N313US

Part: CONNECTOR — MALFUNCTIONED (EMERGENCY LIGHT) · airframe 80,618 hrs · 36,692 cycles

WHILE PERFORMING EMERGENCY LIGHT TEST DURING SERVICE CHECK, HAD MULTIPLE MESSAGES INTERNAL LIGHT FAULT. DISCONNECTED & RECONNECTED R MIN CABIN EPSU CONNECTOR. TEST OK. OK ON EPSU AND FAP.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 80,293 hrs · 36,502 cycles

EMERGENCY LIGHT SEAT 5 LT INOPERATIVE, REPLACED THE LAMPS.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHT) · airframe 79,064 hrs · 35,891 cycles

SERVICE CHECK FOUND EMERGENCY LIGHTS TEST FAILED, REPLACED THE BATTERY.

Part: FRAME — CRACKED (FRM 16) · airframe 78,556 hrs · 35,662 cycles

FRAME 16 WAS FOUND CRACKED, PERFORMED TEMPORARY REPAIR IAW ER/A 551555-14AD REVISION ORIGINAL.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,552 hrs · 35,661 cycles

CORROSION ON STRINGER 31R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 31R IN AFT CARGO COMPARTMENT FROM FRAME 64 TO FRAME 67 AS PER SRM 51-72-11 AND DWG D53480020.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 78,552 hrs · 35,661 cycles

CORROSION ON STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FRAME 65 TO FRAME 66. REPLACED STRINGER 25R IN AFT CARGO COMPARTMENT BETWEEN FR 64 TO FR 67 AS PER SRM 51-72-11 AND DRAWING D53480020.

Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 78,552 hrs · 35,661 cycles

CRACK ON LATERAL FWD SEGMENT FRAME ON EMERGENCY EXIT DOOR 844 IN PASSENGER CABIN, REPLACED LATERAL FWD SEGMENT FRAME IAW SRM 51-72-11 AND DRAWING D52279010

Part: LIGHT — DAMAGED (CABIN) · airframe 75,147 hrs · 33,955 cycles

EMERGENCY SEAT MOUNTED LIGHT DAMAGED. REPLACED LIGHT ASSY.

Part: LIGHT — MISSING (CABIN) · airframe 71,989 hrs · 32,437 cycles

DURING NON-ROUTINE CHECK, FOUND SEAT 20A MISSING AISLE EMERGENCY LIGHT. MAINTENANCE REPLACED EMERGENCY LIGHT AND FUNCTIONAL CHECKED NORMAL.

Part: WIRE — PULLED (EMERGENCY LIGHTS) · airframe 71,466 hrs · 32,182 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY LIGHTS AT SEATS 08C-23C INOPERATIVE. MAINTENANCE FOUND WIRE PULLED FROM SPLICE AT EACH LOCATION. SPLICED WIRES BACK TOGETHER AND FUNCTIONAL CHECK WAS NORMAL.

Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 68,566 hrs · 30,731 cycles

DURING CRUISE EMERGENCY EXIT LIGHTS AND THE EMERGENCY AISLE LIGHTING WERE FLASHING ERRATICALLY ON AND OFF WITH EMERGENCY LIGHT SWITCH IN ARMED POSITION. MX REPLACED FWD LT EPSU AND BATTERY. FUNCTIONAL CHECKED NORMAL.

Part: EPSU — FAILED (EMERGENCY LIGHT) · airframe 68,508 hrs · 30,698 cycles

DURING NON ROUTINE CHECK, FOUND EPSU INTERNAL LOAD EMERGENCY LIGHT FAILED. MX REPLACED EPSU 10WL AND FUNCTIONAL CHECKED NORMAL.

Part: SHEAR TIE — CORRODED (FWD CARGO) · airframe 67,331 hrs · 30,103 cycles

DURING INSPECTION, FOUND FWD CARGO AT FR 31 BET CENTERLINE AND STR 43R, SHEAR TIE HAS CORROSION. CHECKED LIMITS L=1.00" W=1.00" D=0.010". NO ALLOWABLE DAMAGE IAW SRM 53-21-12. REMOVED AND INSTALLED FABRICATED SHEAR TIE ON STAM TRAVELER T13/982826 MAT 2024-0 .063C BATCH 1942022, HEAT.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FOUR FASTENER HOLES HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D52279040.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FRAME 55-56, STR 39-40R WEB PLATE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. FOUND TO BE OUT OF LIMITS IAW ER/A 484892-14MA DIMENSION L=1.80" W=2.00" D=0.047". FABRICATED COVER SHEET IAW STAM TRAVELER T13/979643. R & R WEB PLATE (COVER SHEET) IAW DWG D53475500 & SRM.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT FWD EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLES (5EA) HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" LENGTH OF CRACK, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D52279040, PN D5277902620200.

Part: FLOOR PANEL — CORRODED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 152KF IS CORRODED. REMOVED CORROSION IAW SRM 51-74-00, L=1.0" W=0.70" D=0.050 NO ESTABLISHED SRM LIMITS.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLES IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 5 1-44-11.INSTALLED NEW "T" SECTION IAW SRM 51-42-11 PAINTED FASTENERS IAW SRM 51-75-12. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS L=2.0" W=1.50" D=0.030". NO ALLOWABLE DAMAGE LIMITS IN SRM.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR LOWER AFT TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=.90" W=.80" D=.010" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSP, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOAD TRANSMITTING PROFILE (9EA) FASTENER HOLE HAS CRACKED. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .025" NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT AFT EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=2.0" W=1.5" D=.040" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.

Part: STRUCTURE — CORRODED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT FWD EMERGENCY EXIT DOOR, FWD LOWER TEE SECTION HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00 L=1.0" W=.70" D=.012" NO ALLOWABLE DAMAGE IN SRM. REPLACED T-SECTION PN D5227905420400 IAW SRM 51-42-11 AND DWG D52279040.

Part: STRUCTURE — CRACKED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, RT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE FASTENER HOLE HAS CRACK. HFEC IAW NTM 51-10-08 CRACK INDICATION NOTED .027" LENGTH OF DAMAGE, NO DAMAGE ALLOWED IAW SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D5227940.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO BAY FRAME 59 STR 44 FLOOR SUPPORT HAS CORROSION. REMOVED CORROSION NO LIMITS IN SRM 53-41-14 L=.5" W=.5" D=.020". REMOVED CORRODED PROFILE. LOCATED AND DRILLED NEW PROFILE. TREATED AND PRIMED HOLES IAW SRM 51-21-, INSTALLED NUTPLATES ON NEW PROFILE AND INSTALLED PROFILE IAW SRM 51-44-11, SRM 51-42-11 IPC 53-41-04, FIG 13. TOPCOATED FASTENERS IAW SRM 51-75-12.

Part: PROFILE — CRACKED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR, AFT LOAD TRANSMITTING PROFILE (4EA) FASTENER HOLES HAS CRACK. CRACK INDICATION NOTED .025" LENGTH OF DAMAGE, NO ALLOWABLE DAMAGE IN SRM. REPLACED LOAD TRANSMITTING PROFILE IAW SRM 51-42-11 AND DWG D52279040.

Part: FLOOR SUPPORT — CORRODED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FRAME 58-59, STR 44, FLOOR SUPPORT CORRODED. REMOVED AFT CARGO FLOOR SUPPORT IAW A320 SRM 51-42-11 FR 58-59 STR 44. REMOVED CORROSION IAW SRM 51-74-00 OUT OF LIMITS IAW SRM 53-00-14. NO ESTABLISHED LIMITS L=1.5"W=1.0"D=0.030". R & R FLOOR SUPPORT IAW SRM 51-42-11 & DWG 17 D53470014.

Part: STRUCTURE — GOUGED (LT NACELLE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE AFT GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW A320 TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.284" W=0.062" D=0.063"; AREA 2 L=0.299" W=0.049" D=0.053". FOUND TO BE OUT OF LIMITS IAW TRM 54-51-18 FIG 2. ACCOMPLISHED REPAIR IAW ER/A 509277-14, REV ORIGINAL. REPAIR APPROVAL IS LIMITED TO 6 MONTHS (182 DAYS) OF SERVICE.

Part: DOOR — CORRODED (EMERGENCY EXIT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT EMERGENCY EXIT DOOR FWD LOWER T SECTION HAS CORROSION. REMOVED OLD "T" SECTION IAW SRM 51-42-11. TREATED AND PRIMED HOLE S IAW SRM 51-42-11 LOCATED AND DRILLED NEW "T" SECTION IAW SRM 51-44-11. INSTALLED NEW "T" SECTION IAW SRM 51-42-11. PAINTED FASTENERS IAW SRM 51-75-12. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DIMENSIONS L=2.0" W=1.50" D=0.030". NO ALLOWABLE DAMAGE LIMITS IN SRM.

Part: FRAME SPLICE — GOUGED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT FR26 FRAME SPLICE AFT FACE IS GOUGED STR 35L. REPLACED FISH PLATE IAW SRM 51-42-11 DWG NR C2.D53230405. BLENDED FISH PLATE IAW SRM 51-73-00, L=2.0" W=1.5" D=1.5" NO ESTABLISHED LIMITS IN SRM.

Part: FRAME — GOUGED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO COMPT FR28 FRAME SPLICE AFT FACE IS GOUGED STR 35L. BLENDED FISH PLATE IAW SRM 51-73-00, MEASUREMENTS ARE L=1.5" W=.5" D=. 014, NO LIMITS FOUND IN SRM R & R IAW SRM 51-42-11.

Part: STRUCTURE — GOUGED (LT NACELLE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT PYLON PYRAMID MATING FACE MID GUIDE PIN HOLE HAS GOUGE. REMOVED GOUGE IAW TRM 54-51-18. CHECKED LIMITS: AREA 1L=0.446" W=0.022" D=0.046"; AREA 2 L=0.338" W=0.047" D=0.080"; AREA 3 L=0.360" W=0.071" D=0.156". FOUND TO BE OUT OF LIMITS IAW TRM 54-51-18, FIG 1. ACCOMPLISHED REPAIR IAW ER/A 509277-14 REV, ORIGINAL. REPAIR APPROVAL IS LIMITED TO 6 MONTHS (182 DAYS) OF SERVICE ONLY.

Part: STOP FITTING — CHAFED (DOOR FRAME) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE FRAME 68 ROLLER STOP FITTING ON MID OUTER SURFACE HAS CHAFED. REPLACED ROLLER STOP FITTING AT LT AFT PAX ENTRANCE ON FRAME 68 IAW SRM 51-49-00 (TR14925 TORQUE WRENCH USED) DUE TO NO ESTABLISHED LIMIT FOUND IAW SRM 53-41-69.L=1.5" W=3/8"D=.032".

Part: FRAME — CORRODED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FRAME 55-58, STR 43L HAS CORROSION. REMOVED CORROSION IAW 51-74-00 FROM STRINGER 43L BET FRAME 55-58 AND FOUND NO ESTABLISHED DAMAGE LIMITS. DAMAGE DIMENSIONS L=2.5 "W=1.0" D=0.015". REPAIRED STRINGER IAW SRM 53-00-13, FIG 201. USING REPAIR PN DAN2001T79511, BATCH 1906340. FOLLOW ON INSPECTION REQD AFTER REPAIR EMBODIMENT AT 60000 FLIGHT CYCLES IAW SRI 53-00-13-2-001-00. TOTAL WT OF FABRICATED PARTS 0.800 LBS.

Part: SKIN — GOUGED (NR 4 SLAT) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT NR 4 SLAT LWR T/E SKIN HAS GOUGE 10" INBD OF SLAT TRACK NR 10. ACCOMPLISHED REPAIR IAW ER/A 509275-14 REV ORIGINAL AS PERMANENT REPAIR SECTION I. DAMAGE DIMENSIONS L=0.70", W=0.30", D=0.125". FOUND TO BE OUT OF LIMITS IAW SRM 57-40-00.

Part: STRINGER — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FRAME 56-57, STR 41L HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. CHECKED DAMAGE DIMENSION S L=5.0" W=1.0"D=0.012". NO ESTABLISHED LIMITS IN SRM. REPLACED STRINGER IAW SRM 51-42-11 AND DWG D53470345.

Part: FLOORBOARD — CRACKED (MID CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MID CABIN FLOORBOARD 232MF CORNER EDGE IS CRACKED. FLOORBOARD FABRICATED IAW SRM 53-02-00, FIG 209.

Part: FLOORBOARD — DELAMINATED (MID CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MID CABIN BETWEEN FR35 TO 36 MOST CENTER FLOORBOARD 241AF HAS DELAMINATION. REPLACED FLOORBOARDIAW AMM 53-12-12-400-001-A. FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209 & DWG 3D25-37498.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161 BF IS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-5019 AND DWG 3D25-37705. MISSING INSERTS & EDGE DELAMINATED.

Part: FLOOR SUPPORT — DAMAGED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 16-20 Y-254 UPPER FLANGE HOLES HAS CORROSION. REMOVED DAMAGE IAW SRM 51-74-00. DAMAGE MEASURES: AREA NR 1 L=1.8 W=1.2 D=.010, AREA NR 2 L=1.1 W=1.0 D=.015 NO LIMITS FOUND IN SRM. REPAIRED FLOORBEAM Y-254 BETWEEN FR 16-20 IAW SRM 53-00-14 PARA 4.F. FIG 206. REPAIR PARTS WT 3.02LBS.

Part: FLOOR PANEL — DAMAGED (AFT UTILITY) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261EF INSERTS DAMAGED. FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209. INSTALLED ON WC 2500-6602.

Part: SKIN — GOUGED (FUELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LOWER FUSELAGE JUST AFT OF FR 65 BETWEEN STR 28L - 29L SKIN APPEARS TO BE GOUGED UNDER PAINT. N/R 100/4. CUTOUT DAMAGED SKIN IAW SRM 53-41-11. DIM. L=1.78" W=1.75". FABRICATED DOUBLER FROM 2024T30.071 IAW SRM 53-41-11, FIG 214. INSTALLED DOUBLER IAW SRM 51-42-11 AND 53-41-11, FIG 214.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER DOOR SILL AT FWD FR68 GIRT BAR & INBD HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=1.5" W= 1.0" D=.110" AND FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14, FIG 101. REMOVED FLOORBEAM Y-1292 FROM FR64-FR70 FOR ACCESS IAW SRM 51-42-11. REPLACED R-2 DOOR SILL IAW SRM 51-42-11. RE-INSTALLED Y-1292 FLOORBEAM FROM FR64-70 IAW SRM 51-42-11. DOOR SILL INSTALLATION ACCOMPLISHED IAW DWG D53480020.

Part: FITTING — CORRODED (NR 1 NACELLE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND NR 1 ENGINE SPIGOT RECEPTACLE FITTING BORE AT UPPER SPAR HAS FITTING CORROSION. REMOVED CORROSION IAW SRM 51-74-00 FINAL DIAMETER FOUND TO BE OUT OF LIMITS OF 4.345 ALLOWABLE DIA 4.335 IAW SRM 54-51- 12, FIG 101. REMOVED FITTING IAW SRM 54-51-12. RECEIVED NEW REPLACEMENT FITTING AND PRIMED AND PAINTED NEW PART IAW SRM 51-75-12. TRANSFERRED ALL HOLE AND REAMED NEW FITTING IAW SRM 54-51-12 INSTALLATION OF BALL JOINT BEARING INSTALLED ON W/C 5450-6010-LT.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 261FF HAS CORROSION 4" X 6". REPLACED FLOOR PANEL IAW SRM 51-72-00.

Part: FLOOR PANEL — GOUGED (MAIN CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN FWD AREA FLOOR PANEL 231CF HAS GOUGE 3" X 2". FABRICATED FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN, FWD AREA FLOORBOARD 232DF HAS A HOLE .300" X .500". FABRICATED FLOORBOARD IAW SRM 53-02-00, FIG 209.

Part: WEB — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN RT SIDE STRINGER 23 BETWEEN FR 20 TO 21 UPPER SURFACE WEB CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED WEB IAW SRM 51-42-11.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 161FF IS DAMAGED (3" X 2") PN D5367204800000. N/R 100/69. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00 FIG 209.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152RF PUNCTURED (3" X 1") N/R 100/59. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOORBOARD — DAMAGED (MAIN CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOORBOARD 241JF IS DAMAGED AND MISSING INSERT. FABRICATED NEW FLOORBOARD IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131KF HAS EDGE DAMAGE. FABRICATED NEW SLOPE PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161AF HAS CORNER DAMAGE & EROSION AROUND TOP CUTOUTS. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — ERODED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152EF HAS EDGE EROSION AROUND TOP CUT OUT (9" X 4"). FABRICATED NEW SLOPE PANE IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — PUNCTURED (MAIN CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241LF HAS PUNCTURE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — ERODED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152QF HAS EDGE EROSION (4" X 1") N/R 100/62. FABRICATED NEW SLOPING WALL PANEL IAW SRM 53-02-00 FIG 209.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131BF HAS EDGE DAMAGE. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — PUNCTURED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131GF IS PUNCTURED. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 161DF HAS DAMAGE AT TOP CUTOUT. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131FF HAS EDGE DAMAGE. FABRICATED NEW SLOPE WALL PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DENTED · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN CENTER WING AREA FLOOR PANEL 241DF HAS INDENTION ON BOTTOM. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131EF HAS EDGE DAMAGE. FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: SILL — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE LWR DOOR SILL AT AFT FR66 GIRT BAR HOLES UPPER SURFACE HAS REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=2.0" W= 1.5" D=0.107". ORIG MAT 0.177. FOUND TO BE OUT OF LIMITS IAW SRM 53-41-14 FIG 101. R & R DOOR SILL IAW SRM 51-42-11.

Part: SHACKLE — DAMAGED (RT PYLON) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT PYLON AFT SHACKLE FWD PIECE, FWD FACE CHAFED AROUND THREE BUSHINGS. REPLACED WITH SERVICEABLE PART. SHACKLE INSTALLED ON W/C 5450-6010-RT DUE TO NO SPECIFIC ALLOWABLE DAMAGE SPECIFIED IAW SRM 54-51-17.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 162BF IS DAMAGED (3" X 12"). FABRICATED NEW PANEL IAW SRM 53-02-00 FIG 209.

Part: FLOOR PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO FLOOR PANEL 131AF HAS EDGE DAMAGED 3.0" X 3.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CARGO COMPARTMENT SLOPE PANEL 131CF IS DAMAGED. 1" X 1". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151GF IS DAMAGED, PN D5367205300000. 3" X 2.5". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: SEAT TRACK — CORRODED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN SEAT TRACK BETWEEN FR 20 TO FR 21 Y-765 UPPER CROWN HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. BLENDED AREA MEASURES L=3.330"W=.380"D=.037"ORG MAT .125". FOUND TO BE OUT OF LIMITS IAW SRM 53-00-15, FIG 101. R & R FLOORBEAM Y-765 FROM FR 12-24 IAW SRM 51-42-11.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 161EF HAS EDGE DAMAGE AROUND TDP CUT OUT (1" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (FWD CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FWD CARGO SLOPING WALL PANEL 131JF HAS EDGE DAMAGE 3.5" X 4.0". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INPECTION, FOUND AFT CARGO FLOOR PANEL 151LF IS DAMAGED, 4.0" X 4.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 152CF IS DAMAGED (8" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — PUNCTURED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151MF HAS PUNCTURE & EDGE EROSION A ROUND TDP CUT OUT (4" X 1"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151EF IS DAMAGED 4" X 1". FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151AF IS DAMAGED. 4.5" X 3.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO SLOPING WALL PANEL 151NF IS SOFT (3" X 2.5"). FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — DAMAGED (AFT CARGO) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CARGO FLOOR PANEL 151DF IS DAMAGED. 3.0" X 2.0". FABRICATED NEW FLOOR PANEL IAW SRM 53-02-00, FIG 209.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FLOOR PANEL 221FF HAS CORROSION ON BOTTOM AREA 3" X 1". NO ESTABLISHED LIMITS IAW SRM. REPLACED FLOOR PANEL.

Part: FLOOR PANEL — CORRODED (MAIN CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MAIN CABIN FWD UTILITY AREA FLOOR PANEL 222FF HAS CORROSION ON BOTTOM AREA 6" X 1". NO ESTABLISHED LIMITS IAW SRM. REPLACED FLOOR PANEL IAW SRM 51-72-00.

Part: FITTING — MISMANUFACTURED (PAX DOOR) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND RT AFT PASSENGER ENTRANCE LOWER MID FWD SHAPE FITTING EXISTING HOLES MISDRILLED. REMOVED DOORSILL SHAPE FITTING IAW SRM 51-42-11. RECEIVED NEW DOOR SILL SHAPE FITTING, PN: D5348004800104, BATCH 0002379438. LOCATED AND DRILLED SILL SHAPE FITTING IAW SRM 51-41-11. INSTALLED NEW SILL SHAPE IAW SRM 51-42-11. RETAIN FOR RECORDS.

Part: FLOOR PANEL — CORRODED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT UTILITY FLOOR PANEL 262FF HAS CORROSION. FLOOR PANEL REPLACED IAW SRM 51-72-00.

Part: HINGE PIN — DAMAGED (LT AILERON) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AILERON, HINGE PIN NR 3 SCORED. NEW LT AILERON NR 3 HINGE INSTALLED. SCORED NR 3 HINGE PIN FOUND OUT OF LIMITS PER AMM 27-14-41, PB 601.

Part: STRUCTURE — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND LT AFT PASSENGER ENTRANCE LOWER MID FWD SHAPE FITTING CORRODED. REMOVED CORROSION IAW SRM 51-74-00. REPLACED SHAPE SILL IAW SRM 51-42-11, L=4.0 W=2.0 D=.050.

Part: SEAT TRACK — GOUGED (MID CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND MID CABIN SEAT TRACK BETWEEN FR35-FR36 Y765 HAS GOUGE. REMOVED DAMAGE & FOUND TO BE OUT OF LIMITS IAW TRM 53-00-15, FIG 1, BOTTOM SURFACE. REPLACED Y765 SEAT TRACK BETWEEN FR35-FR36 IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN FLOOR SUPPORT BETWEEN FR20 TO FR23, Y-189 UPPER FLANGE CORROSION AND SCRIBE LINE MARKS. BLENDED FLOOR SUPPORT IAW SRM 51-74-00 AFTER REWORK, D=.024", L=1.5", W=.50". FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 104. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR64 TO FR66, Y765 UPPER FLANGE AND INSIDE HARD POINT HOLES HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00, BLENDED AREA MEASURES L=1.83", W=1.80", D=.055", ORIG MAT 0,087 FOUND TO BE OUT OF LIMITS IAW TRM 53-41-15. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (CABIN) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR12 TO FR22, Y254 UPPER FLANGE HAS CORROSION. REMOVED CORROSION FROM FLOOR SUPPORT IAW SRM 51-74-00, AND CHECK LIMITS ORIG THICKNESS .141", L=7.20", W=1.30", D=0.51 FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 106. REPLACED FLOOR SUPPORT IAW SRM 51-42-11.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND AFT CABIN UTILITY AREA FLOOR SUPPORT BETWEEN FR 65-67, Y-308 INSIDE HARD POINT HOLES 3EA HAS SURFACE CORROSION. BLENDED AREA IAW SRM 51-74-00, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOOR SUPPORT IAW SRM 51-42-11,

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, FOUND FORWARD CABIN UTILITY AREA FLOORBEAM BETWEEN FR 12-16, Y503.2 UPPER FLANGE HAS CORROSION. REMOVED CORROSION IAW SRM 51-74-00. ORIG THICK .149" AFTER BLENDED .089" OUT OF LIMITS IAW SRM 53-11-15, FIG 105 L=1.7 W=1.4" D=.060" REMOVED FLOOR SUPPORT BEAM IAW SRM 51-42-11. INSTALLED NEW FLOOR SUPPORT BEAM Y503.2 FR12 - FR16 IAW SRM 51-42-11.

Part: FLOORBEAM — CORRODED (FUSELAGE) · airframe 67,330 hrs · 30,101 cycles

DURING INSPECTION, AFT CABIN UTILITY AREA FLOORBEAM AT FR 66, Y1292 UPPER FLANGE HAS CORROSION AND ELONGATED HOLE. REMOVED CORROSION IAW SRM 51-74-00. CHECKED LIMITS L=1.9" W=1.3" D=0.020" FOUND TO BE OUT OF LIMITS IAW SRM 53-00-14, FIG 102. REPLACED FLOORBEAM IAW SRM 51-42-11.

Part: CHARGER — FAULTY (EMERGENCY LIGHT) · airframe 66,552 hrs · 29,721 cycles

DURING NON ROUTINE CHECK, FOUND EMERGENCY BATTERY CHARGER UNIT FAULTING FWD LT. MX REPLACED EMERGENCY LIGHTS EPSU AND FUNCTIONAL CHECK WAS NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 6,353 hrs · 2,834 cycles

DURING NON ROUTINE CHECK, FOUND LT AFT EPSU UNIT FAULT TEST. MAINTENANCE REPLACED EPSU UNIT AND OPERATIONAL CHECK WAS NORMAL. AIRCRAFT WAS RETURNED TO SERVICE.

Part: LIGHT — WRONG PART (CABIN) · airframe 63,424 hrs · 28,265 cycles

DURING EMERGENCY LIGHT TEST ALL 4 EMERGENCY EXIT HANDLE LIGHTS WERE NOT WORKING. REPLACED BULBS NO HELP. FOUND WRONG BULBS INSTALLED, REPLACED BULBS AND TESTS OK.

Part: WIRE — BROKEN (CABIN) · airframe 631,442 hrs · 28,134 cycles

DURING NON-ROUTINE CHECK, FOUND THE EMERGENCY ESCAPE LIGHT AT 23C INOPERATIVE. MAINTENANCE REPAIRED BROKEN WIRE AND FUNCTIONAL CHECK WAS NORMAL. AIRCRAFT RETURNED TO SERVICE.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 61,852 hrs · 27,546 cycles

DURING EMERGENCY LIGHT TEST, FOUND LEFT FRONT BATTERY PACK INOP. BATTERY PACK WAS REPLACED AND TESTS OK.

Part: FLOOR PANEL — CRACKED (CARGO BAY) · airframe 61,124 hrs · 27,233 cycles

DURING L-CHECK, FOUND AFT CARGO COMPARTMENT FLOOR PANEL 151PF CRACKED. REMOVED FLOOR PANEL IAW AMM 53-42-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED NEW FLOOR PANEL IAW AMM 53-42-14 -000-0.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,124 hrs · 27,233 cycles

DURING L-CHECK FOUND FWD CARGO COMPARTMENT, ZONE 130 - FLOOR PANEL 131AF DELAMINATED. REMOVED FLOOR PANEL 131AF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AMM 53-22-14-000-001.

Part: FLOOR PANEL — DELAMINATED (CARGO BAY) · airframe 61,124 hrs · 27,233 cycles

DURING L-CHECK, FOUND FWD CARGO COMPARTMENT, ZONE 130 FLOOR PANEL 131EF HAS DELAMINATION. REMOVED FLOOR PANEL 131EF IAW AMM 53-22-14-000-001. FABRICATED NEW PANEL IAW SRM 53-02-00, FIG 209. INSTALLED PANEL IAW AM, M 53-22-14-000-001.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,995 hrs · 26,295 cycles

DURING A NON ROUTINE CHECK, FOUND EMERGENCY LIGHT AT 13WL INOPERATIVE. MX REPLACED POWER SUPPLY AND FUNCTIONAL CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 58,942 hrs · 26,277 cycles

DURING A NON ROUTINE CHECK, FOUND THE EMERGENCY PATH LIGHT AT ROW 13WL INOPERATIVE. MX REPLACED POWER SUPPLY AND OPS CHECK WAS NORMAL. ACFT RETURNED TO SERVICE.

Part: EPSU — INOPERATIVE (EMERGENCY LIGHTS)

EMERGENCY SEAT PATH LIGHTS SEAT ROW 18-21 ARE INOPERATIVE, REPLACED EPSU 13WL AND CHECKS GOOD. (K)

Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 54,539 hrs · 24,361 cycles

EMERGENCY EGRESS LIGHTING TEST FAILS. RELAMPED EXIT SIGN, RESET POWER SUPPLIES 11WL, 12WL, 13WL. REPLACED EPSU 10WL, CHECKS OK.

Part: SKIN VALVE — INOPERATIVE (E/E COMPT)

FOLLOWING TAKEOFF, CREW UNABLE TO PRESSURIZE THE AIRCRAFT. RETURNED TO MCO AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT COOLING SKIN AIR OUTLET VALVE, OPERATIONAL CHECK OK.

Part: SKIN VALVE — FAILED (E/E COMP)

FOLLOWING TAKEOFF, CREW WAS UNABLE TO PRESSURE THE AIRCRAFT. DIVERTED TO LAX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT COOLING SKIN AIR OUTLET VALVE, OPERATIONAL CHECK OK.

Part: BULB — FAILED (CABIN)

DURING TEST OF CABIN EMERGENCY LIGHTS, EMERGENCY EXIT SIGNS AT SEAT ROWS 11, 12, LEFT, AND RIGHT DID NOT ILLUMINATE. MAINTENANCE REPLACED BULBS. OPERATIONAL CHECK OK.

Part: VALVE — FAULTED (FUSELAGE)

DURING CLIMB, RECEIVED VENT SKIN VALVE FAULT AND UNABLE TO PRESSURIZE AIRCRAFT. DIVERTED TO MKE AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SKIN AIR OUTLET VALVE. OPERATIONAL CHECK OK.

Part: VALVE — FAILED (FUSELAGE)

DURING CLIMBOUT, RECEIVED VENT SKIN VALVE FAULT AND UNABLE TO PRESSURIZE THE AIRCRAFT. AIRCRAFT DIVERTED TO PHX AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE SKIN AIR OUTLET VALVE. (22HQ), OPERATIONAL CHECK OK.

Part: WINDOW — SHATTERED (FLIGHT DECK)

CAPTAIN'S WINDSHIELD OUTER PANE SHATTERED AT FL350. RETURNED TO MEM AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE WINDOW, OPERATIONAL CHECK OK.

Part: POWER SUPPLY — DISCHARGED (CABIN)

DURING LINE MAINTENANCE ALL OF FIRST CLASS EMERGENCY FLOOR PROXIMITY LIGHTS FOUND INOPERATIVE. MAINTENANCE REPLACED POWER SUPPLY 110WL-1, OPS CHECKED OK.

Part: SUPPORT — CORRODED (BS 32074 32571)

DURING IL CHECK, FOUND CORROSION ON THE AFT GALLEY FLOOR SUPPORT BETWEEN FRAMES 67 AND 68 AT THE LEFT AFT ENTRY DOOR SILL. REPAIRED SUPPORT PER EA 32-106351.

Part: TR UNIT — MALFUNCTIONED (NR 1 ENGINE)

DURING LANDING, THE NR 1 ENGINE FLAMED OUT AFTER COMING OUT OF SECOND THRUST REVERSER ENGAGEMENT AND ENGINE RESTARTED DURING TAXI INTO GATE. GROUND MAINTENANCE INSPECTED, RAN AND OPERATED NR 1 ENGINE THRUST REVERSER SEVERAL TIMES, NO PROBLEMS FOUND.

Part: LONGERON — CORROSION (FS 14300-14834)

DURING 1C1 MAINTENANCE VISIT, FOUND CORROSION ON STRINGER 41R BETWEEN FRAMES 33-34. REPAIRED STRINGER PER EA 32-104389.

Part: FLT CONTL UNIT — INOPERATIVE (COCKPIT)

DURING CLIMB-OUT, FLIGHT CONTROL UNITS NR 1 AND NR 2 FAILED. RESET CIRCUIT BREAKERS, NO HELP. DECISION WAS MADE TO RETURN TO MSP. REPLACED FLIGHT CONTROL UNIT. SYSTEM TESTS WERE NORMAL.

Part: COMPUTER — FAILED (E/E BAY)

DURING CLIMB-OUT FROM DTW, RECEIVED 'VENT SKIN VALVE' FAULT. UNABLE TO PRESSURIZE AIRCRAFT. RETURNED TO DTW AND LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE AVIONICS EQUIPMENT VENTILATION COMPUTER. OPERATIONAL CHECK OK.