Boeing 747-2F6B

Service difficulty reports · 100

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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 = '7472F6B'
  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 P5CA0601447Lug · elongatedNR 3 ENGINE CORE COWLING - AFT HINGE SUPPORT ASSEMBLY - INTERIM REPAIR TO AFT LUG. REPAIRED PER BOEING 8100-9 DATED 03FEB2006.Feb 15, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon, Main FrameSDR P5CA0601443Web · crackedCRACK IN THE CANTED PRESSURE DECK WEB AT BS 1259 & LBL 32. REPAIRED PER BOEING 8100-9 DATED 27JAN2006, PER EO-4753A624.Feb 6, 2006 · N534MC · Boeing 7472F6B · Fuselage Miscellaneous StructureSDR P5CA0601442Skin · chafedNR 3 PYLON INBOARD SIDE ACCESS PANEL 473BL INTERIOR SKIN AT CUTOUT FORWARD SIDE CHAFING MARKS. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A186.Feb 6, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon, Plate/SkinSDR P5CA0601441Skin · chafedNR 4 PYLON ACCESS PANEL 483BL CUTOUT, FORWARD INTERNAL SKIN CHAFING MARKS. REPAIRED PER BOEING 8100-9 DATED 24JAN2006 PER EO-4754A186.Feb 6, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon, Plate/SkinSDR P5CA0601440Structure · crackedNR 2 PYLON - PRECOOLER ACCESS CUTOUT CRACKED, AFT BOTTOM RIGHT SIDE. REPAIRED PER BOEING 8100-9 DATED 01FEB2006 PER EO-4754A184.Feb 6, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon Miscellaneous StructureSDR P5CA0601439Structure · crackedNR 3 PYLON PRECOOLER CUTOUT CRACK AT FASTENER HOLE, LOWER AFT CORNER. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A184.Feb 6, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon Miscellaneous StructureSDR P5CA0601438Skin · corrodedWING CENTER SECTION UPPER SKIN CORROSION AT BS 1241 BETWEEN BBL 0 AND RBL 11.33. REPAIRED PER BOEING 8100-9 DATED 23JAN2006, PER EO-4757A238.Feb 6, 2006 · N534MC · Boeing 7472F6B · Wing, Plate/SkinSDR P5CA0601437Structure · crackedNR 4 PYLON PRECOOLER CUTOUT CRACKED AT LOWER AFT CORNER BY FASTENER HOLE. REPAIRED PER BOEING 8100-9 DATED 01FEB2006, PER EO-4754A184.Feb 6, 2006 · N534MC · Boeing 7472F6B · Nacelle/Pylon Miscellaneous StructureSDR P5CA0601424Odor · detectedDURING DESCENT HAD STRONG ELECTRICAL SMELL IN COCKPIT. PERFORMED INSPECTION OF COCKPIT, UNABLE TO FIND SOURCE OF ELECTRICAL SMELL.Dec 20, 2005 · N534MC · Boeing 7472F6B · Electrical Power SystemSDR P5CA0501418Tire · blownON TAKEOFF ROLL, CREW HEARD 2 LOUD BANGS AND LOST NR1 HYDRAULIC SYSTEM. FOUND 8 BLOWN TIRES, REPLACED 12 TIRES AND 3 BRAKES IAW MM 32-45-01 AND 32-45-15, ACCOMPLISHED CONDITIONAL INSPECTIONS IAW MM 05-51-10 AND 05-51-09.Nov 9, 2005 · N534MC · Boeing 7472F6B · TireSDR UIEA200500131Actuator · activatedFLT 8867 - WRI-JFK- AFTER TAKEOFF, GEAR RETRACTED WITH NO PROBLEM. THEN DURING CLIMB TO 5,000 FEET THE RED DOOR LIGHT ILLUMINATED WITH PRIMARY AND SECONDARY LIGHT ON ENGINEERS PANEL. USED FHB SECTION 3 TO BRING GEAR UP, RIGHT WING GEAR. VIBRATION WAS ALSO ESep 6, 2005 · N534MC · Boeing 7472F6B · Landing Gear Door ActuatorSDR UIEA200500078Servo Valve · leakingDURING CRUISE, NR 2 HYD QUANTITY WENT FROM 6.1 TO 2.2, 5 HOURS INTO FLIGHT. SUSPECT HYD LEAK. RAN PROCEDURES TO SHUTDOWN HYD SYSTEM NR 2 IAW FLIGHT HAND BOOK. REPLACED LOWER RUDDER POWER PACKAGE SERVO VALVE IAW MM. PRESSURIZED HYD SYSTEM IAW MM. LEAD CHECMay 20, 2005 · N534MC · Boeing 7472F6B · Hydraulic System, MainSDR UIEA200400204Switch · dirtyON TAKEOFF, WHEN GEAR RETRACTED, RED GEAR WARNING LIGHT CAME ON. F/E PANEL RT WING DOOR OPEN LIGHT WAS ON, BOTH PRIMARY AND ALT POSITIONS. DID FHB CHAPTER 3, GEAR HANDLE UP, LIGHT WHEN OUT. GEAR HANDLE OFF, LIGHTS ON AGAIN. LT HANDLE UP. INSPECTED AND FOUDec 23, 2004 · N534MC · Boeing 7472F6B · Landing Gear Position and WarningSDR UIEA200400187Precooler · crackedEK9971 ICN/ANC (ATB) FIRE WARNING: NR 4 ENGINE FIRE LIGHT CAME ON IN-FLIGHT NACELLE INDICATOR WAS ABOUT 3 TO 3.5 EGT APPROX 900 DEGREE HIGH STAGE BLEED LIGHT CAME ON JUST BEFORE FIRE LIGHT AND BELL. FIRE LIGHT CAME ON ABOUT FL 24.2 ENGINE S/D A/WITH FHB. INOct 31, 2004 · N534MC · Boeing 7472F6B · Engine Bleed Air SystemSDR UIEA200400177Latch · looseGROUND ABORT F/O'S FORWARD INSTRUMENT PANEL CAME OUT ON TAKEOFF ROLL. ABORTED AT 60 KNOTS. RESECURED F/O'S FORWARD INSTRUMENT PANEL IAW MM 31-10-00. ALL INSTRUMENT, OPS CHECK GOOD. (M)Sep 24, 2004 · N534MC · Boeing 7472F6B · Instrument PanelSDR P5CA0401180Relief Valve · malfunctionedNR 2 ENG INDICATE A FIRE AT 13:50- 6 MINUTES AFTER TAKEOFF. NACELLE TEMP IN THE FIRE ZONE. ENGINE FIRE PROCEDURE WAS ACCOMPLISHED, PULLED FIRE HANDLE, DID NOT DISCHARGE FIRE BOTTLES. OIL PRESSURE NORMAL. REMOVED AND REPLACED NR 2 ENG PRESSURE RELIEF VALVE Aug 26, 2004 · N534MC · Boeing 7472F6B · Pneumatic Distribution SystemSDR P5CA0401181Engine · malfunctionedDURING T/O AFTER ROTATION NR 2 ENG TEMP ROSE INTO THE YELLOW BAND & THE NACELLE TEMP WAS RISING RAPIDLY, THE THROTTLE WAS RETARDED & TEMP CAME DOWN. ENG FAILURE CHECK ACCOMPLISHED. NR 2 ENGINE REMOVED & REPLACED.Aug 26, 2004 · N534MC · Boeing 7472F6B · Engine (Turbine/Turboprop)SDR P5CA0401120Seal · leakingNR 1 ENGINE OIL QTY DROPPED FROM 5.3 GALLONS AFTER TAKEOFF, QTY DROPPED TO 1.25 GALLONS, OIL PRESSURE CLIMBED FROM 50 PSI TO 75 PSI & TEMP 110C. REMOVED AND REPLACED NR 1 ENGINE GENERATOR & GENERATOR SEAL, ALSO REPLACED NR 1 ENGINE CSD SEAL. OPS CHECK OK IAWJul 17, 2004 · N534MC · Boeing 7472F6B · AC Generator-AlternatorSDR P5CA0401108Manifold · rupturedNR 4 ENGINE 14TH STAGE MANIFOLD RUPTURE AT LEFT HAND SIDE CDP AIR SWIVEL JOINT. REPLACED 14TH STAGE MANIFOLD & CLAMP AS PER AMM 75-23-00. OPS CHECK & LEAK CHECK ACCOMPLISH AS PER AMM 71-00-00.Jun 25, 2004 · N534MC · Boeing 7472F6B · Engine Bleed Air SystemSDR P5CA0401091Speaker · failedTCAS FAILED IN FLIGHT. REPLACED TCAS SPEAKER, OPS CHECK OK MM 34-45-00.May 11, 2004 · N534MC · Boeing 7472F6B · Air Collision Avoidance SystemSDR P5CA0401088Connector · damagedAFTER PUSH BACK ON ENGINE START, NR 2 ENGINE EGT GAUGE HAD FLAG IN VIEW. T/S FOUND BROKEN PIN IN CONNECTOR, REPLACED, ALL INDICATIONS NORMAL.May 7, 2004 · N534MC · Boeing 7472F6B · Electrical ConnectorsSDR P5CA0401089Wire Harness · damagedDURING ENGINE NR 2 START AT GATE, CREW REPORT THAT ENGINE NR 2 EGT NO INDICATION & FLAG IN VIEW. TROUBLE SHOT, FOUND RT UPPER HARNESS AT FAULT. REMOVED AND REPLACE ENGINE HARNESS, ENGINE RUN OPS CHECK OK.May 6, 2004 · N534MC · Boeing 7472F6B · Engine Indicating System WiringSDR UIEA200400023Seat Track · crackedFORWARD CARGO COMPARTMENT SEAT TRACK CRACKED AT BS 576, APPROX RBL 48. REMOVED DAMAGED SEAT TRACK AS PER 747 SRM 51-30-01. INSTALLED SECTION OF SEAT TRACK IN FORWARD CARGO COMPARTMENT AT BS 576 RBL 48 P/N 65B601176-54. P/O NR 5075 LOT NR 01511488 REF 53-10-Feb 23, 2004 · N534MC · Boeing 7472F6B · Fuselage, Seat/Cargo Attach FittingsSDR UIEA200300030Computer · malfunctionedAIR TURNBACK, AT APPROXIMATELY 80-85 KNOTS ON TAKEOFF ROLL, HEADING FLAG ON CAPTAIN'S HSI AND FO'S RMI WITH FILGHT DIRECTOR WARNING LIGHT ON CAPTAINS SIDE. FLAG REMAINED IN FIEW ENTIRE FLIGHT. APPROXIMATELY 5 DEGREES DIFFERENCE IN NR 1 COMPASS VS NR 2 COMPASJun 27, 2003 · N535MC · Boeing 7472F6B · Attitude Gyro and Indicating SystemSDR UIEA200300029Coupler · failedDURING TAKEOFF ROLL, HEADING FLAG ON CAPTAIN'S HSI AND FO'S RMI. AIRCRAFT DIVERTED TO AMS, 23,000 KGS OF FUEL DUMPED. INSTALLED TEMP SPAR WIRE FROM D2206P TO DB105, WING TIP TO WIG DISC, AND REPLACED BOTH COMPASS COUPLER NR 1 AND FO'S RMI IAW MM 34-12-00, RMJun 25, 2003 · N535MC · Boeing 7472F6B · Magnetic CompassSDR UIEA200200058Frame · crackedDURING CURRENT C-CHECK, FOUND CRACKS EMANATING FROM THE LOWER OUTBOARD CORNER OF THE FRAME ACCESS HOLE CUTOUT AT BS 2040, 2080, 2100, 2120, 2160 AT LBL 16 WL 137. EACH FRAME CRACKED AT THE SAME LOCATION. CRACKS STOP DRILLED OR CUT AWAY AS REQUIRED. REPAIR DOct 24, 2002 · N535MC · Boeing 7472F6B · Fuselage Main, FrameSDR UIEA200200056Stringer · corrodedDURING CURRENT C-CHECK FOUND BS 2179 STRINGER 45L CORRODED ON OUTBOARD FLANGE. CUT AWAY CORRODED AREA. MANUFACTURED REPAIR FILLER, SHIMS AND REPAIR DOUBLERS SIMILAR TO SRM 53-10-03 FIG 1. (M)Oct 24, 2002 · N535MC · Boeing 7472F6B · Fuselage Main, Longeron/StringerSDR UIEA200200057Flap Track · corrodedDURING CURRENT "C" CHECK, FOUND NR 6 FLAP OUTBOARD BUSHING OF PIVOT FITTING LOOSE. DISASSEMBLY REVEALED CORROSION ON THE LEFT SIDE TO SIDE LOAD FITTING ON CONTACT AREAS, (NO CORROSION LEVEL DECLARED). REMOVED TRACK, ROUTED TO SHOP. MACHINED FLAP TRACK FLANGOct 24, 2002 · N535MC · Boeing 7472F6B · Trailing Edge FlapsSDR UIEA200200052Mec · inoperativeWHILE CLIMBING THROUGH 13,500 FEET AND ACCELERATING THROUGH 310 KTS, NR 4 ENGINE ROLLED BACK TO IDLE ACCOMPANIED BY A NOTICEABLE YAW. INSTRUMENTS CONFIRMED NR4 ENGINE HAD INDEED ROLLED BACK. AUTO THROTTLES WERE ENGAGED AT TIME. USING CLIMB POWER BUT NO THROOct 10, 2002 · N535MC · Boeing 7472F6B · Fuel Controlling SystemSDR UIEA02005Fitting · corrodedDURING CURRENT C-CHECK AT SIAEC WHILE PRFORMING INSPECTION AND REWORK OF THE RIGHT BS 1480 LONGERON AREA PER SB 747-53A2390 FOUND NR 5 HOLE CORRODED AT BS 1480 RIGHT UPPER LONGERON BULKHEAD FITTING. REAMED HOLE TO .750 INCLUDING INSURANCE CUT. FABRICATED REPFeb 4, 2002 · N534MC · Boeing 7472F6B · Fuselage Main, Attach FittingsSDR UIEA02004Bulkhead · crackedDURING CURRENT C-CHECK AT SIAEC INSPECTION OF BS 2484 UPPER BULKHEAD STRUCTURE DISCOVERED THE WEB CRACKED AT STRINGER 15L LBL 45 WL 287.03. REMOVED STIFFENER 65B02571-153. TRIMMED OUT CRACK IN WEB AREA. DYE CHECKED AREA. NO FINDINGS. FABRICATED REPAIR DOUFeb 4, 2002 · N534MC · Boeing 7472F6B · Fuselage Main, BulkheadSDR UIEA02003Attach Fitting · scoredDURING CURRENT C-CHECK AT SIAEC WHILE PERFORMING TERMINATING ACTION PER ATLAS AIR EO 4757A082, NR 4 PYLON LOWER WING DIAGONAL BRACE ATTACH FITTING, TAPER LOCATION INSTALLATION ' FOUND THE LAST THREE FASTENER HOLES SCORED. POSITIONS ARE ONE EACH AT INBOARD 2NDFeb 4, 2002 · N534MC · Boeing 7472F6B · Nacelle/Pylon, Attach FittingsSDR 2002F00205Spar · crackedDURING CURRENT C-CHECK AT SIAC INSPECTION OF THE RT L/E NR 15 KRUEGER FLAP, A CRACK WAS DISCOVERED IN THE FRONT SPAR INBOARD END OF THE DEVICE (65B39252-2). (M)Feb 4, 2002 · N534MC · Boeing 7472F6B · Wing SparSDR UIEA01108Wire · shortedON TAKEOFF ROLL, FIRE DETECTION MASTER CAUTION LIGHT FLICKERED. NR 2A FIRE LOOP NACELLE JUMPED FROM 1-5. ACCOMPLISHED PNEUMATIC LEAK CHECK. NO LEAKS FOUND. NR 2 ENGINE FIRE DETECTION LOOP 'A' FAILED OPERATIONAL TEST. WIRE NR W3296-2W10-18R FOUND SHORTED TDec 28, 2001 · N534MC · Boeing 7472F6B · Fire Protection System WiringSDR UIEA01005Frame · crackedDURING THE CURRENT A-CHECK, LOWER LOBE FORWARD CARGO DOOR FRAME BS 560 AT STRINGER 38R WAS FOUND CRACKED. CUTOUT SECTION OF CRACKED AREA FROM S37 AND S39. MANUFACTURED FILLER, REPAIR ANGLES, DOUBLERS AND ASSOCIATED FILLERS. INSTALLED IAW ATLAS EO 4753A125. Mar 6, 2001 · N535MC · Boeing 7472F6B · Fuselage Main, FrameSDR UIEA0047Acm · failedFLT 56 - UIO-GYE - PRIOR TO DEPARTURE, NR 3 ACM FAILED ALLOWING SMOKE TO ENTER THE MAIN CARGO DECK AND THE FLIGHT DECK. AIRCONDITIONING SYSTEM WAS DEFERRED PER THE DDPG. ON 10/18/2000 MIA MAINTENANCE REPLAED ACM, OPERATIONAL CHECK SATISFACTORY. (M)Oct 12, 2000 · N535MC · Boeing 7472F6B · Cabin Cooling SystemSDR UIEA00034Skin Panel · damagedDURING INSPECTION OF LOWER WING SKIN, SKIN FOUND DAMAGED AT STRINGER S-3C AND STRINGER S-40C BETWEEN LBL 40 AND LBL 50. SKIN DAMAGED BLENDED OUT, MEASURED, HOLES E/C CHECKED, SKIN FLAT PEENDED AND ALODINED. A 2024-T3 REINFORCEMENT DOUBLER INSTALLED. PER ATLAug 21, 2000 · N534MC · Boeing 7472F6B · Wing, Plate/SkinSDR UIEA00035Blanket · burnedDURING THE INSPECTION OF STRUCTURE BETWEEN STATION 2220 THROUGH 2360, THE INSULATION BLANKETS ON THE APU PNEUMATIC SUPPLY DUCT WERE FOUND WITH BURNED HOLES. THE P/N OF THE DAMAGED BLANKETS WERE CHECKED FOR CORRECT APPLICATION. THE CORRECT P/N WAS INSTALLED. Aug 21, 2000 · N534MC · Boeing 7472F6B · APU Bleed Air SystemSDR UIEA0018Duct · separatedFLT 7150 - GYE - ON TAKEOFF AT 400 AGL, NR 1 ENGINE EXPLODED AND HAD AIRCRAFT VIBRATION. LEVELED AIRCRAFT AT 817 FEET. ADVISED TOWER HAD AN ENGINE FIRE AND DECLARED AN EMERGENCY. DUMPED 30K FUEL AND RETURNED TO GYE. ON ARRIVAL, DETERMINED THAT NR 1 ENGINE Aug 18, 2000 · N534MC · Boeing 7472F6B · Engine (Turbine/Turboprop)SDR UIEA0001Line · crackedFLT 51 - NR 2 ENGINE FIRE WARNING LIGHT AND BELL AT 3500 FEET. ACCOMPLISHED ENGINE FIRE CHECKLIST, SHUTDOWN ENGINE. LIGHT IN FIRE HANDLE WENT OUT IMMEDIATELY. DID NOT DISCHARGE FIRE BOTTLES AND DID NOT DUMP FUEL. LANDING WAS UNEVENTFUL. FOUND CRACKED/LEAKJan 20, 2000 · N534MC · Boeing 7472F6B · Engine Bleed Air SystemSDR UIEA9997Valve · stuckFLT GT57 - NR 2 ENGINE FIRE WARNING ILLUMINATED AFTER TAKEOFF. IT OCCURRED DURING CLIMB WITH CLIMB POWER SET. BOTH NACELLE TEMPS WERE 8.5. ENGINE SECURE DIAW FHB. DECLARE EMERGENCY AND JETTISONED 14 KGS OF FUEL. LANDING WAS UNEVENTFUL. FOUND NR 2 ENGINE Dec 14, 1999 · N535MC · Boeing 7472F6B · Compressor Bleed ControlSDR TWRA9966Reg Valve · inoperativeDURING TAKEOFF AT 142 KNOTS AND PRIOR TO V1 NR 4 ENGNE FIRE WARNING LIGHT AND BELL CAME ON CAPTAIN ABORTED TAKEOFF AND BOTH BELL AND LIGHT WENT OUT AS CAPTAIN INDICATED THE ABORT. REMOVED AND REPLACED NR 4 OVER PRESSURE VALVE AND NR 4 ENGINE BLEED REGULATOR VOct 21, 1999 · N623FF · Boeing 7472F6B · Pneumatic Distribution SystemSDR 99ZZZM774Relief Vlv · inoperativeDURING TAKEOFF AT 142 KNOTS AND PRIOR TO V1 NR 4 ENGNE FIRE WARNING LIGHT AND BELL CAME ON CAPTAIN ABORTED TAKEOFF AND BOTH BELL AND LIGHT WENT OUT AS CAPTAIN INDICATED THE ABORT. REMOVED AND REPLACED NR 4 OVER PRESSURE VALVE AND NR 4 ENGINE BLEED REGULATOR VOct 21, 1999 · N623FF · Boeing 7472F6B · Pneumatic Distribution SystemSDR UIEA9933Bulkhead Splice · crackedCRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 RIGHT AND NR 23 RIGHT. HOLE NR 11 RIGHT, INSTALLED SEPRATE BUSHINGS IN EACH PART PER SB 747-53A2390 FIG 14. HOLE NR 23 RIGHT, REPAIRED OVERSIZE HOLE IN WEB SPLICE PLATE BULKHEAD. CHORD AND WEB PER BUSHING REPAIR Jun 21, 1999 · N534MC · Boeing 7472F6B · Fuselage Main, BulkheadSDR UIEA9932Builkhead Splice · crackedCRACKS FOUND ON WEB SPLICE PLATE HOLES NR 11 LEFT AND NR 21 LEFT. HOLES NR 11 LEFT, INSTALLED SEPARATE BUSHINGS IN EACH PART PER SB 747-53A2390 FIG 14. HOLE NR 21 LEFT, REPAIRED OVERSIZE HOLE IN BULKHEAD. CHORD AND WEB PER BUSHING REPAIR PER SB 747-53A2390 Jun 21, 1999 · N534MC · Boeing 7472F6B · Fuselage Main, BulkheadSDR TWRA9854Fire Loop · malfunctionedDURING CRUISE NR 1 ENGINE 'B' LOOP INDICATED FIRE AND FAULT, NACELLE TEMP FLUX OFF SCALE HIGH AND LOW. NR 1 ENGINE SHUT DOWN, FIRE BOTTLE 'A' DISCHARGED. REPLACED FIRE BOTTLE 'A' PER MM 26-21-03 PAGE 401. CONFIRMED FALSE FIRE WARNING 'B' LOOP. DEFERRED PERNov 15, 1998 · N623FF · Boeing 7472F6B · Fire DetectionSDR TWRA9839Clamp · looseNR 1 ENGINE FIRE WARNING MOMENTARILY INDICATED ON CLIMB-OUT FROM TLV, RETARDED THRUST LEVER TO IDLE BEFORE ANY ACTION TAKEN. LIGHT/HORN EXTINGUISHED, OTHER INDICATIONS NORMAL. 'A' LOOP DROPPED TO NORMAL. 'B' LOOP CONTINUED TO RUN ABOVE 'A' LOOP. FOUND PNEUJul 19, 1998 · N623FF · Boeing 7472F6B · Pneumatic Distribution SystemSDR TWRA9837Clamp · looseFLT 92 - SJU-MIA - ON CLIMB, NR 1 ENGINE FIRE SWITCH ILLUMINATED AND FIRE BELLSOUNDED. ENGINE SHUT DOWN. WHEN START LEVER WAS CUT OFF THE FIRE SWITCH LIGHT STOPPED ILLUMINATION. NACELLE TEMP DROPPED. FIRE BOTTLE WAS NOT DISCHARGED. AIR TURN BACK TO SJU. Jul 12, 1998 · N623FF · Boeing 7472F6B · Pneumatic Distribution SystemSDR 98ZZZX2078Bracket · brokenORY/JFK - FLT 37 - FLIGHT EXPERIENCED TURBULENCE. ON ACOMPLISHMENT OF CONDITIONAL INSPECTION, FOUND SEAT BELTS ATTACH POINT BROKEN AT 55 D & E. REPLACED SAFETY BELTS BRACKET ASSY. OK FOR SERVICE. (X)Apr 18, 1998 · N623FF · Boeing 7472F6B · Passenger Compartment EquipmentSDR TWRA9817Upper Gate · crackedNR 3L ME DOOR, UPPER GATE IS CRACKED AT CENTER. REMOVED AND REPLACED NR 3 ME DOOR UPPER GATE PER MM 52-11-01. LEAK CHECK OK. (X)Mar 26, 1998 · N623FF · Boeing 7472F6B · Electrical/Electronic Compartment Doors
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