N944DL

Part: CABLE — BENT (TAILCONE RELEASE) · airframe 75,540 hrs · 56,810 cycles

CABLE TO OUTSIDE RELEASE HANDLE FOR THE TAILCONE HAD A BENT CABLE LEAD AT THE TURN BARREL SIDE OF CABLE, INSIDE AIRCRAFT. REPLACED THE CABLE ASSY IAW AMM 53-53-02, AND AMDS CARD 5350-01077-0101.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 75,468 hrs · 56,744 cycles

SEAT MOUNTED EMERGENCY LIGHTS, LAST SIX ROWS WERE INOPERATIVE. REMOVED AND REPLACED THE FUSE IN THE POWER SUPPLY B5-112 IAW AMM 33-53. OPS CHECKED OK.

Part: WIRE — BROKEN (CABIN) · airframe 74,076 hrs · 55,612 cycles

SEAT 14DEF IN SEAT EMERGENCY LIGHT INOP. FOUND WIRE BROKEN AT SEAT HARNESS. REPAIRED PER ESPM 20-90. CHECKS GOOD.

Part: DOOR FRAME — CRACKED (RT MLG WW) · airframe 73,827 hrs · 55,425 cycles

FOUND A CRACK AND BROKEN RIVET ON RT MAIN LANDING GEAR DOOR FRAME. REMOVED AND REPLACED THE RT MLG FWD DOOR OPENING CHANNEL IAW DWG 5930584.(LP3817518)

Part: FIRE WARNING — FALSE ACTIVATION (CARGO BAY) · airframe 72,979 hrs · 54,740 cycles

DURING CRUISE AT FL 280 RECEIVED FIRE INDICATION ON AFT CARGO FIRE ARMED SWITCH. DID NOT GET AURAL OR MASTER WARNING. FOLLOWED QRH.AND DISCHARGED BOTTLE 1. FIRE INDICATION REMAINED ILLUMINATED FOR ABOUT 15MINS. REPLACED THE NR 1 CARGO FIRE EXTINGUISHER CONTAINER AND SQUIBS. ALSO REPLACED FIRE CONTROL PANEL. CARGO FIRE PROTECTION OPERATIONAL TESTS OK.

Part: TRANSMITTER — FAILED (LT ENGINE EPR) · airframe 72,888 hrs · 54,662 cycles

DURING CLIMBOUT, A FAINT BURNING ODOR BECAME APPARENT THROUGHOUT THE COCKPIT AND CABIN. AUTO THROTTLES FAILED. NR 1 ENG EPR STUCK AT 1.53 REGARDLESS OF THROTTLE POSITION, EVEN AT SHUTDOWN. NO CIRCUIT BREAKERS TRIPPED. NO OTHER INDICATIONS. ALL OTHER ENG PARAMETERS NORMAL. R & R THE LEFT ENG EPR TRANSMITTER IAW MM 77-11-02 -691460. PERFORMED EPR CHECK WITH AIRDATA BOX. CHECKED NORMAL IAW M M 77-11-311985. RAN BOTH ENGS. EPR CHECKED GOOD. COMPLIED WITH PNEU DIST CABIN SMOKE/ODOR T/S W/C 2120-2367. ALSO C/W PNEU SYS DUCT BURNOUT W/C 7100-2619 UP TO STEP 10. -691460- REPLACED COALESCE BAGS. RAN ENGS WITH ANTI-ICE ON. NO ODOR DETECTED.

Part: FIRE WARNING — FALSE ACTIVATION (AFT CARGO) · airframe 72,734 hrs · 54,529 cycles

DURING DESCENT, AN AFT CARGO FIRE LIGHT ILLUMINATED WITH NO AURAL OR MASTER WARNING LIGHT. NO OTHER INDICATIONS. LIGHT WENT OUT AFTER ABOUT 3 MINUTES. NO WARNINGS OR LIGHTS DISPLAYED AT THIS TIME. FIRE DETECTOR SYSTEMS TESTED OK. NO HISTORY. CANNOT DUPLICATE THE PROBLEM. ACFT OK FOR SERVICE.

Part: CLAMP — WORN (TAILCONE RELEASE) · airframe 72,396 hrs · 54,277 cycles

LEFT & RIGHT TAIL CONE RELEASE CABLE CLAMPS WORN. REPLACED THE CABLE CLAMPS. OPS CHECKED GOOD.

Part: ANTI-ICE VALVE — FAILED (RT ENGINE) · airframe 72,387 hrs · 54,272 cycles

ANTI-ICE VALVE RIGHT ENGINE LEFT CIRCUIT BREAKER FOUND TRIPPED ON ARRIVAL TO AIRCRAFT. WHEN RESET, CIRCUIT BREAKER SPARKED AND SMOKE CAME OUT. RT ENG LEFT ANTIICE VALVE LOCKED OPEN AND CONNECTER REMOVED AND STOWED. THE CIRCUIT BREAKER REMAINS IN. REMOVED FWD F/A PANEL. GVI PERFORMED NO DEFECTS NOTED. R & R THE RT ENGINE LT ANTI ICE VALVE IAW AMM 75-10. R & R THE CIRCUIT BREAKER B1-54 IAW 20-00-00. OPS CHECKED OPERATION OF VALVE SEVERAL TIMES , NO CIRCUIT BREAKERS TRIPPED. VALVE OPERATES NORMAL. ACFT OK FOR SERVICE.

Part: SENSOR — OUT OF ADJUST (LE SLAT) · airframe 71,995 hrs · 53,979 cycles

WHILE IN-ROUTE TO LGA, DIVERTED (DIV) TO BDL DUE TO A "SLAT DISAGREE" INDICATOR LIGHT ILLUMINATED ON APPROACH WHEN FLAPS 11 WAS SELECTED. FOUND LEFT & RIGHT SLAT SENSORS OUT OF ADJUSTMENT. ALSO FOUND RIGHT WING NR 1 SLAT DRIVE CONTROL BRACKET BROKEN. REMOVED SLAT, COMPLETED REPAIR AND RIGGED PER AMM. CHECKS GOOD & REQUIRED INSPECTIONS COMPLETED.

Part: BLANKET — MELTED (RT ENG DUCT) · airframe 71,598 hrs · 53,711 cycles

LEFT REAR LAVATORY SMOKE DETECTOR WENT OFF ON FINAL APPROACH. NO SMOKE OR FUMES OBSERVED. PAX NOTED BURNED RUBBER ODOR IN AFT CABIN. ENGINE AND AIRFRAME ANTI-ICE WERE ON. FOUND RT TAILCONE SECTION COVERED IN DE-ICING FLUID, FOUND RED FIRE BLANKET MELTED TO PNEUMATIC DUCT FROM RT ENG. CLEANED AND RAN BOTH ENG'S NO SMOKE OR FUMES NOTED.

Part: ENGINE — CONTAMINATED (APU) · airframe 71,586 hrs · 53,703 cycles

AFTER TAKE OFF AND ACTIVATION OF AIRFOIL ICE SMOKE HAZE FILLED CABIN AND COCKPIT AFT LAV FIRE DETECTOR ACTIVATED SMOKE DISSIPATED AFTER SELECTING ICE PROTECTION OFF.PREFORMED AIRFOIL ANTIICE OPERATION IAW AMM 30-10. NO SMOKE WAS FORMED IN CABIN NOW FUEL OIL/SWEET ODOR DID PERSIST. FOUND DE-ICE FLUID IN APU INLET. CLEANED SAME AND PERFORMED DUCT BURN.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 71,196 hrs · 53,449 cycles

ESCAPE PATH LIGHTS INOP AT ROWS 28, 29, AND 34. REPLACE LIGHT ASSEMBLIES PER AMM 33-53. OPS CHECK GOOD.

Part: SKIN — WORN (TE FLAP VANE) · airframe 71,012 hrs · 53,307 cycles

WORN OUTBD GUIDE VANE OUTBD FLAP UPPER SURFACE AND OUTBD EDGE AT RIGHT WING. RT WING OUTBD FLAP OUTBD GUIDE VANE WAS REPAIRED PER 57-03D PARAGRAPH 11, FIGURE 11.

Part: DOUBLER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL CUTOUT INTERNAL DOUBLER. LAVATORY SERVICE PANEL CUTOUT WAS REPAIRED PER ETI-88-16-351 REV 2 SECTION II ERA 512863-14 REV A.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN AROUND AFT LAVATORY SERVICE PANEL. THIS REPAIR WILL BE MONITORING UNDER LOG PAGE NBR 2705513 ER/A 512863-14 REV A SEC III.

Part: SKIN — WORN (TE FLAP VANE) · airframe 71,012 hrs · 53,307 cycles

WORN OUTBD GUIDE VANE OUTBD FLAP UPPER SURFACE INBD EDGE AT LEFT WING. LT WING OUTBD FLAP OUTBD GUIDE VANE WAS REPAIRED PER 57-03D PARAGRAPH 11, FIGURE 11.

Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL CUTOUT. LAVATORY SERVICE PANEL CUTOUT WAS REPAIRED PER ETI-88-16-351 REV 2 SECTION II ERA 512863-14 REV A.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

HIDDEN DAMAGE, CORROSION ON ANGLE AT STA Y=1338 BTW LONGERONS 29L AND 29R IN AFT CARGO COMPARTMENT. DOUBLER WAS REPLACED AND PARTS OF AREA WERE REMOVED AND INSTALLED PER SRM 51-30-2, 51-30-5, 51-10-4 51-10-3 PAR 14, 21.

Part: RUDDER — DAMAGED (TAIL) · airframe 71,012 hrs · 53,307 cycles

DAMAGED METALIZED ON RUDDER. AREA WAS REPAIRED PER ERA 092613-14MA REVB AND SRM 51-70-1A PARAGRAPH 23.

Part: CHANNEL — CRACKED (LT MLG WW) · airframe 71,012 hrs · 53,307 cycles

INITIAL: CRACK ON FORWARD DOOR JAMB X=8 AT LT WHEEL WELL. CHANNEL WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 5930584.

Part: LONGERON — CRACKED (FUSELAGE) · airframe 71,012 hrs · 53,307 cycles

CRACKED LONGERON 4LT AT STA Y=160 AT CABIN FUSELAGE. DAMAGE SECTION LONGERON WAS REPLACED IAW SRM 53-02, FIG 18, 51-30-2 AND 51-30-5.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

INITIAL: CORROSION ON PREVIOUS REPAIR AT AFT CARGO COMPARTMENT DOOR JAMB, LOWER POSITION. REPAIR SPACER WAS REPLACED IAW SRM 53-05, FIG 123.

Part: BEAM — CRACKED (ENTRY DOOR) · airframe 71,012 hrs · 53,307 cycles

INITIAL: CRACK ON BEAM 1, FWD EDGE, AT MAIN ENTRANCE DOOR. CRACK ON BEAM 1 FWD EDGE WAS REPAIRED IAW SRM 52-05, FIG 82.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

CORROSION ON PREVIOUS REPAIR AT AFT CARGO COMPARTMENT DOOR JAMB. REPAIR SPLACER WAS REMOVED IAW SRM 51-30-5 AND 51-30-4 NEW SPACER WAS FABRICATED IAW SRM 53-05, PAR 140 NEW SPACER WAS INSTALLED IAW SRM 51-30-5 AND 51-30.

Part: SPACER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 71,012 hrs · 53,307 cycles

INITIAL: CORROSION ON MID CARGO COMPARTMENT LOWER DOOR JAMB BEAM PREVIOUS REPAIR SPACER FROM STA Y=636 TO Y=693. SPACER PREVIOUS REPAIR WAS REMOVED IAW SRM 51-30-5 SPACER WAS FABRICATED IAW SRM 53-05, PAR 140, FIG 123 AND SRM 51-10-4 NEW SPACER WAS INSTALLED IAW SRM 51-30-5.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 70,882 hrs · 53,202 cycles

ROW 13B EMERGENCY LIGHT INOPERATIVE. FOUND PIN PULLED FROM CONNECTOR. PINNED AND OPS CHECKED NORMAL IAW SPWM 20-13 AND AMM 33-53.

Part: VALVE — LEAKING (RUDDER) · airframe 68,737 hrs · 51,645 cycles

FLIGHT CREW REPORTED THAT BOTH AFT LAVATORY SMOKE DETECTORS WERE SOUNDING AND CONFIRMED THERE WAS SMOKE AND FUMES PRESENT. THE ACFT RETURNED TO MSP. MAINTENANCE FOUND THAT THE APU INLET WAS CONTAMINATED WITH HYDRAULIC FLUID AND THAT THE RUDDER POWER-MAN VALVE WAS LEAKING AT A FITTING. MAINTENANCE REPLACED THE UNION AND INSTALLED NEW PACKINGS, SUBSEQUENT LEAK CHECKS WERE GOOD. THE APU INLET WAS CLEANED, COALESCER BAGS REPLACED, AND A DUCT BURNOUT PERFORMED. NO ODOR NOTED ON DUCT BURNOUT, THE COALESCER BAGS WERE REPLACED AGAIN, AND THE ACFT WAS RETURNED TO SERVICE.

Part: WIRE HARNESS — DAMAGED (EMERGENCY LIGHTS) · airframe 67,705 hrs · 50,898 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT SEAT 13DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM. LP 6731688.

Part: LANYARD — FRAYED (L1 DOOR SLIDE) · airframe 66,709 hrs · 50,197 cycles

L1 DOOR SLIDE LANYARD FRAYED. REPLACED LANYARD.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 66,691 hrs · 50,185 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHT AT SEAT 11DE WAS INOPERATIVE. MAINTENANCE FOUND A CONNECTOR DISCONNECTED, CONNECTED AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,645 hrs · 50,155 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE COCKPIT WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND THE OPS CHECK WAS GOOD.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 66,553 hrs · 50,089 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT DOORS L1 & R1 AND SEAT ROWS IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND SOME PINS WIRE IN THE CONNECTOR PULLED OUT. THE PINS WERE SECURED INTO THE CONNECTOR AND THE SYSTEM RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,523 hrs · 50,063 cycles

EMERGENCY LIGHTS INOPERATIVE ROWS 1 THRU 12 AND LT AND RT DOOR EXIT IDENTIFIERS. REPLACED THE BATTERY PACK AND POWER SUPPLY. EMERGENCY LIGHTS TESTED OK IAW AMM 33-51.

Part: GROUND WIRE — BROKEN (EMERGENCY LIGHTS) · airframe 66,018 hrs · 49,697 cycles

DURING CHECK, MAINTENANCE FOUND THE EMERGENCY LIGHT FROM ROWS 13 TO 23 TO BE INOPERATIVE. MAINTENANCE FOUND A WIRE TO GROUND BROKEN AT THE PIN. THE WIRE WAS REPINNED AND THE LIGHTS WERE OPERATIONAL.

Part: WIRE — BROKEN (EMERGENCY LIGHT) · airframe 65,900 hrs · 49,605 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING AT SEAT 27DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPAIRED A BROKEN WIRE UNDER THE SEAT AND THEN OPERATIONALLY CHECKED THE SYSTEM.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,726 hrs · 48,781 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING AT ROWS 32-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS AND OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,640 hrs · 48,744 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING FROM ROW 30 TO AFT PRESSURE DOOR WAS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 64,625 hrs · 48,734 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING IN THE COCKPIT AND AT THE FIRST BULKHEAD IN GALLEY WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,611 hrs · 48,035 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING AT ROWS 12-14 IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS FOR THE NOTED LIGHTED AREAS AND THE OPS CHECK WAS GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,242 hrs · 47,762 cycles

DURING LINE CHECK, THE AFT OVERWING EXIT DOOR EMERGENCY EXIT LIGHTS WERE INOPERATIVE ON BOTH SIDES OF THE CABIN. THE OVERWING DOOR EMERGENCY EXIT LIGHT BATTERIES REPLACED AND OPS CHECKED NORMAL.

Part: SKIN — BULGED (BS 1437) · airframe 62,242 hrs · 47,064 cycles

BULGE IN PREVIOUS REPAIR DOUBLER ON FUSELAGE SKIN STA Y=1437, BETWEEN LONG 1 AND 3LT. (REF 94, ZONE 50). REPAIR WAS ACCOMPLISHED IAW AMR 09531212 REV 1, AND ER/A 384071-14 REV A ASSOCIATED ER/A 38-407117 ADDED FOR AC 0944. SDR REPORTABLE.

Part: CABLE — FRAYED (TAILCONE JETTISO) · airframe 62,242 hrs · 47,064 cycles

MX DISCOVERED THAT THE TAILCONE JETTISON CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: PAN — CORRODED (LAV SERVICE) · airframe 62,242 hrs · 47,064 cycles

CORROSION ON AFT LAVATORY SERVICE PANEL PAN. CORROSION WAS REMOVED, MEASURED IAW SRM 51-10-3, PAR 26 AND SRM 53-01 FIG 1 AND IS OUT OF LIMITS.

Part: SKIN — CORRODED (BS 1155-1174) · airframe 62,242 hrs · 47,064 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BETWEEN Y=1155 TO Y=1174 ON BEAM AT LONGERON 28 RT AT AFT CARGO COMPARTMENT. NEW DOUBLER WAS FABRICATED AND INSTALLED IAW SRM 53-05, FIG 123.

Part: INTERCOSTAL — CORRODED (BS 1148-1155) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON INTERCOSTAL FROM BS 1148-1155 BETWEEN LONGERON 29 AND 30R ALSO CORROSION ON STRAP ABOVE SAME INTERCOSTAL AT AFT CARGO COMPARTMENT. REPAIRED IAW SRM 51-30-2, 51-10-3 PAR 14, 21, 26, AND 38 AND ER/A 511165-14.

Part: DOUBLER — WORN (FUSELAGE) · airframe 62,240 hrs · 47,063 cycles

WORN UPPER & LOWER FWD &AFT CORNERS AT AFT LAVATORY SERVICE PANEL DOOR SETTLEMENT AREA, INTERNAL DOUBLER. TITANIUM DOUBLER WAS REPLACED IAW DWG 5911423, REV CD AND SRM 51-30-2, 51-30-5.

Part: FRAME — CORRODED (BS 1136) · airframe 62,242 hrs · 47,064 cycles

CORROSION ON FRAME ANGLE BS 1136 BETWEEN LONGERONS 27-28RT AT AFT CARGO COMPARTMENT. THE FRAME CLIP WAS REMOVED, NEW FRAME ANGLE FABRICATED, AND INSTALLED IAW SRM 51-30-5.

Part: WEB — CORRODED (BS 1155-1212) · airframe 62,242 hrs · 47,064 cycles

CORROSION ON WEB AT BS 1155 TO 1212 BETWEEN LONGERON 28-29R AT AFT CARGO COMPARTMENT. DUE EXCESSIVE CORROSION, NEW WEB WAS INSTALLED IAW SRM 51-10-3, PAR 14,21, 51-30-2, 51-30-5 AND 51-10-4.

Part: FRAME — CORRODED (BS 1322) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON FRAME STA Y=1322 BETWEEN LONG 28 LT TO 28 RT AT AFT CARGO COMPARTMENT. FRAME WAS REPAIRED IAW SRM 53-03D, FIG 2A.

Part: FRAME — CRACKED (BS 1510) · airframe 62,240 hrs · 47,063 cycles

CRACKED AFT ACCESSORY COMPARTMENT CANTED FRAME BS 1510 AND 11 O'CLOCK POSITION. FRAME WAS REPLACED IAW SRM 51-10-4, 51-30-2, 51-10-3 PAR 21/14; DWG 9911843 REV "AC".

Part: LONGERON SPLICE — CORRODED (BS 1287-1309) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON LONGERON SPLICE 22 LT BETWEEN BS 1287-1309 AFT CARGO COMPARTMENT. LONGERON SPLICE REPLACED IAW SRM 53-02, FIG 18.

Part: BEAM — CORRODED (BS 636-693) · airframe 62,240 hrs · 47,063 cycles

CORROSION FOUND ON DOOR FRAME LOWER BEAM BS 636-693 PROJECTION LONGERON 28RT AT MID CARGO COMPARTMENT. REPAIR DOUBLER INSTALLED IAW SRM 53-05, FIG 123. REQUIRED INSPECTION COMPLETED.

Part: DOOR FRAME — CORRODED (BS 636-693) · airframe 62,242 hrs · 47,064 cycles

CORROSION ON JAMB LOWER BEAM STA Y=636-693 PROJECTION LONG 28 RT AT MID CARGO COMPARTMENT. REF 411, ZONE 51 (T0 274860). CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26, WAS MEASURED, DUE TO EXCESIVE CORROSION, WAS REPAIRED. REPAIR DOUBLER WAS INSTALLED. SPACER NUT STRIPS WERE INSTALLED IAW SRM 53-05, FIG 23; RII COMPLETED BY INSPECTION STAMP 200802742 DELTA ID 866445.

Part: FRAME — CORRODED (BS 1155) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON FRAME ANGLE BS 1155 BETWEEN LONGERON 29L TO 29R AT AFT CARGO COMPARTMENT. FRAME ANGLE REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: LONGERON — CORRODED (BS 1174-1193) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON LONGERON 22L BETWEEN BS 1174 TO 1193 AFT CARGO UTILITARY TUNNEL. SECTION OF LONGERON REPLACED IAW SRM 53-02, FIG 18.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · airframe 62,242 hrs · 47,064 cycles

CORROSION TRACK ON LT TIE TRACK FROM BS 1212 TO 1322 AT AFT CARGO COMPARTMENT. TRACK SECTION REPLACED IAW SRM 51-30-1 AND 51-30-5.

Part: FRAME — CORRODED (BS 1117) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON FRAME, BS 1117 BETWEEN LONGERON 29L-29R AFT CARGO COMPARTMENT. FRAME ANGLE WAS REPLACED IAW SRM 51-30-5 AND SRM 53-14-3 FIG 3.

Part: LONGERON — DAMAGED (BS 1309-1322) · airframe 62,240 hrs · 47,063 cycles

WORN LONGERON 19L BETWEEN BS 1309 & 1322 AT AFT CARGO COMPARTMENT. DAMAGED SECTION LONGERON REPLACED WITH NEW LONGERON SECTION IAW SRM 53-02, FIG 18.

Part: LONGERON — DAMAGED (BS 1437 L3R) · airframe 62,240 hrs · 47,063 cycles

CRACKED LONGERON 3 RT AT INTERSECTION WITH FRAME BS 1437 AFT ACCESSORY BAY. DAMAGED SECTION OF LONGERON REMOVED AND NEW SECTION INSTALLED IAW SRM 51-30-2, 51-10-3 PAR 21/14 AND 53-02, FIG 18.

Part: LONGERON — CRACKED (BS 1437 L3L) · airframe 62,240 hrs · 47,063 cycles

CRACKED LONGERON 3 LT AT INTERSECTION WITH FRAME BS 1437. DAMAGE REMOVED AND REPAIR PARTS INSTALLED IAW SRM 53-02, FIG 18, 51-10-3 PAR 21/14, PS 900-5-1 NR 4.

Part: FITTING — CORRODED (BS 1155-1210) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON FITTINGS AT BS 1155 TO 1157 AND 1212 TO 1210 BETWEEN LONGERON PROTECTION 26 TO 29R FITTINGS WERE REPLACED IAW SRM 51-30-5.

Part: ACCESS PANEL — CORRODED (WING) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON COUNTERSINK HOLES OF CTR FUEL TANK ACCESS PLATE 2302C. CORROSION WAS REMOVED AND COUNTERSINK HOLES WERE MEASURED. TWO COUNTERSINK WERE FOUND TO BE OUT OF LIMITS AND WERE REPAIRED IAW SRM 51-10-3.

Part: ACCESS PANEL — CORRODED · airframe 62,240 hrs · 47,063 cycles

CORROSION ON SETTLEMENT AREA OF FUEL TANK ACCESS PANEL 1436C. FOUND OUT OF LIMITS. ACCESS PANEL WAS REPLACED. REMAINING THICKNESS OF 0.150 IS OUT OF LIMITS IAW SRM 51-22-A.

Part: CUSP WEB — CORRODED (BS 715-805) · airframe 62,240 hrs · 47,063 cycles

CORROSION FOUND ON UPPER AND LOWER SURFACE OF LT CUSP WEB FROM BS 715 TO 805 AT CABIN FLOOR STRUCTURE. REPAIRED IAW SRM 51-10-3 PAR 14, 21, 26 AND ER/A 508307-14.

Part: CUSP WEB — CORRODED (BS 736) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION FOUND ON LT CUSP WEB BS 736 BETWEEN X=54 TO X=60 AT CABIN FLOOR STRUCTURE. REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 715) · airframe 62,240 hrs · 47,063 cycles

CORROSION FOUND ON LT CUSP WEB BS 715 BETWEEN X=54 TO X=60 AT CABIN FLOOR STRUCTURE. WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: SKIN — CRACKED (BS 1418) · airframe 62,240 hrs · 47,063 cycles

DURING NDT INSPECTION, TWO CRACKS (0.625" AND 1.906") WERE FOUND ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 1 AND 2R. REPAIRED IAW ER/A 512857-14AD REV, ORIG.

Part: ACCESS PANEL — CORRODED (RT WING) · airframe 62,240 hrs · 47,063 cycles

CORROSION WAS FOUND ON SETTLEMENT AREA COUNTERSINK HOLE ON RT WING FUEL TANK ACCESS PLATE 1409C. ACCESS PANEL WAS REPLACED IAW SRM 51-22-1A PARA 6 (3) CONDITION 3 (B).

Part: CUSP WEB — CORRODED (BS 1200-1250) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION FOUND ON MEMBRANE CUSP WEB X=54 TO 60 BS 1200-1250. MEMBRANE CUSP WEB. REPLACED IAW SRM 51-30-2 AND 51-30-5, 51-30-1 AND ER/A 511180-14.

Part: FLOORBEAM — CORRODED (BS 522) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, A CRACK WAS FOUND ON THE FLOORBEAM AT BS 522. CRACKED FLOORBEAM WAS REPAIRED AND CORROSION WAS REMOVED AND FOUND TO BE WITHIN ACCEPTABLE LIMITS. REPAIR ACCOMPLISHED IAW SRM 51-10-3 AND ER/A 511165-14MA.

Part: LONGERON — CORRODED (BS 1322-1338) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON LONGERON 24LT BETWEEN BS 1322-1338. LONGERON WAS REMOVED & NEW LONGERON WAS INSTALLED IAW SRM 51-30.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, LIGHTNING STRIKE DAMAGE WAS NOTED ON THE RT WINDOW BELT FRAME AFT UPPER CORNER FROM STA Y=617 TO 636. REWORK C DAMAGE WAS REPAIRED IAW ER/A 511174-14 AND WAS CLASSIFIED AS "MAJOR" IAW ENGINEERING. REWORK DAMAGE WAS REPAIRED IAW ER/A 511172-14 AND WAS CLASSIFIED AS "MINOR".

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON THE LT SEAT TRACK AT X=54 BETWEEN STA Y=1246-1250,1262-1266, 1277-1280 AND 1293-1298 IN THE PASSENGER CABIN. THE SEAT TRACK STA 1174-1309 WAS R & R IAW THE SRM.

Part: LONGERON — CORRODED (BS 1309-1322) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON LONGERON 25LT BETWEEN STA Y=1309 TO Y=1322 IN THE AFT CARGO COMPARTMENT. LONGERON SPLICE 25LT WAS REPLACED IAW SRM 53-02 FIG 18.

Part: LONGERON — CRACKED (BS 200 L4L) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, LONGERON 4LT WAS FOUND CRACKED AT Y=200. REPAIR WAS ACCOMPLISHED IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX THE EXTERIOR METALLIC COATING ON BOTH FACES OF THE RUDDER WAS FOUND TO BE DAMAGED. THE RUDDER WAS REPAIRED IAW SRM 51-70-1AD AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON SETTLEMENT AREA AND COUNTERSINK HOLES OF THE LT WING FUEL TANK ACCESS PANEL NR 1307C. ACCESS PANEL WAS REPLACED.

Part: FRAME — CORRODED (BS 1380) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, CORROSION WAS FOUND ON FRAME TEE STA Y=1380 BTW X=24 TO X=-24 AT THE AFT ACCESSORY COMPARTMENT TAIL BUMPER AREA. DAMAGED FRAME WAS REPLACED IAW DWG 9912246, SRM 51-30-2, 51-30-5.

Part: BUSHING — ELONGATED (LT WING) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, ELONGATED BUSHINGS WERE FOUND ON LT WING T/E HEATER BLANKET AREA IN SEVERAL LOCATIONS. BUSHINGS WERE R & R IAW EA 09-070683-03 AD REV "L" AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: LONGERON — CRACKED (BS 522 L4L) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED INSPECTION, LONGERON 4 LT WAS FOUND CRACKED AT BS 522. REPAIR WAS ACCOMPLISHED IAW SRM 53-02 FIG 18.

Part: BUSHING — ELONGATED (RT WING) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, ELONGATED BUSHINGS WERE FOUND ON RT WING T/E HEATER BLANKET AREA IN SEVERAL LOCATIONS. BUSHINGS WERE R & R IAW EA 09-070683-03 AD REV "L" AND THE REQUIRED INSPECTION WAS COMPLETED.

Part: BARRIER — DAMAGED (CARGO DOOR) · airframe 62,240 hrs · 47,063 cycles

DURING SCHEDULED MX, WEAR, SCRATCHES AND CRACKS WERE FOUND ON THE INNER & OUTER SURFACE OF FWD CARGO COMPARTMENT DOOR BARRIER. CARGO COMPARTMENT DOOR BARRIER WAS REPAIRED IAW ER/A 094625-14MA, REV D ASSOCIATED ER/A 09-462514 ADDED FOR AC 0944.

Part: SEAT TRACK — CORRODED (BS 778-1235) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON LT SEAT TRACK X=54BTW BS 778-1235 IN PAX CABIN. REPAIR PLUGS WITH CORROSION WERE REMOVED AND NEW REPAIR PLUGS WERE INSTALLED IAW ER/A 485415-14MA.

Part: SEAT TRACK — CORRODED (BS 529-954) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON REPAIR PLUGS ON RT SEAT TRACK X=-22 BTW BS 529-954. REPAIR PLUGS WITH CORROSION WERE REMOVED AND NEW REPAIR PLUGS WERE INSTALLED IAW SRM 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 1193-1197) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON RT SEAT TRACK, X=-22 BETWEEN STAY=1193-1197 AND Y= 1225-1228 AT PASSENGER CABIN. DAMAGE AREA WAS CUT OUT, NEWS PLUGS WERE ADJUSTED, TREATED AND PAINTED AND WERE INSTALLED IAW SRM 51-10 -3, PAR 14 AND 21 53-05, FIG 4A.

Part: SEAT TRACK — CORRODED (BS 995-1089) · airframe 62,240 hrs · 47,063 cycles

CORROSION ON REPAIR PLUGS ON LT SEAT TRACK X=22STA Y=516-520, 995-998 AND 1085-1089. NEW REPAIR PLUGS WERE INSTALLED IAW SRM 53-05, FIG 4A.

Part: WIRE HARNESS — SHORTED (EMERGENCY LIGHT) · airframe 61,999 hrs · 46,896 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 12D IN THE CABIN WAS DEFECTIVE AND FLICKERING. MX FOUND A SHORTED WIRE AND REPLACED THE WIRE HARNESS. THE SYSTEM HAS RETURNED TO NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 60,564 hrs · 45,830 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGN ABOVE DOOR 2L AND THE EEPL AT ROWS 32 AND 34 WERE TOO DIM. MAINTENANCE REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: LINK — DAMAGED (CATWALK TAILCONE) · airframe 60,425 hrs · 45,737 cycles

MAINTENANCE DISCOVERED THAT THE TAIL CONE CATWALK OVER THE VENTRAL STAIRWAY WAS STUCK IN THE DOWN POSITION. THE LINK ATTACHING THE CATWALK TO THE STAIRS TORQUE TUBE WAS MISSING HARDWARE AND WAS DAMAGED. THIS COULD HAVE AN ADVERSE AFFECT ON THE OPERATION OF THE EMERGENCY EVACUATION ROUTE AND IS NOT IN COMPLIANCE WITH 14 CFR PART 121.703. THE LINK AND THE HARDWARE WERE REPLACED AND THE SYSTEM WAS RIGGED BACK INTO SPECIFICATIONS.

Part: STRUCTURE — DAMAGED (BS 235) · airframe 57,351 hrs · 43,616 cycles

ON WALKAROUND FOUND DAMAGE AT FS 235, 3 INCHES ABOVE THE CUSP ANGLE ON THE FWD LT SIDE OF ACFT. THE DAMAGE IS SUSPECTED TO BE CAUSED BY A JETWAY. DAMAGE IS TO AN EXISTING REPAIR DOUBLER WHICH WAS PREVIOUSLY INSTALLED.

Part: SWIVEL — LEAKING (HYDRAULIC SYSTEM) · airframe 57,342 hrs · 43,609 cycles

UPON FINAL APPROACH, STRONG "HOT" ODOR WAS REPORTED. NO VISIBLE SMOKE NOTED IN CABIN OR FLIGHT DECK, HOWEVER FIRST CLASS LAVATORY DETECTOR SOUND FOR APPROXIMATELY 1 MINUTE. ENGINE ANTI-ICE WAS ON. PASSENGERS COMPLAINED OF BURNING ODOR THROUGHOUT CABIN WHILE DEPLANING. MAINTENANCE FOUND SWIVEL GLAND ON NOSE GEAR LEAKING. REMOVED AND REPLACED LEFT NOSE STEERING SWIVEL GLAND PER MM. LEAK AND OPERATIONAL CHECKS GOOD. PERFORMED OPERATION 5089 - DUCT BURNOUT. AIRCRAFT CHECKED GOOD. OKAY FOR SERVICE.

Part: LINE — LEAKING (HYDRAULIC SYSTEM) · airframe 57,328 hrs · 43,600 cycles

DURING TAKEOFF, FIRST CLASS PASSENGERS COMPLAINED OF AN ODOR AND BUZZING SOUND ORIGINATING FROM THE LEFT SIDE CEILING. ALL COCKPIT INDICATIONS NORMAL. ODOR DISSIPATED AFTER APPROXIMATELY 10 MINUTES. MAINTENANCE FOUND APU INLET CONTAMINATED WITH OIL. SUSPECT OVER SERVICING. ALSO FOUND HYDRAULIC LEAK IN LEFT WHEEL WELL AT AUXILIARY PUMP LINE. SECURED LINE. LEAK CHECK GOOD. CLEANED APU INLET AND PERFORMED OPERATION 5088 AND 5089. NO SMOKE OR FUMES IN CABIN. AIRCRAFT OKAY FOR SERVICE.

Part: SKIN — WORN (VERTICAL STAB) · airframe 56,701 hrs · 43,165 cycles

DURING CHECK, WEAR DAMAGE WAS NOTED TO UPPER EDGE OF THE VERTICAL STABILIZER LOWER FIXED L/E DUE TO SKIN WASHER INSTALLATION. REPAIR IAW ERA 487430-14.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 55,679 hrs · 42,430 cycles

MAINTENANCE FOUND THE LIGHT AT SEAT 13DE TO BE INOPERATIVE. MAINTENANCE RE-SECURED THE PLUG. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: SKIN — DENTED (BS 1300 L26L) · airframe 54,970 hrs · 41,942 cycles

ACFT RECEIVED DAMAGED AT FS 1300 LONGERON 26L. THE ACFT WAS REPAIRED IAW ERA 480472-14.

Part: SKIN — DENTED (BS 1305 S23-24L) · airframe 54,970 hrs · 41,942 cycles

DENT, LEFT SIDE OF ACFT STA 1305 BETWEEN STRS 23 AND 24, 12 INCHES BELOW OUTFLOW VALVE, 856586. ALL REPAIRS PERFORMED IAW ERA 480472-14 REV A ON N/R CARDS 2-9 AND 24-37 AND ERA 480515-14 REV A ON N/R CARDS 10-19.

Part: SKIN — CRACKED (HORIZ STAB) · airframe 53,666 hrs · 41,085 cycles

HORIZONTAL STABILIZER RT UPPER AFT SKIN WAS CRACKED AND A TIME LIMITED REPAIR HAD BEEN INSTALLED AT A PREVIOUS MTC VISIT. REPLACED THE SKIN PANEL PER ERA 460328-14AD, EA 09-460214-12AD AND DWG SR09550031.

Part: ACTUATOR — LEAKING (MLG) · airframe 51,381 hrs · 39,624 cycles

CLIMBING THROUGH 4000 FT MSL ACID ODOR CAME THROUGH THE CABIN AND COCKPIT. DISSIPATED A FEW MINUTES LATER. FOUND LT AND RT MLG ACTUATORS LEAKING. MOVED ACFT TO THE WASHRACK. REMOVED APU DOOR PANEL FOR CLEANING. REINSTALLED APU DOOR PER M/M AND C/W OPN 5090. ALT DUCT BURNOUT. REMOVED BOTH LT AND RT MLG RETRACT ACTUATORS IAW AMM. REINSTALLED ACTS AFTER SHOP VISIT. OPS AND LEAK CHECK OK.

Part: PUMP — INOPERATIVE (HYD SYSTEM) · airframe 50,298 hrs · 38,899 cycles

RIGHT ENGINE HYDRAULIC PUMP FAILED IN FLIGHT, ZERO PRESSURE PRESSURE GOOD WITH AUX HYD PUMP, RETURNED TO ATL. REPLACED ENGINE HYDRAULIC PUMP, CASE DRAIN AND PRESSURE FILTERS. REPLACED RT HYDRAULIC SYSTEM MAIN FILTERS- OPERATED ENGINE PRESSURE CKS GOOD, LK CKS GOOD.

Part: ENGINE — DAMAGED (RIGHT) · airframe 49,819 hrs · 38,573 cycles

ON DEPARTURE, A LOUD BANG WAS HEARD FOLLOWED BY RIGHT ENGINE ROLLBACK. IDLE OIL PRESS OK. QRH FOLLOWED WITH NO OTHER SIGNIFICANT ISSUES NOTED. REPLACED RT ENGINE PER TRANSMITTAL 9T102.

Part: STALL WARNING — FALSE ACTIVATION · airframe 49,754 hrs · 38,524 cycles

DURING CLIMB-OUT AS SLATS RETRACTED BOTH STALL IND FAIL AND WINDSHEAR INOP LIGHTS ILLUMINATED. REPLACED NR 2 STALL WARNING COMPUTER AND RT AOA TRANSDUCER CHECKS NORMAL. PERFORMED STALL WARNING TROUBLESHOOTING CHEC PER AMM 34-19-00 PAGE BLOCK 101 AND ADJUSTMENT TEST PER AMM 34-19-00-201 WINDSHEAR CHECKS GOOD

Part: LINE — LEAKING (HYDRAULIC SYS) · airframe 48,355 hrs · 37,658 cycles

NUMBER 2 ENGINE HYDRAULIC PRESSURE LINE LEAK AND CAUSE TO LOSE MOST OF THE HYDRAULIC FLUID. REPLACED FLEX LINE FROM NR 2 ENGINE TO PYLON LEAK CHECKS NORMAL.

Part: HOSE — LEAKING (HYD SYSTEM) · airframe 48,355 hrs · 37,658 cycles

FLT 456 ATL-DCA DIVERTING TO IAD DUE TO RT SYSTEM HYD QTY LOSS AT CRUISE. RT SYSTEM QTY DECREASING AT CRUISE FL 330 AT APPROX 2 QUARTS QTY NOTICED RT SYSTEM PRESSURE DECREASING AS WELL. SHUTDOWN RT SYSTEM HYD PER NNC.13.12 AND REVIEWED PROCEDURES. DUE TO POSSIBILITY OF ALT GEAR EXTENSION THE CREW HAS ELECTED TO DECLARE AN EMERGENCY AND DIVERT TO IAD FROM DCA. MTC FOUND HOSE ASSY AE705537-1 IPC 29-10-00-11B ITEM 30 ENG DRIVEN HYD PUMP PRESSURE LINE BROKEN. REPLACED LINE AND SERVICED HYD SYSTEM CLEANED RESIDUE. A/C OK FOR SERVICE.

Part: TAB — DENTED (LT ELEVATOR) · airframe 47,680 hrs · 37,234 cycles

SEVERAL DENTS AT TRAILING EDGE OF THE LT ELEVATOR CONTROL TAB P/N 5910413-513 IN THE VINCINTY AREA OF STA. XET =80.75. PERMANENT REPAIR WAS ACCOMPLISHED IAW SRM 55-04 PARA 3 FIG 2 APPLYING PROCEDURES EST IN SRM 51-70-2.

Part: VANE — DELAMINATED (RT WING TE FLAP) · airframe 47,680 hrs · 37,234 cycles

DELAMINATION AT LOWER SURFACE ON RT WING INBOARD FLAP VANE BETWEEN STATIONXCW=79.00 AND XCW=104.500. AMX PERFORMED PERMANENT REPAIR PER SRM 57-03 FIG 9A.

Part: INTERCOSTAL — CORRODED (BS 1322-1338) · airframe 47,680 hrs · 37,234 cycles

FAA FINDING EXFOLIATION CORROSION ON INTERCOSTAL AND LONGERON 22 LT STA Y=1322 AND STA Y=1338 (TASK CARD 57-53300). INTERCOSTAL FAB PER DWG 5911423 (AMX200302178). LONGERON CLEANED AND REINSPECTED, NO CORROSION FOUND (AMX 200201264). INTERCOSTAL REINSTALLED PER SRM 51-30-2 AND DWG 5911423.

Part: FITTING — CRACKED (BS 218) · airframe 47,680 hrs · 37,234 cycles

FOUND CRACK ON FWD JACK POINT FITTING. NEW JACK POINT FITTING WAS INSTALLED IAW DWG 9951888 (AMX 200301685).

Part: SKIN — DAMAGED (BS 560-588) · airframe 47,680 hrs · 37,234 cycles

LIGHTNING STRIKES DAMAGE AT THREE LOCATIONS ON AIRPLANE SKIN, BETWEEN STA Y=560 AND STA Y=588 AND BETWEEN LONGERONS 26 AND 27 LT. PERMANENT REPAIR INSTALLED IAW AERO MEXICO DRAWING NO#AMR0953606 R02. DOCUMENTED IN DELTA ERA 461310-14.

Part: SKIN — DENTED (BS 332-351 S20R) · airframe 47,680 hrs · 37,234 cycles

DUE AT HMV, 3 SRM 53-04D DENT IN FUSELAGE BETWEEN SAT 332 AND351 STRINGER 19-20 RT PERMENANT REPAIR. REPAIRED PER SRM 53-04D FIG 12C.

Part: MEMBRANE — CRACKED (BS 1485 L6R) · airframe 47,680 hrs · 37,234 cycles

CRACKED MEMBRANE AND REPAIR DOUBLER ON FUSELAGE INNER STRUCTURE AT STA Y=1485 CANT LONG 6 RT. PERMENANT REPAIR INSTALLED PER SRM 53-01 (AMX200602028).

Part: SKIN — DENTED (FUSELAGE) · airframe 47,680 hrs · 37,234 cycles

DENT AND EXISTING PERMANENT REPAIR WERE REPORTED ON FUSELAGE SKIN P/N 5920323-249, BETWEEN Y= 332.00 AND Y=351.00 AND BETWEEN LONGERONS 19 RT AND 20 RT. AMX INSTALLED PERMANENT REPAIR PER SRM 53-04 FIG 12 C.

Part: SKIN — WRINKLED (FUSLEAGE) · airframe 47,680 hrs · 37,234 cycles

WRINKLES IN FUSELAGE SKIN STA Y294.00 TO Y=351.00 AND BETWEEN LONGERONS 24 AND 26 RT. DAMAGED SKIN WAS REPLACED USING A PERMANENT REPAIR IAW SRM 53-04 FIG 12C.

Part: VANE — DENTED (LT TE FLAP) · airframe 47,680 hrs · 37,234 cycles

EROSION AND DELAMINATION ON LOWER SURFACE DENTS ON UPPER SURFACE OF LT INNER FLAP OUTBD VANE. DOUBLER, FILLER REPAIR BONDING WAS DONE IAW SRM 51-70-2D PARA H. REPAIRED IAW SRM 57-03D PARA 8A FIG 9A.

Part: VANE — DELAMINATED (LT TE FLAP) · airframe 47,680 hrs · 37,234 cycles

EROSION AND DELAMINATION ON LOWER SURFACE, DENTS ON UPPER SURFACE OF LT INNER FLAP O/B VANE. AEROMEXICO PERFORMED PERMANENT REPAIR FOR THE DAMAGED SKIN PORTION IAW MD-80 SRM 57-03 FIG 9A (DELTA AIRLINES SRM CHAPTER 57-03D FIG 9A)

Part: PAN — CORRODED (CARGO DOORWAY) · airframe 47,680 hrs · 37,234 cycles

CORROSION FOUND ON FWD CARGO COMP DOOR JAMB PAN BETWEEN STA Y=370.00 AND STA Y=427.00. AMX PERFORMED PERMANENT REPAIR PER SRM 53-05 FIG 804 VIEW C-C AND D.

Part: VANE — DELAMINATED (RH TE FLAP) · airframe 47,680 hrs · 37,234 cycles

INADEQUATE REPAIR AND DELAMINATION ON RT INNER FLAP INNER VANE. FILLER, DOUBLER REPAIR WERE FABRICATED IAW SRM 57-03D PAR 8A FIG 9A ( SHEET 1 AND 2 ) RT INNER FLAP INNER VANE WAS REPAIRED IAW SRM 57-03 PAR 8A FIG 9A SHEET 1 AND 2 (AMX 200202768).

Part: FITTING — CORRODED (RT NACELLE) · airframe 47,680 hrs · 37,234 cycles

CORROSION FOUND ON THE BORE AND SURROUNDING AREA OF THE EXISTING LOWER HOLE (FRONT FACE) OF THE RT PYLON FRONT SPAR ENGINE MOUNT FITTING, P/N 5935711-2 SATATION 1307.00. TIME LIMITED REPAIR PERFORMED IAW ERA 461312-12REV O. AFFECTED HOLE OF FITTING P/N 5935711-2 WAS ENLARGED AND A BUSHING WAS INSTALLED PER SRM 54-04 FIG 12.

Part: STRUT — CORRODED (NLG) · airframe 47,677 hrs · 37,233 cycles

NLG SHOCK STRUT CYLINDER CORROSION CLEANED UP PER CMM, BUT CADMIUM PLATING OMITTED ON A TIME-LIMITED BASIS.

Part: TAB — DENTED (LT ELEVATOR) · airframe 47,677 hrs · 37,233 cycles

SEVERAL DENTS AT TRAILING EDGE OF THE LT ELEVATOR GEARED TA, P/N 5910414-501 IN THE VICINTY AREA OG STATION XET = 119.75. PERMENANT REPAIR WAS PERFORMED IAW SRM 55-04 PARA 3 FIG 2. APPLYING PROCEDURES EST IN SRM 51-70-2.

Part: STRUT — CORRODED (NLG) · airframe 47,677 hrs · 37,233 cycles

PITTING CORROSION ON NOSE GEAR SHOCK STRUT. TIME LIMITED REPAIR INSTALLED PER ERA461314-14. PERMENANT REPAIR TO BE ACCOMPLISHED 500 FLIGHT CYCLES FROM MAY 7,2007 OR NO LATER THAN JULY 4 2007.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 47,677 hrs · 37,233 cycles

DENTS ON LOWER SKIN OF LT INNER FLAP STA XW-49. REPAIRED PER ERA 461313-14 REV O.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 47,677 hrs · 37,233 cycles

CRACK INTERCOSTAL SAT Y=218 BETWEEN LONGERON 30 AND 29RH. AMX PERFORMED PERMENANT REPAIR PER ERA 460138-14.

Part: MOUNT — CORRODED (RT ENGINE) · airframe 47,677 hrs · 37,233 cycles

RT PYLON FRONT SPAR ENGINE MOUNT FITTING LOWER HOLE HAD CORROSION IN THE BORE AND SURROUNDING FORWARD FACE. REPAIRED PER ER/A 461312-14.

Part: SKIN — DAMAGED (BS 560-588) · airframe 47,677 hrs · 37,233 cycles

DURING HMV AT GDL, LIGHTNING STRIKES WERE REPAIRED AT THREE LOCATIONS IN THE FUSELAGE SKIN, P/N 5936434-129 BETWEEN STA 560 AND 588, S-26L AND S-27L. REPAIRED PER AMR0953606R02, ER/A 461310-14.

Part: SKIN — DAMAGED (FS 218 L29R) · airframe 47,677 hrs · 37,233 cycles

DURING HMV, THE FUSELAGE SKIN WAS SEVERELY DAMAGED NEAR FS 218 AND LONGERON 29R. A PERMANENT REPAIR WAS ACCOMPLISHED PER BOEING INSTRUCTIONS, AS CONTAINED IN ERA 460138-14.

Part: CONTROLLER — MALFUNCTIONED (CABIN PRESSURE) · airframe 43,910 hrs · 34,584 cycles

DURING CLIMB FLOW LIGHT ILLUMINATED PASSING 10000 FT AUTO 1 LIGHT ON. DURING RETURN TO ATL CABIN ALTITUDE REACHED 5500 FT VERY LITTLE AIRFLOW WAS PRODUCED BY THE RIGHT PACK. SECURED LOOSE DUCTING AND REPLACED NR 1 PRESSURE CONTROLLER.

Part: BALLAST — BURNED (SEAT 37DE) · airframe 43,157 hrs · 34,030 cycles

ARRIVED IN ATL WITH AN INBOUND WRITE UP THAT READ, ON TAKEOFF RECEIVED BURNING SMELL THROUGHOUT CABIN AND COCKPIT. DISSIPATED WITHIN A FEW MINUTES. IT RETURNED 2 HRS LATER AT CRUISE FOR A FEW MINUTES (SECURED GALLEY POWER). UNABLE TO LOCATE SOURCE. RETURNED 3RD TIME BRIEFLY ON APPROACH, AFTER TROUBLE SHOOTING PER OPN 5088, FOUND THE ODOR COMING FROM INOP BALLAST AT SEAT 37DE. AFTER OPN OF PACKS, APU AND ENGS NO FURTHER ODORS NOTED. BALLAST P/N D773-11-001 AND S/N 4666 WAS CHANGED.

Part: LINE — UNSERVICEABLE (HYDRAULIC SYS) · airframe 39,935 hrs · 31,691 cycles

ON CLIMBOUT, RIGHT HYDRAULIC QTY WENT TO -0- FOLLOWED BY LOSS OF HYDRAULIC PRESSURE. REPLACED RIGHT ENGINE PRESSURE LINE.

Part: BRAKE ASSY — FAILED (MLG) · airframe 39,072 hrs · 31,073 cycles

NR 1 BRAKE ASSY FAILED INTERNALLY AND CAME APART WHICH LOCKED THE BRAKE. REPLACED SAME.

Part: A/C PACK — FAILED (AFT) · airframe 38,931 hrs · 30,958 cycles

NO PACK PRESSURE- LT AND RT ON INITIAL CLIMB TO 6000 FT. NO CABIN DIFF PRESSURE, CABIN ALT ALTITUDE AT AIRCRAFT ALT. COULD NOT REGAIN NORMAL PACK OPERATION. RETURNED TO KSTL. REPAIRED AUTO-SHUTOFF SYSTEM.

Part: ODOR — DETECTED (CABIN) · airframe 37,764 hrs · 30,138 cycles

ON APPROACH TO BOS AFTER LANDING GEAR WAS LOWERED- BOTH AFT LAV SMOKE DETECTORS SOUNDED- AT THE SAME TIME AFT F/AS SMELLED A BURNING ODOR. ALSO BOTH PILOTS SMELLED SAME ODOR IN COCKPIT SIMULTANEOUSLY. AFTER LANDING ALARMS CEASED AND ODOR WENT AWAY. REMOVED RT ACM TURB INLET AND EXHAUST DUCT FOR INSP. NO OIL FOUND. BOROSCOPED NR 1 AND 2 ENGS BEARING AREAS, NO OIL RESIDUE FOUND. C/W OPN 5088 AND OPN 5089, ALL CK OK. INSTALLED GEAR PINS AND CYCLED GEAR HANDLE SEVERAL TIMES. NO LEAKS NOTED. ACFT OK FOR SERVICE.

Part: PACKING — LEAKING (CHIP DETECTOR) · airframe 37,134 hrs · 29,689 cycles

STRONG ODOR IN CABIN WHEN AIRFOIL ANTI ICE SELECTED. FOUND APU INLET CONTAMINATED WITH OIL FROM APU CHIP DETECTOR. REPLACED PACKING ON APU CHIP DETECTOR. PERFORMED OP ON 5088 AND OPN 5089. A/C OK FOR SERVICE.

Part: WIRE — BROKEN (SEAT 10D) · airframe 33,096 hrs · 26,709 cycles

EMERGENCY LIGHT INOP IN SEAT 10D ON L/O INSPECTION. REPLACED LIGHT ASSY CHECKS OK

Part: SMOKE DETECTOR — INTERMITTENT (LAVATORY) · airframe 32,930 hrs · 26,577 cycles

FWD LAV SMOKE ALARM WENT OFF 3 TIMES DURING FLT WITH NO ONE OR NO SMOKE IN LAV. REPLACED FIRST CLASS LAV SMOKE DETECTOR - CKS OK

Part: SKIN — CORRODED (FUSELAGE) · airframe 32,872 hrs · 26,533 cycles

THE FUSELAGE SKIN WAS FOUND WITH AN AREA OF CORROSION, ADJACENT TO AN EXISTING ANTENNA CUTOUT AT FS 610 BETWEEN STRINGERS 29R AND 30. THE CORROSION WAS REMOVED WITH A 5.2X 4.6 CUTOUT. THE CUTOUT WAS REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER PER ER/A 380167-14, REV B.

Part: CONTROL MODULE — CRACKED (LT TR UNIT)

LEFT HYD QUANTITY FELL TO 2 QTS IN FLIGHT. FOUND LEFT REVERSER CONTROL MODULE HOUSING CRACKED. REPLACED SAME.

Part: POWER SUPPLY — INOP (CABIN)

F/C EMERGENCY LIGHTS WOULD NOT TEST. REPLACED PWR SUPPLY B5-211. LIGHTS CK GOOD.

Part: FAN — FAILED (CABIN)

ELECTRICAL ODOR IN CABIN. DIVERTED TO CHS. REPLACED CABIN RECIRC FAN, ALL CKS NORMAL.

Part: SKIN — DAMAGED (BS 1305)

FUSELAGE SKIN FS 1305, L-26L, REPAIR FOR GROUND DAMAGE. THE FUSELAGE SKIN WAS DENTED AND TORN AT THE LONGERON 26L LAP SPLICE AT FS 1305. THE DAMAGE WAS REMOVED WITH A 10.5 BY 9.5 CUTOUT. THE DAMAGE WAS REPAIRED WITH AN STRUCTURAL FILLER AND AN EXTERNAL ALUMINUM DOUBLER PER ER/A 366336-14, REV B.

Part: BRACKET — BROKEN (NR 2 ENGINE)

WITH RT ENG FIRE LOOP SELECTED TO B DUE A ON PREV MCO GOT A FIRE WARNING ON THROTTLE UP FOR T/O TESTED BAD IN B-LOOP. FOUND LOWER FIRE SUPPORT BRACKET BROKEN AND GRD STUD LOOSE. REPLACED SUPPORT FIRE WARNING, TESTED GOOD AND CKED GOOD ON ENG RUN. ALSO, REMOVED MCO ON A LOOP DUE ALSO, TESTED OK.

Part: COALESCER — CONTAMINATED (CABIN)

DURING INITIAL CLIMB, LT REAR LAV SMOKE DETECTOR SOUNDED WITH ODOR SIMILAR TO GLYCOL, DISSIPATED WITHIN 5 MINUTES. PERFORMED DUCT BURNOUT PER M/M. REPLACED BOTH WATER SEPARATORS. NO ODOR.

Part: STRUT — UNDERSERVICED (NLG)

ON TAKEOFF FROM LGA, UPON GEAR RETRACTION, RED NOSE GEAR UNSAFE LIGHT WOULD NOT EXTINGUISH. CYCLED GEAR TO NO SATISFACTION. CONCURRENTLY LOST AUTO PRESSURIZATION, TRANSPONDER AND HAD STALL IND FAILURE AND AUTO SPOILER FAIL MSGS ON OAP. DIVERTED TO JFK. SERVICED NOSE GEAR STRUT PER 32-21-02. PERFORMED BITE OF PROX BOX, SHOWS NO FAULT. CABLE-TO-GROUND CONTROL RELAY OK.

Part: JAMB — CORRODED (C 1 DOOR)

DURING HMV, FOUND FORWARD CARGO DOOR JAMB CORRODED. REPAIRED PER SRM 53-05, FIG 44.

Part: BULB — FAILED (CABIN)

EMERGENCY ESCAPE TRACK LIGHT PULLED OUT AT SEAT 3C. REBULBED AND REINSTALLED LENS.