N469DA
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.
34 reports on file, 1995-03-15 – 1998-10-31.
Part: BATTERY PACK — DISCHARGED (CABIN)
RT WING INTERIOR EMERGENCY EXIT LIGHTS TEST OK BUT DO NOT OPERATE IN THE ARMED POSITION. REPLACED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (EMERGENCY EXIT)
RT OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED BATTERY PACK.
Part: ANGLE — CRACKED (BS 910)
REF SHIP 469 TPA LETTER CHK E-2, VERTICAL ANGLE CRACKED RT WHEEL WELL STA 910. REPAIRED PER M/M 53-11-0.
Part: BATTERY PACK — DISCHARGED (CABIN)
ON PREFLIGHT, EMER STRIP LIGHTING DID NOT ILLUM IN MIDDLE OF CABIN. FERRIED A/C TO DFW. REPLACED M9026 RACK AND BATTERY PACK, SYSTEM CK NORMAL.
Part: RACK — INOPERATIVE (CABIN)
EMER EXIT FLOOR TRACK WILL NOT SHUT OFF. REPLACED EMER LIGHT RACK IN FIRST CLASS OVERHEAD CEILING.
Part: POWER SUPPLY — INOPERATIVE (CABIN)
TRACK LIGHTING OUT BETWEEN ROW 12DEF AND 19DEF. REPLACED POWER SUPPLY.
Part: STIFFENER — CRACKED (LE FLAP)
L/E SPAR STIFFENER CRACKED NR 2 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21 PG 813.
Part: STIFFENER — CRACKED (LE FLAP)
FOUND AT E1 LETTER CK, L/E SPAR STIFFENER CRACKED I/B SIDE OF 7 SLAT I/B TRACK. REPAIRED PER M/M 57-20-21.
Part: STIFFENER — CRACKED (LT FLAP)
FOUND AT LETTER CHECK E1, L/E SPAR STIFFENER CRACKED O/B SIDE NR 7 SLAT O/B TRACK. REPAIRED PER M/M 57-20-21.
Part: BATTERY PACK — DISCHARGED (CABIN)
LIGHTED EXIT SIGN EMERG LIGHT INOP OVER RT OVERWING EXIT. REPLACED BATTERY PACK, OPN CKS OK.
Part: BATTERY PACK — LOOSE (CABIN)
OVERHEAD AISLE EMERG LIGHT INOP AT ROW 26. FOUND BATTERY PACK LOOSE. SECURED, OPN CKS OK.
Part: BATTERY — DISCHARGED (CABIN)
EMERGENCY LIGHTS INOP AT SEVERAL LOCATIONS IN CABIN. REPLACED 3 BATTERY PACKS, OPN NOW NORMAL.
Earlier reports · 1995–1997 · 22 reports
1997
Part: SKIN — CRACKED (L 1 DOOR)
EXTERIOR SKIN CRACKED AT THE UPPER HINGE CUTOUT OF THEL-1 DOOR. ROUTED OUT DAMAGED SKIN AND FABRICATED DOUBLER PER M/M 52-1101 PG 808. INSTALLED DOUBLER PER M/M 52-11-01 PAGE 808.
Part: BATTERY PACK — DISCHARGED (CABIN)
CENTER AISLE EMERG EXIT SIGN AFT SIDE WON'T TEST. REPLACED PWR SUPPLY AND BATTERY PACK, CKS OK.
Part: BATTERY PACK — DISCHARGED (CABIN)
OVERWING EMERG EXIT SIGN OVER RT FWD AND AFT EXITS WON'T TEST. REPLACED BATTERY PACK, OPN CKS OK.
Part: DOUBLER — CRACKED (R1 DOORWAY)
A .625 INCH CRACK WAS FOUND IN THE UPPER HINGE CUTOUT DOUBLER OF THE R-1 DOOR WHILE THE A/C WAS IN TPA. MX COULD NOT ACCOMPLISH THE PERMANENT REPAIR DUE TO INADEQUATE TIME FOR GALLEY REMOVAL. THIS ER/A AUTHORIZED A MINOR DEVIATION, WHICH WAS COMPRISED OF A FASTENER SUBSTITUTION, TO THE MAJOR REPAIR IN B727 MM 53-30-00-807 ON A TIME-LIMITED BAISIS. FURTHER EDDY CURRENT INSP IN ATL ON 10SEPT97 REVEALED A CRACK IN THE BEAR STRAP AND A STOP DRILL IN THE ADJACENT FRAME. A PERMANENT REPAIR WILL BE ACCOMPLISHED AT THIS TIME. REPAIRED PER ERA 362185-14 REV B.
Part: BATTERY PACK — DISCHARGED (CABIN)
EMERGENCY EXIT FLOOR STRIP LIGHTING INOP 1ST CLASS SECTION WOULD NOT ILLUMINATE WHEN SWITCH TURNED ON OR WITH ESSENTIAL PWR IN STBY. REPLACED BATTERY PACK AND BATTERY.
Part: FUSE — BLOWN (CABIN)
FOUND EMERGENCY FLOOR PATH LIGHTS INOP LAST QUARTER OF CABIN. REPLACED AFT BATTERY PACK AND POWER SUPPLY.
Part: BATTERY PACK — DISCHARGED (CABIN)
RT EMERGENCY OVERWING DOOR EXIT LIGHTS INOP. REPLACED BATTERY PACK, CHECKED OK.
1996
Part: BATTERY — DISCHARGED (CABIN)
OVERWING EMERGENCY LIGHT INOP. REPLACED RACK AND BATTERY.
Part: SEAL STRIKER — CRACKED (NR 2 ENG)
FOUND ON C-2 LETTER CHECK, SEAL STRIKER FOR L/E OF RT FORWARD COWLS DAMAGED AT 3.00 AND 9.00 POSITIONS. REPAIRED PER M/M 53-11-0, PAGE 801.
Part: STRINGER — CRACKED (VERT STAB)
FOUND ON C-2 LETTER CHECK, STRINGER CRACKED SECOND BAY DOWN FROM TOP LEFT SIDE INSIDE VERTICAL FIN. REPAIRED PER M/M 55-30-0. FIG 803.
Part: STRINGER — CRACKED (VERT STAB)
FOUND ON C-2 LETTER CHECK, STRINGER CRACKED TOP BAY RT SIDE AT ATTACH BOLT, INSIDE VERTICAL FIN. REPAIRED PER M/M 55-30-0, FIGURE 803.
Part: TORQUE BOX WEB — CRACKED (BS 1263)
FOUND ON C-2 LETTER CHECK, .50 INCH CRACK AT LOWER EDGE OF TORQUE BOX LIGHTING HOLE, STA 1263 RT SIDE. REPAIRED PER M/M 53-11-0.
Part: RIB — WORN (NR 8 LE SLAT)
DURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGED INTERNAL SUPPORT RIB. ACCOMPLISHED REPAIRS PER SRM 57-50-3.
Part: SKIN — DAMAGED (NR 8 LE SLAT)
DURING INSPECTION, NR 8 L/E SLAT WAS FOUND WITH DAMAGE TO OUTBOARD CORNER OF SKIN, APPROX 10 INCHES. REPAIRED PER SRM 57-50-3, FIG 5.
Part: VALVE — STICKING (RT PACK)
AT 18,000 FT CABIN CLIMB 1000 FPM, STANDBY AND MANUAL NO HELP. MADE EMERGENCY DESCENT TO 11,000 FT. FOUND RT PACK VALVE STICKING CLOSED. REPLACED SAME, OPS CKS. REMOVED BOTH WATER SEP BAGS, NO OBSTRUCTIONS FOUND. REINSTALLED PRESSURIZATION, CHECK NORMAL.
Part: SKIN — CORRODED (FS 680-720)
DURING INSPECTION, CORROSION WAS FOUND ON THE FUSELAGE SKIN AT STA 700 TO 720F FROM STR 26R TO 27R. THE SKIN PANEL WILL BE REPLACED IN ACCORDANCE WITH B727 SRM 51-10-1.
Part: FLOORBEAM — CORRODED (BS 344)
FOUND ON MV-1 CHECK, CORROSION ON FLOORBEAM STA 344 RBL 45. REPAIRED PER SRM 53-10-8 FIG 10.
1995
Part: SKIN — CRACKED (BS 1308)
FOUND DURING C-1 LETTER CHECK - .75 INCH HOLE IN 48 SEC TORQUE BOX SKIN RT STA 1308 - .3750 INCH CRACK IN 48 SEC TORQUE BOX SKIN AT LIGHTNING HOLE STA 1235 RT. REPAIRS MADE PER M/M 53-11-0, PGS 802 - 832, AND 833.
Part: DOUBLER — CRACKED (NR 7 LE SLAT)
FOUND DURING C-1 LETTER CHECK - DOUBLER UNDERNEATH I/B STOP PAD NR 7 SLAT IS CRACKED. REPAIRED PER MM 57-54-0 PAR 12.
Part: RIB — CRACKED (NR 7 LE SLAT)
FOUND DURING C-1 LETTER CHECK - 1.25 INCH CRACK IN RIB ON NR 7 SLAT I/B OF I/B TRACK. REPAIRED PER MM 57-54-0.
Part: STIFFENER — CRACKED (1183 BULKHEAD)
FOUND DURING B-2 LETTER CHECK, 1 INCH CRACK AT VERTICAL STIFFENER ON 1183 BULKHED LWR RADIUS BLOCK. INSTALLED DOUBLER PER N.N. 53-11-0 PG 811.
Part: ANGLE — CRACKED (NR 2 FIREWALL)
FWD LEFT COWL LIP ON FIREWALL DAMAGED 8:00 POSITION. NBR 2 ENG. FOUND DURING B-2 LETTER CHECK.