N523AS
Registered owner: WILMINGTON TRUST CO TRUSTEE, DE (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
L1 DOOR UPPER HINGE COVER (INSIDE) JAMS OPEN WHEN CLOSING DOOR. F/A REPORTS COVER WILL CLOSE NORMALLY BY CYCLYING DOOR PARTIALLY OPEN THEN RE-CLOSING. GROUNDED - YES. REF AMM 52-11-00 CYCLE L1 DOOR MULTIPLE TIMES. INTERIOR UPPER HINGE COVER OPERATES NORMALLY. NO DEFECTS NOTED.
PANEL 193B RT SIDE OTBD, PANEL LANDING GOUGED. GROUNDED - YES. REMOVED & REPLACED PANEL 193 RT SIDE OTBD PANEL LANDING IAW SRM 51-40-02-0G-0.
FWD CARGO PIT LH SIDE AFT BULKHEAD LOWER SUPPORT ANGLE HAS MULTIPLE SPOTS OF CORROSION AND BARE METAL. GROUNDED - YES. REMOVED AND REPLACED FWD CARGO PIT L/H SIDE, AFT BULKHEAD LOWER SUPPORT ANGLE IAW B737-800 SRM 51-40-02-0G-0W: 1 O: .071 R: .054 L: 1.3 D: 0.017.
UPON GVI OF LT AC BAY FOUND STA 663 CENTER SECTION REAR SPAR ANGLE CRACKED. GROUNDED - YES. REMOVED DAMAGE, AND REAPIRED IAW SRM 57-10-10-2R-5.
AFT WET AREA FLOOR SUPPORT FROM STA 947 TO STA 967 RBL 47 HAS CORROSION. GROUNDED - YES. REMOVED AND REPLACED ON AFT WET AREA FLOOR SUPPORT FROM STA 947- 967 RBL 47 IAW B737-800 SRM 51-40-02-0G-0W= 1" O= .080 R= .064 L= 1" D= .016".
AFT WET AREA FLOOR STRAP AT STA 1016 RBL 3 HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED AFT WET AREA FLOOR STRAP AT STA 1016 RBL 3 IAW B737-800 SRM 51-40-02-0G-0 W- 1" O= .071 R= .054 L= 1.5" D= .017.
AFT WET AREA FLOOR STRAP AT STA 1016 LBL 3 HAS CORROSION. GROUNDED - YES. REMOVED & REPLACED AFT WET AREA FLOOR STRAP AT STA 1016 LBL 3 IAW B737-800 SRM 51-40-02-0G-0. W 1, O .071, R .059, L 1 1/12, D .018.
LEFT HORIZONTAL STAB RIB NR 6 IS CRACKED. GROUNDED - YES. REPAIRED THE LT HORIZONTAL STAB RIB NR 6 IAW SRM 55-10-09-2R-4.
LEFT HORIZONTAL STAB RIB NR 2 CRACKED. GROUNDED - YES. REPAIRED LT HORIZONTAL STAB RIB NR 2 IAW SRM 55-10-09-2R-4.
PANEL 193B LH OTBD PANEL LANDING GOUGED. GROUNDED - YES. REMOVED & REPLACED PANEL 193B LEFT OTBD PANEL LANDING IAW SRM 51-40-02-0G-0.
PANEL 193B RH AFT OB PNL LANDING GOUGED. GROUNDED - YES. REMOVED AND REPLACED PANEL 193D RH AFT PNL LANDING IAW SRM 51-40-02-0G-0 W= 1 O= .100 R= .084 L= 1 1/2" D= .016.
LEFT HORIZONTAL STAB LOWER SKIN IS CRACKED ON THE I/B SIDE OF STA 147.90 APPROX 8 INCHES FROM REAR SPAR.262A001. GROUNDED - YES. REPAIRED LEFT HORIZ STAB LWR SKIN AT STA 147 IAW B737-800 SRM 55-10-01-2R-11, THIS IS A CAT B REPAIR WITH A THRESHOLD AT 56,000 FLIGHT CYCLES & INTERVAL INSPECTION AT 9,000 FLIGHT CYCLES BY DVI & LFEC.
AFT CARGO RH CARGO TRACK HAS SCRIBE MARKS AROUND CARGO TIEDOWNS AND AREAS OF CORROSION NEAR STA 787. GROUNDED - YES. REPAIR AFT CARGO RH CARGO TRACK IAW SRM 53-00-53-2R-3 W= 1.5" O= .070" R= .045" L= 4" D= .025".
FWD CARGO AFT BULKHEAD RT SIDE LOWER SUPPORT HAS CORROSION AND BARE METAL. GROUNDED - YES. REMOVED AND REMPLACED FWD CARGO AFT BULK HEAD RH SIDE LOWER SUPPORT IAW SRM 51-40-02-0G-0W= 1 O= .071 R= .041 L= 2 D =.030.
RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED ON THE INBD SIDE OF HSS 129.560 APPROX 24 INCHES FROM FRONT SPAR. GROUNDED - YES. REPAIRED RT HORIZONTAL STAB LOWER SKIN AT STA 129 IAW SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR, WITH A THRESHOLD INSPECTION AT 56,000 FLIGHT CYCLES AND A INTERVAL INSPECTION AT 9,000 FLIGHT CYCLES BY METHOD OF DVI & LFEC.
AFT CARGO RT CARGO TRACK CRACKED AT STA 727G AND 727J. GROUNDED - YES. REPAIRED AFT CARGO R/H CARGO TRACK AT STA 727G AND 727J IAW B737-800 SRM 53-00-53-2R-3.
RIGHT HORIZONTAL STAB LOWER SKIN IS CRACKED ON THE I/B SIDE OF STA 138.70 APPROX 9 INCHES FROM FRONT SPAR. GROUNDED - YES. REPAIRED RIGHT HORIZONTAL STAB SKIN AT STA 138.70 APPROX 9 INCHES FROM FRONT SPAR IAW B737-800 SRM 55-10-01-2R-11. THIS IS A CAT B REPAIR WITH A THRESHOLD INSPECTION AT 56,000 FLIGHT CYCLES AND A INTERVAL INSPECTION AT 9,000 FLIGHT CYCLES BY METHOD OF DVI & LFEC.
AFT CARGO DOOR SHIELD FWD OF DOOR HAS AREAS OF CORROSION. GROUNDED - YES. REMOVED & REPLACED AFT CARGO DOOR SHEILD FWD OF DOOR IAW B737-800 SRM 51-40-02-0G-0. W 2, O .050, R 0, L 3, D .050.
AFT CARGO RH TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM STA 727 TO STA 787. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO RH TRANSITION PANEL FROM STA 727 TO STA 787 IAW B737-800 SRM 53-00-53-2R-3W: 3" O: .040 R: O" L: 20" D: .040".
AFT CARGO LH TRANSITION PANEL HAS SEVERAL AREAS OF CORROSION FROM STA 727 TO STA 767. GROUNDED - YES. REMOVED AND REPLACED AFT CARGO LH TRANSITION FROM STA 727 TO STA 767 IAW B737-800 SRM 53-00-53-2R-5W: 2" O: .040" R: 0 L: 20" D: .040".
FWD CARGO LH TRANSITION HAS SCRIBE MARKS AND GOUGES FROM STA 480 TO STA 500D. GROUNDED - YES. REMOVED & REPLACED FWD CARGO LH TRANSITON FROM STA 480 TO STA 500D IAW B737-800 SRM 53-00-53-2R-5. W 1, O .040, R .033, L1, D .007.
AFT CARGO PIT STRAP IB OF LOWER SILL WEB AT STR 24 HAS AREAS OF CORROSION FROM STA 787 TO STA 807. GROUNDED - YES. REMOVED & REPLACED AFT CARGO PIT STRAP IB OF LOWER SILL WEB AT STR 24 IAW B737-800 SRM 51-40-02-0G-0W= 1" O= 0.100" R= .085" L= 1" D= .015.
FWD CARGO RH TRANSITION HAS CORROSION FROM STA 500A TO STA 500I. GROUNDED - YES. REMOVED & REPLACED FWD CARGO RH TRANSITION FROM STA 500A TO STA 500I IAW B737-800 SRM 53-00-53-2R-5. W 1, O .040, R .022, L 1, D.018.
WHILE PERFORMING T.C. #78233001, EMERGENCY LIGHT BATT PACKS REQUIRE REPLACEMENT X3. GROUNDED - YES. REMOVED AND REPLACED BATT PACK AND CHARGER AT M1670, M1695, AND M1675 IAW AMM 33-51-06-960-805/806. NEW UNITS FROM STOCK CHECK GOOD. ALL EMERGENCY LTS ILLUMINATE NORMALLY AS REQ'D.
RUDDER LH SIDE SURFACE HAS SIGNS OF CORROSION NEAR FWD SIDE OF STATIC WICK BASE 3RD FROM THE TOP. GROUNDED - YES. REPAIRED DAMAGE SKIN ON L/H SIDE OF RUDDER BENEATH CONDUCTIVE FRAME & REPLACED DAMAGED CONDUCTIVE FRAME IAW ASA EA# CMPT-55EA-26012. PERORMED CALCULATED BALANCE PROCEDURE, NEW CBM IS +521.088, WITHIN ALLOWABLE LIMITS. THIS REPAIR IS A CAT "A" REPAIR.
AFT INTERIOR AND EXTERIOR EMERGENCY EXIT LIGHTS NEAR AFT ENTRY DOOR INOP. GROUNDED - YES. REMOVED & REPLACED BATTERY PACK MIG 72 ON LOG PAGE 60618032. OPS CHECKS GOOD. REF B737 AMM 33-51-06.
R/H HORIZONTAL STABILIZER LOWER SKIN HAS A 2.5" CRACK INDICATION AT THE REAR SPAR LOCATED AT STAB. STA. 95". AS MARKED. GROUNDED - YES. REPAIRED RIGHT HAND HORIZONTAL STABILIZER LOWER SKIN AT REAR SPAR STABILIZER STATION 95". IAW B737-800 SRM 55-10-01 REPAIR 11THIS IS A CATAGORY B REPAIR WITH INSPECTIONS REQUIRED AT INTERVALS OF 9,000 FLIGHT CYCLES WITH AN INSPECTION THRESHOLD OF 56,000 FLIGHT CYCLES IAW B737 800 SRM 55-10-01-2R-11 PARA 5 TABLE 204.
L/H HORIZONTAL STABILIZER LOWER SKIN HAS A CRACK INDICATION 1/2" IN LENGTH AT STAB. STATION 101.90. LOCATED 19.50" FROM FRONT SPAR. AS MARKED. GROUNDED - YES. REPAIRED L/H HORIZONTAL STABILIZER LOWER SKIN CRACK BY INSTALLING DOUBLER IAW B737-NG SRM 55-10-01-2R-11. P/N: 2024-T3 .100" X 48 = 144". PO: 1028431.1 P/N: 2024-T3 .071" X 48" X 144" PO: 1051295.2.THIS IS A CATAGORY B REPAIR WITH INSPECTIONS REQUIRED AT INTERVALS OF 9,000 FLIGHT CYCLES WITH AN INSPECTION THRESHOLD OF 56,000 FLIGHT CYCLES IAW B737 800 SRM 55-10-01-2R-11 PARA 5 TABLE 204.
WHILE PERFORMING ASA TASK CARD 78233001, 2X EMERGENCY LIGHT BAT PACKS FAIL FUNCTION CHECK. GROUNDED - YES. REMOVED AND REPLACED EMERGENCY LT POWER SUPPLY AND BATT PACK IAW B737-800 AMM 33-51-06-960-806 X2. BOTH NOW PASS FUNCTIONAL CHECK.
DURING DEFERRED ITEM REVIEW, FOUND PLT DEFECT 300009862 REQUIRES RE-EVALUATION FOR CORRECT DEFECT CATEGORY ( REPAIR DOUBLER IN LH PRIMARY STATIC PORT RVSM EXTRA CRITICAL AREA). GROUNDED - YES. ON DEFERRAL.
R/H HORIZ STAB LWR SKIN CRACKED @ 2 PLACES, STAB STA 147.7, 23.5"-25.5" AND 31"-32.5" AFT OF FRONT SPAR GROUNDED - YES. REPAIRED I.A.W. SRM 55-10-01-2R-11 REPAIR 11
R/H HORZ. STAB LWR SKIN CRACKED @ STAB STA 1001.7, 36.75"- 38.5" AFT OF FRONT SPAR. GROUNDED - YES. REPAIRED I.A.W. B737-800 SRM 55-10-01-2R-11 REPAIR 11
LH FWD EXIT ESCAPE DOOR EMERGENCY LIGHT INOP. GROUNDED - YES. REMOVED & REPLACED M2335 (EMERGENCY POWER SUPPLY) REF B737-800 AMM 33-51-06 OPS NORMAL.
EMERGENCY ROW EXIT LIGHT HANGING FROM CEILING. GROUNDED - YES. REINSTALLED MID CABIN EMERGENCY EXIT SIGN IAW B737-800 AMM 33-51-01 - SIGN OPS OK.
R/H FWD OVERWING EXIT LIGHT INOP. GROUNDED - YES. RELAMPED R/H FWD OVERWING EXIT SIGN LAMP, OPS CHECK GOOD REF B737-800 AMM 33-51-01.
FA REPORTS L1 DOOR DIFFICULT TO CLOSE AND HANDLE GOT STUCK BEFORE DOOR WAS FULLY CLOSED. GROUNDED - YES. OPERATED L1 DOOR SEVERAL TIMES, ALL OPERATIONS & INDICATIONS NORMAL, NO DEFECT NOTED. NO RECENT HISTORY.
EMERGENCY LIGHT AISLE LIGHT INOP AT ROW 24 RIGHT. GROUNDED - YES. REMOVED, REPLACED, AND TESTED EMERGENCY LIGHT AISLE LIGHT ASSY AT ROW 24 RIGHT PER AMM 33-51-03-960-802 - OPS NORMAL
EMERGENCY LIGHT SYSTEM OPERATIONAL TEST WITH COCKPIT SWITCH FAILED FOR FORWARD RIGHT SIDE GROUNDED - YES. REMOVED AND REPLACED EMERGENCY POWER SUPPLY M1676 S/N 64177 AND PERFORMED SUCCESSFUL SYSTEM OP CHECK IAW B737-800 AMM 33-51-06-960-806.
R1 DOOR HEADER PANEL HAS INOP EMERGENCY LIGHT. GROUNDED - YES. REMOVED AND REPLACED R1 DOOR HEADER PANEL EMERGENCY LIGHT M1674 IAW AMM 33-51-06, SYSTEMS CHECKS GOOD IAW AMM 33-51-06 AND 33-51-00.
FORWARD PIT RT SIDE ZEE CHANNEL CONTAINS SEVERAL SPOTS OF CORROSION FROM STATION 500B TO 500E. GROUNDED - YES. REMOVED DAMAGED ZEE CHANNEL SECTION FROM STATION 500B-500E + 10 AT FORWARD PIT RT SIDE AFTER IT WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-53-1A-2. ORIG MATERIAL .040, MATERIAL LOSS .006, MATERIAL REMAINING .034. ACCOMPLISHED ZEE CHANNEL REPAIR IAW SRM 53-00-53-2R-5 REPAIR 5.
FORWARD PIT LT SIDE HAS ANGLE BRACKET CRACKED AT LBL 23 APPROX STATION 500H, UNDERNEATH ZEE CHANNEL. GROUNDED - YES. REMOVED CRACKED ANGLE BRACKET LOCATED AT FWD PIT LT SIDE AT APPROX LBL 23, STATION 500H UNDERNEATH ZEE CHANNEL AND REPLACED WITH NEW ANGLE BRACKETIAW SRM 51-40-02 AND BOEING DWG 143A7505 REV-.
FORWARD PIT RT SIDE HAS ANGLE BRACKET CRACKED AT RBL 24 APPROX, STATION 500G AFT SIDE, UNDERNEATH ZEE CHANNEL. GROUNDED - YES. REMOVED CRACKED ANGLE BRACKET LOCATED AT FWD PIT RT SIDE AT APPROX RBL 24, STATION 500G AFT SIDE UNDERNEATH ZEE CHANNEL AND REPLACED WITH NEW ANGLE BRACKET IAW SRM 51-40-02 AND DWG 143A7505 REV-.
AFT CARGO RT TRANSITION PANEL CRACKED STA 727H. GROUNDED - YES. AFT CARGO RT TRANSITION PANEL EVALUATED AND FOUND TO BE OUT OF LIMITS IAW 53-00-53-1A-2 REMOVED AND INSTALLED NEW TRANSITION PANEL IAW SRM 53-00-53-2R-5 AND 51-40-02 REPLACED ZEE CHANNEL FROM BS727-BS767 NUT PLATE INSTALLED ON NON-ROUTINE 30032.
FLOORBEAM TRANSITION PLATE RT FROM STA 767 TO STA 787 IS CORRODED. DOT & STREAMER ATTACHED. GROUNDED - YES. REMOVED CORRODED SHIELD FROM BS767-BS787, LOCATED AND DRILLED NEW SHIELD P/N 146A8127U12 PO# 954475.1 INSTALLED NEW SHIELD PER BAC DWG # 146A0081 REV -.
AFT CARGO DOOR SILL PLATE HAS SEVERAL AREAS CORRODED - DOT & STREAMER ATTACHED. GROUNDED - YES. REMOVED AND REPLACED (WEB) DOOR SILL PLATE REF BAC DRWG 146A8340.
FORWARD FLOOR SUPPORT SHIELD IN FORWARD PIT RT SIDE IS CORRODED (STATION 500 RBL 24 APPROX.). GROUNDED - YES. BLENDED CORROSION FROM SHIELD IN FWD PIT RT SIDE @ BS 500 ORG MAT .032, REMOVED .005, .027 REMAINS. FOUND TO BE OUT OF LIMITS PER 53-30-15. REMOVED AND REPLACED SHIELD WITH NEW SHIELD P/N 143A8126429 PO#954561.1 PER BAC DWG 143A0080 REV A.
FORWARD PIT RT SIDE HAS ANGLE BRACKET CRACKED AT RBL 24 APPROX, STATION 500H, UNDERNEATH ZEE CHANNEL. GROUNDED - YES. REMOVED CRACKED ANGLE BRACKET AND REPLACED WITH NEW ANGLE BRACKET AT FORWARD PIT RT SIDE IAW SRM 51-40-02 AND DWG 143A7505 REV - AT APPROX RBL 24, STA 500H UNDERNEATH ZEE CHANNEL.
FORWARD PIT RT SIDE HAS ANGLE BRACKET CRACKED AT RBL 24 APPROX, STATION 500F, UNDERNEATH ZEE CHANNEL. GROUNDED - YES. REMOVED CRACKED ANGLE BRACKET AT FWD PIT RT SIDE APPROX RBL 24, STATION 500F UNDERNEATH ZEE CHENNEL AND REPLACED WITH NEW ANGLE BRACKET IAW SRM 51-40-02 AND DWG 143A7505 REV-.
FORWARD PIT RT SIDE HAS ANGLE BRACKET CRACKED AT RBL 24 APPROX, STATION 500G, UNDERNEATH ZEE CHANNEL. GROUNDED - YES. REMOVED CRACKED ANGLE BRACKET LOCATED AT FWD PIT RT SIDE AT APPROX RBL 24 STATION 500G UNDERNEATH ZEE CHANNEL AND REPLACED WITH NEW ANGLE BRACKET IAW SRM 51-40-02 AND DWG 143A7505 REV.
FLOORBEAM @ STA 727I LH HAS PULLED THRU FASTENED- DOT & STREAMER ATTACHED. GROUNDED - YES. REMOVED AND REPLACED DAMAGED ZEE CHANNEL SECTION FROM LT STA 727 TO 827+8 IAW SRM 53-00-53-2R-5 REPAIR 5.
FRAME BEEF UP PLATE & SUB STRUCTURE RH @ STA 787 IS CORRODED - DOT & STREAMER ATTACHED. GROUNDED - YES. REMOVED AND REPLACED CORRODED FRAM SPLICE PLATE @ BS787 WITH NEW SPLICE PLATE P/N 146A1300U3 PO# 954829.1 PER BAC DWG #1436A1262 REV -.
MAIN CABIN FLOOR STRUCTURE INTERCOASTAL CRACKED AROUND FASTENER HOLE AREA (CRACK IS ON TOP AND BOTTOM) BETWEEN STATION # 277 AND 294 AT RBL 1. GROUNDED - YES. REMOVED AND REPLACED INTERCOASTAL IAW DEG 141A5400 AND SRM 51-40-02.
WATER SERVICE DOOR #146AR INNER PAN (2EA) AREA CORRODED. GROUNDED - YES. REMOVED AND REPLACED INNER PAN PN 147A7221-30 REF BAC DWG 147A7221 REV "D" AND SRM 51-40-02, WATER TANK DRAIN VALVE OPS CHECK GOOD REF AMM 38-11-08, WATER TANK FILL/OVERFLOW VALVE OPS CHECK GOOD REF AMM 38-11-03, PAINTED AREA REF AMM 51-21-99.
WHILE PERFORMING T/C 78233001, FOUND THE EMERGENCY LIGHTS DID NOT PASS A CAPACITY TEST, OVERWING, AFT EXIT, EXTERNAL LEFT AND RIGHT, LEFT AND RT OVERHEAD BIN ROWS 16 - 25, ENTRY OVERHEAD EXIT, AND L1 DOOR LIGHTS. ACFT GROUNDED. REMOVED & REPLACED THE BATTERY PACKS IAW AMM 33-51-06. OPS CHECKED GOOD.
RT FWD OVERWING EMERGENCY LIGHT INOP. GROUNDED - YES. RELAMPED RT FWD OVERWING EMERGENCY LIGHT REF AMM 33-51-04 OPS CHECK GOOD.
EMERGENCY LIGHT INOPERATIVE AT THE OVERWING EXTERIOR FWD RT. ACFT GROUNDED. REPLACED THE LAMPS, OPS CHECKED NORMAL IAW AMM 33-51-04-960-801.
REACHING TOP OF CLIMB AT FL350, AFT FLT ATTENDANTS REPORTED A METALLIC ODOR STARTING AT THE L2 DOOR AREA AND CONTINUING TO ROW 24. THE ODOR WAS STRONGEST ON LEFT SIDE OF AFT CABIN TO INCLUDE APPARENT DISCHARGE FROM OVERHEAD GASPER VALVES. OVENS WERE ON WITH FOOD BUT F/A CONFIRMED DIFFERENT ODOR THAT REPORTED SHE EXPERIENCED ODOR ON GROUND BEFORE ENGINE START. CHECKLIST COMPLETED TO RECIRCULATION FANS ONLY. ACFT GROUNDED. EMERGENCY DECLARED, APU NOT RUNNING WHEN DEFECT REPORTED BY CREW. COMPLIED WITH CABIN ODOR TROUBLESHOOTING IAW AMM 05-51, TASK 814, RAN ENGINES, ISOLATED PACKS, AND INSPECTED THE AREA AROUND ROW 24ABC, NO DEFECTS NOTED, INSPECTED THE AFT GALLEY OVENS, AND COFFEE MAKERS, NO DEFECTS NOTED, INSPECTED DOOR AREA HEATERS, NO DEFECT NOTED. NO HISTORY REPORTED WITHIN LAST 15 DAYS. COULD NOT DUPLICATE ITEM ON GROUND, IAW AMM 05-51, TASK 814, PAGE 6A.
EMERGENCY LIGHT EXTERIOR SLIDE LIGHT AT THE R2 DOOR WAS INOPERATIVE. ACFT GROUNDED. VERIFIED 6.2 VDC AT L733 SLIDE LIGHT AND GOOD GROUND FOR LIGHT. REPLACED THE LAMP AND TESTED R2 DOOR SLIDE LIGHT IAW AMM 33-51-04-960-801. OPS NORMAL.
MAIN CABIN BS 344-360, LBL 12 FLOOR SUPPORT CRACKED. ACFT GROUNDED. REMOVED AND INSTALLED A NEW FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5410, REV E.
AFT CARGO DOOR SILL CORRODED BS 794 - BS 847, BL R24. ACFT GROUNDED. REMOVED CORROSION IAW SRM 51-10-02, ORIGINAL .050 REMOVED .005 REMAINING .045 FOUND TO BE WITHIN LIMITS IAW SRM 53-60-15, T8225Y. ALODINED IAW SRM 51-20-01, PRIMED IAW AMM 51-21-72, MARKED BLENDOUT IAW AMM 51-05-01, REMOVED DOT.
MAIN CABIN BS 312-328, LBL 48 FLOOR SUPPORT CRACKED. ACFT GROUNDED. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-40-02, PARA 7 AND DWG 141A5400, REV -.
MAIN CABIN BS 312-328, RBL 44 FLOOR SUPPORT CRACKED. ACFT GROUNDED. R & R THE FLOOR SUPPORT IAW SRM 51-40-02 AND BAC DWG 141A5410 REV A.
MAIN CABIN AFT FLOOR WEB, UPPER SURFACE, CORRODED, DOTTED,BS 986 - 988, RBL 30 - 45. ACFT GROUNDED. REMOVED CORROSION IAW SRM 53-70-51-1A-1, FOUND TO BE BEYOND LIMITS IAW SRM 53-70-51-1A-1, FIG 103, DETAIL "C". FABRICATED DOUBLER AND FILLER IAW SRM 51-70-13-2R-3, ALODINED AND PRIMED IAW SRM 51-20-01, INSTALLED DOUBLER & FILLER IAW SRM 51-0-13-2R-3.
MAIN CABIN BS 285-294.5, BL 0 FLOOR SUPPORT CRACKED. ACFT GROUNDED. R & R IAW SRM 51-40-02 AND DWG 141A5400, REV.
MAIN DECK FLOORBEAM ANGLE CRACKED. MARKED & DOTTED. BS 540, BL 0 - RBL 5. ACFT GROUNDED. REMOVED CRACKED FLOORBEAM ANGLE IAW SRM 51-40-02. LOCATED, DRILLED, AND INSTALLED NEW FLOORBEAM ANGLE IAW SRM 51-40-02, 51-40-05, AND DWG 143A0060-51, REV D.
MAIN CABIN FLOOR SUPPORT CRACKED, BS 344-360, BL 0. ACFT GROUNDED. R & R FLOOR SUPPORT IAW SRM 51-40-02 AND DWG 141A5410, REV.
MAIN DECK FLOORBEAM CRACKED. BS 540, BL 0 - LBL 5. ACFT GROUNDED. REMOVED CRACKED FLOORBEAM IAW SRM 51-40-02 LOCATED, DRILLED, AND INSTALLED NEW FLOORBEAM IAW SRM 51-40-02, 51-40-05 AND DWG 143A0060-51, REV D.
CRACK FOUND .740" LONG, 8.5" FWD OF AFT SPAR, RT HORIZONTAL LOWER SKIN INBD OF STABILIZER, BS 138.70, MARKED. ACFT GROUNDED. REPAIRED LOWER SKIN ON RT HORIZONTAL STABILIZER AT BS 138.70 IAW SRM 55-10-01-2R-11, INSPECTION THRESHOLD 56,000 CYCLES AFTER REPAIR INSTALLATION METHOD. DETAIL EDDY CURRENT INSPECTION INTERVAL: 9000 FLIGHT CYCLES, TABLE 204, REMOVED DOT.
CRACK FOUND .840" LONG, 8" FWD OF AFT SPAR, RT HORIZONTAL LOWER SKIN INBD OF STABILIZER BS 184.70. ACFT GROUNDED. REPAIRED LOWER SKIN OF RT HORIZONTAL LOWER SKIN AT BS 184.70 IAW SRM 55-10-01-2R-11, INSPECTION THRESHOLD 56,000 CYCLES AFTER REPAIR INSTALLATION, METHOD: DETAIL VISUAL INSPECTION AND EXTERNAL LOW FREQUENCY EDDY CURRENT INSPECTION INTERNAL: 9000 FLIGHT CYCLES, TABLE 204.
AFT ENTRY DOOR CUTOUT FWD FRAME UPPER NR 1 PRSSURE PAD FITTING GOUGED. ACFT GROUNDED. REMOVED DOOR LINING IAW AMM 25-21-25, R & R FITTING IAW DWG 147AS101, REV D AND SRM 51-40-02 AND REINSTALLED DOOR LINING IAW AMM 25-21-25, DOT REMOVED .
RED & WHITE BACKLIGHT EXIT SIGN BY R1 DOOR FELL OFF. ACFT GROUNDED. REPLACED R1 EXIT LIGHT ASSY. OPS NORMAL.
R1 GALLEY DOOR EXIT LIGHT COVER IS OFF. ACFT GROUNDED. REPLACED R1 GALLEY DOOR EXIT LIGHT COVER REF AMM 33-51-00. OPS TEST NORMAL.
LT HORIZONTAL LOWER SKIN HAS 2 CRACKS AT STA. 138.7, APPROXIMATELY 9' AND 17' FROM THE AFT SPAR. ACFT GROUNDED. REMOVED DAMAGE FABRICATED DOUBLER AND 3 EA FILLERS AND INSTALLED REPAIR IAW SRM 55-10-01-2R-11, REPAIR 11, ALODINED IAW SRM 51-20-01 PRIMED IAW AMM 51-21-72 PAINTED IAW AMM 51-21-99. THIS IS A CAT B REPAIR INSPECTION THRESHOLD IS 56,000 FLIGHT CYCLES AND REPEAT INSPECTION INTERVAL IS 9000 FLIGHT CYCLES IAW TABLE 204 .
DURING EMERGNECY LIGHT TEST, TWO BATTERIES FAILED 15 MINUTE CHECK. ACFT GROUNDED. R & R THE BATTERY PACKS AND REPEATED TEST. TEST PASSED.
L1 DOOR WILL NOT LATCH SHUT FROM THE INSIDE. ACFT GROUNDED. FOUND L1 DOOR GUIDE ARM OUT OF ADJUSTMENT. ADJUSTED GUIDE ARM, OPS CHECKED GOOD IAW MM 52-11-00-820-801, STEP H.
WHILE ACCOMPLISHING L1 DOOR SLIDE OPERATIONAL CHECK, L1 DOOR SLIDE FAILED TO INFLATE AUTOMATICALLY. SLIDE DEPLOYED NORMALLY WITH MANUAL HANDLE. REMOVED AND REPLACED THE L1 DOOR ESCAPE SLIDE.