N14240
Registered owner: UNITED AIRLINES INC, IL (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
AFT CARGO LIGHT WAS EXTIGUISHED FROM GATE TO T/O AND ILLUMINATED ON T/O. REPEAT GRIPE.
FORWARD CARGO DOOR REQUIRES RESKIN. REMOVED WORN OUTER SKIN AND INSTALLED NEW OUTER SKIN REFERENCE IAW SRM 52-30-01-2R-3 AND BAC DWG 143A6110 REV A.
AFT CARGO COMPARTMENT BS 727 +10 BILGE STRINGER 27R ATTACH ANGLE CRACKED. REMOVED DAMAGED SECTION OF INTERNAL KEEL CHORD IAW SRM 53-60-12-2R-1. FABRICATED, LOCATED, DRILLED, TRIMMED REPAIR PARTS IAW SRM 53-60-12-2R-1. INSTALLED REPAIR IAW SRM 51-40-02 AND SRM 53-60-12-2R-1.
LEFT WING TE DEFLECTION CONTROL RIB ATTACH FLANGE FOR THE UPPER FIXED TE PANEL IS CRACKED. REPAIRED DEFLECTION RIB PER B737-800 SRM 57-51-02-2R-3 AND ECRA 5751-01643.
RIGHT WING LE FUEL CONTROL PANEL HAS SURFACE CORROSION AROUND THE FUEL QTY INDICATORS. ACCOMPLISHED -9 PART TRANS TO REMOVE AND REPLACE FUEL PANEL ASSY. REMOVED REFUELING PANEL. INSTALLED REFUELING PANEL, PERFORMED OPS CHECK, CHKD GOOD IAW AMM 28-21-00-400-801.
RH WING INTERNAL FUEL TANK UPPER STRINGER U-9 CRACKED AT THE OB END BETWEEN RIB NR 21 AND RIB NR 22. REPAIRED STRINGER U-9 PERE ECRA 5720-03573, REO G25950 AND ECRA 5723-01058.
FWD PIT DOOR FITTING AFT LOWER GOUGED. REMOVED AND INSTALL NEW STOP FITTING PN:143A6120-10 PO 1147348.1 IAW SRM 51-40-02 AND BAC DWG 143A6117 REV A.
LEFT WING T/E PANEL 571CB, PANEL SUPPORT IS CORRODED. REMOVED BEAM,FABRICATED NEW BEAM AND INSTALLED PER B737-800 SRM 51-40-02 AND BAC DWG 115A4711 REV B.
AFT CARGO DOOR REQUIRES RESKIN. REMOVED AND REPLACED AFT CARGO DOOR SKIN IAW BAC CMM 52-31-14, BAC 737-800 SRM 51-30-01-2R-3,BAC DWG 146A6110 REV C,AND B737-800 SRM 51-40-02.
B737-MP-2100-52-680-00 AFT CARGO COMPARTMENT DOOR FWD LOWER STOP FITTING IS GOUGED. ALL MAINTENANCE WAS ACCOMPLISHED BY AAR/GSO. THE SDR WAS COMPLETED BY UA/OSVQC. REMOVED AND INSTALLED NEW STOP FITTING PN: 146A6120-9 IAW BAC DWG 146A6110 REV C,146A6117 REV J AND B737-800 SRM 51-40-02.
FWD FWD CARGO COMPARTMENT DOOR AFT LOWER STOP FITTING IS GOUGED. REMOVED GOUGED STOP FITTING AND INSTALLED NEW STOP FITTING IAW DWG 146A6110 REV C AND B737-800 SRM 51-40-02.
B737-MP-2000-53-410-00-01 MAIN CABIN FLOOR BEAM STA 947.5 HAS CORROSION ON THE UPPER SURFACE AT APPROX LBL53. REMOVED DAMAGED CHORD (UPPER) REPLACED & INSTALLED NEW REPAIR PARTS AT STA 947.5 FROM LBL41 TO LBL58.6 WL 208 IAW SRM 53-70-51-2R-5 REPAIR 5 ALTERNATIVE 2.
L-1 DOOR HANDLE BOX CUTOUT, UPPER STUB BEAM HAS GOUGES. REMOVED AND REPLACED L-1 DOOR HANDLE BOX CUTOUT UPPER STUB BEAM IAW SRM 51-40-02 AND DWG 141A6163 REV-.
AFTER REMOVAL OF L2 LOWER SILL CHORD FOUND MAIN CABIN BS 927 TO 951 LT CUSP WEB HAS DOUBLE DRILLED HOLE. REMOVED, REPLACED AND INSTALLED NEW WEB AT BS 927 TO 947+ 4 LBL 58.6 WL208. IAW SRM 51-40-02-0G-0, AND DWG 147A8501, REV-.
MAIN CABIN STA 400 RH CREASE BEAM INNER CHORD CORRODED UPPER SURFACE. REPAIRED THE RT CREASE BEAM INNER CHORD AT STA 400 IAW SRM 51-70-12-2R-1 ,51-40-02, AND BAC DWG 143A5900, REV D, AND REV-.
MAIN CABIN L-2 DOOR SILL IS CORRODED ON THE UPPER SURFACE BETWEEN APPROX STA 947.5 AND 986.5 IN MULTIPLE SPOTS APPROX LBL53. REMOVED REPLACED AND INSTALLED NEW DOOR SILL FROM STA 887+6 TO STA 1006 WL208 LBL58. IAW SRM 51-40-02-0G-0 AND DWG 147A8501 REV C.
MAIN CABIN FLOOR SUPPORT IS CORRODED ON THE UPPER SURFACE BETWEEN BS 947.5 & 967 AT APPROX LBL50 . REMOVED, REPLACED, AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0, DWG 147A5650, REV -.
MAIN CABIN FLOOR SUPPORT CHANNEL BETWEEN BS 947.5 & 967 IS CORRODED ON THE UPPER SURFACE AT APPROX RBL50. REMOVED, REPLACED AND INSTALLED NEW FLOOR SUPPORT IAW SRM 51-40-02-0G-0 AND DWG 147A5760, REV -. 194
MAIN CABIN BS 987.5 FLOORBEAM IS CORRODED ON THE UPPER SURFACE AT APPROX RBL48 . REMOVED DAMAGE ON UPPER CHORD REPLACED AND INSTALLED NEW UPPER CHORD FROM LBL50 TO RBL50 WL208 STA987.5 IAW SRM 53-70-51-2R-4, REPAIR 4, ALTERNATIVE 1.
MAIN CABIN RH STA 927-951 WEB IS GOUGED ON UPPER SURFACE. REMOVED REPLACED AND INSTALLED NEW WEB AT STA 927 TO STA 951 RBL 58.6 WL208. IAW SRM 51-40-02-0G-0. DWG 147A8501 REV B.
MAIN CABIN FLOORBEAM BS 947.5 IS CORRODED ON THE UPPER SURFACE AT APPROX RBL50 . REMOVED DAMAGE ON UPPER CHORD AND INSTALLED NEW REPAIR PARTS AT STA 947.5 FROM RBL34 TO RBL58.6 WL208, IAW SRM 53-70-51-2R-5, REPAIR 5, ALTERNATIVE 2.
RIGHT HORIZONTAL STABILIZER,STA 101.90 REQUIRES ACCESS PANEL TO BE FABRICATED FOR #1 AND #2 VERTICAL STIFFNER REPAIRS IAW SRM 55-10-2R-11 FABRICATED REPAIR DOUBLER ON THE RH HORIZ STAB STA 101.90 IAW B737-800 SRM 55-10-01-2R-11. INSTALLED DOUBLER IAW B737-800 SRM 51-40-02 AND B737-800 SRM 55-10-01-2R-11.
MAIN CABIN FLOOR SUPPORT SUBSTRUCTURAL T ANGLE AT APPROX STA 951 IS GOUGED ON THE UPPER SURFACE AT APPROX LBL 20. REMOVED DAMAGE ORIG THICKNESS 0.075, REMOVED 0.012 REMAINING 0.063 AND REPAIRED IAW ECRA 5375-01024.
L1 DOOR CREASE PLATE AT FLOOR BETWEEN STA 290 TO 345 HAS CORROSION IN NUMEROUS PLACES. L-1 DOOR INNER CHORD CORRODED.REMOVED AND REPLACED. NO ISSUES NOTED. ADD EMP:V947134 REMOVED, LOCATED, DRILLED, AND REPLACED NEW INNER CHORD AT L1 DOOR FLOOR STRUCTURE BETWEEN BS 270 TO BS 355 IAW SRM 51-40-02-0G-0, 51-40-05-0G-0 AND DWG 141A8110 REV A.
FRAME AT BS 294.5 HAS NICKS AND BAREMETAL APPOX. STRL3 ON OUTSIDE SURFACE. DENTED FRAME REPAIRED IAW SRM 53-00-07-2R-1, DWG 141A0741 REV:A & REV:- & BAC PL:1410741 REV:J.
B737-MP-2000-53-110-00 ON RH FLOOR CREASE PLATE JUST AFT OF R1 DOOR UNDER FASTENER HOLE AT STA 332.1 HAS CORROSION. REMOVED AND INSTALLED NEW CREASE BEAM ON FLOOR STRUCTURE R1 DOOR BETWEEN BS260 TO BS360 RBL58 IAW B737-800 SRM 51-40 02-OG-0 AND DWG 141A8310 REV-.
RIGHT HORIZ STAB INBD SIDE OF RIB AT STAB STA 101.9 0 VERTICAL STIFFNER NR 1 IS CRACKED AT THE LOWER TRANSITION RADIUS. CUT AND REMOVED THE VISABLE CRACK FROM STIFFENER NO. 1 AT STA 101.90 RH HORIZ STAB IAW B737-800 SRM 55-10-09-2R-4. FABRICATED REPAIR ANGLE SHIMS AND T-ANGLE IAW B737-800 SRM 55-10-09-2R-4. INSTALLED ALL REPAIR PARTS IAW B737-800 SRM 55-10-09-2R-4 AND B737-800 SRM 51-40-02.
EA 5340-02153-003 LH STA 639 LOWER AFT STUB BEAM FASTENER HOLE HAS CRACK INDICATION. REMOVED STRAP ASSY AT STA 639 LH STUB BEAM IAW B737NG SRM 51-40-02. RECEIVED A NEW STRAP ASSY PN 111A6504-9 PO 1145389.1 LOCATED, DRILLED, DEBURRED AND INSTALLED IAW B773-800 SRM 51-40-02, DWG 144A1715 REV - AND EC/RA 5340-02266. PERFORMED BY AAR GSO MECH V932599 INSP QC444
R/H HORIZ STAB INBD SIDE OF RIB AT STAB STA 101. 90 VERTICAL STIFFNER #2 IS CRACKED AT THE LOWER TRANSITION RADIUS. CUT AND REMOVED THE VISABLE CRACK FROM STIFFENER NR 2 AT STA 101.90 RH SIDE IAW B737-800 SRM 55-10-09-2R-4. FABRICATED REPAIR ANGLE SHIMS AND T-ANGLE IAW SRM 55-10-09-2R-4. INSTALLED ALL REPAIR PARTS IAW SRM 55-10-09-2R-4 AND B737-800 SRM 51-40-02.
RIGHT UPPER CENTER WING STA-540 FLOOR SUPPORT STRUCTURE CROSSBEAM HAS CRACKS AND BENT. REMOVED AND REPLACED RT FLOOR SUPOORT BS 540 SRM 51-40-02 AND DWG 143A5240 REV:- .
LEFT UPPER CENTER WING BS 540 FLOORBEAM HAS CRACKS AND BENT. REMOVED AND REPLACEDF LT FLOORBEAM BS 540 IAW SRM 51-40-02 AND DWG 143A5240, REV-.
FLAPS DIDNT EXTEND PAST 2 DEG FSEU SHOWS CURRENT FAULT 27-55259 TE FLAP SENSOR L. CORRECTION. CODE IS 27-52259 SPOKE WITH FLIGHT CREW. ON APPROACH DURING CONFIGURATION SETUP, DEPLOYED FLAPS BUT THEY WOULD NOT EXTEND PAST 2 DEGREES. CREW DECIDED TO GO AROUND AND FOLLOWED FLAP DISAGREE CHECK LIST. CREW USED ALTERNATE FLAPS. LANDED NORMALLY, NO ISSUES WITH BRAKES AND NO ADDITIONAL DEFECTS ON LANDING. PERFORMED BONDING CHECK OF THE NEW FLAP POSITION TRANSMITTER REF AMM 27-58-01-400-801. BONDING CHECK WAS WITHIN LIMITS. REMOVED AND REPLACED FAULTY LH FLAP TRANSMITTER ASSEMBLY WITH "REPAIRED" ASSEMBLY. REFFERENCE A.M.M. 27-58-01. OPS CHECK GOOD.
R1 DOOR FWD FRAME LOWEST POSITION DOOR STOP BEARING PAD CRACKED, ACROSS ENTIRE DIAMETER AT 2 LOCATIONS. REMOVED R1 DOOR FWD DOOR FRAME LOWEST STOP FITTING BEARING PLATE IAW AMM 52-11-01-000-801. CLEAN AND PREPPED AREA FOR STOP PLATE INSTALLATION. REMOVED AND REPLACED LOWEST DOOR STOP PER AMM 52-11-01-400-801. OP CHECK GOOD.
RIGHT AFT OVERWING EMERGENCY ESCAPE LIGHT OUT, RELAMPED, NO HELP. REF AMM 33-51-04 FOR LAMP REPLACEMENT. RT OVERWING ESCAPE LIGHT OP CHKD NORMAL IAW AMM 33-51-00-710-801.
RIGHT AFT EMERGENCY LIGHT, BY THE AFT CARGO DOOR OUT, RELAMPED, NO HELP. BOTH RT OVERWING ESCAPE LIGHT (L7) AND RT OVERWING ESCAPE GROUND ILLUMINATION LIGHT (L548) ARE POWERED BY M1670 POWER SUPPLY. PLACED POWER SUPPLY AND LIGHT ASSEMBLY. OP CHKD NORMAL IAW AMM 33-51-00-710-801.
EXCESSIVE SLIDE MATERIAL ON DOOR 1R REMOVED R1 SLIDE, RE-SECURED GIRT BAR MATERIAL, AND REINSTALLED SLIDE AT DOOR 1R IAW AMM 25-66-01. OPERATIONAL CHECK GOOD, MATERIAL NO LONGER AN ISSUE. PERFORMED RII INSP OF R1 SLIDE INSTALL PER GMM 09-25-05. RII INSP OK.
REMOVED R1 DOOR ESCAPE SLIDE PACK AND COVER FOM REF AMM 25-66-01-000-801. RE-INSTALLED R1 DOOR SCAPE SLIDE PACK AND COVER REF AMM 25-66-01-400-803. VERIFIED R1 DOOR SLIDE INSTALLED IAW AMM 25-66-01-400-803.
L1 WINDOW CRACKED ROTABLE PARTS CHANGE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1564418 SN OFF 3856 WINDSHIELD, B73 OFF 99-5610-9-9001 3856 ON 99-5610-9-9001 8239 REMOVED AND REPLACED L1 WINDSHIELD IN REF TO AMM TASK 56-11-11-400-801. LEAK CHECK GOOD, AND WINDOW HEAT TEST GOOD AT THIS TIME. ADD EMP:U403011
ELECTRIC STAB TRIM STOPPED WORKING DURING CLIMBOUT USING THE TRIM YOKE SWITCH ACCOMPLISH OPERATIONAL TEST OF STAB TRIM NO ANOMOLIES FOUND. DFCS BITE NORMAL. NO INBOUND FLIGHT FAULTS ON CURRENT LEG OR HISTORY. ACCOMP LAND VERIFY TEST AMM 22-11-00-700-001 PASS. ALL STAB TRIM FUNCTIONS CAPT AND FO NORMAL. AC REMAINS FULL CAT CAPABLE.
CORROSION ON FUSELAGE BELLY SKIN AROUND BILGE DRAIN JUST AFT OF BS 727J LEFT DRAIN #35. ACCOMPLISHED FUSELAGE BELLY SKIN REPAIR AT BILGE DRAIN STA 727J. REF ECRA 5330-07105, SEE PARTIAL WORK ACCOMPLISHED. TRANSCRIBED FROM AERSALE DOC # 33748 WORK PERFORMED BY EMP STAMP# ALD011.
(B737-57-4-1202) CORROSION ON LOWER SKIN L/H WING SURFACE IN SPA R AREA OUT BY WING TIP RIB 27.
(737-54-3-0115) R/H WING INBD OF PYLON L/E SUPPORT BRACE HAS CRACK IN RADIUS
5100-02757 FOUND CORROSION ON AFT CARGO FLOOR PNL 140CF AT APPROXIMATELY BS 767 ON NUTPLATE STRIP REMOVED AND REPLACED ''T'' FLOOR AFT CARGO PNL 140CF AT BS767 IAW B737-800 SRM 53-00-53 2R-1. DATA WAS TRANSCIBED FROM PAPER DOC A ERSALE WO 3985 OP 33721 BY MEN V942859 INSP AQC044.
5100-02757 FOUND CORROSION ON AFT CARGO FLOOR PNL 140CF AT APPRO XIMATELY BS 767 ON NUTPLATE STRIP REMOVED AND REPLACED ''T'' FLOOR AFT CARGO PNL 140CF AT BS767 IAW B737-800 SRM 53-00-53 2R-1. DATA WAS TRANSCIBED FROM PAPER DOC A ERSALE WO 3985 OP 33721 BY MEN V942859 INSP AQC044.
RIGHT RAM AIR DEFLECTOR DOOR SUPPORT BRACKET CRACKED SEE PHOTO. ADDED PART #. REF IPC. 21-51-22-21 REMOVED RIGHT RAM AIR DEFLECTOR SHAFT ASSY. REF AMM 21-51-22. SHAFT WAS CORRODED AND LINKAGE SEIZED ONTO SHAFT. ALL NEW HARDWARE ORDERED REPLACED SUPPORT BRACKET REF AMM 21-51-22-400-802
ON TAKE OFF POWER OVER HEAD PANEL LIGHTS LEFT FWD OVERWING LEFT AFT OVERWING R742. NO HELP PROBLEM REMAINS. SWAPPED ENGINE 1 RUNNING RELAY R737. NO HELP PROBLEM REMAINS. T/S REF FIM 52-20 TASK OVERWING EXIT DOOR FLIGHT LOCK SWITCH PSEU BITE FOUND MSG L FL SW FAULT 52-72007 PER OUTBOUND FLT CREW GND SPD REJECTED T/O 20 KNT. REF FIM TASK 52-20 TASK 81. TEST FAILS INITIAL EVALUATION. PROBLEM , FAULT MSG LATCH ON PSEU 52-72007 . LEFT FWD AND AFT OVERING EXIT LIGHTS COME ON, LEFT FWD AND AFT FLIGHT LOCK SOLENIODS DO NOT WORK AND DOORS WILL OPEN. RIGHT OVERWING DOORS OPS CHECK NORMAL. REPLACED LEFT FLIGHT LOCK RELAY FOUND D48112 @J48 UNSEATED. RESEATED AND RESECURED D48112 . REF AWM 52-71-13. OPS CHK GOOD.
LOW PRESSURE LIGHT FOR THE FUEL PUMP LIGHT ON NO. 2 AFT FUEL PUM P PLACED R/H AFT FUEL BOOST PUMP ON MEL 2801A DISPATCH DESK: 85 NAME: N R.DATE: 19-DEC-21- NOCDESK: 800 NAME: R B. DATE: 19-DEC-21- DEFERRED DIRECTLY BY TOMC UPDATED MAA CODE FIX USING VENDOR MAA SCREEN MAC METER INITIATED FOR WITH VENDOR ID V931347 MAC METER INITIATED FOR WITH VENDOR ID V123456 PLEASE CONTACT TOMC BEFORE COMMENCING ANY WORK. MAC RELATED WORK ORDER 000000003029951 AND PRTR MAC RELATED WORK ORDER 000000003029951 AND PRTR PLACED R/H AFT FUEL BOOST PUMP ON MEL 2801A PLACED R/H AFT FUEL BOOST PUMP ON MEL 2801A T/S PER FIM 28-22-00-810-805 FOUND GFI OPENED. PERFORMED STEP RESISTANCE TEST PER AMM TASK 28-22-00-760-802. NO TIME TO COMPLY F FAULT ISOLATION PROCEDURE .REQUIRES FUEL BOOST PUMP INSULATION WITH FUEL PUMP C/B PULLED AND COLLARD AND UFI IS OPEN
DURING PRESSURIZING F/O WINDOW REF LP 6716164 FOUND WINDOW FRAME HORIZONTAL CRACK 2.25'''' AT UPPER R/H CORNER PERFORMED STEP A WINDOW FRAME SEPARATION (1) AND (2) OF AVO9081. RIICW ON AVO 9081 STEP A 1&A2, OK TO CONTINUE. ACCOMPLISHED STEP B 1A PER AVO9081. RII CW PER AVO 9081 STEP 1A, OK TO CONTINUE. COMPLETED STEP C-1 OF AVO9081 REINSTALLED FASTENERS REMOVED IN STEPA1 AVO9081. COMPLETED STEPS 1 THROUGH 17 OF FIGURE 24 PAGES 22 AND 23 OF COMPLETED STEP C-2 OF AVO9081 DID NOT FIT WINDOW IN STEP C-2 OF AVO9081 RII CW IAW AVO 9081 REV B PER FIG 24, STEPS 1-17. VERIFIED REINSTALL OF FASTNERS IAW STEP C 1. WINDOW NEEDS TO BE FITTED IAW STEP C2. OK TO CONTINUE INSTALLED REPAIR WASHERS PER AVO9081 FIG 24 STEP 21. RII CW IAW AVO 9081, FIG 24.1, SREP 21. CW WASHERS INSTALLED NEED OK TO INSTALL FILLER AND FASTENER AS PER FIG 19.3 STEPS 1 AND 2. FILLER AND FASTNER. RII CW IAW AVO 9081, FIG 19-3, STEP 1 AND 2. OK TO INSTALL 2. INSTALLED FILLER AND FASTENSER PER AVO9081, FIG 19-3, STEP 1 AND RII CW IAW AVO 9081. FASTNER AND FILLER INSTALLED IAW 24.1 PREV COMP 21, CW STEPS 18-20 FIG 24-01, ALSO CW STEPS 22 THRU 23. THRU DBLR AND TRPLR WHEN EYEBROW PLUGS INSTALLED. REF LP 6750684 PER AVO 9081, FIG 24-2, FOUR EACH FASTNERS NEED TO BE INSTALLED SEE ATTACHED PICTURE CW WITH AVO9081 STEP D 1. INSTALLATION OF REPAIR DOUBLER AND TRIPLER ON LEFT SIDE NUMBER 1 WINDOW FRAME. RII CW IAW AVO 9081 REV B STEP D1. ACCOMPLISHED STEP D2 AND D3 PER AVO 9081. VERIFIED STEPS D 2 AND 3 COMPLETED. P
EMERGENCY PATH LIGHTING AT SEAT ROWS 14ABC AND 33ABC MISSING WHITE LENS. SEAT ROW IS 32ABC NOT 33ABC. REMOVED AND REPLACED LIGHT ASSEMBLIES AT ROWS 32ABC AND 14ABC REF MM 33-51-11. OPS CK OK. CORRECT COLOR INSTALLED REF CONFIG DRAWING 3350DD14743. VERIFIED IDT REQUIREMENTS
EMERGENCY PATH LIGHTING AT SEAT ROWS 14ABC AND 33ABC MISSING WHITE LENS. SEAT ROW IS 32ABC NOT 33ABC. REMOVED AND REPLACED LIGHT ASSEMBLIES AT ROWS 32ABC AND 14ABC REF MM 33-51-11. OPS CK OK. CORRECT COLOR INSTALLED REF CONFIG DRAWING 3350DD14743. VERIFIED IDT REQUIREMENTS
RIGHT WING OUTBOARD LEADING EDGE LOWER PANEL STICKING OUT. PANEL NR 621HB OF SS 411 REF N/R:99871188. RECEIVED AND ACCOMPLISHED A PERMANENT REPAIR PER PART 3 OF THE LATEST REVISION OF ECRA 5722-01088 ON RT WING LE LOWER SURFACE OF ATTACH STRAP PN 112A4402-4 AT OSS 179. PLANNING TO CONTACT ENGINEERING AFTER SEPTEMBER ADD EAAR N/R:99871188 INSTRUCTIONS 21, 2021 BUT BEFORE OCTOBER 21, 2021 FOR THE PERMANENT REPAIR RII IS COMPLIED WITH.
RIGHT HORIZONTAL STABILIZER REAR SPAR SURFACE FROM SS 221.50 TO SS 203.10 CORROSION NOTED, REF AAR N/R 99871023 RECEIVED AND ACCOMPLISHED INTERIM REPAIR AT RT HORIZ. STAB REAR SPAR UPPER "T" CHORD PER EC/RA 5510-02967 - ON OR BEFORE THE A/C REACHES 56000 TOTAL AIRCRAFT FLIGHT CYCLES, PERFORM AN INSPECTION PER PART 2 OF ECRA 5510-02967. PLANNING ALSO EC/RA 5510-02966 PROVIDES A CATEGORY A REPAIR INSPAR IB AT SSTA 221.50 PER EC/RA 5510-02968 AND INSTALLATION OF THIS REPAIR REQUIRES REWORK TO TE 54000 CYLES FOR THE INSPECTION REQUIREMENTS; TO CONTACT ENG AFTER 53000 CYCLES BUT BEFORE FOR THE CORROSION CLEANED ON THE RIGHT HORIZONTAL STABILIZER REAR SPAR UPPER "T" CHORD FROM SSTA 193.9 TO SSTA 212.30 CORROSION REMOVAL AND REPAIR ACCOMPLISHED. SEE FORMS 44-0008
R1 DOOR INNER SKIN CRACKED (REF AAR NR 99871080) REPAIRED R1 DOOR INNER SKIN CRACK AS PER B737-800 RES# 2015594-25 AND EC/RA# 5211-01658. INSP C/W
FWD CARGO DOOR HAS REPAIR AT EXTERIOR SKIN AFT LOWER CORNER SIZE 7"X6" INC.EVALUATE REPAIR CONFIRM PER THE SRM.AS PER EA5100-0234 5 REV E AND GENERATED FOR AA NR 99870952 RECEIVED AND ACCOMPLISHED A CATEGORY A REPAIR AT FWD CARGO DOOR AFT LOWER CORNER IRW UNITED EC/RA NO. 5231-01132. REF ELB LP 475 3945, PERFORMED CATEGORY A REPAIR.
DURING CIC OF HORIZONTAL STAB BOX FOUND CORROSION AT STA 1104 STR 5R REF AAR N/R 99871082 FOUND WITH CORROSION EXFOLIATION SHEAR TIE CLIP STR 5 STA 1104 REMOVED AND REPLACED SHEAR TIE AS PER REF B737 SRM 51-40-02 AND DWG 148A1225
LT WING FRUNT SPAR NO.3 SLAT O/B AUXILIARYTRACK LOAD RETAINING BRACKET ATTACH TO SPAR FLANGE HAS SPOT OF SURFACE CORROSION REF AAR N/R 99870512 REMOVED AND RPELACED NO.3 SLAT O/B AUX TRACK LOAD RETAINING BRACKET AT LT WING L/E REF B737 SRM 51-40-02 AND 51-40-05
B737-52-3-0683 FWD CGO DOOR SKIN FROM L/E 26.5 INCH. TOP EDGE 19 INCH AREA FOUND DENT MARK FWD CGO DR EXT SKIN AT26.5"FROM FWD EDGE&19"FROM TOP EDGE.DENT AREA MEASURED D0.028"W1.5"&L5"RATIO W/Y=53WITHIN SRM52-30-01 AL LOWABLE DMG1FIG103DETAILF LIMITS HFEC INSP CARRIED OUT AS ER B 737NTM PT6PROC23 NIL CRACK FOUND.DENT DOT INSTALLED AS PER UAL GMM 06-35-05 LOG PAGE WAS CONVERTED TO ELB FORMAT ON DEC 08, 2016 AT 18481667 REINSPECTED DENT PER SRM 52-30-01 FIG 103 DET F. NO FURTHER PROGESSION NOTED. FOUND OUT OF LIMITS AREA DAMAGED PER B-737-800 SRM 52-30-01, FABRICATED DOUBLER REPAIR 3 PER B-737-800 SRM 52-00-01- PAGE 204, FIG 201, TREATED AREA AND DOUBLER REPAIR PER B737-800 SOPM 20-41-02 INSTALLED DOUBLER REPAIR PER B737-800 SRM INSPECTED WORK ACCOMPLISHED REF. AAR N/R:99871062 51-40-02. INSP C/W
AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER SURFACE CORRORED AT STA 986 LBL 45. (REF NR 99870584) REMOVED AND REPLACED THE UPPER CHORD ALONG THE FULL LENGTH OF THE FLOOR BEAM AS PER REF B737-800 SRM 53-70-51 ADD EMP:V891105
AFT FLOOR STRUCTURE WET AREA L2 DOOR LEFT SIDE WEB BETWEEN STA 986.5 TO STA 1016 (WEB CRACKED) (REF NR 99871032) REMOVED AND REPLACED LT WEB AT AFT WET-FLOOR STRUCTURE AREA BETWEEN STA 986 AND STA 1086 LBL40, WL 208.10 IRW B737-800 SRM 51-40-02 AND DWG 147A5700
AFT STRUCTURE WET AREA L2 DOOR MAIN SILL UPPER WED 3EA ELONGATED HOLES NOTED (REF AAR NR 99871045) REMOVED AND REPLACED WEB PLATE AT L2 DOOR MAIN SILL BETWEEN STA 951 TO STA 952 RBL 60 WL 208.10 AS PER B737-800 SRM 51-40-02 AND DRWG NO.147A8501. ADD EMP:V898225
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 450 AND RBL 41. (REF AAR NR 99870741) REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 RBL 41 PER B737-800 SRM 51-40-02 AND DRWG 111A2000. ADD EMP:V891530
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACK AT STA 540 AND RBL 7 REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 RBL 7 PER B737-800 SRM 51-40-02 AND DRWG 111A2000 ADD EMP:V891530
AFT FLOOR STRUCTURE WET AREA L2 DOOR MAIN SILL INNER CHORD ANGLE HAS EVIDENCE OF SURFACE CORROSION BETWEEN BS 951 AND BS 990 APPROX LBL-60 (REF AAR NR 99870632) REMOVED AND REPLACED AFT FLOOR STRUCTURE WET AREA L2 DOOR MAIN SILL INNER CHORD AS PER REF B737-800 SRM 51-40-02 AND DWG 147A8501. ADD EMP:V891105
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND LBL 7. (REF AAR NR 99870736). REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 LBL 7" PER B737-800 SRM 51-40-02 AND EC/RA 5714-01084.
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND RBL 31.5 (REF AAR NR 99870738) REMOVED AND REPLACED SUPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 RBL 31.5" PER B737-800 SRM 51-40-02 AND EC/RA 5714-01087.
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACK AT STA 540 LBL 15 (REF AAR N/R 99871044) REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 LBL 15 PER B737-800 SRM 51-40-02 AND DRWG 111A2000
FWD CABIN WET AREA FLOOR SUPPORT SURFACE CORROSION AT STA 328 RBL 10. (REF AAR NR 99870570) INSTALLED CATEGORY A REPAIR AT FLOOR BEAM STA 328 FROM RBL 1 TO RBL 60 IRW B737-800 SRM 53-10-51 REPAIR 7 FIG 204. ADD EMP:V891530
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND LBL41 (REF AAR NR 99870737) REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 LBL 41" PER B737-800 SRM 51-40-02 AND EC/RA 5714-01085. ADD EMP:V891530
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND RBL 53.5 (REF AAR NR 99870742) REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 RBL 53.5" PER B737-800 SRM 51-40-02 AND EC/RA 5714-01088. ADD EMP:V891530
AFT CABIN FLOOR SUPPORT ANGLE CORR. BETWEEN STA 967 & 986 I/B OF R-2 DOOR SILL MKD DOT 60-024 REF. AAR N/R 99870583 REMOVED AND INSTALLED NEW R-2 DOOR SILL FROM STA 887 TO STA 1006 RBL 60 REF B737-8 SRM 51-40-02 AND DWG # 147A8501 3D ADD EMP:V916938 RII INSPECTION IS ACCOMPLISHED BY AAR INSP. 23
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND LBL 53.5 (REF AAR NR 99870743) REMOVED AND REPLACED SUPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 LBL 53.5 PER B737-800 SRM 51-40-02 AND DRWG NO. 111A2000. ADD EMP:V891530
MAIN CABIN CENTER WING TANK SUPPORT FITTING CRACKS AT STA 540 AND RBL 15 (REF AAR NR 99870733). REMOVED AND REPLACED SUPPORT FITTING AT MAIN CABIN CENTER WING TANK STA 540 RBL 15" PER B737-800 SRM 51-40-02 AND EC/RA 5714-01086. ADD EMP:V891530
REF TO EA 5510-01843 REV H 0P 002 R/H HORIZONTAL STABILIZER IN-SPAR RIB, STAB STA 92.70 CRACK LOCATED IN LOWER TRANSITION RADIUS OF THE VERTICAL STIFFNER #4 AFT. MKD 126-45. REF AAR N/R 99870729 AT RH HORIZONTAL STAB. STA 92.70 RIB #, REMOVED RIB PER REFERENCE B737-800 SRM 51-40-02, REPAIR #4 STIFFENER PER REFERENCE B737-800 SRM 55-10-09, REINSTALLED RIB #1 AT RH HORIZONTAL STAB AFTER REPAIR PER DWG # 182A3001, DWG # 182A4001-1 AND DWG 182A1500 ADD EMP:V894498 RII INSPECTION IS ACCOMPLISHED BY AAR INSP. 23
B737-06-3-0288 FWD FLOOR STRUCTURE WET AREA FLOOR BEAM UPPER CHORD HAS EVIDENCE OF LIGHT SURFACE CORROSION BS 344 BETWEEN LBL 17 AND 17 APROX MKD 126-35 AS PER T/C 58-53-00-1-2700 REF AAR N/R 99870636 REMOVED AND REPLACED EXISTING TRAPED FILLERS AND STRAP REPAIR AT MAIN CABIN STA 344 UPPER CHORD FROM LBL 17 AND RBL 17 REF. B737-800 SRM 53-10-51 FIG 205 REPAIR 8 ADD EMP:V898225 RII INSPECTION ACCOMPLISHED BY AAR INSP 20
AS PER T/C 29-5300-1-2503, FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKS BETWEEN STA 344 AND 360 AND LBL11 MKD DOT60-020 REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 344 & STA 360 LBL 11 REF. B737-800 SRM 51-40-02 / DRWG 141A5410 / DRWG 141A5230 ADD EMP:V898225 RII INSP BY AAR INSP 20
AS PER T/C 58-5320-1-2500, FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKS AT FASTENER HOLE FWD OF STA 294 BL-0 MKD DOT 60-023 REF AAR N/R 99870582 REMOVED AND REPLACED AT FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL, STA 294, BL-0 PER REF. B737-800 SRM 51-40-02 / DRWG 141A5400 / DRWG 141A5410 ADD EMP:V898268 RII INSPECTION ACCOMPLISHED BY AAR INS 1569
AS PER T/C 29-5300-1-2503, FWD CABIN WET ARE FLOOR SUPPORT INTERCOSTAL CRACKS BETWEEN STA 344 AND 360 BL-0 MKD DOT60-019 REF AAR N/R 99870577 REMOVED AND REPLACED INTERCOSTAL P # 29-5310-3-0074 AT FWD AREA BETWEEN STA 344 & STA 36 BL 0 IRW B737 SRM 51-40-02 & DWG # 141A5410 / DRWG 141A5400
FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKS AT FASTERNER HOLE BETWEEN STA 380 AND 400 ,BL-0 MKD DOT AS PER T/C 58-5300-1-2710 REF AAR N/R 99870731 REMOVED AND REPLACED INTERCOSTAL AT MAIN CABIN BETWEEN STA 380 & STA 400 BL-0 REF. B737-800 SRM 51-40-02 AND DWG 143A5400 ADD EMP:V898225 RII INSPECTION ACOMPLISHED BY AAR INSP 20
LEADING EDGE SLATS TRANSIT LIGHT STAYS ON 4 FSCU BITE SHOWS MSG 27-81206, #4 O/B SLAT PROX SNR. FSEU BITE TEST FAULTS SLAT 4 PROX. OUTBOARD. MAINT. MESSAGE 27-81206. ACCOMPLISHED FIM TASK 27-88-00-810-803. FOUND #4 LEADING EDGE SLAT SENSOR S1000 OUT OF TOLERANCE. REMOVED AND REPLACED AND OPS CHECKED GOOD. ADD EMP:U103124
EMERGENCY LIGHTS OUT AT RT AFT OVERWING EXIT, RT FWD EMERGENCY EXIT DOOR, AND LT AFT EMERGENCY EXIT DOOR. RELAMPED RT FWD EMERGENCY EXIT DOOR LIGHT. RELAMPED LT AFT EMERGENCY EXIT DOOR LIGHT. BOTH OPS CHECKED NORMAL. REPLACED M1671 FUSE AND M1676 BATTERY PACK. OPS CHECKED GOOD.
EMERGENCY LIGHT INOP AT AFT RT OVERWING EXIT. RELAMPED RT AFT OVERWING EXIT LIGHT OPS CHECKS GOOD.
AFT DOOR EMERGENCY LIGHTS AND VARIOUS EMER LIGHTS ON LEFT OF AIRCRAFT ARE INOP. REMOVED AND REPLACED AFT EMERGENCY BATTERY PACK PER AMM 33-51-06. OPS CHECK GOOD.
R/W BAY 621KB 1 MAJOR SPOT OF CORROSION ON LOWER SPAR. PERFORMED INTERIM REPAIR PER ECRA 5724-01016 PART 1. PERFORM PERMANENT REPAIR PER PART 3 OF ECRA 5724-01016 WITHIN 24 MONTHS. PLANNING TO CONTACT ENGINEERING AFTER 22 MONTHS AND BEFORE 23 MONTHS FOR PERMANENT REPAIR. INIT: W/I 695 DAYS T/A: W/I 730 DAYS. OP/N084263 PLANNING HAS CONTACTED ENGINEERING FOR PERMANENT REPAIR PLEASE REMOVE INITIAL LIMIT.
FORWARD CARGO BAY 10, STRINGER 28L HAS 1 SPOT OF CORROSION. REMOVED CORROSION, BLEND OUT WAS OUT OF LIMITS. PERFORMED INTERIM REPAIR ON STRINGER 28L FROM STATION 500C TO 500G IAW ECRA 5331-02040.
FORWARD CARGO BAY STRINGER 28R HAS 3 SPOTS OF CORROSION. REMOVED CORROSION & BLEND OUT WAS OUT OF LIMITS. PERFORMED STRINGER REPAIR FOR STRINGER 28R FROM STATION 500F TO 500D IAW SRM 53-00-03 REPAIR 1. REVIEW ATTACHED FORM 44.0008 FOR DETAILS.
FORWARD CARGO BAY 9 STRINGER 28L HAS 2 SPOTS OF CORROSION. REMOVED CORROSION, OUT OF LIMITS. PERFORMED INTERIM REPAIR ON STRINGER 28L FROM STATION 500C TO 500G IAW ECRA 5331-02040 PART 1.
RIGHT MLG WW CTR WING REAR SPAR VERTICAL PRESS WEB WL 198 RBL 30.0 FOUND CRACK AS MARKED. RT MLG WW WL 198 RBL 30 CTR WING REAR SPAR VERTICAL PRESS WEB REPAIRED IAW ECRA 5710-02395 REV FORM 44.0008 ITEM 1 TO ITEM 21. ACCOMPLISHED CREATE A DIP IAW FORM 44.0008 ITEM 22 REF LP 6930321 FOR DIP.
LEFT MLG WW CTR WING REAR SPAR VERTICAL PRESS WEB WL 198 LBL 30.0 FOUND CRACK AS MARKED. REPAIRED IAW ECRA 5710-02397 REV FORM 44.0008 ITEM 1 TO ITEM 30 ACCOMPLISHED CREATE A DIP IAW FORM 44.0008 ITEM 31 IAW LP 6930322 FOR DIP.
FWD CARGO COMPARTMENT STATION 500D - 500E STRINGER 26R FOUND CORROSION AS MARKED. REPAIRED IAW SRM 53-00-03 REPAIR 1 FIG 204 & FORM 44.0008 ITEM 1-15 ACCOMPLISHED.
SUPPORT TASK CABIN LT STATION 440 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND TWO EACH CRACKS APPROX 3/16 INCH & 1/8 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 002 FIG 3 FORM 44.0008 ITEM 1 TO 20 ACCOMPLISHED.
SUPPORT TASK CABIN LT STATION 500C BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND ONE EACH CRACK APPROX 1/8 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 02 FIG 3 FORM 44.0008 ITEM 1 TO 20 ACCOMPLISHED.
SUPPORT TASK CABIN LT STATION 480 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND TWO EACH CRACKS APPROX 3/16 INCH & 1/8 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 02 FIG 3 FORM 44.0008 ITEM 1 TO 20 ACCOMPLISHED.
SUPPORT TASK CABIN RT STATION 400 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND THREE EACH CRACKS APPROX 1/16 INCH, 5/16 INCH & 3/16 INCHES IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 02 FIG 3 FORM 44.0008 ITEM 1 TO 20 ACCOMPLISHED.
SUPPORT TASK CABIN RT STATION 480 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND FOUR EACH CRACKS APPROX 3/8 INCH, 3/16 INCH, 1/4 INCH & 3/16 INCHES IN LENGTH & THE INSIDE RADIUS OF FRAME FOUND CRACK APPROX 3/8 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 02 FIG 3 FORM 44.0008 ITEM 1 TO 20 ACCOMPLISHED.
SUPPORT TASK PAX CABIN FLOOR AT STATION RBL 45.50 FLOORBEAM AREA FOUND 2 EACH FASTENER HOLES CRACKED IN FLOORBEAM LAYER CABIN FLOOR. REPAIRED IAW UAL ECRA 5320-02276 REV FORM 44.0008 ITEM 1 TO 19 ACCOMPLISHED.
SUPPORT TASK PAX CABIN FLOOR AT STATION RBL 24.75 FLOORBEAM AREA FOUND 4 EACH FASTENER HOLES CRACKED IN FLOORBEAM LAYER CABIN FLOOR AT STATION 727B RBL 24.75. FLOORBEAM REPAIRED IAW UAL ECRA 5320-02276 REV FORM 44-0008 ITEM 1 TO ITEM 19 ACCOMPLISH ED.
SUPPORT TASK CABIN LT STATION 87 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND ONE EACH CRACK APPROX 1/8 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 02 FIG 3 FORM 44.0008 ITEM 1 - 20 ACCOMPLISHED.
SUPPORT TASK PAX CABIN FLOOR AT STATION 727B LBL 24.75 FLOORBEAM AREA WAS FOUND ONE EACH FASTENER HOLE CRACKED IN FLOORBEAM LAYER. CABIN FLOOR AT STATION 727B LBL 24.75 FLOORBEAM REPAIRED IAW ECRA 5320-02276 REV FORM 44.0008 ITEM 1 TO 19 ACCOMPLISHED.
SUPPORT TASK CABIN LT STATION 400 BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND TWO EACH CRACKS APPROX 3/16 INCHES & 1/8 INCH IN LENGTH. CABIN LT STATION 400 BETWEEN STRINGER 8 & 9 FRAME REPAIRED IAW EA 5310-04716 REV G OP 2 FIG 3 FORM 44.0008 ITEM 1 - 20 ACCOMPLISHED.
SUPPORT TASK CABIN RT STATION 500F BETWEEN STRINGER 8 & 9 INBD HOLE OF SUPPORT BRACKET FOUND ONE EACH CRACK APPROX 1/16 INCH IN LENGTH. REPAIRED IAW EA 5310-04716 REV G OP 2 FIG 3 FORM 44.0008 ITEM 1 - 20 ACCOMPLISHED.
CABIN BS 500I - 520 FRAME STRINGER 15L CHAFING MARK. REPAIRED IAW SRM 53-00-03 REPAIR 1 FIG 201. ATTACH MX WORK SHEET FORM 44.0008 ITEM 1 TO 12 ACCOMPLISHED.
CABIN BS 500G - 500H FRAME STRINGER 15L SHAFTING MARK. REPAIRED IAW SRM53-00-03 REPAIR 1 FIG 201.
FLT CONTROL PRESS FEELS VERY STIFF DURING ROTATION & FLARE DURING LANDING. PERFORMED ELE FEEL COMPUTER LK CHECK IAW AMM 27-31-37-200-820. CONTROL COLUMN POWER FORCE TEST IAW AMM 27-31-00-700-809 & HIGH CONTROL COLUMN FORCE WITH HYD POWER ON IAW AMM 27-31-00-810-813. FOUND ELE INPUT TORQUE TUBE BEARING DRY, LUBED & NOW OPERATIONS CHECKED GOOD.
EXTERIOR EMERGENCY EXIT LIGHT AFT OF L1 DOOR IS INOPERATIVE. RELAMPED NO HELP. R & R BATTERY & CHARGER ON LOCATION M1675 & PERFORMED OPERATIONS CHECKED IAW AMM 33-51-00-710-801, OPERATIONS CHECKED GOOD.
EXTERIOR EMERGENCY EXIT LIGHTS AT LT OVERWING EXIT DOORS INOPERATIVE. R & R BATTERY PACK AT ROW 15ABC IAW AMM 33-51-06, OPERATIONS CHECKED GOOD.
DURING WALK AROUND, FOUND 2 EA GOUGES MEASURING 4"L X 1" WIDE, BETWEEN & AT STATION 807 TO STATION 827 & BETWEEN S24L & S25L. REMOVED DAMAGED AREA & REPAIRED IAW ECRA 5331-01787.
ON SHORT FINAL, RT MLG GREEN INDICATION ON CENTER PANEL NOT ILLUMINATED WITH GEAR HANDLE DOWN. OVERHEAD RT MAIN GEAR INDICATION WAS ILLUMINATED. PERFORMED PSEU BITE IAW FIM 32-09, TASK 801 "NO FAULTS NOTED" & AMP; RELAMPED FWD RT GEAR DOWN & AMP; LOCKED INDICATOR LIGHTS IAW AMM 33- 18-00-960-801. OPS CK GOOD. OK TO CONT.
WEATHER RADAR FAIL LIGHT ON AFTER TAKEOFF. AIR RETURN BACK. CHECKED ALL WIRINGS NO FINDINGS. REPLACED RELAY R745 AND R746. OPS CHECKED GOOD.
EMERGENCY LIGHT, R2 DOOR INOPERATIVE. R & R POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED GOOD.
FWD GALLEY LT SIDE EMERGENCY LIGHT INOPERATIVE. R & R M1675 POWER SUPPLY BATTERY PACK IAW AMM 31-51-06. OPS CK OK.
SKIN DAMAGED. REPAIRED IAW ECRA 5330-03676, PART 1.
OVERHEAD EMERGENCY LIGHTS ON SEAT ROW 30C AND 32C WILL NOT COME ON. R & R BATTERY PACK POWER SUPPLY IAW AMM 33-51-06 AND BATTERY EMERGENCY POWER CHARGER IAW AMM 33-51-06. OPS CHECKED GOOD.
CABIN G4B GALLEY AREA RT STA 987 FLOORBEAM O/B AREA UPPER SERVICE FOUND CORROSION STA 987 RBL 40-RBL 50 AREA. CABIN G4B GALLEY RT STA 987 FLOORBEAM O/B AREA UPPER SURFACE CORR REMOVED AT SRM 53-70-51 ALLOWABLE DAMAGE 1 FIG 103 LIMITS AND FLOORBEAM UPPER SURFACE CORRODED AREA REPAIRED AS PER SRM 53-70-51 REPAIR 4 FIG 204 AT STA LBL 7.93" TO RBL 53" AND FORM 44.0008 ATTACHED ITEM 1-55 ACCOMPLISHED.
MULT-33-3-0001 SEAT 26ABC TO SEAT 31ABC SEAT EMERGENCY LIGHT FOUND INOP. TROUBLESHOOTING FOUND EMERGENCY LIGHT POWER PACK FAULTY POWER PACK REPLACED AND TEST CARRIED OUT RESULT NORMAL AS PER AMM 33-51-06.
CABIN G4B GALLEY AREA LT STA 987 FLOORBEAM O/B AREA UPPER SURFACE FOUND CORRSION (STA 987 LBL 35" TO LBL 40"). CABIN G4B GALLEY AREA LT STA 987 FLOORBEAM O/B AREA UPPER SURFACE CORRSION REMOVED OUT OF SRM 53-70-51 ALLOWABLE DAMAGE 1 FIG 103 LIMITS AND FLOORBEAM UPPER SURFACE CORRODED AREA REPAIRED AS PER SRM53-70-51 REPAIR 4 FIG 204 AT STA 987 LBL 7.93" TO LBL 53" AND FORM 44.0008 1-53 ACCOMPLISHED.
CABIN LT STA 992 MOST O/B SHEAR UPPER SURFACE FOUND CORRSION AS MARKED LBL 40 AREA. CABIN LT STA 992 MOST O/B LBL 40 AREA SHEAR WEB UPPER SURFACE CORRSION REMOVED OUT OF SRM 53-70-51 ALLOWABLE DAMAGE FIG 103 LIMITS AND CORRSION SHEAR WEB REPLACED AS SRM 51-10-02. NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ITEM 1-7 ACCOMPLISHED.
CABIN RT STA 1010 RBL 32 SHEAR WEB FOUND CORRSION CRACKED. CABIN RT STA 1010 RBL 32 SHEARE WEB REPAIRED AS PER EC/RA 5320-02040 REV_- HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1-18 ACCOMPLISHED.
CABIN RT STA 993 G4B GALLEY RT FWD TIE DOWN AREA O/B SHEAR WEB UPPER SURFACE FOUND CORRSION (RBL 42). CABIN STA 933 RBL 42 O/B SHEAR WEB UPPER SURFACE CORRSION REMOVED OUT OF SRM 53-70-51 ALLOWABLE DAMAGE 1 FIG 103 LIMITS AND CORRSION SHEAR WEB REPLACED AS PER SRM 51-10-02. NEW SHEAR WEB INSTALLED AS PER SRM 51-40-02 AND FORM 44.0008 ITEM 1-6 ACCOMPLISHED.
FUSELAGE SKIN CORRODED AROUND DRAIN PLUG AREA STA 727J S26R TO S27R. FUSELAGE SKIN AT STA 727J S26R - S27R CORROSION REMOVED AS PER SRM 51-10-02 AND REPROTECTED AS PER SRM 51-20-01. HFEC NIL CRACK FOUND, AND REPAIRED AS PER ECRA 5330-04173 REV- ATTACH MAINT WORK SHEET FORM 44.0008 ITEM 1 TO ITEM 2 ACCOMPLISHED.
CABIN LT STA 1010 LBL 32 SHEAR WEB UPPER SURFACE FOUND CORRSION. CABIN LT STA 1010 LBL 32 SHEAR WEB REPAIRED AS PER EC/RA 5320- 02040 REV - HFEC NIL CRACK FOUND ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1- ITEM 20 ACCOMPLISHED.
CABIN - G4B GALLEY LT O/B FLOOR HAT SECTION FOUND CORROSION DURING FLOOR PANEL OPEN UP ( FLOOR PANEL OPEN-UP FOR FERRULE REPLACEMENT) AT STA 990 LBL 30 - LBL 40. CABIN - STA 990 LBL 30 - LBL 40 FLOOR HAT SECTION REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ATTACH MAINTENANCE WORKSHEET FORM 44.0008 ITEM 1 TO ITEM 5 ACCOMPLISHED.
CABIN G4B GALLEY RIGHT O/B FLOOR MAT SECTION FOUND CORROSION DURING FLOOR PANEL OPEN-UP (FLOOR PNL OPEN-UP FOR FERRULE REPLACEMENT AT STA 990 RBL 30 - RBL 40 CABIN STA 990 RBL 30-RBL 40 FLOOR HAT SECTION REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02.
CABIN STA 1016 LBL 32 TO RBL 32 HAT SECTION FOUND CORROSION CRACKED. CORROSION CRACKED HAT SECTION REPLACED AS PER SRM 51-10-02 AND NOW HAT SECTION INSTALLED AS PER SRM 51-40-02 AT CABIN STA 106 LBL 32 TO RBL 32.
CABIN STA 987-1017 LBL 32 HAT SECTION FOUND CORRSION. CABIN STA 987-1017 LBL 32 HAT SECTION REPLACED AS PER SRM 51-10-02 AND FASTENER AS PER SRM 51-40-02 ATTACH MAINTENANCE WORK SHEET FROM 44.0008 ITEM 1-4 ACCOMPLISHED.
CABIN STA 987-1017 RBL 32 HAT SECTION FOUND CORROSION. CABIN STA 987-1017 RBL 32 HAT SECTION REPLACED AS PER SRM 51-10-02 AND FASTENER INSTALLED AS PER SRM 51-40-02 ATTACH MAINTENANCE WORK SHEET FORM 44.0008 ITEM 1-3 ACCOMPLISHED.
NR 1 FUEL BYPASS LIGHT ILLUMINATED IN FLIGHT. CONSULTED MX CONTROL & QRH & RETURNED TO GUM. REMOVED, INSP'D & REPLACED FUEL FILTER PER AMM 73-11-02. NO OBSTRUCTIONS NOTED. REPLACED FUEL FILTER DIFF PRESS SWITCH PER AMM 73-34-01. OPS CHECK NORMAL. NO LEAKS NOTED. OK FOR SERVICE. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1447639 S/N OFF 04986 SWITCH, ENGINE OFF 29-7334-9-9001 4986, ON 29-7334-9-9001 8176.
EMERGENCY LIGHTS (EXIT) IN FIRST CLASS DO NOT ILLUMINATE. R & R POWER SUPPLY BATTERY PACK AT (M1674) RIGHT BATTERY CHARGER. OPS CHECK GOOD PER AMM 33-51-06-960-805.
FEEL DEFF PRESS LIGHT CAME ON AFTER TAKEOFF AND WENT OUT ON SHORT FINAL, IT CAME ON AND OFF AGAIN AFTER PARKING. REMOVE AND REPLACE BOTH ELEV PITOT PROBE PER AMM 27-31-94-000- 400-801. LEAK CHECKS, NO LEAKS.
AFTER TAKEOFF THE "FEEL DIFF PRESS" ILLUMINATED. NOTE: WHEN POWER WAS REDUCED TO RETURN TO THE AIRPORT THE LIGHT WENT OUT. PERFORMED FIM TASK 27-31-00-810-803 INITIAL EVALUATION, CONFIRMED INTERMITTENT FAULT. PERFORMED FAULT ISOLATION PROCEDURE III PER FIM 27-31 TASK 803, FOUND BOTH VISCO JET DRAINS CONTAMINATED. REMOVED AND REPLACED 2EA JET DRAINS PER SAME. PERFORMED ELEVATOR PITOT PROBE HEAT TEST IAW 30-31-00, NO DISCREPANCY FOUND. PERFORMED REPAIR CONFIRMATION IAW FIM 27-31 TASK 803, OPS & LEAK CHECK NORMAL. REF ATTACHED FORM 44.0008CM FOR FULL WORK DETAILS, OK TO CONTINUE.
FWD BIN BAY 5 AFT END ABOVE BELLFRAME CARGO TIE DOWN TRACK CRACK. PERFORM REPAIR 3 OF SRM 53-00-53 RT TIE DOWN ASSY FROM BAY 1-7 P/N BAC1520-1397.
FWD BIN BAY 11 STR 26(R) 9 EA FASTENERS WITH CORROSION. CORROSION REMOVED OUT OF ALLOWABLE LIMITS AS PER SRM 53-00-03. FABRICATED REPAIR PARTS AS PER SRM 53-00-03, INSTALLED SPLICE REPAIR AS PER SRM 53-00-03 REPAIR 1 FIG 202 (S 26R AT BAY 11).
FWD BIN BAY 13 STR 26(R) 21 EA FASTENERS WITH CORROSION. FOUND CORROSION OUT OF LIMITS SRM 53-00-0, ALLOWABLE DAMAGES REPAIR STR 26R BAY 13 SRM 53-00-03 SRM 51-04-02 SEE 44.0008 CM FOR WORK PERFORMED.
AFT BIN BAY 5 AFT END RT CARGO TIE DOWN TRACK CRACK ABOVE BELLFRAME. REMOVED DAMAGED SECTION OF TIE DOWN RAIL. INSTALLED SPLICED REPAIR AS PER SRM 53-00-53 QC-0A359.
CORROSION FOUND ON BS 1088 BULKHEAD LT CHORD. REPAIR CARRIED OUT IAW EC/RA NR 5310-04969.
FOUND CORROSION ON RT WING LEADING EDGE LOWER STRAP AT SS 339. REPAIR CARRIED OUT IAW EC/RA NR 5730-02566.
FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA FLOORBEAM AT BS 328 WITH CORROSION AT RBL35.6. REPAIR CARRIED OUT IAW EC/RA 5321-01650 REV B.
PASSENGER CABIN COMPARTMENT FLOOR SUPPORT STRUCTURE BRACKET FOUND CRACKED AT BS 536.5, LBL 5.5. PART REPLACED IAW EC/RA 5321-01653.
AFT PASSENGER WET AREA FLOORBEAM AT BS 967 FOUND WITH CORROSION AT SCREW HOLES AT LBL 47.5 BS 967. FLOORBEAM UPPER CAP REPAIR WAS CARRIED OUT IAW EC/RA NR 53 21-01657 REV B.
CORROSION FOUND AT FWD WET AREA ON CHANNEL ASSY AT BS 344, RBL 1 AROUND SCREW HOLE AREA. REPAIR CARRIED OUT PER EC/RA NR 5321-01648 REV A.
FWD PASSENGER COMPARTMENT FLOOR STRUCTURE WET AREA FLOORBEAM FOUND CORROSION AT BS 328, RBL11. REPAIR CARRIED OUT IAW EC/RA NR 5321-01649 REV A.
AFT PASSENGER COMPARTMENT FLOOR WET AREA INTERCOSTAL FRAME FOUND WITH CORROSION AT BS 958, RBL 47 INTERCOSTAL. REMOVED AND REPLACED IAW B737-800 SRM 51-10-02 HOLES PICKED-UP PER SRM 51-40-05 AND FASTENERS INSTALLED PER SRM 51-40-02 REV.35.
AFT PASSENGER COMPARTMENT FLOOR WET AREA INTERCOSTAL FRAME FOUND WITH CORROSION AT LBL 47, BS 958 INTERCOSTAL. REMOVED AND REPLACED IAW SRM 51-10-02 HOLES PICKED-UP PER SRM 51-40-05 AND FASTENERS INSTALLED PER SRM 51-40-02 REV.35.
AFT PASSENGER COMPARTMENT WET AREA FLOORBEAM BS 986.5 FOUND WITH CORROSION AT RBL 28 SECTION 47. REPAIR CARRIED OUT PER B737-800 SRM 53-70-51 REPAIR 4 FIG 205 REV 35.
FOR SFR REPORTING PURPOSE- REF, TO HANGAR NRC L/P NR 0978300 CORROSION FOUND AT FLIGHT COMPARTMENT FLOOR STRUCTURE CHANNEL IN BETWEEN BS 270 AND BS 277, BL0 CHANNEL. REMOVED AND REPLACED IAW B737-800 SRM 51-10-02, HOLES PICKED-UP AS PER SRM 51-40-03, FASTENERS INSTALLED AS PER SRM 51-4 0-02 REV 35.
FOR REPORTING PURPOSE- REF TO HANGAR NRC L/P NR 0978226 FWD CABIN WET AREA SEAT TRACK FOUND CORROSION AT BS 380, LBL 45.50 SEAT TRACK REMOVED AND REPLACED IAW SRM 51-10-02, HOLES PICKED-UP AS PER SRM 51-40-05, FASTENER INSTALLED AS PER SRM 51-40-02 R EV.35- SEAT TRACK SUBSTITUTION AS PER EC/RA NR 5321-01379.
FOR SFR REPORTING PURPOSE-REF. TO HANGAR NRC L/P NR 0969988 FWD CABIN WET AREA SEAT TRACK FOUND AT BS 380 LBL 24.75 CORRODED SEAT TRACK REMOVED AND REPLACED IAW SRM 51-10-02, HOLES PICKED-UP AS PER SRM 51-40-05, FASTENER INSTALLED AS PER SRM 51 -40-02 REV 35-SEAT TRACK SUBSTITUTED AS PER EC/RA NR 5321-01379.
THE RT AFT OVERWING DOOR AND LOWER EMERGENCY LIGHT AFT OF RIGHT I/B FLAP ON FUSELAGE WAS FOUND INOPERATIVE. THE M1676 AND M1671 BATTERY PACK ASSEMBLIES WERE REPLACED IAW MM 33-51-05-960-805.
AN ELECTRICAL ODOR CAME FROM THE AFT GALLEY NR 1 OVEN AND THE CIRCUIT BREAKER POPPED WHILE AT CRUISE PORTION OF FLIGHT. THE FLIGHT WAS RETURNED TO GUM WHERE IT LANDED WITHOUT INCIDENT. THE AFT GALLEY NR 1 OVEN AND CONTROLLER WAS REPLACED. A FUNCTIONAL CHECK WAS GOOD IAW MM 25-36-33.
INSPECTION FOUND A .5 INCH CRACK IN AFT CARGO FLOOR PANEL SUPPORT AT STA 727G, RBL 13.84. AN INTERIM REPAIR WAS ACCOMPLISHED IAW ECRA 5320-01816. A DIP WAS ISSUED TO REINSPECT THE REPAIR EVERY 6 MONTHS AND TO PERFORM A PERMANENT REPAIR WITHIN 2 YEARS.
THE EMERGENCY EXIT LIGHTS AT FRONT ENTRY DOOR (L-1) FORWARD EXTERIOR AND OVERHEAD BIN FORWARD OF ROW 2B WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06.
THE EMERGENCY EXIT LIGHTS ON OVERHEAD BIN AT ROWS 14, 16, 19, 21, AND 26 DEF WERE FOUND INOPERATIVE. THE BATTERY CHARGER WAS REMOVED AND REPLACED IAW MM 33-51-06.
INSPECTION FOUND L-1 ENTRY DOOR REPAIR AT UPPER AFT CORNER BENT ON AFT EDGE. REMOVED EXISTING REPAIR AND REINSTALLED EXTERNAL DOUBLER IAW ECRA. (K)
INSPECTION FOUND A DENT IN FUSELAGE SKIN NEAR L-1 DOOR, BELOW EMERGENCY LIGHT AT STA 380, S17L. THE SKIN WAS REPAIRED IAW SRM. (K)