N904DL

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,588 hrs · 63,340 cycles

OVERHEAD CEILING EMERGENCY LIGHTS INOP AT SEATS 22-25. REMOVED AND REPLACED BATTERY PACK B5104 PER MD88 AMM 33-53. OPS CHECKS GOOD. (LP5037552)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,588 hrs · 63,340 cycles

COCKPIT AND FWD GALLEY OVERHEAD EMERGENCY LIGHTS INOP. REMOVED AND REPLACED BATTERY PACK B523. OPS CHECKS GOOD. (LP5037556)

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 82,588 hrs · 63,340 cycles

OVERHEAD EMERGENCY LIGHTS INOP AT L2 DOOR. REMOVED AND REPLACED BATTERY PACK B5-209. LIGHTS OPS CHECK GOOD REF MD88 AMM 33-53. (LP5037553)

Part: PIN — MISSING (TAILCONE) · airframe 82,340 hrs · 63,128 cycles

CANT. FRAME FOR TAILCONE ALL ALIGNMENT PINS FOR TAILCONE HAVE WASHERS ON AFT SIDE OF FRAME. ALIGNMT PIN MISSING AT 3:00 POSITION. FOUND SHIM WASHER ARRANGEMENT ON ALIGNMENT PINS TO BE DEPENDENT ON TAILCONE CLEARANCE CHECK AT EACH ALIGNMENT PIN LOCATION PER AMM 53-53. LOCATED ALIGNMENT PIN AND SHIM WASHER AND REINSTALLED PER AMM 53-53. (LP0795684)

Part: BATTERY — DISCHARGED (CABIN) · airframe 82,167 hrs · 62,969 cycles

DURING SERVICE CHECK MAINTENANCE FOUND THE MID CABIN UPPER EMERGENCY LIGHTS ON THE LEFT & RIGHT TO BE INOPERATIVE. MAINTENANCE REPLACED THE INBOARD MID CABIN UPPER LEFT AND RIGHT EMERGENCY LIGHTS BATTERIES PER MD-88 AMM 33-55. OPERATION NOW CHECKS GOOD.

Part: CONNECTOR — LOOSE (CABIN) · airframe 81,649 hrs · 62,531 cycles

EMERGENCY LIGHT ON SEAT 29D INOP. SECURED LOOSE WIRING CONNECTOR AND REPLACED MISSING LENS IAW AMM 33-53-01.

Part: BATTERY — MALFUNCTIONED (SMOKE DETECTOR) · airframe 81,126 hrs · 62,104 cycles

THE FWD LAVATORY SMOKE DETECTOR ACTIVATED, NO SMOKE OR FUMES NOTED. INSTALLED A NEW SMOKE DETECTOR BATTERY IAW AMM 26-13.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 81,077 hrs · 62,060 cycles

AFT ENTRY DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED THE LAMPS IAW AMM 33-53-00. OPS CHECKED GOOD.

Part: APU — CONTAMINATED · airframe 80,779 hrs · 61,833 cycles

DURING TAXI IN, AFTER APU START, NOTICED ODOR IN COCKPIT & FWD GALLEY, BURNING OIL ODOR. ODOR BECAME STRONGER AT GATE AFTER ENG SHUTDOWN. ON WALK AROUND, FOUND OIL BEING INGESTED INTO APU NON RAM DOOR INLET. PERFORMED CABIN SMOKE AND ODOR TROUBLESHOOTING IAW WORK CARD 2120- 2367. FOUND DEICING FLUID CONTAMINATION IN APU INLET. CLEANED THE APU INLET IAW WORK CARD 4900-1184. PERFORMED ALTERNATE DUCT BURN OUT IAW WC 4950-2215. REMOVED AND REPLACED BOTH COALESOR BAGS.

Part: POWER SUPPLY — BROKEN (CABIN) · airframe 80,275 hrs · 61,450 cycles

AFT CABIN FOUND EMERG LIGHT POWER SUPPLY B5-27 IN AFT RT LAV HAD A BROKEN TERMINAL BLOCK. REPLACED POWER SUPPLY AMM 33-53.

Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 80,275 hrs · 61,450 cycles

DURING SVC CHECK FOUND EXIT SIGN AT 2L DOOR, AFT STAIR DOOR, AND SEVERAL TAIL COMP EXIT LIGHT INOP. FOUND BATTERY PACK AND POWER SUPPLY B5-212 IN AFT RIGHT OVERHEAD BIN TO HAVE A STRONG BURNT ODOR. REPLACED B5-212 POWER SUPPLY.

Part: GAUGE — BROKEN (OXYGEN BOTTLE) · airframe 79,485 hrs · 60,791 cycles

BROKEN PRESSURE GAUGE ON PORTABLE OXYGEN CYLINDER S/N 587131 ALSO ON S/N 241191 AT CABIN PAX. REPLACED BY S/N 684325 AND 821117 DATE OF EXPIRATION 5/2019 AND 8/2019 P/N 9700C2CF20D. (LP 0160731)

Part: FRAME — CRACKED (BS 1418) · airframe 79,485 hrs · 60,791 cycles

CRACKED FRAME CAP AT BS 1418, LONGERON 2L IN THE AFT ACCESORIES COMPARTMENT. THE FRAME CAP WAS REPAIRED THE SRM 53-01, FIG 2. SHEET 4.

Part: DOOR FRAME — CRACKED (CARGO BAY) · airframe 79,485 hrs · 60,791 cycles

FOUR CRACKS ON LOWER AFT DOOR FRAME CORNER BETWEEN BS 416 TO 427 OF FWD CARGO COMPARTMENT. FUSELAGE SKIN AT FWD CARGO DOOR FRAME WAS REPAIRED IAW SRM 53-05, FIG 105.

Part: DOOR FRAME — CRACKED (LT MLG WW) · airframe 79,485 hrs · 60,791 cycles

FOUND LEFT MLG WHEEL WELL CUTOUT FWD LOWER FRAME CRACKED. CRACK IS MULTI DIRECTIONAL AND IS LOCATED APPROX 10 INCHES DOWN FROM UPPER ATTACH FITTING. STOP DRILLED CRACK TIPS PER MD88 SRM 51-01. PERFORMED 10X DETAILED VISUAL INSPECTION. ALL CRACKS CONTAINED TO STOP DRILL HOLES. REMOVED DAMAGED FRAME. INSTALLED REPLACEMENT FRAME DWG 5930584.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 79,458 hrs · 60,773 cycles

FWD OVERWING EXIT DOOR EMERGENCY LIGHT INOPERATIVE. REMOVED AND REPLACED THE POWER SUPPLY BATTERIES IAW AMM 33-53, OPS CHECKED GOOD.

Part: STIFFENER — DAMAGED (FUSELAGE) · airframe 79,407 hrs · 60,728 cycles

REMOVED STIFFENER ABOVE "Y" DUCT DUE TO DAMAGE. INSTALLED NEW STIFFENER PER AMM 53-01.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,308 hrs · 59,186 cycles

DURING EMERGENCY LIGHTS TEST, FOUND LT AND RT EXTERIOR LIGHTS INOPERATIVE. R & R B5-49 EXT EMERGENCY BATTERY PACK AND BATTERY IAW AMM 33-53. EXTERIOR EMERGENCY LIGHTS. CHECK NORMAL IAW AMM 33-53. ACFT OK FOR SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,282 hrs · 58,430 cycles

MAINTENANCE FOUND THE AFT ENTRANCE AND TAIL COMPARTMENT EMERGENCY LIGHTS INOPERATIVE. BATTERY PACK B5-212 WAS REPLACED AND THE LIGHTS CHECKED GOOD.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 76,282 hrs · 58,430 cycles

MAINTENANCE FOUND THE LT AND RT OVERWING EMERGENCY LIGHTS INOPERATIVE. THE BATTERY PACK WAS REPLACED AND THE LIGHTS CHECKED GOOD.

Part: RELAY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 76,249 hrs · 58,408 cycles

THE FLIGHT CREW OF FLIGHT 1798 FOUND THE OVERWING EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED RELAY R2-271 AND THE OVERWING EMERGENCY LIGHTS CHECKED OK.

Part: PIN — DISENGAGED (L1 DOOR SLIDE) · airframe 76,010 hrs · 58,222 cycles

MAINTENANCE FOUND THAT THE L1 DOOR EMERGENCY SLIDE HAD A PARACHUTE PIN DISENGAGED. THE L1 EMERGENCY ESCAPE SLIDE WAS REPLACED.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 75,987 hrs · 58,206 cycles

MAINTENANCE FOUND THE AFT SECTION EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE REPLACED THE BATTERY CHARGER FUSE AND THE LIGHTS OPERATED OK.

Part: SKIN — DAMAGED (HORIZONTAL STAB) · airframe 74,354 hrs · 57,047 cycles

DURING DECAL INSPECTION, FOUND SEVERAL SCRATCHES ON REPAIR DOUBLER OF LT HORIZONTAL STABILIZER L/E. AREA WAS REPAIRED IAW ER/A 531449-14, REV "C" SECTION 3.

Part: PIN — DAMAGED (ESCAPE SLIDE) · airframe 74,354 hrs · 57,047 cycles

MAINTENANCE DISCOVERED THAT THE RELEASE CABLE PIN FOR THE EMERGENCY ESCAPE SLIDE WAS UNSAFE. THE COMPLETE DOOR SLIDE ASSEMBLY WAS REPLACED.

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 74,354 hrs · 57,047 cycles

DURING NDT INSPECTION A DISCREPANT AREA, DOUBLER REPAIR WAS FOUND ON FUSELAGE SKIN AROUND CABIN WINDOWS CUTOUTS BETWEEN STA Y=693 AND Y=731. THE WINDOW BELT PANEL WAS REPLACED FROM STA Y=674 TO Y=750 FOR A NEW WINDOW BELT PANEL IAW ER/A 475245-14 REV "ORIGINAL" RESTRICTIONS, ITEM 4, PERMANENT REPAIR STEP 3, A AND DWG NR: 5932737, REV "P".

Part: GUIDE VANE — DELAMINATED (LT WING TE FLAP) · airframe 74,354 hrs · 57,047 cycles

FOUND A DELAMINATED AREA ON THE LT WIND INBD FLAP OTBD GUIDE VANE LOWER SURFACE. THE VANE WAS REMOVED AND REPLACED IAW AMM 27-51-04 AND AMM 27-51-04.

Part: ANGLE — CRACKED · airframe 74,354 hrs · 57,047 cycles

CRACKED ANGLE AND DOUBLER. REMOVED AND REPLACED THE ANGLE AND DOUBLER IAW SRM 51-30-2, 53-14-4 AND DWG 2923630, REV C, DWG 591842, REV D4, 51-10-3 PAR 14 AND 21 AND 51-30-5.

Part: PAN — CRACKED (BULKHEAD DOOR) · airframe 74,354 hrs · 57,047 cycles

CRACK ON OUTER PAN OF AFT CABIN BULKHEAD DOOR MID SECTION BELOW PRESSURE SEAL. THE BULKHEAD DOOR WAS REPLACED.

Part: SKIN — CRACKED (BS 1485) · airframe 74,354 hrs · 57,047 cycles

CRACK FOUND ON THE FUSELAGE SKIN BS 1485. THE SKIN WAS REPAIRED IAW ETI-88-15-258, ER/A 536515-14, REV ORIGINAL.

Part: SKIN — CORRODED (BS 489) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON INTERNAL FUSELAGE SKIN DOUBLER REPAIR BS 489, AROUND LONGERON 30. THE DOUBLER WAS REPLACED IAW ERA 536490-14, REV ORIG AND 57-10-3, P.21-14, 51-30-5 AND 51-30-2.

Part: SKIN — DAMAGED (BS 800-810) · airframe 74,354 hrs · 57,047 cycles

ELONGATED HOLES ON FUSELAGE SKIN UNDER REPAIR DOUBLER BETWEEN BS 800 - 810 LONGERON 28 - 30R. THE AREA WAS TRIMED, REPAIR FABRICATED, DRILLED, TRIMED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-5, SRM 53-04, SRM 51-10-4, AN DSRM 51-10-3, PAR 14 - 21.

Part: DOOR FRAME — CORRODED (BS 1145-1220) · airframe 74,543 hrs · 57,177 cycles

CORROSION ON WEB AROUND AFT CARGO DOOR JAMB FROM BS 1220 - 1145, LONGERON 29R TO 24R. FOUND TO BE OUT OF LIMITS. FABRICATED AND INSTALLED NEW WEB IAW SRM 51-10-03. 51-30-05 AND 51-30-02.

Part: SKIN — CRACKED (BS 371.5) · airframe 74,354 hrs · 57,047 cycles

A CRACK WAS FOUND ON FUSELAGE SKIN AT BS 371.5 BETWEEN LONGERONS 20 - 21R . THE SKIN WAS REPAIRED IAW SRM 53-05, FIG 105, 51-10-3, P. 21-14, AND 51-30-5.

Part: SKIN — CORRODED (BS 640) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON INNER DOUBLER, THE AREA OF RADIO ALTIMETER ANTENNA BS 640 BETWEEN LONGERON 29 - 30L. DOUBLER WAS REPLACED IAW SRM 51-30-5, 51-30-2 AND DWG 5936004, REV AM.

Part: FRAME — DAMAGED (BS 905) · airframe 74,354 hrs · 57,047 cycles

ELONGATED HOLE ON FRAME BS 905 LONGERON 17R. THE FRAME WAS REPAIRED IAW ETI-88-15-209, R4 & ER/A 536459-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 106) · airframe 74,354 hrs · 57,047 cycles

CRACKS FOUND ON THE FUSELAGE SKIN BS 106, LONGERON 28L AT NLG CUTOUT. THE SKIN WAS REPAIRED IAW SRM 51-30-02, 51-30-5, 51-10-3 PAR 21 AND 14, AND DWG 5913421, REV V.

Part: FRAME — CRACKED (BS 1463) · airframe 74,354 hrs · 57,047 cycles

CRACKED REPAIR DOUBLER ON FRAME BS 1463 LONGERON 18R. THE DOUBLER WAS REPLACED IAW SRM 51-30-5, 53-14-4, FIG 3, SHEET 7, 51-10-3 PAR 14 AND 21 AND DWG 9911839, REV DP.

Part: LONGERON — CORRODED (BS 1287) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION FOUND ON LONGERON 28R BS 1287. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — CORRODED (BS 1312) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON FUSELAGE SKIN REPAIR DOUBLER, BS 1312 LONGERON 22 - 23L. CORROSION BLENDED IAW ER/A 536476-14, REV ORIGINAL.

Part: SKIN — CRACKED (BS 1271) · airframe 74,354 hrs · 57,047 cycles

A CRACK WAS FOUND ON THE FUSELAGE SKIN BS 1271 BETWEEN LONGERONS 1 AND 2R. REPAIRED IAW ETI-88-15-216, REV ORIG AND ERA 536465-14AD, REV ORIGINAL.

Part: TAB — DAMAGED (LT ELEVATOR) · airframe 74,354 hrs · 57,047 cycles

NICKED AND DENTED LT ELEVATOR ANTIFLOAT 30. LT ELEVATOR ANTIFLOAT TAB, WAS REPAIRED IAW SRM 55-04.

Part: CARGO TRACK — CORRODED (BS 1212-1322) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CARGO TRACK BS 1212 - 1322 IN THE AFT CARGO BAY. THE CARGO TRACK WAS REPLACED IAW SRM 51-30-1 AND 51-10-3 PARA 14, NAD 21.

Part: FRAME — CRACKED (BS 750) · airframe 74,354 hrs · 57,047 cycles

CRACKED FRAME BS 750 BETWEEN LONGERONS 26 - 27L. THE FRAME WAS REPAIRED IAW SRM 51-30-2, 51-30-5 , 51-10-3, 51-10-4 AND 53-03D, FIG 4, CLASS A.

Part: SKIN — CORRODED (BS 1485) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON EXTERNAL FUSELAGE SKIN, BS 1485, CANT AND 8 O`CLOCK POSITION APPROXIMATELY. SECTION SKIN WAS REPLACE IAW SRM 51-10-3, 51-10-4, 51-30-2 AND DWG 5910228, REV K,H.

Part: PAN — CORRODED (SERVICE PANEL) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON PAN OF AFT LAVATORY SERVICE PANEL EXTERNAL FACE. PAN WAS REPLACED IAW DWG 5914792-3.

Part: SUPPORT — CRACKED · airframe 74,354 hrs · 57,047 cycles

CRACK ON SUPPORT ABOVE VENTRAL STAIRWAY TORQUE TUBE AND 7 HRS POSITION CLOCK. SUPPORT WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-10-4.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON INTERCOSTAL BS 1309 - 1322 AND BETWEEN LONGERON 27 - 28R. THE INTERCOSTAL WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: SKIN — CRACKED (BS 1418) · airframe 74,354 hrs · 57,047 cycles

CRACK ON FUSELAGE SKIN BS 1418 BETWEEN LONGERONS 1-2 RT SIDE. CRACK ON FUSELAGE SKIN WAS REPAIRED IAW ETI-88-15-205 AND ERA 536454-14AD, REV RIG. PERFORM INITIAL INSPECTION THRESHOLD 75,000, TOTAL CYCLES AND REPEAT INSPECTION INTERNAL TO BE DETERMINATED IAW ER/A NR 536454-14 AD, SEC II.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF THE RT WING FUEL ACCESS PANEL 1472C. CORROSION REMOVED SRM 51-22-2A AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: DOUBLER — CORRODED (BS 1307) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON TITANIUM DOUBLER INTERNAL STRUCTURE ON BS 1307 BETWEEN LONGERON 22 - 23L. DOUBLER INTERNAL WAS REPLACED IAW DWG 59911423-43.

Part: SKIN — CRACKED (BS 1271) · airframe 74,354 hrs · 57,047 cycles

FUSELAGE CROWN SKIN, BS 1271 L1-2R WAS CRACKED. REPAIRED IAW ER/A 536465-14AD,.

Part: FLOOR PANEL — CRACKED (BS 826) · airframe 74,354 hrs · 57,047 cycles

CRACKED FLOOR PANEL BS 826-1003. FLOOR PANEL FABRICATED AND REPLACED IAW AMM 53-20-01-201.

Part: SKIN — CORRODED (BS 765-775) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON REPAIR DOUBLER BETWEEN BS 765 - 775 AND LONGERONS 27 TO 29R ON FUSELAGE SKIN. REPAIR DOUBLER AND TRIPLER WERE REPLACED IAW SRM 51-30-2, 51-30-5, 53-04 FIG 57, 51-10-3, PAR 21 AND 14 AND 38.

Part: TEE FITTING — CORRODED (BS 1380) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON TEE FITTING IN THE AFT ACCESSORY BAY BS 1380 BETWEEN 27RT - 27 LT. THE TEE FITTING WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND DWG 9912246 LEAK CHECK WAS PERFORMED WITH CARD 3600-8310.

Part: FRAME — CRACKED (BS 1474) · airframe 74,354 hrs · 57,047 cycles

CRACK FOUND ON THE FRAME BS 1474 BETWEEN LONGERONS 17-18R. THE CRACK WAS STOP DRILLED IAW SRM 53-01, FIG. 2, AND A DOUBLER WAS INSTALLED IAW SRM 51-30-5.

Part: TEE FITTING — WORN (LG MLG WW) · airframe 74,354 hrs · 57,047 cycles

WEAR ON TEE FITTING IN THE LT MLG WHEEL WELL AFT DOOR FRAME XCW=58. THE TEE FITTING WAS REMOVED AND REPLACED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-3, PAR 21, 14. AND SRM 51-10-4.

Part: SKIN — CORRODED (BS 1322) · airframe 77,669 hrs · 59,461 cycles

CORROSION WAS FOUND ON THE FUSELAGE SKIN AT BS 1322 LONGERONS 21 AND 22L. ERA 536476-14 SECTION I-ACCOMPLISHED DURING H CHECK.

Part: FLOOR PANEL — CRACKED (BS 256-826) · airframe 74,354 hrs · 57,047 cycles

CRACK FLOOR PANEL FORWARD CABIN BS 256-826. FLOOR PANEL FABRICATED IAW AMM 53-20-01-201.

Part: LONGERON — CORRODED (BS 1309-1322) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON LONGERON 27 RT BETWEEN BS 1309 - 1322. LONGERON WAS REPLACED IAW SRM 53-02, FIG. 18, PAR 12, 51-30-2, 51-10-4 AND 51-10-3, PAR 14, 21 AND 38.

Part: FRAME — CRACKED (BS 1446) · airframe 74,354 hrs · 57,047 cycles

A CRACK WAS FOUND ON THE FRAME BS 1446 LONGERON 1. REPAIRED IAW SRM 51-30-2, 51-30-5 AND DWG 9911860, REV L.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 74,354 hrs · 57,047 cycles

CRACKED INTERCOSTAL BETWEEN BEAMS NR 4 - 5. INTERCOSTAL WAS REPLACED IAW SRM 51-30-2, LENGTH OF CRACK.

Part: ACCESS PANEL — CORRODED (NOT REPORTED) · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF THE FUEL ACCESS PANEL 1414C. THE CORROSION WAS REMOVED AND FOUND IN LIMITS, THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: SKIN — CORRODED (BS 1060-1079) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

SURFACE CORROSION ON FUSELAGE SKIN BETWEEN BS 1060-1079 LONGERONS 28L - 29R. CORROSION REMOVED IAW SRM 51-30-2, 51-10-3 PARR. 26. AREA WAS TREATED AND PAINTED IAW SRM 51-10-3 PARR/ 14 AND 21, WITHIN LIMITS IAW SRM 53-04-02.

Part: FRAME — CRACKED (BS 1446) · airframe 74,354 hrs · 57,047 cycles

A CRACK WAS FOUND ON THE FRAME ANGLE AT BS 1446 BETWEEN LONGERONS 1-3L. THE FRAME ANGLE WAS REPAIRED IAW SRM 51-30-2, 51-30-5, 51-10-3 AND DWG 9911860, REV L.

Part: ANGLE — CRACKED (VERTICAL STAB) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LT VERTICAL STABILIZER DORSAL ANGLE. ANGLE DORSAL WAS REMOVED IAW SRM 51-30-2 AND 51-30-5, NEW ANGLE DORSAL WAS DRILLED AND ADJUSTED IAW SRM 51-10-4, NEW ANGLE WAS INSTALLED IAW SRM 51-30-2 AND 51-30-5.

Part: SLIDE — CORRODED (AFT) · airframe 74,354 hrs · 57,047 cycles

WEAR ON AFT ACCCESSORY EMERGENCY ESCAPE SLIDE. BLENDED OUT IAW SRM 53-01, FIG 1, SHEET 3.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF THE ACCESS PANEL ON THE LOWER LT WING. THE CORROSION WAS REMOVED SRM 51-22-24, AND FOUND THE ACCESS PANEL OUT OF LIMITS IAW SRM 51-22-2A. THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL ON THE RT WING. THE CORROSION WAS REMOVED AND FOUND OUT OF LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,354 hrs · 57,047 cycles

LONGERON 16R BS 1437 IS CRACKED. THE LONGERON WAS REPLACED IAW SRM 53-14-4, 51-30-2, AND 51-30-5.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK OF LT WING FUEL ACCESS PANEL 1311C. THE CORROSION WAS REMOVED AND WAS MEASURED AND FOUND OUT LIMITS. THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2.

Part: TAB — CORRODED (RUDDER) · airframe 74,354 hrs · 57,047 cycles

DAMAGED METALLIZED OF RUDDER TAB CORRODED. THE RUDDER TAB WAS REPAIRED IAW SRM 51-70-1A, PAR 23.

Part: CUSP WEB — CORRODED (BS 825) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORRODED REPAIR DOUBLER ON THE RT CUSP WEB BS 825, X -58. THE CUSP WEB WAS REPLACED IAW SRM 51-30-2, 51-30-5, 53-05, FIG 131A-24 AND 51-10-3 PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF ACCESS PANEL ON LT WING . THE ACCESS PANEL WAS REPLACED IAW SRM 51-22-2A.

Part: ACCESS PANEL — CORRODED (LT WING) · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE ON THE LT WING. FUEL ACCESS PANEL WAS REPLACED IAW SRM 52-22-2A.

Part: FINGER DOUBLER — CORRODED (BS 579-598) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON INNER FUSELAGE SKIN BETWEEN BS 579 - 598 AND LONGERONS 25 - 26L. SPLICE AND FINGER DOUBLER WERE REMOVED IAW SRM 51-30-2, 51-30-5. DUE TO EXCESSIVE CORROSION IT WILL BE REPLACED IN DAMAGED AREA. FINGER DOUBLER WAS FABRICATED IAW SRM 53-04-2, FINGER DOUBLER WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21, 14. SPLICE AND FINGER DOUBLER WERE INSTALLED IAW SRM 51-30-2, 51-30-5.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LONGERON 12L, BS 1437. THE LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18, PAR 12. MAJOR REPAIR.

Part: SKIN — WORN (PAX DOOR) · airframe 74,354 hrs · 57,047 cycles

WEAR ON PREVIOUS REPAIR DOUBLER AT FWD PASSENGER DOOR LOWER EDGE SKIN. PREVIOUS REPAIR DOUBLER WAS REPLACED IAW SRM 52-05 "D" FIG 37 AND 51-30-2.

Part: BEAM — CRACKED (PAX DOOR) · airframe 74,354 hrs · 57,047 cycles

CRACKED BEAM NR 8 ON FWD PASSENGER DOOR AFT SECTION. THE BEAM WAS REPAIR IAW SRM 52-05 D, FIG 111.

Part: LONGERON — CORRODED (BS 1287-1322) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON LONGERON 28L, BS 1287 - 1322. REPAIRED IAW SRM 53-02, PAR 13, FIG 19. MAJOR REPAIR.

Part: FAIRING — DAMAGED (RUDDER) · airframe 74,354 hrs · 57,047 cycles

DAMAGE METALLIZATE OF RUDDER FAIRING. RUDDER FAIRING WAS REPAIRED IAW SRM 51-70-1 AD, PAR 23 AND A/C 0904, CARD 2000-8149-06, CREW 02, JIC 9629123, JOB 000-0028.

Part: STRUCTURE — PUNCTURED (APU BAY) · airframe 74,354 hrs · 57,047 cycles

PUNTURE AT APU COMPARTMENT HOIST ACCESS. FLANGE ASSY WAS REPLACED IAW SRM 51-30-2.

Part: SUPPORT — CRACKED (LT WING MLG) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LT WING MLG SUPPORT UPPER SURFACE. DAMAGE WAS REMOVED AND FILLER WAS FABRICATED AND AREA REPAIRED IAW SRM 57-03, FIG 35.

Part: INTERCOSTAL — BENT (BS 864) · airframe 74,354 hrs · 57,047 cycles

BENT INTERCOSTAL BS 864 BETWEEN LONGERON 10 - 11R. THE INTERCOSTAL WAS REPAIRED IAW SRM 53-01, HFEC INSPECT WAS ACCOMPLISHED NO CRACKS WERE FOUND.

Part: LONGERON — CRACKED (BS 275-408) · airframe 74,354 hrs · 57,047 cycles

CRACKED LONGERON 16L BS 408, 332, & 275. LONGERON AND SPLICE REPLACED IAW SRM. 51-30-5, 51-30-2, 53-02 , 51-10-3 .

Part: FRAME — CRACKED (BS 845) · airframe 74,354 hrs · 57,047 cycles

CRACK ON UPPER RADIUS OVERWING FRAME BS 845, RBL 57. THE FRAME WAS REPLACED IAW 5310-01415-0302.

Part: FLOOR PANEL — PUNCTURED (BS 120-256) · airframe 74,354 hrs · 57,047 cycles

PUNCTURED FLOOR PANEL 200C BS 120-256. FLOOR PANEL WAS FABRICATED IAW AMM 53-20-01-201 PAR 7.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1365C ON LOWER LT WING. THE ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1371C ON LOWER LT WING. THE FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT LOWER RT WING. THE FUEL ACCESS PLATE AT LOWER RT WING NR 1470C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTER SINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1335C ON UPPER LT WING. THE ACCESS PLATE WAS REPLACED.

Part: ANGLE — CRACKED (BS 939) · airframe 74,354 hrs · 57,047 cycles

CRACKED ANGLE BS 939, UPPER CORNER AT LT MLG MAIN DOOR. ANGLE WAS REPLACED IAW SRM 51-30-2, 51-10-3, PAR 14 AND 21 AND DWG 5930583, REV DA.

Part: LONGERON — CRACKED (BS 993) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LONGERON 20R BS 993 AFT END OF TRAP PANEL. DAMAGE AREA WAS TRIM OUT IAW SRM 53-02, FIG 21, DOUBLERS AND FILLER WERE FABRICATED IAW SRM 53-02, FIG 22, NEW DOUBLER AND FILLER WERE TREATED AND PAINTED IAW SRM 51-10-3, PAR 14/21 NEW DOUBLER AND FILLER WERE INSTALLED IAW SRM 51-30-5 LENGTH CRACK 1.062.

Part: LONGERON — CRACKED (BS 1380) · airframe 74,354 hrs · 57,047 cycles

CRACKED LONGERON 24L AT BS 1385. LONGERON WAS REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PANEL AT LOWER RT WING . THE ACCESS PANEL WAS REPLACED.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION FOUND ON FUEL TANK ACCESS PLATE 1456C COUNTERSINKS ON RT WING. THE FUEL TANK ACCESS PLATE WAS REPLACED.

Part: SEAT TRACK — DAMAGED (BS 824) · airframe 74,354 hrs · 57,047 cycles

ELONGATED HOLE ON LT SEAT TRACK, X 22, BS 824. SEAT TRACK WAS REPLACED IAW SRM 53-05, FIG 4F, 51-30-1 AND 51-10-3, PAR 14 AND 21.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREAOF FUEL ACCESS PLATE AT LOWER RT WING. THE FUEL ACCESS PLATE 1464C AT LOWER RT WING WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE1357C ON LOWER LT WING. THE FUEL ACCESS PLATE WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTENSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT LOWER LT WING. THE ACCESS PLATE LT WING NR 1363C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1355C ON LOWER LT WING. THE FUEL ACCESS PLATE WAS REPLACED.

Part: FLOOR SUPPORT — CRACKED (BS 905) · airframe 74,354 hrs · 57,047 cycles

FLOOR SUPPORT CRACKED BS 905 BELOW RT OTBD SEAT TRACK. FLOOR SUPPORT WAS REPLACED IAW SRM 51-30-5, 51-10-4 AND 51-10-3, P. 21, 14.

Part: CUSP WEB — CORRODED (BS 1060-1221) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CUSP WEB X -54 TO X -60 BETWEEN BS 1060-1221. THE DAMAGE WAS REMOVED AND A REPAIR FABRICATE, TREATED AND PAINTED AND INSTALLED IAW SRM 53-05, FIG 131A-7, 51-30-2 AND 51-10-3 P. 14, 21.

Part: FRAME — CRACKED (BS 1463) · airframe 74,354 hrs · 57,047 cycles

CRACK ON BULKHEAD FRAME WEB BS 1463 REPAIRED IAW SRM 51-70-4, FIG 1.

Part: FLOOR PANEL — DAMAGED (NOT REPORTED) · airframe 74,354 hrs · 57,047 cycles

CRACKED, DISBONDED, AND CORROSION ON FLOOR PANEL. REPAIRED IAW SRM 53-05, SRM 51-20-0, SRM 51-10-3, 8-26, 21, 14 AND ERA 511165-14, MA REV C.

Part: RIB — CRACKED (HORIZONTAL STAB) · airframe 74,354 hrs · 57,047 cycles

CRACK ON UPPER INBD RIB ON RT HORIZONTAL STABILIZER REMOVABLE, L/E INBD SIDE. REPAIRED IAW SRM 55-01, FIG 2, 51-10-3, P 14, 21 AND 51-30-2.

Part: SKIN — DAMAGED (RUDDER) · airframe 74,354 hrs · 57,047 cycles

DAMAGED METALLIZED COVER ON RUDDER BOTH SIDE SKIN. REPAIRED IAW SRM 51-70-1A, P.23.

Part: LONGERON — CRACKED (BS 408) · airframe 74,354 hrs · 57,047 cycles

CRACKED LONGERON 16R BS 408. SECTION LONGERON BS 380-436 WAS REMOVED AND REPLACED IAW SRM 51-10-4, 51-10-3, 51-30-2 AND 51-30-5, 53-02.

Part: LONGERON — CRACKED (BS 1437) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LONGERON 16L BS 1437. LONGERON SECTION WAS REPLACED IAW SRM 51-30-2, 51-30-5 AND 51-10-3.

Part: SKIN — DAMAGED (CARGO DOOR) · airframe 74,354 hrs · 57,047 cycles

WAVINESS IN SKIN OF FWD CARGO DOOR LOWER EDGE. SKIN WAS REPAIRED IAW SRM 52-05D, FIG 67.

Part: LONGERON — CRACKED (BS 160) · airframe 74,354 hrs · 57,047 cycles

CRACKED LONGERON 3L BS 160. LONGERON SECTION WAS REPLACED IAW SRM 51-30-2.

Part: LONGERON — CRACKED (BS 200) · airframe 74,354 hrs · 57,047 cycles

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

Part: CUSP WEB — CORRODED (BS 530-532) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

EXCCESIVE CORROSION ON LT CUSP WEB, BS 530-532. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-14.

Part: FLOOR PANEL — PUNCTURED (PAX CABIN) · airframe 74,354 hrs · 57,047 cycles

PUNCTURE ON FLOOR PANEL 1250E AT PAX CABIN. FLOOR PANEL WAS REPAIRED IAW SRM 51-70-10, PAR 10.

Part: CUSP WEB — CRACKED (BS 1112-1114) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CUSP WEB X -54 TO X-60 BETWEEN BS 1112 - 1114 . REPAIRED IAW SRM FIG 131-A.

Part: BEAM — CRACKED (PAX DOOR) · airframe 74,354 hrs · 57,047 cycles

CRACKED BEAM NR 2 ON FWD PASSENGER DOOR AFT SECTION. CRACKED BEAM WAS REPAIRED IAW SRM 52-05, FIG 83 AND SRM 51-30-2.

Part: RIB — CRACKED (VERTICAL STAB) · airframe 74,354 hrs · 57,047 cycles

CRACK ON RIBS FIX L/E VERTICAL STABILIZER, STA XFS= 42. REPLACED IAW SRM 51-30-2 AND 51-30-5.

Part: INTERCOSTAL — CRACKED (BS 769-788) · airframe 74,354 hrs · 57,047 cycles

CRACKED INTERCOSTAL X 0, BETWEEN BS 769 - 788. INTERCOSTAL WAS REPLACED SRM 51-10-4, 51-30-2 AND 51-30-5.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 74,354 hrs · 57,047 cycles

CRACKED FWD EDGE BRACKET INTERNAL STRUCTURE OF FWD LT EMERGENCY EXIT DOOR. REPAIRED IAW SRM 52-05D, FIG 51.

Part: CUSP WEB — CRACKED (BS 564) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LEFT CUSP WEB BETWEEN X 54 - 60 BS 564. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13, SHEET 1.

Part: CUSP WEB — CRACKED (BS 984-1003) · airframe 74,354 hrs · 57,047 cycles

CUSP WEB CRACKED BETWEEN BS 984 - 1003 AND X54 - 60. THE CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131-A, 51-10-3 P 14, 21 AND 51-30-2.

Part: CUSP WEB — CRACKED (BS 1207-1208) · airframe 74,354 hrs · 57,047 cycles

CRACK ON RT CUSP WEB X=-54 TO X=-60 BETWEEN STA Y=1207 TO 1208 CABIN FLOOR STRUCTURE. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-5.

Part: CUSP WEB — CRACKED (BS 797) · airframe 74,354 hrs · 57,047 cycles

CRACK ON RT CUSP WEB X -45 BS 797 AT PAX CABIN. CUSP WEB WAS REPLACED IAW SRM 51-30-1, 51-30-2 AND 51-10-4.

Part: CUSP WEB — CRACKED (BS 237-256) · airframe 74,354 hrs · 57,047 cycles

CRACKED CUSP WEB X 54 BETWEEN BS 237 - 256. REPAIRED IAW SRM 53-01, FIG 1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT UPPER RT WING 1410C. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-22-2. COUNTERSINK OF FUEL ACCESS PLATE WAS MEASURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .695, .739, .697 IAW SRM 51-22-2. FUEL ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0390, JOB 001-0394, STEP 13.

Part: BEAM — CRACKED · airframe 74,354 hrs · 57,047 cycles

CRACKED BEAM NR 4 AT FWD GALLEY SERVICE DOOR FWD SECTION. THE BEAM WAS REPLACED IAW SRM 51-30-2 AND 51-30-5. LENGTH CRACK .750".

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT LOWER RT WING 1460C. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-22-2. COUNTERSINK OF FUEL ACCESS PLATE NR 1460C WAS MEASURED AND FOUND OUT OF LIMIT WITH 3 ADJACENT HOLES .570, .550, .580 IAW SRM 51-22-2. FUEL ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0390, JOB 001-0394, STEP 5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1454C LOWER RT WING . CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE NR 1454C WAS REMOVED IAW SRM 51-22-2 COUNTERSINK OF FUEL ACCESS PLATE NR 1454C WAS MEASSURED AND FOUND OUT OF LIMITS WITH 3 ADJACENT HOLES .540, .544, .555 IAW SRM 51-22-2. FUEL ACCESS PLATE NR 1454C WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0390, JOB001-0394, STEP 3.

Part: PAN — CRACKED (CARGO DOOR) · airframe 74,354 hrs · 57,047 cycles

SEVERAL CRACKS ON INNER PAN OF FWD CARGO DOOR. REPAIRED IAW SRM 52-01, FIG 4, 51-30-2, 51-10-3 PAR 14/21.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE 1409, UPPER RT WING . BLENDED OUT OF THE ACCESS PLATE IS NOT PERMITED IAW SRM 51-22-2A. FUEL ACCESS PLATE NR 1409C WAS REPLACED.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTER SINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT UPPER LT WING NR 1307C. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-22-2A. FUEL ACCESS PLATE NR 1307C WAS MEASURED AND FOUND OUT OF LIMIT WITH 3 ADJACENT HOLES .770, .765, .770 IAW SRM 51-22-2A. FUEL ACCESS PLATE NR 1307C WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0120, JOB 001-0388, STEP 13.

Part: ACCESS PANEL — CORRODED (WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON CENTRAL FUEL TANK ACCESS PLATE 2302C, COUNTERSINKS. CORROSION ON COUNTERSINK OF CENTRAL FUEL TANK ACCESS PLATE WAS REMOVED FOUND 3 ADJACENT HOLES OUT OF LIMITS. ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 5730-0655, JOB 001-0416, STEP 5.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTERSINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT UPPER RT WING NR 1436C. CORROSION ON COUNTERSINK OF FUEL ACCESS PLATE WAS REMOVED IAW SRM 51-22-2. COUNTERSINK OF FUEL ACCESS PLATE WAS MEASURED AND FOUND OUT OF LIMIT WITH 3 ADJACENT HOLES .675, .662, .665 IAW SRM 51-22-2. FUEL ACCESS PLATE WAS REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0390, JOB 001-0394, STEP 15.

Part: ACCESS PANEL — CORRODED (LT WING) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON COUNTER SINK AND SETTLEMENT AREA OF FUEL ACCESS PLATE AT UPPER LT WING NR 1303C. BLEND OUT ON SETTLEMENT AREA OF FUEL ACCESS PLATE NR 1303C IS NOT PERMITED IAW SRM 51-22-2A. FUEL ACCESS PLATE NR 1303C WAS REPLACED FOR A NEW ONE AND WILL BE REPLACED FOR A NEW ONE AND WILL BE INSTALLED WITH JIC 2800-0120 JOB NR 001-03-88, STEP 13.

Part: CUSP WEB — CORRODED (BS 1220-1223) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CUSP WEB X -54 TO X -60 BETWEEN BS 1220 - 1223. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, 51-30-5 53-05, FIG 131A-5, SHEET 1 AND 51-10-3, PAR 21,14.

Part: SEAT TRACK — CORRODED (BS 246) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON SEAT TRACK, X 54, BS 246. DAMAGE WAS REMOVED IAW SRM 53-05, FIG 4A. REWORKED AREA WAS TREATED AND PAINTED IAW SRM 51-10-3, PAR 21,14. PLUG WAS INSTALLED IAW SRM 51-30-1, 53-05, FIG 4A CIC WAS APPLIED IAW SRM 51-10-3, PAR 38.

Part: CUSP WEB — CORRODED (BS 1137-1149) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CUSP WEB X=-54 TO X=-60 BETWEEN BS 1137 - 1149. CUSP WEB WAS REPAIRED IAW SRM 51-30-1, 51-30-5 53-05, FIG 131A-10, SHEET 1 AND 51-10-3, PAR 21,14.

Part: CUSP WEB — CORRODED (BS 1086-1096) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON RT CUSP WEB X -54 TO X -60 BETWEEN BS 1086 - 1096. CUSP WEB WAS REPAIRED IAW SRM 53-05, FIG 131A-6.

Part: DOUBLER — WORN (DOOR SKIN) · airframe 74,354 hrs · 57,047 cycles

WEAR ON DOUBLER SKIN OF AFT CARGO COMPARTMENT DOOR SKIN LOWER EDGE. DOUBLER REPLACED IAW SRM 51-30-2.

Part: CUSP WEB — CRACKED (BS 711) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LT CUSP WEB X 59, BS 711 AT PAX CABIN. DAMAGED AREA WAS REPAIRED IAW SRM 53-05, FIG 131A - 9.

Part: SKIN — WORN (CARGO DOOR) · airframe 74,354 hrs · 57,047 cycles

WEAR ON OUTER SKIN OF MID CARGO COMPARTMENT DOOR LOWER EDGE. PRODUCTION DOUBLER WAS REPLACED IAW SRM 51-30 -02, DWG 5910141.

Part: CUSP WEB — DEFORMED (BS 280) · airframe 74,354 hrs · 57,047 cycles

DEFORMED RT CUSP WEB BS 280 X -60. CUSP WEB REPAIRED IAW SRM 51-10-2, 53-05, FIG 131A-13, SHEET 1, 51-10-3, PARR 14-21 AND 51-30-2.

Part: PAN — CRACKED (BS 984) · airframe 74,354 hrs · 57,047 cycles

CRACK ON FORWARD LOWER CORNER RING PAN BS 984 AT RT SIDE. FASTENERS AND DAMAGE WERE REMOVED IAW SRM 51-30-2, 51-30-5 AND SRM 53-05. ANGLE, SHIM AND WASHER WERE FABRICATED IAW SRM 53-05, FIG 122 REPAIR, PART AND REWORKED AREA WERE TREATED AND PAINTED IAW SRM 5, SRM 3, PAR 14 AND 21. REPAIR PARTS WERE INSTALLED IAW SRM 53-05, 51-30-2,51-30-5 AND ER/A 333615-14.

Part: SEAT TRACK — CORRODED (BS 608-610) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON SEAT TRACK X 54. BS 608 - 610. PLUG WAS REMOVED IAW SRM 51-30-1, AND A NEW PLUG WAS INSTALLED IAW SRM 51-30-1, 53-05 FIG 4A.

Part: LONGERON — CRACKED (BS 1401-1437) · airframe 74,354 hrs · 57,047 cycles

CRACK ON LONGERON 13L, Y: 1437, 1401. HFWC INSPECTION WAS ACCOMPLISHED ON LONG 13LT, BS, Y: 1401. NO CRACKS FOUND OAW DC-MD NDT SPM 06-10-01.001, PHASE C 2D, GD-1041, 21 MAR 15, PARTS REPAIR WAS INSTALLED BS 1437 IAW SRM 53-02, FIG 18, 51-10-4, 51-10-3, PAR 14/ 21, 06-10-01.001.

Part: CUSP WEB — CORRODED (BS 1075-1271) · airframe 74,543 hrs · 57,177 cycles

CORROSION ON CUSP WEB RT BS 1250 - 1271, -54 TO -60, BS 1217 - 1219, X=-44 TO -54, BS 1131 -1133, 1079-1098 AND 1075-1076 UPPER/LOWER. BS 1217-1219 AND 1086- 1096 AREAS ARE OUT OF LIMITS.

Part: STOP FITTING — CRACKED (CARGO DOOR) · airframe 74,354 hrs · 57,047 cycles

CRACK ON STOP FITTING NR 4 OF AFT CARGO COMPARTMENT DOOR FWD EDGE. STOP FITTING NR 4 WAS REPLACEMENT IAW SRM 51-30-1, CRACK LONG: 0.125.

Part: FLOORBEAM — CORRODED (BS 255) · corrosion level 2 · airframe 74,354 hrs · 57,047 cycles

CORROSION ON FLOORBEAM, BS 255, BETWEEN X 22-44. THE FLOORBEAM WAS REPLACED IAW SRM 53-14-2.

Part: CUSP WEB — CRACKED (BS 224) · airframe 74,354 hrs · 57,047 cycles

CRACK ON RT CUSP WEB, BS 224, X -56. THE SEAT TRACK WAS REMOVED AND REPLACED IAW SRM 51-30-1, 51-30-5, 51-30-2, 51-10-4, PAR 21, 14.

Part: CUSP WEB — CRACKED (BS 469-471) · airframe 74,354 hrs · 57,047 cycles

CRACK ON CUSP WEB AT BS 469-471, X=-54 TO X=-60. CUSP WEB REPAIRED IAW SRM 53-05, FIG 131A-13.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,950 hrs · 56,113 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROWS 30-36 WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,875 hrs · 56,066 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTING FROM ROW 30 AND AFT IN THE CABIN WERE INOPERATIVE. MAINTENANCE REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPERATIONAL CONDITION.

Part: STRUCTURE — CORRODED (TAILCONE RELEASE) · airframe 70,969 hrs · 54,690 cycles

MAINTENANCE DISCOVERED THAT THE EMERGENCY ESCAPE PATH TAILCONE RELEASE CABLE HAD CORRODED HARDWARE. THE CLIPS WERE REPLACED, ADJUSTED, AND THE RII WAS SATISFACTORY.

Part: SKIN — DENTED (UNKNOWN) · airframe 70,969 hrs · 54,690 cycles

SKIN DENT FOUND OUT OF LIMITS IAW 53-04-1, PG 33, CONDITION 3A. INSTALLED REPAIR DOUBLER IAW SRM 53-04-3 FIG 3 SEALED AND PAINTED.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 70,969 hrs · 54,690 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE SYSTEM LATCH CABLE SAFETY PIN HOLE WAS WORN OUT OF ALLOWABLE LIMITS, IN THE PULLEY BRACKET. LOCATED ON THE LT 9:00 O`CLOCK POSITION. BRACKET REPLACED AND RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: BRACKET — WORN (TAILCONE RELEASE) · airframe 70,969 hrs · 54,690 cycles

MAINTENANCE DISCOVERED THAT THE TAILCONE RELEASE SYSTEM LATCH CABLE SAFETY PIN HOLE WAS WORN OUT OF ALLOWABLE LIMITS, IN THE PULLEY BRACKET. LOCATED ON THE LT 8:30 POSITION. BRACKET REPLACED AND RIGGED TO SPECIFICATIONS. THE RII STEPS WERE COMPLETED.

Part: BULKHEAD WEB — DAMAGED (BS 1338) · airframe 70,968 hrs · 54,690 cycles

BS 1338, BULKHEAD WEB, LBL 19 AND RBL 19 DAMAGED. REPAIRED IAW ERA 523105-14.

Part: FITTING — CORRODED (FUSELAGE) · airframe 77,629 hrs · 59,436 cycles

LONGERON END FITTINGS AT 29L AND 29R, CORRODED, REMOVED, REPLACED.

Part: FRAME — DAMAGED (BS 1338) · airframe 70,968 hrs · 54,690 cycles

AFT PRESSURE BULKHEAD, BS 1338, S-27L, LBL 19 FRAME ANGLE DAMAGED. REPAIRED IAW ERA 523098-14.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 70,049 hrs · 54,028 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING EXIT SIGN AT THE FWD OVERWING EXIT WAS INOPERATIVE. MX REPLACED THE BATTERIES IN THE POWER SUPPLY AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: FUSE — FAILED (EMERGENCY LIGHTS) · airframe 70,049 hrs · 54,028 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING IN ROWS 30-36 AND THE AFT LEFT EXIT SIGN OF THE CABIN, AS WELL AS IN THE TAIL COMPARTMENT WERE ALL INOPERATIVE. MX REPLACED A FAILED FUSE IN THE POWER SUPPLY. OPS CHECK WAS GOOD.

Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 69,930 hrs · 53,935 cycles

DURING ROUTINE LINE CHECK, SEVERAL CABIN EMERGENCY LIGHTS WERE FOUND TO BE INOPERATIVE AND ALSO WITH MISSING PROTECTIVE LENSES. THE INOPERATIVE BULBS WERE REPLACED ALONG WITH THE MISSING LENSES AND THE SYS CHECKED NORMALLY.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 69,846 hrs · 53,874 cycles

DURING LINE CHECK, MX FOUND THAT BOTH THE LT AND RT AFT OVERWING EMERGENCY EXIT SIGNS WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 69,664 hrs · 53,750 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY FLOOD LIGHTING FROM ROWS 20-23 OF THE CABIN WERE INOPERATIVE. MX REPLACED THE BATTERY PACK AND THE LIGHTS RETURNED TO AN OPS CONDITION.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 68,869 hrs · 53,182 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 33DE IN THE CABIN WAS INOPERATIVE. MX REPLACED THE LIGHT ASSY AND FUNCTIONALLY CHECKED IT.

Part: TERMINAL — BROKEN (EMERGENCY LIGHTS) · airframe 68,343 hrs · 52,832 cycles

DURING LINE CHECK, MX FOUND THAT THE SEAT MOUNTED EMERGENCY LIGHTING AT ROW 23D AND 25D INOPERATIVE. MX FOUND TERMINALS AT THE WIRE HARNESS CONNECTOR TO BE BROKEN. A NEW HARNESS WAS SPLICED IN AND A FUNCTIONAL CHECK OF THE SYS WAS GOOD.

Part: SKIN — LOOSE (VERTICAL STAB) · airframe 67,907 hrs · 52,572 cycles

VERTICAL STAB L/E SKIN LOOSE FASTENERS IN CENTER OF REPAIR. WHILE ACCOMPLISHING THE REPAIR TO THE SUBJECT VERTICAL STAB UPPER L/E, NINE (9) FASTENER HOLES COMMON TO THE THIRD ROW FROM THE LOWER EDGE WERE FOUND TO BE DAMAGED. COMPLIED WITH ERA 508630-14AD REV ORIG AND AMOC. REF NR CARDS 99 AND 287.

Part: SKIN — CRACKED (BS 1437) · airframe 67,900 hrs · 52,567 cycles

FUSELAGE SKIN CRACKED AT FASTENER BS 1437, RBL 12 ABOVE STR 3R. CUTOUT DAMAGE, NO CRACKS FROM CUTOUT. REPAIRED IAW ER/A 508460-14, REV ORIG.

Part: SKIN — CRACKED (BS 1437) · airframe 67,900 hrs · 52,567 cycles

SKIN PANEL HAS TWO CRACKS FROM ACCESS PANEL LOWER AFT CORNER BS 1437, 3 INCHES ABOVE FUSELAGE CROWN SKIN CRACKED EMPENNAGE. STOP DRILLED CRACK, HFEC IAW NDTSPM 06-10-01.001 NO CRACK FOUND STOP DRILL. INSTALLED REPAIR DOUBLER SRM 55-01, FIG 2.

Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHTS) · airframe 67,717 hrs · 52,438 cycles

DURING LINE CHECK, MX FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 10DE IN THE CABIN WAS INOPERATIVE. MX REPLACED THE WIRE HARNESS FOR SEATS 10DE AND FUNCTIONALLY CHECKED THE SYS.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 67,514 hrs · 52,273 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 26 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF THE SYSTEM.

Part: WIRE HARNESS — DEFECTIVE (CABIN) · airframe 66,888 hrs · 51,828 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 35 IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 66,530 hrs · 51,569 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY PATHWAY LIGHTING AT ROW 24DE IN THE CABIN WAS INOPERATIVE. MAINTENANCE REPLACED THE WIRE HARNESS CONNECTOR AND FUNCTIONALLY CHECKED THE SYSTEM.

Part: WIRE — BROKEN (CABIN) · airframe 65,263 hrs · 50,718 cycles

THE EEPL WIRE FOR SEAT 25E WAS FOUND TO BE BROKEN. MAINTENANCE REPAIRED THE WIRE WITH A SPLICE AND THE SYSTEM RETURNED TO OPERATIONAL STATUS.

Part: LIGHT — DISCONNECTED (CABIN) · airframe 64,574 hrs · 50,225 cycles

CREW FOUND EMERGENCY PATH LIGHT IN SEAT 25E DISCONNECTED AND ON THE FLOOR. CREW FORWARD LIGHT TO MCO PLACARD. MAINTENANCE REPLACED EMERGENCY LIGHT AT SEAT 25E AS PER MD88 AMM 33-53-01. OPERATION OF LIGHT CHECK OK. MCO PLACARD REMOVED.

Part: SPAR — CRACKED (WING) · airframe 64,277 hrs · 50,027 cycles

WING REAR SPAR CRACKED AT XRS 164. REPAIRED IAW AA 5710-01110.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHT) · airframe 63,311 hrs · 49,381 cycles

DURING LINE CHECK, MX FOUND EMERGENCY PATH LIGHTS AT SEATS 24-30, EXIT SIGNS AND, OVERWING EXIT SIGNS INOPERATIVE. MX REPLACED AFT LT OVERWING EXIT SIGNS, REPLACED BLOWN FUSES, CHECKED FOR SHORTED CABLES, AND CLEANED SEAT LIGHT CONNECTORS. ALL LIGHTS OPERATE NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 62,894 hrs · 49,077 cycles

DURING THE LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHT AT SEAT 3D TO BE INOPERATIVE. MAINTENANCE REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 3D. OPERATION OF LIGHT NOW CHECK OK. (2010-D1260) (DLM88102869)

Part: WIRE HARNESS — FAULTY (CABIN) · airframe 62,292 hrs · 48,668 cycles

MAINTENANCE FOUND THE EMERGENCY CABIN PATH LIGHTS AT SEAT 24DE TO BE INOPERATIVE. MAINTENANCE REPLACED THE EMERGENCY LIGHT WIRING HARNESS AT SEAT 24DE. AN OPERATIONAL CHECK WAS PERFORMED AND THE AIRCRAFT WAS RETURNED TO SERVICE (2010-D0899) (DLM88101963).

Part: LIGHT — INOPERATIVE (SEAT 30D) · airframe 61,769 hrs · 48,315 cycles

MX FOUND THE SEAT MOUNTED EMERGENCY LIGHT AT SEAT 30D TO BE INOPERATIVE. MX REPLACED THE LIGHT ASSY. AN OPS CHECK WAS PERFORMED AND THE ACFT WAS RETURNED TO SERVICE.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 61,334 hrs · 48,003 cycles

AFT OVERWING EMERGENCY EXIT INOP. REPLACED NICAD BATTERIES IAW MM. OPS CHECKS OK.

Part: CONNECTOR — DAMAGED (EMERGENCY LIGHT) · airframe 61,334 hrs · 48,003 cycles

SEATS 14 ED AND 25ED EMERGENCY ESCAPE PATH LIGHT INOP. REPLACED MALE END PLUG SEAT 14ED AND REPLACED FWD LIGHT ASSY AT 25ED. OPS CHECKS OK.

Part: DRUM — DAMAGED (COCKPIT) · airframe 59,826 hrs · 47,024 cycles

FLIGHT 1727/17 UNABLE TO PRESSURIZE ON DEPARTURE FROM JFK. CREW STATED THAT THE OUTFLOW VALVE WHEEL WAS STUCK. REPLACED CABIN PRESS CONT DRUM GEAR PER MM. SYS CHECKS GOOD. FULL TRAVEL OK.

Part: BEAM — CORRODED (CARGO DOOR FRAME) · airframe 59,768 hrs · 46,991 cycles

DURING HMV EXFOLIATION CORROSION WAS FOUND ON C2 LOWER DOOR JAMB BEAM. BEAM WAS REPAIRED IAW SRM 53-05 FIG 123

Part: DOOR FRAME — CORRODED (CARGO DOORWA) · airframe 59,768 hrs · 46,991 cycles

DURING HMV EXFOLIATION CORROSION WAS FOUND ON LOWER DOOR JAMB AT STAY=370 TO 427 AT C1 SECTION OF LOWER DOOR JAMB WAS REPLACED IAW SRM 53-05D FIG 804

Part: SKIN — DAMAGED (WINDOW BELT) · airframe 59,768 hrs · 46,991 cycles

DURING HMV LIGHTNING STRIKES WAS FOUND ON RT WINDOW BELT AT STA Y=930. WINDOW WAS REPLACED IAW ERA 475246-14 REV ORG

Part: STRUCTURE — DAMAGED (RUDDER) · airframe 59,768 hrs · 46,991 cycles

DURING HMV DAMAGED METALIZED ON RUDDER BOTH SIDES WAS FOUND RUDDER WAS REPAIRED IAW SRM 51-70-1AD PARAGRAPH 23

Part: SKIN — MISREPAIRED (FUSELAGE) · airframe 59,768 hrs · 46,991 cycles

DURING HMV AN INADEQUATE REPAIR WAS FOUND AT STA Y=300 TO 341 LONGERON 19-20 LT. REPAIRED AREA IAW SRM 53-04D FIG 12C

Part: ROD END — CORRODED (TAILCONE) · airframe 59,768 hrs · 46,991 cycles

DURING HMV4 CORROSION WAS FOUND ON ROD ENDS OF TAILCONE RELEASE MECHANISM STA 1510 CANT. SURFACE CORROSION WAS REMOVED AND TREATED IAW SRM 51-10-3

Part: SKIN — DAMAGED (BS 110-120) · airframe 59,768 hrs · 46,991 cycles

DURING HMV PROTUDING SKIN WAS FOUND AT STA Y=110-120 LONGERON 24-26 LT. PROTUDING SKIN WAS REPAIRE IAW SRM 53-04D FIG 12C

Part: SKIN — CRACKED (BS 175) · airframe 59,768 hrs · 46,991 cycles

DURING HMV A CRACK WAS FOUND OF 0.8" ON FUSELAGE SKIN AT UPPER FWD CORNER OF THE FWD SERVICE DOOR JAMB AT STA Y=175. FUSELAGE SKIN WAS REPAIRED IAW SRM 53-05 FIG 112.

Part: SKIN — CRACKED (BS 1431-1435) · airframe 59,768 hrs · 46,991 cycles

DURING HMV A CRACK WAS FOUND ON FUSALAGE SKIN AT STA Y=1431-1435 AND LONGERON 4-5 LT FUSALAGE SKIN WAS REPAIRED IAW SRM 53-04D FIG 27.

Part: ENGINE — DAMAGED (NR 1) · airframe 56,927 hrs · 45,148 cycles

NR 1 ENGINE FAILURE ON T/O ROLL, HIGH VIBE ENGINE SHUT DOWN HOT SECTION MISSING BLADES ETC. REMOVED AND REPLACED NR 1 ENGINE PER TRANS 9T102.

Part: CONTROL VALVE — UNSERVICEABLE (TE FLAPS) · airframe 53,596 hrs · 43,033 cycles

ON FINAL APPROACH, FLAPS WOULD NOT EXTEND PAST 11 DEGREES. SLATS EXTENDED TO T/O POS, SOME BINDING WHEN TRYING TO EXTEND FLAPS BEYOND 11. MTC IN PROGRESS. REMOVED AND REPLACED FLAP CONTROL VALVE PER MM. COULD NOT ADJUST. RII OF INSTALL ONLY. FLAP ACT BYPASS TEST AND ADJ OF CONTROL VALVE, WILL NEED RI OF ADJUSTMENT. PERFORMED FLAP CONTROL VALVE ADJUSTMENT PER MM. BLED LARGE AMOUNT OF AIR FROM BOTH FLAP HYD SYSTEMS. PERFORMED ACTUATOR BYPASS TEST ALL NORMAL NTF.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT) · airframe 46,291 hrs · 37,932 cycles

EMERGENCY LIGHTS FROM SEAT 31 AND AFT INOPERATIVE. REPLACED BATTERY PACK.

Part: POWER SUPPLY — INOPERATIVE (SEAT 31/38) · airframe 45,995 hrs · 37,740 cycles

EMERGENCY LIGHTS AT SEAT ROW 31DE THROUGH 38DE INOP. REPLACED POWER SUPPLY. CHECKS NORMAL.

Part: TIRE — DAMAGED (NR 4) · airframe 45,921 hrs · 37,683 cycles

NR 4 TIRE HAS CHUNK MISSING. REPLACED SAME.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 45,552 hrs · 37,424 cycles

ON INSPECTION FOUND AFT CABIN EMERGENCY SEAT ROW LIGHTS RT SIDE WOULD NOT TEST. REPLACED BATTERY AND PWR SUPPLY. OPS NORMAL.

Part: STRINGER — DAMAGED (FUSELAGE) · airframe 44,859 hrs · 36,972 cycles

SPLICE REPAIRS SEVERAL STRINGERS WERE FOUND WITH ELONGATED OR OVERSIZE HOLES AT THE INTERFACE WITH FS 1446 DUE TO LOCAL FRAME REPAIRS. THE DAMAGED SECTIONS OF STRINGERS WERE CUTOUT AND NEW SECTIONS WERE SPLICED. THE STRINGER SPLICES WERE MADE IN THE SAME FRAME BAY BETWEEN CANTED FS 1431 AND 1446. THE REPAIRS WERE ACCOMPLISHED IAW SRM AND IAW ER/A 385473-14.

Part: SENSOR — MALFUNCTIONED (NLG) · airframe 44,713 hrs · 36,869 cycles

RED NOSE GEAR LIGHT ON AFTER HANDLE PLACED UP POSITION. REPLACED NOSE GEAR UP SENSOR.

Part: WIRE — BURNED (POT WATER SWITCH) · airframe 44,456 hrs · 36,693 cycles

POTABLE WATER FILL/VENT VALVE C/B POPPING AND WILL NOT RESET FOUND POTABLE WATER SELECTOR SWITCH AND SOME ASSOCIATED WIRING CHARED. REPLACED SWITCH AND REPAIRED DAMAGED WIRING.

Part: CHARGER — FAILED (E/E BAY) · airframe 44,020 hrs · 36,388 cycles

CREW FOUND SMOKE COMING FROM TWO FUSELAGE HOLES FWD OF CTR E/E COMPARTMENT DURING PREFLIGHT INSPECTION. MTC AND FOUND BOTH SHIPS BATTERIES OVERHEATING AND VENTING THRU OVERBOARD VENT TUBES. REPLACED BOTH SHIPS BATTERIES, BATTERY CHARGER AND R2-50 RELAY. BATTERIES AND CHARGER CHECK NORMAL.

Part: POWER SUPPLY — SHORTED (CABIN) · airframe 41,081 hrs · 34,263 cycles

EMERGENCY SEAT EXIT LIGHTING INOP IN BACK HALF OF AIRCRAFT.

Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 39,839 hrs · 33,292 cycles

EMERGENCY ESCAPE AISLE LIGHTS ROWS 24-38 INOP. REPLACED AFT EMERGENCY LIGHT POWER SUPPLY.

Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 36,700 hrs · 30,982 cycles

FWD EMERGENCY FLASHLIGHT FOUND INOP BY CREW. REPLACED POWER PACK AND REINSTALLED SAME.

Part: POWER SUPPLY — INOP (CABIN)

FOUND FWD OVERWING E-PATH EXIT LIGHTS INOP AND BOTH LEFT AND RIGHT EXT OVERWING LIGHTS INOP. REPLACED POWER SUPPLY B5-104 AND OVERWING POWER SUPPLY AT STATION 1050L, OPS CHECK NORMAL PER MM.

Part: CONNECTOR — FAILED (ROW 18-21)

READING LIGHTS FLASHING IN ROWS 18 - 21. FOUND MID CABIN TRANSFORMER GROUND STUD 3491 BURNED. REPLACED TERMINAL END AND HARDWARE. SECURED WIRES, ALL LIGHTS CK GOOD.

Part: SKIN — CREASED (BS 332-351)

CREASE FOUND IN FUSE SKIN BETWEEN STA 332 AND 351 BETWEEN LONGERONS 24R AND 25R. TRIMOUT IS 19.5 BY 3.8. REPAIRED PER ERA 332691-14.

Part: POWER SUPPLY — INOPERATIVE (CABIN)

AFT PATH LIGHTS INOP. REPLACED POWER SUPPLY.

Part: SPRING — MISSING (STAB TRIM)

LEFT CAPTAINS AUTO PILOT COMMANDED AN UNCONTROLLED NOSE UP TRIM DURING CLIMB. ADDITIONALLY, IT COMMANDED A CLIMB WHEN LEVEL AT CRUISE. FOUND DETENT ROLLER SPRING MAIN HORIZONTAL STAB TRIM RELAY UPPER SPRING MISSING. REPLACED SPRING AND RAN STAB, OPERATION NORMAL.

Part: HOSE — LEAKING (RT HYD SYST)

LOST RT HYD SYS OTY THEN PRESSURE AFTER FLAPS WERE RETRACTED ON TAKEOFF. RETURNED TO ATL. GEAR WAS EXTENDED USING ALT EXTEND. REPLACED RT SYSTEM FILTER MODULE PRESSURE LINE. LEAK CKS GOOD, DL/PN 299201294.

Part: FRAME — CRACKED (LT MLG WW)

DURING C-2 LTR CK, FOUND LEFT WHEELWELL OUTBOARD FWD FRAME WITH 2 INCH CRACK. ACCOMPLISHED REPAIRS PER SRM 53-05 FIG 78A.

Part: TUBE — LEAKING (RT HYD SYST)

DURING CRUISE, HAD LOSS OF RT SYSTEM HYDRAULIC QUANTITY. TURNED SYSTEM OFF, RETURNED ATL. RE-POWERED SYSTEM FOR LANDING, LOST ALL FLUID AND PRESSURE ON BRAKE APPLICATION, AND ROLL-OUT. FOUND RT HYD PRESSURE LINE LEAKING, INSTALLED TEMPORARY LINE FOR RETURN TO SERVICE. PERMANENT LINE REPLACEMENT WAS SCHEDULED.