N83071
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
33 reports on file, 1995-10-03 – 1999-06-04.
Part: SUPPORT — CORRODED (LT & RT MLG)
INSPECTION FOUND LT AND RT MLG A FRAME SUPPORT BEAM BOLT HOLES CORRODED. THE SUPPORT BEAM WAS REPAIRED IAW SRM 57-20-00, PAGE 104.
Part: MOUNTING — CORRODED (BS 1876-1886)
INSPECTION FOUND MOUNTING PLATE ASSEMBLY CORRODED AT STA 1876-1886 FROM POSITION X = 0.02L TO X = 0.10L. THE MOUNTING PLATE WAS REMOVED AND A NEW PLATE WAS INSTALLED IAW SRM 53-16-01.
Part: FLOORBEAM — CORRODED (BS 1903)
INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1903 FROM POSITION X = 0.25L TO X = 0.25R. THE FLOOR SUPPORT BEAM WAS REPLACED IAW 53-16-00, FIGURE 10.
Part: SEAT TRACK — CORRODED (BS 1866-1856)
INSPECTION FOUND LT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74L. THE SECTION OF SEAT TRACK WAS REPAIRED IAW SRM 53-70-00, FIGURE 6.
Part: BEAM — CORRODED (BS 1876-1810)
INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1876 TO 1810 AT POSITION X = 0.36L AND X = 0.36R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: SEAT TRACK — CORRODED (BS 1876-1866)
INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1876-1866 AT POSITION X = 0.60R AND X = 0.60L. THE SEAT TRACK SECTIONS WERE REPAIRED IAW SRM 53-70-00, FIGURE 6.
Part: BEAM — CORRODED (BS 1996-1903)
INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1996 TO 1903 AT POSITION X = 0.20R AND X = 0.20L. THE CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: BULKHEAD TEE — CORRODED (BS 2007)
INSPECTION FOUND T-SECTION ON FORWARD FACE OF REAR PRESSURE BULKHEAD AT STA 2007 FROM POSITION X = 0.55L TO X = 0.65L CORRODED. THE CORRODED SECTION WAS REMOVED AND A SPLICE REPAIR WAS INSTALLED IAW SRM 53-40-00, FIGURE 16.
Part: BEAM — CORRODED (BS 1986)
INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.27R TO X = 0.53R. THE BEAM SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: BEAM — CORRODED (BS 1887-1839)
INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 1887 TO 1839 AT POSITION X = 0.03L AND X + 0.03R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: BEAM — CORRODED (BS 1986)
INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1986 FROM POSITION X = 0.60R TO 0.90R. THE CORRODED SECTION OF BEAM WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: BEAM — CORRODED (BS 2007-1893)
INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1893 AT POSITION X = 0.60L AND X = 0.60R. THE CORRODED BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: FLOORBEAM — CORRODED (BS 1876)
INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X =0.04R TO X = 0.22R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: BEAM — CORRODED (BS 1866)
INSPECTION FOUND LATERAL FLOOR SUPPORT BEAM CORRODED AT STA 1866, POSITION X = 0.03L TO X = 0.28L AND POSITION X = 0.03R TO X = 0.28R. THE BEAM SECTIONS WERE REPLACED IAW SRM 53-16-00 FIGURE 10.
Part: BEAM — CORRODED (BS 2007-1876)
INSPECTION FOUND LONGITUDINAL FLOOR SUPPORT BEAM CORRODED FROM STA 2007 TO 1876 AT POSITION X = 0.25R AND X = 0.25L. THE CORRODED SECTIONS OF BEAM WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: FLOORBEAM — CORRODED (BS 1876)
INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.04L TO X = 0.22L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: FLOORBEAM — CORRODED (BS 1876)
INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27L TO X = 0.38L. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: FLOORBEAM — CORRODED (BS 1876)
INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.60R TO X = 0.90R AND POSITION X = 0.60L TO X = 0.90L. THE FLOORBEAM CAPPING SECTIONS WERE REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: FLOORBEAM — CORRODED (BS 1876)
INSPECTION FOUND FLOORBEAM CAPPING SECTION CORRODED AT STA 1876 FROM POSITION X = 0.27R TO X = 0.33R AND POSITION X = 0.38R TO X = 0.56R. THE FLOORBEAM CAPPING SECTION WAS REPLACED IAW SRM 53-16-00, FIGURE 10.
Part: SEAT TRACK — CORRODED (BS 1866-1856)
INSPECTION FOUND RT SEAT TRACK CORRODED FROM STA 1866 TO 1856 AT POSITION X = 0.74R. THE CORRODED SECTION FOR SEAT TRACK WAS REPLACED IAW SRM 53-70-00, FIGURE 6.
Earlier reports · 1995–1998 · 13 reports
1998
Part: LIGHT — INOPERATIVE (LAVATORY)
INSPECTION FOUND THE EMERGENCY FLOODLIGHT AT LAV B INOPERATIVE. THE FLOODLIGHT WAS REPLACED IAW MM 33-50-00.
Part: BATTERIES — DISCHARGED (MEGAPHONE)
INSPECTION FOUND AFT MEGAPHONE INOPERATIVE. THE MEGAPHONE BATTERIES WERE REPLACED AND OPERATION CHECKED GOOD IAW MM 25-60-00.
Part: ANGLE — CRACKED (WS 118)
INSPECTION FOUND A 1 CRACK IN ANGLE AT LT WHEEL WELL REAR SPAR, WS 118. THE ANGLE WAS REMOVED AND A NEW ANGLE WAS FABRICATED AND INSTALLED IAW SRM 51-20-00, 51-33-01, AND 51-31-01.
Part: TRIM MOTOR — CRACKED (HORZ STAB)
THE HYDRAULIC SYSTEM 3 ELEVATOR OFF LIGHT ILLUMINATED WHILE EN ROUTE TO EWR. APPROPRIATE CHECKLISTS WERE FOLLOWED AND BOTH PUMPS WERE SHUTOFF. THE HYDRAULIC FLUID DEPLETED TO ZERO VERY SLOWLY AND THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE FOUND THE HORIZONTAL STABILIZER TRIM MOTOR HOUSING CRACKED. THE STAB TRIM MOTOR WAS REMOVED AND REPLACED IAW MM 29-00. SYSTEM OPERATIONAL AND LEAK CHECKS WERE GOOD.
Part: SKIN — DENTED (LT LE FLAP)
INSPECTION FOUND A 2 X 3 DENT IN LT INBOARD LEADING EDGE SLAT WITH SIX POPPED RIVETS AT STA XIS 240.844. REPAIRED IAW ECRA 5750-02897 AND PLACED ON DIP TO REPLACE RIB WITHIN 365 DAYS OR NEXT C-CHECK.
1997
Part: FIRE LOOP — CHAFED (NR 2 ENGINE)
THE NR 2 ENGINE FIRE WARNING LIGHT FOR B-LOOP (A LOOP WAS ON PLACARD) ILLUMINATED TEN MINUTES AFTER TAKEOFF. THE NR 2 ENGINE WAS SHUT DOWN, BOTH FIRE BOTTLES WERE DISCHARGED AND THE AIRCRAFT WAS RETURNED TO LGW WHERE IT LANDED WITHOUT INCIDENT. MAINTENANCE FOUND NO EVIDENCE OF FIRE. MAINTENANCE FOUND BOTH A AND B FIRE LOOPS CHAFED THROUGH. BOTH LOOPS WERE REMOVED AND REPLACED. IN ADDITION, BOTH FIRE BOTTLES WERE REPLACED.
Part: SUPPORT — CORRODED (BS 1880-2007)
INSPECTION FOUND FLOOR SUPPORTS CORRODED AT STA 1880-2007, LBL 24 AND RBL 24. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-33-01.
Part: SUPPORT — CORRODED (BS 1887)
INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1887, RBL 24-80, LBL 20-80, AND LBL 3- RBL 3. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01.
Part: SUPPORT — CORRODED (BS 1875)
INSPECTION FOUND CORROSION ON FLOOR SUPPORTS AT STA 1875, LBL 30 AND RBL 30. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 53-16-01 AND 51-35-01.
Part: INTERCOSTAL — CORRODED (BS 1720-1740)
INSPECTION FOUND CENTER CARGO INTERCOSTAL CORRODED BETWEEN STA 1720-1740, STRINGER 51-52R. A NEW INTERCOSTAL WAS FABRICATED AND INSTALLED IAW SRM 53-00-01.
1995
Part: BEARING — FAILED (NR 2 ENGINE)
FLT NR 28 - LGW - THE NR 2 ENGINE WAS SHUT DOWN FOR LOSS OF OIL WHILE EN ROUTE TO LGW. THE ENGINE WAS SHUT DOWN WITH POSITIVE OIL PRESSURE AND THE AIRCRAFT LANDED AT LGW WITHOUT INCIDENT. PRELIMINARY FINDINGS REVEALED THE TRANSFER GEARBOX HAD SEPARATED FROM THE ENGINE. PRIMARY CAUSE OF FAILURE WAS DUE TO FAILURE OF LOWER RADIAL DRIVESHAFT BEARING. (M)
Part: EEL BATT CHRGER — INOPERATIVE (CABIN)
EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED. (X)
Part: EEL BATT CHARGER — INOPERATIVE (CABIN)
EWR - FLT 0012 - WHEN THE EMERGENCY LIGHT SWITCH WAS PLACED ON AFTER ARRIVING IN EWR, THE FORWARD FIRST CLASS AREA AND AFT COACH SECTION TRACK LIGHTING WOULD NOT COME ON. BOTH EMERGENCY LIGHT BATTERY CHARGERS WERE REMOVED AND REPLACED AND OPERATION OF THE TRACK LIGHTING WAS RESTORED. (X)