N658GT
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.
84 reports on file, 2015-03-05 – 2020-09-25.
Part: FAILSAFE — CRACKED (BS 955) · airframe 60,994 hrs · 45,516 cycles
LT FAIL SAFE STRAP AT STA 955 LOWER FASTENER HOLE CRACKED. PERFORMED CUT OUT OF FAILSAFE STRAP, IAW BSB SB 53-A0100 FIG 15 + ATLAS 6753A070 (EO).
Part: STRUCTURE — CORRODED (BS 1375-1417) · airframe 60,994 hrs · 45,516 cycles
CORROSION FOUND BETWEEN 1375 AND 1417 S35R-36R. BLENDED CORROSION AND REPAIRED, IAW AMES DOC 47416 REA 13.
Part: STRINGER — CORRODED (BS 196.5) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORRODED STRINGER. REMOVED DAMAGE IAW DOCUMENT 47416 REA04.
Part: PANEL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON BULGE PANEL. REMOVED CORROSION ON BULGE PANEL IAW B767 SRM 53-60-53.
Part: WEB — CORRODED (BS 544) · airframe 60,994 hrs · 45,516 cycles
FLC FLOOR WEB CORROSION AT STA 544 RBL 32. REMOVED AND REPLACED WEB, IAW 51-40-03 AND BOEING DRAWING 143T5200.
Part: SKIN — CORRODED (BS 1395) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
BULGE IN SKIN (CORROSION). REPAIRED SKIN IAW REA 47416 REA 02.
Part: SKIN — CORRODED (LT WING LE) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORRODED LEADING EDGE SKIN PANEL. REPAIRED IAW REA 47416 REA 04.
Part: SKIN — DAMAGED (BS 676) · airframe 60,994 hrs · 45,516 cycles
FUSELAGE SKIN CREASED AT STA 676 STRINGER 7L. REPAIRED SKIN, IAW AMES DOC 47416 REA 17.
Part: SPLICE — CORRODED (RT WING) · corrosion level 2 · airframe 60,994 hrs · 45,526 cycles
CHORD SPLICE CORRODED. REPLACED CHORD SPLICE, IAW B767 SRM 51-40-02.
Part: STRINGER CLIP — CORRODED (BS 1502) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON STR 21R AND STA 1502 STRINGER CLIP. REMOVED CORROSION FROM 21R AND STA 1522 STRINGER CLIP. REPLACED CLIP, IAW B767 SRM 53-00-03 AND 51-40-02.
Part: SKIN — BENT (BS 259.06) · airframe 60,994 hrs · 45,516 cycles
SKIN BENT AND CREASED. REPAIRED IAW REA 47416 REA 06.
Part: SKIN — CORRODED (WING LE) · airframe 60,994 hrs · 45,516 cycles
CORROSION FOUND LE WING AT LES 897. REPAIRED CORROSION, IAW B767 SRM 57-41-13-2R-1 REPAIR 1.
Part: STRINGER CLIP — CORRODED (BS 740) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
STRINGER CLIP AND FRAME WEB CORROSION. REPLACED STRINGER CLIP AND FRAME WEB, IAW B767 SRM 51-40-02 PG 2.
Part: SKIN — CORRODED (BS 783) · airframe 60,994 hrs · 45,516 cycles
CORROSION ON INTERNAL FUSELAGE SKIN STA 783.5, 13R. REPAIRED IAW REA 47416 REA10.
Part: STIFFENER — CORRODED (BS 1380-1410) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
SKIN STIFFNER CORRODED BEYOND LIMITS AT STA 1380 TO STA 1410, STR 35R-36R. REPAIRED IAW B767 SRM 53-00-03 DETAIL 2.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
LT WING UPPER SKIN PANEL CORRODED. REPAIRED CORROSION IAW AMES 47416REA16.
Part: STRUCTURE — CRACKED (BS 287) · airframe 60,994 hrs · 45,516 cycles
CRACKED CHORD. REPAIRED CHORD, IAW B767 SRM 51-70-12.
Part: SKIN — CORRODED (BS 783) · airframe 60,994 hrs · 45,516 cycles
FUSELAGE SKIN CORROSION AT STA 783 STR 12R. REMOVED CORROSION AND REPAIRED, IAW AMES DOC 47416REA10.
Part: SKIN — CORRODED (RT WING) · airframe 60,994 hrs · 45,676 cycles
CORRODED WING SKIN. REPAIRED IAW REA 47416 REA 20.
Part: STRINGER — CORRODED (BS 1285) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
STRINGER AT 35R IN ALC IS CORRODED STA 1285. REPAIRED STRINGER ON 35R IN ALC STA 1285, IAW B767 SRM 51-40-02 REPAIR 2 AND 53-00-03.
Part: STRINGER — CORRODED (BS 1298-1305) · airframe 60,994 hrs · 45,516 cycles
STRINGER 38R IS CORRODED BETWEEN 1285 AND 1307. REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIRED SECTION, IAW B767 SRM 53-00-03 REPAIR 2.
Part: FITTING — GOUGED (NR 2 NACELLE) · airframe 60,994 hrs · 45,516 cycles
NR 2 PYLON INBOARD SIDE LOAD FITTING IS GOUGED BEHIND PANEL 447. BLENDED GOUGE ON NR 2 PANEL INBOARD REPAIRED, IAW DOC 47416 REA 03.
Part: SKIN — CORRODED (BS 785) · airframe 60,994 hrs · 45,516 cycles
CORROSION ON SKIN. REPAIRED SKIN DAMAGE IAW 47416 REA15.
Part: FAILSAFE — CRACKED (BS 955) · airframe 60,994 hrs · 45,516 cycles
2 EA LOWER BOLT HOLES CRACKED ON RT FAIL SAFE STRAP STA 955 RBL 98. PERFORMED CUT OUT ON FAIL SAFE STRAP, IAW SB 53-A0100 FIG 15 AND ATLAS EO 6753A070.
Part: SUPPORT BRACKET — CORRODED (BS 1310-1323) · airframe 60,994 hrs · 45,516 cycles
ANTENNA AND SUPPORT CORROSION STA 1310 TO 1323. REPLACED CHIP AND SUPPORT BRACKET, REPAIRED IAW 52-60-53.
Part: STRUCTURE — CORRODED (SLAT) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORRODED SLAT. REPLACED SLAT, IAW B767 AMM 27-81-02.
Part: SKIN — CORRODED (BS 783) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON INTERNAL SKIN STA 783 ABOUT STRINGER 13L. REMOVED CORROSION AND REPLACED SKIN, IAW AMES DOC 47416 REA 49.
Part: TEE FITTING — CORRODED (LT MLG WW) · airframe 60,994 hrs · 45,516 cycles
LT WHEEL WELL STA 955 LBL 97 "T" FITTING HAS CORRSION ON RACK AFT OF LT WHEEL WELL. CORRODED "T" ANGLE FOUND TO BE OUT OF LIMITS, IAW SB 767 53A0100 STEP 9. INSTALLED NEW ANGLE ON EO NR 6753A070 STEP NR 11.
Part: ANGLE — CORRODED (BS 955) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
LT WHEEL WELL STA 955 LBL 97 HAS ANGLE CORRODED BEYOND LIMITS, PER SB767 53A0100. NEW ANGLE TO BE INSTALLED ON EO NR 6753A070 STEP 11.
Part: STIFFENER — CORRODED (BS 1380-1410) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
SKIN STIFFENER CORRODED BEYOND LIMITS, STA 1380 TO 1410, STR 35R-STR 36R. REPAIRED IAW B767 SRM 53-00-03 DETAIL 2.
Part: BRACKET — CORRODED (BS 1310-1323) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
WHILE WORKING NR0736, FOUND HF ANTENNA SUPPORT STRUCTURE CORRODED. REMOVED ANTENNA AND SUPPORT STRUCTURE. CHIP AND SUPPORT BRACKET WERE FOUND TO BE OUT OF LIMITS. REPLACED CLIP AND SUPPORT BRACKET. REINSTALLED ANTENNA AND SUPPORT STRUCTURE. ALL IAW B767 SRM 51-40-02 PH 4,7, 53-60-53, AMM 23-12-03-424-007.
Part: FAILSAFE — CRACKED (BS 955) · airframe 60,994 hrs · 45,516 cycles
LOWER 2 BOLT HOLES CRACKED ON RT FAIL SAFE STRAP. PERFORMED FAIL SAFE STRAP CUT OUT, IAW SB 53-A0100 AND ATLAS EO NR 6753A070.
Part: WEB — CORRODED (BS 544) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
FLC STA. 544, RBL 32 TOP OF FLOOR WEB IS CORRODED. REMOVED AND REPLACED WEB, IAW B767 51-40-03 AND BOEING DWG 143T5000.
Part: SKIN — CORRODED (WING) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION FOUND ON LEADING EDGE OF WING UNDER PNL 521ZB AT LES 897.00 UNDER 2 NUTPLATES. PERFORMED B767 SRM 57-41-13-2R-1 REPAIR 1 TO REPAIR CORROSION AT WING LES 897.00 THAT WAS 100% EXFOLIATED ON LEADING EDGE OF WING STATION PNL 521ZB.
Part: FAILSAFE — CRACKED (BS 955) · airframe 60,994 hrs · 45,516 cycles
LOWER FASTENER HOLE CRACKED ON LEFT FAIL SAFE STRAP STA 955. PERFORMED CUT OUT ON FAIL SAFE STRAP, IAW SB 53-A0100 FIG 15 AND ATLAS EO NR 6753A070.
Part: SKIN — CORRODED (BS 785) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON SKIN AT FASTENER FS 785 STR 38R. REMOVED CORROSION FROM SKIN AT FS 785 STR 38, IAW B767 200 SRM 53-00-01 FIG 1 DET II WITH ORIG MAT 0.150", MAT LOSS 0.052". FOUND TO BE OUT OF LIMITS, IAW B767 200 SRM 53-00-01. REPAIRED SKIN DAMAGE IAW 47416REA15.
Part: STRUCTURE — CRACKED (BS 173-287) · airframe 60,994 hrs · 45,516 cycles
NWW RIGHT HAND STA 287 RBL 25 VERT CHORD CRACKED NEXT TO FASTENER HEAD. REPAIR CHORD IAW BOEING 767 SRM, IAW BOEING 767 SRM 51-70-12 FIG 1 SHEET 1-7. SEE PARTIAL WORK ACCOMPLISHED AND PARTIAL SHEET 10 AND BOEING DRAWING 141T2938.
Part: SKIN — CORRODED (BS 783) · airframe 60,994 hrs · 45,516 cycles
CORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13R. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12R, IAW B767 200 SRM 53-00-01 AD 1. WITH 0.027" MAT LOSS, DAMAGE EXCEEDED 15% ALLOWED & FOUND TO BE OUT OF LIMITS. REPAIRED DAMAGE IAW REA NO 47416REA10.
Part: SKIN — CORRODED (BS 1375-1417) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION FOUND BETWEEN FS 1375 AND 1417 STR 35R AND 36R. BLENDED CORROSION BETWEEN STA 1375 TO 1417 STR 35R TO 36R. ORIGINAL THICKNESS .074", REMOVED .041", REMAINING T .033" FOUND TO BE OUT OF LIMITS. REQUESTED ENGINEERING SUPPORT. RECEIVED AMES DOC 47416REA13 FOR REPAIR. OUT OF LIMITS, IAW B767 200 SRM 53-00-01. REPAIRED IAW AMES DOC 47416REA13.
Part: STRINGER — CORRODED (BS 1285) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
STRINGER 35R IN ALC IS CORRODED AT STA 1285. CUT OUT AND REPAIR DAMAGED SECTION STR 35R IN ALC AT STA 1285 DUE TO EXFOLIATION CORROSION ALL, IAW B767 SRM 51-40-02 & 53-00-03 REPAIR 2.
Part: FITTING — GOUGED (NR 2 NACELLE) · airframe 60,994 hrs · 45,516 cycles
NR 2 PYL INBOARD SIDE LOAD FITTING IS GOUGED BEHIND PANEL 447AL. MARKED. BLENDED GOUGE ON NR 2 PYLON INBOARD SIDE LOAD FITTING. NOMINAL .500, REMOVED .134 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-20-90 AD 1. REPAIRED AREA IAW AMES DOC 47416REA03.
Part: SKIN — CORRODED (BS 783) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON INTERNAL FUSELAGE SKIN STA 783 ABOVE STRINGER 13L RUNNING NEXT TO TEAR STRAP. REMOVED CORROSION FROM INTERNAL FUSELAGE SKIN AT STA 783 ABOVE STR 12L, IAW B767-200 SRM 53-00-01 AD1. WITH 0.002" MAT LOSS, DAMAGE FOUND TO BE BEYOND 15% ALLOWED AND BEYOND LIMITS. REPAIRED DAMAGE IAW REA NO 47416REA49.
Part: SKIN — CORRODED (BS 1395) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
BULGE IN SKIN AT FS 1395 AND STR 35L. REPAIRED SKIN AT FS 1395 S35L, IAW AMES REA 47416 REA 02 AND B767 SRM 53-00-01 REPAIR 12.
Part: STRINGER CLIP — CORRODED (BS 1502) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON STR 21R JUST AFT OF FUS STA 1502. REMOVED CORROSION FROM S21R AND STA 1502 STRINGER CLIP. 100% MATERIAL LOSS. MATERIAL IS FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-03 ADI. REPLACED STRINGER CLIP IAW B767 SRM 51-40-02 PG 7.
Part: SKIN — DAMAGED (BS 676) · airframe 60,994 hrs · 45,516 cycles
FUSELAGE SKIN IS CREASED AT STA 676 STRINGER 7L. FUSELAGE SKIN CREASED AT STA 676 7L FOUND TO BE OUT OF LIMITS, IAW B767 SRM 53-00-01 DETAIL III. REPAIRED AREA IAW AMES DOCUMENT #47416REA17.
Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 60,994 hrs · 45,516 cycles
NR 1 PYL INBOARD SKIN IS BENT AND CREASED AT NAC STA 240. MARKED NR 1 PYLON INBOARD SKIN AT NAC STA 240, FOUND TO BE OUT OF LIMITS IAW B767 SRM 54-51-01. ALLOWABLE DAMAGE 1 DETAIL III. REPAIRED BLENDED AREA, IAW REA NR 47416REA06.
Part: SKIN — DELAMINATED (RT WING) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
RIGHT WING UPPER TRAILING EDGE SKIN PANELS AT STA 798 AND 906 NEAR OUTBOARD FLAP OUTBOARD AREA AND NEAR NR 12 SPOILER BOARD, HAVE AREAS WITH SKIN BULGING AND FASTENERS PULLING THRU SKIN. REMOVED AND REINSTALLED RT WING TRAILING EDGE UPPER SKIN PANEL AFTER COMPOSITE REPAIR, IAW B767 SRM 51-40-02 PARAGRAPH 4, 5, AND 9 AT STA 798-906. COMPLIED WITH REA 47416REA20 TO REMOVE CORROSION UNDER BULGING SKIN.
Part: ANGLE — CORRODED (RT NR 8 SLAT) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
RIGHT WING NR 8 SLAT CORRODED AT THE TIA ATTACH POINT TO SLAT. BLENDED CORROSION ON CHORD SPLICE ANGLE ON NR 8 SLAT AT TAI ATTACH POINT. REMOVED .020 FROM NOMUAL .100 FOUND TO BE OUT OF LIMITS, IAW B767 SRM 57-43-02 FIG 101 DETAIL V. REMOVED AND REPLACED ANGLE, IAW B767 SRM 51-40-02 PARA 7.
Part: SKIN — CORRODED (BS 196.5) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
DEFORMITY IN THE SKIN LEFT OF NLG DOOR ON FS 188.5 10" FROM DOOR OPENING. REMOVED DAMAGE AT STA 196.5 10" FROM DOOR OPENING AND REPAIRED, PER AMES DOCUMENT 47416REA07.
Part: STRINGER — CORRODED (BS 1298-1305) · airframe 60,994 hrs · 45,516 cycles
ALC STRINGER 38R IS CORRODED BETWEEN STA 1285 AND 1307. STRINGER CORROSION AT 39R IS FOUND TO BE EXFOLIATED COMPLETELY THROUGH. REMOVED DAMAGED STRINGER SECTION AND INSTALLED REPAIR SECTION, IAW B767 SRM 53-00-03 REPAIR 2.
Part: WEDGE — CORRODED (RT NR 9 SLAT) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
RIGHT WING NR 9 SLAT UPPER WEDGE INNER IS CORRODED IN SEVERAL AREAS. NR 9 SLAT FOUND TO BE CORRODED BEYOND REPAIRABLE LIMITS. REMOVED AND REPLACED NR 9 SLAT WITH SERVICEABLE UNIT, IAW B767 AMM 27-81-02 PARA 3, H.
Part: SKIN — CORRODED (BS 783) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORROSION ON INTERNAL FUSELAGE SKIN AT BS 783, STRINGER 13 RIGHT.
Part: FRAME — CORRODED (BS 740) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
STRINGER CLIP AND FRAME WEB CORROSION.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
CORRODED LEADING EDGE SKIN PANEL.
Part: PANEL — CORRODED (BS 1329-1351) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
BILGE PANEL CORRODED.
Part: SKIN — CORRODED (LWS 433-438) · corrosion level 2 · airframe 60,994 hrs · 45,516 cycles
LT WING UPPER SKIN PANEL.
Earlier reports · 2015–2019 · 28 reports
2019
Part: SKIN — DENTED (BS 246) · airframe 59,622 hrs · 44,718 cycles
DENT AT R/H STA 246 BUTT SPLICE, BETWEEN S-32 AND 33 R.&NBSP;(<P>REPAIRED DAMAGED AREA I.A.W. EA #190058. REMOVED DAMAGED CHORD AT STA 246 S-32 - 33R AND INSTALLED NEW PART I.A.W. B757-200 SRM 51-40-02.</P>)
Part: SEAL — DAMAGED (RT OVERWING DOOR) · airframe 59,622 hrs · 44,718 cycles
R/H OVER WING DOOR SEAL DAMAGE.(<P>INSPECTED R/H OVER WING DOOR. FOUND DOOR SEAL OUT OF RETAINER. INSTALLED SEAL IN RETAINER&NBSP; I.A.W. B767 AMM 52-09-03.</P>)
Part: POUCH — TORN (OXYGEN MASK) · airframe 59,622 hrs · 44,718 cycles
L1 ENTRY WAY OXYGEN MASKS PROTECTIVE POUCH IS TORN AND ARE NO LONGER SERVICEABLE.&NBSP;(<P>R/R L1 ENTRY WAY OXYGEN MASKS PROTECTIVE POUCH I.A.W AMM 25-60-00.&NBSP;</P>)
Part: D-RING — MISSING (ESCAPE HARNESS) · airframe 59,622 hrs · 44,718 cycles
ESCAPE HARNESS MISSING "D" RING.(<P>NEW HARNESS INSTALLED I.A.W. B767 SFMM 25-61-03 TASK 25-25-01-402-803.</P>)
Part: BOOT — INADEQUATE (SMOKE DETECTOR) · airframe 59,622 hrs · 44,718 cycles
AFT CARGO COMPARTMENT, FWD SECTION NEAR WHERE L1 IS STENCILED ON CEILING PANEL, RUBBER BOOT OF SMOKE DETECTOR ORFICE IS FLUSH WITH PANEL. EITHER NEEDS A LONGER BOOT OR THE CEILING IS NOT FASTENED TO THE OVERHEAD FRAME. MARKED WITH STREMER A5/044.(<P>REMOVED, RE-POSITIONED, AND REINSTALLED AFT CARGO COMPARTMENT FWD SECTION NEAR L1 STENCILED IN CEILING PANEL I.A.W B767 AMM 25-52-02-004-001 AND AMM 25-52-02-404-006.</P>)
Part: SEAL — DAMAGED (LT OVERWING DOOR) · airframe 59,622 hrs · 44,718 cycles
L/H OVER WING DOOR SEAL DAMAGED.(<P>DAMAGE REPAIRED ON L/H OVER-WING DOOR SEAL I.A.W B767 AMM 52-09-00-358-053.</P>)
Part: CONNECTOR — DAMAGED (OXYGEN MASK) · airframe 59,622 hrs · 44,718 cycles
CAPTAIN'S OXYGEN MASK ELECTRICAL CONNECTOR IS MISSING BACK-SHELL STRAIN RELIEF AND MISSING EDGE PROTECTION FOR SCREWS.&NBSP;(<P>REPAIRED CAPTAIN OXYGEN MASK BACK-SHELL I.A.W SWPM 20-00-11. OPS CHECK GOOD AMM 35-11-00-715-256.</P>)
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 59,622 hrs · 44,718 cycles
EMERGENCY EXIT SIGN AT L1 DOOR (L312) IS INOP.(<P>DURING T/S, FOUND BAD POWER SUPPLY AT L1 POSITION. REMOVED AND REPLACED L1 POWER SUPPLY BATTERY PACK I.A.W. B767 AMM 33-51-07. PERFORMED OPS CHECKS I.A.W. B767 AMM 33-51-07-402-010 STEP 7D.</P>)
Part: EXTINGUISHER — ABNORMAL · airframe 59,622 hrs · 44,718 cycles
SMOKE BARRIER RH SIDE HALON FIRE EXTINGUISHER FAILS WEIGHT TEST. THERE IS NO WEIGHT TEST TAG FROM THE PREVIOUS TEST.(<P>WEIGHED SMOKE BARRIER HALON FIRE EXTINGUISHER WITH SCALE ASR-382 (DUE DAT 26JAN19) I.A.W. AMM 26-26-02-216-012-001. EXTINGUISHER WEIGHT 3.81 LBS, IN LIMITS.&NBSP;</P>)
Part: EXTINGUISHER — ABNORMAL (COCKPIT) · airframe 59,622 hrs · 44,718 cycles
FLIGHT DECK HALON FIRE EXTINGUISHER FAILED WEIGHT TEST. PREVIOUS WEIGHT WAS 3.6 LBS AND NOW WEIGHS 3.5 LBS. THE PREVIOUS WEIGHT TEST TAG DATES ARE ILLEGIBLE.&NBSP;(<P>WEIGHED FLIGHT DECK FIRE EXTINGUISHER WITH SCALE ASR-348 (DUE DATE: 26JAN19), WEIGHT WITHIN LIMITS I.A.W. B767-200 AMM 26-26-02-216-012-001. LAST WEIGHT 3.60 LBS, NEW WEIGHT 3.56 LBS.&NBSP;</P>)
2018
Part: HOT WATER POT — SHORTED (GALLEY) · airframe 59,561 hrs · 44,686 cycles
HOT CUP INOP. SHORTED WHEN PUSHED INTO THE SOCKET. CREW REPORTED SPARKS. TRANSFERRED TO DMI 104491 IAW DDG 25-20-01 NEF SECTION 4, GALLEY ITEM 2.
2016
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,003 hrs · 43,276 cycles
EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-51-07. OPS GOOD.
Part: TIRE — BLOWN (MLG) · airframe 56,542 hrs · 43,009 cycles
FOUND NR 2 TIRE BLOWN ON WALKAROUND. R & R NR 2 MLG TIRE IAW AMM 32-45-01, NR 1 TIRE REPLACED DUE TO NR 2 FAILURE IAW 32-45-01. PERFORMED BRAKE SEIZURE CONDITIONAL INSPECTION IAW AMM 05-51-15, FOUND NR 1 AND NR 2 BRAKE LINE CROSSED CORRECTED BRAKE LINES PERFORMED ANTI-SKID TRANSDUCER SPIN TEST IAW AMM 32-42-00-705-248. OPS NORMAL. PERFORMED BURST/FLAT SPOT INSPECTION IAW AMM TASK 05--51-212-001, DEBRIS FOUND ON NR 6 TIRE NO FURTHER DAMAGE NOTED. NR 6 TIRE R & R DUE TO DEBRIS IAW 32-45-01.
Part: DOOR FRAME — CORRODED (FUSELAGE) · airframe 56,537 hrs · 43,009 cycles
MAIN DECK OVERWING EXIT AFT FRAME OF CUTOUT DOOR, STA 885.5 JUST ABOVE LOWER DOORSILL FRAME FAILSAFE CHORD IS CORRODED. REMOVED CORROSION IAW SRM 51-10-02, FOUND AREA TO BE OUT OF LIMITS IAW SRM 53-00-15. FABRICATED REPAIR STRAP OUT OF 7075-TG .063 AND INSTALLED IAW MSG PMO-TLS-16-0010-05B.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 56,498 hrs · 42,987 cycles
AFTER TAKEOFF EICAS FWD EQUIP VLV. ACCOMPLISHED QRH & ACFT DID NOT PRESSURIZE. RETURNED TO FIELD, RE-APPLIED MEL 21-58-06 PROCEDURE 2 ALL VLVS CONFIRMED CLOSED. OPERATIONS CHECK PRESS SYS IAW AMM 21-31-00, PRESS ACFT TO 4.0, NO DEFECTS NOTED, MDDR REMAINS OPEN.
2015
Part: D-RING — MISSING (EMERGENCY EQUIP) · airframe 55,500 hrs · 42,431 cycles
DESCENT, HARNESS IN FLIGHT DECK UPPER STORAGE POUCH OUTBOARD HARNESS DOES NOT HAVE A D RING. INSTALLED D RING CARABINEER ON SAFETY HARNESS IAW AMM 25-61-03.
Part: A/C PACK — STIFF (LEFT) · airframe 55,329 hrs · 42,309 cycles
LEFT THROTTLE EXTERIOR STIFF TO ADVANCE, RATCHETS WHEN THRUST LEVER ADVANCES. COMPLIED WITH FIM 76-11 FAULT TREE 805. THROTTLE LEVER FORCE IS 5 LBS, AUTO THROTTLE TEST 10 OK.
Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 55,250 hrs · 42,240 cycles
AFTER TAKEOFF, RT PACK OFF, AFTER PACK OFF EICAS FWD EQUIP OVHT. RAN QRH CHECKLIST, MSG CONTINUED, ALSO NO COOLING LIGHT. EADI DISPLAYED FAILED AT 22.000 FT CABIN ALT EICAS MSG, AUTO CONTROLLER FAILED. PERFORMED FIM 21-51-811, NO FAULTS NOTED IAW WDM 21-51-21. RT PACK FLOW CONTROL VLV FOUND MANIFOLD INTERCONNECT VLV, V90 FAULTY. SEE ITEM 11 LP7117705. PERFORMED FIM 21-31-804 & 806, COULD NOT DUPLICATE ON GND. AS PRECAUTION, R & R LT FLOW CONTROL VLV PN 396496-1, SN 360, & RT FLOW CONTROL VLV PN 396496-1, SN 377, FWD EQUIP COOLING FAN PN 732591B, SN 0666, MANIFOLD INTERCONNECT VLV PN 420035-1, SN 012, LT ACM PN 680640-4, SN 34-669, LT PRESS TIME & DELAY RELAY PN TD-1982-3001, NSN & LT CARGO SMOKE CONTROL RELAY PN BACR13062A, NSN, LT DEP CARGO RELAY PN BACR13CE 2, NSN 9. RT PACK FLOW CONTROL PCB CARD ASSEMBLY PN 285T0093-11, SN D01493, LT PACK FLOW CONTROL PCB CARD ASSEMBLY PN 285T0093-11, SN D01141, LT PACK TEMP CONTROLLER PN 625946-9, SN 069C-3405, & RT PACK TEMP CONTROLLER PN 625946-9, SN 074C-599. COMPLIED WITH TEST FLIGHT GTI9601. ALL SYSTEMS CHECKED NORMAL. NO INBD ITEMS UPON ARRIVAL.
Part: SKIN — CORRODED (RT WING) · airframe 55,086 hrs · 42,145 cycles
RIGHT OVERWING FUEL FILL PORT HAS CORROSION INSIDE OF TANK. REPAIRED AREA AROUND RT OVERWING FUEL FILL INSIDE TANK IAW AREA 47136, REA 04,47136, REA 09, & 47136 REA 10.
Part: SKIN — CORRODED (LT WING) · airframe 55,086 hrs · 42,145 cycles
CORROSION ON LT WING AT FS 939. REMOVED CORROSION, BLENDED AREA IAW REA 47136REA07.
Part: BEAM — DEFECTIVE (TE FLAP) · airframe 55,086 hrs · 42,145 cycles
NUMBER 8 FLAP 1, 2, 3 BEAM HAS DEFECT ON THE .0620 INCH HOLE, DURING HFEC OPEN HOLE SCAN. REPAIRED HOLE TO REMOVE DEFECT & INSTALLED SERVICEABLE BUSHING IAW SRM 51-40-02, CMM 27-51-97 & REA 47136REA12.
Part: SUPPORT ANGLE — DAMAGED (FUSELAGE) · airframe 55,086 hrs · 42,145 cycles
AFT ATTACH BRACKET FOR FLOOR PANEL ABOVE MEC DOOR, OPEN POSITION CHECKED. REMOVED DAMAGED SUPPORT ANGLE, FABRICATED NEW ANGLE FROM 7075-T6,0063 P0 0048004. INSTALLED NEW SUPPORT ANGLE USING SRM 51-40-02 & 51-30-01. VERIFIED MATERIAL NR 15.
Part: BUSHING — WORN (LT WING) · airframe 55,086 hrs · 42,145 cycles
NUMBER 1 SUPPORT BEAM 1,2,3 HAS TWO EACH BUSHINGS WORN, LT WING. INSTALLED TWO EACH NEW BUSHINGS IN LT WING NR 1 SUPPORT BEAM 1,2,3 IAW REA 4713REA14.
Part: RIB — CORRODED (LT WING) · airframe 55,086 hrs · 42,145 cycles
LEFT WING LES INTERNAL RIB IS CORRODED ABOVE WIRE STANDOFF LOCATED AT APPROX LESS 479. FOUND CORROSION BEYOND LIMITS, REPAIRED AIR LOAD RIB IAW SRM 51-70-11.
Part: RIB — CORRODED (LT WING) · airframe 55,086 hrs · 42,145 cycles
LEFT WING LES INTERNAL RIB IS CORRODED AT FWD UPPER CORNER & LOWER EDGE. R & R LES INTERNAL RIB WS 456 IAW REA 47136REA08, WORK ACCOMPLISHED SRM 51-40-02.
Part: SKIN PANEL — CORRODED (RT WING) · airframe 55,086 hrs · 42,145 cycles
RIGHT WING OVERWING FUEL ACCESS HOLE HAS CORROSION ON UPPER SURFACE OF LIP. REMOVED FASTENERS FROM AREA & CLEANED CORROSION. FABRICATED & INSTALLED DOUBLER REPAIR TO AREA IAW REA 47136REA0, 47136REA09 & 47136REA10.
Part: RIB — CORRODED (RT WING) · airframe 55,086 hrs · 42,145 cycles
NUMBER 2 SLAT INBD AUX TRACK ATTACH FITTING LOWER OTBD STRUT CORRODED, AFT OF FITTING. R & R RT WING LOWER STRUT RIB AT STATION 884.732 IAW SRM 51-40-02.
Part: SKIN — CORRODED (WING) · airframe 55,086 hrs · 42,145 cycles
CORROSION ON TOP OF WING AT FS 939 W STRINGER 2. REMOVED CORROSION, BLENDED AREA IAW REA 47136REA06.