# Service difficulty reports: Boeing 727-247

A list on [Boeing 727-247](https://openairdocs.org/model/boeing-727-247.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 54 · 2,669 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 FDEA201301260192](https://openairdocs.org/sdr/FDEA201301260192.md): Uplock Switch · inoperative · Jan 26, 2013 · N234FE · Boeing 727247 · Door Warning System
  > AFT AIRSTAIRS LIGHT ILLUMINATED IN FLIGHT. ADJUSTED UPLOCK SWITCH IAW MM CH 52-70-001-51, CYCLED DOOR NUMEROUS TIMES, ALL INDICATIONS NORMAL.
- [SDR FDEA201212274390](https://openairdocs.org/sdr/FDEA201212274390.md): Slide · dislodged · Dec 27, 2012 · N235FE · Boeing 727247 · Escape Slide
  > FOUND LT ENTRY DOOR ESCAPE SLIDE OUT OF SLIDE COMPARTMENT AND FOUND EMERGENCY LIGHT BATTERY DEAD ON LT ENTRY FROM SLIDE ACTIVATING LIGHT. REINSTALLED ESCAPE SLIDE IAW AMM 25-60-015-2 AND REPLACED LIGHT POWER UNIT MODEL 209A IAW AMM 33-50-051-2. OPS NORMAL.
- [SDR FDEA201212274392](https://openairdocs.org/sdr/FDEA201212274392.md): Retainer · broken · Dec 27, 2012 · N234FE · Boeing 727247 · Emergency Equipment
  > GIRT BAR HOLDER ON L1 DOOR BROKEN. NEED PART RETAINER CLIP. R & R GIRT BAR RETAINER CLIP ON L1 DOOR IAW SMP. R & R GIRT BAR RETAINER CLIP ON L1 DOOR IAW SMP.
- [SDR FDEA201212264391](https://openairdocs.org/sdr/FDEA201212264391.md): Battery Pack · discharged · Dec 26, 2012 · N235FE · Boeing 727247 · Emergency Lighting
  > FOUND LT ENTRY DOOR ESCAPE SLIDE OUT OF SLIDE COMPARTMENT AND FOUND EMERGENCY LIGHT BATTERY DEAD ON LT ENTRY FROM SLIDE ACTIVATING LIGHT. REINSTALLED ESCAPE SLIDE IAW AMM 25-60-015-2 AND REPLACED LIGHT POWER UNIT MODEL 209A IAW AMM 33-50-051-2. OPS NORMAL.
- [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 FDEA201204041247](https://openairdocs.org/sdr/FDEA201204041247.md): Battery Pack · inoperative · Apr 4, 2012 · N234FE · Boeing 727247 · Emergency Lighting
  > CREW ENTRY DOOR EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED EMERGENCY SLIDE LIGHT BATTERY PACK AND OPS CHECKED OK IAW MM 33-50-051. OK FOR SERVICE.
- [SDR FDEA201202150611](https://openairdocs.org/sdr/FDEA201202150611.md): Light · inoperative · Feb 15, 2012 · N234FE · Boeing 727247 · Emergency Lighting
  > PERFORMED TRANSIT CHECK, CABIN EMERGENCY EXIT LIGHTS INOPERATIVE. R & R CABIN EMERGENCY EXIT LIGHT ASSY. OPS NORMAL IAW MM35-50-001-0-0. PREMATURE REMOVAL/INSTALLATION.
- [SDR FDEA201201060060](https://openairdocs.org/sdr/FDEA201201060060.md): Battery · discharged · Jan 6, 2012 · N236FE · Boeing 727247 · Emergency Lighting
  > WHILE PERFORMING TRANSIT CHECK, FOUND BOTH COCKPIT AND ENTRY DOOR PORTABLE EMERGENCY EXIT LIGHTS DEAD. REPLACED BATTERIES IN BOTH PORTABLE EMERGENCY EXIT LIGHTS IAW AMM 33-50-101-2. CHECKS GOOD AND BRIGHT. OK FOR SERVICE. (FINAL CLOSED)
- [SDR FDEA201112205390](https://openairdocs.org/sdr/FDEA201112205390.md): Bulkhead Web · misinstalled · Dec 20, 2011 · N235FE · Boeing 727247 · Fuselage Main, Bulkhead
  > BS 1183 BULKHEAD WEB HAS INSUFFICIENT FASTENER SPACING AT LBL 12. REPAIRED ON NR N00736 AND EA 7-5310-143956.
- [SDR FDEA201112185336](https://openairdocs.org/sdr/FDEA201112185336.md): Battery Pack · inoperative · Dec 18, 2011 · N236FE · Boeing 727247 · Emergency Lighting
  > EMERGENCY SLIDE LIGHT INOPERATIVE. REPLACED BATTERY PACK IAW AMM 33-50-121-2, OPS CHECKED OK.
- [SDR FDEA201112105236](https://openairdocs.org/sdr/FDEA201112105236.md): Seat Track · corroded · Dec 10, 2011 · N235FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK IS CORRODED AT BS 950D, RBL 25. REMOVED SEAT TRACK SECTION RBL 25 FROM BS 950 PLUS 10" TO BS 950F PLUS 10" IAW SRM 53-10-5, FABRICATED NEW SEAT TRACK SECTION FROM 7178T6 IAW SRM 53-10-2, FIG 7 & SRM 51-30-2. INSTALLED NEW SEAT TRACK SECTION IAW
- [SDR FDEA201112085240](https://openairdocs.org/sdr/FDEA201112085240.md): Skin · dented · Dec 8, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > LT INBD MID FLAP L/E AREA HAS DENT AT WBL 95, WS 194. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/E S
- [SDR FDEA201112075203](https://openairdocs.org/sdr/FDEA201112075203.md): Skin · gouged · Dec 7, 2011 · N235FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > SKIN GOUGED SEVERAL PLACES AROUND CARGO DOORWAY BS 620 TO 640, STR 5L TO 16L. REPAIRED IAW SRM 51-30-2 & EA 7-5330-143955.
- [SDR FDEA201112065171](https://openairdocs.org/sdr/FDEA201112065171.md): Skin · dented · Dec 6, 2011 · N235FE · Boeing 727247 · Entrance Stairs
  > AFT AIRSTAIR SKIN HAS DENT ON RT SIDE BS 1283. CUT OUT DAMAGED AREA IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3. INSTALLED REPAIR PARTS IAW SRM 52-10-2, FIG 3.
- [SDR FDEA201112065170](https://openairdocs.org/sdr/FDEA201112065170.md): Skin · dented · Dec 6, 2011 · N235FE · Boeing 727247 · Entrance Stairs
  > AFT AIRSTAIR SKIN HAS DENT ON RT SIDE BS 1296. CUT OUT DAMAGED AREA IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3 INSTALLED REPAIR DOUBLER AND FILLER IAW SRM 52-10-2, FIG 3.
- [SDR FDEA201112045140](https://openairdocs.org/sdr/FDEA201112045140.md): Skin · dented · Dec 4, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > LEFT INBD T/E MIDFLAP TOP AREA INBD SIDE HAS THREE DENTS. FOUND OUT OF LIMITS IAW SRM 57-50-1, FIG 3, CUT-OUT DAMAGE AND FABRICATED REPAIR DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2 & 57-50-2, FIG 3, INSTALLED REPAIR FILLER AND DOUBLER AT LT INBD MID FLAPS L/E
- [SDR FDEA201112045139](https://openairdocs.org/sdr/FDEA201112045139.md): Skin · dented · Dec 4, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > LEFT WING OTBD MIDFLAP HAS A DENT ON LOWER SURFACE OF L/E, 15" FROM OTBD END OF FLAP. CUTOUT DAMAGED AREA IAW SRM 57-50-4, FIG 2. FABRICATED DOUBLER AND FILLER IAW SRM 57-50-4, FIG 2. INSTALLED DOUBLER, FILLER AND FASTENERS IAW SRM 57-50-4, FIG 2 & EA 7-575
- [SDR FDEA201112045138](https://openairdocs.org/sdr/FDEA201112045138.md): Skin · dented · Dec 4, 2011 · N235FE · Boeing 727247 · Entrance Stairs
  > AFT AIRSTAIR SKIN HAS PROTRUDING DENT ON RT SIDE BS1323 CUT OUT DAMAGED AREA AT AFT AIRSTAIR SKIN, RT SIDE BS 1323 IAW SRM 52-10-2, FIG 3. FABRICATED DOUBLER REPAIR IAW SRM 52-10-2, FIG 3 AND 52-10-1, FIG 3. INSTALLED DOUBLER REPAIR IAW SRM 52-10-2, FIG 3.
- [SDR FDEA201112025167](https://openairdocs.org/sdr/FDEA201112025167.md): Bulkhead Web · damaged · Dec 2, 2011 · N235FE · Boeing 727247 · Fuselage Main, Bulkhead
  > FOUND AFT AIRSTAIR UPPER HORIZ SUPPORT ANGLE FASTENERS WITH NO ED AT BS 1183 BULKHEAD JUST BELOW THE AFT ENTRY DOOR DURING ACCESS TO VERT BEAM REPAIR. REMOVED SUPPORT WEB, FABRICATED NEW WEB, TREATED & PRIMED AND INSTALLED IAW SRM 51-30-2, SRM 51-10-2, &
- [SDR FDEA201112025127](https://openairdocs.org/sdr/FDEA201112025127.md): Seat Track · corroded · Dec 2, 2011 · N235FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE BS 760-849 LBL 45. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 8, REMOVED SEAT TRACK SECTION AND SUPPORT IAW SRM 53-30-2, FABRICATED NEW SUPPORT IAW SRM 53-10-2, FIG 7 & SRM 51-30-5, INSTALLED NEW SUPPORT AND
- [SDR FDEA201112025114](https://openairdocs.org/sdr/FDEA201112025114.md): Shear Tie · corroded · Dec 2, 2011 · N235FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > AFT CARGO PIT BILGE SHEAR TIE CORRODED BS 1148, LBL 2. REMOVED CORROSION IAW B727 SRM 51-10-6, C/W U.T. THICKNESS IAW SRM NDTM PT 4, 51-00-00 FIG 2. ORIGINAL:.063, REMAINING.043, MATERIAL LOS.020, FOUND OUT OF LIMITS IAW SRM 53-10-1 FIG 1. CUTOUT DAMAGE AR
- [SDR FDEA201112015111](https://openairdocs.org/sdr/FDEA201112015111.md): Vertical Beam · corroded · Dec 1, 2011 · N235FE · Boeing 727247 · Fuselage Main, Bulkhead
  > AFT PIT, BS 1183 BULKHEAD VERTICAL BEAM AT BL 0 HAS CORROSION AT BOTTOM. CUTOUT DAMAGE AREA IAW SRM 51-40-2, FIG 2. FABRICATED REPAIR PARTS IAW SRM 51-40-2, FIG 2. INSTALLED REPAIR PARTS 3 EA PLATES & STRUCTURAL FILLERS IAW SRM 51-40-4, FIG 2.
- [SDR FDEA201112015110](https://openairdocs.org/sdr/FDEA201112015110.md): Vertical Beam · corroded · Dec 1, 2011 · N235FE · Boeing 727247 · Fuselage Main, Bulkhead
  > AFT PIT, BS 1183 BULKHEAD RBL 26.8 VERTICAL BEAM CHORD HAS CORROSION AT FORWARD SIDE. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW SRM 53-10-1, FIG 1, CUTOUT DAMAGE AND FABRICATED REPAIR FILLER (1 EA) AND 3 EA. REPAIR ANGLES IAW SRM 51-40-4, FIG 2 & SRM 53
- [SDR FDEA201112015109](https://openairdocs.org/sdr/FDEA201112015109.md): Vertical Beam · damaged · Dec 1, 2011 · N235FE · Boeing 727247 · Fuselage Miscellaneous Structure
  > FOUND FASTENERS WITH SHORT EDGE DISTANCE AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AFTER PAINT AND CORROSION REMOVAL. ACCOMPLISHED REPAIR IAW EA 7-5310-143956. ORIGINAL SUBMISSION 12/01/2011
- [SDR FDEA201112015099](https://openairdocs.org/sdr/FDEA201112015099.md): Skin · gouged · Dec 1, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > RIGHT WING OTBD FOREFLAP L/E SKIN GOUGED IN 2 PLACES ABOVE NR 7 FLAP CARRIAGE. REPAIRED IAW SRM 57-50-2, FIG 4 & SRM 57-50-4, FIG 1 & EA 7-5750-143963.
- [SDR FDEA201112015112](https://openairdocs.org/sdr/FDEA201112015112.md): Vertical Beam · corroded · Dec 1, 2011 · N235FE · Boeing 727247 · Fuselage Main, Bulkhead
  > AFT PIT, STA 1183 BULKHEAD LBL 26.8 VERTICAL BEAM CHORD HAS CORROSION. REMOVED CORROSION FROM VERTICAL BEAM IAW SRM 51-10-6 & EA 7-5310-143956, ORIGINAL THICKNESS.200 MATERIAL REMAINING.174, FOUND MATERIAL LOSS OF.026 TO BE WITHIN LIMIT IAW EA 7-5310-14395
- [SDR FDEA201112015100](https://openairdocs.org/sdr/FDEA201112015100.md): Skin · dented · Dec 1, 2011 · N235FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > LT SIDE OF FUSELAGE DENTED AT BS 1348, STRINGER 23L TO 26L. CUT OUT DAMAGED AREA IAW SRM 54-30-3 FIG 7. FABRICATED DOUBLER REPAIR IAW SRM 54-30-3 FIG 7 AND 54-30-2 FIG 4. TREATED AND PRIMED DOUBLER IAW SRM 51-10-2. INSTALLED COUNTERSINK WASHERS IAW SRM 51
- [SDR FDEA201111305095](https://openairdocs.org/sdr/FDEA201111305095.md): Skin · damaged · Nov 30, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > LEFT TE FLAP LE HAS LARGE CREASED AREA TOP SIDE. REMOVED DAMAGE AREA SKIN AND CORE ON LT INBD T/E L/E, FABRICATED, HOT BONDED CORE AND DOUBLER REPAIRS, CLEANED, SEALED, & FINISHED IAW SRM 51-40-20 & EA 7-5750-143964.
- [SDR FDEA201111295069](https://openairdocs.org/sdr/FDEA201111295069.md): Structure · cracked · Nov 29, 2011 · N235FE · Boeing 727247 · Trailing Edge Flaps
  > RT WING INBD MID FLAP T/E CHORD CRACKED AT INBD FLAP CONTROL DRUM, WBL 100. REMOVED MID FLAP T/E CHORD IAW SRM 51-30-2. LOCATED AND DRILLED NEW CHORD IAW SRM 57-50-2, FIG 5 AND INSTALLED NEW CHORD SECTION, USED PREVIOUS REPAIR IAW SRM 57-50-2, FIG 5 & EA 7-57
- [SDR FDEA201111295079](https://openairdocs.org/sdr/FDEA201111295079.md): Shear Tie · damaged · Nov 29, 2011 · N235FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > AFT CARGO BAY BILGE AREA, SHEAR TIE DAMAGED BS 950E BETWEEN S28-29R. REMOVED SHEAR TIE IAW SRM 51-30-02. FABRICATED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 51-30-02 AND 53-10-4 FIG 15.
- [SDR FDEA201111295068](https://openairdocs.org/sdr/FDEA201111295068.md): Stringer · corroded · Nov 29, 2011 · N235FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > CORROSION ON STRINGER 30L BS 1020. CUT OUT DAMAGED STRINGER 46 INCHES IN LENGTH IAW SRM 53-10-3 FIG 1. FABRICATED STRINGER REPAIR HATS AND SPLICES IAW SRM 53-10-3 FIG 1, AND 53-10-2 FIG 9. INSTALLED REPAIR HATS AND SPLICES IAW SRM 53-10-3 FIG 1 AND 51-30
- [SDR FDEA201111295078](https://openairdocs.org/sdr/FDEA201111295078.md): Shear Tie · corroded · Nov 29, 2011 · N235FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 720E BETWEEN STRINGER 27L AND 28L. REMOVED, FABRICATED AND INSTALLED SHEAR TIE IAW SRM 53-10-4 FIG 13.
- [SDR FDEA201111295080](https://openairdocs.org/sdr/FDEA201111295080.md): Shear Tie · corroded · Nov 29, 2011 · N235FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT AFT SIDE OF BS 700, BETWEEN STRINGER 27L AND 28L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-30-2. FABRICATED SHEAR TIE IAW SRM 53-10-4 FIG 15. INSTALLED NEW SHEAR TIE IAW SRM 53-10-4 FIG 15.
- [SDR FDEA201111295074](https://openairdocs.org/sdr/FDEA201111295074.md): Seat Track · corroded · Nov 29, 2011 · N235FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 849 - 870, RBL 25. REMOVED SEAT TRACK SECTION, REMOVED CORROSION, AREA FOUND TO BE OUT OF LIMITS, FABRICATED NEW SEAT TRACK SECTION, TREATED AND PRIMED, INSTALLED IAW SRM 51-30-2, 51-10-6, 53-10-1 FIG 1, 53-10-2 FIG 7.
- [SDR FDEA201111285064](https://openairdocs.org/sdr/FDEA201111285064.md): Seat Track · corroded · Nov 28, 2011 · N235FE · Boeing 727247 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK FLANGE SPLICE BS 849 - 870, LBL 45. REMOVED CORROSION, AREA FOUND TO BE OUT OF LIMITS. FABRICATED NEW SEAT TRACK SECTION, TREATED AND PRIMED AND INSTALLED IAW SRM 51-30-2, 53-10-1, 51-10-6, 53-10-02 FIG 7 AND 51-10-2.
- [SDR FDEA201111275056](https://openairdocs.org/sdr/FDEA201111275056.md): Shear Tie · corroded · Nov 27, 2011 · N235FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE AT BS 720C, BETWEEN STRINGER 27-28L. REMOVED DAMAGED SHEAR TIE IAW SRM 51-30-2 FABRICATED NEW SHEAR TIE AND INSTALLED IAW SRM 53-10-4 FIG 13.
- [SDR FDEA201111275057](https://openairdocs.org/sdr/FDEA201111275057.md): Stringer · corroded · Nov 27, 2011 · N235FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 26R CORRODED BETWEEN BS 720F - 740. CUT OUT DAMAGED STRINGER IAW SRM 53-10-3, FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3, FIG 1 AND 53-10-2, FIG 9 INSTALLED REPAIR PARTS IAW SRM 53-10-3, FIG 1 AND 51-30-02.
- [SDR FDEA201111275055](https://openairdocs.org/sdr/FDEA201111275055.md): Stringer · corroded · Nov 27, 2011 · N235FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > STRINGER 26L BS 720F-740 CORRODED. CUT OUT DAMAGED AREA IAW B727 SRM 53-10-3 FIG 1. FABRICATED REPAIR PARTS IAW SRM 53-10-3 FIG 1 AND 53-10-2 FIG 9. INSTALLED REPAIR PARTS IAW SRM 51-30-2 AND 53-10-3 FIG 1
- [SDR FDEA201110124452](https://openairdocs.org/sdr/FDEA201110124452.md): Shear Tie · corroded · Oct 12, 2011 · N234FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > AFT PIT SHEAR TIE IS CORRODED ON FWD SIDE AT BS 1166, BTWN S29L- S28L. REPLACED SHEAR TIE.
- [SDR FDEA201110124451](https://openairdocs.org/sdr/FDEA201110124451.md): Frame · corroded · Oct 12, 2011 · N234FE · Boeing 727247 · Fuselage Main, Frame
  > AFT PIT FRAME IS CORRODED ON AFT SIDE BELOW FAIL SAFE CHORD AT BS 1166 BETWEEN S29R - S27R. REPLACED FRAME ASSY.
- [SDR FDEA201110124450](https://openairdocs.org/sdr/FDEA201110124450.md): Shear Tie · corroded · Oct 12, 2011 · N234FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > AFT PIT SHEAR TIE IS CORRODED ON AFT SIDE AT BS 1166 BTWN S30 -S29R. REPLACED SHEAR TIE.
- [SDR FDEA201110084386](https://openairdocs.org/sdr/FDEA201110084386.md): Failsafe · corroded · Oct 8, 2011 · N234FE · Boeing 727247 · Fuselage Main, Frame
  > FAILSAFE CORRODED AT BS 1166 BTWN S27-29L. REMOVED FAILSAFE IAW SRM 51-30-2. FABRICATED NEW FAILSAFE IAW SRM 53-10-2 FIG 5 AND 51-20-1. INSTALLED NEW FAILSAFE IAW SRM 51-30-2 AND DWG 65-16349 REV T.
- [SDR FDEA201110084385](https://openairdocs.org/sdr/FDEA201110084385.md): Tee Fitting · corroded · Oct 8, 2011 · N234FE · Boeing 727247 · Cargo/Baggage Doors
  > C2 DOOR LOWER INBD TEE FITTING CORRODED. REMOVED TEE FITTING IAW SRM 51-30-2, FABRICATED, LOCATED AND DRILLED NEW TEE FITTING IAW SRM 52-30-1 FIG 1, INSTALLED NEW TEE FITTING IAW SRM 51-30-2.
- [SDR FDEA201110054316](https://openairdocs.org/sdr/FDEA201110054316.md): Skin · corroded · Oct 5, 2011 · N234FE · Boeing 727247 · Fuselage Main, Plate/Skin
  > CORROSION ON SKIN BS 700 S26L. REPAIRED IAW EA 7-5330-152457.
- [SDR FDEA201110054306](https://openairdocs.org/sdr/FDEA201110054306.md): Frame · corroded · Oct 5, 2011 · N234FE · Boeing 727247 · Fuselage Main, Frame
  > FRAME IS CORRODED ON AFT SIDE BELOW THE FAILSAFE CHORD AT BS 1166 BETWEEN S27-29L. REMOVED & REPLACED FRAME IAW DWG 65- 16349 AND SRM 51-30-2.
- [SDR FDEA201110054300](https://openairdocs.org/sdr/FDEA201110054300.md): Access Panel · gouged · Oct 5, 2011 · N234FE · Boeing 727247 · Trailing Edge Flaps
  > GOUGE - LT INBD FORE FLAP L/E ACCESS PANEL, UPPER SURFACE, APPROX FLAP CENTER LINE. REMOVED & REPLACED LT INBD FOREFLAP ASSY IAW MM 27-51-001-4. OPS CHECKED NORMAL IAW MM 27-51-000-5.
- [SDR FDEA201110044283](https://openairdocs.org/sdr/FDEA201110044283.md): Shear Tie · corroded · Oct 4, 2011 · N234FE · Boeing 727247 · Fuselage Internal Mounting Structure
  > CORROSION ON SHEAR TIE 720E BETWEEN S27-28L. REMOVED SHEAR TIE IAW SRM 53-10-4 FIG 11. FABRICATED DOUBLER AND INSTALLED IAW SRM 53-10-4 FIG 11.
- [SDR FDEA201110034276](https://openairdocs.org/sdr/FDEA201110034276.md): Stringer · corroded · Oct 3, 2011 · N234FE · Boeing 727247 · Fuselage Main, Longeron/Stringer
  > AFT PIT S27L HAS ELONGATED FASTENER HOLES AND CORROSION BTWN BS 680 - BS 690. REMOVED DAMAGED STRINGER SECTION, FABRICATED STRINGER REPAIR PARTS & INSTALLED IAW SRM 53-10-3 FIG 1 & 51-30-2.
- [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.

Next page: https://openairdocs.org/model/boeing-727-247/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 aircraft_model_key = '727247'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-247/reports

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