Boeing 737-2L9

Service difficulty reports · 593

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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 = '7372L9'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR F3LA97107Battery Pack · dischargedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED DOOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK IN AFT BAGGAGE COMPARTMENT AND CHECKED OKAY. (X)Apr 13, 1997 · N270FL · Boeing 7372L9 · Emergency LightingSDR F3LA97106Light · inoperativeDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING INOPERATIVE FROM CENTER OF AIRCRAFT TO AFT GALLEY AREA. MAINTENANCE RE-CONNECTED SECTION OF LIGHTING AND SYSTEM CHECKED OKAY. (X)Apr 13, 1997 · N270FL · Boeing 7372L9 · Emergency LightingSDR F3LA97105Battery · dischargedDEN - FLT 231 - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED THE FORWARD INBOARD EMERGENCY FLASHLIGHT INOPERATIVE. MAINTENANCE REPLACED BATTERY ASSEMBLY AND CHECKED OK. (M)Apr 13, 1997 · N270FL · Boeing 7372L9 · Emergency LightingSDR 97ZZZM557Bulb · failedDURING L.O. CHECK, WHILE TESTING THE EXTERIOR EMERGENCY LIGHTS, IT WAS NOTICED THAT THE RIGHT SIDE FLAP ILLUMINATION LIGHT WAS INOP. TROUBLESHOOTING FOUND BULB TO BE BURNED OUT. NO REPLACEMENT AVAILABLE AT SWF SO THE ITEM WAS DEFERRED. RELAMPED RIGHT AFT EXApr 12, 1997 · N464AT · Boeing 7372L9 · Emergency LightingSDR F3LA97103Battery Pack · dischargedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT OVERWING EMERGENCY EXIT LGIHTS INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OK. (M)Apr 9, 1997 · N271FL · Boeing 7372L9 · Emergency LightingSDR F3LA97104Skin · scratchedPAE - FOUND DENT AND SCRATCH IN SKIN BS 480 FROM STRINGER 26-28 RIGHT. CUT OUT DAMAGED AREA OF SKIN AT BS 480 FROM 1 INCHE BELOW STRINGER 26 TO 2 INCH ABOVE STRINGER 28 RT. FABRICATED AND INSTALLED EXTERNAL REPAIR BS 480 STRINGER 26-28 RT PER SRM 53-30-3, FIApr 8, 1997 · N270FL · Boeing 7372L9 · Fuselage Main, Plate/SkinSDR F3LA97101Frame · corrodedPAE - FOUND CORROSION (C53-202-01) ON FRAME BS 300B BETWEEN STRINGER 24 AND 25 LEFT. REMOVED CORROSION AT BS 500B BETWEEN STRINGER 24 AND 25 LEFT, 2 INCHES LONG BY 1 INCH WIDE, ORIGINAL THICKNESS .050. REMOVED 20 PERCENT, FOUND TO BE OUT OF LIMITS. REMOVED Apr 7, 1997 · N270FL · Boeing 7372L9 · Fuselage Main, FrameSDR F3LA97100Frame · corrodedDEN - FOUND CORROSION ON FRAME BS 500A BETWEEN STRINGER 24L AND 25L. REMOVED .02 BY 1 INCH BY .25 INCH FROM ORIGINAL THICKNESS OF .050. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3, 51-30-2, 51-10-2, 51-10-8, AND MM 51-20-00. (M)Apr 7, 1997 · N270FL · Boeing 7372L9 · Fuselage Main, FrameSDR 97ZZZM478Hyd Filter · rupturedDURING PREFLIGHT CHECK, FOUND HYDRAULIC LEAK IN MAIN LANDING GEAR WHEEL WELL. FOUND THE HYDRAULIC ACCOUSTIC FILTER ASSEMBLY HAD FAILED. THE OUTER CASE RUPTURED. REMOVED AND REPLACED THE ACCOUSTIC FILTER. (M)Mar 16, 1997 · N465AT · Boeing 7372L9 · Hydraulic System, MainSDR 97ZZZM335Circuit Breaker · failedFLT 553 - BUF-MCO - RIGHT SIDE WINDOW HEAT, OVERHEAT CAME ON AND AT THE SAME TIME NR 1 GENERATOR TRIPPED. THE RIGHT SIDE CIRCUIT BREAKER POPPED (WITH WINDOW HEAT SWITCH 'OFF'). RESET NR 1 GENERATOR. POPPED CIRCUIT BREAKER WAS HOT. DID NOT TRY TO RESET IT. Feb 21, 1997 · N737Q · Boeing 7372L9 · Windshield/Door Rain/Ice RemovalSDR 97ZZZM372Link · wornON OVERNIGHT SCHEDULED MAINTENANCE (COMPLIANCE WITH AD 76-11-05R1), IT WAS NOTED THAT THE LEFT ELEVATOR TAB PUSH/PULL ROD ENDS, BOLTS, BUSHING AND LINK WERE WORN BEYOND LIMITS (AT THE ELEVATOR SIDE). INSTALLED NEW BUSHING, BOLT AND LINK IAW BOEING MM 27-31-11Feb 19, 1997 · N737Q · Boeing 7372L9 · Elevator Tab Control SystemSDR 97ZZZM333Engine · fodFLT 730 - MCO-TOL - NR 2 ENGINE STALLED ON POWER UP. IN IDLE, ALL INDICATIONS SHOWED NORMAL (NO OVERTEMP). VISUAL INSPECTION REVEALED MINOR C-1 DAMAGE, MAJOR C-2 AND A SUBSEQUENT BOROSCOPE INSPECTION REVEALED THE C-12 AND C-13 BLADE DISTRESS WAS PRESENT. REFeb 12, 1997 · N737Q · Boeing 7372L9 · Engine (Turbine/Turboprop)SDR 97ZZZM334Engine · fodFLT 681 - LOG STATED 'CHECK NR 2 ENGINE, HEARD LOUD THUMP'. ON INSPECTION OF INLET AND EXHAUST, FOUND FOREIGN OBJECT DAMAGE TO C-1 AND C-2 BLADES. REMOVED AIRCRAFT FROM FLIGHT LINE FOR ENGINE CHANGE AT HANGAR. REMOVED DEFECTIVE ENGINE AND REPLACED IT WITH AFeb 8, 1997 · N465AT · Boeing 7372L9 · Engine (Turbine/Turboprop)SDR 97ZZZX990Door Frame · crackedDEN - DURING SERVICE CHECK, MAINTENANCE REPORTED C1 CARGO DOOR FORWARD FLANGE CRACKED APPROXIMATELY .75 INCH IN RADIUS UNDER DOOR LATCH HOOK. ON 2-8-97, INSTALLED REPAIR PER F.A. 52-737-002, SB 737-52-1090, REV 1.Feb 4, 1997 · N271FL · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 97ZZZX1070Door · crackedDEN - DURING AN A-3 CHECK, INSPECTION REPORTED A 0.75 INCH CRACK ON THE LOWER FORWARD CORNER OF THE FORWARD CARGO DOOR NEAR THE HOLD-OPEN HOOK. REPAIRED PER BOEING SB 737-52-1090, REV 1, FIGURE 2. DETAIL II, FRONTIER E.A. NR 52-737-002 AND E.A. NR 52-737-003Jan 16, 1997 · N270FL · Boeing 7372L9 · Cargo/Baggage DoorsSDR 97ZZZM196Hydraulic Pump · leakingFLT 721 - CAK-MCO - NR 1 ENGINE HYDRAULIC PUMP LEAKING (ON POST FLIGHT AT MCO). FOUND NR 1 ENGINE HYDRAULIC PUMP LEAKING AT THE CASE HALF. REMOVED AND REPLACED NR 1 ENGINE HYDRAULIC PUMP AND PERFORMED OPERATIONAL CHECK IAW BOEING MM 29-11-32. (M)Jan 8, 1997 · N465AT · Boeing 7372L9 · Hydraulic Pump (Electric/Engine), MainSDR 98ZZZM158Wire · looseUPON ARRIVAL OF FLT 607 TO GSO, FOUND LAS 5 WHITE FLOOR PROX LIGHTS INOP. FOUND WIRE PULLED OUT OF SPLICE. RE-SPLICED WIRES PER BOEING SOP 20-11-03. STOWED WIRES AND THE LIGHTS OPS CHECKED GOOD. (M)Jan 7, 1997 · N737Q · Boeing 7372L9 · Light System WiringSDR 97ZZZM195Uplock Sensor · malfunctionedFLT 705 - DAY-MCO - LEFT GEAR RED LIGHT ON INTERMITTENTLY IN FLIGHT WITH GEAR 'UP' OR 'OFF. REMOVE AND REPLACED LEFT GEAR UPLOCK PROXIMITY SENSOR IAW WITH BOEING MAINTENANCE MANUAL 32-61-21. PERFORMED LANDING RETRACTION TO ASSURE OPERATIONAL INTERGRITY. INSJan 7, 1997 · N737Q · Boeing 7372L9 · Landing Gear Position and WarningSDR LR00696Hose Assy · damagedBAQ/SJO - FLT 610 - HYDRAULIC SYSTEM 'A' HAD A TOTAL LOSS OF HYDRAULIC OIL DUE TO FLEX HOSE ASSY, P/N BACH8A04NN0264T, SPRUNG LEAK AT WHEELWELL AND CREW DECLARED EMERGENCY LANDING. AIRCRAFT LANDED WITH NO INCIDENTS AT SJO. HOSE WAS REPLACED AND TEST WAS ACCODec 29, 1996 · N281LF · Boeing 7372L9 · Hydraulic System, MainSDR 97ZZZM258Hose · damagedFLT 610 - BAQ-SJO - HYDRAULIC SYSTEM 'A' HAD A TOTAL LOSS OF HYDRAULIC OIL DUE FLEX HOSE ASSEMBLY, P/N BACH8A04NN0264T SPRUNG A LEAK AT WHEEL WELL AND CREW DECLARED EMERGENCY LANDING. AIRCRAFT LANDED WITH NO INCIDENTS AT SJO. HOSE WAS REPLACED AND TEST WAS ADec 29, 1996 · N281LF · Boeing 7372L9 · Hydraulic System, MainSDR 97ZZZM197Beam · corrodedFOUND CORROSION ON TRAILING EDGE BEAM ON VERTICAL FIN 4H SIDE ATT FIN STATION 127.10 RUD STATION 60.15 (MARKED). REPAIRED TRAILING EDGE BEAM PER TRAMCO EWO 96-09-29. (M)Dec 19, 1996 · N464AT · Boeing 7372L9 · Vertical StabilizerSDR 97ZZZM208Hydraulic Line · pin holeFLT 532 - MCO-SWF - A/C 485 RETURNED TO MCD DUE TO A TOTAL LOSS OF HYDRAULIC FLUID IN 'A' SYSTEM. AFTER LANDING AT MCO THE A/C HAD NO NOSE WHEEL STEERING. THE A/C HAD TO BE TOWED FROM RUNWAY TO THE GATE AREA. PASSENGERS WERE TRANSFERRED TO A/C 737Q TO COMPNov 28, 1996 · N465AT · Boeing 7372L9 · Hydraulic System, MainSDR ZZDA5722896Skin · delaminationNR 3 SPOILER - CUT OUT DELAMINATED AREA ON LOWER SKIN SURFACE 17.50 INCHES BY 7 INCHES. INSTALLED REPAIR IAW B-737 SRM 57-50-5. (X)Nov 8, 1996 · N464AT · Boeing 7372L9 · SpoilersSDR 96ZZZM1561Transmitter · malfunctionedFLT 822 - MCO-MCI - DURING FLAP EXTENSION THE RIGHT T/E FLAP STAYED AT 2 UNITS AND THE LEFT FLAP AT 1 UNIT CAUSING AN ASYMMETRIC SPLIT FLAP LOCKOUT CONDITION. THE MECHANIC IN MCI REMOVED AND REPLACED THE RIGHT FLAP POSITION TRANSMITTER PART NR 10-61841-1 PER Nov 4, 1996 · N737Q · Boeing 7372L9 · Trailing Flap Position Indicating SystemSDR ZZDA2121596Sense Line · malfunctionedMCO - FLT 822 - FLIGHT DEPARTED MCO 10-31-96 WITH THE LEFT AIR CONDITIONING PACK TRIPPING AFTER TAKEOFF. RESET PACK. LOST CONTROL OF LEFT PACK MIX VALVE. ABLE TO CONTROL MIX VALVE AFTER LANDING. TROUBLESHOT SYSTEM PER 737 MM, CHAPTER 21-11-0, AND FOUND LOOOct 31, 1996 · N465AT · Boeing 7372L9 · Cabin Cooling SystemSDR 320796Retract Mech · malfunctionedON TAKEOFF, LANDING GEAR HANDLE WOULD NOT RETRACT. MADE A LOW PASS FOR A TOWER VISUAL CHECK. REFERRED TO NON-NORMAL PROCEDURES CHECK LIST. RESET LEVER LATCH AND LIGHT BREAKER. ALL INDICATIONS WERE NORMAL. USED QRH PROCEDURES AND NORMAL PROCEDURES CHECK LOct 2, 1996 · N465AT · Boeing 7372L9 · Landing Gear Retraction/Extension SystemSDR 96ZZZM1430Fire Loop Conn · dirtyDURING LANDING CHECK AFTER ARRIVAL IN OMA, FLT 800, HAD APU FIRE WARNING INDICATION (AUDIBLE AND VISUAL) DURING APU START. APU SHUTDOWN AUTOMATICALLY. CREW PULLED FIRE WARNING SWITCH AND AGENT WAS DISCHARGED. UPON ARRIVAL AT GATE MAINTENANCE PERFORMED AN INSep 29, 1996 · N464AT · Boeing 7372L9 · Fire DetectionSDR 96ZZZX5580Service Door · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND RT SERVICE DOOR AFT LOWER CORNER HAS 1.50 INCH LONG CRACK AT FUSELAGE EXTERIOR SURFACE AT BS 344.0 WL 208.01. FABRICATED 3 DOUBLERS FROM 2024-T-3 .100 INCH, AND 2 FROM 2024-T-3 .063 INCH IAW SRMSep 10, 1996 · N465AT · Boeing 7372L9 · Service DoorsSDR 96ZZZX5579Angle · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 380.0 LBL 25 TO RBL 25 FRAME L-ANGLE CORRODED. REMOVED HARDWARE, FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-01, FABRICATED NEW L-ANGLE FROM 7075 .050 INCH, 4 INCHES BY 1.50 INCHES BY 2.18Sep 10, 1996 · N465AT · Boeing 7372L9 · Fuselage Miscellaneous StructureSDR 96ZZZX5578Floor Beam · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND CABIN BS 312 RBL 20 FLOOR BEAM UPPER CAP CORRODED. FABRICATED FLOOR BEAM REPAIR FROM 7075-T6 .063 INCH L-ANGLE IAW SRM 53-10-09. ALODINED AND PRIMED IAW SRM 51-10-02 AND MM 51-20-11. INSTALLEDSep 10, 1996 · N465AT · Boeing 7372L9 · Fuselage Main, Floor BeamSDR 96ZZZX5577Frame · crackedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND FRAME AT BS 460.0 BETWEEN STR 20L - STR 21L, AREA HAS TWO EACH CRACKS EMANATING FROM RIVET HOLES AT INNER CORD. FABRICATED FORMED SECTION REPAIR FROM 7075-0 .063 INCH IAW SRM 51-40-3. HEAT TREASep 10, 1996 · N465AT · Boeing 7372L9 · Fuselage Main, FrameSDR 96ZZZX5576Stringer · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND BS 520.0, STR 26L, STRINGER CORRODED. REMOVED THE TRANSITION PANEL. STR 26L OUT OF LIMITS IAW SRM 51-10-6. CUT OUT A 12 INCH SECTION AT STA 520. FABRICATED REPAIR PARTS IAW SRM 53-10-3. INSTSep 10, 1996 · N465AT · Boeing 7372L9 · Fuselage Main, Longeron/StringerSDR 96ZZZX5581Frame · corrodedDURING C-CHECK INSPECTION, REVEALED THAT AFT CARGO COMPARTMENT FRAME HAS CORROSION UNDER NUTPLATES BETWEEN STR 24L AND STR 25L. REMOVED CORROSION, MATERIAL REMOVAL FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED NUTPLATES IAW SRM 51-30-2. FABRICATED FRAMSep 8, 1996 · N465AT · Boeing 7372L9 · Fuselage Main, FrameSDR F3LA96019Bulb · failedDEN - FLT 443 - DURING SERVICE CHECK, MAINTENANCE REPORTED THE EMERGENCY AISLE PATH LIGHTING INOPERATIVE. CLEANED CONTACTS, REPLACED BULBS AND SYSTEM CHECKED OKAY. (X)Jul 21, 1996 · N170PL · Boeing 7372L9 · Emergency LightingSDR 96ZZZM1223Outflow Valve · malfunctionedFLT NR 501 - ALB-MCO - EXPERIENCED PRESSURIZATION PROBLEMS AT FL 350 (MAX PRESS DIFF) CABIN BEGAN CLIMBING AT 1,000 PLUS. OUTFLOW WAS FULL CLOSED AND UNABLE TO CONTROL CABIN PRESSURE. OXYGEN MASKS DEPLOYED. ACCOMPLISHED EMERGENCY DESCENT TO 10,000 AND PERFOJul 16, 1996 · N464AT · Boeing 7372L9 · Pressure Regulator/Outflow ValveSDR F3LA96018Slide · low pressureMSP - DURING SERVICE CHECK, MAINTENANCE REPORTED L-1 DOOR ESCAPE SLIDE BOTTLE PRESSURE LOW. REPLACED L-1 DOOR ESCAPE SLIDE. (M)Jul 14, 1996 · N170PL · Boeing 7372L9 · Escape SlideSDR 96ZZZX3660Light Socket · inoperativeDEN - FLT 65 - UPON ARRIVAL, FLIGHT CREW REPORTED EXTERNAL EXIT LIGHTS INOPERATIVE AT LEFT FORWARD PASSENGER DOOR AND RIGHT AFT SERVICE DOOR. MAINTENANCE REPLACED BATTERY PACKS AND LIGHT SOCKETS FOR BOTH DOORS, AND SYSTEM CHECKED OKAY. AIRFRAME, 34,084.4 HOUJun 19, 1996 · N170PL · Boeing 7372L9 · Emergency LightingSDR 96ZZZX3659Battery Pack · dischargedDEN - FLT 443 - UPON ARRIVAL, FLIGHT CREW REPORTED EXTERNAL EXIT LIGHTS INOPERATIVE AT LEFT FORWARD PASSENGER DOOR AND RIGHT AFT SERVICE DOOR. MAINTENANCE REPLACED BATTERY PACKS AND LIGHT SOCKETS FOR BOTH DOORS, AND SYSTEM CHECKED OKAY. AIRFRAME, 34,084.4 HOJun 19, 1996 · N170PL · Boeing 7372L9 · Emergency LightingSDR 96ZZZM1417Strut · corrodedFLT 561 - MECHANICS OBSERVED HYDRAULIC FLUID LEAKING FROM BOTTOM GLAND NUT ON NOSE LANDING GEAR. UPON TEAR DOWN (FOR A SEAL KIT REPLACEMENT) INSPECTION REVEALED THAT THE OUTER CYLINDER GLAND NUT THREADS WERE PITTED DUE TO CORROSION, UPPER CENTERING CAM INNER Jun 19, 1996 · N737Q · Boeing 7372L9 · Nose/Tail Landing Gear Strut/AxleSDR 96ZZZM1389Gear Assy · corrodedPRIOR TO BOARDING PASSENGERS FOR FLT 561, MECHANICS OBSERVED HYDRAULIC FLUID LEAKING FROM BOTTOM GLAND NUT ON NOSE LANDING GEAR. UPON TEAR DOWN INSPECTION REVEALED THAT THE OUTER CYCLINDER GLAND NUT THREADS WERE SEVERELY PITTED DUE TO CORROSION, SEAL NOT IN PJun 19, 1996 · N737Q · Boeing 7372L9 · Nose/Tail Landing GearSDR 96ZZZX1693Control Panel · shortedAFTER TAKEOFF, CREW TURNED ON THE ENGINE ANTI-ICE AND NOTICED ALL 3 BLUE ADVISORY LIGHTS FLICKERING ON THE NR 1 ENGINE SIDE. SMOKE STARTED APPEARING FROM THE PANEL. ANTI-ICE WAS SELECTED TO THE OFF POSITION AND THE CIRCUIT BREAKER WAS PULLED. THE ACFT RETURMar 11, 1996 · N737Q · Boeing 7372L9 · Air Intake Anti/De-Ice SystemSDR 96ZZZX1399Hyd Line · failedAFTER TAKEOFF FROM BRADLEY, CONN, NLG WOULD NOT RETRACT RESULTING IN AN AIR TURNBACK. FOUND NLG LOCK ACTUATOR HYD FLEX LINE FAILED. REMOVED AND REPLACED FLEX LINE. LEAK CHECK GOOD PER MM 29-12-31.Feb 3, 1996 · N464AT · Boeing 7372L9 · Hydraulic System, MainSDR 95ZZZX6789Pcu · failedDURING MAINTENANCE, DISCOVERED THE RUDDER BEGAN TO FLUTTER WHEN THE SYSTEM WAS PRESSURIZED. VISUAL INSPECTION REVEALED THE RUDDER POWER CONTROL UNIT (PCU) WAS LEAKING AND VERY HOT. REPLACED THE RUDDER PCU. POWER CONTROL UNIT WAS OVERHAULED BY AERO CONTROLS,Oct 31, 1995 · N737Q · Boeing 7372L9 · Elevator Control System
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