N24202
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| UNITED AIRLINES INC | Operator | 2016-12-13 – 2016-12-13 | Operator named in NTSB report |
| UNITED AIRLINES, INC. (CALA) | Operator | 2016-12-13 – 2016-12-13 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
1R GIRT BAR BRACKET IS LOOSE ADJUSTED THE GIRT BAR RETAINER CLIP ON DOOR 1R,AND VERIFIED THE GIRT BAR STAYS INSIDE THE RETAINER CLIP IN REF TO AMM 25-66-01.
SEAT 20F EXIT ROW DOOR LOWER SAFTEY STAP COVER WILL NOT STAY ATTACHED HOOK AND LOOP DAMAGED. INSPECTED HOOK AND LOOP ON EXIT ROW 20F DOOR COVER. NO DAMEGE TO HOOK AND LOOP NOTED. SECURED LOWER SAFTEY STRAP IAW AMM 52-22-51-400-801. OKAY FOR SERVICE.
BIRD STRIKE ON WINDSHIELD, CLEANED BIRD RESIDUE AND INSPECTED WINDSHIELD AND SURROUNDING STRUCTURE, NO EXTERNAL DAMAGE FOUND. EXTENDED AIRCRAFT FLAPS/SLATS AND EXAMINED THE REST OF THE FUSELAGE AS WELL AS THE ENGINES. NO EVIDENCE OF OTHER BIRD STRIKES OR OBVIOUS DAMAGE FOUND. REF. AMM 05-51-18
29C EMERG PATH LGT BROKEN. LIGHT WORKS OK. MAINTENANCE REQUESTS RELIEF UNDER MEL 3319E. APPROVED PLACED 29C EMERGENCY LIGHT ON MEL 3319E. APPLIED PLACARD. R & R LENS COVER 29C PATH LIGHTING OPS CKS OK AT THIS TIME
RIGHT OVERWING EXIT DOOR HANDLE COVER PANEL KEEPS FALLING OFF. REPOSITION OVERWING ESCAPE DOOR STRAP COVER ONTO HOOK AND LOOP. COVER STAYS SECURE.
OIL FILTER BYPASS 3 OCCASIONS ABLE TO GET LIGHT TO EXTINGUISHDURING CLIMB TO 15K OIL DIFFERENTIAL LIGHT ILLUMINATED PROMPTING LEVEL OFF OUR SECOND CLIENT FOR 25,000 FT. THE LIGHT CAME ON AGAIN DURING THE SET TO 8000 FT. IT ILLUMINATED THE THIRD TIME RUSTLE POSITIONS WERE APPROXIMATELY 75% 64% & 33% RESPECTIVE ALTITUDE. THRUST POSITION ENG 1 FMC CDU EEC BITE CHECK PRODUCED NO FAULTS. INPUT MONITORING DISPLAY SHOWS NO FILTER BYPASS, INITIAL WRITE UP WAS FOR ENGINE ONE OIL FILTER BYPASS LIGHT ILLUMINATED. PERFORMED FMC CDU BITE CHECK FOR ENG2, NO RECENT FAULTS AND NO BYPASS ON OIL FILTER. AMM 73-21-00/501. PER TOMC REQUEST ATTEMPTED REPLACEMENT OF SCAVENGER OIL FILTER, UNABLE TO REMOVE BOWL. PERFORMED SCAVENGE OIL FILTER ASSEMBLY REMOVAL UP TO STEP 1A REF AMM 79-21-04-000-801-F00 . REMOVED ENGINE 1 OIL SCAVANGE FILTER BOWL & INSPECTED FILTER, FOUND NO DEBRIS REF AMM TASK 79-21-06-000-801-F00, INSPECTED OIL CLOGGING INDICATOR IAW AMM TASK 79-21-10-000-801-F00. NOT CLOGGED AND NOT POPPED. FILTER BOWL FOR SCAVANGE FILTER CROSS THREADED . R & R SCAVENGE OIL FILTER ASSY AND FILTER REF AMM 79-21-04 UP TO STEP 3 I. POWER PLANT TEST 3A IDLE LEAK CHECK & TEST 7. ACCOMPLISHED EEC BITE TEST, NO FAULTS FOUND. PERFORMED SCAVENGE OIL FILTER ASSY IDLE LEAK CHECK, LEAK CHECK GOOD.
FOUND RH SLIDE OVERWING LIGHT INOP PERFORMED RAR OF RH SLIDE OVERWING LIGHT IAW AMM 33-51-04 . OPC GOOD.
-A- SYSTEM HYD EMDP ELEC CONNECTOR DAMAGED. ON INSP, FOUND HYD PUMP A CONNECTOR (D2664) DAMAGED. REMOVED CONNECTOR D2664 & CLEANED WIRES & CONTACTS, INSPD ALL CONTACTS & FOUND CONTACTS TO BE GOOD. STARTED INSTALL OF CONNECTOR & ABLE TO GET 18AWG WIRES TERMINATED, COULD NOT COMPLETE TERMINATION OF 10AWG WIRES DUE NO WIRE NRS READABLE ON WIRES. SUGGEST REPLACING ALL CONTACTS ON CONNECTOR D2664. SPECIAL 1210 CONTACTS P204541. REF SWPM 20-60-02, 20-60-03, & 20-61-11. REMOVED ALL OLD CONTACTS & TERMINATED ALL WIRES WITH NEW CONTACTS. INSTALLED IN CONNECTOR D2664 IAW WDM 29-11-12-1 & VERIFED CONTINUITY BACK TO R317 IN P92 PANEL. SECURED HARNESS & BACKSHELL & CONNECTED HYD PUMP IAW SWPM 20-61-11, WDM 29-34-11.
B SIDE HYD OVHT LIGHT ILLUMINATED. FOUND ELEC HYD PUMP B CONNECTOR (D2666) DAMAGED. REMOVED ALL OLD CONTACTS AND RETERMINATED ALL WIRES WITH NEW CONTACTS AND INSTALLED IN CONNECTOR D2666 IAW WDM 29-11-12-1 & VERIFYING CONTINUITY BACK TO R318 IN THE P91 PANEL. SECURED HARNESS & BACKSHELL & CONNECTED TO ELEC HYD SYS B PUMP. REF SWPM 20-61-11, WDM 29-34-11. OPS CHECKS TO BE COMPLETED ON LP 6213343.
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK. ONE RED EMERGENCY LIGHT INOPERATIVE AT 20C. REPLACED LIGHT ASSY, GROUND OPS NORMAL.
ON T/O ROLL, SMOKE WITH BURNING ODOR CAME FROM CA SIDE AIR VENTS. R EJ T/O AND SMOKE DISSIPATED CREW ADVISED LOW SPEED ABORT LESS THAN 20 KTS. PER FODM CAPTAIN REPORTED RTO BETWEEN 100 AND 110 KTS. PERFORMED SMOKE CABIN/FLIGHT DECK CONDITIONAL INSPECTION. REF AMM 05-51-26-800-801-C1. NO EVIDENT SMOKE IN CABIN OR FLIGHT DECK AFTER 20 MINUTE ENGINE RUN (BOTH 70% AND IDLE). PERFORMED HIGH ENERGY STOP INSPECTION FOR REJECTED TAKE OFF. NO DAMAGE NOTED. REF AMM 05-51-07-210-801. AC OK TO CONTINUE.
PER ECRA 5725-01156 PART 1, STEP 3 - AFTER MAY 18, 2026, BUT BEFORE JUNE 18, 2026, PLANNING TO CONTACT ENGINEERING FOR THE INSPECTION REQUIREMENTS OF THE INTERIM REPAIR INSTALLED ON THE RIGHT WING OUTBOARD LOWER SKIN PANEL BETWEEN WSTA 564.5 & 591.5 AT STR L-9 ON AIRCRAFT N24202 IN ACCORDANCE WITH PART 2 OF THE LATEST REVISION OF ECRA 5725-01156. CARRY DIP PER ECRA 5725-01156. REF LP 3086790 AND 3947094.
CENTER WING REAR SPAR L/H VAPOR BARRIER HAS 10" CRACKED O/B OF HYD A SYSTEM RETURN FILTER. APPLIED REPAIR PATCH ON L/H VAPOR BARRIER O/B HYD A SYSTEM RETURN FILTER AT CENTER WING REAR ESFR:1038460 SPAR. CRACK LENGTH 10" AS PER B737-800 SRM 57-10-10-2R-2.
NRO.2 EG INBOARD PYLON ATTACH WING LANDIENG EDGE FILLET PANEL HAS DEEP GOUGE REF ARR N/R 9934107 REMOVED AND REPLACED SKIN CLOSEOUT 611A AT R/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. WORK ACCOMPLISHED BY V918489 REMOVED AND REPLACED SKIN CLOSEOUT 611A AT R/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. WORK ACCOMPLISHED BY V918489
R/W FLAP SUPPORT FAIRING #6 AFT BULKHEAD FITTING GOUGED. REF AAR N/R 9933952 REMOVED AND REPLACED FITTING AT FLAP FAIRING. # 6 REF B 737-800 SRM 51-40-02-0G-0, DWN 113A9350. WORK ACCOMPLISHED BY V903523. ESFR NO.1038497. SIGNED U057326.
L/W L/E I/B OF PYLON SKIN GOUGED REF AAR N/R 9934263 REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B73 37-800 SRM 51-40-02-0G-0 AND DWG# 116A4008. REMOVED AND REPLACED SKIN AT L/W L/E INBOARD OF PYLON AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 116A4008.
LOWER WING CENTER SECTION PNEUMATIC SERVICE PORT ACCESS DOOR 192DR EDGES FWD DEEP GOUGES MKD DOT 148 (REF AAR N/R 9934287) REMOVED AND REPLACED LOWER WING CENTER SECTION PNEUMATIC SERVICE ACCESS DOOR 192DR PER SRM 51-40-02-0G-0.
FLIGHT DECK FLOOR SKIN PANEL DENTS AT LBL 11 STA 259 AND STA 277 REF AAR N/R 9933688 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBL 11 STA 259 - STA 277 AS PER SRM 53-10-51-2R-2. WORK ACCOMPLISHED BY V928495 ACCOMPLISHED FLIGHT DECK FLOOR WEB REPAIR AT LBL 11 STA 259 - STA 277 AS PER SRM 53-10-51-2R-2. WORK ACCOMPLISHED BY V936393 REF ESFR:1038366
LOWER FUS. CENTER WING REAR SPAR STIFFENER LOWER RADIUS CRACKED AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST REF AAR N/R 9933669 REMOVED AND REPLACED LOWER FUS. CENTER WING REAR SPAR STIFFENER AT LBL 25 STA 663.75 O/B OF L/H RAM AIR EXIT EXHAUST AS PER SRM 51-40-02-0G-0, DWG#111A1000, AND DWG#149A7210. REMOVED AND REPLACED LOWER FUS. CENTER WING REAR SPAR STIFFENER @ LBL 25 STA 663.75 O/B OF L/H RAM ESFR:1038468 AIR EXIT EXHAUST AS PER SRM 51-40-02-0G-0, DWG#111A1000, AND DWG#149A7210.
LOWER FUS. ATTACH ANGLE WORN O/B OF L/H RAM AIR EXIT EXHAUST MKD DOT 031. (REF AAR N/R 9933670)
AFT CARGO DOOR EXT SKIN HAS SEVERAL DENTS. (REF AAR N/R 9933841)
FWD CARGO DOOR EXT SKIN HAS SEVERAL DENTS. (REF AAR N/R 9933840)
R/H VAPOR BARRIER I/B UPPER ATTACHED ANGLE CRACKED @ RBL 7 STA R/H VAPOR BARRIER I/B UPPER ATTACHED ANGLE CRACKED @ RBL 7 STA REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ANGLE AT STA 663.75 663.75 PER SRM 51-40-02-0G-0 AND DWG#111A1000 REF AAR N/R 9933665. REMOVED AND REPLACED RH VAPOR BARRIER UPPER ATTACH ESFR:1038464 ANGLE AT STA 663.75 PER SRM 51-40-02-0G-0 AND DWG#111A1000.
AS PER T/C 29-5241-2706 FWD R1 DOOR STRAP HAS CRACK ON UPPER AREA REF AAR N/R 9933925 REMOVED AND REPLACED DEPPRESOR(DOOR STRP) AT R1 DOOR AREA AS PER REF B737 SRM 51-40-02=0G-0 AND DWG # 141A8370.
AFT CABIN WET AREA FLOOR SUPPORT BEAM UPPER CAP CORR. LBL 29 TO RBL 33 STA 986.5 MKS DOT 089 REF AAR N/R 9933829
CRACK FOUND AT LOWER FUSELAGE CENTER WING BOX REAR SPAR STA 663 VERTICAL PRESSURE WEB DECK BETWEEN LBL40- LBL 31.83 (CRACK LENGTH 1") REF AAR N/R 9933560
AFT CABIN WET AREA FLOOR SUPPORT INNER CHORD L-2 DOOR LOWER SILL FOUND CORRODED FROM STA 951 TO STA 992.8 MKD DOT 087 REF AAR N/R 9933826
FWD CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CRACKED AT FASTENER HOLE LBL 30 BETWEEN STA 312 AND 328. REMOVED AND REPLACED INTERCOASTAL AT FWD CABIN WET AREA FLOOR SUPPORT LBL 30 BETWEEN STA 312 AND 328 ESFR:1038461 PER REF SRM 51-40-02-0G-0 AND DWG# 141A5400, INSTALLED AND REMOVED EWIS PROTECTION.
FWD CABIN WET AREA FLOOR SUPPORTNINNER CHORD APPEARS CRACK REF AAR N/R 9933798
AFT CABIN WET AREA FLOORBEAM UPPER CAP CORRODED FROM LBL 4 TO RBL 50 STA 947.75.
FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT RBL 13 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT ESFR:1038462 INTERCOSTAL AT RBL 13 BETWEEN STA 380 & 400 AS PER REF B737 SRM 51-40-02-0G-0 & DWG # 143A5400.
FWD CABIN FLOOR SUPPORT INTERCOSTAL CRACKED AT LBL 15 BETWEEN STA 380 AND 400. REMOVED AND REPLACED FWD CABIN FLOOR SUPPORT ESFR:1038463 INTERCOSTAL AT LBL 15 BETWEEN STA 380 & 400 AS PER REF B737 SRM 51-40-02-0G-0 & DWG # 143A5400.
AFT CABIN WET AREA FLOOR SUPPORT INTERCOSTAL CORR. AT FASTENERS HOLES LBL 50 BETWEEN STA 947.75 AND 967. REMOVED AND REPLACED INTERCOSTAL FROM STA 947.5 TO STA 967 AT LBL 50.68 AS PER B737-800 SRM 51-40-02-0G-0 AND DWG# 147A5650.
ACCOMPLISH A PERMANENT REPAIR ON THE RH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 PRIOR TO 02 JULY 2026 SKIN AROUND THE OUTBOARD FASTENER OF STRINGER R-9 BETWEEN WS 564.5 AND WS 591.5 REF NR 002323616 FOUND A CRACK THAT PROPAGATES 0.8" FWD OF THE FASTENER HOLE, AND 1.1" AFT OF THE FASTENER HOLE OF LOWER WING TOMC APPROVES DIP ACCOMPLISH A PERMANENT REPAIR ON THE RH WING TOMC-APPROVAL FROM SC1ELBYC COMMENT LOWER SKIN BETWEEN WSTA 564 AND WSTA 591 PRIOR TO 02 JULY 2026 PER ECRA 5725-01153 APPROVED APPROVED INSPECTIONS CREATED BY AUTODIP PENDING AIRCRAFT RECORDS REVIEW.
PERFORMED INTERIM REPAIR TO LH WING OUTBD LOWER SKIN PANEL CRACK BETWEEN WSTA 564.5 - 591.5 AT S-9L REFER TO EC/RA 5725-01152. REQUIREMENTS PER PART 2 OF EC/RA 5725-01152 ON OR BEFORE 25 MAY 2026. DIP TO BE INITIATED A DTA DIP TO STATE: ON THE LH WING LOWER SKIN BETWEEN WSTA 564 AND WSTA 591, ACCOMPLISH INSPECTION TOMCQC REV PERFORMED NOT RII PER GMM 09-25-05
REF.EA5310-04554 OP002-TYPICAL CRACK FOUND ON RT #1 WINDOW FRAME UPPER AFT CORNER. ACCOMPLISHED RH #1 WINDOW FRAME PERMANENT REPAIR / PREVENTIVE / TRIPLER AS A PERMANENT REPAIR . MODIFICATION IAW EA#5310-04554 REV."C"OP-004,WHICH REQUIRES TO REF. AAR N/R:9910117 REMOVE THE #1 WINDOW ASSY,PERFORM H.F.E.C TO DETECT CRACKS, CUT THE WINDOW FRAME AND AND INSTALL REINFORCING DOUBLERS.
AFTER REMOVING L/H WINDSHIELD, FOUND OUTBOARD POST CRACKED. LOG LOCKED FOR FERRY FLIGHT UNLOCKING FOR ITEM TO BE WORKED ACCOMPLISHED L/H NO.1 WINDOW PERMANENT REPAIR / PREVENTATIVE PERMANENT REPAIR MODIFICATION AS PER EA 5310-04554 REV C. REMOVE THE NO.1 WINDOW ASSY PERFORMED HFEC TO DETECTS CRACKS CUT THE WINDOW FRAME AND INSTALL REINFORCING DOUBLER / TRIPLER AS A
PDA 1 REF. LP 7872896 #1 MLG TIRE HUB CAP AND BOLTS ARE MISSING AND DEPARTED THE AIRCRAFT. ADDED PICTURE
NO FLAP DEPLOYMENT ON APPROACH. NO LEADING EDGE FLAP TRANSIT LIGHT FLAP PRIMARY OR MOVEMENT OF FLAPS PER PROCEDURE 1. FIM POINTS TO WIRING/TRANSMITTER. RAN FLAPS IN PRIMARY AND ALTERNATE NO FLAP MOVEMENT. SLATS MOVED DURING ALTERNATE OPERATION. ALTERNATE FLAPS BRAKE AWAY WIRE BROKEN.PREFORMED BITE ON ON FSEU MX MSG 27-52259. FOLLOWED FIM TASK 27-51 TASK 813 REMOVED PLUG FROM INDICATOR AND RAN FLAPS NO TO ACCOMPLISHED TRANSMITTER INSTALLATION TEST, AND LAND VERIFY CHECK. PARTS USED: 29-2759-9-0004,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1892764 SN OFF 2894 FOUND FAULT TE FLAP SENSOR LEFT ON BITE CHECK. REF. FIM 27-51 RESECURED WIRE BUNDLE AND POSITIONED BUNDLE IN CLAMPS FOR TASK 813. REPLACED L/H FLAP TRANSMITTER REF. AMM 27-58-01. NO CLEARANCE WITH NO CHAFFING. SEE L/P 4430521 FOR WIRE REPAIR. HELP. UPON FURTHER TROUBLESHOOTING FOUND WIRE BUNDLE CHAFFED AT LEFT WING INBOARD GROUND SPOILER AFT OF OUTBOARD ACTUATOR. NEED TRANSMITTER, FL OFF 29-2759-9-0004 2894 ON 29-2759-9-0004 7255 PERFORMED FLAP POSITION SENSOR TESTS REF AMM. 27-58-01 WITH OPS CHECK GOOD. RESECURED BREAKAWAY WIRE ON ALTERNATE FLAPS SWITCH. RAN FLAPS WITH NO FAULTS FOUND. REF AMM. 27-58-01 SYSTEM REQUIRES CAT CHECK FLAGGED ITEM AS CAT.
RIGHT AFT OVERWING EXTERIOR EMERGENCY EXIT LIGHT INOP. RE-LAMPED OVERWING LIGHT REF MM 33-51-04. OPS CK OK. PARTS USED: 767,QTY :1
CREW REPORTS THE FLAPS DID NOT MOVE WHEN SELECTED. HAD TO USE ALTERNATE FLAPS FOR LANDING. REMOVED AND REPLACED L/H FLAP POSITION TRANSMITTER I.A.W. AMM 27-58-01-400-801. OPS CHECKS AND ALL ASSOCIATED TESTS C/W AND CHK GOOD. PERFORMED LAND VERIFY. TESTS PASSED.
LEFT FLAP NEEDLE IS BOUNCING INTERMITANTLY BETWEEN 6 OCLOCK AND 12 OCLOCK POSITION ON GAUGE PERFORMED BITE OF FSEU REF FIM 27-61 TASK 801 LAST FLT SHOWS OK FAULT 27-52259 AND 27-52261. PERFORMED FIM 27-61 TASK 813 AND ROTABLE PARTS CHANGE WAS INDICATED - TT # 1362298 SN OFF 0700 FIM 27-61 TASK 832 ACCORDING FOR RELATED MSG BOTH CK OK. REPLACED FLAP POSITION INDICATOR REF AMM 27-58-02 -400-801 CK ADD EMP:U030756 INDICATOR, POSI OFF 29-2758-9-0001 0700 ON 29-2758-9-0001 3243
SLIDE LIGHT AT R2 DOOR INOP. REMOVED AND INSTALLED NEW SERVICEABLE EMERGENCY BATTERY PACK. OPERATIONAL CHECKED GOOD.
AFT R/H OVERWING EXIT DOOR LIGHT INOP. REMOVED AND REPLACED LAMPS FOR AFT R/H OVERWING EXIT DOOR SIGN. OPERATIONAL TESTED GOOD.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00091. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 6.14 UAL INSPECTION U301243 08/10/2022. DATA WAS TRANSCRIBED FROM IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL NSA EMX N/R 00091, AND HANGER N/R 5867300, WORK ACCOMPLISHED SEE NSA EMX N/R 00091 AND HANGER N/R 5867300 FOR WORK BY V905004, INSPECTED BY V895832. ACCOMPLISHED CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 111A200 REV ORIGINAL SEE 00099, AND HANGER N/R 5867307, WORK ACCOMPLISHED BY V905004, NSA EMX N/R 00099 AND HANGER N/R 5867307 FOR WORK ACCOMPLISHED INSPECTED BY V895832. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 32.40 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 111A200 REV ORIGINAL SEE 00099, AND HANGER N/R 5867307, WORK ACCOMPLISHED BY V905004, NSA EMX N/R 00099 AND HANGER N/R 5867307 FOR WORK ACCOMPLISHED INSPECTED BY V895832. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00100. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 40.87 U301243, 08/09/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R 00100 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE , AND HANGER N/R 5867308, WORK ACCOMPLISHED BY V905004, NSA EMX N/R 00100 AND HANGER N/R 5867308 FOR WORK ACCOMPLISHED INSPECTED BY V912634. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00101. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL ENTERED BY UAL INSPECTION U301243, 08/09/2022. DATA WAS 54.60 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV TRANSCRIBED FROM NSA EMX N/R 00101, AND HANGER N/R 5867309, ORIGINAL SEE NSA EMX N/R 00101 AND HANGER N/R 5867309 FOR WORK ACCOMPLISHED BY V905004, INSPECTED BY V895832. WORK ACCOMPLISHED CIR C/W. SSFR REPORT, FORM 46-0024, COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00096. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL 6.14 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE 00096 AND HANGER N/R 5867305, WORK ACCOMPLISHED BY V905004, AND NSA EMX N/R 00096 AND HANGER N/R 5867305 FOR WORK ACCOMPLISHED INSPECTED BY V895832. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00093. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 32.40 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N/R 00093, AND HANGER N/R 5867302, WORK ACCOMPLISHED BY V905004 NSA EMX N/R 00093 AND HANGER N/R 5867302 FOR WORK ACCOMPLISHED AND INSPECTED BY V895832. CIR C/W. SSFR, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00094. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 40.87 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX N/R IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE 00094, AND HANGER N/R 5867303, WORK ACCOMPLISHED BY V905004, NSA EMX N/R 00094 AND HANGER N/R 5867303 FOR WORK ACCOMPLISHED INSPECTED BY V895832. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00092. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 15.04 UAL INSPECTION U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL FROM NSA EMX N/R 00092, AND HANGER N/R 5867301, WORK SEE NSA EMX N/R 00092 AND HANGER N/R 5867301 FOR WORK ACCOMPLISHED BY V905004, AND INSPECTED BY V895832. ACCOMPLISHED CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00097. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND RBL BY UAL INSPECTION U301243 08/09/2022. DATA WAS TRASCRIBED FROM 15.04 IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV NSA EMX N/R 00097, AND HANGER N/R 5867306, WORK ACCOMPLISHED BY ORIGINAL SEE NSA EMX N/R 00097 AND HANGER N/R 5867306 FOR V905004, INSPECTED BY V895832. WORK ACCOMPLISHED CIR C/W. SSFR REPORT, FORM 46-0024,ENTERED COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00095. REMOVED AND REPLACED SHEAR FITTING AT STATION 540 AND LBL 54.60 U301243, DATE 08/10/2022. DATA WAS TRANSCRIBED FROM NSA EMX IAW B737-800 SRM 51-40-02 AND BAC DWG 111A2000 REV ORIGINAL SEE N/R 00095, AND HANGER N/R 5867304, WORK ACCOMPLISHED BY V905004, NSA EMX N/R 00095 AND HANGER N/R 5867304 FOR WORK ACCOMPLISHED INSPECTED BY V895832. CIR C/W. SSFR REPORT, FORM 46-0024, ENTERED BY UAL INSPECTION COMPLETED INSPECTION
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00099.
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 32.40 IS CRACKED. SUPPORT TASK NSA EMX N/R 00093.
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00094.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00101.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 40.87 IS CRACKED. SUPPORT TASK NSA EMX N/R 00100.
B737-57-4-1262 SHEAR FITTING STA 540 AND LBL 54.60 IS CRACKED. SUPPORT TASK NSA EMX N/R 00095.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00097.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND RBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00096.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 15.04 IS CRACKED. SUPPORT TASK NSA EMX N/R 00092.
B737-57-4-1262 SHEAR FITTING AT STA 540 AND LBL 6.14 IS CRACKED. SUPPORT TASK NSA EMX N/R 00091.
RT WING BOX REAR SPAR VERTICAL PESSURE WEB SHOWS CRACK INDICATION WITH HFEC BETWEEN RBL 31.83 AND 40. REPAIRED REAR SPAR VERT. WEB REF SRM 57-10-10 REPAIR 3 ALT1.ISSU E DIP FOR INSP 56000 FLT CYL FROM INSTALLATION HFEC/LFEC AND INTERVAL 36000 FLT CYL.REF PARA 6 TABLE 203. DIP APPROVED REPAIRED REAR SPAR VERT. WEB REF SRM 57-10-10 REPAIR 3 ALT1. ISSUE DIP FOR INSP 56000 FLT CYL FROM INSTALLATION HFEC/LFEC AND INT ERVAL 36000 FLT CYL.REF PARA 6 TABLE 203 TOMC-APPROVAL FROM SC1ELBYC COMMENT VERIFIED REPAIRED REAR SPAR VERT. WEB REF SRM 57-10-10 REPAIR 3 AND SFR COMPLETED. QC REVIEWED RECORDS UPDATE.....TW QC REVIEWED INIT: 56,000 TAFC (INIT WILL TRIGGER O/C -2177 AND ITO TO RIR) RIR: 36,000 FC.....TW
ELEC TRIM FAILED IN FLT T/S PER FIM 27-41-00-810-804, REMOVED AND REPLACED THE STM PER S TEP F(D)2, OPS CHECK GOOD. ROTABLE PARTS CHANGE WAS INDICATED. TT 1310705 SN OFF 8240 MOTOR, STAB, HO OFF 29-2741-9-0011 8240 ON 29-2741-9-0011 3737.
DURING INSPECTION, FOUND ONE ELEVATOR TAB CONTROL MECHANISM BELLCRANK ASSEMBLY SPRING BROKEN AT ONE END AND WRAPPED AROUND SUPPORT BRACKET, FWD OF MAIN PIVOT POINT.
ROW 20 MISSING 2 RED EMERG PATH LIGHTING LENSES. INSTALLED RED LENSES.
LEFT ENGINE OIL 35-30 PERCENT AFTER 1HR OF FLIGHT /1 ENGINE. EMERGENCY DECLARED. R&R CENTER VENT TUBE O RINGS AND DAMPNER SEALS ON #1 ENG. REF AMM 72-55-00-941-802-F00 AND EA 7255-01044 REV C OP 1. LEAK CHECK GOOD.
THE R2 DOOR EXIT SIGN IS BROKEN. REMOVED AND REPLACED LIGHT ASSY
INTERIOR EMERGENCY LIGHTS ON OVERHEAD BIN BULLNOSE INOPERATIVE AT ROWS 25 AND 28. R & R THE BATTERY POWER SUPPLY M1671. OPS CHECKED GOOD IAW AMM 33-51-06-960-806
RIGHT SIDE AFT OF WING LOWER BODY EMERGENCY LIGHT OUT/INOP REPLACED FUSES AND BATTERY PACK M1670 PER AMM 33-51-06. OPERATIONAL CHECK GOOD.
2 SEGMENTS OF EMERGENCY LIGHTS OUT. R&R BATTERY IN AFT GALLEY AND UNDER 8TH WINDOW FROM EMERGENCY EXIT. OP CHECK GOOD. REF AMM 33-51-06.
EMERGENCY LIGHTS ON LEFT SIDE ROW 21 INOP. R&R POWER SUPPLY IAW AMM33-51-06-960-806. OPS CK OK.
ASSOCIATED EMER LIGHTS FOR BATTERIES PACK M01675 FWD LT, M01674 FWD RT & M01694 OVERWING LT, ARE INOPERATIVE. R & R BATTERY PACKS AT M01675, M01674 & M01694. PERFORMED OPERATIONS CHECK, FOUND NORMAL IAW AMM 33-51-06.
PASSENGERS REPORTED FLUID POURING OUT OF RT WING IN ADDITION TO FLUID REPORTED FLOWING FROM LT WING ON TAKEOFF. FOUND SLIGHT SEEPAGE COMING FROM BOTH WING SURGE TANK ACCESS PANELS. RETORQUED BOTH PANELS IAW AMM 28-11-11. CHECKED FLOAT SWITCHES & SOVS IN ALL 3 FUEL TANKS BY TRANSFERRING & PRESS FUELING IAW FIM 28-21-00. SUMPED BOTH SURGE TANKS BEFORE & AFTER FUELING, FOUND NO FUEL. NO LEAKS NOTED, CANNOT DUPLICATE DISCREPANCY.
SUPPORT TASK FOUND CRACK INDICATION IN HOLE NR 1 OF FIG 001S2 AT SEAT TRACK LBL 24.75 AT STATION 727B. REPAIRED IAW ECRA 5320-02239. ALL PARTIAL WORK HAS BEEN COMPLETED IN FLEET CYCLE .
SUPPORT TASK REF EA 5320-02076 REV B & AD2013-23-04 AMDT 17659 STEP 3, 1C SEAT TRACK SPLICE STRAP SHOWS CRACK INDICATION AT LBL 24.75 STATION 727B, BOTH TRACK & SPLICE PLATE INDICATED CRACK. REPAIRED FOR ECRA 5320-02239.
ATTACH ANGLE FOR WEB AT LOWER LOBE FUSELAGE BETWEEN STATION 312 & STATION 325.38. STRINGER 23L HAS PITTING CORROSION ALMOST THRU ENTIRE FLANGE AT APPROXIMATELY STATION 320. PERFORMED PART 1 INTERIM REPAIR TO STRINGER 23L IAW ECRA 5310-06076. ACCOMPLISH INSPECTION REQUIREMENTS ON OR BEFORE THE ACFT REACHING 50,000 TOTAL FLIGHT CYCLES.
FOUND SCRIBE DAMAGE AROUND THE FOOT PRINT OF THE L BAND ANTENNA. REPAIRED IAW ECRA 5331-01870.
FORWARD CARGO STATION 500A AT RBL 10 FLOOR TIE DOWN TRACK HAS A LARGE GOUGE. STATION 500A FLOOR TIE DOWN TRACK HAS BEEN REPAIRED IAW SRM 53-00-53.
FRAME AS STATION 500A RT IS CRACKED BETWEEN STRINGER 8R & 9R AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT BRACKET INBD FASTENER. FRAME 500A RT HAS BEEN REPAIRED IAW EA 5310-04716 REV G OP 2.
FRAME 480L IS CRACKED BETWEEN STRINGER 8L & 9L AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT BRACKET INBD FASTENER. FRAME 480L HAS BEEN REPAIRED IAW EA 5310-04716 REV G OP 2.
FRAME 380R IS CRACKED BETWEEN STRINGER 8R & 9R AT AIR CONDITIONING OUTLET EXTRUSION SUPPORT BRACKET INBD FASTENER. FRAME 380R HAS BEEN REPAIRED IAW EA 5310-04716 REV G OP 2.
FRAME AT STATION 500C RT IS CRACKED BETWEEN STRINGER 8 & STRINGER 9 AT AIR CONDITION OUTLET EXTRUSION SUPPORT BRACKET INBD FASTENER. REPAIRED FRAME AT STATION 500C RT IAW EA 5310-04716 REV G. SEE WIP FOR WORK PERFORM.
LEFT PACK WILL NOT HEAT COCKPIT. T/S PER FIM 21-61-00 FOUND TEMP SENSOR BAD. REPLACED TEMP SENSOR PER AMM 21-51-52. GND CHECK OK.
TAIL COMPARTMENT STATION 1088 BULKHEAD JUST ABOVE APU INLET BOX (RT SIDE) "L" ANGLE HAS CORROSION. REMOVED AND REPLACED DAMAGED STIFFENER. REF GMM 10-900-02 AND SRM 51-40-02.
STA 270 ATTACH ANGLE FOR LOOK DOWN TUBE MOUNT CORRODED. CUT OUT DAMAGED SECTION OF FLOORBEAM, FABRICATED FILLER AND REPAIR ANGLES, TREATED, PRIMED AND INSTALLED REPAIR FILLER AND ANGLES REF ECRA 5321-01689.
LOOK DOWN TUBE MOUNT FWD OF STA 270 CORRODED. FABRICATED AND INSTALLED NEW INTERCOSTAL REF ECRA 5321-01689.
CABIN FRAME CRACKED AT STA 400 BETWEEN STR 8R-9R. REPAIRED CABIN FRAME AT STA 440 BETWEEN STA 8R-9R PER ECRA 5310-05022.
CABIN FRAME CRACKED AT STA 827 BETWEEN STR 8R-9R. REPAIRED CABIN FRAME AT STA 827 BETWEEN STR 8R-9R PER ECRA 5310-05022.
CABIN FRAME CRACKED AT STA 440 STR 8L-9L. REPAIRED CABIN FRAME AT STA 440 STR 8L-9L PER ECRA 5310-05022.
FRAME CRACKED AT STA 827 BETWEEN STR 8-9R. REPAIRED CABIN FRAME AT STA 827 BETWEEN STR 8-9R PER ECRA 5310-05022.
FRAME CRACKED AT STA 400 BETWEEN STR 8L-9L. REPAIRED CABIN FRAME AT STA 500A BETWEEN STR 8L-9L PER ECRA 5310-05022.
FRAME CRACKED AT STA 500A BETWEEN STR 8L-9L. REPAIRED CABIN FRAME AT STA 500A BETWEEN STR 8L-9L PER ECRA 5310-05022.
FRAME CRACKED AT STA 400 BETWEEN STR 8R-9R. REPAIRED CABIN FRAME AT STA 400 BETWEEN STA 8R-9R PER ECRA 5130-05022.
FRAME CRACKED AT STA 480 BETWEEN STR 8R-9R. REPAIRED CABIN FRAME AT STA 480 BETWEEN STR 8R-9R PER ECRA 5310-05022.
INTERCOSTAL CRACKED STA 312 TO 328, RBL 31. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.
INTERCOSTAL CRACKED STA 312 TO 328, LBL 46. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.
INTERCOSTAL CRACKED STA 328 TO 344, LBL 48. REMOVED AND REPLACED INTERCOSTAL REF SRM 51-40-02.
INTERCOSTAL CRACKED STA 277 TO 294, BL 0. REMOVED AND REPLACED INTERCOSTAL IN REF TO SRM 51-40-02.
INTERCOSTAL CRACKED AT STA 540 LBL 0. REMOVED CRACKED INTERCOSTAL AT STA 540 LBL 0, FABRICATED NEW INTERCOSTAL FROM 7075 .040 (PAC44429), DRILLED INTERCOSTAL, ALODINED & PRIMED PART IAW B737-8 SRM 51-20-01. INSTALLED INTERCOSTAL AT STA 540 IAW BOEING DWG 143A5240 & AMP; B737-8 SRM 51-40-2 & AMP; INSTALLED SHIM FABRICATED FROM .077 2024-T3 (PAC50600).
INTERCOSTAL CRACKED AT STA 540 RBL 0. REMOVED CRACKED INTERCOSTAL AT STA 540 & AMP; RBL 0 FABRICATED NEW INTERCOSTAL FROM 7075 .040 (PAC 44429), DRILLED INTERCOSTAL, ALODINED & AMP; PRIMED PART IAW B737-8 SRM 51-20-01, INSTALLED INTERCOSTAL AT STA 540 RBL 0 IAW BOEING DWG 143A5240 & AMP; B737-8 SRM 51-40-02.
NUT PLATE HOLE CORRODED AT STA 986, RBL 23. REPAIRED IAW SRM 53-00-51.
FOUND EMERGENCY LIGHTS ON OVERHEAD BIN, ROWS 17-20 INOP. REPLACED LIGHT ASSY PER AMM 33-51-06.
L2 DOOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER AMM 33-51-06.
LEFT SEATS 11-14 AND OVERWING HATCH EMERGENCY LIGHTS INOP. REPLACED BATTERY PACK PER AMM 33-51-06.
INSPECTION FOUND CENTER FLOOR SUPPORT BEAM CORRODED AT STA 500I, LBL 30 TO RBL 30. SUPPORT IS LOCATED DIRECTLY BELOW BULKHEAD PANEL AT STA 500I, FORWARD BAGGAGE BIN. THE CENTER FLOOR SUPPORT BEAM WAS REMOVED AND REPLACED IAW SRM 51-40-02.
THE EMERGENCY BATTERY PACK AT LT SEAT ROW 20 & 21 (STA 1250) FAILED TEST. THE BATTERY PACK WAS REMOVED AND REPLACED IAW MM 33-51-00.