Boeing 737-2M8

Service difficulty reports · 65

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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 = '7372M8'
  ORDER BY difficulty_date DESC"

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SDR AWXA200601286Wire Harness · damagedSAL - EEL - MAINTENANCE EMERGENCY EXIT LIGHT INOP SEAT ROW 9. EMERGENCY EXIT LIGHT INOP SEAT ROW 9 WAS CORRECTED. REMOVED AND REPLACED SEAT HARNESS, OPS GOOD.Jul 19, 2006 · N141AW · Boeing 7372M8 · Light System WiringSDR CA021108022Apu · failed(CAN) ON APPROACH, APU WAS STARTED AS NORMAL. SHORTLY AFTER START UP A VIBRATION WAS FELT THROUGHOUT THE AIRFRAME. AUTO SHUTDOWN OF THE APU OCCURRED,AS WELL AS A FIRE WARNING IN THE COCKPIT. APU FIRE QRC WAS ACCOMPLISHED WITH ASSOCIATED FIRE HANDLE PULLED AND Nov 7, 2002 · Boeing 7372M8 · APU Core EngineSDR CA010313021Gearbox · worn(CAN) AIRCRAFT WAS ENROUTE FROM CALGARY TO WINNIPEG WHEN THE RIGHT HAND ENGINE EXPERIENCED A LOSS OF ENGINE OIL. THE CREW SHUT DOWN THE ENGINE WHEN THE OIL PRESSURE STARTED TO DROP AND THE ENGINE OIL TEMPERATURE BEGAN TO CLIMB. THE OIL APPEARED TO HAVE LEAKED Mar 1, 2001 · Boeing 7372M8 · Accessory GearboxesSDR CA001122016Engine · failed(CAN) DURING CLIMB FROM VANCOUVER THE CREW NOTICED NR 2 ENGINE OIL QUANTITY DROP TO ZERO. THEY INITIATED A PRECAUTIONARY SHUT DOWN OF THE ENGINE AND RETURNED TO VANCOUVER. MAINTENANCE PERSONNEL IN VANCOUVER FOUND NORMAL OIL QUANTITY IN THE ENGINE. THEY CARRIEDNov 8, 2000 · Boeing 7372M8 · Engine (Turbine/Turboprop)SDR CA001016011Bolt · missing(CAN) CREW REPORTED ON TAXI OUT WHEN THEY CHECKED THE FLIGHT CONTROLS THE ELEVATOR FELT VERY RESTRICTED IN DOWN TRAVEL MOTION. OPERATION FELT NORMAL WITH A SYSTEM HYDRAULIC DEPRESSURIZED. UPON INVESTIGATION FOUND A SYSTEM ELEVATOR PCU INPUT ROD TO ELEVATOR INPOct 1, 2000 · Boeing 7372M8 · Fuselage Miscellaneous StructureSDR AWXA9900477Battery Pack · dischargedROW 6-14 EMERGENCY EXIT LIGHTS DID NOT WORK DURING TEST. BATTERY CHARGED BY CONTRACT MAINTENANCE PREVIOUS FLIGHT. REPLACED AFT EMERGENCY LIGHT BATTERY PACK IN DROP CEILING. OPS CK GOOD RECOMMENDATION. NO RELATED HISTORY.Dec 16, 1999 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9900400Wire · brokenEMERGENCY LIGHT INOP, ROW 4. REPAIRED BROKEN WIRE, OPS CK NML.Nov 7, 1999 · N141AW · Boeing 7372M8 · Light System WiringSDR AWXA9900337Rib · crackedC-CHECK, 2 INCH CRACK ON I/B UPPER ANGLE ON LEADING EDGE INT OF I/B FRAME AT WS 185.5 RT WING OF PYLON. REMOVED, FABRICATED, HEAT TREATED TO T3 COND, ALODINED AND REPLACED RIB IAW SRM 57-20-2 AND 57-30-2.Jun 10, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, FrameSDR AWXA9900340Tie Clip · crackedC-CHECK, STRINGER TIE CLIP CRACKED, 16L FS 727A. REMOVED STRINGER TIE CLIP IAW SRM 51-30-2, FAB'D NEW STRINGER TIE CLIP IAW 51-10-1. TREATED AND PRIMED NEW CLIP IAW SRM 51-10-2.Jun 3, 1999 · N141AW · Boeing 7372M8 · Fuselage Miscellaneous StructureSDR AWXA9900341Angle · crackedC-CHECK, .75 INCH CRACK ON UPPER ANGLE OF LT WING L/E RIB I/B SIDE OF NR 1 ENG PYLON. FABRICATED AND INSTALLED REPAIR PART AT WING STA 185.5 IAW 51-30-00, MATERIAL 2024-0 .063 HEAT TREATED TO 2024-T4.Jun 2, 1999 · N141AW · Boeing 7372M8 · Wing Miscellaneous StructureSDR AWXA9900339Skin · crackedC-CHECK, APPROX 2.5 INCH CRACK ON FUSLAGE SKIN 3.5 FT BELOW L-2 DOOR. REMOVED EXISTING DOUBLER PER SRM 51-40-2, CUTOUT DAMAGE PER PT6 51-00-00 FIG 23. FABRICATED DOUBLER AND INSTALLED PER SRM 53-30-1 FIG 1 AND 51-30-2 MATL 2024TB .090.Jun 2, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA9900338Skin · crackedC-CHECK, LT FUSLAGE CRACK AT SR17L. ALSO, LT WTB BETWEEN 2ND AND 3RD REPAIR, 4 TO 5 INCHES LONG. BOTH PLACES FABRICATED NEW REPAIR FROM 2024T3 .090 R646704 IAW SRM 53-30-3 FIG 1. TREATED AND PRIMED NEW REPAIR AND AREA, INSTALLED REPAIR DOUBLER PER 53-30-3 FJun 2, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA9900047Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK LEFT SIDE AT STRINGER 17, BS 727, BELOW TEMP REPAIR FWD OF BS 747. INSTALLED REPAIR USING BLIND FASTENERS IAW FIG 1 SHEET 2 OF SRM 53-30-3, REPLACE BLIND FASTENERS AFTER 10,000 FLIGHT CYCLES WITH SFeb 19, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA9900046Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK BELOW STRINGER 16 RT SIDE, AFT OF WING TO BODY FAIRING FROM STATION 747 TO 767. REPAIRED PER ER 2-53-34-09 STEP 7, REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONTHS NOT TO EXCEED 600Feb 19, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA9900045Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND 1 FUSELAGE SKIN CRACK AT STRINGER 19 RT SIDE AT BS 727 TO 747. REPAIRED PER ER 2-53-34-08 STEP 8, NEED TO REPLACE SKIN OR REPAIR WITH SRM APPROVED REPAIR WITHIN 24 MONTHS NOT TO EXCEED 6000 FLIGHT HOURS.Feb 19, 1999 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA9900012Battery Pack · dischargedRT EMERGENCY EXIT LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED R-2 DOOR EMERGENCY EXIT LIGHT BATTERY PACK, OPS CK GOOD.Jan 7, 1999 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9800078Power Supply · inoperativeEMERG EXIT LIGHT CENTER AISLE OVERWING WON'T LIGHT WITH OTHER EXIT LIGHTS. REMOVED AND REPLACED BATTERY PWR SUPPLY UNIT, OPS CKD NORMAL. STC NR SA3432NM.Mar 14, 1998 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9700391Light · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLASHLIGHT INOP AT L-2 DOOR. REMOVED ANDANDREPLACED L-2 DOOR EMERGENCY FLASHLIGHT & HOLDER.Jul 9, 1997 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9700338Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY LIGHT OVER R-2 DOOR INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD. STC - SA3432NM.Jun 11, 1997 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9700329Connector · inoperativeDURING ROUTINE MAINTENANCE CHECK, FOUND SEAT ROW 1 TO 5 EMERGENCY LIGHTS WILL NOT EXTINGUISH WITH EMERGENCY LIGHT SWITCH OFF AND SHIP'S POWER OFF. INSTALLED NEW SOCKET IN POWER SUPPLY CONNECTOR AT ROW 3. STC - SA3432NM.Jun 6, 1997 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9700302Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND FIRST CLASS EMERGENCY LIGHTS COME ON WHEN BATTERY TURNED OFF. REMOVED AND REPLACED EMERGENCY BATTERY PACK, OPS CHECK GOOD. STC - SA3432NMMay 26, 1997 · N141AW · Boeing 7372M8 · Emergency LightingSDR 97ZZZX2843Housing · crackedSPOILER ACTUATOR HAS A HOLE IN HOUSING. FOUND DURING PROOF PRESSURE TESTING FOR REPAIR.May 23, 1997 · Boeing 7372M8 · Drag Control ActuatorSDR AWXA9700233Position Ind · inoperativeUNSCHEDULED LANDING IN LAS. TRAILING EDGE FLAPS SPLIT, 1 AND 5 POSITIONS. REMOVED AND REPLACED FLAP T/E POSITION INDICATOR. CYCLED FLAPS SEVERAL TIMES, OPS CHECKS GOOD.Apr 17, 1997 · N141AW · Boeing 7372M8 · Trailing Flap Position Indicating SystemSDR AWXA9700244Floorbeam · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM UPPER CHORD AT BS 312, WL 208, LBL 11 TO RBL 11. REMOVED UPPER CHORD OF FLOORBEAM AT BS 312 FROM LBL 18 TO RBL 18 AND REPLACED CHORD PER SRM 53-10-9.Apr 7, 1997 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA9700243Floorbeam · corrodedDURING ROUTINE MAINTENANCE CHECK, FOUND CORROSION ON FLOORBEAM BS 328, RBL 11 TO 20, WL 208. REMOVED UPPER CHORD, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 51-30-2, 51-30-5 AND 53-10-9, FIG 5.Apr 7, 1997 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA9700225Battery Pack · dischargedDURING ROUTINE MAINTENANCE CHECK, FOUND OVERWING CEILING PANEL EMERGENCY LIGHT INOP. REMOVED AND REPLACED OVERWING CEILING EMERGENCY LIGHT BATTERY PACK, OPS CHECK GOOD, STC - SA3432NM.Mar 25, 1997 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA9700191Rudder Pcu · malfunctionRUDDER AND AIRCRAFT SHUDDERED EXCESSIVELY DURING DEFLECTION OF RIGHT RUDDER. LEFT RUDDER DEFLECTION NORMAL. REMOVED AND REPLACED RUDDER PCU AND C/W ADJUSTMENT TEST. NO DEFECTS NOTED, OPS NORMAL.Mar 20, 1997 · N141AW · Boeing 7372M8 · Rudder ActuatorSDR AWXA9700190Bolts · looseVIBRATION NOTED BY INBOUND CREW AT FLAPS 2, RT INBOARD FLAP AREA. FOUND LT AND RT INBOARD FOREFLAP TOGGLE BOLTS LOOSE. TIGHTENED AND RE-SAFETIED BOLTS. ALSO, TIGHTENED AND RE-SAFETIED LT INBOARD FOREFLAP TRACK ATTACH BOLTS. INSPECTED ENTIRE FLAP AREA.Mar 18, 1997 · N141AW · Boeing 7372M8 · Trailing Edge Flap Control SystemSDR AWXA9700175Line · blownAIR TURNBACK, LOSS OF SYSTEM-A HYDRAULICS. SHORTLY AFTER TAKEOFF, NR 2 A-HYDRAULIC LOW PRESSURE LIGHT FOLLOWED BY A-SYSTEM QUANTITY TO ZERO. REMOVED AND REPLACED NR 3 BRAKE FLEX LINE AND A-SYSTEM HYDRAULIC CASE DRAIN FILTER, NO DEBRIS. REPLENISHED A-SYSTEM Mar 6, 1997 · N141AW · Boeing 7372M8 · Hydraulic System, MainSDR AWXA960605Power Supply · inoperativePHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. (M)Oct 19, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR 96ZZZM1484Power Supply · inoperativePHX - FLT 2887 - DURING ROUTINE MAINTENANCE CHECK, FOUND L-1 AND R-1 EMERGENCY EXIT LIGHTS INOP. REPLACED BOTH FORWARD EMERGENCY EXIT POWER SUPPLY. OPS CHECK GOOD. REFERENCE AWXA960605.Oct 19, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960592Power Supply · inoperativePHX - FLT 2592 - DURING ROUTINE MAINTENANCE CEHCK, FOUND RIGHT OVERWING EXIT INTERIOR EXIT SIGN ON DOOR FRAME INOP. REPLACED BATTERY POWER CHARGER WITH SERVICEABLE, OPS CHECK NORMAL. (M)Oct 14, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960591Battery · dischargedPHX - FLT 2550 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY EXIT LIGHTS INOP AT L1 AND R1 DOORS. REMOVED AND REPLACED BATTERY PACK, OPS NORMAL AT THIS TIME. (M)Oct 14, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960533Battery Pack · dischargedPHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND EMERGENCY FLOOR LIGHT SIGNS AT R1, L1 AND RIGHT OVERWING INOP. REMOVED AND REPLACED BATTERY PACK M1050. OPS CHECKED GOOD. (M)Sep 27, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960521Connector · shortedPHX - FLT 2267 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT EMERGENCY EXIT AFT VERTICAL EXIT LIGHT INOP. FOUND POWER CONNECTOR SHORTING ON A/C FRAME. REPLACED HEATSHRINK WRAP AND SECURED. (M)Sep 21, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960513Power Supply · inopPHX - FLT 2622 - DURING ROUTINE MAINTENANCE CHECK, FOUND RIGHT OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED MID RIGHT EMERGENCY LIGHT POWER SUPPLY. OPERATES NORMALLY. (M)Sep 18, 1996 · N141AW · Boeing 7372M8 · Emergency LightingSDR AWXA960375Turbine Blade · failedLAS - FLT 2976 - AIR TURN BACK, AT CLIMB POWER FL 200 NR 1 ENGINE COMMENCED SEVERE VIBRATIONS. ALL ENGINE INDICATIONS NORMAL. RETARDED THRUST LEVER. VIBRATIONS CONTINUED. SHUTDOWN ENGINE IAW QRH. RETURNED LAS. FOUND TURBINE WHEEL BLADES MISSING MATERIAL.Sep 9, 1996 · N141AW · Boeing 7372M8 · Turbine SectionSDR AWXA960350Seat · not securedPHX - FLT 2890 - AIR TURNBACK, SEAT ROW 6 A, B, C, NOT SECURED. SECURED SEAT ROW 6 A, B, C IN SEAT TRACK AS NEEDED. (M)Jul 24, 1996 · N141AW · Boeing 7372M8 · Passenger Compartment EquipmentSDR AWXA960331Engine · bird strikeLAS - FLT 0981 - ABORTED TAKEOFF. BIRD STRIKE ON TAKEOFF ROLL. LEFT HAND FORWARD PART OF A/C. C/W AWA FORM 382 FOD INSPECTION PARAGRAPH A, SECTIONS 1 AND 2. FOD DID NOT ENTER ENGINE AND NO DAMAGE NOTED. (X)Jul 8, 1996 · N141AW · Boeing 7372M8 · Engine (Turbine/Turboprop)SDR AWXA960320Engine · overtempPHX/ONT - FLT 2622 - AIR TURNBACK. NR 1 ENGINE OIL TEMPERATURE CLIMBED TO 118 DEGREES AT CRUISE, 123 CELSIUS ON DESCENT, 140 CELSIUS FOR 10 MINUTES AT 110 FEET. POWER UP TEMPERATURE NORMAL. REMOVED AND REPLACED NR 1 ENGINE PER R5M71003, RIGGED PER CARD F5M7Jul 5, 1996 · N141AW · Boeing 7372M8 · Engine (Turbine/Turboprop)SDR AWXA960255Skin · dentedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SMALL DENT AFT OF L-2 DOOR (CENTER OF DOOR, 2 INCH AFT). REFERENCE FORM 106 NR 23581. REPLACED SKIN PER ER 2-53-35-06. ENGINEERING REFERENCE TCO-PAN-95-0605RR-621RR. (M)May 18, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR SWXA960252Seat Track · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON SEAT TRACK BS 947-967, LBL 25, WL 208. REMOVED AND INSTALLED FABRICATED SEAT TRACK AT BS 947-967, LBL 25, WL 208 PER SRM 51-30-2, 51-10-1 AND 51-30-8. ALODINED AND PRIMED. (May 15, 1996 · N141AW · Boeing 7372M8 · Fuselage, Seat/Cargo Attach FittingsSDR AWXA960256Skin · dentedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND SKIN DENTED STATION 1047-1063, STRINGER 18 RT, WL 206. REMOVED DAMAGED SKIN, FABRICATED REPAIR DOUBLER, INSTALLED REPAIR PARTS PER SRM 53-30-3. (M)May 15, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Plate/SkinSDR AWXA960254Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 947, LBL 0-4, WL 208. REMOVED STRAP AND REPAIRED PER ER 2-53-15-44 (TCO-PAN 96-0624RR). (M)May 15, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA960253Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 967, LBL 21-19, WL 208. REMOVED DAMAGED AREA AT BS 967, LBL 21-29, WL 208. FABRICATED PART AND INSTALLED PER SRM 53-10-9. (M)May 15, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA960251Splice · corrodedFLT 7812 - PAE - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON STRINGER 27, RIGHT SPLICE BS 905. REMOVED STRINGER SPLICE AT BS 905 AND STRINGER 27R. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1. ALODINED, PRIMED AND INSTALLED. (M)May 15, 1996 · N141AW · Boeing 7372M8 · Fuselage Miscellaneous StructureSDR AWXA960250Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 1006, LBL 11, WL 208. REMOVED CORROSION BS 1006, LBL 11, WL 208. OUT OF LIMIT PER SRM 53-10-1. REPAIRED IAW ER 2-53-15-43 (TCO-PAN-96-0612RR) (M)May 14, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA960249Floor Beam · corrodedPAE - FLT 7812 - DURING ROUTINE SCHEDULED C-7 MAINTENANCE CHECK, FOUND CORROSION ON FLOOR BEAM BS 986.5, RBL 41, RBL 50, WL 208. REMOVED CORROSION BS 986.5, RBL 37, RBL 39 AND FOUND OUT OF LIMIT PER SRM 53-10-1 AND REPAIR. INSTALLED IAW ER 2-53-15-42 (TCO-PAMay 14, 1996 · N141AW · Boeing 7372M8 · Fuselage Main, Floor BeamSDR AWXA960158Actuator · brokenTUS-PHX - FLT NR 604 - GATE RETURN, A SYSTEM HYDRAULIC FAILURE DURING TAXI. NR 8 SPOILER ACTUATOR BROKEN AT CASTING. REPLACED NR 8 SPOILER ACTUATOR PER CARD R3M27016. LEAK AND OPERATION CHECK GOOD. (M)Mar 25, 1996 · N141AW · Boeing 7372M8 · Drag Control ActuatorSDR AWXA960155Static Inverter · failedLAS - FLT NR 1931 - AIR TURN BACK, AFTER TAKEOFF LOST NAVIGATION AND COMMUNICATION ON CAPTAINS SIDE. REMOVED AND REPLACED STATIC INVERTER AND R-36 RELAY IN P-6. CHANGED R-37 AS A PRECAUTION. (M)Mar 21, 1996 · N141AW · Boeing 7372M8 · DC Rectifier/Converter
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