N37434
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
F/A REPORTS THAT PAPER CAUGHT FIRE IN OVEN 204. REMOVED RACKS FROM OVEN TO REMOVE PAPER AND ASHES FROM HEATING COIL AND MOTOR. WIPED OVEN DOWN. BURNT ODOR PRESENT AFTER OPS CHECK. REMOVED AND REPLACED FWD GALLEY OVEN 204 (G24) IAW AMM 25-34-00. OPS CHECK GOOD. NO ODORS OR FAULTS PRESENT AT THIS TIME.
EMERGENCY LIGHTS OPS CHECK, EMERGENCY SEAT LIGHTS INOPERATIVE ROW 28ABC-34ABC. REMOVED AND REPLACED THE BATTERY M2626 IAW AMM 33-51-06-960-805.
FAS SMELL OLD OIL SMELL AROUND ROW 4. RAN PACK WITH APU BLEED NO ODORS IN CABIN NOTED. RAN ENGINES WITH PACK ON REF AMT TAXI/RUN CHECKLIST FORM 47-0067 FOR TEN MINUTES NO ODORS WERE NOTED IN CABIN.
34ABC AISLE EMERGENCY LIGHT BROKEN REF AMM 33-51-11 REPLACED FLOOR PROXIMITY LIGHT. VERIFIED LIGHT OPERATIONAL.
LT FWD EMERGENCY LIGHT BULB INOPERATIVE. REPLACED BULB.
DOOR 1R SLIDE COVER BRACKET LOOSE. ADJUSTED BRACKET TENSION OF GIRT BAR RETAINER. BAR SNAPS SECURLY INTO PLACE. OPS CHECK OK
RIGHT CENTER FUEL LOW PRESS ON WITH SWITCH SELECTED ON. 6.4 IN TAN K.REQUEST MEL FOR RT CENTER FUEL BOOST PUMP INOP. PULLED AND COLLARED RT CENTER PUMP C/B. PLACED RT CENTER FUEL PUMP ON M.E.L., DDP C/W. TRANSFERRED FUEL INTO CENTER TANK WITH RT CENTER FUEL PUMP ON LOW PRESSURE LIGHT REMAINS ON. PER FIM 28-22 TASK 802 CENTER RIGHT TANK WILL NEED 14,000LBS OF FUEL TO TROUBLESHOOT FURTHER. R & R RT CENTER TANK FUEL BOOST PUMP PRESSURE SWITCH IAW AMM 28-42-11. FAULT STILL REMAINS. PERFORMED CONTINUITY CHECK BETWEEN PINS 2 & 3 ON RT CENTER TANK BOOST PUMP LOW PRESS SWITCH S155. WITH PUMP OFF, CONTINUITY READS .2 OHMS. TURNED PUMP ON & LOW PRESS SWITCH DID NOT OPEN. PUMP IS RUNNING, BUT WILL NOT TRANSFER FUEL FROM CENTER TANK TO WING TANKS. SUSPECT RT CENTER BOOST PUMP SHAFT IS SHEARED. REQUIRES PUMP REPLACEMENT. MEL 2802D REAPPLIED. PLACARDS INSTALLED. R & R RT CENTER BOOST PUMP IAW AMM 28-22-41/401. BONDING CHECK REQUIRED. UNABLE TO ACCOMPLISH DUE SINGULAR REQUIR NOTED AT THIS TIME. REMOVED AND RESET CIRCUIT BREAKERS.TURNED ON PUMP & VERIFIED LOW PRESSURE LIGHT EXTINGUISHED. PUMP FOLLOWED SWITCH COMMANDS.TRANSFERRED 14000 LBS OF FUEL FROM THE CENTER TANK BACK TO BOTH WINGS USING ONLY RIGHT CENTER FUEL PUMP. NO DEFECTS
GEAR FAILED TO RETRACT DEBRIEFED CREW ALTERNATE LANDING GEAR EXTENSION ACCESS PANEL IN COCKPIT NOT FLUSH. PANEL SWITCH NOT PROPERLY ACTIVATING REF AMM 32-34-00-820-802. SSM 32-35-11-101. FOUND MANUAL EXTENSION SYSTEM ACCESS DOOR SWITCH WITHIN LIMITS PER AMM 32-34-00-820-802. REMOVED AND REPLACED BOTH SCREWS AND STUDS ON DOOR ASSEMBLY PER AIPC 52-00-51-03. DOOR ASSEMBLY LATCH OPERATIONAL CHECK GOOD. PERFORMED MAIN LANDING GEAR OPERATIONAL TEST PER AMM TASK 32-32-00-710-801, OPERATIONAL CHECK PASSED. PENDING PROXIMITY SWITCH ELETRONICS UNIT BITE TEST. PERFORMED PSEU BUTE TEST. TEST PASSED REF AMM 32-09-10.
GEAR FAILED TO RETRACT DEBRIEFED CREW ALTERNATE LANDING GEAR EXTENSION ACCESS PANEL IN COCKPIT NOT FLUSH. PANEL SWITCH NOT PROPERLY ACTIVATING REF AMM 32-34-00-820-802. SSM 32-35-11-101. FOUND MANUAL EXTENSION SYSTEM ACCESS DOOR SWITCH WITHIN LIMITS PER AMM 32-34-00-820-802. REMOVED AND REPLACED BOTH SCREWS AND STUDS ON DOOR ASSEMBLY PER AIPC 52-00-51-03. DOOR ASSEMBLY LATCH OPERATIONAL CHECK GOOD. PERFORMED MAIN LANDING GEAR OPERATIONAL TEST PER AMM TASK 32-32-00-710-801, OPERATIONAL CHECK PASSED. SWITCH ELETRONICS UNIT BITE TEST. PARTS USED: 00-0583-3-6842,QTY :1 00-0593-3-8072,QTY :1 PERFORMED PSEU BUTE TEST. TEST PASSED REF AMM 32-09-10.
RF DOOR SLIDE REPLACED. ROTABLE PARTS TRANSACTION REQ'D. REPLACED DOOR SLIDE REF TASK CARD 29-2560-1-9800. FOR INSTALLATION.PARTS USED: 29-2566-9-0007,QTY :1.ROTABLE PARTS CHANGE WAS INDICATED - TT # 1333949 SN OFF 2648 .SLIDE, FWD/AFT OFF 29-2566-9-0007 2648 ON 29-2566-9-0007 2450
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - IN SEAT LIGHTS AT ROWS 15, 20 & 21 DO NOT COME ON. FOUND BAD FUSE ON M1694 BATTERY PACK. R/R FUSE 2 ON M1694 REF AMM TASK 33-51-06-960-804, OPS CHECK OK
HF 1 RADIO RECEPTION AND TRANSMISSION PROBLEM AT ALL STATIONS UNABLE TO TRANSMIT ON HF1 OR HF2 PERFORMED SYSTEM TEST REF AMM HF COMMUNICATION SYSTEM - SYSTEM TEST REFERENCE: TASK 23-11-00-730-801. OPS GOOD TRANMISSION AND RECEIVE CLEAR.
EMERGENCY LIGHT BATTERY PACK M2627 FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED BATTERY PACK M2627 IAW AMM 33-51-06- 960-805, OPS CHECKED GOOD.
PASSENGER CABIN, EMERGENCY LIGHTS BATTERY PACK M1674 FAILS OP CHECK. REMOVED AND INSTALLED NEW EMERGENCY BATTERY PACK LIGHTS POS M1674 IAW B737 AMM 33-51-06-960-805 TEST GOOD.
EMERGENCY LIGHT BATTERY PACK M2626 FAILED FUNCTIONAL CHECK (REF. AAR NR 100004655). REMOVED AND REPLACED BATTERY PACK M2626 I.A.W B737 AMM 33-51-06- 960-805. OPS CHECK PASS GOOD.(WORK ACCOMPLISHED BY V936440 AND A AR QC A-15)
EMERGENCY LIGHTS BATTERY PACK M1673 FAILS OP CHECK (REF. AAR NR 100004741). REMOVED AND REPLACED EMERGENCY BATTERY PACK M1673 IAW B737 AMM 3 3-51-06-960-805, OPS TEST GOOD.
EMERGENCY LIGHT BATTERY PACK M1695 FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M1695 IAW B737 AMM 3 3-51-06-960-805. OPS TEST GOOD.
EMERGENCY LIGHT BATTERY PACK M2503 FAILED FUNCTIONAL CHECK. REMOVED AND REPLACED EMERGENCY BATTERY PACK M2503 IAW B737 AMM 3 3-51-06-960-805 OPS TEST GOOD.
EMERGENCY LIGHT BATTERY PACK M1676 FAILED FUNCTIONAL CHECK (REF. AAR NR 100004644). REMOVED AND INSTALLED NEW BATTERY PACK IAW B737 AMM 33-51-06-960-802, OPS CHECK GOOD (SDR # 1035722) (WORK ACCOMPLISHED BY V934563 AND AAR QC A-16 V931820).
FOUND CRACK ON THE LH WINDOW POST AFTER NDT WAS PERFORMED PER EA 5310-04554 REV C (REF. AAR NR 100004994)
EMERGENCY LIGHT BATTERY PACK M1672 FAILED FUNCTIONAL CHECK. (REF: AAR NR 100004640) REMOVED AND INSTALLED NEW BATTERY PACK M1672 IAW B737 AMM 33-51-06-960-805. TEST GOOD. (WORK ACCOMPLISHED BY V936334 & AAR QC A-14 V935540) ADD EMP:V936334
DR 2 LEFT EXTERIOR EMERGENCY LIGHT NOT ON DURING EMERGENCY LIGHT TEST. RELAMPED WITH #767 BULB. WORKS OK.
PACK TRIP OFF LIGHT LIGHT ON AT CRUISE, LIGHT COMES ON AGAIN AFT ER RESET LEFT REQUESTING DEFERAL. ACCOMPLISHED LEFT RAM AIR DOOR ACTUATOR DE-ACTIVATION REF DDG 21-00-00-040-806. MEL APPLIED COMPLIED WITH - TOMC APPROVED PERFORMED BITE OF LT ZTC. BITE WAS GREEN, PREV FLT FAULT GREEN. VERIFY SHOWS RAM AIR ACT FAULT. AND WILL NOT RESET. REQUESTING DEFERAL 2105G. REMOVED AND REPLACED LEFT RAM AIR INLET ACTUATOR INSTALLATION REFERENCE: TASK 21-51-21-400-801.OPS NORMAL PLACARED REMOVED. PARTS USED: 29-2151-9-0011,QTY :1 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1686578 SN OFF 5964 ACTUATOR, RAM A OFF 29-2151-9-0011 5964 ON 29-2151-9-0011 8036
LE FLAP TRNST LT TE FLAPS NORMAL LE DEVCS OUT AT F330 W FLP HNDL UP. CREW REPORTED THAT THERE WAS NO ROLL INDUCED ONCE FAUL PS AND SLATS OPERATE AS COMMANDED WITH PROPER CORRESPONDING INDICATIONS. CONTINUED.. FAULT CLEARED ON FSEU. PERFORMED INITIAL EVALUATION, FSEU BITE PROCEDURE PERFORMED PER TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND SLATS HAD NO FIM 27-81 TASK 806. RESET BEAKERS P6-2 A8 AND A9. CONTINUED SYMMETRY ISSUES. TRAILING EDGE FLAPS, LEADING EDGE FLAPS AND WITH FIM EVALUATION ALL TESTS PASSED. CREW REPORTED THAT THERE SLATS OPERATE AS COMMANDED WITH PROPER CORRESPONDING WAS NO ROLL INDUCED ONCE FAULT WAS INDICATED. INDICATIONS. NO CURRENT FAULTS ON FSEU.
L/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 138.70, 10" FWD OF REAR SPAR & INBD OF DRAIN HOLE, CRACK LENGTH :0.276" REF AAR NR 9643094 ACCOMPLISHED REPAIR AT STA 138.70 REF B737-900 SRM 55-10-01-2R- 11, INSPECTION REQUIREMENTS VISUAL AND LFEC INSPECT EVERY 9,000 FLIGHT CYCLES WORK ACCOMPLISHED BY V900829 RII UPDATE RII ACCOMPLISHED CYCLES AS WELL AS THE REPEAT CONCURRENT INSPECTION AT 9,000 FLIGHT CYCLES. ITEM PLACED ON DIP IAW B SRM 55-10-01-2R-11 STEP.5, REPAIR 11 DIP 55-DIP SRM 55-10-01-2R-11 R2 TABLE 204 REQUIRES AN DVI AND TABLE 204 FIGURE 206. LFEC INSPECTIONS AT AN INSPECTION THRESHOLD OF 56,000 FLIGHT TOMC APPROVES DIP FOR REPAIRS MADE TO L/H HORIZ STAB - CRACK TOMC-APPROVAL FROM SC1ELBYC COMMENT FOUND AT STAB STA 138.70, 10" FWD OF REAR SPAR & INBD OF DRAIN HOLE, CRACK LENGTH :0.276". CATEGORY B REPAIR INSPECTION REQUIREMENTS, INSPECTION THRESHOLD 56,000 TOTAL FLIGHT CYCLES, REPEAT INSPECTION AT INTERVAL 9,000 FLIGHT CYCLES FOR DVI AND LFEC INSPECTION PER SRM 55-10-01-2R-11 STEP 5. TABLE 204 DIP 55-DIP IN REFERENCE WITH SRM 55-10-01-2R-11 TABLE 204 AN INSPECTION THRESHOLD IS REQUIRED FOR A DVI AND LFEC AT 56,000 FLIGHT CYCLES AS WELL AS A REPEAT CONCURRENT INSPECTIONS AT INTERVALS OF 9,000 FLIGHT CYCLES. QC REVIEWED QC REVIEWED RECORDS UPDATE RECORDS UPDATE RECORDS UPDATE INIT: 56,000 TAFC WILL ITO TO RIR(-0743) RIR: DVI AND LFEC EVERY 9,000 FC...LN/U253409
L/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 138.70, 10" FWD OF REAR SPAR & INBD OF DRAIN HOLE, CRACK LENGTH :0.276" REF AAR NR 9643094 ACCOMPLISHED REPAIR AT STA 138.70 REF B737-900 SRM 55-10-01-2R- 11, INSPECTION REQUIREMENTS VISUAL AND LFEC INSPECT EVERY 9,000 FLIGHT CYCLES WORK ACCOMPLISHED BY V900829
R/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 92.70, 2.5" FWD OF REAR SPAR O/B OF DRAIN HOLE AND PARALLEL WITH REAR SPAR. CRACK LENGTH : 1.417" REF AAR NR 9643096 WORK ACCOMPLISHED BY V934372 ACCOMPLISHED REPAIR RH HORIZONTAL STAB STA 95 IAW B737-900 SRM 55-10-01-2R-11 AND INSTALLED REPAIR FILLER AND DOUBLER INSPECTION REQUIRED 9000 FLIGHT CYCLES PER 55-10-01-2R-11 TABLE 204/REPAIR 11 AND 206/REPAIR 11
R/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 92.70, 2.5" FWD OF REAR SPAR O/B OF DRAIN HOLE AND PARALLEL WITH REAR SPAR. CRACK LENGTH : 1.417" REF AAR NR 9643096 WORK ACCOMPLISHED BY V934372 ACCOMPLISHED REPAIR RH HORIZONTAL STAB STA 95 IAW B737-900 SRM 55-10-01-2R-11 AND INSTALLED REPAIR FILLER AND DOUBLER INSPECTION REQUIRED 9000 FLIGHT CYCLES PER 55-10-01-2R-11 TABLE 204/REPAIR 11 AND 206/REPAIR 11 RII ACCOMPLISHED RII ACCOMPLISHED RII UPDATE ADD EMP:V891438
(B737 -55-3-0239) RH HORIZONTAL STABLIZER INSPAR RIB AT STA 101.0 HAS CRACK AT FWD UPPER WEB EDGE WHERE IT MEETES THE T-CHORD. REF AAR NR 9644092 ACCOMPLISHED REPAIR AT RIGHT HORIZONTAL STAB AT STA 101.0 REF B737-900 SRM 51-40-02-0G-0 AND RES-WI 2017928-30 AND EC/RA 5510-03080 WORK ACCOMPLISHED BY V934372
(B737-55-3-0239) R/H HOR. STAB INSPAR RIB AT STAB STA 92.70 STIFFINER NO. 3 LOWER SECTION WITH WITH A CRACK REF AAR NR 9643436 REMOVED DAMAGE AREA, INSTALLED 1EA REPAIR ANGLE AND 1EA REPAIR T-SECTION ON R/H HOR STAB RIB AT STAB STA 92.70 STIFFNER 3 LOWER SECTION AS PER B737-900ER SRM 55-10-09-2R-4 WORK ACCOMPLISHED BY V920362
L/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 193.90, 10" FWD OF REAR SPAR & I/B OF DRAIN HOLE, CRACK LENGTH :0.984" REF AAR NR 9643095 ACCOMPLISHED REPAIR AT HORIZONTAL STAB STA 193.90, REF B737-900 SRM 55-10-01-2R-11. INSPECTION REQUIREMENTS VISUAL AND LFEC INSPECT EVERY 9,000 FLIGHT CYCLES WORK ACCOMPLISHED BY V900829
SUPPORT TASK - R/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 157, 9.5" FWD OF REAR SPAR & I/B OF DRAIN HOLE .CRACK LENGTH : 0.433" REPAIR 11 AND FIGURE 206/ REPAIR 11 REF NR 9643097 REMOVED CRACK ON R/H HORIZONTAL STAB STA-157 I.A.W B737-900 SRM 55-10-01-2R-11 FIGURE 204, DETAIL F, INSTALLED REPAIR DOUBLER. INSPECTION REQUIERED 9,000 FLIGHT CYCLES PER 55-10-01-2R-11 TABLE 204/ ADD EMP:V900541
SUPPORT TASK - R/H HORIZONTAL STABILIZER - CRACK FOUND AT STAB STA 166.30, 10" FWD OF REAR SPAR & I/B OF DRAIN HOLE ,CRACK LENGTH : 0.669" TABLE 204/ REPAIR AND FIGURE 206/ REPAIR 11 REMOVED CRACK ON R/H HORIZONTAL STAB STA-175 I.A.W B737-900 SRM 55-10-01-11 FIGURE 204, DETAIL F AND INSTALLED REPAIR DOUBLER. INSPECTION REQUIERED 9,000 FLIGHT CYCLES PER 55-10-01-2R-11 ADD EMP:V934372
L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 CRACKED AT LOWER END REF AAR N/R 9643347 REMOVED DAMAGED AREA INSTALLED 1EA REPAIR ANGLE AND 1EA T SEC ON THE L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 LOWER END AS PER B737 SRM 55-10-09-1R-4 INSTALLED I/B WEB AS PER B737 SRM 51-40-02 WORK ACCOMPLISHED BY V920362
SUPPORT TASK-NDT INSPECTION FOUND A CRACK AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64,BETWEEN WL192.0 AND WL 200.6 CRACK LENGTH 0.394IN REF AAR NR 9643110 INICIAL WEB CUTOUT IN REFERENCE WITH B737-900ER REPAIR AREA. FABRICATED REPAIR PARTS IN REF WITH AT CENTER WING REAR SPART VERTICAL PRESSURE WEB AT SRM 57-10-10-2R-3 REPAIR 3 FIG 204, PERFORMED ADVI B737 SRM 57-10-10-2R-3, DOUBLER #2, FILLER #3, RBL 40 IN REF WITH B737-900ER SRM 57-10-10-2R-3 OF REPAIR AREA IN REF WITH B737 SRM 51-10-02, FILLER #4, WEB #1 AND LOCATED AND DRILL #1 REPAIR AND INSTALLED PRESSURE RESERVOIR AND SPOILER PERFORMED HFEC INSPECTION ALONG THE CUT EDGES OF WEB DOUBLER AND TREATED PARTS AND INSTALLED REPAIR CONTROL VALVE. WORK ACCOMPLISHED BY V891116 REMOVED HYDRAULIC SYST B RESERVOIR IAW B737-900ER AMM 29-11-31 AND REMOVED GROUND SPOILER CONTROL VALVE IAW B737-900ER AMM 27-62-41, REMOVED FASTENERS AND ANGLE TO GAIN ACCESS TO REPAIRED
RT HORIZONTAL STAB RIB AT STA 101 LOWER CHORD I/B FASTNER HOLE HAS A SMALL CRACK JUST BELOW CENTER LIGHTING HOLE REF AAR N/R 9644094 REMOVED ANGLE AREA INSTALLED 1EA REPAIR ANGLE ON R/H HORIZONTAL STAB RIT AT STA 101 LOWER CHOED AS PER B737 SRM 55-10-09-2R-5 FIG 204 SHEET 1 WORK ACCOMPLISHED BY V920362
SUPPORT TASK-NDT INSPECTION FOUND A CRACK AT CENTER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN RBL 40.00 AND RBL 45.64,BETWEEN WL192.0 AND WL 200.6 CRACK LENGTH 0.394IN REF AAR NR 9643110 INICIAL WEB CUTOUT IN REFERENCE WITH B737-900ER REPAIR AREA. FABRICATED REPAIR PARTS IN REF WITH AT CENTER WING REAR SPART VERTICAL PRESSURE WEB AT SRM 57-10-10-2R-3 REPAIR 3 FIG 204, PERFORMED ADVI B737 SRM 57-10-10-2R-3, DOUBLER #2, FILLER #3, RBL 40 IN REF WITH B737-900ER SRM 57-10-10-2R-3 OF REPAIR AREA IN REF WITH B737 SRM 51-10-02, FILLER #4, WEB #1 AND LOCATED AND DRILL #1 REPAIR AND INSTALLED PRESSURE RESERVOIR AND SPOILER PERFORMED HFEC INSPECTION ALONG THE CUT EDGES OF WEB DOUBLER AND TREATED PARTS AND INSTALLED REPAIR CONTROL VALVE. WORK ACCOMPLISHED BY V891116 REMOVED HYDRAULIC SYST B RESERVOIR IAW B737-900ER AMM 29-11-31 AND REMOVED GROUND SPOILER CONTROL VALVE IAW B737-900ER AMM 27-62-41, REMOVED FASTENERS AND ANGLE TO GAIN ACCESS TO REPAIRED
RT HORIZONTAL STAB RIB AT STA 101 LOWER CHORD I/B FASTNER HOLE HAS A SMALL CRACK JUST BELOW CENTER LIGHTING HOLE REF AAR N/R 9644094 REMOVED ANGLE AREA INSTALLED 1EA REPAIR ANGLE ON R/H HORIZONTAL STAB RIT AT STA 101 LOWER CHOED AS PER B737 SRM 55-10-09-2R-5 FIG 204 SHEET 1 WORK ACCOMPLISHED BY V920362
L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 CRACKED AT LOWER END REF AAR N/R 9643347 REMOVED DAMAGED AREA INSTALLED 1EA REPAIR ANGLE AND 1EA T SEC ON THE L/H HORIZONTAL STAB STA 92.70 RIB NO.1 STIFFENER NO.2 LOWER END AS PER B737 SRM 55-10-09-1R-4 INSTALLED I/B WEB AS PER B737 SRM 51-40-02 WORK ACCOMPLISHED BY V920362
EMERGENCY EXIT CEILING LIGHT BETWEEN BOTH AFT LAVS INOP. RELAMPED, REF AMM 33-51-03, OPS CHECKED OK. ACCOMPLISHED THE INSPECTION OF EMERGENCY EXIT CEILING LIGHT BETWEEN BOTH AFT LAVS.
EMERGENCY EXIT SIGN AT DOOR 2R INOP. REPLACED LIGHT ASSY REF AMM 33-51-01-960-802. OPS GOOD. ACCOMPLISHED THE INSPECTION OF EMERGENCY EXIT LIGHT AT DOOR 2R.
EMER EXIT FLOOR PATHWAY LIGHT ON SEAT 8ABC INOP. RELAMPED REF AMM 33-51-11, OPS CHECKED OK. ACCOMPLISHED THE INSPECTION OF EMERGENCY FLOOR PATHAWAY LIGHT ON SEAT 8ABC.
EMERGENCY CABIN LIGHT COVERS MISSING. REPLACED MISSING LIGHT COVERS. EMERGENCY LIGHTS TESTED OK.
TWO CRACKS DETECTED WHILE PERFORMING VISUAL AND C-SCAN INSPECTIONS ON LT HORIZ STAB LOWER INSPAR SKIN AT STA 147.9 APPROX 11" AND 18" FROM T/E. ENDS OF CRACK MARKED. REPAIRED PER SRM 55-10-01 REPAIR 11.
TWO CRACKS DETECTED WHILE PERFORMING VISUAL AND C-SCAN INSPECTIONS ON RT HORIZ STAB LOWER INSPAR SKIN AT STA 101.9 APPROX 12" AND 21" FROM T/E. REPAIRED PER SRM 55-10-01 REPAIR 11.
RIGHT AFT OVERWING EMERGENCY SLIDE LIGHT INOP. RELAMPED IAW AMM 31-51-04. OPS CHECK OK.
AFT INBD FA JUMPSEAT EMERG FLASHLT- NO RED STATUS LIGHT, 1 AFT FLIGHT ATTENDANT JUMPSEAT INOP. REPLACED FLASHLIGHT BATTERY AMM25-00-00.
EMERGENCY EXIT LIGHT ABOVE FLIGHT DECK DOOR AND UPPER AND LOWER LIGHTS AT L1 DOOR WERE INOP. REPLACED BATTERY REF MM 33-51-06. OPS CKS NORMAL.
EMERGENCY EXIT SEAT TRACK LIGHTS INOP AT ROWS 8 THROUGH 14 AND 22 THROUGH 34 REPLACED EMER PWR BATTERY PACKS AT M1670,M2503 & M2626,REF AMM 33-51-06-960-805. OPS CK NORMAL.
RED EMERGENCY EXIT SEAT TRACK LIGHT MISSING AT 15C. REPLACED RED LENS AND BULBS AT 15C. OPS CHECKED NORMAL.
SUPPORT TASK, EPL LIGHTING IN FIRST CLASS INOPERATIVE. R & R BATTERY PACK PN D717-01-100, SN 67090, FROM LOCATION STATION 322 WL 291 RBL 7 M1674 WITH BATTERY PACK SN 146654. OPERATIONS CHECKED GOOD IAW AMM 33-51 -06.
RIGHT HORIZONTAL STAB REQUIRES ACCESS HOLES TO BE CUT IN LOWER SKIN AT STATION 129.50 FOR REPAIR 3 STIFFENER ON INTERNAL RIB. CORRECTED ACFT TAIL NR TO READ 428 FROM 434. INSTALLED REPAIR IAW ECRA5510-02467. PLACED ON DIP IAW SRM 55-10-01 REPAIR 11 PAGE 217 TABLE 204 INSPECTION THRESHOLD 56,000 FLIGHT CYCLES AFTER INSTALLATION. REPEAT INSPECTIONS 9,000 FLIGHT CYCLES.
LEFT HORIZONTAL STAB REQUIRES CUT OUT TO BE CUT IN LOWER SKIN FOR STATION 166-30 REPAIR OF NR 2 & 3 STIFFENERS ON INTERNAL RIB. PLACED ON DIP IAW SRM 55-10-01 REPAIR 11 PAGE 217, INSPECT THRESHOLD 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & REPEAT INSPECTION 9000 FLIGHT CYCLES.
LEFT HORIZONTAL STAB REQUIRES ACCESS HOLE TO BE CUT IN LOWER SKIN AT STATION 120.30 FOR REPAIR TO NR 3 & 4 STIFFENERS ON INTERNAL RIB. PLACED ON DIP IAW SRM 55-10-01 REPAIR 11 PAGE 217, INSPECT THRESHOLD 56000 FLIGHT CYCLES AFTER REPAIR INSTALLATION & REPEAT INSPECTION 9000 FLIGHT CYCLES.
FOUND 2 CRACKS COMMON TO THE NR 2 & 3 STIFFENERS ON THE LOWER SIDE, LT STAB STATION 166.30, IN SPAR RIB. REPAIRED IAW ECRA 5510-02467 REV A.
LEFT HORIZONTAL STAB, INSIDE STAB, RIB AT STATION 120.30 NR 3 & 4 STIFFENERS APPEAR TO BE CRACKED AT LOWER SIDE, NR 3 & 4 RIBS FROM LE. REPAIRED IAW ECRA 5510-02467 REV A.
RIGHT HORIZONTAL STAB, INSIDE STAB, RIB AT STATION 129.50 NR 3 STIFFENER APPEARS TO BE CRACKED AT LOWER SIDE, NR 3 RIB FROM LE. REPAIRED RT HORIZONTAL STAB IN SPAR RIB NR 3 STIFFENER IAW ECRA 5510-02467 REV A.
STATION 727B RBL 45.50 BOTH INBD & OTBD FASTENERS HOLES ON SEAT TRACK SHOWING CRACK INDICATION. FOUND DURING HFEC IAW EA5320 -02076. REPAIRED CABIN SEAT TRACK IAW ECRA 5320-02343.
STATION 727 LBL 45.50 INBD AFT FASTENERS SHOWS CRACK INDICATION FOUND DURING HFCE IAW EA5320-02076. REPAIR CABIN SEAT TRACK IAW ECRA 5320-02341.
STATION 727B LBL 24.75 INBD AFT FASTENER SHOWS CRACK INDICATION FOUND DURING HFEC IAW EA5320-02076. REPAIR CABIN SEAT TRACK IAW ECRA 5320-02340.
CABIN FLOOR SEAT TRACK STATION 727B RBL 24.75 REQUIRE REPAIR DURING ACCOMPLISHMENT OF EA5320-02076. REPAIR CABIN SEAT TRACK IAW ECRA 5320-02342.