N949UP

Part: SKIN — CRACKED (STA 1080 S14R)

INSPECTION TYPE:C FUSELAGE SKIN SHOW CRACK INDICATION BS 1080 STR 14R NDT FINDING MARKED RUNNING FORM FASTENER HOLE. VERIFICATION SKIN CRACK AT BS 1080 S14R IAW B727 NDT MANUAL PART 6 51-00-00 FIG 4, CUT OUT DAMAGE AREA AT BS 1080 STR 14R IAW B727 SRM 53-30-3 PERFORMED HFEC AROUND CUT OUT, FOUND NO CRACK NDT INSPECTION AS PER B727 PART 6 51-00-00 FIG 4. INSTALLED DOUBLER AND FILLER RE PAIR AT STA 1080 STR14 IAW SRM B727 53-30-3 FIG 14.

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C FUSELAGE INNER SKIN AT STA 1148-1166 STR 20R CRACKED AND CORRODED OUT OF LIMITS. REMOVE CORROSION FOUND OUT OF LIMITS AS PER SRM 51-10-2, CUT OUT DAMAGED AREA AT STA 1148-1166 STR 20R AND NDT INSPECTION AS PER PART 6 51-00-00 FIGURE 4, NO CRACK FOUND. INSTALLED REPAIR AT FUSELAGE INNER SKIN STA 1148-1166 STR 20R AS PER B727 SRM 53-30-3.

Part: PRESSURE PANEL — CRACKED (FUSELAGE)

INSPECTION TYPE:C NLG WW, BEHIND NOSE LANDING GEAR RT SIDE WALL SHOWS CRACK BETWEEN RIVETS. CUT OUT DAMAGE SECTION AS PER B727 SRM 51-40-2. ACCOMPLISHED NDT AROUND CUT OUT AREAS, NO CRACK AS PER 727 NDT PART 6 53-00-00. INSTALLED REPAIR DOUBLER AS PER B727 SRM 51-40-2.

Part: WEB — CRACKED (STA 277 R/SIDE)

INSPECTION TYPE:C NOSE WHEEL WELL R/T AT STA 277 RIGHT SIDE WALL SHOW CRACK BETWEEN RIVET, CRACK ALREADY VERIFIED IAW P6-51-00-00 FIG 2. REMOVED NOSE LANDING GEAR ACCESS PANEL #3125 RIGHT SIDE FOR REPAIR AS PER 727 SRM 51-30-02, CUT OUT DAMAGE AREA APPROX 2"X1" AND 4"X1" AT RIGHT SIDE WEB STA 274 AS PER B727 SRM 51-40-02. PERFORMED NDT INSP AFTER CUT OUT DAMAGE AREA, NO CRACK FOUND AS PER PART#6 51-00-0 0 FIG 4 INSTALLED DOUBLER REPAIR AT R/SIDE WEB IAW SRM 51-40-02.

Part: DOUBLER — CORRODED (BS1030-1130)

INSPECTION TYPE:C CORROSION AFT CARGO DOOR CUT OUT INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 AND BETWEEN STR 17R AND 20R. REMOVED INNER DOUBLER STRAP BETWEEN BS1030 AND BS1130 STR17 AND STR 20 IAW SRM B727-51-30-02. FABRICATED INNER DOUBLER STRAP IAW UPS DI-00011H AND DRAWING# 65-18622. INSTALL INNER DOUBLER STRAP AT AFT CARGO DOOR CUT OUT AT STA 1030 TO 1130 BETWEEN STR 17R AND STR 20R AS PER DRAWING# 65-18622.

Part: DOUBLER — CORRODED (BS 1040-1080)

INSPECTION TYPE:C AFT CARGO CUT OUT UPER SILL INTERNAL DOUBLER, HAS CORROSION FROM BS 1080. REMOVED CORROSION, FOUNF OUT OF LIMITS AT STA 1040-1080 AS PER B727- SRM 51-10-6 CUT OUT DAMAGE AREA AS PER 53-10-01 UPPER SILL INTERNAL DOUBLER BS 1080 AS PER TELEX #B2-9430 BOEING DROWING #65-18385. TREATED, PRIMED AND INSTALED DOUBLER IAW B727-SRM 51-10-02.

Part: SKIN — CORRODED (BS1080-1130)

INSPECTION TYPE:C FUSELAGE SKIN BULGING AROUND FASTENERS ABOVE UPPER AFT CORNER OF AFT CARGO DOOR BS 1080 TO BS 1130 STR 17R TO STR 20R. REMOVED AND REPLACED FUSELAGE SKIN FROM BS 1080 TO BS 1185 FORM STR 17R TO STR 20R AS PER BOEING DRAWING # 6518385 AND AVITA REPAIR ORDER AVHM 259120-1 AND UPS EO B727-5310-15416-A.

Part: ATTACH ANGLE — CRACKED (WING TO BODY)

INSPECTION TYPE:N/A WING TO BODY ATTACH ANGLE CRACKED REMOVED L BRACKET 6196. REMOVED SLIDING FAIRING STRICKER BRACKET TO FOM 61964 FABRICATED AND REINSTALLED BRACKET PER 51-1-0 OF SRM

Part: LINE — LEAKING (CREW OXYGEN SYS)

INSPECTION TYPE:B REF L/P 640094 ITEM NR 1 FOUND OXY LEAKING AT OXY DISTRIBUTION TUBE B-NUT CONNECTED TO PRESSURE TRANSDUCER AND TO THE OTHER END B-NUT CONNECTED TO THE FOUR WAY FITTING. BAD LINE REMOVED, 02 TURNED OFF AT BOTTLE. REMOVED AND REPLACED 02 LINE (P/N 65-20901-88) IAW STANDARD PRACTICES. LEAK CHECKS GOOD.

Part: BOTTLE — DISCHARGED (ESCAPE SLIDE)

INSPECTION TYPE:IN, GALLEY SLIDE PRESS AT LOWER LIMIT. REMOVED AND REPLACED GALLEY SLIDE ASSY, PRESS GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, LEFT AFT OVERWING SIDE EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK AND EXIT ID PLATE. OPS TEST GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, AFT CABIN ENTRY DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS TEST GOOD.

Part: BATTERY PACK — DISCHARGED (LT GALLEY)

INSPECTION TYPE:N/A, LEFT GALLEY EMERGENCY LIGHT ON BULKHEAD INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (GALLEY)

INSPECTION TYPE:N/A, EMERGENCY LIGHT LOWER GALLEY DUCT INOP. REMOVED AND REPLACED EXIT ID PLATE AND BATTERY PACK. OPS CHECK GOOD.

Part: SMOKE DETECTOR — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A MAIN CABIN SMOKE DETECTOR BACKGROUND LIGHTS DO NOT ILLUMINATE DURING RETURN FLIGHT AT NIGHT SMOKE DETECTOR APPEARED TO WORK NORMAL LY. CREW REPORT NOTED OPS CK OK PER MM 26-17-01

Part: LIGHT — INOPERATIVE (OVERWING EXIT)

INSPECTION TYPE:N/A, RT OVERWING EMER EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECKS GOOD.

Part: BATTERY PACK — INOPERATIVE (ROW 11)

INSPECTION TYPE:WE, AISLE 11 EMERGENCY LIGHT INOP. REMOVED AND REPLACED AISLE 11 BATTERY PACK, OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (ROW 13)

INSPECTION TYPE:WE, AISLE 13 EMERGENCY LIGHT INOP. REMOVED AND REPLACED AISLE 13 BATTERY PACK, OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (ROW 19)

INSPECTION TYPE:PFLT AISLE 19 EMERGENCY LIGHT INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK, OPS CKS GOOD.

Part: BATTERY PACK — INOPERATIVE (ROW 15)

INSPECTION TYPE:WE, AISLE 15 EMERGENCY LIGHT INOP. REMOVED AND REPLACED AISLE 15 BATTERY PACK, OPS CKS GOOD.

Part: LIGHT — INOPERATIVE (AIRSTAIR)

INSPECTION TYPE:N/A, VENTRAL AIRSTAIR EMERGENCY LIGHT INOP. REPLACED VENTRAL AIRSTAIR EMER LIGHT BATTERY PACK IAW 727 MM 33-50-61, OPS CHECKS NORMAL. (P/N 96-2-1015)

Part: LIGHT — INOPERATIVE (EXTERIOR)

INSPECTION TYPE:N/A, EXTERIOR EMERGENCY LIGHTS ON LT SIDE OF FUSELAGE (3 LIGHT ASSY) ARE INOP. REPLACED LT FUSELAGE FWD CONTROL AND AFT EMER LIGHT ASSY BATTERY PACKS 3 EACH, IAW 727 MM 33-50-22. OPS CHECK NORMAL (P/N 6-2 -1015).

Part: LIGHT — INOPERATIVE (EXTERIOR)

INSPECTION TYPE:N/A, EXTERIOR EMERGENCY LIGHTS ON RT SIDE OF FUSELAGE ARE INOP. REPLACED RT FUSELAGE FWD CENTER AND AFT EMER LIGHT ASSY BATTERY PACKS IAW MM 33-50-1015, OPS CHECKS NORMAL. (P/N 6-21-1-1015)

Part: SKIN — CRACKED (FUSELAGE)

INSPECTION TYPE:C FORWARD LOWER CARGO DOOR CUTOUT FS 520 FORWARD FRAME CRACKED LOWER END JUST INBOARD OF LIGHT SWITCH. ACCOMPLISHED REPAIR IAW EO B727-5310-12841-A, AVITAS ENGINEERING REP AIR ORDER AVHM-131 RO-1 AND BOEING TELEX UPS-MIA-OO-000005H. REPAIR DOUBLER INSTALLED, MATERIAL USED 7075-T6, 0.080, 19.5 X 6.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C BS259.5 INTERIOR SKIN BONDED EDGES AND SPICE DOUBLERS HAVE WHITE POWDER FROM STR 3 TO STR 4 LEFT. ACCOMPLISHED REPAIR IN ACCORDANCE WITH UPS E0 B727-5310-1371-E APPX 8.5 DOUBLER INSTALLED MATERIAL USED 2024-T3, 0.063, 12 X 4.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C, FUSELAGE SKIN BULGING AND CORROSION EMANATING FROM BELOW LAP SEAM 24 RIGHT, BS 294.5 TO 312. LFEC INSPECTION FOUND CORROSION EXCEEDING 10 PERCENT SKIN THICKNESS BETWEEN BS 294.5 TO BS 306. INSTALLED DOUBLER REPAIR IN ACCORDANCE WITH BOEING 69-61590. MATERIAL USED, 2024-T3, 0.090, 2024-T3, 0.071, 2024-7 3, 0.050, 2024-T3, 0.032 24 X 9.

Part: DOUBLER — CRACKED (FUSELAGE)

INSPECTION TYPE:C, AS VIEWED THROUGH ACCESS 3403-AFT INBOARD CORNER HAS REPAIR DOUBLER CRACKED BETWEEN STATION 870 BULKHEAD AND DELTA BEAM. REPLACED DOUBLER IN ACCORDANCE WITH SRM 51-40-2.

Part: SPAR — CORRODED (FUSELAGE)

INSPECTION TYPE:C, CENTER SECTION, FORWARD SPAR, LOWER CHORD AREA AT APPROX BUTT LINE 15 HAS EVIDENCE OF CORROSION. REPLACED WING CENTER SECTION FRONT SPAR LOWER CHORD WITH SPLICE LOCATED AT LBL 24.61. ACCOMPLISHED REPAIRS IN ACCORDANCE WITH UPS EO B72 7-5710-12840-A, AVITAS ENGINEERING REPAIR ORDER AVHM 132RO-1, AND BOEING TELEX UPS-MAI-00-00003H. EO NR B727-5710-12840-A.

Part: SKIN — CORRODED (FUSELAGE)

INSPECTION TYPE:C, FUSELAGE SKIN BULGING AT LAP SEAM 19 LEFT, BS 640 - 660. FOUND CRACKED INNER SKIN BETWEEN ROW A AND SKIN EDGE. CUT OUT DAMAGE, INSTALLED REPAIR PER BAC REPAIR DRAWING 69-61590 SHEET NR 13 MATERIAL USED FOR DOUBLER, 2024-T3, 0.090, 14.5 X 10.

Part: SPAR — CORRODED (HS STA 155-190)

INSPECTION TYPE:C, CORROSION, LEFT HORIZONTAL STABILIZER, REAR SPAR, UPPER CAP, BALANCE PANEL BAY 4 STABILIZER STATION 155 - 190. CUT OUT DAMAGED SECTION, CORROSION FOUND OUT OF LIMITS. INSTALLED RE AIR IN ACCORDANCE WITH SRM 55-10-5 FIG 1, MATERIAL USED, 7075-T6, 0. 080, 20.0 X 1 X 1 INCH.

Part: BATTERY PACK — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT LENS COVER LOOSE. REPLACED COVER AND FOUND BATTERY DEAD. REPLACED BATTERY PER MM 33-50 -01.

Part: FLASHLIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE:N/A REF M186032, AFT F/A EMERGENCY FLASHLIGHT INOP. REPLACED FLASHLIGHT, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, LEFT OUTSIDE FWD OVERWING EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: CONTROLLER — INOP (COCKPIT)

PRESSURIZATION INOP IN MANUAL AND AUTO MODE.

Part: LIGHT — INOP (ROW 11 & 19)

EMERGENCY LIGHT AT ROW 11 AND 19 INOP. REMOVED AND REPLACED BATTERY PACK IN ROW 11 AND 19, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 6A)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AT SEAT ROW 6A INOP. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT SEAT ROW 6A, OPS CHECK NORMAL.

Part: SKIN — DELAMINATED (LT TE FOREFLAP)

INSPECTION TYPE:N/A, LEFT O/B FOREFLAP DELAMINATED REMOVED L/H FOREFLAP PER MM 27-51-11. INSTALLED TEMPORARY REPAIR PER EO B727-5750-3081-C. INSTALLED LT FOREFLAP PER MM 27-51-11, OP CHECKS NORMAL.

Part: BATTERY PACK — DISCHARGED (ROW 10R)

INSPECTION TYPE:N/A, EMERGENCY LIGHTS AT SEAT ROW 10R OVERWING DOOR, LOWER WOULD NOT ILLUMINATE. REMOVED AND REPLACED BATTERY PACK, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 12R)

INSPECTION TYPE:N/A, EMERGENCY LIGHT, SEAT ROW 12R OVERWING DOOR LOWER WOULD NOT ILLUMINATE, OPERATIONAL CHECKS OK AFTER TIGHTENING BATTERY PACK.

Part: WIRE — LOOSE (ROW 1R)

INSPECTION TYPE:N/A, POS NR 1R FLOOR LIGHT INVERTER WIRE PULLED FROM CONNECTOR. RECONNECTED WIRE.

Part: BATTERY PACK — DISCHARGED (EMER EXIY)

RIGHT EXTERIOR MIDDLE OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

RIGHT EXTERIOR BOTTOM OVERWING EMERGENCY EXIT LIGHT OUT/DIM. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

RIGHT LOWER FWD OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (LT EMER EXIT)

RIGHT LOWER AFT OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: LAMP — FAILED (LT GALLEY)

LEFT GALLEY EMERGENCY LIGHT ABOVE FLIGHT ATTENDANT SEAT OUTBOARD LAMP IS BURNT OUT. REMOVED AND REPLACED LIGHT AND BATTERY ASSY OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (OVERWING)

RIGHT EXTERIOR TOP OVERWING EMERGENCY EXIT LIGHT OUT/DIM. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (VENTRAL STAIRS)

AFT VENTRAL STAIRS EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT LOWER FWD OVERWING EMERGENCY EXIT LIGHT OUT. REMOVED AND REPLACED BATTERY. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT EXTERIOR MIDDLE OVERWING EMERGENCY EXIT LIGHT OUT. REPLACED BATTERY. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 4)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT, SEAT ROW 4 INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT ROW 4, OPS CHECKS GOOD.

Part: BATTERY PACK — DISCHARGED (RT GALLEY)

INSPECTION TYPE:N/A, EMERGENCY LIGHT AT RT GALLEY INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY RT GALLEY, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (ROW 4)

INSPECTION TYPE:N/A, EMERGENCY EXIT LIGHT, SEAT ROW 4 INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY AT SEAT ROW 4, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE:N/A, FLOOR EMER LIGHTS OUT IN SEAT POS 13 & 15. REPLACED BATTERY PACKS IN POS 13 & 15.

Part: BATTERY — DISCHARGED (GALLEY DOORWAY)

INSPECTION TYPE:N/A, EMERG EXIT LIGHT OVER GALLEY DOOR DOES NOT ILLUMINATE. REPLACED BATT PACK, CKS OK.

Part: BATTERY PACK — DISCHARGED (ROW 9 & 17)

EMERGENCY LIGHTS OUT AT SEAT NR 9 AND 17 AND LT UPPER REAR LAV. REMOVE AND REPLACE BATTERY PACK. OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERHEAD EMERGENCY LIGHTS ON RT SIDE WILL NOT TEST. REPLACED BATTERY PACKS IN OVERHEAD EMERGENCY LIGHTS ON RT SIDE, OPS CK GOOD.

Part: MASK — FELL OUT (ROW 6)

INSPECTION TYPE-N/A, O2 MASKS ROW C ON LEFT SIDE OF CABIN FELL OUT. STOWED O2 MASKS AT ROW 6 LT SIDE.

Part: BATTERY PACK — FAILED (EMERGENCY EXIT)

INSPECTION TYPE-N/A, R-1 DOOR EMERGENCY EXIT LIGHT ON CEILING FWD POSTION INOP. REMOVED AND REPLACED BATTERY PACK, OPS CHECK NORMAL.

Part: WIRE — BROKEN (ROW 3)

INSPECTION TYPE-N/A, POS NR 2 EMERGENCY EXIT LIGHT AT SEAT 3. FOUND BROKEN WIRE. REPAIRED BROKEN WIRE, OPS CHK GOOD.

Part: LIGHT — INOP (CABIN)

INSPECTION TYPE-N/A, LT UPPER 2 OVERWING EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED 3 EXTERNAL BATTS, OPS CHECK GOOD.

Part: LIGHT — INOP (ROW 2)

INSPECTION TYPE-N/A, ROW 2 EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CHECK GOOD.

Part: BATTERY — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, AFT BULLNOSE EMERGENCY EXIT LIGHTS INOP. REMOVED AND REPLACED BATTS, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (EMER EXIT)

INSPECTION TYPE-N/A, ALL EMERG EXIT LIGHTS ABOVE WING EXIT DOORS INOP. REMOVED AND REPLACED ALL EMER EXIT LIGHTS BATTERY PACKS, OPS CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (L1 DOOR)

INSPECTION TYPE-N/A, L1 DOOR INTERIOR (FOOT LEVEL EMER LIGHT WILL NOT TEST). REMOVED AND REPLACED L1 BATTER PACK, TEST OK.

Part: CIRCUIT BREAKER — FAILED (COCKPIT)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS ON WHILE IN ARMED POSITION. ILLUMINATED IN FLIGHT, DISARMED, CHECKS OK. REPLACED CIRCUIT BREAKER EMERGENCY EXIT LIGHT, OPS CK NORM.

Part: SWITCH — DIRTY (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHTS DISARM SWITCH STICKS WHEN SELECTED OFF. LIGHT CAME ON ABOUT 3 MIN AFTER SWITCH SELECTED OFF. CLEANED EMERGENCY LIGHT SWITCH, OPS GOOD.

Part: STRINGER — CRACKED (WS 171.5)

INSPECTION TYPE:SI L-W UPPER STRINGER NR 8 IS CRACKED AT WS 171.5. REPAIRED L-WING STRINGER NR 8 UPPER IAW SRM 57-10-4.

Part: SPAR WEB — CORRODED (BS 870)

INSPECTION TYPE:SI WING CENTER SECTION REAR SPAR WEB IS CORRODED BS 870 RBL 22-46 LBL 46. REMOVED AND REPLACED WING CENTER SECTION REAR SPAR WEB, UPPER CHORD, AND LOWER CHORD PER ER 99-5018.

Part: FITTING — CORRODED (NR 3 SPOILER)

INSPECTION TYPE:SI NR 3 FLIGHT SPOILER ACTUATOR SUPPORT FITTING HAS EXCESSIVE PITTING CORROSION ON I/B FACES OF BOTH I/B MOUNTING LUGS FOR SPOILER CENTER HINGE. REPLACED MOUNT (SUPPORT FITTING PN 65-21622-22) PER 727 MM 27-61-81.

Part: STRINGER — CRACKED (VERT FIN)

INSPECTION TYPE:SI INTERNAL VERTICAL FIN STRINGER 5-11R IS CRACKED AT BS 1362, 9 INCHES ABOVE FIN STA 6.0. REMOVED AND REPLACED STRINGER SEGMENT PER FER 99-5059.

Part: FITTING — CORRODED (RT AILERON)

INSPECTION TYPE:SI R/W O/B AILERON, UPPER QUADRANT HINGE HAS PITTING AROUND HINGE BOLT. REMOVED PITTED FITTING, INSTALLED NEW FITTING IAW SRM 51-30-2 PG 14 PARA 7 AND PG 8 PARA A5.

Part: SUPPORT — CORRODED (BS 1176.9)

INSPECTION TYPE-SI, CORROSION ON REINFORCEMENT CHORD BS 1176.9 FROM LBL 30 TO RBL 30 WL 208. REMOVED AND REPLACED CHORD.

Part: SKIN — CORRODED (NR 7 SPOILER)

INSPECTION TYPE-SI, NR 7 SPOILER PANEL HAS SEVERAL SMALL AREAS OF CORROSION ON LOWER SURFACE AT TRAILING EDGE 7 INCHES I/B OF O/B END. REPLACED SPOILER IAW MM 27-62-1.

Part: FLOORBEAM — CORRODED (BS 600)

INSPECTION TYPE-SI, CORROSION ON LOWER SURFACE OF FLOORBEAM AT BS 600, RBL 12 TO RBL 21 WL 200. REMOVED CORROSION AND REPAIRED FLOORBEAM PER ER 99-5042P3.

Part: ANGLE — CRACKED (PAX DOOR)

INSPECTION TYPE-SI, FWD ENTRY DOOR TRANSVERSE BEAM IS CRACKED WL 223 BS 336 LBL 65. REMOVED AND REPLACED L ANGLE FWD LOWER AFT POSITION (DOOR CLOSED) AND REINSTALLED LOWER TRANSVERSE BEAM PANEL REMOVED FOR ACCESS PER 727 SRM 51-30-2, 51-20-1 AND MM 52-11-0.

Part: SKIN — CORRODED (LT WING)

INSPECTION TYPE-SI, CORROSION ON UPPER AND LOWER SURFACE OF LEFT WING FUEL TANK ACCESS CUTOUT 7205. REPAIRED WING SKIN PER ER 99-5021.

Part: TRACK — CORRODED (TE FLAP)

INSPECTION TYPE-SI, NR 7 FLAP TRACK HAS CORROSION ON FWD O/B MOUNT 106, O/B SIDE. REPLACED TRACK IAW MM 27-51-31.

Part: INTERCOSTAL — CORRODED (BS 300)

INSPECTION TYPE-SI, CORROSION (C53-221-01-01-01) ON INTERCOSTAL AT BS 300, LBL 13, WL 208. FABRICATED AND REPLACED INTERCOSTAL BS 294.5 TO BS 312 PER SRM 51-10-2 AND 51-20-01 AND 51-30-2.

Part: STRINGER — CORRODED (BS 460)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-01) ON STRINGER BS 460 STR 21R WL 175. REMOVED CORRODED PORTION OF STRINGER, FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 51-30-2, 53-10-3.

Part: BULKHEAD — CORRODED (BS 875)

INSPECTION TYPE:SI, RE-INFORCEMENT DOUBLER CORRODED AND BULKHEAD CRACKED AT BS STA 875 LBL 60 WL 182. REMOVED AND REPLACED DOUBLER AND REPAIRED BULKHEAD PER SRM 53-10-9 FIG 4.

Part: FLAP TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI CORROSION ON WING ATTACH PAD AND FWD ATTACH LUGS OF NR 8 FLAP TRACK. REMOVED AND REPLACED.

Part: FRONT SPAR — CORRODED (LT WING)

INSPECTION TYPE-SI, CORROSION (C57-571-01.05-01) ON LEFT WING FRONT SPAR FUEL TANK ACCESS CUT OUT 7340 AFT SURFACE. REMOVED CORROSION AND REPAIRED PER EO 99-5020.

Part: BULKHEAD — CRACKED (BS 870)

INSPECTION TYPE:SI, RE-INFORCEMENT DOUBLER CORRODED AND BULKHEAD CRACKED AT BS STA 870 RBL 60 WL 182. REMOVED AND REPLACED DOUBLER AND REPAIRED BULKHEAD PER SRM 53-10-9 FIG 4.

Part: CARRIAGE — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION ON THRUST WASHER AND AFT SPINDLE BEARING SURFACE OF NR 8 MID FLAP CARRIAGE ASSEMBLY. REMOVED AND REPLACED CARRIAGE ASSEMBLY.

Part: FLAP TRACK — CORRODED (TE FLAP)

INSPECTION TYPE:SI, CORROSION (C57-581-01-1B) ON NR 2 FLAP TRACK FWD LUG AND INSIDE AFT MOUNT BARREL NUT HOLES. REMOVED CORRODED FLAP TRACK, INSTALLED SERVICEABLE FLAP TRACK IAW MM 51-30-2. TRACK WILL BE INSTALLED ON TC C57-581-04-3D.

Part: RIB — CRACKED (WS 519)

INSPECTION TYPE-SI, LEFT WING RIB UPPER CHORD CRACKED AT WING STA 519. REPAIRED UPPER CHORD PER SRM 51-40-4.

Part: MOP SILL — CORRODED (BS 340-308)

INSPECTION TYPE-SI, CORROSION (C53-224-06-1B) MAIN DECK ENTRY MOPSILL BS 340 TO 308 WL 208 LBL 72. REMOVED CORRODED MOPSILL, INSTALLED NEW MOPSILL IAW SRM 51-20-1, 51-30-2, 51-30-8.

Part: SEAT TRACK — CORRODED (BS 620-700)

INSPECTION TYPE-SI, CORROSION (C53-224-01-1B) ON MAIN DECK SEAT TRACK BS 620 TO 700 RBL 65 WL 208 (TOP AND BOTTOM SURFACES, LT FLANGE AND IN WELL AT BS 680). REMOVED CORRODED SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED IAW SRM 51-30-1, 51-30-2.

Part: SEAT TRACK — CORRODED (BS 700-740)

INSPECTION TYPE-SI, CORROSION (C53-224-01-1B) ON SEAT TRACK STA 700 TO 740, RBL 25. REMOVED CORROSION FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 53-10-5.

Part: STRINGER — CRACKED (WS 171.5)

INSPECTION TYPE-SI, LT WING UPPER STRINGER 19 IS CRACKED AT WS 171.5 (VENT STRINGER). REPAIRED SECTION OF STRINGER 19 AT WS 171.5 PER SRM 57-10-4.

Part: SEAT TRACK — CRACKED (BS 1010)

INSPECTION TYPE:SI, CRACKED SEAT TRACK FLANGE AT BS 1010, RBL 16, WL 156. REMOVED CRACKED SEAT TRACK SECTION FROM BS 950 TO 1010, RBL 16, WL 156. INSTALLED NEW SEAT TRACK PER SRM 51-10-1.

Part: TIE DOWN TRACK — CORRODED (BS 520)

INSPECTION TYPE-SI, CORROSION (C53-113-01.00-01) ON CARGO TIE DOWN TRACK, BS 520 LBL 15 FWD CARGO BAY AT NET ATTACH POINT. EVALUATED CORROSION, FOUND TO BE OUT OF LIMITS. REPLACED TIE DOWN TRACK PER SRM 51-30-02, SRM 57-30-05.

Part: TRACK — CORRODED (NR 4 TE FLAP)

INSPECTION TYPE:C (CORROSION C57-581-06.00-03) ON NR 4 FLAP TRACK IN SPOILER BEAM ATTACH HOLES AND AROUND MLG BEAM HOLES. REMOVED OLD FLAP TRACK, INSTALLED NEW FLAP TRACK ON CARD NR 838849, 838505.

Part: BATTERY PACK — DISCHARGED (CABIN)

ROW 19 EMERGENCY LIGHT FAILED TEST. REPLACED BATTERY. CHECKS GOOD

Part: SPAR — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAYS VIEW 22 FRONT SPAR OUT OF FASTENER HOLE AT ELEV STA 150. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.

Part: SPAR — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATIONS NOTED ON X-RAY VIEW 24, 8 AFT OF FRONT SPAR ELEV STA 167. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR 2 CRACK INDICATIONS NOTED ON X-RAYS VIEW 14 AT ELEV STA 99 8 AND 10 FROM LEADING EDGE. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR 4 CRACK INDICATIONS NOTED ON X-RAYS VIEW 13 ALONG LEADING EDGE 79 TO 99 ELEV STA. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 20 ELEV STA 130, 6 AFT OF FRONT SPAR. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 7 ON 1ST RIB AFT OF FRONT SPAR AT ELEV STA 40. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.

Part: SPAR — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 28, 8. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY AT VIEW 16 10 AFT OF LEADING EDGE AT ELEV STA 125. RT ELEVATOR WAS REMOVED AND REPLACED ON NRC NR 838862.

Part: RIB — CRACKED (RT ELEVATOR)

INSPECTION TYPE-SI, RT ELEVATOR CRACK INDICATION NOTED ON X-RAY VIEW 31 ON 1ST RIB FWD OF REAR SPAR AT ELEVATOR STATION 200. RT ELEVATOR WAS REMOVED AND REPLACED ON CARD NR 838862.

Part: CHORD — CORRODED (BS 320)

INSPECTION TYPE-SI, CORROSION (C53-111-01.05-01) RT MID NOSE CHORD (NOSE WHEEL WELL STRUCTURE) AT BS 320, RBL 10. RT MID NOSE CHORD FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. PERFORMED CHORD REPAIR PER SRM 51-30-5, SRM 51-30-02, SMR 51-30-04 AND MM 51-31-0.

Part: FLOORBEAM — CORRODED (BS 1090)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) ON FLOORBEAM UPPER FLANGE BS 1090 LBL 56, WL 208. FLOORBEAM UPPER FLANGE FOUND TO BE OUT OF LIMITS PER SRM 51-10-1. PERFORMED STANDARD T-CHORD REPARIED PER SRM 53-10-8, SRM 51-30-2 AND OHM 20-41-03.

Part: FLOORBEAM — CORRODED (BS 598)

INSPECTION TYPE:SI CORROSION (SDN C53-111-01.00-02) ON LOWER SURFACE OF LONGITUDINAL FLOORBEAM AT BS 598, BL 0, WL 200. REMOVED ALL CORROSION, FLAT PEENED AREA, FABRICATED AND INSTALLED REPAIR STRAP IAW ER NR 99-5029.

Part: RIB — CRACKED (NR 4 LE SLAT)

INSPECTION TYPE-SI, NR 4 SLAT O/B ACTUATOR RIB IS CRACKED. REMOVED AND REPLACED NR 4 SLAT WORK ACCOMPLISH ON NRC 838733.

Part: FRAME — CORRODED (BS 520)

INSPECTION TYPE-SI, CORROSION (C53-224-01.00-01) ON MAIN DECK FRAME UPPER FLANGE (TOP SURFACE) BS 520 STR 2R-STR 2L. MAIN DECK FRAME UPPER FLANGE FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. INSTALLED J CHANNEL REPAIR PER SRM 53-10-04 AND MM 51-20-1.

Part: STRAP — CRACKED (BS 328-344)

INSPECTION TYPE-SI, STABILIZER STRAP BETWEEN BS 328 AND BS 344 AT BL 0 WL 200 IS CRACKED. REMOVED CRACKED STRAP, FABRICATED AND INSTALLED NEW STRAP IAW SRM 51-20-1, SRM 53-10-2, SRM 51-30-2.

Part: RIB — CRACKED (NR 2 LE SLAT)

INSPECTION TYPE:SI NR 2 SLAT I/B TRACK I/B MOUNTING BRACKET SUPPORT RIB IS CRACKED. REPLACE NR 2 SLAT PER MM 27-81-11.

Part: TRACK — CORRODED (NR 3 TE FLAP)

INSPECTION TYPE-SI, CORROSION (C57-581-01.02-01) ON NR 3 FLAP TRACK AT SPAR MOUNT PAD AND INSIDE HOLES. REMOVED AND REPLACED THE NR 3 FLAP TRACK DUE TO TIME RESTRAINTS MM 27-51-4.

Part: SEAT TRACK — CORRODED (BS 1063-1168)

INSPECTION TYPE-SI, CORROSION (C53-111-01.00-03) IN AFT CARGO BAY LBL 16 WL 150 BS 1063 TO 1168 (CARGO TRACK). REMOVED, FABRICATED AND INSTALLED NEW CARGO TRACK WORK DONE IAW SRM'S 53-10-1, 53-10-5, 51-10-3, 51-10-2, 51-20-1, 51-30-2.

Part: BULB — FAILED (CABIN)

AIRSTAIRS EMER LIGHT INOP. RELALMPED AIRSTAIR EMER LIGHT, OPS CKS NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN)

LEFT AFT EMER EXIT LIGHT OVERWING AT SEAT POS 12 FAILED TEST. REMOVED AND REPLACED BATTERY PACK FOR LEFT AFT OVERWING EXIT, OPS CK NORMAL PER UPS DWG 727-33A-006.

Part: BATTERY PACK — DISCHARGED (CABIN)

AISLE SEAT EMER LIGHTS POS 9-11-15 FAILED TEST. REMOVED AND REPLACED BATTERY PACKS FOR AISLE SEATS EMER LIGHTS, SEAT 9-11-15, OPS CK NORMAL PER UPS DWG 727-33A-006.

Part: BATTERY — DISCHARGED (COCKPIT)

INSPECTION TYPE-N/A, EMER LIGHTS WOULD NOT TEST PROPERLY (COCKPIT ENTRY UNIT). CHANGED EXIT LIGHT BATTERY ON DOOR, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

L1 FWD LOWER EEL REMAINS ON AT ALL TIMES. REMOVED AND REPLACED EXIT LT BATT PACK. OPS CK OK P/N ON AND OFF 96-2-1015 SN ON TAG 315525 OFF TAG 937150.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, RIGHT SIDE FWD OVERWING EMER LIGHT DOES NOT TEST. REMOVED AND REPLACED EMER LIGHT BATTERY PACK, OP'S CHECK GOOD.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, FWD ENTRY OVERHEAD EMER LIGHT INOP. REPLACED BATTERY, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMER LIGHT AT SEAT 6C INOP. REMOVED AND REPLACED BATTERY, CHECKS OK.

Part: BATTERY PACK — DISCHARGED (CABIN)

OVERWING EMERGENCY LIGHTS AND AFT STAIR EMERGENCY LIGHTS ARE WEAK. REMOVED AND REPLACED EMERGENCY LIGHTS BATTERY PACKS. LIGHTS OPS CHECK NORMAL IAW M/M 33-50-11, P\N'S ON 96-21015 S\N'S ON NSN P\N'S OFF 96-2-1015 S\N OFF NSN.

Part: LIGHT — INOPERATIVE (CABIN)

INSPECTION TYPE-N/A, EMERGENCY ESCAPE EXIT LIGHT HAS GREEN LIGHTS FLASHING. PERFORMED EMERGENCY LIGHT TEST PER 33-50-00 P101 LIGHTS WENT OUT, OPS CK NML.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT ASSY AT GALLEY SERVICE DOOR INOP AFT ASSY. REMOVED AND REPLACED BATTERY PACK, OPS IAW 33-10-00 (P/N 96-21024).

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, FWD ENTRY DOOR EMERGENCY LIGHT INOP. REMOVED AND REPLACED BATTERY PACK.

Part: BATTERY PACK — DISCHARGED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY LIGHT OUT FWD BULKHEAD. REMOVED AND REPLACED BATTERY PACK.

Part: SKIN — DELAMINATED (LT TE FLAP)

INSPECTION TYPE-C, LT WING O/B AFT FLAP HAS A 1.5 AREA OF T/E EDGE SEPARATION AT 42 FROM O/B END. REMOVED DAMAGE AREA AND REPAIRED IN ACCORDANCE WITH SRM 51-40-6.

Part: SKIN — DELAMINATED (LT TE MIDFLAP)

INSPECTION TYPE-C, LT WING O/B MIDFLAP HAS A 2 BY 2 AREA OF DELAMINATION ON T/E WEDGE LOWER SURFACE AT 81 FROM I/B END AND A 1 BY 3 AREA 73 FROM I/B END. REMOVED DAMAGE AND REPAIRED IAW SRM 51-40-6.

Part: SKIN — DELAMINATED (RT TE MIDFLAP)

INSPECTION TYPE-C, RING WING O/B MIDFLAP DELAMINATED ON T/E LOWER SURFACE 96 FROM I/B END. REPAIRED SURFACE AND OVERLAID WITH RESIN IMPREGNATED GLASS FABRIC AND CURED PER SRM 51-40-6, INSTALLED NEW RUB STRIP PER MM 51-51-11.

Part: SKIN — DELAMINATED (RT SPOILER)

INSPECTION TYPE-C, NR 3 SPOILER HAS A 1.5 BY 1.5 AREA OF DELAMINATION ON UPPER SURFACE 13 FROM I/B EDGE AND 13 FROM T/E. REPAIRED SPOILER IAW SRM 57-50-6 USING WET LAY-UP REPAIR PLIES.

Part: SPAR — CRACKED (RT AILERON)

INSPECTION TYPE-C, WHILE WORKING CARD 718833 FOUND RT WING O/B AILERON REAR AILERON SPAR CRACKED AT CENTER I/B TAB HINGE CUTOUT. REPAIRED SPAR AT I/B TAB HINGE ON RT WING O/B AILERON IAW SRM 51-40-3. THEN AILERON WAS REPLACED DUE TO EXTENSIVE REPAIRS ON NRC 718801.

Part: TAB — DELAMINATED (LT AILERON)

INSPECTION TYPE-C, LT O/B AILERON TAB HAS A 5 BY 4 AREA OF DELAMINATION ON I/B END LOWER SURFACE. REPAIRED LT O/B AILERON TAB I/B END LOWER SURFACE AND REBALANCED IAW SRM 51-40-6 AND SRM 51-80-6.

Part: FRAME — CRACKED (PAX DOOR)

INSPECTION TYPE-C, FORWARD SIDE FRAME CRACKED AT LOWER HINGE CUTOUT ON FORWARD ENTRY DOOR. REMOVED DAMAGED FRAME, INSTALLED NEW FRAME PER SRM 51-10-01, 51-10-02, 51-30-2.

Part: CASTING — CORRODED (CARGO COMPT)

INSPECTION TYPE-C, BARRIER NET CASTING LBL 5 HAS CORROSION IN BOTTOM AND RECEPTICAL IS HARD TO MOVE. REMOVED CORROSION FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED CASTING IAW SRM 51-30-02.

Part: LIGHT — MALFUNCTIONED (CABIN)

INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT R1 DOOR CONTINUOUSLY ILLUMINATED BY DOOR. FOUND GREEN LED ON, CYCLED POWER CKD OK. GREEN LED IS INDICATION OF PROPER OPERATION.

Part: BATTERY PACK — DISCHARGED (L1 DOOR)

INSPECTION TYPE:SP, FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT IS INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-00 AND DWG 727-33A006.

Part: LIGHT — INOPERATIVE (COCKPIT)

INSPECTION TYPE:SP, COCKPIT EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED BATTERY PACK IAW MM 33-50-00 AND DWG 727-33A-006.

Part: FLOORBEAM — CORRODED (BS 560)

INSPECTION TYPE-MOD, STA 560 RBL 55, I/G CORROSION ON TOP OF FLOORBEAM. REPAIRED IAW SRM 53-10-8.

Part: BATTERY PACK — OUT OF POSITION (FLT DECK)

WHILE IN MEX CREW REPORTED, ON T/O ROLL THE COCKPIT EMERGENCY EXIT LIGHT FELL OFF THE BULKHEAD AND HIT THE FLOOR. LIGHT IS NOW INOP. REPOSITIONED BATTERIES AND LAMPS. CHECKS NORMAL.

Part: CHORD — CRACKED (VERT STAB)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INNER CHORD FIN STA 22.5 IS CRACKED. REMOVED DAMAGED AREA I.A.W. BOEING DWG 65C20296. INSTALLED REPAIR DOUBLER PER BOEING DWG 65C20296 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 1243-1342)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11L-14L HAS GOUGE. REMOVED SKIN, FABRICATED AND INSTALLED STRINGER PER BOEING DWG 65-17528 AND SRM 51-30-2.

Part: SKIN — GOUGED (BS 1243-1342)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED SKIN PANEL STA 1243-1342, STR 11R-14R HAS GOUGE. REMOVED SKIN, FABRICATED, AND INSTALLED STRINGER PER BOEING DWG 65-17558 AND SRM 51-30-2.

Part: SPAR CHORD — CRACKED (LT TE MIDFLAP)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED LT INBOARD MID-FLAP WBL 124.2 REAR SPAR 4TH FASTENER HOLE REVEALED A CRACK ON SPAR CAP BELOW SKIN AT 3 O'CLOCK POSITION. LOWER PANEL WAS OPENED, 10 EACH FASTENERS REMOVED. REPAIRED HOLE AREA I.A.W. DHC SK 949-436 AND E.O. B727-5750-3582 APP AND C-5750-7667A.

Part: WINDOW FRAME — CORROSION (BS 530)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 530 AFTER CORROSION REMOVAL, FLANGE FOUND BEYOND LIMITS PER SRM 56-20-1 ON NR 408505. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG 1. INSTALLED REPAIR DOUBLER PER SRM 56-20-3, FIG 1.

Part: WINDOW FRAME — CORROSION (BS 590)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT WINDOW FRAME FS 590 AFTER CORROSION REMOVAL. LOWER FLANGE FOUND BEYOND LIMITS PER SRM 56-20-1 ON NR 408510. FABRICATED DOUBLER AND INSTALLED CONICAL WASHERS PER SRM 56-20-3, FIG. 1. INSTALLED REPAIR DOUBLER PER SRM 56-20-3, FIG.1.

Part: SPAR — CRACKED (VERT STAB)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED FS 1342, THE VERTICAL FIN REAR SPAR CHORD CRACKED. REPAIRED I.A.W. BOEING DWG 69-70556.

Part: ANGLE — CRACKED (FS 1345)

WHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT SKIN SUPPORT ANGLE CRACKED FS 1345 FIN STA 22.5. REMOVED, FABRICATED AND INSTALLED NEW ANGLE SECTION IAW SRM 51-40-3 AND 51-30-2.

Part: RIB — CRACKED (VERT STAB)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED RT RIB CRACKED BS 1367 FIN STA 22.5. CUT OUT DAMAGE AND REPAIRED WEB I.A.W. SRM 51-40-2.

Part: STRINGER — CORROSION (BS 294.5)

WHILE IN FOR MOD WORK, MAINTENANCE REPORTED STR 26L AT BS 294.5 HAS HEAVY CORROSION. INSTALLED REPLACEMENT ANGLE PER SRM 51-30-2 AND SRM 53-10-2.

Part: SKIN — DELAMINATED (LT TE MIDFLAP)

WHILE ON GROUND, MAINTENANCE FOUND LEFT MIDFLAP DELAMINATED MIDDLE TRAILING EDGE 2 PLACES O/B FLAP. DEFERRED PER D-98013 INTERM REPAIR PER 57-50-1.

Part: SKIN — DELAMINATED (TE FLAP)

WHILE ON GROUND, MAINTENANCE FOUND FLAP DELAMINATED AT RT, O/B TRAILING EDGE. REPAIRED IAW B727-5750-3081C.

Part: FLAP — CORRODED (NR 1 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION NR 1 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.

Part: BEAM — CORRODED (BS 830)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON STUB BEAM AT STA 830 RBL 55 TO 65. REPLACED PER SRM 51-10-1, 51-10-2, 51-20-31.

Part: FLAP — CORRODED (NR 3 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 3 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.

Part: SLAT — CORRODED (NR 1 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 1 SLAT. REPLACED NR 1 SLAT PER MM 27-81-32.

Part: CHORD — CORRODED (BS 743)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM CHORD ON UPPER SIDE AT STA 743 LBL 13 WL 154. INSTALLED REPAIR PER SRM 53-10-1, 51-40-4.

Part: SEAT TRACK — CRACKED (BS 845)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK ON SEAT TRACK O/B FLANGE AT BS 845, LBL45, WL 208. INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, MM 51-20-151.

Part: LAP FILLER — DISBONDED (BS 948)

WHILE IN C-CHECK, MAINTENANCE FOUND LAP FILLER TO BE DISBONDED AT BS 948 LBL 27 WL 142. FABRICATED AND INSTALLED NEW FILLER PER SRM 51-30-2.

Part: FLAP — CORRODED (NR 6 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 6 K-FLAP ASSY. REPLACED K-FLAP ASSY PER MM 27-81-01.

Part: FLAP — CORRODED (NR 5 LE FLAP)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON NR 5 K-FLAP ASSY. REPLACED K-FLAP ASSY PER NMM 27-81-01.

Part: FLOORBEAM — CORRODED (BS 800)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF LONGITUDINAL FLOORBEAM AT STA 800, LBL 45, WL 208. FLAP PEENED PER UPS EO FILE 727-57-1365.

Part: PANEL — CRACK (HORIZ STAB)

WHILE IN C-CHECK, MAINTENANCE FOUND CRACK IN HORIZONTAL STAB. L/E PANEL 9203, AT 4TH RIB FROM I/B EDGE. INSTALLED REPAIR PER SRM 55-10-3.

Part: BALANCE PANEL — CORRODED (ELEVATOR)

WHILE IN C-CHECK, MAINTENANCE FOUND CORROSION ON ELEVATOR NR 5 BALANCE PANEL WHERE WEIGHT AND HINGE CONTACT PANEL. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-1, NMM 51-20-21, 51-20-31.

Part: INTERCOSTAL — CORRODED (BS 259-276)

DURING 'C' CHECK, MAINTENANCE FOUND FILLER PLATE CORRODED ON 25 G-BEAM BS 259 TO 276. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-30-2, 51-10-2.

Part: TE WEDGE — CORRODED (TE FLAP)

DURING 'C' CHECK, MAINTENANCE FOUND L/W O/B MID FLAP T/E WEDGE DELAMINATED AT O/B. FABRICATED AND INSTALLED REPAIR PER SRM 51-40-6.

Part: INTERCOSTAL — CORRODED (BS 259-277)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 259 TO 277, WL 208, LBL 15. REPLACED INTERCOSTAL PER SRM 51-10-1, 51-20-1, 51-10-2.

Part: FLOORBEAM — CORRODED (BS 277)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM AT STA 277, WL 208, LBL 7 TO 12, RBL 4 TO 16. FABRICATED AND INSTALLED REPAIR PER SRM 51-10-2, 51-40-4, 51-30-2.

Part: INTERCOSTAL — CORRODED (BS 277-294)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 277 TO 294, WL 208, LBL 14. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, 51-20-1.

Part: INTERCOSTAL — CORRODED (BS 277-294)

DURING 'C' CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT STA 277 TO 294, WL 208, RBL 15. FABRICATED AND INSTALLED REPAIR PER SRM 51-30-2, 51-10-2, 51-20-1.