N908UP
Registered owner: RYAN AIR LLC, NY (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| CIRCADIAN AVIATION LLC (O2GA) | Certificate holder | — | Matched by certificate designator |
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
IN CRUISE FLIGHT AT FL430, 'A' HYDRAULIC SYSTEM INDICATOR WENT TO ZERO QUANTITY. CREW RAN THE APPROPRIATE CHECKLISTS AND MADE AN EMERGENCY LANDING INTO KSDF. LANDING WAS UNEVENTFUL. MAINTENANCE TROUBLESHOT THE DISCREPANCY TO A DEFECTIVE LEFT ENGINE HYDRAULIC PUMP PULSATION DAMPENER O-RING. O-RING REPLACED, N2 BOTTLE SERVICED, SYSTEM BLED AND GEAR SWINGS WERE PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
DURING CLIMB AT APPROXIMATELY 30,000 FEET THE BAGGAGE SMOKE WARNING LIGHT ILLUMINATED. FOLLOWED CHECKLIST, EMERGENCY DECLARED, AND DIVERTED TO THE KSMF. LANDING WAS UNEVENTFUL. INSPECTION OF THE BAGGAGE COMPARTMENT SHOWED NO EVIDENCE OF SMOKE OR FIRE. THE WARNING LIGHT REMAIN ILLUMINATED. MAINTENANCE REPLACED THE BAGGAGE COMPARTMENT SMOKE DETECTOR. A SUCCESSFUL OPERATIONAL CHECK FLIGHT WAS PERFORMED WITH NO DEFECTS NOTED. AIRCRAFT WAS RETURNED TO SERVICE.
INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE.
INSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2
INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURES
INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIRED IAW SRM.
INSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLACED IAW DWG 65-16350
INSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRM
INSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRM
INSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INSTALLED PER SRM
INSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3
INSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM.
INSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM.
INSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRM
INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM.
INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
INSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611B
INSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2
INSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417
INSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRM
INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRM
INSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509
INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRM
EMERG EXIT LIGHT INOP. REPLACED BULB OP CHECKS GOOD
INSPECTION TYPE:AS-E INFLIGHT, EMERGENCY EXIT LIGHTS ILLUMINATED FOR APPROX 2 MINUTES, THEN EXTINGUISHED. SWITCH WAS CHECKED TO BE IN ARMED THE ENTIRE TIME. UNABLE TO DUPLICATE PROBLEM. TESTED NORMAL PER MM 33-50-101.
INSPECTION TYPE:N/A, LT OUTBOARD AILERON HAS DELAMINATION AND .25 INCH CRACK AILERON REMOVED WD 66470 INSTALLED LT OUTBOARD AILERON TO STEP D (4) MM 27-10-31. OK FOR SERVICE.
INSPECTION TYPE:N/A EMERGENCY LIGHT AT ENTRY DOOR INOP LIGHT SWITCH LEFT ON. REPLACED BATTERIES. OPS CK OK
INSPECTION TYPE:N/A DURING APPROACH INTO SDF FLAP EXTENSION OTBD FLAPS EXTENDED ASYMETRI CALLY RT AT APROX 1 DEG AND LT APROX 5 DEGS. RAN APPROPRIATE CK LIST AND LANDED. ***SUPPLEMENTAL*** REMOVED & REPLACED OTBD FLAP POS XMTR. CYCLED FLA P THRU FULL RANGE. OPS CKD GOOD. MX REF 27-52-13.
INSPECTION TYPE:N/A, OUTBOARD FLAPS VERY SLOW TO RETRACT OUT OF CAE WOULD NOT EXTEND PAST 15 DEGREES AT ROA WITH NORMAL HYD FLAPS OPERATED NORMAL INTO CAE. A/C DID NOT LAND AT ROA, AIR TURNBACK TO CAE. REPAIRS IN PROGRESS AT CAE.
INSPECTION TYPE:C&SI, STR 24R BETWEEN BS 360 AND BS 259.5 IS CORRODED AT BS 277 AND END OF STRINGER AT BS 360 HAS CRACK FROM PREVIOUS STOP DRILL HOLE. STRINGER INSTALLED IAW BOEING DRG 65-18420.
INSPECTION TYPE:C&SI, CORROSION ON SKIN BETWEEN BS 1080 AND BS 1183 STRINGER 4 RT TO STRINGER 10 RT. SKIN REMOVED IAW SRM 51-30-2. NEW SKIN DRILLED AND TRIMMED IAW SRM 51-30-2 AND DRG 65-18382. NEW SKIN INSTALLED IAW DRG 65-18382 AND SRM 51-30-2 AND 51-30-3
INSPECTION TYPE:C&SI, CONTROL CABIN ENTRY DOOR SILL, STA 303.9, EVIDENCE OF CORROSION ON DOOR SILL BOTH UPPER AND LWR SURFACES AND BRACKET ON RT SIDE OF SILL CORRODED. CORROSION REMOVED IAW SRM 51-10-06, CORROSION FOUND TO BE WITHIN LIMITS OF SR 53-10-1 MAX DEPTH. REMOVED 0.002 AREA REPROTECTED IAW SRM 51-10-02, HINGE BRACKET ON LWR AREA REPLACED IAW SRM 51-30-2
INSPECTION TYPE:C&SI, CRACK ON ATTACH LUG OF FLAP POSITION TRANSMITTER HOUSING LEFT I/B FLAP CORRODED DRUM CRACKED HOUSING REPLACED IAW OHM 27-54-06.
INSPECTION TYPE:C&SI, NR 3 SLAT, O/B SLAT TRACK, O/B RIB ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED OUT AS PER SRM 51-40-2.
INSPECTION TYPE:C&SI, CRACK ON SHEAR TIE CLIP BETWEEN STIFEFNER AND UPPER CHORD AT FWD WALL OF CENTER TANK BS 740 AT LBL 45.61. CHANGED SHEAR TIE CLIP IAW EO B727-5710-4595.
INSPECTION TYPE:C&SI, ENGINE NR 1 THROTTLE SHUT OFF CONTROL BRACKET ASSY IN FWD END OF PYLON IS CRACKED. BRACKET REPLACED IAW MM 76-11-21.
INSPECTION TYPE:C&SI, ULTRASONIC INSPECTION OF HORIZ STAB HINGE LUGS (ON VERT STAB) LT AND RT, I/B AND O/B DUE SUSPECT INDICATION FROM HFEC INSPECTION. ULTRASONIC INSPECTION CARRIED OUT BOTH LEFT AND RIGHT BORES REPAIRED IAW UPS EO B727-5510-2284.
INSPECTION TYPE:C&SI, FWD CARGO LEFT FLOOR TRACK UPPER SURFACE CORRODED AT BS 482 ALSO CORROSION EVIDENT ADJACENT ANCHOR NUTS LWR SURFACE BS 480 - BS 540. FWD CARGO BAY LEFT FLOOR TRACK REPLACED FROM BS 480 TO 680 IAW SRM 51-30-2, 7 SRM 53-10-5 FIG 8.
INSPECTION TYPE:C&SI, SUSPECT CORROSION ON LAP JOINT AT BS 300 TO BS 320 STRINGER 24 RT. LAP REPAIRED IAW EO B727-5330-0509 AND SRM 53-30-15A.
INSPECTION TYPE:C&SI, CRACK INDICATION FOUND AT BS 740 FWD LWR HOLE IN LINE WITH STR 16R. REPAIR CARRIED OUT IAW SMRO EO 2000-04-008 UPS ENGINEERING FILE NO 727-53-2231.
INSPECTION TYPE:C&SI, CORROSION ON WING CENTER SECTION UPPER SKIN AT BS 865 LBL 65.5. REPAIR CARRIED OUT IAW SMRO EO 200-004-004 UPS ENGINEERING FILE NR 727-57-2145.
INSPECTION TYPE:C&SI, ON INSPECTION OF ENG NR 3 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
INSPECTION TYPE:C&SI , ON INSPECTION OF ENG NR 1 MOUNT HOLES CORROSION FOUND IN ALL HOLES. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
INSPECTION TYPE:C&SI NR 4 FLAP TRACK CORROSION ON FACES OF FWD SUPPORT LUGS. REPAIR CARRIED OUT IAW SMRO EO 2000-004-10 UPS ENGINEERING FILE NR 727-57-2147.
INSPECTION TYPE:C&SI, CORROSION ON SEAT TRACK UPPER FLANGE I/B AT BS 740 RBL 24.75. CORROSION REMOVED, LIMITS CHECKED AND FOUND OUTSIDE REF SRM 51-10-6. REPAIR CARRIED OUT IAW SRM 53-10-5.
INSPECTION TYPE:C&SI, NR 2 SLAT, I/B TRACK ATTACH POINT HAS SUSPECT CRACK. REPAIR CARRIED IAW SRM 51-40-2.
INSPECTION TYPE:C&SI, FLAP CARRIAGE NR 2 PITTING CORROSION IN BORE OF SPINDLE. CARRIAGE REPLACED IAW OHM 57-52-11..
INSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140 BETWEEN STR 3R AND STR 4R. REPAIR CARRIED OUT IAW B727 NDM PT6 51-00-00 FIG 4 AND 5.
INSPECTION TYPE:C&SI, SUSPECT CORROSION BETWEEN SKIN AND DOUBLER AT BS 1120 - BS 1140, BETWEEN STR 3R AND 4R. REPAIR CARRIED OUT IAW SRM 51-00-00.
INSPECTION TYPE:C&SI, SUSPECT CRACK ON MAIN CARGO DOOR SILL SKIN LWR SURFACE AT BS 488. MAIN CARGO DOOR SILL SKIN REPAIRED IAW SRM 51-40-2 FIG 1.
INSPECTION TYPE:C&SI, LEFT WING REAR SPAR TO BODY BOTTLE PIN HAS PITTING CORROSION ON FLANGE THAT SITS AGAINST SPAR TO BODY FITTING. BOTTLE PIN REPLACED IAW MM 57-41-01.
INSPECTION TYPE:C&SI, AFT CARGO BAY FLOOR SUPPORT CRACKED AT BS 1070 RBL 12. AFT CARGO BAY FLOOR SUPPORT BEAM REPLACED IAW SRM 53-10-5.
INSPECTION TYPE:C&SI RT BS 740 FITTING CRACKED BEYOND LIMITS. RT BS 740 FITTING REPLACED IAW EO B727-5310-7477-E.
EMERGENCY EXIT LIGHT IN COCKPIT AND MAIN ENTRY DOOR INDICATE LOW BATTERY. REMOVED AND REPLACED EMERGENCY LT BATTERIES.
ATB - LANDING GEAR WOULD NOT RETRACT. REMOVED AND REPLACED LANDING GEAR SAFETY SWITCH AND LINK ASSY, OPS CHECKS GOOD IAW MM 32-09-21
INSPECTION TYPE-C, NLG W/W CEILING HAS VISUAL CRACK INDICATION AT RIVET HOLE STA 288 BL 0. REMOVED AND REPLACED DAMAGED SECTION OF WEB NWW CELING BS 288 TO 270 BL 9 LT TO BL 9 RT AS PER B727 SRM 53-10-2 FIG 2 AND 51-30-2. MATERIAL USED 7075-T6 .040 18 X 18 LOT 219081 P O 8312438.
INSPECTION TYPE:N/A, DURING FLIGHT EXPERIENCED A TEN MINUTE PERIOD OF INTERMITTENT ILLUMINATION OF NR 1 ENG A/SS 13 FIRE DETECTION FAULT LIGHTS. REMAINED OUT FOR REST OF FLIGHT. FOUND NR 1 ENGINE FIREWALL CONNECTOR (D9511P) WIRES CHAFING TO GROUND WIRES. REPAIRED USING SELF FUSING TAPE (P/N 410) AND REPOSITIONED. SYSTEM OPS CHECKED AND FOUND SERVICEABLE.
FLT DECK EMERG EXIT LIGHT FELL OFF AND BROKE DURING LANDING (NOT DUE TO HARD LANDING). REINSTALLED LIGHT ASSY.
INSPECTION TYPE-C, CORROSION ON CARGO SEAT TRACK, STA 538 RBL 12. CORROSION REMOVAL OUT OF LIMITS. REMOVED SEAT TRACK FROM BS 480 TO 540, FABRICATED NEW SECTION OF SEAT TRACK, INSTALLED PER SRM 51-10-06, 53-10-05.
INSPECTION TYPE-C, WHILE WORKING CARD 509145 FUSEL 43 FOUND CARGO FLOOR TRACK CRACKED BETWEEN BS 558 AND BS 564 RBL 12. REMOVED CRACKED SECTION OF SEAT TRACK, FABRICATED REPLACEMENT PART, INSTALLED PER SRM 53-10-5, 51-10-6.
INSPECTION TYPE-C, WHILE WORKING CUST CARD 509379 FUSEL 71 FOUND FRAME BELOW CARGO TRACK TO BE CRACKED BS 540 RBL 15. REMOVED DAMAGED FRAME, FABRICATION, INSTALLATION ALL WORK DONE PER SRM 51-40-3.
INSPECTION TYPE-C, CORROSION ON FLOORBEAM TOP CHORD FORWARD SIDE STA 328, WL 208 RBL 39. CORROSION REMOVAL OUT OF LIMITS. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS, INSTALLED PER SRM 53-10-1, 53-10-8, 51-20-4 MM 51-20-131.
INSPECTION TYPE-C, CORROSION ON INNER SKIN BS 1080 BETWEEN STR 5L AND STR 6L ON AFT SKIN. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER EO B727-5330-1177K.
INSPECTION TYPE-C, CORROSION ON INNER SKIN BS 1080 BETWEEN STR 1 TO 4 LEFT OF STR 2L. REMOVED DAMAGED AREA, FABRICATED REPAIR PARTS AND INSTALLED PER EO B727-5330-1177K.
INSPECTION TYPE-C, POSSIBLE CRACK ON BEAM AT LIGHTENING HOLE BS 1183 LBL 26.83 WL 259.5. STOP DRILLED CRACK, HFEC CONFIRMED CONTAINMENT, REPAIRED IAW B727-5310-1116-D.
INSPECTION TYPE-C, RIB AT LEFT WING BL 620 IS CRACKED. STOP DRILLED CRACK, VERIFIED CONTAINMENT, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-2, 51-40-2.
INSPECTION TYPE-C, NR 6 SPOILER HAS 8 BY 18 AREA OF DELAMINATION UPPER SURFACE I/B FWD CORNER. REMOVED DAMAGED AREA REPAIRED IAW SRM 57-60-6.
INSPECTION TYPE-C, WHILE WORKING CUST ID 509318 FOUND CORROSION ON THE NR 6 SPOILER CENTER HINGE. REMOVED CORRODED FITTING AND REPLACED WITH NEW PART IAW SRM 51-30-5 MM 27-62-81 SRM 51-30-2 MM 27-50-00.
INSPECTION TYPE-C, NR 1 SPOILER IS DISBONDED AND CORRODED. REMOVED DAMAGED PANEL AND REPLACED WITH SERVICEABLE PANEL IAW MM 27-61-01.
INSPECTION TYPE-C, CORROSION SKIN AT OXYGEN SERVICING PANEL BULGING. FABRICATED AND INSTALLED REPAIR PARTS IAW SRM 53-30-3, 51-20-15, 53-10-3, 51-10-1, 51-40-3.
INSPECTION TYPE-C, FWD ENTRY DOOR NR 1 LOWER LONGITUDINAL BEAM CRACKED IN OUTBOARD RADIUS ALONG AFT END. STOP DRILLED CRACK, VERIFIED CONTAINMENT, FABRICATED REPAIR PARTS, INSTALLED IAW SRM 51-40-3, 51-30-2.
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP AT MAIN ENTRY DOOR. REPLACED BATTERIES, OPS CHECKS OK.
INSPECTION TYPE DLY, SKIN CRACK LEFT SIDE OF FUSELAGE STA 572 JUST ABOVE STR 25. REMOVED DAMAGE FROM SKIN AND STRINGER IAW 53-20-3 AND 53-30-3. DAMAGE REMOVED, FABRICATED DOUBLER, PICKED UP HOLES FROM A/C PER 53-30-3.
INSPECTION TYPE-N/A, EMERGENCY EXIT LIGHT INOP AT CREW ENTRY DOOR AND EMERGENCY LIGHT INOP AT COCKPIT DOOR. REMOVED AND REPLACED BATTERY PACKS.
WHILE ON GROUND, MAINTENANCE FOUND FWD CARGO DOOR FUSELAGE FRAME, FWD SIDE, 4TH STOP UP, DOUBLER CRACKED BEYOND STOP DRILL LIMITS.
CREW REPORTED ON TAKEOFF, WHEN LDG GEAR WAS RETRACTED, RED WARNING LIGHTS ILLUMINATED. RECYCLED AND DOOR WARNING LIGHT WORKED NORMAL. AMBER F/E LIGHTS OPS NORMAL. RED WARNING LIGHTS REMAINED ILLUMINATED UNTIL LANDING, WHEN GEAR WAS SELECTED DOWN, THEN THEY EXTINGUISHED UNTIL ROLL OUT, WHEN THE RUB NOSE GEAR WARNING LIGHT ILLUMINATED AND REMAINED ON. T/S WITH REF TO WDM 32-64-01 AND -02. FOUND C/P D298 PIN-C SHORTED TO GROUND. REPLACED D298, JACKED A/C AND PERFORMED EXTENSION AND RETRACTION SEVERAL TIMES. ALL GEAR POSITION INDICATING GROUND CKS GOOD AND ALL WITH REF TO M/M 07-11-00 AND 32-31-00.
WHILE ON GROUND MAINTENANCE, FOUND EMERGENCY EXIT LIGHT ON FORWARD ENTRY DOOR INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY.
WHILE ON GROUND, MAINTENANCE FOUND PASSENGER ENTRANCE DOOR EMER EXIT LIGHT FAILS TEST. REPLACED 2 S-106 BATTERIES AND OPS OK.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-571-01.02-01) ON UPPER SURFACE FORWARD STRINGER S-5 AT WING STATION 232.5. MAINTENANCE FABRICATED REPAIR PARTS PER MM 28-10-0, SRM 57-20-2 AND 51-20-4.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE TENSION TIE RIB AFT SHEAR FITTING VERTICAL BOLT HOLES HAVE CORROSION IN BORES. MAINTENANCE REMOVED THE CORROSION, REPLACED THE BUSHING DUE TO MISALIGNMENT. ALL WORK WAS PERFORMED BY BOEING PER CONTRACT 6-1171-TA-377 AND SB 727-55-56.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 SLAT O/B TRACK I/B SUPPORT FITTING TO BE CRACKED. MAINTENANCE REPLACED RIB, WORK DONE IAW SRM 51-30-02, 51-10-01, 57-51-51, AND MM 27-81-00.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED STIFFENER ON RT L/E AT APF 99 486 JUST O/B OF NR 6 SLAT I/B TRACK. MAINTENANCE REPLACED THE CRACKED STIFFENER IAW SRM 51-30-2, MM 27-81-00.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND SPOILER NR 14 X-RAY VIEWS NR 3, 4, 5 AND 6 SHOW CORE DAMAGE AND CONTAMINATION. MAINTENANCE REPAIRED IAW SRM 57-50-6 AND SRM 57-50-6.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-01.05-03) ON FLOORBEAM AT BS 1110 RBL 46 TO 52 WL 208. MAINTENANCE FABRICATED REPAIR PARTS AND INSTALLED PER B727-5310-7278A.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE LT NR 5 BALANCE PANEL FITTING TO BE CORRODED. MAINTENANCE REPLACED THE LT BALANCE PANEL HINGE FITTING IAW SRM 51-30-2 AND SRM 51-30-5.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK AT RT WING RIB AT WS 546.5. MAINTENANCE REMOVED AND INSTALLED A NEW RIB IAW EO B727-5710-13256.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE TOPSIDE OF PLUS CHORD AT BS 759 AND 761 RBL 68 WL 206. REPAIRED IAW EO B727-5710-1271 AND UPS EO B727-5710-7298-A.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND THE RT WING RIB AT WS 546.5 WAS CRACKED AT S-6 LOWER AND S-9 UPPER. MAINTENANCE REPLACED THE RIB IAW UPS EO B727-5710-1325-6 AND MM 28-10-00.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN STRINGER 18L BS 850 RBL 70.5 WL 192. MAINTENANCE REPAIRED PER UPS EO B727-5310-7314-A.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C57-224-01.05-01) ON FLOORBEAM AT BS 640 LBL 5 TO 33 WL 208. MAINTENANCE FOUND THE CORROSION REMOVAL WAS OUT OF LIMITS AND REMOVED THE DAMAGED AREA. FABRICATED AND INSTALLED REPAIR PARTS IAW UPS EO B727-5310-7313-A.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FWD SIDE OF FRAME AT BS 760, LBL 67, WL 212. MAINTENANCE REPAIRED IAW SRM 51-10-1, 51-20-4, AND 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM WEB AFT SIDE AT STA 900, RBL 2 TO RBL 23, WL 201 TO 203. MAINTENANCE REPAIRED IAW 53-10-1.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 740 TO 760 LBL 45 WL 208. MAINTENANCE INSTALLED NEW PARTS PER SRM 51-10-02, 51-20-04, 51-10-1, 51-30-2 AND OHM 20-44-04.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON THE UPPER SURFACE OF THE LOWER WING IN SPAR STIFFENER STR 5. MAINTENANCE REPAIRED IAW 727-57-1424.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND A CRACK IN THE TORQUE BOX WEB AT BS 1263, WL 150, RBL 18. MAINTENANCE REPAIRED THE WEB IAW SRM 51-40-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND NR 6 SLAT I/B TRACK SUPPORT FITTINGS AND RIBS CRACKED BEYOND STOP DRILL. MAINTENANCE REMOVED AND REPLACED THE RIBS PER SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON L/W O/B AILERON CENTER, I/B BEARING BLOCK ATTACH CASTING, ATTACHING BEARING BLOCK TO AILERON. MAINTENANCE REMOVED AND REPLACED PER SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOORBEAM UPPER CHORD BS 312, LBL 0 LBL 29. FABRICATED REPAIR PARTS AND INSTALLED PER SMR 53-10-8.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND STRINGER 9 UPPER CRACKED AT 546.5 ON LEFT WING. INSTALLED REPAIR IAW EO B727-5710-0314-F.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION RT PRESSURE BOX FORMED STIFFENER AT BS 740 TO BE CRACKED, FORWARD STIFFENER. FABRICATED PART AND INSTALLED ALL PART IAW SRM 51-20-1, 51-10-2, 51-30-2 AND MM 51-20-151.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND SEAT TRACK AT BS 760 TO 850 RBL 65 TO BE CORRODED ON BOTTOM FLANGE. FABRICATED REPLACEMENT TRACK PER SRM 51-10-2 AND INSTALLED TRACK PER SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACK SUPPORT RIB IN THE R/W I/B MIDFLAP TRAILING EDGE COVE 52 INCHES FROM THE I/B END. INSTALLED NEW RIB IAW SRM 51-30-5, 51-10-1, 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON BEAM STA 760 TO 860 LBL 45 WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM STA 760 TO 860, BLO WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LONGITUDINAL BEAM STA 760 TO 860 RBL 25 WL 208, AROUND NUTPLATE HOLES. REPAIRED IAW UPS EO NR 727-53-1646.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND STRINGER TO FRAME ATTACHMENT POINT CRACKED ON STRINGER NR 9 LT, BS 400. FABRICATED NEW PARTS AND INSTALLED PARTS WITH FASTENERS IAW SRM 51-30-2, 53-10-3.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CRACKED SUPPORT RIB ON THE R/W I/B MIDFLAP IN THE TRAILING EDGE COVE 53 INCHES FROM THE O/B END. INSTALLED NEW RIB IAW SRM 51-101 AND 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON FLOOR BEAM BS 720, RBL 45, 50, RBL 22, 35, WL 208. FABRICATED FLOORBEAM T-CHORD IAW SRM 53-10-8, 51-30-2, 51-10-02 AND MM 51-20-151.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL BS 295 TO 303 LBL 11 WL 208. REPLACED NEW PART IAW 51-30-5, 51-30-8.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND ELEVATOR NOSE RIB AT STA 208.16 TO BE CORRODED ON LT ELEVATOR. REPLACED NOSE RIB IAW SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON LEFT ELEVATOR I/B STATIC WICK BASE. REPLACED SKIN IAW 51-30-2, 55-20-1 AND 55-20-3.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON INTERCOSTAL AT BS 277 TO 294, WL 208 LBL 11. REMOVED AND REPLACED CORRODED INTERCOSTAL IAW SRM 51-30-2 AND 53-10-1.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STR 25 TOP OF FLANGE, BS 415 RBL 30 WL 155. REPLACED STRINGER PER SRM 53-10-3.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND REPAIR ANGLE TO BE CORRODED AND GOUGED AT BS 441 STR 26R. FABRICATED NEW REPAIR ANGLES AND INSTALLED WITH FASTENERS IAW SRM 51-30-2 AND 51-20-1.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STRINGER NR 1 BETWEEN STA 360 AND 380. FABRICATED STRINGER AND SPLICE PARTS IAW SRM 53-10-3. ALL OTHER WORK DONE IAW SRM 53-10-1, 51-30-2, 51-10-02, 51-10-6 AND MM 51-20-151.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON 380 FRAME STRAP AT BS 380 LBL 12 RBL 12 WL 148. FABRICATED NEW REPAIR ANGLE AND INSTALLED WITH FASTENERS IAW SRM 51-40-3, 51-10-6 AND 53-10-1.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON STR 21 FLANGE AT BS 308 LBL 54 WL 220. REPAIRED IAW SRM 53-10-1, 53-10-3.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK AT BS 640 TO 660 RBL 45 WL 208. REPAIRED IAW SRM 53-10-5, 53-10-1, 51-10-6.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK FLANGE AROUND NUTPLATE HOLES BS 344 TO 360 LBL 55 WL 208. REPAIRED IAW SRM 53-10-01, SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND R/W STA 171.5 UPPER RIB CHORD CRACKED AT STRINGER 5 TO 20 ATTACH POINT. REMOVED FASTENERS AND CUT OUT DAMAGED AREA IAW SRM 51-40-4. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-40-2, 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON PREVIOUS SPLICE REPAIRS OF FLOORBEAM BS 344 LBL 35 RBL 14 AND 23 WL 208. INSTALLED NEW UPPER FLOORBEAM IAW SRM 53-10-8 AND 51-30-2, 53-10-1.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON FUEL CELL UPPER SKIN BS 760 TO 870 BL 0 LBL 25. REMOVED CORROSION PER UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON UPPER SURFACE OF FUEL CELL SKIN BS 780 TO 800 LBL 47 TO 62. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00.01), ON FUEL CELL UPPER SKIN BS 740 TO 870 RBL 47 TO 62. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON SEAT TRACK BS 1130 TO 1138 RBL 45 WL 208. REMOVED, FABRICATED, REPLACED SEAT TRACK IAW SRM 53-10-1, M/M 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND LT INBOARD DOG HOUSE FLOOR TO BE CRACKED AT BS 294 LBL 25. REPAIRED IAW SRM 51-40-02 AND 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION WHILE WORKING FUSE 82 ON TOP SIDE OF FUEL CELL SKIN AT BS 759 AND 761 RBL 67 WL 206. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00-01), ON FUEL CELL UPPER SKIN FROM BS 857 TO 860 RBL 66 TO 69. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05,00-01), ON FUEL CELL UPPER SKIN FROM 756 TO 796 RBL 32 TO 45 WL 203. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION ON TOP AND BOTTOM OF SEAT TRACK BS 360 TO 365 LBL 23 WL 208. INSTALLED FABRICATED PARTS IAW SRM 51-10-2, 51-10-6, MM 51-20-151 SRM 51-30-2.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (CS53-224-05.00-01), ON FUEL CELL SKIN UPPER SURFACE BS 804 TO 860 LBL 47 TO 62 WL 203. REPAIRED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (CS53-224-05.00-01), ON FUEL CELL UPPER SKIN BS 837-870 LBL 25 TO 45. REPAIRED IAW UPS EO NR 727-57-1116.
WHILE IN FOR C-CHECK, MAINTENANCE FOUND CORROSION (C53-224-05.00-01), ON FUEL CELL UPPER SKIN BS 761 TO 765 RBL 11 TO 17. REMOVED CORROSION AND BLENDED AREA, SHOT PEENED AREA, ALODINED AND PRIMED IAW UPS EO NR 727-57-1416.
WHILE IN FOR C-CHECK, MAINT FOUND CORR ON TEE INTERCOSTAL AT STA 266 LBL 7 TO 11 WL 208. REMOVED AND REPLACED PART IAW SRM.
WHILE IN FOR C-CHECK, MAINT FOUND RT WING INBD FOREFLAP HAS 1 DELAM ON UPPER SURFACE AT INBD END. REPAIRED PER SRM 51-40-0.
WHILE IN FOR C-CHECK, MAINT FOUND CORROSION C53-224-01.00-02, ON STRINGER 6 LT STA 760 TO 868. CORR REMOVAL WAS OUT OF LIMITS FROM STA 781 TO 768 ON STR 6L. REMOVED DAMAGED AREA FROM BS 781 TO 768, FABRICATED AND INSTALLED REPAIR PARTS. ALL WORK DONE PER SRM 53-10-3, 51-10-2, 51-10-6. ALL OTHER AREAS BETWEEN STA 760 TO 848, WERE WITHIN LIMITS.
WHILE IN FOR C-CHECK, MAINT FOUND CORROSION C53-391-01.00-02, ON RT NR 5 BALANCE PANEL ATTACHING DOUBLER. REMOVED, FABRICATED NEW DOUBLER AND INSTALLED PER DWG 65-27917, MM 51-20-00, MM 51-20-21, MM 27-30-21.
WHILE IN FOR C-CHECK, MAINT FOUND CORR ON SEAT TRACK BS 1067 TO 1071 RBL 62 WL 208. REMOVED CORR AND FOUND OUT OF LIMITS. FABRICATED NEW SEAT TRACK, FINISHED INSTALLATION PER SRM 51-10-6, 51-30-2, 51-10-2, MM 51-20-151.
WHILE IN FOR C-CHECK, MAINT FOUND LFEC INSPECTION SHOWS A 10 PERCENT MATERIAL LOSS AT BS 360 STR. REMOVED PREVIOUS REPAIR, CUT OUT DAMAGED AREA, FABRICATED REPAIR PART. INSTALLED COUNTERSUNK FILLERS AND FINAL INSPECTION PER DRAWING 69-62161, SRM 51-30-2, 53-30-2, MM 51-20-151.
WHILE IN FOR C-CHECK, MAINT FOUND FWD ENTRY DOOR LWR FWD FRAME IS CRACKED. REMOVED DAMAGE, ALODINED AND PRIMED EDGE. FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 51-10-2, 51-40-3 AND 51-30-2.
WHILE IN FOR C-CHECK, MAINT FOUND STRINGER 8 LT STA 400 HAS 9 SHEARED FASTENERS GOING THROUGH FRAME AND CRACKS DISPERSING FROM HOLE. REPAIRED STRINGER IAW 53-10-3, 51-30-2.
WHILE IN FOR C-CHECK, MAINT FOUND RT WING STA 171.5 OB SIDE OF RIB, FWD VENT BOX AFT FLANGE CRACKED. REPAIRED IAW SRM 57-10-4, BY REMOVING AND REPLACING VENT STRINGER TAB.
WHILE IN FOR C-CHECK, MAINT FOUND CORR C53-221-01.01-01, AROUND NUTPLATES ON 25 G-BEAM AT STA 265 WL 208 LBL 6 TO RBL 15. CORR REMOVAL WAS OUT OF LIMITS. REMOVED DAMAGED 25 G-BEAM DRILLED UP NEW PART, INSTALLED PER SRM 53-10-1, 51-30-2.
WHILE IN FOR C-CHECK, MAINT FOUND CORR C53-221-01.01-01, ON INTERCOSTAL AT STR 259 TO 277 WL 208 LBL 11. REMOVED CORR, REMOVED INTERCOSTAL AND INSTALLED NEW INTERCOSTAL SRM 53-10-1, 51-30-8, 51-20-151 AND 51-30-2.
MAINTENANCE REPORTED, NR 3 FLIGHT SPOILER DELAMINATED AT FWD CORNERS. REPLACED NR 3 SPOILER PER SRM 27-61-01.
MAINTENANCE REPORTED EMERGENCY EXIT LIGHTS WOULD NOT ILLUMINATE IN THE ON POSITION OR WHEN POWER WAS REMOVED FROM THE A/C IN THE ARM POSITION. INSTALLED 2 EA NEW LIGHT ASSY. OPS CK NORMAL.