N273AT
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
28 reports on file, 1995-09-23 – 2014-08-09.
Part: LENS — LOOSE (CABIN) · airframe 300,250 hrs · 13,322 cycles
L1 DOOR LOWER EXIT LENS COVER LOOSE. R & R LIGHT ASSEMBLY IAW AMM.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 29,924 hrs · 13,284 cycles
FORWARD EXIT LIGHT INOPERATIVE. R & R LIGHT ASSEMBLY IAW MM.
Earlier reports · 1995–2013 · 26 reports
2013
Part: BATTERY PACK — INOPERATIVE (CABIN) · airframe 26,528 hrs · 11,935 cycles
LT EMERGENCY LIGHT BATTERY PACK ASSEMBLY INOPERATIVE AT STATION 727. R&R BATTERY PACK ASSEMBLY IAW MM.
Part: ROD END — CORRODED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
STATION 1016 STABILIZER TRIM ACCESS DOOR 311AL HOLD OPEN ROD END CORRODED. R&R ROD END IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
INTERCOSTAL CRACKED BETWEEN STATION 312 TO STATION 328, RBL 31. R&R INTERCOSTAL IAW SRM.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
INTERCOSTAL CRACKED BETWEEN STATION 312 TO STATION 328, LBL 45. R&R INTERCOSTAL IAW SRM & DRAWING.
Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
R1 CORD CORRODED BETWEEN STATION 303 TO STATION 328. R&R CHORD IAW SRM.
Part: WEB — CORRODED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
FWD CARGO DOOR CUTOUT DOOR SEAL WEB CORRODED. R&R WEB IAW SRM & DRAWING.
Part: CREASE BEAM — CRACKED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
R1 DOOR CUTOUT CREASE BEAM INNER CORD CRACKED AT STATION 310. R&R CLIP IAW SRM & DRAWING.
Part: SILL — CORRODED (FUSELAGE) · airframe 26,528 hrs · 11,935 cycles
C2 CUTOUT LOWER SILL WEB CORRODED BETWEEN STATION 807 TO STATION 840. R&R WEB IAW SRM & DRAWING.
Part: SLIDE — DAMAGED (L1 DOOR) · airframe 26,528 hrs · 11,935 cycles
L1 DOOR EMERGENCY EVAC SLIDE GIRT PROTECTIVE RUBBER LAMINATE TORN, FRAYED & DISBONDED. R&R SLIDE IAW MT.
Part: PIN — MISSING (EVAC SLIDE) · airframe 26,528 hrs · 11,935 cycles
L2 DOOR EMERGENCY EVAC SLIDE SAFETY PIN MISSING. INSTALLED PIN IAW AMM.
Part: BATTERY — DISCHARGED (CABIN) · airframe 26,857 hrs · 12,056 cycles
EMERGENCY LIGHT ABOVE R1 DOOR INOP. R & R BATTERY IAW AMM.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 26,003 hrs · 11,711 cycles
AFT EMERGENCY FLASHLIGHT INOP. REMOVED AND REPLACED FLASHLIGHT PER MM.
2012
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 25,586 hrs · 11,543 cycles
F/A EMERGENCY FLASHLIGHT NOT BLINKING ON INBOUND AFT FLASHLIGHT. REMOVED AND REPLACED BATTERY IAW AMM, OPS CHECK GOOD.
Part: COVER — DAMAGED (R1 DOOR) · airframe 25,192 hrs · 11,380 cycles
R1 DOOR SLIDE COVER DAMAGED. REPLACED R-1 DOOR SLIDE COVER ASSY PER AMM 25-61.
Part: SLIDE — UNWANTED DEPLOY (R1 DOOR) · airframe 25,192 hrs · 11,380 cycles
R1 SLIDE DEPLOYED BY CATERING TRUCK. INSTALLED R-1 SLIDE ASSY PER AMM 25-61.
Part: LEAD — OUT OF POSITION (EVAC SLIDE) · airframe 25,180 hrs · 11,374 cycles
CONNECTOR SHOWING AT BOTTOM OF R1 EMERGENCY SLIDE. PERFORMED VISUAL INSPECTION OF SLIDE PACK, RESTOWED BATTERY TEST LEAD PER AMM.
Part: HOLDER — LOOSE (GIRT BAR) · airframe 25,138 hrs · 11,357 cycles
R1 DOOR EMERGENCY EVAC SLIDE GIRT BAR HOLDER LOOSE. SECURED HOLDER PER MM.
2011
Part: FLOORBEAM — CORRODED (FUSELAGE)
FLOORBEAM, STA 678, RBL 45, CORROSION. ACCOMPLISHED FLOORBEAM REPAIR PER B737 SRM 51-70-12.
Part: SEAT TRACK — CORRODED (FUSELAGE)
SEAT TRACK, STA 540 TO 727, RBL 48, CORROSION. ACCOMPLISHED SEAT TRACK REPLACEMENT PER B737 SRM 53-00-52 AND 51-20-01.
Part: BATTERY PACK — DISCHARGED (CABIN)
THE 22DEF TO AFT RT EMERGENCY LIGHTS FAIL T/C 33-055-00-01. REMOVED AND REPLACED MO1672 AFT RT BATTERY PACK IAW MM 33-51. OPS CHECK OK T/C 33-055-01 CHECKS OK.
Part: COVER — MISSING (CABIN)
A/C RIGHT FWD BUSINESS CLASS EMERGENCY LIGHT STRIP NEON COVERING MISSING. REPLACED RIGHT FWD FLOOR STRIP AS PER AMM 33-31.
2009
Part: BATTERY — DISCHARGED (CABIN)
EPL WILL NOT CHARGE DUE TO CABIN LIGHTS BEING INOP. FAILED TO CHARGE DURING F/A PREFLIGHT CKS. CHARGED EPL. REF MM 33-51. OK FOR SERVICE.
2007
Part: WIRE HARNESS — ARCED (NR 1 GENERATOR)
ON ROUTINE INSPECTION FOUND NR 1 GENERATOR FEEDER CABLE ARCED, FAN COWL CENTER FITTING HAS BURN MARKS FROM ARCING. REMOVED AND REPLACED GENERATOR HARNESS ASSY.
Part: FEEDER CABLE — ARCED (NR 1 GENERATOR)
ON ROUTINE INSPECTION FOUND NR 1 GENERATOR FEEDER CABLE ARCED, FAN COWL CENTER FITTING HAS BURN MARKS FROM ARCING. REMOVED AND REPLACED FAN COWL O/B.
2005
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT)
EXTERIOR EMERGENCY LIGHT INOP LEFT AFT LOWER. REMOVED AND REPLACED LAMP IAW MM 33-51, OPS CHECKS GOOD.
1995
Part: FITTING — CRACKED (PWR BRAKE VLV)
ORD - FLT NR 4246 - LOW LEVEL HYDRAULIC GREEN SIDE IN FLIGHT. AIRCRAFT RETURNED TO ORD AND LANDED WITHOUT INCIDENT. FOUND FITTING GOING TO THE INLET PORT OF DUAL POWER BRAKE VALVE CRACKED. REMOVED AND REPLACED NR 6 FITTING AT VALVE. OPS AND LEAK CHECKS GOOD. AIRCRAFT RETURNED TO SERVICE. (M)