N25705
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
Maintenance disclosures
RIGHT WING AT RIB 27. THE LOWER FWD TENSION FITTING AT THE AFT ATTACH HOLE HAS PITTING CORROSION AT 11:00 O'CLOCK FACING INBD. REPAIRED R/W AT RIB 27 LOWER FWD TENSION FITTING AT AFT ATTACH HOLE IAW UAL AVO17710 REV ORIGINAL AND UAL ECRA 5720- 03661 REV ORIGINAL WITH NO DEVIATIONS.
CRACK FOUND AT RIGHT HORIZONTAL STAB LOWER SKIN AT HSS 129.50 , INBD ROW , 9" FROM FRONT SPAR. CRACK LENGTH 1". REPAIRED RT HORIZONTAL STAB LOWER SKIN AT APPROX STA 129.5 IAW SRM 55-10-01-2R-11. ESFR ENTRY REQUIRED, DIP ENTRY REQUIRED. CATEGORY B REPAIR INSPECTION REQUIREMENTS AS PER SRM 55-10-01-2R-11 PARAGRAPH 5. ACCOMPLISH A DETAIL VISUAL INSPECTION AND AN EXTERNAL LFEC INSPECTION EVERY 9000 FLIGHT CYCLES WITH AN INSPECTION THRESHOLD OF 56000 FLIGHT CYCLES.
FOUND CRACK ON RIGHT HORIZONTAL FRONT SPAR WEB AT APPROXIMATLY STA. 129.5 ON CIRCUMFERANCE OF LIGHTENING HOLE.REF BY AAR NR 100009960. REPAIRED RIGHT HORIZONTAL FRONT SPAR WEB AT APPROX STA 129.5 ON CIRCUMFERANCE OF LIGHTENING HOLE AS PER SRM 55-10-10-2R-1. WORK ACCOMPLISHED BY V929396. ESFR ENTERED. REPAIRED RIGHT HORIZONTAL FRONT SPAR WEB AT APPROX STA 129.5 ON CIRCUMFERANCE OF LIGHTENING HOLE AS PER SRM 55-10-10-2R-1.WORK ACCOMPLISHED BY V929396,INS-93. INSP C/W
LEFT WING FRONT SPAR BOOST PUMP SKIN CUTOUT UPPER SURFACE HAS CORRODED. REPAIRED LEFT WING FRONT SPAR WEB AT THE FUEL BOOST PUMP CUTOUT IAW ESR-WI 2024282-9-14664 WITH THE APROVAL OF EC/RA 5720-03617.
RIGHT NR 3 WINDOW FRAME FOUND CRACKED ON HOLES 3 & 4. PERFORMED REPAIR ON THE RT NR 3 WINDOW FRAME IAW EO 250450 REV. P1, P2, P3 AND IR, EA 5310-08195 REV. C, AND ECRA 5310-08750.
WATER EXTINGUISHER AT 1L USED AS A PRECAUTION AND IT DID NOT OPERATE NORMALLY. CREW USED H2O EXTINGUISHER PRECAUTIONARILY ON CIGARETTE IN FWD LAV, NO SMOKE, NO ODOR, REMOVED AND REPLACED H2O EXTINGUISHER REF AMM 26-26-02
AFT LEFT SECTION OF CABIN EMERGENCY LIGHT INOP. POWER SUPPLY BATTERY PACK REPLACED REF AMM 33-51-06-960-805, OPS CHECK GOOD.
2L DOOR - FA STATES CAN FIT HAND BETWEEN DOOR AND SLIDE COVER. CHECKED AND FOUND 2L DOOR SLIDE COVER INSTALLED PER AMM 25-66-01-400-803. NO DEFECTS NOTED. CHECKED AND FOUND 2L DOOR SLIDE COVER INSTALLED PER AMM 25-66-01-400-803. NO DEFECTS NOTED.
STABILIZER FAILS TO TRIM NOSE UP ASSOCIATED SPEED TRIM FAIL LIGHT ILLUNINATED PER CREW, BOTH CAPT AND F/O SWITCHES WOULD NOT TRIM NOSE UP BUT TRIMMING DOWN WAS OK. INITIAL EVAL CYCLED STAB TRIM BREAKERS AND GOT BOTH ELECTRIC STAB TRIM SWITCHES TO MOVE UP AND DOWN. DFCS BITE SHOWS TWO FAULTS ON LAST LEG, SAME FAULTS ON CHANNEL A & B. RESET BOTH FCCS AND PERFORMED SPEED/STAB TRIM SURFACE TEST REF FIM 22-11 TASK 849. TEST PASSED. STAB TRIM ABLE TO TRIM UP AND DOWN WITH NO DISCREPANCIES.
EMERGENCY FUEL SHUTOFF VALVE BATTERY NEEDS CHANGED DUE TO LIFE LIMIT REMOVED AND REPLACED EMERGENCY FUEL SHUT OFF VALVE BATTERY IAW AMM 28-22-14 OPS CHECK GOOD
FLAPS STUCK AT 25 SETTING. REPLACED LH FLAP POS TRANSMITTER IAW AMM TASK 27-58-01-000-801 AND AMM TASK 27-58-01-400-801. ALL REQUIRED OP CHECKS TESTED OK.
STRINGER 25L BETWEEN STA 827 & 847 IS CORRODED.CORROSION IS IN TWO EACH SPOTS. VERIFY REPLACEMENT STRINGER AS 146A3233-6, PO# 4429978. PER AVO 13590 REV B STEP 15. PERFORMED MATERIAL VERIFICATION, PO 4429978. TRIMMED OUT DAMAGED SECTION OF S-25L STRINGER FROM 8.0 INCH. FORWARD STA. 827 TO 1.5 INCH. FWD OF STA. 887 TOTAL TRIM OUT SECTION = 67.0 INCH. REMOVED PRODUCTION FASTENERS IN FUSELAGE SKIN AND AT PRODUCTION SPLICE COUPLER AT STA. 887 REF. AVO13590 REV.B, STEP: 14 & SRM 53-00-03-2R-1 PARG. 4.B. READY FOR HFEC INSPECTION. PER. AVO13590 REV.B, STEP 15, FABRICATED A REPLACEMENT STRINGER SECTION USING P/N 146A3233-6 AND FAB. FWD HAT SECTION SPLICE COUPLER FROM BAC1498-162 REF. SRM 53-00-03-2R-1 TABLE 203, 0.063 THICH. TYPE: I, STRINGER I.D. REQUEST OK TO INSTALL REPAIR PARTS. ACCOMPLISHED HFEC PART 6 51-00-00 PROCEDURE 16 ON 43 FASTENER LOCATIONS. PERFORMED HFEC PART 6 51-00-00 PROCEDURE 23 ON STRINGER CUT OUT SECTION. NO DEFECTS NOTED. REPLACEMENT STRINGER SECTION OK TO INSTALL. NOTE: AVO13590 REV.C, ISSUED CHANGING AND RENUMBERING STEPS: 10 THRU. 16, FOR S-25L STRINGER REPAIR INSTRUCTIONS IS NOW STEPS: 10 THRU 12. AND INCORPORATING DEVIATIONS TO STRINGER SPLICE LOCATIONS PER. STEP 10, AND APPROVAL TO USE THE NEXT HIGHER ASSY. STRINGER P/N: 146A3233-6 PER. STEP: 16,
FOUND CORROSION ON EXTERIOR SKIN AROUND LAV PAN OPENING AFTER OUTER LAV PAN REMOVAL.ADDED 3EA PICS. BLENDED OUT CORRODED LOWER SKIN REF SRM 51-10-02. THICKNESS OF SKIN REMOVED IS BEYOND ALLOWABLE LIMITS. ACCOMPLISHED STEPS 1. THROUGH 5. OF AVO 13590. REQUEST INSPECTION FOR HFEC ON BLENDED SKIN AREA. PER STEP 6. AND HOLE PROBE INSPECTION PER STEP 7 OF AVO. 13590. PREFORMED HFEC INSPECTION PER NDTM 51-00-00 PROCEDURE#23 OF BLENDED AREA WITH NO CARCK INDICATIONS AS DIRECTED IN AVO#13590, STEP #6 PREFORMED HFEC INSPECTION OF ALL OPEN HOLES PER NDTM 51-00-00 PROCEDURE #16 AS DIRECTED IN AVO #13590 STEP #7, NO CRACK INDICATIONS NOTED. LAID OUT 1/4 INCH GRID ON BLENDED AREA FOR INSPECTOR/ENGINEERING PER AVO13590. REMAINING THICKENESS CHECK IS REQUIRED. MEASURED REMAINING THICKNESS PER AVO13590 STEP 8, REF NDT MANUAL PART 4, 51-00-00 PROCEDURE 3. MEASURED ROW "A" UP TO AND INCLUDING ROW "AJ-20" REMAINDER OF. NDT THICKNESS OF MATERIAL MEASUREMENT AT LOWER AREA OF LAV PAN. CORROSION AFFECTED AREA. PERA AVO. 13590. STEP 8. , REF. NDT MANUAL. PART 4. 51-00-00. PROCEDURE 3. FROM. ROW AJ-20 TO ROW. . ACCOMPLISHED TRIM OUT OF DAMAGED SKIN PER AVO13590 REV.A STEP 9.A AND B. NEED TO ACCOMPLISH HFEC OF TRIMMED EDGE PER STEP 9.C. PREFORMED HFEC OF TRIMMED OUT EDGE SKIN PER NDTM PART 6, 51-00-VERIFIED COMPLETION OF AVO# 13590 STEPS 1-23. NOW AWAITING FINAL ECRA FOR REPAIR.
EMERGENCY LIGHT BATTERY PACK M1675 FAILED CAPACITY CHECK.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REPLACED BATTERY PACK AS PER MM 33-51-06, OPS CKS GOOD
STAB OUT OF TRIM LIGHT ILLUMINATED ON TAKEOFF AT ABOUT 60 KTS REPLACED STAB OUT OF TRIM LIGHT M&E 29-3311-3-0062 REF FIM 22-11-851 AND AMM 22-11-00-740-806 . ACCOMPLISHED DFCS AUTOTESTS PASSED.ACCOMPLISHED DFCS SPEED/STAB CHANNEL A & B TEST THAT ENGAGES AP A AND B TO RUN STAB. PASSED. STAB OUT OF TRIM LIGHT NEVER CAME ON DURING STAB MOVEMENT BY THE AP . SURFACE TEST PASSED 14.32 . AC IS FULL AUTOLAND STATUS.
R/H HORIZONTAL STAB FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE CRACKED (REF AAR N/R 975407) ACCOMPLISHED REPAIR AT R/H HS FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE AS PER ESR/RES WI 2020476-18-4125 AND ECRA 5510-03172. (WORK ACCOMPLISHED BY V930393)
R/H HORIZONTAL STAB FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE CRACKED (REF AAR N/R 975407) ACCOMPLISHED REPAIR AT R/H HS FRONT SPAR INTERNAL RIB NO2 FWD UPPER FLANGE AS PER ESR/RES WI 2020476-18-4125 AND ECRA 5510-03172. (WORK ACCOMPLISHED BY V930393)
EA5100-02345 REV E FOUND REINFORCINGT DOUBLER REPAIR ON AFT CARGO DOOR EXTERNAL SKIN AT 6OCLOCK FROM UPPER EDGE 13IN FROM AFT EDGE SIZE 13/12X9 REPAIR HAS A DEEP SCRATCH 3IN LONG REF AAR N/R 975221 REMOVED EXISTING DOUBLER AND REINSTALLED NEW DOUBLER ON AFT CARGO DOOR AS PER B737 SRM 52-00-01-2R-2 AND SRM 51-40-02-0G-0 MAT USED ID 2024-T3 0.080 CLAD NO EXTRA WEIGHT ADDED WORK ACCOMPLISHED BY V894534
DENT AT FLIGHT DECK FLOOR AT WEB STA 260LBL 14 REF AAR N/R 974862 CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,000TFC PLANNING TO CONTACT ENGINERING FOR INSP REQUIREMENT CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,000TFC PLANNING TO CONTACT ENGINERING FOR INSP REQUIREMENT PART 1.1 WITH AAR-MIA ESR-WI 2020476-6-4077 INCLUDED. INITIATE D S. PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQD. FOR SPECTION REQUIREMENTS OF THE LATEST REVISION FOR ECRA 5322-01118 IP LP ON OR BEFORE THE ACCUMULATION OF 48,000 TOTAL FLIGHT CYCLE THE FD FLOOR WEB REPAIR ON A/C N25705 IN ACCORD WITH PART 2 - IN PERFORMED INTERIM REPAIR OF FLIGHT DECK FLOOR WEB BETWEEN LBL 20 AND RBL 7.5 AND BETWEEN STA 250 AN STA 270 PER ECRA 5322-01118 ADD EMP:V894534 TOMC APPROVED DIP, ON OR BEFORE THE ACCUMULATION OF 48,000 TOTAL TOMC-APPROVAL FROM SC1ELBYC COMMENT AIRCRAFT FLIGHT CYCLES, PLANNING TO CONTACT / ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE FLIGHT DECK FLOOR WEB REPAIR BETWEEN LBL 20 AND RBL 10 AND BETWEEN STA 250 AND STA 270 ON AIRCRAFT N25705 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5322-01118. QC QC REVIEW T/A : PLN/ENG (48,000 TAFC).....AS/U393878 RECORDS UPDATE
DENT AT FLIGHT DECK FLOOR AT WEB STA 260LBL 14 REF AAR N/R 974862 CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,000TFC PLANNING TO CONTACT ENGINERING FOR INSP REQUIREMENT CUTOUT DAMAGED AREA AND INSTALLED REPAIR ON FLIGHT DECK FLOOR WEB BETWEEN STA 250 AND STA 270 AT LBL20 - RBL7.5 AS PER ECRA 5322-01118 THIS IS A CAT BREPAIR ON OR BEFORE THE ACCUMULATION OF 48,000TFC PLANNING TO CONTACT ENGINERING FOR INSP REQUIREMENT PART 1.1 WITH AAR-MIA ESR-WI 2020476-6-4077 INCLUDED. INITIATE D S. PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQD. FOR SPECTION REQUIREMENTS OF THE LATEST REVISION FOR ECRA 5322-01118 IP LP ON OR BEFORE THE ACCUMULATION OF 48,000 TOTAL FLIGHT CYCLE THE FD FLOOR WEB REPAIR ON A/C N25705 IN ACCORD WITH PART 2 - IN PERFORMED INTERIM REPAIR OF FLIGHT DECK FLOOR WEB BETWEEN LBL 20 AND RBL 7.5 AND BETWEEN STA 250 AN STA 270 PER ECRA 5322-01118 ADD EMP:V894534 TOMC APPROVED DIP, ON OR BEFORE THE ACCUMULATION OF 48,000 TOTAL TOMC-APPROVAL FROM SC1ELBYC COMMENT AIRCRAFT FLIGHT CYCLES, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS FOR THE FLIGHT DECK FLOOR WEB REPAIR BETWEEN LBL 20 AND RBL 10 AND BETWEEN STA 250 AND STA 270 ON AIRCRAFT N25705 IN ACCORDANCE WITH / PART 2 OF THE LATEST REVISION OF ECRA 5322-01118. QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS AUDIT & UPDATE.
AFT WET AREA WEB STA 986.5 - STA 1016 AND RBL 33 - RBL 45 FOUND CRACKED. (REF AAR NR 975230) REMOVED AND REPLACED AFT WET AREA WEB AT STA 986.5 TO STA 1016 AND RBL 33- RBL 45 AS PER SRM 51-40-02-0G-0 AND DRAWING # 147A5700. ACCOMPLISHED BY V928494.
FWD PASSENGER COMP WET AREA R/H CORROSION ON INNER CHORD STA 277+14 TO 328+4 REF AAR N/R 974893 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V894534
FWD PASSENGER COMP WET AREA R/H CORROSION ON INNER CHORD STA 277+14 TO 328+4 REF AAR N/R 974893 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V894534 REMVOED AND REPLACED THE INNER CHORD STA 251 TO STA 360 AT FWD PASSENGER CABIN COMP WET AREA R/H PER B737 SRM 51-40-02-0G-0 AND DWG 141A8310 WORK ACCOMPLISHED BY V894534
AFT WET AREA FLOOR BEAM STA 986,LBL 24 TO LBL 55 HAS SEVERAL SPOTS OF CORROSION.(REF AAR NR 975082) REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 53-70-51-2R-4. ALTERNATE 1 ESR 2020476-14-4110 0.150 IN MAT. REMAINING 0.085 IN MAT. LOSS 0.065 (WORK ACCOMPLISHED BY V931343) IN. FOUND OUT LIMITS AS PER SRM 53-70-51-1A-1. ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM 53-70-51-2R-4. ALTERNATE 1 ESR 2020476-14-4110 WORK ACCOMPLISHED BY V931343. REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 0.150 IN MAT. REMAINING 0.085 IN MAT. LOSS 0.065 IN. FOUND OUT LIMITS AS PER SRM 53-70-51-1A-1. ADD EMP:V931343
AFT WET AREA FLOOR BEAM STA 986,LBL 24 TO LBL 55 HAS SEVERAL SPOTS OF CORROSION.(REF AAR NR 975082) REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 53-70-51-2R-4. ALTERNATE 1 ESR 2020476-14-4110 0.150 IN MAT. REMAINING 0.085 IN MAT. LOSS 0.065 (WORK ACCOMPLISHED BY V931343) IN. FOUND OUT LIMITS AS PER SRM 53-70-51-1A-1. ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM 53-70-51-2R-4. ALTERNATE 1 ESR 2020476-14-4110 WORK ACCOMPLISHED BY V931343. REMOVED CORROSION ON FLOOR BEAM STA 986.5 LBL TO LBL 55 AS PER SRM 51-10-02-0G-0 ORIGINAL MAT. 0.150 IN MAT. REMAINING 0.085 IN MAT. LOSS 0.065 IN. FOUND OUT LIMITS AS PER SRM 53-70-51-1A-1. ADD EMP:V931343
AFT WET AREA WEB STA 986.5 - STA 1016 AND RBL 33 - RBL 45 FOUND CRACKED. (REF AAR NR 975230) REMOVED AND REPLACED AFT WET AREA WEB AT STA 986.5 TO STA 1016 AND RBL 33- RBL 45 AS PER SRM 51-40-02-0G-0 AND DRAWING # 147A5700. ACCOMPLISHED BY V928494.
RH LOWER INNER CHORD FROM STA937 TO STA 992.5 HAS SPOTS OF CORROSION. (REF AAR NR 975073) REMOVED AND REPLACED R2 DOOR INNER CHORD P/N: 147A8540U8 PO#2004755, M&E 58-5300-3-0028 AND DRAWING #147A8501. ACCOMPLISHED BY V894534.
AFT WET AREA FLOOR BEAM STA 986.5 ,RBL24 TO RBL50 HAS SPOTS OF CORROSION. (REF AAR NR 975077) REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 53-70-51-2R-4 ALTERNATE 1 0.150IN MAT REMAINING 0.089IN MAT LOSS 0.061IN (WORK ACCOMPLISHED BY V931343) FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1. ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM 53-70-51-2R-4 ALTERNATE 1 WORK ACCOMPLISHED BY V931343. REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 0.150IN MAT REMAINING 0.089IN MAT LOSS 0.061IN FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1. ADD EMP:V931343
AFT WET AREA FLOOR BEAM STA 986.5 ,RBL24 TO RBL50 HAS SPOTS OF CORROSION. (REF AAR NR 975077) REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 53-70-51-2R-4 ALTERNATE 1 0.150IN MAT REMAINING 0.089IN MAT LOSS 0.061IN (WORK ACCOMPLISHED BY V931343) FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1. ACCOMPLISHED FLOOR BEAM REPAIR AS PER SRM 53-70-51-2R-4 ALTERNATE 1 WORK ACCOMPLISHED BY V931343. REMOVED CORROSION ON FLOOR BEAM STA 986.5 RBL 24 TO RBL 50 AS PER SRM 51-10-02-0G-0. ORIGINAL MAT 0.150IN MAT REMAINING 0.089IN MAT LOSS 0.061IN FOUND OUT OF LIMITS AS PER SRM 53-70-51-1A-1. ADD EMP:V931343
R/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 REMOVED EXISTING REPAIR BETWEEN STAB STA 138.7 AND 147.9 COTOUT DAMAGED AREA STA 129.5 19IN FROM FRONT SPAR AND INSTALLED NEW DOUBLER SIZE 16X28 ACTUAL STAB STA 124 STA 152 REF B737 SRM 55-10-01-2R-11 REPAIR 11 THIS IS A CAT B REPAIR INSP THRESHOLD
AFT CARGO COMPARTMENT CORROSION @ WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND 867, BETWEEN S-25L AND S-26L. (REF AAR N/R 975224) AFT CARGO COMP WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND STA 867 FOUND OUT OF LIMITS AS PER SRM 51-10-02-0G-0. REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02-0G-0 (WORK ACCOMPLISHED BY V894534)
AFT CARGO COMPARTMENT CORROSION @ WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND 867, BETWEEN S-25L AND S-26L. (REF AAR N/R 975224) AFT CARGO COMP WASTE TANK DUMP CHUTE ENCLOSURE SUPPORT STRUCTURE BETWEEN STA 847 AND STA 867 FOUND OUT OF LIMITS AS PER SRM 51-10-02-0G-0. REMOVED AND REPLACED INTERCOSTAL AS PER SRM 51-40-02-0G-0 (WORK ACCOMPLISHED BY V894534)
RH LOWER INNER CHORD FROM STA937 TO STA 992.5 HAS SPOTS OF CORROSION. (REF AAR NR 975073) REMOVED AND REPLACED R2 DOOR INNER CHORD P/N: 147A8540U8 PO#2004755, M&E 58-5300-3-0028 AND DRAWING #147A8501. ACCOMPLISHED BY V894534.
R/H HORIZONTAL STAB LOWER SKIN HAS A 0.750 CRACK LOCAQTED AT ATAB STA 129.50 I/B RIVET ROW 19.00 FROM FRUNT SPAR REF NDTM UAL PART 6 SECTION 55-10-01 REF AAR N/R 974677 THRESHOLDS 56,000 TFC AND REPEAT INSP AT 9,000 F.C INTERVALS PER TABLE 204 WORK ACCOMPLISHED BY V894534 REMOVED EXISTING REPAIR BETWEEN STAB STA138.7 AND STA147.9 CUTOUT DAMAGED AREA STA 129.5 19IN FROM REAR SPAR AND INSTALLED NEW DOUBLER SIZE 16X28 ACTUAL STAB STA124 - STA152 REF B737 SRM 55-10-01-2R-11 REPAIR 11 THIS IS A CAT B REPAIR INSP THRESHOLDS
CABIN FLOOR STRUCTURE SHOWS EVIDENDE OF CORROSION AT L-2 DOOR INNER CHORD LOWER SURFACE AND AROUND ANCHOR NUTS STA 917 REF AAR N/R 975506 REMOVED AND REPLACED NEW CABIN FLOOR L-2 DOOR INNER CHORD FROM STA 897 TO STA 1016 LBL 60 PER REF B737 SRM 51-40-02-0G-0 AND DWG 147A8501 WORK ACCOMPLISHED BY V894534 INSP C/W
AFT WET AREA FLOOR BEAM STA 947.5 AND LBL 25 HAS EVIDENCE OF CORROSION REF AAR N/R 975299 ACCOMPLISHED FLOOR BEAM UPPER CHORD REPAIR AT STA 947.5 RBL 2 TO LBL 60 REF USED B737 SRM 53-70-51-2R-5 FIG 206 DETAIL A WORK ACCOMPLISHED BY V899763
AFT WET AREA FLOOR BEAM STA 947.5 AND LBL 25 HAS EVIDENCE OF CORROSION REF AAR N/R 975299 ACCOMPLISHED FLOOR BEAM UPPER CHORD REPAIR AT STA 947.5 RBL 2 TO LBL 60 REF USED B737 SRM 53-70-51-2R-5 FIG 206 DETAIL A WORK ACCOMPLISHED BY V899763
FWD CARGO DOOR FWD CARGO DOOR AREA BELOW SCUFF PLATE WEB STA 440 TO STA 492.4 HAS SPOT EVIDENCE OF CORROSION REF AAR N/R 975096 REMOVED AND REPLACED FWD CARGO DOOR AREA BELOW SCUFF PLATES WEB STA 440 TO STA 492.4 PER REF B737 SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 AND DWG 143A8330 WORK ACCOMPLISHED BY V894534
FWD CARGO DOOR FWD CARGO DOOR AREA BELOW SCUFF PLATE WEB STA 440 TO STA 492.4 HAS SPOT EVIDENCE OF CORROSION REF AAR N/R 975096 REMOVED AND REPLACED FWD CARGO DOOR AREA BELOW SCUFF PLATES WEB STA 440 TO STA 492.4 PER REF B737 SRM 51-40-02-0G-0 AND SRM 51-40-05-0G-0 AND DWG 143A8330 WORK ACCOMPLISHED BY V894534
FWD PASSENGER COMP WET AREA HAS EVIDENCE OF CORROSION ON INNER CHORD STA 380 AND LBL 64 REF AAR N/R 974900 CUTOUT DAMAGE AREA OF INNER CHORD STA 380 LBL64 AND INSTALLED SPLICE REPAIR REF AAR-MIA ESR 2020476-9 REV IR AND ECRA 5315-011878 WORK ACCCOMPLISHED BY V922796
AS PER T/C EA 5310-04554 REV B OP004 ACCOMPLISHED THE R/H NO.1 WINDOW FRAME INSP AND PREVENTITIVE MOD AS PER T/C EA 5310-04554 REV B OP-004 ACCOMPLISHED THE R/H NO.1 WINDOW FRAME AND PREVENITIVE MODIFICATION WORK ACCOMPLISHED BY V917221
FWD PASSENGER COMP WET AREA HAS EVIDENCE OF CORROSION ON INNER CHORD STA 380 AND LBL 64 REF AAR N/R 974900 CUTOUT DAMAGE AREA OF INNER CHORD STA 380 LBL64 AND INSTALLED SPLICE REPAIR REF AAR-MIA ESR 2020476-9 REV IR AND ECRA 5315-011878 WORK ACCCOMPLISHED BY V922796
WING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHED BY V894534
INSTALL PERMANENT REPAIR AT RT W/W VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.61 REF LP 8609260 REF AAR N/R 974811 INTERVALS HFEC AND LFEC INSP PER B737 SRM 57-10-10-2R-3 STEP 7.B WORK ACCOMPLISHED BY V894534 ACCOMPLISHED VERTICAL PRESSURE DECK WEB REPAIR AT RT SIDE FROM RBL 25 TO RBL48 STA 663 REF B737 SRM 57-10-10-2R-3 FIG 204 DETAIL A-A AND B-B CAT B REPAIR INSP REQUIREMENTS INITAL THRESHOLD AT 56,000 TFC AFTER REPAIR INSTALLED AND 36,000 TFC N/R 974811 CATEGORY B REPAIR INSP REQUIREMENTS INIATE A DIP TO AFTER REPAIR INSTALLATION AND 36,000 FC INTERVALS HFEC & RE-INSPECT AT INITIAL THRESHOLD IN 56,000 FLIGHT CYCLES LFEC PER SRM 57-10-10-2R-3 STEP 7.B INSTALL PERMANENT REPAIR AT RT W/W VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.61 REF LP 8609260 REF AAR
WING CENTER SECTION UPPER SURFACE HORIZONTAL PRESSURE WEB STA 665 RBL 40 CRACKED REF AAR N/R 974984 ACCOMPLISHED HORIZONTAL PRESSURE DECK WEB REPAIR BETWEEN STA 663 TO STA 675 FROM RBL38 TO EBL60 PER REF B737 SRM 53-40-51-2R-2 FIG 202 DETAIL A WORK ACCOMPLISHED BY V894534
INSTALL PERMANENT REPAIR AT RT W/W VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.61 REF LP 8609260 REF AAR N/R 974811 INTERVALS HFEC AND LFEC INSP PER B737 SRM 57-10-10-2R-3 STEP 7.B WORK ACCOMPLISHED BY V894534 ACCOMPLISHED VERTICAL PRESSURE DECK WEB REPAIR AT RT SIDE FROM RBL 25 TO RBL48 STA 663 REF B737 SRM 57-10-10-2R-3 FIG 204 DETAIL A-A AND B-B CAT B REPAIR INSP REQUIREMENTS INITAL THRESHOLD AT 56,000 TFC AFTER REPAIR INSTALLED AND 36,000 TFC
GEAR WOULD NOT RETRACT ON TO OUT OF RDU ACP ALTERNATE LANDING GEAR TEST REF AMM 32-31-51-400-801 AFTER CLOSING ALT GEAR EXTENSION ACCESS DOOR, ALTERNATE LANDING GEAR TEST CHECKED NORMAL. AIRCRAFT WAS JACKED AND LANDING GEAR WAS RETRACTED AND EXTENDED RETRACT BUT RED LANDING GEAR LIGHTS WILL NOT EXTINGUISH UNTIL MULTIPLE TIMES PER AMM 32-61-00-710-801. TESTED LANDING GEAR ALTERNATE EXTENSION DOOR IS CLOSED FLUSH WITH FLOOR. WITH SEVERAL CONFIGURATIONS AND FOUND THAT PREVIOUS FINDING OF ALTERNATE GEAR EXTENSION DOOR NOT CLOSED WILL SHOW LANDING GEAR
PDA 3 LEFT PACK EXHAUST DIFFUSER DOOR STOP (L-ANGLE) CRACKED AND PARTIALLY MISSING.
RIGHT WHEEL WELL VERTICAL PRESSURE DECK WEB CRACKED BETWEEN RBL 40.0 AND RBL 45.64 -- SEE PHOTO,S PHOTO ADDED -- CRACK IS APPROX 2" LONG ......IDT AC NEEDED TO VERIFY AND MARK ENDS OF CRACK REPAIR AS GIVEN IN REPAIR 3 NO MORE THAN 6000 FLIGHT CYCLES OR 24 MONTHS AFTER INSTALLATION, WHICH EVER COMES FIRST. REPAIRED UPPER R/H VAPOR BARRIER CRACK PER SRM 57-10-10-2R-4 REPAIR 4. PLACED ON DIP TO REPLACE REPAIR 4 WITH A PERMENANT DIP APPROVED FOR RIGHT WHEEL WELL VERTICAL PRESSURE DECK WEB TOMC-APPROVAL FROM SC1ELBYC COMMENT CRACKED BETWEEN RBL 40.0 AND RBL 45.64 ACCOMPLISHED INTERM REPAIR REF SRM 57-10-10-2R-4. REPAIR AS GIVEN IN REPAIR 3 NO MORE THAN 6000 FLIGHT CYCLES OR 24 MONTHS AFTER INSTALLATION, WHICH EVER COMES FIRST PERFORMED HFEC TO VERIFIED BOTH ENDS OF CRACK REF. NDT. PART 6 PERFORMED HFEC AND VERIFIED BOTH ENDS HAS BEEN STOP DRILLED. NO C/W SRM 57-10-10-2R-4 STEP 4.E PERFORMED HFEC ON TRIMMED EDGED VERIFIED MATERIAL FOR REPAIR PARTS AS .100" 2024-T3 BARE VERIFIED FABRICATED REPAIR PARTS WAS TREATED AND PRIMED PER SRM VERIFIED REPAIR PARTS WAS INSTALLED WET AND FILLET SEALED THE INSPECTED COATING APPLICATION AND PERFORMED THICKNESS CHECK. REPAIR COMPLETED. 51-00-00 PROCEDURE 23. CRACKS NOTED REF. NDT. PART 6 51-00-00 PROCEDURE 23. REF. NDT PT 6 51-00-00 PROC. 23. NO DAMAGE NOTED. PO#806480381 PER SRM 57-10-10-2R-4 STEP 4.F AND TABLE 201. GAVE 57-10-10-2R-4 STEP 4.F AND 4.G, GAVE OKAY TO INSTALL REPAIR EDGES PER SRM 57-10-10-2R-4 STEPS 4.H THRU 4.J. GAVE OKAY TO FOUN
STANDBY RUDDER POWER CONTROL UNIT APPEARS TO BE LEAKING AT FORWARD LOWER "B" NUT OR UNION. SECURED B NUTS. CLEANED AREA. OPPERATED STANDBY HYDRAULICS AND CYCLED RUDDER SEVERAL TIMES. NO LEAKS NOTED.
SMALL CRACK NOTED ON L1 WINDOW FRAME WHILE AIRCRAFT WAS PRESSURIZED. SEE ATTACHED PICTURES ADDITIONAL PICS.CRACK LOCATED ON C-D POST.CRACK. MEASURES 0.9" LENGTH. IAW AVO#ESC210516-0705-1 R.A. PERFORMED HFEC INSPECTION ABOVE WELL AS DVI OF SAME AREA. CRACK INDICATIONS NOTED. NEW LOG PAGE GENERATED PER PART C OF THE REFERENCED AVO. AND BELOW IN AREAS DEFINED BY FIGURE 8 ON L1 WINDOW FRAME, AS REF TO LP 6315678 FOR CRACK DOCUMENTATION. REMOVED A-C SILL PANEL P/N 141A8815-7 AND BRACKET 141A9504-7 AL ONG WITH FASTENERS REF AVO ESC210516-0705-2 STEP A-1 ACCOMPLISHED STEPS A1, A2 AND B1, OF AVO# ESC210516-0705-2. RII CW ON STEPS A1, A2 AND B1, OF AVO# ESC210516-0705-2.OK TO CONTINUE. TRIMMED OUT EXISTING COUNTERSINK FASTENER IAW FIGURE 14, STEP 1 AND BEGAN STEP C.1. BY INSTALLING 16 BACB30YP6K5 FASTENERS IAW AVO ESC210516-0705-2 REV -. STEP C.1. NOT COMPLETE. C. 1 REF TORQUE VALUES SRM 51-40-04-0G-0 PAGE 10 OF 17. COMPLIED WITH RII PART OF (AVOID VERBAL ORDER) PAGE 4 OF 34 STEP FURTHER ISSUE SHEETMETAL LEAD NOTIFIED ENGINEERING WITH 1) BEING ON PAGE 17 OF 34 OF AVO STEP 2 REQUIRING INSTALL FILLER (NOT SPECIFIED) FOR RELIEF CUT MADE. WAITING ON DAY SHIFT ENGINEER ESC210516-0705-2. ACCOMPLISHED COUNTERBORE PER STEP 17 OF PAGE 25 IAW AVO COMPLETED STEPS 1 AND 2 ON PAGE 17 OF AVO#ESC210516-0705-2 REV A SEALED, INSTALLED FASTENERS, FABRICATED AND INSTALLED FILLER. COMPLETED STEPS 1 THRU 16 ON PAGE 24 AND 25 OF AVO#ESC210516-0705-2 LOCATED DOUBLER AND TRIPLER AND DRILLED HOLES TO SECUR
REFERENCE LOG PAGE 6300515 COCKPIT AIR NOISE / LEAK. FOUND UPPER FWD EYEBROW WINDOW LEAKING FROM LOWER SEAL AREA.UPON PRESSURIZING ACFT, FOUND LH #4, LH #5, AND LH #2 SLIDING WINDOW LEAKING SEVERELY.#4 LH AND #5 LH WINDOW BLANKING PLATES REMOVED FOR INSPECTION AND RESEALING, IAW AMM 56-11-31.REINSTALLED #4 AND #5 LH WINDOW BLANKING PLATES REF EA5610-01137 REV G. ALSO REMOVED AND REPLACED LH SLIDING WINDOW IAW AMM 56-12-11. OPS CHECK GOOD OF WINDOW HEAT. LEAK CHECK REQUIRED FOR LH SLIDING WINDOW AND BLANKING PLATES #4 & #5. ADD EMP:U345750,U346584 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1995346 SN OFF 2486.WINDSHIELD, B73 OFF 29-5612-9-9005 2486 ON 0000 WINDSHIELD, B73 OFF 29-5612-9-9005 2486 ON 29-5612-9-9011 6129.#2 SLIDING WINDOW AND #5 BLANKING PLATE LEAK CHECK GOOD. #4 BLANKING PLATE STILL SLIGHTLY LEAKS AT AFT UPPER CORNER. WILL REQUIRE RESEALING, AND LEAK CHECK.RESEALED #4 BLANKING PLATE IAW EC5610-01137. SEALED AT 0800. REQUIRES 4 HOURS CURE TIME.LH #4 BLANKING PLATE REQUIRES PRESSURIZATION LEAK CHECK, NO SOONER THAN 1200 EASTERN TIME, DUE TO RESEALING.PRESSURIZED AIRCRAFT IAW AMM TASK 05-51-91-790-801. LEAK CHECK GOOD.
GEAR WOULD NOT RETRACT AFTERTAKEOFF FOUND ALT LANDING GEAR DOOR IN CP NOTLATCH. CLEANED LATCH AND SECURED DOOR CLOSED. PREFORMED CHECK PER AMM 32-35-00-820-801 ALL GEAR ACT WENT TO RAISED POSITION . AC OK FOR SERVICE
SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED. SUPPORT TASK 5845 835 REMOVED AND REPLACED SHEAR FITTING. IAW B737200 SRM 51-40-02 AND DWG AND 111 A 2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED. SUPPORT TASK 5845 841 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED. SUPPORT TASK 58458 33 REMOVED AND REPLACED SHEAR FITTINGIAW B737-700. SRM 51-40-02 AND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. SUPPORT TASK 5845 834 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL U3 56089, 12/23/19
SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SUPPORT TASK 5845 837 REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG NO 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INS PECTION U356089,12/23/19
SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED. SUPPORT TASK 58458 38 REMOVED AND REPLACED SHEAR FITTING IAW B737-700. SRM 51-40-02 AN D DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL IN SPECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. SUPPORT TASK 5845 839 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRN 51-40-02 A ND DWG NO.111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL IN SPECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. SUPPORT TASK 5845 840 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02 A ND DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL I NSPECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED. SUPPORT TASK 5845 843 REMOVED AND REPLACED SHEAR FITTING. IAW B737-700. SRM 51-40-02, DWG NO. 111A2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSP ECTION U356089, 12/23/19
SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED SUPPORT TASK 58458 36 REMOVED AND REPLACED SHEAR FITTINGS IAW B737-700. SRM 51-40-02 A ND DWG NO 111 A 2000. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION, 12/23/19
ENTRY DOOR PROBLEM REPORTED BY OPERATIONS UPDATED MAA CODE FIX USING VENDOR MAA SCREEN INSPECT THE ENTRY DOOR FOR ANY DEFECTS AND CONTACT TOMC LOCKED BY TOMC OCM FOUND 1L DOOR EXT HANDLE WILL NOT SPRING BACK INTO RECESSED POSITION. ADD EMP: MTC FERRY COMPLETED, LOG UNLOCKED FOUND EXTERIOR DOOR HANDLE SHAFT SPRING BROKEN. R&R SAME. FIM 52-10-00-810-811 STEP D1F2. LINER AND SLIDE "NOT" REMOVED. DOOR HANDLE OPS GOOD.
ON TAKEOFF GEAR DID NOT RETRACT. RAN GEAR DISAGREE CHECKLIST. NO CHANGE PERFORMED BITE ON PSEU AND FOUND NO CURRENT /EXISTING OR FAULT HISTORY. JACKED PLANE FOR GEAR SWING AND FOUND HE GER HANDLE NOT GOING PAST THE "OFF" POSITION. COULD NOT HEAR CONTROL LEVER LOCK SOLENOID OPERATE EVEN WHEN BREAKER WAS PULLED. GEAR RETRACTED WHEN OVERRIDE TRIGGER PULLED. R&R LANDING GEAR CONTROL LEVER DEFECTS NOTED. INDICATIONS, GEAR HANDLE AND GEAR OP''S CHECKED GOOD. NO OTHER ADVERTISED. SWUNG GEAR 10 TIMES WITH NO DEFECTS OR FAULTS. ALL LOCK SOLENOID IRW 32-31-31-400-801. GEAR HANDLE OPERATES AS
CABIN EMERGENCY LIGHT MOUNTED ON OVERHEAD BIN ABOVE PAX SEAT ROW 24DEF INOPERATIVE. REMOVED AND REPLACED BATTERY PACK & CHARGER. OPS CHECKS NORMAL IAW WDM 33-51-14.
RT WINDOW ESCAPE EMERGENCY EXIT LIGHT BATTERY WEAK. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AND PREFORMED OPS TEST NORMAL REF B737 AMM 33-51-06
MAIN CABIN FLOOR STRUCTURE STA 328 BETWEEN RBL 46 AND RBL 53 HAS 2EA SPOTS OF CORROSION AT FLOOR SUPPORT BEAM UPPER FLANGE. REMOVED CORROSION FROM FLOORBEAM AT STA 328 RBL 46 AND 53 REF SRM 51-10-02 FOUND REWORKED AREA RBL 53 OUT OF LIMITS REF ECRA 5321-01330. REPAIRED FLOORBEAM FROM RBL 40 TO THE END OF BEAM REF SRM 53-10-51 REP 7 ALTERNATIVE 3 FIG 206.
AFT CARGO COMPARTMENT FRAME AS BS 727E DENTED BETWEEN STR 24L AND 25L. PERFORM REPAIR TO STA 727E FUSELAGE LOWER FRAME PER MIA RES 2011833 WITHOUT DEVIATIONS THE APPLICABLE WORK INSTRUCTIONS AND REPAIR FIGURE FROM RES 2011833-46 ARE INCLUDED ON PAGES 3-6 OF ECRA 5310-07078 ACCOMPLISH A PERMANENT REPAIR PER ECRA5310-07 078 ON OR BEFORE 16FEB2018 PER ECRA 5310-07078
CRACK FOUND AT RT HORIZONTAL STAB LOWER SKIN HSS 138.70 AND 26 INCHES FWD OF AFT SPAR. CRACK LENGTH .500 INCH. REPAIRED THE SKIN IAW SRM 55-10-01, REPAIR 11, FIGURE 204.
CRACK FOUND ON RT HORIZONTAL STAB LOWER SKIN. REPAIRED IAW SRM 55-10-01, FIGURE 204.
BS 303 BETWEEN STRINGERS 16 - 17L INBD FLANGE OF FRAME HAS CORROSION. REPAIRED IAW ECRA 5310-7073.
R1 DOOR INTERNAL STRUCTURE AT BOTTOM GATE ACTUATING ROD PASS THRU HOLE CRACKED. REPAIRED IAW ECR A 5210-02805, FIGURE 3.
NOSE LANDING GEAR NOSE GEAR GREEN LIGHT DOES NOT GO OFF WITH LANDING GEAR LEVER AT UP, NOSE GEAR RED LIGHT ON NOSE GEAR UNSAFE INDICATION. REPLACED SENSOR PER AMM32-61-51-400-802. ACCOMPLISHED PSEU BITE CHECK NO FAULTS AND PERFORMED OPS TEST AMM32-61-51-710-801
FL 390, CABIN ALTITUDE WARNING HORN AND LIGHT, PRECEDED BY RIGH T BLEED TRIP OFF LIGHT. PERFORMED NR 2 ENG HEALTH CHECK IAW AMM 36-11-00-700-803, REPLACED THE NR 2 ENG HIGH STAGE VALVE IAW AMM 36-11-06.
FOUND HEAVY INTERGRANULAR CORROSION ON AFT CARGO INTERCOSTAL AT BS 847 BETWEEN STRINGERS 25L & 26L AT BASE OF BULKHEAD VERTICAL STANCHION. INSTALLED FABRICATED INTERCOSTAL IAW DWG 149A8102 REV B & SRM 51-40-02.
RAMP DISCOVERED AFT CARGO DOOR DENT LOCATED 18.5 INCHES FROM AFT EDGE & 13.5 INCHES FROM TOP EDGE. INSPECTED DENT & FOUND TO BE OUT OF LIMITS, DEPTH IS .147 INCHES, MAX ALLOWED IS .125 INCHES. INSTALLED, SEALED & PAINTED REPAIR IAW SRM 52-00-01 REPAIR 2.
CENTER WING BOX REAR SPAR VERTICAL PRESS WEB CRACKED BETWEEN LBL 40.00 & 45.64. INSTALLED REPAIR IAW SRM 57-10-10 REPAIR 3 & REPAIRED SECONDARY FUEL VAPOR BARRIER IAW AMM 28-11-00.
LEFT WING TE CAVITY BULB SEAL RETAINER CRACKED WERE IT ATTACHED TO THE DEFLECTOR RIB. R & R CLIP 115A6260-1 IAW DWG 115A6260 & 737SRM 51-40-02.
LOWER RAIL ASSEMBLY AT STATION 500D FOR FBB AFT BULKHEAD CTR WALL PNL HAS CORROSION. R & R LOWER RAIL ASSEMBLY. PN 143A9485Y35 AT STATION 500D IAW SRM 51-40-02 & IPC 53-11-01-43.
DIVERT TO LAX. ON APPROACH TO SNA WHEN EXTENDING FLAPS TO 1 THE FLAP INDICATOR NEEDLE STOPPED JUST PRIOR TO 1 BAND & LE FLAPS TRANSIT LIGHT ILLUMINATED. RAN QRH & THEN DIRECTED TO A MANUAL FLAP EXTENSION, USED ALT FLAP EXTENSION TO EXTEND FLAPS TO 15 IAW QRH & NON-NORMAL LANDING DIST CHART, ALL INDICATIONS WERE NOW NORMAL. DID NOT OVER SPEED FLAPS & WAS NOT AN OVERWEIGHT LANDING. R & R THE LT FLAP POSITION TRANSMITTER. PERFORMED ADJUSTMENT, TESTED IAW MM 27-58-01-820-801, OPERATIONS CHECKED GOOD, L & VERIFY BITE PERFORMED ACFT FULLY AUTO LAND CAPABILITY REMAINS IAW MM 22-11-00-201. ROTABLE PARTS CHANGE WAS INDICATED TT 1645692, SN OFF 00098 TRANSMITTER, FL OFF 29-2759-9-0001 0098 ON 29-2759-9-0001 0609.
CRACK INDICTION FOUND FRAME BS 400 MID FREQ ONLY. INBD FASTENER NOT EXTENDING INTO RADIUS ACCOMPLISHED REPAIR IAW ECRA 5310-05459.
CMM 78-31-37 REV 23 FIG 35 ITEM 40B. THE 315A2101-41 INNER WALL BONDED PANEL HAS AN AREA OF DISBOND (PERF SKIN TO CORE) THAT MEASURES 1.5 X 24.5". AFTER REMOVING THE DISBONDED PORTION OF THE SKIN IT WAS DISCOVERED THAT THE PERF SKIN WAS PERPARED INCORRECTLY PRIOR TO ORIGINAL BONDING. THE DISBOND AREA KEEPS GROWING AND NOW MEASURES 5.5 X 33.5".
THE 315A2222-5 CASCADE RING HAS EXTENSIVE WEAR/DAMAGE CT THE AFT LWR ATTACHING BOLT LOCATION. HOLE SHOULD BE .3750 -.3754. ACTUAL IS ELONGATED TO APPROX .6210 WITH HEAVY WEAR/MISSING MATERIAL CT THE NUT SIDE. THE 315A2402-5 LATCH BEAM HAS A CORRESPONDING ELONGATED HOLE CT THE AFT LOCATING HOLE CT THE CASCADE RING. HOLE IS ELONGATED OUT TO .4950, SHOULD BE .3750-.3754. ADDITIONAL MATERIAL WEAR/DAMAGE ON THE LOCATING FASTENER HEAD SIDE THAT MEASURES APPROX .070 DEEP X .10 WIDE THE OUTSIDE DIA OF HOLE.
SUPPORT TASK REF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 907L BOTH MID AND HIGH FREQ INB FASTENER NOT EXTENDING INTO RADIUS. REPAIRED PER ECRA 5310-05458.
SUPPORT TASK - REF EA 5310-04716 REV C CRACK INDICATION FOUND AT FRAME 440 L MID FREQ ONLY INBD FASTENER NOT EXTENDING INTO RADIUS CABIN FRAME 440 L. REPAIRED IAW EA 5310-04716 REV C.
SUPPORT TASK - REF EA 5310-04716REV C CRACK FOUND FRAME STA 727D R MID FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED IAW EA 5310-04716 SEE ATTACHED 44.0008FOR ADDITIONAL WORK ACCOMPLISHED.
REF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 747L BOTH MID AND HIGH FREQ-NOT EXTENDING INTO RADIUS. REPAIRED PER EA 5310-04716 REV C.
SUPPORT TASK - REF EA 5310-04716 REV C OP1 CRACK INDICATION FOUND FRAME 747R BOTH MID AND HIGH FREQ INBD FASTENER NOT EXTENDING INTO THE RADIUS. REMOVED DAMAGED AREA FABRICATED REPAIR PARTS AND INSTALLED PARTS AS PER EA 5310-04716 REV C.
SUPPORT TASK - REF EA5319-04716 REV C CRACK FOUND FRAME 787 R MI D FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED STA 787 FRAME BETWEEN STR 8 AND STR 9 REF EA 5310-04716 REV C REF FORM 44.0008 FOR WORK DETAILS.
SUPPORT TASK - REF EA5310-04716 REV C CRACK FOUND FRAME STA 867L NOT INTO THE RADIUS. SHOULD BE A/C 705 ACCOMPLISHED PERMANENT REPAIR PER EA5310-04716 REV C .
REF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 827L MID FREQUENCY INBD FASTENER NOT EXTENDING INTO RADIUS. REPAIRED FRAME AT STA 827L IN ACCORDANCE WITH EA 5310-04716 REV C.
SUPPORT TASK - REF EA5310-04716 REV C CRACK FOUND FRAME STA867R M ID FREQ AND HIGH FREQ I/B FASTENER NOT INTO RADIUS. REPAIRED AS PER ECRA 5310-04716 REV C SEE FORM 44.0008 FOR WORK ACCOMPLISHED.
REF EA 5310-04716 REV C CRACK INDICATION FOUND FRAME 787L BOTH MID AND HIGH FREQ INBD FASTERNER NOT EXTENDING INTO RADIUS. REPAIRED FRAME AT STATION 787L PER EA 5310-04716 REV C SEE FORM 44.0008 FOR WORK PERFORMED.
SUPPORT TASK REF EA5310-04716 REV C CRACK INDICATION FOUND AT FRAME 827R, NO EXPENDING INTO THE RADIUS. REPAIRED PER EA5310-04716 REV C .
SUPPORT TASK - C SCAN INSP OF RIGHT STAB PER EA 5510-01843 FOUND A CRACK INDICATION AT LOWER SKIN SURFACE STA 161.04 RIB 9 AND AFT OF FRONT SPAR APPROX 6". REPAIRED RT STAB LOWER SKIN PER SRM 55-10-01 REPAIR 11 SEE BL0 CK 42 AND ATTACHED 44.0008 FOR ALL PARTIAL WORK ACCOMPLISHED.
SUPPORT TASK: RT HORIZONTAL STAB I/B LEADING EDGE SKIN HAS DENT REF L/P 7850545. PERFORMED PERMANENT REPAIR TO RT HORIZONTAL STABILIZER INBOARD FIXED LEADING EDGE SKIN P/N 186A2013-2 REF ECRA 5510-02101.
CORROSION ON UPPER INSIDE OF THRESHOLD Z-ANGLE MARKED R2. INSTALLED R2 DOOR CHORD PER SRM 51-40-02.
INSPECTION FOUND FLOOR SUPPORT BETWEEN FLOORBEAM AT STA 947-967, RBL 62 (LAV E) CORRODED. REPAIRED FLOOR SUPPORT IAW ECRA 5321-01265.
INSPECTION FOUND INTERCOSTAL CORRODED AROUND TWO NUTPLATES I/B OF L-2 DOOR AT STA 947.5-967, LBL 62. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
INSPECTION FOUND FLOOR SUPPORT CORRODED AT SEVERAL FASTENER HOLES I/B OF L-2 DOOR AT STA 947.5-967, LBL 45 TO LBL 62. REPLACED FLOOR SUPPORT IAW ECRA 5321-01263.
INSPECTION FOUND A 1INCH CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 328-344, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
INSPECTION FOUND A 1" CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 277-294, BL 0. A REPAIR WAS INSTALLED IAW SRM 51-40-02.
INSPECTION FOUND A 1INCH CRACK IN INTERCOSTAL BETWEEN FLOORBEAM AT STA 312-328, RBL 40. A REPAIR WAS PERFORMED IAW SRM 51-40-02.
INSPECTION FOUND LIGHT CORROSION ON STRAP/FLOORBEAM I/B OF R-1 DOOR THRESHOLD PLATE FROM STA 294.5 - 344. THE STRAP AND FLOOR CHORD WERE REMOVED AND REPLACED IAW SRM 51-10-02, 51-40-02, AND 53-10-15.
INSPECTION FOUND A 12 INCH CRACK IN INTERCOSTAL TWELVE INCHES I/B OF THRESHOLD PLATES BETWEEN STA 312 AND 328, LBL 50. THE INTERCOSTAL WAS REMOVED AND REPLACED IAW SRM 51-40-02.
INSPECTION FOUND TWO DENTS IN FUSELAGE SKIN AT BS 385, BETWEEN S17L AND 18L. THE DENTED AREA WAS REPAIRED IAW ECRA 5331-01126.