N207AU
Registered owner: HALE JOHN W, VA (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| FRONTIER AIRLINES, INC. (F3LA) | Operator | on 1996-06-22 | Operator named in NTSB report |
Accident & incident history
Operated by FRONTIER AIRLINES (per NTSB report)
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.
79 reports on file, 1995-01-30 – 1999-07-10.
Part: FAIRING — CRACKED (NR 1 NACELLE)
DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT FORWARD OUTBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
Part: FAIRING — CRACKED (NR 1 NACELLE)
DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE NACELLE TAILCONE FAIRING AT AFT INBOARD ATTACH POINT. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
Part: WIRE HARNESS — DAMAGED (VERTICAL STAB)
DURNG C-CHECK INSPECTION, REPORTED DAMAGED WIRING IN THE VERTICAL STABILIZER. CAUSE OF DAMAGE APPEARS TO BE SKYDROL HYDRAULIC FLUID. THE DAMAGE BEGAN APPROX 8 INCHES FROM RUDDER PCU ELECTRICAL CONNECTORS D-289 AND D-291 AND CONTINUED FOR APPROX 5 FEET, AFFECTING A TOTAL OF 20 WIRES. (M)
Part: RIB — CRACKED (NR 1 ENGINE)
DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER LOWER SIDE. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
Part: RIB — CRACKED (NR 1 ENGINE)
DEN - DURING C-CHECK INSPECTION, REPORTED CRACK IN NR 1 ENGINE UPPER DOG HOUSE TAIL FAIRING RIB, INNER AFT END. MAINTENANCE FABRICATED AND REPLACED RIB PER SRM 51-40-3 AND EA 51-737-003. (M)
Part: CHORD — CRACKED (BS 663.75)
DEN - DURING C-CHECK INSPECTION, REPORTED THREE CRACKS FOUND IN PRESSURE DECK COMPRESSION CHORD AT STATION 663.75, RBL 25 AND LBL 25. MAINTENANCE FABRICATED AND REPLACED RIB PER EA 51-737-003 AND SRM 51=40-3. (M)
Part: IGV — CRACKED (NR 1 ENGINE)
DEN - DURING C-CHECK INSPECTION REPORTED, NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE, 10 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4. STRESS RELIEVED PER P/W E/M 72-23-01. (M)
Part: IGV — CRACKED (NR 1 ENGINE)
DEN - DURING C-CHECK, INSPECTION REPORTED NR 1 ENGINE INLET GUIDE VANE CRACKED ON WELD AT 'A' FLANGE AT 2 O'CLOCK POSITION. MAINTENANCE STOP DRILLED CRACK PER P/W JT8D MM 72-00, PAGES 664A, 664B AND 665. CRACK AREA WELDED PER P/W E/M 72-23-01, REPAIR NR 14, SUBTASK 1, 2, 3 AND 4. STRESS RELIEVED PER P/W E/M 72-23-01, REPAIR 14. (M)
Part: ANGLE — CRACKED (NR 2 COWL)
DEN - DURING C-CHECK, INSPECTION REPORTED CRACK AT NR 2 ENGINE NOSE COWL FAIRING (SUGAR SCOOP) SEAL RETAINER INNER ANGLE. MAINTENANCE FABRICATED AND INSTALLED REPAIR PER SRM 51-40-3. (M)
Part: SHEAR TIE — CRACKED (BS 294.5)
DEN - DURING C-CHECK INSPECTION REPORTED, CRACK IN SHEAR TIE, LAST RIVET TO EDGE OF TIE, AT BS 294.5 ABOVE STRINGER 13L. MAINTENANCE REPAIRED CRACKED AT SHEAR TIE PER SRM 53-10-4, FIG 8. (M)
Part: SKIN — CRACKED (PYLON)
DEN - DURING C-CHECK, INSPECTION REPORTED CRACK IN PYLON INNER SKIN WHERE PANEL 5243 ATTACHES. MAINTENANCE REMOVED AND DAMAGED AREA AND REPAIRED PER SRM 51-40-3. (M)
Part: EXHAUST CASE — CRACKED (NR 2 ENGINE)
DEN - DURING C-CHECK INSPECTION, REPORTED NR 2 ENGIEN EXHAUST CASE CRACKED AT 3 O'CLOCK STRUT, TOP SIDE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54 PAGE 204 AND BAC 5975. (M)
Part: STRINGER — CRACKED (BS 360)
DEN - DURING C-CHECK, INSPECTION REPORTED STRINGER 7R CRACKED ON AFT SIDE OF CIRCUMFERENTIAL FUSELAGE SPLICE AT BS 360. MAINTENANCE REMOVED DAMAGED AREA, AND FABRICATED AND INSTALLED STRINGER PER SRM 51-10-2, 51-30-2 AND 51-20-01. (M)
Part: EXHAUST CASE — CRACKED (NR 2 ENGINE)
DEN - DURING C-CHECK INSPECTION, REPORTED A 3 INCH CRACK IN THE NR 2 ENGINE EXHAUST CASE UNDER 3 O'CLOCK POSITION STRUT, EXTENDING TOWARD CENTER OF CASE. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC 5975. (M)
Part: EXHAUST CASE — CRACKED (NR 2 ENGINE)
DEN - DURNG C-CHECK INSPECTION, REPORTED NR 2 ENGINE EXHAUST CASE STRUT CRACKED AT 9 O'CLOCK POSITION AT ROOT. MAINTENANCE STOP DRILLED AND WELDED CRACK PER P/W MM 72-54, PAGE 204 AND BAC5975. (M)
Part: IGV — CRACKED (NR 2 ENGINE)
DEN - DURING C-CHECK INSPECTION REPORTED NR 2 ENGINE INLET GUIDE VANE CRACKED AND STOP DRILLED AT 2 O'CLOCK POSITION, AFT WELD. MAINTENANCE WELDED CRACK IAW P/W E/M 72-23-04, REPAIR 14, PAGES 901 AND 902, SUBTASK 1, 2, 3 AND 4 AND STRESS RELIEVED IAW P/W E/M 72-23-01, REPAIR 14. (M)
Part: FITTING — CRACKED (AIRSTAIR DOOR)
DEN - DURING C-4 CHECK INSPECTION, REPORTED LEFT UPPER FORWARD STOP FITTING ON AFT AIRSTAIR DOOR CRACKED. MAINTENANCE INSTALLED REPLACEMENT FITTING PER SRM 51-30-2. (M)
Earlier reports · 1995–1998 · 62 reports
1998
Part: WIRE — LOOSE (ROW 17)
PHX - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 17 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
Part: ACTUATOR — FAILED (SPOILER)
DEN - UPON ARRIVAL, FLT CREW REPORTED LOSS OF 'A' SYSTEM HYDRAULIC PRESSURE DURING LANDING. MAINTENANCE REPLACED NR 5 GROUND SPOILER OUTBOARD ACTUATOR, SERVICED HYDRAULIC SYSTEM. PERFORMED LEAK CHECK AND CHECKED OK. (M)
Part: GASPER FAN — MALFUNCTIONED (CABIN)
PIH - EN ROUTE TO SEA, FLT CREW REPORTED A STRONG ELECTRICAL ODOR IN AFT PASSENGER CABIN. AIRCRAFT WAS DIVERTED TO POCATELLO AND LANDED WITHOUT INCIDENT. MAINTENANCE DETECTED ODOR COMING FROM AIR VENTS WITH GASPER FAN 'ON'. INSPECTED AIR CONDITIONING DISTRIBUTION BAY FOR ABNORMALITIES AND PLACARDED SYSTEM PER MEL 21-24. UPON ARRIVAL IN DEN, MAINTENANCE REPLACED GASPER FAN AND SYSTEM CHECKED OK. (M)
Part: SKIN — CORRODED (BS 294)
PAE - DURING C-CHECK, INSPECTION REPORTED BULGING SKIN AT AFT CORNER OF CUTOUT AT BS 294.5 WL 148, RBL 24. MAINTENANCE REMOVED CORRODED AREAS. FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-1, 51-30-2 AND ER 96-0315. (M)
Part: SKIN — CRACKED (CARGO DOOR)
PAE - DURING C-CHECK INSPECTION, FOUND 1.5 INCH CRACK IN LOWER CORNER OF AFT CARGO DOOR. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1, FIGURE 2, SRM 51-10-6, SRM 51-30-2 AND ER 98-0291. (M)
Part: SKIN — CORRODED (BS 415-430)
PAE - DURING C-CHECK, INSPECTION REPORTED SKIN PILLOWING AT BS 415-430, STRINGER 18R TO 19R. MAINTENANCE REMOVED A 13 INCH BY 20 INCH CORRODED AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-10-2, 51-30-2, AND 53-30-3. (M)
Part: LIGHTS — INOPERATIVE (CABIN)
DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 15 INOPERATIVE. MAINTENANCE REPAIRED WIRING AND SYSTEM CHECKED OK. (M)
Part: SKIN — CORRODED (BS 1018)
PAE - DURING C-CHECK, INSPECTION REPORTED BULGE IN SKIN AT BS 1018 BETWEEN STRINGER 27-R AND 28-R. MAINTENANCE REMOVED DAMAGED AREA (7.1 INCH BY 2 INCH). FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-30-3, PAGE 97, SRM 53-30-3, FIGURE 128, SRM 51-30-2, AND SRM 51-20-4, PARAGRAPH B. (M)
Part: STRINGER — CORRODED (BS 360-540)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-R, BS 360-540. MAINTENANCE REMOVED CORRODED AREAS, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3, FIGURE 16, AND SRM 51-30-2. (M)
Part: STRINGER — CORRODED (BS440-500)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 14-R, BS 440-500, AND CRACK IN STRINGER 14-R, BS 440-448. MAINTENANCE REPAIRED CORRODED AREAS, PER SRM 51-30-2, 53-30-1,53-30-3 AND 51-40-2. FABRICATED REPLACEMENT PARTS AND REPAIRED CRACK PER SRM 53-30-3, FIGURE 16, SRM 53-30-30 AND SRM 51-40-2. (M)
Part: STRINGER — CRACKED (BS 500)
PAE - DURING C-CHECK, INSPECTION REPORTED STRINGER 16-R CRACKED AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE REMOVED A 1 INCH BY 1.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, AND ER 98-0277. (M)
Part: FRAME — CRACKED (BS 360)
PAE - DURING C-CHECK INSPECTION REPORTED, FRAME CRACKED AT BS 360 BETWEEN STRINGER 20R AND 21R. MAINTENANCE REMOVED A 1. INCH BY 3.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-1 AND 51-40-3. (M)
Part: SKIN — CRACKED (BS 950)
PAE - DURING C-CHECK INSPECTION REPORTED, CRACK AT BS 950 BELOW STRINGER 14R AT EDGE OF SKIN LAP. MAINTENANCE REMOVED A 1 INCH BY 3 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)
Part: STRINGER — CRACKED (BS 500)
PAE - DURING C-CHECK INSPECTION, FOUND STRINGER 16L CRACKED AT BS 500B PLUS 19 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, SRM 51-10-1 AND ER 98-0277. (M)
Part: STRINGER — CRACKED (BS 500)
PAE - DURING C-CHECK INSPECTION REPORTED, CRACK IN STRINGER 16L AT BS 500B PLUS 8 INCHES, FORWARD OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0277. (M)
Part: STRINGER — CRACKED (BS 500)
PAE - DURING C-CHECK INSPECTION REPORTED CRACK IN STRINGER 16R AT BS 500B PLUS 16 INCHES, AFT OF WING ILLUMINATION LIGHT. MAINTENANCE FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2 AND ER 98-0275. (M)
Part: SKIN — DELAMINATED (NR 4 LE FLAP)
PAE - DURING C-CHECK, MAINTENANCE REPORTED DISBONDING ON NR 4 SLAT TRAILING EDGE WEDGE OUTBOARD UPPER END. MAINTENANCE REMOVED 52.0 INCHE OF DELAMINATED SKIN FROM OUTBOARD LOWER SURFACE, 13 INCHES OF DELAMINATED SKIN FROM OUTBOARD UPPER SURFACE AND 15 INCHES OF DAMAGED HONEYCOMB CORE, FABRICATED REPAIR PARTS AND APPLIED BONDING PRIMER PER SRM 51-40-6, PAGES 8 TO 8H. (M)
Part: FRAME — CRACKED (BS 7472)
DURING C-CHECK, MAINTENANCE REPORTED FRAME CRACKED AT STA 7472, STR 9L. MAINTENANCE FABRICATED AND INSTALLED REPAIR PARTS PER SRM 51-40-3. (X)
Part: STRINGER — CORRODED (BS 450-459)
PAE - DURING C-CHECK, INSPECTION REPORTED CORROSION ON STRINGER 10-L, BS 450-459. MAINTENANCE REMOVED A 3 INCH BY 2.5 INCH AREA, FABRICATED REPLACEMENT PARTS AND REPAIRED PER SRM 51-30-2, PAGES 3 AND 4, SRM 53-30-3, FIGURE 16, SRM 53-30-3, PAGES 51-53, AND SRM 51-30-00. (M)
Part: SKIN — CORRODED (BS 500)
PAE - DURING C-CHECK INSPECTION REPORTED, CORROSION ON STRINGER 4L SKIN LAP AT BS 500A PLUS 10 INCHES. MAINTENANCE REMOVED A 1.2 INCH BY 2 INCH CORRODED AREA, FABIRCATED REPLACEMENT PARTS AND REPAIRED PER SRM 53-30-3. (M)
Part: FLOORBEAM — CORRODED (BS 328)
DURING C-CHECK, MAINTENANCE REPORTED CORROSION ON UPPER CHORD BS 328 FLOORBEAM, LBL 30-4, WL 208. MAINTENANCE REMOVED DAMAGED SECTION OF BS 328 BEAM UPPER CHORD FROM LBL 28 TO LBL 65. FABRICATED REPAIR PARTS AND INSTALLED WET WITH FASTENERS PER SRM 53-10-9, FIG 5 AND SRM 53-10-1. (M)
1997
Part: BATTERY PACK — FAILED (CABIN EEL)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED RIGHT OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED BATTERY PACK AND SYSTEM CHECKED OKAY.
Part: PRESSURE WEB — CRACKED (BS 259)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED EIGHT .5 INCH CRACKS IN LEFT PRESSURE WEB AT STATION 259 AND TWO .5 INCH CRACKS IN RIGHT PRESSURE WEB AT STATION 259 FORWARD OF DOOR IDLER FITTING. MAINTENANCE TRIMMED OUT CRACKS. FABRICATED FILLER AND INSTALLED DOUBLER 202413 .050 PER FRONTIER EA'S 53-737-026 AND 53-737-027, BOEING TELEX NRS FRO-DEN-97-0075RR AND M-7272-97-3951, AND FAA FORM 8110-3, DATED 8-1-97. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
DEN - DURING SERVICE CHECK, MAINTENANCE REPORTED FLOOR PROXIMITY LIGHTING AT ROW 11 INOPERATIVE. MAINTENANCE REPLACED BATTERY PACK AND CHECKED OKAY. (X)
Part: LIGHT — MALFUNCTIONED (CABIN)
UPON ARRIVAL, FLIGHT CREW REPORTED FORWARD GALLEY DOOR EMERGENCY LIGHT ILLUMINATED AND WOULD NOT EXTINGUISH. REPLACED LIGHT ASSEMBLY AND CHECKED OK. (M)
Part: SLIDE — LOW PRESSURE (R2 DOOR)
DEN - PRIOR TO DEPARTURE, FLIGHT CREW REPORTED R-2 DOOR EMERGENCY ESCAPE SLIDE PRESSRUE LOW. REPLACED ESCAPE SLIDE. (M)
Part: DOUBLER — CORRODED (BS 580)
UPON REMOVAL OF NR 2 DME ANTENNA FOR BS 520 FRAME REMOVAL FOUND CORROSION ON NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0 WL 148.5. REMOVED CORROSION FROM AROUND NR 2 DME ANTENNA MOUNTING STRUCTURE BS 580, BL 0, WL 148.5 AREA FOUND TO BE OUT OF LIMITS. (M)
Part: DOUBLER — CORRODED (BS 520)
PAE - UPON REMOVAL OF NR 1 ADF ANTENNA FOR BS 520 FRAME REMOVAL, FOUND CORROSION ON NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. REMOVED CORROSION FROM AROUND NR 1 ADF ANTENNA MOUNTING STRUCTURE BS 560, BL 0, WL 148.5. AREA FOUND TO BE OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED PORTION OF KEEL BEAM AT BS 539-571, RBL 6.5 REPAIRED IAW EWO NR 96-0959. (M)
Part: NOSE CHORD — CORRODED (BS 237)
FOUND CORROSION ON RIGHT LOWER NOSE CHORD HORIZONTAL FLANGE BS 237 TO 250 RBL 18, WL 164. REMOVED RT LOWER NOSE CHORD DUE TO CORROSION WAS BEYOND LIMITS IN A ONE INCH AREA IAW SRM 53-10-1. INSTALLED NEW NOSE CHORD WITH A SPLICE IAW SRM 51-40-3, 53-10-2, 51-30-2. (M)
Part: FRAME — DAMAGED (BS 520)
FOUND CORROSION ON THE FORWARD SIDE OF THE 520 FRAME IN THE FORWARD CARGO BAY BS 520 LBL 18 TO RBL 14, WL 149. REMOVED DAMAGED FRAME, STRINGER CLIPS, STRINGER 26 LT (30 INCH) AND DAMAGED INTERCOSTALS AS WELL AS FLOOR TO SIDEWALL SUPPORT PLATES. FABRICATED NEW PARTS FOR DAMAGED FRAME IAW DRAWING 65-46534 SHEET 4, SRM 51-20-1, 51-10-1, INSTALLED ALL PARTS IAW SRM 51-30-2 AND SEALED ALL PARTS WET ON INSTALLATION IAW SRM 51-20-4. (M)
Part: SKIN — GOUGED (RT ENGINE)
PAE - WHILE WORKING ENGINE NR 195 FOUND RT LOWER RAM AIR INTAKE SKIN GOUGED AT BS 500B PLUS 7 STRINGER 24 RT. REMOVED DAMAGED WEB AT BS 500B PLUS7, STRINGER 24 RT FABRICATED WEB FROM MATERIAL 2024-T3, .040 INCH PER SRM 51-20-01. ALODINED, PRIMED AND INSTALLED WEB ASSEMBLY PER MM 21-52-51. (M)
Part: DELTA BEAM — CRACKED (BS 574-579)
PAE - FOUND CRACK ON PREVIOUS REPAIR BEHIND RAM AIR DUCT RIGHT SIDE AT BS 574-579, RBL 40, WL 152 ON DELTA BEAM. REMOVED 2 INCH CRACK BY REMOVING DAMAGE AREA, REPAIRED LOWER DELTA BEAM WEB, RT SIDE BS 574-579, RBL 40, WL 152 IAW SRM 53-10-6 FIG 1 WITH PART FABRICATED FROM SHEET STOCK OF 2024-T3 .063 INCH MATERIAL. (M)
Part: WEB — CORRODED (NLG WW)
PAE - FOUND CORROSION IN NOSE WHEEL WELL UPPER HORIZONTAL WEB AROUND RT ACCESS PANEL CUTOUT BS 236 TO 252, LBL 2 TO 16, WL 190. FOUND CORROSION ON NOSE WHEEL WELL UPPER HORIZ WEB AND STIFFENERS TO BE OUT OF LIMITS, FABRICATED DOUBLERS FROM .080 7075 T6. INSTALLED DOUBLERS AND NEW STIFFENERS WITH HI-LOCKS AND RIVETS. ALODINED, PRIMED, PAINTED AND INSTALLED WEB PER SRM 51-10-2, 51-10-6, 51-20-1, FIG 7, 51-30-2, 53-10-1, OHM 20-41-02, AND DRAWING NR 65-45819. (M)
Part: DOUBLER — CORRODED (BS 983)
PAE - FOUND CORROSION ON OUTFLOW VALVE INTERNAL DOUBLER BS 983 RBL 20 WL 183. FOUND DOUBLER TO BE OUT OF LIMITS. REMOVED OUTFLOW VALVE AND DOUBLER, FABRICATED NEW DOUBLER, BACK DRILLED HOLES, DEBURRED, ALODINED, PRIMED AND INSTALLED. REINSTALLED OUT FLOW VALVE AND SEAL, RESTORED TO ORIGINAL FINISH. ALL WORK DONE IAW SRM 51-10-1, 51-30-2, 51-10-6, 51-10-2, MM 21-31-11, AND EWO 96-0941. (M)
Part: SHEAR TIE — CORRODED (BS 420)
PAE - FOUND CORROSION (C53-028-01) ON UPPER SURFACE OF SHEAR TIE IN FORWARD CARGO BAY AT BS 420 LBL 9 WL 148. BLENDED OUT CORROSION ON UPPER SURFACE OF SHEAR TIE IN FORWARD CARGO BAY AT BS 420 LBL 9 WL 148. REMOVED 2 INCHES BY 1 INCH BY .005 INCH WITH ORIGINAL THICKNESS AT .045 OUT OF LIMITS PER SRM 53-10-1. CUT OUT DAMAGED AREA AND FABRICATED AND INSTALLED SHEAR TIE REPAIR IAW SRM 53-10-4 AND 51-10-2. (M)
Part: SEAT TRACKS — CORRODED (BS 328)
PAE - FOUND CORROSION (53-107-02) ON SEAT TRACK BS 328 TO 360, RBL 22 WL 208. REMOVED CORRODED SEAT TRACK AT BS 328 TO 360 RBL 22 WL 208 AND REPLACED WITH NEW SEAT TRACK IAW SRM 51-30-2, MM 51-21-1 AND 51-21-171. (M)
Part: SKIN — DENTED (CARGO DOOR)
FOUND FORWARD CARGO DOOR OUTER SKIN IS DENTED AND GOUGED ALONG ENTIRE LENGTH OF LOWER SKIN. REMOVED DAMAGED AREAS, FABRICATED REPAIR PARTS AND INSTALLED IAW SRM 52-00-3, 51-40-3 ON FORWARD CARGO DOOR OUTER LOWER SKIN. (M)
Part: FRAME — CRACKED (CARGO DOORWAY)
PAE - FOUND FORWARD CARGO DOOR FORWARD SIDE FRAME AROUND LATCH CAM IS CRACKED. REMOVED AND REPLACED FORWARD CARGO DOOR FORWARD SIDE FRAME AROUND LATCH CAM PER SRM 51-30-2 AND 51-30-8. (M)
Part: FLOORBEAM — CORRODED (BS 294)
PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 294 LBL 12 TO RBL 34 WL 208. REMOVED AND REPLACED UPPER CHORD OF FLOORBEAM BS 294 WL 208 FROM RBL 60 TO LBL 60 IN IAW SRM 53-10-9, SRM 53-10-1. (M)
Part: BULKHEAD WEB — CRACKED (BS 178)
PAE - AT BS 178 BULKHAD, NDI SHOWED 12 CRACK INDICATIONS AT VARIOUS LOCATIONS BETWEEN WL 184 TO WL 234, RBL 17.5 TO LBL 17.5. BLIND FASTENERS INSTALLED IN PREVIOUS REPAIR AT WL 234, RBL 12 AND LBL 12. REMOVED CENTER WEB, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR WEB IAW, SRM 53-10-11, 51-30-2, MM 51-21-41 AND DRAWING NR 65-16300. (M)
Part: FLOORBEAM — CORRODED (BS 344)
PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 344, RBL 10, WL 208. REMOVED .028 INCH OF MATERIAL 4 INCHES BY 2 INCHES FROM ORIGINAL THICKNESS OF .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. FABRICATED AND REPLACED IAW SRM 53-10-09 INSTALLED PARTS IAW SRM 51-40-03 ON FLOOR BEAM, BS 344 RBL 10, WL 208. (M)
Part: FLOORBEAM — CORRODED (BS 986)
PAE - FOUND CORROSION (C53-202-04) ON AFT SIDE OF FLOOR BEAM (PREVIOUS REPAIR) BS 986, LBL 5 TO RBL 5, WL 208. BLENDED OUT CORROSION, FOUND TO BE OUT OF LIMITS ON AFT SIDE OF FLOOR BEAM, REPAIRED PE SRM 53-10-9. (M)
1996
Part: DOME — MIS REPAIRED (DOME BS 1016)
PAE - REPAIR ON BS 1016 PRESSURE DOME DOES NOT CONFORM TO THE SRM. REMOVED OLD REPAIR AND INSTALLED NEW REPAIR ON PRESSURE DOME BS 1016, LBL 19, WL 244 PER SRM 53-10-4 FIGURE 3. (M)
Part: FORGING — CRACKED (BS 727)
PAE - FOUND CRACK IN FORGING AT BS 727 BL 0, WL 208, 1.5 INCH LONG. REMOVED AND REPLACED FORGING AT BS 727 BL 0, WL 208 IAW SRM 51-10-1 AND SRM 51-30-2. (M)
Part: FLOORBEAM — CORRODED (BS 1006)
PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 1006 LBL 10 TO LBL 36 WL 208. CORROSION DAMAGE FOUND TO BE OUT OF LIMITS. REMOVED DAMAGED AREA AND INSTALLED REPAIR PART IAW SRM 53-10-1, 53-10-6 AND 53-10-9 AT BS 1006 LBL 10 TO LBL 36 WL 208. (M)
Part: FLOORBEAM — CORRODED (BS 947)
PAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 947 RBL 40-47 WL 208 AND RBL 5-15. FOUND TO BE OUT OF LIMITS. REPLACED TOP CHORD AT STATION 947 LBL 35 TO RBL 61 WL 208 IAW SRM 53-10-9 AND EWO 96-0931. (M)
Part: ANGLE — CRACKED (LT WING)
PAE - INBOARD LOWER RIB ANGLE CRACKED ON AFT END AT L/W AILERON NR 3 HINGE FITTING. REMOVED AND REPLACED INBOARD AND OUTBOARD LOWER RIB ANGLE ON L/W AILERON NR 3 HINGE FITTING IAW OHM 20-50-1. (M)
Part: FRAME — CRACKED (GALLEY DOOR)
PAE - FORWARD GALLEY DOOR AFT SIDE FRAME IS CRCKED, 3 INCHES TO 5 INCH CRACKS FOUND. REMOVED AND REPLACED FORWARD GALLEY DOOR AFT SIDE FRAME PER SRM 51-30-2. (M)
Part: FLOORBEAM — CORRODED (BS 967)
PAE - FOUND CORROSION (C53-107-02) ON TOP OF FLOORBEAM BS 967 RBL 50, LBL 25, WL 208. FOUND CORROSION ON FLOORBEAM TO BE OUT OF LIMITS. REPLACED FLOORBEAM PER EWO 96-0930 AND SRM 53-10-9. (M)
Part: FLOORBEAM — CORRODED (BS 312)
PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED CORROSION ON TOP CHORD OF FLOORBEAM, BS 312, RBL 10 TO RBL 12, WL 208. REMOVED 3 INCH BY 3 INCH BY .024 INCH ORIGINAL THICKNESS .080 INCH. FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01. REMOVED DAMAGED AREA AND REPAIRED IAW SRM 53-10-9. (M)
Part: FLOORBEAM — CORRODED (BS 328)
PAE - FOUND CORROSION (C53-107-02) ON FLOORBEAM BS 328, RBL 10 TO RBL 41, WL 208. REMOVED CORROSION IN AN AREA OF 3 INCH BY 18 INCH WITH A DEPTH OF .028 INCH AND AN ORIGINAL THICKNESS OF .080 INCH, FOUND TO BE OUT OF LIMITS PER SRM 53-10-01. REMOVED AND REPLACED UPPER T-CHORD. ALL WORK DONE IAW SRM 53-10-01, 53-10-02, AND 53-10-9. (M)
Part: SKIN — CRACKED (BS 791)
PAE - FOUND CRACK IN EXTERNAL SKIN AT BS 797, STRINGER 24 LEFT, CRACK WAS APPROXIMATELY 4 INCHES LONG. STOP DRILLED CRACK. FABRICATED REPAIR DOUBLER AND INSTALLED PER SRM 53-30-3. WORK WAS DOCUMENTED ON TRAMCO CARD NR FUSELAGE 240, CUST ID NR 0732. (M)
Part: SILL — CORRODED (BS 920-960)
FOUND CORROSION 9C53-107-02) THROUGH R/T MOP SILL, BS 920-960, RBL 60, WL 208. FOUND R/T MOP SILL (CREASE BEAM) CORRODED OUT OF LIMITS PER SRM 53-10-3. REMOVED AND REPLACED MOP SILL AT BS 920-960, RBL 60, WL 208 PER SRM 51-30-02. (M)
Part: CLIP — CRACKED (BS 727)
PAE - FOUND CRACKED STRINGER CLIP BS 727A STRINGER 21R. REMOVED STRINGER CLIP BS 727A STRINGER 21R. FABRICATED STRINGER CLIP, ALODINED AND PRIMED. INSTALLED STRINGER CLIP IAW SRM 51-20-1 AND SRM 51-30-02. (M)
Part: FLOOR BEAM — CRACKED (BS 663)
DURING SERVICE CHECK, INSPECTION REPORTED A 1.25 INCH CRACK IN THE CABIN FLOOR BEAM WEB AT STATION 663, BBL 0. REPAIRED PER BOEING SERVICE BULLETIN 737-57-121D, FIG 4 AND BOEING TELEX M-7272-96-4639. (M)
Part: ESCAPE SLIDE — LOW PRESSURE (PASSENGER DOOR)
DEN - FLT 601 - UPON ARRIVAL, FLIGHT CREW REPORTED THE FORWARD ENTRY DOOR ESCAPE SLIDE BOTTLE PRESSURE AT ZERO. MAINTENANCE REPLACED ESCAPE SLIDE.
Part: CONNECTOR — DIRTY (CABIN)
MSP - DURING SERVICE CHECK, MAINTENANCE REPORTED LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHTS INOPERATIVE. CLEANED LIGHT ASSEMBLY CONTACTS AND CHECKED OK. (M)
1995
Part: LINE — FAILED (B-HYD SYSTEM)
FLT NR 221 - DEN - AIR TURN BACK, DURING CLIMB-OUT OF DEN, FLIGHT CREW REPORTED B-SYSTEM HYDRAULIC FAILURE. THE AIRCRAFT WAS RETURNED TO DEN WITHOUT INCIDENT. MAINTENANCE REPLACED THE HYDRAULIC LINE FROM THE NR 2 B-SYSTEM MODULE. PERFORMED LEAK CHECK AND SYSTEM CHECKED OK. (M)
Part: PITCH CONTROL — MALFUNCTIONED (AUTO PILOT)
DEN - UPON DESCENT INTO DEN, FLIGHT CREW REPORTED THEY WERE UNABLE TO MOVE THE ELEVATOR WITH THE CONTROL WHEEL WHILE THE AUTO PILOT WAS ENGAGED. THE AUTO PILOT WAS DISENGAGED, NORMAL CONTROL WAS RESUMED AND AIRCRAFT LANDED WITHOUT INCIDENT. MAINTENANCE REPLACED THE PITCH CONTROL CHANNEL AND CHECKED OK. (W)
Part: EEL BATTERY PACK — DISCHARGED (CABIN)
DEN - PRIOR TO DEPARTURE, MAINTENANCE REPORTED THE LT EXTERIOR OVERWING EMERGENCY EXIT LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LT AFT BATTERY PACK AND CHECKED OKAY. (X)
Part: YAW DAMP COUPLER — MALFUNCTIONED (AUTOPILOT)
BZN - UPON APPROACH, AIRCRAFT STARTED TO YAW LEFT AND RIGHT AFTER SELECTING 40 DEGREE FLAP SETTING. PILOT TURNED OFF YAW DAMPER AND YAW PROBLEM WAS CORRECTED. PLACARDED PER MEL 22-3. ON JANUARY 31, 1995, MAINTENANCE REPLACED YAW DAMPER COUPLER AND THE RUDDER PCU. SYSTEM CHECKED OKAY. REFERENCE CONTROL NR F3LA95004.
Part: PCU — MALFUNCTIONED (RUDDER)
BZN - UPON APPROACH, AIRCRAFT STARTED TO YAW LEFT AND RIGHT AFTER SELECTING 40 DEGREE FLAP SETTING. PILOT TURNED OFF YAW DAMPER AND YAW PROBLEM WAS CORRECTED. PLACARDED PER MEL 22-3. ON JANUARY 31, 1995, MAINTENANCE REPLACED YAW DAMPER COUPLER AND THE RUDDER PCU. SYSTEM CHECKED OKAY. REFERENCE CONTROL NR 95ZZZX784. (X)