N367FE
Registered owner: FEDERAL EXPRESS CORPORATION, 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
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
138 reports on file, 1999-11-24 – 2013-06-02.
Part: WEB — CRACKED (MLG WW) · airframe 81,300 hrs · 33,868 cycles
THREE CRACKS LT MLG WW INBD BULKHEAD 25 INCHES AND 27 INCHES AFT OF FWD BULKHEAD AND BOTH 4 INCHES DOWN FROM UPPER BULKHEAD. LAST CRACK IS 23 INCHES AFT OF FWD BULKHEAD AND 3 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED BULKHEAD IAW EA 8-5310-T0300629.
Part: BULKHEAD — CRACKED (MLG WW) · airframe 81,300 hrs · 33,868 cycles
TWO CRACKS CENTER MLG WW LT BULKHEAD 25 INCHES AFT OF FWD BULKHEAD AND 4 INCHES AND 5.5 INCHES DOWN FROM UPPER BULKHEAD. REPAIRED IAW EA 8-5310-T0300629.
Part: LINE — CLOGGED · airframe 80,826 hrs · 33,619 cycles
ENGINE FAIL WARNING ILLUMINATED ON GLARESHIELD ON TAKEOFF, NR 1 ENG N1 DID NOT ACCELERATE PAST 87 PERCENT. ENG DID NOT FAIL. DISCONNECTED NR 1 ENG CDP LINE. BLEW LINE CLEAR, FOUND MINOR DEBRIS IN LINE. CAPPED LINE AND PRESSURE CHECKED FOR LEAKS, NONE FOUND. RECONNECTED CDP LINE IAW AMM 73-20-01-2. PERFORMED MAX POWER ASSURANCE TEST IAW JRH 7-31. ALL PARAMETERS WITHIN LIMITS. PERFORMED ENGINE ACCELERATION TEST IAW JRH 7-17. ENGINE ACCELERATION ALSO WAS WITHIN LIMITS. ACFT OK FOR SERVICE. PERFORMED MAX POWER ASSURANCE TEST IAW JRH CHAPTER 7-31. ALL PARAMETERS WITHIN LIMITS. PERFORMED ENGINE ACCELERATION TEST IAW JRH 7-17. ENGINE ACCELERATION ALSO WAS WITHIN LIMITS. ACFT OK FOR SERVICE.
Earlier reports · 1999–2012 · 135 reports
2012
Part: BOLT — CORRODED (MLG TRUNNION) · airframe 79,742 hrs · 33,003 cycles
FOUND TRUNNION BOLT CORRODED. REMOVED AND INSTALLED NEW FWD TRUNNION BOLT ON RT MLG. IAW E.O 8-3210-7-5004 PT 2.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 79,742 hrs · 33,003 cycles
AFT CARGO COMPARTMENT WASTE TANK AREA HAS 2 EA CORRODED SHEAR TIES AT STA. 1997 BETWEEN LONGERON L51-52 AND R50-51. REMOVED AND REPLACED SHEAR TIES AT STA 1997 BETWEEN LONGERONS 50-51R AND 50-52L, REF SRM 51-33-01, VOL II.
Part: ANGLE — CORRODED (BS 1964) · corrosion level 2 · airframe 79,742 hrs · 33,003 cycles
AFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT BS 1964 BETWEEN R51L AND L51L IS SHOWING EVIDENCE OF EXFOLIATION. REMOVE AND REPLACE WITH NEW ANGLE. LOCATED, DRILLED, AND INSTALLED PER SRM 51-30-01 VOL.II AND INSTALLED IAW SRM 51-30-01.
Part: SHEAR TIE — CORRODED (BS 1975) · airframe 79,742 hrs · 33,003 cycles
AFT CARGO BAY ANGLE COMMON TO FRAME AND SKIN AT STA.1975 BETWEEN R51L AND L51L HAS EVIDENCE OF CORROSION. LOCATED, DRILLED AND INSTALLED NEW ANGLE IAW SRM 51-40-00, VOL II.
Part: STRUCTURE — GOUGED (ZONE 500) · airframe 79,742 hrs · 33,003 cycles
LEFT WING NR 1 SLAT TRACK IS RIDING AND CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. BURNISHED THE SLAT TRACK IAW CMM 57-55-04. ALODINE AND PAINT AND PRIMERED IAW SRM 51-21-01 AND 51-21-02. R & R NR 1 LT SLAT AND CLEARANCE AND OPS CHECK C/W IAW MM 27-80-01-4.
Part: SLAT TRACK — GOUGED (ZONE 500) · airframe 79,742 hrs · 33,003 cycles
LEFT WING NR 16 SLAT TRACK INBD SIDE IS RIDING INTO L/E STRUCTURE. L/E STRUCTURE HAS DAMAGE DUE TO THIS RIDING CONDITION. BLENDED DAMAGE AREA IAW SRM 57-00-01, VOL 1 AND EA 8-5710-156743.
Part: STRUCTURE — GOUGED (ZONE 500) · airframe 79,742 hrs · 33,003 cycles
LT WING NR 3 SLAT TRACK IS RIDING/CUTTING INTO L/E SUPPORT STRUCTURE. FWD UPPER TRACK CORNERS. CLEARANCE CHECKED GOOD.
Part: BEAM — CRACKED (ZONE 800) · airframe 79,742 hrs · 33,003 cycles
R3 DOOR BEAM IS CRACKED. R & R CRACKED DOOR BEAM, REF SRM 51-35-01, VOL II.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 79,637 hrs · 32,950 cycles
RT DOOR DISARMED LIGHT LENS IS MISSING. FOUND LENS ON FLOOR. REINSTALLED LENS. LIGHTS WORK OK.
2011
Part: BATTERY — INOPERATIVE (ESCAPE SLIDE) · airframe 78,815 hrs · 32,515 cycles
R1 DOOR CIRCUITRY TEST LIGHT INOPERATIVE. REMOVED AND REPLACED THE R1 DOOR REMOTE SLIDE PRESSURE INDICATOR AND REPLACED BATTERIES. OPS CK GOOD.
2010
Part: CONTROLLER — FAILED (FIRE DETECTION) · airframe 78,183 hrs · 32,160 cycles
AT CRUISE FL330, AIR MANF 2 FAIL. COMPLIED WITH QRH AND DIVERTED. RELEASED FOR SERVICE IAW MEL: 36-23-01-02, CATEGORY: C EXPIRATION: 13DEC10 "MEL 36-23-01-02: NR 2 MANIFOLD FAIL DETECTION LOOP NR2 INOP. NO HISTORY 99 DAYS ON SYS 2 MAN FAIL. NO CURRENT FAULTS AIU 1 IAW FIM 36-23 SUSPECT MAN FAIL DET CONTROLLER. R & R MAN FAIL DET CONTROLLER IAW AMM 36-23-01-4. AIR SYS TEST, OPS CHECKS NORMAL IAW AMM 36-23-01-5 WITH NO FAULTS. ALL MAIN LOOPS RESTORED TO NORMAL SELECTION.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 77,281 hrs · 31,724 cycles
RT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 FOUND 1 EACH DENT WITH DEEP NICK DURING BLEND OUT. DENT WITH DEEP NICK AT RT WING INBD FLAP UPPER SURFACE AT APPROX XIFH 215 REPAIRED IAW SRM 57-10-00 FIG 85 VOL I REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
Part: SKIN — DEFORMED (LT WING TE FLAP) · airframe 77,281 hrs · 31,724 cycles
LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE, FOUND SKIN DEFORMED. LT WING INBD FLAP LOWER L/E INBD OF OTBD HINGE DEFORMED SKIN EVALUATED AND FOUND WITHIN LIMIT IAW SRM 57-00-01 FIG 1B VOLUME I REVISION 96. DEPTH OF DENT = 0.013", DIAMETER OF DENT = 3.0".
Part: SEAT TRACK — CORRODED (BS 1963) · airframe 77,281 hrs · 31,724 cycles
AFT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK FOUND CORROSION. FT CABIN AT STA 1963, X= -107.25 RT CURVE SEAT TRACK R & R IAW SRM 51-31-01, VOL II REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
Part: SKIN — DENTED (HORIZONTAL STAB) · airframe 77,281 hrs · 31,724 cycles
EMPENNAGE- RT HORIZONTAL STABILIZER NR3 L/E (FROM INBD) FOUND DENTED. DENT AREA TRIMMED OUT AND FABRICATED REPAIR DOUBLER, REPAIR SKIN AND REPAIR CARRRIED OUT IAW SRM 55-10-00 VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
Part: SKIN — DENTED (RT WING TE FLAP) · airframe 77,281 hrs · 31,724 cycles
DENT - RT WING INBD FLAP LOWER SURFACE. REPAIR CARRIED OUT IAW SRM 57-10-00 FIG 3, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
Part: STRUCTURE — CRACKED (LT WING) · airframe 77,281 hrs · 31,724 cycles
LT WING - NR 1 SLAT LOWER SIDE BETWEEN NR 1 AND NR 2 TRACK FOUND EXTRUSION WITH CRACK. REPAIR CARRIED OUT IAW EA 8-5750-137977: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
Part: SKIN — DENTED (ZONE 100) · airframe 77,281 hrs · 31,724 cycles
FUSELAGE - AFT OF NOSE RADOME AT STA 305 LOWER CTR AREA WITH EXISTING BLEND OUT. EXISTING BLEND OUT AT FUSELAGE AFT OF NOSE RADOME AT STA 305, LOWER CTR AREA EVALUATED AND FOUND OUT OF LIMIT IAW SRM 53-10-00 VOL I, REV 96. ORIGINAL THICKNESS = 0.063", MATERIAL REMOVED = 0.028" AND REMAINING THICKNESS = 0.035". REPAIR CARRIED OUT IAW SRM 53-20-00 FIG 6 VOL I REV 96. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
Part: PANEL — BULGED (LT WING) · airframe 77,281 hrs · 31,724 cycles
LT WING T/E UPPER PANEL AT REAR SPAR APPROX XORS 860 FOUND WITH BULGING. CORROSION FOUND AT BULGING AREA REMOVED AND REPROTECTED IAW SRM 51-21-01 VOL II, REV 96, FOUND WITHIN LIMIT IAW SRM 57-20-00 FIG 37, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV. 110.
Part: DOOR FRAME — DAMAGED (CARGO DOORWAY) · airframe 77,281 hrs · 31,724 cycles
FWD CARGO DOOR JAMB-UPON REMOVAL OF AFT LOWER DOOR JAMB SEAL RETAINER, RIVET HOLES ON WEB STRUCTURE FOUND ELONGATED. REPAIR CARRIED OUT IAW EA NR 8-5310-137983, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
Part: BEAM — CRACKED (DOOR FRAME) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLE C. REPAIR CARRIED OUT IAW EA 8-5310-137972. REPAIR CLASSIFIED MAJOR GMM 6-2-100, REV 110.
Part: BEAM — CRACKED (DOOR FRAME) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSPECTION ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLE B. REPAIR CARRIED OUT IAW EA NR 8-5310-137972, TITLE: FUSELAGE - MAIN FRAME LOWER JAMB REPAIR TO BORE HOLES COMMON TO NR 1, NR 6 AND NR 7 SPOOL FITTINGS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV. 100.
Part: BEAM — CRACKED (DOOR FRAME) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 7 LOWER JAMB FITTING AT HOLES B AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
Part: BEAM — CRACKED (ZONE 200) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 2ND LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1 LOWER JAMB FITTING AT HOLES A, B AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB NR 4 SUPPORT FITTING AT HOLES A, B, C AND D IAW SRM 53-50-00 FIG 17 VOLUME I REVISION 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6- 2-100 REV 110.
Part: SKIN — DAMAGED (ZONE 100) · airframe 77,281 hrs · 31,724 cycles
FUSELAGE - FWD CARGO DOOR CUT-OUT LOWER AFT EXISTING DOUBLER FOUND DAMAGED. REPAIR CARRIED OUT AS PER SRM 53-50-00 FIG 26 VOL. I REV. 96. REPAIR CLASSIFIED AS MAJOR AS PER GMM 6-2-100 REV. 110.
Part: SUPPORT FITTING — CRACKED (ZONE 200) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND DURING HFEC OPEN HOLE INSP ON 0.460" HOLES AT MAIN CARGO DOOR LOWER JAMB NR 2 SUPPORT FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT AT MAIN CARGO DOOR LOWER JAMB NR2 SUPPORT FITTING AT HOLES A, B, C AND D IAW SRM 53-50-00 FIG 17, VOL I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
Part: ANGLE — CRACKED (BS 899) · airframe 77,281 hrs · 31,724 cycles
FWD CARGO BILGE AREA - APPROX STA 899 FRAME 'L' CLIP FOUND CRACKED. FWD CARGO BILGE AREA STA 899 FRAME 'L' CLIP REPAIR CARRIED OUT IAW SRM 53-30-00, FIG.10, VOL. I, REV 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
Part: RIB — CRACKED (RT WING) · airframe 77,281 hrs · 31,724 cycles
RT WING FIXED L/E LOWER FOUND CRACKED ON SLAT TRACK NR 16 INBD FWD RIB. CRACKED AT RT WING FIXED L/E LOWER ON SLAT TRACK NR 16 INBD FWD RIB REPLACED IAW SRM 51-31-01, VOLUME II REVISION 96. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 REV 110.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 77,281 hrs · 31,724 cycles
WHILE ACCOMPLISHING EA 8-5230-137737 PART 3 -TO REPAIR SKIN OF AFT LOWER CARGO DOOR OUTER SKIN, FOUND REPAIR AREA CLOSE TO COVER CUT-OUT AND PLACARD INSTALLATION. COMPLIED WITH EA 8-5230-132409: DOORS - LOWER CTR CARGO DOOR SKIN - REPAIR. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100, REV 110.
Part: BEAM — CRACKED (ZONE 200) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 1, LOWER JAMB FITTING AT HOLES A, B, C AND D. REPAIR CARRIED OUT IAW EA 8-5310-137972: REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 110.
Part: BEAM — CRACKED (DOOR FRAME) · airframe 77,281 hrs · 31,724 cycles
CRACK INDICATION FOUND ON 1ST LAYER WEB FROM TOP DURING HFEC OPEN HOLE INSP ON 0.520" HOLE AT MAIN CARGO DOOR NR 6 LOWER JAMB FITTING AT HOLES C. REPAIR CARRIED OUT IAW EA 8-5310-137972: FUSELAGE - MAINFRAME - MCD LOWER JAMB REPAIR TO BORE HOLES COMMON TO NR1. NR6, NR7 SPOOL FITTINGS. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 110.
2009
Part: VALVE — LEAKING (HYD SYSTEM) · airframe 76,786 hrs · 31,492 cycles
AT FL 280 GOT LEVEL-1 "HYD 3 ELEV OFF" FLUID IN NR 3 3.5 GAL. SECURED HYD SYS NR 3 FOR LANDING. AFTER DIRTY UP LOST REMAINING FLUID FOLLOWED BY "HYD 3 FAIL" TOWED TO GATE. FOUND HORIZONTAL STABILIZER PRIMARY CONTROL VALVE LEAKING. R & R HORIZONTAL STABILIZER PRIMARY CONTROL VALVE AMM 27-43-03-4.
2008
Part: LEAD — MALFUNCTIONED (NR 3 ENGINE) · airframe 75,049 hrs · 30,660 cycles
WHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS EGT 3 INDICATION. SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASH CREW REPORTED NO HIGH TEMPS, NO FLUIDS LEAKING. NO DEFECTS FOUND IN INTAKE/EXHAUST AREA. AIU-3 FAULT REVIEW HAS IN AIR FAULT 314174 ENG 3 EGT OUT OF RANGE,PROBABLE CAUSE ENG 3 EGT SENSOR,THIS SHOWS AS A INTERMITTENT FAULT. REMOVED AND REPLACED FWD THERMOCOUPLE LEAD IAW MM 77-21-02-2. ALL INDICATIONS NORMAL. RESET EXCEDENCE ON ENGINE DISPLAY. OK FOR SERVICE.
Part: LEAD — FAILED (ENGINE EGT) · airframe 75,049 hrs · 30,660 cycles
WHEN DESCENDING OUT OF FL240 FOR LANDING, GOT "ENG 3 EGT HI" AND ENG 3 EXCEEDANCE ALERTS, EGT 3 INDICATIONS SEQUENCED BETWEEN HIGH INDICATIONS (1053) AND AMBER "X", NO SECONDARY INDICATIONS. SHUT DOWN ENGINE IAW QRH, EGT WAS HIGH APPROX 30 SEC ON LANDING CRASH CREW REPORTED NO HIGH TEMPS, NO FLUIDS LEAKING. NO DEFECTS FOUND IN INTAKE/EXHAUST AREA. AIU-3 FAULT REVIEW HAS INAIR FAULT 314174 ENG 3 EGT OUT OF RANGE, PROBABLE CAUSE ENG 3 EGT SENSOR, THIS SHOWS AS A INTERMITTENT FAULT. REMOVED AND REPLACED FWD THERMOCOUPLE LEAD IAW MD10-10 MM 77-21-02-2. ALL INDICATIONS NORMAL. RESET EXCEEDENCE ON ENGINE DISPLAY. OK FOR SERVICE
Part: PRESSURE SWITCH — FAILED (ENGINE FUEL) · airframe 74,820 hrs · 30,548 cycles
DURING CLIMB-OUT, ABOVE 10,000 FT, RECEIVED LEVEL 1 HYD 2 OFF ALERT WITH SUBSEQUENT SHUTDOWN OF LT AND RT NR 2 ENGINE DRIVEN PUMPS. DURING APPROACH AND LANDING RMP'S REPRESSURIZED SYSTEM AND ACCOMPLISHED NORMAL FLAPS 35 LANDING. GVI DP INDICATORS ON NR 2 ENG HYD FILTER PCKG, NO FAULTS. REMOVED AND REPLACED NR 2 ENG RT PMP L PRESS SWITCH IAW 29-31-02-2 LK CK AND OPS CK NORMAL. PERFORMED HSC ADJ AND TEST IAW AMM 29-08-01-5 OPS CK NORMAL. PEFORMED AUTO FUNCTION OF NR 2 EDP'S IAW AMM 29-11-01-2 OPS CK NORMAL. REMOVED AND REPLACED ENG 2 LOW PUMP PRESS RELAY PRECAUTIONARY. CLOSED NR 2 ENG FAN COWL IAW AMM 71-00-00-2.
Part: PANEL — DELAMINATED (RT WING) · airframe 74,463 hrs · 30,363 cycles
RIGHT WING PANEL 635 BL HAS DELAMINATION AND A PUNCTURE. REPAIRED PANEL BY FABRICATING A NEW INNER SKIN IAW E.A. 8-5720-118490 & TPS 1001, REV E. DURING POST CURE CLEAN UP FOUND 4 CRACKS IN THE PANEL. HEAT TREATED IAW TPS 1003, REV A. FABBED REPAIR DOUBLERS IAW DWG ARC0795 & TPS 1001, REV E. PREPPED REPAIR AREAS ; LAYED UP THE REPAIR; VACUUM BAGGED & CURED REPAIR IAW SRM 51-71-00; VOL II.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
THE CENTER CARGO COMPARTMENT, LEFT TRANSITION PANEL SUPPORT HAS CORROSION AT STATION 1601, STRINGER 43L. REMOVED CORROSION IAW SRM 51-21-01; VOL II. FOUND TO TO BE EXFOILEATED. REMOVED AND REPLACED ADJ 7003-1 FITTING, IAW SRM 51-33-01; VOL II.
Part: SKIN — CORRODED (T/E FLAP) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
RIGHT WING INBD FLAP; INBD UPPER AFT SKIN IS CORRODED. REMOVED AND REPLACED THE SKIN IAW DC/MD-10 SRM 51-35-01; VOL II. FABRICATED NEW PANEL IAW DAC DWG NR ARC 2746, REV Z. ALODINED AND PRIMED IAW DC/MD-10 SRM 51-21-08. PART MARKED P/N FX-ARC 2746-24 IAW FEDEX GMM 7-0-1001.
Part: BRACKET — GOUGED (T/E FLAP) · airframe 74,463 hrs · 30,363 cycles
RIGHT WING INBD FLAP, INBD HINGE POINT IS GOUGED. BLENDED AREA. FOUND TO BE OUT OF LIMITS IAW SRM 57-00-01 AND DWG ARC 2518. REMOVED DAMAGED FAIL SAFE STRAP AND RECEIVED A NEW STRAP. LOCATED, DRILLED AND INSTALLED THE NEW STRAP IAW SRM 51-35-01, SRM 1-31-01, SRM 51-33-01& DWG ARC 2518. REMOVED BUSHING; FABRICATED / MACHINED A NEW BUSHING & INSTALLED THE NEW BUSHING IAW CMM 51-52-01. ALODINED & PRIMED IAW SRM 51-21-01.
Part: HINGE — CORRODED (T/E FLAP) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 OUTBD BORE IS CORRODED. REMOVED CORROSION FROM THE OUTBD BORE OF THEN 3 LUG IAW CMM 57-44-01. MACHINED BUSHING FOR THE OUTBD BORE IAW 57-44-01. CAD PLATED BUSHING IAW QQP-416-TY2-CL2 7. INSTALLED THE BUSHINGS IAW CMM 57-44-09. COMPLIED WITH FEDEX EA 8-5740-116979 DATED 5/1/2008.
Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
RIGHT WING OUTBD FLAP, OUTBD HINGE LOCATION NR 3 INBD BORE IS CORRODED. REMOVED THE CORROSION FROM THE INBD BORE IAW CMM 57-44-01. MACHINED NEW BUSHINGS FOR THE INBD BORE IAW CMM 57-44-09. CAD PLATED BUSHING IAW QQP-416-7Y2- CL2. INSTALLED THE NEW BUSHING INTO INBD THE BORE OF THE NR 3 LUG IAW CMM 57-44-01. COMPLIED WITH FEDEX EA 8-5740-116979 DATED 5/1/2008.
Part: HINGE — CORRODED (T/E FLAP) · airframe 74,463 hrs · 30,363 cycles
RIGHT WING OUTBD FLAP, INBD HINGE, LOCATION NR 3 INBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM LUG FACE NR 3 INBD TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-08. ETCHED NR 3 LUG FACE IAW SOPM 20-11-02. FLAP PEENED NR 3 INBD LUG FACE IAW SOPM 20-11-01. CAD PLATING REQUIRED AND ACCOMPLISHED ON N/R N00629 FOR THE TOTAL SURFACE AREA.
Part: HINGE — CORRODED (T/E FLAP) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 MOUNTING SURFACE IS CORRODED. REMOVED THE CORROSION FROM THE NR 3 LUG FACE IAW CMM 57-44-08. FABRICATED SHIMS IAW CMM 57-44-08. CAD PLATED SHIMS IAW QQP 416 TY2 CL2 AND INSTALLED SHIMS ON THE NR 3 LUG IAW CMM 57-44-01. COMPLIED WITH FEDEX EA 8-5740-116978 DATED 5/1/2008.
Part: FITTING — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
CENTER CARGO COMPARTMENT LT TRANSITION PANEL SUPPORT FITTING HAS CORROSION; MOUNTED ON THE FRAME AT FS 1661 LBL 43. REMOVED CORROSION IAW 51-21-01; VOL II. FOUND TO BE EXFOLIATED. REMOVED & REPLACED ADJ7003-1 FITTING. IAW SRM 51-33-01; VOL II.
Part: HINGE — CORRODED (ZONE 600) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
RIGHT WING OUTBD FLAP, INBD HINGE LOCATION NR 3 OUTBD LUG FACE OUTER SURFACE IS CORRODED. LUG THICKNESS VERIFIED TO BE .421 IAW BAC CMM 57-44-01. CORROSION FOUND AND REMOVED FROM THE LUG FACE TO .405. LUG FOUND TO BE OUT OF LIMITS IAW BAC CMM 57-44-01. ETCHED NR 3 LUG FACE IAW SOPM 20-11-02. CAD PLATING REQUIRED AND ACCOMPLISHED ON N/R N00629 FOR THE TOTAL SURFACE AREA.
Part: SKIN — DENTED (RT WING) · airframe 74,463 hrs · 30,363 cycles
RIGHT WING FIXED LEADING EDGE SKIN IS DENTED IN 4 PLACES AT STA XFS 627 TO XFS 653. DEPTH OF THE DENTS ARE0.045 TO 0.120. DENTS ARE OUT OF LIMITS IAW SRM 57-00-01 VOL I FIG 1B. FABRICATED REPAIR IAW SRM 52-00-01 VOL I FIG 4. ALODINED IAW SRM 51-21-01 VOL II. PRIMED IAW SRM 51-21-01 VOL II. INSTALLED THE REPAIR IAW SRM 51-00-01 VOL I FIG I.
Part: FRAME — GOUGED (RT WING TE FLAP) · airframe 74,463 hrs · 30,363 cycles
RIGHT WING T/E FLAP OUTBD ACTUATOR FAIRING, OUTBD L/E UNDER FAIRING MOUNT FRAME HAS 2 GOUGES. BLENDED GOUGES AND FOUND 1 EACH 0.030 DEEP TO BE OUT OF LIMITS IAW CMM 57-44-01. FABRICATION OF ANGLES WAS ACCOMPLISHED ON N/R N01025. REMOVED CLIPS FABBED IAW SRM 57-20-00; VOL I. ALODINED; PRIMED & PAINTED IAW SRM 51-21-01; VOL II. INSTALLED ANGLES IAW SRM 57-70-00.
Part: SUPPORT ANGLE — CRACKED (AFT PRESS BLKHD) · airframe 74,463 hrs · 30,363 cycles
UPPER INTERMEDIATE AFT FUSELAGE (ZONE 312); AFT PRESSURE BULKHEAD (STA 2007), AFT FACE UPPER CENTER SECTION. THE FUSELAGE SKIN SUPPORT ANGLE IS CRACKED. REMOVED AND REPLACED THE SUPPORT ANGLE IAW SRM 51-31-01 & 51-35-01; VOL II; PG 1. ALODINED & PRIMED IAW SRM 51-21-01; VOL II; PG 1. REINSTALLED PANEL IAW SRM 51-31-01; VOL II; PG 1. SEALED PANEL IAW SRM 51-41-01; VOL II; PG 1.
Part: WEB — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
CENTER PIT DOORWAY AT STA 1770 THE WEB BELOW THE AFT PDU HAS SIGNS OF CORROSION. WEB AREA IS OUT OF LIMITS IN REF TO SRM 53-00-01 VOL I FIG 1-B. CHANNEL AREA IS OUT OF LIMITS IAW SRM 53-00-01 VOL I FIG 1B. FABRICATED NEW CHANNEL IAW DWG AFA0154, REV AD. FABRICATED DOUBLER & FILLER FOR THE WEB REPAIR IAW SRM 53-00-01 VOL I FIG 10. ALODINED & PRIMED IAW SRM 51-21-01 VOL II. INSTALLED CHANNEL & REPAIR PARTS IAW SRM 51-33-01 VOL II.
Part: SHEAR TIE — CORRODED (ZONE 100) · corrosion level 2 · airframe 74,463 hrs · 30,363 cycles
SURFACE CORROSION FOUND AT BS 1997, BETWEEN LONGERON 50R AND LONGERON 49R IN THE AFT FUSELAGE COMPT. REMOVED THE CORROSION IAW SRM 51-21-01. ORIGINAL METAL THICKNESS WAS 0.071 IAW DWG AJC 7363. AFTER CORROSION REMOVAL THERE WAS 100% MATERIAL LOSS WHICH IS OUT OF LIMITS IAW SRM 53-00-01 VOL I FIG 1B. FABBED A NEW SHEAR TIE IAW DWG AJC 7363. INSTALLED SHEAR TIE IAW SRM 51-33-01.
Part: PLATE — CORRODED (ZONE 100) · airframe 74,463 hrs · 30,363 cycles
FWD CARGO COMP BILGE AT BS 753, THE DOUBLER BETWEEN STRINGER 48R TO STRINGER 49R IS CORRODED. REMOVED THE SPLICE IN REF TO SRM 51-33-01. FOUND TO BE CRACKED & CORRODED OUT OF LIMITS IN REF TO SRM 53-00-01. FABRICATED A NEW ARC3155-7 SPLICE IN REF TO DWG ACA 3155. ALODINED & PRIMED IN REF TO SRM 51-21-01. TOP COATED IN RF TO SRM 51-21-01. INSTALLED SPLICE IN REF TO SRM 51-33-01.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 74,463 hrs · 30,363 cycles
MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 9. DAMAGED SCALLOPS ON THE SEAT TRACK AT LBL 9 BS 755-763, FOUND TO BE OUT OF LIMITS REF SRM 53-70-00. REMOVED FLOOR PANELS TO GAIN ACCESS AT BS 615-890 LBL 9-28. REMOVED THE SEAT TRACK FROM BS 725-755 LBL 9. SPLICED A NEW SECTION AT BS 755 IAW SRM 53-70-00 VOL I FIG I SHEET I.
Part: SEAT TRACK — GOUGED (ZONE 200) · airframe 74,463 hrs · 30,363 cycles
MAIN CABIN FLOOR SEAT TRACK SCALLOPS GOUGED AT STA 635 RBL 28. BLENDED GOUGES. GAP BETWEEN SCALLOPS IS 0.500 MAX ALLOWED. REMAINING 0.515. OUT OF LIMITS IAW SRM 53-70-00; VOL I; PG 21. REMOVED & REINSTALLED (2) FLOOR PANELS IAW SRM 51-31-01; VOL II; PG 1. REMOVED DAMAGED TRACK SECTION & INSTALLED FABBED SECTION IAW SRM 51-31-01; VOL II. SPLICE HAT & PLATE IAW SRM 53-70-00; VOL I; PG 4 & DAC DWG 1428; REV I . ALODINED; PRIMED & TOP COATED IAW SRM 51-21-01; VOL II; PGS 1-24.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 74,463 hrs · 30,363 cycles
MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES AT STA 755 TO STA 763 LBL 28. SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00 VOL I FIG 5. REMOVED FLOOR PANELS AT BS 625-890 LBL 28-48 TO GAIN ACCESS. REMOVED TRACK FROM BS 725-755 & SPLICED IN A NEW SECTION AT BS 755 IAW SRM 53-70-00 VOL I. INSTALLED FLOOR PANELS BS 675-890 LBL 28 & 48 IAW AMM 53-21-01-2.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 74,463 hrs · 30,363 cycles
MAIN CABIN SEAT TRACK IN BALLMAT AREA SCALLOPS BROKEN AND SEVERAL GOUGES STA 753 TO STA 763 RBL 9. THE DAMAGED SCALLOPS ON THE SEAT TRACK AT RBL 9 & BS 753-763 FOUND TO BE OUT OF LIMITS IN REF TO SRM 53-70-00 VOL I FIG 5 SHEET 1. REMOVED DAMAGED SECTION AT BS 725-784 RBL 9. INSTALLED FABBED SEAT TRACK SECTION IAW SRM 53-70-00 VOL I FIG 1. REMOVED & REINSTALLED THE FLOOR PANELS IAW SRM 51-31-00 VOL II PG 1. MATERIAL ID SECTION; SPLICE HAT & PLATE IAW SRM 53-70-00 VOL I FIG 1 SHEET 2 & RAM DRAWING 1428, REV I. ALODINED & PRIMED PATS IAW SRM 51-21-1 VOL II PGS 1-25.
Part: FLOORBEAM — CRACKED (BS 1295) · airframe 74,463 hrs · 30,363 cycles
CABIN OVERWING FLOORBEAM IS CRACKED AT STA 1295 RBL 107 AT THE R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1295 BY SPLICING IN A NEW SECTION IN REF TO EA 8-5310-118482.
Part: FLOORBEAM — CRACKED (BS 1276) · airframe 74,463 hrs · 30,363 cycles
CABIN OVERWING FLOOR SUPPORT BEAM IS CRACKED AT STA 1276 RBL 107; AT R-3 DOOR THRESHOLD. REPAIRED CRACKED BEAM AT STA 1276 BY SPLICING IN A NEW SECTION IN REF TO E.A. 8-5310-118481.
2007
Part: DOOR — SEPARATED (RT WING) · airframe 73,785 hrs · 30,050 cycles
POST FLIGHT WALK AROUND, DISCOVERED RT WING FUEL DOOR MISSING FROM A/C. INSTALLED RT WING REFUELING ACCESS PANEL DOOR IAW SMP. OPS CHECKS NORMAL. OK FOR SERVICE.
2006
Part: RIB — CRACKED (RT WING) · airframe 71,855 hrs · 29,167 cycles
RT WING, L/E CRACK LONG 0.75" ON INTERNAL RIB AT STA XOS 498. REPAIRED RIB IAW SRM 57-20-00 FIG 1 SHT 1 AND 6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT STA XOS 632 ON RIB FOUND CRACK .75"LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1SHT 1 AND 6 VOL 1.
Part: SKIN — CRACKED (HORIZONTAL STAB) · airframe 71,855 hrs · 29,167 cycles
DURING INSPECTION, FOUND LOWER INTERIOR AND EXTERIOR SKIN PANEL ON HORIZONTAL STABILIZER, WITH CRACKS, SEE ATTACHED SHEET FOR BEST DETAIL. PANEL ALC7205-1 REMOVED AND REPLACED IAW SB 53-16 GROUP 1 AND FIG 7 SHT 1 STEPS 1-3, PANEL ALC7438-2 REPAIRED IAW SB 55-16 GROUP 1, FIG 20 AND EA NR 8-5510-96108A, LIGHT CORROSION REMOVED ON SPAR CAP. MAX MATERIAL LOSS FROM 2 AREAS = .010": SECTION (A) N = .170", R = .163"; SECTION (B) N = .354", R = .344", AREA TREATED IAW SRM 51-21-01 VOL 2 PAR 31-24. AREA WITHIN LIMITS.
Part: FRAME — CRACKED (BS 1159 S29-30L) · airframe 71,855 hrs · 29,167 cycles
LWR FUSELAGE CAC AT STA 1159 BTW LONG NR 29 AND LONG NR 30 LT SIDE ON FRAME FOUND CRACK 1" LONG AREA CLEANED IAW SRM 51-31-01 VOL 2 PAR 22. NDI INSP CARRIED OUT (SEE JPF). CRACK REMOVED IAW SRM 53-30-00 VOL 1 FIG 7 P/N'S I015877-3; -5; -13; -15. INSTALLED IAW SRM 53-30-00 VOL 1 FIG 7. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I015877/N00877 AND IAW SRM 53-30-00 VOL 1 FIG 7.
Part: PRESSURE BLKHD — CRACKED (BS 1381-1401) · airframe 71,855 hrs · 29,167 cycles
CLG W/W FOUND 1 CRACK 1" LONG ON VERTICAL BLKHD BTWN STA 1401 STA 1381 X = 32. DISASSEMBLED PNEU DUCTS ASSY ON BLKHD IAW MM 36-14-02-04. REMOVED SENSING ELEMENT IAW MM 36-23-00-00. REMOVED RIVETS ON STIFFENERS AND ON REINFORCE DOUBLER IAW SRM 51-35-01 VOL 2. CLEANED REMOVED PARTS. TRIMMED OUT CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 53-00-01 FIG 10 RIF SRM 51-33-01. INSTALLED PNEU DUCTS ASSY IAW MM 36-14-02-04. LEAK TEST WILL BE DONE BY JC 36C1608.
Part: SHEAR TIE — CORRODED (BS 939 S47-48R) · airframe 71,855 hrs · 29,167 cycles
DURING INSPECTION FWD CARGO BILGE FOUND SEVERE CORROSION WITH EXFOLIATION ON SHEAR CLIP AT STA 939 FROM STR NR 47 RT TO STR NR 48 RT. REMOVED CLIP IAW SRM 51-35-01 PAR 1-5 VOL 2. TRIMMED OUT SECTIONS OF SHEAR CLIP IAW SRM 53-00-00 FIG 10 VOL 1. INSTALLED NEW SECTIONS OF SHEAR CLIP AND NEW SPLICE IAW SRM 53-00-00 FIG 10 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELERS N00226/I015226 AND IAW SRM 53-00-00 FIG 10 VOL 1 AND 53-13-01 FIG 8 A SHT 3 VOL 1.
Part: RIB — CRACKED (RT WING) · airframe 71,855 hrs · 29,167 cycles
RT WING TANK NR 3 STATION XORS 345 FWD OF STRINGER 43 CRACK ON RIB LOWER FRAME CHORD APPROX 0.45" LONG WING RIB XORS 346. CRACK STARTING FROM RADIUS AND RUNNING FORWARD. DAMAGED FLANGE TRIMMED. NEW PART P/N N01167-3. FABRICATED AND INSTALLED IAW SRM 57-20-00 FIG 27 SHT 2,4 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER I016167/N01167 AND IAW SRM 57-20-00 FIG 27 SHT 2-4.
Part: SKIN — DAMAGED (BS 1019-1029) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE FWD CARGO COMPARTMENT FROM STA 1019 TO STA 1029 AT LONGERON 40 RT INTERNAL DOUBLER ON SKIN. REMOVED AND REPLACED FASTENERS IAW SRM 53-20-00 FIG 13 VOL 1.
Part: SKIN — BULGED (BS 445 S26R) · airframe 71,855 hrs · 29,167 cycles
UPPER FUSELAGE EXT SKIN FOUND SKIN BULGE ON R1 DOOR AT STA 445 LONG NR 26 RT. REPAIRED SKIN WITH FILLER AND DOUBLER IAW SRM 52-10-00 FIG 12A VOL 1 AND PROTECTED AREA IAW SRM 51-21-01 PAG 16 VOL 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I015181/N00181 AND SRM 52-10-00 FIG 12A VOL 1.
Part: FRAME — CRACKED (BS 1505) · airframe 71,855 hrs · 29,167 cycles
RT MLG W/W FOUND 1 CRACK 2" LONG ON FRAME AT STA 1505 X= -98. DISCONNECTED PIPES IAW MM 20-10-01-2. REMOVED PARTS IAW SRM 51-35-01 VOL 2 PAR 1-5. REPAIRED FRAME IAW SRM 53-00-01 VOL 1 FIG 8 SHEET 2-4. REINSTALLED PARTS IAW SRM 51- 35-01 VOL 2 PAR 1-5. RECONNECTED PIPES IAW MM 20-10-01-2 AND PERFORMED LEAK TEST IAW MM 29-00-00-2. TEST OK.
Part: SEAT TRACK — DAMAGED (BS 515-535) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE MAIN CABIN FROM STA 515 TO STA 535 X= -47 RT SIDE SEAT TRACK REPAIR. REMOVED AND REINSTALLED NEW SEAT TRACK IAW DWG SP10580218.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT STA XOS 454 ON RIB FOUND CRACK 1" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1.
Part: SKIN — WORN (CARGO DOOR) · airframe 71,855 hrs · 29,167 cycles
CTR CARGO DOOR FOUND DEEP WEAR ON EXT SKIN LOWER SIDE. TRIMMED OUT DAMAGED PORTION OF SKIN, AND INSTALLED 1EA FILLER AND 1EA EXTERNAL. REPAIR DOUBLER IAW SRM 52-10-00 VOL 1 FIG 17. FABRICATED PARTS IAW DETAIL PARTS TRAVELER N/R N00621 AND IAW SRM 52-10-00 VOL 1 FIG 17.
Part: PRESSURE PANEL — UNKNOWN (FUSLEAGE) · airframe 71,855 hrs · 29,167 cycles
HORIZONTAL PRESSURE PANEL BETWEEN STA 535 AND 555 X= 86 LT SIDE WEB FOUND EXISTING DOUBLER. ACCOMPLISHED EA NR 8-5330-99720. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016410/N01410 AND IAW EA NR 8-5330-99720.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
AIR CONDITION COMPT LT FOUND 2 CRACKS 2" LONG ON VERTICAL BULKHEAD FROM STA 480 TO STA 493 Z=-58 X= 24. REPAIRED WEB IAW SRM 53-30-00 VOL 1 FIG 6 SHT 4,5,10. THIS NRC COVER FEDEX NRC N00845. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016370/N01370 AND IAW SRM 53-30-00. TOUCHED UP REPAIR AREA WITH WHITE TOPCOAT IAW SRM 51-21-02 VOL 2.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
NLG W/W FOUND 4 CRACKS ON VERTICAL BULKHEAD BTWN STA 583 AND STA 588 Z=-37 X=-24. ACCOMPLISHED NR 8-5330-100639. FABRICATED PARTS IAW DETAIL PARTS TRAVELER NR I015840/N00840 AND IAW EA NR 8-5330-100639, TOUCH UP WITH WHITE TOPCOAT IAW SRM 51-21-02 VOL 2.
Part: RIB — CRACKED (BS 1026) · airframe 71,855 hrs · 29,167 cycles
LEFT WING L/E AT STA XOS 1026 ON RIB FOUND CRACK 1" LONG. REPAIRED RIB IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1. FABRICATED PARTS IAW DETAIL PART TRAVELER I015458/N00458 AND IAW SRM 57-00-01 FIG 3 SHT 2 VOL 1.
Part: BULKHEAD — CORRODED (BS 2007) · airframe 71,855 hrs · 29,167 cycles
AFT WASTE TANK COMPT FOUND SEVERE CORROSION ON "T" CAP VERTICAL BULKHEAD AT STA 2007 Z= -19 X= -55. REMOVED FLOOR PANELS TO ACCESS REPAIR IAW MM 20-50-02-2. REMOVED DAMAGED SECTION OF "T", FABRICATED AND INSTALLED "T" AND ANGLES IAW SRM 53-40-00 VOL 1 FIG 16 AND REINSTALLED FLOOR PANELS IAW MM 20-50-02-2. FABRICATED PARTS IAW DETAILED PARTS TRAVELER I015830/N00830 AND SRM 53-40-00 VOL 1 FIG 16.
Part: RIB — CRACKED (LWS 856) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT STA XOS 856 ON RIB FOUND CRACK 0.50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1/6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E CRACK LONG 0.5" ON RIB STA XORS 873 REPAIRED IAW SRM 57-00-01 FIG 3 SHEET 2 VOL 1.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE AVIONICS COMPT AT STA 322 X=60 EXISTING FRAME REPAIR, REPLACE PARTS IAW DWG ABA 7034 AND ABA 7202.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 71,855 hrs · 29,167 cycles
AFT CARGO DOOR EXT SKIN LWR CORNER EX REPAIR REMOVED AND REPAIRED IAW SRM 52-10-00 FIG 17 VOL 1.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 RT R3 DOOR JAMB EXISTING REPAIR REMOVED AND REPAIRED IAW SRM 53-50-00 FIG 19 VOL 1.
Part: BULKHEAD — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE AFT CARGO COMPT AT STA 2007 PRESS BULKD BETWEEN 51 LT TO 51 RT, EXISTING REPAIR REPAIRED IAW SRM 53-40-00 FIG 9 VOL 1.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 1781 L13 LT SIDE ON FRAME FOUND CRACK 6" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E CRACK LONG 1" ON RIB STA XORS 824 REPAIRED IAW SRM 57-20-00 FIG 1 SHEET 3.
Part: FRAME — CORRODED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
AIR COND COMPT LT FOUND CORROSION ON FRAME AT STA 542 X=30 CUT FRAME AND REPAIR IAW SRM 53-30-00 VOL 1 FIG 5.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE MAIN CABIN STA 1249-1254 BETWEEN LONG 26 LT TO 27 L3 DOOR JAMB EXISTING REPAIR REMOVER AND REPAIRED IAW SRM 53-50-00 FIG 19 VOL 1.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 1801 L13 LT SIDE ON FRAME FOUND CRACK 6" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
RT MLG W\W FOUND 1 CRACK 0.25 LONG AND 3 RIVETS LOOSE ON VERTICAL BLKD AT STA 1395 X=-32. REPAIRED IAW SRM 53-00-01 VOL1 FIG 4.
Part: BEAM — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
FWD CARGO STA 1099 STRINGER 43 LT BILGE AREA CRACK 4.5' ON BEAM. REPLACED BEAM IAW DWG AFA0039.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 1761 L13 RT SIDE ON FRAME FOUND CRACK 5" LONG CUT FRAME AND REPAIRED IAW SRM 53-30-00 FIG 5 VOL 1.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 1721 L13 RT SIDE ON FRAME FOUND CRACK 5" LONG CUT FRAME IAW SRM 53-30-00 FIG 5 VOL 1.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
EXTERNAL FUSELAGE AT STA 415 X=-8 LT SIDE LWR SIDE EXISTING REPAIR REMOVED AND REPLACED REPAIR IAW SSRM 53-20-00 FIG 6 VOL 1.
Part: FRAME — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 1741 L13 RT SIDE ON FRAME FOUND CRACK 0,5" LONG REPAIRED FRAME IAW SRM 53-30-00 FIG 4 VOL 1.
Part: INTERCOSTAL — CRACKED (RT WING) · airframe 71,855 hrs · 29,167 cycles
RT WING L/E CRACK LONG 1" ON INTERNAL INTERCOSTA AT STA XORS 540 REPAIRED IAW SRM 57-00-01 FIG 10 SHEET 1.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 RT R3 DOOR JAMB EXISTING REPAIR REVED AND REPAIR IAW SRM 53-50-00 FIG 19 VOL 1.
Part: DOOR FRAME — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
INTERNAL FUSELAGE MAIN CABIN STA 1305 TO 1315 BETWEEN LONG 26 TO 27 LT R3 DOOR JAMB EXISTING REPAIR REMOVED AND REPAIRED IAW SRN 53-50-00 FIG 19 VOL 1.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
EXTERNAL FUSELAGE MAIN CABIN STA 481 X= 70 LT SIDE EXISTING DOUBLER REMOVED AND REPAIRED IAW SRM 53-20-00 FIG 6 VOL 1.
Part: BULKHEAD — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
LT MLG WW AT STA 1490 X=32 Z=-65 ON SKIN BULKHEAD FOUND 4 CRACK 1" LONG TRIM DAMAGED AREA AND REPAIR IAW SRM 53-00-01 FIG 10 SHEET 4.
Part: FRAME — CORRODED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
AIR CONDITIONING COMPT LT FOUND CORROSION WITH EXF ON FRAME AT STA 547 X= 30. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5 (REF SRM 53-00-01 VOL 1 FIG 8). FABRICATE PARTS IAW DETAIL PARTS TRAVELER I016354/N01354 & IAW SRM 53-30-00 VOL 1 FIG 5.
Part: SEAT TRACK — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
MAIN CABIN AT STA 475 X= - 8.5 Z= -19 ON SEAT TRACK FOUND CRACK 5 INCHES LONG. REMOVED AND REPLACED TRACK IAW SRM 53-70-00 AND REPLACED CHANNEL IAW SRM 51-35-01 VOL 1.
Part: FRAME — CORRODED (BS 501) · airframe 71,855 hrs · 29,167 cycles
AIR CONDITIONING COMPT LT FOUND CORROSION WITH EXF ON FRAME AT STA 501 X= 30. REPAIRED FRAME IAW SRM 53-30-00 VOL 1 FIG 5 (REF SRM 53-00-01 VOL 1 FIG 8 ). FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016366/N01366 & IAW SRM 53-30-00 VOL 1 FIG 5.
Part: RIB — CRACKED (RT WING) · airframe 71,855 hrs · 29,167 cycles
RTH WING L/E CRACK LONG .75" ON INTERNAL RIB AT STA XOS 857. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 559 ON RIB FOUND CRACK .75" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: DOUBLER — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT STA XOS 645 ON DOUBLER FOUND NR 3 CRACKS 0.50" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 71 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 971 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT STA XOS 555 ON RIB FOUND CRACK .75" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 971 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 636 ON RIB FOUND CRACK .75". REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1 AND 6 VOL 1.
Part: MEMBRANE — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
COCKPIT AREA FOUND 1 EA CRACK 1 INCH LONG ON MEMBRANE OF FLOOR AT STA 303 X=13 RT SIDE. TRIMMED OUT DAMAGED PORTION OF MEMBRANE THEN INSTALLED REPAIR DOUBLER. FABRICATED PARTS IAW DETAIL PART SRM 53-00-01 FIG 4 SHT 2 VOL 1.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
AIR CONDITIONING COMPT LT FOUND 1 EA CRACK 2 INCHES LONG ON INTERCOSTAL AT STA 587 Z= -53 X= 70. CUT LOWER JAMB OF AFTER DOOR CUTOUT APPROX MIDWAY AND INSTALLED REPAIR JAMB IAW SRM 53-00-01 VOL 1 FIG 8 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016348/N01348 AND IAW SRM 53-00-01 FIG 8 SHT 2 VOL 1.
Part: WEB — CRACKED (BS 303) · airframe 71,855 hrs · 29,167 cycles
COCKPIT AREA FOUND 1 EA CRACK 1 INCH LONG ON MEMBRANE OF FLOOR AT STA 303 X=13 LT SIDE. TRIMMED OUT DAMAGED PORTION OF MEMBRANE THEN INSTALLED FILLER REPAIRED DOUBLER. FABRICATED PARTS IAW DETAIL SRM 53-00-01 FIG 4 SHT 2 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LEFT WING L/E AT STA XOS 458 ON RIB FOUND CRACK 1 INCH LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 3 VOL 1.
Part: DOUBLER — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
LT WING L/E AT XOS 626 ON DOUBLER FOUND NR 3 EA CRACKS 0.50 INCH LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 71 VOL 1. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I015512/N00512 AND IAW SRM 57-10-00 FIG 71 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 879 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: RIB — CRACKED (LT WING) · airframe 71,855 hrs · 29,167 cycles
FOUND LT WING L/E AT STA XOS 956 ON RIB FOUND CRACK .50" LONG. REPAIRED FORMER IAW SRM 57-20-00 FIG 1 SHT 1-6 VOL 1.
Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 71,855 hrs · 29,167 cycles
AIR CONDITIONING COMPT LT FOUND 1 EA CRACK 2 INCHES LONG ON INTERCOSTAL AT STA 587 Z= -53 X= 70. CUT LOWER JAMB OF AFTER DOOR CUTOUT APPROX MIDWAY AND INSTALLED REPAIR JAMB IAW SRM 53-00-01 VOL 1 FIG 8 SHT 2. FABRICATED PARTS IAW DETAIL PARTS TRAVELER I016348/N01348 AND IAW SRM 53-00-01 FIG 8 SHT 2 VOL 1.
2005
Part: PANEL — CRACKED (MLG WW) · airframe 71,178 hrs · 28,861 cycles
NOSE LANDING GEAR WHEEL WELL RT SIDE WEB UPPER FWD CORNER APPROX 2' FROM FWD PRESSURE BULKHEAD HAS 6" DIAGONAL CRACK. CUT OUT DAMAGED SECTION OF RT UPPER WEB IN NOSE WHEEL WELL LANDING GEAR. INSTALLED REPAIR DOUBLER REF: SRM 53-00-01. SNRM N00025 EMP. 356511
Part: WARNING LIGHT — ILLUMINATED (STALL WARNING) · airframe 70,975 hrs · 28,744 cycles
ON ROTATE STICK SHAKER ACTIVATED 140KTS A/C FULL BUFFET TO 3000 FT 180 KTS. DID NOT CHANGE T/O CONFIG. A/C STALL AT 15DGS AOB 210 KTS 15DGS FLAP. FLAPS 50, A/C BUFFETED AT 160KTS IN A FULL STALL LANDING, 20KTS FASTER THAN BUG. CKD FOR FULL EXT OF FLAPS /SLATS. INSP ALL FLT CONT SURFACES WERE CONFIG CORRECTLY. CKD SPOILERS FULL UP AND DOWN. NO DEFECTS. PERF STALL ADJ/TST AND AT/SC ADJ/TST IAW DC-10MM'S 22-33-00-2, AND 22-30-00 REF WRI 34-18/7405 FOR WORK ACCOMP, C/W ELEV LOAD FEEL AND MECH TESTS REF DC-10 MM 27-30-00-5. CKD FLAP AND AOA VANE FOR PROPER OP. REMOVED AND REPLACED AT/SC NR 2. REMOVED AND REPLACED NR 2 LAU PER M/M22-11-01-2. PURGED AND LEAK CKD CAPT'S AND F/O'S PITOT SYSTEMS.
Part: ATTACH FITTING — BROKEN (ZONE 600) · airframe 70,882 hrs · 28,694 cycles
RT I/B FLAP, I/B ACTUATOR AFT ATTACH FITTING BROKEN. REMOVED RT I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-01-2 STEPS A1 THRU ALL. INSTALLED NEW R/H I/B FLAP I/B ACTUATOR SUPPORT FITTING PER MM 27-52-1-2. ENLARGED & REAMED FOUR HOLES IN FITTING PER SERVICE BULLETIN 57-76. DAMAGED LOCK FASTENERS ON LOWER BOTTOM SIDE OF ACTUATOR SUPPORT. STRUCTURE TO BE REPLACED AT NEXT C-CHECK PER EA 8-5750-86513. INSTALLED NEW HYD LINES PER MM 27-52-01-2. LEAK & OPERATIONAL CHECKS COMPLIED WITH PER MM 27-52-01-2
2004
Part: LONGERON — CHAFED (ZONE 400) · airframe 69,609 hrs · 28,032 cycles
FOUND LONGERON FLANGE CHAFED BEYOND LIMITS, AREA 2.5 INCHED LONG BY 0.250 INCHES WIDE, COMPLETELY THROUGH .063 INCH FLANGE, NR 2 RIGHT HAND COWL, JUST AFT OF CENTER HINGE POINT. FABRICATED REPAIR AND INSTALLED REPAIR IAW FEDEX EA 8-5410-81503.
Part: LONGERON — WORN (ZONE 400) · airframe 69,609 hrs · 28,032 cycles
REMOVED UPPER COWL CHAFE STRIPS AND FOUND LONGERON FLANGE CHAFED AREA 2.5 INCHES LONG BY 1.5 INCHES WIDE JUST AFT OF CENTER LINE, NR 1 ENGINE RIGHT HAND COWL. REPAIRED DAMAGED LONGERON IAW FEDEX EA 8-5410-81504.
Part: DUCT — BROKEN (ZONE 400)
NR3 ENGINE PNEUMATIC DRIVE MOTOR PNEUMATIC SUPPLY DUCT ADEL CLAMP MOUNT TAB BROKEN OFF. REMOVED, WELD REPAIRED AND REINSTALLED NR 3 ENGINE PNEUMATIC DRIVE MOTOR SUPPLY DUCT IAW DC10 MM 36-14-02-4 AND FEDEX EA 8-7830-81506. REFERENCE NON-ROUTINE N01094.
Part: PANEL — DEBONDED (ZONE 600) · airframe 69,609 hrs · 28,032 cycles
RIGHT WING PANEL NR 661 EB IS DISBONDED AT FINGER DOUBLER AT MIDDLE FASTENER HOLE. REPAIRED BY FABRICATING AND BONDING NEW INNER AND OUTER SKIN, DOUBLER AND CORE IAW DAC DWG ARC0633 AND FEDEX EA 8-5710-81508. REMOVED AND REINSTALLED HINGED PANEL 661 EB SEAL RETAINER AND SEAL IAW DC10 SRM 51-35-01 AND 51-31-01 VOL 2.
Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 69,609 hrs · 28,032 cycles
LEFT WING INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT INBOARD BORE GOUGED. REMOVED DAMAGE IAW DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00416.
Part: HINGE FITTING — CORRODED (ZONE 500) · airframe 69,609 hrs · 28,032 cycles
LEFT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE PITTED. REMOVED DAMAGE, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57- 52-01 AND FED-EX EA 8-5750-81492 REFERENCE NON-ROUTINE NR N00417.
Part: ROLLER — WORN (ZONE 600) · airframe 69,609 hrs · 28,032 cycles
RIGHT WING INBOARD FLAP INBOARD MOST FORWARD TOP ROLLER IS WORN. REMOVED AND REPLACED RIGHT WING INBOARD FLAP INBOARD TRACK MOST FORWARD TOP ROLLER I/A/W DC10-10 MAINTENANCE MANUAL 20-50-02-2 AND EA 8-5750-81490. REFERENCE NON-ROUTINE NR N00776.
Part: HINGE FITTING — CORRODED (ZONE 600) · airframe 69,609 hrs · 28,032 cycles
RIGHT WING INBOARD FLAP, OUTBOARD SUPPORT, PIVOT ATTACH POINT, OUTBOARD BORE GOUGED. REMOVED DAMAGE I/A/W DOUGLAS CMM 57-52-01, BORE FOUND OUT OF LIMITS. REPAIRED BORE I/A/W DOUGLAS CMM 57-52-01 AND FED-EX EA 8-5750-81491 REFERENCE NON-ROUTINE NR N00412.
2003
Part: SENSOR — MALFUNCTIONED (CARGO TEMP) · airframe 67,974 hrs · 27,230 cycles
CARGO BAY TEMP AFT WAS PEGGED AT 170 DEG. RETURNED FLIGHT TO LAX. REMOVED AND REPLACED CARGO COMPARTMENT TEMP SENSOR (TRANSMITTER) PER MM 21-41-01-2, OP'S CK'D GOOD.
Part: WARNING LIGHT — ILLUMINATED (A/C DOOR) · airframe 67,300 hrs · 26,915 cycles
IN CRUISE AT FL330 30 MIN AFTER TAKEOFF THE AIR COND DOORS CAUTION LIGHT ILLUMINATED. CABIN PRESS WAS ON SCHED IN STBY MODE. RED TABS RAN, DIVERT TO KMEM. DUPLICATED INTERMITTENT LIGHT AT PACK NR 3 COMPARTMENT DOOR. FOUND PLUG P1-1616 CORRODED. REPLACED PLUG P1-1616 AND SWITCHED S1-255 AND S1-257 REF DC-10 WDM 52-71-02, SWMP AND MM 52-70-07-2. PLUG P1-1617 AND P1-1618, AND SWITCH S1-256 PREVIOUSLY CHANGED. ALL 3 AIR CONDITIONING COMPARTMENT DOOR WARNING SWITCHES CHECK NORMAL REF DC-10 MM 52-70-07-2.
2001
Part: GEARBOX — MALFUNCTIONED (NR 1 T/R) · airframe 64,850 hrs · 25,710 cycles
NR 1 THRUST REVERSER FAILED TO STOW AFTER LANDING. REMOVED AND REPLACED ALL CABLES AND GEAR BOX ASSY PER MM 78-32-07.
2000
Part: PROXIMITY SWITCH — FAULTY (LT MLG)
00-378 LEFT GEAR UNSAFE LIGHT ILLUM. R&R PROX SWITCH ELECTRONIC CONTROL UNIT IAW DC10-10 MM 32-61-01-2. PERF GEAR RETRACTION AFT PROX ELEC UNIT REPLACEMENT NO DEFECTS NOTED. SYS OPERATES NORM PER MM 7-11-00 & MM 32-30-00.
Part: SWITCH — INOPERATIVE (MLG)
00-1 - UPON GEAR EXT, 3 RED LIGHTS BOTH PNLS PERF RED TABLS 2-6-5. ALT GEAR EXT LEVER WAS RAISED AND 3 GREEN LIGHTS ILLUM BOTH PNLS. REMOVED AND REPLACED SWITCH ACTUATOR IAW MM 32-61-04-2. REMOVED 3 JACKS AND PADS FROM AC.
1999
Part: LEVER — STICKING (MLG)
LOWERED GEAR DIDN'T GET LIGHT ON EITHER PNL. WHEN GEAR ALT HANDLE IS STOW AFT LAND RED LIGHTS ILLUM. LUBED LANDING GEAR CONTROL LEVER MECHANISM. OPS CK GOOD. GROUND LIGHT ON BOTH POS.
Part: TERMINAL — FAILED (PRESS CONTROLLER)
AC WOULD NOT PRESSURIZE. ALL DOORS CLOSED. REPAIRED TERMINAL END IAW SMP. IND LIGHT WORKS NORM, SYS CK NORM.