N424FE

Part: STRUCTURE — CORRODED (PAX DOOR) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N369): RT AFT PAX DOORS FWD LWR CORNER, CORROSION FOUND AT DOOR SILL CORNER SEATING. REPAIRED IAW SRM 53-18-12 FIG. 201 REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED AS (MAJOR).

Part: SKIN — DEBONDED (ELEVATOR) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N00094) LT HORIZ STAB, ELEVATOR WITH DEBONDING ON TRAILING EDGE UPPER AND LOWER SIDE SKIN SURFACES (FRACTION NR 2) REPAIR CONFORMS TO EXISTING ENGINEERING AUTHORIZATION EA 6-5510-94659. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MAJOR.

Part: SKIN — CRACKED (LT WING) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N400): LT WING - CRK AT UPPER SKIN SURFACE AT WING NEXT TO (AFT NAVIGATOR LIGHT) REPAIR CONFORMS TO AN EXISTING ENGINEERING AUTHORIZATION 6-5710-93236. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MINOR.

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 33,767 hrs · 23,499 cycles

AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121.370A COMPLY WITH AGING 9-AGING-INSP. RUDDER TRAILING EDGE DAMAGED BETWEEN STA 270 AND STA 330. REPAIRED IAW SRM 55-41-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: TRACK — CRACKED (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N585): AFT MDCC FLOOR STRUCTURE, CROSSTRACK AT FR47 BETWEEN Y450 AND Y953 FOUND CRACKED. REPLACED IAW EA 6-5310-94662 AND SRM 51-40-21 AND 51-40-44, 51-72-10.

Part: SKIN — DEBONDED (ELEVATOR) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NR 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N618): LT ELEVATOR T/E, DEBONDING AT UPPER AND LOWER SURFACE (FRACTION NR 3) REPAIR CONFORMS TO EXISTING ENGINEERING AUTHORIZATION EA 6-5510-94659. REPAIR EVALUATED IAW GMM 6-2-100 AND CLASSIFIED MAJOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1. PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, L2 FORWARD DOOR FRAME AT STA 4551, FS 73A, STR 20 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA.

Part: REPAIR — MISREPAIRED (RUDDER) · airframe 33,767 hrs · 23,499 cycles

COMPLY WITH AGING 9-AGING-INSP, PREVIOUS MAJOR REPAIR INSTALLED ON RUDDER FRONT SPAR PER FEDEX EA 6-5540-89212 IS NOT IN ACCORDANCE REPAIR DATA SRM 51-77-12 REFERENCED IN EA INJECTION HOLES ARE NOT COMPLETELY FILLED LEAVING AVOID. REPAIRED PER SRM 51-77-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — MISMANUFACTURED (BS 771-805) · airframe 33,767 hrs · 23,499 cycles

2PREVIOUS REPAIR INSTALLED AT LOWER FUSELAGE 6 O'CLOCK POSITION AT STA 771 TO STA 805, FR1 TO FR2. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 53-11-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE, L2 REAR DOOR FRAME AT STA 4669, FR75A, STR 20LH TO STR 24LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA.

Part: REPAIR — NONE (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LEFT HAND SIDE, BELOW REGISTRATION NR N424FE AT STA 4181 TO STA 4241, FR77 TO FR78, STR 23 LT TO STR 24 LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 53-10-12 FIG.224 SHEET 1 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — UNKNOWN (T/E FLAP) · airframe 33,767 hrs · 23,499 cycles

COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND OUTBOARD FLAP (TOP TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 823 TO WS 835. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED IAW SRM 57-53-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NO. PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NO. POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N0497): PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 2231 TO STA 2251, FR39, STR 35LH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. **S/D COMING**

Part: REPAIR — NONE (FUSLEAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE RIGHT SIDE, BELOW R1 DOOR AT STA 1187 TO STA 1212, FS 14A TO FS 15. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 53-12-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (TE FLAP) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 67 TO WS 207. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — UNKNOWN (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE RT SIDE OF TAIL CONE AT STA 5094 TO STA 5122, FR101 TO FR102, STR 07RH TO STR 08RH. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. CORRECTIVE ACTION:**S/D COMING**

Part: REPAIR — MISINSTALLED (TE FLAP) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 60 TO WS 110. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: DATA PLATE — MISSING (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

DISCREPANCY (N0633 AND N0634): UNABLE TO VALIDATE MFG P/N AND S/N OF INSTALLED AIRFRAME LIFE LIMITED PARTS LT AND RT MLG RETRACT CYLINDERS DUE TO MISSING DATA PLATES. NSTALLED NEW DATA PLATE PER FEDEX DRWG. Z-20-001 REV. A AND AMM 11-22-32

Part: REPAIR — UNKNOWN (T/E FLAP) · airframe 33,767 hrs · 23,499 cycles

COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRED IAW SRM 57-52-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NONE (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1202 TO STA 1214, FR14B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 52-10-00 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — NOT AN SDR (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LOWER EDGE OF R1 DOOR AT STA 1250 TO STA 1262, FS 15B. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM SRM 52-10-00 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MINOR.

Part: REPAIR — MISINSTALLED (HORIZ STAB) · airframe 33,767 hrs · 23,499 cycles

COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND HORIZONTAL STABILIZER (LEADING EDGE ROOT SECTION) AT WS 95 TO WS 105. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 55-12-12 FIG 203 AND 55-12-19 FIG 201 REPAIR EVALUATED OPER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (METAL CENTER SECTION), AT WS 192 TO WS 222. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 57-52-12 FIG.205 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (TE FLAP) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - LOWER SIDE - COMPOSITE) AT WS 40 TO WS 50. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED PER FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISINSTALLED (TE FLAP) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT RIGHT HAND INBOARD FLAP (TRAILING EDGE WEDGE SECTION - TOP SIDE - COMPOSITE) AT WS 115 TO WS 200. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. TRAILING EDGE WAS REPLACED IAW FEDEX E.A. 6-5710-94665 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — MISMANUFACTURED (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE BELOW AOA SENSOR AT STA 1364 TO STA 1386, FR18 TO FR19, STR 39LT TO 44LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR NEW REPAIR ACCOMPLISHED PER SRM 53-10-12 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — NONE (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

PREVIOUS REPAIR INSTALLED AT FUSELAGE LT SIDE AT STA 1923, FR35, STR 22LT. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR CONFORMS TO AN EXISTING FEDEX ENGINEERING AUTHORIZATION 6-5330-94663 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: REPAIR — NONE (FUSELAGE) · airframe 33,767 hrs · 23,499 cycles

SMIS 424 51-00 0007102 27SEP05 MC1 CLOSE R MOD TYPE Y MOD NO. 9-AGING-INSP REV NR PS PT1 AGING AIRPLANE SAFETY RULE (AASR) 14CFR 121.368, 121 .370A COMPLY WITH AGING 9-AGING-INSP REV NR POS PT1 ENT BY: 067708 INFO 30NOV05 21:26 MC1 R DISCREPANCY (N0500): PREVIOUS REPAIR INSTALLED BELOW L2 DOOR HANDLE AT STA 3998 TO STA4042, FR74 TO FR75. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIR EVALUATED AND FOUND TO CONFORM TO SRM 52-10-00 FIG.206 REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR

Part: REPAIR — UNKNOWN (LT WING) · airframe 33,767 hrs · 23,499 cycles

COMPLY WITH AGING 9-AGING-INSP, PREVIOUS REPAIR INSTALLED AT LEFT HAND WING ROOT (LEADING EDGE ABOVE KRUEGER FLAP) AT WS 57 TO WS 77. UNABLE TO DETERMINE APPROVED REPAIR DATA AT TIME OF AIRCRAFT INSPECTION NEED EVALUATION FOR MAJOR/MINOR CLASSIFICATION AND APPROVED REPAIR DATA. REPAIRS CONFORMS TO EXISTING FEDEX ENG EA 6-5710-94660. REPAIR EVALUATED PER GMM 6-2-100 AND CLASSIFIED AS MAJOR.

Part: PYLON — DAMAGED (NR 1 ENGINE) · airframe 31,572 hrs · 22,069 cycles

NR 1 ENGINE PYLON HAS I/B CENTER SECTION AT CENTER T/R HINGE POINT BOWED INWARD APPROX 17 INCHES HIGH AND 20 INCHES LONG WITH 1 INCH DEPTH. SUBSEQUENT DISASSEMBLY AND INSPECTION REVEALED, I/B SIDE OF SKIN AT RIB 7 HAD DEFORMED GUSSET, PYLON PLANK FROM RIB 1 TO RIB 8 BEND, I/B T/R SEAL CHANNEL AT RIB 4 12:00 POSITON GOUGED 1 INCH X 0.25 DEEP, INBOARD T/R FWD HINGE POINT CRACKED, INBOARD T/R CENTER HINGE BRACKET BEARING BROKEN, HYD/FUEL LINE ANGLE BRACKETS AT L/E RIB 3 BENT, I/B SIDE OF PYLON AT RIB 3 HAD 3 RIVETS SHEARED. R/R NR 1 PYLON ON S00010 PER E.A. 6-5450-69698.

Part: INDICATOR — OUT OF POSITION (LT MGL DAMPER) · airframe 30,001 hrs · 21,126 cycles

UNABLE TO RAISE LG IN POS 1. SWITCH TO POS 2, NO SUCCESS. RESET LT MLG PITCH DAMPER PRESS DROP IND. CHECK OK.

Part: WARNING SYSTEM — ACTIVATED (COCKPIT) · airframe 30,001 hrs · 21,126 cycles

AS SOON AS MLG BROKE OFF GROUND ECAM IND LG RETRACT FAULT.

Part: CONTROLLER — FAILED (CABIN)

ON DEPARTURE, AIRCRAFT WOULD NOT PRESSURIZE, THE NR 2 FWD OUTFLOW VALVE INDICATED OPEN AND RED ON ECAM. REMOVED AND REPLACED NR 2 PRESSURIZATION CONTROLLER.