N918DL

Part: COVER — BROKEN (LIGHT SWITCH) · airframe 74,952 hrs · 57,578 cycles

FLIGHT CREW REPORTED THE CAPTAIN GOT SHOCKED WHEN TURNING ON NOSE LANDING LIGHTS. FOUND SWITCH COVER UNDER GLARESHIELD BROKEN. REMOVED AND REPLACED COVER. ACFT OK FOR SERVICE IAW AMM 33-41.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 74,405 hrs · 57,146 cycles

AFTER TAKE OFF, PASSENGERS AND AFT FLIGHT ATTENDANTS REPORTED AN ODOR OF HYDRAULIC FLUID AND A LIGHT A HAZE IN CABIN. THE ODOR AND HAZE DISIPATED QUICKLY. NO ABNORMAL HYD INDICATIONS IN FLIGHT DECK. PERFORMED WORKCARD 2120-2367. AFTER INSPECTION OF APU, APU INLET, WHEEL WELLS, FOUND A HYD LINE ASSOCIATED WITH PTU WITH SLIGHT LEAK. PERFORMED TASK 6 OF FLOW CHART STEP 6,11,13. REPAIRED THE LEAK, COMPLIED WITH WORKCARD 4950-2215, ALT DUCT BURN. NO SMOKE OR ODOR. CLEANED BELLY, APU INLET. NO FURTHER LEAKS NOTED. R & R AIR COND COALESCER BAGS IAW AMM 21-20-02. OPS NORMAL. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 73,753 hrs · 56,654 cycles

TAIL CONE EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACKS IAW AMM 33-53.

Part: TIRE — FAILED (LT MLG) · airframe 73,721 hrs · 56,618 cycles

AFTER TAKEOFF, AIRFRAME VIBRATION AND BURNING RUBBER ODOR FOLLOWED BY LEFT MAIN GEAR UNSAFE INDICATION WITH GEAR STILL EXTENDED. CHECKED LANDING GEAR VISUALLY AND NOW HAVE 3 GREEN DOWN AND LOCKED GEAR SAFE LIGHTS. FOUND THE NR 2 MAIN TIRE BLOWN AND RECAP SEPARATED. REPLACED BOTH LEFT MAIN GEAR WHEELS IAW AMM 32-40, NR 2 BRAKE IAW AMM 32-42, LEFT GEAR DOWN AND LOCKED PROXIMITY SWITCH HARNESS IAW AMM 32-60, AND PLACED THE LT MLG INBD DEBRIS DEFLECTOR ON CDL 32-12-03. NO OTHER DAMAGE NOTED.

Part: CAM — WORN (TAILCONE RELEASE) · airframe 73,583 hrs · 56,534 cycles

FOUND BASE OF THE TAILCONE RELEASE MECHANISM CAM WORN. REPLACED TAILCONE RELEASE MECHANISM CAM BASE IAW AMM 53-53-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,805 hrs · 55,935 cycles

COCKPIT AND FWD ENTRY EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK. OPS CHECKED OK IAW AMM 33-50.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,328 hrs · 55,584 cycles

FIRST CLASS AISLE EMERGENCY LIGHTS INOPERATIVE. FOUND FIRST CLASS POWER SUPPLY BAD. REMOVED & REPLACED POWER SUPPLY IAW AMM 33-53. BATTERY NOT REPLACED. OPS CHECKED OK.

Part: WIRE — SHORTED (EMERGENCY LIGHTS) · airframe 71,283 hrs · 54,808 cycles

THE FLIGHT CREW FOUND THAT THE EMERGENCY LIGHTING BETWEEN ROWS 32 AND 36 WERE INOPERATIVE. THE TAIL COMPARTMENT EMERGENCY LIGHTS WERE FOUND INOPERATIVE. MAINTENANCE FOUND THE TAILCONE INTERIOR HANDLE LIGHT SHORTED AND REPAIRED THE WIRES. THE EMERGENCY LIGHTS CHECKED OK.

Part: STRUCTURE — MISSING (RUDDER) · airframe 70,913 hrs · 54,557 cycles

FLAME SPRAY MISSING FROM CRITICAL ZONES ON RUDDER IAW SRM 55-03, PAGE 91 AND 92. RUDDER REQUIRES REPLACEMENT. RUDDER ASSY, PN 5955501-1, SN 0327 REMOVED. INSTALLED RUDDER IAW AMDS WC 2720-4421 AND 2720-7454. OK FOR SERVICE.

Part: SKIN — DAMAGED (RT WING) · airframe 70,345 hrs · 54,178 cycles

SEVERAL GOUGES ON FIXED L/E BETWEEN BS XIS=83 AND XIS=73 AT RT WING. FIXED L/E BETWEEN BS XIS=83 AND XIS=73 AT RT WING WAS REPAIRED IAW ER/A 541584-14, REV ORIGINAL AND SLAT TRACK NR 3 WAS REMOVE/INSTALL IAW AMM 27-80-01; AFTER BLEND OUT, ORIGINAL THICKNESS 0.145" AND 0.044 AND REMAINING RESPECTIVELY IS 0.0106 AND 0.029 THEREFOR ARE OUT OF LIMITS IAW SRM 57-01, FIG 1.

Part: SKIN — CRACKED (CARGO DOOR) · airframe 70,338 hrs · 54,173 cycles

CRACKED FWD CARGO DOOR OTBD SKIN AROUND OTBD HANDLE. CRACK ON FWD CARGO DOOR OTBD SKIN AROUND OTBD HANDLE, C1 WAS REPAIRED IAW ER/A 591590-14 REV ORIGINAL.

Part: SKIN — CRACKED (BS 1437) · airframe 70,338 hrs · 54,173 cycles

CRACK ON EXTERNAL FUSELAGE SKIN BETWEEN LONGERONS 2 - 3RT BS 1437. REPAIRED IAW ER/A 541550-14, REV ORIG SECTION I.

Part: SKIN — DAMAGED (BS 788-807) · airframe 70,338 hrs · 54,173 cycles

LIGHTNING STRIKE ON RT WINDOW BELT BETWEEN BS 788 - 807 AT FWD AREA. LIGHTNING STRIKE ON RT WINDOW BELT WAS BLENDED OUT, POLISHED, MEASURED AND TREATED IAW SRM 53-05, FIG 111 AND ER/A 541586-14 REV ORIGINAL.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 70,338 hrs · 54,173 cycles

LIGHTNING STRIKES ON FWD, AFT UPPER CORNER AT WINDOW BELT NR 59 EXTERNAL FUSELAGE SKIN. LIGHTNING STRIKES ON WINDOW BELT NR 59 EXTERNAL FUSELAGE SKIN WERE BLENDED OUT AND ARE WITHIN LIMITS IAW SRM 53-05, FIG 111 AND ER/A 541585-14, REV.A.

Part: DOOR FRAME — CRACKED (LT MLG) · airframe 70,338 hrs · 54,173 cycles

CRACKED TEE ON AFT DOOR JAMB AT LT MLG. TEE ON AFT DOOR JAMB AT LT MLG WAS REPAIRED IAW SRM 53-05, FIG 141.

Part: SKIN — WORN (VERTICAL STAB) · airframe 70,338 hrs · 54,173 cycles

WEAR ON RT SKIN BETWEEN BS ZFS 180 AND ZFS 165 AT VERTICAL STABILIZER. RT SKIN WAS REPLACED DUE EXCESSIVE WEAR IAW SRM 55-32-0, FIG 3 AND DWG 5936143, REV.

Part: LONGERON — CRACKED (BS 200) · airframe 70,338 hrs · 54,173 cycles

CRACKED LONGERON 4L AT BS 200. THE LONGERON WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-02, FIG 18.

Part: LONGERON — CORRODED (BS 1287-1295) · corrosion level 2 · airframe 70,338 hrs · 54,173 cycles

SEVERAL CORROSION POINTS ON LONGERON 30 FROM BS 1287 - 1295. THE LONGERON WAS REPLACED IAW SRM 53-02, FIG 18.

Part: RIB — CRACKED (LT WING) · airframe 70,338 hrs · 54,173 cycles

CRACKED CLIP AND RIB L/E AREA BS XRS=414.100 APPROXIMATELY LT WING. RIB AND CLIP WERE REPLACED IAW DWG 9919329-7, REV T AND SRM 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (NR 1 SLAT) · airframe 70,338 hrs · 54,173 cycles

CRACK ON RT SLAT PANEL NR 1 XIS=133 APPROXIMATELY CRACK WAS FOUND OUT OF LIMITS 2.750" IN REF ERA 519116-14MA, REV ORIGINAL THEREFORE SLAT PANEL NR 1 AT RT WING WAS REMOVED AND WILL BE INSTALLED AND ADJUSTED UNDER JIC CARD 2700-4224-RH-01, JOB 000-0011.

Part: FRAME — CORRODED (BS 1288) · corrosion level 2 · airframe 70,338 hrs · 54,173 cycles

SEVERAL CORROSION POINTS ON FRAME CLIPS BS 1288 FROM LONGERON 28L - 28R. FRAME CLIP AND SPLICES WERE REPLACED BY EXCESS COROOSION IAW SRM 53-03, FIG 3.

Part: WEB — CRACKED (BS 200) · airframe 70,338 hrs · 54,173 cycles

CRACK ON MEMBRANE BS 200, X=-22, Z=0 AT CEILING OF ELECTRONIC EQUIPMENT COMPARTMENT. MEMBRANE WAS REPAIRED IAW SRM 51-30-2, SRM 51-70-4, SRM 51-10-3 PAR 14, 21, SRM 51-30-8.

Part: SKIN — DAMAGED (RT AILERON TAB) · airframe 70,338 hrs · 54,173 cycles

EXPOSED COMPOUND MATERIAL ON RT AILERON ON TABS. REPAIRED IAW SRM 51-70-1D, PAR 3.

Part: SPACER — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 70,338 hrs · 54,173 cycles

SEVERAL CORROSION POINTS ON AFTER CARGO COMPARTMENT LOWER DOOR JAMB SPACER. SPACER WAS REPLACED IAW SRM 53-05, FIG 123, 51-30-5, 51-10-3 PAR 14, 21 AND 38.

Part: STRUCTURE — CRACKED (RADIO RACK) · airframe 70,338 hrs · 54,173 cycles

CRACKED RADIO RACK EXHAUST BS 256-275. RADIO RACK EXHAUST BS 256-275 WAS REPAIRED IAW ER/A 464964, 14 MAR, REV C.

Part: RIB — CRACKED (RT WING) · airframe 70,338 hrs · 54,173 cycles

CRACK ON RIB OF RT WING FIXED L/E STA XRS= 418 APPROXIMATELY RIB WAS REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-4, SRN 51-10-3, PAR14 AND 21.

Part: LANYARD — FRAYED (TAILCONE SLIDE) · airframe 69,216 hrs · 53,340 cycles

KEVLAR CABLE IN TAIL CONE FRAYED, RII: N ENTR 448527 W, R & R KEVLAR TAILCONE SLIDE DEPLOYMENT LANYARD IAW AMM REF 25-62-01.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 69,063 hrs · 53,229 cycles

CORROSION ON LT MAIN FUEL TANK ACCESS PLATE NR 1361C COUNTERSINK HOLES AND SETTLEMENT AREA. CORROSION ON COUNTERSINKS AND SETTLEMENT AREA WAS REMOVED, COUNTERSINKS WERE MEASURED AND MAXIMUM DIAMETER ALLOWABLE IS .532" AND WAS FOUND 3 COUNTERSINKS OUT OF LIMITS. MEASURE 0.558", 0.555", AND 0.560". THEREFORE ACCESS PLATE WILL BE REPAIRED, SETTLEMENT AREA WAS MEASURED, ORIGINAL THICKNESS IS 0.150" REMAINING THICKNESS IS 0.148". THEREFORE IT IS WITHIN LIMITS IAW SRM 51-22-2A, CONDITION II. HOLES AND COUNTERSINKS WERE REWORKED, AND MEASURED WITH 0.360", 3 EA AND COUNTERSINK 0.630" 3 EA. THEREFORE OUT OF LIMITS. REPAIR AND ACCESS PLATE WAS REPLACED IAW SRM 57-22-2A PAR 6, FIG 8. MEASURING STICK WAS REMOVED AND INSTALLED ON NEW ACCESS IAW AMM 28-40-02.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,063 hrs · 51,741 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTS AT ROWS 22-25 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACKS. OPS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 66,756 hrs · 51,502 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY EXIT SIGNS AT BOTH OF THE OVERWING HATCHES WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,692 hrs · 51,457 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE OVERWING EXIT LIGHTS WERE INOPERATIVE ON THE RT AND LT AT ROW 25. MAINTENANCE REPLACED THE BATTERIES FOR THE OVERWING EXIT LIGHTS AND THE LIGHTS BECAME OPERATIONAL.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 66,083 hrs · 51,028 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS IN ROWS 31-36 IN CABIN AND CATWALK IN TAIL, WERE INOPERATIVE. MAINTENANCE REPLACED THE FAILED FUSE AT THE POWER SUPPLY AND THE BULBS IN TAILCONE HANDLE. THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,531 hrs · 50,637 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY LIGHTING IN THE COCKPIT AND AT DOORS L1 & R1 INOPERATIVE. MAINTENANCE REPLACED THE BATTERY PACK AND OPS CHECKED GOOD.

Part: SLIDE — MISINSTALLED (TAILCONE) · airframe 65,502 hrs · 50,622 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE WAS IMPROPERLY INSTALLED. THIS CONFIGURATION OF THE SLIDE WOULD HAVE PREVENTED PROPER DEPLOYMENT OF THE ESCAPE SYSTEM AND IS NOT IN COMPLIANCE WITH 14 CFR, PART 121.703. THE TAILCONE SLIDE WAS REINSTALLED CORRECTLY AND THE RII WAS COMPLETED SATISFACTORILY.

Part: FITTING — WORN (TAILCONE RELEASE) · airframe 65,502 hrs · 50,622 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE EXTERNAL RELEASE HANDLE FITTINGS WERE WORN. FITTINGS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: CABLE — FRAYED (TAILCONE RELEASE) · airframe 65,502 hrs · 50,622 cycles

MAINTENANCE DISCOVERED THAT THE RT RELEASE LATCH CABLE FOR THE TAILCONE WAS FRAYED BEYOND ALLOWABLE LIMITS. CABLE REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS. THE FUNCTIONAL CHECK WAS COMPLETED SATISFACTORILY.

Part: CLAMP — OBSTRUCTED (TAILCONE LOCK) · airframe 65,502 hrs · 50,622 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE LOCKING CABLE CLAMP DOES NOT CLEAR THE CONDUIT BY .5. CLAMPS REPLACED AND THE CONDUIT ADJUSTED IAW MM.

Part: GROUND WIRE — LOOSE (EMERGENCY LIGHTS) · airframe 64,724 hrs · 50,070 cycles

DURING LINE CHECK, MX FOUND THAT THE CEILING MOUNTED EMERGENCY EXIT LIGHTS AT SEAT ROWS 16, 18, AND 20 WERE TOO DIM TO PROVIDE ESCAPE GUIDANCE. MX FOUND THE POWER SUPPLY GROUND TERMINAL LOOSE AND RE-SECURED IT. THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: CABIN PRESSURE — LOW · airframe 64,630 hrs · 49,991 cycles

FLIGHT CREW DIVERTED THE ACFT, FOLLOWING THE LOSS OF CONTROL OF CABIN PRESSURIZATION AT FL330. PASSENGER O2 MASKS DID NOT DEPLOY BUT ACFT WAS REQUIRED TO DESCEND TO 10,000 FT AND DECLARED AN EMERGENCY. MX FOUND BOTH PACKS SHUTTING OFF AT CRUISE POWER SO BOTH OF THE PRVS AND THE AC PILOT PRESSURE REGULATOR WERE REPLACED.

Part: CABLE — BROKEN (TAIL CONE) · airframe 63,738 hrs · 49,398 cycles

MX DISCOVERED THAT THE TAILCONE RETRACT CABLE WAS BROKEN AT THE TURN-BUCKLE. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,106 hrs · 48,950 cycles

DURING LINE CHECK, MX FOUND THAT THE OVERHEAD EMERGENCY PATHWAY LIGHTING IN THE COCKPIT AND AT DOORS L1 & R1 WERE INOPERATIVE. MX REPLACED THE BATTERIES. OPS CHECKED GOOD.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,885 hrs · 48,801 cycles

DURING LINE CHECK, MX FOUND THAT MULTIPLE OVERHEAD EMERGENCY PATHWAY LIGHTING WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER PACKS B5-100 & B5-102, AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY — FAILED (EMERGENCY LIGHTS) · airframe 62,837 hrs · 48,761 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN THE COCKPIT HAD FAILED. MX REPLACED THE BATTERIES. OPS CHECK WAS GOOD.

Part: POWER SUPPLY — MISWIRED (EMERGENCY LIGHTS) · airframe 62,242 hrs · 48,284 cycles

DURING LINE CHECK, MAINTENANCE FOUND THEY HAD NO CONTROL OF THE EMERGENCY PATHWAY LIGHTING IN THE CABIN, THEY WOULD COME ON WHEN ALL AIRCRAFT POWER WAS OFF. MAINTENANCE FOUND THE POWER SUPPLY (B5-104) IN THE CABIN CEILING TO BE MISWIRED. THE POWER SUPPLY WAS REWIRED AND IT RETURNED TO AN OPERATIONAL CONDITION.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 62,198 hrs · 48,250 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE OVERHEAD EMERGENCY ESCAPE LIGHTING IN THE FORWARD HALF OF THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY BATTERY POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: PLACARD — WRONG PART (LT OVERWING) · airframe 62,081 hrs · 48,170 cycles

MAINTENANCE FOUND THE LEFT FORWARD OVERWING EXIT IDENTIFIER ARROW TO BE POINTING THE WRONG WAY. ARROW ACTUALLY INDICATED AWAY FROM EXIT DOOR. PROPER EMERGENCY EXIT IDENTIFIER, WITH THE ARROW POINTING CORRECT DIRECTION WAS INSTALLED IN PLACE OF THE INCORRECT SIGN.

Part: SPAR — CRACKED (VERTICAL STAB) · airframe 62,233 hrs · 48,279 cycles

CRACK ON VERTICAL STAB FRONT SPAR RT CHORD ZFS-53. ACCOMPLISHED ERA 477465-14 REV B CODE 9-55-31 REPAIRED.

Part: FRAME — CORRODED (BS 1322 L27L-28R) · airframe 61,939 hrs · 48,063 cycles

UPON REMOVAL OF FORMERS FOUND FRAME BS 1322 BETWEEN L27L-28R HAS CORROSION 90 PERCENT LOSS OF MATERIAL. CUT OUT DAMAGED FRAME SECTION. FABRICATED AND INSTALLED NEW SECTION AT BS 1322 L25L- L29R IAW SRM 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 1322-1307) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO BAYSTA 1322-1307 RT LONGERON 28R INTERCOSTAL HAS CORROSION AT TOP FLANGE AT NUT PLATES, OUT OF LIMITS. REPLACED INTERCOSTAL AT BS 1322-1307 L28R PER SRM 51-30-2.

Part: FLOORBEAM — CORRODED (BS 1322) · airframe 61,939 hrs · 48,063 cycles

AFTER REMOVAL OF FLOORBEAM STRUCTURE AT AFT CARGO BS 1322 BETWEEN L23L-L23R. FOUND CORROSION ON TEE AT BS 1322. CORROSION ON TEE WAS OUT OF LIMITS. REPLACED TEE PER SRM 51-30-02.

Part: RUB STRIP — CORRODED (RT WING) · airframe 61,939 hrs · 48,063 cycles

ON REMOVAL OF RT WING UPPER FUEL ACCESS PANEL 1436C RUB STRIP FOUND CORRODED. COMPLIED ER/A 504287-14 REV ORIG.

Part: CUSP WEB — CRACKED (BS 218) · airframe 61,939 hrs · 48,063 cycles

AFTER REMOVAL OF MAIN CABIN SEAT TRACK AT RBL 54.5 BS 218-790 FOUND CUSP WEB CRACK AT STA 218 RBL 54.5 ON CUSP WEB. CUT OUT DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW SRM 53-05 FIG 131A-10.

Part: CUSP WEB — CORRODED (BS 389 RBL 54.5) · airframe 61,939 hrs · 48,063 cycles

FOUND CUSP WEB TORN AND CORRODED AT BS 389 RBL 54.5. REMOVED DAMAGE, FABRICATED AND INSTALLED FILLER AND DOUBLER IAW SRM 53-05 FIG 131A-23.

Part: SEAT TRACK — CORRODED (BS 218-790) · airframe 61,939 hrs · 48,063 cycles

AFTER REMOVAL OF MAIN CABIN SEAT TRACK AT RBL 54.5 STA218 TO 790 FOUND G2 GALLEY MOUNT AT 55.27 RBL STA 215.60 P/N3953059-501 FOUND CORROSION ON MOUNT. FOUND 100 PERCENT MATERIAL LOSS OUT OF LIMITS DRILLED NEW GALLEY MOUNT INSTALLED G2 GALLEY MOUNT, PN 3953059-501 ONTO SEAT TRACK IAW DC9 MD80 SRM 51-30-2 AT SAA SAT ON HMV4.

Part: PAN — CORRODED (SERVICE PANEL) · airframe 61,939 hrs · 48,063 cycles

AFTER CLEANING OF THE AFT LAVATORY SERVICE PANEL PAN, AFT SIDE, FOUND CORROSION AT ACCESSORY THROUGH HOLES, DRAIN VALVE CONTROL AND DRAIN TUBE, AND LT ANGLE SUPPORT. FOUND PANEL AND LT ANGLE CORROSION TO BE OUT OF LIMITS. REPLACED PANEL AND LT ANGLE PER SRM 51-30-2.

Part: SKIN — CORRODED (BS 440 L30) · airframe 61,939 hrs · 48,063 cycles

AFTER ANTENNA REMOVED FOUND SURFACE CORROSION ON EXTERIOR SKIN AT STA 440 L30. REMOVED ANTENNA RUB PLATE AND FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANTENNA RUB PLATE IAW SRM 51-30-2. SURFACE CORROSION FOUND IN LIMITS.

Part: BALANCE WEIGHT — CORRODED (RT ELEVATOR) · airframe 61,939 hrs · 48,063 cycles

RT ELEVATOR LEADING EDGE PANEL NR 1 BALANCE WEIGHT BRACKET AND HARDWARE CORRODED. REPLACED NR 1 RT ELEVATOR BALANCE WEIGHT AND HARDWARE IAW AMM 20-30-01-201.

Part: LONGERON — CRACKED (BS 1418 L2R) · airframe 61,939 hrs · 48,063 cycles

LONGERON 2R END FITTING CRACKED AT FRAME BS 1418. FABRICATED NEW LONGERON SECTION . INSTALLED NEW SECTION IAW SRM 51-30-05.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 61,939 hrs · 48,063 cycles

FUEL ACCESS PANEL 1307 WITH CORROSION ON THE EDGES, LOCATED ON THE UPPER LEFT WING, BETWEEN STA XRS 91 AND STA XRS 111.500. BLENDED CORROSION, BLEND EXCEEDS LIMITS. INSTALLED NEW PANEL DURING HMV.

Part: STEP — CORRODED (AIRSTAIR) · airframe 61,939 hrs · 48,063 cycles

VENTRAL STAIR 14TH STEP FROM BOTTOM HAS FRETTING WEAR, DENTS AND CORROSION. FOUND CORROSION TO BE OUT OF LIMITS. REMOVED AND REPLACED 14TH STEP PER SRM 51-10-3.

Part: RISER — CORRODED (AFT STAIRS) · airframe 61,939 hrs · 48,063 cycles

VENTRAL STAIR 14TH STEP FROM BOTTOM RISER HAS CORROSION. FOUND OUT OF LIMITS. REPLACED RT ANGLE IAW SRM 51-10-01.

Part: LONGERON — CORRODED (BS 1279-1338) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 29L HAS CORROSION FROM BS 1287-1338. CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LONGERON 29L IAW SRM 51-30-2.

Part: LONGERON — CORRODED (BS 1287-1322) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 27L HAS CORROSION FROM BS 1287-1322 INCLUDING END FITTING AT BS 1338, FOUND TO BE WITH-IN LIMITS. END FITTING OUT OF LIMITS. REPLACED FITTING L27L STA 1338 IAW SRM 51-30.

Part: FINGER DOUBLER — CORRODED (BS 1301-1330) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO L26L FINGER DOUBLER HAS CORROSION AT STA 1322-1330. REMOVED CORROSION AND FOUND IT TO BE OUT OF LIMITS, AFTER REMOVAL OF STRINGER END FITTING FOUND CORROSION AROUND FASTENER HOLES. REMOVED DAMAGED FINGER DOUBLER AND FABRICATED. INSTALLED NEW FINGER DOUBLER BETWEEN STA 1301-1330 L26L PER MD8 SRM 51-30-5. REF ER/A504265-14 REV1, REV4 FOR 5 EACH ELONGATED HOLES SEE NR224150AT SAA SAT HMV.

Part: ANGLE — CORRODED (BS 1007 L28L) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO BAY BS 1007 UNDER SEAT TRACK AND ABOVE L28L NUT PLATE AND STRUCTURES HAS CORROSION. REMOVED DAMAGED ANGLE. REPLACED ANGLE IAW MD88 SRM 51-30-5 AND 51-30-01.

Part: FRAME — CORRODED (BS 1322 L23L-28R) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO FRAME HAS CORROSION FROM L23L-L28R AT BS 1322. CORROSION OUT OF LIMITS. REPLACED FRAME BS 1322 L30-L23R IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 1219-1212) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LOWER BILGE GUSSETS HAVE CORROSION AT BS 1219, 1212 STR 29R. FOUND TO BE OUT OF LIMITS AT FASTENER HOLES ON FLANGE. INSTALLED NEW FLOOR SUPPORT IN AFT CARGO STA 1212 BETWEEN L28R-L28L IAW SRM 51-30-5 PG12 AT SAA SAT HMV4.

Part: SHEAR TIE — CORRODED (BS 1148) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO PIT LOWER BILGE SHEAR TIE HAS CORROSION ON FWD AND AFT SURFACES AT BS 1148 BTW L29L-L29R. FOUND TO BE OUT OF LIMITS REPLACED SHEAR TIE PER SRM 51-30-5.

Part: SKIN — CORRODED (BS 598) · airframe 61,939 hrs · 48,063 cycles

CORROSION ON CUTOUT SUPPORT EDGE EXTERNAL, AT THE RADIO ALTIMETER ANTENNA POS 1, BS 598 BETWEEN L30 AND 29L AT THE EXTERIOR LOWER FUSELAGE OF MID CARGO. DOUBLER SUPPORT FOUND TO BE OUT LIMITS. REPLACED DOUBLER RADIO ALTIMETER ANTENNA BS 598 IAW SRM 51-30-2 AND DWG 593600L1.

Part: LONGERON — CORRODED (BS 1287-1338) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 28L HAS CORROSION FROM BS 1287-1338 INCLUDING END FITTING AT BS 1338. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED LONGERON 28L FROM 1260-133 PER SRM 51-30-2.

Part: GUSSET — CORRODED (BS 1155 RBL 3) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LOWER BILGE GUSSET HAS CORROSION AT BS 1155 RBL 3. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED GUSSET, FABRICATED AND INSTALLED NEW GUSSET IAW SR, 51-30-5.

Part: LONGERON — CORRODED (BS 1294 L22L) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 22L HAS CORROSION FROM STA 1287-1322. REMOVED CORROSION AND FOUND BS 1294 AND L22L END FITTING TO BE OUT OF LIMITS. FABRICATED AND INSTALLED TWO NEW SECTIONS FROM STA 1279-1335 PER SRM 51-30-5.

Part: CARGO TRACK — CORRODED (BS 1222-1322) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO TRACK HAS CORROSION BETWEEN L27L AND L28L FROM BS 1222-1322. FOUND OUT OF LIMITS. REMOVED AND REPLACED CARGO TRACK PER SRM 51-30-1 AND 51-30-5.

Part: LONGERON — CORRODED (BS 1277-1326) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 25L HAS CORROSION FROM BS 1277-1326 INCLUDING BOTH SIDES OF DRAIN HOLES. CORROSION IS OUT OF LIMITS. REPLACED LONGERON SECTION FROM BS 1277-1326 PER MD-88 SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CORRODED (BS 1212-1219) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LOWER BILGE INTERCOSTAL HAS CORROSION FROM STA 1212-1219 RBL3. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW INTERCOSTAL REF MD-88 SRM 51-30-02 AT SAA SAT HMV.

Part: LONGERON SPLICE — CORRODED (BS 1287-1297) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO LONGERON 30 HAS CORROSION FROM BS 1287-1297 INCLUDING END SPLICE. FOUND END SPLICE TO BE OUT OF LIMITS. REMOVED AND REPLACED END SPLICE PER SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS BS 1212) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO BAY FLOOR SUPPORT ANGLE HAS CORROSION AT BS 1212 RBL8. REMOVED FLOOR SUPPORT FROM FS 1136-1212 RBL 8. FABRICATED AND INSTALLED FLOOR SUPPORT FS 1136-1212 IAW SRM 51-30-5 PG 12.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 61,939 hrs · 48,063 cycles

FUEL ACCESS PANEL 1307 WITH CORROSION ON THE EDGES, LOCATED UPPER LT WING BETWEEN STA XRS91 AND XRS111.500. ACCESS PANEL REPLACED PER ER/A 420431-14 MA.

Part: FITTING — CORRODED (BS 1154) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO PIT DOOR FUSELAGE CUTOUT FWD JAMB LOWER CORNER FITTING HAS CORROSION AT BS 1154. REMOVED AND REPLACED FITTING PER SRM 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1193-1297) · airframe 61,939 hrs · 48,063 cycles

CORROSION ON MAIN SEAT TRACK X22 BS 1297-1193. FOUND TO BE OUT OF LIMITS. REPLACEMENT OF SEAT TRACK FROM BS 1183-1309 X22 ACCOMPLISHED ON OPN 0101 CARD E 127.

Part: SEAT TRACK — CORRODED (BS 200-237) · airframe 61,939 hrs · 48,063 cycles

SEAT TRACK HAS CORROSION AND GOUGES BETWEEN BS 200-237 RBL44. CORROSION OUT OF LIMITS AT STA 231-232. REPLACED SEAT TRACK STA 200-265 IAW SRM 51-30-1 AND 51-30-5.

Part: SEAT TRACK — CORRODED (BS 1060-1271) · airframe 61,939 hrs · 48,063 cycles

CORROSION AND CHAFING MARKS ON MAIN CABIN SEAT TRACK BS 1060-1271 RBL 22. REMOVED CORROSION. FABRICATED NEW SEAT TRACK, SPLICE AND INSTALLED AT BS 1031-1309 RBL22 IAW SRM FIG 4F, 51-10-01, 51-10-02.

Part: SEAT TRACK — CORRODED (BS 229) · airframe 61,939 hrs · 48,063 cycles

SEAT TRACK WITH CORROSION AND GOUGES LBL22 BS 229 AT THE LEFT CABIN FLOOR AREA. REMOVED DAMAGE AND REPLACED SEAT TRACK FROM BS 209-257 IAW SRM 53-05 FIG 4F.

Part: LONGERON — CRACKED (BS 465 L4R) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN LONGERON CRACKED AT BS 465 L4R. REMOVED DAMAGE. FABRICATED AND INSTALLED NEW LONGERON SECTION FROM BS 437-474 IAW SRM 51-30-02 AND 53-02 FIG 18.

Part: FLOORBEAM — CORRODED (BS 1174) · airframe 61,939 hrs · 48,063 cycles

LIGHT CORROSION ON MAIN CABIN FLOORBEAM BS 1174 BETWEEN STA BL 0 - RBL 22. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW ANGLE IAW SRM 51-30-5 PG12.

Part: CUSP WEB — CORRODED (BS 502-589) · airframe 61,939 hrs · 48,063 cycles

RT CUSP WEB FROM BS 502-589 CORRODED. REPLACED CUSP WEB RT IAW SRM 51-30-1, 51-30-5 AT SAA SAT HMV4.

Part: FLOORBEAM — CORRODED (BS 1174) · airframe 61,939 hrs · 48,063 cycles

LIGHT CORROSION ON MAIN CABIN FLOORBEAM BS 1174 BETWEEN STA RBL 0-22. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED IAW MD88 SRM 51-30-5 PG12.

Part: SEAT TRACK — CORRODED (BS 1297) · airframe 61,939 hrs · 48,063 cycles

CORROSION ON MAIN CABIN SEAT TRACK LBL 54 BS 1297. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS. REPLACED TRACK SECTION FROM BS 1170-1309 WITH NEW TRACK IAW SRM 51-30-01.

Part: SEAT TRACK — CORRODED (BS 229) · airframe 61,939 hrs · 48,063 cycles

SEAT TRACK WITH CORROSION AND GOUGES, LBL44 BS 229 AT THE LEFT CABIN FLOOR AREA. REMOVED AND FABRICATED REPAIR TRACK AT BS 210-312 LBL44. INSTALLED REPAIR IAW MD80 SRM 53-05 FIG 4F AND 51-60-0, AT SAA SAT HMV4.

Part: CUSP WEB — CORRODED (BS 589-712) · airframe 61,939 hrs · 48,063 cycles

RT CUSP WEB FROM BS 589-712 CORRODED. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-30-1 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 200-209) · airframe 61,939 hrs · 48,063 cycles

RT CUSP WEB CORRODED BETWEEN BS 200-209 RBL 50. FOUND OUT OF LIMITS. REPLACED CUSP WEB IAW SRM 51-30-2.

Part: SEAT TRACK — CORRODED (BS 200-655) · airframe 61,939 hrs · 48,063 cycles

SEAT TRACK HAS CORROSION BETWEEN BS 200-655 RBL 22. FOUND OUT OF LIMITS AT SEVERAL STATIONS. REPLACED SEAT TRACK FROM BS 436-798 RBL 22 IAW SRM 51-30-1 AND 51-30-2.

Part: CUSP WEB — CORRODED (BS 1212-1231) · airframe 61,939 hrs · 48,063 cycles

RT CABIN FLOOR CUSP WEB IS CORRODED AT UPPER SURFACE BETWEEN BS 1212-1231. FOUND 1212 AREA TO BE OUT OF LIMITS. CUT OUT DAMAGE AREA BS 1212. FABRICATED REPAIR DOUBLE AND SHIM AND INSTALLED AT BS 1212 IAW SRM 53-05 FIG 131A-10.

Part: CUSP WEB — CORRODED (BS 598-610) · airframe 61,939 hrs · 48,063 cycles

CUSP WEB WITH CORROSION ON UPPER SURFACE BETWEEN STA 598-617 LBL 56 AT THE LEFT CABIN FLOOR AREA. OUT OF LIMITS. CUT OUT CORROSION AND INSTALLED REPAIR PER SRM 53-05.

Part: SEAT TRACK — CORRODED (BS 218-408) · airframe 61,939 hrs · 48,063 cycles

CORROSION AND GOUGES AT RT SEAT TRACK BS 218-408 RBL 54. FABRICATED AND INSTALLED SEAT TRACK, STRAP, SPLICE IAW SRM 51-30-01.

Part: LONGERON — CRACKED (BS 1287 L12L) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN LONGERON 12L IS CRACKED AT BS 1287. REMOVED DAMAGE. FABRICATED AND INSTALLED NEW END IAW SRM 53-02 FIG 18.

Part: FRAME — CRACKED (BS 1174) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN FUSELAGE FRAME IS CRACKED BS 1174 BETWEEN LONGERON 7L AND 5L. REMOVED DAMAGE. FABRICATED REPAIR ANGLE, FILLER, PLATE AND INSTALLED IAW MD88 SRM 53-03 PG28.

Part: CUSP WEB — CORRODED (BS 1212-1231) · airframe 61,939 hrs · 48,063 cycles

RT CABIN CUSP WEB IS CORRODED AT UPPER SURFACE BETWEEN BS 1212 AND 1231. FOUND BS 1212 OUT OF LIMITS. FABRICATED AND INSTALLED REPAIR DOUBLER IAW SRM 53-05.

Part: SKIN — CORRODED (BS 674-693) · airframe 61,939 hrs · 48,063 cycles

CORROSION ON SKIN PANEL BS 674-693 FROM L29R-28R INTERNAL SURFACE. FOUND MORE CORROSION IN AREA. REMOVED DAMAGE AND FABRICATED AND INSTALLED NEW SKIN, FINGER DOUBLERS, EXTERNAL SKIN DOUBLER, AT BS 588-759 PER MD88 SRM 51-30-5. INSTALLED INTERNAL DOUBLER ON NRC 220071.

Part: LONGERON — CRACKED (BS 541) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN LONGERON 4R CRACKED BS 541. REMOVED DAMAGE, FABRICATED AND INSTALLED NEW SECTION FROM 513-550 IAW SRM 51-30-2.

Part: FLOOR SUPPORT — CORRODED (BS 180 LBL10) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN AT BS 180 LBL 10 CORROSION ON FLOOR SUPPORT ANGLE. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW FLOOR SUPPORT ANGLE STA 180 LBL10 IAW SRM 51-30-2 PG 28 FIG20.

Part: CUSP WEB — CORRODED (BS 905-927) · airframe 61,939 hrs · 48,063 cycles

MAIN CABIN FOUND CORROSION ON CUSP WEB STA 905-927 LT. FABRICATED AND INSTALLED NEW CUSP WEB IAW SRM 51-30-05, 51-30-01, 51-30-02.

Part: PAN — CORRODED (CARGO DOOR) · airframe 61,939 hrs · 48,063 cycles

FWD CARGO DOOR LOWER PANEL, AFT SIDE BETWEEN BS 370-389 AND 408-427 . DOOR PAN AND ANGLE CORROSION OUT OF LIMITS. REMOVED AND REPLACED DOOR PAN AND ANGLES PER SRM 51-30-2.

Part: SUPPORT — CORRODED (BS 825) · airframe 61,939 hrs · 48,063 cycles

RT LWR WING TO BODY FAIRING SUPPORT FORMER HAS CORROSION AT STA 825 RBL 9-RBL 52 ON LWR FLANGE UPPER AND LOWER SURFACES. CLIP NUT HOLE IN LOWER FLANGE UPPER SURFACE AT BS 825 RBL 15 IS CORRODED BEYOND LIMITS. REMOVED AND REPLACED WTB FAIRING FORMER PER SRM 51-30-5.

Part: DOOR FRAME — CORRODED (BS 1154-1211) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO DOOR FRAME LOWER BTW BS 1154 -1211 IS CORRODED AROUND FASTENER HOLES. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW AFT CARGO DOOR LOWER FRAME BETWEEN BS 1154-1211 IAW MD-88 SRM 51-30-5 PG12.

Part: THRESHOLD — CORRODED (AFT CARGO BAY) · airframe 61,939 hrs · 48,063 cycles

AFT CARGO INTERNAL THRESHOLD SCUFF PLATE IS CORRODED. FOUND OUT OF LIMITS. FABRICATED NEW THRESHOLD IAW SRM 51-10-4.

Part: SKIN — DENTED (FUSELAGE) · airframe 61,939 hrs · 48,063 cycles

RT FUSELAGE EXTERNAL SKIN HAS A REPAIR AND DENT UNIDENTIFIED STA 44 4 O`CLOCK POSITION. ACCOMPLISHED REPAIR WITH ERA 503030-14 REV ORIG AT SAA SAT HMV.

Part: SKIN — CRACKED (BS 1380) · airframe 61,939 hrs · 48,063 cycles

RT FUSELAGE EXTERNAL SKIN HAS A CRACK AT THE FASTENER HOLE STA 1380 L14R. CUT OUT DAMAGE. COMPLIED WITH ER/A 503722-14 REV O.

Part: CONTAINER — LEAKING (GALLEY) · airframe 60,211 hrs · 46,868 cycles

ON FINAL APPROACH, FORWARD GALLEY FLUORESCENT LIGHT STARTED SMOKING. FLIGHT CREW PULLED BREAKER AND TURNED OFF GALLEY POWER NUMBER 207. MAINTENANCE FOUND ICE BUCKET LEAKING / SWEATING IN A COMPARTMENT ABOVE WORK LIGHT MCO/PLACARD INSTALLED PER MEL 33 -00-02.

Part: WIRE — DAMAGED (AC BAY) · airframe 59,506 hrs · 46,371 cycles

DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATHWAY SIDEWALL LIGHTS LOCATED IN THE TAIL SECTION INOPERATIVE. MAINTENANCE REPAIRED DAMAGED WIRE PER MAINTENANCE MANUAL. OPERATION CHECKS GOOD.

Part: SPAR CAP — DAMAGED (HORIZ STAB) · airframe 58,273 hrs · 45,637 cycles

HORIZONTAL STABILIZER REAR SPAR UPPER CAP REPAIR IAW 09-460214-12.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 58,073 hrs · 45,505 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATH LIGHT AT SEAT 21DE INOPERATIVE. MX RE-TERMINATED BROKEN WIRE. OPERATION OF LIGHT NOW CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 57,353 hrs · 45,021 cycles

INSP MAINTENANCE FOUND THE FIRST SEVEN ROWS OF THE EMERGENCY LIGHTS TO BE INOPERATIVE. MAINTENANCE REPLACED THE FORWARD BATTERY PACK. AN OPS CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 57,283 hrs · 44,976 cycles

MX FOUND THE L1 AND COCKPIT EMERGENCY LIGHTS TO BE INOPERATIVE. MX REPLACED THE POWER SUPPLY BATTERIES. THE SYS CHECKED NORMALLY AND THE ACFT WAS RETURNED TO SERVICE. (2010-D0744) (DLM88101672)

Part: STRIP — CORRODED (BS 1136-1174) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON 26MAY10, THE AFT CARGO HAD A NUT PLATE STRIP AT STA 1136-1174 INBD OF L-28R THAT WAS CORRODED BEYOND SRM LIMITS. REPLACED NUTPLATE STRIP IAW SRM 53-01. (DLM88101645)

Part: LONGERON — CORRODED (L28R) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

THE C2 CARGO DOOR SILL LWR LONGERON WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REPLACED LONGERON IAW ER/A 09-482741-14MA REV ORIG. (LONGERON 28R) (DLM88101648)

Part: STRIP — CORRODED (BS 1155-1163) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON 26MAY10, AN AFT CARGO NUTPLATE STRIP WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. LOCATED AT STA 1155-1163, INBD OF L-28R. FABRICATED AND INSTALLED NEW STRIP IAW SRM 53-01 (DLM88101642)

Part: STRIP — CORRODED (BS 1174-1183) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON 26MAY10, THE AFT CARGO HAD A NUTPLATE STRIP AT STA 1174-1183 INBD OF L-28R THAT WAS CORRODED BEYOND SRM LIMITS. REPLACED NUTPLATE STRIP IAW SRM 53-01.

Part: ANGLE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON 26MAY10, THE AFT CARGO DOOR SILL HAD A CORRODED AFT ANGLE THAT WAS BEYOND SRM LIMITS. REPLACED ANGLE IAW SRM 53-01.

Part: FLOOR SUPPORT — CORRODED (BS 1155 L29R) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON26MAY10, AN AFT CARGO FLOOR SUPPORT AT STA 1155 OTBD OF L-29R WAS FOUND TO BE CORRODED BEYOND SRM LIMITS. REPLACED FLOOR SUPPORT IAW ER/A 09-482741-14MA REV ORIG. (DLM88101641)

Part: STRIP — CORRODED (BS 1193-1203) · corrosion level 2 · airframe 57,222 hrs · 44,939 cycles

ON 26MAY10, THE AFT CARGO HAD A NUTPLATE STRIP AT STA 1193-1203 INBD OF L-28R THAT WAS CORRODED BEYOND SRM LIMITS. FABED AND INSTALLED NUTPLATE STRIP IAW SRM 53-01.

Part: STRUCTURE — CRACKED (VERTICAL STAB) · airframe 55,787 hrs · 44,001 cycles

ACCOMPLISHMENT OF EA 09-470871-12, REV A. OPN 0101 HFEA SHOWS 2ND, 3RD AND 6TH HOLES LT SIDE WITH CRACK INDICATIONS. 2ND AND 3RD HOLES RECHECK OK AFTER REMOVAL OF NUTPLATE GANG CHANNEL. 6TH HOLE REPAIRED IAW ER/A 477465-14 REV 0.

Part: LINE — LEAKING (HYD SYSTEM) · airframe 53,005 hrs · 42,197 cycles

LT ENG HYD FLUID DEPLETED IN FLT, LT ENG HYD PUMP PRESS LINE LEAK IN TAIL OF A/C. REPLACED ENG DRIVEN PUMP AND INSTALLED TEMP FLEX LINE PER M/M.

Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHT) · airframe 52,185 hrs · 41,642 cycles

DURING L1 LETTER CHECK REF NR 99, FOUND FWD EMERGENCY FLOOR LIGHTS BATTERY PACK NOT CONNECTED TO EEPLS. FOUND ALL SEAT HARNESS CONNECTED END TO END FROM THE AFT BATTERY PACK ONLY. REWIRED PER WDM 33-51-14

Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,553 hrs · 38,648 cycles

EMERGENCY PATH LIGHT INOP AT SEAT 2R. REPLACED LIGHT ASSY.

Part: SKIN — DENTED (FS 427-446 L19L) · airframe 47,409 hrs · 38,543 cycles

THE FUSELAGE SKIN FROM FS 269-275 AT L29R TO L30 IS DENTED. THE DAMAGED SKIN WAS REMOVED AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — DENTED (BS 522 S19R) · airframe 47,409 hrs · 38,543 cycles

FOUND FUSELAGE SKIN HAS A DENT AT FS 522.541 BETWEEN S-19R AND S-20R. CUTOUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER.

Part: SKIN — GOUGED (FS 427-446 L19L) · airframe 47,409 hrs · 38,543 cycles

THE FUSELAGE SKIN HAS DAMAGE THAT WAS BLENDED BEYOND SRM ALLOWABLES AT FS 427 - 446 BETWEEN L19L AND L23L. THE DAMAGED SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: SKIN — CRACKED (FUSELAGE) · airframe 47,409 hrs · 38,543 cycles

THE FUSELAGE SKIN WAS DENTED AND CRACKED. THE DAMAGED SKIN WAS CUT OUT AND A DOUBLER WAS INSTALLED REF AD 98-17-06.

Part: FITTING — CORRODED (RT SIDE) · airframe 47,409 hrs · 38,543 cycles

RIGHT MLG RETRACT ACTUATOR SUPPORT FITTING BORE DIAMETERS ARE CORRODED. THE CORROSION WAS REMOVED AND OVERSIZED BUSHINGS WERE INSTALLED. REF AD 2004-25-14, 9-093855-03AD, DC9-57-222.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,818 hrs · 38,104 cycles

TAIL COMPARTMENT OVERHEAD EMERGENCY LIGHTS INOP. REPLACED B5-28 POWER SUPPLY BATTERIES, CHECKS GOOD.

Part: ACM — FAILED (LEFT) · airframe 46,261 hrs · 37,697 cycles

ODOR IN FLIGHT COMPARTMENT DURING CLIMB - REPLACED LEFT AIR CYCLE MACHINE

Part: SLIDE — DEPLOYED (TAILCONE) · airframe 45,488 hrs · 37,124 cycles

TAIL CONE WAS ACCIDENTALLY DEPLOYED AT THE GATE, SLIDE DID NOT DEPLOY. REPLACED DEPLOYMENT LANYARD AND REINSTALLED TAIL CONE.

Part: STRINGER — CRACKED (FUSELAGE) · airframe 44,276 hrs · 36,235 cycles

CRACKED STRINGER 2 LT IN STA 160 AEROMEXICO NRC T0024065 CRACKED STRINGER 3 LT IN STA 160 AEROMEXICO NRC TOO24064 CRACKED STRINGER 4 LT IN STA 160 AEROMEXICO NRC T0024063 ABOVE STRINGERS REPAIRED IAW SRM 53-02 FIG 18.

Part: BULKHEAD — CRACKED (FUSLAGE) · airframe 44,276 hrs · 36,235 cycles

CRACKED WEB IN FWD FACE OF AFT P-DOME AT X=0. REPLACED WEB IN UPPER FWD EDGE OF AFT P-DOME AT X=0.

Part: BEAM — CRACKED (R1 DOOR) · airframe 44,276 hrs · 36,235 cycles

CRACKED CLIP IN FWD EDGE OF NR 1 BEAM OF R1 DOOR. CRACKED FWD EDGE OF NR 4 BEAM OF R1 DOOR AEROMEXICO NRCS T0024037,T0024036. REPLACED R1 DOOR BEAM NR 4 AND CLIP ON BEAM NR 1.

Part: BATTERY — SMOKE (E AND E) · airframe 42,919 hrs · 35,282 cycles

FOUND BY ACS, SMOKE COMING OUT OF BATTERY VENT LINE BEHIND NOSE GEAR. REPLACED BATTERIES, CHARGER, AND CABLES.

Part: CONTROL CABLE — LOOSE (MLG) · airframe 42,843 hrs · 35,230 cycles

ON TAKEOFF GEAR WOULD NOT RETRACT. FOUND RETRACT CABLES 118A AND 118B LOOSE. RIGGED SYSTEM, CHECKS GOOD.

Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 40,899 hrs · 33,921 cycles

TOOL DAMAGE (DRILL MARKS) WERE FOUND ON AFT PRESSURE BULKHEAD LOWER CAP NEAR SKIN DRAIN HOLES. REPAIRED BY BLENDING 0.007 INCH DEPTH LHS AND 0.009 INCH DEPTH RHS PER FAA DER APPROVED REPAIR INSTRUCTIONS.

Part: PANEL — MISSING (FWD SERVICE DOOR) · airframe 40,388 hrs · 33,565 cycles

ON ARRIVAL FOUND FORWARD AIR CONDITIONING PANEL MISSING - PANEL HAD COME OFF DURING FLIGHT SUSPECT RAMP PERSONNEL FAILED TO LATCH PANEL SECURE AT DOWNLINE STATION - REPLACED SAME

Part: PUMP — FAILED (RT ENGINE) · airframe 39,406 hrs · 32,833 cycles

LOST RT HYD PRESS IN FLT, QTY NORMAL. EMERGENCY GEAR EXTENTION ACCOMPLISHED. LOST LT PRESSURE WHEN FLAP / SLATS EXTENDED. REPLACED RT ENGINE DRIVEN HYDRAULIC PUMP.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 38,710 hrs · 32,322 cycles

RED EMERGENCY EXIT LIGHTS INOP AT ROW 24 DE (EXIT ROW). FOUND WIRE HARNESS UNPLUGGED UNDER SEAT. LIGHTS OP NORMAL AFTER PLUG RECONNECTED.

Part: HYDRAULIC LINE — LOOSE (THRUST REVERSER) · airframe 37,925 hrs · 31,700 cycles

THERE WAS A SLOW LOSS OF HYDRAULIC FLUID OF THE LEFT SYSTEM QUANTITY EN ROUTE. LEFT HYDRAULIC SYSTEM QUANTITY SHOWED 3 QUARTS ON LANDING AND TAXI IN. TIGHTENED PRESSURE LINE FOR LT THRUST REVERSER AT CONTROL VALVE.

Part: LINE — LOOSE (HYD SYSTEM) · airframe 36,088 hrs · 30,339 cycles

LEFT HYD QTY DECREASED TO 3 QTS CLIMBING THRU 17K. TURNED OFF LEFT ENG HYD PUMP AND QTY INCREASED TO 15 QTS. ON FINAL W/ LEFT ENG PUMP AND XFER PUMP ON LEFT HYD QTY AND PRESS WENT TO 0. MTC NOTED EMPTY RESERVOIR. FOUND T/R CNTRL VLV LINE LEAKING. SECURED SAME. LEAK CHECK OK.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 35,846 hrs · 30,155 cycles

AT FL 370 WITH ENGINE ANTI-ICE SELECTED THE MASTER CAUTION LITE ILLUMINATED FOLLOWED BY THE RIGHT ENGINE OIL STRAINER CLOG LITE. ACCOMPLISHED POM PROCEDURES AND AFTER THROTLE WAS RETARDED THE LITE REMAINED ILLUMINATED CONTINUOUSLY. ENGINE WAS SHUTDOWN IAW POM. REPLACED ENGINE OIL STRAINER

Part: UPLOCK SWITCH — FAILED (AFT AIRSTAIR DR) · airframe 35,541 hrs · 29,909 cycles

AIR TURNBACK, AFT AIRSTAIR DOOR ILLUMINATED DURING CLIMBOUT. VERIFIED DOOR CLOSED AND FWD TO MCO. REPLACED UPLOCK SWITCHES S1-276 AND S1-277, LIGHT CHKS GOOD.

Part: A/C PACK — SMOKE (LEFT) · airframe 35,377 hrs · 29,796 cycles

SMOKE IN CABIN WHEN LEFT PACK A/C SWITCH TURNED ON. LEFT COCKPIT TEMP WENT FULL HOT, TURNED SWITCH OFF, SMOKE SUBSIDED. PERFORMED DUCT BURNOUT.

Part: GCU — FAILED (NR 2 ENGINE) · airframe 34,550 hrs · 29,183 cycles

RIGHT GENERATOR OFF MESSAGE (NO VOLTS AND FREQS). REPLACED RIGHT GENERATOR CONTROL UNIT.

Part: PROXIMITY SWITCH — DIRTY (RIGHT) · airframe 34,098 hrs · 28,835 cycles

RT MAIN GEAR LIGHT REMAINED RED AFTER GEAR RETRACTION. AFTER ABOUT 2 MINUTES IT WENT OUT. CLEANED PROX SENSOR AND TARGET. LUBED SENSOR LEVER ASSY. VERIFIED GAP. VERIFIED OPERATION WITH PSEU MONITOR.

Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 33,952 hrs · 28,732 cycles

FORWARD LOWER EMERGENCY FLASHLIGHT INOP. REPLACED LOWER FORWARD EMERGENCY FLASHLIGHT.

Part: LINE — LOOSE (HYDRAULIC SYS) · airframe 33,897 hrs · 28,683 cycles

IN FLIGHT, RT ENG HYDRAULIC QTY WENT TO 1 QT WITH AMBER LIGHT, HAD NORMAL PRESS INDICATION. LATER LOST HYDRAULIC PRESSURE AND QTY. FOUND HYDRAULIC RETURN LINE IN 48 SECTION WITH NUT LOOSE. REMOVED LINE, REPOSITIONED ANTI ROTATION BLOCK AND RE-INSTALLED LINE ON UNION. LEAK CHECK GOOD.

Part: LINE — LOOSE (HYD PRESSURE) · airframe 33,574 hrs · 28,429 cycles

RIGHT HYD SYS QTY DECREASED TO 4 QTS. RT HYD SYS TURNED OFF. SECURED LOOSE HYD PRESS LINE IN RIGHT SIDE OF TAIL COMPARTMENT.

Part: CYLINDER — BROKEN (NLG STEERING) · airframe 33,081 hrs · 28,072 cycles

ON APPROACH DURING LANDING GEAR EXTENSION A LOUD POPPING NOISE WAS HEARD FROM THE NLG AREA. NLG STEERING WORKED ON LANDING ROLLOUT THEN QUIT WHEN THE RUNWAY WAS CLEARED. STEERING FROZEN IN BOTH DIRECTIONS. FOUND THE RIGHT STEERING CYLINDER AFT MOUNT ATTACH LUG BROKEN REF IPC 32-52-02-2. REMOVED AND REPLACED RIGHT STEERING CYLINDER HYDRAULIC LINES TO CYLINDER AND I/B SWIVEL ASSY.

Part: ROD — BROKEN (NLG STEERING) · airframe 33,081 hrs · 28,072 cycles

NOSE WHEEL STEERING INOP IN EITHER DIRECTION. GOOD HYD PRESS ON BOTH SIDES. A COUPLE LOUD POPS WERE HEARD FROM NOSE GEAR AREA DURING GEAR EXTENSION. NOSE WHEEL STEERING WORKED ON LANDING ROLLOUT THEN QUIT CLEARING RUNWAY. ACTUATOR ROD BROKEN. REPLACED SAME.

Part: POWER SUPPLY — INOP (ROW 1-4&10-12)

FOUND EMERGENCY LIGHTS AT DOORS 1L, 2L AND SEATROWS 1, 2, 3, 4, 10, 11 AND 12 INOP. FOUND WIRES AT SEATROW 11 BROKEN AND REPAIRED SAME, NO HELP. REPLACED POWER SUPPLY B5-211, LIGHTS TEST NORMAL P/N 337701962, S/N 5122.

Part: BATTERY — DISCHARGED (GALLEY)

AFT GALLEY FLASHLIGHT INDICATOR WOULD NOT BLINK AND HAD BROKEN STRAP. REPLACED FLASHLIGHT AND BATTERY ASSY, LIGHT TESTS OK.

Part: FILTER — DIRTY (NR 2 ENGINE)

FIFTY MILES EAST OF JAN, THE RT OIL FILTER CLOG MSG ILLUM. CREW FOLLOWED POM AND THE MSG DID NOT EXTINGUISH. THE CREW SHUT DOWN THE ENGINE AND DIVERTED TO JAN. JAN MTC REMOVED THE OIL FILTER AND FOUND FULL OF CARBON. MTC REPLACED THE FILTER AND PERFORMED AN ENG RUN AND HAD NO LEAKS AND THE CLOG MSG DID NOT RETURN.

Part: DUCT — FAILED (RT ACM)

ATB - AT FL240, AUTO PRESS INOP, BLUE LIGHT CAME ON. PRESSURE CONTINUED TO CLIMB AT 700 FT/MIN PASSING 5500 CN PRESSURE. INITIATED DESCENT TO 10000. AIRBORNE RETURN TO DFW. FOUND BLOWN DUCT ON RT ACM. REPLACED DUCT. CHECKS NORMAL.

Part: ACM — OVERSERVICED (AFT FUSELAGE)

PASSING 31,000 FEET IN CLIMB, FLIGHT ATTENDANT REPORTED LIGHT SMOKE IN AFT PASSENGER COMPARTMENT AND SMOKE DETECTORS IN AFT LAV WERE ON. BEGAN DESCENT AND SMOKE DISSIPATED AND CLEARED CABIN FOR DURATION OF FLIGHT. FOUND RT ACM OVERSERVICED. SERVICED TO PROPER LEVEL AND PERFORMED DUCT BURNOUT AND WATER SEPARATOR BAG REPLACEMENT PER M/M. NO FURTHER SMELLS OR SMOKE.

Part: STARTER — FAILED (NR 2 ENGINE)

ON ENG START NR 2 ENG STARTER FAILED. PIECES DAMAGED THE CSD WIRE HARNESS AND PUNCTURED A 3 X 1 HOLE IN THE FWD LOWER COWLING. REPLACED STARTER AND TEMP REPAIRED COWLING.

Part: SWITCH — FAILED (COCKPIT)

JUST AFTER IGN OVER-RIDE WAS SELECTED ARCING OCCURRED IN AREA OF IGN SWITCH. COCKPIT HAD SMOKE. DIVERTED TO LIT. CONTRACT MTC REPORTS IGN C/BERS ARE TRIPPED AND IGN SW TERMINALS ARE BURNT ALONG WITH 2 FUEL HETA SWITCHES AND THE DC STREAT PUMP SW ALL DAMAGED WHEN WIRING TOUCHED SWITCHES. REPLACED AFFECTED SWITCHES AND REPAIRED WIRING AS NECESSARY.

Part: TIRE — FAILED (RT MLG)

RIGHT INBOARD TIRE BLEW ON TAKEOFF. REPLACED WHEEL ASSY. REPAIRED PROX SWITCH, SWUNG GEAR.

Part: PROX CONTL BOX — INOPERATIVE (RT MLG)

AFTER T/O, RT MAIN GEAR RED UNSAFE LIGHT STAYED ON FOR APPROX 1 MINUTE AFTER OTHER GEAR LIGHTS WENT OUT. REPLACED PROX BOX, SWUNG GEAR SEVERAL TIMES.

Part: TRACK — INOPERATIVE (CABIN)

EMERGENCY TRACK LIGHTING INOPERATIVE AT FWD CABIN DOOR. REPLACED SECTION OF TRACK WIRING.

Part: HYD LINE — CRACKED (TAIL COMPT)

AFTER T/O DURING SLAT RETRACT GOT MASTER CAUTION LIGHT AND RT HYDRAULIC PRESS LOW ON OAP. RT PRESS WAS -0- AND QTY WAS 1 QT. RAN CK LIST AND AFTER FLAP SLATS EXT TO 15 DEGR QTY WAS 3 QTS. AFTER LDG AND FLAPS SLATS WERE RETRACT QTY WENT UP TO 6 QTS. FOUND CRACKED RIGID LINE AT RT ENG FILTER MODULE TO RT ENG PUMP. REPLACED LINE.

Part: SPOILER LIGHT — ILLUMINATED (COCKPIT)

SPOILER DEPLOYED, MESSAGE ILLUMINATED ON OAP. MSG ON WITH HANDLE ARMED. ALL SPOILERS DOWN FWD TO MCO AND PLAC PER MEL 27-00-32. NO MRR, REJECTED 12-28-95 GT 595.

Part: ENGINE — LEAKING OIL (NR 2)

ON TAKEOFF BETWEEN 2,000 AND 14,000 FT, MILD SMOKE ODOR IN CABIN. ALL FDW AND AFT LAV SMOKE DETECTOR ACTIVATED. FOUND OIL IN 8TH STAGE SADDLE DUCT. FERRY A/C TO ATL AND REPLACED ENG.

Part: HYD FITTING — LOOSE (TAIL COMP)

SMOKE IN CABIN JUST AFTER T/O. REPLACED COALESCER BAGS, INSP BOTH MAIN WHEEL WELLS. HYDRAULIC FLUID OVERFLOW BOTTLES EMPTY AND FOUND RT HYD SYSTEM FILTER LEAKING. SECURED FITTING, LEAK CHECK GOOD. CLEANED LOWER FUSELAGE, RAN ENGINES AND PACKS, NO SMOKE NOTED, RETURNED TO SERVICE.

Part: HOSE — BROKEN (RT HYD SYST)

AFTER TAKEOFF ON CLIMBOUT, RIGHT HYDRAULIC SYSTEM PRESSURE WENT TO 0 QUANTITY 3 QTS. FOUND FLEX LINE 153-08-0254, FROM FILTER MODULE BROKEN. REPLACED LINE, OPERATION NORMAL.

Part: GEN CONTROL — FAILED (EE COMPT)

ON CLIMBOUT, LOST RIGHT ENGINE GENERATOR. APU WAS DEFERRED, RETURNED JFK. REPLACED GENERATOR CONTROL UNIT OPERATION NORMAL.