N475DA
Registered owner: AEROSIM ACADEMY INC, FL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| Delta Connection Academy, Inc. | Operator | on 2008-06-05 | Operator named in NTSB report |
Accident & incident history
Operated by Delta Connection Academy, Inc. (per NTSB report)
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.
23 reports on file, 1995-02-06 – 1998-09-27.
Part: BATTERY PACK — DISCHARGED (CABIN)
LT OVERWING EXIT DOOR(S), EMERGENCY LIGHTS INOP. REPLACED LT OVERWING EXIT DOOR(S) BATTERY PACK, SYSTEM OPS. NORMAL PER MM.
Part: BATTERY PACK — DISCHARGED (CABIN)
FOUND LEFT OVERWING EMERGENCY EXIT LIGHT FWD POS INOP. REPLACED BATTERY PACK.
Part: BATTERY PACK — DISCHARGED (CABIN)
FIRST CLASS CEILING EMERGENCY LIGHT OUT. REPLACED BATTERY PACK.
Part: BYPASS LIGHT — ILLUMINATED (NR 3 ENGINE)
NR 3 ENG FILTER BYPASS LIGHT ILLUM. ENG WAS SHUTDOWN. ENG WINDMILLED FOR REST OF FLT. REMOVED AND INSPECTED NR 3 OIL FILTER, NO MATERIAL IN FILTER. CHIP DETECTOR ALSO CLEAN. FWD OIL BYPASS SYS TO MCO AND PLAC PER 79-00-02. WINDMILLING OK PER MM 71-00 PG 2.
Part: AUX SPAR — CHAFED (LT WING)
FOUND ON A1 LTR CHECK, MLG CHAFING FWD SURFACE OF AUX SPAR I/B END. REPAIRED PER M/M 57-43-0.
Part: RIB — CRACKED (NR 4 LE SLAT)
FOUND ON A1 LTR CHECK, NR 4 SLAT NOSE RIB CRACKED 1.5 INCH O/B SIDE OF ACTUATOR ROD END. REPAIRED PER M/M 57-54-0.
Part: FITTING — CRACKED (FUSELAGE)
FOUND ON A1 LETTER CK, UPPER FLANGE OF LT INBD TENSION TIE FITTING CRACKED. REPLACED FITTING PER BOEING DWG NR 65-17509 REV M.
Part: STIFFENER — CRACKED (RT LE SPAR)
FOUND ON A1 LETTER CK, 2 SPAR STIFFENERS CRACKED AT NR 7 SLAT INBD AND OUTBD STIFFENERS AT THE OUTBD TRACK. REPLACED STIFFENERS PER MM 57-20-21.
Earlier reports · 1995–1997 · 15 reports
1997
Part: LINE — FAILED (NR 5 SPOILER)
HYD LINE TO NR 5 SPOILER CRACKED. CRACK IS OUTBD OF T-FITTING AND BENDS. LOST B-SYSTEM HYD FLUID. EMERGENCY EQUIPMENT CALLED OUT.
Part: WEB — CRACKED (BS 1303)
VERT WEB ABOVE S-DUCT AT STA 1303 HAS 2 INCH CRACKS AT LT SIDE ONE AT LWR CORNER AND ONE APPROX SIX INCHES ABOVE LWR CORNER. VERT WEB ABOVE S-DUCT AT STA 1303 HAS 1 INCH CRACK AT LWR RT CORNER. REPAIRED PER MM 53-11-0 FIG 825.
Part: DOOR FRAME — CRACKED (BS 783.95)
DURING INSPECTION, FOUND TWO CRACKS AT THE LT OVERWING EXIT FRAME AT STATION 783.95. REPAIRED PER S/B 727-53-0197 REV 2 (DELTA EO 4-61904-3AD).
Part: FLOORBEAM — CORRODED (BS 344)
FOUND FLOORBEAM CORRODED AROUND SCREW HOLES 2BL, 30 TO SIDEWALL STA 344. REPAIRED CHORD PER SRM 53-10-8 FIG 11.
Part: FLOORBEAM — CORRODED (BS 344)
AT MIDVISIT, THE FLOORBEAM AT STA 344 WAS FOUND TO BE CORRODED. CORR WAS REMOVED PER SRM 51-10-6 OUT OF LIMITS. REMOVED FLOORBEAM FROM SPLICE TO O/B WALL LT SIDE, DRILLED, REPLACED CHORD PER SRM 53-10-8 FIG 11 AND SPLICE INSTALLED PER SRM 53-10-8.
Part: FITTING — CHAFED (LT WING)
FOUND ON F1 LETTER CK, MLG CHAFING FWD SIDE OF AUX SPAR. REPAIRED PER MM 57-43-0.
Part: STIFFENER — CRACKED (LT WING)
FOUND DURING F-1 LETTER CHECK, I/B SPAR STIFFENER CRACKED AT NR 3 L/E SLAT O/B TRACK. REPAIRED PER M/M 57-20-21.
1996
Part: LIGHT — INOPERATIVE (AFT AIRSTAIR)
FOUND BOTH EMERGENCY EXIT LIGHTS IN AFT AIRSTAIR INOPERATIVE. CLEANED BATTERY TERMINALS, OPS CK OK.
Part: SKIN — GOUGED (NR 5 LE SLAT)
DEEP GOUGE IN LWR SKIN BY LINE UP SPADE. REPAIRED PER SRM 57-50-3.
Part: LIGHT — INOPERATIVE (AIRSTAIRS)
EMERGENCY EXIT LIGHT OVER BOTTOM STEP OF AIRSTAIRS INOP. REPLACED BATTERIES AND BULB, NO HELP. REPLACED LIGHT ASSY, OPN NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN)
ON L/O CHECK, FOUND EMERGENCY LIGHTS OUT FROM ROW 27 AFT TO F/A SEAT. REPLACED BATTERY PACK M9027 AND OPS CHECKS NORMAL.
1995
Part: STIFFENER — CRACKED (WS 588)
FRONT SPAR STIFFENER, NOSE RIB ATTACH BRACKET CRACKED BETWEEN TWO LOWER FASTENERS AT NR 7 SLAT INBOARD TRACK AT APPROX IWS 588. REPLACED STIFFENER PER MM 57-20-21.
Part: LE SKIN — DAMAGED (NR 3 FOREFLAP)
FOUND DURING D-2 LETTER CHECK - NR 3 T/E FOREFLAP LEADING EDGE SKIN DAMAGED. REPAIRED PER SRM 57-50-4 FIG 1.
Part: SKIN — CRACKED (FUSELAGE)
FOUND DURING D-2 LETTER CHECK - 1 INCH CRACK AT SKIN WHERE NR 4 JACKSCREW FAIRING BUTTS. REPAIRED PER SRM 53-50-3 FIG 2.
Part: RIB — CRACKED (NR 3 LE FLAP)
DURING SHOP INSPECTION, FOUND LEFT WING NR 3 SLAT WITH THE LOWER CHORD DAMAGED OUBOARD OF THE INBOARD UP STOP FITTING AND RIB NR 10 CRACKED AT ITS LOWER END, OUTBOARD OF ACTUATOR ATTACH FITTING. REPAIRED PER MM 57-54-0.