This N-number isn't registered right now. Below is its last known registration, canceled Sep 10, 2012.
Safety record in brief:1 NTSB incident (minor damage, Sep 1992)23 ADs may apply87 service difficulty reports
We never show street addresses, even though they appear in the public FAA file. Individual owners are shown by city and state only.
Total time and engine hours aren't public. They appear here once the owner adds logbooks.
Individual owners are shown by city and state only.
INADEQUATE LUBRICATION WHICH CAUSED STRESS CORROSION CRACKING AND THE SEPARATION OF THE RIGHT WING NUMBER TWO FLAP VANE.
From NTSB records; matched by serial number.Read NTSB report (search CAROL for BFO92IA145)
These match the airframe or engine model. Whether each one applies, and whether it's been complied with, depends on serial numbers, equipment and logbook entries. Applicability must be confirmed by a mechanic against the aircraft's records.
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2008-11-02 R1 | Lockheed Model L-1011 Series Airplanes | Dec 18, 2009 | Airframe (L-1011-385-1) |
| 2008-12-17 | Lockheed Model L-1011 Series Airplanes | Jul 23, 2008 | Airframe (L-1011-385-1) |
| 2005-15-01 | Lockheed Model L-1011-385 Series Airplanes | Aug 26, 2005 | Airframe (L-1011-385-1) |
| 2004-09-28 | Lockheed Model L-1011 Series Airplanes | Jun 17, 2004 | Airframe (L-1011-385-1) |
| 2000-17-10 R1 | Lockheed Model L-1011 Series Airplanes | Sep 26, 2001 | Airframe (L-1011-385-1)Only with: Equipped with Rolls Royce Model RB211-524 series engines. |
| AD | Subject | Effective | Applies to |
|---|---|---|---|
| 2001-08-27 | Lockheed Model L-1011 Series Airplanes | May 14, 2001 | Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-30-060, dated March 6, 2001, and Lockheed Service Bulletin 093-30-057, dated April 27, 1984 |
| 2000-21-01 | Lockheed Model L-1011-385 Series Airplanes | Nov 24, 2000 | Airframe (L-1011-385-1) |
| 2000-17-10 | Lockheed Model L-1011-385 Series Airplanes | Oct 6, 2000 | Airframe (L-1011-385-1) |
| 2000-16-08 | Lockheed Model L-1011-385 Series Airplanes | Sep 20, 2000 | Airframe (L-1011-385-1)Certain serial numbers: 1013–1250 |
| 2000-08-20 | Lockheed Model L-1011-385 Series Airplanes | Jun 5, 2000 | Airframe (L-1011-385-1)Only with: Equipped with high pressure bleed valve controller Hamilton Standard P/N 739084-2 or 739084-3 (Lockheed P/N 672286-103 or 672286-105). |
| 99-13-08 R1 | Lockheed Model L-1011-385 Series Airplanes | May 22, 2000 | Airframe (L-1011-385-1) |
| 99-24-12 | Lockheed Model L-1011-385 Series Airplanes | Jan 4, 2000 | Airframe (L-1011-385-1) |
| 99-17-13 | Lockheed Model L-1011-385 Series Airplanes | Sep 24, 1999 | Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-27-306, dated January 14, 1998 |
| 99-13-08 | Lockheed Model L-1011-385 Series Airplanes | Jul 28, 1999 | Airframe (L-1011-385-1) |
| 99-09-14 | Lockheed Model L-1011-385 Series Airplanes | Jun 1, 1999 | Airframe (L-1011-385-1) |
| 99-08-20 | Lockheed Model L-1011-385 Series Airplanes | May 19, 1999 | Airframe (L-1011-385-1) |
| 99-07-05 | Lockheed Model L-1011-385 Series Airplanes | Apr 30, 1999 | Airframe (L-1011-385-1) |
| 99-02-05 | Lockheed Model L-1011-385-1 Series Airplanes | Feb 19, 1999 | Airframe (L-1011-385-1)Only with: Equipped with lower deck galleys. |
| 98-10-14 | Lockheed Model L-1011-385 Series Airplanes | Jun 19, 1998 | Airframe (L-1011-385-1) |
| 98-09-23 | Lockheed Model L-1011 Series Airplanes Equipped With Rolls Royce Model RB211-22B Engines | Jun 3, 1998 | Airframe (L-1011-385-1)Only with: Equipped with Rolls Royce RB211-22B engines. |
| 95-26-11 | Lockheed Model L-1011-385 Series Airplanes | Jan 11, 1996 | Airframe (L-1011-385-1) |
| 95-10-17 | Lockheed Model L-1011-385 Series Airplanes | May 23, 1995 | Airframe (L-1011-385-1) |
| 95-06-51 | Lockheed Model L-1011-385 Series Airplanes | Apr 21, 1995 | Airframe (L-1011-385-1)Serial numbers per Lockheed Service Bulletin 093-28-A091, dated March 8, 1995 |
AI-extracted — verify against original. Matched from each AD's applicability section; ADs replaced by a later AD are left out.
Reports of failures and defects that operators and repair stations sent to the FAA since 1995. A report describes one finding; it is not an accident.
LOST C-HYD SYS QUANTITY DROPPED TO QUARTER. NECESSARY TO LOWER MLG VIA ALT GEAR EXTENSION. FOUND LEAK AT GEAR UP LINE. INSTALLED TEMP LINE.
From FAA Service Difficulty Reports; matched by N-number and serial number.LOWER GALLEY EMERGENCY CEILING LIGHT AND R2 DOOR EXITS AND CEILING LIGHT INOP. REPLACED 2 EACH POWER PACKS.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE UPPER CAP OF THE CENTER WING INTERMEDIATE SPAR AT FS 1043 WAS FOUND CRACKED BEYOND LIMITS AT THE LT OUTBD END. THE CAP WAS CUT NEAR LBL 80 AND A NEW OUTBD END WAS SPLICED IN WITH 4 STEEL SPLICE ANGLES AND 2 SPLICE STRAPS. THE REPAIR WAS ACCOMPLISHED PER ER/A 365093-14, REV A.
From FAA Service Difficulty Reports; matched by N-number and serial number.MASKS DID NOT DROP IN D-ZONE DURING OXY DROP CHECK. REPLACED SEQUENCING TIMER (P/N 25720481) OPS CHECK GOOD.
From FAA Service Difficulty Reports; matched by N-number and serial number.OVERSIZED FASTENER HOLES WERE FOUND IN THE VERTICAL FLANGE OF THE LT WING LWR REAR SPAR CAP AT APPROX IWS 258. THE FASTENER FINAL DIAMETER WAS 0.3428. REPAIRED PER ERA 331709-14AD.
From FAA Service Difficulty Reports; matched by N-number and serial number.RT MLG ATTACH RIB FITTING FOUND WITH CORROSION ON FACES AND IN BORES OF MLG ATTACH LUGS. REPAIRED PER ERA 331716-14.
From FAA Service Difficulty Reports; matched by N-number and serial number.A AND B LOOP FIRE WARNING ON NR 3 ENG. FOUND BOROSCOPE PLUG LOOSE AT THE NUMBER TWO FUEL NOZZLE.
From FAA Service Difficulty Reports; matched by N-number and serial number.THE CENTER WING INTERMEDIATE SPAR UPPER CAP LOCATED AT STA 1103 WAS FOUND TO HAVE A 2 INCH CRACK ON THE RT O/B SIDE. THE CRACK WAS TYPICAL OF THOSE DESCRIBED IN S/B 093-57-087, BUT IS BEYOND THE ALLOWABLE LIMITS. THIS ER/A REPAIRS THE CRACKED UPPER CAP BY CUTTING AWAY THE DAMAGED SECTION AND…
From FAA Service Difficulty Reports; matched by N-number and serial number.ONE OF THE SIX SPOKES ON THE LT NEGATIVE PRESSURE RELIEF VALVE ON THE AFT PRESSURE BULKHEAD WAS FOUND CRACKED. THE REPAIR/ MODIFICATION WAS ACCOMPLISHED PER L-1011 S/B 093-53-249, REV 2.
From FAA Service Difficulty Reports; matched by N-number and serial number.ON T/O, NUMBER 3 ENGINE INGESTED AT LEAST ONE LARGE BIRD. PERFORMED FIRST STAGE HPC BORESCOPE INSPECTION AS PER MM. ENGINE FAILED INSPECTION, WILL REQUIRE ENGINE REPLACEMENT AS PER FIM 71-99-00 AND MM.
From FAA Service Difficulty Reports; matched by N-number and serial number.Showing the 10 most recent of 87 reports.