# Service difficulty reports: N267FE, cancelled Oct 12, 2012

A list on [N267FE, cancelled Oct 12, 2012](https://openairdocs.org/deregistered/N267FE-2012-10-12.md).

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

Page 1 of 3 · 121 reports

- [SDR FDEA201205031738](https://openairdocs.org/sdr/FDEA201205031738.md): Light · detached · May 3, 2012 · N267FE · Boeing 727233 · Emergency Lighting
  > EMERGENCY 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.
- [SDR FDEA201006152020](https://openairdocs.org/sdr/FDEA201006152020.md): Stringer · corroded · Jun 15, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION 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" LO
- [SDR FDEA201006142002](https://openairdocs.org/sdr/FDEA201006142002.md): Rib · gouged · Jun 14, 2010 · N267FE · Boeing 727233 · Leading Edge Devices
  > UPON 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" & IN
- [SDR FDEA201006142000](https://openairdocs.org/sdr/FDEA201006142000.md): Rib · gouged · Jun 14, 2010 · N267FE · Boeing 727233 · Leading Edge Devices
  > UPON 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
- [SDR FDEA201006121972](https://openairdocs.org/sdr/FDEA201006121972.md): Skin · damaged · Jun 12, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > UPON 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, DIMENSIONS
- [SDR FDEA201006101937](https://openairdocs.org/sdr/FDEA201006101937.md): Web · cracked · Jun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT 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 I
- [SDR FDEA201006101936](https://openairdocs.org/sdr/FDEA201006101936.md): Web · cracked · Jun 10, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT 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 BOX
- [SDR FDEA201006101946](https://openairdocs.org/sdr/FDEA201006101946.md): Shear Tie · cracked · Jun 10, 2010 · N267FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > CRACKED 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.
- [SDR FDEA201006091908](https://openairdocs.org/sdr/FDEA201006091908.md): Stringer · cracked · Jun 9, 2010 · N267FE · Boeing 727233 · Wing, Longeron/Stringer
  > RT 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 7-5710
- [SDR FDEA201006091917](https://openairdocs.org/sdr/FDEA201006091917.md): Skin · corroded · Jun 9, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION 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 51-10-6
- [SDR FDEA201006081873](https://openairdocs.org/sdr/FDEA201006081873.md): Seat Track · corroded · Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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
- [SDR FDEA201006081871](https://openairdocs.org/sdr/FDEA201006081871.md): Skin · gouged · Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN 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 C
- [SDR FDEA201006081900](https://openairdocs.org/sdr/FDEA201006081900.md): Intercostal · corroded · Jun 8, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR FDEA201006071859](https://openairdocs.org/sdr/FDEA201006071859.md): Skin · corroded · Jun 7, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > CORROSION 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 SRM
- [SDR FDEA201006051840](https://openairdocs.org/sdr/FDEA201006051840.md): Floorbeam · corroded · Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION 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:
- [SDR FDEA201006051839](https://openairdocs.org/sdr/FDEA201006051839.md): Floorbeam · corroded · Jun 5, 2010 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION 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: 11
- [SDR FDEA201006041825](https://openairdocs.org/sdr/FDEA201006041825.md): Fitting · corroded · Jun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > CORROSION 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.
- [SDR FDEA201006041821](https://openairdocs.org/sdr/FDEA201006041821.md): Stringer · corroded · Jun 4, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION 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-T
- [SDR FDEA201006031833](https://openairdocs.org/sdr/FDEA201006031833.md): Skin · damaged · Jun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > MAIN 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", FABRICAT
- [SDR FDEA201006031812](https://openairdocs.org/sdr/FDEA201006031812.md): Stringer · corroded · Jun 3, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION 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 WITH
- [SDR FDEA201006031810](https://openairdocs.org/sdr/FDEA201006031810.md): Angle · cracked · Jun 3, 2010 · N267FE · Boeing 727233 · Trailing Edge Flaps
  > RT 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.
- [SDR FDEA201006031809](https://openairdocs.org/sdr/FDEA201006031809.md): Structure · cracked · Jun 3, 2010 · N267FE · Boeing 727233 · Leading Edge Devices
  > NR 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.
- [SDR FDEA201006031801](https://openairdocs.org/sdr/FDEA201006031801.md): Seat Track · corroded · Jun 3, 2010 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION 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 DI
- [SDR FDEA201006021802](https://openairdocs.org/sdr/FDEA201006021802.md): Structure · corroded · Jun 2, 2010 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION 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
- [SDR FDEA201006011764](https://openairdocs.org/sdr/FDEA201006011764.md): Fitting · corroded · Jun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > CORROSION 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 E
- [SDR FDEA201006011758](https://openairdocs.org/sdr/FDEA201006011758.md): Stringer · cracked · Jun 1, 2010 · N267FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CRACK 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,
- [SDR FDEA201005311747](https://openairdocs.org/sdr/FDEA201005311747.md): Angle · cracked · May 31, 2010 · N267FE · Boeing 727233 · Wing Miscellaneous Structure
  > CRACKED 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 SR27
- [SDR FDEA200911133948](https://openairdocs.org/sdr/FDEA200911133948.md): Actuator · leaking · Nov 13, 2009 · N267FE · Boeing 727233 · Trailing Edge Flap Control System
  > COMPLETE 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 1
- [SDR 08FDEA00336](https://openairdocs.org/sdr/08FDEA00336.md): Floorbeam · damaged · Jan 31, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR 08FDEA00333](https://openairdocs.org/sdr/08FDEA00333.md): Skin · dented · Jan 30, 2008 · N267FE · Boeing 727233 · Fuselage Main, Plate/Skin
  > AFT 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 REF
- [SDR 08FDEA00330](https://openairdocs.org/sdr/08FDEA00330.md): Channel · cracked · Jan 30, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > MAIN 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
- [SDR 08FDEA00279](https://openairdocs.org/sdr/08FDEA00279.md): Floorbeam · corroded · Jan 25, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > CORROSION 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 68
- [SDR 08FDEA00277](https://openairdocs.org/sdr/08FDEA00277.md): Skin · cracked · Jan 25, 2008 · N267FE · Boeing 727233 · Wing, Plate/Skin
  > CRACK 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.
- [SDR 08FDEA00257](https://openairdocs.org/sdr/08FDEA00257.md): Angle · corroded · Jan 24, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > CORROSION 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 848
- [SDR 08FDEA00241](https://openairdocs.org/sdr/08FDEA00241.md): Rib · cracked · Jan 23, 2008 · N267FE · Boeing 727233 · Wing, Rib/Bulkhead
  > LT 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 5
- [SDR 08FDEA00240](https://openairdocs.org/sdr/08FDEA00240.md): Bracket · cracked · Jan 23, 2008 · N267FE · Boeing 727233 · Wing, Plate/Skin
  > RT 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
- [SDR 08FDEA00239](https://openairdocs.org/sdr/08FDEA00239.md): Frame · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Frame
  > LWR 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, D
- [SDR 08FDEA00238](https://openairdocs.org/sdr/08FDEA00238.md): Frame · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Frame
  > LWR 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
- [SDR 08FDEA00236](https://openairdocs.org/sdr/08FDEA00236.md): Floorbeam · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR 08FDEA00235](https://openairdocs.org/sdr/08FDEA00235.md): Floorbeam · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN 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 950D
- [SDR 08FDEA00234](https://openairdocs.org/sdr/08FDEA00234.md): Floorbeam · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage Main, Floor Beam
  > MAIN 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.
- [SDR 08FDEA00233](https://openairdocs.org/sdr/08FDEA00233.md): Seat Track · corroded · Jan 23, 2008 · N267FE · Boeing 727233 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT 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/
- [SDR 08FDEA00221](https://openairdocs.org/sdr/08FDEA00221.md): Intercostal · cracked · Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > LEFT 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, A
- [SDR 08FDEA00220](https://openairdocs.org/sdr/08FDEA00220.md): Rib · cracked · Jan 22, 2008 · N267FE · Boeing 727233 · Wing, Rib/Bulkhead
  > NR 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.
- [SDR 08FDEA00219](https://openairdocs.org/sdr/08FDEA00219.md): Frame · corroded · Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Main, Frame
  > CORROSION 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. TH
- [SDR 08FDEA00218](https://openairdocs.org/sdr/08FDEA00218.md): Stringer Clip · torn · Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Main, Attach Fittings
  > CABIN 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.
- [SDR 08FDEA00217](https://openairdocs.org/sdr/08FDEA00217.md): Floor Support · cracked · Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > AFT 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.
- [SDR 08FDEA00216](https://openairdocs.org/sdr/08FDEA00216.md): Intercostal · corroded · Jan 22, 2008 · N267FE · Boeing 727233 · Fuselage Miscellaneous Structure
  > MAIN 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, L
- [SDR 08FDEA00212](https://openairdocs.org/sdr/08FDEA00212.md): Bracket · cracked · Jan 22, 2008 · N267FE · Boeing 727233 · Wing Miscellaneous Structure
  > RT 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 S
- [SDR 08FDEA00211](https://openairdocs.org/sdr/08FDEA00211.md): Link · corroded · Jan 22, 2008 · N267FE · Boeing 727233 · Passenger/Crew Doors
  > MAIN 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.

Next page: https://openairdocs.org/deregistered/N267FE-2012-10-12/reports.md?page=2

## The whole list in SQL

Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS:

```sql
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
```

This list as a web page: https://openairdocs.org/deregistered/N267FE-2012-10-12/reports

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