N727NK

BOEING 727-212 · 1979 · Fixed-wing multi-engine · 3 engines · 170 seats · Valid Registration

Registered owner: ANTARES AVIATION LLC, FL (owner ≠ operator)

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.

92 reports on file, 2004-05-21 – 2013-01-31.

OTHER · 2013-01-31 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

LEFT BUTTLINE 55 SEAT TRACK HAS SEVERAL AREAS OF CORROSION BETWEEN STA 991 TO 1030.

Source: SDR R5KB2013013150398
OTHER · 2013-01-31 Matched by certificate designator
ATA 5347

Part: SUPPORT — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SEAT TRACK SUPPORT CORRODED AT LEFT BUTTLINE 45.5, STA 1090 TO 1110.

Source: SDR R5KB2013013150432
OTHER · 2013-01-31 Matched by certificate designator
ATA 5740

Part: PIN — CORRODED (RT WING) · airframe 42,419 hrs · 26,696 cycles

RIGHT WING AFT BOTTLE PIN CUP HAS EVIDENCE OF CORROSION UNDER PIN CUP.

Source: SDR R5KB46252
OTHER · 2013-01-31 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

CORROSION AROUND EDGE OF WALL AND FLOOR WEB AT STA 1148, RIGHT BUTTLINE 63.

Source: SDR R5KB2013013150368
OTHER · 2013-01-31 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

CORROSION AROUND PINS IN FLOOR WEB AT STA 1146 BETWEEN RIGHT BUTTLINE 54 AND 58.

Source: SDR R5KB2013013150369
OTHER · 2013-01-31 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

EVIDENCE OF CORROSION BETWEEN STA 950E AND 950E, STRINGER 15L.

Source: SDR R5KB2013013150258
OTHER · 2013-01-31 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SEAT TRACK CORRODED BETWEEN STA 800 TO 815, LEFT BUTTLINE 25.

Source: SDR R5KB2013013150349
OTHER · 2013-01-31 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

LEFT BUTTLINE 56, STA 344 SEAT TRACK CORRODED.

Source: SDR R5KB2013013150353
OTHER · 2013-01-31 Matched by certificate designator
ATA 7120

Part: MOUNT — CORRODED (NR 2 ENGINE) · airframe 42,419 hrs · 26,696 cycles

NR 2 ENGINE, UPPER FORWARD MOUNT ASSY CORRODED.

Source: SDR R5KB2013013150501
OTHER · 2013-01-31 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

INTERCOSTAL CORRODED AT STA 1060 STRINGER 20 LEFT.

Source: SDR R5KB2013013146411
OTHER · 2013-01-31 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

TOP CORD OF FLOORBEAM CORRODED ON FLOORBEAM AT STA 1110, LEFT BUTTLINE 24 TO 52.

Source: SDR R5KB2013013150363
OTHER · 2013-01-31 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

INTERCOSTAL AT STA 1060, LEFT BUTTLINE 26 AREA OF CORROSION.

Source: SDR R5KB46410
OTHER · 2013-01-28 Matched by certificate designator
ATA 5542

Part: PANEL — DELAMINATED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

LEFT UPPER RUDDER PANEL BETWEEN STA 212 AND 220 HAS ONE AREA OF DELAMINATION.

Source: SDR R5KB2013012850560
OTHER · 2013-01-28 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED STA 1166 BETWEEN STR 29 AND 30 LEFT.

Source: SDR R5KB2013012846435
OTHER · 2013-01-28 Matched by certificate designator
ATA 5420

Part: STRUCTURE — CRACKED (NR 1 PYLON) · airframe 42,419 hrs · 26,696 cycles

CRACK ON TOP OF NR 1 PYLON OUTBD FASTENER HOLE"P" OF S/B 727-54A0010R6, FROM HOLE TO OTBD EDGE OF LOWER ANGLE.

Source: SDR R5KB2013012846170
OTHER · 2013-01-28 Matched by certificate designator
ATA 5542

Part: SKIN — DAMAGED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

SKIN DAMAGED ON LOWER RUDDER LEFT SIDE BETWEEN STA 113-118.

Source: SDR R5KB2013012846281
OTHER · 2013-01-28 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOORBEAM CORRODED ON UPPER AND LOWER SURFACE AT STA 1110 LEFT BUTTLINE 1 TO RIGHT BUTTLINE 12.

Source: SDR R5KB2013012850439
OTHER · 2013-01-28 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 29 AND 30 LEFT.

Source: SDR R5KB2013012846405
OTHER · 2013-01-28 Matched by certificate designator
ATA 5542

Part: SKIN — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON LEFT SIDE OF UPPER RUDDER TRAILING EDGE BETWEEN RS 220 AND 242.

Source: SDR R5KB2012012846190
OTHER · 2013-01-28 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.

Source: SDR R5KB2013012846403
OTHER · 2013-01-28 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FRAME AT STA 1148 CORRODED AT STR 26R.

Source: SDR R5KB2013012846396
OTHER · 2013-01-28 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOOR TO SKIN WEB CRACKED, .25' AT EDGE OF LIGHTENING HOLE AT STA 490, RIGHT BUTTLINE 72.

Source: SDR R5KB2013012850324
OTHER · 2013-01-28 Matched by certificate designator
ATA 5542

Part: SKIN — DAMAGED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

UPPER RUDDER SKIN CORRODED RIGHT SIDE TRAILING EDGE BETWEEN STA 220-247.

Source: SDR R5KB2013012846194
OTHER · 2013-01-28 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FLOORBEAM CORRODED STA 1110 LEFT BUTTLINE 12 TO LEFT BUTTLINE 24 TOP AND BOTTTOM.

Source: SDR R5KB2013012850361
OTHER · 2013-01-28 Matched by certificate designator
ATA 5542

Part: SKIN — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON RIGHT SIDE OF UPPER RUDDER TRAILING EDGE AT RS 175.

Source: SDR R5KB2013012846287
OTHER · 2013-01-28 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STA 1110, BETWEEN STR 28 AND 29 LEFT.

Source: SDR R5KB2013012846406
OTHER · 2013-01-28 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED AT STATION 1130 BETWEEN STR 27 AND 28 LEFT.

Source: SDR R5KB2013012846404
OTHER · 2013-01-28 Matched by certificate designator
ATA 5544

Part: STRUCTURE — CORRODED (RUDDER) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON LEFT SIDE OF UPPER RUDDER BETWEEN STA 212 AND 220.

Source: SDR R5KB2013012846189
OTHER · 2013-01-28 Matched by certificate designator
ATA 5320

Part: WEB — CRACKED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

SUPPORT WEB CRACKED LEFT BUTTLINE 25 FROM STA 1130 TO 1110.

Source: SDR R5KB2013012850553
OTHER · 2013-01-28 Matched by certificate designator
ATA 5311

Part: FRAME — DAMAGED (FUSELAGE) · airframe 42,419 hrs · 26,696 cycles

FRAME DAMAGED AT STA 1130 BETWEEN STR 27 AND 28 RIGHT.

Source: SDR R5KB2013012850568
OTHER · 2013-01-03 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — DAMAGED (BS 950E) · airframe 42,419 hrs · 26,696 cycles

OTBD STRUCTURE AT DOOR FRAME, BS 950E DAMAGED AT STR 27R.

Source: SDR R5KB2013031150569
Earlier reports · 2004–2012 · 61 reports

2012

OTHER · 2012-12-29 Matched by certificate designator
ATA 5311

Part: DOUBLER — CORRODED (BS 1166) · airframe 42,419 hrs · 26,696 cycles

FRAME DOUBLER CORRODED AT BS 1166, BETWEEN STR 25L AND 25R.

Source: SDR R5KB2013031150559
OTHER · 2012-12-18 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (BS 990) · airframe 42,419 hrs · 26,696 cycles

WEB AT BS 990 CORRODED FROM RBL 27 TO RBL 29.

Source: SDR R5KB2013031150544
OTHER · 2012-12-16 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (BS 1130) · airframe 42,419 hrs · 26,696 cycles

CORROSION ON BOTTOM CORD OF FLOORBEAM AT STA 1130, LBL 28.

Source: SDR R5KB2013031150365
OTHER · 2012-12-14 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (BS 950B) · airframe 42,419 hrs · 26,696 cycles

FRAME AT BS 950B CORRODED ABOVE STR 28L.

Source: SDR R5KB2013031150525
OTHER · 2012-12-14 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 950F-960F) · airframe 42,419 hrs · 26,696 cycles

STRINGER 29L, CORRODED BETWEEN STA 950F AND 960F.

Source: SDR R5KB2013031146431
OTHER · 2012-12-14 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (BS 950E-960E) · airframe 42,419 hrs · 26,696 cycles

FLOOR SUPPORT, CORRODED BETWEEN STA 950E AND 960E AT STR 27R.

Source: SDR R5KB2013031146434
OTHER · 2012-12-12 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (BS 990) · airframe 42,419 hrs · 26,696 cycles

FRAME AT BS 990, RBL 22 AREA OF CORROSION.

Source: SDR R5KB2013031150428
OTHER · 2012-12-12 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 990) · airframe 42,419 hrs · 26,696 cycles

EVIDENCE OF CORROSION AT LOWER AFT CORNER CUTOUT STA 990, STR27R.

Source: SDR R5KB2013031146430
OTHER · 2012-12-12 Matched by certificate designator
ATA 5313

Part: STRINGER — CRACKED (BS 985 S29R) · airframe 42,419 hrs · 26,696 cycles

STRINGER 29R CRACKED AT BS 985.

Source: SDR R5KB2013031150504
OTHER · 2012-12-12 Matched by certificate designator
ATA 5330

Part: SKIN — CORRODED (BS 950E) · airframe 42,419 hrs · 26,696 cycles

SKIN CORRODED UNDER EDGE OF DOUBLER AT STA 950E, STR 27R.

Source: SDR R5KB2013031150507
OTHER · 2012-12-12 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 42,419 hrs · 26,696 cycles

SHEAR TIE CORRODED ON AFT SIDE STA 1148 BETWEEN STR 28R AND 29R.

Source: SDR R5KB2013031146390
OTHER · 2012-12-06 Matched by certificate designator
ATA 5310

Part: DOOR FRAME — CORRODED (BS 950F) · airframe 42,419 hrs · 26,696 cycles

DOOR FRAME AT BS 950F HAS AREA OF CORROSION ABOVE STR 27R ON WEB.

Source: SDR R5KB2013031150373
OTHER · 2012-12-04 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — CORRODED (BS 950F-970) · airframe 42,419 hrs · 26,696 cycles

INTERCOSTAL CORRODED AT STR 28R BETWEEN STA 950F AND 970.

Source: SDR R5KB2013031146428

2011

OTHER · 2011-01-27 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 720A) · airframe 42,109 hrs · 26,502 cycles

LT RAM AIR INLET LOWER FUSELAGE SKIN BULGED STA 720A. CORROSION FOUND AT STRINGER AT KEELBEAM.

Source: SDR 2011FA0000045
NO TEST · 2011-01-18 Matched by certificate designator
ATA 3350

Part: LIGHT — INOPERATIVE (CABIN)

EXIT LIGHT INOP ABOVE L2 DOOR.

Source: SDR 2011FA0000029
OTHER · 2011-01-13 Matched by certificate designator
ATA 5313

Part: STRINGER — CORRODED (BS 1013 S30R) · airframe 42,109 hrs · 26,502 cycles

STRINGER 30R CCORRODED ON LOWER SIDE AT BS 1013.

Source: SDR 2011FA0000026
OTHER · 2011-01-13 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (BS 420 S28L/R) · airframe 42,109 hrs · 26,502 cycles

SHEAR TIE CORRODED AT STA 420 BETWEEN STR 28L AND 28R.

Source: SDR 2011FA0000025

2010

NO TEST · 2010-02-26 Matched by certificate designator
ATA 3350

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 41,904 hrs · 26,374 cycles

CENTER CABIN EMERGENCY EXIT LIGHT INOP. REPLACED BATTERY PACK.

Source: SDR 2010FA0000187

2009

OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (BS 680) · airframe 41,363 hrs · 21,167 cycles

STA. 680, STR 23R TO 24R, FRAME DENTED

Source: SDR R5KB16005
OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

STA 660, STRINGER 24R, FRAME DENTED.

Source: SDR R5KB16004
OTHER · 2009-01-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

STA 1130, RBL 51, FLOORBEAM CHORD CORRODED.

Source: SDR R5KB16027
OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FRAME AT STATION 950 DENTED.

Source: SDR R5KB15650
OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

STA 340, RBL 19 TO RBL24, FRAME CORRODED

Source: SDR R5KB15983
OTHER · 2009-01-11 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

RBL 16, STA 350, BILGE AREA, LOWER CHORD CORRODED.

Source: SDR R5KB15862
OTHER · 2009-01-11 Matched by certificate designator
ATA 5322

Part: SHEAR TIE — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SHEAR TIE CORRODED STA 350 FROM RBL 19 TO RBL 24.

Source: SDR R5KB15982
OTHER · 2009-01-11 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

UPPER FLOORBEAM CORRODED FS 1070, LBL 56.

Source: SDR R5KB15798
OTHER · 2009-01-11 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

LBL 44, SEAT TRACK CROWN CORRODED FROM STA 760 TO 848.

Source: SDR R5KB15756
OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

1/2 INCH CRACK IN FRAME AT STA 580 ABOVE FWD SERVICE DOOR.

Source: SDR R5KB15789
OTHER · 2009-01-11 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FRAME AT STA 26 LEFT DENTED.

Source: SDR R5KB15651
OTHER · 2009-01-09 Matched by certificate designator
ATA 5520

Part: HINGE — CORRODED (ELEVATOR) · airframe 41,363 hrs · 21,167 cycles

TOP OF ELEVATOR HINGE CHORD CORRODED FROM STA 70 THRU 170.

Source: SDR R5KB15752
OTHER · 2009-01-09 Matched by certificate designator
ATA 5311

Part: FRAME — DENTED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FRAME AT STATION 950 DENTED.

Source: SDR R5KB15652
OTHER · 2009-01-01 Matched by certificate designator
ATA 5320

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

'T' CHORD AT STA 350 CORRODED.

Source: SDR R5KB15981

2008

OTHER · 2008-12-20 Matched by certificate designator
ATA 5320

Part: BEAM — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

LOWER BEAM CORRODED.

Source: SDR R5KB15950
OTHER · 2008-12-20 Matched by certificate designator
ATA 3270

Part: BEAM — CORRODED (TAIL SKID) · airframe 41,363 hrs · 21,167 cycles

TRANSVERSE BEAM AT TAIL SKID CORRODED.

Source: SDR R5KB15914
OTHER · 2008-12-20 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SUB FLOOR CORRODED

Source: SDR R5KB15776
OTHER · 2008-12-20 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FLOOR BEAM UPPER CHORD CORRODED AT NUTPLATE.

Source: SDR R5KB15927
OTHER · 2008-12-20 Matched by certificate designator
ATA 3270

Part: ANGLE — CORRODED (AUX GEAR) · airframe 41,363 hrs · 21,167 cycles

VERTICAL ANGLE CORRODED.

Source: SDR R5KB15916
OTHER · 2008-12-20 Matched by certificate designator
ATA 3270

Part: BEAM — CORRODED (TAIL SKID) · airframe 41,363 hrs · 21,167 cycles

TAIL SKID TRANSVERSE BEAM FWD ATTACH ANGLE CORRODED.

Source: SDR R5KB15945
OTHER · 2008-12-20 Unresolved
ATA 5320

Part: WEB — CORRODED (BS 1213) · airframe 41,363 hrs · 21,167 cycles

WEB CORRODED AT BS 1213 WL 177 RBL 5.

Source: SDR R5KB20081220001
OTHER · 2008-12-20 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FLOOR SUPPORT CORRODED.

Source: SDR R5KB15936
OTHER · 2008-12-20 Matched by certificate designator
ATA 5320

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

HAT CHANNEL CORRODED

Source: SDR R5KB15774
OTHER · 2008-12-19 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FLOOR SUPPORT EXTRUSION CORRODED.

Source: SDR R5KB15804
OTHER · 2008-12-19 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SUBFLOOR WEB CORRODED AFT LAV.

Source: SDR R5KB15807
OTHER · 2008-12-19 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CORRODED.

Source: SDR R5KB15791
OTHER · 2008-12-19 Matched by certificate designator
ATA 5260

Part: WEB — CRACKED (STAIRS) · airframe 41,363 hrs

VERTICAL WEB CRACK AT LIGHTNING HOLE.

Source: SDR R5KB15838
OTHER · 2008-12-19 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CORRODED.

Source: SDR R5KB15803
OTHER · 2008-12-19 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

UNDER FLOOR WEB CORRODED.

Source: SDR R5KB15808
OTHER · 2008-12-19 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK FLANGE CORRODED.

Source: SDR R5KB15825
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK FLANGE CORRODED.

Source: SDR R5KB15781
OTHER · 2008-12-18 Matched by certificate designator
ATA 5330

Part: SKIN — DENTED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

DENT IN SKIN STA 328 ABOVE FWD ENTRY DOOR

Source: SDR R5KB15546
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CORRODED.

Source: SDR R5KB15782
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CORRODED.

Source: SDR R5KB15795
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CROWN CORRODED.

Source: SDR R5KB15779
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CROWN CORRODED.

Source: SDR R5KB15784
OTHER · 2008-12-18 Matched by certificate designator
ATA 5315

Part: SEAT TRACK — CORRODED (BS 1130) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CORRODED BS 1130.

Source: SDR R5KB081218001
OTHER · 2008-12-18 Matched by certificate designator
ATA 5520

Part: HINGE FITTING — CORRODED (ELEVATOR) · airframe 41,363 hrs · 21,167 cycles

ELEVATOR UPPER HINGE CORD CORRODED.

Source: SDR R5KB15750
OTHER · 2008-12-18 Matched by certificate designator
ATA 5347

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

SEAT TRACK CROWN AND FLANGE CORRODED

Source: SDR R5KB15785
OTHER · 2008-12-18 Matched by certificate designator
ATA 5315

Part: FLOORBEAM — DAMAGED (FUSELAGE) · airframe 41,363 hrs · 21,167 cycles

FLOORBEAM WEB DAMAGED BELOW UPPER CHORD, STA 460, RBL-25.

Source: SDR R5KB15678

2007

OTHER · 2007-10-27 Matched by certificate designator
ATA 5720

Part: STIFFENER — CORRODED (LT WING) · airframe 41,341 hrs · 26,026 cycles

LEFT WING REAR SPAR VERTICAL STIFFENER CORRODED AT LOWER END W.S. 200

Source: SDR 5700

2005

OTHER · 2005-09-22 Unresolved
ATA 2497

Part: WIRE — BURNED (FWD GALLEY)

DURING FLIGHT, ALL 8 RT READING STATION CB`S POPPED SIMULTANEOUSLY. PA INOPERATIVE ALL STATIONS. NO SMOKING CB POPPED, PASSENGER AND CREW CALL CB POPPED. ATTEMPTED TO RESET CB`S IAW AOM PROCEDURES. CB`S IMMEDIATELY POPPED. DID NOT ATTEMPT TO RESET, AGAIN. ON POST FLIGHT INSPECTION FOUND 28V DC BATTERY CHARGER CB POPPED. REPLACED APPROXIMATELY 80 BURNED WIRE SEGMENTS BEHIND FWD GALLEY BY DOUBLE SPLICING IAW SWP 20-30-12 AND REPAIRS IAW SWP 20-10-13. ALL SYSTEMS OPS CHECKED GOOD IAW MM. (K)

Source: SDR MYW2006F00000

2004

NO TEST · 2004-05-21 Unresolved
ATA 3350

Part: POWER SUPPLY — WEAK (L2 DOOR)

DURING PREFLIGHT TRANSIT FOUND WHITE EMERGENCY DOOR LIGHTS AT L-2 AFT DOOR VERY WEAK. REMOVED AND REPLACED POWER SUPPLY BATTERY CHARGER ASSY. OPS CHECK OK IAW MM 33-50-02. (SDR040010)

Source: SDR MYW2004F00003