N912FD
Registered owner: FEDERAL EXPRESS CORP, TN (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
DURING RAMP TRAINING L1 DOOR GUST LOCK WOULD NOT RELEASE. AMM 52-11-08-8 INSTALLED SERVICEABLE SPLIT COLLAR IN REF TO AMM. CLEARED MEL.
RH WING SLAT # 9 LOWER SURFACE O/N MAIN TRACK BRACKET AREA WITH CRACK APPLIED PERMANENT REPAIR AT RH WING SLAT # 9 LOWER FLEXIBLE SKIN PANEL BTW OSS 675 TO OSS 680 IAW B757 SRM 57-43-01-2R, FIG 201, RPR 10, SHEET 1 AND SRM 51-70-07-0G REPAIR DIM 2=5.100", W=1.600"
SEC 48 UPPER FUSELAGE BETWEEN BS 1896 AND BS 1918 HAS A CUSTER OF 04 DENTS (TWO ARE LOCATED AROUND THE AREA, AND TWO ARE LOCATED OVER A PREVIOUS REPAIR) APPLIED PERMANT REPAIR AT SEC 48 UPPER FUSELAGE LH BTW STA 1896 TO 1918 IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06- 2R
SEC 48 UPPER FUSELAGE BETWEEN BS 1941 AND BS 1963 WITH 03 DENTS APPLIED PERMANENT REPAIR AT SEC 48 UPPER FUSELAGE BTW STA 1941 TO 1963 IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06- 2R
APU COMPARTMENT INTERNAL SKIN AT BS 1900 DELAMINATED APPLIED PERMANENT AT APU COMPARTMENT INTERNAL SKIN IAW B757 SRM 51-70-10-2R AND PERFORMED TAP TEST AFTER REPAIR IS SATISFACTORY IAW B757 SRM 51-10-06-2R
MAIN CABIN SEAT TRACK BETWEEN BS 660.0 TO 885.0 RBL 58.22 WITH CORROSION EVALUATED SEAT TRACK FOUND DATA NOT ALLOWED DAMAGE OUT OF LIMITS IAW SRM 53- 00-52-1A FIG 101 SHEET 1, REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN BS 660 TO 885, RBL 58.22 IAW B757 SRM 51-40-02-0G AND B DWG # 657N3332 REV A
MAIN CABIN SEAT TRACK BETWEEN BS 660 TO 885 RBL 58.22 WITH CORROSION.
PYLON NR 1 AROUND THE CUT OUT FOR ACCESS PANEL 433JR INTERNAL SKIN SHOWS CORROSION. REMOVED AND REPLACED INBD PYLON SKIN PANEL IAW B DWG 012N8774 REV A AND SRM 51-40-02-0G.
L/H WING INB MAIN FLAP TRAILING EDGE PREVIOUS REPAIR IS DEBONDED REMOVED PREVIOUS REPAIR LOWER SKIN FOUND DEBONDED AND INSTALLED PERMANENT REPAIR AT LH WING I/B MAIN FLAP TRAILING EDGE IAW B757 SRM 57-53-01-2R, FIG 201, RPR 1, SHEET 2, DETAIL I, AND SRM 51-70-10-2R FIG 201, SHEET 1
R1 DOOR EXTERIOR EMERGENCY SLIDE LIGHT INOP. AMM: 33-51-06-2 RELAMPED R1 DOOR EXTERIOR SLIDE LIGHT IAW ABOVE REF. OPS CHK SERVICEABLE.
RIGHT ENTRY SLIDE LIGHT REMAINS ON AFTER DISARMING. REPLACED BATTERY AT M730. REMOVED SOURCE MANUFACTURING BATTERY ASSEMBLY MPN 2013-1ASMI S/N 3341. TEST GOOD.
WHEN ARMING THE SLIDES FOR DEPARTURE, RT SLIDE LIGHT DID NOT ILLUMINATE. RELEASED FOR SERVICE IAW MEL 25-66-04-B, CATEGORY C. VERIFIED SLIDE ARMED LT DOES NOT ILLUMINATE WHEN R1 DOOR SLIDE IS ARMED. PERFORMED GVI OF R1 DOOR ESCAPE SLIDE GIRT BAR, SKIRT & LANYARDS, NO DEFECTS. GIRT BAR ENGAGES NORMAL WITH NO DEFECTS. NO RIGGING OR ADJUSTMENTS MADE TO R1 DOOR ESCAPE SYS. CHECKED R1 DOOR SLIDE ARMED LT MODULE FUNCTION AT L1 DOOR POSTION, SLIDE ARMED LIGHT FUNCTIONS NORMAL. REINSTALLED SLIDE ARMED LIGHT MODULE. REINSTALLED R1 DOOR SLIDE ARMED LIGHT MODULE, SLIDE ARMED LIGHT OPS CHECKS GOOD. BOTH R1 & L1 DOOR SLIDE ARMED LIGHTS FUNCTION NORMAL. REINSTALLED R1 DOOR SLIDE COVER. ACFT OK FOR SERVICE.
COURIER AREA CENTER OVERHEAD EMERGENCY EXIT LIGHT, R1 DOOR OVERHEAD EMERGENCY EXIT LIGHT AND EXTERIOR R1 SLIDE LIGHT INOP. AMM: 33-51-07-2 REMOVED AND REPLACED EMERGENCY POWER SUPPLY BATTERY IAW ABOVE REF. CTR & R1 OVERHEAD EXIT LIGHTS AND R1 EXTERIOR SLIDE LIGHT OPS CHK SERVICEABLE.
R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-60-01-2. RT EMERGENCY EXIT SIGN OPS CHECKED NORMAL IAW MM 33-51-01-2.
R1 DOOR INTERIOR EMERGENCY EXIT LIGHT WILL NOT TEST. TROUBLESHOT RT EMERGENCY EXIT SIGN FAULT IAW WDM 33-51-12. RESET EMERGENCY LIGHT CIRCUIT BREAKER IAW MM 20-60-01-2. R/H EMERGENCY EXIT SIGN OPS CHECKED NORMAL IAW M/M 33-51-01-2.
LEFT MAIN AIRCRAFT DOOR GUST LOCK STUCK. CANNOT CLOSE THE DOOR. REPLACED L1 DOOR HOLD OPEN LOCK PER ABOVE REF. OPS CHECKS GOOD.
PRIOR TO DESCENT, L AFT FUEL PUMP EICAS MESSAGE AND PRESS LIGHT IN L AFT PUMP SWITCH. COMPLIED WITH QRH PROCEDURE. WHILE DEBRIEFING CREW, FOUND "L AFT FUEL BOOST PUMP" CIRCUIT BREAKER TRIPPED. COLLARED CB PER MEL. A/C OK FOR SERVICE. TROUBLESHOT PER FIM WITH NO DEFECTS NOTED. FIM DETERMIND THAT CONDITON THAT CAUSED CIRCUIT BREAKER TO OPEN IS NOT PRESENT. AC OK TO CONTINUE
L1 DOOR GUST LOCK IS BROKE. STUCK IN THE UP POSITION. REPLACED L1 DOOR HOLD-OPEN LOCK COLLAR
CLIMBING THROUGH FL200; EICAS R HYD QTY MSG FOLLOWED BY R HYD SYS PRESS MSG. COMPLETED QRH. AMM 29-18-04-4 FOUND BLOWN O-RING IN RT IN/BO ENG PYLON ON HYD FILTER CASING. REMOVED AND REPLACED THE RT HYD EDP FILTER MODULE ASSY IAW AMM 29-11-17-4-0 UP TO STEP 3 L (2). SYSTEM STILL REQUIRES SERVICING, OPS CHECK AND LEAK CHECK. AMM: 29-11-17-4, AMM: 12-12-01-3, C/W FLUID SERVICING , LEAK & OPS CHECKS. ALL LEAK & OPS CHECKS ARE GOOD.
NLG EMERGENCY LIGHT SWITCH INOP. REPLACED ONE TERMINAL ON WIRE W2052-0013-18 IAW WDM 33-51-11 SHEET 1 AND SWPM 20-30- 11, OP. TEST SATISFACTORY IAW AMM 33-51-00-5.
DOT #106-10; MAIN CABIN BETWEEN STA. 1620 & STA. 1640, LBL 45.5 SEAT TRACK HAS CORROSION. CUT OUT SECTION SEAT TRACK, INSTALLED SEAT TRACK REPAIR SPLICE P/N BAC 1509100449 BATCH #0004281080 & SEAT TRACK P/N BAC 1520793A BATCH #0002663579 IAW SRM 53-00-52-2R, FIG.201 REPAIR 3, PART MARKED SEAT TRACK REPAIR FX5300522R-1 PER GMM 7-0-1001, MAJOR REPAIR.
MAIN CABIN STA. 1320, LBL 24.75 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK SECTION BETWEEN STA 1320 TO STA 1350 LBL 24.75 PER SRM 53-00-52-2R FIG 201 REPAIR 3 OPTION 2, MAJOR REPAIR.
FLOORBOARD PANEL 222MEF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 222MEF ON VTMAE TRAVELER #T24/1753851 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR
MAIN DECK CARGO COMPT FLOORBOARD PANEL 232 MYF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232 MYF ON VTMAE TRAVELER #T24/1752806 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
MAIN CABIN CARGO COMPT FLOORBOARD PANEL 241MNF IS DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MNF ON VTMAE TRAVELER #T24/1752825 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANEL 252MVF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MVF ON VTMAE TRAVELER #T24/1752843 IAW DWG SRZ-25-005 REVISION R. MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MEF DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 232MEF ON VTMAE TRAVELER #T24/1752792 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANELS 252MUF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MUF ON VTMAE TRAVELER #T24/1752842 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANELS 251MWF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 251MWF ON VTMAE TRAVELER #T24/1752837 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANELS 252MRF IS DAMAGED. FABRICATED ZONE 250 FLOORBOARD PANEL 252MRF ON VTMAE TRAVELER #T24/1752840 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANEL 241MRF IS DAMAGED. FABRICATED ZONE 240 FLOORBOARD PANEL 241MRF ON VTMAE TRAVELER #T24/1752834 IAW DWG SRZ-25-005 REVISION R MAJOR REPAIR.
MAIN DECK CARGO COMPT FLOORBOARD PANEL 232MJF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD 232MJF ON VTMAE TRAVELER #T24/1752794 IAW DWG SRZ- 25-005 REVISION R MAJOR REPAIR
MAIN CABIN CARGO COMPT FLOORBOARD PANEL 231 MYF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231 MYF ON VTMAE TRAVELER #T24/1752802 IAW DWG SRZ25-005 REVISION R MAJOR REPAIR.
MAIN DECK CARGO CMPT FLOORBOARD 231 MRF IS DAMAGED. FABRICATED ZONE 230 FLOORBOARD PANEL 231 MRF ON VTMAE TRAVELER #T24/1752801 IAW DWG SRZ25-005 REVISION R, MAJOR REPAIR.
MAIN DECK CREASE BEAM CORRODED BETWEEN STA 860-880 LH. REMOVED AND REPLACED CREASE BEAM BETWEEN STA 860-880 LH P/N BAC1515-553 (143N5540-9) BATCH 0002677936 IAW B757 SRM 51-40-02 AND SRM 53-30-13-01. CORROSION FOUND OUT OF LIMITS IAW SRM 53-00-52-2R. MAJOR REPAIR
FLOORBOARD PANELS 221AF DAMAGED FABRICATED ZONE 220 FLOORBOARD PANEL 221AF ON VTMAE TRAVELER #T24/1753756 IAW DWG. SRZ-25-005 REVISION R, MAJOR REPAIR.
FLOORBOARD PANEL 222AF DAMAGED. FABRICATED ZONE 220 FLOORBOARD PANEL 222AF ON VTMAE TRAVELER # T24/1753759 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
FLOORBOARD 221MAF IS DAMAGED. FABRICATED ZONE 220 FLOORBOARD PNL 221MAF ON VTMAE TRAVELER #24/1753757 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAIR.
FLOORBOARD PANEL 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR PANEL 221MBF ON VTMAE TRAVELER # T24/1753758 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
FLOORBOARD PANEL 222MAF IS DAMAGES FABRICATE ZONE 220 FLOORBOARD PANEL 222MAF ON VTMAE TRAVELER # T24/1753760 IAW DWG SRZ-25-005 REVISION R, MAJOR REPAAIR.
RBL 63 STATION 860 TO 880 CREASE BEAM HAS AREAS OF CORROSION. CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED CREASE BEAM P/N BAC 1515 553124 BATCH NUMBER 0002677936 IAW SRM 53-30-13-01 AND SRM 51-40-02. MAJOR REPAIR
DURING SVC WHILE DOING A LEAK INSPECTION ON APU AREA FOUND APU SURGE DUCT CASING BROKEN AND MISSING MATERIAL RELEASED FOR SERVICE PER MEL : 49-11-01. REMOVED AND REPLACED APU PER MM 49_11_01_4_0 PERFORMED OPERATIONAL TEST ON APU PER MM 49_11_00_2_0 ALL TEST PASSED , NO FAULT NOTED . A/C OK FOR SERVICE
WHILE WORKING ON TSI 25-60/5212, FOUND RH DOOR ARMED LIGHT WORKING INTERMITTENTLY. RELEASED FOR SERVICE PER MEL : 25-66-05-A CATEGORY : C EXPIRATION : 03FEB24 "MEL 25-66-05-A: R1 ESCAPE SLIDE GIRT BAR ENGAGEMENT LIGHTS - INOP. REMOVED AND REPLACED FWD GIRT BAR SLIDER AS PER AMM 25-66-11-2.PERFORMED ADJ TESTS 52-11-00-5.A/C OK FOR SERVICE.MEL COLSED PLACARD REMOVED.
RIGHT ENTRY DOOR SLIDE LIGHT INOP. REPEAT GRIPE. REFER TO ATTACHED PICTURES: SLIDE ARMED THREE TIMES IN A ROW: SLIDE LIGHT COMES UP EVERY TIME. FOLLOWED FIM 25-66 FAULT TREE 802, IAW AMM 25-66-11-2 CLEARANCE DIMENSIONS WITH THE FOLLWING FINDINGS: ON FIG 201 FOUND: CLEARANCE A-A ON AFT SIDE MICROSWITCH: 3.8 MM, CLEARANCE A-A ON FWD SIDE MICROSWITCH 8.0 MM OUT OF LIMITS (3.3 MM - 4.3 MM). RIGHT DOOR SLIDE ARMING GIRT BAR AND SLIDERS CLEANED IAW AMM 12-21-18-3, THEN MEASURED CLEARANCE A-A IAW AMM 25-66- 11-2 AND FOUND FWD SIDE CLEARANCE WITHIN ALLOWABLE DIMENSIONS NOW.
SLIDE LIGHT ON RIGHT ENTRY DOOR BURNED OUT. AMM: 33-16-02-2 RELAMPED PER MM 33-16-02-2.OPS CHECK OK.
RIGHT SIDE ENTRY DOOR SLIDE LIGHT NOT ILLUMINATING WHEN ARMED. AMM: 25-66-11-02. DEBRIS FOUND BETWEEN PROX SWITCH AND GIRT BAR SLIDER, AREA CLEANED, "SLIDE" LIGHT ILLUMINATE IAW AMM 25-66-11-02.
DURING PUSH BACK FROM HANGAR L/H VERTICAL STABILIZER SKIN BETWEEN FIN STA 375-400 AND BETWEEN REAR SPAR AND STR-3 WAS DAMAGED WORK ACCOMPLISHED IN ACCORDANCE WITH FEDEX E.A # F-5530-T0371030, VERTICAL STABILIZER - GOUGE REPAIR ON L/H AFT TORQUE BOX SKIN AND STRINGER S-2 FIN STA 375-400 MAJOR REPAIR
FOUND CORROSION IN FASTENER HOLE #3 UPPER SKIN STRUT AREA L/H WING ACCOMPLISHED IAW FEDEX E.A #F-5730-T0370691 P1 MAJOR REPAIR
FOUND CRAKES CORROSION ,DAMGE IN HOLES #2,#4,#5,#7,#10,#12 AT UPPER SKIN R/H WING STRUT ATTACH AREA ACCOMPLISHED IAW FEDEX E.A # F-5730-T0370683 P1
PDIS 912 29-02 3898 10AUG22 TLV OPEN U LOGPAGES:3336064 UPON REACHING CRUISE FL380 THE '' R HYD QTY'' MESSAGE APPEARED R QTY WAS APPROX 0.48 AND DECREASING. COMPLIED WITH QRH AND CONSULTED GOC. DECLARED EMERGENCY WITH ATC AND RETURNED TO TLV. AMM27-41-05-2 FOUND RH STCM LEAKING. REMOVED AND REPLACED RH STCM AS PER AMM 27-41-05-2. ALL TESTS PASSED. PERFORMED INSPECTION PER 29-11-00-2 TABLE201 , CONDITION 1 (PRESSURE AND CASE DRAIN MODULE FILTER DIFFERENTIAL PRESS INDICATORS) WITH NO FINDINGS. SERVICED RH HYD SYS PER AMM 12-12-01-3.
MDIS 912 33-50 3682 22JUN22 HAJ FACT U LH EMERGENCY SLIDE LIGHT IS NOT ILLIMUNATE FACT 22JUN22 11:56 HAJ U LH DOOR SLIDE EMERGENCY LIHT BULB HAS BEEN REPLACED ACC TO AMM: 33-51-06-2-1
MDIS 912 33-10 3670 17JUN22 VIE FACT U DURING BULB REPLACEMENT FOUND FWD PART OF EMERGENCY LIGHTS "UNARMED" ANNUNCIATOR LIGHT BROKEN. FACT 17JUN22 06:13 VIE U REPLACED EMERGENCY LIGHTS UNARMED ANNUNCIATOR LIGHT IAW AMM 33-16-02 WITH SPARE FROM KORE KIT . MPN 674-1031-2234
STA 1681 FRAME APPROX STR17R HAS CRACK INDICATION ALL WORK ACCOMPLISHED IAW FEDEX EA F-5310-T0356589 P1 FUSELAGE - EXISTING FLOOR BEAM REPAIR AT STA 1681, RBL44 TO RBL50 (EO F-5310-E0329555)
LT WING NR 2 SLAT LOWER COVE PANEL HAS EVIDENCE OF A CRACK ON INBOARD SIDE INBOARD MAIN TRACK ATTACH POINT TO SLAT REMOVED. FABRICATED AND INSTALLED NEW COVE PANEL, IAW B757 SRM 51-40-02, 51-40-05 AND BOEING DWG 114N4076 REV C. PERFORMED SATISFACTORY OPERATIONS CHECK, IAW B757 AMM 27-81-02-4 FIG 401.
LT ELELATOR UPPER SKIN HAS A GOUGE AT OUTBOARD SIDE, DOT 168 004. APPLIED PERMANENT REPAIR TO LT ELEVATOR UPPER SKIN, IAW B757 SRM 55-20-01-2R FIG 201 TABLE 1 AND SRM 51-70-17-OG PAR 4B.
N912FD FOUND EMERGENCY BATTERY PACK OF DOOR L1 LOW REASON CODE : FAILED OPS CK. & REPLACED WITH SERVICABLE UNIT OFF MPN: 2013-1A CPN: 3301128 POS: 1 SRL: 39538 TAG NBR: 7I9496 ON MPN: 2013-1A CPN: 3301128 SRL: 110063 TAG NBR: I62685 REPLACED EMERGENCY BATTERY PACK ACC AMM: 33-51-07-2 REV 125. OLD BATTERY PACK NOT CHARGING PROPERLY ANYMORE
PDIS 912 25-60 0889 23OCT19 BSL OPEN L SLIDE RAFT COVER TORN. FOUND THE ATTACHMENTS OF THE COVER WITH DAMAGE. MEL RAISED FOR RECTIFICATION. "MEL 52-11-01-A: L1 SLIDE INOP."
CORROSION "T" CAP FLOORBEAM MAIN CARGO CABIN STA 1661 LBL 18. REMOVED CORROSION FROM MAIN CABIN FLOOR BEAM "T" CAP, MATERIAL LOSS ".019 FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-1A DETAIL III. REMOVED DAMAGED "T" CAP, FABRICATED NEW "T" CAP FROM BAC1505-100880, DIM. 129", AND INSTALLED NEW "T" CAP REPAIR TO MAIN CABIN FLOORBEAM STA 1661 RBL 58 TO LBL 58 IAW SRM 53-00-51-2 2R REPAIR 9.
MAIN CABIN FLOOR STA 580 LBL 45.5 STUB FLOORBEAM IS CRACKED AFT SIDE IN RADIUS COMPLIED WITH EA TF-5310-T0342277 P1. FLOORBEAM SPLICE SEGMENT UPPER AFT FLANGE CRACK REPAIR LBL 45.5.
MAIN CABIN SEAT TRACK APPROX STA 1185 RBL 24 OUTER FLANGE HAS AREA OF CORROSION AT NUT-PLATE LOCATION. BLENDED AREA OF SEAT TRACK FLANGE AND EVALUATED DAMAGE. ORIGINAL MAT .080" MAT REM .050", MAT LOSS .030", FOUND SEAT TRACK TO BE OUT ALLOWABLE LIMITS IAW SRM 53-00-52-1A. REMOVED DAMAGE SEAT TRACK, FABRICATED NEW SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW DWG 146N5130 REV A, SRM 51-40-02-OG, 51-40-05-OG FROM STA 1180 TO 1280 RBL 24.75.
FOUND CORROSION AT MAIN CABIN FLOOR STRUCTURE "T" CHORD STA 1070 BLB 44.5. FOUND TO BE OUT LIMITS IAW SRM 53-40-01, SRM 53-00-51-1A. REMOVED, FABRICATED NEW "T" CHORD FROM BAC1506-1108, AND INSTALLED NEW "T" CHORD SECTION TO MAIN CABIN FLOOR STRUCTURE STA 1040-STA 1080 LBL 44.5 IAW SRM 51-40-02-0G, DWG 111N5201 REV REV E & DWG 111N5207 REV C.
PASSING 4000 FEET DURING CLIMB OUT, THE MAIN CARGO DOOR LIGHT ILLUMINATED, MCD INDICATIONS, AND OPERATIONS ARE NORMAL WITH NO DEFECTS IAW AMM 52-72-00-5.
BEFORE DEPARTURE, FOUND THE L1 DOOR SLIDE COVER DAMAGED. REPAIRED THE DAMAGED INSERTS ON THE L1 SLIDE COVER IAW AMM 25-00-00-8.
L1 DOOR DOES NOT PROPERTY SEAT WHEN CLOSING, DOES NOT SHOW ARMED. FOUND THE GIRT BAR END NOT ATTACHED TO SLIDE ASSY. SECURED THE GIRT BAR AND ENSURED GOOD FLOOR CLEAT ENGAGEMENT IAW AMM 25-66-01-4. DOOR NOW ARMS NORMALLY. ACFT OK FOR SERVICE.
L1 DOOR IS VERY HARD TO CLOSE WITH HANDLE IN THE VERY LAST PORTION OF TRAVEL WHEN IT LOCKS. REMOVED AND REPLACED THE L1 DOOR HOLD OPEN LOCK COLLAR IAW AMM 52-11-08-8. OPS CHECKED OK. ACFT OK FOR SERVICE.
L1 SLIDE ARMED LIGHT WILL NOT ILLUMINATE WHEN DOOR ARMED. RELAMP L1 SLIDE LIGHT IN REF TO SMP A/C OK FOR SERVICE.
DURING TAKE OFF, THE NR 1 ENGINE EPR GAUGES MATCH UP, BUT N1, EGT, N2, N3, FF WERE 30% LESS. THE AIRCRAFT CLIMBED OUT AND CONTINUED TO HAVE ASSY METRIC THRUST AND PASSED 10K FT ALTITUDE ENGINES CONTINUED TO RUN ABOUT 30 PERCENT APART WITH NOT MUCH THRUST TO CLIMB. AT THAT POINT, DECIDED TO RETURN TO BASE. INSPECTED THE NR 1 ENGINE P1 PROBE, AND FOUND DEBRIS CLOGGING THE PROBE INLET. REMOVED ALL DEBRIS AND INSPECTED P1 PROBE MM 73-21-04-6.
EICAS MSG R EMER DOOR, PRESSURIZATION NORMAL AT FLIGHT LEVEL 390. OPENED R3 EMER DOOR FOR MX IAW 52-21-01-2. REMOVED AND REPLACED RT EMERGENCY DOOR PROX SWITCH SENSOR REFERENCE 757 WDM 52-71-21, ADJ/TEST REFERENCE AMM 52-71-00-5-0, BITE TEST DOOR WARNING SYSTEM REFERENCE FIM 32-09 FAULT TREE 813 ALL TEST NORMAL. REINSTALLED RT EMERGENCY DOOR REFERENCE AMM 52-21-01-2.
R EMER DOOR EICAS MES INTERMITTENT AT FL390. PRESSURIZATION INDICATED NORMAL. ADJUSTED RIGHT FWD DOOR WARNING SENSOR (S10090) REF AMM 52-71-00-5 OPS CHECK GOOD.
WHILE CONFIGURING ACFT FOR LANDING AT 220KTS, POSITIONED FLAP LEVER TO 1. FLAP GAUGE SHOWED BETWEEN UP 1, EICAS SHOWED LE SLAT DISAGREE. COMPLIED WITH QRH. NO PROBLEM LANDING. SECURED THE INBD AND OTBD TORQUE TUBE COUPLINGS ON THE SLAT ROTARY ACTUATORS NR 13 , 11, AND 17 IAW AMM 27-81-18-4. ACFT OK FOR SERVICE.
LE SLAT DISAGREE CAUTION. COULDNT FIX USING QRH. INDICATION BETWEEN UP AND 1. R & R NR 1 FSEU AND OPS CHECK IAW MM 27-51-01-2. OPS NORMAL IAW MM -32.
ON FINAL APPROACH GEAR DOORS LIGHT REMAINED ILLUMINATED DISCONTINUED APPROACH. DURING GO-AROUND LIGHT WENT OUT. LIGHT STAYED OUT THROUGH LANDING. CYCLED GEAR DOORS IAW AMM 32-00-15-2. CHECKS GOOD. PERFORMED PSEU BITE PROCEDURE IAW FIM 32-30 FIG 802. NO FAULTS NOTED AT THIS TIME. A/C OK TO CONTINUE.
LT WING IB FLAP LOWER SURFACE DEEPLY GOUGED WITH POSSIBLE CRACK.
IN APPROACH ENVIRONMENT, WE SLOWED TO 210 KTS AND FLAP INDICATOR TWITCHED BETWEEN FLAPS UP & 1. WE EXTENDED FLAPS TO FLAPS 1 & WE GOT L/E SLAT ASYM & SLAT DISAGREE. RAN L/E SLAT ASYM CK LIST, THEN DISAGREE CK LIST, LANDED. ALSO, L/E AMBER LIGHT CAME ON WHEN WE EXTENDED FLAPS WITH ALTERNATE FLAPS. NO ADVERSE FLT CONTROL ISSUES. FIM 27-51, FAULT TREE 805, R & R NR 3 FSEU IAW AMM 27-51-01-2 .
DOOR L1 SEEMS TO BE HANGING OR CATCHING ON THE LOWER PART WHEN OPENING & CLOSING. THE BOTTOM HALF OF THE DOOR STARTS TO FALL AWAY FROM THE DOOR BODY. UPDATED 27 MAY 16. READJUSTED COVER LINING FOR THE ESCAPE SLIDE IAW AMM 52-11-02-4. OPERATIONS & CHECK OF THE L1 DOOR IAW AMM 52-11-00-2 OK. ACFT OK FOR SERVICE.
DURING SERVICE CHECK FOUND EMERGENCY SLIDE LIGHT L25 & EXIT SIGN DOOR LIGHT L31 INOPERATIVE. POWER SUPPLY M731, CHARGER ASSEMBLY & BATTERY PACK REPLACED IAW AMM 33-51-07-2. OPERATIONS TESTED SATISFACTORY, OK FOR SERVICE. R & R CHARGER ASSEMBLY & BATTERY PACK. REPLACED IAW AMM 33-51-07-2.
REJECTED TAKEOFF DUE TO TAKEOFF CONFIG PREVIOUS WRITE-UP. OCCUPIED AS SOON AS I PUSHED THE THROTTLE MODULE & THE POWER CAME UP. RELEASED THE BRAKES. DURING TAKEOFF CONFIGURATION WARNING TEST AMM 31-51-00-5 FOUND CONFIG LIGHT & AURAL WARNING ON WITHOUT ASSOCIATED EICAS MSG. REMOVAL & INSTALLATION OF TAKEOFF CONFIGURATION WARNING MODULE M620, PERFORMED IAW AMM 31-51-04-4, ALL TEST PASSED. NO MORE CONFIG WARNING DURING TAKEOFF. ACFT OK FOR SERVICE.
TAKEOFF CONFIG WARNING WHEN AUTO THROTTLES ENGAGED FOR TAKEOFF, EICAS STABILIZER. STABILIZER CONFIRMED AT 4.0 AFTER REJECTED TAKEOFF. ATTEMPTED TAKEOFF AGAIN WITH SAME RESULT. REMOVAL & INSTALLATION OF STAB TRIM LIMIT POSITION TRANSMITTER MODULE CTR PERFORMED IAW AMM 27-48-01-4. ACFT IS OK FOR SERVICE.
NUMBER 2 ENG OTBD T/R AFT HINGE FITTING UPPER AFT BOLT HOLE IS CRACKED. COMPLIED WITH EA F-5450-T0311024. NACELLES / PYLON - NACELLE STRUT - NR 2 PYLON OTBD THRUST REVERSER HINGE FITTING ATTACH HOLE CRACK.
NUMBER 2 ENG INBD TR AFT HINGE FITTING UPPER AFT BOLT HOLE IS CRACKED. COMPLIED WITH EA F-5450-T0310949 PT 1 NACELLES / PYLON - NR 2 PYLON INBD THRUST REVERSER HINGE FITTING ATTACH HOLE CRACK
INSIDE FWD NOSE COMPARTMENT, BS 231 LOWER FRAME IS DAMAGED AT BL 0. COMPLIED WITH EA F -5310-T0310898, TITLE: FUSELAGE - MAINFRAME - BS 231.25 FRAME INNER CHORD REPAIR BETWEEN BL 6L - 6R.
FUSELAGE HAS A DENT AT BS 680 BETWEEN STRINGERS 26L & 27L. COMPLIED WITH EA F-5330-T0310867. TITLE: FUSELAGE - PLATES AND SKINS - STA 680 SKIN DENT JUST BELOW S26L.
LOWER FUSELAGE HAS A DENT AT BS 1357 STRINGER 27L. CUT OUT DAMAGED AREA, FABRICATED REPAIR PARTS (DOUBLER AND FILLER), AND INSTALLED REPAIR PARTS (DOUBLER AND FILLER) ON SKIN AT BS 1357 BETWEEN STRINGERS 26L AND 27L IAW B757 SRM 53-00-01 REPAIR 15 AND 51-40-02.
ON PREFLIGHT CHECK FOUND L1 DOOR INTERIOR & EXTERIOR EMER LIGHTS INOPERATIVE. R & R EMER LIGHTS POWER SUPPLY ASSEMBLY M731 & EMER LIGHTS BATTERY PACK IAW AMM 33-51-07-2. EMER LIGHTS TEST OK, ACFT OK FOR SERVICE.
UPON TAKEOFF ROLL CAPTAIN`S SPEED TAPE, ALTIMETER & VVSI STARTED TO FLASH INTERMITTENTLY, THEN FASTER, THEN FAILED. PERFORMED LOW SPEED REJECT. R & R LT ADC IAW 34-12-01-4. ACCOMPLISHED OPERATIONAL TEST IAW 34-12-00-5 & ACCOMPLISHED TEST 30 IAW AMM 22-00-00, NO DEFECTS NOTED. ACFT REMAINS CAT III & RVSM IAW GMM 6-5-495.
CAPTAIN'S SLIDING WINDOW LEVER EXTREMELY DIFFICULT TO OPEN & PULL BACK. OPENED CAPTAIN'S NR 2 WINDOW, INSPECTED WINDOW COMPONENTS FOR DAMAGE, NO DEFECTS NOTED. FOUND ALL 4 WINDOW LATCH STUDS TO BE COATED WITH A STICKY FILM & LIGHT DEBRIS, SUSPECT FILM TO BE CORROSION PREVENTATIVE. CLEANED ALL LATCH PINS. ACCOMPLISHED TEST OF CAPTAIN'S NR 2 WINDOW LATCH MECHANISM IAW MM 56-11-02-5. WINDOW LATCH OPERATION IS NOW WITH IN MM LIMITS.
EMERGENCY EXIT LIGHT ABOVE COCKPIT DOOR INOPERATIVE. ALL OTHER EMERGENCY LIGHTS WORK NORMAL. RELEASED FOR SERVICE IAW MEL 33-51-01-01 CATEGORY D. INTERIOR EMERGENCY LIGHTS INOPERATIVE. TROUBLESHOOTING FOUND POWER CIRCUIT DISCONNECT AT LIGHT CONNECTOR. RECONNECT POWER SUPPLY WIRE CONNECTOR, OPERATES NORMALLY.
L1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE DURING TEST. REPLACED LAMP IAW AMM 33-51-06-2-1, OPS CHECKED NORMAL.
L/E FLAPS DISAGREE INDICATION. R & R NR 5 SLAT INBD ROTARY ACTUATOR IAW AMM 27-81-18-4, UP TO STEP 5(K). COMPLETED INSTALLATION OF NR 5 L/E INBD SLAT DRIVE ROTARY ACTUATOR IAW AMM: 27-81-18-4. OPS CHECKED GOOD. ACFT OK TO CONTINUE.
CONFIGURING TO FLAPS 1 TRIGGERED A L/E. SLAT DISAGREE ALERT. WHILE RUNNING QRH CHECKLIST. THE ALT FLAPS SELECTOR WAS FOUND TO BE INOPERATIVE. FLAPS REMAINED STUCK BETWEEN THE UP AND ONE POSITION. FOUND FAULT ON NR 3 FSEU WHICH READ 'FLAP DISAGREE MESSAGE 328. FOUND THIS FAULT WHILE T/E DISAGREE LIGHT ON AND FLAPS LOCKED OUT AND WOULD NOT RESPOND. WHEN FLAPS WERE BEING TESTED IN THE ALTERNATE. WHEN TESTING FLAPS HYDRAULICALLY NO FAULTS FOUND. POWERED DOWN ACFT AND TESTED ALTERNATE AND HYDRAULICALLY NORMAL WITH NO FAULTS. IAW AMM 27-51-00-5 AS PRECAUTIONARY, CHANGED NR 3 FSEU IAW AMM: 29-51-01/201 AND OPERATED FLAPS HYDRAULICALLY AND IN ALTERNATE IAW AMM: 27-51-00-5 OPS CHECK NORMAL. AC OK FOR SERVICE.
CONFIGURING TO FLAPS 1 TRIGGERED A L/E SLAT DISAGREE ALERT. WHILE RUNNING QRH CHECKLIST, ALT FLAPS SELECTOR WAS FOUND TO BE INOPERATIVE. FLAPS REMAINED STUCK BETWEEN THE UP AND ONE POSITION. FOUND FAULT ON NR 3 FSEU WHICH READ "FLAP DISAGREE" MESSAGE 328. FOUND THIS FAULT WHILE T/E DISAGREE LIGHT ON AND FLAPS LOCKED OUT AND WOULD NOT RESPOND. WHEN FLAPS WERE BEING TESTED IN THE ALTERNATE. WHEN TESTING FLAPS HYDRAULICALLY NO FAULTS FOUND. POWERED DOWN ACFT AND TESTED ALTERNATE AND HYDRAULICALLY NORMAL WITH NO FAULTS. AMM 27-51-00-5 AS PRECAUTIONARY CHANGED NR 3 FSEU IAW AMM: 29-51-01/201 AND OPERATED FLAPS HYDRAULICALLY AND IN ALTERNATE IAW AMM: 27-51-00-5, OPS CHECKED NORMAL. ACFT OK FOR SERVICE.
L1 DOOR LOWER HINGE GUIDE, ARM SUPPORT BACKET FOUND DETATCHED FROM THE DOOR. FOUND IMPROPER HINGE BOLTS INSTALLED IN LOWER L1 DOOR HINGE PLATE INSTALLED PN BACB30 NM4K13, BOLTS IN HINGE PLATE AND THEY GRIPPED PROPERLY AMM 52-11-01-4 AND REF PN, CMM 52-11-07, FIG 2, ITEM 632D. FINISHED INSTALL OF SLIDE AND COVER REF AMM 52-11-00-5. OPS CHECKED GOOD AND ALSO COMPLIED WITH EA F-5210-16842. OK FOR SERVICE.
ON ARRIVAL L1 DOOR GIRT BAR ASSY REMAINED ATTACHED TO FLOOR WHEN DOOR WAS OPENED. L-1 DOOR WOULD NOT CLOSE AND LOCK WITH SLIDE INSTALLED. REMOVED SLIDE AND PLACED BEHIND RCB DOOR, NOW CLOSES AND LOCKS. FOUND FWD RADIUS ROD RIG PIN OUT A HALF HOLE. ADJUSTED ROD AND LINK ADJUSTMENT SCREW REF MM 52-11-25-5. RIG PIN NOW FITS SMOOTHLY. CYCLED DOOR ARM LEVER SEVERAL TIMES. COMPLIED WITH ADJUSTMENT & TEST OF L1 DOOR GIRT BAR IAW AMM 52-11-25-5 , REMOVED AND REPLACED GIRT BAR IAW AMM 52-11-25-5. DOOR ARMS AND DISARMS NORMALLY.
ABOUT 2000 FT AGL ON CLIMBOUT "LT FWD ENT DOOR" EICAS MESSAGE ILLUMINATED W/CORRESPONDING DISCRETE "ENTRY DOORS" LIGHT ILLUMINATED ON OVERHEAD PANEL. JUMPSEATER IN COURIER AREA WITNESSED DOOR HANDLE MOVE APPROX 5-6", DOOR ARMED BLOCKER DID NOT MOVE AND DOOR SLIDE REMAINED ARMED. ACFT PRESSURIZED NORMALLY. PERFORMED GVI ON L1 DOOR IAW MTSI 52-10/4281. FOUND ALL FWD SIDE OF DOOR STOP PINS OUT OF ADJUSTMENT. ADJUSTED DOOR STOP PINS IAW MM 52-11-00-5. PRESSURIZED ACFT & CHECKED HANDLE. DOES NOT POP OUT OF CLOSED POS. ARMED & DISARMED, BOTH THE SAME. HANDLE TENSION NORMAL.
LEFT FWD ENTRY DOOR EICAS AND ENTRY DOORS LIGHT ON CLIMBOUT. HEARD A NOISE COMING FROM THE L1 DOOR AND WITNESSED THE HANDLE POP UP AND THE DOOR ARMED BLOCKER RETRACT. DURING THE CHECK FOR THE ADJUSTMENT OF THE HANDLE MECHANISM, FOUND COCKING PUSHROD TOO LONG. ADJUSTED PUSHROD IAW AMM 52-11-13-2. FOUND EXTERIOR DOOR HANDLE LATCH OVERLAP GAP OUT OF TOLERANCE TOO SHORT. ADJUSTED OVERLAP IAW AMM 52-11-13-2. ALSO, FOUND EXTERIOR HANDLE LATCH STICKING IN THE OPEN POSITION. RETORQUED LATCH IAW STANDARD TORQUE AND IT BEGAN TO OPERATE SMOOTHLY. REINSTALLED ESCAPE SLIDE IAW AMM 25-66-01-4. REINSTALLED DOOR LINING IAW AMM 52-11-02-4. OK FOR SERVICE.
DURING APPROACH, AT ABOUT 700 FT AGL, LEFT FWD ENTRY DOOR EICAS AND DISCRETE ENTRY LIGHTS ILLUMINATED. AFTER SHUTDOWN, THE LT FWD DOOR HANDLE WAS FOUND IN THE PARTIALLY OPEN POSITION. DOOR TORQUE FOR UNLATCHING INTERIOR DOOR HANDLE WAS BELOW MINIMUMS. ADUSTED L1 DOOR UNLATCHING TORQUE IAW AMM 52-11-00-206. OPS CHECKED L1 DOOR IAW AMM 52-11-00. ACFT RELEASED FOR SERVICE.
L1 DOOR SLIDE WILL NOT ARM. FOUND UPPER FWD LATCH ROLLER BROKEN. R & R UPPER FWD LATCH ROLLER IAW AMM 52-11-00-5.
L1 DOOR EXTREMELY HARD TO CLOSE AND ARM. COVER OVER SLIDE IS LOOSE. FOUND L1 SLIDE COVER NOT PROPERLY LATCHED AT TOP LEFT ATTACHMENT. PROPERLY INSTALLED COVER ASSY IAW AMM CH 52-11-02-4. DOOR OPERATES AND ARMS/DISARMS PROPERLY. OK TO CONTINUE.
L1 DOOR WILL NOT ARM. FOUND RT SIDE LOWER SLIDE PAN MOUNT BOLT LOOSE. TIGHTENED BOLT. RE-ROUTED SLIDE RETENTION CORD IAW AMM 25-66-01-4. OPS CHECKED GOOD.
SEAT TRACK CORRODED STA 900-1070, LBL 45.5. FOUND OUT OF LIMITS IAW SRM 53-00-52 AD1. REMOVED, FABRICATED, AND INSTALLED NEW SEAT TRACK SECTION IAW SRM 53-40-52 FIG 1, DWG 144N5002 REV H AND SRM 51-40-02.
LEFT FORWARD DOOR WILL NOT CLOSE OR OPEN. APPEARS TO HAVE JUMPED OFF A ROLLER. REMOVED SLIDE PACK COVER FROM L1 DOOR. FOUND GIRT BAR SLIDER NOT COMPLETELY CLEAR OF AFT FLOOR FITTING. FOUND ONCE GIRTBAR WAS FREED, THE MODE SELECTOR WAS FULLY DISARMED WITH DOOR PARTIALLY OPEN CAUSING DOOR TO BIND DUE TO GIRT BAR. OPENED AND CLOSED DOOR SEVERAL TIMES DOOR OPS NORMAL PER MM 52-11-00-2. CHECKED GIRT BAR PER MM 52-11-25-5. GIRT BAR ARMS AND DISARMS NORMAL.
LT FORWARD WINDOW SHATTERED ENROUTE, DIVERTED.
FOUND GIRT BAR OUT OF TRACK. ADJUSTED GIRT BAR MECHANISM IAW MM 52-11-25-5. DOOR OPENED AND CLOSED NORMAL.
DOOR SLIDE ILLUMINATION LIGHT INOPERATIVE. RELAMPED IAW AMM 33-51-06-2-1. OPS CHECKED GOOD.
FUSELAGE SKIN DAMAGED FOLLOWING TAIL STRIKE, BS 1701 TO 1745, REPAIRED IAW EA F-5330-158298, REV NR POS P1.
WHEN ARMING RT ENTRY DOOR ARM LIGHT WILL NOT ILLUMINATE. FOUND SLIDE COVER CORD TANGLED IN GIRT BAR. INSTALLED SLIDE COVER CORRECTLY IAW MM 52-11-02. OPS CKD GOOD. FINAL CLOSED.
R1 DOOR SLIDE ARM LIGHT WILL NOT COME ON WHEN SLIDE IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE AND CLEANED TRACK. DOOR LIGHT OPERATED NORMALY WHEN DOOR IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE AND CLEANED TRACK. DOOR LIGHT OPERATED NORMALY WHEN DOOR IS ARMED.
R1 DOOR SLIDE ARM LIGHT WILL NOT COME ON WHEN SLIDE IS ARMED. FOUND GREASE AND ICE BLOCKING PROXIMITY SWITCH. REMOVED ICE AND CLEANED TRACK. DOOR LIGHT OPERATED NORMALY WHEN DOOR IS ARMED.
DENT IN FUSELAGE SKIN AT STATION 475, STR 19L. EVALUATED DENT AND FOUND OUT OF LIMITS IAW SRM 53-00-01 FIG 101, TRIMMED OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND REPAIR FILLER 2 AND STRUCTURAL FILLER IAW EA F-5330-143914. TREATED, PRIMED AND INSTALLED REPAIR IAW SRM 51-20-1 AND EA F-5330-143914.
LANDING GEAR FAILED TO COME UP. RAN QRH PROCEDURE USING LOCK OVERIDE AND GEAR CAME UP. UNCOVERD AND SELECTED TO ALTN POSITION. ALL 3 MLG PINS INSTALLED AND SAFETIED. GEAR LEVER LOCK CB ON P11 PANEL FOUND PULLED AND COLLARED. UNCOLLARED LEVER LATCH CB, ERASED PSEU MEMORY, SIMULATED FLT MODE IAW MM 32-09-02-2. PLACED GEAR HANDLE IN UP POSITION. LANDING GEAR LEVER LATCH CHECKS GOOD. RESTORED ACFT TO GROUND MODE IAW MM 32-09-02-2. REPLACED VMO/MMO S10471 TO THE NORMAL POSITION AND SHEAR WIRED. REMOVED ALL 3 GEAR PINS AND STOWED. ACFT OK TO CONTINUE, RII COMPLIED WITH.
ON APPROACH, PUT GEAR LEVER DOWN. GOT NO NOSE GEAR INDICATION. HAD GEAR DISAGREE MESSAGE, GEAR AND DOOR LIGHTS. RAN CHECKLIST AND LOWERED GEAR WITH ALT IXT SWITCH. COULD HEAR NOSE GEAR EXTENDING. GOT 3 GREEN INDICATIONS AND DOOR LIGHT. LANDED NORMALLY. RELEASED FOR SERVICE IAW MEL: 32-30-01.
FRAME AT STA 1280 RT, STR 14-10 HAS GOUGES. REPLACED FRAME SEGMENT FROM STR 7R TO 14R IAW SRM 51-40-05. FRAME SEGMENT FABRICATED ON MAE TR T/9/812786, CHANNEL 1 FABRICATED ON MAE TR T9/812787, CHANNEL 2 FABRICATED ON MAE TR T9/812788. ORIG MAT'L .071 AFTER .046. DAMAGE MEASUREMENTS .025"D X .200"W. MAJOR REPAIR, CATEGORY 'A'.
DENT ON FUSELAGE SKIN AT BS 1575, S-26R. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 16. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
DENT ON FUSELAGE BS 1628, AT S-26L. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01, DETAIL 3. HFEC ACCOMPLISHED WITH NO CRACKS NOTED. ACCOMPLISHED REPAIR AND INSTALLED IAW SRM 53-00-01, REPAIR NR 7, FIG 1 AND 2. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
VERTICAL STAB, RT SIDE CROWN PANEL ATTACHMENT STRIP HAS DAMAGED HOLES, LOWER AFT CORNER. ACCOMPLISHED VERTICAL STAB FIXED T/E BEAM REPAIR AND FITTING REPLACEMENT IAW EA F-5530-124086, AND ATTACHMENTS A AND B OF EA, RELEASE DATE 04/20/09. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
LOWER LOBE FUSELAGE SKIN, BS 485, LBL, DENTED. REPAIR ACCOMPLISHED ON MAE 757-5300-16-A1824.
MAIN CABIN FLOORBEAM UPPER CHORD LOWER SURFACE HAS CORROSION, STA 1681. MAIN CABIN FLOORBEAM UPPER CHORD REPAIRED IAW EA 757-5365-16-F1710 REV-C AT STA 1681, LBL- 58, TO RBL- 58. REPAIR CLASSIFIED AS MAJOR ALTERATION.
AFT CARGO DOOR LOWER FWD CORNER, REPAIR DOUBLER IS DAMAGED. REPAIRED IAW SRM 52-30-01 FIG 201 REPAIR NR 4. THIS REPAIR IS A CATEGORY "B" MAJOR REPAIR. REFER TO SRM 52-30-01 PAGE 204 TABLE IV FOR INSPECTION REQUIREMENT.
LOWER FUSELAGE SKIN, DENT AT BS 1395 BL 0. CHECKED LIMITS IAW SRM 53-00-01 FIG 101 DETAIL LLL FOUND TO BE WITHIN LIMIT DEPTH=.016" WIDTH=0.69" LENGTH=0.75" A/Y RATIO=43. NDT CHECKED FOUND CRACK 0.075". REPAIRED CRACK IAW SRM 53-00-01 REPAIR 16 FIG 201 PAGE 201. THIS REPAIR IS CATEGORY "B" MAJOR REPAIR.
RT WING SLAT NR 7 SKIN BETWEEN STA OSS 404.80 AND OSS 427.85 MISREPAIRED. REPAIRED IAW SRM 57-43-01, REPAIR 1, MAJOR REPAIR, CATEGORY "A".
DURING FOLLOW ON INSPECTION, FOUND FRAME AT BS 1420, 3" BELOW AFT CARGO DOOR SILL TO BE CHAFED. REMOVED 3 SUPPORT ANGLE, DOUBLER, DOOR STOP SUPPORT AND SUPPORT WEB PER SRM 51-40-02 AT BS 1420, BETWEEN RBL 16-23. REMOVED DAMAGED AREA OF FRAME AT BS 1420, 3 INCH BELOW AFT CARGO DOOR SILL PER SRM 51-70-11. REPAIR CHANNEL FABRICATED ON MAE TRAVELER NR T9/775858. LOCATED, DRILLED, TREATED, PRIMED AND TOP COATED REPAIR CHANNEL PER SRM 51-40-05, 51-20-01, AMM 51-21-10. INSTALLED 3 SUPPORT ANGLE, SUPPORT DOUBLER, DOOR STOP SUPPORT, SUPPORT WEB AND REPAIR CHANNEL PER SRM 51-70-11 AND 51-40-02 AT BS 1420, RBL 16-23, 3 INCH BELOW AFT CARGO DOOR SILL. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR.
FRAME STA 860 CRACKED BETWEEN STRINGER 3L AND 4L DAMAGE AREA 0.6" OUT LIMITS IAW 757 SF SRM 53-00-07. FABRICATED REPAIR CHANNELS -1,-2. REMOVED DAMAGE AREA IAW 757 SRM 53-00-07. INSTALLED REPAIR IAW SRM 53-00-07, REPAIR 3, FIG. 201. MAJOR REPAIR, CATEGORY "B".
3 HOLES AT STA 1300 BETWEEN STRINGER 5R AND 4R ARE OUT OF LIMIT. REMOVED DAMAGED AREA IAW 757 SF SRM 53-00-07 REPAIR NR3 FIG 201. FABRICATED REPAIR CHANNELS -1 AND -2. INSTALLED REPAIR CHANNELS IAW SRM 53-00-07 REPAIR NR 3 FIG 201. THIS REPAIR IS A CATEGORY "B" MAJOR REPAIR.
LT WING FRONT SPAR STA FSS 295 VERTICAL ANGLE STIFFENER CRACKED AT UPPER END. REMOVED STIFFENER IAW SRM 51-40-02. FABRICATED NEW STIFFENER ON MAE TRAV NR T9/ 777512 DRAWING NR 112N2036. INSTALLED STIFFENER NR 1 PYLON STA FSS 295, IAW SRM 51-40-02. CATEGORY A, MAJOR REPAIR.
DURING INSPECTION FOUND AFT CARGO PIT DOOR LOWER SILL TEE CHORD FIRST SCREW HOLE FROM STA 1400 TO BE ELONGATED. REMOVED AND REPLACED WITH NEW TEE CHORD P/N 146N8522-57. THIS IS A MAJOR CATEGORY 'A' REPAIR. NO FOLLOW-UP REQUIRED .
AFT CARGO PIT STA 1380, STR 25-26L FRAME HAS MISDRILLED HOLE AND IS GOUGED. REPAIRED IAW SRM 53-00-07 REPAIR NR 5 FIG 201. THIS IS A MAJOR CATEGORY 'B' REPAIR WITH INITIAL INSPECTION 37,500 FLIGHT CYCLES OR 50,000 AIR FRAME CYCLES WHICHEVER COMES FIRST-REPEAT-HFEC AT 12,000 FLIGHT CYCLES PER NDT, PAT 6, 51-00-01.
FWD PIT BILGE, BS 770, LBL 15, S-27L, HAS CORROSION UNDER EXISTING REPAIR DOUBLER. REMOVED EXISTING REPAIR SPLICE IAW SRM 53-00-03, REPAIR NR 1, FIG 201. THERE WAS 100 PERCENT MATERIAL LOSS, REMOVED SPLICE. LOCATED AND DRILLED NEW STRINGER SPLICE IAW SRM 53-00-03, REPAIR NR 1, FIG 201, P/N 654N0010-133. INSTALLED NEW STRINGER SPLICE AT BS 770, LBL 15, S-27L, IAW SRM 53-00-03, REPAIR NR 1. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.
MAIN CABIN FLOORBEAM WEB AT STA 365 RBL 41 HAS DAMAGE. REPAIRED IAW EA 757-5315-16-F1708, REV A. AS PER EA FUNCTION IS ALTERATION AND CLASSIFICATION IS FORM 8110-3/RAS/8100-9.
FRAME STA 940 UPPER FLANGE HAS DENT AT STR 6L. REPAIRED FRAME AT STA 940 STR 6L IAW SRM 53-00-07 REPAIR NR 1 DETAIL II. THIS REPAIR IS A CATEGORY "A" MAJOR REPAIR AND NO FOLLOW UP ACTION REQUIRED.
AFT CARGO PIT STA 1340, STR 25-27L FRAME IS GOUGED. REPAIRED FRAME AT STA 1320 BET STR 25-27L IAW SRM 53-00-07 FIG 201 REPAIR NR 5 DETAIL I. THIS REPAIR IS CATEGORY "B" MAJOR REPAIR.
AFT CARGO PIT STA 1320 STR 26-27L FRAME IS GOUGED. REPAIRED FRAME AT STA 1320 STR 26-27L IAW SRM 53-00-07 FIG 201 SHEET 4. THIS REPAIR IS A CATEGORY "B" MAJOR REPAIR.
INTERCOSTAL ON L-1 DOOR THRESHOLD AREA HAS CORROSION, APPROX BS 346-361. REMOVED CHANNEL ON L-1 DOOR THRESHOLD FROM STA 346-STA 361 LT SIDE IAW SRM 51-40-02. REMOVED CORROSION IAW SRM 53-10-15. ORIG MAT 0.050 INCH REMAINING MAT 0.041 INCH FOUND TO BE OUT OF LIMIT. RECEIVED NEW CHANNEL ON MAE TRAVELER T8/774315. INSTALLED NEW CHANNEL ON STA 346-361 LBL 60 IAW SRM 51-70-12 AND SRM 51-40-02. THIS IS A CATEGORY "A" MAJOR REPAIR.
SEAT TRACK STA 650 RBL 24 CORRODED. REMOVED CORROSION FOUND TO BE OUT OF LIMIT IAW SRM 53-00-52, ORIG MAT 0.100 REMAINING MAT 0.074. REMOVED SEAT TRACK IAW SRM 51-40-02 AND 53-00-52. FABRICATED NEW SEAT TRACK IAW SRM 53-00-52 FROM BAC1520-792/24 BATCH NR 1142187. INSTALLED NEW SEAT TRACK IAW SRM 51-40-02. THIS IS A CATEGORY "A" MAJOR REPAIR.
MAIN CABIN FLOORBEAM STA 345 LBL 5 UPPER CHORD HAS CORROSION. REMOVED DAMAGED AREA STA 345 RBL 9 - LBL 52. FABRICATED T-CHORD MATERIAL BAC 1505-100617 BATCH NR 1512047. FABRICATED AND RECEIVED REPAIR PARTS ON MAE TRAVELER'S T8/775104, T8/775103, T8/775107, T8/775108 AND T8/774642 IAW SRM 53-00-51 FIG 201 REPAIR 3. INSTALLED TEE CHORD AND REPAIR PARTS IAW SRM 53-00-51 FIG 201 REPAIR NR 3. THIS IS A CATEGORY "A" MAJOR REPAIR.
ELEVATOR COMPARTMENT BILGE AREA STRINGER SPLICE INNER SKIN OTBD OF DOOR 313AB LT CUTOUT AT STA 1868-1880 HAS SURFACE CORROSION. REMOVED CORROSION IAW SRM 51-10-02, FOUND OUT OF LIMITS IAW SRM 53-00-03 FIG 101 DETAIL II. RECEIVED NEW STRINGER ON TRAVELER NR T8/773379. INSTALLED NEW STRINGER IAW SRM 51-40-02 AND SRM 53-00-03. THIS IS A CATEGORY "A" MAJOR REPAIR.
AFT CARGO PIT, BS 1480, S-26L, FRAME IS BENT AND GOUGED. CUT OUT DAMAGE AREA PER SRM 53-00-07, REPAIR NR 5, AT BS 1480, S-26L. REFORMED AREA PER NTM51-00-19, PART 6, NO CRACKS NOTED. FABRICATED AND RECEIVED REPAIR "J" CHANNEL PER MAE TRAVELER NR T8/772967. LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED REPAIR PARTS AT BS 1480, S-26L, PER SRM 51-40-05, 51-20-01, 51-21-00-7, AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING REQUIREMENTS: INITIAL AT 37,500 FC; THEREAFTER EVERY 12,000 FC.
R1 DOOR INNER SKIN 5 INCH FROM TOP 10 INCH FROM AFT EDGE IS DAMAGED. REMOVED DAMAGED PORTION OF INNER SKIN IAW SRM 51-10-02 AND SRM 51-70-13 FIG 1. FABRICATED REPAIR DOUBLER PER MAE TRAVELER NR T8/773998. INSTALLED REPAIR DOUBLER IAW SRM 51-70-13 FIG 1 AND SRM 51-40-02. TOP COATED REPAIR IAW SRM 51-20-01. THIS IS A CATEGORY "A" MAJOR REPAIR.
SEAT TRACK AT BS 640, RBL 45, HAS CORROSION. REMOVED CORROSION AT BS 640, RBL 45, IAW SRM 53-00-52, FIG 101. CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101; ORIGINAL MATERIAL WAS .125 INCH, AFTER REWORK .070 INCH (L=1.0 INCH, W=.250 INCH, D=.055 INCH). FABRICATED REPLACEMENT SEAT TRACK ASY IAW SRM 53-00-52, REPAIR INCH 1. REMOVED DAMAGED SEAT TRACK AND INSTALLED REPLACEMENT SEAT TRACK, AT BS 600-640, RBL 45, IAW SRM 53-00-52, REPAIR NR 1. THIS REPAIR IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.
SEAT TRACK, BS 1080-1180, RBL 45, HAS LUG DAMAGE. REMOVED AND REPLACED SEAT TRACK ASSY, IAW SRM 51-40-02. REPLACEMENT SEAT TRACK ASSY FABRICATED ON MAE TRAVELER T8/771189 IAW SRM 53-00- 52. LUG REWORK DIMENSIONS, ON DAMAGED SEAT TRACK, WERE AS FOLLOWS: L=.250 INCH, W=.100 INCH, D=.035 INCH. THIS IS CLASSIFIED AS A CAT. "A" MAJOR REPAIR.
MAIN CABIN METAL FLOOR PANEL STA 1681 TO STA 1720 HAS CORRROSION SEVERAL SPOTS. ENTIRE AREA. REMOVED CORROSION ON IAW SRM 51-10-02, FOUND (2) SPOTS OUT OF LIMITS, FABRICATED. (2) DOUBLER REPAIRS IAW SRM 53-60- 51; ALTERNATIVE 1-REPAIR 2, TREATED, PRIMED AND INSTALLED (2) DOUBLER REPAIRS IAW SRM 51-20-01 AND 51-40-02.THIS IS CATEGORY "A" AND MAJOR REPAIR.
FRAME BS 760 S23 AND 24L DENTED. REPAIRED FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5. THIS IS A MAJOR AND CATEGORY "B" REPAIR.
NR 2 PASS DOOR RT SIDE LOWER CUT-OUT FRAME WEB SUPPORT ANGLE HAS SURFACE CORROSION. REMOVED AND REPLACED NR 2 PASS DOOR RT SIDE LOWER SUPPORT ANGLE IAW SRM 51-40-02 USING FABRITAED NEW CREASE BEAM . THIS IS A MAJOR AND CATEGORY "A" REPAIR.
NR 2 PAX DOOR LEFT LOWER CUT OUT FRAME WEB AND ANGLE SUPPORT HAVE SEVERAL SPOT OF CORROSION AT STA 690-730. REMOVED ANGLE SUPPORT AND FABRICATED, LOCATED, DRILLED,TREATED, PRIMED AND INSTALLED NEW ANGLE SUPPORT IAW SRM51-40-02, 51-40-05, 51-40-06 AND 51-20-01. REMOVED WEB ON STA 680-700 AND FABBED NEW WEB ON MAE TRAVELER NR T8/767742, LOCATED, DRILLED, TREATED, PRIMED AND INSTALLED NEW WEB IAW SRM 51-40-02, 51-40-05, 51-40-06, 51-20-01. THIS IS A MAJOR AND CATEGORY "A" REPAIR.
FWD PIT, FUSELAGE FRAME BS 780, INNER CHORD, (SLOPING), BETWEEN S24R AND S25R, HAS A DENT. REMOVED DAMAGED SECTION OF BS 780 FRAME, BETWEEN S24R AND S25R, PER SRM 53-00- 07, REPAIR NR 5. RECEIVED FABRICATED FRAME REPAIR PARTS ON MAE TRAVELER NR T8/772747. LOCATED, DRILLED, TREATED AND PRIMED REPAIR PARTS PER SRM 51-20-01, 51-21-00 AND 51-40-02. INSTALLED BS 780 FRAME REPAIR, BETWEEN S24R AND S25R, PER SRM 51-40-02, 51- 20-05, AND 53-00-07, REPAIR NR 5. THIS REPAIR IS CLASSIFIED AS A CAT "B" MAJOR REPAIR WITH THE FOLLOWING TRACKING REQUIREMENTS: INITIAL AT 37,500 FC AT TIME OF REPAIR OR 50,000 FC WHICHEVER OCCURS FIRST, THEREAFTER EVERY 12,000 FC.
MAIN CABIN FLOORBEAM UPPER CHORD STA 365 FROM BL 0 TO RBL 65 HAS CORROSION. REMOVED PREVIOUS TEE REPAIR FROM STA 365 LBL 17 TO RBL 70 IAW SRM 53-00-51 FIG 201 REPAIR NR 3. FABRICATED TEE AND REPAIR PARTS IAW SRM 53-00-51 FIG 201. INSTALLED TEE AND REPAIR PARTS AT STA 365, LBL 17 TO RBL 70 IAW SRM 53-00-51 FIG 201 REPAIR NR 3. THIS REPAIR IS CLASSIFIED AS CATEGORY "A" MAJOR REPAIR.
MAIN CABIN STA. 1280 STR.11-14L FRAME IS GOUGED. CUT, REMOVED, FABRICATE AND INSTALLED REPAIR PARTS AS PER MAE TRAVELER NR T8/769971 AND T8/769950 IAW SRM 53-00-07 FIG 201, SRM 51-40-05 AND AMM 51-21-00-7. REPAIRED GOUGED FRAME IAW SRM 53-00-07, REPAIR NR 1 AT BS 1280, STR 11- 14L. THIS IS A MAJOR AND CATEGORY "A" REPAIR.
AFT CARGO PIT STA 1560 STR 24-25R, FRAME AND FRAME SPLICE ARE GOUGED. BLENDED AND SMOOTHED FRAME FOUND WITHIN LIMITS IAW SRM 53-60-07 AND SRM 53-00-07 FIG 101 DETAIL 2. REMOVED AND FABRICATED NEW SPLICE FRAME WITH MAE TRAVELER NR T8/771003, LOCATED, DRILLED HOLES, TREATED, PRIMED, PAINTED AND INSTALLED SPLICE FRAME IAW SRM 51-40-02. THIS IS MAJOR AND CATEGORY "A" REPAIR.
AFT CARGO PIT STA.1540 STR 25R FRAME HAS A MISDRILLED HOLE. REPAIRED AFT CARGO PIT STA 1540 STR 25R FRAME IAW SRM 53-00-07 FIG 201 REPAIR 5 ZONE 1.I INSPECTION THRESHOLD 37500 FLIGHT CYCLES AFTER REPAIR INSTALLATION OR 50000 AIRFRAME FLIGHT CYCLES, WHICHEVER COMES FIRST. REPEAT INSPECTIONS , HIGH FREQUENCY EDDY CURRENT AND DETAILED INSPECTION AT 12000 FLIGHT CYCLES PER NDT, PART 6, 51-00-01. THIS IS A MAJOR AND CATEGORY "B" REPAIR.
SEAT TRACK BS 418-440, RBL 24, GOUGED AND CORRODED. AFTER EVALUATION, DAMAGE ON SEAT TRACK, RBL 24, BS 418-440, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52. REMOVED SEAT TRACK IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON MAE TRAVELER NR T8/769432. LOCATED AND DRILLED NEW SEAT TRACK, TREATED AND PRIMED AND PAINTED NEW SEAT TRACK IAW SRM 51-20-01. INSTALLED NEW SEAT TRACK, BS 418-440, RBL 24, IAW SRM 51-40-02/53-00-52. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.
SEAT TRACK BS 418-440, RBL 45, IS GOUGED AND CORRODED. REMOVED CORROSION FROM SEAT TRACK, BS 418-440, RBL 45, IAW SRM 53-00-52. FOUND CORROSION TO BE OUT OF LIMITS IAW SRM 53-00-52. .021 INCH MATERIAL REMOVED. REMOVED SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02. RECEIVED NEW SEAT TRACK ON MAE TRAVELER NR T8/769433. LOCATED, DRILLED, TREATED AND PRIMED AND PAINTED NEW SEAT TRACK, BS 418-440, RBL 45, IAW SRM 51-40-02/51-20-01. INSTALLED NEW SEAT TRACK, BS 418- 440, RBL 45, IAW SRM 51-40-02. THIS REPAIR IS CLASSIFIED AS A CAT "A" MAJOR REPAIR WITH NO FOLLOW UP TRACKING.
SEAT TRACK BS 418-440 LBL 24 GOUGED AND CORRODED. R & R, TREATED AND PRIMED NEW FABBED SEAT TRACK ON MAE TRAVELER T8-769431 AND INSTALLED ON STA 418-440 LBL24 IAW SRM 51-40-02, 1 REPAIR CATEGORY A.
SEAT TRACK STA 418-440 LBL 24 GOUGED AND CORRODED. REMOVED, REPLACED, TREATED AND PRIMED NEW FABRICATED SEAT TRACK ON MAE TRAVELER NR T8-769431 AND INSTALLED ON STA 418-440 LBL24 IAW SRM 51-40-02 NR 1 REPAIR CATEGORY A.
SEAT TRACK STA 418-440 LBL 45 GOUGED AND CORRODED. REMOVED, REPLACED, TREATED AND PRIMED NEW FABRICATED SEAT TRACK ON MAE TRAVELER NR T8-769420 AND INSTALLED ON STA 418 -440 LBL 45 IAW SRM 51-40-02. THIS IS A NR 1 REPAIR CAT A.