N75435
Registered owner: UNITED AIRLINES INC, IL (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
PILOT REPORTS EXHAUST ODOR IN CABIN, FOUND PORTABLE AC CART UPWIND OF AIRCRAFT. SHUT DOWN AMD DISCONNECTED PORTABLE AC CART. ODOR CLEARED THE CABIN. NO DEFECTS NOTED.
EMERGENCY LIGHTS - OPERATIONAL CHECK EMERGENCY LIGHTS OPERATIONAL CHECK - R1 DOOR EXIT SIGN AND OVERHEAD LIGHT NOT ILUMINATING DURING EMER LIGHT TEST. REMOVED AND REPLACED FWD RH POWER SUPPLY FUSES REF AMM 33-51-06. NO FIX R1 DOOR EXIT SIGN DOES NOT COME ON. SWAPPED LH AND RH FWD PSU, NO CHANGE TO INDICATION. SWAPPED BACK TO ORIGINAL POSITION. WHEN CHECKING CONTINUITY FROM EXIT SIGN TO BATTERY PACK REF WDM 33-51-12-6.1. FOUND CIRCUIT TO BE OPEN FROM BATTERY PACK CONNECTOR D10748 TO EMERGENCY EXIT SIGN ISOLATED AT CONNECTOR D2968 AND STILL READ AN OPEN CIRCUIT. UPON FURTHER INVESTIGATION FOUND CONNECTOR D40042 DISCONNECTED. SAID CONNECTOR IS ABOVE THE GALLEY AND WILL REQUIRE FURTHER DISASSEMBLY OR MOVING OF THE GALLEY TO REACH AND RECONNECT DISPLACED FWD GALLEY AREA CEILING PANEL REF AMM 25-21-34. CONNECTED CONNECTOR D40042 REF WIRING DIAGRAM 33-51-12. RESTORED FWD GALLEY CEILING PANEL REF AMM TASK 25-21-34-400-801. OPERATIONAL TEST OF EMERGENCY LIGHTS PASSED REF AMM 33-51-00-710-801.
PASSENGER CABIN SEATS, GENERAL VISUAL INSPECTION PROCEDURE, INSEAT AISLE PATH LIGHTING INOP 10ABC. REMOVED AND REPLACED AISLE PATH LIGHTING HARNESS ON SEAT IAW CMM 25-21-57. OPS CHKD GOOD.
ENG 2 FUEL FILTER BYPASS LIGHT ON ENG SLOW TO RESPOND AT IDLE POWER SETTING, ENG 2 FUEL FILTER BYPASS CAME ON DURING APPROACH AT AROUND 14,000. FT. IDLE POWER SETTNGS WERE SLOW TO RESPOND. N1/N2 IDLE FLUCTUATING AROUND 30-35. FLUCTUATION ON N1 ONLY, ON ENG 2 R & R ENG 2 FUEL FILTER, NO CONTAMINATION FOUND. FUEL FILTER BYPASS LIGHT STILL CAME ON DURING ENG RUN. SUSPECT FUEL FILTER DIFFERENTIAL PRESSURE SWITCH OR FUEL FILTER CLOGGING INDICATOR. REQ MEL 7304B FOR FUEL FILTER DIFFERENTIAL PRESSURE INDICATOR ON NR 2 ENG. COMPLIED WITH MEL. ENGINE 2 FUEL FILTER DIFFERENTIAL PRESSURE WARNING SYSTEM INOP. TECHS COMPLIED WITH MEL 7304B METHOD 2 FOR COMPLIANCE. R & R FUEL FILTER DIFFERENTIAL PRESSURE SWITCH, IAW AMM 73-34-01. OPS CK GOOD & LEAK CK GOOD, FILTER BYPASS LIGHT EXTINGUISHED, BYPASS IN THE CDU, REF FIM 73-05 TASK 801.
DOOR WARNING ANNUNCIATOR IS ON AFT SERVICE S195 SHOWING INTERMITTENTLY TARGET FAR WITH DOOR CLOSED AND LOCKED, REQUESTING 5203C VERIFIED ONLY AFT SERVICE DOOR IS INTERMITTENT. WILL VERIFY R2 DOOR IS CLOSED AND LOCKED PRIOR TO DEPARTURE. DISPATCH DESK: TOMC APPROVED MEL 5203C VERIFIED R2 DOOR IS CLOSED AND LOCKED PRIOR TO DEPARTURE. ADJUSTED AND TESTED AFT SERVICE DOOR IAW AMM 52-41-00. OPERATION CHECK GOOD, NO DOOR ANNUNCIATOR LIGHT ON.
MOST AFT RT OVERHEAD BIN EMERGENCY LIGHT INOPERATIVE. REMOVED & REPLACED FUSE IAW AMM 33-51-06. OPS CHECK GOOD PER AMM 33-51-00-710-801.
R1 EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP ON THE R1 EXTERIOR EMEREGENCY SLIDE LIGHT, OPS CHECKS GOOD IAW AMM 33-51-04.
COORDINATE WITH UAL REP TO BUILD A DOUBLER IDENTICAL TO THE DOUBLER INSTALLED ON FRAME 727C, S5L WITH ONE EXCEPTION, EXTEND THE DOUBLER 3 RIVET ROWS BEYOND UPPER INBD END. DO NOT DRILL INTO FRAME OR NEW DOUBLER, JUST FABRICATE DOUBLER. REMOVED AND REPLACED EXISTING DOUBLER AT FRAME 727C S5L WITH LARGER, -1 REPAIR DOUBLER TO ACCOMMODATE STOW BIN MOD STRUCTURE PER EC/RA 5311-03413 REV-.
SUPPORT TASK: WHILE PERFORMING B737-900ER SRM 57-41-01-2R-7 REPAIR 7 FOR LOOSE FASTENERS AT LH WING FIXED LEADING EDGE, FOUND CRACKED STIFFNER PN# 116A4530-1. REMOVED AND REPLACED STIFFENER PN 116A4530-1 IAW BOEING DWG 116A4008 RV - AND REPLACED 2 RIVETS ON OUTBOARD SIDE WITH HILOCKS IAW SRM 57-41-01-2R-7.
RIGHT WING LEADING EDGE LOWER SKIN UPPER SURFACE FROM OFSS 706 TO 696 HAS CORROSION. ACCOMPLISHED INTERIM REPAIR FOR CORROSION ON RT WING LOWER SKIN PANEL FORWARD OF FRONT SPAR BETWEEN OFSS 692 AND OFSS 704 IAW ECRA 5724-01040 REV A, PART 1.
CRACK INDICATIONS FOUND ON RT HORIZ STAB HSS 129.50 IN LWR SKIN RIB, (SECOND LAYER). REMOVED FWD SPAR WEB TO GAIN ACCESS IAW SRM 51-40-02. REMOVED & CUT CRACKED AREAS IAW SRM 55-10-09-2R-5 REPAIR 5. NDT VERIFIED NO CRACKS. FABRICATED TWO FILLERS AND TWO ANGLES IAW SRM 55-10-09-2R-5, REPAIR 5. REINSTALLED WEB IAW DWG 182A2401, REV F, AND SRM 51-40-02.
COCKPIT FLOOR DENTED JUST AFT OF PEDESTAL. ELEVATED FLIGHT DECK FLOOR WEB BETWEEN BS 250-260 LBL20-RBL20, FOUND AREAS WITH SHARP GOUGES, OUT OF LIMITS IAW SRM 53-10-51-1A-1 ALLOWABLE DAMAGE 1 SECT 41. FLOOR STRUCTURE FIG 105 SHT 2 DETAIL D. REMOVED DAMAGED FLOOR WEB AND INSTALLED REPAIR PARTS -1 FLOOR WEB, -2 AND -3 REPAIR DOUBLERS IAW REO-G25639, DWG 141A0631 REV- AND SRM 53-10-51-2R-2, REPAIR 2, SECT 41, 51-40-02-0G-0.
CRACK INDICATION FOUND AND VERIFIED: R/H HORIZ STAB LOWER SKIN STA 120.30 MARKED #1 .900"L 17" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVALUATED CRACK ON LOWER SKIN AND CUT OUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 55-10-01- 2R-11. FABRICATED FILLER AND NEW DOUBLER AND INSTALLED IAW SRM 55-10-01, SRM 51-40-05 AND SRM 51-40-02.
CRACK INDICATION FOUND AND VERIFIED, R/H HORIZ ST AB LOWER SKIN STA 120.30 .800L 25.5" AFT OF FRONT SPAR I/B OF I/B FASTENER ROW. EVAL CRACK ON LOWER SKIN STA 120.30, 25.5 INCHES OF FRONT SPAR, CUTOUT DAMAGE AND REMOVED EXISTING DOUBLER AT STA 120 IAW SRM 55-10-01-2R-11, FABRICATED FILLER AND INSTALLED PER SRM 55-10-01-2R-11 NEW DOUBLER INSTALLED AND FABRICATED ON CARD 9282785.
R-1 DOOR HANDLE BOX CUTOUT UPPER TORQUE TUBE BUSHING STUB BEAM IS GOUGED. REMOVED STUB BEAM GOUGED IAW B737-900 SRM 51-40-02. INSTALLED NEW STUB BEAM IAW B737-900 SRM 51-40-02, BAC DWG 141A6523.
NR 1 PYLON AFT TRAILING EDGE FAIRING O/B FITTING CRACKED. REMOVED AND REPLACED NR 1 PYLON T/E FAIRING IAW SRM 51-40-02 AND DWG 313A2700 REV-.
EA-3271-01017-001 TAIL SKID ASSEMBLY SUPPORT FITTING REPLACEMENT UNDER WORK INSTRUCTIONS STEP 7 (B)(4) PRE-EXISTING HOLE AT .250. COMPLETED ALL STEPS PER UAL ECRA 5380-01430 REV- FOR REPAIR.
AFT ENTRY DOOR (L2) UPPER STOP FITTING HAS GOUGE. REMOVED AND REPLACED L-2 DOOR UPPER FWD STOP FITTING IAW DWG 147A6125 REV- AND SRM 51-40-02-0G-0.
BS 847 RBL 45 HAS CORROSION ON UPPER SURFACE ACCOMPLISHED SEAT TRACK REPAIR ON RBL-45, STA 847 IAW SRM 53-00-52-2R-5.
MAIN CABIN SEAT TRACK AT LBL 45 STA 820 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW B737-900 SRM 53-00-52-2R-5 DUE TO CORROSION BEING BEYOND LIMITS IAW B737-900 SRM 53-00-52-1A-1.
CRACK INDICATION FOUND & VERIFIED: RT HORIZ. STAB LOWER HSS STA.147.90. 1 .600"L 15.5" AFT OF FRONT SPAR I/B OF I.B FASTENER ROW. DOT:B616. REMOVED EXISTING DOUBLER, FABRICATED AND ALODINED, PRIMED AND INSTALLED NEW DOUBLER AND FILLER AT R/H HORIZONTAL LOWER SKIN STA 147.90 IAW B737 SRM 51-20-01, SRM 55-10-01.
B737-53-3-0714 FWD PIT R/H SUPPORT ASSY CORRODED AT LOWER AREA AT BS 500L APPROX AT RBL-24. REMOVED AND REPLACED FWD PIT R/H SUPPORT ASSY AT BS 500L IAW B737-900ER SRM 51-40-02 AND DWG 143A7902 ID37 REV 'E'.
FWD PIT LEFT TRANSITION PANEL ASSY CORRODED ON UPPER SURFACE FROM BS 500D TO BS 500L APPROX LBL-24. REMOVED AND REPLACED BAC1496-444 7075-T62C TRANSITION PANEL IAW B737-900ER SRM 51-40-02 AND SRM 51-40-05, SRM 53-00-53-2R-5.
SUPPORT TASK: FWD CARGO PIT BAFFLE BETWEEN STA 500J AND 500K IS CRACKED. . REMOVED AND REPLACED CRACKED BAFFLE IAW B737-900ER SRM 51-40-02 AND SRM 51-40-05 AND DRAWING 143A7505.
FWD PIT RT SIDE, ONE CLIP CRACKED AT BS 500K APPROX. STRINGER S-26R. REMOVED AND REPLACED 1EA CLIP PN: 143A7502U158 PO# 1134152.1 AT BS 500K STR 26R IAW SRM 51-40-02 AND DWG 143A7505 REV-.
(SUPPORT TASK) FWD CARGO PIT AT S-26L BETWEEN STA 500H - STA 500I BAFFLE IS CORRODED ON UPPER FLANGE. REMOVED AND REPLACED 1EA BAFFLE PN: 143A7510-21 PO# 1134747.1 IAW UNITED B737-900ER SRM 51-40-02 AND BAC DWG #143A7505 REV -.
FWD PIT R/H SIDE, 1 EACH ANGLE CRACKED AT BS 500K APPROX. STRINGER S-26R. REMOVED AND REPLACED 1EA CLIP PN: 143A7502-156 BS 500K STR 26R IAW UNITED B737-900ER SRM 51-40-02 AND BAC DWG #143A7505 REV B.
FWD CARGO PIT LT SIDE BETWEEN BS 500D - STA 500E BAFFLE IS CORRODED ON UPPER FLANGE. MATERIAL IS FOUND TO BE 100% OUT OF LIMITS DUE TO EVIDENT EXFOLIATION IAW SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED 1EA BAFFLE ASSY AT FWD CARGO BAY LT SIDE BETWEEN BS 500D TO 500E IAW SRM 51-40-02 AND BAC DWG 143A7505 REV-.
FWD PIT LT SIDE, ONE CLIP CRACKED AT BS 500J APPROX STRINGER 26L. REMOVED AND REPLACED CRACKED CLIP IAW SRM 51-40-02 AND 51-40-05 AND DWG 143A7505.
AFT CARGO COMPARTMENT LT TRANSITIONAL PANEL BETWEEN BS 727I-727J HAD CORROSION. REMOVED AND REPLACED TRANSITION PANEL BS 727I-727J & FABRICATED REPAIRS SPLICE IAW SRM 51-40-02, 53-00-53-2R-5 & DWG 146A7500 0169.
FWD CARGO BAY, LT SIDE CLIP CRACKED AT BS 500K, STRINGER 26L. REMOVED AND REPLACED CRACKED CLIP IAW SRM 51-40-02 AND SRM 51-40-05 AND DWG 143A7505.
FWD CARGO BAY AT STRINGER 26L BETWEEN BS 500G - 500H BAFFLE IS CORRODED ON UPPER FLANGE. REMOVED AND REPLACED CORRODED BAFFLE IAW SRM 51-40-02 AND DWG 143A7505.
FWD CARGO PIT GUSSET AT STA 500L S-19R IS CRACKED. REMOVED AND REPLACED FWD CARGO GUSSET AT STA 500L STR 19R IAW B737-900ER SRM 51-40-02 AND DWG 143A7902 0206.
SUPPORT TASK: MAIN CABIN SEAT TRACK AT LBL45 STA 700-727 HAS MULTIPLE GOUGES AND CORROSION. REMOVED CORROSION FROM MAIN CABIN SEAT TRACK STA 700-727 LBL45. MATERIAL REMOVED 0.028, MAX MATERIAL ALLOWED IS 0.020, SEAT TRACK SECTION FOUND OUT OF LIMITS IAW B737 SRM 53-00-52-1A-1. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED, LOCATED AND DRILLED NEW SEAT TRACK SECTION IAW B737 SRM 53-00-52-2R-3. ALODINED AND PRIMED IAW SRM 51-20-01 AND SOPM 20-41-02. INSTALLED NEW SEAT TRACK SECTION IAW B737 SRM 53-00-52-2R-3.
(SUPPORT TASK) FWD CARGO PIT AT S-26 BETWEEN BS 500E - BS 500F BAFFLE IS CORRODED ON UPPER FLANGE. AFTER INVESTIGATION OF DAMAGE AREA IT WAS CONCLUDED THAT MATERIAL IS FOUND TO BE 100% OUT OF LIMITS DUE TO EVIDENT EXFOLIATION IAW SRM 53-00-53-1A-2 FIG 103. REMOVED AND REPLACED 1EA BAFFLE ASSY AT FWD CARGO PIT L/H SIDE BETWEEN STA 500E AND STA 500F IAW SRM 51-40-02 AND IAW BAC DWG 143A7505 REV-.
AFT CARGO COMPARTMENT RIGHT SIDE TRANSITIONAL PANEL BETWEN STA 727H-727I HAS CORROSION. MARKED WITH RED PEN. REMOVED AND REPLACED TRANSITION PANEL FROM BS727-727I USING 'Z' ANGLE PN# BAC1496-377 7075-T62 FOR 2EA TRANSITION PANELS AND 1EA SPLICE REPAIR PARTS IAW SRM 53-00-53-2R-5 REPAIR 5 AND BDWG 146A7500 REV-.
FWD PIT DOOR CUTOUT, LOWER SILL CORRODED ON UPPER SURFACE. CORROSION FOUND TO BE 100% OUT OF LIMITS. REMOVED AND REPLACED LOWER MAIN SILL WEB PN 143A8122- 10 IAW BOEING DWG 143A8122 AND SRM 51-40-02-0G-0.
FWD PIT, R/H TRANSITION PANEL CORRODED ON UPPER SURFACE FROM BS 492 TO BS 500A APPROX. RBL- 24. BLENDED AND REMOVED CORROSION IN SEVERAL AREAS 100% MATERIAL LOSS FOUND OUT OF LIMITS IAW SRM 53-00-53-1A-2. REMOVED DAMAGE TRANSITION PNL FROM FWD CARGO COMPARTMENT R/H BS 492 TO BS500A RBL 24 IAW: B737-900ER,SRM 51-40-02, RECEIVED NEW SHIELD AND LOCATE AND DRILLED IAW BAC DWG 143A8126 REV.A AND B737-900ER SRM 51-40-05. INSTALLED 1 EA NEW SHIELD AT FWD PIT R/H AREA, BS492 TO BS500A APPROX RBL -24 IAW: B737-900ER SRM 51-40-02 AND BAC DWG # 143A0080 REV:A.
AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL HAS CORROSION AT MULTIPLE PLACES. AFT CARGO COMPARTMENT DOOR CUTOUT LOWER SILL WEB FOUND TO BE OUT OF LIMITS IAW 737-800ER SRM 53-30-15-1A-1 FIG 103 REMOVED AND REPLACED WEB PART #146A8123U25 ATSMRO PO # 1133565 IAW 737-900ER SRM 51-40-02 AND BOEING DWG # 1465A8123 ID 21.
FWD PIT, LEFT SUPPORT ASSY CORRODED AT LOWER AREA AT BS 500L APPROX. AT LBL-24. REMOVED SUPPORT ASSY (ANGLE) IAW SRM 51-40-02 AND REMOVAL DAMAGE CORROSION. MAT. REMAINED .037" FOUND WITHOUT LIMITS OF .056". LOCATED & DRILLED 1EA NEW SUPPORT ASSY (ANGLE) IAW SRM 51-40-05. INSTALLED IAW SRM 51-40- 02 AND DWG 143A9481, REV A.
FWD CARGO BAY, STRINGER 26L BETWEEN BS 500F - 500G BAFFLE IS CORRODED ON UPPER FLANGE. AFTER INVESTIGATION, DAMAGED AREA AT WAS CONCLUDED THAT THE MATERIAL IS FOUND TO BE 100% OUT OF LIMITS DUE TO EVIDENT EXPOLATION IAW SRM 53-00-53-1A-2, FIG 103. LOCATED AND DRILLED A NEW BAFFLE IAW SRM 51-40-05, INSTALLED THE NEW BAFFLE IAW SRM 51-40-02 & BAC DWG 143A7505 REV -.
FWD CARGO PIT FLOOR PANEL 120CF HAS TWO PUNCTURES. IAW SRM 53-30-53. FABRICATED NEW FWD CARGO FLOOR PANEL 120CF IAW EC/RA 5320-02744 REV A. PRIMED AND ALODINED FLOOR PANEL IAW SRM 51-20-01.
MAIN CABIN FLOOR SUPPORT INTERCOSTAL FLOOR BOARD FASTENER HOLES 2EA HAVE CORROSION IN THE BORE BETWEEN STA 294.5 AND 312 AT APPROX LBL12. MAIN CABIN FLOOR STA 294.5 - 312 LBL 11.1 BLENDED AFFECTED AREA ON INTERCOSTAL TO REMOVED CORROSION, REMAINING MATERIAL FOUND TO BE BEYOND LIMITS IAW BOEING SRM 53-10-51. REMOVED AND REPLACED INTERCOSTAL IAW BOEING DWG 141A5600 REV:N SHEET 2 AND SRM 51-40-02.
MAIN CABIN L/H SIDE CREASE BEAM WEB IS CORRODED ON THE UPPER SURFACE AT THE MID EXIT DOOR PLUG FWD LOWER BONDING WIRE CONTACT POINT. REMOVED DAMAGE FOUND TO BE OUT OF LIMITS. ORIG MAT .063,MAT LOSS .014, REMAINING MAT .049 IAW SRM 51-10-02.
(B737-53-3-0711) MAIN CABIN FLOOR SUPPORT INTERCOSTAL UPPER SURFACE IS CRACKED AT THE FLOOR BOARD FASTENER HOLE STA 312 AND 328 AT APPROX LBL46. BLENDED OUT INTERCOSTAL, FOUND 100% OUT OF LIMITS. REMOVED, LOCATED AND DRILLED NEW INTERCOSTAL AND INSTALLED AT M/C BS312 AND BS328 LBL46 IAW BDWG 141A5400 REV-, SRM 51-40-02 AND SRM 53-10-15.
MAIN CABIN FLOOR SUPPORT INTERCOSTAL HAS 2EA CRACKS BETWEEN STA 277 AND 294.5 AT BLO IN THE UPPER SURFACE COMMON TO THE FLOOR BOARD FASTENER HOLES. CLEANED INTERCOSTAL, FOUND 100% OUT OF LIMITS. LOCATED AND DRILLED AND INSTALLED NEW INTERCOSTAL IAW BDWG 141A5410 REV V, SRM 51-40-02, SOPM 20-30-03 AT M/C STA 277 AND STA 294.5 AT BL0.
MAIN CABIN FLOORBEAM AT BS 987 LBL45 CORRODED AT GIRT BAR FITTING HOLE (DOME NUT) LOCATION. REMOVED CORROSION, FOUND TO BE 100%, OUT OF LIMITS IAW SRM 53-70-51-1A-1 DETAIL C. REPAIRED AREA IAW SRM 53-70-51-2R, REPAIR 6, & SRM 51-20-01. ACCOMPLISHED DVI IAW SRM 51-10-04. ACCOMPLISHED HFEC IAW NDT PART 651-00-00 PROCEDURE 4, NO CRACK NOTED. SHOT PEEN AREA IAW SRM 20-10 -03.
MAIN CABIN FLOORBEAM AT STA 987 RBL45 CORRODED AT GIRT BAR FITTING HOLE. CORROSION LEVEL. 2 - OUT OF LIMITS ON PRIMARY STRUCTURE. REPAIRED BS 987 FLOORBEAM AT RBL 45 IAW SRM 53-70-51-2R-6.
STRONG ELEC BURNING SMELL AT ROW 28 JUST PRIOR TO DECENT. LASTED 5 MINS C/W SMOKE/ODOR IN THE FLIGHT DECK/CABIN - CONDITIONAL INSPECTION UP TO F1 NO FURTHER SMELL BY MX OR FLT CREW, A/C OK TO CONTINUE.
EMER EXIT HANDLE ROW 21 RIGHT SIDE FALLING OFF RESECURED EMERGENCY EXIT DOOR HANDLE COVER IAW AMM 52-22-00.
RIGHT AISLE EMERGENCY LIGHTS FROM ROW 4 TO OVERWING EXIT AND FWD RT OVERWING EXTERIOR LIGHT INOP. REPLACED FUSES IN POWER SUPPLY M1676 REF MM 33-51-06. NO HELP. REMOVED AND REPLACED M1676 BATTERY PACK AND CHARGER REF MM 33-51-06. OPS CK OK.
LEFT STAB LOWER SURFACE SKIN IS CRACKED I/B OF RIB STA. 138.70 T/E AT REAR SPAR AREA. 4, S NOT EXCEEDED.
LH HORIZONTAL STAB LOWER SKIN CRACKED AT STA 157.10 23 INCHES AFT OF FORWARD SPAR. STEP 5 TABLE 204. CRACK REPAIR ACCOMPLISHED ON BAM N/R 001145780. ACCOMPLISH INSPECTION REQUIREMENTS OF REPAIR PER SRM 55-10-01 REPAIR 11
RIGHT HORIZ STAB LOWER SKIN AT STA.120.30 & APPROX 11" FROM AFT EDGE AREA HAS CRACK. CW. STEP 4, S NOT EXCEEDED.
SEAT 15ABC EMER. PATHWAY EXIT LIGHT LENS MISSING. REPLACED LIGHT ASSY REF AMM 33-51-11-960-802 OPS CHECKED OK. ACP IDT INSP OF REPLACING EPL AT SEAT 15ABC REF GMM 09-10-05 AND AMM 33-51-11. OPS CHK GOOD.
LT HORIZ. STAB. SKIN HAS CRACK INDICATION BETWEEN STAS. 129.5-13 8.7 2" FWD OF AFT SPAR. (REF FLEET CYCLE LOG PAGE #9704508) SEE FLEET CYCLE LOG PAGE #9704508 FOR WORK ACCOMPLISHED. DIP FOR INSPECTION IS INCLUDED IN ELB LOG PAGE#9865718. NO CHANGES MADE TO DIP REQUIREMENTS.
WHILE WORKING EA 3351-01167 OP 7 L-2 DOOR LENS MOD STEP 12 REQUI RES OP CHECK OF EMERGENCY LIGHTS.L-2 DOOR FAILED.LIGHT DOES NOT COME ON AT ALL. REMOVED AND REPLACED BATTERY PACK AND CHARGER ASSY OPS CHECKS GOOD REF AMM 33-51-06.
WHILE PERFORMING EA 3351-01167 LENS MOD OP6 R-2 DOOR STEP 12 REQUIRES OPS CHECK OF EMERGENCY LIGHTS.R-2 DOOR FAILED.LIGHT COMES ON THEN GOES RIGHT OUT. REMOVED AND REPLACED THE BATTERY ASSY OPS CHECKS GOOD REF AMM 33-51-06. ADD EMP:U335635
L2 DOOR SLIDE LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04-960-801. OPS TESTED NORMAL.
FIRST CLASS EMERGENCY LIGHT INOPERATIVE. REPLACED FWD RIGHT BATTERY ON POWER SUPPLY IAW AMM 33-51-06. OPS CHECKED OK.
EMERGENCY LIGHTS FAILED TO TEST. REMOVED AND REPLACED THE BATTERY PACK ABOVE ROW 29 DEF IAW AMM 33-51-06. OPS CHECKED GOOD.
FLOOR EMERGENCY LIGHT DOES NOT TURN ON AT 24C. REPLACED HOUSING AND BACK PLATE, TESTED OK
EMERGENCY FLASHLIGHT AT 4L INOP. REPLACED BATTERY ON EMERGENCY FLASHLIGHT AT DOOR 4L. OPS NORMAL.
LEFT EMERGENCY LIGHTS IN THE FIRST 6 ROWS OF THE ACFT WERE INOPERATIVE. REMOVED AND REPLACED THE BATTERY PACK AND CHARGER IAW 33-51-06-960-806. OPS CHECKED GOOD.
EMERGENCY LIGHT OVERHEAD BIN BETWEEN ROWS 8 & 9 LT SIDE INOP. REMOVED AND REPLACED EMERGENCY POWER SUPPLY PACK. OPS CHECKED GOOD
AT BS 380 BETWEEN STRINGERS 7 AND 8L, THERE IS A GOUGE IN THE SKIN IAW ECRA 5331-02120 . THE SKIN WAS REPAIRED IAW SRM 53-00-01 REP 3 TABLE 204
RIGHT HORIZONTAL STAB LOWER IN SPAR SKIN HAS A CRACK INDICATION AT HSS 157.10, ABOUT 9.5" AND 16.5" FROM AFT SPAR. THE SKIN WAS REPAIRED IAW SRM 55-10-01 REP 11.
REF EA 5510-01843 REV E, RIGHT HORIZONTAL STABILIZER LOWER SKIN CRACK LOCATION FOUND AT STA 101.90 AT 19"AND 28" FROM FWD SPAR. RT STAB LOWER INSPAR SKIN HAS BEEN REPAIRED IAW SRM 55-10-01 REP 11 1. COMMON DOUBLER INSTALLED OVER BOTH AREAS.
SEAT ROW 26 - 32, EMER PATH LIGHTING INOPERATIVE. R & R BATTERY PACK AT SEAT ROW 27L IAW AMM 33-51-06-960-805, SUB TASKS 960-005, 960-006 & 710-004. OPERATIONS CHECKED GOOD.
LEFT AFT EXTERIOR EMER LIGHT IS OUT. REPLACED FUSE FOR EMER LIGHTS POWER SUPPLY M1670 IAW AMM 33-51-06-960-804. RELAMPED LT AFT EXTERIOR EMER LIGHT. OPERATIONS CHECKED GOOD IAW AMM 33-51-04-960-801.
DURING KA BAND, WI-FI INSTALLATION, THE FUSELAGE SKIN PANEL EXISTING PRESSURE FEED THRU DOUBLER WAS 1 ROW FASTENER LARGER THAN IT SHOULD BE AT BS 727E-727F AT LBL 4.78. REPAIRED BODY BS 727E-727F FUSELAGE SKIN PANEL IAW ECRA 5310-05925.