N467DA

Part: WEB — CRACKED (BS 1235)

A .25 INCH CRACK AT UPPER LIGHTENING HOLE ON VERTICAL WEB STA 1235 R IN 48 SECTION. REPAIRED PER M/M 53-11-0.

Part: STIFFENER — CRACKED (LT LE SLAT)

FOUND DURING F-1 LETTER CHECK, 1.25 INCH CRACK NR 4 L/E SLAT I/B TRACK ROLLER BOX I/B STIFFENER. REPLACED STIFFENER PER M/M 57-20-21.

Part: BATTERY PACK — DISCHARGED (CABIN)

MSU - CK OP OF ALL EMER LIGHTS. FOUND LT OVERWING EXIT SIGNS INOP. REPLACED BATTERY PACK. OPS NML.

Part: FRAME — DOUBLE DRILLED (BS 784)

DURING THE PERFORMANCE OF SI 4-61904-12, THE SECOND FASTENER HOLE ABOVE THE FLOORBEAM ON THE INBOARD FLANGE WAS DISCOVERED TO HAVE BEEN LOCATED CLOSE ENOUGH TO A PILOT HOLE TO CREATE A DOUBLE DRILLED HOLE. THE DOUBLER DRILLED HOLE WAS OVERSIZED TO 0.403 THROUGH BOTH THE FRAME AND THE REINFORCING STRAP TO ELIMINATE THE PILOT HOLE. A FREEZE PLUG WAS INSTALLED IN THE REINFORCING STRAP AND A MODIFICATION WAS ACCOMPLISHED PER 65C36280-24.

Part: SOCKETS — MISSING (CABIN)

2 TRACK LIGHT SOCKETS RIPPED LOOSE FROM FLOOR TRACK, AT ROWS 16 AND 20. REPLACED SOCKETS AND CAPSULES, CKS NORMAL.

Part: TRACK LIGHTS — LOOSE (CABIN)

EMERGENCY TRACK LIGHTING AFT CABIN LOOSE FROM FLOOR. REPLACED LIGHT SEGMENT, CKS OK.

Part: WEB — CRACKED (BS 1273)

FOUND DURING E-1 LETTER CHECK, .1875 INCH CRACK LWR TORQUE BOX VERTICAL WEB BS 1273 LEFT SIDE AT LIGHTENING HOLE. REPAIRED PER M/M 53-11-0.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

ON LAYOVER, FOUND EMERGENCY EXIT LIGHT ABOVE R-2 DOOR INOPERATIVE. REPLACED POWER SUPPLY AND BATTERY PACK. OPS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, FOUND CENTER AISLE EMERGENCY EXIT LIGHT INOPERATIVE AT ROW 3. REPLACED BATTERY PACK. OPS NORMAL.

Part: CIRCUIT BREAKER — CRACKED (E/E COMPT)

ON FINAL, ALL 3 BUS TIE BREAKERS TRIPPED, PHASE UNBALANCE, OVER EXCITED NR 2 AND NR 3, NR 1 TR UNIT C/B POPPED. FOUND APU GEN BREAKER CRACKED WITH LOOSE CONNECTIONS. REPLACED SAME. ALSO, REPLACED NR 1 ENG GEN BREAKER. RAN ENGS PARALLELED, ALL CHECKS NORMAL.

Part: SPAR — CRACKED (AILERON)

SPAR WAS FOUND CRACKED NEAR TAB FITTING. SPLICED SPAR SECTION PER SRM 51-40-3 FIG 1. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.

Part: SKIN — CRACKED (FS 345)

DURING INSPECTION, THREE CRACKS WERE FOUND IN THE SKIN AND DOOR SURROUND STRUCTURE IN THE LOWER AFT CORNER OF THE L1 DOOR CUTOUT. ALL CRACKS GO THROUGH THE SKIN, BONDED DOUBLER AND THE BEAR STRAP. CRACK LENGTH VARIED FROM 1 TO 2 INCH LENGTH. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 02-28-96, THE DAMAGED AREA WAS CUT OUT AND A DOUBLER AND TRIPLER WERE INSTALLED.

Part: BEAR STRAP — CORRODED (FS 1070)

DURING INSPECTION, CORROSION WAS FOUND ON THE INTERNAL SKIN DOUBLER OF THE R-2 DOOR CUTOUT AT STATION 1070. IN ACCORDANCE WITH FAA/DER FORM 8110-3 DATED 2-8-96, THE DAMAGE WAS CUT OUT AND A DOUBLER AND TRIPLER INSTALLED.

Part: SKIN — WORN (AILERON)

LOWER SKIN WAS FOUND WITH OVERSIZED HOLES. SPLICED SKIN SECTION PER M/M 57-51-0 FIG 801. FOUND DURING SHOP INSPECTION OF AILERON ASSEMBLY.

Part: TRANSVERSE BEAM — CRACKED (BS 1263)

THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM AND AFT CHANNEL OF THE RT TORQUE BOX AT FS 1263. THIS AREA OF THE TORQUE BOX IS THE SUBJECT OF AIRWORTHINESS DIRECTIVE 94-07-08, WHICH REQUIRES INSPECTION PER S/B 53-0129. REPAIRED PER ERA 303225-14AD.

Part: DOOR ACTUATOR — ICED UP (RT MLG)

ON DEPARTURE, RT MAIN GEAR WOULD NOT RETRACT, TRANSIT LIGHT ON AND SECOND OFFICER'S PANEL NEVER ILLUMINATED. REMOVED ICE BUILD-UP ON RT GEAR DOOR ACTUATOR, LUBED GEAR AND DOORS, PERFORMED GEAR SWING AND OPS NORMAL.

Part: EEL — INOPERATIVE (AFT AIRSTAIR)

AFT AIRSTAIR EMERGENCY EXIT LIGHTS ARE INOP. REPLACED LIGHT ASSEMBLY AND BATTERY PACK OPERATION NORMAL.

Part: WEB — CRACKED (BS 294.5)

LT VERTICAL WEB OF NWW HAS 2.0 CRACK BETWEEN STA 294.5 AND STA 285.5, APPROX WL 170. REPAIRED PER DL ERA 302166-14AD.

Part: PLATE WEB — CRACKED (BS 270 RH SIDE)

DURING INSPECTION AT CV-2, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL WAS FOUND CRACKED AT STA 270. IN ACCORDANCE WITH BAC S/B 727-53-145, THE DAMAGED PORTION OF THE WEB WAS TRIMMED OUT, AND A DOUBLER AND 4 REPAIR STRAPS WERE INSTALLED.

Part: SKIN — CORRODED (FS 720)

DURING CV-2 CK, FOUND FUSELAGE SKIN DAMAGED BETWEEN STA 720E AND 720F AT STR 27L. INSTALLED DOUBLER PER SRM 53-30-3 FIG 3.

Part: BEAM — CRACKED (FS 1263)

DURING INSPECTION, THE FWD TRANSVERSE BEAM AT FS 1263 WAS FOUND CRACKED IN THE ANGLE. THE BEAM WILL BE REPLACED IN ACCORDANCE WITH B727 S 53-0129 REV 4.

Part: WEB — CRACKED (FS 285)

DURING INSPECTION, THE RT SIDEWALL WEB OF THE NOSE WHEEL WELL HAD A 0.25 INCH CRACK AT STA 285. THE DAMAGED PORTION OF THE WEB WILL BE TRIMMED OUT AND A REPAIR DOUBLER AND FOUR STRAPS WERE INSTALLED IN ACCORDANCE WITH S/B 727-53-145.

Part: STRINGER — CORRODED (FS 520)

DURING CV-2 CK, FOUND CORROSION AT STR 23R JUST FWD OF STA 520. REPAIRED PER SRM 53-10-3 ID PER PS 900-5-1 NR 4.

Part: FLOOR SUPPORT — CRACKED (FS 950)

FOUND ON LTR CK - 1 INCH CRACK THROUGH MOUNT BOLT HOLE FLOOR PANEL SUPPORT CHANNEL FWD SIDE STA 950C BL 18R - REPAIR - REPAIRED PER SRM 53-10-5 AND I.D. PER P.S. 900-5-1 NR 4.

Part: ANGLE — CRACKED (NR 2 SLAT)

DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT O/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER MM 57-20-21 PG 813.

Part: SEAT TRACK — CORRODED (FS 344)

FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 344 TO 360 AT LBL 22 - REPAIR - REPLACED SEAT TRACK PER SRM 53-10-5 FIG 7.

Part: ANGLE — CRACKED (NR 2 SLAT)

DURING CV-2 CK, FOUND CRACK ON NR 2 SLAT OUTBOARD TRACK INBOARD VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED ANGLE PER M/M 57-20-21 PG 813.

Part: ANGLE — CRACKED (NR 3 SLAT)

DURING CV-2 CK, FOUND CRACK ON NR 3 SLAT I/B TRACK O/B VERTICAL ANGLE AT SPAR (SPAR ON WING L/E). REPLACED STIFFENER.

Part: FLOOR BEAM — CORRODED (FS 1110)

FOUND ON CV2 CK - CORROSION AT FLOOR BEAM AT BL 0 TO LBL 16 STA 1110 - REPAIR - INSTALLED REPAIR ANGLE PER MM 53-20-11 FIG 804A.

Part: STRINGER — CORRODED (FS 720)

FOUND ON CV2 CK - CORROSION INSIDE STRINGER 27L FWD STA 720F - REPAIR - REPLACED SECTION OF STRINGER PER SRM 53-10-3 FIG 1.

Part: CLIP — CORRODED (FS 303)

FOUND ON CV2 CK - CORROSION AT LOWER FWD FUSELAGE SKIN CLIP STA 303 AT NOSE W/W CHORD - REPAIR - REPAIRED PER SRM 51-40-3 FIG 1.

Part: SEAT TRACK — CORRODED (FS 480)

FOUND ON CV2 CK - CORROSION AT SEAT TRACK STA 480 LBL 22 - REPAIR - REPLACED DAMAGED SEAT TRACK FROM 440-480 PER SRM 53-10-5 FIG 7.

Part: FLOOR BEAM — CORRODED (FS 380)

FOUND ON CV2 CK - CORROSION AT FLOOR BEAM TOP SIDE AND BOTTOM WHERE CLIP NUTS ATTACH STATION 380 RBL 12 TO 63 - REPAIR - REPLACED TEE CAP PER SRM 53-10-8.

Part: RIB — CRACKED (NR 3 SLAT)

DURING CV-2 CK, FOUND RIB CRACKED 1 INCH ON NR 3 SLAT JUST OUTBD OF OUTER TRACK. REPAIRED PER SRM 57-50-3 FIG 9.