# Service difficulty reports: Boeing 727-100

A list on [Boeing 727-100](https://openairdocs.org/model/boeing-727-100.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 288 reports

- [SDR 06FDEA2569](https://openairdocs.org/sdr/06FDEA2569.md): Blade · damaged · Jul 15, 2006 · N185FE · Boeing 727100 · Engine (Turbine/Turboprop)
  > AS POWER WAS ADVANCED TO MAX POWER FOR T/O, THERE WAS A LOUD BANG AND THUMP IN THE THROTTLE QUADRANT, FOLLOWED BY THE SOUND OF A CABLE UNWINDING. T/O WAS DISCONTINUED AND AIRCRAFT RETURNED TO MX. AFTER DEBRIEFING FLIGHT CREW PROCEEDED TO INSPECT NR 2 ENGINE
- [SDR 06FDEA1800](https://openairdocs.org/sdr/06FDEA1800.md): Skin · damaged · May 11, 2006 · N192FE · Boeing 727100 · Horizontal Stabilizer, Plate/Skin
  > LT HORIZONTAL STAB HAS A BLEND OUT THAT EXCEEDS SRM LIMITS AT STAB STA 77.1,.500 FWD OF THE EDGE OF THE T/E SKIN. REPAIRED LT HORIZONTAL STAB LWR SKIN PER FED EX EA 7-5510-102242.
- [SDR 06FDEA1777](https://openairdocs.org/sdr/06FDEA1777.md): Skin · dented · May 10, 2006 · N192FE · Boeing 727100 · Cargo/Baggage Doors
  > LWR FWD CARGO DOOR FWD EDGE OF EXTERIOR SKIN HAS SEVERAL DENTS. *S/D* REMOVED AND REPLACED LWR FWD CARGO DOOR IAW FED EX MM 52-31-000-4.
- [SDR 06FDEA1738](https://openairdocs.org/sdr/06FDEA1738.md): Attach Fitting · unknown · May 8, 2006 · N192FE · Boeing 727100 · Wing, Attach Fittings
  > N01182 COMPLY WITH EO 7-5710-7-2314D PT5- WINGS MLG TRUNION ATTATCH FITTING MODIFICATION SB 727-57A0132R3 AD 2004-18-08, LT SIDE. COMPLIED WITH FED EX EO 7-5710-7-2314D PT 5 AND FED-EX EA 7-5710-96632.
- [SDR 06FDEA1702](https://openairdocs.org/sdr/06FDEA1702.md): Frame · gouged · May 4, 2006 · N192FE · Boeing 727100 · Fuselage Main, Frame
  > LWR FWD CARGO DOOR CUTOUT AFT SIDE FRAME IS GOUGED FWD OF LATCH FITTING STR 23 RT. REPAIRED LOWER FWD CARGO DOOR CUTOUT AFT SIDE FRAME IAW FED EX EA 7-5310-99516.
- [SDR 06FDEA1703](https://openairdocs.org/sdr/06FDEA1703.md): Skin · corroded · May 4, 2006 · N192FE · Boeing 727100 · Trailing Edge Flaps
  > LT WING, I/B MID FLAP UPPER SKIN IS CORRODED, 4 INCHES FROM T/E AND 12 INCHES AND 58 INCHES FROM I/B END. *S/D* REMOVED & REPLACED FLAP PER FED EX MM 27-51-013.
- [SDR 06FDEA1664](https://openairdocs.org/sdr/06FDEA1664.md): Support Fitting · corroded · May 1, 2006 · N192FE · Boeing 727100 · Nacelle/Pylon, Main Frame
  > NR 1 ENG PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON HAS CORROSION ON FWD AND AFT SIDES IN SEVERAL AREAS. COMPLIED WITH FED EX EA 7-5410-99512 ON NR 1 ENGINE PYLON ON FWD ENG MOUNT CASTING O/B OF PYLON ON FWD AND AFT SIDES.
- [SDR 06FDEA1663](https://openairdocs.org/sdr/06FDEA1663.md): Support Fitting · corroded · May 1, 2006 · N192FE · Boeing 727100 · Nacelle/Pylon, Main Frame
  > NR 1 ENG PYLON HAS CORROSION ON FWD ENG SUPPORT FITTING WEB FWD LWR I/B JUST ABOVE LWR HORIZONTAL FLANGE COMMON TO EO 7-5410-7-3304 P9 PAGE 12 FIG 2. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.
- [SDR 06FDEA1662](https://openairdocs.org/sdr/06FDEA1662.md): Flange · corroded · May 1, 2006 · N192FE · Boeing 727100 · Engine Mount Section
  > NR 1 ENG PYLON ON FWD ENG SUPPORT HORIZONTAL FLANGE HAS CORROSION ON UPPER FWD EDGE. *S/D* COMPLIED WITH FED EX EA 7-5410-99512.
- [SDR 06FDEA1657](https://openairdocs.org/sdr/06FDEA1657.md): Attach Fitting · cracked · May 1, 2006 · N185FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EO 7-5710-7-2314D PT6 EOCN D1 WINGS - MLG TRUNNION ATTACH FITTING MODIFICATION BOEING S/B 72 7-57AD132 R3 AD 2004-18-08. COMPLIED WITH EO 7-5710-7-2314D PT6 RII:536327.
- [SDR 06FDEA1612](https://openairdocs.org/sdr/06FDEA1612.md): Stringer Clip · corroded · Apr 26, 2006 · N192FE · Boeing 727100 · Fuselage Main, Attach Fittings
  > STA 380 STR 19L CORROSION ON STR CLIP. *S/D* REMOVED AND REPLACED STRINGER CLIP AT BS 380, STR 19L, PER SRM 51-30-2.
- [SDR 06FDEA1576](https://openairdocs.org/sdr/06FDEA1576.md): Shear Tie · corroded · Apr 24, 2006 · N192FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > STA 1030 STR 29R, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REMOVED AND REPLACED SHEAR TIE ON BS 1030, STR 29R FRAME OUTBOARD FLANGE IAW SRM 53-10-4.
- [SDR 06FDEA1577](https://openairdocs.org/sdr/06FDEA1577.md): Structure · cracked · Apr 24, 2006 · N192FE · Boeing 727100 · Fuselage Main, Structure
  > BS 961, RBL 10, STR 29R AT BS 961, RBL 10, STR 29R, STRUCTURE IS CRACKED. REMOVED DAMAGE AND REPAIRED CHORD PER SRM 51-40-04.
- [SDR 06FDEA1566](https://openairdocs.org/sdr/06FDEA1566.md): Frame · corroded · Apr 21, 2006 · N192FE · Boeing 727100 · Fuselage Main, Frame
  > STA 970 BETWEEN STR 29L AND STR 30, CORROSION ON FRAME OUTBOARD FLANGE. *S/D* REPAIRED PER SRM 53-10-4.
- [SDR 06FDEA1565](https://openairdocs.org/sdr/06FDEA1565.md): Tee Fitting · corroded · Apr 21, 2006 · N198FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > DURING EMBODIMENT OF SB 727-57A0132, CORROSION WAS FOUND AFFECTING THE OUTBOARD TEE FITTING ASSOCIATED WITH THE RT MLG. CORROSION WAS REMOVED BY REAMING TO 0.875 INCH AND INSTALLED A REPAIR BUSHING IN THE ADJACENT ATTACH FITTING AND REPAIR IS CLASSIFIED AS MA
- [SDR 06FDEA1486](https://openairdocs.org/sdr/06FDEA1486.md): Skin · delaminated · Apr 17, 2006 · N192FE · Boeing 727100 · Trailing Edge Flaps
  > RIGHT WING I/B FORE FLAP DELAMINATED MID SPAN ON UPPER SURFACE. *S/D* REPAIRED DELAM ON UPPER SURFACE ON RIGHT WING I/B FORE FLAP PER SRM 51-40-20.
- [SDR 06FDEA1360](https://openairdocs.org/sdr/06FDEA1360.md): Bulkhead · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Main, Bulkhead
  > CRACK IN BULKHEAD AT BS 870, LBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870, LBL 12, WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1359](https://openairdocs.org/sdr/06FDEA1359.md): Bulkhead · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Main, Bulkhead
  > CRACK IN BULKHEAD AT BS 870, RBL 12, WL 138. *S/D* REPAIRED CRACK IN BULKHEAD BS 870 RBL 12 WL 138 IAW SRM 53-10-9 FIG 4.
- [SDR 06FDEA1358](https://openairdocs.org/sdr/06FDEA1358.md): Support Angle · cracked · Apr 10, 2006 · N192FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > FOUND CRACK ON LOWER SUPPORT ANGLE AT BS 870 LBL 12 WL 138. REPAIRED CRACKED ANGLE AT BS 870 RBL 12 WL 138 IAW SRM 54-10-9.
- [SDR 06FDEA1335](https://openairdocs.org/sdr/06FDEA1335.md): Gusset · damaged · Apr 7, 2006 · N192FE · Boeing 727100 · Fuselage Main, Structure
  > UPON REMOVAL OF SHEAR WEB AT BS 1176, FOUND GUSSET TO BE DAMAGED AROUND LUG AT BS 1176, WL 208, LBL 18. *S/D* REMOVED AND REPLACED GUSSET BS 1176, LBL 18, WL 208 IAW SRM 51-40-2.
- [SDR 06FDEA1307](https://openairdocs.org/sdr/06FDEA1307.md): Angle · corroded · Apr 4, 2006 · N192FE · Boeing 727100 · Fuselage Miscellaneous Structure
  > STA 348 LBL 17 WL 149, CORROSION ON LOWER NOSE ANGLE (AFT OF NLG). REMOVED AND REPLACED CHORD AT STA 348 LBL 17 WL 149 IAW SRM 51-30-2.
- [SDR 06FDEA1246](https://openairdocs.org/sdr/06FDEA1246.md): Skin · dented · Mar 27, 2006 · N192FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > N00969 DENT IN SKIN, BS 748, JUST BELOW STR2R. REPAIRED DENT PER FED EX E.A. 7-5330-96624
- [SDR 06FDEA0889](https://openairdocs.org/sdr/06FDEA0889.md): Skin · cracked · Mar 2, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REMOVED REPAIR BS 352, LBL 18, WL 145, REPAIRED IAW FED EX EA 7-5330-96595.
- [SDR 06FDEA0814](https://openairdocs.org/sdr/06FDEA0814.md): Skin · debonded · Feb 23, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > N01287 REWORK OF CARD N01229 REQUIRED. WHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION, FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148. REWORK REQUIRED BECAUSE REPAIR WAS INSTALLED IN A RESTRICTED AREA IAW SRM 53-30-3 FIG. 12. ** SD **
- [SDR 06FDEA0578](https://openairdocs.org/sdr/06FDEA0578.md): Stringer · corroded · Feb 7, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > WHILE WORKING N01286 FOUND STRINGER 27 LEFT CORRODED AT BS 1176. REMOVED AND REPLACED STR 27L, BS 1090 - 1183 IAW SRM 53-10-3, 51-10-2, AND 51-30-2.
- [SDR 06FDEA0467](https://openairdocs.org/sdr/06FDEA0467.md): Angle · unknown · Feb 1, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > COMPLY WITH EA 7-5710-96564, RIGHT MAIN LANDING GEAR TRUNNION SUPPORT FITTING, -TEE ANGLE- HOLE LOCATION -E- REPAIR- AD 2004-18-08. COMPLIED WITH FED-EX EA 7-5710-96564, REFERENCE CUSTOMER CARD 7-5710-7-2314 PT 4.
- [SDR 06FDEA0431](https://openairdocs.org/sdr/06FDEA0431.md): Web · damaged · Jan 30, 2006 · N191FE · Boeing 727100 · Vertical Stabilizer
  > WHILE WORKING FED EX CARD N00897 FOUND AN EXTRA HOLE ON WEB UNDER UPPER PANEL SUPPORT CHORD ON VERTICAL STAB AT FIN STA 247 UPPER RIGHT SIDE. *S/D* REPAIRED PANEL SUPPORT CHORD ON VERTICAL STAB IAW FED-EX EA 7-5530-96566.
- [SDR 06FDEA0430](https://openairdocs.org/sdr/06FDEA0430.md): Skin · unknown · Jan 30, 2006 · N191FE · Boeing 727100 · Aircraft Structures
  > DURING ACCESS FOR STR 30 REPAIR, (CUSTOMER CARD N00999), UPON REMOVAL OF EXISTING REPAIR DOUBLER BS 1165 - 1183 RBL 12 - LBL 10 FOUND ORIGINAL SKIN HAS CUTOUT BS 1175 - 1183 RBL 1 - 6.5 AND BS 1183 LWR CHORD CUTOUT IN A 1 X 2 INCH AREA. ALL WORK WAS ACCOMPLISH
- [SDR 06FDEA0404](https://openairdocs.org/sdr/06FDEA0404.md): Spar · corroded · Jan 27, 2006 · N191FE · Boeing 727100 · Wing Spar
  > RT WING FRONT SPAR HAS AREAS OF CORROSION AT LES 340-345. REPAIRED PER FED EX EA 7-5710-96562.
- [SDR 06FDEA0405](https://openairdocs.org/sdr/06FDEA0405.md): Trunnion · unknown · Jan 27, 2006 · N191FE · Boeing 727100 · Wing, Landing Gear Attach Fittings
  > WHILE WORKING E.O. 705710-7-2314 P4, FOUND BOTH "C" HOLES IN TRUNION ATTACH FITTING TO BE SPOTFACED ON INNER SURFACE AROUND HOLES. REPAIRED RT MLG FWD TRUNNION FITTING SPOT FACED AREAS AT "C" HOLE LOCATIONS IAW FED-EX EA 7-5710-96561. THIS IS A MAJOR REP
- [SDR 06FDEA0375](https://openairdocs.org/sdr/06FDEA0375.md): Flap · corroded · Jan 25, 2006 · N191FE · Boeing 727100 · Leading Edge Devices
  > NR 5 K-FLAP HAS CORROSION AT OB BULLNOSE TO K-FLAP BONDING WIRE BOTH ATTACH POINTS. REPAIRED NR 5 K FLAP BULLNOSE PER SR DRAWING SR 27-57-010 REV C.
- [SDR 06FDEA0374](https://openairdocs.org/sdr/06FDEA0374.md): Stringer · corroded · Jan 25, 2006 · N191FE · Boeing 727100 · Fuselage Main, Longeron/Stringer
  > AFT CARGO COMPARTMENT, CORROSION ON STR. 30 BS 1166 TO BS 1183 BL 0. REPAIRED STR 30 BS 1140 - 1183 IAW SRM 53-10-3, 51-10-2 AND 51-30-2.
- [SDR 06FDEA0308](https://openairdocs.org/sdr/06FDEA0308.md): Lamp · inoperative · Jan 21, 2006 · N185FE · Boeing 727100 · Landing Gear Position and Warning
  > LT MLG GREEN LIGHT DID NOT ILLUMINATE FOR LANDING. CREW REPORTED GEAR WAS DOWN BY VISUAL INSPECTION UPON ARRIVAL RE-LAMPED LEFT MAIN GEAR GREEN LIGHT OPS CHECK GOOD IAW MMSP.
- [SDR 06FDEA0298](https://openairdocs.org/sdr/06FDEA0298.md): Structure · corroded · Jan 20, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > WHILE WORKING N01170 FOUND CORROSION ON EXTERIOR FUSELAGE STRUCTURE AT BS 352, LBL 17, WL 145. REMOVED AND REPLACED STRUCTURE IAW SRM 53-10-1, 51-30-2.
- [SDR 06FDEA0304](https://openairdocs.org/sdr/06FDEA0304.md): Flap Track · corroded · Jan 20, 2006 · N191FE · Boeing 727100 · Trailing Edge Flaps
  > CORROSION ON NR 2 FLAP TRACK, AFT O/B MOUNTING HOLE. NEW NR 2 FLAP TRACK WAS INSTALLED ON FED-EX W/C 27X5706-03.
- [SDR 06FDEA0286](https://openairdocs.org/sdr/06FDEA0286.md): Door Frame · corroded · Jan 19, 2006 · N191FE · Boeing 727100 · Emergency Exits
  > CORROSION ON RIGHT FWD EMERGENCY EXIT HATCH EXTERIOR LWR EDGE FRAME UNDER PRESS SEAL. *S/D* RIGHT FWD EMERGENCY EXIT DOOR WAS OVERHAULED IAW WORK ORDER MR1382409.
- [SDR 06FDEA0214](https://openairdocs.org/sdr/06FDEA0214.md): Stringer · cracked · Jan 16, 2006 · N191FE · Boeing 727100 · Wing, Longeron/Stringer
  > LT WING, STA 629.00 THIRD STRINGER FROM REAR SPAR IS CRACKED.
- [SDR 06FDEA0181](https://openairdocs.org/sdr/06FDEA0181.md): Floorbeam · corroded · Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION STA 312 LBL 30 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT STA 312, LBL 30, WL 208 PER SRM 53-10-8, 53-10-1.
- [SDR 06FDEA0180](https://openairdocs.org/sdr/06FDEA0180.md): Floorbeam · corroded · Jan 13, 2006 · N191FE · Boeing 727100 · Fuselage Main, Floor Beam
  > CORROSION STA 328 LBL 30 AND LBL 40 WL 208 CORROSION ON FLOORBEAM UPPER CHORD. *S/D* REPAIRED FLOORBEAM AT BS 328, LBL 30 AND 40, WL 208 PER SRM 53-10-8, 53-10-1, 51-30-02.
- [SDR 06FDEA0157](https://openairdocs.org/sdr/06FDEA0157.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145. *S/D* REPAIRED SKIN IAW SRM 53-30-3.
- [SDR 06FDEA0155](https://openairdocs.org/sdr/06FDEA0155.md): Skin · dented · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > DENT IN EXTERNAL FUSELAGE SKIN AT BS 1163, STR 9L. *S/D* DENT IN FUSELAGE SKIN AT BS 1163, STR 9L REPAIRED IAW SRM 53-30-3.
- [SDR 06FDEA0158](https://openairdocs.org/sdr/06FDEA0158.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR FUSELAGE SKIN HAS A CRACK AT BS 352, LBL 18, WL 145.
- [SDR 06FDEA0156](https://openairdocs.org/sdr/06FDEA0156.md): Skin · cracked · Jan 12, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > EXTERIOR SKIN HAS A CRACK AT FASTENER HOLE AT BS 352, RBL 18, WL 145. REPAIRED CRACK PER ER 06-1285 AND FED EX EA 7-5330-96592.
- [SDR 06FDEA0149](https://openairdocs.org/sdr/06FDEA0149.md): Shear Tie · corroded · Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1110. *S/D* REMOVED FASTENERS COMMON TO SHEAR TIE, REMOVED CORROSION OUT OF LIMITS. CUT OUT DAMAGE, FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-4.
- [SDR 06FDEA0148](https://openairdocs.org/sdr/06FDEA0148.md): Skin · corroded · Jan 11, 2006 · N191FE · Boeing 727100 · Fuselage Main, Plate/Skin
  > WHILE INSPECTING LT LOWER NOSE CHORD INSTALLATION FOUND SKIN DISBONDED AND CORRODED AT BS 297, LBL 20, WL 148.
- [SDR 06FDEA0135](https://openairdocs.org/sdr/06FDEA0135.md): Failsafe · cracked · Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > FAIL SAFE CHORD CRACKED BS 990 STR 25L. *S/D* CUT OUT AND REMOVED DAMAGED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIR SECTION PER SRM 51-40-3 FIG 1, IAW SRM 51-30-2.
- [SDR 06FDEA0134](https://openairdocs.org/sdr/06FDEA0134.md): Failsafe · cracked · Jan 10, 2006 · N191FE · Boeing 727100 · Fuselage Main, Structure
  > FAIL SAFE CHORD CRACKED BS 1030 STR 25L. *S/D* REMOVED FAIL SAFE CHORD, FABRICATED AND INSTALLED REPAIR AND REPAIRED SECTION PER SRM 51-40-3, 51-30-2.
- [SDR 06FDEA0104](https://openairdocs.org/sdr/06FDEA0104.md): Shear Tie · unknown · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT ON SHEAR TIE BETWEEN STR 30 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.
- [SDR 06FDEA0103](https://openairdocs.org/sdr/06FDEA0103.md): Shear Tie · corroded · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Internal Mounting Structure
  > AFT CARGO COMPARTMENT, CORROSION ON SHEAR TIE BETWEEN STR. 28 LT AND 29 LT BS 1130. REPLACED SHEAR TIE IAW SRM 51-30-2.
- [SDR 06FDEA0102](https://openairdocs.org/sdr/06FDEA0102.md): Frame · corroded · Jan 9, 2006 · N191FE · Boeing 727100 · Fuselage Main, Frame
  > WHILE WORKING ON ACCESSING FOR N00743, FOUND CORROSION ON LT MIDDLE NOSE CHORD AT BS 297-BS 352, WL 169, LBL 16. ** SD ** COMING

Next page: https://openairdocs.org/model/boeing-727-100/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 = '727100'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-100/reports

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