N904DE

Part: B-NUT — LEAKING (HYD SYSTEM) · airframe 71,761 hrs · 53,109 cycles

AFTER TAKEOFF FA INFORMED US OF A STRONG ELECTRICAL ODOR IN THE FWD GALLEY. ODOR BEGAN DISSAPATING AND LASTED APPROX 5 MINUTES UNTIL COMPLETELY DISSAPATED. NO ODOR IN COCKPIT OR MAIN CABIN. NO CB POPPED. FOUND APU INLET CONTAMINATED WITH HYD FLUID. FOUND LT T/R CONTROL VALVE LINE LEAKING. TIGHTENED B NUT ,LK CKS GOOD. PERFORMED ALT DUCT BURNOUT PER W/C 49950-2215,CKS GOOD. OK FOR SERVICE. REPLACED A/C COALESCER BAGS.

Part: CONNECTOR — DIRTY (TAILCONE) · airframe 71,317 hrs · 52,678 cycles

TAILCONE UNSAFE ILLUMINATED IN FLIGHT. 53. INSPECTED TAILCONE CABLES AND SWITCHES. CLEANED CONNECTOR PLUGS FOR INDICATIONS SWITCHES. INDICATION NOW NORMAL. OK FOR SERVICE. (LP6205584)

Part: MECHANISM — NOT SEATED (TAILCONE RELEASE) · airframe 71,317 hrs · 52,678 cycles

"TAILCONE UNSAFE" ILLUMINATED INFLIGHT. FOUND RELEASE MECH UNSEATED FROM CLIPS. ALLOWED LOCK CABLE TO SWITCH TO COME LOOSE. RESEATED LOCK CABLE TO SWITCH & INSTALLED MECH IN CLIPS. VERIFIED TAILCONE UNSAFE LIGHT OUT PER MD88 AMM 53-53. J DAVIS 311408 VERIFIED RELEASE MECHANISM INSTALLED CORRECTLY AND TAILCONE LOCK CABLE INSTALLED/ UNSAFE LIGHT. FOUND RELEASE MECHANISM UNSEATED FROM CLIPS. ALLOWED LOCK CABLE TO SWITCH TO COME LOOSE. RESEATED LOCK CABLE TO SWITCH & INSTALLED MECHANISM IN CLIPS. VERIFIED TAILCONE UNSAFE LIGHT OUT PER MD88 AMM 53-53. VERIFIED RELEASE MECH INSTALLED CORRECTLY AND TAILCONE LOCK CABLE INSTALLED/ UNSAFE LIGHT EXTINGUISHED. (LP6205585)

Part: FAIRING — MISSING (FLAP HINGE) · airframe 71,431 hrs · 52,787 cycles

FLAP SECONDARY FAIRINGS LT WING NBR 3 OUTBD FLAP HINGE FARING MISSING INBD AND OUTBL SECONDARY FARINGS. INSTALLED LT WING #3 FLAP SECONDARY FAIRING IAW ERA 4577261-14MA. (LP5999946)

Part: WIRE — BROKEN (CABIN) · airframe 70,797 hrs · 52,184 cycles

DURING SVC CHECK FOUND ROW 24ED EMER LT INOP. FOUND WIRE BROKEN UNDER SEAT. SPLICED PER AMM 20-10 OPS CHECK GOOD. (LP5999942)

Part: FAIRING — MISSING (FLAP HINGE) · airframe 71,431 hrs · 52,787 cycles

FLAP SECONDARY FAIRINGS LT FLAP INBD FLAP HINGE MISSING INBD SECONDARY FARING. INSTALLED LT WING (INBD AND OUTBD) FLAP FAIRING SECONDARY FAIRING IAW ERA 580914-14 REV ORIGINAL. (LP4694744)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,642 hrs · 52,048 cycles

EMERGENCY LIGHT CHECK FOUND TAIL CONE UPPER LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE AFT LAV RIGHT SIDE. OPERATIONAL CHECK WAS GOOD. (LP #4694736)

Part: CONTROLLER — DEFECTIVE (COCKPIT) · airframe 69,997 hrs · 51,492 cycles

ELECTRICAL SMELL IN COCKPIT SLIGHT SMELL EMANATING FROM NAV2 CONTROL HEAD. DFGC BACK LIGHTING INOP. FOLLOWED THE NO/GO ODI ATA 2172 PROCEDURES. FOUND CB L16 POPPED & UNABLE TO RESET. TROUBLESHOT AND FOUND B5-87 DFGC LIGHT CONTROLLER BEING THE SOURCE OF THE ELECTRICAL SMELL. CONTROLLER LOCATED NEAR FO'S RT KNEE. REPLACED B5-87 - REF WDM 33-13-08. DFGC BACK IGHTING OPS NORM. (LP5528512)

Part: NOSE COWL — DAMAGED (NR 1 ENGINE) · airframe 69,930 hrs · 51,438 cycles

FOUND DAMAGE TO NR 1 ENG NOSE COWL LIP. REMOVED AND INSTALLED NR 1 ENGINE NOSE COWL PER AMM 71-10-01. INSPECTED FAN BLADES NO DAMAGE FOUND.

Part: COWLING — DENTED (LT ENGINE) · airframe 69,165 hrs · 50,775 cycles

LEFT ENG, SMALL DEN ON COWLING. REMOVED AND REPLACED NR 1 ENG NOSE COWL PER AMM 71-11, ERA 572607-14 ORIG. (LP3762710)

Part: SMOKE DETECTOR — FALSE ACTIVATION (AFT LAVATORY) · airframe 68,713 hrs · 50,368 cycles

SMOKE ALARM IN THE AFT LEFT LAVATORY WENT OFF. NO SMOKE OBSERVED, BATTERY DISCONNECTED. R & R THE SMOKE DETECTOR & BATTERY, OPS CHECKED GOOD.

Part: SPAR CAP — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 68,106 hrs · 49,873 cycles

HIDDEN CORROSION: CORROSION WAS FOUND ON RT HORIZONTAL STABILIZER REAR SPAR LWR BARREL NUT HOLE DURING REAR SPAR CAP REMOVAL IN REF NRC 00100. LEVEL CORROSION 2. CORROSION ON RT HORIZONTAL STABILIZER REAR SPAR LWR BARREL NUT HOLE WAS REPAIRED PER SRM 55-03D PARA 30.

Part: SPAR CAP — CRACKED (RT HORIZ STAB) · airframe 68,106 hrs · 49,873 cycles

CRACK (0.093" OF LENGTH) ON RT HORIZ STAB UPPER REAR SPAR AFT BARREL NUT HOLE. RT HORIZ STAB UPPER REAR SPAR CAP WAS REPAIRED PER DWG N SR09550027 REV F, SRM 51-30-2 / 51-30-5 / 51-30-1 AND AMM 20-10-14.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 68,106 hrs · 49,873 cycles

CRACK INTERCOSTAL BTW Y=1474 CANT AND Y=1485 CANT AT 7 HRS POSITION , AFT ACCESSORY COMPARTMENT. INTERCOSTAL WAS REPAIRED PER SRM 53-01 FIG 2.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 68,063 hrs · 49,840 cycles

FOUND THE EMERGENCY LIGHT ON SEAT 14 ED AND 16ED INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY ON SEAT 16ED AND CHECKED GOOD. REPAIRED SEAT 14ED WIRING IAW WIRING PRAC MANUAL CHP 20.

Part: CLAMP — DISCONNECTED (CABIN) · airframe 68,001 hrs · 49,786 cycles

EMERGENCY ISLE LIGHT INOP AT SEAT 26CD. RECONNECTED WIRE BUNDLE CLAMP UNDER SEAT 26CD. OPS CK GD.

Part: JACKSCREW — DAMAGED (HORIZ STAB) · airframe 67,447 hrs · 49,337 cycles

AC FAILED JACK SCREW INSPECTION AMDS 2740-01113-08. RMVD JACKSCREW ASSY IAW AMDS WC 2742-4540. REPLACED JACKSCREW ASSY PER WC 2742-4540.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,377 hrs · 49,285 cycles

FWD EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED THE BATTERIES.

Part: UNKNOWN — ODOR (CABIN AIR) · airframe 66,995 hrs · 48,990 cycles

ODOR OF OIL COMING THRU AIR VENTS, WORSE ON GROUND WITH APU RUNNING. DUCTS AND MANIFOLDS INSPECTED AND DUCT BURNOUT COMPLETED WITH NO FINDINGS.

Part: CONNECTOR — DAMAGED (THROTTLE) · airframe 65,061 hrs · 47,484 cycles

LEAVING CRUISE AT FL350, RIGHT THROTTLE WAS PHYSICALLY STUCK, UNABLE TO MOVE WITH OR WITHOUT AUTOTHROTTLES ON. AFTER APPROXIMATELY 6 MINUTES DURING DESCENT, IT FREED UP AND WAS NORMAL FOR REMAINDER OF FLIGHT. R & R THE CONNECTOR IAW SWPM CH.20. COMPLIED WITH PRECISSION TRIM IAW AMDS 7321-01224-01-02.

Part: UNKNOWN — ODOR (CABIN & COCKPIT) · airframe 64,945 hrs · 47,387 cycles

AFTER TAKEOFF COCKPIT AND CABIN CREW OBSERVED RUBBER SMELL. DISSIPATED AFTER APPROX 10 MIN. FOLLOWED NO-GO ODI PREVENTION 2172. NO DEFECTS NOTED. C/W PNEUMATIC SYSTEM DUCT BURN-OUT PER JOB CARD 7100-2619. ALL CHECKS GOOD. A/C OK FOR SERVICE.

Part: WIRE HARNESS — BURNED · airframe 64,765 hrs · 47,253 cycles

AT CRUISE, MASTER WARNING CAME ON OAP DISPLAY MACH TRIM INOP/ YAW DAMP INOP/ IRS1 BATT FAIL/STALL IND FAILURE. BOTH AP AND ATNOP- ATL WINDOW BLANK & COULD NOT ADJUST SPD INDICATOR. MASTER WARNING WOULD NOT RESET C/BS C12 AND C17 POPPED AND WOULD NOT RESET. ILS/LOC INOP CAPTS SIDE. STA 160-21. WIRES FOUND DAMAGED DUE TO CHAFING WITH A/C STRUCTURE. FOUND WIRE BUNDLE BURNED AT BS 160R.

Part: BOOT — DETACHED (RT ACM) · airframe 64,634 hrs · 47,159 cycles

DURING CLIMB OUT, THE CREW REPORTED FAILURE OF THE LEFT PACK. THE RIGHT PACK WAS UNABLE TO MAINTAIN CABIN PRESSURIZATION UNTIL DESCENDING TO FL180. OVER TIME THE RIGHT PACK BECAME MORE WEAK AND REQUIRED FURTHER DESCENT TO FL 100 WHERE CABIN ALTITUDE HELD AT 4000 WITH AN INTERMITTENT FLOW LIGHT. THE FLIGHT CONTINUED WITH NO MENTION OF EXPEDITED OR EMERGENCY DESCENT. MAINTENANCE FOUND THE DISCHARGE BOOT FOR THE RIGHT ACM OFF. THE BOOT WAS INSTALLED AND THE RIGHT PACK OPERATED NORMALLY. THE LEFT PACK HAD NO AIRFLOW DOWNSTREAM OF THE PRV. AN AIR LINE WAS REPORTED LOOSE. THE PRV WAS REPLACED AND THE AIR LINE WAS SECURED. SINGLE PACK CONFIDENCE CHECKS WERE ACCOMPLISHED FOR BOTH PACKS AND A HULL DECAY CHECK WAS PERFORMED WITH NO ADDITIONAL FINDINGS . THE AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,596 hrs · 47,121 cycles

EMERGENCY LIGHTS IN 1ST CLASS WILL NOT COME ON. DISCONNECTED AND RECONNECTED BATTERY PACKS, LIGHTS CHECKED GOOD IAW MM 33-53.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 64,294 hrs · 46,895 cycles

OVERHEAD EMERGENCY LIGHTS INOPERATIVE AT ROWS 11 TO 15. REPLACED THE BATTERY PACK IAW AMM 33-53-00 OP CHECKED GOOD.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 62,884 hrs · 45,831 cycles

DELAMINATED LOWER/UPPER FACE, LEFT SIDE PREVIOUSLY REPAIRED AT OTBD VANE/INBD FLAP LT WING. OTBD VANE, INBD FLAP LT WING WAS REPLACED IAW SRM 57-04, PAR 2.

Part: VANE — DELAMINATED (LT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

DELAMINATED LOWER/UPPER FACE LT SIDE PREVIOUSLY REPAIR AT OTBD VANE, INBD FLAP LT WING IN REF CARD 62, ZONE 10. OTBD VANE, INBD FLAP LT WING WAS REPLACED IAW SRM 57-04 PAR 2.

Part: ACCESS PANEL — UNKNOWN (RT WING) · airframe 62,883 hrs · 45,830 cycles

INAPPROPRIATE FUEL ACCESS PANEL AT POSITION 1414C RT WING. FUEL ACCESS DOOR 1414C WAS REPLACED IAW AMM 28-00-00.

Part: SUPPORT FITTING — GOUGED (RT MLG) · airframe 62,883 hrs · 45,830 cycles

DURING MAINTENANCE ACTIVITIES WAS FOUND A GOUGE AT RT MLG SUPPORT FITTING BEARING BORE. THE REPAIR WAS PERFORMED IAW ER/A 543217-14AD, REV A.

Part: LONGERON — CRACKED (BS 1431) · airframe 62,883 hrs · 45,830 cycles

CRACKED LONGERON 12R, BS 1431 CANT AT AFT COMPARTMENT. THE LONGERON WAS REPAIRED IAW ER/A 543219-14, REV ORIG AND ETI-88-16-125, REV 1.

Part: SPAR CAP — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION WAS FOUND ON THE 3 FASTENER HOLES OF THE HORIZONTAL STABILIZER REAR LT UPPER SPAR CAP. FASTENER HOLES WERE REPAIRED IAW ER/A 543184-14AD, REV ORIGINAL AND ETI 88-16-095, REV 7.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON 14 INNER HOLE AT RT LOWER ACCESS DOOR CUTOUT BETWEEN XRS 189 TO 214. HOLES ON LWR ACCESS DOOR CUTOUT WERE REPAIRED IAW ER/A 543204-14AD, REV ORIGINAL SECTION I: PERMANENT REPAIR ER/A APPROVAL IS LIMITED TO 67,000 TOTAL CYCLES ONLY IAW ER/A 543204AD, REV ORIG.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON 4 INNER HOLES AT LT LOWER ACCESS DOOR CUTOUT XRS=189 TO 214. HOLES ON LOWER ACCESS DOOR CUTOUT WERE REPAIRED IAW ER/A 543204-14AD REV ORIGINAL SECTION I: PERMANENT REPAIR ER/A APPROVAL IS LIMITED TO 67,000 TOTAL CYCLES ONLY IAW ER/A 543204-14AD, REV ORIGINAL.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON LT BARREL NUT NR 24 AT LT UPPER SURFACE OF HORIZONTAL STABILIZER REF CARD 12, ZONE 60. DUE TO EXCESSIVE CORROSION ON BARREL NUT PANEL WAS REPLACED IAW DWG 5922575, REV DA AND ER/A 543203-14, REV ORIGINAL.

Part: SKIN — DAMAGED (BS 1211) · airframe 62,883 hrs · 45,830 cycles

FUSELAGE EXTERIOR SKIN DOUBLER/TRIPLER REPAIR DAMAGED AT FORWARD END JUST AFT OF C3 DOOR CUTOUT AT BS 1211. DOUBLER AND TRIPLER WERE REPLACED IAW ER/A 271897-14 REV C STEP 4, 8, 9 AND SRM 51-10-3, 5130-5, 51-10-2, PERMANENT REPAIR: REQUIREMENT REPAIR APPROVAL IS LIMITED TO 60,000 TOTAL AIRFRAME CYCLES IAW ER/A 271897-14, REV C.

Part: HINGE — WORN (CARGO DOOR) · airframe 62,883 hrs · 45,830 cycles

FREE PLAY ON FWD/AFT HINGE AT FWD CARGO COMPARTMENT. HINGE AFT AT FWD CARGO DOOR WERE REPAIRED AND FWD HINGE HARDWARE WERE REPLACED AND FREE PLAY WAS CORRECTLY IAW AMM 52-31-02 AND ER/A 497387-14MA, REV B.

Part: SKIN — WORN (VERTICAL STAB) · airframe 62,883 hrs · 45,830 cycles

WORN VERTICAL STABILIZER SKIN BS 170, LT SIDE. WORN VERTICAL STABILILZER SKIN BS 170, LT SIDE WAS ATTENDED WITH ER/A 543218-14, REV A.

Part: CHANNEL — CRACKED (BS 940) · airframe 62,883 hrs · 45,830 cycles

CRACK ON CHANNEL BS 940 X=47 LT AT LT MLG WHEEL WELL, DOOR JAMB CHANNEL. CRACK WAS STOP DRILLER IAW SRM 53-01, FIG 2, SHEET 4 AND AREA WAS REPAIRED IAW ER/A 497265-14, MA REV ORIGINAL.

Part: SKIN — WORN (LT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

WEAR ON T/E UPPER AND LOWER SURFACE AT LT OTBD FLAP, OTBD GUIDE VANE XVZ=297. SKIN REPAIRED IAW SRM 57-03D PAR II.

Part: INTERCOSTAL — CORRODED (BS 1212-1231) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON INTERCOSTAL FROM BS 1212 TO 1231, LONGERON 29L IN AFT CARGO BAY. A NEW INTERCOSTAL WAS INSTALLED IAW SRM 53-14-3, FIG 3, SHEET 4 AND 51-30-2.

Part: CARGO TRACK — DAMAGED (BS 1003-1155) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AND ELONGATED HOLES ON RT CARGO TRACK FROM BS 1003 TO 1155. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-2, 51-30-5, AND SRM 51-10-4.

Part: FRAME — CRACKED (BS 1510) · airframe 62,883 hrs · 45,830 cycles

CRACKED FRAME BS 1510, CANT BETWEEN 6 AND 9 HRS POSITION AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5, DWG 9911843, REV AC.

Part: INTERCOSTAL — CORRODED (BS 1148-1155) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON INTERCOSTAL, BS 1148 TO 1155 BETWEEN LONGERONS 29 - 30R. INTERCOSTAL REPLACED IAW SRM 51-30-5 AND 51-30-2.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,883 hrs · 45,830 cycles

CRACKED PAN AT CUT OUT OF AFT RT EMERGENCY EXIT. PAN WAS REPAIRED IAW SRM 53-05, FIG 32.

Part: PAN — CRACKED (EMERGENCY EXIT) · airframe 62,883 hrs · 45,830 cycles

CRACKED PAN AT CUT OUT OF AFT LT EMERGENCY EXIT OVERWING. PAN AT CUT OUT OF AFT LT EMERGENCY EXIT WAS REPAIRED IAW SRM 53-05, FIG 32. CRACK WAS FOUND 0.500" OF LENGTH.

Part: FRAME — CRACKED (BS 1448) · airframe 62,883 hrs · 45,830 cycles

CRACKED FRAME BS 1448 BETWEEN LONGERON 1 - 3R. FRAME WAS REPLACED IAW SRM 51-30-5, 51-30-2, 51-10-4 AND 51-10-3 PAR 14 AND 21 AND DWG 9911860, REV L. CRACK 1.125".

Part: PROBE — WORN (FUEL SYSTEM) · airframe 62,883 hrs · 45,830 cycles

WEAR ON FUEL ACCESS PROBES 1460C, 1466C, 1373C. PROBES WERE REPLACED IAW AMM 28-40-02 AND EA 09-2122-14, REV B.

Part: FLOORBEAM — CORRODED (BS 1380) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON FRAME TEE BS 1380 BETWEEN X= 25 TO X= -23 . FRAME TEE WAS REPLACED IAW SRM 51-10-3, 51-10-4, 51-30-2, 51-30-5 AND DWG 9912246, REV CE.

Part: SKIN — WORN (VERTICAL STAB) · airframe 62,883 hrs · 45,830 cycles

LOOSE FASTENERS, 2 ROWS ABOVE AND BELOW BS ZFS=52 AT VERTICAL STABILIZER L/E REMOVABLE. DUE TO EXCESSIVE WEAR ON THE UPPER COUNTERSINK THE L/E SKIN WAS REPAIRED AND THE LOWER SKIN WAS FOUND WITHIN LIMITS IAW SRM 55-03D, PAR 28, 27 AND DWG SG09550004. REV D. THEREFORE WITHIN LIMITS IAW SRM 55-03D, PAR 27 AND DWG SG09550004. PERFORM DETAILED VISUAL INSPECTION INITIAL 3000 CYCLES, REPETITIVE 3,000 CYCLES AND CONTACT BOEING FOR APPROVALS IAW SRM 55-03D, PAR.28,27.

Part: HEATER BLANKET — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON HEATER BLANKET SECUNDARY ACCESS PANEL NR 1303C. REMOVED AREA LT WING. AREA WAS REPAIRED IAW 543196-14AD REV ORIGINAL.

Part: HEATER BLANKET — GOUGED (LT WING) · airframe 62,883 hrs · 45,830 cycles

GOUGE ON HEATER BLANKET AT BS XCW=114 APPROXIMATELY LT WING. GOUGE ON LT HEATER BLANKET WAS REPAIR IAW ER/A 543196-14AD, REV ORIGINAL.

Part: HEATER BLANKET — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON HEATER BLANKET SECONDARY ACCESS PANEL NR 1307C. REMOVED AREA LT WING. AREA ON LT HEATER BLANKET WAS REPAIRED IAW ER/A 543196-14AD REV ORIGINAL.

Part: HINGE — WORN (CARGO DOOR) · airframe 62,883 hrs · 45,830 cycles

FREE PLAY ON FWD/AFT HINGE AT AFT CARGO COMPARTMENT DOOR. FREE PLAY ON FWD /AFT HINGE AT AFT CARGO COMPARTMENT DOOR WAS CORRECTLY IAW ER/A 497387-14MA, REV B AND AMM 52-31-02.

Part: SKIN — DAMAGED (BS 370-375) · airframe 62,883 hrs · 45,830 cycles

ELONGATED HOLE ON FUSELAGE SKIN, BS 370-375 OVER LONG 29 LT. ELONGATED HOLE WAS REPAIRED IAW ETI-88-16-102, REV 1 AND ERA 543192-14, REV ORIGINAL.

Part: SERVICE PANEL — CORRODED (LAVATORY) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FWD LAVATORY SERVICE PANEL. LAVATORY SERVICE PANEL WAS REPLACED IAW SRM 51-02 PAR 6A AND DWG 5922013, REV AS AND SRM 51-10-3, 51-30-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON FUEL ACCESS PLATE. FUEL ACCESS PLATE WERE REPLACED IAW AMM 28-00-00.

Part: FINGER DOUBLER — CORRODED (BS 234) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON FINGER DOUBLER BS 234 BETWEEN LONGERON 26 LT TO 25 LT AT FWD CARGO COMPARTMENT. DUE EXCESSIVE CORROSION SECTION FINGER DOUBLER WAS REPAIRED IAW SRM 53-04, FIG 12E.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON SETTLEMENT AREA AND COUNTER SINK AT FUEL ACCESS PLATE NR 1361C. FUEL ACCESS DOOR WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — DELAMINATED (BS 826-1003) · airframe 62,883 hrs · 45,830 cycles

FLOOR PANEL DELAMINATED FROM BS 826 TO BS 1003 IN CABIN PAX. FLOOR PANEL REPLACED IAW AMM 53-02-01-201.

Part: DOOR FRAME — CORRODED (BS 1154-1212) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON PREVIOUS REPAIR LOWER DOOR JAMB BS 1154-1212 CARGO BAY. PREVIOUS REPAIR WAS REPLACED IAW SRM 53-05, FIG 123.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1409C. FUEL ACCESS PLATE NR 1409C WAS REPLACED IAW SRM 51-22-2A AND IPC 57-30-00-31A.

Part: SUPPORT FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON RT HORIZONTAL STABILIZER SUPPORT FITTINGS BORES AT VERTICAL REAR SPAR. BORES AT VERTICAL REAR SPAR WERE REPAIRED, REAMED WITH FINAL DIMENTION OF REWORK: ID= 1.436" THEREFORE WITHIN LIMITS OF REWORK AND REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 55-02D, PAR 24.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FUEL ACCESS PANEL 1460C ON COUNTERSINK. CORROSION ON COUNTERSINK WAS REMOVED 3 HOLES ON ADJACENT OUT OF LIMITS, HOLES AND COUNTERSINK OUT OF LIMITS WERE REWORKED AND REPAIRED IAW SRM 51-22-2A, CONDITION II, AREA REWORKED WERE TREATED IAW SRM 51-10-3, PAR 21 AND FUEL ACCESS PANEL WAS PAINTED IAW PS 900-3-6, NR 36.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINKS ON FUEL PANEL ACCESS NR 1377C, LT WING. CORROSION ON SETTLEMENT AREA AND COUNTERSINKS WAS REMOVED, 3 HOLES NO ADJACENT OUT OF LIMITS, HOLES AND COUNTERSINK OUT OF LIMITS WERE REWORKED AND REPAIRED IAW SRM 51-22-2A, CONDITION II. AREA REWORKED WERE TREATED IAW SRM 51-10-3 PAR 21 AND FUEL ACCESS PANEL WAS PAINTED IAW PS 900-3-6, NR 36.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FUEL ACCESS PANEL 1454C ON COUNTERSINK . CORROSION ON COUNTERSINK WAS REMOVED, 2 HOLES NO ADJACENT OUT OF LIMITS, HOLES AND COUNTERSINK OUT OF LIMITS WERE REWORKED AND REPAIRED IAW SRM 51-22-2A, CONDITION II. AREA REWORKED WERE TREATED IAW SRM 51-10-3, PAR 21 AND FUEL ACCESS PANEL WAS PAINTED IAW PS 900-3-6, NR 36.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK FUEL PANEL ACCESS NR 1478C, RT WING. CORROSION ON COUNTERSINK WAS REMOVED 3 HOLES NO ADJACENT OUT OF LIMITS, HOLES AND COUNTERSINK OUT OF LIMITS WERE REWORKED AND REPAIRED IAW SRM 51-22-2A CONDITION II. AREA REWORKED WERE TREATED IAW SRM 51-10-3, PAR 21 AND FUEL ACCESS PANEL WAS PAINTED IAW PS900-3-6, NO 36.

Part: CUSP WEB — CORRODED (BS 503-579) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON CUSP WEB FROM BS 503 TO BS 579 BETWEEN X=-60 TO X=-54 AT RT FLOOR CABIN. REASON FOR RE-WRITE: TOOL MARKS RT CUSP WEB BS 538, X=-60. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-9.

Part: CUSP WEB — CORRODED (BS 1244-1249) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON CUSP WEB BETWEEN BS 1244 TO BS 1249 BETWEEN X=-60 TO X=-54. CUSP WEB BETWEEN BS 1244 TI BS 1249 WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: PAN — CRACKED (BS 1060-1079) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BS 1060-1079. REASON FOR RE-WRITE: IMPROPERLY DRILLED RT FWD LOWER CORNER AT RING PAN BS 1060-1079. RT FWD LOWER CORNER RING PAN BS 1060-1079 WAS REPAIRED IAW ER/A 543190-14, REV ORIGINAL.

Part: FRAME — CRACKED (BS 1485) · airframe 62,883 hrs · 45,830 cycles

CRACKED FRAME BS 1485 CANT AND 5 HRS POSITION RT SIDE AT AFT ACCESSORY COMPARTMENT. FRAME WAS REPARED IAW SRM 53-03, FIG 43.

Part: FLOOR SUPPORT — DAMAGED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

BROKEN REPAIR DOUBLER ON FLOOR SUPPORT AT FLOOR PANEL 1079E. DOUBLER ON FLOOR SUPPORT WAS REPAIRED IAW SRM 53-05, FIG 131C.

Part: CHANNEL — WORN (BS 845-927) · airframe 62,883 hrs · 45,830 cycles

WEAR ON FRAME C-RECEIVER OF W-CHANNEL X= 20 AND X= -20 BS 845, BS 864, BS 886, BS 905 AND BS 927 AT FLOOR STRUCTURE CABIN. CHANNELS WERE INSTALLED ON FLOOR PANELS NRS 826D SIDE LT AND 886 C SIDE LT IAW REMOVED AND INSTALLED, SRM 51-30-1 DRILLED SRM 51-10-4 DWG 9936639, REV P.

Part: SPAR CAP — DAMAGED (HORIZONTAL STAB) · airframe 62,883 hrs · 45,830 cycles

DAMAGED AT TEE OF LT HORIZONTAL STABILIZER REAR SPAR UPPER CAP. TEE OF LT HORIZONTAL STABILIZER WAS REPAIRED IAW SRM 55-01, FIG 1, SHEET 2, 51-10-3, PAR 21 AND 14-51-30-1.

Part: FLOOR SUPPORT — CRACKED (BS 1287-1309) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CRACK AND CORROSION ON FLOOR SUPPORT BETWEEN BS 1287 TO 1309 AND X=0 AT CABIN PAX. FLOOR SUPPORT WAS REPLACED IAW DWG 9936580, REV BW AND BS, AND SRM 51-10-3 PAR 21 AND 14; 51-10-4; 51- 30-2; 51-30-5.

Part: CUSP WEB — CRACKED (BS 905) · airframe 62,883 hrs · 45,830 cycles

CRACKED LT CUSP WEB AT BS 905, X 54 PAX CABIN FLOOR STRUCTURE. REPAIRED IAW SRM 53-05, FIG 131A-1, SHEET 1- 10.

Part: CUSP WEB — CORRODED (BS 598-712) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

DUE TO EXCESIVE CORROSION REPLACE LT CUSP WEB FROM BS 598 TO BS 712. LT CUSP WEB FROM STA 598 TO BS 712 WAS REPLACED IAW SRM 53-05, FIG 131A-24 AND DWG 9930538, REV CF SRM 51-30-2, SRM 51-30-1.

Part: CUSP WEB — CORRODED (BS 795-807) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER ON RT CUSP WEB BS 795 TO 807, X=-60 TO X=-54 AT FLOOR STRUCTURE CABIN. RT CUSP WEB BS Y=788 TO Y=807 WAS REPLACED IAW SRM 53-05, FIG 131A-2, DWG 9930538 REV CF, SRM 51-30-2, 51-30-5.

Part: CHANNEL — CRACKED (HORIZONTAL STAB) · airframe 62,883 hrs · 45,830 cycles

CRACKED CHANNELS AT REAR SPAR LT HORIZONTAL STABILIZER BETWEEN BS XHS = 23 TO 38 AND XHS= 62 APPROXIMATE CHANNELS WERE REPLACED IAW SRM 55-12-0D, FIG 4; 51-10-3, PAR 21 AND 14; 51-30-2 AND 51-10-2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK FUEL ACCES PLATE NR 1466C. ACCESS DOOR 1466C WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,883 hrs · 45,830 cycles

FLOOR PANEL DELAMINATED IN CABIN PAX. FLOOR PANEL REPLACED IAW AMM 53-20-01-201.

Part: CARGO TRACK — CORRODED (BS 1003-1220) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AND ELONGATED HOLES ON LT CARGO TRACK FROM BS 1003 - 1220 AT AFT CARGO COMPARTMENT. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-30-5.

Part: CUSP WEB — MISREPAIRED (BS 994-1003) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

IMPROPER REPAIR ON RT CUSP WEB X=-50 TO X=-60 BETWEEN BS 994 TO BS 1003 AT FLOOR STRUCTURE CABIN. DUE EXCESIVE DAMAGE CUSP WEB WAS REPLACED IAW SRM 53-05, PAR 144.C.(2) AND 51-30-2, 51-30-5, 51-30-1, 51-30-8, 51-10-4, 51-10-3 PAR 14 AND 21 DWG 9930612, REV CG.

Part: PAN — CRACKED · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BS=1212- BS 1231. REASON FOR RE-WRITE: IMPROPERLY DRILLED ON RT FWD LOWER CORNER RING PAN BS=1212-BS 1231. DAMAGE AREA WAS REPAIRED IAW ETI 88-16-104, REV 3 AND ER/A 543194-14, REV ORIGINAL.

Part: FLOOR PANEL — DELAMINATED (PAX CABIN) · airframe 62,883 hrs · 45,830 cycles

FLOOR PANEL DELAMINATED IN CABIN PAX. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FLOOR SUPPORT — BROKEN (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

BROKEN FLOOR CHANELS ON FLOOR PANEL NR 1155A LOWER SURFACE. BROKEN FLOOR CHANELS ON FLOOR PANEL NR 1155A LOWER SURFACE WAS REPAIRED IAW SRM 51-70-1D.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

ELONGATED HOLES ON FLOOR PANEL NR 1155A. ENLONGATED HOLE ON FLOOR PANEL NR 1155A WERE REPAIRED IAW SRM 51-70-1D.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

CRACKED FLOOR PANEL 1250A. CRACKED FLOOR PANEL WAS REPAIRED IAW SRM 51-70-1D, PAR 10.

Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

DELAMINATION ON LWR SURFACE OF LT OTBD FLAP INBD VANE, BELOW PREVIOUS REPAIRED DOUBLER AREA. DELAMINATION ON LWR SURFACE OF LT OTBD FLAP, INBD VANE, BELOW PREVIOUS REPAIR DOUBLER AREA WAS REPAIRED IAW SRM 57-03, PARR 11 AND CARD 2000-8149-06, 1996707, JOB 000-0014.

Part: CUSP WEB — CORRODED (BS 1220) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON LT CUSP WEB BS 1220. LT CUSP WEB BS 1220 WAS REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON SETTLEMENT AREA AND COUNTERSINK AT FUEL ACCES PLATE NR 1367C. CORROSION ON COUNTERSKIN WAS REMOVED AND MEASURE 3 HOLES ADJACENT WERE FOUND WITH .545", .542", .540". THEREFORE IT IS OUT LIMITS FUEL ACCESS DOOR 1369C WAS REPLACED IAW IPC 57-30-00 AND SRM 51-22-2A.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

BROKEN AND MISSING NUT ON FLOOR PANEL 200A. THE FLOOR PANEL WAS REPAIRED IAW SRM 51-70-10, SRM 51-30-2 AND DWG 9952523.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK FUEL ACCESS PANEL 1363C LT WING. ACCESS DOOR WAS REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,883 hrs · 45,830 cycles

CRACKED LONG 12 LT FROM BS 1437 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK AT FUEL ACCES PLATE NR 1311C. FUEL ACCESS DOOR 1311C WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSKIN FUEL ACCESS PANEL NR 1456C RT WING. FUEL ACCESS DOOR 1456C WAS REPLACED IAW SRM 51-22-2A.

Part: CUSP WEB — CORRODED (BS 503-579) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON CUSP WEB FROM BS 503 TO 579 BETWEEN X=60 TO X=54 AT RT FLOOR CABIN PAX. CUSP WEB 503 TO 598 WAS REPLACED DUE TO EXCESSIVE DAMAGE IAW SRM 51-300-2, 51-30-5, 51-10-3 PAR 14, 21 AND DWG 9930538, REV BF.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK AT FUEL ACCESS PLATE NR 1335C. FUEL ACCESS DOOR 1335C WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — WORN (RT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

WEAR ON INBD EDGE ON OTBD FLAP, INBD GUIDE VANE RT WING. INBD GUIDE VANE RT WING WAS REPAIRED IAW SRM 57-03D, PAR 11.

Part: CUSP WEB — CORRODED (BS 1098-1117) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON RT CUSP WEB, UPPER AND LOWER SURFACE, BS 1098 TO BS 1117 X=-54 TO X=-60 AT FLOOR STRUCTURE CABIN PASSENGER AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-13, SHEET 1-9.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK FUEL ACCESS PANEL 1371C LT WING. FUEL ACCESS DOOR 1371C WAS REPLACED IAW SRM 51-22-2A.

Part: ANGLE — CRACKED (BS 1309) · airframe 62,883 hrs · 45,830 cycles

CRACK ON ANGLE BETWEEN X 34 TO X 44, BS 1309 . ANGLE WAS REPLACED IAW 51-30-5, DWG 9912243, REV JS.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINKS FUEL ACCESS PANEL 1357C LT WING. FUEL ACCESS DOOR 1357C WAS REPLACE IAW SRM: 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSINK FUEL ACCESS PANEL 1355C LT WING. FUEL ACCESS DOOR 1355C WAS REPLACED IAW SRM 51-22-2A.

Part: FLOOR SUPPORT — CRACKED · airframe 62,883 hrs · 45,830 cycles

CRACKED CHANNEL AT FLOOR PANNEL 1079A, CHANNEL WAS REPAIRED IAW 51-70-1D.

Part: CUSP WEB — CORRODED (BS 808-813) · airframe 62,883 hrs · 45,830 cycles

CRACKED RT CUSP WEB X=-60 TO X=-54 BETWEEN BS 808 TO BS 813 AT FLOOR STRUCTURE CABIN. CUSP WEB REPAIRED IAW SRM 51-30-2, 51-01, PAR 4, 21, FIG 131A-1 AND 51-10-3, PAR 38.

Part: SKIN — DENTED (VERTICAL STAB) · airframe 62,883 hrs · 45,830 cycles

DENT AT VERTICAL STABILIZER TIP AT BS YV 215.200. DENT ON VERTICAL STABILIZER WAS REPAIRED IAW SRM 55-01, FIG 4, SHEET 2.

Part: EXHAUST DUCT — CRACKED (APU) · airframe 62,883 hrs · 45,830 cycles

CRACKED EXHAUST DUCT OF APU BETWEEN LONGERON 12 RT AND 14 RT BS 1401 TO BS 1416. CRACKS EXHAUST DUCT OF APU WERE REPAIRED, WELD CRACKS IAW ER/A 473221-14MA REV ORIGINAL.

Part: CUSP WEB — CORRODED (BS 664-665) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON RT CUSP WEB FROM BS 665 TO BS 664 AND X=-54 TO X=-60 AT CPAX. AREA WAS REPAIRED IAW SRM 53-05, FIG 131A-5, SHEET 1, 51-30-2, 51-30-8, 51-10-3 PAR.14,21,26-38.

Part: CUSP WEB — NOT REPORTED (BS 772-775) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

AREA OUT OF LIMITS ON LEFT CUSP WEB X=54/60 FROM BS 772 TO 775 AT CABIN PASSENGER AREA. AREAS WAS REPAIRED IAW SRM 53-05, FIG 131A-113, SHEET 1.

Part: LONGERON — CRACKED (BS 1437) · airframe 62,883 hrs · 45,830 cycles

CRACKED LONGERON 16 LT FROM BS 1437 AT AFT ACCESSORY COMPARTMENT. LONGERON WAS REPLACED IAW SRM 51-30-2, 51-10-4, 51-10-3, PAR 21 /14 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 193) · airframe 62,883 hrs · 45,830 cycles

CRACKED INTERCOSTAL BS 193 X+30 TO X=+50 Z=1, AT W1. INTERCOSTAL WAS REPAIRED IAW SRM 51-70-5, 51- 30-2, 51-30-1, 51-30-5.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,883 hrs · 45,830 cycles

DAMAGED METALIZER ON RUDDER ACCESS NR 6513G, 6508G AND 6502G. METALIZER ON RUDDER ACCESS NR 6513G, 6508G AND 6502G WERE REPAIRED IAW SRM 51-70-1A.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

AFTER CARGO INTERCOSTAL CORRODED AT UPPER HORIZONTAL ANGLE UNDER SIDE BETWEEN BS 1309-1322 L27L- L28L. INTERCOSTAL WAS REPLACED IAW DWG N9936718, REV M SRM 51-30-2, 51-10-4, 51-10-3 PAR. 14, 21 51-30-5.

Part: SUPPORT FITTING — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON LT HORIZONTAL STABILIZER SUPPORT FITTINGS BORES AT VERTICAL STAB REAR SPAR. BORES AT VERTICAL STAB WERE REPAIRED, REAMED WITH FINAL DIMENTION: ID=1.436", THEREFORE WITHIN LIMITS OF REPAIR. REPAIR BUSHINGS WERE FABRICATED AND INSTALLED IAW SRM 55-02D, PAR.24.

Part: DOUBLER — CORRODED (BS 640-651) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON DOUBLER REPAIR FROM BS 640 TO BS 651 BETWEEN X=60 TO X=54 AT RT FLOOR CABIN PASSENGER AREAS WERE REPAIR IAW SRM 53-05, FIG 131A-2, SHEET 5.

Part: SKIN — OUT OF LIMITS (BS 610-695) · airframe 62,883 hrs · 45,830 cycles

SKIN OUT OF LIMITS BETWEEN LONGERONS 3 & 4L AT BS 610 - 695. REPAIRED IAW SRM 51-30-2, 51-10-4, 51-10-3. PAR 14 AND 21 AND 53-04-2, FIG 2, SHEET 6 AND 17.

Part: ANGLE — CRACKED (BS 237) · airframe 62,883 hrs · 45,830 cycles

CRACK ON ANGLE BS 237 BETWEEN LONGERON 27 TO 28R IN FWD CARGO COMPARTMENT. NEW ANGLE WAS INSTALLED IAW SRM 51-30-2, 51-30-5, 51-10-3. PAR 14/21, 51-10-4, 51-10-2 AND DWG 9915554, REV U.

Part: CUSP WEB — CORRODED (BS 446-500) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON REPAIR DOUBLER ON RH CUSP WEB X=-54, X=-60 BETWEEN BS 446 - 500 AT FLOOR STRUCTURE CABIN. REPAIR DOUBLERS WERE REPLACED NEW REPAIR, 3 EA WERE FABRICATED AND INSTALLED IAW SRM 53-05, FIG 131A-14 AND 131A-7.

Part: CUSP WEB — CORRODED (BS 541-560) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON LT CUSP WEB UPPER AND LOWER SURFACE FROM BS 541 TO BS 560 BETWEEN X=54 TO X=60. CUSP WEB WAS REPAIRED IAW 53-05, FIG 131A-14.

Part: CUSP WEB — DAMAGED (BS 715-716) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

REWORK OUT OF LIMITS ON CUSP WEB BETWEEN X=60 TO X=54 AND BS 715 - 716. CUSP WEB WAS REPAIRED IAW SR, 53-05, FIG 131A-6 SRM 51-10-4, SRM 51-10-3, PAR 14, 21 & 38 SRM 51-30--5.

Part: CUSP WEB — CORRODED (BS 317-320) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON RT CUSP WEB FROM BS 317 TO 320 BETWEEN X=-54 TO X =-60. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A-13.

Part: CUSP WEB — CORRODED (BS 560-598) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON REPAIR DOUBLER LT CUSP WEB X=54 TO X=60 BETWEEN BS 560 TO BS 579, Y=585 TO Y=598 AT FLOOR STRUCTURE CABIN. REPAIR DOUBLERS WERE REPLACED IAW SRM 53-05, FIG 131A-6.

Part: CUSP WEB — CORRODED (BS 693-741) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON REPAIR DOUBLER LT CUSP WEB X=54 TO X=60 BETWEEN BS 693 TO 710, 712 TO 723 AND 731 TO 741 AT FLOOR STRUCTURE CABIN. REPAIR DOUBLERS WERE REPLACED IAW SRM 53-05, FIG 131A-13 AND FIG 131A-6. REPAIR DOUBLER 693 TO 710 WILL BE ATTENDED WITH CARD NR 277, ACFT ZONE 201, NRC 20000105686.

Part: FLOOR PANEL — DELAMINATED (MAIN CABIN) · airframe 62,883 hrs · 45,830 cycles

FLOOR PANEL DELAMINATED FROM BS 110 TO 256 AT CABIN PAX. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: FITTING — CORRODED (GIRT BAR) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON FITTING, 2EA OF FLOOR PANEL 160G, LATCH GIRT BAR. FITTINGS WERE REPLACED NEW, 2 EA WERE ADJUSTED IAW SRM 51-10-4.

Part: FLOOR PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION OR FLOOR PANEL 160G. FLOOR PANEL 160G WAS REPLACED; A NEW WAS FABRICATED IAW SRM 51-10-2, 51-10-4 AND DGW 9957828AB.

Part: SKIN — DENTED (LT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

DENT ON UPPER FACE MID FIXED VANE LT WING OTBD FLAP NR 4. DENT ON UPPER FACE MID FIXED VANE LT WING OTBD FLAP WAS REPAIRED IAW SRM 57-03D, PARR 11 AND CARD 2000-8149-07.

Part: INTERCOSTAL — CRACKED (BS 173) · airframe 62,883 hrs · 45,830 cycles

CRACK ON INTERCOSTAL BS 173, Z=0, X=55 BELOW SIDE OF W1 AT LT FLOOR CABIN PAX. INTERCOSTAL WAS REPAIRED IAW SRM 51-70-5, FIG 1.

Part: CUSP WEB — DEFORMED (BS 770-775) · airframe 62,883 hrs · 45,830 cycles

DEFORMED LIGHTNING HOLE ON RT CUSP WEB X=-54 TO X=-60 BETWEEN BS 770 TO 775 AT FLOOR STRUCTURE CABIN. REPAIR PARTS WAS FABRICATED IAW SRM 53-05, FIG 131A-13, SHEET 1, TREATED AND PAINTED IAW SRM 51-10-3, PAR 21 AND 14 AND INSTALLED IAW SRM 51-30-2.

Part: ANGLE — CRACKED (BS 674) · airframe 62,883 hrs · 45,830 cycles

CRACKED INTERCOSTAL ANGLE ON BS 674 BETWEEN EDGE AND BEAM 1 AT MID CARGO COMPARTMENT DOOR. CRACKED INSTERCOSTAL ANGLE WAS REPLACED IAW SRM 51-30-2 AND 51-3-5.

Part: SKIN — CORRODED (BS 1338) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FUSELAGE, BS 1338, BETWEEN LONGERON 19L/20 LT. REPAIR WAS ACCOMPLISHED IAW ER/A 543198-14, REV ORIGINAL AND ETI-88-16-105 OF DATE: 04-MAR-16.

Part: SKIN — CORRODED (BS 130) · airframe 62,883 hrs · 45,830 cycles

BULGE OUTER FUSELAGE SKIN AND DOUBLER BETWEEN LONG 30 TO LONG 28, RT BS 130 APPROXIMATELY AT E/E DOOR JAMB. BULGE WAS EVALUATED WITH NEXT DIMENTIONS: D=1.5", X=0.095", D/X=15.78. THEREFORE IT IS WITHIN LIMITS IAW SRM 53-04-1, PAR 7 E CONDITION 1B. HFEC INSPECTION, 10X MAGNIFIED INSPECTION AND DETAILED VISUAL INSPECTIONS WERE ACCOMPLISHED, NIL DAMAGE FOUND. PERFORM DECAL CONDITION INSPECTION EVERY C-CHECK.

Part: SKIN — WORN (BS 192) · airframe 62,883 hrs · 45,830 cycles

WEAR ON OUTER SKIN FWD SIDE OF BS 192 AND BEAM NR 6 AT FWD ENTRY DOOR. DUE EXCESSIVE DAMAGE AREA WAS REPAIRED IAW ER/A 486216-14 MA, REV A.

Part: LUG — CRACKED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

CRACK ON LUG WYE DUCT. LUG ON WYE DUCT WAS WELDED IAW ER/A 494638-14MA, REV B.

Part: SKIN — DAMAGED (RUDDER) · airframe 62,883 hrs · 45,830 cycles

DAMAGE ALLUMINIZED ON RT/LT SIDES OF RUDDER SKIN AT VERTICAL STABILIZER. METALLIZED ON RT/LT SIDES OF RUDDER SKIN AT VERTICAL STABILIZER WERE REPAIRED IAW ER/A 092613-14MA REV A, SRM 51-70-1A D, PAR 23.

Part: PAN — CRACKED (BS 196) · airframe 62,883 hrs · 45,830 cycles

CRACK ON INNER PAN OF AFT UPPER CORNER BETWEEN BEAM NR 1 AND BS 196 AT FWD ENTRY DOOR. INNER PAN OF FWD ENTRY DOOR WAS REMOVED, DUE TO CRACK AND NEW PAN WAS DRILLER AND INSTALLED IAW SRM 51-30-1, 51-30-2 AND 51-30-4.

Part: CUSP WEB — CRACKED (BS 241) · airframe 62,883 hrs · 45,830 cycles

CRACK ON CUPS WEB BS 241 BETWEEN X= -60 TO X= -54 AT RT FLOOR CABIN PASSENGER. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, SRM 51-30-5, SRM 51-01, SRM 51-30-2, SRM 53-05 FIG 131A-6, SRM 51-10-3, PAR 14,21,38.

Part: DOOR FRAME — CRACKED (BS 941) · airframe 62,883 hrs · 45,830 cycles

CRACKED DOOR JAMB CHANNEL BS 941, X=7LT AT LT MLG WHEEL WELL. CRACKED DOOR JAMB CHANNEL BS 941 AT LT MLG W/W WAS REPLACED IAW SRM 51-3-2, 51-30-5, 51-10-4 AND 51-10-3 PAR 14 AND 21 DWG 5930584, REV.

Part: STRUCTURE — WORN (TAILCON) · airframe 62,883 hrs · 45,830 cycles

WEAR ON SLIDE PLATFORM OF TAIL CONE. REPAIR DOUBLER WAS REPLACED IAW ER/A 497244-14MA REV ORIGINAL.

Part: FLOORBEAM — CORRODED (BS 160) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FLOORBEAM BS 160 X31 IN ELECTRONIC EQUIPMENT COMPARTMENT. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. REPAIR WAS ACCOMPLISHED IAW SRM 53-01 FIG 2.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION AT FUEL ACCESS PANEL 2302C ON COUNTER SKIN. ACCESS IS OUT LIMITS AND IT WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 62,883 hrs · 45,830 cycles

CORROSION ON COUNTERSUNK AT FUEL ACCESS PLATE NR 1307C. CORROSION ON COUNTERSINK WAS REMOVED AND MEASURED 3 HOLES ADJACENT WERE FOUND OUT LIMITS WITH 0.664", 0.671" AND 0.688". THEREFORE IT IS OUT LIMITS AND IT WAS REPLACED IAW SRM 51-22-2A.

Part: CHANNEL — CRACKED (NLG DOOR FRAME) · airframe 62,883 hrs · 45,830 cycles

CRACK ON LT FORMER CHANNEL BS 46 NLG DOOR JAMB WHEEL WELL. DAMAGE WAS REMOVED AND DOUBLER REPAIR WAS TREATED, PAINTED AND INSTALLED IAW SRM 53-05, FIG 110, SRM 51-10-3 PAR 14, 21 AND 51-30-5.

Part: FITTING — CRACKED (CARGO DOOR) · airframe 62,883 hrs · 45,830 cycles

CRACKED FITTING ON FWD EDGE BS 636 AND BEAM 5 ATMID CARGO COMPARTMENT DOOR. SEAL RETAINER AND T-FITTING WERE REMOVED IAW SRM 51-30-1 AND 51-30-2. NEW T-FITTING WAS DRILLER IAW SRM 51-10-4. NEW T- FITTING WAS TREATED PAINTED AND INSTALLED IAW SRM 51-10-3 PAR 14 AND 21 AND 51-30-5.

Part: BEAM — CRACKED · airframe 62,883 hrs · 45,830 cycles

CRACKED BEYOND STOP DRILL ON FWD EDGE OF BEAM NR 1 AT FWD ENTRY DOOR. FWD EDGE OF BEAM NR 1 WAS REPAIRED IAW SRM 52-05D, FIG 98.

Part: INTERCOSTAL — CRACKED (BS 186) · airframe 62,883 hrs · 45,830 cycles

CRACK ON INTERCOSTAL OF INTERNAL STRUCTURE BETWEEN BEAMS NR 4 TO NR 5 AND BS 186 AT FWD ENTRY DOOR. INSTERCOSTAL OF INTERNAL STRUCTURE BETWEEN BEAM NR 4 TORN 5 WAS REMOVED DUE TO CRACK, AND NEW INSTERCOSTAL WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: WEB — CRACKED (BS 218) · airframe 62,883 hrs · 45,830 cycles

CRACK ON WEB BS 218 BETWEEN X=-40 TO X= -44 AT FLOOR STRUCTURE CABIN. CRACK WAS REMOVED BY DRILLING IT AND OPENING A HOLE OF 0.125" IAW SRM 51-10-4 AND 53-01, FIG 1, SHEET 2 PLUG WAS INSTALLED IAW SRM 51-60-0 AND 51-30-8.

Part: PAN — CRACKED (CARGO DOOR) · airframe 62,883 hrs · 45,830 cycles

CRACK PAN BELOW STOP FITTING NR 4 AT AFT CARGO COMPARTMENT DOOR. PAN WAS REPAIRED IAW SRM 52-05, FIG 50.

Part: WEB — CRACKED (BS 864) · airframe 62,883 hrs · 45,830 cycles

CRACK ON MEMBRANE BS 864 X=47 AT LT FLOOR CABIN PAX. REPAIR WAS ACCOMPLISHED IAW SRM 53-05, FIG 131A-121.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

CRACK ON FLOOR PANEL SKIN 1003A. FLOOR PANEL WAS REPAIR IAW SRM 53-05, FIG 4.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 62,883 hrs · 45,830 cycles

WORN LOWER FWD & AFT DOUBLER AT FWD CARGO COMPARTMENT DOOR. DOUBLERS FWD/AFT POSITION WERE REPLACED IAW SRM 51-30-2 AND ER/A 486624-14 MA, REV ORIGINAL.

Part: FLOOR PANEL — CRACKED (NOT REPORTED) · airframe 62,883 hrs · 45,830 cycles

CRACK ON FLOOR PANEL NRS 769G, 927A AND CHANNEL AREA. CRACKS ON FLOOR PANELS WERE REPAIRED IAW SRM 53-05, FIG 131C.

Part: SKIN — DENTED (ELEVATOR TAB) · airframe 62,883 hrs · 45,830 cycles

DENTS ON LT ELEVATOR CONTROL TAB UPPER SKIN BETWEEN BS XET, CANT=80 TO XET=65. LT ELEVATOR CONTROL TAB WAS REPLACED IAW SRM 51-50-2, P.4, 3.

Part: SKIN — DENTED (LT ELEVATOR TAB) · airframe 62,883 hrs · 45,830 cycles

DENTS ON GEARED TAB UPPER SKIN BETWEEN BS XET=100 TO XET=143 ALSO NICK ON LWR SKIN BS XET=147 AT LT ELEVATOR. DENTS ON GEARED TAB UPPER SKIN BETWEEN BS XET=100 TO XET=143 ALSO NICK ON LOWER SKIN BS XET=147 AT LT ELEVATOR.

Part: FLOOR PANEL — CRACKED (PAX CABIN) · airframe 62,883 hrs · 45,830 cycles

CRACK ON CHANNEL AT FLOOR PANEL 541A IN PASSENGER CABIN. FLOOR PANEL REPAIRED IAW SRM 53-05, FIG 131B, HFEC INSPECTION WAS PERFORMED AND NO CRACKS INDICATION WERE FOUND AFT STOP DRILL.

Part: SKIN — CRACKED · airframe 62,883 hrs · 45,830 cycles

CRACKED APU EXHAUST INNER AREA. APU WAS REPLACED AND WILL BE TO INSTALLED WITH CARD 4900-4573, JOB 001-0381.

Part: SPAR — NOT REPORTED (LT WING) · airframe 62,883 hrs · 45,830 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, SEVEN DIFERENT FASTENERS OF PSE, LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT LT WING. NRC IS ATTENDED WITH ER/A NR 543169-14AD, REV ORIGINAL.

Part: SPAR — NOT REPORTED (RT WING) · airframe 62,883 hrs · 45,830 cycles

DURING NDT INSPECTION A DISCREPANT AREA WAS FOUND, SEVEN DIFERENT FASTENERS OF PSE, LOWER SKIN REAR SPAR BETWEEN XRS=163 TO 168 AT RT WING. REPAIRED IAW ER/A NO 543169-14AD, REV ORIGINAL.

Part: SIGN — INOPERATIVE (EMERGENCY LIGHTS) · airframe 62,883 hrs · 45,830 cycles

MAINTENANCE FOUND THE COCKPIT DOOR EXIT SIGN ILLUMINATION OUT OF LIMITS. THE SIGN WAS REPLACED.

Part: PAN — CRACKED (BS 1212-1231) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BS 1212-1231. FASTENERS AND DAMAGE AREA WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED/PAINTED IAW 51-10-3 PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122 AND ER/A'S 493648-14MA, REV A AND 487747-14MA, REV ORIGINAL.

Part: PAN — CRACKED (BS 1079-1117) · airframe 62,883 hrs · 45,830 cycles

CRACKED LOWER FWD CORNER OF LT RING PAN BETWEEN BS 1098 TO 1117, 1079 TO 1098 AND 1060 TO 1079 AT INTERNAL STRUCTURE CABIN. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/AS 493648-14MA, REV A AND 487747-14MA, REV ORIGINAL. AT BS 1098 TO 1117 AND BS 1060 TO 1079 HFEC INSPECTION WAS ACCOMPLISHED BETWEEN BS 1079 TO 1098. NO CRACK FOUND IAW NDT SPM 06-10-01.001.

Part: PAN — CRACKED (BS 1174-1193) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BS 1174-1193. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED/PAINTED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122 AND ER/AS 493648-14MA, REV A AND 487747-14MA REV ORIGINAL.

Part: PAN — CRACKED (BS 1060-1079) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN BS 1060-1079. FASTENERS AND DAMAGE AREA WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED/PAINTED IAW SRM 51-10-3, PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, FIG 122 AND ER/A'S 493648-14MA, REV A, 487747-14MA, REV ORIGINAL.

Part: PAN — WORN (BS 1060-1079) · airframe 62,883 hrs · 45,830 cycles

WEAR ON RT LOWER AFT CORNER RING PAN, BS 1060-1079. RING PAN WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05, FIG 122 AND ER/A 497747-14MA, REV ORIGINAL AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1041-1060) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT AFT UPPER CORNER RING PAN BS 1041-1060. RING PAN RT AFT UPPER CORNOR AT STA 1041-1060 WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05, FIG 122 AND ER/A'S 497747-14. REV ORIGINAL AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 1098-1117) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT FWD LOWER CORNER RING PAN, BS 1098-1117. RING PAN RT FWD LOWER CORNER AT BS 1098-1117 WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-2, 51-10-3 AND 53-05 FIG 122 AND ER/AS 497747-14MA REV ORIGINAL AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 465) · airframe 62,883 hrs · 45,830 cycles

CRACK ON LT WINDOW RING PAN LOWER AFT SECTION BS 465 AT PAX CABIN INNER STRUCTURE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/AS 493648-14MA, REV A AND 487747-14MA REV ORIGINAL.

Part: PAN — CRACKED (BS 788) · airframe 62,883 hrs · 45,830 cycles

CRACK ON LT WINDOW WING PAN UPPER FWD CORNER BS 788 AT PAX CABIN INNER STRUCTURE. RING PAN WAS REPAIRED IAW SRM 53-05, FIG 122 AND ER/AS 493648-14MA, REV A AND 487747-14MA REV ORIGINAL.

Part: ANGLE — CRACKED (BS 984-1003) · airframe 62,883 hrs · 45,830 cycles

CRACK ON ANGLE FITTING AT RT AFT UPPER CORNER RING PAN BS 984-1003. DAMAGE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122 AND REPAIRED IAW SRM 53-05, FIG 122, 51-10-3, PAR 14 AND 21 AND ER/AS 497747-14MA, REV. ORIGINAL AND 493648-14MA, REV A.

Part: PAN — CRACKED (BS 886-905) · airframe 62,883 hrs · 45,830 cycles

CRACK ON RT LOWER AFT CORNER OF RING PAN BETWEEN BS 886-905. FASTENERS AND DAMAGE AREA WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND 53-05, FIG 122. REPAIR PARTS WERE FABRICATED IAW SRM 53-05, FIG 122. REPAIR PARTS WERE TREATED/PAINTED IAW SRM 51-10-3, PAR 14 AND 21.

Part: SKIN — DENTED (RT WING TE FLAP) · airframe 62,883 hrs · 45,830 cycles

DURING CHECK DENTS ON INBD FIXED VANE, RT WING INBD FLAP WAS FOUND DELAMINATED UPPER SKIN BETWEEN BS XIVIF=63 TO XIVIF=67. INBD FIXED VANE, RT WING INBD FLAP WAS REPLACED IAW SRM 57-03, PAR 11 DUE SEVERAL DAMAGE.

Part: PIN — DETACHED (L1 DOOR SLIDE) · airframe 62,384 hrs · 45,510 cycles

MAINTENANCE FOUND PIN OUT OF L1 DOOR EMERGENCY ESCAPE SLIDE. THE SLIDE RAFT WAS REPLACED.

Part: PIN — UNSECURE (L1 DOOR SLIDE) · airframe 61,749 hrs · 45,026 cycles

ACFT MAINTENANCE FOUND L1 SLIDE PARACHUTE PIN IS NOT ENGAGED. 1L DOOR SLIDE WAS REPLACED.

Part: PIN — OUT OF TOLERANCE (TAILCONE) · airframe 61,314 hrs · 44,714 cycles

DURING TAILCONE RELEASE CHECK, FOUND DIMENSION AT LEVER TO PIN OUT OF TOLERANCE. FOUND EXCESSIVE PLAY IN AFT PAX ENTRY DOOR LOWER HINGE PLATES.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,235 hrs · 44,662 cycles

LEFT SIDE UPPER AFT HORIZONTAL SKIN PANEL HAS INDICATION ON LFEC INSPECTION. APPROXIMATELY 1" LONG. CRACK INDICATION CONFIRMED IAW NDTSPM 06-10-02.005. COMPLIED WITH PRI 537341-14AD, REV O. TEMPORARY REPAIRED IAW ER/A 537341-14AD, REV ORIG.

Part: SKIN — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 59,237 hrs · 43,273 cycles

DURING WALKAROUND, FOUND FWD RADIO ALTIMETER ANTENNA WITH PULLED RIVETS IN SKIN WITH POSSIBLE CORROSION. FWD RADIO ALTIMETER ANTENNA REMOVED IAW AMM 34-42-01. REMOVED INTERNAL ANTENNA DOUBLER AND INTERNAL FINGER DOUBLER. DRILLED NEW ANTENNA DOUBLER AND FINGER DOUBLER IAW DWG 5911412. INSTALLED NEW DOUBLERS IAW DWG 5911412, CLOSED FLOOR PANEL AND REINSTALLED ANTENNA IAW AMM 34-42.

Part: PIN — DETACHED (L1 DOOR SLIDE) · airframe 58,096 hrs · 42,471 cycles

DURING LINE CHECK, NOTED THE L1 DOOR EVACUATION SLIDE PARACHUTE PINS HAD BECOME DETACHED. REPLACED L1 DOOR SLIDE IAW WC 2500-4484 AND COMPLIED WITH REQUIRED INSPECTION.

Part: SKIN — DENTED (BS 583) · airframe 57,912 hrs · 42,337 cycles

FUSELAGE DENT AT BS 583, L21R. FOUND TO BE OUT OF LIMITS, CUT DAMAGE AREA, FABRICATED DOUBLER REPAIR & FINGER DOUBLER. TREATED, PRIMED, TOP COATED & INSTALLED REPAIR PARTS IAW SRM 53-04-01 PARA 7, 53-34-0 FIG 2, 53-04-2, FIG 2, 53-10-02, 51-10-3, 51-10-08 & NDTSPM PART 6, 06-10-01.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 57,626 hrs · 42,115 cycles

DURING LINE CHECK, NOTED EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE FROM SEAT ROW 31 TO 36. REPLACED EMERGENCY LIGHT BATTERY PACK AND OPS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 56,784 hrs · 41,515 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY LIGHTING AT SEATS 22 AND 24D IN THE CABIN WAS INOPERATIVE. MX REPLACED THE LIGHT ASSEMBLIES AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THEM.

Part: PIN — OUT OF POSITION (L1 DOOR SLIDE) · airframe 55,992 hrs · 40,917 cycles

DURING A ROUTINE LINE CHECK, MECHANIC NOTICED THAT THE SLIDE INFLATION PIN WAS NOT VISIBLE THROUGH THE PRESSURE GAUGE WINDOW. L1 DOOR SLIDE REPLACED IAW WC 2500-4484.

Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 55,124 hrs · 40,300 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 16-20 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 54,615 hrs · 39,932 cycles

EMERGENCY CEILING LIGHT AT L1 DOOR INOPERATIVE. ATTACHED WIRE TO TERMINAL STRIP AND TESTED OK.

Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 54,615 hrs · 39,932 cycles

EMERGENCY PATH LIGHT AT SEAT 22D INOPERATIVE, ATTACHED CONNECTOR AND TESTED.

Part: SKIN — CRACKED (BS 1418 RBL 10) · airframe 54,210 hrs · 39,616 cycles

FUSELAGE CROWN SKIN BS 1418 RBL 10 CRACKED. REPAIRED PER ER/A 506416-14AD BY CUTOUT AND INSTALLATION OF TITANIUM DOUBLER.

Part: DOUBLER — CORRODED (BS 1307 L22L) · airframe 54,210 hrs · 39,616 cycles

AFT LAV SERVICE PANEL LOWER SERVICE PANEL PILLOWING CORROSION. CONTAINED CORROSION FOUND TO BE OUT OF LIMITS. INSTALLED REPAIR DOUBLER AND TRIPLER PER ER/A 506434-14.

Part: SKIN — CRACKED (BS 1418 LBL 10) · airframe 54,210 hrs · 39,616 cycles

FUSELAGE CROWN SKIN STA 1418 LBL 10 CRACKED. REPAIRED PER ER/A 506417-14AD BY CUTOUT AND INSTALLATION OF TITANIUM DOUBLER.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 53,003 hrs · 38,816 cycles

DURING SERVICE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS ON AFT SECTION OF PASSENGER SEATS AND TAIL COMPARTMENT INOPERATIVE. REPLACED AFT BATTERY PACK PER AMM AND OPERATION CHECKS GOOD.

Part: ENGINE — MALFUNCTIONED (NR 2) · airframe 52,826 hrs · 38,683 cycles

FLIGHT DIVERTED DUE TO THE RIGHT ENGINE NEEDING TO BE SHUT DOWN FOLLOWING COMPRESSOR STALL WITH LOSS OF OIL QUANTITY. UPON ARRIVAL, MAINTENANCE FOUND 4TH STAGE TURBINE DAMAGE, THRUST REVERSER DAMAGE, AND OIL IN THE TAIL PIPE. THE ENGINE WAS REPLACED.

Part: COFFEEMAKER — MALFUNCTIONED (GALLEY) · airframe 52,289 hrs · 38,332 cycles

THE COFFEEMAKER SKILLET, IN THE FIRST CLASS GALLEY, MELTED TO THE HOT PLATE AND CAUSED A BURNT ODOR IN THE CABIN. FLIGHT CREW HAD TO PULL AND SECURE THE CIRCUIT BREAKERS FOR THE COFFEEMAKER. FLIGHT CONTINUED TO SCHEDULED DESTINATION AND LANDED WITHOUT FURTHER INCIDENT.

Part: BATTERY — DISCHARGED (CABIN) · airframe 52,124 hrs · 38,206 cycles

DURING LINE CHECK, MAINTENANCE FOUND BOTH LEFT AND RIGHT AFT OVER WING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REMOVED AND REPLACED BATTERIES. OPERATION CHECKS GOOD.

Part: UNKNOWN — ODOR (COCKPIT & CABIN) · airframe 51,998 hrs · 38,117 cycles

FLIGHT TURNED BACK DUE TO AN UNIDENTIFIABLE ODOR IN THE COCKPIT AND A SMOKE SMELL IN CABIN DURING CLIMB. DECLARED EMERGENCY BY ATC. MAINTENANCE FOUND EVIDENCE OF A BIRD STRIKE IN THE NUMBER 1 ENGINE. ENGINE WAS BORESCOPED AND NO RESTRICTIVE ITEMS FOUND. RAN BOTH ENGINES TO TAKEOFF POWER, ONE AT A TIME, TO ISOLATE SMELL. RAN PACKS HOT, WITH NO ODOR FROM EITHER SIDE. AIRCRAFT OKAY FOR SERVICE.

Part: THRESHOLD — CORRODED (FUSELAGE) · airframe 51,189 hrs · 37,549 cycles

C3 THRESHOLD CORRODED BETWEEN 25 -50 PERCENT OF THE THICKNESS. REMOVED CORROSION AND REPAIRED THRESHOLD PER SRM 53-05 FIG 123.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 50,373 hrs · 37,047 cycles

DURING LINE CHECK, MX FOUND EMERGENCY EXIT LIGHT AT ROW 15 INOPERATIVE. MX FOUND CONNECTOR DISCONNECTED AT SEAT HARNESS AND RECONNECTED IT. OPS CHECKS GOOD.

Part: SUPPORT — DAMAGED (MLG) · corrosion level 2 · airframe 49,347 hrs · 36,356 cycles

SCRATCHES AND PITTING CORROSION ON THE GEAR SUPPORT FITTING BUSHING BORE AND THE BOTTOM BUSHING BORE AREA LW. SCRATCHES AND PITTING WERE BLENDED OUT IAW 51-02D PARA 1 A(6),PS900-2-4-1 NO 01,AMR 0957306 REV2, AMR 0957306, REV 3 STEP 4B AND TREATED IAW 51-10-3.

Part: SUPPORT FITTING — CORRODED (LT WING MLG) · corrosion level 2 · airframe 49,347 hrs · 36,356 cycles

CORROSION ON LT GEAR SUPPORT FITTING BEARING BORE OTBD FACE LT WING. PITTING CORROSION WAS BLENDED OUT IAW SRM 51-02 D, EA 09-093855-03, AD 0104 AND TREATED IAW SRM 51-10-3.

Part: BEAM — CORRODED (DOOR FRAME) · airframe 49,347 hrs · 36,356 cycles

EXFOLIATION CORROSION ON LOWER DOOR JAMB BEAM REPAIR MRB 53-017-02. LOWER DOOR BEAM REPAIR PARTS WERE REMOVED IAW SRM 51-30-2 AND SRM 51-30-2. CORROSION WAS REPAIRED IAW SRM 53-05, FIG 804. NEW DOUBLERS WERE INSTALLED IAW SRM 53-05, FIG 804.

Part: SUPPORT — DAMAGED (LT MLG) · airframe 49,347 hrs · 36,356 cycles

SCRATCHES ON LT GEAR SUPPORT FITTING BEARING BORE. SCRATCHES ON BORE WHERE CLEANED UP IAW EA 09-093855-03AD SRM 51-02 PARA 1A (6)(A)AND TREATED IAW SRM 51-10-3.

Part: CLAMP — WORN (TAILCONE) · airframe 49,347 hrs · 36,356 cycles

WORN CLAMP TAILCONE RELEASE CONTROL CABLE LT SIDE. REMOVED CLAMP IAW AMM 53-53-00-501 AND NEW CLAMP INSTALLED IAW AMM 53-53-00-501. OPS CHECK WAS DONE.

Part: SUPPORT FITTING — CORRODED (MLG) · corrosion level 2 · airframe 49,347 hrs · 36,356 cycles

SCRATCHES AND PITTING CORROSION ON RT GEAR SUPPORT FITTING BUSHING BORE ALSO DEEP DEPRESSION ON AFT MID SECTION OF SAME BUSHING BORE. BORE HOLE REWORKED IAW AMR 0957306, REV 2, REPAIR INST 2. FINAL DIAMETER 2.4560", BOTTOM FLANGE THICKNESS 1.1110". BEARING INSTALLED ON OPN 0204, CARD E 186.

Part: FRAME — CRACKED (BS 886) · airframe 49,347 hrs · 36,356 cycles

CRACK WAS FOUND ON UPPER RADIUS OF THE FRAME TAB OF THE OVERWING FRAM AT STA 886 RT REF EA 09-460094-12, AD OPN NR 0104. CRACKED FRAME WAS REMOVED IAW SRM 51-30-2 AND NEW FRAME WAS INSTALLED IAW SR09530282, REV ORG REF ALL AM NRCS T0180442,T0181246,AND T0181254.

Part: SKIN — CORRODED (HORIZONTAL STAB) · corrosion level 2 · airframe 49,347 hrs · 36,356 cycles

CORROSION ON BARREL NUT 2EA OF RT HORIZONTAL STABILIZER UPPER SKIN STA XH=27 REF NRC T0180054 VHS MRB 55-056-02. REPAIR WAS ACCOMPLISHED IAW AMR 0955139, REV1 AND ERA 483916-14 REV ORIG.

Part: FASTENER — IMPROPER PART · airframe 49,347 hrs · 36,356 cycles

LOCK FASTENER INSTALLED ON POSITION 48 IS NOT PN HLT 427-6 AS STATED ON VA 71126AD OF EA 09-460094-12AD, REV A ME-03 OPN 0302 STEP 15. INCORRECT FASTENERS WERE REMOVED IAW SRM 51-30-5 PAR 8 AND CORRECT FASTENERS WERE INSTALLED IAW 51-30-5 PAR7.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 49,347 hrs · 36,356 cycles

NICK ON LT ELEVATOR TAB T/E APROX XHS=35 (VHS). NICK ON LT ELEVATOR TAB WAS REPAIRED IAW AM OPN NR 1031, 1337 TO 1345 AND SRM 55-04 PARA 3 (3).

Part: SKIN — DAMAGED (FUSELAGE) · airframe 48,598 hrs · 35,861 cycles

DENT IN FUSELAGE RT SIDE JUST BEHIND RADOME. GROUND DAMAGE CAUSED BY ACS. REPAIRED ALL DAMAGE IAW ERA 481137-14. REPLACED FUSELAGE SKIN, REPLACED DAMAGED FRAME AND INSTALLED FLUSH DOUBLER REPAIR.

Part: LINE — LEAKING (APU OIL SYSTEM) · airframe 40,322 hrs · 30,549 cycles

ON TAKEOFF AND ENGINE START ODOR FROM A/C SYSTEM CAUSED SMOKE DETECTORS IN REAR TO GO OFF. ODOR DISSIPATED AFTER 15 MINUTES BUT STILL LINGERS A BIT IN CLIMB. FOUND APU OIL LINE B NUT LOOSE. TIGHTENED SAME LEAK CKS GOOD CLEANED INLET. PERFORMED PHEN SYS DUCT BURNOUT OP 5089. OK FOR SVC.

Part: CLAMP — FAILED (DUCT) · airframe 39,018 hrs · 29,662 cycles

CLIMBING OUT OF FL320, FLOW LIGHT ILLUMINATED. CABIN WAS CLIMBING AT 1500 FPM. IMMEDIATE DESCENT AS STARTED. RIGHT PACK PRESSURE -0-, LEFT PACK PRESSURE 3500 PSI. RT PACK TEMP CONTROLLER AT 10 O'CLOCK POSITION, LEFT WAS IN MANUAL COLD. CABIN PRESSURE WAS STILL UNCONTROLLABLE. EMERGENCY DESCENT MASK, PASSENGER, DEPLOYED. CABIN REGAINED AFTER LEVEL OFF. FOUND V-BAND CLAMP, RIGHT WATER SEPARATOR, FAILED. REPLACED CLAMP, SEPARATOR BAGS. LEAK CHECKS GOOD. CLAMP P/N U3452-9005.

Part: HARNESS — BROKEN (CABIN) · airframe 29,315 hrs · 22,935 cycles

ROW 24ED PAX EMERGENCY ESCAPE PATH ISLE INSEAT LIGHT (RED) INOP CA FND BROKEN HARNESS, REPAIRED SAME.

Part: BATTERY — OVERHEATED (E.E COMPARTMENT) · airframe 27,236 hrs · 21,350 cycles

AT APU START ATTEMPT ON GATE A LOUD BANG WAS HEARD UNDER TH E GALLEY - FOUND A/C BATTERY SWELLED - PROBABLE EXPLOSION

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 26,889 hrs · 21,079 cycles

BOTH FWD OVERWING EMERGENCY LIGHTS INOP. REPLACED POWER SUPPLY.

Part: APU — LEAKING (APU BAY) · airframe 24,244 hrs · 19,109 cycles

AIR TURNBACK. SMOKE IN CABIN AFTER T/O. FOUND APU OIL LEAK. REPLACED BOTH WATER SEP BAGS. PERF DUCT BURN OUT PER M/M. NO SMOKE PRESENT. REPLACED APU.

Part: STRUT — LEAKED (NLG)

UPON GEAR RETRACTION NOSE GEAR RED LIGHT STAYED ON. RECYCLED GEAR, NO HELP AND VERY NOISY. ON ARRIVAL FOUND NOSE STRUT BOTTOMED OUT. SERVICED NOSE STRUT PER M/M, NO LEAKS FOUND. REPLACED SCHRADER VALVE AS PRECAUTIONARY. JACKED NOSE PER M/M AND CYCLED NOSE GEAR, ALL INDS NORMAL.

Part: FAN — FAILED (CABIN)

AFTER T/O, F/A REPORTED A STRONG ELEC/CHEM ODOR COMING FROM THE AFT OF A/C. ODOR BECAME SO STRONG F/A COULD NOT GO AFT OF THE GALLEY. EMERGENCY LANDING BY CREW AT YYZ. CAPT REFUSED AIRCRAFT. CABIN RECIRC FAN FOUND TO HAVE INTERNAL DAMAGE. PLACARD PER MEL 21-00-43. C/BS J-8 J-9 J-10 PULLED AND COLLARED.

Part: STRUT — REQD SERVICE (NLG)

NLG WOULD NOT RETRACT. SERVICED NOSE STRUT.

Part: APU — LEAKING (AFT FUSELAGE)

AFTER T/O, CABIN FILLED WITH ENOUGH HAZE TO SETOFF ALL LAV SMOKE DETECTORS. FLT ATTENDANT REPORTED NO SMOKY SMELL, JUST HAZE IN CABIN, ALSO REPORTED ON SHORT FINAL WITH POWER CHANGES. FOUND APU OIL LEAKING INTO INLET FWD TO MCO/PLAC PER MEL 49-00-01A. RAN BOTH ENGINES AT TAKEOFF PWR. RAN PACKS ISOLATED BLEEDS, ALL CHECKED OK FOR SERVICE.

Part: JAMB — CORRODED (CARGO DOORWAY)

THE LOWER JAMB PAN OF THE C1 DOOR SURROUND LOWER SILL WAS FOUND CORRODED AND REQUIRED SPLICING. THE CORRODED SECTION WAS CUTOUT AND A NEW SECTION WAS SPLICED IN PER THE GUIDLINES OF THE MD-88 SRM 53-05, FIG 44 AND ER/A 364414-14.

Part: THRESHOLD — CORROSION (C1 DOOR)

CORROSION ALONG C-1 DOOR THRESHOLD SEVERAL PLACES. CLEANED CORROSION, FOUND TO BE OUT OF LIMITS PER SRM 53-01. REMOVED DAMAGED SECTION AND FABRICATED REPAIR DOUBLERS AND REPLACEMENT SECTION PER ERA 364414-14. FINISHED INSTALLATION PER ERA 364414-14.

Part: TURBINE — DAMAGED (NR 1 ENGINE)

ON CLIMB-OUT OF DCA AT 5,000 FEET AGL, THE NR 1 ENGINE STALLED. FLIGHT DIVERTED TO IAD. ENGINE DID NOT SHUT DOWN. MECHANIC REPORTED THE TURBINE WAS SEVERELY DAMAGED. ENGINE CHANGE IS IN WORK.

Part: LIGHT — INOPERATIVE (CABIN)

EXTERIOR EMERGENCY LIGHTS WOULD NOT TEST. REPLACED AFT RACK ASSY.

Part: LANYARD — DETACHED (L1 DOOR SLIDE)

L1 DOOR GIRT BAR HARD TO OPERATE. FOUND SLIDE PACK LANYARD DETACHED FROM SLIDE. REMOVED AND REPLACED SLIDE ASSY.

Part: EEL PWR SUPPLY — INOPERATIVE (CABIN)

EMERGENCY EXIT TRACK LIGHTING INOP BETWEEN ROWS 24 TO 38. REPLACED POWER SUPPLY, OPERATION NORMAL.

Part: HYD RESERVOIR — FAILED (LT HYD SYST)

IN CRUISE FL 330, LEFT HYD TEMP HI TEMP HI MSG ILLUM. PRESS/ QTY NORMAL. FOLLOWED POM PROC. WHEN LEFT SYSTEM REINSTATED, ZERO HYD PRESS, QTY-19. FOLLOWED LOSS OF HYD SYS PROCEDURES, RETURNED ATL. REPLACED HYD RESERVOIR, LEFT ELEVATOR RETURN CHECK VALVE, AND ELEVATOR BYPASS VALVE, OPERATION NORMAL.

Part: RIB — CRACKED (KEEL BEAM)

FOUND ON C2 LTR CK - CRACK LOCATED ON KEEL BEAM RIB AFT END REPAIR - REPAIRED PER SRM 53-05, FIG 101.