N287FE
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FEDERAL EXPRESS CORP | Operator | 2023-10-18 – 2023-10-18 | Operator named in NTSB report |
| FEDERAL EXPRESS CORPORATION (FDEA) | Operator | 2023-10-18 – 2023-10-18 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
EXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 654+110 TO 654+115, S37R. MEASURED ORIGINAL THICKNESS AT .085 AND REMAINING AT .067 FOR A DIFFERENCE OF .018 REMOVED, PER 767 NDTM PART 4 51- 00-10 PROCEDURE 2. BLEND FOUND TO BE OUT OF LIMITS EXCEEDS 15% PER SRM 53-00-01-1A. FIG 101 SHEET 6. CON'T WITH REPAIR. NO CRACKS IDENTIFIED. REPAIRED SKIN USING B767 SRM 53-00-01-2R REPAIR 12 LAP SPLICE EXTERNAL REPAIR. THIS IS A CAT B MAJOR REPAIR
EXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 541 BETWEEN S39R AND S39L. EXTERIOR FUSELAGE, ZONE 100, LIGHTNING STRIKE AT F.S. 541 BETWEEN S39R AND S39L, FUSELAGE SKIN DOUBLER REPAIR PERFORMED IAW SRM 53-00-01-2R REPAIR 10. MAJOR REPAIR.
THE MAIN DECK CARGO CENTERLINE FLOORBOARD AT APPROXIMATELY STA 720, LBL4, REQUIRES REPAIR. FABRICATED NEW FLOORBOARD PANEL #231RFF AT STA 686 TO STA 730 & LBL 11 TO RBL 11 IN REF. TO FEDEX DWG # SRZ-25-005. SEE JPF FOR OTHER WORK ACCOMPLISHED. THIS IS A MAJOR.
ON DEPARTURE LOUD BANG FOLLOWED BY ENGINE FIRE LIGHT AND WARNING BELL. HAD A FIRE LIGHT IN LEFT FUEL CONTROL SWITCH AS WELL AS LEFT ENGINE FIRE SWITCH. ACCOMPLISHED QRC AND QRH FOR ENGINE FIRE OR SEVERE DAMAGE OR SEPARATION. BOTH BOTTLES OF FIRE SUPPRESSION WERE USED. LANDING WEIGHT 345,000. EMERGENCY DECLARED. TFOA CATEGORY: 2 INFO 19OCT23 00:27 MC1 R ENGINE APPROVED FOR REMOVAL PER SERVICE ENGINEERING. REMOVED #1 ENG S/N 707605 REF FEDEX WIC: 7100000-01-03 AND COMPLETED LH ENG INSTALL IAW B767 WIC 71-00000-01-04, OPS AND LEAK CHECKS GOOD.
NUMBER 2 R/H TRANSLATING COWL FAIRING ABOVE UPPER BLOCKER DOOR HAS SECTION MISSING. 0000452710 : ROSNER, DANIEL D - 07-OCT-2023 01:29 REPAIRED T/R O/B STRUCTURE SLEEVE. COMPLIED WITH E.A. H-7833-T0376515 P1.
DURING CRUISE, FL320, PILOTS L1 WINDOW OUTER FRAME CRACKED. MUTIPLE BROWN MARKS ALONG TOP WITH DELAMINATION. COMPLIED WITH QRH, TURNED OFF L1 WINDOW HEAT. INSPECTED WINDOW AND FOUND GLASS PANELS TO BE OK. THE INNER VINYL PANEL IS SEPARATED. 1 "CRACK" STARTS IN CENTER OF WINDOW AT THE TOP AND FORMS A "L" WITH 5" LEGS. THE OTHER "CRACK" STARTS 9" FROM UPPER INBD CORNER ON TOP OF WINDOW AND ENDS 2" BELOW UPPER INBD CORNER. R & R PILOTS L1 WINDSHIELD IAW AMM 56-11-011-4 WINDOW HEAT. OPS CHECK GOOD.
ON INBOUND WALK AROUND, FOUND ESCAPE SLIDE PRESSURE GAUGE READING BELOW LIMITS. R & R ESCAPE SLIDE IAW 25-60-015-2. ACFT OK FOR CONT SERVICE.
CAPT AIRSPEED INDICATOR FAILED ON TAKE OFF. PULLED AND RESET CIRCUIT BREAKER, INDICATOR NORMAL. PERFORMED TEST ON DADC-1 AIR SPEED INDICATOR FAILS TEST. R & R CAPT'S AIRSPEED INDICATOR IAW MM 34-12-021-4. OPS CHECKED IAW MM 34-12-000-5-2, 8A. OPS CHECKED NORMAL.
FWD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK REF AMM 33-50-051-2.
FORWARD ENTRY DOOR ESCAPE SLIDE LIGHT INOPERATIVE. R & R ESCAPE SLIDE LIGHT BATTERY PACK. OPS CHECKED NORMAL IAW MM 33-50-051-2.
ON CLIMBOUT THRU 20K NOTICED OCCASIONAL VIBRATION IN THE CONTROL COLUMN SPOILERS WERE SLIGHTLY DEPLOYED. NUMEROUS RESETS WITH THE SPOILER HANDLE. SLIGHTLY DEPLOYING SPOILERS DID NOT HELP. ON BLOCK IN DISCOVERED LT INBD FLAP OUTER CABLE BROKEN, ALONG WITH AFT FLAP PANEL DAMAGED BY AFT FLAP NOT EXTENDING ALL THE WAY ON THE OTBD SIDE. INBOARD T/E FLAP EXTENDED NORMALLY. R & R LT INBD FLAP OTBD FLAP ACTUATOR CABLES IAW AMM 27-51-005-4, ACFT OK FOR SERVICE. ASSOCIATED INSP PANELS, FLAP TRACK FAIRING AND SKIN RESECURED IAW SMP. ACFT OK FOR SERVICE.
C2 DOOR EXTERIOR SKIN AFT LOWER EDGE HAS FASTENERS WITH IMPROPER SPACING. REMOVED EXISTING REPAIR ANGLE IAW SRM 51-30-2. FABRICATED REPAIR ANGLE, FILLER, DOUBLER AND TRIPLER. INSTALLED REPAIR PARTS IAW EA 7-5230-136769.
MCD INNER SURROUND SKIN GOUGED STA 620 STR 4L. REMOVED DAMAGED UPPER INNER SKIN SECTION, FABRICATED & INSTALLED NEW INNER SKIN IAW SRM 51-30-2, SRM 51-10-2 & SRM 53-10-2 FIG 3A.
AFT AIRSTAIRS LT LOWER TORQUE BOX UPPER WEB IS PUNCTURED AND CRACKED AT BS 1225, (BELOW BAZOOKA VALVE STAND-OFF) CUTOUT DAMAGE ON LT LWR TORQUE BOX UPPER WEB IAW SRM REV 103, 51-40-2 FIG 1 AND 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 53-10-2 FIG 6 AND 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-2 FIG 1.
CORROSION FOUND ON INNER SKIN TRIPLER STA. 1164 STR 21L REMOVED DAMAGED INNER SKIN TRIPLER, FABRICATED & INSTALLED NEW TRIPLER AT BS 1164 IAW SRM 51-10-2, SRM 51-30-2 & DWG 65-25607.
C2 DOOR CUTOUT LOWER SECTION, INNER CHORD HAS DOUBLE DRILLED HOLES AND HOLES WITH INSUFFICIENT SPACING AT RBL 21 BETWEEN BS 980- BS 990. REMOVED C2 DOOR CUTOUT FITTING AND TRANSITION FITTING FOR ACCESS AND REMOVED TEE FROM STA 950D TO 1010 IAW SRM 51-30-2. FABRICATED, LOCATED AND DRILLED NEW TEE IAW DWG 65-56129. TREATED AND PRIMED NEW TEE IAW SRM 51-10-2. INSTALLED NEW TEE IAW SRM 51-30-2.
CORROSION FWD SIDE STA 1166 FRAME STR 21L. REMOVED DAMAGED FRAME SECTION, FABRICATED NEW FRAME SECTION & 2 EA. SPLICES, INSTALLED NEW FRAME IAW SRM 51-30-2, SRM 53-10-2 FIG 5, SRM 51-20-1, SRM 51-10-2 & SRM 51-40-3 FIG 1 AND DWG 65-16549.
LT SIDE OF FUSELAGE HAS A DENT AT BS 1260 BETWEEN STRINGER 21L AND 22L. CUTOUT DAMAGE AREA ON LT SIDE OF FUSELAGE BS 1260 BETWEEN STR 21L AND 22L IAW SRM 53-30-3. FABRICATED DOUBLER FROM 2024T3 .063 IAW SRM 53-30-3. INSTALLED DOUBLER IAW SRM 53-30-3, FIG 1.
INNER SURROUND SKIN GOUGED STA 620, STR 16L. REMOVED MCD INNER SURROUND SKIN LOWER SECTION, FABRICATED & INSTALLED NEW INNER LOWER SKIN IAW SRM 51-30-2, SRM 51-10-2 & DWG 53FX1535 & SRM 53-10-2 FIG 3A.
CORROSION ON STRINGER 27R AT BS 720F. CUTOUT DAMAGED STRINGER SECTION IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION AND SPLICE REPAIR IAW SRM 53-10-3 FIG 1. TREATED AND PRIMED PARTS IAW SRM 51-10-2. INSTALLED REPAIR PARTS IAW SRM 53-10-3 FIG 1.
LEFT I/B FLAP, AFT FLAP I/B TRACK CUTOUT CRACKED. REMOVED MID FLAP LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD IAW SRM 57-50-2 FIG 5 AND 51-30-5. INSTALLED I/B LT MID FLAP CHORD IAW SRM 51-30-2, REV 103
RT WW BS 870, BULKHEAD IS CRACKED BELOW LOAD CONTROL VALVE, (NDT VERIFIED). CUT OUT DAMAGE ON BULKHEAD BELOW LOAD CONTROL VALVE IAW SRM REV 103, 51-10-1. FABRICATED REPAIR DOUBLERS IAW SRM 53-10-9 FIG 5. INSTALLED DOUBLERS IAW SRM 53-10-9 FIG 5.
CORROSION ON SHEAR TIE AT BS 700 (AFT SIDE) BETWEEN STRINGER 28L AND 27L.
FWD CARGO COMPT LOWER STUB FRAME EXTENSION BETWEEN STR 21L-22L AT BS 600 IS CRACKED AT THE LOWER END, IN THE UPPER RADIUS. REMOVED LOWER STUB FRAME AT BS 600, STRINGER 21L-22L IAW B727 SRM 51-30-2. FABRICATED STUB FRAME IAW DRAWING 53FX1350 REV A. INSTALLED STUB FRAME IAW DRAWING 53FX1350 REV A, AND SRM, REV 103, 51-30-2.
FWD CARGO COMPT. LOWER STUB FRAME EXTENSION BTWN STR 21L-22L AT BS 560 IS CRACKED AT THE LOWER END, IN THE RADIUS. (NDT VERIFIED) REMOVED LOWER STUB FRAME EXTENSION IAW SRM 51-30-2, FABRICATED NEW STUB FRAME IAW DWG 53FX1350, HEAT TREATED STUB FRAME TO -T6 CONDITION IAW FAS ER 2-37153-801 REV A. LOCATED AND DRILLED IAW SRM 51-30-5, TREATED AND PRIMED IAW SRM 51-10-2. INSTALLED NEW FRAME EXTENSION IAW SRM 51-30-2 REV 103.
UPPER RUDDER RT SIDE HAS SMALL AREA OF CORROSION ON EXTERIOR SKIN AT TOP OF RUDDER. REMOVED CORROSION ON RH SIDE OF UPPER RUDDER IAW SRM REV 103, 51-10- 6. FABRICATED DOUBLER IAW SRM 55-20-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-40-20 AND 55-20-3 FIG 1 AND EA 7-5540-136771.
MCD INNER SURROUND SKIN GOUGED STA 620 STR 10L. REMOVED DAMAGED MCD INNER SKIN (UPPER AFT) SPLICE, FABRICATED NEW, AND INSTALLED IAW SRM 51-30-2 & SRM 53-10-2 FIG 3A.
AFT AIRSTAIR AREA RT TORQUE BOX UPPER LIGHTENING HOLE AT BS 1320 HAS A SMALL CRACK AT EDGE. CUT OUT DAMAGED AREA IAW B727 SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2 REV 103.
BS 1183 PRESSURE BULKHEAD - LBL 17.8 VERT BEAM HAS SEVERAL FASTENERS WITH INSUFFICIENT SPACING. TRIMMED OFF AFT FLANGE AND LOWER END OF 65-16350-299 BEAM, REMOVED EXISTING 65- 16350-284 STRAP. TRIMMED OUT BULKHEAD WEB (3 PLACES) MAINTAINING 0.5" TRIM RADIUS. MAINTAINED 2D ED AT ALL EXISTING FASTENER LOCATIONS. PERFORMED HFEC INSP OF TRIMMED EDGES TO ENSURE NO CRACK EXISTS. FABRICATED REPAIR DOUBLER FOR BULKHEAD WEB. MODIFIED STRAP INSTALLATION AT WL 173 PER 65C33041 AND SB 727-53- 0175. FABRICATED TWO SPLICE REPAIR DOUBLERS FOR THE LOWER END OF THE STIFFENER 65-16350-299. LOCATED ALL REPAIR / MODIFICATION PARTS IN PLACE AND DRILLED OUT EXISITING AND ADDITIONAL FASTENERS. INSTALLED ALL REPAIR PARTS USING THIN COAT OF BMS5-95. ALL ACCOMPLISHED REPAIRS AT BS 1183 PRESSURE BULKHEAD IAW EA 7-5310-123600.
STRINGER 28R IS CORRODED AT BS 990. REMOVED CORROSION, MATERIAL LOSS FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1 FIG 1 AND STRINGER DRAWING 65-58387, TREATED AND PRIMED IAW SRM 51-10-2
SHEAR TIE IS CORRODED ON LWR FWD FLANGE AT BS970 BTWN STR 29L - 28L.
FRAME BS 1090 HAS IMPROPER REPAIR BTWN STR 27L - 28L. REMOVED REPAIR FROM BS 1090 FRAME BETWEEN STR 27L- 28L IAW SRM REV 103, 51-30-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-3, FIG 1 AND 53-10-2, FIG 5 INSTALLED DOUBLER IAW SRM 51-40-3, FIG. 1.
C-1 DOOR CUTOUT, FWD FRAME BS 560, WEB AND OUTER ANGLE HAVE DRILL DAMAGE AT STR 22R, IN TWO PLACES. REMOVED DAMAGED FRAME WEB, FABRICATED & INSTALLED NEW WEB IAW DWG 65-56100, CUTOUT BS 560 CHORD, FABRICATED REPAIR PARTS & INSTALLED REPAIR IAW EA 7-5310-151200.
STRINGER 27L IS CORRODED WITH EXFOLIATION BETWEEN BS 970-990. REMOVED SECTION OF STRINGER 27L BETWEEN BS 970 AND 990 IAW SRM 53-10-3 FIG 1. FABRICATED FILLER AND STRINGER SECTION IAW SRM 53-10-3 FIG 1. INSTALLED FILLER AND REPAIR SECTION IAW SRM 53-10-3 FIG 1
AFT AIRSTAIRS, RT LWR TORQUE BOX INBD WEB IS CRACKED AT LIGHTING HOLE AT BS 1223, 7 INCHES. CUT OUT DAMAGED AREA IAW SRM REV 103 51-40-2. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.
AFT AIRSTAIRS, RT LOWER TORQUE BOX INBD WEB HAS A CRACK AT EDGE OF UPPER ROW RIVET. CUT OUT DAMAGED AREA IAW SRM REV 103 51-10-1. FABRICATED FILLER & DOUBLER IAW SRM 53-10-2 & 51-40-2 FIG 1. INSTALLED FILLER & DOUBLER IAW SRM 51-30-2.
AFT AIRSTAIR LT LOWER TORQUE BOX UPPER WEB HAS PUNCTURE HOLE AT STAND-OFF BRACKET. CUT OUT DAMAGE IAW SRM REV 103 51-10-1. FABRICATED REPAIR DOUBLER IAW SRM 51-40-2 FIG1 REV 103. INSTALLED DOUBLER IAW SRM 51-30-2.
AT FL 350 LOWER AFT BODY OVERHEAT LIGHT ILLUMINATED. COMPLIED WITH QRH EMERGENCY PROCEDURE WHICH REQUIRES TURNING OFF RT PACK, WITH ONLY THE LT PACK ON ACFT WOULD NOT MAINTAIN CABIN ALTITUDE. WE HAD TO DECEND TO 11,000 FT TO GET CABIN ALT TO 9,500 FT. R & R RT AFT BODY OVERHEAT SENSING ELEMENT IAW AMM REF 26-14-001-2. RAN ALL 3 ENGINES IAW JRH. OPS CHECK WAS NORMAL. PERFORMED EXCESSIVE CABIN PRESSURE LEAKAGE CONDITION- CONDITIONAL INSP IAW AMM, REF NR 05-51-101-2 OPS TEST WAS FOUND TO BE WITHIN LIMITS.
SKIN DAMAGE FROM STA 560 TO 580 STRINGER'S 27L TO 28R REPAIRED SKIN DAMAGE FROM STA 560 TO 580 STRINGERS 27L TO 28R IAW EA NR 7-5330-126895, FUSELAGE SKIN DENTS BETWEEN BS 560 AND 580 STR 27L AND 28R REPAIR.
FLIGHT TEST OUTBOARD FLAP GAUGE INDICATED BETWEEN 20 DEGREES AND 25 DEGREES AT FLAPS 25 DEGREES AND BETWEEN 25 INCH AND 30 INCH AT FLAPS 30 INCH ALL OTHER POSITIONS OK (REPEAT) PERFORMED ADJUSTMENT AND TEST ON OTBD T/E FLAP POSITION TRANSMITTER REF MM 27-52-013-5. OPS CK GOOD POINTERS IN TOLERANCE THIS IS CLASSIFIED AS A MINOR REPAIR CHECKED T/E FLAP DRIVE SYSTEM FOUND PLAY IN FLAP CONTROL LEVER DRUM FLAP CONTROL LEVER DRUM. REMOVED REPAIRED AND REINSTALLED ON EA NR 7-2750-123828 CHECKED ADJUSTED AND TESTED T/E FLAP DRIVE SYSTEM REF MM 27-51-000-5 PAGES 2 THRU 5 AND 9 THRU 11 T/E FLAP DRIVE SYSTEM. OPS CHECKED GOOD.
ANGLE FOR FLOOR JUST FWD OF FLIGHT DECK DOOR CUT OUT IS CRACKED REMOVED FLOOR SUPPORT AND ATTACH BRACKET, FABRICATED DRILLED, TRIMMED, TREATED AND PRIMED NEW ATTACH ANGLE. INSTALLED FLOOR SUPPORT AND NEW ANGLE. REFERENCE BOEING DWG NR 65-17593/ITEM NR -239 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
LWR EXTERIOR FUSELAGE BS 740, LBL6 TO LBL 10, WL 148.5 TO WL 150 JUST AFT OF GROUND A/C HOOK UP DUCT CORRODED REMOVED PANEL, A/C DUCT AND BODY FAIRING, AND HYD LINES FOR ACCESS REF SRM 51-30-02. REMOVED AND FABRICATED L ANGLE AND INSTALLED NEW L ANGLE REF 51-30-02 PGS 1-13. RE INSTALLED HYD LINES, A/C GROUND DUCT PANELS. REMOVED FOR ACCESS REF MM 21-20-004-4, 20-10-005-4, SRM 51-30-1, HYD LEAK CHECK GOOD, PNEUMATIC LEAK. OPS CHECK ACP ON W/C 7-5100-7-4310 70C055-00, THIS IS CLASSIFIED AS A MAJOR REPAIR.
RADAR R/T SHELF TRAY CRACKED AT AFT RT AND LT FOOT REMOVED AND REPLACED RT SHELF REF SRM 51-30-02.
EXTERIOR LWR FUSELAGE INSIDE DELTA BEAM BS 740 LBL5 TO RBL 5 WL 148.5 LOWER ANGLE UPPER SURFACE CORRODED. REMOVED AND REPLACED T-ANGLE REF SRM 51-30-2 ORIGINAL MATERIAL THICKNESS .125. REMOVED .025 MATERIAL REMAINING .100 OUT OF LIMITS REF SRM 53-10-1 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
LT WING L/E RIB LWR CHORD HAS 2 CRACKS AT 5 INCH AND 18 INCH FROM SPAR, FSS 122. REMOVED PNL 6301 TO FOM. FABRICATED ANGLE REF DWG 64-8342-19 DRILLED-UP, TREATED, PRIMED, AND INSTALLED ANGLE REF SRM 51-30-5, MM 51-20-021, MM 51-20-051, AND SRM 51-30-2. INSTALLED PANEL 6301 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
WHILE ACCOMPLISHING "OK TO WORK" STEP ON SNRM (N00791)) FOUND WING L/E SKIN CRACKED (LT WING) AT FSS 122, LWR SURFACE OF SKIN. REMOVED AND REINSTALLED ANTI-ICE DUCT (LT L/E WING ROOT) REF MM 36-00-001-2, LEAK CHECK GOOD. REPAIRED CRACK REF SRM 57-30-4 FIG 8. THIS IS CLASSIFIED AS A MINOR REPAIR TREATED AND PRIMED REF SRM 51-10-2.
RT MLG W/W CUTOUT SEAL BEAM (STR 19R), AREAS OF CORROSION ON TOP SIDE OF BEAM FROM FS 906 TO FS 930, RBL 74, WL 105 REMOVED CORROSION FROM BRACKET, STA 920 ORIG T .094, REMAINING T .071, .023 MATERIAL LOSS OUT OF LIMITS. REPLACED BRACKET STA 920. REMOVED CORROSION FROM BEAM, ORIG T .080' REMAINING T .076. .004 MATERIAL REMOVED WITHIN ALLOWABLE DAMAGE. REF SRM 51-30-2 PG 1-7, SRM 53-10-1 PG 2A, AMM 51-20-021-7 PG 1-3, AMM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.
FWD CARGO COMPARTMENT, PFM BOX, PUNCTURE JUST BELOW PFM DOOR REPAIRED PUNCTURE IN PFM BOX REF SRM 51-40-20 PAR'S 7, 14, 15, 19, 20, AND FIG'S 8, 211, SRM 51-20-4 AND AMM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
RADAR R/T SHELF, RT SIDE HAT CANNEL ON UPPER SIDE OF SHELF IS CRACKED. REPLACED RT SIDE HAT CHANNEL ON RADAR R/T SHELF IN ACCORDANCE WITH BOEING DRAWING 65C16129 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR
LT MLG WHEEL WELL APU AIR INLET MOUNT FLANGES CORRODED REMOVED CORROSION REF SRM 51-10-1 ORIGINAL THICKNESS .150', REMOVED .018', REMAINING THICKNESS, .132' OUT OF LIMITS REF SRM 53-10-1 FIG 1. REPLACED 323 STIFFENER REF DWG 65-18636, AND SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.
AFT CARGO PIT STATION 1030 FRAME SPLICE AT APPROX STRINGER 24L IS DAMAGED. REPLACED FRAME SPLICE REF SRM 51-30-02 AND DRAWING 69-47200. THIS IS CLASSIFIED AS A MAJOR REPAIR
AFT PIT S27L LONGERON/FITTING HAS CORROSION AT BS 1130 REMOVED FASTENERS, REMOVED CORROSION, NDT (HFEC) BLENDOUT AREA AND FASTENER HOLES. ALODINED AND CIC, D AREA. WITH NO LIMITS REF EA 7-5310-123810, THIS IS CLASSIFIED AS A MINOR REPAIR.
AFT CARGO PIT STATION 1050 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED DAMAGE ON STA 1050 AT STR 26R. REF SRM 51-40-05 PG1 FABRICATED AND INSTALLED DOUBLER FOR FRAME. REF SRM 51-20-1 PG 1 SRM 51-30-02 PG 1-12 FABRICATED AND INSTALLED NEW END ATTACH ANGLE FOR INTERCOSTAL FWD OF 1050 AT STR 26L. REF. SRM 51-40-02 PG 1-6 SRM 51-30-02 PG 1-6. THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT CARGO PIT STATION 1010 FUSELAGE FRAME DAMAGED AT STRINGER 26L. REPAIRED FRAME REF SRM 51-40-03 FIG1 AND FABRICATED CHANNEL ANGLE REF DWG 65-84827-8 SRM 51-30-02 PG 1-5
AFT CARGO PIT STATION 1030 FUSELAGE FRAME DAMAGED AT STR 26L. REMOVED FRAME DAMAGE STA 1030 STR 26L REF SRM 51-40-3 FIG 1 PGS 1-6. FORMED DOUBLER REF SRM 51-20-1 PG 1 HEAT TREAT DOUBLER TRACKING 2008-11-129. REMOVED INTERCOSTAL STA 1030, INSTALALED INTERCOSTAL STA 1030 STR 24-26L REF SRM 51-30-2 PGS 1-17. FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. TREATED PRIMED REPAIR DOUBLER REF SRM 51-10-2 MM 51-30-151-7. INSTALLED REPAIR DOUBLER REF SRM 51-40-3 FIG 1.
MLG WW KEEL BEAM INTERIOR, UPPER BLEED DUCT RT SUPPORT BRACKET IS CRACKED BS 950. REPLACED UPPER BLEED DUCT RT SUPPORT BRACKET BS 950 MLG WW KEEL BEAM INTERIOR IN ACCORDANCE WITH BOEING DRAWING 69-48851 AND SRM 51-20-01 AND 51-30-02. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR.
LOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL- 0" REF DUPLICATE SDR #08-4824. FAA PLEASE DELETE THIS SDR- ADMINISTRATOR
FUSELAGE UPPER LOBE INTERIOR STRUCTURE CRACKED ON GILL LINER SUPPORT AT STA 1180, RBL 68, STRINGER R 11. REPLACED SUPPORT STRUCTURE REF SRM 51-40-03 PG 1-5. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE STRUCTURE, SEAT TRACK HAS LONG CHAFE AT STA 520, RBL 64 BLENDED CHAFED AREA. MAPPED OUT AND SENT TO EG FOR BLEND ALLOWABLE LIMITS. BLEND IS WITHIN LIMITS. REF EA 7-5310-118317, ALODINED AND PRIMED REF SRM 51-10-02. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON GILL LINER SUPPORT AT STA 1180, RBL68, AT STRINGER R9. REMOVED CORROSION AND INSTALLED REPAR DOUBLER AND FILLER REF SRM 1-40-23 FIG 1.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT CORROSION AT STA 600 - 620, RBL 47 UPPER AND LOWER SURFACE REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. FABRICATED AND NEW STRAP, TREATED AND PRIMED AND INSTALLED. CLASSIFIED AS A MINOR REPAIR.
MAIN CARGO BAY, GILL LINER MOUNT FRAME CRACKED AT AFT BULKHEAD TOP RT CORNER, FS 1176, 27, WL 292. FABRICATED AND INSTALLED NEW ANGLE REF DRW 25FX1253, SRM 51-30-02 PG 1-12, SRM 51-10-2 PG 7, MM 51-20-151-7 PG 1, THIS IS CLASSIFIED AS A MINOR REPAIR.
EDGE SUPPORT PANEL, BS 1030 TO BS 1166, LBL 19 TO LBL28, UPPER AND LOWER SURFACES CORRODED EDGE SUPPORT FOUND TO BE OUT OF LIMITS REF SRM 53-10-1 PGS 30-31. FABRICATED NEW EDGE SUPPORT REF 65-57570 65-57568. TREATED AND PRIMED NEW EDGE SUPPORT REF SRM 51-10-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
FWD PIT DOOR CUTOUT FWD FRAME CLOSER WEB LOWER CORNER CRACKED, BS 560 RBL 26, WL 158. REMOVED DAMAGED WEB. FABRICATE NEW WEB. TREATED, PRIMED AND INSTALLED WEB REF: SRM 51-30-02 PG 1-12, SRM 51-1-2, PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION AT STA 600 RBL 51 "I" FRAME BOTTOM FLANGE. REPAIRED FRAME IAW EA 7-5310-123811 SEE JPF FOR PARTIAL WORK ACCOMPLISHED, REPAIR CLASSIFIED AS MAJOR.
FWD PIT DOOR CUTOUT FWD FRAME CLOSURE WEB FWD LOWER ANGLE STIFFENER CRACKED AT 4 LOWER INTERCOSTAL CUTOUTS BS 555. REMOVED CRACKED STIFFENER, FABRICATED NEW STIFFENER, BACK DRILLED TRIMMED TO FIT. ALSO, FABRICATED NEW FRAME CLIP FOR NEW STIFFENER, CLASSIFIED AS A MINOR REPAIR. ALSO, FABRICATED DOUBLER FOR NEW END OF STIFFENER FOR ALIGNMENT OF HOLES, REF DWG 65-67231, DWG 69-4745-3, AND SRM 51-40-3P 2-6.
RADAR R/T SHELF CENTER LT SUPPORT BRACKET IS CRACKED REMOVED DAMAGED ANGLE. FABRICATED NEW ANGLE PER REF SRM 51-30-02, AND DRW NR 66-14848. INSTALLED NEW ANGLE REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.
PANEL RACK, AFT PIT FLOOR PANEL SPLICE AT BS 1035 BOTTOM SURFACE CORRODED BLENDED CORROSION. ORIGINAL MATERIAL .125 MATERIAL LOSS OF .030 REMAINING .095, FOUND OUT OF LIMITS REF SRM 53-10-1 PG 30-3. FABRICATED NEW SPLICE PLATE P/N BAC1511-3795 2024-T3. TREATED AND PRIMED REF BOEING DWG 65-67245, SRM 51-10-2 AND MM 51-20-151-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
PASSENGER CABIN GILL LINER "Z" CHANNEL STA 1148 STR 14L CHAFED INTO FRAME SPLICE BLENDED CHAFED AREA FRAME SPLICE STA 1148 STR 14L REF SRM 53-10-1 ORIG "T" .112 LOSS .040 OUT OF LIMITS REF SRM 53-10-1 P1-2. REPLACED FRAME SPLICE REF SRM 51-30-2, P2 THIS IS CLASSIFIED AS A MAJOR REPAIR.
LOWER FWD CARGO PIT, CORROSION ON UNDERSIDE AT NUTPLATES OF FLOOR SUPPORT STRINGER STA 700 15 INCH, RBL 2.5.
LOWER FWD CARGO PIT BILGE, CORROSION SPOT ON FUSE SKIN AT AFT SIDE OF STA 700, BL 0". REMOVED DAMAGE FABRICATED REPAIR DOUBLER ANDINSTALLED REPAIR PER REF SRM'S 51-10-6,51-10-2, 51-30-02 AND 53-30-3 FIG1 . THIS IS CLASSIFIED AS A MAJOR REPAIR. CATEGORY "B" REPAIR
FUSELAGE UPPER LOBE INTERIOR STRUCTURE FRAME SUPPORT BETWEEN STA 500 AND STA 520 RBL 45 CORRODED. REMOVED OUTBOARD BLOW OUT PANEL FRAME SEGMENT TO ACCESS CORROSION UNDER THE NUT PLATES, ALSO REMOVED ALL NUT PLATES ON FRAME SUPPORT STRAP FROM STA 520 TO STA 552, REF SRM 51-30-2, P1-27. REMOVED CORROSION FROM UNDER ALL NUT PLATES, REF SRM 51-10-1,P1-16. FOUND CORRODED OUT OF LIMITS AT STA 520, USED POINT MIKE NR IN17-0112 CAL DUE DATE 12-11-08. REF: SRM 53-10-2, P.42G AND P.40E. FABRICATED REPAIR PART REF: SRM 51-40-2,P.5. TREATED, PRIMED REPAIR. REF: SRM 51-10-2. INSTALLED REPAIR. REF SRM 51-30-2, P.1-27, STA 520 FLOORBEAM REPAIR TRANSFERED TO NR N00701. THIS IS CLASSIFIED AS A MINOR REPAIR.
RT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
RT WING L/E RIB UPPER CHORD HAS SEVERAL CRACKS ALONG EXISTING REPAIRS AT 9 INCHES-20 INCHES FROM SPAR, FSS 122. REMOVED REPAIR, FABRICATED REPAIR DOUBLER REF SRM 51-40-3 FIG 1. INSTALLED RT WING LF RIB CHORD REPAIR REF SRM 51-40-3 FIG 1. THIS IS CLASSIFIED AS A MINOR REPAIR.
LOWER FWD CARGO PIT, CORROSION ON FRAME SHEAR TIE, AFT SIDE OF STA 700, LBL 5 INCH. REPLACED SHEAR TIE IAW DRAWING 69-14871 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
DITCHING PAN AFT ANGLE AT STA 1183 RBL 53 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED AND SEALED NEW ANGLE CLASSIFIED AS A MINOR REPAIR, REF DWG 65-29567, SRM 51-40-02.
UPPER LOBE INTERIOR STATION 776 LBL 2 INCH FLOORBOARD ATTACH ANGLE CRACKED. REPAIRED ATTACH ANGLE REF SRM 51-40-03 FIG 1 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR.
PASSENGER CABIN, BULKHEAD 1183 DITCH PAN, LBL 28 CRACKED REPLACED DITCHING PAN 1183 BLKHD LBL 28 REF BOEING DWG 65-29567 AND SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.
PASSENGER CABIN FLOOR WEB BS 1110 - 1130 LBL 69 FWD OUTBOARD FASTENER HAS CORROSION AROUND IT FABRICATED NEW FLOOR WEB IAW DWG 65-22735-35. INSTALLED NEW FLOOR WEB IAW SRM 51-30-02 PG 5. THIS IS CLASSIFIED AS A MINOR REPAIR.
LT LWR FUSE TO BODY FAIRING SUPPORT (STA 870) HAS A CRACKED CLIP. REMOVED AND REPLACED CRACKED ANGLE CLIP STA 870 LT WING TO BODY FAIRING SUPPORT CLIP ALL WORK ACCOMPLISHED REF DRW 66-47181-3 AND SRM 51-30-02 AND 51-10-3. THIS IS CLASSIFIED AS A MINOR REPAIR.
MAIN CARGO BAY-GILL LINER MOUNT FRAME ATTACH BRACKET CRACKED AT 1110 FRAME, FS 1110, RBL 44, WL 287. REMOVED DAMAGED CLIP REF SRM 51-30-2. FABRICATED NEW CLIP REF DWG 25FX1253, SRM 51-20-1. INSTALLED ANGLE CLIP REF SRM 51-30-2 PGS 1-17. IDENTIFIED ANGLE CLIP REF GMM 7-0-1001 PG 1-2, THIS IS CLASSIFIED AS A MINOR REPAIR
MAIN CARGO BAY-GILL LINER MOUNT FRAME ATTACH ANGLE CRACKED ON 1148 FRAME, FS 1148, BRL 54, WL 273 REMOVED DAMAGED CLIP REF SRM 51-30-2. FABRICATED NEW CLIP REF DWG 25FX1253 AND SRM 51-20-1. INSTALLED ANGLE CLIP REF SRM 51-30-2 PGS 1-17. IDENIFIED ANGLE CLIP REF GMM 7- 0-1001 PGS 1-2 THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE- CORROSION ON FRAME SUPPORT BETWEEN BS 620-640 RBL 48 REMOVED DAMAGED AREA, INSERTION REPAIR REQUIRED. REF SRM 51-30-02, P1-27. FABBED REPAIR PARTS FOR INSERTION REPAIR AND ALSO END PLATE SPLICE. REF SRM 51-40-3 AND SRM 53-10-8. TREATED & PRIMED REPAIR PARTS. REF: SRM 51-10-2. ASSEMBLED REPAIR PARTS. REF: SRM 51-30-2. INSTALLED ASSEMBLED PARTS. REF: SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
LEFT WING INBD T.E., CORROSION ON SEAL RETAINER OF LWR. SURFACE PANEL AT REAR SPAR CHORD, 16" O.B. OF WING ROOT AND BELOW T/T ANGLE GEARBOX REMOVED DAMAGED PARTS. SEAL RETAINER AND ZEE ANGLE RETAINERS. FABRICATED SEAL RETAINER. FABRICATED ZEE ANGLE RETAINER NDT. ALODINED AND PRIMED PARTS. CLEANED AND PROTECTED AREA. INSTALLED SEAL RETAINER AND ZEE ANGLE RETAINER IAW SRM 51-30-2 PG 1-10, SRM 51-10-2. DWG 65-21656 THIS IS CLASSIFIED AS A MINOR REPAIR GMM 6-2-100 PG 2-3
LEFT WING OTBD L/E NR 4 SLAT S/N BN605, 2 CRACKED INTERNAL BRACKET TABS ON AFT WEB BELOW EACH SIDE OF ACTUATOR BOLT HEAD AND NUT. REPLACED 2 CRACKED RIBS REF SRM 51-30-02 PG 1-5. THIS IS CLASSIFIED AS A MAJOR REPAIR.
LWR FUSELAGE DELTA BEAM LT LWR CHORD IS CRACKED ON LWR INBD FLANGE AT BS 740 TO 743 LBL 6 INCHES. REMOVED DAMAGE, NDT TRIMMED EDGES, MADE INSURANCE CUT, FABRICATED REPAIR ANGLE AND FILLER, FABRICATED ONE T-CLIP, FABRICATED INTERCOSTAL, ALODINED AND PRIMED AND INSTALLED ALL PARTS, REF FED EX EA 7- 5310-123817. THIS IS CLASSIFIED AS A MAJOR REPAIR.
PASSENGER CABIN FRAME STA 1090-LBL 68-1 1/2 INCH UP FROM FLOOR CORRODED. REMOVED FRAME CORROSION, FOUND OUT OF LIMITS. ORIGINAL "T" 0.063, LOSS .035, REMAINING .028. FABRICATE REPAIR PARTS, ANGLE AND FILLER AND SUPPORT ANGLE (CLIP), ALODINED AND PRIMED PARTS. REPAIR ANGLE, RADIUS FILLER AND SUPPORT ANGLE. INSTALLED REPAIR FRAME AND SUPPORT ANGLE (CLIP) REF SRM 51-30-2, 53-10-1, 53-10-2, 51-40-3 DWG 65-58636. THIS IS CLASSIFIED AS A MAJOR REPAIR GMM 6-2-100 PG 2-3.
LOWER FWD CARGO PIT, CORROSION AT NUT PLATE HOLE UPPER AND LOWER SURFACE OR FLOOR SUPPORT STA. 720C 3 INCHES, LBL 2.5. REMOVED CORROSION ORIG T= .064 RE= .009, LOSS OUT OF LIMITS REF SRM 51-10-1 PG 5. INSTALLED REPAIR STA 720C REF SRM 53-10-5 FIG 4. THIS IS CLASSIFIED AS A MINOR REPAIR.
LT MLG WHEEL WELL AFT BULKHEAD BS 950 LBL 30, REINFORCEMENT WEB HAS LIGHT CORROSION. REMOVED CORROSION, ORIGINAL MATERIAL THICKNESS .050 MATERIAL LOSS OF .020. REMAINING MATERIAL .030, FOUND OUT OF LIMITS REF SRM 53-10-1 PG 2. INSTALLED NEW WEB P/N 69-15443-1 REF SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR
LOWER FUSELAGE DELTA BEAM LT LOWER CHORD IS CRACKED ON LOWER INBD FLANGE AT BS 740 TO 743 LBL 6 INCHES.
LEFT WING OTBD LE, CRACK IN CLOSE OUT WEB AT TIP INBD EDGE, AT OTBD END OF NR 1 SLAT WEDGE WHEN EXTENDED REMOVED CLOSEOUT WEB. INSTALLED NEW WEB, IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
RT WING TE FLAP WELL LOWER FIXED PANEL CHANNEL IS CRACKED AT DIAGONAL STRUT ATTACHMENT WS 521 REMOVED CHANNEL REF SRM 51-30-02. FORMED NEW CHANNEL REF DWG 65-21658 ITEM 23. INSTALLED NEW CHANNEL REF SRM 51-30-02, THIS IS CLASSIFIED AS A MINOR REPAIR.
LT WING OTBD LE APPROX CLOSE OUT WEB UPPER ANGLE IS CRACKED REMOVED DAMAGED ANGLE. INSTALLED NEW ANGLE, IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
SEAT TRACK HAS CORROSION UNDER O/B FLANGE BS 690 LBL-2, UNDER SEAT TRACK SPLICE ANGLE. REPLACED DAMAGED SECTION OF SEAT TRACK REF SRM 53-10-5. THIS REPAIR IS CLASSIFIED AS A MINOR REPAIR
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, SEAT TRACK AT STA 600-620 LBL 24 CORROSION. REPLACED SEAT TRACK REF S.R.M. 51-10-2 AND 51-30-2 THIS IS CLASSIFIED AS A MINOR REPAIR.
UPPER LOBE INTERIOR STATION 760 TO 850 RBL 45 INCH, 24' FLOOR BOARD ATTACH ANGLE HAS WEAR IN SEVERAL AREAS. REMOVED NUT PLATE 8 SRM 51-30-02, BLENDED WEAR MARKS STA 760 - 850 RBL 24 REF SRM 51-10-1 ORIG "T'' .088, WORST "T" REMOVED .035 INCH. REMAINING "T' .053 INCH STA 808 RBL 24, OUT OF LIMITS. REPAIR REF EA 7-5310-118309, STA 760 - 850 RBL45 WEAR MARKS THROUGH PAINT, CLEANED, TREATED AND PRIMED REF MM 20 151 7. TREATED AND PRIMED STA 760 - 802/817 - 850 RBL 24 SOPM 20-43-05, SOPM 20-44-04, HFEC PER EA 7-5310-118309 STEP 3 PART. NO CRACKS DECTECTED, ROTO PEENED STA 808-RBL 24. TREATED AND PRIMED, FILLED BLEND WITH SEALANT APPLIED CORROSION INHIBITOR REF EA NR 7-5310-118309 PG 2 ITEM 3-7.
FWD PIT LEFT SIDE FRAME, BS 520 AT STR 24L , UPPER FLANGE HAS 2 EA.DENTS WITIN 3". INSTALLED FRAME REPAIR AFTER REMOVING DAMAGE FROM FRAME. (CLASSIFIED AS A MAJOR REPAIR) REF SRM 51-40-06 PG 1-6 2 EA. DENTS REMOVED BY CUTOUT. FABRICATED NEW FRAME REPAIR, ALODINE, PRIMED PART. INSTALLED REPAIR AS REQUIRED. NO OTHER DEFECTS NOTED THIS IS CLASSIFIED AS A MAJOR REPAIR
LT AFT EMERGENCY HATCH, SEAL RETAINER ATTACH FLANGE IS CRACKED IN SEVERAL PLACES. MATCH DRILLED NEW SEAL RETAINER REF SRM 51-30-5 P 1/5. REMOVAL AND INSTALLATION COMPLETED ON NON ROUTINE NR N11265 ITEM NR 3/4. THIS IS CLASSIFIED AS A MINOR REPAIR.
CORROSION ON BOTTOM AFT OF FLOORBEAM, FS 1034, LBL 13 TO LBL16, WL 208. REMOVED CORROSION ORIGINAL THICKNESS .100 .083 REMAINING OUT OF LIMITS FLOORBEAM REMOVED. NEW FLOOR SUPPORT LOCATED, DRILLED AND INSTALLED REF SRM 51-30-2 PG 13-16. THIS IS CLASSIFIED AS A MINOR REPAIR.
UPPER LOBE INTERIOR STATION 760 RIGHT, BELOW WINDOW AT DOOR CUTOUT, CILL LINER ATTACH BRACKET IS CRACKED. REMOVED CRACKED BRACKET VERIFIED MATERIAL FOR BRACKET AND FABRICATED NEW BRACKET. TREATED AND PRIMED INSTALLED NEW BRACKET IDENTIFIED P/N ON BRACKET IN REF TO GMM 7-0-1000 PG 2 SRM 51-30-2 PG 1-13 AND DWG BY 25FX1432. THIS IS CLASSIFIED AS A MINOR REPAIR.
RT WING LE, ANTI-ICE DUCT BOX WEB AT NR 4 KRUEGER FLAP POS, IS CRACKED AND HAS SEVERAL IMPROPERLY INSTALLED FASTENERS. REPLACED LOOSE AND WORN FASTENERS, FABRICATED AND INSTALLED DOUBLER FOR CRACK IN PANEL, REF SRM 51-30-02 PG 1-12 AND SRM 51-40-02
LOWER FWD CARGO PIT, STA 600 RBL 2 INCH WL 155 FLOOR SUPPORT STRINGER IS CORRODED. REPAIRED LOWER FWD CARGO PIT FLOOR SUPPORT STRINGER STA 600 RBL 2 WL 155 REF SRM 51-40-3 PGS 1-6. THIS IS CLASSIFIED AS A MAJOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION STA 310 LBL 3, ON FLOORBEAM. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, FABRICATED REPAIR ANGLE, HFEC BLEND OUT AREA AND TO ALL FASTENER HOLES IN FLOOR BEAM. INSTALLED REPAIR. REF EA 7-5310-123807 STEP 1 THRU 13. THIS IS CLASSIFIED AS A MAJOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, CORROSION ON FWD SHEAR DECK STA 360 RBL 30-37. FASTENERS REMOVED FROM FLOORBEAM STA 360 RBL 30-37 REF SRM 51-30-02. ACCOMPLISHED EA 7-5310-123806 FASTENERS INSTALLED IT FLOORBEAM REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR
UPPER LOBE FLOORBEAM 520, RBL 45 LOWER LEG CORRODED REMOVED CORROSION REF: SRM 51-10-1, P1-27. MATERIAL REMOVED IS BEYOND LIMITS: REF; P- F SRM 53-10-1, PAGE 6. FABRICATED REPAIR PARTS, REF: P/F SRM 53-10-8, PAGES 8-17. TREATED AND PRIMED REPAIR PARTS, REF:SRM 51-10-2. INSTALLED REPAIR PARTS, REF, SRM 51-30-2, P.1-27. THIS IS CLASSIFIED AS A MAJOR REPAIR.
UPPER LOBE INTERIOR STATION 804 LBL68" FLOORBEAM LOWER CHORD CORRODED. REMOVED CORROSION OVER 50 PERCENT MATERIAL LOSS OUT OF LIMITS REF SRM 53-10-1 FIG 1. REMOVED AND REPLACED BEAM LOWER CHORD REF SRM 51-30-2 P8. THIS IS CLASSIFIED AS A MAJOR REPAIR.
FWD PIT BS 620 FRAME CRACKED RBL 2 TO RBL 3 WL 155, BELOW FLOOR SUPPORT. REPAIRED IAW SRM 51-40-3. THIS IS CLASSIFIED AS A MAJOR REPAIR.
FWD PIT FRAME BS 580 RBL2 WL 155, UPPER FLANGE CRACKED UNDER FLOOR SUPPORT AS SEEN FROM LOWER SIDE. SDR OPENED IN ERROR DUPLICATE OF SDR 08-4613, FAA PLEASE DELETE THIS SDR.
FWD PIT FRAME BS 580 RBL2 WL 155, UPPER FLANGE CRACKED UNDER FLOOR SUPPORT AS SEEN FROM LOWER SIDE. INSTALLED REPAIR COMPLETED REF SRM 51-30-2. CUT OUT DAMAGED AREA. NDT'D TO VERIFY TERMINATION OF CRACK, NO DEFECTS NOTED REF SRM 51-40-2, NDT MANUAL. 51-00-00. REPAIRED FRAME PER SRM 51-40-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
LOWER FWD CARGO PIT, CORROSION ON UNDERSIDE AT NUT PLATES OF FLOOR SUPPORT STRINGER STA 700 15 INCH, RBL 8. CUT DAMAGE SECTION OUT. FABRICATED NEW SECTION AND SPLICE TARTS REF SRM 51-40-4. PRIMED ALL PARTS AND MATING SURFACES REF SRM 51-10-3. INSTALLED REPAIR PARTS REF SRM 51-30-2 AND 51-40-4. THIS IS CLASSIFIED AS A MINOR REPAIR.
LOWER FWD CARGO PIT, FLOOR SUPPORT STRINGER IS BENT WITH A CRACK ON SIDE STA 720C 10", LBL 8 INCH.
EDGE SUPPORT PANEL BS950 TO 95C LBL 19 TO LBL 28 UPPER AND LOWER SURFACE CORRODED. FABRICATED NEW Z-ANGLE AND STIFFENER, INSTALLED NUT PLATE AND SPLICE OLD STIFFENER W/NEW REPAIR PART & SPLICED BOTH HALVES OF Z-ANGLE REF.DWG 65-57568 & DWG 65-67245 ITEM 12 & SRM 51-40-04 PG 14-17 (CLASSIFIED AS A MINOR REPAIR)
MAIN DECK FLOOR SUPPORT INTERCOSTAL IS CORRODED BS 1067, LBL 12 WL 208. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1. REMOVED & REPLACED FLOOR SUPPORT IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE-LEFT FWD ENTRY DOOR THRESHOLD CORROSION ON "L" ANGLE AND ONE ELONGATED HOLE AND ONE FASTENER HOLE WITH "0" EDGE DISTANCE. REMOVED DAMAGED CHANNEL AND REPLACED WITH NEW 65-31787-5. REINSTALLED DOOR GUTTER ASSY. AND SEALED IAW SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR.
UPPER LOBE INTERIOR STATION 804 LBL 68 INCH FLOORBEAM LOWER CHORD CORRODED.
RT FWD EMERGENCY EXIT HATCH, SEAL RETAINER ATTACH FLANGE IS CRACKED IN SEVERAL PLACES. REPLACED RETAINERS IAW SRM 51-30-2 AND SRM 51-30-5. THIS IS CLASSIFIED AS A MINOR REAPAIR.
EMERGENCY ESCAPE HATCH LT FWD, SEAL RETAINER ATTACH FLANGE IS CRACKED AND WORN IN SEVERAL AREAS. REPLACED UPPER AND LOWER SEAL RETAINERS REF SRM 51-30-2 P. 3&4 AND SRM 51-30-5 P.5 THIS IS CLASSIFIED AS A MINOR REPAIR.
PNL RACK, MAIN DECK CREASE BEAM WEB UPPER SURFACE BS 1000-1006 LBL 68 HAS CORROSION. REMOVED DAMAGED PARTS PER REF SRM 51-30-02, FABRICATED NEW PARTS REF DWG 65-56148-15 AND -23. TREATED AND PRIMED PER REF SRM 51-10-3. INSTALLED NEW PARTS PER REF SRM 51-30-02. THIS IS CLASSIFIED AS A MINOR REPAIR
LEFT WING OTBD L/E, CRACKS IN INBD AND OTBD REINFORCEMENT ANGLES AT FWD FASTENERS LOCATIONS ABOVE NR 2 SLAT ACTUATOR LWR FAIRING. REMOVED INBD AND OTBD REINFORCEMENT ANGLES, MFG NEW ANGLES REF DWG 65-21672 PGS 1- 3 USING A63549 FOR ANGLE MATERIAL PRIMED AND INSTALLED ANGLES REF SRM 51-30-02 AND SRM 51-10-2. REINSTALLED SLAT ACTUATOR FAIRING NR 2 REF SRM 51-30-2 PG 1-7. THIS IS CLASSIFIED AS A MINOR REPAIR.
LOWER FWD CARGO PIT, CORROSION ON FRAME SHEAR TIE AT AFT SIDE OF STA 720B, STR 26-R. REMOVED & REINSTALLED ZEE ANGLE, STRINGER CLIP AND TIE DOWN FITTING REF SRM 51-30-2. REMOVED CORROSION REF SRM 53-10-1. FOUND TO BE OUT OF LIMITS. MEASURED REF NDT MAN PART 4.51-00-00 FIG 2. REPAIRED REF SRM 53-10-4 FIG 13. THIS IS CLASSIFIED AS A MAJOR REPAIR.
1148 FRAME DAMAGED FROM GILL LINER ATTACH FRAME, FS 1148, LBL 65, WL 254.
FWD PIT BS 560 STR 27R STRINGER CLIP CORRODED. REMOVED DAMAGED STRINGER CLIP, AND REPLACED IAW SRM 51-30-2. DWG 65-56100. THIS IS CLASSIFIED AS A MAJOR REPAIR REF GMM 6-2-100 PG 2-3.
PANEL RACK-PANEL 8805 CRACKED RIGHT WING OB AILERON REMOVED SEAL ANGLE, TRANSFERRED HOLES TO NEW ANGLE P/N 65-19287-15. INSTALLED ANGLE REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MINOR REPAIR.
PANEL RACK, EDGE PANEL STA 1030 TO STA 1166 RBL 19 TO 28 AFT PLATE OB EDGE BROKEN AND CORRODED UPPER SURFACE BLENDED CORROSION ORG "T" .040, MATERIAL LOSS OF .005 AT DEEPEST POINT WITHIN LIMITS. REF SRM 53*-10-1 FIG 7 TOOL NR AAR20278 CAL DUE 12-11-08. REPAIRED EDGE CRACK WITH WEB REPAIR REF SRM 51-40-2. REPAIR CLASSIFIED AS MINOR.
AFT PIT BILGE BODY FRAME STR CLIP IS CORRODED BS 950F, STR 27L WL 141. INSTALLED NEW STRINGER CLIP 65-12434-3 REF SRM 51-10-1 AND ARM 53-10-1. THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT LOWER CARGO COMPARTMENT STA 950F, 4 INCHES STR 27L, STRINGER CORRODED AT FASTENER. REMOVED DAMAGED SECTION OF STRINGER, INSTALLED STRINGER REPAIR SPLICE SRM 51-10-1 AND 53-10-03 AND 51-30-02. THIS IS CLASSIFIED AS A MAJOR REPAIR.
LEFT WING INBD L/E CAVITY, SUPPORT BRACKET CRACKED AT FWD FIXED L/E 3 INCH OTBD NR 1 FLAP INBD HINGE. REMOVED SUPPORT BRACKET ASSY REF: SRM 51-30-02. CRACKS FOUND .25 INCH AND 1 INCH LONG ON PARTS 65-17356-39 AND -87, OUT OF LIMITS. FABRICATED -39 AND -87 REF, DWG 65-17356, SRM 51-30-05 ID MATERIAL -39 BULKHEAD 2024T3 .032 ATAG 69787, -87 2024 .063 ATAG A33090 REF: DWG 65-17356, TREATED SOPM 20-43-03P3, PRIMED 20-44-04P3, INSTALLED ASSY REF SRM 51-30-02P1. THIS REPAIR IS CLASSIFIED AS MINOR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE CORROSION ON FWD SHEAR DECK STA 382 RBL 46-55. REPAIRED FLOORBEAM REF EA 7-5310-123808 AND DWG SR27-53-034 REV F REPAIR 5. THIS IS CLASSIFIED AS A MAJOR REPAIR. (ORIGINAL MATERIAL THICKNESS .125, MATERIAL LOSS .027, REMAINING .098 OUT OF LIMITS)
PFM BOX SHROUD SEVERED ON ONE END AND CRACKED AT OTHER END, PANEL RACK, DOT 3 REPAIRED PFM BOX SHROUD REF SRM 51-40-9 PAR 3 AND 7. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, FRAME 1166 SCRATCHED RBL 68 AT STR R11- R12 BLENDED DAMAGE REF SRM 53-10-1 PG 1-2A, OUT OF LIMITS, HEAT TREATED NEW REPAIR. REMOVED DAMAGE REF SRM 51-40-3 PG 1-6. TREATED AND PRIMED REPAIR REF SRM 51-20-13 AND 51-20-21. FABRICATED NEW STRINGER CLIP REF DWG 66-15883 ITEM 1, TREATED AND PRIMED CLIP SRM 51-20-13 AND 51-20-21. INSTALLED REPAIR AND STRINGER CLIP REF SRM 51-30-2 PG 2-14. THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT PIT BS 1130 FRAME UPPER CHORD HAS DOUBLE DRILLLED HOLE IB OF TIE DOWN FITTING AT S27L. REMOVED AND INSTALLED FLOOR SUPPORT BRACKET, TIE DOWN BRACKET, FLOOR SUPPORT REF 51-30-2. REPAIRED DAMAGED FRAME REF SRM 51-40-3 FIG 1. TREATED AND PRIMED REF SRM 51-10-2 THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT PIT BS 1130 FRAME UPPER CHORD HAS TRIPLE DRILLED HOLE INBD OF TIE DOWN FITTING AT S27R. CUTOUT DAMAGE, REMOVED FASTENERS FROM FRAME AT REPAIR AREA. FABRICATED REPAIR ANGLE & HEAT TREATED TO T6 CONDITION. TREATED, PRIMED, & INSTALLED FRAME REPAIR ANGLE. REF: SRM 51-40-3, FIG. 1 / SRM 51-30-2, PG. 8 / SRM 51-10-2, PG. 1-2 / SHOP REPAIR NON ROUTINE CARD NO. N00953. THIS IS CLASSIFIED AS A MAJR REPAIR
AFT PIT BS 1090 FRAME HAS DOUBLE DRILLED HOLE INBD OF TIEDOWN FITTING AT S27R. REPAIRED IAW SRM 51-40-3. FABRCATED BRACKET IAW DWG 69-44106 TREATED, PRIMED IAW SRM 51-10-2. THIS CLASSIFIED AS A MAJOR REPAIR.
R-1 DOOR CREASE BEAM WEB CRACKED AT FWD END OF CUT-OUT. REMOVED AND REPLACED RT CREASE BEAM WEB REF DWG 65-56153 AND SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR
FWD PIT (STA 740), STR 27L, END CLIP ON STRINGER CORRODED FABRICATED NEW STRINGER CLIP, TREATED AND PRIMED. REFERENCE BOEING DRAWING NR 69-45628/ITEM NR 2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT PIT BS 1130 SHEAR TIE HAS CORROSION ON LOWER FLANGE BETWEEN S27L AND 28L. FABRICATED SHEAR TIE. REMOVED AND REPLACED SHEAR TIE REF DWG 69-20813, SRM 51-30, OLD SHEAR TIE WAS BLENDED OUT OF LIMITS. ORIG "T" .050', .042 INCH REMAINING .008' MAT LOSS. THIS IS CLASSIFIED AS A MAJOR REPAIR.
AFT PIT BS 1130 S27L STRINGER CLIP SPLIT REMOVED, FABRICATED, TREATED, PRIMED AND INSTALLED STR CLIP REF SRM 51-30-02, 51-10-2 AND BOEING DWG 69-44104. THIS IS CLASSIFIED AS A MAJOR REPAIR.
MED FWD LWR CORNER INTERIOR SURFACE OF THE LOWER DOOR WEB IS CRACKED. REMOVED LOWER PORTION OF INNER SKIN FOR ACCESS REF SRM51-30-2 PG 32. REMOVED LWR FWD STOP FITTING REF SRM 51-30-2 PG 8 HAD WEB NDT'ED, AND NO CRACK WAS FOUND, TOOL NR IN22-0043 WAS USED CAL DUE 3/26/09. REINSTALLED INNER SKIN REF SRM 51-30-2 PG 4. REINSTALLED LWR FWD STOP FITTING REF SRM 51-30-2 PG 8. THIS IS CLASSIFIED AS A MINOR REPAIR.
AFT LOWER CARGO PIT STA 950E STR 29L ATTACH FITTING CORRODED ON LEFT SIDE. REMOVED ATTACH FITTING REF SRM 51-30-2 PG 32, MATCH DRILLED NEW ATTACH FITTING REF SRM 51-30-5, INSTALLED NEW ATTACH FITTING REF SRM 51-30-2 PG 2-12 THIS IS CLASSIFIED AS A MAJOR REPAIR.
FWD PIT BS 620 STR 27R STRINGER CLIP CORRODED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR IAW GMM 6-2-100.
CABIN BS 360 S4R FRAME INNER CHORD WORN. BLENDED AREA, FOUND OUT OF LIMITS IAW SRM 53-10-04. FABRICATED REPAIR PART IAW SRM 53-10-04, REMOVED DAMAGE AND INSTALLED FARICATED REPAIR PART IAW SRM 53-10-4. TREATED AND PRIMED. THIS IS CLASSIFIED AS A MAJOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN FWD SUPPORT ANGLE AT BS 1176 RBL 53-70 IS CRACKED. REMOVED DAMAGED ANGLE, FABRICATED HEAT TREATED NEW ANGLE. INSTALLED NEW ANGLE (CLASSIFIED AS A MINOR REPAIR) REF DWG 65-29548-11& 51-30-02.
PASSENGER CABIN, BULKHEAD 1183 DITCHING PAN, LBL 19 ATTACH BRACKET CRACKED. REPLACED ANGLE IAW SRM 51-30-02 & DWG 65-29-567. THIS IS CLASSIFIED AS A MINOR REPAIR.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PANEL CRACKED AT STA 1183 RBL 70. REMOVED DAMAGED DITCHING PAN, FABRICATED AND HEAT TREATED NEW DITCHING PAN, INSTALLED NEW DITCHING PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29548-53 & SRM 51-30-02
PASSENGER CABIN BULKHEAD 1183 DITCH PAN, LBL 28 CRACKED.
FUSELAGE UPPER LOBE INTERIOR STRUCTURE, DITCHING PAN CORRODED AT BS 1183 RBL 53. REMOVED PAN & FABRICATED NEW PAN HEAT TREATED, INSTALLED NEW PAN (CLASSIFIED AS A MINOR REPAIR ) REF DWG 65-29567 & SRM 51-40-02.
AFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODED
PNL RACK, FWD PIT SIDEWALL TO FLOOR RT NR 2 STRAP IS CORRODED, STRAP IS CRACKED, CORROSION FOUND TO BE OUT OF LIMITS REF 53-10-1 PG 30 NOTE A. FABRICATED, TREATED, PRIMED, AND IDENTIFIED NEW STRAP REF DWG 65-67205, SRM 51-10-2, AND FED EX MM1805 SEC 11-0-2700. THIS IS CLASSIFIED AS A MINOR REPAIR.
AFT LOWER CARGO PIT STA 1010 BETWEEN STR 28R AND 27R FRAME CORRODED. REPAIRED FRAME BY INSTALLING REPAIR ANGLE REF SRM 51-40-03. THIS IS CLASSIFIED AS A MAJOR REPAIR.
PNL RACK, FWD PIT SIDEWALL TO FLOOR STRAP NR 5 IS CRACKED REPLACED STRAP ORIGINAL THICKNESS .063 2024 T3 A24170 PO NR 1039696, TREATED AND PRIMED NEW STRAP REF DWG 65-67205 AND MM 51-20-151-7 PG 1-6. THIS IS CLASSIFIED AS A MINOR REPAIR.
CABIN BS 950B S7L STRINGER CLIP CRACKED. REMOVED AND REPLACED STRINGER CLIP IAW SRM 51-30-2 & 51-30-5. THIS REPAIR IS CLASSIFIED AS A MAJOR REPAIR.
UPPER INTER FUSELAGE BS 600 STR 9R STRINGER CLIP OTBD LOWER RADIUS CRACKED. REMOVED STRINGER CLIP REF. SRM 51-30-02 P1, LOCATED AND DRILLED FASTENERS HOLES REF SRM 51-30-05 P1 INSTALLED STRINGER CLIP 65-45313-14 A45966 REF SRM 51-30-02 P1, APPLIED CORROSION INHIBITOR REF SRM 51-10-02 P14. THIS IS CLASSIFIED AS A MINOR REPAIR.
CABIN BS 950B S6L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP AND INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
INTERIOR UPPER FUSELAGE BS 680 STR 10R CRACKED LOWER FLANGE RADIUS, OB OF CLIP. NDT VERIFIED CRACK, SPLICE ANGLES REMOVED REF SRM 51-30-2, DRILLED NEW STRINGER CLIP REF SRM 51-30-5. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. APPLIED CIC TO INTERIOR AND RECONDITIONED EXTERIOR SURFACE OF REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR
INTERIOR UPPER FUSELAGE BS 640 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED CRACKED STRINGER CLIP REF: SRM 51-30-02 P1. LOCATED AND DRILLED FASRENER HOLES IN CLIP REF SRM 51-30-05, INSTALLED STRINGER CLIP REF SRM 51-30-02 P1. APPLIED CORROSION INHIBITOR REF 51-10-02 P14. THIS IS CLASSIFIED AS A MAJOR REPAIR.
INTERIOR UPPER FUSELAGE BS 680 STR 10R STRINGER CLIP CRACKED. REMOVED STRINGER CLIP REF SRM51-30-2, DRILLED NEW CLIP REF SRM 51-30-5. INSTALLED NEW CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR
INTERIOR UPPER FUSELAGE BS 660 STR 9R STRINGER CLIP LOWER OB RADIUS CRACKED. REMOVED STRINGER CLIP, CLEANED AND FOUND NO CRACKS. REINSTALLED STRINGER CLIP REF SRM 51-30-02 THIS IS CLASSIFIED AS A MINOR REPAIR.
INTERIOR UPPER FUSELAGE BS 480 STR 10R STRINGER CLIP OB RADIUS CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES AND INSTALLED STRINGER CLIP REF SRM 51-30-2 PG 1-10. THIS IS CLASSIFIED AS A MAJOR REPAIR.
CABIN BS 950B S4L STRINGER CLIP CRACKED. REMOVED DAMAGED STRINGER CLIP REF 51-30-02, LOCATED AND DRILLED FASTENER HOLES REF SRM 51-30-05, INSTALLED STRINGER CLIP 65-45313Y2/A23841 REF SRM 51-30-02 P1, APPLIED CORROSION INHIBITING COMPOUND REF SRM 51-10-02 P14 THIS REPAIR IS CLASSIFIED AS MAJOR
CABIN BS 950B S5L STRINGER CLIP CRACKED. REMOVED STRINGER CLIP, TRANSFERED HOLES TO NEW CLIP AND INSTALLED REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.
INFLIGHT, LOWER AFT BODY OVERHEAT LT ILLUMINATED. ACCOMPLISHED QRH PROCEDURES AND DETERMINED THAT THE LEAK IS BETWEEN NR 3 BLEED VLV AND PACK VALVE. HAD TO DESCEND TO FL250 TO CONTROL CABIN ALTITUDE AT 10000 FT. RAN ENGINES AT H/P. NO OVERHEAT LIGHT CHECKED PLUMBING IN AFT STAIR AND FOUND CLAMP LEAKING AT AIR CLEANER. TIGHTENED CLAMP. OHMED OUT SENSORS, CHECKING FOR SHORTS TO GROUND, NONE FOUND. CHECKED ALL DUCT WORK INSIDE AND OUT INCLUDING KEEL BEAM WITH HAND HELD FLIR IMAGING SYSTEM. ALL TEMPS WELL BELOW TRIGGER THRESHOLD OF OVERHEAT SYSTEM IAW TSM 26-14-000. REMOVED AND REPLACED CONTROL UNIT. OPS CK GOOD IAW AMM 26-14-000-5.
DOORS LIGHT ILUMINATED WITH LANDING GEAR DOWN, NOSE GEAR LIGHT ILLUMINATED ON S/O PANEL. FLIGHT-GO-AROUND, RAN QRH LANDED UNEVENTFULLY. OBSERVED NG DOORS DROPPING 1 INCH, FOUND EXCESSIVE AMOUNT OF RUBBER BUILD UP ON FWD EDGE OF BOTH NG FWD FRAMES, CAUSING BOTH DOORS TO BIND WHEN CLOSING. CLEANED BOTH LEADING EDGES OF NG DOOR FWD FRAMES THAT CONTACT WITH NOSE GEAR WHEEL WELL FWD SEAL. CLEANED RUBBER BUILDUP FROM SEAL LUBED SEAL WITH SILICONE AND FRAMES WITH GREASE. TEST GOOD WITH MANUAL OPERATION. REF AMM 32-33-051-4 NSP.
OTBD FLAP GAUGE SHOWED ASYMMETRY WHEN RETRACTING FLAPS FOR 15 DEGREE TO 5 DEGREE. RIGHT NEEDLE STAYED AT FLAPS 15, LEFT NEEDLE MOVED TO 5 DEGREE AND STOPPED. ON TOUCHDOWN, FLAPS TRACKED NORMALLY TO FLAPS 25. T/S AND FOUND OUTBOARD FLAP INDICATOR INTERMITTENTLY SPLIT. REPLACED OUTBOARD FLAP INDICATOR REF MM 27-52-021-2. R/I FROM FACT REMOVAL/INSTALLATION OFF MFG 18-1299-4-2F1, POS OB SRL 0349G TAG 280B87 ON MFG 18-1299-4-2F1, SRL 0110G.
OUTBOARD FLAP GAUGE SHOWED ASYMMETRY WHEN RETRACTING FLAPS FOR 15 DEGREE TO 5 DEGREE. RIGHT NEEDLE STAYED AT FLAPS 15, LEFT NEEDLE MOVED TO 5 DEGREE AND STOPPED. ON TOUCHDOWN FLAPS TRACKED NORMALLY TO FLAPS 25. T/S AND FOUND OUTBOARD FLAP INDICATOR INTERMITTENTLY SPLIT. REMOVED AND REPLACED OUTBOARD FLAP INDICATOR REF MM 27-52-021-2. ALL FLAP OPERATION NORMAL. OK FOR SERVICE.
AFTER TAKEOFF WITH GEAR UP DURING FLAP RETRACTION, HYD SYSTEM-A BEGAN DECREASING TOWARD ZERO. RAN CHECK LIST AND LEAK DIDN'T STOP. INSTALLED NEW OUTBD FLAP HYD PUMP PER M/M 27-51-062-4. REPLACED NR 1 AND NR 2 ENG CASE DRAIN FILTERS PER M/M 29-11-041-2, NO CONTAMINATION IN FILTER. SERVICED A-SYSTEM HYDRAULICS PER M/M 12-12-000-2 AND OPS CHECKED ALL FLIGHT CONTROLS WITH NO LEAKS NOTED. GROUND RAN NR 1 AND NR 2 ENGINES PER JRH AND ALL OPS NORMAL. OFF MFG MS9-3911-30ZE-4C, ON MFG MS9-3911-30ZE4C.
EMERGENCY EXIT LIGHT ABOVE L-1 ENTRY DOOR INOP. REPAIR GROUND WIRE W102B-090-20 IAW BSWPM 20-20-00. LIGHT OPS CHECK GOOD IAW FEDEX B727-200 MM 33-50-101-2. FOR REFERENCE SEE FEDEX SNRM N00970.
CREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01 INFO 16NOV05 18:20 MC1 R. PLEASE WORK IN CONJUNCTION WITH TSI: 77-10 7868.
CREW REPORTS NR 3 EPR IND INOP/ERRATIC ON TAKEOFF ROLL. REPORTS ALL OTHER INDICATIONS NORMAL. RELEASED FOR SERVICE PER MEL/CDL: 77-01-01. MEL 77-01-01: NR 3 ENGINE EPR INDICATOR INOP. PLACED ON MEL DEFERRAL 77-01-01. EXPIRES 19 NOV 2005. OK FOR SERVICE. REMOVED AND REPLACED NR 3 ENGINE EPR INDICATOR AND TRANSMITTER PER AMM 77-11-011-4. AND OPS CHECKS NORMAL PER AMM 77-11-000-5.
WHILE DESCENDING ON GLIDESLOPE, ELEVATOR LOW PRESSURE LIGHT FLICKERED, CROSS CHECKED WITH HYDRAULIC PANEL AND NOTICED "A" SYSTEM AT ABOUT 1 QT. C/W QRH PROCEDURES. ENT BY: 448879 ADDED MPN BACH8A06NN0300T CPN 0109172 QTY 1 HOSE MSN 904416 ENT BY: 448879 . FOUND BRAIDED LINE ON LT BODY GEAR DOOR ACTUATOR RUPTURED. ORDERED HOSE CPN 0109172 MSN 904416. ENT BY: 448879 FACT 02NOV04 22:35 MCI R. REMOVED AND REPLACED BODY DOOR ACTUATOR LINE FOLLOWING FX MM 32-32-081-4, LEAK CHECK GOOD. ALSO, FOLLOWED FX MM 29-11-000-1 CASE DRAIN AND PRESSURE FILTER CHECK/REPLACEMENT. NO CONTAMINATION FOUND. LEAK CHECK GOOD. ENT BY: 393294 RPT BY: 393294.
DURING CLIMBOUT LIGHTS FLICKERED ON & OFF, A/P CYCLED. ALL GEN LOADS VARIED FROM 18 KW TO 30 KW, SIMULTANEOUSLY APPROX 1/2 SEC IN DURATION. GEN VOLT STEADY; FREQUENCY SPIKED WITH GEN SPIKES. INITIALLY OCCURRED AT HIGH POWER SETTINGS. STABILIZED ON POWER REDUCTION DURING DESCENT AND THEN REOCCURRED, WITH SPEED BRAKE DEPLOYED LIGHT CYCLED FROM ARMED TO DO NOT ARM.
WHILE WORKING FOUND DAMAGED SHEAR TIE AT BS 720A LBL 12 WL 156. REPAIRED SHEAR TIE AT BS 720A, LBL 12, WL 156 PER SRM 53-10-4 FIG 15 AND FED EX EA 7-5310-55179.
CORROSION WHILE WORKING FLOOR CLOSE FOUND CORROSION ON CENTER TANK SKIN BS 825 LBL 10.
STRINGER 27R CORRODED AT BS 740.
CORROSION ON STRINGER CLIP BS 990 STR 27 LT. REMOVED & REPLACED STRINGER CLIP AT BS 990, STR 27 LT THAT WAS OUT OF LIMITS PER SRM 51-20-1 & SRM 51-30-2.
CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 344 RBL 19. REMOVED AFT LAV WALLS FOR ACCESS. CUT OUT AND REPLACED DAMAGED FLOORBEAM BS 344, RBL 6 - RBL 65. MATERIAL BAC 1505-29222, LOT 525160 DRILLED AND COUNTERSUNK FASTENER HOLES. ALODINED, PRIMED FLOORBEAM. INSTALLED FLOORBEAM. REINSTALLED AFT LAV WALLS. IAW SRM 53-10-1, SRM 51-30-2, SRM 51-30-5, SRM 51-30-8, SRM 51-10-2.
CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 360 LBL 0 TO 10.
BS 720 STR 6 LT STRINGER CLIP IS CRACKED. REMOVED AND REPLACED STRINGER CLIP BS 720, STR 6L IAW SRM 51-30-02.
STRINGER CLIP CRACKED, STR 4L, BS 950C. REMOVED & REPLACED STRINGER CLIP AT BS 950C, STR 4L IAW SRM 51-30-2
INTERIOR FUSELAGE STRINGER CLIP IS CRACKED AT STR 4L, BS 783. REMOVED AND REPLACED STRINGER CLIP BS 783, STR 4L IAW SRM 51-30-02
N00325 BULGE IN LOWER FUSELAGE SKIN BETWEEN FASTENERS BS 704 STR 28L LBL 6. CUT OUT STR 28L BETWEEN B/S 700-720. FOUND SPLICE PIECE TO BE OUT OF LIMITS (CORRODED). SKIN WAS NOT AFFECTED BY CORROSION. DRILLED UP NEW STR SPLICE SECTION FROM BAC1498-144 LOT 478915. ALODINED AND PRIMED SECTION AND INSTALLED. ALL IAW SRM 53-10-1, 51-30-2, 53-10-3 AND 51-40-2.
STRINGER CLIP CRACKED, STR 6R, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STRINGER 6R IAW SRM 51-30-2.
VERTICAL FIN STR 8L AT FIN STA 157 IS CRACKED. REPAIRED CRACK IN STRINGE 8 LT AT FIN STA 157 PER SRM 55-30-4 FIG 1.
VERTICAL FIN STR 8L AT FIN STA 180 IS CRACKED.
STR 4 LT BS 720A STRINGER CLIP IS CRACKED.
VERTICAL FIN STR 8L AT FIN STA 133 IS CRACKED ** SD ** COMING
N01305 CORROSION ON FLOORBEAM AT BS 480 LBL 45 TO RBL 45 UPPER AND LOWER SURFACE ** SD ** COMING
STRINGER CLIP CRACKED, STR 5L, BS 950E. REMOVED AND REPLACED STRINGER CLIP AT BS 950E, STR 5L IAW SRM 51-30-2
FWD CARGO BAY, LWR DOOR CUTOUT THRESHOLD FRAME TOP FLANGE HAS 4 DAMAGED NUT PLATE HOLES. REPAIRED FLOOR BOARD BS 950F-1030, RBL 45-65, WL 208 BY REPLACING MISSING INSERTS PER FED EX DWG SRZ-25-005 REV E.
FWD CARGO STA 520 STR 23L FRAME IS DENTED. REMOVED DAMAGE ON FRAME BS 520, STR 23L. FABRICATED FRAME DOUBLER FOR CUT OUT. ALODINED, PRIMED & INSTALLED IAW SRM 51-40-3 AND EA 7-5310-70600.
STRINGER CLIP CRACKED, STR 4L, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 4L PER SRM 51-30-2. FABRICATED, LOCATED, DRILLED, ALODINED, PRIMED AND INSTALLED NEW STRINGER CLIP BS 950F, STR 4L PER SRM 51-20-1, 51-10-2, 51-30-2 AND FED EX MM 51-20-151-7. CLIP WAS FABRICATED FROM .032 7075 T6.
STRINGER CLIP CRACKED, STR 6L, BS 950C. REMOVED AND REPLACED STRINGER CLIP AT BS 950C, STR 6L IAW SRM 51-30-2.
CORROSION ON INTERCOSTAL, BS 312-344, LBL 29, WL 208. REMOVED CORROSION ON INTERCOSTAL STA 312-344, LBL 29, WL 208. REMOVED .001 1X1 INCH FROM .075. IN LIMITS. REMOVED CORROSION ON SHIM STA 328-344, LBL 29, WL 208. REMOVED .013 1 X1 INCH FROM .100. OUT OF LIMITS. FABRICATED & INSTALLED NEW SHIM.
BS 720B STR 9 RT STR CLIP IS CRACKED. REMOVED CRACKED STR CLIP AT BS 720B STR 9 RT PER SRM 51-30-2. LOCATED, DRILLED, AND INSTALLED NEW STRINGER PER SRM 51-30-5, 51-30-6 AND 51-30-2.
STRINGER CLIP CRACKED, STR 6R, BS 950F. REMOVED CRACKED STRINGER CLIP BS 950F, STR 6 RT PER SRM 51-30-2. FABRICATED, LOCATED, ALODINED, PRIMED, DRILLED AND INSTALLED NEW STRINGER CLIP BS 950F, STR. 6 RT PER SRM 51-20-1. NEW CLIP FABRICATED FROM .032 7075-T6 LOT 508473.
CORROSION ON STRINGER BS 1166 STR 24 RT. REMOVED CORROSION & FOUND OUT OF LIMITS. REPAIRED STRINGER BS 1166, STRINGER 24 RT PER SRM 53-10-3 AND 53-10-1.
CORROSION (C53-113-01), IN STRINGER BS 1010-1030 STR 27 LT. FOUND CORROSION ON STRINGER BS 1010-1030, STR 27LT TO BE OUT OF LIMITS PER SRM 53- 10-1. REPAIRED STRINGER IAW SRM 53-10-3.
CORROSION ON FRAME STA 540 RBL 5 WL 147. FRAME AT BS 540, RBL 5, WL 147 FOUND TO BE OUT OF LIMITS DUE TO CORROSION REMOVAL. REPAIRED FRAME SHEAR TIE PER SRM 53-10-1, 53-10-4 FIG 12.
CORROSION FLOORBEAM HAS SEVERAL AREAS OF CORROSION STA 380 RBL 45 TO 56.
FRAME AT BS 950D BETWEEN STR 26-27 LT HAS HOLE IN UPPER FLANGE RADIUS.
CORROSION ON BS 312 FLOORBEAM UPPER CHORD, LBL 19.5, WL 208. REMOVED CORROSION ON BS 312 FLOOR BEAM UPPER CHORD AT LBL 19.5 IN AREA OF 1 X 1 X .025 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE REPAIR PART MADE FROM 7075-T6 0.063, AND INSTALLED THE REPAIR PARTS IAW SR DRAWING 27-53-0
WHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1070 LBL 18 WL 150 TO BE DOUBLE HOLED. REMOVED DAMAGE ON FRQME QT BW 1070, LBL 18, WL 150 UPPER FLANGE. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1070, WL 150, LBL 18 IAW SRM 51-40-3.
WHILE WORKING FOUND UPPER FLANGE OF FRAME BS 1090 LBL 18 WL 150 TO BE TRIPLE HOLED. REMOVED DAMAGE ON UPPER FLANGE OF FRAME BS 1090, LBL 18, WL 150. INSTALLED NEW FABRICATED DOUBLER FOR FRAME AT BS 1090, WL 150, LBL 18 IAW SRM 51-40-3.
CORROSION ON FRAME BS 1148 BETWEEN STR 25-26 LT. BLENDED CORROSION FROM FRMAE BS 1148 BETWEEN STR 25-26 LT. REMOVED .040 FROM ORIGINAL THICKNESS OF .065. FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGE MATERIAL 1 X 2.5 INCH. FABRICATED AND INSTALLED REPAIR IAW SRM 51-40-3 USING LOT 518135 AND ER NO. 03-4723 AND FED EX EA 7-5310-55168.
CREASE BEAM WEB BS 740 TO BS 730F IS CORRODED. REMOVED CORROSION ON CREASE BEAMM WEB BS 740 TO 720F, LBL 65, WL 208. 1X2 INCH. MAXIMUM MATERIAL WAS .020. ORIGINAL THICKNESS .040. OUT OF LIMITS. CUT OUT DAMAGE. FABRICATED FILLER AND DOUBLER LOT 519938. 7075 T6 .040. ALODINED AND PRIMED AND INSTALLED FILLER AND DOUBLER IAW SRM 51-10-1/ SRM 53-10-1/ SRM 51-40-2/ SRM 51-10-2/ SRM 51-30-2/ FED EX MM 51-20-151-7.
CORROSION ON FRAME SPLICE STA 500 RBL 26.5 WL 156. REMOVED CORROSION FWD CARGO ON FRAME SPLICE AT BS 500, RBL 26.5, WL 156 IN AREA OF 1 X1 X .020 INCH MAX REMOVED. FOUND TO BE OUT OF LIMITS. FABRICATED THE DOUBLER MADE FROM 7075-T6 0.071, AND INSTALLED THE REPAIR DOUBLER IAW SRM 51-40-3.
LEADING EDGE FLAPS WOULD NOT RETRACT AFTER T/O. AMBER L/E FLAPS LIGHT DID NOT EXTINGUISH AT 2 DEG. AMBER IN TRANSIT LIGHT ON NR 2 SLAT LEFT WING WAS ILLUMINATED ON S/O PANEL. ENG ANTI-ICE WAS ON, WING ANTI-ICE WAS CLOSED. NR 2 L/E SLAT HAS JUMPER INSTALLED PER B-727-200 MM27-82-000. CYCLED FLAPS INITIALLY WITH ALL INDICATIONS NORMAL. CLEANED CONNECTERS AND INSTALLED JUMPER PRE- CAUTIONARY FOR POSSIBLE INTERMITTENT INDICATION.
HYDRAULIC A SYSTEM FAILURE DURING GEAR RETRACT FLUID QTY DEPLETED TO ZERO, EXCEEDED HYD FLUID S/O VALVE LIMITATION. REMOVED AND REPLACED LINE, CHECKED ALL A-SYS. LEAK CHECK GOOD.
AFTER T/O AMBER LIGHT DID NOT EXTINGUISH ON RETRACTION TO FLAPS 2 DEG, S/O AUX PANEL SHOWED A RIGHT NR 5 L/E FLAP INTRANSIT LIGHT. RECYCLED WITH SAME RESULT. REMOVED AND REPLACED NR 5 L/E FLAP POS SWITCH DUE TO FLT CREW WRITE UP. REF MM 27-82-001-4.
01-300 LWR AFT BODY HEAT LIGHT CAME ON. CK DUCTS IN AIR CONDITION COMP & AFT AIRSTAIR AREA. NO DEFECTS NOTED. OPS CK PER MM 26-14-00-1.
LWR AFT BODY OVERHEAT LIGHT ILLUM'D AFTER LEVEL OFF, ACCOMP'D RED TABS, RED TABS CONFIRMED NR 3 BLEED LEAK BET BLEED VALVE & PACK VALVE. REMOVED AND REPLACED COUPLING, SLEEVE, RING AND RETAINER PER SMP.
FRAME IS DENTED AT BS 680 AT STRINGER 24 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3.
NR 703 BULGE EXTERIOR SKIN BS 950E+3, STR 28 LH. ** S/D ** R&R SKIN PER IAW FEDEX EA 7-5330-57274.
NR 838 WHILE WORKING N0301 FND CRACK EMANATING FROM OPEN HOLE AT BS 460, STR 3 L/H. ** S/D ** R&R STRING PER FEDEX SRM 53-10-3, 51-20-151, 53-10-3.
EXTERIOR SKIN BULGED BS 500 BETWEEN STR 25 & 26 RT. *S/D* REMOVED AND REPLACED CORRODED SHEAR TIE PER IAW FEDEX SRM 51-10-6, 51-30-2, FEDEX MM 51-20-191, 51-20-21.
FRAME IS DENTED AT BS 660 AT STRINGER 25 RT. *S/D* REMOVED AND REPLACED PER IAW FEDEX SRM 51-30-2, 51-40-3.
CORROSION ON STR 28L, BS 700+15, WL 153. *S/D* REMOVED AND REPLACED STR PER IAW FEDEX SRM 53-10-1, 53-10-3.
BULGE IN EXT BELLY SKIN BS 950+5 INCH BL 0. REMOVED AND REPLACED PER FEDEX SRM 53-10-3 FIG 1, EA 7-5330-57281.
FRAME IS DENTED AT BS 700 BETWEEN STR 23 RT AND 24 RT.
FRAME DENTED TWO PLACES AT BS 500 BETWEEN STR 23 LT AND 25 LT.
FRAME IS DENTED AT BS 560 AT STRINGER 24 LT.
CREASE IN EXTERNAL SKIN AT BS 1193 JUST BELOW STR 16R. *S/D* REMOVED AND REPLACED SKIN PER FEDEX SRM 53-30-3 FIG 1.
FRAME IS DENTED AT BS 600 BETWEEN STRINGER 23 LT & 24 LT.
BULGE IN EXTERIOR SKIN BS 700 JUST ABOVE STR 26 RT.
ON T/O, GLARESHIELD ENG FAIL AND MASTER WARNING LIGHT WITH BELL ILLUM. REMOVED AND REPLACED ALL 3 AUTO PACK TRIP SYS PRESSURE SWITCHES PER B727-200 MM 21-11-011-4. REPLACED F/O''S FIRE BELL RESET LIGHT ASSY PER SMP.
T/O ROLL FIRE WARNING LIGHT CAME ON GLARESHIELD ILLUMINATED WITH ALARM BELL. REMOVED AND REPLACED APU FIRE AND OVERHEAT DET PWR UNIT PER IAW 727-200 MM 26-15-003-4 AS PRECAUTIONARY. SYS OPS CK NORMAL.
AFT T/O DURING FLAP RETRACT BOTH INBOARD AND OUTBOARD TRAILING EDGE FLAP IND STOPPED. AMBER LIGHT ILLUM, BUT EDGE DEVICE SHOW ALL GREEN ON 2ND OFF PNL. *S/D* CLEAN, LUB JACKSCREWS, GIMBALS, ROD ENDS, PULLEYS, AND CABLES PER MM 12-22-001-2. REMOVED AND REPLACED OUTBOARD T/E FLAP CONTROL LINK ASSY PER 727-200 MM 27-51-051-4. CK GOOD PER MM 27-51-000-5.
LWR AFT BODY OVERHEAT LIGHT IN FLT. PERFORMED PROC ON 2-7-14 TO STEP 14, LIGHT WENT OUT. FOUND CLAMP ON PURGE AIRLINE TO AIR CLEANER IN LEFT AFT AIRSTAIRS LEAKING. TIGHTENED CLAMP PER STANDARD MAINT PRACTICES. RAN APU PER JET RUN HDBK, NO LEAKS NOTED.
THE 2 FIRE WARN BELL CUTOUT LIGHTS ILLUM. ALL ENG INSTRUMENTS AND IND WERE NORMAL. TESTED ALL ENGINE FIRE LOOPS PER 727 MM 26-11-001-0, ALL TEST NORM. RAN ALL ENG PER JET RUN HDBK, NO DEFECTS NOTED.
98-295 - TAIL SKID LIGHT REMAIN ON AFT T/O, CYCLED THE LAND ONCE, LIGHT STILL ON. REMOVED AND REPLACED GEAR PINS. CLEAN AND LUBE TAIL SKID UP SWITCH. TAIL SKID IS FAIRED WITH FUSELAGE WHEN IN RETRACT POSITION.
CLIMBOUT, AC ELEV BUMPED IN LEFT TURN. AUTO PILOT SERVO IN AB. AFT LEVEL OF FLT LEVEL 310 ELEV TRIM RAN AWAY. AUTO PILOT DISCONN AND CRUISE CONT TO RUN. COULD NOT DUP PROBLEM. REMOVED AND REPLACED AUTO PILOT ACCY BOX PER MM 22-11-141 AND RELAY R102 AUTO PILOT AND STAB TRIM SYS. REPLACED RELAY. AC DOWNGRADED TO NOT CATEGORY 2 CHECK A AND B.
97-0257 - NR1 ENGINE FAILURE AT 400 FEET ABOVE GROUND LEVEL. POP HEARD IN COCKPIT. ENGINE WINDMILLED WITH NORMAL INDICATIONS. RESTART UNSUCCESSFUL. FOUND INPUT SHAFT FOR FUEL PUMP SPLINES STRIPPED INSIDE PUMP. REMOVED AND REPLACED NR 1 ENGINE FUEL PUMP PER MAINTENANCE MANUAL 73-11-01, AND REMOVED AND REPLACED FUEL CONTROL PER MAINTENANCE MANUAL 73-20-01. INSPECTED INLET AND EXHAUST, NO DEFECTS FOUND. NR 1 ENGINE LEAK AND OPERATIONAL CHECK GOOD. PERFORMED TAKEOFF EPR CHECK PER JET RUN HANDBOOK 6-15, CHECK GOOD.
97-0095, WHEN GEAR SELECTED DOWN THE RIGHT MAIN LIGHT DID NOT COME ON. TEST WAS GOOD. THE DOOR OPENED WITH THE HANDLE. RECYCLED THE GEAR THREE TIMES AND IT FINALLY CAME ON. PHYSICALLY CHECKED WIRE CONNECTIONS AT DOWN LOCK SWITCH. COULD NOT FIND PROBLEM OR MAKE LIGHT GO OUT. REPLACED LANDING GEAR ACCESSORY MODULE AND LANDING GEAR INSTRUMENT DISPLAY MODULE. TESTED UNIT PER 727-200 MAINTENANCE MANUAL 32-09-122 PAGE 501-506, OPERATIONAL CHECK GOOD.
GASPER FAN INOPERATIVE. CIRCUIT BREAKER POPPED OUT 3 TO 4 SECONDS AFTER TURNING GASPER FAN ON, BAD SMELL CAME OUT OF THE GASPER SOCKETS. REMOVED AND REPLACED GASPER FAN PER B727 MAINTENANCE MANUAL 21-23-11, OPERATIONAL CHECK GOOD.
NR 0141, 024 CORROSION (C53-1113-0141) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 600 WL 150 RBL 17. *S/D* REMOVED CORRODED SHEAR TIE AT BS 600 WL 150 RBL 1. FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 600 WL 150 RBL 17 PER FEDEX SRM 53-10-4.
NR0360 AND 025, NR 1 ENG CONTROL QUADRANT SUPPORT CASTING CRACKED JUST FORWARD AND I/B OF THRUST CRACK. *S/D* REMOVED AND REPLACED NR 1 ENG CONTROL QUADRANT SUPPORT CASTING PER FEDEX MM 76-12-0, 71-21-22, 71-21-21, 78-30-15, 76-12-41 AND 71-00.
NR 0386 023. FRAME IS CRACKED UNDER UPPER FLANGE AT STA 950E, 4.50 INCHES INBOARD OF STR 26L FROM HI-LOCK FASTENER HOLE INTO RADIUS OF FLANGE (OVER .25 INCH LONG). REMOVED DAMAGE AND REPAIRED FRAME UNDER UPPER FLANGE AT BS 950E, LBL 7 - 35 PER FEDEX SRM 51-40-3.
NR 01148 022. CORROSION C53-113-01(1) IN THE FORWARD CARGO BAY ON INTERCOSTAL BS 720, WL 148, LBL 10. ****S/D***** COMING.
DISCREPANCY: NR 0103 (20) SKIN DENT BS 267, WL 152, RBL 24. OUT OF LIMITS SRM 53-30-1. CORRECTIVE ACTION: REPAIRED SKIN DENT AT BS 267, WL 152, RBL 24, PER FEDEX SRM 53-30-3.
DISCREPANCY: NR 0305 (21) CRACK IN PLUS CHORD AT BS 760, LBL 70.5, WL 205. CORRECTIVE ACTION: *****S/D *****COMING.
DISCREPANCY: (NR 0383)(019) CORROSION (C53-113-01) IN THE FORWARD CARGO BAY ON STR 28R, BS 680, WL 148. CORRECTIVE ACTION: *****S/D******* COMING.
NR 0462, 015 CORROSION (C53-224-05) UPPER EXTERIOR SKIN ON CENTER WING FUEL TANK BS 825 RBL 65, WL 199. *S/D* REPAIRED UPPER EXTERIOR SKIN ON CENTER WING FUEL TANK AT BS 825 RBL 65 WL 199 PER FEDEX EA NR 7-5710-29704.
DISCREPANCY: NR 0155 (017) CORROSION (C53-113-01(1) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 700, WL 148, LBL 10. CORRECTIVE ACTION: ***S/D *** REMOVED OLD SHEAR TIE BS 700, WL 148, LBL 10. FABRICATED AND INSTALLED NEW SHEAR TIE BS 700 PER SRM 51-20-01.
DISCREPANCY: NR 0430 (016) WHILE WORKING 7-5310-7-432913 PT3 CORRECTIVE ACTION: ****S/D**** REPAIRED STR 18A AT BS 945 - 950, LBL 67, WL 109 PER EA 7-5310-29607.
DISCREPANCY: (NR 0147) (014) CORROSION (C53-113-01(2) IN THE AFT CARGO BAY FRAME SHEAR TIE BS 1148, WL 138, BLB 5, CORROSION FOUND TO BE OUT OF LIMITS. REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE AT BS 1148, WL 138, BLB 5, IAW 53-10-4.
DISCREPANCY: (NR 0137) (013) CORROSION (C53-113-01)(1) IN THE FORWARD CARGO BAY STRAP AND SKIN BS 680, WL 148, RBL 10. CORRECTIVE ACTION: CORROSION ON SKIN AND TEARSTRAP FOUND TO BE OUT OF LIMITS. ACCOMPLISHED SKIN AND TEAR STRAP REPAIR AT BS 680, RBL 10, WL 148, IAW SRM 53-30-4 AND SRM 53-10-04.
NR 0348, 012, WHILE WORKING NR 0148 FOUND SHEAR TIE CORRODED BS 720, LBL 11, WL 148. *S/D* CORROSION FOUND TO BE OUT OF LIMITS. REMOVED OLD SHEAR TIE AND INSTALLED NEW IAW SRM 53-10-4.
DISCREPANCY: NR 00157 (011) CORROSION (C53-113-01 )(1) IN FORWARD CARGO BAY ON STR 27 AROUND BOLTS WL 148, BS 720C. CORRECTIVE ACTION: REPAIRED CRACK ON LEFT INTERNAL RIB, STR 13, AFT SIDE BS 870 TERMINAL FITTING IAW FEDEX EA 7-5310-29173.
NR 0149, 007, CORROSION (C53-113-01) IN THE FWD CARGO BAY ON FRAME SHEAR TIE BS 720D, LBL 16, WL 148.
NR 0104, 006, SKIN DENT BS 416 RBL 40 WL 168. *S/D* REPAIRED SKIN DENT AT BS 416, RBL 40, WL 168 FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED DAMAGE, FABRICATED FILLER AND DOUBLER AND INSTALLED IAW 53-30-01.
NR 0145, 005, CORROSION (C53-113-01) IN AFT CARGO BAY ON FRAME SHEAR TIE BS 1130, WL 138, RBL 5. *S/D* REMOVED SHEAR TIE CROWN BS 1130, WL 138 RBL 5, FABRICATED SHEAR TIE PER FEDEX SRM 53-20-1. ALODINED, PRIMED, SEALED AND INSTALLED SHEAR TIE AT BS 1130, WL 138, RBL 5.
NR 0181, 008, NR 1 K-FLAP DATA PLATE AREA HAS CORROSION. *S/D* REMOVED CORROSION BY CUTTING OUT DAMAGED AREA AND INSTALLING FILLER AND REPAIR PLATES IAW SRM 29-57-010 AND 51-10-06.
DISCREPANCY: NR 0186 (002) CORROSION (C53-100-01) IN FORWARD NOSE COMPARTMENT ON CIRCUMFERENTIAL CHORD AND SURROUNDING STRUCTURE AT BS 227.8, RBL 7 TO LBL 7, WL 156. REMOVED CORRODED CIRCUMFERENTIAL CHORD BS 227.8, LBL 37 - RBL 37. FABRICATED AND INSTALLED CIRCUMFERENTIAL CHORD BS 227.8 LBL - RBL 37. ALL WORK DONE PER FEDEX DWG 65-16306 AND SRM 51-40-4.
DISCREPANCY: NR 0223 (004) LEFT WING, OUTBOARD MIDFLAP, LOWER SURFACE, TRAILING EDGE WEDGE DISBOND OUTBOARD OF OUTBOARD AFT FLAP TRACK. ***S/D*** REPAIRED LEFT WING O/B MIDFLAP LOWER SURFACE T/E WEDGE OUTBOARD OF OUTBOARD AFT FLAP TRACK IAW SRM 57-40-06.
DISCREPANCY: NR 0224 (003) LEFT WING, OUTBOARD MID-FLAP, UPPER SURFACE, TRAILING EDGE HAS 6 INCHES BY 1 INCH DISBOND FROM INBOARD END. REPAIRED LEFT WING OUTBOARD MID-FLAP UPPER SURFACE TRAILING EDGE 74 INCHES FROM INBOARD END IAW SRM 51-40-06.
DISCREPANCY: NR 0189 (009) CORROSION (C53-100-01) ON UPPER SURFACE OF THE HORIZONTAL FLANGE OF RT LOWER NOSE CHORD BETWEEN BS 322 AND 336, RBL 16, WL 148. CORRECTIVE ACTION: REMOVED CORRODED RT LOWER NOSE CHORD AND INSTALLED NEW RT LOWER NOSE CHORD BS 282 - 360, RBL 16, WL 148.
DISCREPANCY: NR 0157 (010) CORROSION (C53-113-01) IN THE FORWARD CARGO BAY ON FRAME SHEAR TIE BS 700, WL 148, RBL 10. CORRECTIVE ACTION: REMOVED CORRODED SHEAR-TIE AT BS 700, WL 148, RBL 10. FABRICATED NEW SHEAR-TIE AND INSTALLED REF SRM 53-10-4.
DISCREPANCY: (NR 0156) (018) CORROSION (C53-115-010) IN THE FORWARD CARGO BAY SHEAR-TIE, BS 700, WL 148, LBL 5. CORRECTIVE ACTION: REMOVED CORRODED SHEAR TIE, FABRICATED AND INSTALLED NEW SHEAR TIE ALL PER SRM 53-10-1 AT BS 700, WL 148, BLB, CORROSION FOUND TO BE OUT OF LIMITS.
INBOARD T/E FLAPS SPLIT. REMOVED AND REPLACED L/FLAP I/B TRANSMISSION PER MM 27-51-41, OPS CK GOOD. REQ ITEM INSP COMPLIED WITH.
SHUTDOWN NR 2 ENGINE DUE TO LOW OIL PRESSURE IN FLT. OIL PRESS DECREASED TO 20 PSI JUST PRIOR TO SHUTDOWN. FOUND LINE LEAKING OIL AT OIL PRESS TRANSMITTER. TIGHTENED LINE LEAK, CHECKS GOOD. PERFORMED INSPECTION IAW JET RUN HANDBOOK 6-59. NO DEFECTS, SERVICED OIL TO FULL PRESS NOW NORMAL.
MAIN CARGO DOOR LIGHT CAME ON IN FLIGHT ON CLIMBOUT. DEFERRED PER MEL 52-4 (A) MAIN CARGO DOOR VISUALLY CHECKED LOCKED EXPIRES 3/16/96 CONTROL0314030. REMOVED AND REPLACED AFT CARGO DOOR UNLOCKED LIGHT RECEPTACLE, OPS CHECKED GOOD.
TAIL SKID EXTENDED LIGHT ILLUMINATED AFTER TAKEOFF, WHEN GEAR HANDLE WAS PLACED TO THE OFF POSITION. RECYCLED GEAR TO UP AND LIGHT EXTINGUISHED. RECYCLED TO OFF. HANDLE AND LIGHT ILLUMINATED AGAIN. CONTACTED GOCC AND GOT NEW FUEL NUMBERS. TAKEOFF PLUS 10 MINUTES. LIGHT OUT WHEN LANDING GEAR DOWN. TESTED TAIL SKID AS PER MM 32-71-01, PAGE 503. SKID LIGHT DOES COME ON WITH GEAR HANDLE IN OFF POSITION. REPLACED TAIL SIDE ACTUATOR PER MM 32-71-12. GROUND OPS CHECK GOOD.
UNRELIABLE FUEL QTY IND ON FUEL GAUGES AFTER TAKEOFF. FOUND NR 2 FUEL GAUGE IN NR 3 POSITION AND NR 3 FUEL GAUGE IN NR 2 POSITION. SWAPPED FUEL GAUGES TO NORMAL POSITION, A/C REQUIRED DEFUELING. DEFUELED AND SUMPED NR 1, NR 2 AND NR 3 FUEL TANKS. CALIBRATED NR 2 AND NR 3 FUEL TANKS PER MM 28-41-02. SYSTEM OK FOR SERVICE. FOUND NR 1 TANK TO BE BAD, NO TIME TO WORK. DEF NR 1 FUEL QTY SYSTEM ON A/C MX LOG 440478.