N218FR
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.
61 reports on file, 2013-07-13 – 2018-03-19.
Part: WINDOW FRAME — DAMAGED (COCKPIT) · airframe 52,395 hrs · 19,956 cycles
CAPTAIN'S SLIDING WINDOW FRAME DAMAGED NEAR RELEASE LEVER. REPAIRED THE SLIDING WINDOW FRAME TRACK IAW EA RES 13652, AMM 25-13-41-00-001-A, 25-00-00-330-02, 56-12-11-010-001-A, SRM 51-73-00, 51-75-12, 51-42-11, NTM 51-10-01, 51-10-08, AND EA A2-56R34167.
Part: STRINGER — CORRODED (FRAME 58) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT CARGO STRINGER 32 AT FR 58 HAS CORROSION. REPAIRED THE STRINGER IAW EA 13597, SRM 53-21-13, 51-42-11, 51-10-01, AND 51-73-00.
Part: THRESHOLD — CORRODED (R1 DOOR) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
GIRT BAR FITTING ATTACH HOLES ON THRESHOLD ARE CORRODED AT THE R1 DOOR. REMOVED AND REPLACED R1 DOOR THRESHOLD IAW SRM 51-72-11, 51-42-11, 53-11-14, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 20) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
L1 DOOR AREA AT FRAME 20, UPPER FLOORBEAM CORRODED AT Y1732. CLEANED & EVALUATED THE FLOORBEAM, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14. REMOVED AND REPLACED THE DAMAGED FLOORBEAM IAW SRM 51-44-11, & 51-42-11.
Part: FLOORBEAM — CORRODED (FRAME 14) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
RIGHT FWD CABIN AT FRAME 14 CENTER FLOORBEAM BETWEEN Y254 AND -Y254 CORRODED ON THE TOP SURFACE. BLENDED THE DAMAGED AREA, FOUND TO BE OUT OF LIMITS IAW SRM 53-11-14, FIG 01. REMOVED AND REPLACED THE FLOORBEAM IAW 51-42-11.
Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
FWD CABIN FLOOR SUPPORT AT FRAME 14, Y503 HAS CORROSION ALONG ATTACHMENT HOLES. FOUND TO BE OUT OF LIMITS & REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, SRM 51-44-11, SRM 51-21-11 AND SRM 53-11-14 FROM FRAMES 14 TO 16.
Part: DOOR SILL — CORRODED (FRAMES 16-20) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
L1 DOOR SILL, FRAMES 16 TO 20, CORRODED AROUND ATTACHMENT HOLES. REPAIRED THE DOOR SILL IAW SRM 53-11-14-283-005, SRM 51-21-11, 51-23-11, 51-42-11, NTM 51-10-01, AMM 52-11-21-000-001-A, AND 52-11-00-820-001-A.
Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
FWD CABIN FLOOR SUPPORT AT FRAME 14, Y765 HAS CORROSION ALONG THE ATTACHMENT HOLES. . REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 12 - 26 IAW SRM 51-72-11, SRM 53-11-14, AND SRM 51-21-11.
Part: FLOORBEAM — CORRODED (FRAME 16) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
L1 DOOR AREA, AT FRAME 16 UPPER FLOORBEAM CORRODED AT Y1732. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, AND SRM 53-11-14.
Part: FLOOR SUPPORT — CORRODED (FRAME 14) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
CABIN RT SIDE AT FRAME 14 BETWEEN Y254 AND -Y254, FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 12 TO 16 IAW SRM 51-72-11, SRM 51-44-11, AND SRM 53-11--14-283-003.
Part: FLOOR SUPPORT — CORRODED (FRAMES 68-69) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT -Y1292 CORRODED BETWEEN FRAMES 68 - 69. REMOVED AND REPLACED THE FLOOR SUPPORT IAW 51-72-11, 51-74-00, AND 53-41-14-283-001.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT -Y1292 CORRODED, FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 51-74-00, AND SRM 53-00-14-283-002.
Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT Y765 WAS FOUND CORRODED AT FRAME 66. FOUND TO BE OUT OF LIMITS. REMOVED AND REPLACED THE FLOOR SUPPORT BETWEEN FRAMES 66-70 IAW SRM 51-72-11, 51-44-11, AND 53-41-14-283-001.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOORBEAM -Y254 CORRODED AT FRAME 68-70. REMOVED FLOORBEAM AFT -Y254 FRAME 68-70 AND REPLACED IAW SRM 51-72-11-911-001.
Part: FLOOR SUPPORT — CORRODED (FRAME 66) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT CORRODED OTBD OF Y765, FRAME 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND SRM 53-41-14-283-001.
Part: FLOOR SUPPORT — CORRODED (AFT) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT CORRODED -Y512 AROUND F/A SEAT MOUNT. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, 53-00-14-283-002, AND 51-44-11.
Part: FLOOR SUPPORT — CORRODED (NOT REPORTED) · corrosion level 2 · airframe 52,395 hrs · 19,956 cycles
AFT WET AREA FLOOR SUPPORT CORRODED -Y512 AROUND F/A SEAT MOUNT. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, SRM 53-00-14-283-002, AND SRM 51-44-11.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 52,395 hrs · 19,956 cycles
LEFT AFT EMERGENCY EXIT DOOR HAS INDICATIONS OF A CRACK AT MULTIPLE RIVETS LOCATIONS AND FWD INBD FRAME. REMOVED AND REPLACED THE LT AFT EMERGENCY DOOR FWD INBD FRAME IAW SRM 51-42-11, AND SRM 51-72-11. REMOVED AND REPLACED THE LT AFT EMERGENCY EXIT DOOR WINDOW IAW AMM 56-31-17.
Part: FRAME — CRACKED (DOOR) · airframe 52,395 hrs · 19,956 cycles
RIGHT FWD DOOR HAS INDICATIONS OF CRACKS, AFT INBD FRAME. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-42-11, 56-31-17, 51-72-11, 51-21-11, AND 51-75-12.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 52,395 hrs · 19,956 cycles
LEFT AFT EMERGENCY EXIT DOOR HAS INDICATIONS OF CRACKS AT MULTIPLE RIVET LOCATIONS ON THE AFT INBD FRAME. REMOVED AND REPLACED THE LT AFT DOOR FRAME IAW SRM 51-72-11, AND 51-42-11.
Part: DOOR FRAME — CRACKED (EMERGENCY EXIT) · airframe 52,395 hrs · 19,956 cycles
RIGHT AFT EMERGENCY EXIT DOOR HAS INDICATIONS OF CRACKS ON AFT INBD FRAME. REMOVED AND REPLACED THE DOOR FRAME IAW SRM 51-42-11, AND SRM 51-72-11.
Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 52,395 hrs · 19,956 cycles
LEFT AFT EMERGENCY EXIT DOOR HAS INDICATIONS OF CRACKS AT MULTIPLE LOCATIONS OF THE FWD INBD FRAME. REMOVED AND REPLACED THE LT EMERGENCY EXIT DOOR FRAME IAW SRM 51-42-11, 51-72-11, 51-21-11, AND 51-75-12. REMOVED AND INSTALLED RT AFT EMERGENCY EXIT DOOR WINDOW IAW AMM 56-31-17.
Part: FRAME — CRACKED (EMERGENCY EXIT) · airframe 52,395 hrs · 19,956 cycles
LEFT AFT EMERGENCY EXIT DOOR HAS INDICATION OF CRACKS AT MULTIPLE RIVET LOCATIONS ON AFT INBD FRAME. REMOVED AND REPLACED THE FRAME IAW SRM 51-42-11, AND SRM 51-72-11.
Earlier reports · 2013–2017 · 38 reports
2017
Part: BLOWER — SEIZED · airframe 51,503 hrs · 19,608 cycles
BLOWER FAULT ENROUTE WITH ASSOCIATED WITH STRONG ELECTRICAL SMOKE ODOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,453 hrs · 19,585 cycles
RT OVERWING EMERGENCY EXIT LIGHT WILL NOT ILLUMINATE. AIRCRAFT CONSIDERED AOG. REMOVED AND REPLACED RT OVERWING EMERGENCY LIGHT ASSY IAW AMM 33-51-15 PB401. OPS CHECK GOOD PER AMM TASK 33-51-00-710-001-A. AIRCRAFT OKAY FOR CONTINUED SERVICE.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 51,320 hrs · 19,529 cycles
CCR EXIT LIGHT SIGN INOPERATIVE. REMOVED AND REPLACED THE BULBS IAW AMM 33-51-16, PB401 AND OPS CHECKED GOOD. AIRCRAFT WAS RETURNED TO SERVICE.
Part: A/C PACK — MALFUNCTIONED (NR 1) · airframe 49,506 hrs · 18,843 cycles
NR 1 A/C PACK , OVERHEATT FOLLOWED BY FUMES IN THE CABIN. OPEN
Part: HMU — SHUTDOWN (ZONE 500) · airframe 49,375 hrs · 18,793 cycles
ENG 1 FAILED, RESTART DURING DESCENT. PERFORMED FADEC OPERATIONAL TEST IAW AMM 73-29-00-710-040B TEST FAILED FOUND J8 & HMU (FMVRES) ECU FAULT. DUE TO TEST FAILED AIRCRAFT REQUIRES HMU CHANGE. REMOVED AND REPLACED HYDROMECHANICAL UNIT FIN 4000KC1 IAW AMM 73-21-10 PB 401. OPS CHECK GOOD, LEAK CHECK BAD, FOUND FUEL FLOW TRANSMITTER LEAKING DURING LEAK CHECK. REMOVED AND REPLACED NR 1 ENG FUEL FLOW TRANSMITTER AND PERFORMED IDLE ENGINE RUN NO LEAKS WERE NOTED IAW AMM 73-31-10 PB 401. OK FOR SERVICE.
Part: FLOOR SUPPORT — CORRODED (FRAMES 65-67) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
AFT LAVATORY FLOOR SUPPORT HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT, BETWEEN FRAMES 65 AND 67 IAW SRM 51-72-11, 53-00-14-283-002, AND 51-72-11-911-001.
Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
RIGHT CABIN FLOOR SUPPORT -Y765 HAS CORROSION BETWEEN FRAMES 64 - 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11, AND 53-00-14.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
FLOOR SUPPORT -Y464 AT FRAMES 66 - 68 HAS CORROSION. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001.
Part: FLOOR SUPPORT — CORRODED (FRAMES 64-66) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
RT FLOOR SUPPORT -Y1292 HAS CORROSION BETWEEN FRAMES 64 - 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 53-00-14.
Part: FLOOR SUPPORT — CORRODED (FRAMES 65-66) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
CABIN FLOOR SUPPORT Y1292 HAS CORROSION BETWEEN FRAMES 65 - 66. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, 53-00-14-283-002, AND 51-72-11-911-001.
Part: FLOORBEAM — CORRODED (FRAME 66) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
FLOORBEAM Y464 AT FRAME 66 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 53-00-14-283-002, 51-72-11-911-001, 51-51-11, 51-42-11, AND 51-44-11.
Part: FLOORBEAM — CORRODED (FRAME 68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
FLOORBEAM Y765 AT FR68 HAS CORROSION. REMOVED AND REPLACED THE FLOORBEAM IAW SRM 51-42-11, 51-44-11, 51-72-11, AND 53-00-14.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
RT FLOOR SUPPORT -Y765 CORRODED ON THE TOP SURFACE BETWEEN FRAMES 66-68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-42-11, AND 51-72-11-911-001.
Part: FLOOR SUPPORT — CORRODED (FRAME 68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
LEFT FLOOR SUPPORT Y1292 CORRODED TOP SURFACE AT FRAME 68. REMOVED AND REPLACED THE FLOOR SUPPORT FROM FRAMES 68 - 69 IAW SRM 51-72-11-911-001, AND 53-00-14.
Part: FLOOR SUPPORT — CRACKED (FRAME 66) · airframe 49,081 hrs · 18,681 cycles
LT FRAME 66 FLOOR SUPPORT CRACKED BELOW DOOR SILL. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-75-12, AND SRM 51-44-11, SRM 51-42-11./END/
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
LEFT FLOOR SUPPORT Y1292 CORRODED THE TOP SURFACE AT FRAMES 66 - 68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-72-11-911-001, AND 53-00-14.
Part: FLOOR SUPPORT — CORRODED (FRAMES 66-68) · corrosion level 2 · airframe 49,081 hrs · 18,681 cycles
FLOOR SUPPORT Y254 CORRODED ON TOP SURFACE, FRAMES 66-68. REMOVED AND REPLACED THE FLOOR SUPPORT IAW SRM 51-75-12, SRM 51-72-11, SRM 51-44-11, SRM 51-42-11, AND SRM 53-00-14.
2015
Part: TRAY — CRACKED (PAX DOOR) · corrosion level 2 · airframe 42,212 hrs · 15,969 cycles
C 7 CHECK. MAIN CABIN FLOOR TRAY CRACKED AT FRAME 68, Y1292. REMOVED CRACKED FLOOR TRAY AT FRAME 68, Y1292. INSTALLED NEW TRAY PN D5348002069601 IAW SRM 51-42-11 PAR 6 B PAR7 B PAR 13 D. ACFT DUE OUT OF C CHECK 7 28 2015 NON-ROUTINE 27087.
Part: TRAY — CRACKED (PAX DOOR) · corrosion level 2 · airframe 42,212 hrs · 15,969 cycles
C 7 CHECK. MAIN CABIN FLOOR TRAY CRACKED AT FRAME 68, -Y1292. REMOVED CRACKED FLOOR TRAY AT FRAME 68, -Y1292. INSTALLED NEW TRAY PN D5348002069601 IAW SRM 51-42-11, PAR 6 B PAR 7 B PAR 13 D. AIRCRAFT DUE OUT OF C CHECK 7 28 2015 NON-ROUTINE 27088.
Part: SHEAR PLATE — CORRODED (FRAMES 69-70) · corrosion level 2 · airframe 42,212 hrs · 15,969 cycles
AIRCRAFT DUE C 7 CHECK. MAIN CABIN AFT GALLEY FLOOR, LEFT SHEAR PLATE HAS CORROSION. MAIN CABIN AFT GALLEY FLOOR, LEFT SHEAR PLATE R & R IAW EO A0-53EO-31434 & SRM 51-42-11, PAR 6 B, PAR 7 B, PAR 13 D. AIRCRAFT DUE OUT OF C CHECK 7 28 2015 NON-ROUTINE 27541.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 40,837 hrs · 15,420 cycles
DISCREPANCY, EMER LIGHT TEST FAILS, EPSU INT LOAD FWD LT. RE-SEATED CONNECTOR 10WL-A ON EPSU 10WL IAW AMM 33-51-38. OPERATIONS CHECKED NORMAL IAW AMM AMM 33-51-00.
Part: PIN — DISPLACED (ZONE 200) · airframe 40,837 hrs · 15,420 cycles
DISCREPANCY, 108VU PANEL SHORTED, EXT POWER AVAIL LIGHT & ELT LIGHT DIMLY LIT WITH NO EXT POWER SOURCE. WHEN ELT WAS TESTED SMOKE CAME FROM ELT CONTROL PANEL & PANEL 108VU. RE-INSERTED PINS 1B & 3B THAT WERE FOUND DISPLACED FROM LIGHT TEST P PSW 34LP. REPLACED ELT RCP ELT INDICATOR LIGHT & DIODE BLOCK 1191VD. OPERATIONS CHECKED NORMAL IAW AMM 25-65-00 & AMM 33-14-00.
2014
Part: HORN — DEFECTIVE (COCKPIT DOOR) · airframe 37,578 hrs · 13,955 cycles
SMELL OF BURNING PLASTIC 10 MINUTES PRIOR TO LANDING. PERFORMED INSPECTION OF ALL AVIONICS COMPARTMENTS NO TROUBLES NOTED. SUSPECT SMELL COMING FROM COCKPIT DOOR LOCKING SYS BUZZER. R & R BUZZER 23MQ OPERATIONS TESTED GOOD, NO TROUBLES NOTED IAW AMM 52-51-13-000-001-A.
2013
Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 35,742 hrs · 13,176 cycles
CABIN HIGH ALTITUDE WARNING AT 9,999 FT, COMPLETED RAPID DESCENT TO 9,000 FT. SWITCHED SYS TO MANUAL AND THAN BACK TO AUTO. NR 2 SYS RETURNED TO NORMAL. TROUBLESHOT IAW SRM TSM 21-31-00-810-827. REPLACED CPC 1 AND CPC 2 REF AMM 21-31-34 PB 40. OPS CHECK NORMAL.
Part: SKIN — DENTED (ZONE 100) · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. DENT ON FUSELAGE BETWEEN FR 10 - 11 ABOVE STRINGER 25L WITHIN LIMITS IAW SRM 53-11-11, FIG 105, DIAGRAM 103. DETAILED VISUAL INSPECTION SHOWED NO DEFECTS NOTED. INSTALLED PERMANENT REPAIR IAW SRM 53-11-11, PB201, PARA J, FIG 212.
Part: WEB — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOOR WEB LOCATED BY R1 DOOR, FR 20 CORRODED OUT OF LIMITS. R & R WEB IAW SRM 51-42-11 AND SRM 51-42-11.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOORBEAM Y1292, FR20 HAS MINOR CORROSION. REMOVED CORROSION IAW SRM 51-74-00, STEP 5, PAR(3). FOUND TO BE WITHIN LIMITS, IAW SRM 53-11-14, FIG 105. TREATED AND PRIMED.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 INSPECTION. MAIN CABIN FLOORBEAM HAS CORROSION AT FR66, -Y1732. REPAIRED IAW SRM 53-41-14, PB101, FIG 101, SHEET 1, SRM 53-41-14 PB201 AND SRM 53-41-14 PB201, FIGURE 201, SHEET 4.
Part: STRUCTURE — DAMAGED (RT ELEVATOR) · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. RT ELEVATOR THERMOGRAPHIC INSPECTION REVEALED INDICATIONS ON BOTH UPPER AND LOWER PANELS IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00 PB201, PARA. 2.A.(1)(A-C), 2.A.(2)(A-J), 2.B.(2)(A)1-1O FIGURE 204-205 AND SRM 55-21-11 PB201, PARA. 5.D.(2)(B)1 PARA.5.D(2)(D)1-6, 5.D.(2)(E), 5.E.(2)(F)1-6, 5.E.(2)(G) AND CMM 55-21-45-210-010-G01, PARA. A.(1-9)
Part: STRUCTURE — DAMAGED (LT ELEVATOR) · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. LEFT ELEVATOR THERMOGRAPHIC INSPECTION REVEALED INDICATIONS ON UPPER PANEL IRREGULAR IN SHAPE AND BLACK IN COLOR. REPAIRED IAW SRM 55-20-00 PB201, PARA 2.A.(1-2), 2.B.(1), 2.B.(2)(A)1-10 AND SRM 55-21-11 PB201, PARAGRAPH 5.E.(2)(B)1 FIGURE 205, PARAGRAPH 5.E.(2)(F)1-6, 5.E.(2)(G) AND CMM 55-21-45-210-010-G01, PARAGRAPH A.(1-9)
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOORBEAM Y254 HAS CORROSION AT FRAME 19. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 AND 7.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
ACFT IS OUT OF SERVICE DUE TO C6/S2 CHECK. FLOOR SUPPORT -Y254 HAS CORROSION FROM FR18 - 20. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5 AND 7.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOOR SUPPORT Y765 HAS CORROSION AT FRAME 66. R & R FLOOR SUPPORT IAW SRM 51-42-11 PARA 5 AND 7.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
ACFT OUT OF SERVICE DUE TO C6/S2 CHECK. FLOOR SUPPORT APPROX 6" FWD OF THE R2 DOOR HAS CORROSION. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5 A-C AND 7 BD.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
ACFT IS OUT OF SERVICE DUE TO C6/S2 CHECK. FLOOR SUPPORT Y765 HAS CORROSION AT FR16. R & R FLOOR SUPPORT IAW SRM 51-42-11, PARA 5 AND 7.
Part: FLOOR SUPPORT — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOOR SUPPORT Y1292 HAS CORROSION AT FRAME 66. R & R FLOOR SUPPORT IAW SRM 53-00-14-PB101, FIG 102 AND SRM 51-42-11, PARA 7.
Part: FLOORBEAM — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. FLOORBEAM BETWEEN FLOOR SUPPORTS Y254 AND -Y254 AT FRAME 15 HAS CORROSION. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5.A.-C. AND 7.B.D.
Part: SEAT TRACK — CORRODED (ZONE 200) · corrosion level 2 · airframe 35,134 hrs · 12,924 cycles
DURING C6/S2 CHECK. PASSENGER CABIN, THE SEAT TRACK HAS CORROSION AT THE NUT CLIP FASTENER HOLES ON UPPER SURFACE OF SEAT TRACK AT BS 8433/FR21 AND AT -Y1292. R & R FLOORBEAM IAW SRM 51-42-11, PARA 5 A -C AND 7 BD.