N37437
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 Air Lines | Operator | 2019-08-05 – 2019-08-05 | Operator named in NTSB report |
| UNITED AIRLINES INC | Operator | 2019-08-05 – 2019-08-05 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
L1 DOOR EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M1675 BATTERY PACK IAW AMM 33-51-06, OPS CHECK NORMAL.
L2 EMERGENCY LIGHTS INOPERATIVE. REMOVED AND REPLACED M1673 BATTERY PACK IAW AMM 33-51-06. OPS CHECKED NORMAL.
RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REMOVED AND RELACED M1695 BATTERY PACK IAW AMM 33-51-06, OPS CHECKED NORMAL
BATTERY PACK INOP AT SEAT 31DEF ABOVE CELING PANEL. REMOVED AND REPLACED M2627 BATTERY PACK IAW AMM 33-51-06. OPS CHECK NORMAL.
MAIN CABIN RT SIDE,FRAME CRACKED AT BS 727D BETWEEN STRINGER S8R & S-9R. REPAIRED MAIN CABIN RT FRAME, BS 727D BTWN S8-9R IAW ECRA 5362-01042 AND REO-G25793, REV IR.
BATTERY PACK INOPERATIVE AT SEAT 29ABC ABOVE CEILING PANEL. REMOVED AND REPLACED M2626 BATTERY PACK IAW AMM 33-51-06, OPS CHECKED NORMAL.
MAIN CABIN RT SIDE, FRAME CRACKED AT BS 727D BETWEEN STRINGER S-8R & STRINGER S-9R. REPAIRED THE FRAME AT BS 727D BETWEEN S-8R AND S-9R IAW EC/RA 5362-01042, & REO-G25793, REV IR.
MAIN CABIN FLOORBEAM BS 987, LBL 2L - RBL 2R, TWO EACH HOLES ARE IN A PREVIOUS FLOORBEAM REPAIR. REPAIRED THE MAIN CABIN FLOORBEAM AT BS 987 LBL 2 - RBL 2 IAW REO-G25823, REV IR, & EC/RA 5370-01218.
MAIN CABIN SEAT TRACK AT RBL45 STA 727E- 727F HAS CORROSION. REPAIRED MAIN CABIN SEAT TRACK AT RBL45 STA 727B TO 727I IAW SRM 53-00-52-2R-5 CATEGORY A REPAIR NO FURTHER INSPECTION REQUIRED DOT REMOVED.
FWD CARGO BAY LT TRANSITION PANEL FROM BS 500C+15 - 500L, LBL 21 CORRODED. THE CORRODED AREA ON THE TRANSITION PANEL FROM BS 500C+15 - 500K, LBL 21 FOUND TO BE 100% MATERIAL LOSS IN MULTIPLE AREAS IAW SRM 53-00-53-1A-2, FIG 103, REMOVED DAMAGED TRANSITION PANEL.
MAIN CABIN SEAT TRACK AT RBL 45, BS 847 -877 CORRODED. REPAIRED SEAT TRACK IAW SRM 53-00-52-2R-5, REPAIR 5.
COCKPIT AFT OF PEDESTAL FLOOR PANEL, SKIN HAS SEVERAL DENTS AND BARE METAL. REPAIRED COCKPIT FLOOR SKIN IAW REO-G25794, REV IR, & EC/RA 5310-08803.
REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL 45.64 AND LBL 40.00 CRACKED. REPAIRED CENER WING REAR SPAR VERTICAL PRESSURE WEB BETWEEN LBL45.64 AND LBL40.
MAIN CABIN SEAT TRACK, LBL 45, BS 727B - 727C CORRODED AND GOUGED, REMOVED AND REPLACED THE SEAT TRACK IAW SRM 53-00-52-2R-5.
R-1 DOOR, HANDLE BOX CUTOUT, LOWER TORQUE TUBE BUSHING STUB BEAM IS GOUGED. REMOVED WORN STUB BEAM AND INSTALLED NEW STUB BEAM REFERENCE DWG 141A6525 AND SRM 51-40-02, RESTORED FINISH, REFERENCE AMM 51-21-99.
R1 DOOR, HANDLE BOX CUTOUT, UPPER TORQUE TUBE BUSHING STUB BEAM IS GOUGED. REMOVED AND REPLACED THE STUB BEAM IAW DWG 141A8525 REV B AND 141A6516 REV B.
MAIN CABIN AFT WET AREA, ONE WEB CORRODED ON UPPER SURFACE BETWEEN BS 986.5 AND BTWN RBL 24 & 45. R & R THE WEB SUPPORT IAW DWG 147A5116, REV-, SRM 51-40-02.
B737-MP-20FW-53-820-00: FWD CARGO COMPARTMENT L/H TRANSITION PANEL FROM STA 500C+15 TO 500L LBL 21.0 IS CORRODED. TRANSCRIBED FROM AAR GSO NON-ROUTINE 9286411 THE CORRODED AREA ON TRANSITION PNL FROM STA 500C+15 TO 500K LBL 21 FOUND TO BE 100% MATERIAL LOSS IN MULTIPLE AREAS IAW ER SRM 53-00-53-1A-2 FIG 103, REMOVED DAMAGE TRANSITION PNL FROM FWD CARGO STA 500C+15 TO STA 500J+10 LBL21 IAW SRM 51-40-02 MATERIAL ID FOR NEW TRANSITION PNL AND NEW SPLICE IS PN BAC 1496-444 7075 T6 EXTRUSION PO: 1138312.1 IAW B737-900ER 53- 00-53-2R-5 TABLE 201, TRIMED AND LOCATED+DRILLED 1EA TRANSITION PNL AND 1EA SPLICE IAW SRM 53-00-53-2R-5 AND IAW B737-900ER SRM 51-40-05, ALODINED AND PRIMED 1EA TRANSITION PNL AND 1EA SPLICE IAW SRM 51-20-01, INSTALLED 1EA TRANSITION PNL AT FWD CARGO STA 500C+15 TO STA 500J+10 LBL 21 AND INSTALLED 1EA SPLICE AT FWD CARGO STA 500K TO 500J LBL 21 IAW SRM 53-00-53-2R-5 AND IAW B737-900ER SRM 51-40-02 INSTALLED NUTPLATES ON TRANSITION PNL AND SPLICE AND CURE TIME COMPLETED 24HRS IAW BAC DWG #140N4500 REMOVED DOT #X905
MAIN CABIN FLOOR SUPPORT INTERCOSTAL BETWEEN STA 312 AND 328 IS CRACKED ON THE FLOOR UPPER ATTACH FLANGE AT APPROX LBL45. LOCATED AND DRILLED INTERCOSTAL IAW SRM 51-40-05. REMOVED AND REPLACED CRACKED FLOOR SUPPORT AT BS 312 AND STA 328 IAW DWG 141A5400 IAW SRM 51-40-02.
R2 DOOR CUTOUT AREA, INNER CHORD HAS CORROSION ON UPPER SURFACE BETEWEEN BS 947 TO 986.5 APPROX. RBL-56. REMOVED AND REPLACED INNER CHORD AT R2 DOOR CUTOUT AREA BETWEEN BS947 TO 986.5 RBL56 PART NUMBER 147A8540Y3D PO NO. 1140348.18 IAW B737-900 SRM 51-40-02 AND BOEING DRAWING 147A8501 REV:-
MAIN CABIN AFT WET AREA WEB HAS CORROSION ON UPPER SURFACE BETWEEN BS 986.5 AND BETWEEN LBL-24 & LBL-45. R & R NEW WET SUPPORT IAW DWG 147A5116, REV.A, SRM 51-40-02.
B737-MP-2000-53-380-00 MAIN CABIN FLOOR SUPPORT BETWEEN BS 277 & 294.5 WAS CRACKED ON FLOORBOARD UPPER ATTACH FLANGE AT APPROX RBL 1. REPLACED FLOOR SUPPORT, BS 277 - 294.5 RBL 1 IAW DWG 141A540 REV-, SRM 51-40-05, SRM 51-40-02.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 312 & 328 CRACKED ON THE UPPER ATTACH FLANGE AT APPROX RBL31. RECEIVED A NEW INTERCOSTAL IAW AIPC 53-42-00-59D. LOCATED AND DRILLED FLOOR SUPPORT IAW SRM 51-40-05. INSTALLED THE FLOOR SUPPORT BS 312 - 328 IAW DWG 141A5400, & SRM 51-40-02.
ONE WIGGLE PLATE IS CRACKED ON RT WING REAR SPAR LOWER CHORD AT APPROX ORSS 290. REMOVED AND REPLACED THE ONE WIGGLE PLATE IAW SRM 51-40-02 & DWG 115A3700, REV B.
MAIN CABIN FLOOR SUPPORT BETWEEN BS 344 & 360 CRACKED ON UPPER ATTACH FLANGE AT APPROX BL 0. R & R THE FLOOR SUPPORT IAW SRM 51-40-02, & DWG 141A5400, REV -.
DOOR WARNING ANNUNCIATOR IS ON EQUIP LIGHT ILLUMINATED INFLIGHT. PRESSURIZATION REMAINS NORMAL. PERFORMED FIM TASK 52-10 TASK 802, PERFORMED PSEU OPS CK IAW MM TASK 32-09-10-710-801.NO FAULTS DETECTED AFTER RUNNING TEST.NO FURTHER MX ACTION REQ.OK TO CONT
RH MID PLUG DOOR FWD AND AFT BONDING STRAP LUGS AND HARDWARE ARE CORRODED AT WEB ATTACH POINTSREMOVED CORROSION AS PER SRM 53-60-15-1A-2 PARAGRAPH 4.D.3 REWORKED AREA REQUIRES THICKNESS CHECK. INSPECTED THE FWD AND AFT BLEND-OUTS PER NDT/NTM 00-04/ PART-4-00-04-02 ULTRASONIC INSPECTION OF THIN MATERIALS WITH OLYMPUS 35, THE THINNEST PART OF THE FWD BLEND-OUT IS 0.055 INCH AND THE THINNEST PART OF THE AFT BLEND-OUT IS 0.056 INCH. ACP GRID MAP THICKNESS MEASUREMENTS OF FWD AND AFT REPAIR AREAS REF NTM PART 4-00-04-02 . THINNEST MATERIAL WAS 0.052 INCH AT FWD REPAIR AREA AND 0.056 INCH AT AFT REPAIR AREA. GRID MAP MEASUREMENT PICTURES ATTACHED. AFTER EVALUATION FOUND ALLOWABLE DAMAGE OF 10%, MATERIAL THICKNESS IS 0.063'', ON THE AFT SIDE DEEPEST POINT IS 0.056'' WHICH IS 11.2%. ON THE FWD SIDE DEEPEST POINT IS 0.052'' WHICH IS 18%. FOUND TO BE OUT OF LIMITS AS PER SRM 53-60-15-1A-2 PARAGRAPH 4.D.(3) FIGURE 103. PART REQUIRES REPLACE. REMOVED FWD SEAL RETAINER REF SRM 51-40-02. REMOVED CENTER SEAL RETAINER REF SRM 51-40-02. REMOVED DAMAGED WEB ASSY REF SRM 51-40-02. CLEANED AREA AND PREPARED HOLES FOR HFEC. REF SRM 51-10-02-0G-0 PARAGRAPH 11. MATERIAL ID FOR WEB 7075 T6. THICKNESS 0.063" REF DWG 146A8702-1 MATERIAL ID FOR WEB 7075 T6. THICKNESS 0.063" PO: 1566166. REF DWG 146A8702-1 COMPLETED HFEC PER SRM 51019002-0G-0 PAR. 11 TO ZERO TIME THE HOLES, PER HFEC ROTARY HOLE PER NDT 6-51-00-00 P16 AND COUIINSTALLED NEW WEB AND COMPLETED ESFR
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - FOUND EMERGENCY AISLE LIGHT ABOVE ROW 9 INOP, AND AISLE LIGHT ABOVE ROW 12 TURNING ON AND OFF INTERMITTENTLY. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY PACK AT POWER SUPPLY M01676, REF WDM 33-51-12-6 AND AMM 33-51-06-960-805. NO FIX. REMOVED AND REPLACED FUSES AT POWER SUPPLY M01676, REF AMM 33-51-06-960-804. NO FIX. REMOVED AND REPLACED POWER SUPPLY M01676, REF 33-51-06-960-806. NO FIX. REQUIRES FURTHER TROUBLESHOOTING.PARTS USED: 29-3351-3-0031,QTY :1 99-3351-3-0015,QTY :1 REQUESTING TO DEFER PER MEL 3315A TOMC APPROVED 2 BULLNOSE LIGHTS INOP, NOT OPPOSITE EACH OTHER INSTALLED INOPERATIVE STICKER ADJACENT TO EMER EXIT LIGHTS SWITCH ON THE FORWARD OVERHEAD PANEL AND ADJACENT TO EMER EXIT LIGHT SWITCH AT DOOR 2L FLIGHT ATTENDANT PANEL.
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - R/H FWD OVERWING EMERGENCY LIGHT INOP. RELAMPED R/H FWD OVERWING EMERGENCY LIGHT PER MM 33-51-04. OPS CHECK GOOD.
EQUIPMENT DOOR LIGHT CAME ON CLIMBING PASSING 9500 FEETATTEMPTED TO OPEN EQUIPMENT DOOR. FOUND DOOR TO BE DIFFICULT TO OPEN FOUND NO FAULT CODE ON PSEU BITE IN REFERENCE TO FIM 32-62 TASK 801 RANG AND MEGGER WIRES FROM PSEU CONNECTORS D10986 PIN 6, D10988 PIN 6 TO DOOR SWITCH S197 & S196 & TO CONNECTOR D1406 PIN 6. WDM 52-71-12-4 PG 4 & SSM52-71-12-103 PG103. D10986 AND D10988 CONNECTORS SECURED TO PSEU & D1406P SECURED TO P5-20 ( DOOR WARNING ANNUNICATOR PANEL). PER TST REQUEST CHANGED S197 SWITCH IAW WDM 52-71-12-04. REMOVED E&E DOOR FOR CONDITIONAL INSPECTION. PRESSURE SEAL IS IN SERVICEABLE CONDITION. ALL ROLLERS, TRUCKS, & BEARINGS ARE IN GOOD CONDITION. OPS OF LOCKING MECHANISM AND PINS ARE WITHIN SERVICE LIMITS. RE-INSTALLED E&E DOOR. PERFORMED MULTIPLE OPERATIONAL CHECKS. DOOR OPENS & LOCKS IN PLACE WITH NO BINDING AND NORMAL EFFORT. E&E DOOR OPERATION IS IN SERVICEABLE CONDITION. REF AMM 52-48-41-200-801, AMM 52-48-41-200-802, AMM 52-48-41-00-801, AND AMM 52-48-41-400-801 PERFORMED CABIN PRESSURE LEAK TEST UP TO 4 PSI REF AMM 05-51-91-790-801. DOOR OPEN INDICATION LIGHT DID NOT COME ON. PERFORMED DETAILED INSPECTION OF FWD ACCESS DOOR. ALL STOPS ARE INTACT AND SAFETIED. THE DOOR HINGE BUSHINGS ARE WITHIN LIMITS AND THE DOOR SEAL IS PROPER CONDITION. OPS CHECKED DOOR MULTIPLE TIMES AND IT PASSESRECEIVED APPROVAL FROM TOM-C CONTROLLER AND SENIOR MANAGER TO CLEAR THIS DISCREPANCY.
PASSING 16000 FEET THE EQUIP WARNING LIGHT CAME ON FOUND DOOR CLOSED AND HANDLE STOWED. HAD TO PRY HANDLE OPEN FWD E&E DOOR HINGES ARE LOOSE AND WORN, BUSHINGS APPEAR TO BE REMOVED FWD ACCESS DOOR IAW AMM 52-48-31-000-801 TO INSPECT FOUND HANDLE TO BE LOOSE AND EXSESIVE FOR AND AFT PLAY IN WORN. DOOR BUSHINGS. NO DEFECTS NOTED IN BUSHINGS THEY ARE SLOTTED FOR HANDLE WHEN STOWING DOES NOT FEEL NORMALE. EASE OF OPENING DOOR. INSTALLED ORIGINAL FWD EQUIPMENT ACCESS DOOR IAW B737 AMM 52-48-31-400-801. REF LOGPAGES 8222470 & 8222495 FOR CORRECTIVE ACTION ON THE EQUIP DOOR WARNING LIGHT. DUE TO RETURN TO THE FIELD EVENT SUGGEST REPLACE MAIN E&E DOOR SENSOR, REF TASK 52-71-42-400-801. REF LP 8219983. REPLACED MAIN E&E DOOR SWITCH S187, OP CKS GOOD PER TASK 52-71-42-710-801.
CABIN ALTITUDE WAS SLOWLY RISING BUT NEVER EXCEEDED 10000 BITE OF DCPC SHOWED NO FAULTS. PERFORMED PRESSURIZATION CHECK PHASE 1 UP TO 4 PSI IAW AMM 21-00-05-780-801. AIRPLANE PRESSURIZED NORMALLY AND NO LEAKS WERE FOUND, NO FAULTS ON PSEU BITE. OK PER TASK 52-71-42-710-801.
2L DOOR HANDLE HARD TO DEPRESS COMPLETELY DOOR EXTERIOR HANDLE DIFFICULT TO OPERATE HARD TO CLOSE. REF TO FIN 52-10-810. INSPECTED DOOR AND FOUND FORWARD STOP PINS OUT OF ADJUSTMENT. ADJUSTED STOP PINS IAW AMM 52-13-00-820-801. CHECKED HANDLE TORQUE IAW AMM 52-13-00-700-805. DOOR OPERATES AND LATCHES NORMAL. VERIFIED ADJUSTMENT MADE TO DOOR AND DOOR HANDLE TORQUE ARE WITHIN LIMITS REF. AMM 52-13-00-700-805 AND GMM 09-25-05.
AFTER HFEC INSPECTION ON THE LH WINDOW FRAME AT THE UPPER AFT CORNER AND INNER CORNER RADIUS FOUND TO BE CRACK PER EA 5310-04554 REV B STEP 9.1 AND 9.2. (REF: AAR NR 99965475) SFR NO 1031988. PERFORMED CUT OUT ON LH WINDOW FRAME OF THE CRACK FOUND. (WORK ACCOMPLISHED BY V937984 AND AAR QC A-82 UPPER CORMER & INNER CORNER RADIOS IAW B737-900ER, UNITED V931568) EA 5310-04554, REV. B STEP 15.2, 15.3 FIG 7 CONF "B", NDT PERFORMED IAW B737 PART 6, 51-00-00 PROC 23, AFTER CUT OUT NO
EMEGENCY POWER PACK, M1670, FAILS EMERGENCY LIGHTING FUNCTIONAL CHECK. BATTERY DISCHARGES IN LESS THAN 5 MINS (REF AAR NR 99965141) REMOVED AND INSTALLED NEW BATTERY PACK (M1670) AND PERFORMED OPERATIONAL TEST GOOD IAW B737 AMM 33-51-06-960-805.
EMEGENCY POWER PACK, M1694, FAILS EMERGENCY LIGHTING FUNCTIONAL CHECK. BATTERY DISCHARGES IN LESS THAN 8 MINS (REF AAR NR 99965140) REMOVED AND INSTALLED NEW BATTERY PACK (M1694) AND PERFORMED OPERATIONAL TEST GOOD IAW B737 AMM 33-51-06-930-805.
EMEGENCY POWER PACK, M1673, FAILS EMERGENCY LIGHTING FUNCTIONAL CHECK. BATTERY DISCHARGES IN LESS THAN 10 MINS (REF AAR NR 99965142) REMOVED AND INSTALLED NEW BATTERY PACK ON M1673 IAW B737 AMM 33- 51-06-960-805, OPS CHECK GOOD.
AFTER HFEC INSPECTION ON THE LH WINDOW FRAME AT THE UPPER AFT CORNER AND INNER CORNER RADIUS FOUND TO BE CRACK PER EA 5310-04554 REV B STEP 9.1 AND 9.2. (REF: AAR NR 99965475)
EMERGENCY LIGHTING SYSTEM OPERATIONAL CHECK {B737-33-3-0235} - EXTERIOR EMERGENCY LIGHT AT R1 DOOR INOP. RELAMPED EMERGENCY LIGHT REF MM 33-51-04. OPS CK OK.
BIRDSTRIKE ON T/O CLIMBI NG THRU 2000 FT. 200KTS. LARGE BIRD 5FT SPAN HIT RT SIDE NOSE + WING. ACCOPLISHED BIRD STRIKE INSPECTION IAW SRM 53-00-01. FOUND DENT AT SECTION 41 STATION 219.8 W4" L380" D.085". ALLOWABLE DAMAGE 1 PARAGRAPH 4 SECTION 3 DENTS, DETAIL G TABLE 103 WITH IN LIMITS LESS THAN .125" NO REPAIR NESSESARY.
SUPPORT TASK: P/R (721771) MULTIPLE PASSENGER CABIN EMERGENCY LI GHTING ZONES FAIL TO ILUMINATE. REF BY PEMCO NR 2710N69 REMOVED AND REPLACED EMERNCY BATTERY PACKS AT ALL FWD, MID AND A FT LOCATIONS PER B737 AMM 33-51-06. TEST OK 12 EA. PACKS REPLICE D EQUIPMENT NO.5 M1672, M1673, M1674, M1675, M2626, M2627 TO CAPACITY CHECK FAIL.WRK PERFORMED BY P431, ENTERED, I NSP.
B737-35-3-0149 (ORANGE PARTS RACKS 11 SHELF C): O2 GEN 24LH FOUN D EXPENDED UPON. REF BY PEMCO NR 2710N359
(EA 5510-01843 REV H) R/H HORZ STAB, RIB STA 92.70 VERTICAL VERT ICAL STIFFENER NO.1 CRACKED.REF BY PEMCO NR 2710N315. REPAIRED RIB 92.70 ON R/H HORZ STAB IAW B737-900 ER SRM 55-10-09 4 PLACES PER NON-ROUTINE 2710N316 N317 AND N318 WRK PERFORMED B Y V915737, ENTERED Y V928371, INSP BY Q995 REPAIRED RIB 92.70 ON R/H HORZ STAB IAW B737-900 ER SRM 55-10-09 4 PLACES PER NON-ROUTINE 2710N316 N317 AND N318 WRK PERFORMED B Y V915737, ENTERED Y V928371, INSP BY Q995
RETURNED TO AIRPORT DUE TO STRONG ODOR ONCE A/C WAS AIRBORNE WIT H TAKEOFF THRUST PER FLT CREW DEBRIEF A/C UNDER MAX LANDING WEIGHT SMOOTH LANDING NORMAL SPEED. NO ABNORMAL INDICATIONS,"SMOKE SMELL"AND "LIGHT HAZE" DISSAPATED IN FLIGHT WITH NO REOCCURENCE PRIOR TO LANDING CREW COMPLETED SMOKE/ODOR QUESTIONAIRE. DUE TO WORK ON #2 ENG, OPENED COWLING AND CHECKED, NOTHING ABNORMAL FOUND, PERFORMED HIGH POWER RUN ON BOTH ENGS AND PACKS, NO ODOR, FOUND OVEN 204 WITH ODOR, REPLACED OVEN 204. ADD EMP:U54382 ROTABLE PARTS CHANGE WAS INDICATED - TT # 1013868 SN OFF 4359 OVEN, SMALL, ST OFF 99-2532-9-0001 4359 ON 99-2532-9-0001 8014
CREW REPORTS LOUD BANG FOLLOWED BY UNCOMMANDED SHUTDOWN OF THE RIGHT ENGINE, ENGINE WAS SUCCESFULLY RESTARTED AFTER APPROX 10 MIN, POSITIVE OIL PRESS MAINTAINED DURING WINDMILL. ENGINE OPERATED NORMALLY AFTER RESTART AND RESPONDED TO THRUST COMMANDS. CREW REPORTS NORMAL LANDING UNDER MAX LIMIT.ACP EEC BITE CK AND POWER ASSURANCE CK. ALL NORMAL.
L2 DOOR EMERGENCY EXIT SIGN LENS MISSING. REPLACED THE LENS.
EMERGENCY AISLE AREA LIGHTS AT 24DEF AND 27DEF ARE INOPERATIVE. REPLACED CHARGER AND BATTERY PACK. OPS CHECKED GOOD IAW AMM 33 -51-06.
RT FWD EMERGENCY EXIT EXTERIOR LIGHT INOP. RELAMPED OPS CHECK OK. OK TO CONTINUE.
RIGHT WING FWD OVERWING EMERGENCY LIGHT NOT WORKING. RELAMPED IAW AMM 33-51-04. OPS CHECKS GOOD.
STATION 727B LBL 45.5 SEAT TRACK FASTENERS HOLES DON`T HAVE EDGE MARGIN. TRIMMED, PERFORMED HFEC, FABRICATED REPAIR PARTS & INSTALLED ON SEAT TRACK FLANGE IAW ECRA 5320-02289.
SEAT TRACK FLANGE AT STATION 727B, RBL 45.50 INBD & OTBD HAVE NO ED IAW EA 5320-02076 & OP 3 - 4. TRIMMED, PERFORM HFEC, FABRICATED REPAIR PARTS & INSTALLED ON SEAT TRACK FLANGE AT STATION 727B RBL 45.50 IAW ECRA 5320-02289.
SEAT TRACK STATION 727B AT LBL 45.50 CRACKED AT HOLE COMMON TO SPLICE PLATE IAW EA 5320-02076 OP 3 STEP 4.1 C. TRIMMED, PERFORMED HFEC, FABRICATED REPAIR PARTS & INSTALLED ON SEAT TRACK FLANGE IAW ECRA 5320-02289.
STATION 727B LBL 24.72 SEAT TRACK FASTENERS HOLES DON'T HAVE EDGE MARGIN. TRIMMED, PERFORMED HFEC, FABRICATED REPAIR PARTS & INSTALLED ON SEAT TRACK FLANGE IAW ECRA 5320-02289.
WHEN PERFORMING A C SCAN INSPECTION ON RT HORIZ LOWER IN SPAR SKIN FOUND CRACK INDICATION AT SS 101.9 & 10 INCHES FROM AFT SPAR. SEE WIPS FOR DETAILS OF WORK ACCOMPLISHED. TRIMMED OUT CRACK & INSTALLED REPAIR DOUBLER IAW SRM 55-10-01 REPAIR 11. INITIATED DIP 28557 TO DO INSPECTION AS GIVEN IN TABLE 204 REPAIR 11 & FIG 206 AT 56000 FLIGHT CYCLES AFTER INSTALLATION & 9000 FLIGHT CYCLES INTERVALS THEREAFTER IAW SRM 55-10-01 REPAIR 11
MAIN CABIN FORWARD ENTRY DOOR (1L) JAMMED WILL NOT OPEN ON ARRIVING IN SJU REF PREV/WRITEUP 8503603 INSTALLED SCREW & WASHER IAW AMM52-11-21-410-802. ENSURE DOOR IS ADJUSTED PROPERLY IAW AMM52-11-00-820-801. ENSURE LATCH TORQUE TUBES, ADJ PROP IAW AMM52-11-00-820-802. PERFORM DOOR SYS TEST IA AMM52-11-00-200-809. INITIATE DIP IAW ECRA 5211-01163 TO PERF PERM REPAIR PER PART 3 WITHIN 1 FLT CYCLE. INSTALLED PROPER HARDWARE AS PER IPC 52-11-21-01, ECRA 5211-01163 AND AMM 52-11-21. OPS CHECKED DOOR 1L, NO DEFECTS NOTED. DIP CLOSED. "Q/C" ACCOMPLISH A PERMANENT REPAIR WITHIN 1 FLT CYCLE FROM DATE 10/02/2010 PER PART 3 OF ECRA 5211-01163. REMOVED INTERIM SCREW AND INSTALL SCREW P/N BACS12ER06K6. DIP C/N 07276 ISSUED.