N657GT
Registered owner: JETRAN LLC, TX (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.
49 reports on file, 2015-11-06 – 2020-08-11.
Part: SENSOR — FAILED (FAN AIR TEMP) · airframe 61,979 hrs · 44,319 cycles
L ENG HI STAGE EICAS MSG DURING CLIMB. REMOVED AND REPLACED FAN AIR TEMP SENSOR IAW AMM 36-11-17. OPS CK GOOD.
Part: TRUNNION — CORRODED (RT MLG) · corrosion level 2 · airframe 61,903 hrs · 44,262 cycles
RT MLG FORWARD TRUNNION WAS CORRODED IN THE LOWER SUPPORT ASSEMBLY BUSHING SHOULDER. REMOVED CORROSION AND INSTALLED OVERSIZED BUSHING PER 47401REA18 WITH 8100-9 BY AR-831084. REFERENCE NR 123447.0007
Part: KEELBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
KEEL PANEL CROSS MEMBER CORROSION UNDER NUT PLACES.(<P>REPLACED KEEL PANEL IAW B767 SRM 51-10-02.</P>)
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
STA 1065 LOWER INTERNAL SKI AND STRINGERS HAVE SURFACE CORROSION.(<P>REMOVED CORROSION. DID SCAN INSPECTION, FOUND SKIN TO BE OUT OF LIMITS. INSTALLED DOUBLER AND TRIPLER IAW REA 47401 REV A.</P>)
Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 61,764 hrs · 44,180 cycles
RT SIDE VERTICAL STAB SKIN DELAMINATED.(<P>REMOVED AND REPAIRED SKIN PANEL AND INSTALLED STAB SKIN WITH INTERIM FASTENERS PER 47401REA15.</P>)
Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
H2 STAB STRINGER 11 CORRODED.(<P>REPLACED STRINGER PER 767-200 SRM 51-40-02 AND REA 47401FAB03.</P>)
Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
H2 STAB STRINGER 8 CORRODED.(<P>REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03 AND REA 47401FAB</P>)
Part: PANEL — BULGED (LT WING) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
LH WING UPPER T/E PANEL SURFACE BULGED BEYOND LIMITS.(<P>REPAIRED DAMAGED CHORD IAW REA 47401 REV. 3 AND B767 SRM 57-20-10.</P>)
Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
HORIZONTAL STAB STRINGER 11 CORRODED. REPLACE STRINGER PER B767-200 SRM 51-40-02 AND REA 47401FAB03.
Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
HORIZONTAL STAB STRINGER 8 CORRODED. REPAIRED WITH SPLICE PER B767-200 SRM 55-10-03
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
ALC STA 1065 LOWER INTERNAL SKIN AND STRINGERS BETWEEN FUSELAGE DRAINS HAVE SURFACE CORROSION. BLEND OUT REQUIRED AT CORRODED AREA, REMOVED CORRODED AREA AT LOWER FUSELAGE SKIN STA 1080 TO STA 1131, STRINGER 38L TO 38R IAW B767-200 SRM 53-60-01 ALLOWABLE DAMAGE 2.DID UT INSP FOUND TO OUT OF LIMITS INSTALLED DOUBLER AND TRIPLER IAW REA47401REA14 REV A
Part: PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
THE LEFT WING, UPPER T/E PANEL, UPPER SURFACE IS BULGED, ON THE FWD O/B CORNER, LOCATED JUST FWD OF THE O/B AILERON'S I/B END.BLENDED CORROSION AND FOUND TO BE OUT OF LIMITS PER SRM 57-20-10 DET V. REPAIRED DAMAGED UPPER CHORD IAW AMES REA # 47401 REA 03.
Part: ATTACH FITTING — CORRODED (FUSELAGE) · corrosion level 2 · airframe 61,764 hrs · 44,180 cycles
KEEL PANEL ATTACH CROSS MEMBER AT STA.967 CORRODED UNDER NUT PLATES ON FORWARD AND AFT SIDES.BLENDED CORROSION AT STA 967 KEEL PANEL ATTACH CROSS MEMBER IAW B767 SRM 51-10-02 MEASURED T. 0.100. REMOVED T 0.055 FOUND TO BE OUT OF LIMITS TAG 8720 INSTALLED PN 145T8629-3 KEEL PANEL ATTACH CROSS MEMBER AT STA 967 IAW B767 SRM 51-40-02 PARA 4
Earlier reports · 2015–2019 · 36 reports
2019
Part: ESCAPE REEL — UNWANTED DEPLOY (CABIN) · airframe 61,597 hrs · 44,076 cycles
EMERGENCY INERTIAL ESCAPE REELS AT POSITION 2, 4, AND 7 DEPLOYED AND REMOVED.(<P>TRANSFERRED TO MDDR 122754 AS PER DDG 25-61-01-01, CAT 'C'.</P><P>LP&NBSP;<SPAN>1112482 -&NBSP;</SPAN>INSTALLED GALLEY EMERGENCY DESCENT DEVICES IAW AMM 25-61-02.</P><P>POS. #7 - PN OFF 379103D-29, SN OFF 21941</P><P>POS. #4 - PN OFF 379103D-29, SN OFF 12043 </P><P>POS. #2 - PN OFF 379103D-29, SN OFF 28448</P><P>THIS CLEARS DMI 122754. MCC NOTIFIED. PLACARDS REMOVED.&NBSP;</P><P>(NOTE: REMOVAL OF DEPLOYED DEVICES LOGGED ON LP 1112476 AND LP 1112477)</P>)
Part: ADC — MALFUNCTIONED (RIGHT) · airframe 61,508 hrs · 44,024 cycles
LEAVING FL410 FOR FL390, CAUTION MSG IAS DISAGREE WAS DISPLAYED ALONG WITH L & R ENG EEC, AILERON LOCKOUT APPEARED, & RUDDER RATIO. F/O A/S INDICATION DECREASED AS WE DESCENDED, AND PASSING FL250, THE F/O A/S INDICATION RETURNED TO NORMAL.(<P>PERFORMED PITOT HEAT TEST IAW AMM 30-31-00, NO DEFECTS NOTED. PERFORMED F/O'S PITOT SYSTEM LEAK TEST IAW AMM 34-11-00, NO DEFECTS NOTED. REMOVED AND REPLACED RIGHT ADC IAW AMM 34-12-01, OPS CHECK GOOD.<BR /></P>)
Part: DISPLAY — FAILED (EHSI) · airframe 60,859 hrs · 43,653 cycles
DURING CLIMB, CAPTAINS EHSI TURNED INTO PINK TINT, SHORTLY FOLLOWED BY F/O'S EHSI FAILING&NBSP; (BLANK). THIS WAS FOLLOWED BY SCENT OF BURNING.(<P>PERFORMED INSP. OF CAPT'S & FO'S&NBSP; EHSI IAW BOEING 767 AMM 20-60-00. CLEAN FILTERS AND VERIFIED AIR COOLING. NO DISCREPANCIES FOUND.</P>)
2018
Part: PUMP — FAULTED (HYD SYSTEM) · airframe 60,537 hrs · 43,474 cycles
AFTER GEAR SELECTED UP GEAR DISAGREE & GEAR DOOR EICAS ALSO DOOR LT NEXT TO GEAR INDICATOR LTS STAYED ON, RAN CHECKLIST , RETURNED TO CVG&NBSP;(<P>FOUND CENTER HYD SYSTEM ADP AT FAULT , REPLACED ADP ( LP 1018242 ITEM # 5 ) AND ASSOCIATED COMPONENTS I.A.W AMM 29-11-00 & AMM 29-11-03 OPS AND LEAK CHECK GOOD&NBSP; , PERFORMED GEAR SWING NO DEFECTS NOTED&NBSP;</P>)
Part: WIRE — CORRUPTED (CONNECTOR) · airframe 60,456 hrs · 43,428 cycles
DURING CRUISE FLT DECK TEMP REACHED 36 C PER QRH TURNED OFF TRIM AIR STILL COULD NOT CONTROL FLT DECK TEMP&NBSP;(<P>FOUND POORLY CONNECTED WIRE TO PIN 2 CONNECTOR D490 RETERMINATED WIRE IAW B767 SWPM 20-60-00 SYSTEM OPS CHECKS GOOD AT THIS TIME&NBSP;</P>)
Part: CIRCUIT CARD — FAILED (FLOW CONTROL) · airframe 60,456 hrs · 43,428 cycles
FWD CABIN TEMP CAUTION MSG(<P>REMOVED AND REPLACED&NBSP; L/H PACK FLOW CONTROL CARD IAW B767 AMM 20-41-01 OPS GOOD AT THIS TIME&NBSP;</P>)
Part: ADI — INOPERATIVE · airframe 60,431 hrs · 43,413 cycles
DURING TAXI OUT CA ADI BLANKED, ALTN EFI DID NOT RETURN SCREEN WE THEN HAD ELECTRICAL SMOKE / BURNING SMELL. SUBSEQUENTLY LOST CA HSI AND UPPER EICAS SCREENS&NBSP;(<P>REMOVED ADI & HSI(CAPT) FOUND WATER BLOWING INTO DISPLAYS. REMOVED & RESEATED EICAS-DISPLAY OPERATES NORMALLY. PERFORMED GVI OF EQUIP COOLING SYS & LRU'S NO WATER FOUND, NO DEFECTS NOTED AT THIS TIME. REF B767 AMM 34-22-03, AMM 34-22-04, SUBTASK 21-58-00-017-025, SUG TASK 20-60-06-012-002.</P>)
Part: DOUBLER — CHAFED (APU BAY) · airframe 85,237 hrs · 24,637 cycles
CHAFING FROM RT APU DOOR CATCH ON FIRE WALL IN APU COMPARTMENT LOWER AREA RIGHT OF CENTERLINE. REMOVED AND REPLACED APU FIRE WALL DOUBLER LINE IAW SRM 51-40-02 AND SRM 53-80-08-2R-5.
2017
Part: WARNING MESSAGE — ILLUMINATED (CARGO DOOR) · airframe 59,351 hrs · 42,867 cycles
MAIN CARGO DOOR WARNING ANNUNCIATED DURING CLIMB PASSING FL240.
Part: WARNING MESSAGE — ILLUMINATED (RT EEC) · airframe 58,994 hrs · 42,665 cycles
RIGHT EEC EICAS MESSAGE AT 240 KTS.
Part: UNKNOWN — ODOR (CABIN) · airframe 58,868 hrs · 42,575 cycles
PASSING THRU 11K FEET ON CLIMB OUT, CAPTAINS ND BEGAN TO CYCLE ON AND OFF WITH STRONG ELECTRICAL ODOR. LEVELED OFF, TURNED BACK AND RAN- C&D SMOKE, FIRE OR FUMES QRH. MX PULLED C/B ANDTHE ODOR DIMINISHED. DURING BASE TURN, LOST THE FO'S CDU SCREEN, AFTER LANDING, LOST THE LOWER EICAS SCREEN. MECHANIC PULLED ALL BREAKERS ASSOCIATED WITH ALL 3 LOST CRT SCREENS. REMOVED AND REPLACED CAPT. HSI IAW AMM 34-24-04. OPS CHECK GOOD AT THIS TIME. PERFORMED OPS CHECK OF LOWER EICAS SCREEN IAW AMM 34-41-01, OPS CHECKED GOOD AT THIS TIME. ITEM M3 REMOVED AND REPLACED F/O CDU IAW AMM 34-61-02, OPS CHECKED GOOD AT THIS TIME. REMOVED AND REPLACED LT THRUST REVERSER UNLOCK RELAY IAW WDM 78-34-11. PERFORMED OPS CHECK OF LT THRUST REVERSER. OPS CHECKED GOOD IAW AMM 78-31-00, REMOVED AND REPLACED NR 1 PACK DUMP & SPRAY NOZZLE IAW AMM 21-53-05, OPERATION CHECK PASSED, ACCOMPLISHED AMM 05-51-56 NO DAMAGE OR DISCREPANCIES NOTED AIRCRAFT OK FOR SERVICE. REPLACED L/H PACK SPRAY/DUMP NOZZLE AND ACCOMPLISHED AMM 21-51-03. TEST PASSED, NO FURTHER HUMIDITY NOTED.
Part: FMC — FAILED (RIGHT) · airframe 58,864 hrs · 42,571 cycles
DURING TAXI OUT, RT FMC WENT BLANK WITH ELECTRICAL SMOKE ODOR. REMOVED AND REPLACED RT CDU IAW AMM 34-61-02, OPS CHECKED NORMAL.
Part: DISPLAY — INOPERATIVE (COCKPIT) · airframe 58,864 hrs · 42,572 cycles
DURING TAXI IN, NOTICED A BURNING ODOR, OZONE TYPE. REMOVED THE RT FMC CDU, FOUND A SLIGHT SMOKEY ODOR. R & R THE RT CDU IAW AMM 34-61-02. OPS CHECKED NORMAL.
Part: CIRCUIT BREAKER — TRIPPED (LT FMC) · airframe 58,812 hrs · 42,535 cycles
DURING BLOCK IN LEFT FMC CIRCUIT BREAKER TRIPPED WITH ELECTRICAL SMOKE ODOR IN THE COCKPIT. PERFORMED INSPECTION FOR SMOKE ODOR IAW AMM 05-51-56. NO DEFECTS NOTED.
Part: STRINGER — CRACKED (BS 1083) · airframe 58,755 hrs · 42,508 cycles
AFT CARGO BAY STRINGER 29R, BS 1083 IS CRACKED AT THE END OF THE FITTING. REMOVED AND REPLACED THE STRINGER IAW EA 17076PI.
Part: FRAME — CRACKED (BS 859.5) · airframe 58,755 hrs · 42,508 cycles
FRAME BS 859.5, RBL 89, BELOW 200, TRANSITION RADIUS HAS .5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-534-0209.</P>)
Part: SKIN — DAMAGED (NR 1 NACELLE) · airframe 58,755 hrs · 42,508 cycles
NR 1 PYLON BLEND DAMAGE UNDER THE 431 BT PANEL INBD OF SUPPORT FITTING. REPAIRED THE PYLON IAW EA 170189.
Part: FRAME — CRACKED (BS 883.5) · airframe 58,755 hrs · 42,508 cycles
FRAME BS 883.5, LBL 89, BELOW WL 200, TRANSITION RADIUS HAS A .5 INCH CRACK. REPAIRED THE FRAME IAW SB 767-53A-0209.
Part: UNKNOWN — SMOKE (CABIN) · airframe 58,553 hrs · 42,390 cycles
ON SHUTDOWN OF ENGINES SMOKE FILLED THE COCKPIT, APU SHUTOFF ON ITS OWN. PERFORMED CHAPTER 5 INSPECTION IAW AMM 21-00-21-862-051.
2016
Part: MODULE — FAULTY (TE FLAP) · airframe 58,010 hrs · 42,080 cycles
REJECTED T/O DUE TO T/O WARNING HORN. STATUS MESSAGE FLAP/SLAT ELECTRONIC LESS THAN 20KTS ACHIEVED. FOUND C FSPM FAULTING R & R C FSPM MODULE M839 IAW AMM 27-58-01. OPS CKS OK.
2015
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 8 FLAP SUPPORT, NR 2 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED SUPPORT HOLES IAW REA 47177REA04.
Part: DOUBLER — CRACKED (THRUST REVERSER) · airframe 57,006 hrs · 41,504 cycles
INBOARD THRUST REVERSER ON NR 2 ENG HAD CRACKED DOUBLER. REPLACED DOUBLER IAW 47177REA02.
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 1 FLAP SUPPORT, NR 2 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.
Part: SUPPORT — DAMAGED (TE FLAP) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
NUMBER 1 FLAP SUPPORT, NR 4 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 FLAP SUPPORT HOLES 3 & 4 IAW 4717 REA 04.
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 8 FLAP SUPPORT, NR 3 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 3 & 4 SUPPORT HOLES IAW REA47177REA04.
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 1 FLAP, NR 3 TENSION BOLT HOLE HAS DEFECT INDICATION. REAMED HOLES OVERSIZE IAW RFA 47177 REA 04.
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 8 FLAP SUPPORT, NR 4 TENSION BOLT HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 3 & 4 SUPPORT HOLES IAW 47177REA04.
Part: SUPPORT BEAM — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 8 FLAPS, SUPPORT 1 - 3 BEAM HAS 2 HOLES WITH DEFECT INDICATIONS WITH HFEC ROTARY SCAN. REAMED DISCREPANT HOLES IAW SRM 51-40-02 - PAR 7D 47177 REAOG.
Part: RIB — DAMAGED (TE FLAP) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
THE LT WING NR 2 FLAP SUPPORT, OTBD RIB ACTUATOR BORE UPPER FWD SURFACE HAD A DEFECT INDICATION DURING AN HFEC SURFACE SCAN. BLENDED CORROSION IAW SRM 57-51-90 FIG 101.
Part: BEAM — CORRODED (RT WING) · airframe 57,006 hrs · 41,504 cycles
RIGHT WING LE NOSE BEAM FROM LES 395 - 421 IS CORRODED ON THE INBD UPPER FLANGE. REMOVED CORROSION & REPAIRED IAW SRM 57-41-13 FIG 101 & SRM 51-70-11 FIG 101 RESPECTIVELY.
Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
RIGHT WING OTBD FLAP, LOWER FWD INBD STRESS PANEL HAD A SPOT OF CORROSION THAT WAS BLENDED OUT OF LIMITS ON NR-0570. REPAIRED PANEL IAW VACUUM CUT METHOD IAW SRM 57-53-01 & 51-70-01 & REA 47177REA03.
Part: STRINGER — CORRODED (HORIZ STAB) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
HORIZONTAL STAB BOX STRINGER U3, BETWEEN RIBS 1L & 2L, CORRODED ON AFT FLANGE. REMOVED CORROSION & BLENDED AREA.
Part: SKIN — CRACKED (RT WING) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
RIGHT WING LE SKIN CLOSE CUT CRACKED AT LES 446. REPAIRED IAW SRM 51-70-11 FIG.
Part: PANEL — CORRODED (TE FLAP) · corrosion level 2 · airframe 57,006 hrs · 41,504 cycles
RIGHT WING OTBD FLAP CORRODED. BLENDED & REPAIRED ON NR-0713 REFERENCING REA 47177REA03.
Part: SUPPORT — DAMAGED (TE FLAP) · airframe 57,006 hrs · 41,504 cycles
NUMBER 1 FLAP SUPPORT, NR 1 HOLE HAS A DEFECT INDICATION WITH HFEC ROTARY SCAN. REAMED NR 1 & 2 HOLES IAW 47177REA04.
Part: STRINGER — CORRODED (HORIZ STAB) · airframe 57,006 hrs · 41,504 cycles
CORROSION, HORIZONTAL STAB BOX, CTR INTERIOR, OTBD RIB 2L, UPPER NR 6 STRINGER, AFT HORIZONTAL LEG UPPER. R & R STRINGER NR 6, DOCUMENT 47177FAB08.