N78009
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
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
81 reports on file, 1999-10-19 – 2026-08-27.
Part: BATTERY PACK — NO TEST (ZONE 200) · airframe 128,557 hrs · 13,186 cycles
EMERGENCY LIGHTS AROUND DOOR 3R GOES OFF AFTER FEW MINUTES BEING TESTED. TROUBLESHOOTED PER FIM 33-51 TASK 806 AND FOUND EMERGENCY POWER SUPPLY M33401 WITH BATTERY DISCHARGED. REPLACED BATTERY PACK OF POWER SUPPLY M33401 PER AMM TASK 33-51-06-960-802. LIGHTS OPS TESTED SATISFACTORILY.
Part: SEAL — MISSING (ZONE 500) · airframe 127,886 hrs · 13,112 cycles
LEFT INBORD FLAPERON SEAL MISSING ON ARR. CLEATED CDL LOG PG 9586033. NO OTHER DAMAGE NOTED. LEFT FLAPERON INBOARD SEAL MISSING 4 FOOT ADD PIC INFORMATION FOR PDA PAGE REF LP9586114 PREVIOUS PDA 3 LP 9586114 WRONG, SHOULD READ PDA 2 REF LP 9586228 4 FOOT OF SEAL MISSING ON ARR, REQUEST CDL DEFERRAL ITEM PLACED ON CDL, SEAL NIS HND DISPATCH DESK: 56 NAME: TA DATE: 13-JUL-26- APPROVED CDL 57DE
Part: COMPRESSOR — STALLED (RT ENGINE) · airframe 127,737 hrs · 13,096 cycles
RIGHT ENG COMPRESSOR STALL AND EGT EXCEEDANCE AT V1 REVIEWED AHM DATA, FOUND EGT DATA PEAKED AT 138.5 FOR 6 SECS. REF AMM 71-00-00-200-814-G00 7.C.(2)(B) TAKEOFF AND MAX CONTINUOUS EGT FIG 603, 1038.5 FOR 6 SECS PUTS US IN AREA B AND DOES NOT REQ IMMEDIATE ENGINE CHANGE. AREA B REQ'S A BSI OF THE HPT. ALSO, REVIEWED AHM DATA FOR PREVIOUS EXCEEDANCES, NONE NOTED.
Part: HMU — FAULTED (NR 2 ENGINE) · airframe 127,737 hrs · 13,096 cycles
RIGHT ENGINE COMPRESSOR STALLED ON ROTATION NO EXCEEDENCES. PERFORMED FAULT ISOLATION NR 2 ENG IAW FIM 71-05, TASK 807, STEPS A - E, NO DEFECTS NOTED. NR 2 ENGINE BORESCOPE PLUGS REMOVAL & INSTALL CONTINUED FAULT ISOLATION PROCEDURE ON FIM 71-05, TASK 807, STEP E (1) THRU (B) 2), ENG CONTROL RT OR ENG EEC C1 R MESSAGES NOT PRESENT. ALSO ON EXISTING SCHEDULED MAINTENANCE TASK SCREEN ENG EEC C2 R MSG NOT PRESENT. CONTINUED FAULT ISOLATION PROCEDURE ON FIM 71-05 TASK 807 - STEP E.(2). IP CHECK VALVE FOUND TO BE SERVICABLE. R & R NR 2 ENGINE HMU. CONTINUED WITH FIM 71-05 TASK 807 FROM STEP E.(6)(A). NO STATUS OR MX MESSAGES PRESENT. R & R NR 2 ENGINE HMU IAW AMM UP TO AND INCLUDING STEP. I. (11)(G)1). .
Part: CHARGER — FAULTY (ZONE 200) · airframe 127,708 hrs · 13,091 cycles
EMERGENCY LIGHTS - OPERATIONAL TEST WITH THE TEST SWITCHES PROCEDURE - EMERGENCY LIGHTS BETWEEN ROW 22 AND DOOR 3 RH DOES NOT GO ON. POWER SUPPLY REPLACEMENT IAW AMM 33-51-06-960-803. TEST OK.PARTS USED: 29-3351-3-0031,QTY :1
Part: BATTERY — INOPERATIVE (EPAS) · airframe 126,409 hrs · 12,953 cycles
EMERGENCY POWER ASSIST SYSTEM (EPAS) BATTERY - ELECTRICAL CHARGE CHECK (PED 1, 2, 3, 4) EPAS BATTERY ELECTRICAL CHARGE CHECK - EPAS BATTERY DOESNT BLINK. REQUIRES BATTERY REPLACEMENT REPLACED 9V BATTERY PACK IAW AMM TASK 52-11-20-400-806-002.
Earlier reports · 1999–2025 · 75 reports
2025
Part: SLIDE — NO DISCREPANCY (ZONE 800) · airframe 124,267 hrs · 12,737 cycles
SLIDE RAFT PRESSURE GAUGE NOT IN GREEN. THE PRESSURE INDICATOR NEEDLE IS IN THE GO BAND (GREEN).REF AMM TASK 52-11-22-200-801.
Part: SEALANT — DETERIORATED (ZONE 200) · airframe 124,206 hrs · 12,730 cycles
WHILE PRESSURIZING AIRCRAFT TO LEAK CHECK CAPT WINDSHIELD FOUND 3 LOCATIONS LEAKING. STARTED TO REMOVE SEALANT AND REMOVED WINSHIELD WIPER. SEALANT DID NOT APPEAR TO BE FULLY CURED HAD A CRUMBLY TEXTURE AND SMELLED UNCURED. REMOVED OLD SEALANT, RETORQUED AND RESEALED CAPT WINDSHIELD REF AMM 56-11-01. SEALED AT 01:30. LEAK CHECK STILL REQUIRED AFTER SEALANT CURES. PRESSURIZED AIRCRAFT TO 2 DPSI NO LEAKS NOTED. OPS CK GOOD, AMM 56-11-01
Part: STARTER — LEAKING (NR 1 ENGINE) · airframe 124,235 hrs · 12,734 cycles
OIL QTY LOW ENG 1. DROP TO ZERO IN FLT. LOSS OF 1 QT EVERY 20-25 MINS. REPLACED STARTER REF AMM 80-11-01. ACCOMPLISHED 10 MIN IDLE RUN NO EXTERNAL LEAKS NOTED.
Part: CIRCUIT BREAKER — NO DISCREPANCY (ZONE 200) · airframe 123,567 hrs · 12,661 cycles
PULLED C/B H9 EMERGENCY LIGHTS DOOR 1L, H10 EMERGENCY LIGHTS DOOR 2R, H11 EMERGENCY LIGHTS DOOR 1R & 2L, H16 EMERGENCY LIGHTS DOOR 3L, H17 EMERGENCY LIGHTS DOOR 3R, H18 EMERGENCY LIGHTS DOOR 4L & 4R ON P11 FOR EPAS BATTERY REPLACEMENT. CLOSED C/BS H9, H10, H11, H16, H17, H18 ON P11 AFTER EPAS BATTERY REPLACEMENT.
Part: SKIN — DENTED (ZONE 600 SLAT) · airframe 123,471 hrs · 12,650 cycles
FOUND DENT ON SLAT 13 DURING POST ARRIVAL WALK AROUND WIDTH 4", HEIGHT 1.5", DEPTH 0.085". NO LOOSE OR MISSING FASTERS. WITHIN 20" AND DENT DOES NOT CREASE ALONG UNDERLYING STRUCTURE. HFEC INSPECTION PERFORMED. ACCOMPLISHED ECRA 5740-03356 PART 1 INTERIM REPAIR.
2024
Part: DOOR — MISSING (ZONE 400) · airframe 120,906 hrs · 12,398 cycles
PDA 2 #1 ENGINE RH INBOARD TR MID PANEL 416FR HINGE AND SMALL DOOR ASSY FOUND MISSING ON ARRIVAL SEE LP 3042567. MISSING COMPONENT APPROX 6X3 INCHES, METALLIC IN CONSTRUCTION. A/C LANDED ON RUNWAY 1R AND AIRPORT OPS ADVISES RUNWAY CHECKED NO DEBRIS WAS FOUND INSTALLED REPLACEMENT DOOR AND HINGE ON EXISTING PANEL REF SRM 51-40-02 INSTALLED RH INBOARD TR MID PANEL 416FR REF AMM 78-31-09. ADD EMP:U416528
Part: SLIDE — UNKNOWN (ZONE 800) · airframe 120,838 hrs · 12,392 cycles
R2 PASSENGER DOOR WAS MADE SAFE AS INSTRUCTED IN AMM SUBTASK 52-11-26-860-001. INSTALLED SLIDE SAFETY PINS (2 EACH) ON DOOR R2. CORRECTION: REMOVED AND STOWED PINS (2 EACH). UNABLE TO PIN BOTTOM PIN DUE TO SLIDE NOT BEING DISARMED, IN REFERENCE TO AMM SUBTASK 52-11-26-860-001. RECONFIGURED DOOR R2 TO NORMAL POSITION. REVERSED AMM SUBTASK 52-11-26-860-001. C/B'S (2EACH) CLOSED. SWITCH IN ARM POSITION. PINS VERIFIED STOWED. ACP RII INSP OF DOOR 2 RH VERIFY DOOR CIRCUITS BREAKERS ARE IN, EPAS IS ARMED, DOOR LEVER IS IN THE DISARMED POSITION AND SAFTY PINS ARE STOWED IN THE POUCH. REF GMM 09-25-05.
Part: WARNING LIGHT — UNKNOWN (ZONE 800) · airframe 120,825 hrs · 12,391 cycles
DOOR FLIGHT LOCK 2R EICAS STATUS #2 RIGHT PASSENGER ENTRY DOOR FLIGHT LOCK COMMAND/FLT LK RLY/SEN SOR DISAGREEMENT. DB PSEU 2 (R2) DB PSEU 2 (L2) ITEM ALREADY ON MEL. REFERENCE LOGPAGE 9967740 FOR MEL DDP PRIOR TO EACH FLIGHT.
Part: SENSOR — FAULTY (LT A/C PACK) · airframe 119,660 hrs · 12,265 cycles
PACK L EICAS STATUS, OVERHEAT AT LT PACK OUTLET OR LT PACK COMPRESSOR OUTLET OR. LT PACK FLOW CONTROL VALVES (FCVS) ARE CLOSED DUE TO: FCV S FAILED CLOSED, FCVS LATCHED CLOSED BY CABIN TEMP CONTROLLER (C TC) BECAUSE OF FAULT, OVERHEAT, OR PACK FLOW SENSING FAILURE, OR, BOTH FCVS FAILED IN ANY POSITION. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 2123491 FLIGHT STATUS: L INTERMITTENCE CODE: M. CABIN TEMPERATURE CONTR OLLER (L CHAN1) POST LT PACK COMPRESSOR DISCHARGE TEMP SENSOR REPLACEMENT, MAT SYSTEM AIR ON TEST CARRIED OUT FOUND TEST PASSED. NIL RELATED FAULTS NOTED AFTER PROLONGED PACKS OPERATION ON GROUND. EXISTING FAULTS NOTED ON MAT. SATIS. BOTH L & RT PACKS OPS SATIS . CMPRSR TEMP SENSOR L EICAS STATUS FAILURE OF BOTH CABIN TEMPERATURE CONTROLLER (CTC) LT PACK COM PRESSOR OUTLET TEMPERATURE SENSORS IN LT PACK. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 2123441 FLIGHT STATUS: L INTERMITTENCE CODE: M PH, CABIN TEMPERATURE CONTROLLER (L CHAN2) FIM TASK 21-52-00-810-850 R101 C/OUT, LT PACK COMP RESSOR DISCHARGE TEMP SENSOR REPLACED IAW AMM 21-52-41 PB401 R10 1. MAT SYSTEM AIR ON TEST C/OUT FOUND TEST PASSED.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 117,751 hrs · 12,064 cycles
M/D R2 DOOR 1EA EMER LT POWER PACK (M33097) FOUND LOW CAPACITY. REPLACED M/D R2 DO OR EMER LT POWER PACK (M33097) AND PERFORMED THE PACK INSTALLATI ON TEST, THE RESULT FOUND NORMAL AS PER AMM 33-51-06-960-803 REV .100.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 117,751 hrs · 12,064 cycles
M/D L3 DOOR 1EA EMER LT POWER PACK (M33406) FOUND LOW CAPACITY. REPLACED M/D L3 DO OR EMER LT POWER PACK (M33406) AND PERFORMED PACK INSTALLATION T EST, THE RESULT FOUND NORMAL AS PER AMM 33-51-06-960-803 REV,100 .
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 117,751 hrs · 12,064 cycles
M/D OHAR AREA 1EA EMER LT POWER PACK FOUND LOW CAPACITY REF HAECO NON-ROUTINE NO.9482787, ORIGINATED BY EMP V905377, SPEC NO.B77 7-25-3-7250. PERFORMED BY EMP V903218, IDT BY EMP V905377, REPLACED M/D OHAR AREA 1EA EMER LIGHT POWER PACK AND PERFORMED THE PACK INSTALLATI ON TEST, THE RESULT FOUND NORMAL AS PER AMM 33-51-06-960-803 REV .100.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 117,751 hrs · 12,064 cycles
M/D R3 DOOR 1EA EMER LT POWER PACK (M33404) FOUND LOW CAPACITY. REPLACED M/D R3 DO OR 1EA EMER LIGHT POWER PACK (M33404) AND PERFORMED THE PACK INS TALLATION TEST, THE RESULT FOUND NORMAL IAW AMM 33-51-06-960-803 REV.100.
Part: SCANNER — FAILED (WX RADAR) · airframe 117,370 hrs · 12,022 cycles
WXR SYS EICAS STATUS WXR DISPLAY IS NOT PRESENT WHEN WXR SELECTED ON EFIS CONTROL PAN EL. FIM TASK REF : FIM TASK REFERENCE NOT FOUND CMC MSG# 3189124. DISPLAYS-1 IN RIGHT AIM S CMC MSG# 318912. DISPLAYS-2 IN RIGHT AIM S CMC MSG# 3189113. DISPLAYS-1 IN LEFT AIMS PER FLIGHT CREW: HAD A WXR FAIL AMBER ON CAPT AND FO'S ND AND WASN'T PAINTING ON EITHER. REMOVED AND REPLACED WXR PEDESTLE AMM 34-43-03-400-801 OPS INITIALLY GOOD BUT RIGHT TRANSCEIVER FAILED DURING TEST. SWAPPED RIGHT TO LEFT AND FAILURE FOLLOWED TO LEFT SIDE. FAILED R/T IS STILL IN LEFT POSITION.
Part: PAINT — DAMAGED (RT STATIC PORT) · airframe 117,106 hrs · 11,994 cycles
RT CENTRE STATIC PORT HAS PAINT DAMAGE NEAR RVSM AREA 1120-01518. INSP DAILY AND RECTIFY WITHIN 5 DAYS. PHOTO TO FOLLOW STATIC PORT CIRCULAR STENCIL TRIMMED AND STILL LEGIBLE, P/N 777-53-11S. MISSING AREA FILLED IN WITH SHARPIE PER ECRA, OK TO PLACE ON DIP PER ECRA 1120-01518 REV A, PART 1 INTERIM TOMC-APPROVAL FROM SC1ELBYC COMMENT REPAIR COMPLETED, ACCOMPLISH REPETITIVE INSPECTION PER PART 2 DAILY AND ACCOMPLISH A PERMANENT REPAIR PER PART 3 WITHIN 5 CALENDAR DAYS. RECORDS UPDATE ALLOWABLE LIMITS. REF SRM 51-10-03-0G-0. TOMCQC REV PERFORMED VERIFIED PAINT CURED. VERIFIED PAINT CURED REF. ECRA 1120-01518 REF. A, SRM 51-10-03-0G-0. IN REF TO ECRA 1120-01518, APPLIED TOUCH UP PAINT AROUND RT. INSPECTED RT CTR STATIC PORT EXTRA CRITICAL AREA, FOUND BLACK CONTINUED TO APPLIED HEAT, PAINT DRY VERIFIED PAINT CURED , AREA WITHIN RVSM LIMITS. REF. ECRA CENTER STATIC PORT, MORE TIME NEEDED FOR PAINT CURE COLOR CIRCLE PAINT SMOOTHNESS IS MORE THAN MAX. OF + 0.003" 1120-01518 REF. A, SRM 51-10-03-0G-0. REMOVED ALL BLACK PAINT FROM STATIC PORT AREA, APPLIED PRIMER AND NEW BLACK PAINT. REF 51-103-0G-0 & 51-10-00-200-804 TOMC APPROVED : QC REVIEWED. RIR: DAILY ("D" METER) NO M&E REQUIRED T/A: 5 DAYS.
2023
Part: PANEL — UNKNOWN (ENG 1 INLET) · airframe 114,016 hrs · 11,634 cycles
PDA 1 REF LP 4785250, FLAGGING PDA. NO 1 ENG FAN STATOR CASE OUTER ACOUSTIC LINER BETWEEN 4 & 6 O''CLOCK FACING AFT DEBONDED. TOTAL SURFACE OF DEBONDING IS 47" X 12" = 564 " SQ. FOUND ON WALKAROUND.
Part: IDG — INOPERATIVE (LT GENERATOR) · airframe 112,255 hrs · 11,431 cycles
ABORTED T/O @ 80 KNOTS DUE TO LEFT GEN DRIVE. WHILE ATEMPTING TO APPLY MEL2411B THE LEFT IDG OIL LEVEL READS SERVICE. RAMP IS CURRENTLY CLOSED FOR WEATHER. REQUEST MEL 2411B DUE TO ABOVE MX MESSAGE LOW FREQ. PLACED NR 1 ENG IDG ON MEL 2411B. PERFORMED DDP. ENGINE DRIVEN GENERATOR LT, MEL 2411B SERVICED NR 1 ENG IDG TO FULL, READS NORMAL.IAW AMM 12-13-03-600-802. EF AMM 24-11-01-000-801-001. ACP IDT INSP OF #1 ENG IDG FEEDER CABLES INSTALLATION & TORQUED QUAD RING IAW AMM 24-11-01-400-801-001. PERFORMED ELOTO ON LE AND LT THRUST REVERSER, REPLACED LT ENGINE IDG IAW MM 24-11-01-400-801-001. REMOVED NR 1 ENGINE IDG. NEW TORQUED QUAD RING AND IDG FEEDER CABLES . REPLACED LT ENGINE IDG IAW MM 24-11-01-400-801-001-001 OPS CHKS GOOD, ALL INDICATIONS NORMAL.
2022
Part: FRAME — CRACKED (BS 2370 BLKHEAD) · airframe 111,549 hrs · 11,350 cycles
SUPPORT TASK - EA-530-0113 REV B OP.17 AD 2022-06-07 LH BS 2370 PIVOT B/HEAD FWD OUTER CHORD. LH BS 2370 PIVOT BULKHEAD FWD OUTER CHORD REPLACED AND INSTALLED AS PER EA5380-01113 REV B OP025.
Part: FRAME — CRACKED (BULKHEAD) · airframe 111,549 hrs · 11,350 cycles
SUPPORT TASK - EA 5380-01113 REV B OP.18 AD 2022-06-07 RH BS 2370 PIVOT B/HEAD FWD OUTER CHORD FOUND CRACKED, BS 2370 PIVOT BULKHEAD FWD OUTER CHORD REPLACED AND INSTALLED AS PER EA5380-01113 REV B OP026.
Part: BATTERY — INOPERATIVE (L2 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - R2 DOOR GALLEY CEILING AREA EMER LIGHT FOUND DIM TRANSFER REF HXWO 1232121 AND ORIGINATED BY EMP V934740 L2 DOOR EMER LIGHT POWER PACK (M33096) (BATTERY AND CHARGER) REPLACED AND INSTALLATION TEST RESULT NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810 CORRECTION MADE BY V926996 DEFECT LOCATION SHOULD BE L2 DOOR ADD EMP:V926996
Part: BATTERY — INOPERATIVE (R4 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - SEAT 46-52KL CEILING AREA EMER LIGHT DOUND DIM TRANSFER REF HXWO 1232120 AND ORIGINATED BY EMP V934740 R4 DOOR EMER LIGHT POWER PACK M33409 (BATTERY AND CHARGER) REPLACED AND INSTALLATION TEST RESULT NORMAL AS PER AMM 33-51-06 WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810
Part: BATTERY — INOPERATIVE (L1 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 SEAT 1-9A CEILING EMERG AREA LT FOUND DIM TRANSFER REF HXWO 1233584 AND ORIGINATED BY EMP V934740 L1 DOOR EMER LIGHT POWER PACK M33424 (BATTERY AND CHARGER) REPLACED AND INSTALLATION TEST RESULT NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810
Part: BATTERY — INOPERATIVE (R3 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - ZONE C EY SEAT FLOOR PROX LIGHT FOUND DIM TRANSFER REF HXWO 1232130 AND ORIGINATED BY EMP V934740 R3 DOOR EMER LIGHT POWER PACK BATTERY AND CHARGER REPLACED (M33401) AND OPERATION TEST NORMAL REF AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V907889 INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810
Part: BATTERY — INOPERATIVE (L1 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - SEAT 1-9L CEILING AREA EMER LIGHT FOUND DIM TRANSFER REF HXWO 1232129 AND ORIGINATED BY EMP V934740 L1 DOOR EMER LIGHT POWER PACK (BATTERY AND CHARGER) (M33093) REPLACED AND INSTALLATION TEST RESULT NORMAL AS PER AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V907892 INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810
Part: BATTERY — INOPERATIVE (R2 DOOR) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - ZONE B BC SEAT FLOOR PROX LIGHT FOUND DIM TRANSFER REF HXWO 1232115 AND ORIGINATED BY EMP V934740 R2 DOOR EMER LIGHT BATTERY (M33098) REPLACED AND INSTALLATION TEST RESULT NORMAL AS PER AMM 33-51-06 WORK ACCOMPLISHED BY MECHANIC V907892 AND INSPECTED BY V926996 IDT INSPECTED BY HX136003 ADD EMP:V897810
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 111,549 hrs · 11,350 cycles
B777-33-3-7019 - ZONE A BC SEAT FLOOR PROX LIGHT FOUND DIM TRANSFER REF HXWO 1232113 AND ORIGINATED BY EMP V934740 ZONE A R1 DOOR (M33094) EMERGENCY BATTERY AND CHARGER REPLACED AND INSTALLATION TEST NORMAL REF AMM33-51-06 WORK ACCOMPLISHED BY MECHANIC V907889 INSPECTED BY V896995
Part: BATTERY PACK — INOPERATIVE (DOOR 3L) · airframe 110,244 hrs · 11,206 cycles
FOUND EMERGENCY BATTERY PACK M33405 ABOVE DOOR 3 LEFT NEEDS NEW BATTERY PACK, M&E 99-3351-3-0015 NIS IN IAH BATTERY PACK IS FOR EMERGENCY LIGHTS INSTALLED NEW BATTERY PACK. OPS CHECK OK REF AMM 33-50 VERIFIED BATTERY INSTALLED REF AMM 33-51-06. OPS CHECK GOOD.
2021
Part: RELAY — ARCED · airframe 106,997 hrs · 10,633 cycles
GATE RETURN SMOKE IN THE CABIN. FOUND ELECTRICAL ARCING ON THE P300 PANEL UPON ASESSMENT OF DAMAGE TO P300 PANEL, REMOVED AND FOUND RELAY K24002 GROUND SERVICE SELECT RELAY SEVERELY DAMAGED, SUSPECT INTERNAL FAILURE. NO FOD NOTED IN AREA. REFERENCE SSM 24-22-41, WDM 24-21-31, 24-51-41. AC AND (1 EA.) P-49 PANEL A-5 VOICE RCDR RELAY. REF. AMM TASK # 23-71-01. [ACFT. # 0009]. VOX RCDR; (2 EA.) P-210 PANEL L-12 FLT. RCDR DC & E-23 FLT. RCDR F.O.M. (REF. L.P. # 6861022). LOCATION: (1 EA.) P-11 PANEL E-13 DE-ACTIVATED (PULLED) 4 EA. FLT. RECORDER CIRCUIT BREAKERS. FOUND WIRE W4830-0301-1/0 BURNED AT P-300 PANEL. FOUND WIRE W4830-0401-1/0 BURNED AT P-300 PANEL. FOUND WIRE W4830-0302-1/0 BURNED AT P-300 PANEL. FOUND WIRE W4830-0402-1/0 BURNED AT P-300 PANEL. FOUND WIRE W4830-0303-1/0 BURNED AT P-300 PANEL. FOUND WIRE W4830-0403-1/0 BURNED AT P-300 PANEL. ADD EMP:U131143 24-41-31. FOUND WIRE W4030-0001-2/0 BURNED AT P-300 PANEL. REFERENCE WDM FOUND WIRE W4030-0002-2/0 BURNED AT P-300 PANEL. REFERENCE WDM 24-41-31. 24-41-31. FOUND WIRE W4030-0003-2/0 BURNED AT P-300 PANEL. REFERENCE WDM FOUND WIRE W4030-0004-04 BURNED AT P-300 PANEL. REFERENCE WDM 24-41-31. 24-22-41. FOUND WIRE W4228-0004-02 BURNED AT P-300 PANEL. REFERENCE WDM FOUND WIRE W4228-0005-02 BURNED AT P-300 PANEL. REFERENCE WDM 2
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - EMER LT PWR PACK M33407 OPERATION TEST FAIL. REF NR LP 9131393. PWR PACK M33047 BATTERY REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06. IDT INSPECTED BY HX102640. ADD EMP:V926992
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - EMER LT PWR PACK M33408 OPERATION TEST FAIL. REF NR LP 9131395. PWR PACK M33048 BATTERY REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06. ADD EMP:V897810 IDT INSPECTED BY HX102640. ADD EMP:V896992
Part: SKIN — DAMAGED (LH STATIC PORT) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - LH L SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131404. LH L SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR, AND SMOOTHED OUT AREA MEASURED REMAINING THICKNESS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPAIR 1 WITH CONFIRMED NO CRACK FOUND AND SKIN WAVINESS CHECK CARRIED OUT AND AVERAGE PORT WAVINESS IS ADD EMP:V906449 -0.0005 IN WITHIN LIMIT AS PER AMM 51-10-00-200-801. RII INSPECTED BY HX247305.
Part: SKIN — DAMAGED (RH STATIC PORT) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - RH R SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131401. RH R SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS IS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPAIR 1 WITH CONFIRMED NO CRACK FOUND SKIN WAVINESS CHECK CARRIED OUT AND AVERAGE PORT WAVINESS IS 0.0015 ADD EMP:V906449 IN. WITHIN LIMIT AS PER AMM 51-10-00-200-801. RII INSPECTED BY HX247305.
Part: SKIN — DAMAGED (RH CTR STATIC P) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - RH CTR SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131403. RH CTR SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS 0.128" ORIGINAL 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPAIR 1 WITH CONFIRMED NO CRACK FOUND, SKIN WAVINESS CHECK CARRIED OUT AND AVERAGE PORT WAVINESS IS -0.0005 IN WITHIN LIMIT AS PER AMM ADD EMP:V906449 51-10-00-200-801. RII INSPECTED BY HX247305
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - EMER LT PWR PACK M33099 CANNOT BE CHARGED UP. REF NR LP 9131392. PWR PACK M33099 CHARGER REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06. IDT INSPECTED BY HX102640. ADD EMP:V926992
Part: SKIN — DAMAGED (RH STATIC PORT) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - RH L SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131402. RH L SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS 0.129" ORIGINAL THICKESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPAIR 1 WITH CONFIRMED NO CRACK FOUND. SKIN WAVINESS CHECK CARRIED OUT AND AVERAGE PORT WAVINESS IS -0.0005 IN WITHIN ADD EMP:V906449 LIMIT AS PER AMM 51-00-00-200-801. RII INSPECTED BY HX247305.
Part: SKIN — DAMAGED (LH STATIC PORT) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - LH R SYS STATIC PORT FOUND SURFACE ROUGH. REF NR LP 9131400. LH R SYS STATIC PORT ROUGH SURFACE SMOOTHED OUT AS PER SRM 51-10-01-2R-1 REPAIR 1 AND MEASURED REMAINING THICKNESS IS 0.129" ORIGINAL THICKNESS 0.130" WITHIN LIMIT AS PER SRM 51-10-01-2R-1 REPAIR 1 WITH CONFIRMED NO CRACK FOUND SKIN WAVINESS CHECK CARRIED OUT AND AVERAGE PORT WAVINESS IS -0.0005 ADD EMP:V906449 IN. WITHIN LIMIT AS PER AMM 51-10-00-200-801. RII INSPECTED BY HX247305.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,230 hrs · 10,477 cycles
SUPPORT TASK - EMER LT PWR PACK M33099 OPERATION TEST FAIL. REF NR LP 9131397. PWR PACK M33099 BATTERY REPLACED AND INSTALLATION TEST CARRIED OUT WITH NORMAL RESULT AS PER AMM 33-51-06. ADD EMP:V897810 IDT INSPECTED BY HX102640.
2020
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · airframe 105,129 hrs · 10,329 cycles
EMERGENCY BATTERY PACK PN AD-717-01-100 FOUND INOPERABLE AT L3 DOOR. REPLACED EMERGENCY BATTERY PACK, IAW AMM 33-51-06-960-803 AT L3 DOOR. OPS CHECK GOOD. WORK ACCOMPLISHED ON AERSALE NR 489613 BY V 931306.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 105,129 hrs · 10,329 cycles
EMERGENCY BATTERY PACK PN AD-D717-01-100 FOUND INOPERABLE AT R3. REPLACED EMERGENCY BATTERY PACK, IAW AMM 33-51-06-960-803 AT R3 DOOR. OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 105,129 hrs · 10,329 cycles
EMERGENCY BATTERY PACK PN AD-D717-01-100 FOUND INOPERABLE AT R3 DOOR. REPLACED EMERGENCY BATTERY PACK, IAW AMM 33-51-06-960-803 AT R3 DOOR. OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 105,129 hrs · 10,329 cycles
EMERGENCY BATTERY PACK PN AD D717-01-100 AT L3 DOOR INOPERABLE. REPLACED EMERGENCY BATTERY PACK, IAW AMM 33-51-06-960-803 AT L3 DOOR. OPS CHECK GOOD. WORK ACCOMPLISHED ON AERSALE NR 489613 BY V 931306.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 105,113 hrs · 10,327 cycles
B777-33-3-7007 DR4 EMER LIGHT POWER SUPPLY M33408 BATTERY PACK C APCITY LOW REF NR LP 9130406 DR4 EMER LIGHT POWER SUPPLY M33408 BATTERY PACK AND CHARGER REPL ACED AND TESTED NORMAL AS PER AMM 33-51-06
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 105,113 hrs · 10,327 cycles
B777-33-3-7007 DR R1 EMER LIGHT POWER SUPPLY M33094 BATTERY PACK CAPACITY LOW REF NR LP 9130408 DR R1 EMER LIGHT POWER SUPPLY M33094 BATTERY PACK REPLACED AND T ESTED NORMAL AS PER AMM 33-51-06
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 105,113 hrs · 10,327 cycles
B777-33-3-7007 DR R3 EMER LIGHT POWER SUPPLY M33401 BATTERY PACK CAPACITY LOW REF NR LP 9130410 DR R3 EMER LIGHT POWER SUPPLY M33401 BATTERY PACK PLACED AND TES TED NORMAL AS PER AMM 33-51-06
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 105,113 hrs · 10,327 cycles
B777-33-3-7007 DR R3 EMER LIGHT POWER SUPPLY M33404 BATTERY PACK CAPACITY LOW REF NR LP 9130409 DR R3 EMER LIGHT POWER SUPPLY M33404 BATTERY PACK REPLACED AND T ESTED NORMAL AS PER AMM 33-51-06
2019
Part: CONTROL VALVE — MALFUNCTIONED (AC BAY) · airframe 104,319 hrs · 10,246 cycles
PACK FCV LWR L STATUS MESSAGE LT PACK OFF LT ON T/S PER FIM 21-51-00-810-831, 28VDC PRESENT AT DV21513A. PER FIM NEEDS NEW FCV. FAULT. CONTINUED WITH FIM AND VERIFED FCV POSITION SENSOR WIRING. CHANGED LOWER FLOW CONTROL AND SHUT OFF VALVE REF AMM 21-51-02. ROTABLE PARTS CHANGE WAS INDICATED - TT # 1225725 SN OFF 9277 VALVE, AIR, PAC OFF 25-2151-9-0002 9277 ON 25-2151-9-0002 0918 FOUND MX MSG 21-24303. TS PER FIM AND FOUND IT WAS INTERMITENT
2018
Part: NOT REPORTED — SPARKS (CABIN) · airframe 99,309 hrs · 9,730 cycles
PAX SAW SPARKS FROM UNDER SEAT 17K SPARK ORIGINATED FROM 16K. SPM DISCONNECTED AT 16K (PRECAUTIONARY) NO DAMAGE OR WIRING FAULTS FOUND. IFE INOP AT SEATS 16-17 JKL.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,936 hrs · 9,607 cycles
R2 DOOR AREA CEILING EMERGENCY LIGHT POWER SUPPLY M33097 CHARGER WAS INOPERATIVE. THE CHARGER WAS REPLACED AND OPS CHECKED NORMAL IAW AMM 33-51-06.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,936 hrs · 9,607 cycles
L3 DOOR AREA CEILING EMERGENCY LIGHT POWER SUPPLY M33406 CHARGER WAS INOPERATIVE. THE CHARGER WAS REPLACED, OPS CHECKED NORMAL IAW AMM 33-51-06.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 97,936 hrs · 9,607 cycles
R2 DOOR AREA CEILING EMERGENCY LIGHT POWER SUPPLY M33098 BATTERY CAPACITY WAS LOW. THE BATTERY PACK WAS REPLACED, OPS CHECKED NORMAL IAW AMM 33-51-06.
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHT) · airframe 97,936 hrs · 9,607 cycles
R2 DOOR AREA CEILING EMERGENCY LIGHT POWER SUPPLY M33097 BATTERY CAPACITY WAS LOW. THE BATTERY PACK WAS REPLACED, OPS CHECKED NORMAL IAW AMM 33-51-06.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHT) · airframe 97,936 hrs · 9,607 cycles
L3 DOOR AREA CEILING EMERGENCY LIGHT POWER SUPPLY M33406 BATTERY CAPACITY WAS LOW. THE POWER SUPPLY BATTERY PACK WAS REPLACED AND CHECKED NORMAL IAW AMM 33-51-06.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 97,936 hrs · 9,607 cycles
CEILING EMERGENCY LIGHT POWER SUPPLY M33098 CHARGER WAS INOPERATIVE. THE CHARGER WAS REPLACED, OPS CHECKED NORMAL IAW AMM 33-51-06.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 96,946 hrs · 9,506 cycles
R4 DOOR EXIT LIGHT LENS WAS MISSING. SECURED THE LENS, ALL OK.
2017
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 90,846 hrs · 8,947 cycles
IN FA CREW REST AREA FLASH LIGHT UNDER BUNK 3 INOP. REPLACED F/A EMERGENCY FLASHLIGHT BATTERY, OPS CHECK GOOD.
Part: BATTERY — DISCHARGED (R4 DOOR) · airframe 90,022 hrs · 8,876 cycles
DOOR 4R EPAS FAILED OPERATIONAL TEST NO GREEN OR AMBER LIGHTS. REF W/C 25-5210-1-9801 PARA D STEP G7. REMOVED AND REPLACED EMERGENCY POWER ASSIST SYSTEM BATTERY REF AMM 52-11-25 OPS CHECK GOOD INSPECTED 4R DOOR OPS CHECK OF EMERGENCY POWER ASSIST BATTERY, OPS CHECK GOOD..
2015
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,353 hrs · 8,205 cycles
SUPPORT TASK, CABIN ZONE B LT STATION 845 - 1097, FOUR EACH EMER AREA LIGHT FOUND DIM. CABIN ZONE B LT DOOR NR 2 OVERHEAD, ONE EACH BATTERY PACK M33099 REPLACED IAW AMM 33-51-06 & EMER LIGHT TEST FOUND NORMAL IAW AMM 33-51-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,353 hrs · 8,205 cycles
SUPPORT TASK, CABIN ZONE D RT STATION 1581 - 1665, TWO EACH EMER AREA LIGHTS FOUND DIM. CABIN ZONE D RT DOOR NR 3 OVERHEAD ONE EACH BATTERY PACK M33401 REPLACED IAW AMM33-51-06 & EMER LIGHT TEST FOUND NORMAL IAW AMM 33-51-00.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 82,353 hrs · 8,205 cycles
SUPPORT TASK, CABIN ZONE B LT STATION 1181 - 1433, FOUR EACH EMER AREA LIGHTS FOUND DIM. CABIN ZONE D LT DOOR NR 3 OVERHEAD, ONE EACH POWER SUPPLY M33400 & ONE EACH POWER PACK 33400 REPLACED IAW AMM 33-51-06. EMER LIGHT TEST FOUND NORMAL IAW AMM 33-51-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,353 hrs · 8,205 cycles
SUPPORT TASK, CABIN ZONE A RT STATION 423 - 676, FOUR EACH EMER AREA LIGHTS FOUND DIM. CABIN RT DOOR NR 1 OVERHEAD, ONE EACH POWER SUPPLY M33093 & ONE EACH BATTERY PACK M33093 REPLACED IAW AMM 33-51-06. EMER LT TEST FOUND NORMAL IAW AMM 33-51-00.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,353 hrs · 8,205 cycles
LEFT DOOR 1 EXTERIOR EMER LIGHT FOUND DIM. CABIN LT DOOR NR 1 OVERHEAD, ONE EACH POWER SUPPLY M33424 & ONE EACH BATTERY PACK M33424 REPLACED IAW AMM 33-51-06 & EMER LIGHT TEST FOUND NORMAL IAW AMM 33-51-00.
Part: GENERATOR — ARCED (APU) · airframe 82,353 hrs · 8,205 cycles
APU GENERATOR T2 TERMINAL FOUND ARCING. APU GENERATOR ASSEMBLY REPLACED IAW AMM 24-21-01. APU GENERATOR FEEDER HARNESS REPLACED IAW AMM 24-21-02 & 24-21-01. APU GENERATOR INSTALLATION TEST IAW AMM 24-21-01, CARRIED OUT NORMAL. ROTABLE PARTS CHANGE WAS INDICATED TT 1706206, SN OFF 00329 GENERATOR, APU OFF 25-2421-9-0001 0329 ON 25-2421-9-0001 0376.
Part: COMPRESSOR — STALLED (NR 2 ENGINE) · airframe 79,808 hrs · 7,987 cycles
RIGHT ENG COMP STALL & DISPLAYED ENG FAIL AT 80 KTS ON FULL POWER TO DUE STRONG LT CROSSWINDS & WIND SHEAR. COMPLIED WITH ENG STALL INSPECTION IAW MM 71-00-00-200-809. ALL CHECKED OK. COMPLIED WITH NR 2 ENG BORESCOPE IAW 71-00-00-200. ALL DAMAGE FOUND, ALL WITHIN LIMITS IAW AMM 72-00-00-290-814-G00 & 72-00-00-290-812-G00.
2011
Part: PLUG — MISSING (NR 1 ENGINE) · airframe 63,166 hrs · 6,507 cycles
WHILE PERFORMING T/S ON NR 1 ENG, FOUND DAMAGE ON LEFT T/R FIRE BLANKET ALSO FOUND HIGH PRESS COMPRESSOR BOROSCOPE PLUG MISSING ON LEFT SIDE (8TH STAGE VANE H.P.C ROTOR). INSTALLED REPLACEMENT BOROSCOPE PLUG (J) PER AMM 72-00-00-290 812-G00, (NOTE) FIRE BLANKET DAMAGE TRANSFER TO L/P 4523119,20 AND 21.
Part: OUTLET — DEFECTIVE (CABIN) · airframe 62,890 hrs · 6,480 cycles
NOTED ACRID BURNING ODOR IN AREA OF SEATS 42 TO 43 PERFORMED TASK 05-51-58-910-801C5 FOUND IN SEAT POWER OUTLET AT 4 40K INTERMITTING WHEN A POWER SOURCE WAS PLUGGED IN ALSO SMELL R&R IPO OPS CHECKS GOOD NO SMELLS NOTED.
2010
Part: INDICATION SYS — MALFUNCTIONED (O2 SYSTEM) · airframe 55,804 hrs · 5,829 cycles
CLIMBING THRU 16.000 RECEIVED A CLEAR O2 LOW EICAS MSG. PRESSURE READ 50 PSI BUT 1400 PSI DURING PRE FLIGHT. PLACED INDICATION ON DEFERRAL INOP CONFIRMED BOTTLE NR 1 AT 1700 PSI, BOTTLE NR 2 AT 1700 PSI, OK TO CONTINUE.
2007
Part: LONGERON — CRACKED (BS 2272 L26R) · airframe 39,439 hrs · 4,360 cycles
INSPECTION FOUND A .5 INCH CRACK IN AFT LOWER LONGERON STRAP AT RIGHT LOWER SEAL FAIRING AREA, STA 2272, S26R. REPAIRED IAW ECRA 5310-04631.
Part: SKIN — CRACKED (BS 2272) · airframe 39,439 hrs · 4,360 cycles
INSPECTION FOUND A .5 INCH CRACK IN RIGHT LOWER SEAL FAIRING SKIN AT BS 2272, S26R. THE SKIN WAS REPAIRED IAW SRM 53-80-70, REPAIR 1, FIGURE 204.
Part: SKIN — CORRODED (BS 2344-2370) · airframe 39,439 hrs · 4,360 cycles
INSPECTION FOUND SKIN CORRODED AT BS 2344-2370, S38R-S43R (TAIL COMPARTMENT AREA). THE SKIN WAS REPAIRED IAW SRM 53-00-01, REPAIR 7, FIGURE 202.
2005
Part: CONTROL UNIT — SHORTED (L-3 DOOR) · airframe 32,126 hrs · 3,681 cycles
PASSENGERS AND FLIGHT ATTENDANT'S REPORTED A WHIFF OF ELECTRICAL ODOR IN THE CABIN AT A ZONE, B ZONE, AND IN AFT CABIN NEAR ROW 25 WHILE EN ROUTE TO IAH. THE ODOR RETURNED LATER WITH A VISIBLE HAZE. THE APPROPRIATE CHECKLIST WAS RUN AND THE ODOR AND HAZE CEASED. THE AIRCRAFT LANDED AT IAH WITHOUT FURTHER PROBLEM. MAINTENANCE FOUND THE OEU (OVERHEAD ELECTRONICS UNIT) AT L-3 DOOR SHORTED. THE OEU WAS REMOVED AND REPLACED, OPERATIONAL CHECKS WERE GOOD.
2003
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,846 hrs · 2,313 cycles
INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1513, LBL 85. THE SEAT TRACK WAS REPLACED IAW SRM 51-10-02 AND 51-40-02.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,846 hrs · 2,313 cycles
INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1497-1530, RBL 74. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 3, FIGURE 202.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 19,846 hrs · 2,313 cycles
INSPECTION FOUND SEAT TRACK CROWN CORRODED AT BS 1513-1530, RBL 108. THE SEAT TRACK WAS REPAIRED IAW SRM 53-00-52, REPAIR 4, FIGURE 202.
Part: SKIN — DENTED (FUSELAGE) · airframe 19,846 hrs · 2,313 cycles
INSPECTION FOUND FUSELAGE SKIN DENTED 3 INCHES FORWARD OF STA 676, FORWARD OF L-2 DOOR BETWEEN STRINGERS 27L AND 28L. REPAIRED IAW SRM 53-00-01, REPAIR 7.
1999
Part: SELECT VLV — INOP (MLG DOOR)
A POP WAS HEARD WHILE ON APPROACH TO EWR AT 4,000 FEET. THE GEAR WAS LOWERED, BUT THE GEAR DOOR REMAINED OPEN. THE AIRCRAFT LANDED AT EWR WITHOUT INCIDENT. MAINTENANCE REMOVED AND REPLACED THE MLG SELECTOR /BYPASS VALVE IAW MM 32-31-03, PAGE 401. LEAK AND OPERATIONAL CHECKS WERE GOOD.