# Service difficulty reports: N233FE, cancelled Apr 25, 2013

A list on [N233FE, cancelled Apr 25, 2013](https://openairdocs.org/deregistered/N233FE-2013-04-25.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 · 127 reports

- [SDR FDEA201302190372](https://openairdocs.org/sdr/FDEA201302190372.md): Slide · dislodged · Feb 19, 2013 · N233FE · Boeing 727247 · Escape Slide
  > GROUND CREW OPENED DOOR ON BLOCK IN DEPLOYING ESCAPE SLIDE. FOUND SLIDE OUT OF THE STORAGE COMPARTMENT. REPOSITIONED THE SLIDE BACK IN THE STORAGE COMPARTMENT IAW MM 25-60-015-2.
- [SDR FDEA201212044244](https://openairdocs.org/sdr/FDEA201212044244.md): Bracket · broken · Dec 4, 2012 · N233FE · Boeing 727247 · Emergency Equipment
  > THE GIRT BAR BRACKET BROKE WHILE DISARMING THE SLIDE. REPLACED BRACKET IAW SMP, CHECKED GOOD.
- [SDR FDEA201110024267](https://openairdocs.org/sdr/FDEA201110024267.md): Battery · inoperative · Oct 2, 2011 · N233FE · Boeing 727247 · Emergency Lighting
  > EMERGENCY ESCAPE SLIDE LIGHT INOPERATIVE. R & R EMERGENCY ESCAPE SLIDE LIGHT BATTERY IAW AMM 33-50-121-2.
- [SDR FDEA201107112642](https://openairdocs.org/sdr/FDEA201107112642.md): Light · inoperative · Jul 11, 2011 · N233FE · Boeing 727247 · Emergency Lighting
  > EMERGENCY EXIT LIGHT ABOVE ENTRY DOOR 1L DOES NOT TEST. REPLACED BATTERIES. NO HELP. REPLACED LIGHT ASSY AND BATTERIES. OPS CHECKED GOOD IAW AMM33-50-101. PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA201103211106](https://openairdocs.org/sdr/FDEA201103211106.md): Control Valve · leaking · Mar 21, 2011 · N233FE · Boeing 727247 · Hydraulic System, Main
  > LOSS OF ALL SYS "A" HYD FLUID ON FLAPS 2 DEGREES SELECTION. PERFORM APPROPRIATE CHECKLISTS. REGAINED 1.2 GALLONS OF SYS A FLUID ON MANUAL GEAR EXTENSION. FOUND LWR RUDDER LOAD-LIMITING CONTROL VALVE LEAKING AT SEAL. R & R LOAD LIMITING CONTROL VALVE REF A
- [SDR FDEA201012124646](https://openairdocs.org/sdr/FDEA201012124646.md): Seat Track · corroded · Dec 12, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORRODED SEAT TRACK FLANGE STA 580-600, RBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792, 7178-T6511, DIMS 17' 5.3750", FABRICATED 2 SPLICES USING BAC1503-100122 DIMS 15.1250" AND 14.5", FABRICATED STRAP USING 7075T6.250
- [SDR FDEA201012124643](https://openairdocs.org/sdr/FDEA201012124643.md): Floorbeam · corroded · Dec 12, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TOP "T" CAP STA 720D, RBL 45- LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED UPPER CHORD, ANGLES AND STRAPS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.
- [SDR FDEA201012114636](https://openairdocs.org/sdr/FDEA201012114636.md): Skin · cracked · Dec 11, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > FS 359 STR 28L EXTERNAL REPAIR CRACKED. CUT OUT DAMAGED SKIN AREA, FABRICATED REPAIR DOUBLER AND FILLER AND INSTALLED IAW EA 7-5330-123573.
- [SDR FDEA201012114639](https://openairdocs.org/sdr/FDEA201012114639.md): Floorbeam · corroded · Dec 11, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950B, RBL 25- 45. CUT OUT DAMAGED AREA, FABRICATED REPAIR ANGLES, FILLERS AND INSTALLED IAW SRM 53-10-8 AND SRM 51-30-2.
- [SDR FDEA201012094620](https://openairdocs.org/sdr/FDEA201012094620.md): Floorbeam · corroded · Dec 9, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950D, BL 0 TO RBL 25. CUT OUT DAMAGED AREA OF UPPER FLANGE, DIM (3 3/4" X 1") IAW SRM 53-10-8 FIG 8. FABRICATED 2EA ANGLES USING BAC1490-2888 7075-T6 (13 1/4" X 3") AND (9 1/4" X 3") AND 1EA FILLER USING BAC1
- [SDR FDEA201012084619](https://openairdocs.org/sdr/FDEA201012084619.md): Floorbeam · corroded · Dec 8, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION ON UPPER FLANGE OF FLOORBEAM AT BS 660, LBL 10. CUTOUT DAMAGED AREA APPROX DIM: 3" X 2" AND FABRICATED UPPER CHORD FROM BAC1505- 160617-7075T7 APPROX DIM: 16" LONG, FABRICATED 2 EA. ANGLES MATERIAL USED BAC1490 2785 7075T6 APPROX DIM: 16" X 2 3/4
- [SDR FDEA201012084618](https://openairdocs.org/sdr/FDEA201012084618.md): Stringer · corroded · Dec 8, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION IN STRINGER 27L, FROM BS 1080 TO 1110. CUT OUT DAMAGED SECTION OF STR 27L, 21" LONG IAW SRM 53-10-3 FIG 1 REV 103 FABRICATED STRINGER SECTION FROM BAC1498-145, 7075 T62 21" LONG AND 2 SPLICES FROM BAC1498-131, 7075 T6 14 1/4" X 14 3/8" LON
- [SDR FDEA201012074611](https://openairdocs.org/sdr/FDEA201012074611.md): Floorbeam · corroded · Dec 7, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE OF FLOORBEAM, BS 950D BL 0 TO LBL 25. CUT OUT DAMAGED AREA, FABRICATED NEW FLOORBEAM REPAIR IAW SRM 53-10-8 FIG 3 AND SRM 51-30-2 REV 103
- [SDR FDEA201012064638](https://openairdocs.org/sdr/FDEA201012064638.md): Seat Track · corroded · Dec 6, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 950, PLUS 10" - STA 1010, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-7927178-T65, DIMS 270" AND INSTALLED IAW SRM 53-10-5 AND SRM 51-30-2.
- [SDR FDEA201012044602](https://openairdocs.org/sdr/FDEA201012044602.md): Shear Tie · corroded · Dec 4, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > UPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STA 1148 FRAME, STRINGER 27L TO 26L. REMOVED SHEAR TIE ON AFT SIDE OF BS1148 FRAME BETWEEN STRINGER 27L AND 26L IAW SRM, REV 103, 51-30-2. FABRICATED SHEAR TIE USING 7075-0,.063" X 2" X 6" IAW SRM 51-20-1,
- [SDR FDEA201012044601](https://openairdocs.org/sdr/FDEA201012044601.md): Shear Tie · corroded · Dec 4, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > UPON REMOVAL, FOUND SHEAR TIE CORRODED - AFT SIDE OF STATION 1148 FRAME, STRINGER 26L TO 25L. REMOVED SHEAR TIE FROM AFT SIDE OF BS 1148 FRAME BETWEEN STRINGER 26L AND 25L IAW SRM REV 103, 51-30-2. FORMED SHEAR TIE USING 7075-0,.063" X 2" X 4" IAW SRM 51-2
- [SDR FDEA201012034640](https://openairdocs.org/sdr/FDEA201012034640.md): Seat Track · corroded · Dec 3, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA 848 - STA 765, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1506-1108-7075T6 DIMS 9.2', AND INSTALLED IAW DWG 65-16279 AND SRM 51-30-2.
- [SDR FDEA201012034562](https://openairdocs.org/sdr/FDEA201012034562.md): Flap Track · cracked · Dec 3, 2010 · N233FE · Boeing 727247 · Trailing Edge Flaps
  > RT INBD FLAP CUTOUT FOR AFT FLAP NR 2 TRACK CRACKED, WS 200. REMOVED R/H I/B MIDFLAP LOWER AFT CHORD IAW SRM 51-30-2 FABRICATED LOWER CHORD 3 SECTIONS FROM BAC1503-100046 7075 T6 47.5", 32.25" AND 96.75" LONG AND 2 SPLICES FROM BAC1503-100046 7075 T6
- [SDR FDEA201012034560](https://openairdocs.org/sdr/FDEA201012034560.md): Shear Tie · corroded · Dec 3, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION - AFT SIDE OF FRAME SHEAR TIE, STATION 1148, STRINGER 28R TO STRINGER 27R. REMOVED SHEAR TIE FROM BS 1148 FRAME AFT SIDE BETWEEN STR 28R AND 27R IAW SRM 51-30-2 REV 103, FABRICATED SHEAR TIE FROM 7075 O.063" X 6" X 3" IAW SRM 51--20-1 FIG 7, INS
- [SDR FDEA201012034576](https://openairdocs.org/sdr/FDEA201012034576.md): Stringer · misrepaired · Dec 3, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > FS 680, STR 28R STRINGER REPAIR. REPAIR NON COMPLIANT IAW SRM 53-10-3. REMOVED EXISTING REPAIR, FABRICATED NEW STRINGER USING BAC1498-142 7075T-62 DIMS 27", FABRICATED REPAIR SPLICE USING BAC1458-132 7075T-6 DIMS 12" IAW SRM 53-10-2 AND SRM 53-10-3, FABRICATE
- [SDR FDEA201012034556](https://openairdocs.org/sdr/FDEA201012034556.md): Support Angle · cracked · Dec 3, 2010 · N233FE · Boeing 727247 · Vertical Stabilizer Miscellaneous Structure
  > VERTICAL STAB INTERIOR AT BS 1343 HAS CRACK INDICATION ON RT UPPER WEB SUPPORT ANGLE, UNDERNEATH. REMOVED CRACKED SHEAR TIE. FABRICATED NEW SHEAR TIE USING 2024T-3.050 DIMS 7 1/8" X 3 3/4" AND INSTALLED IAW SRM 51-20-1, SRM 55-30-2 AND SRM 51-30-2.
- [SDR FDEA201012034579](https://openairdocs.org/sdr/FDEA201012034579.md): Floorbeam · corroded · Dec 3, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION "T" CAP FLOORBEAM STA 328 LBL 50 - BL 0. CUTOUT DAMAGED SECTION SIZE 3" AT STA 328 AT LBL 10- LBL 13 IAW SRM 53-10-8, FIG 9. FABRICATED FILLER FROM BAC 1505-100246-7075-T6 SIXE 3" AND 4 EA SPLICE ANGLES FROM 7075-O.071 SIZES 13" X 2.2500" (2 EA) AN
- [SDR FDEA201012024538](https://openairdocs.org/sdr/FDEA201012024538.md): Skin · bulged · Dec 2, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > BULGE EXTERIOR SKIN STA 720E- 720F STR 23R. CUT OUT DAMAGED PORTION OF STRINGER 23R, BS 720E PLUS 10" TO 720F PLUS 10" IAW SRM 53-10-3 FIG 1. FABRICATED TWO PORTIONS OF STRINGER USING BAC1498-142-7075T62 DIMENSIONS 17 7/8" AND 8 5/8", AND FABRICATED TWO SPLI
- [SDR FDEA201012014637](https://openairdocs.org/sdr/FDEA201012014637.md): Stringer · corroded · Dec 1, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION RT WHEEL WELL OTBD SIDE STA 880, STR 18A. REMOVED DAMAGED STR 18A SHELF, FABRICATED NEW STR 18A SHELF AND INSTALLED IAW SRM 51-30-2, SRM 53-10-2, SRM 51-20-1 AND SRM 51-30-5.
- [SDR FDEA201011304528](https://openairdocs.org/sdr/FDEA201011304528.md): Floorbeam · corroded · Nov 30, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM, STA 312 TEE CAP TOP LBL 55 - BL 0 L1 ENTRY. CUTOUT DAMAGED SECTION DIM: 3 1/2" IAW SRM 53-10-8 FIG 9 AND FABRICATED 4 EA. ANGLES FROM 7075-O.071 SIZES 15" X 2 3/4" AND 2 EA. 13" X 2 3/4" HEAT TREATED TO T6 CONDITION IAW ENG REPORT 2-371
- [SDR FDEA201011304520](https://openairdocs.org/sdr/FDEA201011304520.md): Floorbeam · corroded · Nov 30, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION FLOORBEAM TEE CAP TOP MAIN CABIN STA. 480 RBL 45 - 61 REMOVED CORROSION AT BS 480 RBL 45 - 61 AREA FOUND TO BE OUT OF LIMITS, CUTOUT DAMAGED AREA AT RBL 51. DIM: 2.5" X.90", FABRICATED NEW ANGLE REPAIRS ( 2 EACH) FROM BAC 1490-2888 7075T6. DIM: 16
- [SDR FDEA201011304525](https://openairdocs.org/sdr/FDEA201011304525.md): Skin · dented · Nov 30, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > DENTED EXTERIOR FUSELAGE STA. 1090 - 1110 S22-23R. CUTOUT DAMAGE AREA AND FABRICATED REPAIR DOUBLER IAW SRM 53-30-3 FIG 1. INSTALLED DOUBLER IAW SRM 51-30-2.
- [SDR FDEA201011304524](https://openairdocs.org/sdr/FDEA201011304524.md): Skin · cracked · Nov 30, 2010 · N233FE · Boeing 727247 · Trailing Edge Flaps
  > LT WING INBD AFT FLAP HAS CRACK ON LOWER SKIN AT FASTENER, WBL 203. REMOVED 6 EA FASTENERS AT AREA LT WING INBD AFT FLAP LOWER SKIN IAW SRM 51-30-2. FABRICATED REPAIR PLATE IAW SRM 57-50-4, FIG 5 AND INSTALLED REPAIR PLATE IAW SRM 51-30-2 AND 57-50-4, FIG 5
- [SDR FDEA201011304519](https://openairdocs.org/sdr/FDEA201011304519.md): Seat Track · corroded · Nov 30, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE STA. 848 - STA. 765 LBL 45. REMOVED DAMAGED SEAT TRACK TEE AND FABRICATED NEW TEE FROM BAC 1506-1108-7075T6, AND INSTALLED IAW SRM 51-30-2, SRM 51-30-5, SRM 51-10-2, & DWG NR 65-16279.
- [SDR FDEA201011294508](https://openairdocs.org/sdr/FDEA201011294508.md): Seat Track · corroded · Nov 29, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE MAIN CABIN STA 950 PLUS 10" TO STA 890, LBL 25. REMOVED DAMAGED SEAT TRACK SECTION. FABRICATED NEW SECTION USING BAC1520-792 7178T65 DIMS 3 1/4" X 69 1/2", FABRICATED 2 SPLICES USING BAC1503-100122 7178T6 DIMS 13 3/4" X 2 1/2" EA
- [SDR FDEA201011294514](https://openairdocs.org/sdr/FDEA201011294514.md): Shear Tie · corroded · Nov 29, 2010 · N233FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > CORROSION - FRAME SHEAR TIE FORWARD FLANGE, STATION 1148, STRINGER 27L TO STRINGER 26L. REMOVED CORROSION FROM SHEAR TIE WITH A MATERIAL LOSS OF.004, FOUND TO BE WITHIN LIMITS IAW SRM 53-10-1. TREATED AND PRIMED AREA IAW SRM 51-10-2.
- [SDR FDEA201011294513](https://openairdocs.org/sdr/FDEA201011294513.md): Skin · cracked · Nov 29, 2010 · N233FE · Boeing 727247 · Vertical Stabilizer, Plate/Skin
  > VERT STAB INTERIOR AT BS 1303 VERT FRAME HAS 3 EA CRACKS ON LWR LT & RT WEB. CUTOUT DAMAGED AREAS AND FABRICATED REPAIR DOUBLERS & FILLERS & INSTALLED REPAIR DOUBLERS 2 EA & FILLERS 2 EA AT VERT STAB BS 1303 VERT FRAME WEB IAW SRM 53-10-9, FIG 4, SRM 55-30-2
- [SDR FDEA201011294507](https://openairdocs.org/sdr/FDEA201011294507.md): Seat Track · corroded · Nov 29, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK FLANGE, MAIN CABIN STA 950 PLUS 10" TO STA 870, RBL 45. REMOVED SEAT TRACK SECTION. FABRICATED NEW SEAT TRACK & INSTALLED IAW SRM 53-10-5, FIG 1AND SRM 51-30-2, REV 103.
- [SDR FDEA201011284515](https://openairdocs.org/sdr/FDEA201011284515.md): Floorbeam · corroded · Nov 28, 2010 · N233FE · Boeing 727222 · Fuselage Main, Floor Beam
  > CORROSION TOP "T" CAP FLOORBEAM STA 440, BL 0 - LBL 25, MAIN CABIN CUTOUT DAMAGE AREA AT FLOORBEAM BS 440, LBL 10 IAW SRM 53-10-8 FIG 8, FABRICATED (2) ANGLES REPAIR IAW SRM 53-10-8 FIG 8, & INSTALLED NEW ANGLES REPAIR AT LBL 5 - LBL 13 BS 440 IAW SRM 53-1
- [SDR FDEA201011264509](https://openairdocs.org/sdr/FDEA201011264509.md): Floorbeam · corroded · Nov 26, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION TOP "T" CAP MAIN CABIN STA 440, LBL 61- LBL 45 CUTOUT DAMAGE AREA IAW SRM 53-10-8, FIG 8, FABRICATED (2) ANGLES REPAIR FROM BAC 1490-2888-7075T6, & FILLER FROM 2024T3.125 IAW SRM 53-10-8, FIG 8, INSTALLED NEW REPAIR AT LBL 45 - LBL 61, BS 440 IAW S
- [SDR FDEA201011234475](https://openairdocs.org/sdr/FDEA201011234475.md): Shear Tie · corroded · Nov 23, 2010 · N233FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 720D (AFT SIDE OF FRAME) RBL 5 CUT OUT DAMAGED SHEAR TIE AT BS 720D RBL 5 IAW B727 SRM REV 103, 53-10-4 FIG 15. FABRICATED SHEAR TIE USING 7075-0,.071" X 2" X 4.7500" IAW SRM 53-10-4, FIG 15. INSTALLED SHEAR TIE IAW SRM 53-10-4
- [SDR FDEA201011234478](https://openairdocs.org/sdr/FDEA201011234478.md): Stringer · gouged · Nov 23, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > GOUGE INSIDE CHANNNEL - STRINGER 30, BETWEEN STA 950A - 950B. BLENDED GOUGE INSIDE STRINGER 30 BETWEEN BS950A- 950B IAW SRM REV 103, 51-10-1. C/W UT THICKNESS IAW NDTM, PT4, 51-00-00 FIG 2. ORIGINAL.130", REMOVED.027", REMAINING.103". FOUND TO BE WITHIN LI
- [SDR FDEA201011234467](https://openairdocs.org/sdr/FDEA201011234467.md): Duct · dented · Nov 23, 2010 · N233FE · Boeing 727247 · Engine Air Intake System
  > #2 ENGINE INLET "S" DUCT INTERIOR HAS DENT AT BS 1320, 9 O'CLOCK POSITION. CUTOUT DAMAGED AREA OF SKIN, CUTOUT CHANNEL SECTION, FABRICATED DOUBLER PLATE, FILLER PLATED, SHIMS, FABRICATED RIB REPAIR CHANNEL AND TWO ANGLES, LOCATED & DRILLED PARTS, TREATED A
- [SDR FDEA201011234480](https://openairdocs.org/sdr/FDEA201011234480.md): Stringer · corroded · Nov 23, 2010 · N233FE · Boeing 727233 · Fuselage Main, Longeron/Stringer
  > CORROSION - INSIDE CHANNEL, STRINGER 22R, FWD SIDE OF STA 1166 FRAME. REMOVED SECTION OF STRINGER 22R, 23" IN LENGTH IAW SRM, REV 103, 53-10-3, FIG 1. FABRICATED STRINGER SECTION USING BAC1498-144, 7075-T6, 23" IN LENGTH AND STRAP USING 2024-T3,.125" X 1" X
- [SDR FDEA201011234479](https://openairdocs.org/sdr/FDEA201011234479.md): Shear Tie · corroded · Nov 23, 2010 · N233FE · Boeing 727233 · Fuselage Internal Mounting Structure
  > CORROSION - FWD LOWER FLANGE OF FRAME 950B, SHEAR TIE, BETWEEN STRINGER 30 AND STRINGER 29R. CUT OUT DAMAGED AREA OF SHEAR TIE IAW SRM, REV 103, 53-10-4, FIG 12. FABRICATED SHEAR TIE, & FILLER IAW SRM 53-10-4, FIG 12 AND 53-10-2, FIG 5. INSTALLED SHEAR TIE
- [SDR FDEA201011224457](https://openairdocs.org/sdr/FDEA201011224457.md): Skin · corroded · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > UPON REMOVAL STRINGER 27L STA. 1015 FOUND CORROSION ON INTERIOR SKIN. CUT OUT 2 AREAS AT BS 1010 STRINGER 28L DIM 10" X 5 7/8", AND BS 1010 STRINGER 27L DIM 7 1/2" X 3 1/4" IAW SRM 53-30-3 FIG 3A. FABRICATED DOUBLER USING 2024-T3.080", DIM 21 1/2" X 14 1/2
- [SDR FDEA201011224455](https://openairdocs.org/sdr/FDEA201011224455.md): Stringer · corroded · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION - INSIDE STRINGER 27L, STA 1010 - 1030. REMOVED STRINGER SECTION AND 2EA SPLICES FROM BS 1010 TO 1040 IAW SRM 51-30- 2. FABRICATED STRINGER USING BAC1498-145, 7075-T62, 29" IN LENGTH IAW SRM 53-10-3 FIG 1 AND 51-30-5. INSTALLED STRINGER SECTIN AND 2
- [SDR FDEA201011224460](https://openairdocs.org/sdr/FDEA201011224460.md): Stringer Splice · corroded · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > AFT PIT STRINGER SPLICE CORRODED BS 1124 TO BS 1136 STR 30 CUT OUT DAMAGED STRINGER DIM.19" IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER SECTION USING BAC1448-147, 7075T6 19" IN LENGTH AND SPLICES (2EA) USING BAC1498-131- 7075T6 10 1/4" LONG EA IAW SRM 53-10-3
- [SDR FDEA201011224459](https://openairdocs.org/sdr/FDEA201011224459.md): Stringer · corroded · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION STRINGER 30 AT STA 1166, EXTERIOR SIDE OF LT CHANNEL RISER. REMOVED STRINGER SECTION FROM STATION 1142 TO 1183 AND 1EA SPLICE IAW SRM 51-30-2. FABRICATED 2 STRINGER REPAIR SECTIONS USING BAC1498-147 7075T6 19" LONG AND 19 1/2" LONG AND 2 SPLICES U
- [SDR FDEA201011224458](https://openairdocs.org/sdr/FDEA201011224458.md): Frame · dented · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Frame
  > FWD PIT UPPER FLANGE OF FRAME IS DENTED AT BS 720, RBL 35. CUT OUT DAMAGE AREA DIMENSION 1" X 1 1/2" IAW SRM 51-40-3 FIG 1. FABRICATED FRAME REPAIR USING 7075-0,.063" IAW SRM 51-40-3 FIG 1 AND 53-10-2 FIG 3. LOCATED AND DRILLED FRAME REPAIR DIMENSION 8 7/
- [SDR FDEA201011224456](https://openairdocs.org/sdr/FDEA201011224456.md): Stringer · corroded · Nov 22, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION INSIDE STRINGER 27L, STA 950D - 1010. REMOVED SECTION OF STRINGER IAW SRM REV 103 51-30-2 AND 53-10-3, FIG 1 FABRICATED STRINGER SECTIONS, & SPLICES IAW SRM 53-10-3, FIG 1 AND 53-10-2, FIG 9 INSTALLED STRINGER AND SPLICES IAW SRM 51-30-2 AND 51-10-
- [SDR FDEA201011204647](https://openairdocs.org/sdr/FDEA201011204647.md): Floorbeam · corroded · Nov 20, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION TOP TEE CAP FLOORBEAM MAIN CABIN STA 950F RBL 25 - RBL 45 CUT OUT DAMAGED AREA, FABRICATED REPAIR FILLER, ANGLES AND STRAPS, INSTALLED. REPAIR PARTS AT BS 950F, RBL 25 TO RBL 55 IAW SRM 51-30-2, SRM 51-10-2 AND SRM 53-10-8, FIG 1.
- [SDR FDEA201011204440](https://openairdocs.org/sdr/FDEA201011204440.md): Seat Track · corroded · Nov 20, 2010 · N233FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK STA 950, PLUS 10" TO STA 1010, RBL 25. REMOVED CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1, REMOVED SEAT TRACK IAW SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520-792-7178-T6511 DIM: 20' X 3 3/8" IAW SRM 53-10-5 FIG 1, TREATE
- [SDR FDEA201011204615](https://openairdocs.org/sdr/FDEA201011204615.md): Stringer Splice · corroded · Nov 20, 2010 · N233FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 27R STRAP CORRODED ON OTBD FLANGE AFT OF STA 1010 CORROSION OUT OF LIMITS. REMOVED STRAP. FABRICATED NEW STRAP USING 7075T6 FLAT BAR DIMS 20.5" X 1.3" AND INSTALLED IAW DWG 69-45584 AND SRM 51-30-2.
- [SDR FDEA201011204462](https://openairdocs.org/sdr/FDEA201011204462.md): Floorbeam · corroded · Nov 20, 2010 · N233FE · Boeing 727247 · Fuselage Main, Floor Beam
  > CORROSION MAIN CABIN FLOORBEAM TOP TEE CAP STA. 440 BL 0 - RBL 25 CUTOUT DAMAGED AREA, FABRICATED FLOORBEAM REPAIR PARTS & INSTALLED FLOORBEAM REPAIR AT BS 440 RBL 25 IAW SRM 51-10-6, SRM 53-10-1 FIG 4B, SRM 53-10-8 FIG 3, SRM 51-10-2, & SRM 51-30-2.

Next page: https://openairdocs.org/deregistered/N233FE-2013-04-25/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 = 'N233FE' AND deregistration_id = 'N233FE-2013-04-25'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N233FE-2013-04-25/reports

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