N499DA

Part: ANGLE — CORRODED (NR 2 ENGINE)

NR 2 ENG AFT MOUNT LOWER CHORD WAS CORRODED. REPLACED CHORD.

Part: ANGLE — CORRODED (NR 2 ENGINE)

NR 2 ENG AFT MOUNT SUPPORT ANGLE LEFT HAND WAS CORRODED. REPLACED ANGLE.

Part: WIRE — SPLIT (NR 1 ENGINE)

ON HUSH-KIT MOD, FOUND NUMEROUS LONGITUDINAL SPLITS ON INSULATION OF ALL 3 GEN FEEDER CABLES IN MID PYLON AREA. REPLACED CABLES FROM SPLICES IN LT 48SEC TO FIREWALL DISCONNECT WITH NEW TYPE CABLES BMS 13-58 DL P/N 012210733 PER BOEING SER- VICE LETTER 727-SL-24-026-A.

Part: OIL FILTER — CONTAMINATED (NR 3 ENGINE)

NR 3 OIL FILTER BYPASS LIGHT CAME ON AT 17K FT. OIL PRESS TEMP AND QTY ARE GOOD POM PROCEDURES COMPLIED WITH. LIGHT REMAINED ON AND NR 3 ENGINE WAS SHUT DOWN IAW POM PROCEDURES. REMOVED FILTER, FOUND CARBON BUILDUP. INSTALLED NEW FILTER AND RAN ENG PER MM. REMOVED NEW FILTER AND FOUND MORE CONTAMINATION, CARBON CONTAMINATION IS WITHIN MM. LIMITS FOR 50 HOUR FLY BACK. INSTALLED NEW OIL FILTER. GOOD FOR SERVICE. MCC AND EQUIPMENT CONTROL WERE NOTIFIED.

Part: CONTROLLER — FAILED (CABIN)

DURING CLIMB-OUT, CABIN ALT BEGAN TO CLIMB AT 1000 FT, BOTH PACKS APPEARED TO OP. NORMAL CABIN CLIMBED TO AN ALT OF 12,000 AND DESCENT BEGAN. POM PREC FOLLOWED STBY AND DC HAD NEG EFFECT TO CLOSE OUTFLOW FURTHER CARGO V. CLOSED LIGHT ILLUMINATED ENTIRE TIME ANOMALLY OCCURED. REPLACED PRESSURE CONTROLLER, REMOVED AND REPLACED RT PACK FWD VLV. PERFORMED TEST PER M/M. PRESS OF A/C TO CK FOR LEAKS. NO LEAKS NOTED A/C PRESSURIZATION GRD CKS NORMAL. PRESSURIZED A/C ALL INDICATION NORMAL.

Part: SKIN — CRACKED (BS 681-740)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 36 CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366872-14AD, REV A.

Part: SKIN — CRACKED (BS 360-480)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 7 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT ALONG ITS ENTIRE LENGTH AND REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366866-14, REV B.

Part: SKIN — CRACKED (BS 481-681)

LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC CONFIRMED 69 CRACKS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUTOUT ALONG THE ENTIRE LENGTH OF THE PANEL AND REPAIRED WITH AND EXTERNAL ALUMINUM DOUBLER PER ER/A 366873-14, REV A.

Part: OIL FILTER — DIRTY (NR 3 ENGINE)

NR 3 ENGINE OIL FILTER INDICATED BYPASS IN CRUISE FL280. PRECAUTIONARY, SHUTDOWN PROCEDURE ACCOMPLISHED. REPLACED OIL FILTER, LOP SWITCH, FILTER BYPASS SWITCH, DRAINED OIL RES, PERFORMED OIL BREATHER PRESS CK TEST 'Z' PER PFHB AND OPN OK. REPLACED OIL FILTER PER M/M.

Part: FILTER — CLOGGED (NR 3 ENGINE)

NR 3 ENGINE OIL FILTER BYPASS ILLUMINATED IN FLIGHT. THE LIGHT EXTINGUISHED AT 45 TO 50 PERCENT N1 ALL ON SHORT FINAL. LIGHT RE-ILLUMINATED AT IDLE. PER T/S CHART REPLACED FILTER, PERFORMED BREATHER PRESS CK, CKS GOOD. REPLACED FILTER, OK FOR SERVICE.

Part: SKIN — CRACKED (BS 373)

THE R1 DOOR SURROUND SKIN ASSY WAS FOUND WITH A 2.25 INCH TYPICAL CRACK IN THE BEAR STRAP AT THE UPPER HINGE CUTOUT. THE CRACK WAS REPAIRED PER BAC S/B 727-53-0136, REV 3. THE REPAIR WAS DOCUMENTED PER ER/A 365667-14. NOTE: THE BEAR STRAP HAD THE S/B 53-0136 CORNER RADIUS TRIM MODIFICATION ACCOMPLISHED PRIOR TO CRACK INITIATION.

Part: BULB — FAILED (CABIN)

EMERGENCY LIGHT OUT AT RIGHT WING ROOT FAIRING. RELAMPED.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER CK, FOUND LT OVERWING EMERGENCY EXIT SIGN NOT ILLUMINATING. REPLACED BATTERY PACK.

Part: CONTROLLER — MALFUNCTIONED (LT/RT PACK)

AT FL 2500 WITH ONE PACK RUNNING, CABIN STARTED TO CLIMB, DIVERTED INTO DFW. MAINTENANCE IN PROGRESS. RT PACK ON PREVIOUS MCO. RT PACK REPLACED ACM. CKS GOOD. LT PACK REPLACED 35 DEGREE SENSOR AND 35 DEGREE CONTROLLER. PRESSURIZED A/C USING BOTH PACKS, CKS GOOD.

Part: WEB — CRACKED (BS 1223)

A 1 INCH CRACK IN LIGHTENING HOLE TORQUE BOX WEB RT SIDE STA 1223. REPAIRED PER MM 53-11-0 PG 828.

Part: LIGHT — INOPERATIVE (CABIN)

DURING SVC CHK AD9 FOUND L1 AND L2 DOOR EMERGENCY LIGHT INOP. REPLACED LIGHT ASSYS. OPS NML.

Part: RELAY — INOPERATIVE (COCKPIT)

EMERGENCY EXIT LTS AND EMERG PATH LTS CAME ON DURING CLIMB-OUT. COCKPIT SW IN ARMED POS AND CABIN SW IN NORM. REPLACED R70 CHARGING RELAY.

Part: TANK PLATE — LEAKING (LT WING)

FUEL LEAK LEFT WING, IN-FLIGHT. REPORTED BY PASSENGER. DIVERTED ATL. FOUND FIFTH TANK PLATE FROM LT WING TIP LEAKING FUEL. SECURED TANK PLATE. NO LEAKS NOTED.

Part: ANGLE — CRACKED (NR 5 SLAT)

FOUND DURING A-1 LETTER CHECK, NR 5 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.

Part: ANGLE — CRACKED (NR 5 LE SLAT)

DURING LETTER CHECK, NR 5 L/E SLAT AFT ANGLE CRACKED AT I/B STOP PAD. REPAIRED PER MM 57-54-0 PAR 12.

Part: ANGLE — CRACKED (NR 7 SLAT)

FOUND DURING A-1 LETTER CHECK, NR 7 L/E SLAT LOWER COVE SKIN ATTACH ANGLE CRACKED AT I/B UPSTOP PAD. REPAIRED PER M/M 57-54-0 PAR 12.

Part: ANGLE — CRACKED (NR 4 LE FLAP ACT)

FOUND DURING A-1 LETTER CHECK, .75 INCH CRACK NR 4 KRUEGER FLAP ACTUATOR MOUNT BOX AT UPPER I/B FWD CORNER. REPAIRED PER M/M 57-20-21.

Part: CABLE — BROKEN (L2 DOOR SLIDE)

LEFT SERVICE DOOR EVACUATION SLIDE FAILED TO DEPLOY AND PULL HANDLE CAME OFF WHEN PULLED. CABLE ON PULL HANDLE BROKE. REPLACED DOOR SLIDE PER M/M 25-60-15.

Part: SPAR — CRACKED (NR 3 TE MIDFLAP)

AFT SPAR CHORD WAS FOUND CRACKED 33, 54 AND 61 FROM IB END OF NR 3 MIDFLAP. THE DAMAGED SECTION WAS REPLACED AND SPLICED IN PER MM 57-50-00.

Part: ANGLE — CRACKED (NR 6 SLAT)

NR 6 SLAT, .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB, 6 INCHES O/B OF TAI DUCT. REPAIRED PER MM 57-54-0 FIG 805A.

Part: RIB — CRACKED (NR 1 SLAT)

DURING HMV, FOUND NR 1 SLAT WITH CRACKED RIB AT TRACK ATTACH AREA. REPAIRED PER MM 57-40-0 PG 806 AND 807.

Part: RIB — CRACKED (NR 1 SLAT)

NR 1 SLAT I/B TRACK I/B RIB CRACKED. DRILLED DOUBLER AND INSTALLED PER M/M 57-54-0 PG 806 AND 807.

Part: SKIN — CRACKED (NR 2 SLAT)

DURING HMV, NR 2 SLAT LOWER SKIN ATTACH ANGLE CRACKED UNDER I/B STOP PAD. REPAIRED PER MM 57-54-0 PG 816.

Part: STRINGER — CRACKED (WS 686.5)

WING UPPER STRINGER TO RIB WS 686.5 STRINGER NR 5 IS CRACKED. STOP DRILLED CRACK PER M/M 57-13-0 PG 802. FABRICATED REPAIR PARTS AND INSTALLED PER M/M 57-13-00 PG 802.

Part: ATTACH LUG — BROKEN (PAX DOOR)

AT HMV, FWD ENTRY DOOR UPPER GATE STOP ROD ATTACH LUG FOUND BROKEN. REPAIRED PER 52-10-2 FIG 10.

Part: ACT ATTACH — CRACKED (NR 6 LE FLAP)

NR 6 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LOWER I/B CORNER. REPAIRED PER M/M 57-20-21 PG 811.

Part: SPAR — CRACKED (NR 2 TE MIDFLAP)

DURING SHOP INSPECTION, NR 2 MIDFLAP HAS A CRACKED AFT SPAR CHORD 22 FT AND 53 FROM I/B END OF FLAP AND A CRACK AT I/B ACTUATOR CUTOUT. SPLICED IN NEW SECTIONS OF AFT SPAR CHORD AND INSTALLED DOUBLERS, PER MM 57-52-00 PG 807.

Part: SKIN — CRACKED (NR 5 SLAT)

NR 5 SLAT SKIN WORN ON UPPER SURFACE AT FENCE ATTACHMENT. BURNISHED WORN AREA AND DYE PENETRANT INSP SHOWS CRACKS AT 3 FENCE ATTACH HOLES. ROUTED DAMAGE AT ATTACH HOLES, FABRICATED AND DRILLED DOUBLER PER M/M 57-54-0.

Part: ACT ATTACH — CRACKED (NR 5 LE FLAP)

NR 5 L/E FLAP ACTUATOR ATTACH STRUCTURE CRACKED AT LWR O/B CORNER. REPAIRED PER M/M 57-20-21 PG 811. CRACK WAS FOUND AT HMV.

Part: RIB — CRACKED (NR 7 SLAT)

DURING HMV, FOUND NR 7 SLAT RIB CRACKED AT FASTENER HOLE, I/B OF I/B STOP PAD. FABRICATED REPAIR PER M/M 57-54-0 PG 807 AND INSTALLED REPAIR PER MM 57-54-0 PG 807.

Part: SEAT TRACK — CORRODED (FS 400)

FWD CABIN SEAT TRACK, RT SIDE STA 400 OB, AND 470 OB, REMOVED CORR PER SRM 51-10-6. STA 470 WITHIN LIMITS PER SRM 53-10-1 FIG 3, STA 400 OUT OF LIMITS PER SRM 53-10-1 FIG 3. ALSO, FS 400 SHOWS EVIDENCE OF PREVIOUS CORROSION REMOVAL. PREPARED NEW SEAT TRACK SECTION PER MM 53-20-11 FIG 802. INSTALLED SEAT TRACK AS PER MM 53-20-11 FIG 802.

Part: SEAT TRACK — CORRODED (STA 1090)

SEAT TRACK AFT CABIN CORRODED RT SIDE OB TRACK STA 1090. REMOVED CORROSION PER SRM 51-10-6, OUT OF LIMITS PER SRM 53-10-1 FIG 1. REMOVED CORROSION BETWEEN STA 1090 TO 1110 WITHIN LIMITS PER SRM 53-10-1 FIG 1. REMOVED PIGTAIL STA 1110 TO 1130, BEGAN REPLACEMENT OF TRACK PER MM 53-20-11 FIG 802. OK TO TREAT AND PAINT 1090 TO 1110, INSTALLED TRACK 1110 TO 1130. TREATED AND PAINTED SEAT TRACK STA 1090 TO 1110, AS PER PS 900-3-6.

Part: STRINGER — CRACKED (WS 629)

LEFT WING UPPER STRINGER TO RIB WS 629 STRINGER NR 3 CRACKED. FABRICATED AND INSTALLED PARTS PER M/M 57-13-00 FIG 804. CRACK WAS FOUND AT HMV.

Part: SKIN — WORN (NR 6 SLAT)

NR 6 SLAT SKIN WORN AND CHAFED INBD OF INBD TRACK FAIRING AND BELOW SLAT ACTUATOR ON LWR TRAILING EDGE. TRIMMED AWAY DAMAGED PORTION OF TAB AND FABRICATED DOUBLER AND FILLER PER MM 57-54-0 PG 820.

Part: RIB — CRACKED (NR 8 SLAT)

DURING HMV, NR 8 L/E SLAT WAS FOUND WITH CRACKED INTERNAL SUPPORT RIB. REPAIRED PER MM 57-54-0 PG 814.

Part: WEB — CRACKED (NR 5 SLAT)

DURING HMV, FOUND WEB CRACKED NR 5 SLAT. REPAIRED WEB PER MM 57-54-0 FIG 805.

Part: ANGLE — CRACKED (NR 6 LE SLAT)

UPON HMV, FOUND .25 INCH CRACK AT FASTENER HOLE IN ATTACH ANGLE AFT OF RIB 6 OUTBD OF T.A.I. DUCT. REPAIRED PER M/M 51-54-0, FIG 805A.

Part: RIB — CRACKED (NR 4 SLAT)

DURING HMV, FOUND NR 4 SLAT RIB CRACKED .5 INCH, ON O/B SIDE OF O/B TRACK FITTING. REPAIRED RIB PER MM 57-45-0 FIG 814.

Part: SKIN — CRACKED (NR 5 SLAT)

DURING HMV, FOUND NR 5 SLAT RIVET MISSING IN LWR T/E SKIN O/B OF O/B TRACK. SKIN WORN AT FENCE ATTACHMENT AND WORN THIN AT BOLT HOLE ON LWR T/E SKIN. REF NR CARD 1148, BURNISHED WORN AREA. DIE PENETRANT INSP SHOWS CRACK AT 3 FENCE ATTACH HOLES. FABRICATED AND DRILLED DOUBLER PER MM 57-54-0.

Part: BLKHD BOLTS — WORN (BS 720)

DURING HMV, FOUND MOUNT BOLTS WORN FWD CARGO BULKHEAD AT FS 720D VERTICAL SUPPORT BEAMS ATTACH POINT AT STR 26L AND 26R. REPAIRED PER SRM 53-10-9 FIG 9.

Part: ACTUATOR — LOOSE (NR 13 SPOILER)

ITEM: SPOILER ACTUATOR SUPPORT FITTING LOOSE INBD LOWER BOLT AT NR 13 SPOILER. REPAIRED FITTING PER MM 57-42-0 REV D.

Part: FITTING — LOOSE (NR 2 SPOILER)

THE NR 2 SPOILER ACTUATOR SUPPORT FITTING LOWER TWO ATTACH BOLTS, AT REAR SPAR ARE VERY LOOSE IN MOUNT LUGS. REPAIRED PER MM 57-42-00 PG 804 STEP D.

Part: RIB — CRACKED (NR 6 LE SLAT)

ITEM NR 1, .5 INCH CRACK IN NR 14 RIB. REPAIRED PER M/M 57-54-0. ITEM NR 2, .25 INCH CRACK AT ANTI-ICE DUCT CUTOUT. REPAIRED PER M/M 57-54-0, FOR NR 6 L/E SLAT AT SHOP VISIT.

Part: RIB — CRACKED (NR 6 LE SLAT)

A .5 INCH CRACK UPPER/FWD END OF RIB NR 10. REPAIRED PER M/M 57-54-0, FOUND AT SHOP VISIT FOR NR 6 L/E SLAT.

Part: ANTI ICE DUCT — CRACKED (RT WING)

ANTI-ICE DUCT CRACKED 22 INCHES FROM OUTBOARD END. REPAIRED PER SRM 57-50-03, FIG 12, AT HMV SHOP VISIT FOR WING L/E KRUGER FLAP.

Part: SPAR — CRACKED (LT ELEVATOR)

DURING SHOP INSPECTION, THE LOWER FORWARD SPAR CAP WAS FOUND CRACKED 8 FEET FROM THE INBOARD EDGE. THE SPAR WAS REPAIRED PER SRM 55-20-5.

Part: SKIN — CRACKED (NR 2 ENG INLET)

NR 2 ENG INLET HOUSING OUTER SKIN CRACKED .375 INCH AT ROUND ACCESS PANEL JUST ABOVE VERT STAB FWD SPAR. FOUND DURING F-1 LTR CK TPAMM. REPAIRED PER MM 54-30-0 PG 803.

Part: SKIN — DAMAGED (LT ELEV)

L/T ELEV UPPER SKIN HAS 1 IN BY .5 INCH HOLE I/B END, 1 FT FWD OF TRAILING EDGE. FOUND AT F-1 LETTER CHECK. REPAIRED PER SRM 55-22-3 FIG 5.