Boeing 737-277

Service difficulty reports · 1,584

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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 = '737277'
  ORDER BY difficulty_date DESC"

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SDR AWXA9900171Skin · crackedFUSELAGE SKIN CRACK ABOVE WTB FAIRING AT STRINGER 17 BETWEEN 727A AND 727, REPAIRED.Apr 28, 1999 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900170Skin · crackedFUSELAGE SKIN CRACK ABOVE WTB AT STRINGER 17, FWD OF STATION 747, REPAIRED.Apr 28, 1999 · N184AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900161Fluid · lossHYD FLUID LOSS. LOSS OF 'A' SYS HYD QUANITY INFLIGHT. (DROPPED TO APPR .75 GAL) ACCOMPLISHED LOSS OF SYS 'A' CHECKLIST DIVERTED TO LAS. SERVICE HYD SYS WITH 6 QUARTS. RAN ELEC PUMPS, INTERCONNECT OPEN AND CLOSED, NO LEAKS FOUND. RAN ENGINES WITH PUMPS ON. Apr 24, 1999 · N188AW · Boeing 737277 · Hydraulic System, MainSDR AWXA9900159Skin · crackedIN MAINTENANCE, FOUND SKIN CRACK, FUSELAGE LT SIDE AFT OF UPPER WING TO BODY FAIRING, 1 INCH LONG. VERIFIED BY HFEC AND MARKED ENDS. REPAIRED WITH BLIND RIVET REPAIR PER SRM 53-30-3, FIG 6, INSPECT BLIND RIVET REPAIR AT 3000 FLT CYC THEN 2500 FLT CYC THERE AApr 24, 1999 · N185AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900160Line · leakedAIR TURN BACK, HYD FLUID LOSS. AIRCRAFT TOOK OFF FROM PHOENIX AND LOST HYDRAULIC FLUID IN THE 'A' SYSTEM. AIRCRAFT AIR RETURNED TO PHX. 'A' SYS AILERON PRESSURE LINE FOUND TO BE LEAKING. REMOVED AND REPLACED AILERON PRESSURE LINE OPS CK GOOD.Apr 23, 1999 · N188AW · Boeing 737277 · Hydraulic System, MainSDR AWXA9900175Stringer · corrodedCORROSION OUT OF LIMITS ON STRINGER 27L AT FRAME 967. REMOVED STRINGER 27L AT STA 967 TO 1016. FABRICATED 3 EA STRINGERS 6 EA SPLICE ANGLES 2 EA N CHANNELS. TREATED PRIMED AND INSTALLED NEW PARTS PER SRM 51-30-2, 51-10-2, 57-30-3 FIG 1 AND TORQUED 2 EA STRIApr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA9900163Clip · crackedIN MAINTENANCE, FOUND CRACKS, STRINGER CLIPS AT THE FOLLOWING LOCATIONS ARE CRACKED CABIN FS 947.6 STR 25R, FS 787 STR 1, FS 767 STR 5L, 6R, 6L, 7R, FS 727A STR 4L, 7R, FS 727B STR 5R, FS 688 STR L2, FS 639 STR L2. REMOVED AND REPLACED STRINGER CLIPS PER SRM Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900155Floorbeam · corrodedCORROSION ON BEAM FS 986.5 LBL 42-46. REMOVED DAMAGED CAP, FABRICATED NEW CAP, TREATED PRIMED AND INSTALLED IAW SRM 53-10-9, SRM 51-10-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900154Support · corrodedCORROSION ON THRESHOLD SUPPORT FOR L-2 DOOR FS 947 LT BL 54-55. REMOVED DAMAGED PART AND INSTALLED NEW PART PER SRM 51-30-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900153Floorbeam · corrosionCORROSION ON BEAM FS 1016 LT BL 6 12 AFT LAV GALLEY FLOOR. CUT OUT CORROSION, FABRICATED NEW PARTS, TREATED, PRIMED AND INSTALLED IAW SRM 53-10-09, 51-30-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900152Support · corrodedCORROSION ON SECONDARY SUPPORT STRUCTURE AT FS 992 LT BL 15-20. REMOVED CORRODED SUPPORT IAW SRM 51-10-3 FIG 2, ALODINED AND PRIMED IAW 51-10-2, AND INSTALLED PER SRM 51-30-02.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900151Floorbeam · corrodedEXISTING FLOORBEAM REPAIR AT STA 968.5 RBL 49 CORRODED BEYOND LIMITS. REMOVED EXISTING T-CHORD PER SRM 51-30-2, FABRICATED T-CHORD REPLACEMENT PER SRM 53-10-9 FIG 2, TREATED AND PRIMED PARTS PER SRM 51-10-6 AND INSTALLED REPAIR IAW SRM 51-30-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900150Sill · corrodedCORROSION ON FWD LT DOOR SILL, I/B OF L-1 DOOR. REMOVED CORRODED AREA, FABRICATED AND INSTALLED FILLER AND DOUBLER PER SRM 53-10-2, 51-40-3, 51-10-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900149Frame · crackedAPU COWL DOOR RIGHT AFT LATCH MOUNT STRUCTURE FRAME IS BROKEN AND CRACKED ON BOTH THE FORWARD AND AFT FRAMES. REMOVED CRACKED FRAMES, FABRICATED AND INSTALLED REPAIRED FRAMES PER SRM 52-40-1, 51-30-2, 51-10-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900148Bulkhead Doubler · misrepairedAFT PRESSURE BULKHEAD, FUSELAGE STATION 1016, RBL 20, EXISTING REPAIR DOES NOT CONFORM TO SRM 53-10-4 FIG 3. REMOVED DOUBLER, FABRICATED AND INSTALLED REPLACEMENT DOUBLER PER SRM 53-10-4 FIG 3.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, BulkheadSDR AWXA9900147Stringer · crackedRT SKIN AT STR 17R BETWEEN STA 787 AND 607 HAD TWO CRACKS VERIFIED BY HFEC. CUT OUT CRACK, VERIFIED WITH HFEC. FABRICATED AND INSTALLED REPLACEMENT DOUBLER IAW SRM 53-30-3, QQA-250/5.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900146Doubler · corrodedFLOOR SUPPORT, MAIN CABIN FS 967 - 986.5, RBL 18 TOP OF FLOOR SUPPORT HAS CORROSION. REMOVED FLOOR SUPPORT DOUBLER, FABRICATED, ALODINED AND PRIMED DOUBLER IAW SRM 53-10-2 FIG 7 AND SRM 51-10-2.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900145Keel Beam · crackedSTATION 700 KEEL BEAM CLOSEOUT PANEL BOTTOM SIDE OF FUSELAGE AT MLG HAS 1.5 INCH CRACK. REMOVED CRACKED SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN PER SRM 51-10-2, 51-30-2, 53-10-2 FIG 4.Apr 20, 1999 · N183AW · Boeing 737277 · Fuselage Main, KeelSDR AWXA9900143Transmitter · malfunctionedDIVERSION: HYDRAULIC QTY INDICATION DISCREPANCY: 'A' SYSTEM HYDRAULIC QUANITY WAS NORMAL DURING PREFLIGHT AND T/O, 3.5 GALLONS. 'A' SYSTEM QUANITY DECREASED AFTER T/O TO 2.1 GALLONS AND THEN TO 1.4 DIVERTED TO LAS. SYSTEM RETURN TO 3.0 GALLONS UPON LANDING. Apr 17, 1999 · N180AW · Boeing 737277 · Hydraulic Quantity SensorSDR AWXA9900142Air Dist · odorNORMAL OPS, ODOR IN CABIN DISCREPANCY: IN BOUND SMELL OF OIL IN CABIN, MID-CABIN TO AFT FROM RT PACT. CK'D RIGHT PACK FOR LEAKS, NO LEAKS FOUND. RAN PACKS AND NO SMELL NOTED AT THIS TIME.Apr 17, 1999 · N188AW · Boeing 737277 · Air Distribution SystemSDR AWXA9900176Wire · brokenD-EMERGENCY EXIT LIGHT ON CEILING PANEL FOR OVERWING EXIT IS NOT WORKING. REPAIRED BROKEN WIRE AT CONNECTOR ON TOP OF EMERGENCY LIGHT, CHECKS OK.Apr 2, 1999 · N189AW · Boeing 737277 · Emergency LightingSDR AWXA9900121Skin · crackedNORMAL OPS, SKIN CRACK. SKIN AT STRINGER 17R BETWEEN STA 787 AND STA 607 HAS 2 CRACKS. VERIFIED WITH HFEC. REMOVED DAMAGED AREA, FABRICATED AND INSTALLED EXTERNAL DOUBLER PER SRM 53-30-3 FIG 1. PLACED ON MCK. INSPECT EVERY 3000 CYC'S, TERM AT C-CK.Mar 22, 1999 · N183AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900071Power Supply · inopIN MAINTENANCE, EMERGENCY EXIT LIGHT. EMERGENCY EXIT LIGHTS OUT AT LT OVERWING EXIT AND L-2, R-2 DOORS. REMOVED AND REPLACED AFT POWER SUPPLY, L-2 AND R-2 CK GOOD. REMOVED AND REPLACED LIGHT ASSY AT THE LEFT J OVERWING EXIT.Mar 7, 1999 · N186AW · Boeing 737277 · Emergency LightingSDR AWXA9900084Skin · crackedIN MAINTENANCE, FOUND SKIN CRACK, KEELBEAM SKIN CRACKED APPROX STA 780 RT BETWEEN TWO PREVIOIUS REPAIRS. REMOVED OLD SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW SRM 53-10-2 FIG 4, SRM 51-40-6 AND SRM 51-30-04 AND SRM 51-30 -2, STA 700 KEELBEAM.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900083Support · corrodedIN MAINTENANCE, FLOOR STRUCTURE CORRODED UNDER FWD LAV (LAV WALL HAT SECTION) LBL 13 STA 303.9 EXFOLIATION CORROSION. REMOVED DAMAGED SECTION FLOOR SUPPORT IAW SRM 51-30-2 AND DRAWING 65C33533 FABRICATED FLOOR SUPPORT IAW BAC1510-3357075-T6 QQA 200/11. INSTAMar 1, 1999 · N186AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900082Stringer · crackedIN MAINTENANCE,STRINGER CRACKED, CABIN AFT OF RT STA 500B STR 16R IS CRACKED FWD OF LIGHT ASSY. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR SECTION STRINGER BAC 1498-138/7075-T6, SPLICE ANGLES 7075-T6, AND U CHANNEL 7075-T6 .Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900081Stringer · crackedIN MAINTENANCE, STRINGER CRACK CABIN FWD OF RT STA 520 STR 16R AFT OF LIGHT ASSY. REMOVED STRINGER PER SRM 51-30-02, FABRICATED REPLACEMENT STRINGER FROM BAC 1498-1557075-T6 PER SRM 53-10-2, FIG 9. INSTALLED PER SRM 51-30-02.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900080Stringer · crackedIN MAINTENANCE, STRINGER CRACK STA 500B HAS 2 CRACKS AROUND FASTENERS. CUT OUT DAMAGED SECTION PER SRM 53-10-3 FIG 1. FABRICATED AND INSTALLED NEW STRINGER, U-CHANNEL, AND J ANGLES PER SRM 53-10-3 FIG 1 AND SRM 51-30-0. ALODINED AND PRIMED PER SRM 51-10-2. Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900079Stringer · crackedIN MAINTENANCE, CRACKED STRINGER 16L AT STA 520 HAS 3 CRACKS AROUND FASTENERS. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-30-0. FABRICATED AND INSTALLED STRINGER BAC 1498-1557075-T6 IAW SRM 51-10-2 FIG 9 AND SRM 51-30-0.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900078Doubler · crackedIN MAINTENANCE, FOUND CRACKED DOUBLER BS 1138, WL 282, LBL 27.5, HAS A CRACKED INTERNAL DOUBLER. REMOVED AND REPLACED DOUBLER FABRICATED FROM 7075-T6 .063 AND QQA- 250/13 HEAT TREATED AND PRIMED, INSTALLED PER SRM 53-30-3 FIG 37.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900077Floorbeam · corrodedIN MAINTENANCE, FOUND CORRODED FLOORBEAM AT STA 328 RBL 20 CORRODED OUT OF LIMITS. REMOVED AND REPLACED THE DAMAGED PORTION OF FLOORBEAM CAP PER SRM 53-10-9, 51-10-2, 51-30-2.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900076Stringer · wornIN MAINTENANCE, DAMAGED FLOORBEAM STRINGER 18L UNDER FLOORBEAMS 887 TO 907 HAS A HOLE WORN BY A LOOSE CONNECTOR. REMOVED AND REPLACED STRINGER SECTION IAW 53-10-03 REPAIR WAS INSTALLED FROM FS 867-907 SPLICED IN AT STA 877. REPAIR PARTS MADE FROM 7075-T6 .04Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900075Frame · crackedIN MAINTENANCE, FOUND STA 1138 WL 262 RBL 26.5 FWD SIDE OF FRAME IS CRACKED IN RADIUS. REMOVED AND REPLACED CRACKED ANGLE IAW SRM 51-30-2, SRM 51-40-3 BAC 5602 AND SRM 51-10-2 SRM 55-10-6. MAT 7075-0 QQU250/3 HEAT TREATED TO T-6.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA9900074Floorbeam · corrodedIN MAINTENANCE FOUND CORRODED FLOORBEAM,STA 294.5 LBL 36 CORROSION. REMOVED DAMAGED AREA PER SRM 53-10-9 FIG 1. FABRICATED T CAP FROM BAC1505-100617 R642686 PER SRM 53-10-9 FIG 1 INSTALLED PER SRM 51-30-2.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900073Skin · dentedIN MAINTENANCE, DENT REPAIR STA 185R EXISTING REPAIR DENTED. REMOVED EXISTING REPAIR AT STA 185. CUT OUT DAMAGE PER SRM 53-30-3 FIG 2. ALODINED AND PRIMED PER SRM 51-10-2.Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900072Clip · brokenIN MAINTENANCE, STRINGER TIE CLIPS. STRINGER TIE CLIPS BROKEN, CRACKED, OR DAMAGED AT THE FOLLOWING LOCATIONS, STA 344 STR 6R, STA 500 STR 27R, STA 500A STR 27R, STA 706 STR 4L, STA 727A STR 4R, STA 727B STR 3R, STA 727B STR 4R, STA 727B STR 8R, STA 747 STR 5Mar 1, 1999 · N186AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900063Clip · crackedSTRINGER CLIPS CRACKED. REMOVED AND REPLACED CLIPS PER EO 53-12-01.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Miscellaneous StructureSDR AWXA9900062Stringer · crackedSTRINGER 15R AT STA 603 CRACKED ON END APPROX .25 INCH LONG. BLENDED STRINGER END TO REMOVE CRACK, NDT INSP RADIUS BLENDED AREA, ALODINED AND PRIMED. MAT LOSS .020 AND NO EFFECT TO FASTENER EDGE MARGINS, WORK DONE PER SRM 53-10-1 FIG 1, 51-10-2 AND HFEC INSPFeb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900061Frame · crackedBS 1138, WL 262, RBL 26.5 FORWARD SIDE OF FRAME, THE FRAME IS CRACKED IN THE RADIUS. REMOVED CRACKED ANGLE, FABRICATED REPLACEMENT PART AND INSTALLED IAW SRM 51-30-2, SRM 51-40-3, BAC 5602, SRM 51-40-3, SRM 51-10-2, AND SRM 55-10-6.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, FrameSDR AWXA9900060Fitting · damagedTOP OF RIGHT WING FILLET AREA, STA 663 SPLICE FITTING HAS A HOLE/DRILL START WBL 71.24. REMOVED FASTENER ON FITTING, SPOT FACED HOLE TO REMOVE DAMAGE, SHOT PEENED PER BAC 5730, ALODINED AND PRIMED PER SRM 51-10-2 IAW AND ER 2-57-31-17. REINSTALLED FASTENER IFeb 8, 1999 · N186AW · Boeing 737277 · Aerodynamic FairingsSDR AWXA9900059Floorbeam · corrodedFLOORBEAM AT STA 294.5 LBL 36 CORROSION OUT OF LIMITS. REMOVED DAMAGED AREA PER SRM 53-10-9 FIG 1. FABRICATED T-CAP PER SRM 53-10-9 FIG 1. INSTALLED PER SRM 51-30-2.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900058Floorbeam · corrodedFLOORBEAM AT STA 328 RBL 20 CORRODED OUT OF LIMITS. REMOVED DAMAGED CAP, FABRICATED AND INSTALLED REPLACEMENT CAP PER SRM 53-10-9, 51-10-2, 51-30-2.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Floor BeamSDR AWXA9900057Stringer · wornSTRINGER 18L UNDER FLOORBEAMS 887 TO 907 HAS A HOLE WORN IN IT BY LOOSE AV CONNECTOR. REMOVED AND REPLACED STRINGER SECTION IAW SRM 53-10-3. REPAIR WAS INSTALLED FROM FS 867 TO 907, SPLICED IN AT STA 877. REPAIR PARTS, CHANNEL AND ANGLE MADE FROM 7075-T6.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900056Stringer · crackedSTRINGER 16L AT STA 520 HAS 3 CRACKS AROUND FASTENERS. REMOVED DAMAGED SECTION OF STRINGER IAW SRM 51-30-0, FABRICATED AND INSTALLED STRINGER IAW SRM 51-30-2 FIG 9 AND SRM 51-30-0.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900055Stringer · crackedSTRINGER 16L AT STA 500B HAS 2 CRACKS AROUND FASTENERS TL-70. CUT OUT DAMAGED SECTION PER SRM 53-10-3 FIG 1, FABRICATED AND INSTALLED NEW STRINGER U-CHANNEL, AND J-ANGLES PER 53-10-3 FIG 1, SRM 51-30-0. APPLIED ALODINE AND PRIMER PER SRM 51-10-3.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900054Stringer · crackedCABIN FWD OF RT STA 520 STR 16R IS CRACKED AFT OF LIGHT ASSY. REMOVED STRINGER PER SRM 51-30-02, FABRICATED REPLACEMENT STRINGER FROM BAC 1498-1557075-T6 R 608816 PER 53-10-2 FIG 9. INSTALLED PER SRM 51-30-02.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900053Stringer · crackedCABIN AFT OF RT STA 500B STRINGER 16R IS CRACKED FWD OF LIGHT ASSY. CUT OUT DAMAGED SECTION OF STRINGER IAW SRM 53-10-3 FIG 1. FABRICATED REPAIR SECTION STRINGER, SPLICE ANGLES, AND U-CHANNEL OUT OF 7075-T6 IAW SRM 53-10-3 FIG 1. ALODINED, PRIMED PARTS IAW Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Longeron/StringerSDR AWXA9900052Skin · crackedDURING ROUTINE MAINTENANCE CHECK, FOUND SKIN CRACK AT APPROX STA 780 RT BETWEEN TWO PREVIOUS REPAIRS. REMOVED OLD SKIN, FABRICATED AND INSTALLED REPLACEMENT SKIN IAW 53-10-2 FIG 4, SRM 51-40-6, SRM 51-30-04, SRM 51-30-02.Feb 8, 1999 · N186AW · Boeing 737277 · Fuselage Main, Plate/SkinSDR AWXA9900038Fan · failedAIR TURNBACK, BURNING ODOR IN CABIN AND FLIGHT DECK. SLIGHT BURNING ODOR NOTICED IN CABIN AND FLIGHT DECK AFTER TAKEOFF. RETURNED TO PHOENIX. FOUND GASPER CIRCUIT BREAKER POPPED. REMOVED AND REPLACED GASPER FAN PER MM21-24-21. OPERATIONAL CHECKED GOOD.Feb 3, 1999 · N182AW · Boeing 737277 · Air Distribution FanSDR AWXA9900032Transmitter · failedOIL QTY CHECKED BEFORE ENGINE START NR 2 ENGINE HAD JUST OVER 3 GALLONS. T/O ROLL ENGINE INSTRUMENTS NORMAL, JUST AFTER ROTATION NOTICED OIL PRESSURE IN RED AND ENGINE OIL TEMP CLIMBING THROUGH 170 DEGREES C. SHUT ENGINE DOWN AND RETURNED TO SMF. REMOVED ANJan 25, 1999 · N182AW · Boeing 737277 · Engine Oil Pressure
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