N223DZ
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.
15 reports on file, 2000-04-25 – 2006-06-08.
Part: ATTACH FITTING — DAMAGED (HORIZ STAB) · airframe 42,804 hrs · 24,074 cycles
DURING AN A-CHECK/BRIDGING CHECK FOR RETURN TO SERVICE FROM STORAGE, MAINTENANCE DISCOVERED A TIME LIMITED BLENDOUT REPAIR TO THE AFT FACE OF THE LEFT HORIZONTAL STABILIZER LOWER FORWARD ATTACH LUG. REWORKED AFT FACE OF LOWER FORWARD ATTACH LUG PER DELTA ENGINEERING REPAIR/AUTHORIZATION 089066-14 REVISION D DATED 5/10/06 WITH FAA 8100-9 APPROVAL DATED 5/30/2006.
Part: SKIN — CHAFED (TR FLAPS) · airframe 42,804 hrs · 24,074 cycles
INSPECTION NOTED A CHAFED AREA ON AN EXISTING SRM ALUMINUM REPAIR DOUBLER ON THE RIGHT WING OUTBOARD FLAP MID-FLAP LEADING EDGE 20 INCHES FROM THE INBOARD END. REPAIRED DAMAGED AREA IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE REPORT EA 57-145 DATED 05/25/06 WITH FAA DER APPROVAL FORM 8110-3 DATED MAY 30, 2006.
Part: SKIN — CRACKED (NR 5 SLAT) · airframe 42,804 hrs · 24,074 cycles
INSPECTION NOTED CRACKS AT SEVERAL FASTENER LOCATIONS IN THE NR 5 SLAT LOWER TRAILING EDGE SKIN PANEL UNDER THE SLAT ACTUATOR. REPAIRED DAMAGED AREA IN ACCORDANCE WITH SRM 57-43-01.
Part: SKIN — CRACKED (NR 3 SLAT) · airframe 42,804 hrs · 24,074 cycles
INSPECTION NOTED SEVERAL CRACKS IN THE NR 3 SLAT LOWER TRAILING EDGE SKIN BELOW THE SLAT ACTUATOR. REPAIRED DAMAGED AREA PER SRM 57-43-01.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 42,804 hrs · 24,074 cycles
AN EXISTING REPAIR TO THE FUSELAGE SKIN BETWEEN THE L1 DOOR HINGES JUST FORWARD OF THE DOOR REQUIRES REWORK TO REMOVE THE DAMAGE. REWORKED DAMAGED AREA IAW EA NR 53-146 DATED 05/26/06 WITH FAA DER APPROVED 8110-3 DATED MAY 27, 2006..
Part: SKIN — CRACKED (NR 5 SLAT) · airframe 42,804 hrs · 24,074 cycles
INSPECTION NOTED A GOUGE ON THE NR 5 SLAT UPPER LEADING EDGE SURFACE 28 INCHES FROM THE INBOARD END (SS169.0). REPAIRED DAMAGED AREA IN ACCORDANCE WITH PACE AIRLINES REPAIR PROCEDURE REPORT EA 57-140 DATED 05/20/06 WITH FAA DER APPROVED 8110-3 DATED MAY 20, 2006.
Earlier reports · 2000–2004 · 9 reports
2004
Part: SKIN — DENTED (FUSELAGE) · airframe 40,343 hrs · 20,708 cycles
A DENT AND GOUGE WERE NOTED IN THE UPPER SKIN AT BS 807 NEAR S25R. DAMAGE WAS REMOVED AND REPAIRED IAW ERA 089247-14.
Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 40,343 hrs · 20,708 cycles
CORROSION WAS NOTED ON THE UPPER CAP OF THE BS 986.5 FLOORBEAM. UPPER CAP REMOVED AND NEW SECTION SPLICED IN PER ERA 089197-14.
Part: SKIN — DENTED (FUSELAGE) · airframe 40,343 hrs · 20,708 cycles
TWO DENTS WERE NOTED IN THE FUSELAGE SKIN JUST ABOVE S16L, NEAR BS 384 AND 400. DAMAGE WAS REWORKED PER ERA 089089-14.
Part: SPAR — FATIGUED (RT WING) · airframe 40,343 hrs · 20,708 cycles
THE LEFT WING REAR SPAR CHORD WAS FOUND TO BE CRACKED AT APPROX RSS 223. THE SUBJECT HOLE IS COMMON TO THE MLG BEAM ATTACH FITTING. DAMAGE WAS REMOVED AND REWORKED PER ERA 386257-14.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 40,343 hrs · 20,708 cycles
DAMAGE WAS NOTED TO THE FUSELAGE SKIN AT THE FWD EDGE OF THE C1 DOOR CUTOUT. DAMAGE WAS REMOVED AND REPAIRED PER ERA 089422-14.
2003
Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 39,632 hrs · 19,752 cycles
EMERGENCY LIGHTING AT ROW 5DEF INOP. REPLACED E-PATH SEAT CABLE ASSY PER AMM. E-PATH LIGHTING CHECKS GOOD.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 39,153 hrs · 19,092 cycles
THE FS 178 BULKHEAD WEB WAS FOUND WITH 3 TYPICAL CRACKS, 1 AT LBL 5.7 & WL 200, 1 AT RBL 5.7 & WL 200, AND 1 AT RBL 5.7 & WL 211. THE CRACKS ARE TYPICAL OF AD 2000-05-29 AND BAC S/B 737-53A1173. THE CRACKS WERE REPAIRED WITH ALUMINUM REPAIR DOUBLERS PER THE BAC 737 SRM AND PER ER/A 384881-14AD.
2000
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,136 hrs · 15,236 cycles
THE STATION 178 BULKHEAD WEB WAS FOUND TO BE CRACKED AT WL 213 NEAR LBL 5.7. THE RESULTING CUTOUT MEASURED APPROX 1 INCH UP/DOWN BY 1 INCH I/B - O/B. CORRECTIVE ACTION: ER/A 334374-14AD REV C.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 35,136 hrs · 15,236 cycles
STA 178 BULKHEAD WEB FOUND CRACKED AT WL 213 NEAR LBL 5.7. RESULTING CUTOUT MEASURED APPROXIMATELY 1 UP/DOWN BY 1 INBOARD/OUTBOARD. ER/A 334374-14AD.