Boeing 737-214

Service difficulty reports · 209

Newest first. General aviation reporting is voluntary.

Query with SQL
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 = '737214'
  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 ZZDA5321597Floorbeam · corrodedDURING C-CHECK AT AERO CORP, AFT LAVATORY FLOOR BEAM UPPER CHORD BS 1006 HAS CORROSION AT LBL 9. FABRICATED DOUBLER FROM 7075 T6 .071 INCH 10.50 INCHES, 1.0625 INCH, AND 10.0625 INCHES BY 1.0625 INCHES. FABRICATED FILLER FROM BAC 1505-100817, 44 INCHES BY 3 Sep 4, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR AADA5323597Support · corrodedDURING C-CHECK AT AERO CORP, FOUND AFT LAVATORY FLOOR SUPPORT BEAM BS 986.5 - BS 1016 LBL 20 DIAGONALLY TO LBL 4 CORRODED BEYOND LIMITS. REMOVED FLOOR SUPPORT FROM STA 986.5 - STA 1016. CORROSION REMOVAL BEYOND LIMITS PER 737 MM 51-10-6 AND MM 51-10-2. FABRSep 4, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR 98ZZZX108Skin · corrodedDURING C-CHECK AT AERO CORP, FOUND E/E BAY SKIN HAS CORROSION ON INTERNAL SURFACE, UNDER DOUBLERS, STRINGERS, AND CLIPS FROM LT TO RT STA 259.5 - STA 360. REMOVED AND REPLACED SKINS AT STA 259.5 - STA 360, BL ZERO, STR 24L AND 24R IAW B 373 SRM 51-30-2 AND BASep 4, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR ZZDA5317997Skin · corrodedDURING C-CHECK, LT FS 967 FOUND CORROSION UNDER FASTENER HEAD AT STR 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. FABRICATED FILLER FROM 2024 T3 .071 INCH 1.1250 INCHES BY 1 INCH. FABRICATED REPAIR DOUBLER FROM 2024 T3 .090 INCH 11.50 INCHES BY 6 INCHES. INSTALSep 2, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR 97ZZZM1052Skin · corrodedDURING C-CHECK, LEFT FUSELAGE STATION 967 CORROSION UNDER FASTENER HEAD AT STRINGER 19L OUT OF LIMITS IAW B 737 SRM 53-10-1. (M)Sep 2, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR ZZDA5322997Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR SUPPORT AT LBL 12 IAW B 737 51-30-2 AND FABRICATED NEW FLOOR SUPPORT FROM 60-8004 15 INCHES BY 2 INCHES IAW B 737 SRM 51-30-2. Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5322897Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM BS 328 HAS CORROSION ON UPPER CHORD FROM RBL 48 TO LBL 12, FOUND TO BE BEYOND LIMITS. REMOVED CORROSION ON FLOOR BEAM PER 737 SRM 51-20-6. REMOVED OVER 20 PERCENT MATERIAL LOSS, OUT OF LIMITS PER Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5322797Floor Beam · corrodedPASSENGER CABIN FLOOR BEAM BS 294 HAS CORROSION ON UPPER CHORD FROM RBL 12 TO RBL 50. REMOVED CORROSION FROM THE UPPER CHORD FLOOR BEAM IAW B737 SRM 51-10-1. MATERIAL LOSS MORE THAN 50 PERCENT OUT OF LIMITS IAW SRM 53-10-1. FABRICATED NEW UPPER CHORD AND 10Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5321797Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND PASSENGER CABIN FLOOR BEAM LONGITUDINAL SUPPORT AT LBL 12 HAS CORROSION AT BS 310. REMOVED FLOOR BEAM AT LBL 12 IAW B 737 SRM 51-30-2. FABRICATED NEW FLOOR SUPPORT IAW B 737 SRM 53-40-4. TREATED AND PRIMED IAW B 737 SRM 51Aug 30, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5323797Beam · crackedDURING C-CHECK AT AERO CORP, BS 675 TRANSVERSE BEAM RBL 1 CRACKED .75 INCH. INSTALLED REPAIR AT STA 675 BL ZERO, AND INSTALLED PREVENTIVE MODS AT STA 685 BL ZERO AND BL ZERO FLOOR BEAM IAW SB 737-57-1106 (675 AND 685 TRANSVERSE BEAMS). (X)Aug 28, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5323697Skin · corrodedDURING C-CHECK AT AERO CORP, FOUND AFT LEFT FUSELAGE PULLED FASTENERS, STA 767 BETWEEN STR 24L AND STR 25L AND FORWARD SIDE STA 767 OR STR 25L, CORROSION BEYOND LIMITS. REMOVED FASTENERS AND CORROSION. MATERIAL LOSS OUT OF LIMITS. CUT OUT SE CTION OF THE SKIAug 28, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR ZZDA5323297Skin · corrodedDURING C-CHECK AT AERO CORP, FOUND AFT FUSELAGE HAS CORROSION AT CIRCUMFERENTIAL SKIN BUTT JOINT STA 1016, STR 26R WITH LAP SEAM LIFTING AT STR 28L, FOUND TO BE BEYOND LIMITS. REMOVED FASTENERS, REMOVED CORROSION, MATERIAL LOSS WITHIN LIMITS FROM STR 27L TO SAug 28, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR ZZDA5327597Floor Beam · corrodedDURING C-CHECK AT AERO CORP, RIGHT HAND FLOOR BEAM 967, BL ZERO, TO FUSELAGE SKIN FOUND CORRODED. FABRICATED 2 SUPPORT ANGLES FROM 7075 0 .070 INCH 18 INCHES AND 16 INCHES. FABRICATED 2 SUPPORT ANGLES FROM 7075 0 .080 INCH 18 INCHES AND 16 INCHES IAW 53-10-9Aug 27, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5322697Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND INTERIOR FUSELAGE, RT SIDE FLOOR BEAM, BS 947, BL ZERO TO FUSELAGE SKIN CORRODED. FOUND TO BE BEYOND LIMITS. REMOVED CORROSION IAW SRM 51-30-2, MATERIAL LOSS BEYOND LIMITS IAW B 737 SRM 53-10-1. CUT OUT SECTION OF UPPER CHAug 27, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5322597Floor Beam · corrodedDURING CHECK AT AERO CORP, FOUND BS 1016, BL ZERO TO FUSELAGE FLOOR BEAM CORRODED. CUT OUT CORRODED AREA AND FABRICATED THE REPAIR. INSTALLED REPAIR. BLENDED CORROSION, MATERIAL LOSS BEYOND LIMITS IAW B 737 53-10-1. CUT OUT AREA BEYOND LIMITS AND INSTALLEDAug 27, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5723997Skin · corrodedDURING C-CHECK AT AERO CORP, LEFT WING T/E OUTBOARD FLAP, MID-FLAP LOWER EXTERNAL SKIN CORRODED AT T/E WS 342. REMOVED CORROSION IAW SRM 51-10-8. CORROSION REMOVAL OUT OF LIMITS AT EDGE OF THE PANEL IAW SRM 53-10-1. BLENDED EDGE OF PANEL .080 INCH LESS THAN Aug 26, 1997 · N460AT · Boeing 737214 · Trailing Edge FlapsSDR ZZDA5721397Skin · corrodedDURING C-CHECK AT AERO CORP, FOUND LEFT WING OUTBOARD TE FLAP, MID-FLAP UPPER EXTERNAL SKIN CORRODED WS 300 TO WS 320. REMOVED CORROSION FROM MID-FLAP PER 737 SRM 51-10-6 FIG 20. MATERIAL LOSS WAS .010 INCH OUT OF LIMITS PER 737 SRM 57-50-1 BONDED FILLER REPAug 26, 1997 · N460AT · Boeing 737214 · Trailing Edge FlapsSDR ZZDA5524097Panel · separatingDURING C-CHECK AT AERO CORP, RT HORIZONTAL STABILIZER INBOARD BALANCE PANEL BAY HAS A METAL BOND PANEL ASSY SEPARATING (OUTBOARD PANEL). REMOVED FASTENERS, STOP-DRILLED CRACK IAW B 737 SRM 51-10-1, FABRICATED DOUBLER REPAIR FROM 2024 T3 .016 INCH, DIMENSIONS Aug 26, 1997 · N460AT · Boeing 737214 · Horizontal Stabilizer, Plate/SkinSDR ZZDA5327497Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FLOOR BEAM CHORD FS 312 QL 208.1 LBL 20 TO RBL 20 IS EXFOLIATED. FABRICATED FLOOR BEAM FROM 7075T6 56 INCHES BY 2 INCHES. FABRICATED ANGLE SPLICES FROM 7075 0 .063 INCH, HEAT TREATED TO 7075 T6 8.50 INCHES BY 2 INCHES, 12 INCHES Aug 26, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5327397Support · corrodedDURING C-CHECK AT AERO CORP, FOUND FLOOR SUPPORT AT FS 328-344 WL 208.1 RBL 20 IS EXFOLIATED. FABRICATED FLOOR SUPPORT FROM 7075T6 15.50 INCHES BY 2 INCHES BY 1.1250 INCH IAW B 737 SRM 53-10-2. INSTALLED IAW B 737 SRM 51-30-2. (X)Aug 26, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5327297Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND FLOOR BEAM UPPER CHORD FS 344 WL 208.1 LBL 20 IS EXFOLIATED. FABARICATED T-ANGLE FROM AND10136-2401 50 INCHES BY 2.50 INCHES IAW B 737 SRM 53-10-9. FABRICATED SPLICE ANGLES FROM 7075 0 .083 INCH (8) 7 INCHES BY 2 INCHES ANDAug 26, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5327197Support · corrodedDURING C-CHECK AT AERO CORP, FOUND FOUND FLOOR BEAM SUPPORT AT FS 328 - FS 344 WL 208.1 LBL 20 EXFOLIATED. FABRICATED FLOOR SUPPORT FROM 7075 T6 15.50 INCHES BY 1 INCH BY 2.25 INCHES IAW B737 SRM 53-10-2, FIG 7. INSTALLED IAW B 737 SRM 53-10-2. (X)Aug 26, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5327797Chord · damagedDURING C-CHECK AT AERO CORP, REMOVED AND REPLACED DAMAGED BS 727 LT LOWER CHORD AT STR 18A. REMOVED AND REPLACED WITH NEW CHORD IAW B 737 SB 53-1088. (X)Aug 25, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5324197Floor Beam · corrodedDURING C-CHECK AT AERO CORP, FOUND HOLE CORRODED IN FLOOR BEAM/FRAME AT STA 986.5 AFT SIDE 24 INCHES OF CENTER LINE. REMOVED FLOOR BOARDS FOR ACCESS, MECHANIC REMOVED THE CORROSION FROM FLOOR BEAM IAW B 737 SRM 51-10-6. MATERIAL LOSS OF .079 INCH, OUT OF LIMAug 25, 1997 · N460AT · Boeing 737214 · Fuselage Main, Floor BeamSDR ZZDA5322397Strap · corrodedDURING C-CHECK AT AERO CORP, FOUND AFT CARGO PIT FORWARD CENTER FLOORBOARD ATTACHMENT STRAP HAS CORROSION ON UPPER AND LOWER SURFACES AT STA 750. REMOVED CORROSION OF STRAP. MATERIAL LOSS MORE THAN 50 PERCENT. FABRICATED NEW STRAP IAW B 737 SRM 53-20-0. FAAug 25, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5322297Strap · corrodedDURING C-CHECK AT AERO CORP BS 858, FOUND AFT CARGO TIE-DOWN TRACK SUPPORT STRAP CORRODED BEYOND LIMITS. REMOVED STRAP IAW B 737 SRM 51-30-2. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW B 737 SRM 53-30-1. FABRICATED NEW PART OUT OF 7075 T6 .080 INCH, DAug 25, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5326997Strap · corrodedDURING C-CHECK AT AERO CORP, BS 492, ONE STRAP ASSY CORRODED AT AFT FRAME OF FWD CARGO DOOR CUT-OUT, STR 25R. FABRICATED NEW STRAP FROM 2024 T3 .080 INCH 32.75 INCHES BY 1 INCH BY 4.25 INCHES IAW B 737 SRM 51-4-2. INSTALLED IAW B 737 SRM 51-3-2. (X)Aug 23, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5321297Frame · corrodedDURING C-CHECK AT AERO CORP, FOUND CORROSION ON INSIDE ON FORWARD PIT DOOR FRAME TOP CENTER. REMOVED CORROSION MATERIAL, LOSS IN EXCESS OF 20 PERCENT, OUT OF LIMITS IAW B 737 SRM 51-10-6 AND SRM 53-10-1. BLENDED OUT LIP PER E.O. 04427 GUIDELINES, ALODINED AAug 23, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR ZZDA5317697Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN EXTERIOR BS 440, FORWARD CARGO COMPARTMENT CUT-OUT SKIN HAS INTERGRANULAR CORROSION, BULGES, AND PULLING RIVETS BETWEEN STR 20 AND STR 23, RT SIDE. FABRICATED FILLER AND DOUBLER FROM 2024 T3 .050 INCH, .040 INCH 28.5 INCHESAug 23, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR 97ZZZM1051Skin · corrodedDURING C-CHECK, FOUND FUSELAGE SKIN EXTERIOR BS 440, FWD CARGO COMPARTMENT CUTOUT SKIN HAS I/G CORROSION, BULGES AND PULLING RIVETS BETWEEN STRINGER 20 AND STRINGER 23 RT SIDE.Aug 23, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR ZZDA5327897Spar · crackedDURING C-CHECK AT AERO CORP, ACCOMPLISHED AD 90-06-02, REPLACED THE LT WING CRACKED FRONT SPAR UPPER CHORD BETWEEN FS 97 TO FS 225 IAW SB 737-57A1081 (R10) PART III OR IV OF ACCOMPLISHMENT INSTRUCTIONS. REMOVED CRACKED LT UPPER WING SPAR CHORD FROM STA 90 - SAug 15, 1997 · N460AT · Boeing 737214 · Wing SparSDR BJNA970702Cover · missingEMERGENCY EXIT LIGHT COVER MISSING ON SIDEWALL AT ROW 10 ABC. REMOVED AND REPLACED EMERGENCY EXIT LIGHT COVER ASSEMBLY PER BS WPM. OPS CHECK GOOD. (X)Jul 22, 1997 · N457TM · Boeing 737214 · Emergency LightingSDR BJNA970701Power Supply · inoperativeFORWARD SECTION OF EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND REPAIRED POWER SUPPLY POWER BMM 33-51-51. (X)Jul 11, 1997 · N457TM · Boeing 737214 · Emergency LightingSDR ZZDA3310197Bulb · missingDURING GATE WALK-AROUND, FOUND E-PATCH LIGHTING MISSING ONE BULB AND TWO EACH RED LENSES AT OVERWING EXIT LIGHT. REPLACED BULB AND TWO EACH RED LENSES AT OVERWING EMERGENCY EXIT. REF. B737 MM 3351-00 AND BR 2013-7372AQ REV G. FUNCTIONALLY CHECK NORMAL. REJun 3, 1997 · N460AT · Boeing 737214 · Emergency LightingSDR 97ZZZX2976Lens · missingDURING GATE WALK-AROUND, FOUND E-PATCH LIGHTING MISSING ONE BULB AND TWO EACH RED LENSES AT OVERWING EXIT LIGHT. REPLACED BULB AND TWO EACH RED LENSES AT OVERWING EMERGENCY EXIT. REF. B737 MM 3351-00 AND BR 2013-7372AQ REV G. FUNCTIONALLY CHECK NORMAL. REJun 3, 1997 · N460AT · Boeing 737214 · Emergency LightingSDR BJNA970602Battery Pack · dischargedL-2 DOOR SLIDE EMERGENCY LIGHT BATTERY LOW VOLTAGE. REPLACED BATTERY PACK L-2 DOOR SLIDE PER BMM. TESTS NORMAL. (M)May 30, 1997 · N457TM · Boeing 737214 · Emergency LightingSDR BJNA970601Battery Pack · dischargedL-1 DOOR SLIDE EMERGENCY LIGHT BATTERY LOW VOLTAGE. REPLACED BATTERY PACK L-1 DOOR SLIDE PER BMM. TESTS NORMAL. (M)May 30, 1997 · N457TM · Boeing 737214 · Emergency LightingSDR BJNA97602Wheel · damagedLEFT LANDING GEAR CHATTERING. UPON INSPECTION, FOUND NR 2 MAIN WHEEL ASSY DAMAGED. REMOVED AND REPLACED NR 2 WHEEL ASSY EPR BMM 32-45-11. (X)May 23, 1997 · N457TM · Boeing 737214 · Wheel/Ski/FloatSDR BJNA97601Brake · damagedLEFT LANDING GEAR CHATTERING. FOUND NR 2 BRAKE ASSY DAMAGED. REMOVED AND REPLACED NR 2 BRAKE ASSY PER 32-45-41. (X)May 23, 1997 · N457TM · Boeing 737214 · Landing Gear Brake SystemSDR BJNA970403Wire · brokenROW 10 A, B, C, EMERGENCY EXIT WIRING BROKEN. SPLICED WIRES PE BSWPM. OPS CHECK GOOD. (M)Apr 23, 1997 · N457TM · Boeing 737214 · Light System WiringSDR CALA9700350Hyd Line · leakingTHE COCKPIT AND CABIN FILLED WITH SMOKE AFTER TAKEOFF FROM EWR. THE AIR CONDITIONING SMOKE CHECKLIST WAS ACCOMPLISHED AND A RETURN TO EWR WAS BEGUN. THE CREW NOTED A HYDRAULIC SYSTEM LOSS ON FINAL APPROACH. THE A/C LANDED WITHOUT INCIDENT. MX FOUND THE NR Mar 17, 1997 · N14239 · Boeing 737214 · Hydraulic System, MainSDR 97ZZZM481Frame · corrodedDURING A SCHEDULED INSPECTION AT AERO CORP FL, THE FOLLOWING WAS FOUND, AFT FUSELAGE AT BS 950 FRAME STRINGER 21 LEFT HAS LEVEL 2 CORROSION TO STR 20 LEFT. FORMED FRAME AND SUPPORT ANGLE OUT OF 7075 T6.071 5.75 INCH BY 1 INCH BY 1 INCH IAW SRM 51-40-3. INSTAMar 5, 1997 · N460AT · Boeing 737214 · Fuselage Main, FrameSDR 97ZZZM479Skin · crackedDURING SCHEDULED INSPECTION AT AERO CORP FL, THE FOLLOWING WAS FOUND, STATION 827 LEFT AFT LOWER FUSELAGE SKIN CRACKED RIVET TO RIVET 1.75 INCH LONG IN LENGTH STRINGER 25. FABRICATED DOUBLER 14 INCH BY 8 INCH OUT OF 2024 T3.071 AND FILLER 3.70 INCH BY 2.20 INMar 3, 1997 · N460AT · Boeing 737214 · Fuselage Main, Plate/SkinSDR 97ZZZM480Stiffener · crackedDURING A SCHEDULED INSPECTION AT AERO CORP FL, THE FOLLOWING WAS FOUND, FORWARD PIT AFT BLKHEAD, UPPER FORWARD CENTER FUEL TANK 'U' STIFFENER IS CRACKED 4.5 INCH AT FS 540, RBL 25. FABRICATED NEW STIFFENER FROM 7178-T611 'U' CHANNEL 54 INCH BY 2.5 INCH BY 1 IMar 2, 1997 · N460AT · Boeing 737214 · Fuselage Miscellaneous StructureSDR BJNA97021Bleed Valve · inoperativeLOSS OF CABIN PRESSURE, UNABLE TO MAINTAIN ALTITUDE IN MANUAL MODE. DEPLOYED OXYGEN MASKS. FOUND NR 2 ENGINE BLEED VALVE STUCK IN THE CLOSED POSITION. REMOVED AND REPLACED VALVE IAW BOEING MM 36-11-11. (M)Feb 2, 1997 · N457TM · Boeing 737214 · Compressor Bleed ValveSDR 98ZZZM173Seal · leakingDURING FLT 920 FROM CMO, THE NR 2 FUEL QTY INOP. THE NR 2 FUEL QTY WAS ALREADY ON MEL. THE AIRCRAFT RETURNED TO MCO. REMOVED WATER FROM THE FUEL TANKS. REMOVED AND REPLACED THE NR 1 AND NR 2 FUEL CAP SEALS. PERFORMED FUEL QTY CHECK USING TESTER ON BOTH NR Jan 9, 1997 · N460AT · Boeing 737214 · Fuel StorageSDR BJNA961201Trim Tab · loose screwsPRECAUTIONARY LANDING AT OMA FOR IN FLIGHT VIBRATION. FOUND LOOSE SCREWS RIGHT ELEVATOR TRIM TAB P/N 657379945 SECURED SCREWS PER CASINO EXPRESS MM REFERENCE 27-31-31. AIRCRAFT RELEASED BACK TO SERVICE. INSPECTED WORK IN EKO OF LOOSE SCREWS, INSTALLATION CHDec 14, 1996 · N457TM · Boeing 737214 · Elevator Tab Control SystemSDR 97ZZZM198Panel · malfunctionedFLT 570 - MCO-ROC - NR 1 CSD LOW OIL PRESS LIGHT INTERMITTENT AND DRIVE TEMP FLUCTUATES INTO THE CAUTION RANGE, DISCONNECTED THE CSD. REPLACED P-5 CONTROL PANEL AS WELL AS NR 1 CSD OIL IN TEMP BULB IAW WITH B737 MM 24-11-0. OPERATIONAL CHECK ACCOMPLISHED SATDec 11, 1996 · N460AT · Boeing 737214 · AC Indicating SystemSDR BJNA9611110Mount · corrodedDURING SCHEDULED INSPECTION AT AERO CORP IN LAKE CITY, FL, FOUND THE NR 1 ENGINE FORWARD MOUNTS MISSING SUPPAGE MARKS FOR ELASOMETRIC MATERIAL. REMOVED ISOLATORS, REMOVED CORROSION. SHOT PEENED AND REWORKED AREA. ULTRASONICALLY INSPECTED, APPLIED PRIMER, ANNov 22, 1996 · N457TM · Boeing 737214 · Engine Mount SectionSDR BJNA961105Spar · crackedUPON A SCHEDULED INSPECTION AT AERO CORP, THE LEFT INBOARD MID FLAP FRONT SPAR WAS FOUND WITH A GOUGE AND A 1.5 INCH CRACK AT THE NR 7 RIB FROM THE INBOARD END. (M)Nov 19, 1996 · N457TM · Boeing 737214 · Trailing Edge Flaps
Back to Boeing 737-214