N23657

No registry detail on file · not in current registry

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.

7 reports on file, 1999-07-20 – 2005-08-29.

OTHER · 2005-08-29 Matched by certificate designator
ATA 3210

Part: TRUNNION PIN — FRACTURED (RT MLG) · airframe 19,513 hrs · 10,114 cycles

THE FLIGHT CREW REPORTED A LOUD NOISE UPON LANDING AT ORD. INSPECTION BY MAINTENANCE FOUND THE RT MLG TRUNNION PIN FRACTURED. THE RT MLG WAS REMOVED AND REPLACED. AN FCD WAS ISSUED TO INSPECT THE REMAINDER OF THE FLEET.

Source: SDR CALA0500286
OTHER · 2004-02-27 Matched by certificate designator
ATA 5730

Part: SKIN — CRACKED (RT WING LE) · airframe 15,859 hrs · 8,221 cycles

INSPECTION FOUND A 2.125 INCH CRACK IN RIGHT WING L/E SKIN AT NR 3 KRUEGER FLAP. THE AREA WAS REPAIRED IAW SRM 57-41-01, FIGURE 203.

Source: SDR CALA0400179
OTHER · 2004-02-23 Matched by certificate designator
ATA 5510

Part: ATTACH FITTING — GOUGED (HORIZ STAB) · airframe 15,859 hrs · 8,221 cycles

INSPECTION FOUND HORIZONTAL STABILIZER FORWARD RIGHT LOWER ATTACH LUG GOUGED BY CLEVIS PIN FROM LOWER RIGHT SLIDER. THE GOUGE WAS BLENDED, FLAP PEENED, TREATED AND PRIMED IAW SRM 55-10-10 AND 51-20-06.

Source: SDR CALA0400156
OTHER · 2004-02-19 Matched by certificate designator
ATA 5320

Part: WEB — CORRODED (FUSELAGE) · airframe 15,859 hrs · 8,221 cycles

INSPECTION FOUND THE C-2 DOOR THRESHOLD WEB CORRODED. THE THRESHOLD WEB WAS REMOVED AND REPLACED IAW SRM 51-10-2.

Source: SDR CALA0400137
OTHER · 2004-02-19 Matched by certificate designator
ATA 5320

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 15,859 hrs · 8,221 cycles

INSPECTION FOUND FLOOR SUPPORTS CRACKED AT FASTENER HOLES AT STA 540, RBL 2 AND LBL 2. THERE WAS ONE CRACK IN EACH SUPPORT AND BOTH WERE TWO INCHES LONG. THE FLOOR SUPPORTS WERE REPLACED IAW SRM 51-40-2.

Source: SDR CALA0400139
OTHER · 2004-02-18 Matched by certificate designator
ATA 5320

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 15,859 hrs · 8,221 cycles

INSPECTION FOUND A HOLE IN CABIN FLOOR INTERCOSTAL JUST FORWARD OF STA 360, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-10-02.

Source: SDR CALA0400134
OTHER · 1999-07-20 Matched by certificate designator
ATA 2565

Part: SLIDE — LOW PRESSURE (CABIN)

INSPECTION FOUND RIGHT AFT SLIDE PRESSURE IN THE RED BAND. THE SLIDE WAS REMOVED AND REPLACED IAW MM 25-61-35.

Source: SDR CALA9900841