N938FD
Registered owner: FEDERAL EXPRESS CORP, TN (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
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.
87 reports on file, 2012-12-12 – 2023-10-30.
Part: STATIC INVERTER — BURNED (ZONE 100) · airframe 91,025 hrs · 30,414 cycles
MDIS 938 24-22 9631 30OCT23 IND FACT U UPON POWERING UP AIRCRAFT, NOTICED AN ACRID SMELL IN COCKPIT WITH ASSOCIATED STBY INVERTER EICAS MSG. PART 30OCT23 16:24 MC1 U IDENTIFIED PARTS STATIC INVERTER MPN: 1-002-0102-2090 CPN: 2413802 QTY: 1 R/I 30OCT23 16:33 IND U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 707760-4 POS: ONL ON MPN: 1-002-0102-2090 SRL: CJ002100 TAG NBR: 8G9069 FACT 30OCT23 16:33 IND U AMM: 24-33-03-4 R&R STATIC INVERTER REF AMM, VOLTS AND FREQS NORMAL, CHECKS OK. FACT 30OCT23 16:33 IND AMM: 24-33-03-4 R&R STATIC INVERTER REF AMM, VOLTS AND FREQS NORMAL, CHECKS OK.
Part: UNKNOWN — SHEARED (UNKNOWN) · airframe 90,855 hrs · 30,302 cycles
MDIS 938 32-42 9432 27JUL23 BUR FACT U AT PUSHBACK #7 MLG TIRE BLEW, UPON INSPECTION FOUND EIGHT TIE BOLTS HAD SHEARED OFF. 5 R/I 27JUL23 04:06 BUR U REASON CODE : PREMATURE REMOVAL/INSTALLATION OFF MPN: 160N0001-38 POS: 8 SRL: A0681 ON MPN: 160N0001-38 CPN: 3215827 SRL: A0396 TAG NBR: I41446 FACT 27JUL23 04:06 BUR U AMM: 32-45-01-4 REMOVED AND REPLACED #7 MAIN TIRE AND WHEEL ASSY PER M/M 32-45-01-4 FACT 27JUL23 04:06 BUR U AMM: 32-45-01-4 REMOVED AND REPLACED #7 MAIN TIRE AND WHEEL ASSY PER M/M 32-45-01-4 AMM: 32-45-01-4 REMOVED AND REPLACED THE #8 MAIN TIRE AND WHELL ASSY PER M/M 32-45-01-4.
Part: SKIN — DAMAGED (N/A) · airframe 90,693 hrs · 30,197 cycles
R/H EXTERIOR FUSELAGE SKIN DOUBLER HAS 2EA DENTS BETWEEN BS 540 AND BS 560 AND STRINGER S-22R AND STRINGER S23R REPAIRED PER FEDEX EA # F-5330-165083-P3
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,693 hrs · 30,197 cycles
AREA OF AFT CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX RBL 13 REMOVED AND REPLACED ANGLE (FLOOR SUPPORT) AND NUTPLATE STRIP IAW BAC DWG 146N5300 REC C 140N2524 REV A, B757 SRM 51-40-02-0G
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,693 hrs · 30,197 cycles
AREA OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE AND NUTSTRIP ARE CORRODED BETWEEN STA 1701 AND 1720 APPROX LBL5 REMOVED AND REPLACED ANGLE ( FLOOR SUPPORT) WITH NUTPLATE STRIP IAW BAC DWG 146N5300 REV C 140N2524 REV A B757 SRM 51-40-02-0G
Part: PANEL — DELAMINATED (N/A) · airframe 90,693 hrs · 30,197 cycles
R.WING L/E PANEL 611DB HAS COMPOSITE DAMAGE ON MULTIPLE AREAS. ACCOMPLISHED PERMANENT REPAIR ON R/W L/E PANEL 611DB COMPOSITE DAMAGE PER B757 SRM 57-41-01-4R, 51-70-08-0G AND FIG 201, AND BOEING DWG 114N1523 REV D
Part: ANGLE — CORRODED (ZONE 200) · corrosion level 2 · airframe 90,693 hrs · 30,197 cycles
AREA AFT OF THE BULK CARGO COMPARTMENT, MAIN CABIN FLOOR SUPPORT STRUCTURE & NUT STRIP ARE CORRODED BETWEEN STA 1701 & 1720 APPROX RBL 5 REMOVED AND REPLACED FLOOR SUPPORT AND NUTPLATE STRIP IAW B757 SRM 51-40-02-0G AND BAC DWG 146N5300 REV C AND 140N2524 REV A
Part: PANEL — DELAMINATED (N/A) · airframe 90,693 hrs · 30,197 cycles
#1 PYLON PANEL 432AL AFT 2 CORNERS ARE DELAMINATED AND DAMAGED. ACCOMPLISHED PERMANENT REPAIR OF PANEL PER B757 SRM 51-40-02, 54-50-70-0G, 51-70-17-0G AND BOEING DWG 313N5003.
Part: STRAP — CRACKED (N/A) · airframe 90,693 hrs · 30,197 cycles
#2 ENG I/B T/R L/E RADIAL STRAP IS CRACKED AT APPROX 8 0CLOCK POS. REMOVED AND REPLACED PER B757 AMM 78-31-20-8
Part: UNKNOWN — UNKNOWN (N/A) · airframe 90,616 hrs · 30,149 cycles
PDIS 938 52-10 9099 09FEB23 PHX FACT U ON FO S PRE-FLIGHT FO DISCOVERED R1 DOOR SLIDE CABLE EXPOSED. CALLED MX TO VERIFY AND CHECK THAT IT WOULD NOT CATCH ON THRESHOLD, AND POTENTIALLY DEPLOY SLIDE. FACT 09FEB23 17:52 MEM U AMM: 25-66-01-4 AMM: 52-11-00-2 INSP R1 DOOR ESCAPE SLIDE ASSY. RESTOWED ESCAPE SLIDE STATIC LINE. SLIDE ASSY CHECKS GOOD IAW AMM 25-66-01-4. R1 DOOR OPERATION CHECKS GOOD IAW AMM 52-11-00-2. THIS CLEARS MEL.
Earlier reports · 2012–2022 · 77 reports
2022
Part: SURVIVAL KIT — OUT OF POSITION (R1 DOOR SLIDE) · airframe 90,129 hrs · 29,814 cycles
R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP NOT STOWED PROPERLY. REMOVED SLIDE COVER AND PROPERLY STOWED THE R1 DOOR EMERGENCY SLIDE SURVIVAL KIT STRAP AND INSTALLED THE SLIDE COVER IAW B757 AMM: 25-66-01-4.
Part: GIRT BAR — DIRTY (N/A) · airframe 90,077 hrs · 29,778 cycles
PDIS 938 25-60 8387 10MAY22 SJO FACT U ENTRY DOOR KNUCKLE BUSTER WILL NOT DEPLOY WHEN ARMING DOOR. FACT 10MAY22 01:43 SJO U INSPECTED L1 ENTRY DOOR AND REMOVED DEBRIS FROM GIRT BAR , PERFORMED OPS CK IAW AMM 25-66-10-2. ALL CKS NORM
Part: HOSE — FAILED · airframe 89,961 hrs · 29,696 cycles
L HYD QTY L HYD SYS PRESS TE FLAP DISAGREE COMPLIED WITH QRH, DECLARED EMERGENCY. LANDED RWY 31, SHUTDOWN ON RWY. PERFORMED EDP INSPECTION/CHECK REF AMM 29-11-05-6...NO CONTAMINATION FOUND...REPLACED EDP PRESSURE & CASE DRAIN FILTERS REF AMM 29-11-00-6-0, INPECTED ALL SYSTEM DPI'S...NONE POPPED. INSTALLED HYDRAULIC LINES ON DOWNLOCK ACTUATOR REF AMM 32-32-02-4...CYCLED GEAR HANDLE, LEAK CHECK GOOD...PERFORMED LEAK CHECK ON PRESSURE AND CASE DRAIN FILTERS, NO LEAKS NOTED...SERVICED HYDRO QTY REF AMM 12-12-01-3...RAN BOTH ENGINES AND CYCLED FLIGHT CONTROLS...ALL PARAMETERS NORMAL FOR SERVICE...HYDRAULIC FLEX LINES REPLACED .
2021
Part: SEAT TRACK — CORRODED (MAIN CARGO) · corrosion level 2 · airframe 89,282 hrs · 29,258 cycles
DOT# 106-12, MAIN CARGO COMPT APPROX. STA. 1340, RBL 45.50 SEAT TRACK HAS CORROSION. CUT OUT DAMAGE SEAT TRACK FROM STA 1300 TO STA 1350 RBL 45.5 IAW SRM 53-00-52-2R, REPAIR SEAT TRACK IAW SRM 53-00-52-2R. (INSTALLED NEW SEAT TRACK SECTION) MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 89,282 hrs · 29,258 cycles
COURIER FLOOR PANEL 221MBF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221MBF ON VTMAE TRAVELER #T21/1548304 IAW DWG SRZ- SRZ-25-005 REV R CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 89,282 hrs · 29,258 cycles
COURIER FLOOR PANEL 221BF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221BF ON VTMAE TRAVELER #T21/1548308 IAW FEDEX DWG. DWG. NO. SRZ-25-005 REV. R CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 89,282 hrs · 29,258 cycles
COURIER FLOOR PANEL 221AF DELAMINATED. FABRICATED COURIER FLOOR PANEL 221AF ON VTMAE TRAVELER #T21/1548307 IAW FEDEX DWG DWG NO. SRZ-25-005 REV R. CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 89,282 hrs · 29,258 cycles
COURIER 222AF FLOOR PANEL DELAMINATED. FABRICATED 222AF COURIER FLOOR PANEL ON VTMAE TRAVELER #T21/1548306 IAW DWG SRZ-25- SRZ-25-005 REV R, CAT "A" MAJOR REPAIR.
Part: FLOOR PANEL — DELAMINATED (ZONE 200) · airframe 89,282 hrs · 29,258 cycles
COURIER FLOOR PANEL 222MAF DELAMINATED. FABRICATED FLOOR PANEL 222MAF ON VTMAE TRAVELER #T21/1548305 IAW DWG SRZ-25-005 REV REV R CAT "A" MAJOR REPAIR.
2020
Part: UNKNOWN — MALFUNCTIONED (EXTERNAL POWER) · airframe 88,472 hrs · 28,766 cycles
DURING POWER TRANSFER ON SHUTDOWN, ALL SCREENS WENT BLANK AND LEFT ENGINE POWER WAS INCREASING WITH THE THRUST LEVER AT IDLE. BLOCK IN FUEL 10.0 CREW DEBRIEFED AND STATED EXTERNAL POWER LATCHED ON AT FIRST AND BECAME UNSTABLE, THEN STABILIZED. PERFORMED BPCU BITE REF FIM 24-20 FAULT TREE 801 FIG 101. CURRENT FAULTS 'BPCU AIR/GND SWITCH', 'UNDER VOLT TRIP', 'NO EXT POWER'. NO FAULTS ON PREVIOUS LEG. ERASED FAULTS PERFORMED BPCU OPS REF AMM 24-41-03-4. OPS CHECK GOOD WITH NO OTHER ABNORMALTIES AT THIS TIME. A/C OK TO CONTINUE FOR SERVICE.
Part: SELECTOR — FAILED · airframe 88,061 hrs · 28,520 cycles
CABIN ALTITUDE WARNING ANNUNCIATED AT CRUISE FL370. VERIFIED CABIN ALT, DON MASKS. QRH COMPLIED WITH DECENT TO 15,000. CABIN PRES STABILIZED. CLIMBED TO FL250 CABIN REMAINED STABLE. WITH OUTFLOW VALVE SHOWING FULL CLOSED, CABIN STILL CLIMBED USING AUTO1 OR AUTO2. REMOVED AND REPLACED CABIN PRESSURE SELECTOR IN REF TO AMM 21-31-01-4. TESTS GOOD. OK FOR SERVICE.
Part: VALVE — LEAKING (EQUIP COOL EXHST) · airframe 88,062 hrs · 28,521 cycles
30 MINUTES INTO FLIGHT AT FL340 EXPERIENCED "CABIN ALTITUDE" ALERT. NOTED A DIFFERENTIAL OF 6.0 WITH CABIN ALT OF 11,000. RAN QRH AND PROCEEDED TO KICT AT 10.000 FT.. MODE SELECTOR WAS IN AUTO 1 WHEN THIS OCCURED. WHILE TROUBLE SHOOTING NOW FOUND THAT THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE WILL NOT CLOSE AT ALL DURING THE PRRESURIZATION LEAK CHECK WHICH KEPT THE AIRCRAFT FROM PRESSURISING. REMOVED AND REPLACED THE MARKED BELLY DRAINS AND THE EQUIPMENT COOLING OVERBOARD EXHAUST VALVE REF B757 AMM 21-58-05-4 OPS CHECK GOOD. PERFORMED LEAK CHECK REF B757 AMM 05-51-24-2. LEAK CHECK GOOD. A/C OK FOR SERVICE.
2019
Part: STRINGER — GOUGED (FUSELAGE) · airframe 87,280 hrs · 28,068 cycles
STRINGER 1 HAS EXISTING GOUGE NEAR HILOCK COLLAR APPOX STA. 1505 AND ELONGATED FASTENER HOLE AT EXISTING HILOCK APPROX STA. 1515. CUT OUT DAMAGED SECTION OF MAIN CABIN STRINGER 1 FROM STA.1505 TO STA.1554, FABRICATED NEW STRINGER SECTION & REPAIR SPLICES 2EA, SHIMS AND INSTALLED NEW STRINGER SECTION & REPAIR PARTS AT STRINGER 1 STA. 1505 TO STA. 1554 IAW SRM 53-00-03-2R REPAIR 2 FIG.201.
2018
Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 86,919 hrs · 27,811 cycles
CABIN ALT WANING -LOSS OF PRESSURIZATION AT FL310 ON CLIMB OUT. HAD MEL 77-12-03 (N3 TACHOMETER NR 1 ENG) AND RAN QRH FOR L ENG BLEED OFF EICAS MSG. APPROX 10 MINS LATER LOSS ALL CABIN PRESS, AFTER EMERG DESCEND TO 12000 (FOR TERRAIN). I TURNED L PACK BACK ON-SOMETIMES LATER (5 MINS) CABIN PRESSURE RETURNED TO NORMAL. R/R LT ENG PRESSURE REGULATIND AND SHUTOFF VALVE ( PRSOV ) IAW AMM 36-11-09-2-1. C/W BACK PRESSURE LEAK CHECK TEST IAW AMM 36-11-00-5. NO LEAKS NOTED. C/W IDLE RUN, CHECKED BOTH LEFT AND RIGHT DUCT PRESSURES. PRESSURES WERE NORMAL. PRESSURIZED AIRCRAFT USING ONLY THE LEFT ENGINE AND THEN THE RIGHT INDEPENDENTLY PRESSURE HELD STEADY AT 4 PSI DIFF. FOR 10 MINUTES EACH SIDE. NEVER GOT EITHER LEFT OR RIGHT BLEED OFF LIGHT OR ALERT. REF. JRH AND FORM M-3615. A/C OK FOR SERVICE.
2017
Part: CONTROL UNIT — FAILED (SPOILERS) · airframe 85,987 hrs · 27,243 cycles
SPOILER ALERT ILLUMINATED ON THE EICAS AND OVERHEAD. ALL HYDRAULICS GOOD. NO ROLL OR BUFFET. PERFORMED BITE TEST OF THE SMCS AND FOUND 2R SCM FAULT ON THE LAST 2 FLIGHT LEGS IAW FIM 27-09, FT807. REMOVED AND REPLACED THE R2 SCM IAW AMM 27-09-00-2. OPS CHECKED GOOD.
Part: ACTUATOR — MISSING (GIRT BAR) · airframe 85,981 hrs · 27,237 cycles
SLIDE LIGHT ABOVE THE R1 DOOR FOUND INOPERATIVE WITH DOOR CLOSED AND SLIDE HANDLE IN ARMED POSITION. FOUND THE PROXIMITY SENSOR -A S10216. PROXIMITY ACTUATOR MISSING FROM THE GIRT BAR. INSTALLED A NEW PROXIMITY ACTUATOR. OPS CHECKED GOOD IAW AMM 25-66-11-2, AND 25-66-10-2.
Part: INDICATOR — OBSTRUCTED (DOOR SLIDE) · airframe 85,652 hrs · 27,035 cycles
ARMING INDICATION IS NOT POPPING OUT CORRECTLY. IT WAS CORRECTLY INDICATING AT PUSH BACK. BUT TOOK A FEW TRIES. FOUND THAT THE L1 DOOR ARM INDICATOR STICKER WAS SNAGGING ON THE DOOR COVER EDGE. CLEANED STICKER AND CLEANED THE OPENING EDGE ON THE DOOR LINER. OPS IAW AMM 52-11-20-5 POP OUT DOOR CHECKS GOOD AT THIS TIME. NO PARTS WERE CHANGED. ACFT OK FOR SERVICE.
Part: STIFFENER — CRACKED (RT MLG WW) · airframe 85,562 hrs · 26,979 cycles
RT WW AFT PRESSURE BULKHEAD LWR INBD STIFFENER CRACKED. REMOVED THE STIFFENER LOCATED, DRILLED NEW AND INSTALLED IAW SRM 51-40-02-0G AND SRM 51-40-05-0G.
Part: STIFFENER — CRACKED (LT MLG WW BLKHD) · airframe 85,562 hrs · 26,979 cycles
LEFT MLG WW AFT PRESSURE BULKHEAD LOWER INBD STIFFENER CRACKED. REMOVED THE STIFFENER. LOCATED, DRILLED A NEW STIFFENER AND INSTALLED IAW SRM 51-40-02-0G, AND SRM 51-40-05-0G.
Part: SKIN — DENTED (BS 520) · airframe 85,562 hrs · 26,979 cycles
FUSELAGE SKIN HAS THREE PROTUDING DENTS IN EXTERNAL SKIN LOWER FUSELAGE AT BS 520 AND TWO INCHES INBD OF STRINGER 26L. SKIN REPAIRED IAW EA F-5330-T0332752 P1.
2016
Part: MODULE — INOPERATIVE (STAB TRIM) · airframe 85,333 hrs · 26,830 cycles
DURING DECENT, AUTOPILOT FAILED TO CAPTURE ALTITUDE (5000'). ALT WARNING WORKED. R&R THE STAB TRIM ASSY MODULE, PASSES MCDP TEST 65 AS WELL AS MCDP GROUND TEST 30 AND AUTOLAND TEST 40. RESET 30 DAY TIMER, OK FOR SERVICE. IAW AMM 27-09-00-2, 22-00-00-2.
2015
Part: SWITCH — STUCK (L1 DOOR) · airframe 840 hrs · 25,975 cycles
WHILE TROUBLESHOOTING ACARS SYS, FOUND L1 DOOR SWITCH S10094 STUCK IN THE CLOSED POSITION. OPERATIONS CHECKED OK.
Part: DOUBLER — DAMAGED (APU BULKHEAD) · airframe 839 hrs · 25,861 cycles
APU FWD BULKHEAD RT SIDE HAS A DAMAGED AND GOUGED PREVIOUS REPAIR. REMOVED DAMAGE DOUBLER IAW SRM 51-40-02, FABRICATED NEW DOUBLER IAW SRM 53-80-08-2R, INSTALLED NEW DOUBLER AFT APU FWD BULKHEAD RH SIDE IAW SRM 51-40-02 AND 53-80-08-2R.
2014
Part: SLIDE RAFT — PARTIAL DEPLOY (R1 DOOR) · airframe 83,227 hrs · 25,419 cycles
AFTER DISARMING CREW ENTRY DOOR 1R SLIDE PARTIALLY DEPLOYED UPON OPENING DOOR. REMOVED AND REPLACED THE R1 DOOR SLIDE/RAFT
Part: HANDLE — LOOSE (L1 DOOR) · airframe 83,227 hrs · 25,419 cycles
L1 DOOR HANDLE PLASTIC, TOP RT IS LOOSE. SECURED THE L1 DOOR ASSIST HANDLE PER B757 AMM.
2013
Part: SKIN — CHAFED (ZONE 200) · airframe 82,270 hrs · 24,774 cycles
AFT FUSELAGE SKIN BELOW STRINGER 9L AFT OF BULKHEAD BS 1787, EXT SURFACE CHAFED BY STAB FAIRING. COMPLIED WITH EA F-5330-T0300225, CAT "A" MAJOR REPAIR.
Part: SKIN — DENTED (ZONE 20) · airframe 82,270 hrs · 24,774 cycles
FUSELAGE SKIN DENTED BS 443 AT S15R. A SKIN REPAIR WAS ACCOMPLISHED IAW EA 757 -5331-16-F4106, REV. MAJOR REPAIR
Part: SKIN — MISREPAIRED (NR 2 SLAT) · airframe 82,270 hrs · 24,774 cycles
LT WING, NR 2 SLAT COVE PANEL INBD OF OTBD DRIVE TRACK MISREPAIRED. R & R, NR 2 SLAT, INBD OF OTBD DRIVE TRACK, COVE SKIN IAW DWG 114N4026 AND INSTALLED IAW SRM 51-40-02, CAT "A" MAJOR REPAIR.
Part: STRUCTURE — DAMAGED (LT WING TE FLAP) · airframe 82,270 hrs · 24,774 cycles
OTBD FLAP LT WING BETWEEN STA 565 -600 HAS ELONGATED HOLE. A REPAIR WAS ACCOMPLISHED IAW EA 757-5753 -16 -F4116, REV-. MAJOR REPAIR.
Part: SKIN — FAILED (VERTICAL STAB) · airframe 82,270 hrs · 24,774 cycles
TWO MISDRILLED HOLES AT VERTICAL STAB LT PANEL 322DL ATTACHMENT. COMPLIED WITH EA F-5530-TO300208. MAJOR REPAIR.
Part: SKIN — CRACKED (R2 DOOR) · airframe 82,270 hrs · 24,774 cycles
R2 DOOR FWD FRAME FACE HINGE CUTOUT CRACKED A REPAIR WAS ACCOMPLISHED ON R2 DOOR FWD FRAME UPPER HINGE CUTOUT IAW EA 757-5211-16-F4100 REV, MAJOR REPAIR.
Part: SKIN — DENTED (ZONE 100) · airframe 82,270 hrs · 24,774 cycles
INCOMING EXTERNAL FUSELAGE SKIN DENTED BS 1618, BETWEEN S17-18L, REPAIRED IAW EA 757-5361-16-F4111, REV. MAJOR REPAIR.
Part: STIFFENER — GOUGED (BS 1180 BULKHEAD) · airframe 82,270 hrs · 24,774 cycles
BS 1180 BULKHEAD STIFFENER, LBL 45.57 WL 182, GOUGED. BLENDED GOUGE ON STA 1180 BULKHEAD IAW SRM 51-10-02. L= 1.25 W= .75 D= .046 ORIGINAL MATERIAL .107 OUT OF LIMITS IAW SRM 53-40-0 FIG 101, DETAIL III. R & R STIFFENER IAW SRM 51-40-02 AND DWG 144N2509.
Part: SKIN — DENTED (BS 1701-1720) · airframe 82,270 hrs · 24,774 cycles
EXTERNAL FUSELAGE SKIN BS 1701-1720 BETWEEN S28-29R DENTED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-01 FIG 101 DETAIL III. REPAIRED IAW SRM 53-00-01 FIG 201.
Part: INTERCOSTAL — CORRODED (DOOR FRAME) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
AFT CARGO DOOR FRAME BS 1380-1400 INTERCOSTAL CORRODED. REPAIRED IAW EA 757-5360-16-F4146. MAJOR REPAIR
Part: SKIN — CORRODED (NR 1 NACELLE) · airframe 82,270 hrs · 24,774 cycles
NR 1 PYLON INSIDE AREA, INBD SKIN IS CORRODED TWO PLACES. ACCOMPLISHED EA F- 5450- TO300125.
Part: SKIN — DENTED (ZONE 100) · airframe 82,270 hrs · 24,774 cycles
FUSELAGE SKIN DENTED BS 550 BETWEEN S-18R TO S-19R. A SKIN DENT REPAIR BS 540-560, STRINGER S18-20R WAS ACCOMPLISHED IAW EA 757-5331-16-F 4088, REV.
Part: SKIN — DENTED (BS 395) · airframe 82,270 hrs · 24,774 cycles
FUSELAGE SKIN DENTED BS 395 BETWEEN S-16R TO S-17R FOUND TO BE OUT OF LIMITS IAW SRM 53-00-010, FIG 101, DETAIL III. REPAIRED IAW SRM 53-00-01, REPAIR 16. MAJOR REPAIR,
Part: SKIN — CORRODED (NR 2 PYLON) · airframe 82,270 hrs · 24,774 cycles
NR 2 PYLON INTERNAL SKIN SURFACES LT SIDE FROM PPS 138 - 174, HAS SIGN OF CORROSION. REPAIRED IAW EA F-5450-T0300141. MAJOR REPAIR
Part: SKIN — CORRODED (NR 2 PYLON) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
NR 2 PYLON LEFT SKIN PANEL 443GL CUTOUT, EDGE CORRODED. REPAIRED IAW EA F-5450-T0300094. MAJOR REPAIR
Part: FRAME — DAMAGED (BS 1140) · airframe 82,270 hrs · 24,774 cycles
MAIN DECK FRAME BS 1140 HAS A DOUBLE DRILLED HOLE BETWEEN S-2R & S-3R (INCOMING CONDITION). REMOVED DAMAGED AREA OF FRAME STA 1140 BETWEEN S-2R AND S-3R IAW SRM 51-10-02, SRM 53-00-07, REPAIR 3. FABRICATED REPAIR CHANNELS AND FILLER IAW SRM 53-00-07 FIG 201 TABLE I. DRILLED AND LOCATED -1, -2, CHANNEL, AND -3 FILLER IAW SRM 51-40-05. INSTALLED REPAIR CHANNELS -1, -2, AND -3 FILLER IAW SRM 51-40-02 , AND SRM 53-00-07 REPAIR 3. MAJOR REPAIR.
Part: FRAME — DAMAGED (BS 1100) · airframe 82,270 hrs · 24,774 cycles
MAIN DECK FRAME BS 1100 HAS A DOUBLE DRILLED HOLE BETWEEN S-2R AND S-3R. REMOVED DAMAGE IAW SRM 53-00-07. REPAIR FRAME IAW SRM 53-00-07, FIG 201, REPAIR NR 3, CATEGORY "B" REPAIR LOCATED STA 1100 BETWEEN S-2-3R.
Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 82,270 hrs · 24,774 cycles
MISDRILLED HOLE AT VERTICAL STAB REAR SPAR WEB CUT-OUT FOR PANEL 324KZ. COMPLIED WITH EA F- 5530 -TO 300189. MAJOR REPAIR.
Part: SKIN — CORRODED (NR 5 SLAT) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
NR 5 SLAT OTBD AFT SIDE HAS SPOTS OF CORROSION WHERE SLAT SEAL GOES. REMOVED CORROSION IAW SRM 51-10-02. CHECK LIMITS ORIG MATERIAL .080 MATERIAL LOSS .011, FOUND OUT OF LIMITS IAW SRM 57-43-01, FIG 101, DETAIL V, PG 104. REMOVED AND INSTALLED NEW NOSE SKIN IAW SRM 51-40-02 AND DWG 149N7552, DWG 114N3002. MAJOR REPAIR.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 82,270 hrs · 24,774 cycles
RT OTBD MAIN FLAP DENT WITH LOWER SKIN DELAMINATION AND DAMAGE TO HONEYCOMB STRUCTURE FS 520. REPAIRED FLAP IAW-SRM 51-70-17, PARA 4M, BETWEEN RWS 520-530. REPAIR CAT "A" MAJOR.
Part: SKIN — CORRODED (STRUT) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
NR 1 ENG STRUT HAS CORROSION ON SKIN INSIDE STRUT AT ACCESS 433CL ACCOMPLISHED EA F-5450-165133. NACELLES/OYLONS- NR 1 PYLON OUTBD SKIN CORROSION. MAJOR REPAIR.
Part: FLOORBEAM — MISREPAIRED (BS 324) · airframe 82,270 hrs · 24,774 cycles
FLOORBEAM AT BS 324 BETWEEN BL 0 AND LBL 24 MISREPAIRED. REPAIRED IAW SRM 53-10-08, REPAIR 1, PG 207. MAJOR REPAIR.
Part: FRAME — DAMAGED (BS 1280) · airframe 82,270 hrs · 24,774 cycles
MDC FRAME INCLUDING FASTENER COLLARS AT BS1280 BETWEEN STR S10-16R HAS SEVERAL AREAS WITH NICKS AND GOUGES REMOVED DAMAGE ON FRAME AT BS1280, BETWEEN S10R-S16R IAW SRM 51-10-02. CHECKED LIMITS; SECTION OF FRAME AT S10R STA 1280 FOUND TO BE OUT OF LIMITS. REPAIRED FRAME IAW SRM 53-00-07 FUSELAGE FORMED ZEE FRAME REPAIR 757-SF FIG 201 SH. 1 & 2 REPAIR 3. CATEGORY "B". MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 755-900) · airframe 82,270 hrs · 24,774 cycles
RIGHT CREASE BEAM AT BS 755- 900 HAS SCRATCHES AND CORROSION. REMOVED CORROSION IAW SRM 51-20-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30 -13 FIG 101, DETAIL III. R & R CREASE BEAM SECTION IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 660-690) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
RT CREASEBEAM AT BS 660 -690 CORRODED. REMOVED CORROSION IAW SRM 51-10-02. FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, FIG 101, DETAIL VIII. R & R RT INBD CREASE BEAM IAW SRM 51-40-02 AND DWG 143N8322. MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 660-690) · airframe 82,270 hrs · 24,774 cycles
RT CREASE BEAM AT BS 660 -690 HAS CORROSION.
Part: CREASE BEAM — CORRODED (BS 660-690) · airframe 82,270 hrs · 24,774 cycles
RT CREASE BEAM AT BS 660 -690 HAS CORROSION.
Part: FRAME — DENTED (BS 1340) · airframe 82,270 hrs · 24,774 cycles
AFT CARGO BAY RT FRAME AT STA BS 1340 BETWEEN STRINGER 26-27R, DENTED. REMOVED FRAME IAW SRM 51-40-02. FABRICATED FRAME IAW DWG 146N1028, LOCATED AND DRILLED IAW SRM 51-40-05. INSTALLED LOWER FRAME IAW SRM 51-40-02 AND DWG 146N1008. MAJOR REPAIR.
Part: FRAME — GOUGED (BS 760) · airframe 82,270 hrs · 24,774 cycles
MAIN DECK CARGO FRAME AT BS 760, FROM STRINGER S8-S9R, GOUGED. FOUND OUT OF LIMITS IAW SRM 53-00-07, FIG 101 AD 2. REPAIRED FRAME IAW SRM 53-00-07, FIG 201, REPAIR NR 3. THIS IS A CAT 'B' REPAIR.
Part: FRAME — GOUGED (BS 780) · airframe 82,270 hrs · 24,774 cycles
MAIN DECK CARGO FRAME AT BS 780, FROM STRINGER S8-S9R, GOUGED. REPAIRED FRAME IAW SRM 53-00-07, FIG 201, REPAIR NR 3. THIS IS A CATEGORY "B" REPAIR. REPAIR LOCATED AT STA 780.
Part: STRINGER — DAMAGED (BS 1645-1670) · airframe 82,270 hrs · 24,774 cycles
STRINGER 18L AT BS 1645-1670 HAS ENLONGATED FASTENER HOLES. REMOVED AND REPLACED SRINGER IAW-SRM-51-40-02 AND DWG 146N3110, CAT."A" MAJOR REPAIR.
Part: FLOORBEAM — DAMAGED (BS 1681) · airframe 82,270 hrs · 24,774 cycles
FLOORBEAM UPPER CHORD AT STA 1681 UNDERSIDE HAS SEVERAL AREAS W/ SCRATCHES, GOUGES AND CORROSION AT RUSTED NUTPLATES AND ADJACENT FASTERNERS. REMOVED AND REPLACED FLOORBEAM IAW SRM 51-40-02 & DRAWING 146N5111. CHECKED LIMITS, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51 FIG 101 DETAIL II AND VI. MAJOR REPAIR
Part: SKIN — MISREPAIRED (BS 700-720) · airframe 82,270 hrs · 24,774 cycles
SKIN BS 700 -720, BETWEEN S23 TO 24L MISREPAIRED. REPAIRED IAW SRM 51-40-02, & 53-00-01 REPAIR NR 16, FIG 201, PAGE 201. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 1320-1540) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
SEAT TRACK, BS 1320-1540, LBL 24 CORRODED AND GOUGED. REMOVED DAMAGE IAW SRM-51-10-02, FOUND TO BE OUT OF LIMITS IAW SRM-53-00-52, R & R SEAT TRACK IAW DWG 146N5130, AND SRM-51-40-02, CAT "A" MAJOR REPAIR.
Part: SHEAR WEB — CORRODED (BS 1680-1720) · airframe 82,270 hrs · 24,774 cycles
SHEAR WEB UPPER SURFACE AT BS 1680-1720, FROM LBL 58 TO RBL 58, HAS SEVERAL AREAS OF CORROSION AROUND FASTENERS HOLES AND SEVERAL AREAS OF ELONGATED HOLES AND EVIDENCE OF WORKING RIVETS. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DT III. R & R SHEAR WEB IAW SRM 51-40-02 AND DWG 146N5336. MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
SEAT TRACK AT BS 640-780, RBL 45 HAS SEVERAL NICKS, GOUGES,AND CORROSIONS. REMOVED CORROSION IAW SRM-51-10-02, FOUND SEAT TRACK TO BE OUT OF LIMITS IAW SRM-53-00-52, DETAIL I, FIG 101. R & R SEAT TRACK IAW SRM-51-40-02 AND SRM-51-40-05. LOCATED AND DRILLED SEAT TRACK IAW SRM-51-40-05. TREATED AND PRIMED IAW-SRM-51-20-01, CAT "A" MAJOR REPAIR.
Part: SEAT TRACK — CORRODED (BS 365-418) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
SEAT TRACK SUPPORT STA 377-440 RBL 45 IS CORRODED, FOUND AFTER REMOVAL OF THE SEAT TRACK CROWN. R & R SEAT TRACK SUPPORT AT RBL 45, STA 365-418, IAW- DWG 141N5131, CAT "A" MAJOR, ALSO IAW-SRM-53-00-52, FIG 101.
Part: CREASE BEAM — CRACKED (BS 598) · airframe 82,270 hrs · 24,774 cycles
RT CREASE BEAM BS 598, HAS CRACKED AND CORRODED FASTENER HOLE VIEWED UNDERSIDE. REMOVED CORROSION IAW-SRM-53-30-13, FOUND TO BE OUT OF LIMITS IAW SRM-53-30-13, FIG 101, DETAIL V. R & R WEB IAW SRM-51-40-02, AND DWG NR 143N5520, CAT."A" MAJOR REPAIR.
Part: CREASE BEAM — DAMAGED (BS 450-665) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
RIGHT INBD CREASE BEAM AT BS450-665 HAS NICKS, SCRATCHES AND CORROSION. REMOVED DAMAGE ON INBD CREASE BEAM AT BS 450 - 665, ORIGINAL MATERIAL .070, .056. REMAINING REWORK, FOUND TO BE OUT OF LIMITS IAW SRM 53-30-13, DETAIL VIII. R & R CREASE BEAM IAW SRM 53-30-13 AND DWG 143N5520. MAJOR REPAIR.
Part: SKIN — CRACKED (NR 2 SLAT) · airframe 82,270 hrs · 24,774 cycles
NR 2 SLAT CONE SKIN CRACKED AT INBD MAIN TRACK. REMOVED COVE SKINS IAW SRM 51-40-2. INSTALLED NEW COVE SKINS IAW SRM 51-40-2 AND DWG 114N4076. MAJOR REPAIR.
Part: SKIN — CRACKED (RT WING) · airframe 82,270 hrs · 24,774 cycles
NR 8 SLAT COVE SKIN CRACKED AT OTBD MAIN TRACK. REMOVED NR 8 SLAT COVE SKIN IAW SRM 51-40-02. ROUTED TO FAB SHOP. FABRICATED NEW COVE SKIN ON STAM TRAVELER NR T12/976166. LOCATED AND DRILLED COVE SKIN IAW SRM 51-40-02. TREATED AND PRIMED IAW SRM 51-20-01. INSTALLED COVE SKIN IAW SRM 51-40-02. MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 1180-1290) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
RT CREASE BEAM BS 1180-1290 HAS SCRATCHES AND AREAS WITH CORROSION, TOP AND UNDERSIDE AROUND FASTENER HOLES. BLENDED AREA IAW-SRM-51-10-02, FOUND OUT OF LIMITS IAW-SRM-53-60-13, DETAIL VIII, FIG 101. R & R IAW DWG D634N201 CAT "A" MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 1405-1630) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
RT INDB CHORD CREASE BEAM AT STA 1405-1630 HAS SCRATCHES AND AREAS W/ CORROSION, TOP & UNDERSIDE, AROUND FASTENER HOLES. REMOVED CORROSION IAW SRM 51-10-02. FOUND OUT OF LIMITS IAW SRM 53-60-13, DETAIL II, FIG 101. FABRICATED NEW CREASE BEAM IAW DWG 146N5590. INSTALLED CREASE BEAM IAW SRM 51-40-02 AND DWG 146N5590, STA 1405-1630 RT. MAJOR REPAIR.
2012
Part: FLOORBEAM — GOUGED (BS 365.23) · airframe 82,270 hrs · 24,774 cycles
CABIN FLOORBEAM, BS 365.23 UPPER TEE GOUGED AT FASTENER HOLES. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101 DETAIL 3. R & R FLOORBEAM IAW DWG 141N5112 & SRM 51-40-02.
Part: FLOORBEAM — CORRODED (BS 377.7) · airframe 82,270 hrs · 24,774 cycles
CABIN FLOORBEAM BS 377.7 UPPER TEE CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL 3. R & R FLOORBEAM AT STA 377.7 IAW BAC DWG 141N5113 AND SRM51-40-02. CLASSIFIED MAJOR REPAIR.
Part: BEAM — CORRODED (BS 345) · airframe 82,270 hrs · 24,774 cycles
CABIN BEAM BS 345, CORRODED. R & R FLOORBEAM IAW SRM 51-40-02 AND DWG 141N5111. OUT OF LIMITS IAW SRM 53-00 -51. MAJOR REPAIR.
Part: CREASE BEAM — CORRODED (BS 1600-1620) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
RIGHT CREASE BEAM WEB AT BS 1600-1620 HAS CORRISION TOP AND UNDERSIDE. REMOVED CORROSION IAW-SRM-51-10-02 FOUND TO BE OUT OF LIMITS, FABRICATED IAW DWG 146N8722. LOCATED AND DRILLED IAW-SRM-51-40-05, INSTALLED IAW-SRM-51-40-02. CAT."A" MAJOR REPAIR.
Part: SKIN — CRACKED (RT WING) · airframe 82,270 hrs · 24,774 cycles
NR 9 SLAT COVE SKIN CRACKED AT OTBD MAIN TRACK. R & R COVE SKIN IAW SRM 57-43-01 AND SRM 51-40-02. FABRICATED NEW SKIN. MAJOR REPAIR.
Part: WEB — DAMAGED (BS 365-377) · airframe 82,270 hrs · 24,774 cycles
RIGHT CREASE WEB, UNDERSIDE, AT BS 365 TO BS 377 HAS ENLONGATED HOLE.
Part: FLOORBEAM — DAMAGED (BS 1640) · airframe 82,270 hrs · 24,774 cycles
FLOORBEAM AT STA 1640 UPPER CHORD HAS SEVERAL GOUGES, SCRATCHES, AND CORROSION. R & R FLOORBEAM STA 1640 IAW SRM 51-40-02 AND DWG 146N5111. CHECKED LIMITS FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51, FIG 101, DETAIL II AND VI. MAJOR REPAIR.
Part: FLOORBEAM — CORRODED (BS 1661) · corrosion level 2 · airframe 82,270 hrs · 24,774 cycles
FLOORBEAM AT BS 1661 UPPER TEE TOP AND UNDERSIDE HAS SEVERAL AREAS WITH SCRATCHES, GOUGES, AND CORROSION. R & R FLOORBEAM IAW SRM 51-40-01 AND DWG 146N5090-16. MAJOR REPAIR.
Part: CARGO TRACK — DAMAGED (BS 1540-1640) · airframe 82,270 hrs · 24,774 cycles
MAIN DECK CARGO TRACK AT BS 1540-1640, RBL 45 HAS AREAS WITH SCRATCHES, GOUGES, AND CORROSION. CHECKED LIMITS, SEAT TRACK FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52, FIG 101 DETAIL I. R & R SEAT TRACK IAW SRM 51-40-02 AND DWG 146N5120. MAJOR REPAIR.