# Service difficulty reports: N275AF, cancelled Jun 12, 2003 A list on [N275AF, cancelled Jun 12, 2003](https://openairdocs.org/deregistered/N275AF-2003-06-12.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 3 · 137 reports - [SDR SCNA01716](https://openairdocs.org/sdr/SCNA01716.md): Battery Pack · discharged · Sep 28, 2001 · N275AF · Boeing 727227 · Emergency Lighting > RIGHT AFT EXTERIOR EMERGENCY LIGHT INOPERATIVE. CORRECTED BY REPLACING BATTERY PACK. - [SDR SCNA01045](https://openairdocs.org/sdr/SCNA01045.md): Gearbox · Jun 18, 2001 · N275AF · Boeing 727227 · Turbine Engine Oil System > On climbout from MSP the number one engine low oil pressure light illuminated, oil quantity dropped and oil pressure gauge started to drop verifying the warning light. Removed and replaced the gearbox, found oil pressure line leaking. - [SDR SCNA01043](https://openairdocs.org/sdr/SCNA01043.md): Duct · contaminated · Jun 6, 2001 · N275AF · Boeing 727227 · Air Distribution System > DURING TAXI OUT FROM THE GATE, HYDRAULIC FLUID HAZE WAS DETECTED IN THE AFT CABIN. FOUND AND REMOVED HYDRAULIC RESIDUE FROM DUCTING IN AFT STAIRWELL. ALSO, FOUND AND REMOVED DEBRIS FROM DUCTS. - [SDR SCNA01026](https://openairdocs.org/sdr/SCNA01026.md): Battery · discharged · Apr 6, 2001 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENANCE LINE CHECK THE OVERHEAD EMERGENCY EXIT LIGHT BETWEEN THE AFT LAVS WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT BATTERY AND CHARGER ASSEMBLY BETWEEN THE AFT LAVS. - [SDR SCNA01021](https://openairdocs.org/sdr/SCNA01021.md): Light · broken · Mar 1, 2001 · N275AF · Boeing 727227 · Emergency Lighting > EMERGENCY EXIT LIGHT ON LEFT REAR OVERWING DOOR CASE WAS FOUND BROKEN. REMOVED AND REPLACED EMERGENCY EXIT ASSEMBLY. - [SDR SCNA01020](https://openairdocs.org/sdr/SCNA01020.md): Light · broken · Feb 28, 2001 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENANCE INSPECTION THE EMERGENCY PATH LIGHTING WAS FOUND BROKEN AT THE L2 DOOR. REMOVED AND REPLACED THE L2 DOOR EMERGENCY EXIT LIGHING ASSY. - [SDR SCNA01013](https://openairdocs.org/sdr/SCNA01013.md): Light · inoperative · Feb 8, 2001 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENANCE LINE CHECK THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY LIGHT IN THE AFT STAIRWAY OVERHEAD. OPERATIONAL CHECKS GOOD. - [SDR SCNA01012](https://openairdocs.org/sdr/SCNA01012.md): Detector · malfunctioned · Feb 4, 2001 · N275AF · Boeing 727227 · Overheat Detection > DURING DEPARTURE FROM MSP THE NUMBER THREE ENGINE OVERHEAT LIGHT ILLUMINATED. PERFORMED COM PROCEDURES THE LIGHT EXTINGUISHED. CLIMB TO 25,000 WAS RESUMED, THE CABIN PRESSURE CONTINUED TO CLIMB AT 400 FPM IN BOTH MANUAL AND AUTO MODE. RETURNED TO MSP, REMOV - [SDR SCNA01006](https://openairdocs.org/sdr/SCNA01006.md): Light · inoperative · Jan 9, 2001 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENANCE LINE CHECK THE THE FORWARD OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REPAIRED THE WIRING AND REMOVED AND REPLACED SELF CONTAINED OVERHEAD EMERGENCY LIGHT. OPERATIONAL CHECKS GOOD. - [SDR SCNA00127](https://openairdocs.org/sdr/SCNA00127.md): Jackscrew · broken · Dec 2, 2000 · N275AF · Boeing 727227 · Trailing Edge Flap Actuator > DURING CLIMB OUT FROM MSP THE INBOARD FLAPS WOULD NOT RETRACT PAST THE TWO DEGREE POSITION. THE FLIGHT CREW RETURNED TO MSP. THE LEFT INBOARD JACKSCREW END TIP WAS FOUND BROKEN OFF, ALSO FORWARD ELEPHANT EAR BEARING DAMAGE WAS FOUND. REMOVED AND REPLACED JA - [SDR SCNA00388](https://openairdocs.org/sdr/SCNA00388.md): Floorbeam · corroded · Nov 13, 2000 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOORBEAM AT STA 1110 RBL 12. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 511001 AND 531008. FABRICATED FLOOR BEAM REPAIR FROM BAC 14902773 7075 AND 0.125 - [SDR SCNA00389](https://openairdocs.org/sdr/SCNA00389.md): Seat Track · corroded · Nov 12, 2000 · N275AF · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS RT SIDE SEAT TRACK BETWEEN STATIONS 420 AND 440 RBL 48. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION OF SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE - [SDR SCNA00387](https://openairdocs.org/sdr/SCNA00387.md): Floorbeam · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OF LIMITS ON THE FLOORBEAM AT STA 344 RBL 12 THROUGH 24. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION IAW B727 SRM 511001 AND 531008. FABRICATED NEW FLOORBEAM REPAIR FROM BAC 15061451 - [SDR SCNA00385](https://openairdocs.org/sdr/SCNA00385.md): Floorbeam · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM AT STA 380, BL 0 THROUGH RBL 24. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED 1 TEE CAP FROM BAC 14902785, 1 ANGLE FROM BAC 14902831, 1 STRAP FORM BAC 15123353, AND 1 - [SDR SCNA00384](https://openairdocs.org/sdr/SCNA00384.md): Floorbeam · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM AT STA 360, LBL 24 THROUGH RBL 12. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW REPAIR PARTS FROM BAC 1505100617, BAC 14902785, BAC 14902831, BAC 15123353 AND BAC - [SDR SCNA00383](https://openairdocs.org/sdr/SCNA00383.md): Floorbeam · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON THE FLOORBEAM AT STA 440, BL 0 - RBL 12. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SECTION, FABRICATED 1 EACH T-CAP FROM BAC 1505100617, 1 ANGLE FROM BAC 14902785, 1 ANGLE - [SDR SCNA00382](https://openairdocs.org/sdr/SCNA00382.md): Seat Track · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK UPPER AND LOWER SIDE AT BS 380 TO BS 420, RBL 40. REMOVED CORROSION IAW B727 SRM 51-10-06. REMOVED SEAT TRACK IAW B727 SRM 51-30-02 AND 53-10-05. FABRICATED NEW SEAT TRACK F - [SDR SCNA00381](https://openairdocs.org/sdr/SCNA00381.md): Seat Track · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENACE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON INBOARD SIDE OF SEAT TRACK AT BS 380 TO BS 420, RBL 20. REMOVED CORROSION IAW B727 SRM 51-10-06. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792 7075 T6. TREATED AND PRIMED IAW B7 - [SDR SCNA00379](https://openairdocs.org/sdr/SCNA00379.md): Seat Track · corroded · Nov 10, 2000 · N275AF · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SEAT TRACK OUTBOARD SIDE RBL 42. REMOVED CORROSION IAW B727 SRM 511006. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 15207887188. TREATED AND PRIMED IAW B727 SRM 511002 AND MM 5 - [SDR SCNA00386](https://openairdocs.org/sdr/SCNA00386.md): Seat Track · corroded · Nov 9, 2000 · N275AF · Boeing 727227 · Fuselage, Seat/Cargo Attach Fittings > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON SEAT TRACK AT FS 1090 THROUGH 1136 LBL 25. REMOVED CORROSION IAW B727 SRM 511006. REMOVED DAMAGED SEAT TRACK IAW B727 SRM 513002. FABRICATED NEW SEAT TRACK PER SAMPLE FROM BAC 1520792. TR - [SDR SCNA00380](https://openairdocs.org/sdr/SCNA00380.md): Floor Support · corroded · Nov 9, 2000 · N275AF · Boeing 727227 · Fuselage Miscellaneous Structure > DURING HEAVY MAINTENANCE INSPECTION CORROSION WAS FOUND OUT OF LIMITS ON FLOOR SUPPORT AT FS 1067, LBL 13 - 25. REMOVED CORROSION IAW SRM 51-10-06. FABRICATED NEW SUPPORT AS PER SAMPLE FROM BAC1518344. TREATED AND PRIMED IAW SRM B727 51-10-02 AND MM 51-20-0 - [SDR SCNA00099](https://openairdocs.org/sdr/SCNA00099.md): Compressor · stalled · Sep 8, 2000 · N275AF · Boeing 727227 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL, ENGINE NUMBER TWO COMPRESSOR STALL DURING THE TAKEOFF ROLL AT LAS (10 KNT) CROSS WIND. SLIGHT EPR FLUCUATION, SLIGHT NOISE, AIRFRAME PULSATED, SOFT STALL. INSPECTED INLET AND EXAUST NR 2 ENGINE, NO DEFECTS NOTED ALL PARAMETERS CHECK NORM - [SDR SCNA00074](https://openairdocs.org/sdr/SCNA00074.md): Bulb · failed · Jul 6, 2000 · N275AF · Boeing 727227 · Landing Gear Position and Warning > DURING FINAL APPROACH WHEN THE LANDING GEAR WAS EXTENDED ONE OF THE GEAR INDICATION LIGHTS FAILED TO ILLUMINATE. THE CREW EXECUTED A GO-AROUND AT MSP. THE CREW CHANGED THE INDICATION BULB, OPERATIONAL CHECKED GOOD, AND LANDED WITHOUT INCIDENT. - [SDR SCNA00058](https://openairdocs.org/sdr/SCNA00058.md): Light · missing · Jun 19, 2000 · N275AF · Boeing 727227 · Emergency Lighting > DURING MAINTENANCE LINE CHECK, THE RIGHT FORWARD OVERWING EXIT DOOR WAS FOUND TO BE MISSING THE EMERGENCY EXIT LIGHT ASSEMBLY. REPLACED LIGHT ASSEMBLY FOR THE RIGHT FORWARD OVERWING DOOR EMERGENCY EXIT LIGHT ASSEMBLY. OPERATIONALLY CHECKS GOOD. - [SDR SCNA00056](https://openairdocs.org/sdr/SCNA00056.md): Motor · leaking · Jun 10, 2000 · N275AF · Boeing 727227 · Trailing Edge Flap Actuator > DURING CRUISE FLIGHT THE A-SYSTEM LOST ALL FLUID, THE FLIGHT CREW EXECUTED EMERGENCY CHECK LIST PROCEDURES. PERFORMED MANUAL FLAP AND GEAR EXTENSION AND LANDED. REMOVED AND REPLACED THE FLAP POWER UNIT HYDRAULIC MOTOR IAW B727 MM CH 275162, OPERATIONAL AND L - [SDR SCNA00050](https://openairdocs.org/sdr/SCNA00050.md): Outflow Valve · failed · Jun 4, 2000 · N275AF · Boeing 727227 · Pressure Regulator/Outflow Valve > AFTER TAKEOFF FROM LAS, THE AIRCRAFT WAS UNABLE TO PRESSURIZE. THE FLIGHT CREW DUMPED FUEL AND RETURNED TO POINT OF ORIGIN LAS. THE RIGHT PACK VALVE WAS REMOVED AND REPLACED, PRESSURE AND LEAK CHECK GOOD ON ENGINE RUN. - [SDR SCNA00043](https://openairdocs.org/sdr/SCNA00043.md): Battery · discharged · May 6, 2000 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENACE LINE CHECK, THE OVERWING EMERGENCY EXIT LIGHTS WERE FOUND TO BE DIM. REMOVED AND REPLACED BATTERY AT M1086, ALL EMERGENCY LIGHTS CHECK GOOD. - [SDR SCNA01022](https://openairdocs.org/sdr/SCNA01022.md): Battery Pack · discharged · Mar 26, 2000 · N275AF · Boeing 727227 · Emergency Lighting > DURING A MAINTENANCE LINE CHECK THE AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND INOPERATIVE. REMOVED AND REPLACED BATTERY PACK, OPERATIONAL CHECKS GOOD. - [SDR SCNA00301](https://openairdocs.org/sdr/SCNA00301.md): Wire · broken · Jan 25, 2000 · N275AF · Boeing 727227 · Light System Wiring > DURING SCHEDULED HEAVY MAINTENANCE CHECK THE CENTER AISLE OVERWING EMERGENCY EXIT LIGHT HAD BROKEN WIRE. REPLACED PIN IN CONNECTOR IAW SWP 206111. OPS CHECK GOOD IAW B727 MM 335001. - [SDR SCNA00300](https://openairdocs.org/sdr/SCNA00300.md): Light · inoperative · Jan 25, 2000 · N275AF · Boeing 727227 · Emergency Lighting > DURING SCHEDULED HEAVY MAINTENANCE CHECK THE LEFT FORWARD EMERGENCY EXIT DOOR OVERHEAD LIGHT WAS FOUND INOP AT ROW 18A. RELAMPED AND OPS CHECK GOOD IAW B727 MM 335011. - [SDR SCNA99131](https://openairdocs.org/sdr/SCNA99131.md): Start Valve · inop · Oct 31, 1999 · N275AF · Boeing 727227 · Engine Start Valves/Controls > DURING THE TAKEOFF ROLL, THE NUMBER THREE ENGINE START VALVE LIGHT ILLUMINATED. REMOVED AND REPLACED THE NUMBER THREE ENGINE START VALVE PER MM 801111. OPERATIONAL AND LEAK CHECKS GOOD. - [SDR SCNA99117](https://openairdocs.org/sdr/SCNA99117.md): Battery Pack · discharged · Sep 5, 1999 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE MAINTENANCE CHECK, THE EMERGENCY LIGHT ABOVE THE R2 DOOR WAS FOUND TO BE DIM. REMOVED AND REPLACED THE BATTERY PACK IAW MM 345001. OPERATIONALLY CHECKS GOOD. - [SDR SCNA99092](https://openairdocs.org/sdr/SCNA99092.md): Hydraulic Line · fractured · Jul 19, 1999 · N275AF · Boeing 727227 · Hydraulic System, Main > DURING CLIMB, AIRCRAFT EXPERIENCED A SYSTEM HYDRAULIC LOSS. COMPLIED WITH COM ABNORMAL PROCEDURES AND RETURNED TO THE AIRPORT. UPON INSPECTION FOUND PRESSURE LINE FROM THE NUMBER ONE ENGINE SPLIT. REPLACED LINE AND SERVICED HYDRAULICS. SYSTEM LEAKS AND OPER - [SDR SCNA99090](https://openairdocs.org/sdr/SCNA99090.md): Compressor · stalled · Jul 9, 1999 · N275AF · Boeing 727227 · Turbine Engine Compressor Section > DURING TAKEOFF ROLL AT ABOUT 40 KNOTS, NUMBER TWO ENGINE COMPRESSOR STALLED THREE TIMES. ABORTED TAKEOFF AND TAXIED BACK TO RAMP. INSPECTED NUMBER TWO ENGINE INLET AND EXHAUST WITH NO DAMAGE FOUND. RAN ENGINE PER MAINTENANCE MANUAL WITH ALL PARAMETERS NORMA - [SDR SCNA99075](https://openairdocs.org/sdr/SCNA99075.md): Sense Line · damaged · May 25, 1999 · N275AF · Boeing 727227 · Pneumatic Distribution System > DURING CLIMB WITH TAKEOFF POWER GOT MOMENTARY ILLUMINATION OF THE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT. ALL OTHER INDICATIONS NORMAL. REPLACED DAMAGED SENSE LINE ON THE NUMBER ONE ENGINE 13TH STAGE MODULATING AND SHUTOFF VALVE PER BMM CHAPTER 75-30-00. RA - [SDR SCNA99074](https://openairdocs.org/sdr/SCNA99074.md): Clamp · loose · May 24, 1999 · N275AF · Boeing 727227 · Pneumatic Distribution System > DURING CLIMB, THE NUMBER ONE ENGINE STRUT OVERHEAT LIGHT ILLUMINATED. UPON INSPECTION OF THE NUMBER ONE STRUT FOUND A LOOSE CLAMP. REMOVED AND REPLACED CLAMP AS REQUIRED. OPERATIONALLY CHECKS GOOD, NO FURTHER DISAGREEMENT NOTED. - [SDR SCNA99705](https://openairdocs.org/sdr/SCNA99705.md): Floorbeam · corroded · Apr 26, 1999 · N275AF · Boeing 727227 · Fuselage Main, Floor Beam > DURING A HEAVY MAINTENANCE CHECK, FOUND CORROSION OUT OF LIMITS ON FLOORBEAM AT BS312 BL0. REMOVED CORROSION IAW SRM 511006, OUT OF LIMITS PER SRM 531001. CUTOUT DAMAGED AREA IAW SRM 514004. FABRICATED REPAIR DOUBLER FROM EXTRUSION BAC14902831 7075 T6 IAW S - [SDR SCNA99051](https://openairdocs.org/sdr/SCNA99051.md): Oil Pump · inoperative · Mar 14, 1999 · N275AF · Boeing 727227 · Turbine Engine Oil System > DURING DESCENT AT APPROXIMATELY FL200, CREW OBSERVED LOW OIL PRESSURE LIGHT ON NR 2 ENGINE. OIL PRESSURE DECAYED TO 15 PSI, QUANTITY WAS 2 QTS AND TEMPERATURE STAYED IN GREEN BAND. ENGINE WAS SHUT DOWN AND SECURED PER COM PROCEDURES. THE APPROACH AND LANDIN - [SDR SCNA99021](https://openairdocs.org/sdr/SCNA99021.md): Oven · sparking · Jan 23, 1999 · N275AF · Boeing 727227 · Buffet/Galleys > THE FRONT LEFT OVEN WAS OBSERVED TO HAVE SPARKS EMITTING FROM THE FRONT VENT AREA. OVEN WAS SHUT DOWN. REMOVED AND REPLACED THE FORWARD LEFT OVEN UNIT, OPERATIONALLY CHECKS GOOD. - [SDR SCNA99005](https://openairdocs.org/sdr/SCNA99005.md): Light · inoperative · Jan 10, 1999 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE MAINTENANCE CHECK, THE AFT LEFT SERVICE DOOR (L2) OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE IN THE ARM POSITION. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSEMBLY AT THE L2 DOOR, OPERATIONALLY CHECKS GOOD. - [SDR SCNA98152](https://openairdocs.org/sdr/SCNA98152.md): Batteries · discharged · Dec 27, 1998 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE MAINTENANCE CHECK, THE AFT AIRSTAIR OVERHEAD EMERGENCY LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE BATTERIES. OPERATIONALLY CHECKS GOOD IAW MM 335061. - [SDR SCNA98137](https://openairdocs.org/sdr/SCNA98137.md): Light · inop · Nov 8, 1998 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE MAINTENANCE CHECK, THE L2 EMERGENCY EXIT LIGHT WAS FOUND TO BE INOPERATIVE. REMOVED AND REPLACED THE EMERGENCY EXIT LIGHT ASSEMBLY. TESTED EMERGENCY LIGHT FOR PROPER OPERATION AND OPERATIONALLY CHECKS GOOD. - [SDR SCNA98134](https://openairdocs.org/sdr/SCNA98134.md): Switch · failed · Oct 31, 1998 · N275AF · Boeing 727227 · Engine Oil Pressure > DURING CLIMBOUT, THE NUMBER ONE ENGINE OIL PRESSURE LOW LIGHT ON FILTER BYPASS INDICATOR. RETURNED AIRCRAFT TO LAS. REMOVED AND REPLACED BYPASS DIFFERENTIAL PRESSURE SWITCH REF MM 793300. OPERATIONALLY CHECKS GOOD. - [SDR SCNA98100](https://openairdocs.org/sdr/SCNA98100.md): Wire · broken · Sep 1, 1998 · N275AF · Boeing 727227 · Landing Gear System Wiring > ON DESCENT HAD AN UNSAFE GEAR INDICATION ON THE RIGHT MAIN LANDING GEAR. FOLLOWED COM PROCEDURES AND LANDED UNEVENTFULLY. FOUND A BROKEN WIRE UNDERNEATH A CLAMP IN THE RIGHT MAIN WHEEL WELL. REPAIRED WIRE AND GEAR POSITION INIDCATING SYSTEM OPERATIONALLY CH - [SDR SCNA98050](https://openairdocs.org/sdr/SCNA98050.md): Light · inoperative · May 23, 1998 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE CHECK, FOUND AN EMERGENCY LIGHT OUT AT THE R1 DOOR EXIT. REMOVED AND REPLACED R1 DOOR EMERGENCY EXIT LIGHT ASSEMBLY AND OPERATIONALLY CHECKS GOOD. - [SDR SCNA98049](https://openairdocs.org/sdr/SCNA98049.md): Light · inoperative · May 23, 1998 · N275AF · Boeing 727227 · Emergency Lighting > DURING A LINE CHECK, FOUND THE EMERGENCY TRACK LIGHTING INOPERATIVE AT SEATS'S 5ABC, 28DEF AND 29DEF. REMOVED AND REPLACED THE EMERGENCY TRACK LIGHTING PIGTAILS AT SEATS 5ABC, 28DEF AND 29DEF. OPERATIONALLY CHECKS GOOD. - [SDR SCNA98700](https://openairdocs.org/sdr/SCNA98700.md): Web · cracked · May 2, 1998 · N275AF · Boeing 727227 · Fuselage Miscellaneous Structure > DURING A HEAVY MAINT CHECK, AT FUSE STA 1303 SECTION 48 CROWN WEB RT SIDE HAS 2 CRACK. CUT-OUT DAMAGE AREA IN ACCORANCE WITH B727 SRM 51-40-2. MATERIAL IS PER B727 SRM 53-10-2 FIG 6 AS 7075-T6.025C. FABRICATED DOUBLER FROM 7075-T6.032C IAW/B727 SRM 51-40- - [SDR SCNA98035](https://openairdocs.org/sdr/SCNA98035.md): Tr Valve · failed · Apr 15, 1998 · N275AF · Boeing 727227 · Engine Thrust Reverser > NUMBER THREE THRUST REVERSER OPERATION LIGHT ILLUMINATED AT APPROXIMATELY 1.95 EPR ON TAKEOFF ROLL. TAKEOFF ABORTED AT 60 KNOTS. REMOVED AND REPLACED THRUST REVERSER DIRECTIONAL VALVE PER MAINTENANCE MANUAL CHAPTER 783015, OPERATIONAL CHECK GOOD. - [SDR SCNA98034](https://openairdocs.org/sdr/SCNA98034.md): Tr Light · illuminated · Apr 8, 1998 · N275AF · Boeing 727227 · Engine Thrust Reverser > ON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED, ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL. - [SDR SCNA98033](https://openairdocs.org/sdr/SCNA98033.md): Tr Light · illuminated · Apr 8, 1998 · N275AF · Boeing 727227 · Engine Thrust Reverser > ON TAKEOFF ROLL, NUMBER THREE REVERSER LIGHT ILLUMINATED. ABORTED TAKEOFF. MEGGED WIRES BACK TO THRUST REVERSER SWITCH AND FUNCTIONALLY TESTED GOOD. SYSTEM OPERATIONAL CHECKS NORMAL. Next page: https://openairdocs.org/deregistered/N275AF-2003-06-12/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 n_number = 'N275AF' AND deregistration_id = 'N275AF-2003-06-12' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N275AF-2003-06-12/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.