Boeing 727-225

Service difficulty reports · 4,226

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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 = '727225'
  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 95FDEA01528Beam · corrodedCORROSION (73C032-03), ON THE T/E AFT UPPER CHORD AT STAB STA 206 AND STA 161 RIGHT HORZ STAB. REMOVED AND REPLACED T/E AFT UPPER CHORD ON RIGHT HORZ STAB, ALL WORK DONE IAW.Oct 9, 1995 · N464FE · Boeing 727225 · Horizontal Stabilizer StructureSDR 95FDEA01527Stringer · corrodedCORROSION ON STR AT BS 740 LBL 23 WL 150. CORROSION ON STR AT BS 740 LBL 23 WL 150 OUT OF LIMITS PER FEDEX SRM 53-10-1. CUT OUT DAMAGED AREA AND REPAIRED PER FEDEX SRM 53-10-3.Oct 9, 1995 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 95FDEA01519Stringer · corrodedCORROSION ON STRINGER AT BS 530 LBL 23 WL 151. REMOVED DAMAGE, FABRICATED SPLICE, FILLER AND INSTALLED PER SRM 53-10-3.Oct 9, 1995 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 95FDEA01518Skin · corrodedCORROSION ON SKIN UNDER LEVELING COMPOUND AT BS 481, BL 0 WL 150 (C53-113-0161). REPAIRED CORRODED AREA PER FEDEX EA 7-5310-25902 AND SRM 53-10-4.Oct 9, 1995 · N464FE · Boeing 727225 · Fuselage Main, Plate/SkinSDR 95FDEA01517Shear Tie · corrodedAFT CARGO BAY, THERE IS CORROSION ON SHEAR TIES ON AFT SIDE OF FRAME AT BS 1166 RBL 4 LBL 18 WL 150. REMOVED AND REPLACED CORROSION ON SHEAR TIES BS 1166 RBL 4 LBL 18 WL 150, PER FEDEX SRM 53-10-1.Oct 9, 1995 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 95FDEA01516Skin · lightning strikeLOWER FWD CARGO DOOR HAS MULTIPLE LIGHTNING STRIKES ALONG LOWER OUTER SKIN. REPAIRED 10 AREAS OF LIGHTNING STRIKES ALONG OUTER SKIN OF FWD CARGO DOOR LOWER, BS 560 TO 620 3.23 INCHES UP FROM BOTTOM OF DOOR, PER FEDEX SRM 52-00-2, 52-00-3 AND 53-30-3.Oct 9, 1995 · N464FE · Boeing 727225 · Cargo/Baggage DoorsSDR 9515262710Brakes · on fireAFTER LANDING AND PARKED AT THE GATE, GROUND CREW ADVISED THAT THE LEFT MAIN LANDING GEAR WAS ON FIRE. EMERGENCY EQUIPMENT WAS CALLED OUT, BUT NOT REQUIRED. MAINTENANCE REPORTED GREASE FIRE ON THE NR 1 BRAKE. REPLACED THE NR 1 BRAKE AND TIRE. CAUSE FOR EXCOct 8, 1995 · N820EA · Boeing 727225 · BrakeSDR 95FDEA01509Pack · malfunctionedON CLIMBOUT, FLT ENG NOTICED FLUX OF 30 TO 40 DEGREES IN R/PACK TEMP AND ABNORMAL LOW R/BLEED PRESS. ALMOST SIMULTANEOUSLY ENG NR 3 OVERHEAT LIGHT ON FLT ENG'S PANEL ILLUMINATED. R/PACK WAS SHUTDOWN AND R/BLEED CLOSED. THE NR 3 ENG STRUT OVERHEAT LIGHT WENTOct 6, 1995 · N468FE · Boeing 727225 · Cabin Cooling SystemSDR 95FDEA01503Torque Box · crackedTHE RT TORQUE BOX IS CRACKED BEYOND THE DOUBLER IN THE FWD RADIUS OF THE SUPPORT ANGLE, JUST BELOW THE VERTICAL ACTUATOR SUPPORT, TEMP REPAIR INSTALLED AND LOGBOOK ENTRY REQ. REPAIRED RT TORQUE BOX PER EA 7-5310-25836.Oct 5, 1995 · N464FE · Boeing 727225 · Fuselage Miscellaneous StructureSDR 96ZZZX1751Floor Beam · corrodedDURING D-CHECK, BS 480 FLOOR BEAM CAP IS CORRODED AT TWO NUT-CLIP LOCATIONS, BL ZERO AND RBL 10. CUT OUT DAMAGED AREA PER SRM 53-10-8, 13 INCH LENGTH OF CUT-OUT ALODINED AND PRIMED PER SRM 51-10-2. FABRICATED REPAIR PARTS PER SRM 53-10-3. ALODINED AND PRIMEOct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR 96ZZZX1750Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 1 LBL 45 IS CORRODED FROM BS 1058 TO BS 1075. REMOVED TRACK STA 1050 TO STA 1090 PER SRM 51-30-2. FABRICATED NEW TRACK PER SRM 51-10-1. ALODINED AND PRIMED NEW TRACK PER SRM 51-10-2. INSTALLED NEW TRACK PER SRM 51-30-2.Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZX1749Floor Beam · corrosionDURING D-CHECK, BS 1030 FLOOR BEAM CAP IS CORRODED AT LBL 9 FLOOR PANEL ATTACH HOLES. REMOVED DAMAGED AREA BS 1030 FLOOR BEAM CAP AT LBL 9 PER SRM 51-10-6 AND INSTALLED UPPER CHORD BEAM REPAIR PER SRM 53-10-8 P.18 FIG. 3. SIZE OF REPAIR 14 INCH BY 2 INCH BY Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, Floor BeamSDR 96ZZZX1748Seat Track · corrodedDURING D-CHECK, SEAT TRACK NR 2 LBL 24 IS CORRODED FROM BS 1030 TO BS 1130. REMOVED FASTENERS FOR REMOVAL OF SEAT TRACK PER SRM 51-30-2. FABRICATED TO FIT IN PLACE. NEW SEAT TRACK BS 1030 TO BS 1130 OF 7075-T6. ALODINED AND PRIMED PER 51-10-2. INSTALLED SOct 4, 1995 · N742DH · Boeing 727225 · Fuselage, Seat/Cargo Attach FittingsSDR 96ZZZX1747Angle · corrosionDURING D-CHECK, COCKPIT LT SIDEWALL FLOOR SUPPORT ANGLE CORRODED BETWEEN STA 277 AND STA 303.9. REMOVED CORROSION AND Z-ANGLE BRACKET PER SRM 51-10-2. INSTALLED Z-ANGLE PER SRM 51-30-2 AND SRM 51-10-1 P.4, SIZE 8 INCHES BY 6 INCHES .050 INCH 2024-T3. TAT: Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 96ZZZX1746Frame · bentDURING D-CHECK, FWD BAGG COMPT FRAME IS DAMAGED AT SPLICE DOUBLER AT STA 500 STR 25R. REMOVED DOUBLER AND STRAIGHTENED FRAME PER SRM 51-10-1. FABRICATED DOUBLER AND ALODINED AND PRIMED PER SRM 51-40-2 AND SRM 51-10-2, 7075-T6, 6.5 INCHES BY 4 INCHES, .071 INOct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, FrameSDR 96ZZZX1745Skin · dentedDURING D-CHECK, FUSE EXT SKIN IS DENTED AT STA 251.6 STR 15 AND STR 16L. CUT OUT DAMAGED AREA FOUND OUT OF LIMITS PER SRM 51-10-1. INSTALLED DOUBLER REPAIR 15 INCHES BY 12 INCHES 2024-T3 .063 INCH ON FUS EXT SKIN STA 251.6, STR 15 AND STR 16L PER SRM 5330-3,Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR 96ZZZX1744Stringer · corrosionDURING D-CHECK, AFT B/B BS 985 - BS 990 STR 29R CORR LEVEL 2. REMOVED CORROSION ON STR 29R OUT OF LIMITS. ORIGINAL THICKNESS .185 INCH AFTER CORROSION REMOVAL THICKNESS .071 INCH AT LOWEST POINT PER SRM 51-10-6 BEYOND LIMITS. INSTALLED DOUBLER REPAIR PER AVOct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 96ZZZX1743Splice · corrosionDURING D-CHECK, FORWARD BAGG COMPT - FS 680 STR 26L SPLICE HAS CORROSION FWD AND AFT OF CIRCUMFERENTIAL FRAME. REMOVED SPLICE PER SRM 53-10-3. MADE NEW SPLICE PER SRM 51-10-1 P.4 10 INCHES 7075-T6. INSTALLED SPLICE AT STA 680 STR 26L PER SRM 53-10-3 AND SRMOct 4, 1995 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 96ZZZX1742Door Frame · bentDURING D-CHECK, LOWER AFT CARGO BENT FRAME STA 950 AT STR 26L. FABRICATED AND INSTALLED FRAME REPAIR PER SRM 53-10-4 AND SRM 51-30-2, 10 INCHES BY 3.5 INCHES, 7075-T6 .071 INCH. TAT: 45,788.3 HRS. TAC: 29,959.Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 96ZZZX1741Door Frame · crackedDURING C-CHECK, LOWER AFT CARGO BENT FRAME STA 950, STR 26R. ROUTED OUT CRACK FOUND ON FRAME 950C, STR 26R, PER SRM 51-10-1. ALODINED AND PRIMED AREA PER SRM 51-10-6. FABRICATED AND INSTALLED FRAME REPAIR 11 INCHES BY 3.5 INCHES .071 7075-T6 PER SRM 53-10-4Oct 4, 1995 · N742DH · Boeing 727225 · Fuselage Miscellaneous StructureSDR 96ZZZX1740Skin · gougeDURING D-CHECK, FORWARD CARGO DOOR EXT STA 604 AT BOTTOM - SMALL GOUGE. CUT OUT DAMAGE AREA PER SRM 53-30-3, FIGURE 13. FABRICATED DOUBLER AND INSTALLED REPAIR PER SRM 53-30-3, FIGURE 13. SIZE 4.25 INCH DIA .063 INCH 7075-T6. TAT: 45,788.3 HRS. TAC: 29,Oct 4, 1995 · N742DH · Boeing 727225 · Cargo/Baggage DoorsSDR 96ZZZX1739Skin · crackedDURING D-CHECK, AFT LOWER CARGO DOOR AFT UPPER PRESSURE RELEASE, PREVIOUS STOP DRILL NEEDS REPAIR ON CUT-OUT. STOP DRILLED CRACK PER SRM 51-10-1. INSTALLED DOUBLER REPAIR PER SRM 57-40-2, 4 INCHES BY 6 INCHES, .050 INCH 2024-T3. TAT: 45,788.3. TAC: 29,95Oct 4, 1995 · N742DH · Boeing 727225 · Cargo/Baggage DoorsSDR 96ZZZX1738Skin · gougedDURING D-CHECK, FUSE EXT SKIN STA 325 STR 18-STR 19R - 2 EA GOUGES/DENTS. BURNISH OUT GOUGES, FORWARD GOUGE BEYOND LIMITS. REMOVED FASTENERS PER SRM 51-30-2. CUT OUT DAMAGED AREA PER SRM 51-10-1. FABRICATED AND INSTALLED DOUBLER REPAIR 8 INCHES BY 9 INCHESOct 4, 1995 · N742DH · Boeing 727225 · Fuselage Main, Plate/SkinSDR 96ZZZX1737Skin · crackDURING D-CHECK, WING LEADING EDGE CUT-OUT FOR THE NR 6 SLAT OUTBOARD SLAT HOOK FOUND CRACKED AT THE AFT END. REMOVED ALL ATTACHING HARDWARE PER SRM 51-30-2. CUT FILLER STRIP PER SRM 57-30-4. STOP DRILLED CRACK PER SRM 51-10-1. ALODINE AND PRIMED PER SRM 51Oct 4, 1995 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR 96ZZZX1736Skin · gapDURING D-CHECK, FOUND THE WING LEADING EDGE CUT-OUT FOR THE NR 4 SLAT ACTUATOR HAS A LARGE GAP AT THE AFT END. FABRICATED DOUBLER 5.5 INCH BY 5.5 INCH 2024-T3 .080 INCH ALODINED AND PRIMED PER SRM 51-10-2. INSTALLED DOUBLER AT WING L/E CUT-OUT NR 7 SLAT PER Oct 4, 1995 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR 96ZZZX1735Skin · crackedDURING D-CHECK, NR 3 SLAT OUTBOARD SLAT HOOK WING LEADING EDGE CUT-OUT FOUND CRACKED AT AFT END. STOP DRILLED CRACK PER SRM 51-10-1. INSTALL DOUBLER REPAIR LEADING EDGE CUT-OUT PER SRM 57-30-4. SIZE OF REPAIR 6 INCHES BY 5 INCHES. MATERIAL USED 0.020 INCH Oct 4, 1995 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR 96ZZZX1734Skin · crackedDURING D-CHECK, WING LEADING EDGE CUT-OUT FOR THE NR 7 SLAT OUTBOARD HOOK FOUND CRACKED AT THE AFT OUTBOARD CORNER. STOP DRILLED CRACK. INSTALLED DOUBLER PER SRM 57-30-4 FROM 301 1/2 HARD 7.5 INCH BY 7.5 INCH DOUBLER. TAT: 45,788.3 HRS. TAC: 29,959.Oct 4, 1995 · N742DH · Boeing 727225 · Wing, Plate/SkinSDR 95FDEA01502Frame · puncturedIN THE AFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AND HAS A DOUBLE HOLE AT BS 1050, RBL 19, WL 148. REPAIRED UPPER FLANGE OF FRAME AT BS 1050, RBL 19, WL 148 PER FEDEX SRM 51-40-3.Oct 4, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01501Frame · crackedTHE UPPER FLANGE OF FRAME IS CRACKED AT BS 1090 STA 27R. REMOVED DAMAGE, FABRICATED REPAIR DOUBLER AND REPAIRED UPPER FLANGE OF FRAME AT BS 1090 STR 27R PER FEDEX SRM 51-40-3.Oct 4, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01472Stringer · corrodedCORROSION ON STR 3 PLACES, BS 525, 528 AND 530 LBL 15 WL 150. MECHANICALLY REMOVED CORROSION ON STR 27 BS 525 TO 530 LBL 15 WL 150, FOUND TO BE OUT OF LIMITS PER FEDEX SRM 53-10-1 AND 53-10-0. REPAIRED STR 7 AT BS 525 TO 530 LBL 15 WL 150 PER FEDEX SRM 53-1Oct 2, 1995 · N464FE · Boeing 727225 · Fuselage Main, Longeron/StringerSDR 95FDEA01471Frame · crackedFRAME DENTED AT BS 700 RBL 32 WL 160 AND CRACKED. REMOVED DAMAGED AREA, FABRICATED REPAIR PART, ALODINED, PRIMED, INSTALLED AND PAINTED REPAIR PART PER FEDEX SRM 51-40-3.Oct 2, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01470Frame · crackedCRACKED FRAME AT BS 312 LBL 45 WL 173 NEAR STR 22L. REMOVED CRACKED FRAME AT BS 312 LBL 45 WL 173 AND INSTALLED NEW FRAME.Oct 2, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR SCNA95202Eel · inoperativeTHE AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED AFT AIRSTAIR OVERHEAD EMERGENCY EXIT LIGHT ASSEMBLY IAW MM 33-50-61 AND LIGHT TESTED GOOD.Sep 30, 1995 · N282SC · Boeing 727225 · Emergency LightingSDR 95FDEA01464Lock Solenoid · malfunctionedREPEAT WRITE UP - ON INITIAL RETRACTION, GEAR WOULD NOT COME UP, SEVERAL ATTEMPTS WITH NO SUCCESS. RED TAB CHECKLIST RAN, LANDING GEAR LEVER LATCH FAILED TO RELEASE RESULTING IN LATCH BEING RAISED, AND GEAR RETRACTED. FOUND LANDING GEAR CONTROL LEVER LOCK SOSep 30, 1995 · N469FE · Boeing 727225 · Landing Gear Retraction/Extension SystemSDR TAOA099513Eel · missingTWO 'E' PATH LIGHT ASSEMBLIES MISSING AT ROW 10. REPLACED LIGHT ASSEMBLIES. OPERATIONAL CHECK OK. (M)Sep 29, 1995 · N923TS · Boeing 727225 · Emergency LightingSDR 95FDEA01452Frame · damagedAFT CARGO BAY, THERE IS MECHANCIAL DAMAGE ON UPPER FLANGE OF FRAME AT BS 1190 RBL 20 WL 151. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01451Frame · puncturedAFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01450Frame · puncturedAFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 RBL 20 WL 148. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01449Frame · puncturedAFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1010 RBL 24 WL 146. REPAIRED FLANGE OF FRAME PER SRM 53-10-1. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01448Frame · damageAFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 RBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01447Frame · damagedAFT CARGO BAY, THE UPPER FLANGE OF FRAME HAS MECHANICAL DAMAGE AT BS 1110 LBL 20 WL 150. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR 95FDEA01446Frame · puncturedAFT CARGO BAY, THE UPPER FLANGE OF FRAME IS PUNCTURED AT BS 1090 LBL 22 WL 149. REPAIRED FLANGE OF FRAME PER SRM 53-10-1.Sep 28, 1995 · N464FE · Boeing 727225 · Fuselage Main, FrameSDR DL72P953937Skin · corrosionDURING INSPECTION OF THE LOWER WING SKIN PER EO 4-37113-3, CORROSION WAS DISCOVERED ON THE AFT SKIN BETWEEN S-5C AND S-3C AT APPROXIMATELY LBL 30 AND RBL 30. MTC REPORTS A MINIMUM REMAINING THICKNESS OF .067 AT THE RT DAMAGE AREA AND A MINIMUM REMAINING THICKSep 26, 1995 · N8891Z · Boeing 727225 · Wing, Plate/SkinSDR IXKA9500029Oil Bypass Ind · illuminatedFLT NR 40 - TPA-EWR - DIVERTED TO ATL, NR 3 ENGINE LOW OIL PRESSURE FILTER BYPASS LIGHT CAME ON IN FLIGHT. BURNED OUT TWO BULBS, ALL OTHER ENGINE INDICATIONS NORMAL. PERFORMED PRECAUTIONARY SHUTDOWN. FORTY MINUTES OF WINDMILL AT 30 PSI. CLEANED OIL IN CANNSep 25, 1995 · N356PA · Boeing 727225 · Engine Oil Indicating SystemSDR TA0A099511Eel Lamp · failedAISLE PATH LIGHTING HAS BULB BURNED OUT AT ROW 17. RELAMPED ROW 17 AISLE PATH LIGHT BULB. OPS CHECKS OK. (M)Sep 24, 1995 · N923TS · Boeing 727225 · Emergency LightingSDR 95ZZZX5917Overheat Loop · out of positionLOG REPORT: F-GL534 AT CHS, ON TAKEOFF ROLL, NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. ABORTED TAKEOFF. LIGHT WENT OUT ON POWER REDUCTION. INSPECTION OF NR 3 ENGINE STRUT FOUND OVERHEAT LOOP TOUCHING DUCT ASSY. REPOSITIONED OVERHEAT LOOP. PEFORMED LESep 24, 1995 · N887MA · Boeing 727225 · Overheat DetectionSDR TAOA099510Gear Light · failedDURING GEAR EXTENSION, RIGHT MAIN GEAR GREEN LIGHT WOULD NOT ILLUMINATE UNTIL PRESSED TO TEST. REPLACED RIGHT GEAR GREEN LIGHT ASSEMBLY, OPS CHECKED OK. (M)Sep 23, 1995 · N919TS · Boeing 727225 · Landing Gear Position and WarningSDR IXKA9500028Flap Pos Ind · stuckFLT NR 80 - ATL - DURING FLAP RETRACTION, OUTBOARD FLAPS STAYED AT 2 DEGREES WHEN FLAPS WERE POSITIONED TO UP. CYCLED FLAPS AND OUTBOARDS STAYED AT 2 DEGREES. RETURNED TO ATL. INSPECTED FLAPS, NO ABNORMALITIES FOUND. REMOVED AND REPLACED OUTBOARD FLAP INDISep 23, 1995 · N353PA · Boeing 727225 · Trailing Flap Position Indicating SystemSDR 95FDEA01406Lines · chafedTHE B-SYS LOSS NR 1 PUMP IND LOW PRESS, 20 SEC LATER PRESS ZERO, QTY ZERO. CREW REPORTED B-SYS SHUTOFF BEFORE QTY DROPPED. REMOVED AND REPLACED NR 1 AND NR 2 B-SYS CASE DRAIN FILTERS. NO METAL CONTAMINATION FOUND FLL-1365, FILTERS LEAK CK'D OK. FOUND SUPPLSep 23, 1995 · N469FE · Boeing 727225 · Hydraulic System, MainSDR SCNA95196Coffee Maker · failedCOFFEE MAKER BEGAN SMOKING IN GALLEY. THE CIRCUIT BREAKER WAS PULLED FOR THE COFFEE MAKER AND THE SMOKE CEASED. REMOVED AND REPLACED COFFEE MAKER AND NEW UNIT TESTED GOOD.Sep 21, 1995 · N282SC · Boeing 727225 · Buffet/Galleys
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