# Service difficulty reports: Boeing 727-254 A list on [Boeing 727-254](https://openairdocs.org/model/boeing-727-254.md). Newest first. General aviation reporting is voluntary. Page 1 of 3 · 149 reports - [SDR USAA119907](https://openairdocs.org/sdr/USAA119907.md): Socket · missing · Nov 15, 1999 · N912TS · Boeing 727254 · Emergency Lighting > FLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKET ASSEMBLY AND LENS ASSEMBLY. (M) - [SDR 99ZZZM801](https://openairdocs.org/sdr/99ZZZM801.md): Lens · missing · Nov 15, 1999 · N912TS · Boeing 727254 · Emergency Lighting > FLT 6359 - LGA-DCA - FOUND ON POST FLIGHT INSPECTION, ON WHITE EPL LIGHT MISSING AT ROW 5 DEF. REPLACED EPL LIGHT SOCKET ASSEMBLY AND LENS ASSEMBLY. (M) - [SDR USAA119906](https://openairdocs.org/sdr/USAA119906.md): Light · corroded · Nov 12, 1999 · N916TS · Boeing 727254 · Emergency Lighting > OVERNIGHT L/S DCA- EMERGENCY LIGHT INOPERATIVE RIGHT OVERWING EXIT. CLEANED CORROSION FROM LIGHT SOCKETS. OPERATIONAL CHECK NORMAL. (M) - [SDR USAA119905](https://openairdocs.org/sdr/USAA119905.md): Light · inoperative · Nov 12, 1999 · N912TS · Boeing 727254 · Emergency Lighting > FLT 6364 - DCA-LGA - ESCAPE PATH LIGHTING AT SEAT 10D INOPERATIVE. INSTALLED EPL LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M) - [SDR USAA119904](https://openairdocs.org/sdr/USAA119904.md): Light · inoperative · Nov 12, 1999 · N916TS · Boeing 727254 · Emergency Lighting > OVERNIGHT L/S DCA - AFT AIRSTAIR EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED EMERGENCY EXIT LIGHTS ASSEMBLY. OPERATIONAL CHECK NORMAL. (M) - [SDR USAA119902](https://openairdocs.org/sdr/USAA119902.md): Lens · missing · Nov 12, 1999 · N912TS · Boeing 727254 · Emergency Lighting > FLT 6376 - DCA-LGA - EMERGENCY PATH LIGHTING HAS ONE LIGHT OUT ADJACENT TO ROW 10. REPLACED MISSING LENS. (M) - [SDR USAA119901](https://openairdocs.org/sdr/USAA119901.md): Battery Pack · discharged · Nov 6, 1999 · N913TS · Boeing 727254 · Emergency Lighting > EMERGENCY EXIT LIGHTS AT L-1 DOOR AND COCKPIT DOOR WON'T TEST. REPLACED EMERGENCY EXIT LIGHTS (S/N 2019 AND 4459) AT L-1 DOOR AND COCKPIT DOOR. (M) - [SDR USAA109903](https://openairdocs.org/sdr/USAA109903.md): Accessory Unit · inoperative · Oct 14, 1999 · N916TS · Boeing 727254 · Landing Gear Position and Warning > FLT 6050 - LGA-BOS - HAD TO USE GEAR TRIGGER TO RAISE GEAR. OIL COOLER CSD RETURNED TO NORMAL WHEN FLAPS RAISED FROM 5-2 DEGREES. AURAL WARNING SOUNDED. HAD TO PULL C/B TO SILENCE HORN. ALL OTHER INDICATIONS NORMAL. T/S TO LANDING GEAR ACCESSORY UNIT, REP - [SDR USAA109901](https://openairdocs.org/sdr/USAA109901.md): Pump · failed · Oct 2, 1999 · N913TS · Boeing 727254 · Engine Fuel Pump > FLT 6470 - DCA-LGA - ON TAKEOFF, DURING GEAR RETRACTION, NR 3 ENGINE FAILED. EMERGENCY DECLARED, RETURNED TO DCA. REPLACED NR 3 ENGINE DRIVEN FUEL PUMP. (M) - [SDR USAA099903](https://openairdocs.org/sdr/USAA099903.md): Smoke Detector · failed · Sep 17, 1999 · N913TS · Boeing 727254 · Smoke Detection > FLT 6511 - LGA-DCA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED SMOKE DETECTOR. OPERATIONAL CHECK NORMAL. (M) - [SDR USAA079901](https://openairdocs.org/sdr/USAA079901.md): Battery Pack · discharged · Jul 21, 1999 · N916TS · Boeing 727254 · Emergency Lighting > RIGHT FORWARD OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK OPERATIONAL CHECK OK. (M) - [SDR USAA069943](https://openairdocs.org/sdr/USAA069943.md): Accumulator · ruptured · Jun 13, 1999 · N912TS · Boeing 727254 · Hydraulic Power Accumulator, Main > SYSTEM 'B FAILURE EN ROUTE TO LGA. AS PER ABNORMAL, SAFETY WIRE BROKEN ON GPWS AND PNEUMATIC BRAKE. FOUND BRAKE ACCUMULATOR RUPTURED. REPLACED SAME PER MM 29-32-40. RESAFTIED GPWS SWITCH AND PNEUMATIC BRAKE HANDLE. BLED PNEUMATIC BRAKE LINE PER MM 32-43-0 - [SDR USAA069942](https://openairdocs.org/sdr/USAA069942.md): Fuel Control · malfunctioned · Jun 9, 1999 · N914TS · Boeing 727254 · Fuel Control/Turbine Engines > FLT 6461 - LGA-DCA - AT 10,000 FT CRUISE, PULLED ALL POWER LEVERS TO IDLE. NR 3 WENT TO FULL POWER, NO CONTROL WITH POWER LEVER. ENGINE LIMITS NOT EXCEEDED. SHUT DOWN ENGINE. 10 MINUTES WINDMILL AT 15 PSI OIL PRESSURE. REPLACED NR 3 ENGINE FUEL CONTROL PE - [SDR USAA049905](https://openairdocs.org/sdr/USAA049905.md): Duct · damaged · Apr 15, 1999 · N916TS · Boeing 727254 · Pneumatic Distribution System > FLT 6520- DCA-LGA - AIR RETURN TO DCA - NR 1 ENGINE FIRE LIGHT ILLUMINATED ON TAKEOFF, REDUCED THROTTLE TO IDLE, LIGHT EXTINGUISHED MOMENTARILY. RANCID SMELL IN CABIN, NO SECONDARY ENGINE INDICATIONS. REPLACED 8TH STAGE DUCT. (M) - [SDR USAA049902](https://openairdocs.org/sdr/USAA049902.md): Light · inoperative · Apr 3, 1999 · N913TS · Boeing 727254 · Emergency Lighting > COCKPIT DOOR EMERGENCY EXIT LIGHT WOULD NOT WORK. REPLACED LIGHT ASSEMBLY, OPERATIONAL CHECK NORMAL. (M) - [SDR USAA039914](https://openairdocs.org/sdr/USAA039914.md): Module · leaking · Mar 19, 1999 · N916TS · Boeing 727254 · Hydraulic System, Main > FLT 6470 - DCA-LGA - EN ROUTE LOST ALL SYSTEM 'A' HYDRAULIC FLUID. EMERGENCY DECLARED. MANUAL LANDING GEAR EXTENSION PERFORMED. FOUND SYSTEM 'A' AILERON MODULAR PACKAGE SEPARATED. REPLACED AILERON PACKAGE PER MM 27-10-141. REPLACED NR 1 AND NR 2 ENGINE HY - [SDR USAA039902](https://openairdocs.org/sdr/USAA039902.md): Coalescer · dirty · Mar 9, 1999 · N913TS · Boeing 727254 · Humidity Control System > FLT 6161 - BOS-LGA - ON APPROACH, FLIGHT ATTENDANTS REPORT A BURNING SMELL IN FORWARD CABIN BY L1 DOOR. SMELL WAS BURNING PLASTIC OR WAX LIKE ORDER. TROUBLESHOT SMELL TO DEICING/ANTI-ICING FLUID IN RIGHT PACK SYSTEM. REPLACED RIGHT WATER SEPARATOR BAG PER M - [SDR USAA069909](https://openairdocs.org/sdr/USAA069909.md): Web · cracked · Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Miscellaneous Structure > NOSE WHEEL WELL PRESSURE WEB CRACKED ONE INCH ABOVE RIGHT AFT ACCESS PANEL. INSTALLED REPAIR AT NOSE WHEEL WELL PRESSURE WEB, ABOVE RIGHT AFT ACCESS PANEL. MATERIAL USED, 2024-T3,.050 INCH, 11 INCH BY 8 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0145. (M) - [SDR USAA069908](https://openairdocs.org/sdr/USAA069908.md): Strap · cracked · Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Miscellaneous Structure > CRACKS ON CIRCUMFERENTIAL SPLICE STRAP BS 930, STRINGER 14R. INSTALLED FUSELAGE FRAME REPAIR AT BS 930, STRINGER 14R. MATERIAL USED, 7075-T6,.125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR ACCOMPLISHED IAW SB 727-53-0162. (M) - [SDR USAA069907](https://openairdocs.org/sdr/USAA069907.md): Circumferential · cracked · Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, Frame > CRACK ON CIRCUMFERENTIAL AT BS 930 STRINGER 13L. INSTALLED FUSELAGE FRAME REPAIR AT BS 930 BETWEEN STRINGER 11 AND STRINGER 12, AND BETWEEN STRINGER 13 AND STRINGER 14 LEFT. MATERIAL USED, 7075-T6,.125 INCH, 14.5 INCH BY 1.25 INCH. REPAIR INSTALLED IAW SB - [SDR USAA069906](https://openairdocs.org/sdr/USAA069906.md): Skin · corroded · Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, Plate/Skin > EXTERIOR SKIN HAS POPPED RIVET HEAD (MISSING) STATION 720D AT STRINGER 28L. INSTALLED FUSELAGE EXTERIOR SKIN REPAIR AT BSB 720D, STRINGER 28L. MATERIAL USED 7075-T6,.125 INCH, 17 INCH BY 13.5 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M) - [SDR USAA069905](https://openairdocs.org/sdr/USAA069905.md): Skin · corroded · Mar 6, 1999 · N913TS · Boeing 727254 · Fuselage Main, Plate/Skin > EVIDENCE OF CORROSION AT BS 351 STRINGER 26R EXTERIOR. INSTALLED FUSEALGE EXTERIOR SKIN REPAIR AT BS 351, STRINGER 26R. MATERIAL USED, 2024-T3,.063 INCH, 19 INCH BY 11 INCH. REPAIR ACCOMPLISHED IAW SRM 53-30-3 FIG 1. (M) - [SDR USAA029905](https://openairdocs.org/sdr/USAA029905.md): Drive Motor · failed · Feb 8, 1999 · N912TS · Boeing 727254 · Trailing Edge Flap Actuator > 'A' SYSTEM HYDRAULICS WENT OT ZERO DURING CLIMB-OUT. PERFORMED ABNORMAL CHECK LIST, GEAR AND FLAPS WERE LOWERED USING ALTERNATE METHOD. REPLACED HYDRAULIC FLAP DRIVE MOTOR PER MM 27-51-62 DUE TO LEAK. REPLACED NR 1 ENGINE DRIVEN HYDRAULIC FLAP DRIVE MOTOR P - [SDR USAA129808](https://openairdocs.org/sdr/USAA129808.md): Engine · vibrates · Dec 19, 1998 · N913TS · Boeing 727254 · Engine (Turbine/Turboprop) > NR 1 ENGINE VIBRATION ABNORMAL ON START BETWEEN 35-45 PERCENT N2. AT REDUCED TAKEOFF POWER 1.81 EPR, N1 INDICATION 96 PERCENT VS 91 PERCENT ON NR 2 AND NR 3 ENGINES. IN FLIGHT VIBRATION IN TAIL SECTION OF CABIN NOTED. EMERGENCY WAS NOT DECLARED, ENGINE WAS - [SDR USAA129810J](https://openairdocs.org/sdr/USAA129810J.md): Floorbeam · corrosion · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Floor Beam > CABIN FLOOR STRUCTURE BEAM UPPER FLANGE, LOWER SECTION BS 1148, AT RBL 12 EVIDENCE OF CORROSION. INSTALLED REPAIR ON CABIN FLOORBEAM UPPER FLANGE BS 1148, RBL 12. ACCOMPLISHED IAW 727 SRM 53-10-8, FIG 8. MATERIAL USED 7075T-6,.090 INCH. - [SDR USAA129810I](https://openairdocs.org/sdr/USAA129810I.md): Skin · damaged · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/Skin > FUSELAGE EXTERIOR - TEMPORARY PLUG REPAIR INSTALLED IN FUSELAGE SKIN BETWEEN BS 950D AND BS 950E, BETWEEN STR 22R AND STR 23R. INSTALLED FLUSH REPAIR AT FUSELAGE EXTERIOR SKIN BETWEEN BS 950D AND BS 950E, STR 22R AND STR 23R. ACCOMPLISHED IAW B727 SRM 53-30- - [SDR USAA129810H](https://openairdocs.org/sdr/USAA129810H.md): Skin · corroded · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/Skin > BULGE ON FUSELAGE EXTERIOR SKIN LEFT HAND SIDE STA 1183, BETWEEN STR 20 AND STR 22 NEXT TO LAVATORY SERVICE PANEL. INSTALLED STRINGER AND EXTERNAL DOUBLER REPAIR AT LEFT HAND BS 1183 FROM STR 20L TO STR 22L. ACCOMPLISHED IAW AVITAS ENGINEERING ORDER NR 98PMS - [SDR USAA129810G](https://openairdocs.org/sdr/USAA129810G.md): Frame · cracked · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Frame > RIGHT CABIN FRAME STA 930 CRACKED BETWEEN STR 14R - STR 15R BELOW CABIN WINDOW. ACCOMPLISHED RIGHT CABIN FRAME REPAIR BS 930 BETWEEN STR 14 - STR 15R. INSTALLED KIT NR 65C25313-2. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X) - [SDR USAA129810F](https://openairdocs.org/sdr/USAA129810F.md): Frame · cracked · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Frame > LEFT CABIN FRAME STA 930 CRACKED BETWEEN STR 14L - STR 15L BELOW CABIN WINDOW. ACCOMPLISHED LEFT CABIN WINDOW FRAME REPAIR BS 930 BETWEEN STR 14L AND STR 15L. INSTALLED KIT NR 65C25313-1. ACCOMPLISHED IAW SB 727-53-130 AND SB 727-53-162. (X) - [SDR USAA129810E](https://openairdocs.org/sdr/USAA129810E.md): Seat Track · corroded · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage, Seat/Cargo Attach Fittings > CABIN SEAT TRACK LIGHT CORROSION FROM BS 380 THROUGH BS 760.95 LBL 25.5. REPLACED CABIN SEAT TRACK LBL 25.5 FROM BS 380 TO BS 480. MATERIAL USED BAC 1570-797, 100 INCHES LONG. ACCOMPLISHED IAW SRM 51-30-2 FIG 1. (X) - [SDR USAA129810D](https://openairdocs.org/sdr/USAA129810D.md): Tube · worn · Dec 17, 1998 · N916TS · Boeing 727254 · Aircraft Fuel Distribution System > RIGHT WING FUEL VENT TUBE SURFACE AND CLAMPS WORN BETWEEN WS 491 - WS 686 INTERIOR. ACCOMPLISHED RIGHT WING FUEL VENT TUBE REPAIRS WS 491.5, 546.5, 574.0, 601.5, 629.0, 656.5, AND 686.5. MATERIAL USED 2024T-3,.040 INCH, 2.5 INCHES BY 3.0 INCHES. ACCOMPLISH - [SDR USAA129810C](https://openairdocs.org/sdr/USAA129810C.md): Skin · cracked · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Main, Plate/Skin > FUSELAGE SKIN CRACKED ABOVE THE RBL 70.5 CHORD ANGLE, BS 848.95 WL 196. EMANATING FROM THE FLOOR BEAM ATTACH ANGLE, LOWER FASTENER. INSTALLED FUSELAGE SKIN REPAIR RIGHT BS 848.95. MATERIAL USED 15-5PH HT 180-200 KSI 12 INCHES BY 31 INCHES. ACCOMPLISHED IAW - [SDR USAA129810B](https://openairdocs.org/sdr/USAA129810B.md): Angle · cracked · Dec 17, 1998 · N916TS · Boeing 727254 · Fuselage Miscellaneous Structure > VERTICAL FLANGE OF THE RBL 70.5 WING TO CENTER TANK CHORD ANGLE IS CRACKED IN TWO PLACES, LOWER FASTENER. BS 846, WL 193, 15 INCHES BELOW CABIN FLOOR. INSTALLED BS 870 PREVENTIVE MOD RT SIDE KIT NR 65-92431-2. ACCOMPLISHED IAW SB 727-53-116. INSTALLED RT S - [SDR USAA129810A](https://openairdocs.org/sdr/USAA129810A.md): Chord · corrosion · Dec 17, 1998 · N916TS · Boeing 727254 · Horizontal Stabilizer Structure > LEFT HORIZONTAL STABILIZER AFT SPAR AT UPPER AND LOWER CHORDS HAS CORROSION AT ATTACH ANGLE TO AFT HINGE FITTING AT STABILIZER STA 32 INCH. ACCESS THROUGH LOWER INBOARD ACCESS PANELS 9112, 9121. INSTALLED DOUBLER REPAIR ON LEFT HORIZONTAL STABILIZER LOWER CH - [SDR USAA129806](https://openairdocs.org/sdr/USAA129806.md): Pulley · jammed · Dec 17, 1998 · N914TS · Boeing 727254 · Landing Gear Steering System > FLT 6531 - LGA-DCA - AFTER LANDING NOSE STEERING INOPERATIVE FOR RIGHT TURNS. CONTROL STEERING TILLER BINDING WHEN TURNED TO RIGHT, TOWED AIRCRAFT FROM RUNWAY. CHECKED AND LUBED RUDDER STEERING SYSTEM, CHECKED STEERING CABLES AND PULLEYS FOUND PULLEY ON LEFT - [SDR USAA129805](https://openairdocs.org/sdr/USAA129805.md): Smoke Detector · malfunctioned · Dec 11, 1998 · N914TS · Boeing 727254 · Smoke Detection > FLT 6540 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR INOPERATIVE. REPLACED FORWARD LAVATORY SMOKE DETECTOR, OPERATIONAL CHECK NORMAL. (M) - [SDR USAA119804](https://openairdocs.org/sdr/USAA119804.md): Battery · discharged · Nov 19, 1998 · N913TS · Boeing 727254 · Emergency Lighting > BOTH LEFT AND RIGHT FORWARD OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. BOTH LEFT AND RIGHT MID OVERWING EXTERIOR EMERGENCY EXIT LIGHTS INOP. REPLACED LEFT AND RIGHT FORWARD EXTERIOR EMERGENCY EXIT LIGHT BATTERIES PER MM 33-50-0. REPLACED MID LEFT OVERWING - [SDR TAOA109806](https://openairdocs.org/sdr/TAOA109806.md): Indicator · malfunctioned · Oct 17, 1998 · N912TS · Boeing 727254 · Trailing Flap Position Indicating System > FLT 6500 - DCA-LGA - ON APPROACH, UPON FLAP EXTENSION, INBOARD FLAPS WOULD NOT EXTEND BEYOND 25 DEGREES. REPLACED INBOARD FLAP POSITION INDICATOR. (M) - [SDR TAOA109802](https://openairdocs.org/sdr/TAOA109802.md): Light · inoperative · Oct 11, 1998 · N914TS · Boeing 727254 · Emergency Lighting > FLT 6540 - DCA-LGA - LEFT OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED LIGHT ASSEMBLY OPERATIONAL CHECK NORMAL. (M) - [SDR TAOA099810](https://openairdocs.org/sdr/TAOA099810.md): Battery Pack · discharged · Sep 11, 1998 · N914TS · Boeing 727254 · Emergency Lighting > FLT 6030 - LGA-BOS - LEFT AFT OVERWING EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES, TEST OK. (M) - [SDR 98ZZZX3577](https://openairdocs.org/sdr/98ZZZX3577.md): Fasteners · loose · Sep 11, 1998 · N912TS · Boeing 727254 · Wing Spar > LOOSE FASTENERS AT RT WING FRONT SPAR UPPER CHORD. WS 330.5. - [SDR TAOA099805](https://openairdocs.org/sdr/TAOA099805.md): Smoke Detector · failed · Sep 6, 1998 · N916TS · Boeing 727254 · Smoke Detection > FLIGHT 6520 - DCA-LGA - FORWARD LAVATORY SMOKE DETECTOR GOES OFF CONTINOUSLY. REPLACED FORWARD LAVATORY SMOKE DETECTOR OPERATIONAL CHECK NORMAL. (M) - [SDR TAOA099804](https://openairdocs.org/sdr/TAOA099804.md): Flashlight · discharged · Sep 5, 1998 · N913TS · Boeing 727254 · Emergency Lighting > FLT 6050, FOUND ON L/S CHECK, EMERGENCY FLASH LIGHT AT L-1 DOOR INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT AT L-1 DOOR CHECKS OK. (M) - [SDR TAOA099803](https://openairdocs.org/sdr/TAOA099803.md): Modular Unit · leaking · Sep 4, 1998 · N913TS · Boeing 727254 · Hydraulic System, Main > LGA-DCA - FLT 6451 - 'A' HYDRAULIC SYSTEM FAILURE IN FIGHT AFTER FLAP RETRACTION. FOUND 'A' SYSTEM MODULAR UNIT LEAKING DUE TO CRACKED FITTING REPLACED MODULE. REPLACED 1 AND 2 HYDRAULIC PUMPS, CASE DRAIN RETURN AND PRESSURE FILTERS. SERVICED HYDRAULIC SYST - [SDR TAOA079809](https://openairdocs.org/sdr/TAOA079809.md): Fire Loop · malfunctioned · Jul 16, 1998 · N916TS · Boeing 727254 · Fire Detection > FLT 6480 - DCA-LGA - WHEEL WELL FIRE WARNING LIGHT CAME ON IN FLIGHT FOLLOWED EMERGENCY PROCEDURES. REPLACED NOSE WHEEL WELL FIRE LOOP ALSO REPLACED MAIN LEFT AND RIGHT WHEEL WELL FIRE LOOP. REPLACED FIRE AND OVERHEAT CONTROL BOX. PERFORMED RESISTANCE CHECK - [SDR TAOA079805](https://openairdocs.org/sdr/TAOA079805.md): Valve · malfunction · Jul 10, 1998 · N914TS · Boeing 727254 · Cabin Cooling System > FLT 6420 - DCA-LGA - RIGHT PACK OVERHEATED ON TAXI OUT WITH RIGHT PACK SWITCH IN OFF POSITION. REPLACED RIGHT PACK SHUT OFF VALVE. OPERATIONAL CHECK NORMAL. (M) - [SDR TAOA059815](https://openairdocs.org/sdr/TAOA059815.md): Fan · shorted · Jun 1, 1998 · N914TS · Boeing 727254 · Air Distribution Fan > FLT 6480 - DCA-LGA - GASPER FAN CIRCUIT BREAKER POPPED FOLLOWED BY BURNING SMELL FROM GASPER FAN VENTS. GASPER FAN SWITCH WAS PLACED TO OFF. REPLACED GASPER FAN IAW MM CHAPTER 21-23-1. OPERATIONAL CHECK NORMAL. (M) - [SDR TAOA059811](https://openairdocs.org/sdr/TAOA059811.md): Switch · failed · May 21, 1998 · N913TS · Boeing 727254 · Fire Detection > NR 1 ENGINE FIRE WARNING AT 3000 FT FIRE WARNING LIGHT AND BELL REPEATEDLY CYCLED ON AND OFF AFTER ENGINE SHUTDOWN. FIRE BOTTLE EXPENDED BOTH SIDES. FOUND WIRE NR W150-028-28 CHAFED AND SHORTING TO GROUND IN NR 1 ENGINE PYLON, REPAIRED WIRE PER CHAPTER 20 ST - [SDR TAOA059809](https://openairdocs.org/sdr/TAOA059809.md): Fire Sensor · malfunctioned · May 18, 1998 · N913TS · Boeing 727254 · Fire Detection > FLT 6160 - LGA-BOS - ENGINE NR 1 FIRE WARNING IN FLIGHT. UNABLE TO PUT OUT LIGHT. SHUTDOWN ENGINE AND DISCHARGED FIRE BOTTLE, AFTER COMPLETING PROCEDURE LIGHT REMAINED ILLUMINATED. REPLACED NR 1 ENGINE LOWER FIRE WARNING SENSOR AND FIRE WARNING CONTROL UNIT - [SDR TAOA059803](https://openairdocs.org/sdr/TAOA059803.md): Fire Loop · malfunctioned · May 4, 1998 · N913TS · Boeing 727254 · Fire Detection > NR 1 ENGINE FIRE WARNING ILLUMINATED ON DESCENT AT IDLE POWER, DESCENDING THROUGH 15,000 FEET AT 300 KNOTS, WHILE ACCOMPLISHING AIRCRAFT OPERATIONS PROCEDURE, FIRE WARNING EXTINGUISHED. ENGINE AT IDLE POWER REMAINDER OF FLT NO FURTHER FIRE INDICATION. INSPEC Next page: https://openairdocs.org/model/boeing-727-254/reports.md?page=2 ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql 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 = '727254' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-727-254/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.