N806FT
Registered owner: JOHNSON DANIEL S, KY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FLYING TIGER | Operator | on 1983-10-11 | Operator named in NTSB report |
Accident & incident history
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.
56 reports on file, 1998-07-28 – 2002-08-28.
Part: GEARBOX — FAILED (#1 ENGINE) · airframe 66,563 hrs · 17,078 cycles
SHORTLY AFTER T/O, #1 ENG. LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE DROPPED TO 10psi & WAS STEADY; OIL QTY SHOWED FULL & WAS STEADY. PERFORMED LOSS OF OIL PRESSURE PROCEDURE IAW AFM. COULD NOT RESTORE ENG. OIL PRESSURE OR EXTINGUISH LIGHT, THEREFORE A PRECAUTIONARY ENG. SHUTDOWN WAS PERFORMED IAW AFM. AFTER SHUTDOWN, OIL PRESSURE DROPPED TO ZERO & OIL TEMP ROSE TO 10 DEGREES ABOVE THE GREEN BAND. FLT RETURNED TO CAI WHERE ENG. PROBLEM WAS FOUND TO BE CAUSED BY GEARBOX FAILURE. IT HAD BEGUN TO DISINTEGRATE INTERNALLY REQUIRING AN ENGINE CHANGE.
Part: AUTOPILOT SYS — MALFUNCTIONED (COCKPIT) · airframe 65,986 hrs · 16,968 cycles
B-AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODE. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM.
Part: WIRE — BROKEN ("A" AUTOPILOT) · airframe 65,986 hrs · 16,968 cycles
"A" AUTOPILOT WILL NOT ACCEPT STEERING COMMANDS IN HDG OR INS MODES. ALSO INOP IN MANUAL. TRANSFERRED TO DEFERRED MX ITEM ID #036042 CTR #29299 IAW MEL 02-22-2-1 IN CONSULT W/ MTC & PLACARD INSTALLED. JFK MX FOUND BROKEN WIRE AT PINS 9 & 10 ON CONNECTOR DB193 "A" A/P CCA. REPINNED & SECURED WIRE AS PER MM 20-60-07. PERFORMED OPS CK PER MM 22-10-00. "A" A/P CHKD GOOD - DMI CLEARED.
Part: SHROUD — CRACKED (NR 1 ENGINE) · airframe 65,978 hrs · 16,966 cycles
CRACKS FOUND ON NR 1 ENG TURBINE COOLING SHROUD AT 8 & 2 O'CLOCK POSITIONS. RT (2 CRACKS) NR 1 IS 5 INCHES LONG & NR 2 IS 2 INCHES LONG. LT (4 CRACKS) NR 1 IS 3 INCHES LONG, NR 2 IS 5 INCHES LONG, NR 3 IS 1.5 INCH LONG & NR 4 IS 1.5 INCH LONG. ALSO BRACKET HAS A 1 INCH LONG CRACK. NR 1 ENG TCC MANIFOLD WELD REPAIRED IAW P&W STD PRACTICES 70-42-01 USING AMS 5832 FOR INCONEL.
Part: ACOUSTIC PANEL — DAMAGED (APU) · airframe 65,978 hrs · 16,966 cycles
APU EXHAUST ACOUSTIC LINER DAMAGED AT 01:30 O'CLOCK POSITION. APU LINER REMOVED & REPLACED IAW MM 49-81-02.
Part: PANEL — CRACKED (RH WING) · airframe 65,978 hrs · 16,966 cycles
CRACK 15" LONG FOUND RH WING UPPER SKIN LE FIXED PANEL AT WS 834 TO WS 862. PANEL SHOWS 15 X 30 IN. SQ AREA DELAMINATED. LEADING EDGE FIXED PANEL AT WS 834 TO WS 862 REMOVED & NEW PANEL INSTALLED IAW SRM 51-10-01, PG 8, SECT 6, PARA A-B-C. ALSO SRM 51-30-02.
Part: DOOR — CRACKED (APU) · airframe 65,978 hrs · 16,966 cycles
A 2 INCH LONG CRACK FOUND ON APU INLET DOOR OUTSIDE LOWER FORWARD CORNER. COMPOSITE REPAIR CARRIED OUT WITH REF TO SRM 51-40-06. AREA PROTECTED WITH REF TO SRM 51-21-01.
Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 65,171 hrs · 16,796 cycles
LEVEL 1 CORROSION: FOUND LIGHT CORROSION, AREA 500, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 1, 2, 3 & 4 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.
Part: FLAP TRACK — CORRODED (T/E FLAP) · airframe 65,171 hrs · 16,796 cycles
FOUND LIGHT CORROSION, AREA 600, ON UPPER FLAP TRACKS AND CENTER TOGGLE ROLLERS ON NR 5, 6, 7 & 8 FLAP TRACKS. REMOVED CORROSION AND RETREATED IAW MM 27-51-22 & 27-51-23, PAGE 801.
Part: BOLT — WORN (LT MLG DOOR) · airframe 65,171 hrs · 16,796 cycles
WORN LT WING BODY GEAR, AREA 751; SUPPORT ROD BOLT WORN. REMOVED BOLTS/BUSHINGS AND CLEANED UP. REASSEMBLED IAW MM 32-13-00 WITH LUBRICATION AND NEW WASHERS INSTALLED TO CORRECT ITEM. FOUND DOOR TO ROD BEARINGS AND BOLTS NOW WITHIN LIMITS. OK FOR SERVICE.
Part: WIRE — BROKEN (NR 11 BRAKE) · airframe 64,924 hrs · 16,743 cycles
RT BODY GEAR LEFT REAR (NR 11) ANTI-SKID LIGHT CAME ON AND WOULD NOT RESET. WHEEL ASSY RETORQUED FOR PRECAUTION PER MM 32-45-01. NR 11 BRAKE DEACTIVATED PER MEL. REPAIRED BROKEN WIRES AT TRANSDUCER ELECT CONNECTION PER MM STANDARD PRACTICES. REACTIVATED NR 11 BRAKE. NORMAL OPERATIONS RESTORED.
Earlier reports · 1998–2001 · 45 reports
2001
Part: FAIRING — DAMAGED (STAB STA 560) · airframe 64,532 hrs · 16,661 cycles
L/H HORIZONTAL STABILIZER STA 560 OUTBOARD TIP - AFT WEDGE 6" SECTION BROKEN OFF. REMOVED & REPLACED T/E & BOTTOM ACCESS PANELS PER SRM 51-10-01.
Part: WEB — CRACKED (NOSE WHEEL WELL) · airframe 64,378 hrs · 16,628 cycles
NOSE GEAR WHEEL WELL FRAME WEB CRACKED, APPROX. 1/8" LONG, BY INSULATION HOLES FIRST & FOUR FROM FLOOR CHORD ANGLE ON RIGHT SIDE. OPENED HOLES TO 7/16", RE-INSPECTED BY H.F.E.C. - NO INDICATIONS. REPAIRED IAW BOEING SERVICE LETTER PAO-LGB-01-0015514, SB74752a2293 & MA #a5310-33-01.
Part: SLIDE — DEFECTIVE (CABIN) · airframe 63,594 hrs · 16,457 cycles
RT UPPER DECK SLIDE BLOWN BY MAINTENANCE AND ONLY HALF INFLATED. REPLACED U/D RIGHT SLIDE ASSIST BOTTLE. REMOVED AND REPLACED U/D RIGHT SLIDE FOUND SHEARED CABLE. P/N ON 7A1248-36 S/N ON G476.
Part: FIRE WARNING — ACTIVATED (NR 2 ENGINE) · airframe 62,947 hrs · 16,323 cycles
NR 2 ENG FIRE DET LIGHT AND FAULT LIGHT CAME ON A-LOOP WITH A FIRE WARNING. ENGINE SHUT DOWN AND BOTTLE FIRED. REPLACED NR 2 LFT FIRE BOTTLE. P/N ON 33603903P, S/N M2621
2000
Part: FRAME — CRACKED (COCKPIT) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND ON FRAME 320 RHS AT WINDOW POST INTERSECTION, DURING COCKPIT WINDOW INSPECTION. FRAME 320 RHS TEE CHORD REPAIR C/OUT PER SRM 51-40-04.
Part: HOOK — LOOSE (RT WING) · airframe 61,450 hrs · 16,030 cycles
ABNORMALITY FOUND ON RT WING NR 7 POSITION SEQUENCE CARRIAGE HOOK ASSY FOUND LOOSE. REPLACE WITH NEW TOGGLE SEQUENCE ASSY P/N 65B17198-10, INSTALLED PER MM 27-51-30.
Part: BOLT — BROKEN (LT WING TE FLAP) · airframe 61,450 hrs · 16,030 cycles
OUTBOARD T/E AFT FLAP ATTACHMENT FITTING TO MID FLAP MOUNTING BOLTS FOUND SHEARED DURING NISPECTION. ATTACH FITTING MOUNTING BOLTS REPLACED PER MM 27-51-04.
Part: FRAME — CRACKED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND ON FRAME 320 RHS AT COCKPIT WEB. WEB REPAIR C/OUT PER SRM 51-40-02.
Part: BOLT — BROKEN (LT WING) · airframe 61,450 hrs · 16,030 cycles
NR 2 SEQUENCE CARRIAGE ASSY HOOK BOLT FOUND SHEARED DURING INSPECTION. BOTH HOOK BOLTS REPLACED PER MM 27-51-30.
Part: PANEL — CRACKED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND AT BS 1241 CANTED BULKHEAD CLOSEOUT PANELS (LHS 2.5 AT O/B LOWER CORNER, RHS 5.0 AT O/B EDGE FASTENERS). BS 1241 LT & RT CANTED BULKHEAD CLOSEOUT PANELS REPLACED PER SB 747-53-2329.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
DAMAGE FOUND ON FUSELAGE SKIN NOT SMOOTH AT BS 1826 TO BS 1837 BETWEEN 542L AND 543L. PAINT REMOVED NDT INSPECTED AND NO CRACKS NOTED, AREA RESTORED PER SRM 51-40-01 AND PAINTED.
Part: SKIN — CORRODED (RT WING TE FLAP) · airframe 61,450 hrs · 16,030 cycles
LEVEL 1 CORROSION FOUND RT WING I/B MID FLAP TOP SKIN PANELS FOUND WITH CORROSION IN SEVERAL PLACES ON THE UPPER T-CHORD. CORRODED TJ-CHORD REPLACED PER SRM 51-40-04 FIG 1.
Part: SKIN — CORRODED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
LEVEL 1 CORROSION FOUND ON UPPER SURFACE OF UPPER SKIN PANEL OF WING CTR TANK JUST FWD OF BS 140 BETWEEN RBL 2 AND RBL 9. CORROSION BLENDED OUT AND REPAIRED PER PAO-SIN-00-00043F & -00045H. FAA FORM 8110-3 ISSUED.
Part: ROD — DAMAGED (WING LE FLAP) · airframe 61,450 hrs · 16,030 cycles
DAMAGE FOUND L/E SUPPORT ROD ASSY FOR RIB AT WING STA 878.55 FOUND CHAFED THRU. SUPPORT ROD ASSY REPLACED PER SRM 51-30-04.
Part: BEAM — CRACKED (NLG WW) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND ON NOSE WHEEL WELL VERTICAL BEAM WEB AT STA 320 LHS, FOUND 2 CRACKS APPROX .75 & .1875 INCH LENGTH NDT REPORT POLAR/4284/00 REFERS. STA 320 LHS VERT BEAM WEB REPARI C/OUT PER SRM 51-40-02.
Part: FITTING — DAMAGED (RT WING LE FLAP) · airframe 61,450 hrs · 16,030 cycles
ABNORMALITY FOUND ON RT WING I/B FOREFLAP O/B SEQ CARRIAGE ATTACHMENT FITTING BEARING FOUND MIGRATED. NEW FITTING P/N 65B39025-34 INSTALLED PER MM 27-51-02.
Part: STRUCTURE — CORRODED (VERTICAL STAB) · airframe 61,450 hrs · 16,030 cycles
LEVEL 1 CORROSION FOUND ON VERTICAL FIN 4TH BALANCE WEIGHT (COUNTING FROM TOP TO BOTTOM). CORROSION TREATMENT PER CPM PART 1, 20-40-00 P.24 C/OUT WEIGHT REINSTALLED, MM 20-51-01.
Part: DRAIN VALVE — CRACKED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND ON 13 OFF DRAIN VALVE ASSY AT BELLY FUSELAGE BS 2160 TO BS 2180. ALL 13 DRAIN VALVE ASSY REPLACED PER MM 51-41-03.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND ON MAIN DECK STA 997 INTERCOSTAL AT RBL 75 FOUND ALONG FASTENER HOLE. MAIN DECK STA 997 INTERCOSTAL REPAIR C/OUT PER SRM 51-40-03.
Part: DUCT — BROKEN (NR 3 ENGINE)
NR 3 ENGINE FIRE WARNING ON TAKEOFF. BOTTLE DISCHARGED. ENGINE SHUT DOWN. AIRCRAFT RETURNED TO AKL. FOUND BROKEN 8TH STAGE ANTI-ICE DUCT THROTTLE CABLE MELTED AND JUMBLED. WIRE BUNDLES MELTED, ENGINE CHANGED. OPERATOR: POLAR AIR CARGO AKL TO KHG. (X)
Part: PANEL — CRACKED (FUSELAGE) · airframe 61,450 hrs · 16,030 cycles
CRACK FOUND AT BS 1240 RBL 5.0 CLOSURE PANEL AT CANTED BULKHEAD COMMON TO APU FUEL FEED LINE/SHROUD FOUND CRACKED AROUND FASTENER LOCATION. CLOSURE PANEL REMOVED AND NEW PANEL INSTALLED PER SRM 51-30-02.
1999
Part: ANGLE — CRACKED (BS 434)
FOUND 1.6 INCH CRACK ON RADIUS OF ANGLE FWD OF BS 434 UNDER STR 26. FABRICATED PARTS AND REPLACED PER SRM 51-30-02.
Part: FLOORBEAM — DAMAGED (BS 400)
FOUND SHEARED RIVETS AT BS 400 ON FLOORBEAM LEFT SIDE. REPLACED RIVETS PER SRM 51-30-02.
Part: VERTICAL BEAM — CRACKED (BS 320)
FOUND INDICATION OF CRACKS AT HOLE ON VERTICAL BEAM AT BS 30L. STOP DRILLED AND FABRICATED REPAIR PER SRM 53-10-04 FIG 94 PG 8 DETAIL 5.
Part: CLIPS — CRACKED (BS 340)
FOUND CRACKS ON CLIPS AT NOSE WHEEL WELL VERTICAL BEAM WEB AT BS 340 R. REPLACED CLIPS PER SRM 51-30-02.
Part: BULKHEAD FLANGE — CRACKED (BS 140)
FOUND CRACK ON FLANGE OF PRESSURE BULKHEAD AT BS 140 WL 280 BL 10L. TRIMMED DAMAGED AREA AND FABRICATED NEW ANGLE PER SRM 51-40-03 AND 51-10-02.
Part: BULKHEAD — CRACKED (BS 1000)
CRACKS FOUND ON BS 1000 IN THE RADIUS BETWEEN STR 46 AND 47 LEFT AND RIGHT SIDES. STOP DRILLED, EDDY CURRENT PER SB 530-2316R1 AND SRM 51-10-01 FIG 2.
Part: WEB — CRACKED (BS 434)
FOUND WEB CRACKED AT BS 434L NR 1 MED. TRIMMED AREA AND FABRICATED PART FOR REPAIR PER SRM 53-10-04 AND 51-30-02.
Part: SKIN — DAMAGED (CARGO DOOR)
DURING CLOSING LOWER FWD CARGO DOOR, AEROGROUND HIGH LOADER HIT DOOR AND CAUSED DAMAGE TO LOWER AFT CORNER. REWORKED LOWER CORNER OF FWD CARGO DOOR PER SRM 51-10-01.
Part: ANGLE — CRACKED (BS 1726L)
AFT PIT STAT 1726 BL 30L ANGLE FOUND CRACKED JUST BELOW TRACK. REMOVED AND FABRICATED NEW ANGLE AND INSTALLED PER SRM 51-10-01, 51-10-03 AND 51-30-02.
Part: KEEL BEAM — CORRODED (BS 1100-1300)
LEVEL 1 CORROSION FOUND ON KEEL BEAM AFT END LEFT AND RIGHT SIDE BS 1100 TO 1300. REMOVED CORROSION, TREATED AND PRIMED PER SRM 53-10-01 AND 53-10-02.
1998
Part: FAIRING — DELAMINATED (TAIL CONE)
NR 8 FIXED FAIRING TAIL CONE LOWER SKIN FOUND DELAMINATED. SANDED DOWN DELAMINATION AREA AND REPARIED PER SRM 51-40-09.
Part: PANEL — CRACKED (RT MLG DOOR)
RIGHT WING GEAR FLYING DOOR PANEL CRACKED. REPAIRED PANEL IAW 747 SRM 51-40-09.
Part: PANEL — DELAMINATED (RT WING)
RIGHT WING UPPER SURFACE OF FLYING PANEL HAS A 2X2 AREA OF DELAMINATION AT TITANIUM COFFIN DOUBLER. REMOVED AND REPLACED RIGHT HAND WING FLYING PANEL IAW SRM 57-22-89, 51-30-02 AND POLAR MA A5730-02:01.
Part: FLOOR — DELAMINATED (UPPER DECK)
LEVEL 1 CORROSION ON FLOOR PANEL UNDER LT UPPER DECK SLIDE CARRIAGE DELAMINATED AND MINOR CORROSION. FOUND MINOR SURFACE CORROSION, REMOVED IAW SRM 51-10-06 AND REPAIRED DELAMINATION IAW SRM 51-40-05.
Part: SUPPORT — DAMAGED (BS 860)
FWD LOWER CARGO COMPARTMENT STA 860 CENTER GUIDE FLOOR SUPPORT DAMAGED. REMOVED DAMAGED FLOOR SUPPORT AND WEB REINSTALLED PERMANENT REPAIR IAW SRM 51-40-02.
Part: SKIN — CORRODED (FUSELAGE)
LEVEL 1 CORROSION UNDER THE ATC ANTENNAS. REMOVED CORROSION FROM UNDER A/C ATC ANTENNAS WITH MINIMAL MATERIAL LOSS IAW SRM 51-10-01.
Part: EXHAUST SLEEVE — DELAMINATED (NR 4 ENGINE)
NR 4 ENGINE EXHAUST SLEEVE INNER SKIN DELAMINATED AT 6 O'CLOCK POSITION. REMOVED AND REPLACED NR 4 ENG EXHAUST SLEEVE ASSY IAW MM 78-11-02.
Part: COWL — DELAMINATED (NR 2 ENGINE)
DENTED AND DELAMINATION NR 2 ENGINE INBOARD FAN COWL EXTERNAL SKIN AT LOWER CENTER. REPAIRED PER BOEING SRM 51-40-06.
Part: ANTENNA — CORROSION (FUSELAGE)
LEVEL 1 CORROSION ON THE NR 1 AND NR 2 ANTENNA BODY. REPLACED NR 1 AND NR 2 ATC ANTENNAS IAW MM 34-53-03.
Part: COWL — DAMAGED (NR 1 ENGINE)
DAMAGED AND BENT LOWER CORNER ON NR 1 ENGINE FAN COWL. REMOVED DAMAGED AREA FABRICATED NEW FILLER AND DOUBLER PER BOEING SRM 51-40-05
Part: PANEL GUIDE — CRACKED (NR 4 ENGINE)
CRACKED NR 4 ENGINE PANEL GUIDE AT 11:30 POSITION AT FAN EXIT. FABRICATED NEW PANEL GUIDE PER BOEING SRM 51-40-00.
Part: SKIN — CRACKED (LT TE FLAP)
CRACKED AND DAMAGED AREA ON INBOARD EDGE NR 9 VARIABLE CAMBER FLAP. BLENDED DAMAGED AREA AND FOUND WITHIN LIMITS PER BOEING SRM 57-50-01.
Part: EXHAUST SLEEVE — CRACKED (NR 4 ENGINE)
CRACKED NR 4 ENGINE EXHAUST SLEEVE AT 1:00 AND 6: POSITIONS. REPAIRED CRACK PER BOEING SRM 54-30-3.
Part: SKIN — CRACKED (RT TE FLAP)
CRACKED AND BENT AREA ON INBOARD EDGE NR 17 VARIABLE CAMBER FLAP. BLENDED DAMAGED AREA AND FOUND WITHIN LIMITS PER BOEING SRM 57-50-01.