N2822W
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.
13 reports on file, 1995-02-05 – 1995-12-05.
Part: SKIN — CRACKED (BS 580)
LEFT FUSELAGE SKIN CRACKED TWO STRINGERS ABOVE THE 'E' IN 'DELTA', JUST FORWARD OF STA 580 AND UNDER STR 4. CUT OUT DAMAGED AREAS AND INSTALLED DOUBLERS PER ERA 302855-14 ON NR 011.
Part: BATTERY PACK — DISCHARGED (CABIN)
CENTER AISLE EMERGENCY EXIT SIGN FLASHES. REPLACED BATTERY PACK, CHECKS GOOD.
Part: SHUT DN SWITCH — FAILED (APU)
APU FIRE TEST INCOMPLETE, RED WARNING LIGHT IN FIRE HANDLE DOES NOT ILLUMINATE DURING TEST (HORN SOUNDS GOOD). APU STARTS NORMALLY AFTER RESET. REPLACED THE APU FIRE SHUT-DOWN SWITCH. SYSTEM TEST NORMAL.
Part: PBE — POPPED INDICATOR (CABIN)
DURING PRE-FLIGHT, FOUND FWD CABIN PBE INDICATOR POPPED. REPLACED PBE.
Part: RIBS — CRACKED (NR 3 SLAT)
DURING SHOP INSPECTION FOR NR 3 L/E SLAT, CRACKS WERE FOUND IN THE L/E SUPPORT RIBS ON INBD AND OTBD SIDES OF ACTUATOR SUPPORT FITTING. REPAIRED PER MM 57-54-0.
Part: ACTUATOR — FAILED (NR 3 SLAT)
FLT 1400 CALLED EMERGENCY APPROACH INTO SFO, A HYD SYST LEAKING RAPIDLY. CREW FREE FEEL LANDING GEAR TO ACCOMPLISH LDG GEAR EXTENSION. MTC TOWED A/C TO GATE AND FOUND NR 3 LEADING EDGE SLAT ACTUATOR END BLOWN /SEPERATED FROM PISTON. ACTUATOR END REMOVAL AND REPLACEMENT OF ACTUATOR COMPLIED WITH. GEAR SWING ACCOMPLISHED, SYST OPS CHECK NORMAL.
Part: FRAME — CRACKED (BS 913)
FOUND DURING E-2 LETTER CHECK, BS 913 FRAME CRACKED LT MLG WHEEL WELL. REPAIRED PER MM 53-11-0 PAR 20.
Part: RIB — CRACKED (NR 4 LE SLAT)
FOUND DURING E-2 LETTER CHECK, NR 4 L/E SLAT L/E RIB CRACKED I/B OF ACTUATOR ROD END AND RIB CRACKED O/B OF ACTUATOR ROD END. REPAIRED PER MM 57-54-0 PAR 3.
Part: SKIN — WORN (NR 3 TE FLAP)
LE SKIN WAS FOUND WORN APPOX 16 INCHES FROM IB END. DAMAGE WAS REPAIRED PER SRM 57574, BY INSTALLING A REPAIR DOUBLER. ALL THE ABOVE ACTION WAS DURING A SHOP VISIT, FOR NR 3 FORE FLAP.
Part: SKIN — WORN (NR 2 TE FLAP)
THE LEADING EDGE HAD A WORN AREA APPROX 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE AREA WAS REPAIRED PER SRM 57-50-4 FIG 1, FOR NR 2 FLAP PANEL DURING SHOP INSPECTION.
Part: SKIN — WORN (LT TE FLAP)
THE LE WAS WORN 51 INCHES FROM THE I/B END. AN EXTERNAL DOUBLER WAS INSTALLED PER SRM 57-50-4 FIG 1 DURING SHOP INSPECTION OF NR 2 FORE FLAP.
Part: SKIN — WORN (LT TE FLAP)
TRANSFER FROM N/R CARD NR 6348, THE L/E WAS WORN 2 INCHES FROM THE O/B END ON THE BOTTOM SIDE. THE WRONG TYPE OF RIVETS WERE INSTALLED ON THE ORIGINAL DOUBLER. CARD 6477 WAS ISSUED TO CORRECT THIS ACTION. THE REPAIR WAS PER SRM 57-50-4 FIG 1.
Part: DETECTOR UNIT — FAILED (NR 1 ENGINE)
ON CLIMB-OUT, NR 1 ENGINE STRUT OVERHEAT ILLUMINATED, UNABLE TO EXTINGUISH, SHUT DOWN NR 1 ENGINE. REPLACED DETECTOR UNIT, SECURED DUCT CLAMP AT 13TH STAGE VALVE, RETURNED TO SERVICE.