0.001 INCH. REPLACED THE BS 178 BULKHEAD INTERCOSTAL AT WL 196 FROM LBL 25 TO RBL 25 IAW BOEING SB 737-53A1173 REV 3 DATED MAY 6, 1999, SECTION IINov 22, 2000 · N5WM · Boeing 737297 · Fuselage Main, BulkheadSDR P2EA00396Channel · corrodedSJO - DURING Q-CHECK, THE CABIN FLOOR CHANNEL AT BS 296.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS, LENGTH 2.5 INCH, WIDTH 2 INCHES, DEPTH .025 INCH. REPLACED THE CABIN FLOOR CHANNEL AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 IANov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00413Floor Support · corrodedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5 AND LBL 41 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 0.50 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR ANGLE AT BS 286.5 BETWEEN LBL 11.5Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00412Floor Support · corrodedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO BS 312 LBL 11 WL 208.5 WITH CORROSION OUT OF LIMITS. L = 4.00 INCHES. W = 1.00 INCH. D = 0.040 INCH. REPLACED THE PASSENGER CABIN FLOOR SUPPORT STIFFENER AT BS 294.5 TO Nov 19, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00449Channel · crackedDURING Q CHECK, FOUND THE RT HAND WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK L/0.50 W/0.005 REPLACED RT HAND WING TE CAVITY LOWER CHORD CHANNEL.Nov 17, 2000 · Boeing 737297 · Wing Main, Frame StructureSDR P2EA00389Channel · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING TRAILING EDGE CAVITY LOWER CHORD CHANNEL AT RSS 180 WITH CRACK. (M)Nov 17, 2000 · N5WM · Boeing 737297 · Wing Miscellaneous StructureSDR P2EA00457Web · crackedDURING Q CHECK, FOUND THE FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END, WITH CRACK. L/1.00 W/0.001. REPAIRED FORWARD CARGO DOOR NR5 CROSS BEAM WEB, AFT END.Nov 16, 2000 · Boeing 737297 · Cargo/Baggage DoorsSDR P2EA00387Crossbeam · crackedSJO - DURING Q-CHECK, FOUND THE FORWARD CARGO DOOR NR 5 CROSSBEAM WEB AFT END WITH CRACK. (M)Nov 16, 2000 · N5WM · Boeing 737297 · Passenger/Crew DoorsSDR P2EA00455Flap Track · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NR'S 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS .313 LENGTH, .001 INCH WIDE, AND .250 INCH LENGTH, .001 INCH WIDE. REPLACED THE RIGHT WING OUTBOARD FLAP TRNov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge FlapsSDR P2EA00459Angle · corrodedDURING Q CHECK, FOUND APU TORQUE BOX RT SIDE ANGLE FROM BS 1118 TO 1138 WITH CORROSION, OUT OF LIMITS L/12.00 W/1.250 D/0.50. REPLACED THE APU TORQUE BOX RT SIDE ANGLE.Nov 14, 2000 · Boeing 737297 · Fuselage Main, StructureSDR P2EA00435Frame · crackedDURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 440 BETWEEN STR 23,24R.Nov 14, 2000 · Boeing 737297 · Fuselage Main, FrameSDR P2EA00440Frame · crackedDURING Q CHECK, FOUND FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R WITH CRACK L/0.250 W/0.005. REPAIRED FORWARD CARGO FRAME WEB AT BS 492.4 BETWEEN STR 23, 24R.Nov 14, 2000 · Boeing 737297 · Fuselage Main, FrameSDR P2EA00384Flap Track · crackedSJO - DURING Q-CHECK, FOUND THE RIGHT WING OUTBOARD FLAP TRACK LOWER INBOARD FLANGE BETWEEN NRS 30 AND 35 HORIZONTAL ATTACHMENT SCREWS WITH TWO CRACKS. (M)Nov 14, 2000 · N5WM · Boeing 737297 · Trailing Edge FlapsSDR P2EA00386Angle · corrodedSJO - DURING Q-CHECK, FOUND THE APU TORQUE BOX RIGHT ANGLE FROM BS 1118 TO 1138 WITH CORROSION OUT OF LIMITS. (M)Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00379Web · crackedSJO - DURING Q-CHECK, FOUND THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 WITH CRACK. L = 0.500 INCH. W = 0.005 INCH. REPAIRED THE CABIN FLOOR WEB FROM BS 1016 TO BS 1028 RBL 5 TO LBL 5 WL 208 IAW BOEING SRM 51-40-2 FIG 1. (X)Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00380Channel · crackedSJO - DURING Q-CHECK, FOUND THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL WITH CRACK. L = 0.50 INCH. W = 0.005 INCH. REPLACED THE PASSENGER CABIN AT BS 257 TO BS 267 BL ZERO WL 208 CHANNEL IAW BOEING SRM 51-10-1 PAGE 8 AND SRM 51-30-2. (X)Nov 14, 2000 · N5WM · Boeing 737297 · Fuselage Miscellaneous StructureSDR P2EA00393Slat Track · crackedSJO - DURING Q-CHECK, FOUND THE LT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER WITH CRACK LENGTH .50 INCH, WIDTH .50 INCH. REWORKED THE LEFT WING NR 1 SLAT AUXILIARY TRACK UPPER INBOARD CORNER AND WAS FOUND TO BE WITHIN LIMITS IAW BOEING SRM 57-20-1 FNov 13, 2000 · N5WM · Boeing 737297 · Leading Edge Devices
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