N418DA

Part: FRAME — CRACKED (PAX DOORWAY)

FOUND AT F-1 LETTER CK, AFT ENTRY WALL LT FRAME HAS .5 INCH VISIBLE CRACK APPROX 6 INCHES BELOW UPPER STOP CASTING. REPAIR PER SRM 53-10-9.

Part: RIB — CRACKED (LT LE FLAP)

LOWER SKIN CUT TO FACILITATE REPAIR OF RIBS. REPAIRED SKIN PER M/M 57-54-0.

Part: COFFEEMAKER — FAILED (GALLEY)

ELECTRICAL BURNING SMELL EMITTING FROM F/C GALLEY. REPLACED F/C COFFEEMAKER AND CANNON PLUG.

Part: MOUNT — CRACKED (NR 3 ENGINE)

DURING MODIFICAITON OF THE FASTENER HOLES IN THE NR 3 ENGINE MOUNT PER S/B 727-54A0010R4, FASTENER HOLE C WAS FOUND CRACKED. THE HOLE WAS SUBSEQUENTLY OVERSIZED LARGER THAN IS ALLOWED BY THE S/B. REPAIRED PER ERA 331809-14.

Part: FRAME — CUT (BS 1090)

FUSELAGE FRAME AT FS 1090 AND S28R WAS FOUND TO HAVE A CUT ACROSS A ROW OF FASTENERS AT THE SHEAR CLIP. REPAIRED PER ERA 331789-14.

Part: STRINGER — CRACKED (BS 950)

S29R WAS FOUND CRACKED NEAR FS 950F. REPAIRED PER ERA 331781-14.

Part: S-DUCT — CRACKED (NR 2 ENGINE)

S-DUCT LEADING EDGE ROLLED OVER AND CRACKED JUST AFT OF NOSE COWL AT 12 O'CLOCK POSITION. REMOVED DAMAGED AREA AND FABRICATED REPAIR PER SRM 54-10-3 FIG 13. OK TO INST REPAIR. INSTALLED REPAIR PER SRM 54-10-3 FIG 13. OK TO CLOSE. CLOSED OUTER SKIN.

Part: WEB — CRACKED (VERT STAB)

STA 1303 WEB CRACKED LT AND RT SIDE AT BOTTOM INSIDE VERT STAB. REPAIRED PER SRM 53-10-4 FIG 17.

Part: FITTING — CORRODED (NR 4 TE FLAP)

NR 4 FLAP TRACK FWD ATTACH FITTING LARGE HOLE HAS CORROSION IN HOLE. REPAIRED PER M/M 57-42-0.

Part: SKIN — DELAMINATED (RT ELEVATOR)

RIGHT ELEVATOR TRAILING EDGE DELAMINATED 2 PLACES. REPAIRED PER M/M 55-20-0 PG 801.

Part: SKIN — CRACKED (WING)

SKIN CRACKED INNER L/E SKIN IS CRACKED AT FASTENERS 36 O/B OF FUSELAGE. AREA REPAIRED PER M/M 57-54-0 PG 804A.

Part: FITTING — BROKEN (NR 3 SPOILER ACT)

NR 3 SPOILER O/B ACTUATOR ATTACH CASTING BROKEN. REPLACED FITTING PER M/M 57-42-0.

Part: SKIN — CRACKED (NR 3 LE FLAP)

A 1.5 INCH CRACK AT NR 3 L/E FLAP I/B LIP HINGE CUTOUT. REPAIRED PER M/M 57-53-0 AND ERA 364735-14.

Part: ACTUATOR ROD — FAILED (NLG)

NOSE LANDING FAILED TO RETRACT ON CLIMB-OUT OF LEX. C/W POM CONTINUED TO CVG. LUBED NOSE GEAR AND FOUND NOSE GEAR DOWN LOCK ACTUATOR ROD FAILED. REPLACED N OSE GEAR DOWNLOCK ACTUATOR ASSY 324003683 S/N ON 1255 S/N OFF 283.

Part: BATTERY PACK — DISCHARGED (CABIN)

EMERG LIGHT AT F/C BULLNOSE INOP WHEN TESTED. REPLACED BATTERY PACK, OPN CKS OK.

Part: HINGE — CRACKED (NR 3 LE FLAP)

FOUND ON D2 LETTER CHECK, .5 INCH CRACK AT NR 3 L/E FLAP OUTBD HINGE. REPAIRED PER ERA 363018-14 CODE 4-57-54.

Part: SKIN — CORROSION (BS 1050-1060)

THE FUSELAGE SKIN BETWEEN FS 1050 TO 1060 AND STR 28L WAS FOUND CORRODED. THE REPAIR CUTOUT IS APPROXIMATELY 11.375 IB/OB. THE CUTOUT EXTENDS FROM FS 1050 TO 1060 ALONG STRINGER 28L. REPAIRED PER ERA 362905-14.

Part: HYDRAULIC LINE — LEAKING (RT MLG WW)

CLIMBING THROUGH FL310, TOTAL HYD LOSS DETECTED BEFORE A-SYS LOST PRESSURE. PUMPS OFF IMMEDIATELY NO CAVITATION QTY WENT TO ZERO. REPLACED A-SYSTEM RETURN LINE IN RT WHEEL WELL CHECKS GOOD.

Part: ANGLE — CRACKED (NR 8 SLAT AC)

FOUND ON D1 LETTER CK, NR 8 SLAT ACTUATOR INBD AND OUTBD ATTACH ANGLES CRACKED. REPAIRED PER MM 57-20-21.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

R1 DOOR EMERG SLIDE LIGHT INOP. REPLACED PWR SUPPLY M982, OPS CHKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AND RIGHT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOP. REPLACED RACK AND BATTERY PACK, CHECKS NORMAL.

Part: SKIN — CORROSION (BS 1010)

CORROSION REMOVAL RESULTED IN TWO NEW CUTOUTS JUST AFT OF FS 1010, BETWEEN S-29L AND S-28R. THE FIRST, JUST OUTBOARD OF S-28R AND EXTENDS FURTHER OUTBOARD, MEASURES 6.5 FWD TO AFT BY 3.125 INBOARD AFT. EXT DOUBLER REMOVED REVEALING CUTOUT, EXISTING INTERNAL DOUBLER WAS REMOVED REVEALING A CUTOUT. THE LOCAL SKIN AT ALL DAMAGE LOCATIONS IS 0.070 THICK 2024-T3 CLAD ALUMINUM.

Part: FLOOR BEAM — CORRODED (BS 1110)

FOUND ON MV-1 CHECK CORROSION AT STA 1110, FLOOR BEAM LBL 12, REF N/R 123. REPAIR: REPAIRED PER M/M 53-20-11.

Part: BULLNOSE — CRACKED (NR 4 LE FLAP)

INBOARD ATTACH POINT FOR BULLNOSE CRACKED. REPAIRED PER SRM 57-50-3.

Part: TRANSVERSE BEAM — CRACKED (FS 1263)

THERE IS A CRACK IN THE ANGLE OF THE FWD TRANSVERSE BEAM 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. THIS ER/A WILL REPLACE THE DAMAGED PART IN ACCORDANCE WITH THE S/B.

Part: BRACKET — CRACKED (LE FLAP ACT)

FOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 1 L/E FLAP ACTUATOR ATTACH BRACKET I/B LWR SIDE. REPAIRED PER M/M 57-20-21 PAR 12.

Part: BRACKET — CRACKED (LE FLAP ACT)

FOUND DURING C-1 LETTER CHECK, .375 INCH CRACK NR 2 L/E FLAP ACTUATOR ATTACH BRACKET AT I/B LWR END. REPAIRED PER M/M 57-20-21 PAR 12.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND DURING C-1 LETTER CHECK, .5 INCH CRACK NR 7 L/E SLAT LWR COVE SKIN ATTACH ANGLE BELOW I/B TRACK. REPAIRED PER M/M 57-54-0.

Part: BATTERY — DISCHARGED (CABIN)

AFT AIRSTAIR EMER LIGHT INOP. REPLACED BATTERY, OPERATION NORMAL.

Part: ANGLE — CRACKED (NR 3 SLAT)

COVE SKIN ANGLE CRACKED UNDER NR 3 SLAT TAI DUCT. FOUND DURING B-2 LTR CK. REPAIRED PER 57-54-0, PAR 2.

Part: SKIN — DAMAGED (RT ELEV)

FOUND DURING B-2 LETTER CHECK - HOLE BURNED THROUGH RT O/B ELEVATOR STATIC WICK BASE. REPAIRED PER SRM 55-20-3, FIG 2 SHT 1.

Part: EEL BATTERY — DISCHARGED (CABIN)

DURING PREFLIGHT INSP, EMERGENCY EXIT LIGHT AT AF AIRSTAIR INOP. REPLACED BATTERIES OPERATION NORMAL.

Part: SKIN — WORN (LT AILERON)

FASTENERS PULLED THROUGH SKIN AT 2ND TAB HINGE FITTING FROM INBRD, UPPER SKIN OF LEFT OUTBOARD AILERON. REPAIRED DURING SHOP VISIT`PER SRM 57-50-5 FIG 3.