N267FE, cancelled Oct 12, 2012

Service difficulty reports · 121

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE n_number = 'N267FE' AND deregistration_id = 'N267FE-2012-10-12'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR FDEA201205031738Light · detachedEMERGENCY LIGHT OVER COCKPIT DOOR CAME UNATTACHED FROM ATTACHMENT ON TAKE OFF ROLL. REINSTALLED COCKPIT EMERGENCY LIGHT ASSY IAW MM 33-50-001-2-0. OPS CHECKED NORMAL. ACFT OK FOR SERVICE.May 3, 2012 · N267FE · Boeing 727233 · Emergency LightingSDR FDEA201006152020Stringer · corrodedCORROSION IN CHANNEL -STRINGER 27L, STA 950 - 950C. CUT OUT SECTION OF STRINGER 27L FROM BS 950A PLUS 10" TO 950C PLUS 10", 38 3/4" IN LENGTH, IAW SRM, REV 103, 51-10-1 AND 53-10-3 FIG 1. FABRICATED (2) STRINGER SECTIONS USING BAC1498-147, 7075-T6, 19" LOJun 15, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006142002Rib · gougedUPON REMOVAL OF NO. 7 SLAT, FOUND OB END CAP RIB CHAFFED AND GOUGED, EXTERIOR SURFACE. REMOVED DAMAGE OB RIB AND FABRICATED NEW RIB FROM 2024O .040 HEATED TREATED TO T4 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A APPROX DIM: 15 3/4" X 7" & INJun 14, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006142000Rib · gougedUPON REMOVAL OF NR 7 SLAT FOUND IB END CAP RIB CHAFED AND GOUGED, EXTERIOR SURFACE REMOVED DAMAGED IB RIB, FABRICATED NEW RIB FROM 2024O .040 APPROX DIM: 15 3/4" X 7" HEATED TREATED TO T4 CONDITION IAW FAS ENGINEERING REPORT 2-37153-801 REV A & INSTALLED Jun 14, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006121972Skin · damagedUPON REMOVAL OF BLIND FASTENER AT BS 950E, AT STRINGER 26L TO 25L, FOUND DOUBLE DRILLED HOLE. CUT OUT DAMAGED AREA OF SKIN, DIMENSIONS 4" X 4" IAW SRM 53-30-3 FIG 5 AND 51-10-1. FABRICATED STRUCTURAL FILLER USING 2024 T3 .080", PO NR 9009585, DIMENSIONSJun 12, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006101937Web · crackedAFT AIRSTAIRS RT LOWER TORQUE BOX WEB AT BS 1243 HAS UPPER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7075T6 .032 APPROX DIM: 4" X 1 1/4" & INSTALLED REPAIR DOUBLER AT BS 1243 RH LOWER TORQUE WEB IJun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006101936Web · crackedAFT AIRSTAIR RT LOWER TORQUE BOX WEB AT BS 1243 HAS LOWER LIGHTNING HOLE CRACKED. CUTOUT DAMAGED AREA APPROX DIM: 5/8" X 3/8", FABRICATED REPAIR DOUBLER FROM 7075T6 .032 APPROX DIM: 4" X 1 1/4" & INSTALLED REPAIR DOUBLER AT BS 1243 RH AFT AIRSTAIR TORQUE BOXJun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006101946Shear Tie · crackedCRACKED SHEAR TIE - STA 950E AT STR 26L. REMOVED SHEAR TIE 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING BAC1505-100261 7075-T6511, 7 3/8" LONG IAW DWG 65-56123 REV A. INSTALLED SHEAR TIE IAW DWG 65-56123 REV A AND SRM 51-30- 2.Jun 10, 2010 · N267FE · Boeing 727233 · Fuselage Internal Mounting StructureSDR FDEA201006091908Stringer · crackedRT WING, WS 629 STR 9 HAS A CRACK. STOP DRILLED CRACK DIM: .0187" IAW EO 7-5710-7-4322 PART 1. FABRICATED REPAIR ANGLES FROM AND10134-2001 7075T6 DIM: 10.6" X 2" AND 3.4" X 2" AND FABRICATED 2 EA. RADIUS FILLER FROM AND 10137-3004 DIM: 3" X 1" IAW EO 7-5710Jun 9, 2010 · N267FE · Boeing 727233 · Wing, Longeron/StringerSDR FDEA201006091917Skin · corrodedCORROSION IN SKIN BS 600, STR 28L. CUTOUT DAMAGED AREA APPROX DIM: 2.5" X 1" AND FABRICATED REPAIR DOUBLER FROM 2024T3 .100 APPROX DIM: 8 3/4" X 12 5/8". INSTALLED REPAIR DOUBLE AT BS 600 STR 28L IAW SRM 53-30-3 FIG 1, SRM 51-30-2, SRM 51-10-2, & SRM 51-10-6Jun 9, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006081873Seat Track · corrodedCORROSION SEAT TRACK SECTION BS 1130-BS 1176, RBL 25. REMOVED CORRODED SEAT TRACK AT BS 1130 - BS 1176 RBL 25 IAW SRM 51-30-2 FOUND CORROSION OUT- OF-LIMITS IAW SRM 53-10-1 FIG 3. FABRICATED SEAT TRACK PN RCV 7075T65105X4IN DIM: 44" 3/4 IAW DWG 53FX976 REV Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006081871Skin · gougedMAIN CARGO AREA, MAIN CARGO INNER SKIN, BS 620 - 640, STR 4L GOUGED. REMOVED DAMAGE MAIN CARGO DOOR INNER SKIN FROM BS 594- BS 642 STR 9L - STR 4L, FABRICATED NEW SKIN FROM 2024T3 .125 APPROX DIM: 79" X 48" & INSTALLED NEW SKIN AT MAIN CABIN CARGO DOOR CJun 8, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006081900Intercostal · corrodedCORROSION IN STR 28L AT BS 600. CUTOUT DAMAGED AREA APPROX DIM: 17" IN LENGTH, AND FABRICATED NEW STRINGER SECTION FROM BAC 1498-141 APPROX DIM: 17" IN LENGTH AND FAB'D 2 EA. SPLICES FROM BAC 1498-132 APPROX DIM: 12", ALSO FAB'D NEW INTERCOSTAL FROM 7075 O Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006071859Skin · corrodedCORROSION ON SKIN UNDER INTERCOSTAL AT BS 970 BETWEEN STR 28L AND 27L. CUT OUT DAMAGE, 15 1/4" X 2 7/8" ON SKIN AT BS 950E TO 970 BETWEEN STRINGER 28L AND 27L IAW SRM, REV 103, 53-30-3 FIG 3. FABRICATED DOUBLER USING 2024 T3, .125" X 27 1/4" X 11 1/2" IAW SRMJun 7, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006051840Floorbeam · corrodedCORROSION TOP OF FLOORBEAM MAIN CABIN BS 620 BETWEEN LBL 25 - LBL 45. CUT-OUT DAMAGED AREA AT TOP OF FLOOR BEAM BS 620 LBL 25 -LBL 45 APPROX DIM: 3" 5/8 X 1". FABRICATED ANGLES REPAIR HEAT TREATED TO T6, FIRST ANGLE DIM: 22" 1/4 X 3" AND SECOND ANGLE DIM:Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201006051839Floorbeam · corrodedCORROSION FLOORBEAM TOP FLANGE BS 1130, RBL 35. CUT-OUT DAMAGED AREA APPROX DIM: 3" X 1" 1/4, FABRICATED REPAIR PARTS, ANGLE APPROX DIM 11" 1/8 X 3", FABRICATED STRAP DIM 11" 1/4 X 2", FABRICATED FILLER DIM 2" 7/8 X 1" 3/8, FABRICATED RADIUS FILLER DIM: 11Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR FDEA201006041825Fitting · corrodedCORROSION ON LOWER CHORD AT BS 950, STRINGER 30. REMOVED LOWER CHORD SPLICE AT BS950, BL 0, IAW SRM, REV 103, 51-30-2. LOCATED, DRILLED AND DEBURRED LOWER CHORD SPLICE FITTING IAW SRM 51-30-5. INSTALLED LOWER CHORD SPLICE FITTING IAW SRM 51-30-2.Jun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201006041821Stringer · corrodedCORROSION ON STR 27L BETWEEN BS 950F AND 970. REMOVED SECTION OF STRINGER 38 1/2" IN LENGTH IAW B727 SRM, REV 103, 53-10-3 FIG 1. FABRICATED (2)EA. STRINGER SECTIONS USING BAC1498-146, 7075-T6, 19 1/4" IN LENGTH, AND (3)EA. SPLICES USING BAC1498-131, 7075-TJun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006031833Skin · damagedMAIN CARGO AREA, BS 660, BETWEEN STR 3L -4L. FASTENERS WITH NO SPACING. DAMAGED AT TEAR STRAP AND SKIN BS 660 STR 3L - 4L DIM: 3" X 2" 1/2 - 2" 1/2 X 1". FABRICATED DOUBLER APPROX DIM: 12" 1/8 X 11" 1/8, FABRICATED TRIPLER APPROX DIM: 9" 3/4 X 9", FABRICATJun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR FDEA201006031812Stringer · corrodedCORROSION ON STRINGER 29L, FROM BS 950B TO 950C. REMOVED FASTENERS IAW SRM 51-30-2. REMOVED CORROSION FROM STR 29L IAW SRM 51-10-6. UT INSPECTED AREA IAW NDTM 51-00-00, FIG 3 PART 4, ORIGINAL .150", REMAINING .136". FOUND MATERIAL LOSS OF .014" TO BE WITHJun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201006031810Angle · crackedRT WING INBD MID FLAP LOWER T/E CHORD ANGLE IS CRACKED, 2 PLACES, WBL 100. R & R DUE TO DELAMINATION ON SNRM NR N00544, WO NR00048343.Jun 3, 2010 · N267FE · Boeing 727233 · Trailing Edge FlapsSDR FDEA201006031809Structure · crackedNR 7 SLAT T/E CHORD CRACKED AT INBD UP STOP. REMOVED NR 7 SLAT LOWER CHORD IAW SRM 51-30-2. FABRICATED NEW CHORD USING BAC1514-1559, 2024-T3511, 113.7500", IAW SRM 57-50-2 FIG 2 AND 51-30-5. INSTALLED LOWER CHORD IAW SRM 51-30-2.Jun 3, 2010 · N267FE · Boeing 727233 · Leading Edge DevicesSDR FDEA201006031801Seat Track · corrodedCORROSION SEAT TRACK FLANGE MAIN CABIN BS 680 TO BS 620, LBL 45. REMOVED DAMAGED SEAT TRACK SECTION FROM BS 480 - 690 LBL 45 AND FABRICATED NEW SEAT TRACK SECTION FROM BAC 1520-792 APPROX DIM: 209" .5, FABRICATED SPLICE ANGLES FROM BAC 1503-100122 APPROX DIJun 3, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR FDEA201006021802Structure · corrodedCORROSION AT REINFORCEMENT CHORD, BS 1176, MAIN CABIN, LBL 46. REMOVED REINFORCEMENT CHORD BS 1176, LBL 46, IAW SRM 51-30-2 AND FABRICATED NEW REINFORCEMENT CHORD, MATERIAL PN 65-31773-1 DIM: 33" IAW DWG NR 65-31773. INSTALLED NEW REINFORCEMENT CHORD IAW IAW Jun 2, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR FDEA201006011764Fitting · corrodedCORROSION BS 740 FITTING EXTERIOR FUSELAGE KEELBEAM AREA LBL 10. REMOVED KEEL BEAM FITTING AT BS 740 LBL 10 IAW SRM 51-30-2 REV 103 AND FABRICATED FITTING FROM 70750 .190 DIM: 190" X 10 1/4' X 7" IAW DWG 69-43695 OF AND HEAT TREATED TO T6 CONDITION IAW FAS EJun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR FDEA201006011758Stringer · crackedCRACK AFT END OF STRINGER 27L AT BS 740, AC DISTRIBUTION COMPARTMENT. CUT OUT DAMAGED SECTION OF STR 27L AT BS 740, 11.5" LONG IAW SRM, REV 103, 53-10-3 FIG 1. FABRICATED STRINGER USING BAC 1498-146, 7075-T6, 11.5" LONG AND SPLICE USING BAC1498-131, 7075-T6,Jun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/StringerSDR FDEA201005311747Angle · crackedCRACKED ANGLE CHORD FALSE SPAR AT NR 8 SPOILER ACTUATOR ATTACH FITTING. CUT OUT DAMAGED SECTION OF WEB, 9.5" IAW DWG SR27-57-038, REV C. FABRICATED NEW DOUBLER USING 20245-T3, .050" X 12" X 9.7500" IAW DWG SR27-57-038, REV C. INSTALLED DOUBLER IAW DWG SR27May 31, 2010 · N267FE · Boeing 727233 · Wing Miscellaneous StructureSDR FDEA200911133948Actuator · leakingCOMPLETE LOSS OF SYS A HYDRAULICS DURING FLAP RETRACTION. FOUND ACTUATOR ABOVE TAIL SKID LEAKING OUT OF THE HSG. ORDERING NEW ACTUATOR. R&R TAIL SKID ACTUATOR PER MM 32-71-012-4 AND HAD TO ADJUST ACTUATOR PER MM 32-71- 001-5 LEAK AND OPS CKS GOOD. RAN NR 1Nov 13, 2009 · N267FE · Boeing 727233 · Trailing Edge Flap Control SystemSDR 08FDEA00336Floorbeam · damagedMAIN DECK FLOORBEAM, UPPER CHORD FWD FLG, IS MISDRILLED, BS 480, LBL 62, WL 208 ACCOMPLISHED HFEC, NO DEFECTS NOTED. APPLIED SEALANT TO AFFECTED HOLE. REF FED EX EA NR 7-5310-113134. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 31, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00333Skin · dentedAFT LOWER EXTERIOR FUSELAGE, SKIN CREASED WITH SMALL GOUGE, STA 1183 5", 2" BELOW STR 20L. REMOVED DAMAGE AREA OF SKIN. HFEC CUTOUT, NO DEFECTS NOTED. FABRICATED REPAIR DOUBLER AND FILLER, ALODINED AND PRIMED AND INSTALLED REPAIR, REF SRM 53-30-3 FIG 28 REFJan 30, 2008 · N267FE · Boeing 727233 · Fuselage Main, Plate/SkinSDR 08FDEA00330Channel · crackedMAIN CARGO DOOR SILL, HAT CHANNEL, ATTACHED TO FLOORBEAM HAS A CRACK AT FASTENER HOLE AS MARKED, LOCATED AT STA 540 8", LBL 61", WL 208". REPLACED DAMAGED HAT CHANNEL AT MAIN CARGO DOOR SILL ATTACHED TO FLOORBEAM STA 4404 TO 560 LBL61. MATERIAL IS BAC1517 Jan 30, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00279Floorbeam · corrodedCORROSION ON LOWER AFT SIDE OF FLOORBEAM TO CAP AT FLOORBOARD ATTACH FWD HOLE AT FS 720D, LBL 48, WL 208. REMOVED CORROSION AND FLOORBEAM WAS FOUND TO BE OUT OF LIMITS. FABRICATED REPAIR PARTS AND INSTALLED. REMOVED UPPER "T" CHORD CAP FROM LBL 10 - LBL 68Jan 25, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00277Skin · crackedCRACK IN UPPER RIGHT WING OUTBD PANEL AT WBL 602.5, OF OUTBD AILERON REPAIRED UPPER WING OUTBD. PANEL AT WBL 602.5 REF EA NR 7-5720-113964. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 25, 2008 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 08FDEA00257Angle · corrodedCORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL FRAME AT STA 1166 AROUND CAMLOC RECEPTACLE HOLES FRONT AND BACK SIDE. LOWER AFT CARGO COMPARTMENT REMOVED BULKHEAD SUPPORT ANGLE, IN REF TO SRM 51-30-2. VERIFIED MAT'L ID AS BAC 1506-1707 7075-T6, A 848Jan 24, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00241Rib · crackedLT WING, FWD SPAR, STA 467, LE RIB, UPPER RADIUS CRACKED. REMOVED BLEED AIR DUCT TO GAIN ACCESS. REMOVE WEB AT STA 467 ON FWD SPAR. FABRICATED WEB REF BAC DWG 65-17218, HEAT TREATED ON FORM 8130-1 NR 2008-01-075, TREATED AND PRIMED AND INSTALLED. REF SRM 5Jan 23, 2008 · N267FE · Boeing 727233 · Wing, Rib/BulkheadSDR 08FDEA00240Bracket · crackedRT WING O/B MOST UPPER TRAILING EDGE PANEL I/B SIDE SPOILER SEAL BRACKET CRACKED AT AFT EDGE AND AT SPOILER DOWN STOP PAD CUTOUT. REMOVED CRACKED BRACKET AND FABRICATED NEW SEAL DEPRESSOR BRACKET REF BOEING DRAWING 65-21657/ITEM NR 155 AND INSTALLED ON PANEL Jan 23, 2008 · N267FE · Boeing 727233 · Wing, Plate/SkinSDR 08FDEA00239Frame · corrodedLWR FWD CARGO PIT FRAME UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE STA. 720D ABOVE STR 26R. FOUND FRAME TO BE OUT OF LIMITS. CUT OUT DAMAGE AND REPAIRED FRAME. REINSTALLED Z-ANGLE, VERTICAL BULKHEAD SUPPORT IAW SRM 51-30-2 PG 1-16 SRM 51-40-2 PG 1-6, DJan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00238Frame · corrodedLWR FWD CARGO PIT FRAME, UPPER FLANGE HAS SURFACE CORROSION, AFT SIDE OF STA 720D ABOVE STR 26L. FRAME DAMAGE FOUND TO BE OUT OF LIMITS, CUT OUT DAMAGE, FABRICATED REPAIR DOUBLER AND FILLER. REMOVED AND REINSTALLED Z-ANGLE, BULKHEAD SUPPORT AND INTERCOSTAL TO Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00236Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER "T" CAP CORRODED, BS 950D, RBL 9-23 THIS SDR WAS ENTERED IN ERROR AND WILL NOT BE USED. THIS IS A DUPLICATE OF SDR NR 08-0235. THIS SDR ENTERED IN ERROR - ADMINISTRATOR.Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00235Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, RBL 9-23. REMOVED CORROSION. OUT OF LIMITS IAW SM 53-10-8, SRM 51-10-6. DISPLACED SEAT TRACK BS 950-950F RBL 25 IAW SRM 51-30- 2. REMOVED CHANNEL STIFFNER BS 950D, RBL 25. REMOVED CHANNEL SUPPORT BS 950DJan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00234Floorbeam · corrodedMAIN DECK FLOORBEAM UPPER TEE CAP CORRODED, BS 950D, LBL 10-13. REMOVED CORROSION. FOUND OUT OF LIMITS IAW PF SRM 53-10-1 FIG 4C. REPAIRED DAMAGED FLOORBEAM IAW SRM 53-10-8 PG 18 FIG 3 UPPER CHORD REPAIR. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor BeamSDR 08FDEA00233Seat Track · corrodedSEAT TRACK CORRODED, STA 880-950, RBL 47 REMOVED CORROSION, FOUND TO BE OUT OF LIMITS, REMOVED SEAT TRACK. FABRICATED NEW SEAT TRACK, ALODINED AND PRIMED AND INSTALLED AT STA 870-950. REF BAC DWG 65-19601, SRM 51-10-2, SRM 51-30-2. REMOVED FUEL SHROUD IN W/Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach FittingsSDR 08FDEA00221Intercostal · crackedLEFT LOWER FUSELAGE "B" SYSTEM HYD COMPARTMENT HYDRAULIC LINE SUPPORT INTERCOSTAL CRACKED 3 AREAS IN RADIUS, STA 950A PLUS 4, TO 950A PLUS 7 JUST O/B OF RESERVOIR REMOVED CRACKED INTERCOSTAL, FABRICATED NEW INTERCOSTAL, P/N 69-14299-1. TREATED AND PRIMED, AJan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00220Rib · crackedNR 2 FLAP TRACK MID FRG AFT RIB IS CRACKED REMOVED CRACKED RIB REF SRM 51-30-2 P1, PRIMED AND PAINT FLAP TRACK FRG, REF 51-10-2 PG 1-4. INSTALLED REPLACEMENT RIB REF SRM 51-30-2 P 1-3. THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 22, 2008 · N267FE · Boeing 727233 · Wing, Rib/BulkheadSDR 08FDEA00219Frame · corrodedCORROSION AT SEVERAL AREAS ON AFT WALL GILL LINER PANEL UPPER FRAME AT STA 1166, AROUND CAM LOC RECEPTACLE HOLES FRONT AND BACK FABRICATED UPPER FRAME AT STA 1166 WL 200, AFT CARGO COMP BULKHEAD, REF SRM 51-30-2 PG 4. REF BOEING DWG 65-67250-5 SHEET 1-5. THJan 22, 2008 · N267FE · Boeing 727233 · Fuselage Main, FrameSDR 08FDEA00218Stringer Clip · tornCABIN BS 660, S 5L STRINGER CLIP TORN. REMOVED STRINGER CLIP, TRANSFERRED HOLD TO NEW CLIP. INSTALLED NEW STRINGER CLIP REF SRM 51-30-2. THIS IS CLASSIFIED AS A MAJOR REPAIR.Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Main, Attach FittingsSDR 08FDEA00217Floor Support · crackedAFT CARGO PIT CAP STRIP, 950D TO 990 LT, CRACKED AT FASTENER HOLE FABRICATED NEW CAP STRIP. REF BOEING DWG NR 65-67278/SRM 51-20-1 FIG 2/SRM 51-10-1, PG 12. TREATED AND PRIMED CAP STRIP, REF SRM 51-10-2 PG 1, THIS IS CLASSIFIED AS MINOR REPAIR.Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00216Intercostal · corrodedMAIN CARGO DECK INTERCOSTAL CORRODED, BS 1030-1050, LBL 19 REMOVED CORROSION AND FOUND OUT OF LIMITS. MATERIAL THICKNESS IS .071". REMAINING MATERIAL IS .051", AND MATERIAL LOSS AT .019'' REF SRM 53-10-1. BACKED DRILLED NEW INTERCOSTAL AT BS 1030-1050, LJan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous StructureSDR 08FDEA00212Bracket · crackedRT WING, NR 6 FLAP TRACK FAIRING, O/B SKATE ANGLE ATTACH BRACKET, CRACKED AT I/B AFT SIDE REMOVED RT WING NR 6, FLAP TRACK FAIRING O/B SKATE ANGLE ATTACH BRACKET I/B AFT SIDE IAW SRM 51-30-2 PG3, VERIFIED MATERIAL AS MATERIAL 2024-T3 .071" IAW DWG 65-28115-5 SJan 22, 2008 · N267FE · Boeing 727233 · Wing Miscellaneous StructureSDR 08FDEA00211Link · corrodedMAIN DECK 1L DR CUTOUT LWR HINGE RADIUS LINK IS CORRODED. INSTALLED NEW RADIUS LINK, REF MM 52-11-001-PG 2, OPS CHECKED GOOD THIS IS CLASSIFIED AS A MINOR REPAIR.Jan 22, 2008 · N267FE · Boeing 727233 · Passenger/Crew Doors
Back to N267FE, cancelled Oct 12, 2012