# Service difficulty reports: Boeing 727-108C

A list on [Boeing 727-108C](https://openairdocs.org/model/boeing-727-108c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 255 reports

- [SDR UPS07248814](https://openairdocs.org/sdr/UPS07248814.md): Latch · broken · Jan 1, 2007 · N936UP · Boeing 727108C · Emergency Equipment
  > INSPECTION TYPE:N/A MAIN CABIN DOOR ENTRY EMERGENCY DOOR SLIDE LATCH ASSY BROKEN. INSTALLED NEW LATCH ON EMERGENCY SLIDE ASSY AS OUTLINED IN AMM 25-60-15-2 (IPC 25-60-00 ITEM 015).
- [SDR UPS06248627](https://openairdocs.org/sdr/UPS06248627.md): Light · malfunctioned · Nov 14, 2006 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHT ILLUMINATED IN FLIGHT COULD NOT RESET. STAYED ON. ACCOMPLISHED EMERGENCY LIGHTING ADJUSTMENT/TEST IAW MM 33-50-01-5. SYSTEM CHECKS GOOD. UNABLE TO DUPLICATE PROBLEM.
- [SDR UPS06247727](https://openairdocs.org/sdr/UPS06247727.md): Shear Tie · cracked · Aug 19, 2006 · N936UP · Boeing 727108C · Fuselage Internal Mounting Structure
  > INSPECTION TYPE:SV SHEAR TIE CRACKED AT STA 441 STR 26L. REMOVED CRACKED SHEAR TIE AT STA 441 STR 26L IAW SRM 51-30-02, FABRICATED AND INSTALLED SHEAR TIE AT STA 441 STR 26L IAW DWG 6913293 AND SRM 51-30-02.
- [SDR UPS06246772](https://openairdocs.org/sdr/UPS06246772.md): Connector · inoperative · Apr 29, 2006 · N936UP · Boeing 727108C · Navigation System Wiring
  > IN FLIGHT, CAPTAIN'S VOR/FLAG INDICATED RED. STATIONS SELECTED ALL ALONG FLIGHT WITH NO GOOD INDICATION ON EASI. TAE NAV 1 DENTS WERE GOOD, DME AND RMI NEEDLES MATCHED FO'S INDICATIONS. NORMAL AND OVERRIDE WERE ALSO SELECTED ON RADIO CONTROL. DIVERSION. R
- [SDR UPS06246100](https://openairdocs.org/sdr/UPS06246100.md): Skin · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C EVIDENCE OF FRETTING FOUND AT BS 1080 TO 1139.5 FROM STR 24L TO STR 26 L ON THE SKIN. SKIN REPLACMENT REQUIRED AT THIS LOCATION, CARRIED OUT IAW AAAE EO NR 2006-003-001 - UPS REF NR B727-5330-23687-A.
- [SDR UPS06246098](https://openairdocs.org/sdr/UPS06246098.md): Mount · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Engine Mount Section
  > INSPECTION TYPE:A ENG NR 1 PYLON FWD ENGINE MOUNT, AFT O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246097](https://openairdocs.org/sdr/UPS06246097.md): Mount · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Engine Mount Section
  > INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT FWD O/B HOLE, HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246096](https://openairdocs.org/sdr/UPS06246096.md): Mount · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Engine Mount Section
  > INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, AFT O/B HOLE HAS PITTING CORROSION IN BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246095](https://openairdocs.org/sdr/UPS06246095.md): Mount · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Engine Mount Section
  > INSPECTION TYPE:C NR 3 PYLON FWD ENGINE MOUNT, FWD O/B HOLE PITTING CORROSION IN BORE OF HOLE. REPAIR CARRIED OUT IAW EO B727-5440-11592-A.
- [SDR UPS06246094](https://openairdocs.org/sdr/UPS06246094.md): Mount · corroded · Jan 13, 2006 · N936UP · Boeing 727108C · Nacelle/Pylon, Attach Fittings
  > INSPECTION TYPE:C NR 3 PYLON FWD MOUNT, FWD I/B HOLE HAS PITTING CORROSION. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS06246102](https://openairdocs.org/sdr/UPS06246102.md): Beam · corroded · Jan 12, 2006 · N936UP · Boeing 727108C · Fuselage Main, Structure
  > INSPECTION TYPE:C CORROSION FOUND ON RT FWD FACE OF HORIZONTAL BEAM ATTACH POINT TO BS 740 FITTING. REPLACED HORIZONTAL BEAM IAW SRM NR 51-30-2 AND DRW NO.65-15927.
- [SDR UPS06246101](https://openairdocs.org/sdr/UPS06246101.md): Floorbeam · corroded · Jan 12, 2006 · N936UP · Boeing 727108C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C ON REMOVAL OF FLOORBOARD AT BS 360 EVIDENCE OF CORROSION FOUND. UPPER CHORD OF FLOORBEAM REMOVED BETWEEN RBL 12 AND LBL 67 AT BS 360. REPAIR CARRIED OUT IAW SRM NR 53-10-5.
- [SDR UPS06246085](https://openairdocs.org/sdr/UPS06246085.md): Angle · corroded · Jan 10, 2006 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C RT FUSE ABOVE NR 2 ENG AT THE ANGLE BETWEEN FUSE AND VERT STAB HAS LIGHT SURFACE CORROSION AT BS1428 TO 1464. DAMAGED ANGLE REMOVED AND REPLACEMENT ANGLE FABRICATED IAW DRW. NR QF5314263. REPLACEMENT ANGLE INSTALLED IAW SRM51-30-02 AND DR
- [SDR UPS06246099](https://openairdocs.org/sdr/UPS06246099.md): Mount · corroded · Jan 3, 2006 · N936UP · Boeing 727108C · Engine Mount Section
  > INSPECTION TYPE:C NR 1 PYLON FWD ENGINE MOUNT, FWD I/B HOLE, PITTING CORROSION IN THE BORE OF HOLE. REPAIRED IAW EO B727-5440-11592-A.
- [SDR UPS05244442](https://openairdocs.org/sdr/UPS05244442.md): Oxygen Mask · inoperative · May 12, 2005 · N936UP · Boeing 727108C · Crew Oxygen System
  > CREW PREFLIGHT - F/O O2 MASK WOULD NOT TRANSMIT. REMOVED AND REPLACED F/O'S 02 MASK ASSY. OPS CKS GOOD IAW MM 35-11-00.
- [SDR UPS04243067](https://openairdocs.org/sdr/UPS04243067.md): Attach Angle · corroded · Aug 26, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, DURING INSPECTION OF SKIN REPAIR, AT 1334 LT SIDE AFT AIRSTAIRS, SKIN ATTACH ANGLE FOUND CORRODED. REPLACED ATTACH ANGLE IAW SRM 51-10-01.
- [SDR UPS04243032](https://openairdocs.org/sdr/UPS04243032.md): Support Bracket · cracked · Aug 26, 2004 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE: C, SUPPORT BRACKET FOR NR 5 FWD FLAP TRACK FAIRING FOUND CRACKED ON O/B SIDE OF NR 5 FLAP TRACK. SUPPORT BRACKET REMOVED IAW SRM 51-30-02, NEW ANGLE FABRICATED IAW SRM 51-20-01, ANGLE PROTECTED IAW SRM 51-10-01, ANGLE INSTALLED ON FLAP TRACK
- [SDR UPS04243079](https://openairdocs.org/sdr/UPS04243079.md): Casting · cracked · Aug 23, 2004 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE: C, CRACK ON NR 7 FLAP TRACK CASTING ON VERTICAL FLANGE SECOND FROM I/B. HFEC CARRIED OUT - CRACKS CONFIRMED AND ENDS MARKED. STOP DRILLED CRACKS IAW SRM 51-10-1. OUTSIDE LIMITS PER SRM 51-10-6. CASTING REPLACED AND INSTALLED IAW DRG 65-162
- [SDR UPS04243070](https://openairdocs.org/sdr/UPS04243070.md): Stiffener · corroded · Aug 23, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C, HORIZONTAL STIFFNER CORRODED AFT OF APU EXHAUST PORT ON LOWER SURFACE OF UPPER PANEL AT 2 LOCATIONS. CORROSION FOUND TO BE OUTSIDE LIMITS. STIFFNER REMOVED IAW SRM 51-30-02. NEW STIFFNER INSTALLED IAW DRG 65-21655.
- [SDR UPS04243068](https://openairdocs.org/sdr/UPS04243068.md): Strap · corroded · Aug 23, 2004 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C ON INSP FLOOR PANEL SPLICE STRAP FOUND BADLY CORRODED AT BS 520 BETWEEN RBL 24 AND LBL 24. SPLICE STRAP REPLACED IAW SRM 51-20-01
- [SDR UPS04243066](https://openairdocs.org/sdr/UPS04243066.md): Light · defective · Aug 23, 2004 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION TYPE: C-COCKPIT EMERGENCY LIGHT DOES NOT ILLUMINATE WITH SWITCH ON P5 PANEL TO ON. LIGHT ASSEMBLY FOUND DEFECTIVE IAW WDM 33-51-01. LIGHT ASSY REPLACED IAW MM 33-50-01. FUNCTION CHECKED OK.
- [SDR UPS04243080](https://openairdocs.org/sdr/UPS04243080.md): Skin · corroded · Aug 22, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SUSPECT CORROSION BS 1340 BETWEEN STR 8L AND 9L DAMAGED SKIN REMOVED FROM BS 1323 TO BS 1342, FROM FIN TO STR 10L IAW SRM 51-10-6 AND REPAIRED IAW AAAE EO 2004-077-007. REF UPS FILE 727-53-20160.
- [SDR UPS04243077](https://openairdocs.org/sdr/UPS04243077.md): Doubler · cracked · Aug 22, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, CRACK ON DOUBLER RT SIDE BS 1444 APPROX. CRACK CUT OUT IAW SRM 51-40-02. HFEC CARRIED OUT IAW NDT MANUAL 51- 00-00 PT 6 FIG 4. NO DEFECTS FOUND. REPAIR DOUBLER FABRICATED IAW SRM 51-40-02 AND INSTALLED IAW SRM 51-30-02.
- [SDR UPS04243081](https://openairdocs.org/sdr/UPS04243081.md): Spar · corroded · Aug 17, 2004 · N936UP · Boeing 727108C · Wing Spar
  > INSPECTION TYPE: C, CRACK INDICATION AT WS 205 ON LT UPPER CHORD REAR SPAR. REPAIR CARRIED OUT IAW AAAE EO 2004-077-005. REF UPS EO B727-5710-20995.
- [SDR UPS04243062](https://openairdocs.org/sdr/UPS04243062.md): Skin · debonded · Aug 17, 2004 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE:C LT OB MIDFLAP T-EDGE WEDGE UPPER SKIN DISBOND 45 INCHES IB OF OB EDGE. DAMAGE REPAIRED IAW SRM 51-40-5
- [SDR UPS04243063](https://openairdocs.org/sdr/UPS04243063.md): Lap Joint · corroded · Aug 16, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SUSPECT CORROSION AT LAP JOINT S19L BETWEEN BS 390 AND BS 441, CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 51-30-02. REPAIR CARRIED OUT IAW AAAE 2004-077-006 AND UPS EO B727-5330-21003-A.
- [SDR UPS04243076](https://openairdocs.org/sdr/UPS04243076.md): Skin · corroded · Aug 13, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE: C, SUSPECT CORROSION BETWEEN SKIN AND INTERNAL STRUCTURE BS 217 STR 25L. AREA PAINT STRIPPED IAW MM 51-20-15. TRIMMED CORRODED AREA IAW SRM 53-30-03 AND REPAIRED AREA IAW SRM 53-30-3 FIG. 3.
- [SDR UPS04243064](https://openairdocs.org/sdr/UPS04243064.md): Skin · cracked · Aug 12, 2004 · N936UP · Boeing 727108C · Fuselage Main, Plate/Skin
  > C-CRACKS ON CENTER POST OF COCKPIT WINDOWS, NR 1 LT AND NR 1 RT, LOWER IB CORNERS. HFEC CARRIED OUT AND CRACKS CONFIRMED. CRACKED SKIN REPLACED IAW AAAE EO 2004-077-004 AND UPS FILE NR 727-53-20157.
- [SDR UPS03241671](https://openairdocs.org/sdr/UPS03241671.md): Light · inoperative · Dec 23, 2003 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHT FOR CABIN INOP. REMOVED AND REPLACED CABIN EMERGENCY LIGHTING FIXTURE PER MM 33-50. OPS CHECKS NORMAL AT THIS TIME.
- [SDR UPS03241668](https://openairdocs.org/sdr/UPS03241668.md): Light · inoperative · Dec 18, 2003 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION TYPE:PFLT CABIN DOOR EMERGENCY EXIT LIGHT INOP. RELAMPED CABIN DOOR, EMERGENCY EXIT LIGHT OPS CHECKS NORMAL AT THIS TIME PER MM 33-50.
- [SDR UPS03241214](https://openairdocs.org/sdr/UPS03241214.md): Battery · discharged · Sep 10, 2003 · N936UP · Boeing 727108C · Emergency Lighting
  > INSPECTION TYPE: ASV, EMERGENCY EXIT LIGHTS INOPERATIVE IN COCKPIT AND FORWARD ENTRY REMOVED AND REPLACED EMERGENCY EXIT LIGHT BATTERY. OPS CKS GOOD.
- [SDR UPS03240298](https://openairdocs.org/sdr/UPS03240298.md): Floorbeam · corroded · Feb 28, 2003 · N936UP · Boeing 727108C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 950 LBL 50. REPAIR CARRIED OUT IAW SRM EO 2003-008-022. UPS ENGINEERING FILE 7 27-53-20100.
- [SDR UPS03240279](https://openairdocs.org/sdr/UPS03240279.md): Doubler · corroded · Feb 26, 2003 · N936UP · Boeing 727108C · Fuselage Main, Structure
  > INSPECTION TYPE: C&SI, ON REMOVAL OF WINDOW FRAME TO FACILITATE BS 870 FITTING REPLACEMENT CORROSION FOUND ON FLANGE OF WINDOW FRAMES, FRAME AT BS 880 AT LWR AFT CENTER. CORROSION BLENDED OUT IAW SRM 51-10-6 & AREA OF DAMAGE FOUND OUTSIDE LIMITS IAW SRM 56-2
- [SDR UPS03240293](https://openairdocs.org/sdr/UPS03240293.md): Fitting · cracked · Feb 25, 2003 · N936UP · Boeing 727108C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE: C&SI, DURING REMOVAL OF UPPER AIRSTAIR THREADS IT WAS NOTED THAT THE TAILSKID ACTUATOR FITTING (RT SIDE) WAS CRACKED (TRUNNION FITTING). TAILSKID TRUNNION FITTING REMOVED & REPLACED IAW SRM 51-10-01 & DRG 65-25992.
- [SDR UPS03240292](https://openairdocs.org/sdr/UPS03240292.md): Yoke · cracked · Feb 25, 2003 · N936UP · Boeing 727108C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE: C&SI, DURING REMOVAL OF TAILSKID ACTUATOR FITTING, TAILSKID YOKE ASSY FOUND CRACKED. TAILSKID YOKE ASSY REPLACED IAW MM 32-71-41.
- [SDR UPS03240278](https://openairdocs.org/sdr/UPS03240278.md): Stiffener · cracked · Feb 25, 2003 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI #6 FLAP TRACK AFT O/B ATTACH POINT VERTICAL STIFFENER ON R/H FALSE S PAR CRACKED STIFFENER REMOVED IAW SRM 51-30-2. STIFFENER REPLACED IAW SRM 51-30 -02 & DRAWING 65-16216
- [SDR UPS03240256](https://openairdocs.org/sdr/UPS03240256.md): Pad · corroded · Feb 25, 2003 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE:C&SI #6 FLAP TRACK AFT ATTACH POINT LWR PAD ON R/H FALSE SPAR HAVE EVIDEN CE OF CORROSION REMOVED PAD IAW SRM 51-30-02. ON REMOVAL OF CORROAION, CORROSION FOU ND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPLACED PAD IAW SRM 51-30- 02
- [SDR UPS03240300](https://openairdocs.org/sdr/UPS03240300.md): Skin · corroded · Feb 23, 2003 · N936UP · Boeing 727108C · Wing, Plate/Skin
  > INSPECTION TYPE:C&SI EVIDENCE OF CORROSION BETWEEN WING CENTER SECTION UPPER SKIN & SKIN UPPER SPLICE @ BS 856 - 860 I/B OF WBL 70.5 RIGHT REPAIR CARRIED OUT IAW SRM 51-10-1, 51-10-2, 51-30-02 & SMRO EO 2003 -008-018 UPS ENGINEERING FILE NO B727-5730-18440
- [SDR UPS03240254](https://openairdocs.org/sdr/UPS03240254.md): Stiffener · corroded · Feb 23, 2003 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C&SI, CORROSION ON INTERNAL SIDE OF NLG LT SIDE WALL AT BS 285 (FWD OF VERTICAL STIFFENER) LWR END CORROSION FOUND AT BS 280 & 285 BETWEEN STIFFENER AND SKIN. SKIN CUTOUT MADE AT VERT STIFFENER TO REMOVE CORROSION IAW SRM 51-10-6. DOUBLER F
- [SDR UPS03240290](https://openairdocs.org/sdr/UPS03240290.md): Seat Track · corroded · Feb 21, 2003 · N936UP · Boeing 727108C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C&SI CABIN SEAT TRACK AT STA 650 TO 680 HAS CORROSION ON O/B FLANGE OF T RACK LBL 45.5. CORROSION REMOVED IAW SRM 53-10-1 OUT OF LIMITS. SEAT TRACK SECTION REMOVED BETWEEN BS 650-740 LBL 45.5 IAW SRM 51-30-2. NEW SECTION OF SEAT TRACK FABRIC
- [SDR UPS03240274](https://openairdocs.org/sdr/UPS03240274.md): Stiffener · corroded · Feb 21, 2003 · N936UP · Boeing 727108C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C+SI, VERT STIFFENER HAS INTERGRANULAR CORROSION AT BS 343 APPROX AT NLG CUTOUT LT VERT WEB. INSTALLED NEW STIFFENER IAW SRM 51-30-02.
- [SDR UPS03240255](https://openairdocs.org/sdr/UPS03240255.md): Casting · corroded · Feb 21, 2003 · N936UP · Boeing 727108C · Aileron Tabs
  > INSPECTION TYPE: C&SI, LT O/B AILERON TAB FIRST & SECOND FROM O/B HINGE CASTINGS HAVE PITTING CORROSION. HINGE CASTINGS REPLACED IAW MM 27-10-19.
- [SDR UPS03240294](https://openairdocs.org/sdr/UPS03240294.md): Seat Track · corroded · Feb 20, 2003 · N936UP · Boeing 727108C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI CORROSION ON SEAT TRACK LBL 42.84 BETWEEN BS 344 & 480 SEAT TRACK REMOVED IAW SRM 51-30-2. NEW SEAT TRACK FABRICATED IAW S RM 51-20-1. NEW SEAT TRACK REPROECTED IAW SRM 51-10-2.NEW SEAT TRACK INSTALLED IAW SRM 51-30-2
- [SDR UPS03240289](https://openairdocs.org/sdr/UPS03240289.md): Fitting · cracked · Feb 19, 2003 · N936UP · Boeing 727108C · Fuselage Main, Structure
  > INSPECTION TYPE:C&SI L/H 870 FITTING HAS 2 CRACKS FWD OF CENT. LINE IN 1ST ROW OF FASTENE RS (HOLES 3 & 4) AND 1 CRACK IN AFT OF BUTT LINE 1ST ROW 3RD FASTENE R FROM TOP FITTING REPLACEMENT CARRIED OUT IAW UPS EO B727-5310-3056 APPENDIX E
- [SDR UPS03240281](https://openairdocs.org/sdr/UPS03240281.md): Frame · cracked · Feb 19, 2003 · N936UP · Boeing 727108C · Fuselage Main, Frame
  > INSPECTION TYPE: C&SI, SUB FRAME AT BS 920 RT HAS SMALL CRACK AT STR 15. SUB FRAME AT BS 920 RT REPAIRED IAW SRM 51-40-03.
- [SDR UPS03240280](https://openairdocs.org/sdr/UPS03240280.md): Floorbeam · corroded · Feb 19, 2003 · N936UP · Boeing 727108C · Fuselage Main, Floor Beam
  > INSPECTION TYPE: C&SI, CORROSION ON FLOORBEAM TOP CAP BS 344 RBL 24.75 TO 24.75 LBL. CORROSION REMOVED IAW SRM 51-10-6 DEPTH OF BLEND-OUTS MEASURED AND FOUND TO BE OUT OF LIMITS IAW SRM 53-10-01 IN SEVERAL AREAS. FLOORBEAM TOP CHORD REPLACED IAW BOEING DRAW
- [SDR UPS03240273](https://openairdocs.org/sdr/UPS03240273.md): Carriage · corroded · Feb 19, 2003 · N936UP · Boeing 727108C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C+SI NO.7 FLAP TRACK CARRIAGE HAS PITTING COROSION ON BEARING MOUNT HOLE. FLAP TRACK CARRIAGE REPLACED IAW SB 27-112.
- [SDR UPS03240309](https://openairdocs.org/sdr/UPS03240309.md): Flap Track · corroded · Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE: C&S, NR 3 FLAP TRACK HAS SURFACE CORROSION IN THE FOLLOWING AREAS, INSIDE HOLE D, INSIDE HOLE E, INSIDE HOLE F, INSIDE HOLE G & FLAP AFT PAD (B). REPAIR CARRIED OUT IAW SRMO EO 2003-008-006 & 2003-008-012 UPS ENGINEERING FILE NR 727-57-20094.
- [SDR UPS03240308](https://openairdocs.org/sdr/UPS03240308.md): Attach Fitting · corroded · Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE: C&SI, NR 7 FLAP TRACK HAS SURFACE CORROSION ON FWD MOUNT LUG FACES A & D AND IN FWD LUG BOREHOLES. REPAIR CARRIED OUT IAW SRMO EO'S 2002-008-002 & 2003-008-011. UPS ENGINEERING FILE NR 727-57-20093.
- [SDR UPS03240307](https://openairdocs.org/sdr/UPS03240307.md): Attach Fitting · corroded · Feb 18, 2003 · N936UP · Boeing 727108C · Trailing Edge Flaps
  > INSPECTION TYPE: C&SI, ON INSPECTION OF NR 2 FLAP TRACK CORROSION FOUND ON FWD MOUNT LUG FACES A, B, C & D AND IN FWD LUG BOREHOLES A & B. REPAIR CARRIED OUT IAW SRMO EO'S 2003-008-001 & SMRO 2003-008-014. UPS ENGINEERING FILE NR 727-57-20096.

Next page: https://openairdocs.org/model/boeing-727-108c/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 = '727108C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-108c/reports

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.