N15712

Part: BULB — INOPERATIVE (ZONE 200) · airframe 82,735 hrs · 29,677 cycles

EMERGENCY EXIT LIGHTS NOT ARM AND NR 2 TANK FWD LOW PRESS INDICATION LIGHTS HAVE ONE LIGHT BULB INOPERATIVE EACH. R & R LIGHT BULBS PER AMM33-18-00, OPS CHECKED GOOD.

Part: BATTERY PACK — DISCHARGED (ZONE 200) · airframe 82,053 hrs · 29,305 cycles

ROW 29-34 IN SEAT EMERGENCY LIGHTS INOP T/S AND FOUND BATTERY DEAD DUE TO INOP CHARGER. REMOVED AND REPLACED BOTH BATTERY AND CHARGER IAW AMM 33-51-06/201. OPS CHECK GOOD. OK FOR CONTINUED SERVICE.

Part: BATTERY — FAILED (ZONE 200) · airframe 82,053 hrs · 29,305 cycles

AFTER LAYOVER CREW FOUND EMERG EXIT LIGHT SWITCH NOT DISARMED. REPLACED AIRCRAFT BATTERY ON L/P 6240561 ALL EMERGENCY LIGHTS OPERATIONAL CHECK GOOD AFTER BATTERY REPLACEMENT IAW 33-51-00 .

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 81,757 hrs · 29,165 cycles

EMERGENCY LIGHT BATTERY PACK M1673 FAILED CAPACITY CHECK. EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR). REMOVED AND REPLACED IAW AMM 33-51-06-960-805. OPS CHECK GOOD.

Part: BATTERY PACK — FAULTY (ZONE 200) · airframe 81,757 hrs · 29,165 cycles

EMERGENCY LIGHT BATTERY PACK M1672 FAILED CAPACITY CHECK.EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR). REMOVED AND REPLACED BATTERY PACK IAW AMM 33-51-06-960-805. OPS CHECK GOOD.

Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 81,757 hrs · 29,165 cycles

EMERGENCY LIGHT BATTERY PACK M1668 FAILED CAPACITY CHECK. EMERGENCY LIGHTING SYSTEM FUNCTIONAL CHECK (INTERIOR AND EXTERIOR) {MULT-33-3-0004} - REMOVED AND REPLACED BATTERY PACK IAW AMM TASK 33-51-06-960-805. OPS CHECK GOOD.

Part: SLIDE — UNPACKED (ZONE 800) · airframe 81,757 hrs · 29,165 cycles

R2 DOOR SLIDE HAS EXCESSIVE EXPOSED GIRT CAUSING DOOR TO NOT CLOSE PROPERLY. RE-PACKED R2 DOOR SLIDE IAW AMM 25-66-01.OPS CHECK GOOD VERIFIED INSTALLATION OF SLIDE IAW AMM 25-66-01.

Part: COVER — NO DISCREPANCY (ZONE 800) · airframe 81,530 hrs · 29,056 cycles

REMOVED L1 DOOR ESCAPE SLIDE PACK AND COVER ASSY FOR MX, REF AMM 25-66-01-000-801. REINSTALLED L1 DOOR ESCAPE SLIDE IN REF TO AMM TASK 25-66-01-400-803. OPS CHECK GOOD. ACCOMPLISHED RII INSPECTION OF L1 DOOR SLIDE INSTALLATION REF AMM 25-66-01 AND GMM 09-25-05.

Part: COALESCER BAG — FAULTED (ZONE 100) · airframe 81,388 hrs · 28,978 cycles

EXCESSIVE ODOR ON TAKOFF ODOR CONTINUED FOR 10 MINS BEFORE DISSI PATING DEBRIEFED INBOUND FLT CREW AND ADDED FORM 46-6020 IN PICS. PULLED AFT WALL OF FORWARD CARGO PIT. REPLACED RIGHT RECIRCULATION FILTER, PER AMM 21-25-01-000-801. INSTALLED FWD CARGO PIT AFT WALL. *INFO NOTE THAT #1 ENG COMPRESSOR WASH WAS COMPLETED DURING OVERNIGHT MAINT PRIOR TO INBOUND FLT TO ORD. WORKED ODOR CONDITION IAW AMM 05-51-26. REMOVED AND REPLACED LH PACK COALESCER BAG IAW AMM 21-51-05 - LEAK CHK GOOD. RAN BOTH ADD EMP:U010764 ENGINES, BOTH PACKS, AND BOTH BLEEDS IN MULTIPLE CONFIGURATIONS. RAN BOTH PACKS OPERATED IN FULL COLD AND FULL NOT WITH ENG BLEED SOURCE FOR OVER 10 MINUTES WITH NO ODOR NOTED IN FLT DECK. OK F/SVC.

Part: UNKNOWN — LEAKING (TOILET) · airframe 81,248 hrs · 28,902 cycles

BLUE JUICE LEAKING FROM AFT LAVS ONTO CARPET. SMELLS BAD BLUE JUICE (WASTE TANK DISINFECTANT) RESIDES IN THE WASTE TANK NOT THE LAV. NONETHELESS, LAV E TOILET SHROUD WAS REMOVED AND REPLACED AS IT WAS CRACKED SECONDARY THE TROUBLESHOOTING AND LEAK CHECKING OF THE TOILET AND IT'S ASSESSARY PARTS. LAV E WAS FURTHER INSPECTED AND LEAKED CHECED BY REMOVAL OF AFT CARGO PIT PANELS TO CHECK DRAIN AND FEED LINES. THERE ARE NO SIGNS OF AN ACTIVE LEAK ANTWHERE. MORE SPECIFICALLY; EVERYWHERE BUT THE CARPET BETWEEN LAVS D & E WAS DRY. IF IT IS THE CASE THAT THIS WAS FIRST R...

Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 81,194 hrs · 28,874 cycles

OPS REPORTED THAT FLT ATT SAID R1 DOOR SLIDE APPEARS TO HAVE EXCESS FABRIC SHOWING. VERIFIED Z FOLD WITHIN LIMITS APPROXIMATELY 11 INCHES REF AMM TASK 25-66-01-400-804. OK FOR SERVICE. VERIFIED Z FOLD WITHIN LIMITS APPROXIMATELY 11 INCHES REF AMM TASK 25-66-01-400-804. OK FOR SERVICE

Part: WARNING LIGHT — FALSE ACTIVATION (ZONE 800) · airframe 81,096 hrs · 28,821 cycles

DOOR WARNING ANNUNCIATOR IS ON EQUIP ILLUMINATED BRIEFLY DURING GEAR RETRACTION AND IMMEDIATELY WENT OUT REQUEST MEL 5203G FOR EQUIP DOOR ANNUNCIATION. FOUND MX MSG 52-72004 ON PREVIOUS LEGS DURING PSEU BITE PROCEDURE. DUE TO HISTORY REPLACED E/E ACCESS DOOR INDICATION SWITCH IAW AMM 52-71-42/201. NO EXISTING FAULTS FOUND ON PSEU AFTER TEST. CYCLED DOOR AND VERIFIED INDICATION WAS WORKING AS IT SHOULD.

Part: SLIDE — LOOSE (ZONE 800) · airframe 80,997 hrs · 28,768 cycles

ESCAPE SLIDE ON R1 DOOR IS LOOSE AND COMING OUT OF PACK SLIDE PACK AT DR 1R NORMAL REF AMM 25-66-00 OK TO CONTINUE

Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 80,444 hrs · 28,507 cycles

FLOOR PROXIMITY EMERGENCY LIGHT INOP ON SEAT 8C REMOCED & REPLACED SEAT 8C EMERGENCY LIGHT ASSY.OPS CHECKED GOOD.

Part: WINDOW FRAME — CRACKED (ZONE 200) · airframe 80,038 hrs · 28,315 cycles

ACCOMPLISH INSPECTON REQUIREMENTS OF L/H #3 FLIGHT DECK WINDOW FRAME E-F POST, PER PART 2 OF EC/RA 5311-03308 ON OR BEFORE THE AIRCRAFT REACHING 50,000 TOTAL FLIGHT CYCLES. 5311-03308 FOR DEVIATION PERFORMED. ACCOMPLISH INSPECTION PART 2 OF EC/RA 5311-03308 ON OR BEFORE THE AIRCRAFT REACHING REQUIREMENTS ON THE LH #3 FLIGHT DECK WINDOW FRAME E-F POST, PER 50,000 FLIGHT CYCLES. WHILE ACCOMPLISHING EA 5310-8195 OP 003. DEVIATION WAS REQUIRED TO ACCOMPLISH THE CUTTING OF THE WINDOW POST. REF. EC/RA TOMC APPROVED TO ACCOMPLISH INSPECTION REQUIREMENTS OF THE LH TOMC-APPROVAL FROM SC1ELBYC COMMENT #3 FLIGHT DECKWINDOW FRAME E-F POST, PER PART 2 OF EC/RA 5311-03308 ON OR BEFORE THE AIRCRAFT REACHING.50,000 TOTAL FLIGHT CYCLES QC QC REVIEW INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS REVIEW.

Part: ADIRU — INTERMITTENT (STA318.75, E/E B) · airframe 77,669 hrs · 27,225 cycles

AIRSPEED AND ALTITUDE DISAGREE IN FLT. CAPT SIDE WAS RELIABLE. CLEARED BELOW 7000 AGL. UNIT, ADIRU, AI OFF 29-3421-9-0010 5345 ON 29-3421-9-0010 6370 UNIT, ADIRU, AI OFF 29-3421-9-0010 5345 ON 0000 INSPECTED PITOT PROBES AND AOA VANE. NO DEFECTS FOUND. CHECKED PITOT FOR WATER IN PITOT SIGHT GLASS. NO MOISTURE FOUND. REPLACED RIGHT AIR DATA INERTIAL REFERENCE UNIT REF 34-21-01 AMM. PERFORMED OPERATIONAL TEST OF THE RIGHT ADIRU SYSTEM REF ADD EMP:U114750 34-21-00-710-801 AMM. OPS CHECK GOOD. ACCOMPLISHED LAND VERIFY TEST REF 22-11-00 AMM. OPS CHECKED NORMAL AIRCRAFT OK FOR FULL CATIII SERVICE.

Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 77,101 hrs · 26,974 cycles

PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1676 FAILS OP CHECK (REF: AAR NR 99986434) REMOVED & REPLACED BATTERY PACK IN RH SIDE M1676 IAW B737 AMM 33 -51-06-960-805. TEST PASS GOOD.

Part: BATTERY PACK — INOPERATIVE (M1673) · airframe 77,099 hrs · 26,972 cycles

BATTERY PACK M1673, LIGHTS SHUT OFF PRIOR TO 15 MINUTES MINIMUN (REF. AAR NR 99981333). REMOVED & INSTALLED NEW BATTERY PACK M1673 IAW B737 AMM 33-51-06 -960-805. TEST PASS GOOD. (WORK ACCOMPLISHED BY V936440 AND AAR QC A-37 V937288) (SDR NO. 1033989).

Part: BATTERY PACK — INOPERATIVE (M1672) · airframe 77,099 hrs · 26,972 cycles

BATTERY PACK M1672, LIGHTS SHUT OFF PRIOR TO 15 MINUTES MINIMUN (REF AAR NR 99981334). REMOVED AND INSTALLED NEW BATTERY PACK M1672 IAW B737 AMM 33-51-06-960-805. TEST PASS GOOD.

Part: SKIN — CORRODED (FWD CARGO DOOR) · airframe 77,099 hrs · 26,972 cycles

AFTER EVALUATING CORROSION ON PREVIOUS REPAIR FOUND OUT OF LIMITS AND REQUIRED REPLACEMENT ON FWD CARGO DOOR CUT OUT (REF. AAR NR 99982221). PERFORMED PERMANENT REPAIR ON FWD CARGO DOOR CUT OUT IAW EA#2302 99 REV IR AND EC/RA# 5331-03061 B737-700 SRM 51-10-02-0G-0, 51-4 0-02-0G-0. THIS REPAIR CLOSE LOG PAGE 4002954 (WORK ACCOMPLSIHED BY V936445 AND AAR QC V931821)

Part: SKIN — DENTED (AFT CARGO DOOR) · airframe 77,099 hrs · 26,972 cycles

AFT CARGO DOOR HAS 10 DENTS IN OUT SIDE SKIN WORST DENT IS L=3.0" W=1.8" D=0.042" A/Y=42.8 DENT IS WITH IN L IMITS PER SRM 52-30-01 FIG. 103 DETAIL F A/Y MUST BE 30 OR MORE INSPECTED AREA. NO PROGRESSION NOTED. DMG REMAINS. OK TO CONT INUE. INSPECTED DAMAGES NO PROGRESSION NOTED. W/I LIMITS PER SRM 52-30 -01 FIG103F DMG REMAINS , OK TO CONTINUE. RE-INSPECTED DENTS AT AFT CARGO DOOR EXTERNAL SKIN FOUND TO BE W ITHIN ALLOWABLE DAMAGE LIMITS REF. SRM 52-30-01, FIG. F AND INST ALLED DENT DOT REF. GMM 06-35-05 LOG PAGE WAS CONVERTED TO ELB FORMAT ON JAN 17, 2017 AT 10140151 INSPECTED DENTS AND FOUND TO BE WITHIN LIMITS REF BOEING 737-700 SRM 52-30-01-FIG 103/ ALLOWABLE DAMAGE 1,DETAIL F. INSTALLED DE NT DOTS REF UAL GMM 06-35-05. REINSPECTED DENTS AND FOUND WORST DENT TO BE L=3.0" W=1.8" D=.042" A/Y=42.8" WITHIN LIMITS REF. SRM52-30-01 FIG.103 DET.F REMOVED AND DAMAGED SKIN FABRICTAED AND INSTALLED NEW AFT CARGO DOOR SKIN IAW B737-700 SRM 51-40-02-0G-0,52-30-01-01-01, 52-30-0 1-2R-3, REFRENCE WORK ORDER 3501941/8000/0050 SERIAL 99982064,

Part: FLOORBEAM — CORRODED (STA986.5) · airframe 77,099 hrs · 26,972 cycles

FOUND POSSIBLE CORROSION ON FLOOR BEAM AT STA .986.5 FROM RBL 29 THRU LBL 49 (REF AAR NR 99981524) REPAIRED FLLOR BEAM STA 986.5 FROM RBL 29 THRU LBL 49 IAW B737-7 00 SRM 53-70-51-2R-4, 51-40-02-0G-0,51-10-02-0G-0, 51-40-05-0G-0 , 53-70-51-1A-1.

Part: FLOORBEAM — CORRODED (STA .947.5) · airframe 77,099 hrs · 26,972 cycles

FOUND CORROSION ON FLOOR BEAM STA .947.5 APPROX RBL 53 (REF AAR NR 99986348) REPAIRED FLOOR BEAM STA 947.5 APPROX RBL 53 I.A.W B737-700 SRM 5 7-70-51-2R-5, 51-40-02-0G-0,51-40-05-0G-0, 51-10-0G-0 AND 53-70- 51-1A-1.(WORK ACCOMPLISHED BY V940516 AND AAR QC A-11 V931821).

Part: FLOORBEAM — CORRODED (STA947.5 LBL53) · airframe 77,099 hrs · 26,972 cycles

FOUND POSSIBLE CORROSION ON FLOOR BEAM AT STA. 947.5 LBL 53. (RE F AAR NR 99981533) REPAIRED FLOOR BEAM AT STA 947.5 LBL 53 I.A.W B737-700 SRM 53-70 -51-2R-5, 51-40-0G-0 51-40-05-0G-0, 51-10-02-0G-0 AND 53-70-51-1 A-1.

Part: UNKNOWN — CORRODED (STA947.5 TO 986) · airframe 77,099 hrs · 26,972 cycles

FOUND POSSIBLE CORROSION ON R2 DOOR INNER CHORD FROM STA. 947.5 TO STA 986. (REF AAR NR 99981529) REMOVED AND REPLACEDR2 DOOR INNER CHORD FROM STA 947.5 TO STA 98 6 I.A.W B737-700 SRM 51-40-02-0G-0, 51-40-05-0G-0,51-10-02-0G-0, 53-70-15-1A-1.SFR NO.1033756.

Part: WEB — CORRODED (STA986.5-1016) · airframe 77,099 hrs · 26,972 cycles

AFT WET AREA, FLOOR STRUCTURE, POSSIBLE CORROSION AT WET BTW STA 986.5 TO STA 1016 LBL 36 (REF AAR NR 99981994) REMOVED AND REPLACED WEB ON AFT WET AREA FLOOR STRUCTURE AT STA 986.5 TO STA 1016 RBL 36 IAW B737-700 SRM 51-40-02-0G-0, 51-40-0 5-0G-0, 51-40-05-0G-0, 53-70-51-1A-1.

Part: UNKNOWN — CORRODED (STA. 927) · airframe 77,099 hrs · 26,972 cycles

FOUND POSSIBLE CORROSION ON L2 DOOR INNER CHORD AT STA. 927 TO S TA. 1006 (REF. AAR NR 99981534). REMOVED AND REPLACED INNER CHORD ON L2 AT STA 927 TO STA 1006 I. A.W B737-700 SRM 51-40-02-0G-0 51-10-02-0G-0,51-40-05-0G-0 AND 5 3-70-15-1A-1.

Part: LINE — BROKEN (BLEED AIR) · airframe 76,752 hrs · 26,781 cycles

AT FL370 CABIN ALT WARNING LIGHT CAME ON AND CABIN PRESSURE REACHED 10000 IN AUTO. CARRIED BY ELB FOUND BLEED AIR LINE TO PRECOOLER CONTROL VALVE BROKE. REPLACED LINE REF AMM 36-12-02. PERFORMED ENGINE RUN SYSTEM OPS CHECK GOOD.

Part: ADIRU — FAILED (NA) · airframe 75,398 hrs · 26,141 cycles

SPEED TRIM FAIL, THE RIGHT ADM AND RIGHT ADIRU REPLACED AS WELL AS A PITOT STATIC FLUSHING/LEAK CHECK ACCOMPLISHED ALL TESTS PASSED. SPEED TRIM PORTION OF LAND VERIFY TEST PASSED.

Part: DOOR — NONE (NLG) · airframe 72,673 hrs · 25,068 cycles

NOSE GR DOOR LT AND DWN GREENLIGHT ON WITH GR BACK TO OFF QRC GO OD 3 DWN LOCKED LOCKED BY TOMC MGR DUE TO EMERGENCY DECLARED FOR LANDING. UNLOCK TO CLEAR DEBRIEFED CREW NLG WAS RETRACTED, BROUGHT HANDLE TO OFF POSITION AND NLG INDICATION AND NLG DID FREEFALL. FOLLOWED QRH WITH TOMC INPUT. NLG CYCLED NORMALLY. GEAR LEFT IN UP POSITON AND TO DOW N DURING LANDING. PERFORMED OPERATIONAL TEST OF NLG REF AMM 32-33-00-710-801 AND 802 NO DEFECTS NOTED AT THIS TIME

Part: DRAIN — LEAKING (NR 1 HYD CASE) · airframe 70,439 hrs · 24,222 cycles

ENG 1 HYD LOW PRESS LIGHT ON IN FLIGHT QUAN DROPED TO 0 FOUND HYD LEAK COMING FROM RETURN FILTER CASE & CLAM FOUND RETURN FILTER CASE BEND FOUND LEAK COMMING FROM THE FILTER CASE DRAIN ASSY. REPLACED CAS E AS PER AMM 29-11-61 PB401. PRECAUTIONARY REPLACED EDP ENG 1 AS PER AMM 29-11-11 PB401. RAN THE ENGINES FOR 10 MINS. NO LEAKS N OTED AT THIS TIME. ALL INDICATIONS NORMAL IN COCKPIT ADD EMP:U247191, U362339, U372867 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1169014 SN OFF 1639 PUMP, HYD ENG D OFF 29-2910-9-0003 1639 ON 29-2910-9-0003 4006

Part: SKIN — CORRODED (LH WING) · airframe 69,515 hrs · 23,884 cycles

CORROSION FOUND ON LOWER SURFACE OF LT WING AT BBL 70.85, OUTBOARD OF T-CHORD FASTNER 10-3. SPT L/P 5866413. ACCOMPLISHED ALL REWORK, IAW ECRA 5725-01069. NO FURTHER ACTION REQUIRED. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION U 354653, DATE 1/27/2021 INSPECTION ACCOMPLISHED.

Part: SKIN — CORRODED (LH WING BBL 70) · airframe 69,515 hrs · 23,884 cycles

CORROSION FOUND UNDER LT WING AT BBL 70.85, OUTBOARD OF T-CHORD FASTNER 11-4 ON LOWER SURFACE. SPT LP 5866412 ACCOMPLISHED ALL REWORK, IAW ECRA 5725-01069, NO FURTHER ACTION REQUIRED. DATA WAS TRANSCRIBED FROM N/R 5866412 WORK ACCOMPLISHED INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 RBL 32.40 IS CRACKED SPT 5866418. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01188 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 RBL 40.87 IS CRACKED. SPT 5866417 REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5741-01189 REV ORIGI NAL SSFR REPRT FORM 46-0024 ENTERED BY UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 RBL 54.60 IS CRACKED. SPT 5866418. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01190 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 LBL 32.40 IS CRACKED. SPT 5866426. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01183 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BU UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 LBL 15.04 IS CRACKED. SPT 5866424. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01182 REV ORIGINAL SSFR FORM 46-0024 ENTERED BU UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 RBL 15.04 IS CRACKED. SPT 5866419. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01187 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/23/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 LBL 40.87 IS CRACKED, SPT 5866422. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01184 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/22/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 RBL 6.14 IS CRACKED, SPT 5866420. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01186 REV ORIGI NAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/22/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 LBL 6.14 IS CRACKED, SPT 5866425. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01181 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/22/21 INSPECTION ACCOMPLISHED.

Part: FITTING — CRACKED (FUSELAGE) · airframe 69,515 hrs · 23,884 cycles

SHEAR FITTING AT STA 540 LBL 54.60 IS CRACKED, SPT 5866421. REMOVED AND REPLACED SHEAR FITTING, IAW ECRA 5714-01185 REV ORIGINAL SSFR REPORT FORM 46-0024 ENTERED BY UAL INSP U354653 1/22/21 INSPECTION ACCOMPLISHED.

Part: PROBE — DAMAGED (INLET PORT) · airframe 63,764 hrs · 21,611 cycles

DURING DESCENT, AIRSPEED AND ALTIMETER UNRELIABLE ON CAPTAIN`S AND FIRST OFFICER`S SIDES. ENGINE LIGHT ILLUMINATED. PERFORMED PITOT-STATIC FULL RATE LEAK CHECK TO 35000 FT & 300 KTS ON LEFT & RIGHT SYSTEMS, ALL PARAMETERS MATCH, NO DISAGREE FAULTS IAW AMM 34-11-00. PERFORMED AN AOA VANE POSITION CHECK IAW AMM 34-21-05, NO FAULTS. REPLACED THE AIR TEMP PROBE.

Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 63,709 hrs · 21,597 cycles

SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 22ABC THROUGH 28ABC WERE INOPERATIVE. REPLACED THE M1670 POWER SUPPLY ASSY IAW AMM 33-51-06. CHECKED NORMAL.

Part: INTERCOSTAL — CORRODED (BS 907-927) · airframe 62,635 hrs · 21,257 cycles

AFT CARGO STRUCTURE UNDER LAV TANK IS CORRODED, BS 907 - 927 BETWEEN STRINGERS 23L AND 24L. INSTALLED A NEW INTERCOSTAL IAW DWG 147A7401, AND SRM 51-40-02.

Part: WINDOW FRAME — CRACKED (L1) · airframe 61,356 hrs · 20,892 cycles

DURING INSPECTION, FOUND THE L1 WINDOW POST TO BE CRACKED. REPAIRED IAW ECRA 5610-01409.

Part: SUPPORT FITTING — CORRODED (LT MLG TRUNNION) · airframe 61,356 hrs · 20,892 cycles

LEFT MLG FWD TRUNION SUPPORT ASSY ATTACH POINTS HAS CORROSION. REPLACED THE TRUNNION SUPPORT FITTING ASSY IAW SRM 51-40-02, 51-40-04, DWG 115A5002, AND ECRA 5720-02953

Part: BEAM — DAMAGED (VERTICAL STAB) · airframe 61,356 hrs · 20,892 cycles

LT TRAILING EDGE OF VERTICLE STAB AFT BEAM DAMAGED. REMOVED DAMAGED AREA AND INSTALLED A REPAIR DOUBLERS AND FILLER IAW ECRA 5330-01859.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,356 hrs · 20,892 cycles

PRESSURE BULKHEAD WEB CRACKED BS 663, LBL 40 TO 45.64, WL 192 AND 200.6. REPAIRED THE BULKHEAD WEB.

Part: BULKHEAD WEB — CRACKED (BS 663) · airframe 61,356 hrs · 20,892 cycles

PRESSURE BULKHEAD WEB CRACKED BS 663, RBL 31.83 TO RBL 40 BETWEEN WL 192.0 AND WL 200.6 . REPAIRED THE BULKHEAD WEB IAW SRM 57-10-10, REPAIR 3, ALT 1.

Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 60,924 hrs · 20,759 cycles

RT OVERWING EMERGENCY LIGHT DOES NOT COME. PRESSURE NORMAL, FOUND WIRE W5158-0006-200 DAMAGED APPROX 4IN BEHIND CONNECTOR D40702P. REPAIRED THE WIRE IAW SWPM 20-10-13. OPS CHECKED IAW FIM 52-20-00. NO DEFECTS.

Part: PSEU — FAULTY (E&E BAY) · airframe 60,638 hrs · 20,672 cycles

EMERGENCY SLIDE/OVERWING LIGHT DOES NOT GO OFF. R&R PSEU PER AMM 32-09-10-401-801 AND R&R RELAY R743 AND R738 IN JUNCTION BOX 24 PER WDM 52-71-14.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 60,242 hrs · 20,553 cycles

EXTERIOR RT NR 3 EMERGENCY LIGHT INOPERATIVE . REPLACED THE BATTERY PACK AND CHARGER IAW AMM 33-51-06. CHECKED NORMAL.

Part: LIGHT — DETACHED (SEAT 24C) · airframe 60,147 hrs · 20,527 cycles

ROW 24C OVERHEAD EMERGENCY LIGHTING WAS INOPERATIVE. FOUND THE EMERGENCY LIGHT ASSY DETACHED FROM BASE. R & R IAW AMM 33-51-03-960-802. OPS CHECKED GOOD.

Part: WIRE — UNSECURE (EMERGENCY LIGHT) · airframe 60,147 hrs · 20,527 cycles

EMERGENCY EXIT LIGHTS AT ROWS 22 - 28 INOPERATIVE. SECURED WIRE UNDER SEAT 22A, OPS CHECKED OK IAW AMM 33-51-00.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,566 hrs · 20,350 cycles

EMERGENCY LIGHTS, SEAT ROW 22-28ABC AISLE LIGHTS INOP. CHARGED EMERGENCY LIGHTS, ALL CHK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 56,835 hrs · 19,464 cycles

EMERGENCY EXIT AISLE LIGHTS INOPERATIVE, ROWS 22 ABC - 28 ABC. R & R M1670 BATTERY PACK & POWER SUPPLY IAW MM 33-51-06. OPERATIONS CHECKED GOOD. OK FOR SERVICE.

Part: BEAM — CRACKED (R1 DOOR) · airframe 56,636 hrs · 19,400 cycles

R1 DOOR BEAM CRACKED ON HORIZONTAL, BETWEEN VERTICAL FLANGE RADIUS & TORQUE BOX LOWER FWD INBD ATTACH BOLT, VIEWED WITH DOOR CLOSED. INSTALLED NEW BEAM PN 141A6536U-20 IAW DWG 141A6535 & SRM 51-40-02.

Part: SKIN — CRACKED (FUSELAGE) · airframe 56,636 hrs · 19,400 cycles

WHILE ACCOMPLISHING EA 5310-05878 OP 1, THE 2ND SET OF HOLES, FWD & AFT, FROM THE TOP, BOTH HAVE CRACK INDICATIONS IN THE SKIN. STATION LOCATION 540, BETWEEN STRINGERS 22R & 23R. REPAIRED FUSELAGE SKIN AT STATION 540, BETWEEN STRINGER 22R & 23R IAW EA 5310-05878 REV C OP 5.

Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 56,636 hrs · 19,400 cycles

MAIN CABIN SEAT TRACK FLANGE HAS A CRACK INDICATION LOCATED AT STATION 727B-2 & RBL-26.25 FASTENER HOLE. CUT OUT DAMAGE, FABRICATED REPAIR PARTS & INSTALLED IAW ECRA 5320-02654.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,636 hrs · 19,400 cycles

RIGHT HORIZONTAL STAB STATION 101.90, INBD SIDE OF RIB, NR 2 VERTICAL STIFFENER CRACKED APPROX 1" UP FROM LOWER SKIN STEP 2 A. INSTALLED T ANGLE DOUBLER REPAIR IAW ECRA 5510-02596.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,636 hrs · 19,400 cycles

RIGHT HORIZONTAL STAB STATION 101.90, INBD SIDE OF RIB, NR 4 VERTICAL STIFFENER CRACKED, APPROX 1" UP FROM LOWER SKIN, STEP 2 A. INSTALLED T ANGLE DOUBLER REPAIR IAW ECRA 5510-02596.

Part: STIFFENER — CRACKED (RT HORIZ STAB) · airframe 56,636 hrs · 19,400 cycles

RIGHT HORIZONTAL STAB STATION 101.90, INBD SIDE OF RIB, NR 3 VERTICAL STIFFENER CRACKED, APPROX 1" UP FROM LOWER SKIN, STEP 2 A. INSTALLED T ANGLE DOUBLER REPAIR IAW ECRA 5510-02596.

Part: SKIN — DENTED (FUSELAGE) · airframe 56,636 hrs · 19,400 cycles

DENT AT STATION 270, 1" BELOW STRINGER -18R, RIVET LINE IS OUT OF LIMITS IAW SRM 53-00-01. ALLOWABLE DAMAGE 1 PAR 3 B 3 DETAIL G. CHEM-MILL STEP IS WITHIN DENT RESIDUAL PERIMETER. REPAIRED DENT IAW SRM 53-00-01 REPAIR 3.

Part: OVERHEAT LOOP — DEFECTIVE (NR 1 ENGINE) · airframe 56,394 hrs · 19,288 cycles

DURING TAXI OUT NR 1 ENG START, THE OVERHEAT DETECTOR ANNUNCIATOR LIGHT CAME ON. SHORTLY AFTER THE NR 1 ENG FIRE SWITCH LIGHT ALSO ILLUMINATED, NO BELL. ENG WAS SHUT DOWN, QRH FOLLOWED. BOTH FIRE BOTTLES USED. FOUND HIGH RESISTANCE LOOP M1759, REPLACED SAME. R & R AFT ENG FIRE BOTTLE IAW AMM 26-21-01-400-801.

Part: SKIN — DAMAGED (L1 DOOR) · airframe 55,783 hrs · 19,017 cycles

DOOR SKIN DAMAGE AT LOWER HINGE CUT OUT V DIMENSION 1 1/2 INCH BY 1/8 DEEP. REPAIRED IAW ECRA 5210-02652 PART 1. INTERIM REPAIR STEPS 1 - 9. REF FORM 44.0008 FOR PARTIAL WORK ACCOMPLISHED. DIP CLOSED. INSPECT L1 DOOR SKIN DAMAGE WITHIN 5 CYCLES. DOCUMENT ALL DAMAGE FOUND & PROPERLY DISPOSITION IAW SRM & GMM 06-35-05.

Part: HMU — UNSERVICEABLE (NR 2 ENGINE) · airframe 54,183 hrs · 18,413 cycles

NUMBER 2 ENG SURGE, CRUISE FL 220, ENGS WERE RUNNING AROUND 74% N1 NR 2 ENG SURGED UNCONTROLLED AT 20 TO 305 TO 40%. BROUGHT NR 2 ENG BACK UNDER 60% & STABILIZED. STAYED UNDER 60% UNTIL LANDING, RT ENG CONTROL LIGHT ILLUMINATED ON GND. TROUBLE SHOT IAW FIM TASK 71-05-00-810-805-F00. RUN NR 2 ENG, FOUND NO FAULTS. OPERATIONS CHECKED NORMAL. LP 9127188 PRECAUTION. R & R NR 2 HMU IAW 73-21-10. OPERATIONS & LEAK CHECKED GOOD.

Part: FLOORBEAM — CORRODED (BS 344) · airframe 48,944 hrs · 16,414 cycles

CABIN FWD WET AREA, CORROSION AT FLOORBEAM AT BS 344, BETWEEN LBL 18 TO RBL 18. REPAIRED IAW ECRA 5310-05738 AND SRM 53-10-51, REPAIR 9.

Part: FLOORBEAM — CORRODED (BS 947) · airframe 48,944 hrs · 16,414 cycles

PASSENGER COMPARTMENT AFT WET AREA, HEAVY CORROSION AT FLOORBEAM BS 947 LBL 53. FABRICATED REPAIR PARTS AND INSTALLED FLOORBEAM BS 947, IAW SRM 53-40-51, REPAIR 5.

Part: ANGLE — CORRODED (BS 927-990) · airframe 48,944 hrs · 16,414 cycles

PASSENGER COMPARTMENT AFT WET AREA, HEAVY CORROSION AT L2 DOOR ZEE ANGLE BETWEEN BS 927 - 990 AT SEVERAL LOCATIONS. R & R ZEE ANGLE IAW SRM 51-40-02 AND DWG 147A8501.

Part: FRAME — CRACKED (BS 867) · airframe 48,944 hrs · 16,414 cycles

CABIN FRAME CRACKED AT BS 867, BETWEEN S8-9R AROUND RIVET AT AIR CONDITIONING SUPPORT BRACKET. INSTALLED INTERIM REPAIR IAW ECRA 5310-05743.

Part: FRAME — CRACKED (BS 827) · airframe 48,944 hrs · 16,414 cycles

CABIN FRAME CRACKED, BS 827, BETWEEN S8-9R AROUND INBD RIVET AT AIR CONDITIONING OUTLET SUPPORT BRACKET. INSTALLED REPAIR IAW ECRA 5310-057 41.

Part: FRAME — CRACKED (BS 827) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 827 AT LT AIR CONDITIONING RAIL BRACKET. INSTALLED REPAIR IAW EA 5310-04716, REV D, OP 01 AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 400) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED BS 400. REPAIRED CRACKED FRAME IAW EA 5310-04716, REV E OP1 AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 787 S8-9R) · airframe 48,944 hrs · 16,414 cycles

FRAME CRACKED BETWEEN STRINGER 8 & 9R BS 787. REPAIRED FRAME IAW EA 5310-04716, REV E OP1 AND ECRA 5310-05728.

Part: SKIN — DAMAGED (BS 280) · airframe 48,944 hrs · 16,414 cycles

BS 280, CROWN SKIN HAS A HOLE BETWEEN S2-3L. REPAIR INSTALLED IAW SRM 53-00-01 REPAIR 6.

Part: FRAME — CRACKED (BS 500A) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED BS 500A. REPAIRED FRAME IAW EA 5310-04716, REV E OP1 AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 727 S8-9R) · airframe 48,944 hrs · 16,414 cycles

FRAME CRACKED BETWEEN STRINGER 8 & 9R BS 727D. REPAIRED FRAME IAW EA 5310-04716 REV E OP1 AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 480) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED BS 480. REPAIRED FRAME IAW EA 5310-04716, REV E, OP1 AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 787) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 787 AT AIR CONDITIONING BRACKET. FRAME REPAIRED IAW EA 5310-04716, REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 480) · airframe 48,944 hrs · 16,414 cycles

CABIN FRAME CRACKED BETWEEN STRINGERS 8 & 9R BS 480, AROUND INBD RIVET AT AIR CONDITIONING OUTLET SUPPORT BRACKET. FRAME REPAIRED IAW EA 5310-04716, REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 727B) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 727B AT AIR CONDITIONING BRACKET. REPAIRED FRAME IAW EA 5310-04716 REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 727D) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 727D, LT AIR CONDITIONING BRACKET. FRAME WAS REPAIRED AS REF EA 5310-04716 REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 747) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT BS 747, LEFT AT AIR CONDITIONING BRACKET. FRAME WAS REPAIRED AS REF EA 5310-04716, REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 400) · airframe 48,944 hrs · 16,414 cycles

CABIN FRAME CRACKED BETWEEN STRINGER 8 & 9R BS 400, AROUND INBD RIVET AT AIR CONDITIONING OUTLET SUPPORT BRACKET. FRAME REPAIRED IAW EA 5310-04716, REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 500A) · airframe 48,944 hrs · 16,414 cycles

FRAME CRACKED BETWEEN STRINGER 8 AND 9R BS 500A, AROUND INBD RIVET AT AIR CONDITIONING OUTLET SUPPORT BRACKET. FRAME WAS REPAIRED IAW EA 5310-04716 REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 867) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 867 AT AIR CONDITIONING BRACKET. FRAME WAS REPAIRED AS REF EA 5310-04716, REV E AND ECRA 5310-05728.

Part: FRAME — CRACKED (BS 727B) · airframe 48,944 hrs · 16,414 cycles

FRAME FOUND CRACKED AT INBD RIVET BS 727B AT AIR CONDITIONING BRACKET. REPAIRED FRAMEIAW EA 5310-04716, REV E AND ECRA 5310-05728.

Part: CHARGER — INOPERATIVE (CABIN) · airframe 37,103 hrs · 12,139 cycles

LEFT OVERWING EMERGENCY LIGHT NOT WORKING. REMOVED AND REPLACED EMERGENCY LIGHT POWER SUPPLY (CHARGER) AT SEAT 10A IAW AMM 33-51-06, OPS CHECK GOOD.

Part: STRUCTURE — WORN (CENTER WING) · airframe 33,414 hrs · 10,800 cycles

WING CENTER SECTION RIGHT-HAND LOWER CHORD AT STATION 530 40RBL HAS A HOLE. REPAIR COMPLETED PER ECRA 5351-01064 ON WING TO BODY FAIRING SUPPORT RBL 40.1 LOWER CHORD REPAIR.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

MAIN DECK FLOOR SUPPORT WEB UPPER ANGLE CRACKED BODY STATION 380 TO 400 BL 0. REMOVED AND REPLACED UPPER L-ANGLE REF SRM 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

MAIN DECK FLOOR SUPPORT CRACKED AT STATION 312 TO 328 RBL 28. REMOVED AND REPLACED FLOOR SUPPORT AT BODY STATION 312 TO 328 RBL 28 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01.

Part: ANGLE — CORRODED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

L2 DOOR Z-ANGLE HAS LITE CORROSION ENTIRE LENGTH OF DOOR CUTOUT. REMOVED AND REPLACED Z-ANGLE REF SRM 53-70-15 AND 51-40-02.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

MAIN DECK FLOOR SUPPORT CRACKED AT STATION 344 TO 360 BL 0. REMOVED AND REPLACED FLOOR SUPPORT AT BODY STATION 344-360 BL 0 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01.

Part: FLOOR SUPPORT — CRACKED (CABIN) · airframe 33,414 hrs · 10,800 cycles

MAIN DECK FLOOR SUPPORT CRACKED STATION 277 TO 294.5 RBL 1. REMOVED AND REPLACED FLOOR SUPPORT BODY STATION 277 TO 294.5 RBL1 REF SRM 51-40-02, APPLIED CIC REF SRM 51-20-01.

Part: FRAME — CRACKED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

FRAME STATION 440 RIGHT CRACKED AT S-9R. INSTALLED REPAIR ON FRAME AT STATION 440 S9R PER ECRA 5311-01410.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 33,414 hrs · 10,800 cycles

CRACK IN MAIN DECK FLOOR SUPPORT STATION 328 TO 344 LBL 42. REMOVED AND REPLACED FLOOR SUPPORT STATION 328 TO 344 LBL 42 REF 51-10-02.

Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 25,481 hrs · 8,149 cycles

R2 EXIT DOOR EMERGENCY LIGHT DOES NOT COME ON. RELAMPED LIGHT BULB TWICE. OPS CHECK OK. PER AMM 33-51-00.

Part: WEB — CRACKED (FUSELAGE) · airframe 19,048 hrs · 6,078 cycles

INSPECTION FOUND A 4 INCH CRACK IN RIGHT MLG SKI JUMP O/B WEB. THE WEB WAS REPLACED IAW SRM 51-40-02.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 4,934 hrs · 1,602 cycles

SMOKE WITH A PETROLEUM SMELL ENTERED THE COCKPIT UPON ROTATION LEAVING EWR. A RETURN TO EWR WAS BEGUN AND THE SMOKE CEASED AFTER FIVE MINUTES WITH NO FURTHER PROBLEMS NOTED. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. THE #1 ENGINE WAS REMOVED AND REPLACED. THE SDR WILL REMAIN OPEN FOR PART INFORMATION PENDING INVESTIGATION. **S/P** INVESTIGATION DETERMINED THAT THE SMOKE AND ODOR WERE THE RESULT OF LUBRICANTS USED IN ACCOMPLISHMENT OF ENGINE TOP CASE PRIOR TO THIS FLIGHT(ENGINE HAD JUST BEEN INSTALLED). ECRA 7100-01296 WAS RELEASED AS A RESULT TO SCREEN FOR VIBRATION, SMOKE, AND FUMES FOLLOWING TOP CASE/INSTALLATION. BOEING IS IN THE PROCESS OF REVISING ENGINE INSTALLATION TEST REQUIREMENTS. GE-ON-WING SUPPOR