# Service difficulty reports: Boeing 727-1A7C

A list on [Boeing 727-1A7C](https://openairdocs.org/model/boeing-727-1a7c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 3 · 118 reports

- [SDR UPS07249687](https://openairdocs.org/sdr/UPS07249687.md): Duct · blown · Apr 24, 2007 · N935UP · Boeing 7271A7C · Air Distribution System
  > EMERGENCY DECLARED, LWR AFT BODY OVERHEAT WARNING LIGHT ILLUM. ALL EPR INDICATIONS INOP. STDBY HYD OVERHEAT LT ILLUM. CAPT'S RADIO INTERMITTENT CREW WAS ASKED TO DEVIATE DUE TO WEATHER, BUT DECLARED EMERGENCY DUE TO VARIOUS MALFUNCTIONS. FOUND BLOWN DUCT I
- [SDR UPS06247519](https://openairdocs.org/sdr/UPS06247519.md): Web · cracked · Jul 26, 2006 · N935UP · Boeing 7271A7C · Leading Edge Devices
  > CRACK FOUND ON I/B WEB OF REMOVABLE LEADING EDGE AT BS 740 RT. DAMAGED AREA REMOVED AND REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS06247593](https://openairdocs.org/sdr/UPS06247593.md): Skin · corroded · Jul 14, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C HTD B-NUT HAS FRETTED SKIN IN HYD BAY AT BS 1000 AT STR 23 LEFT. MEASURED AND EVALUATED FRETTED SKIN AND FOUND OUT OF LIMITS IAW SRM 53-30-01. PREVIOUS REPAIR REMOVED IAW SRM 51-30-02. DAMAGE REPAIRED IAW SRM 53-30-3.
- [SDR UPS06247457](https://openairdocs.org/sdr/UPS06247457.md): Carriage · worn · Jul 14, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C WEAR IN NR 7 FLAP CARRIAGE SIDE ROLLER ASSY BRACKETS. FLAP CARRIAGE REPLACED IAW MM 27-51-13.
- [SDR UPS06247428](https://openairdocs.org/sdr/UPS06247428.md): Link · corroded · Jul 14, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 5 FLAP CARRIAGE BEARING LINK BEARING A DRIFT AND BUSHING CORRODED. CORROSION FOUND ON INNER SURFACE OF BEARING LINK. BEARING LINK ASSY AND BUSHING REPLACED IAW MM 27-51-03.
- [SDR UPS06247460](https://openairdocs.org/sdr/UPS06247460.md): Seat Track · corroded · Jul 13, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C SEAT TRACK AT RBL 40 2 BETWEEN BS 740-760 CORRODED. CORROSION FOUND OUT OF LIMITS IAW SRM 51-30-02. REPLACED SEAT TRACK IAW SRM 51-30-02.
- [SDR UPS06247456](https://openairdocs.org/sdr/UPS06247456.md): Carriage · worn · Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 8 FLAP CARRIAGE AFT SIDE ROLLERS FWD ATTACH HOLES WORN. FLAP CARRIAGE REPLACED IAW MM 27-51-13.
- [SDR UPS06247436](https://openairdocs.org/sdr/UPS06247436.md): Beam · corroded · Jul 13, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SIDE LOAD BEAM AT RIGHT BS 740 CORRODED. ANGLE FABRICATED IAW DRWG 65-15940. INSTALLED SIDE LOAD BEAM ANGLE IAW B727-5310-7477.
- [SDR UPS06247434](https://openairdocs.org/sdr/UPS06247434.md): Carriage · corroded · Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 4 FLAP CARRIAGE FWD LOWER FLANGE CORRODED. FLAP CARRIAGE REPLACED IAW MM 27-51-03.
- [SDR UPS06247386](https://openairdocs.org/sdr/UPS06247386.md): Carriage · corroded · Jul 13, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 5 FLAP CARRIAGE HAS CORROSION ON LWR FWD FLANGE UPPER AND LOWER SURFACES CARRIAGE REPLACED IAW MM 27-51-03.
- [SDR UPS06247385](https://openairdocs.org/sdr/UPS06247385.md): Carriage · corroded · Jul 12, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE-C, 3 SEQUENCE CARRIAGE HAS CORROSION ON AFT UPPER LUGS SEQUENCE CARRIAGE REPLACED IAW MM 27-51-04.
- [SDR UPS06247373](https://openairdocs.org/sdr/UPS06247373.md): Floor Support · cracked · Jul 12, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C AND SI FLOOR SUPPORT CRACKED AT BS 850 RBL 24.75. FLOOR SUPPORT REMOVED IAW SRM 51-30-02. NEW FLOOR SUPPORT FABRICATED I AW SRM 51-40-03. FLOOR SUPPORT PROTECTED IAW SRM 51-10-02. FLOOR SUP PORT PAINTED AND INSTALLED IAW SRM 51-40-03, 51-3
- [SDR UPS06247433](https://openairdocs.org/sdr/UPS06247433.md): Flap Track · corroded · Jul 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C CORROSION IN \1 FLAP TRACK HOLES E, D AND C. BUSHING FABRICATED IAW AAAE EO 2006-042-005. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.
- [SDR UPS06247429](https://openairdocs.org/sdr/UPS06247429.md): Flap Track · corroded · Jul 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C CORROSION IN NR 6 FLAP TRACK HOLES G AND F. BUSHINGS FABRICATED IAW AAAE-EO-2006-042-08. HEAT TREATED IAW 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.
- [SDR UPS06247375](https://openairdocs.org/sdr/UPS06247375.md): Floorbeam · corroded · Jul 11, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C AND SI CORROSION ON UPPER SURFACE OF FLOORBEAM UPPER FLANGE REPAIR AT BS 560 LBL 37. CORROSION REMOVED IAW SRM 51-10-6 AND FOUND TO BE OUT OF LIMITS. REPA IR STRAP REMOVED, NEW REPAIR STRAP FABRICATED IAW SRM 51-20-1. REPAIR STRAP REPROTE
- [SDR UPS06247353](https://openairdocs.org/sdr/UPS06247353.md): Support · corroded · Jul 11, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C AND SI CORROSION ON INTERCOSTAL SUPPORT CONTROL CABIN FLOOR, BL 0, FS 277 TO 29 4.5. CORROSION CLEANED AND SUPPORT FOUND TO BE OUTSIDE LIMITS. NEW SUPPORT FABRICATED IAW BOEING DRG 65-17593. NEW SUPPORT INSTALLED IAW SRM 51-30-2 WITH REFE
- [SDR UPS06247568](https://openairdocs.org/sdr/UPS06247568.md): Structure · corroded · Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Structure
  > INSPECTION TYPE:C EVIDENCE OF CORROSION AT BS 850 RT UNDER STR 18A. FASTENER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06. FASTENER REINSTALLED IAW SRM 51-30-02.
- [SDR UPS06247463](https://openairdocs.org/sdr/UPS06247463.md): Seat Track · corroded · Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 690-720 RBL 65. CORROSION OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.
- [SDR UPS06247432](https://openairdocs.org/sdr/UPS06247432.md): Attach Fitting · corroded · Jul 10, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C CORROSION ON NR 7 FLAP TRACK ATTACH PAD HOLE E. BUSHING FABRICATED IAW EO 2006-042-0009. HEAT TREATMENT REFERENCE 06-4 2-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.
- [SDR UPS06247431](https://openairdocs.org/sdr/UPS06247431.md): Attach Fitting · corroded · Jul 10, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE:C NR 8 FLAP TRACK ATTACH PAD HAS CORROSION IN HOLES E, D AND C. BUSHINGS FABRICATED FOR HOLES IAW AAAE EO 2006-042-10. HEAT TREATMENT REFERENCE 06-42-03. CAD PLATED IAW SOPM 20-42-10. INSTALLED IAW SOPM 20-50-03.
- [SDR UPS06247381](https://openairdocs.org/sdr/UPS06247381.md): Web · cracked · Jul 10, 2006 · N935UP · Boeing 7271A7C · Wing Miscellaneous Structure
  > INSPECTION TYPE-C SI RT WING STRUCTURE INNER WEB CRACKED AT NR 8 SLAT ACTUATOR CUTOUT, REPAIR OR REPLACE. REPAIRED IAW SRM 51-40-02 FIG 1.
- [SDR UPS06247365](https://openairdocs.org/sdr/UPS06247365.md): Seat Track · corroded · Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C AND SI EVIDENCE OF EXFOLIATION CORROSION ON UPPER FLANGE OF SEAT TRACK AT BS 5 92 RBL 45. NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-20-90 AND SRM 51-30-2, 53-10-5, AND 51-10-2.
- [SDR UPS06247364](https://openairdocs.org/sdr/UPS06247364.md): Seat Track · cracked · Jul 10, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C AND IS CRACKED ON SEAT TRACK TOP BS 397 RBL 23 NEW SEAT TRACK FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90, SRM 5 1-10-2 AND 51-30-2.
- [SDR UPS06247626](https://openairdocs.org/sdr/UPS06247626.md): Skin · damaged · Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SMALL NICK ON FUSE SKIN, DAMAGE LOCATED AT BASE OF C, D WINDOW POST. FASTENERS REMOVED FROM REPAIR AREA AND DAMAGE BLENDED OUT IAW SRM 53-30 -03. REPAIR DOUBLER INSTALLED IAW SRM 53-30-03.
- [SDR UPS06247462](https://openairdocs.org/sdr/UPS06247462.md): Stiffener · corroded · Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CORROSION ON FLOOR STRUCTURE STIFFENER AT RT SIDE AT BS 230 RBL 36. STIFFENER REPLACED IAW SRM 51-30-02.
- [SDR UPS06247374](https://openairdocs.org/sdr/UPS06247374.md): Intercostal · corroded · Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE-C AND SI CORROSION AROUND ANCHOR NUT HOLE UNDER COCKPIT DOOR SILL BS 303. REMOVED INTERCOSTAL UNDER COCKPIT DOOR IAW SRM 51-30-02. FABRICATED I NTERCOSTAL IAW SRM 51-20-1. INTERCOSTAL REPROTECTED IAW SRM 51-10-2. INTERCOSTAL PAINTED IAW MM
- [SDR UPS06247352](https://openairdocs.org/sdr/UPS06247352.md): Intercostal · gouged · Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 328 AND 334 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. INTERCOSTAL REMOVED AND NEW INTERCOSTAL INSTALLED IAW SRM 51-30-2 AND DRG 6
- [SDR UPS06247351](https://openairdocs.org/sdr/UPS06247351.md): Intercostal · gouged · Jul 8, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C AND SI DEEP GOUGE ON UPPER SURFACE OF INTERCOSTAL BETWEEN BS 312 - 328 LBL 30. DEEP GOUGE ON INTERCOSTAL REMOVED AND FOUND TO BE OUTSIDE LIMITS OF SRM 51-10-6. INTERCOSTAL REMOVED AND REPLACED IAW MM 51-20-90.
- [SDR UPS06247520](https://openairdocs.org/sdr/UPS06247520.md): Rib · cracked · Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge Devices
  > SUSPECT CRACK ON NR 6 SLAT ON 4TH RIB OB OF ACTUATOR AT UPPER AFT CORNER RIB REPLACED IAW SRM 51-30-02.
- [SDR UPS06247518](https://openairdocs.org/sdr/UPS06247518.md): Rib · cracked · Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge Devices
  > SUSPECT CRACK ON NR 6 SLAT ON 1ST RIB O/B OF I/B TRACK ALONG AFT FLANGE. RIB REPLACED IAW SRM 51-10-02, AND INSTALLED IAW SRM 51-30-02.
- [SDR UPS06247437](https://openairdocs.org/sdr/UPS06247437.md): Rib · cracked · Jul 7, 2006 · N935UP · Boeing 7271A7C · Leading Edge Devices
  > INSPECTION TYPE:C SUSPECT CRACK ON NR 5 SLAT 3RD RIB O/B OF IB TRACK AT AFT UPPER CORNER. SLAT REPLACED.
- [SDR UPS06247366](https://openairdocs.org/sdr/UPS06247366.md): Seat Track · corroded · Jul 7, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C AND SI CORROSION ON SEAT TRACK TOP CHORD BS 590-630 LBL 45.5 NEW SEAT TRACK FABRICATED, PAINT AND INSTALLED IAW MM 51-20-90, SRM 51- 30-2, 53-10-5
- [SDR UPS06247636](https://openairdocs.org/sdr/UPS06247636.md): Wedge · delaminated · Jul 6, 2006 · N935UP · Boeing 7271A7C · Ailerons
  > RT O/B AILERON HAS DELAM ON TRAILING EDGE WEDGE. AILERON BEYOND REPAIRABLE LIMITS, AILERON REPLACED IAW MM 27-10-14.
- [SDR UPS06247569](https://openairdocs.org/sdr/UPS06247569.md): Structure · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Wing Main, Frame Structure
  > INSPECTION TYPE:C SURFACE CORROSION AT BOTH I/B STATIC DISCHARGERS LEFT WING TIP T/E. CORROSION REMOVED IAW SRM 51-10-01 AND FASTENERS REMOVED IAW SRM 51-3 0-02. AREA O/B FOUND TO BE OUT OF LIMITS IAW SRM 57-20-01. DAMAGED AREA REPAIRED IAW SRM 57-20-05.
- [SDR UPS06247566](https://openairdocs.org/sdr/UPS06247566.md): Fitting · cracked · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C BS 740 TERMINAL FITTING REQUIRES REPLACING. FITTING REPLACED IAW EO B727-5310-7477 AND DRWG 65C13724.
- [SDR UPS06247464](https://openairdocs.org/sdr/UPS06247464.md): Seat Track · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE:C CORROSION ON SEAT TRACK TOP CHORD AT BS 950-962 RBL 62.5. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK REPLACED IAW SRM 51-30-02.
- [SDR UPS06247461](https://openairdocs.org/sdr/UPS06247461.md): Floorbeam · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 950 RBL 51-56. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06 AND 53-1001. FLOORBEAM TOP CHORD REPLACED IAW SRM 51-30-02.
- [SDR UPS06247455](https://openairdocs.org/sdr/UPS06247455.md): Panel · delaminated · Jul 6, 2006 · N935UP · Boeing 7271A7C · Wing, Plate/Skin
  > INSPECTION TYPE:C LT WING UPPER SURFACE PANEL FWD OF NR 5 AND 6 SPOILERS DELAM AT PREVIOUS REPAIR. DAMAGE FOUND TO BE OUT OF LIMITS IAW SRM 51-40-20. PANEL REPLACED IAW SRM 51-30-02.
- [SDR UPS06247430](https://openairdocs.org/sdr/UPS06247430.md): Floorbeam · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > INSPECTION TYPE:C CORROSION ON FLOORBEAM TOP CHORD BS 420 RBL 52-55. SPLICE ANGLE AND FILLER INSTALLED IAW SRM 53-10-8.
- [SDR UPS06247384](https://openairdocs.org/sdr/UPS06247384.md): Seat Track · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C CORROSION ON SEAT TRACK TOP BS 418-427 RBL 45.5. SEAT TRACK REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.
- [SDR UPS06247369](https://openairdocs.org/sdr/UPS06247369.md): Floorbeam · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 328 LBL 27-31 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. NEW FLOOBEAM TOP CHORD FABRICATED, PAINTED AND INSTALLED IAW MM 51-21-90 AND SRM 53-10-8.
- [SDR UPS06247368](https://openairdocs.org/sdr/UPS06247368.md): Floorbeam · corroded · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > INSPECTION TYPE-C AND SI CORROSION ON FLOORBEAM TOP CHORD BS 344 LBL 16-23 CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-6. FLOORBEAM TOMP P CHORD FABRICATED, PAINTED AND INSTALLED IAW SRM 53-10-08 AND MM 51-21- 90.
- [SDR UPS06247354](https://openairdocs.org/sdr/UPS06247354.md): Fitting · cracked · Jul 6, 2006 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C AND SI CRACKS DETECTED ON BS 740 STR 18R - STR 24R. ON INVESTIGATION CRACKS FOUND TO BE OUTSIDE LIMITS IAW SB 727-53-0062. REFERENCE NRC 100347 FOR BS 740 FITTING REPLACEMENT.
- [SDR UPS06247567](https://openairdocs.org/sdr/UPS06247567.md): Channel · corroded · Jul 5, 2006 · N935UP · Boeing 7271A7C · APU Exhaust System
  > INSPECTION TYPE:C AFT SUPPORT CHANNEL FOR APU EXHAUST ON THE LOWER SIDE UPPER WING PANEL IS CORRODED. CHANNEL REPLACED IAW SRM 51-20-01.
- [SDR UPS06247383](https://openairdocs.org/sdr/UPS06247383.md): Seat Track · corroded · Jun 11, 2006 · N935UP · Boeing 7271A7C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE-C CORROSION ON SEAT TRACK, TOP CHORD BS 481 RBL 45.5 CORROSION FOUND OUTSIDE LIMITS IAW SRM 53-10-1. SEAT TRACK AND CONNECT OR REPLACED IAW SRM 53-10-05 AND SRM 51-30-02.
- [SDR UPS06247382](https://openairdocs.org/sdr/UPS06247382.md): Flap Track · corroded · Jun 11, 2006 · N935UP · Boeing 7271A7C · Trailing Edge Flaps
  > INSPECTION TYPE-C CORROSION IN NR 5 FLAP TRACK HOLE G. CORROSION REMOVED IAW OHM 57-40-01. MPI CARRIED OUT IAW BSOPM 20-20-0 1. BUSHING FABRICATED IAW EO 20065-042-007. STYLUS CAD PLATING CARRIED OUT IAW SOPM 20-42-10. INSTALLED BUSHING IAW SOPM 20-50-03.
- [SDR UPS05243879](https://openairdocs.org/sdr/UPS05243879.md): Angle · cracked · Feb 3, 2005 · N935UP · Boeing 7271A7C · Wing Miscellaneous Structure
  > LT WING PANEL ON UPPER SURFACE ABOVE NR 1 TRANSMISSION AFT FAIRING I/B ANGLE AND REPAIR CRACKED. ANGLE REPLACED IAW SRM 51-30-01 AND 51-30-02.
- [SDR UPS05243890](https://openairdocs.org/sdr/UPS05243890.md): Floorbeam · corroded · Feb 2, 2005 · N935UP · Boeing 7271A7C · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT BS 680 LBL 56 FOUND ON REMOVAL OF FLOOR PANELS FOR DOOR SILL INSPECTION. REPAIR CARRIED OUT IAW SRM 51-10-2, 53-10-8, 51-20-4 AND AAAE EO 2005-01 0-004 UPS ENGINEERING FILE NR 727-53-20183.
- [SDR UPS05243888](https://openairdocs.org/sdr/UPS05243888.md): Angle · cracked · Feb 1, 2005 · N935UP · Boeing 7271A7C · Fuselage Miscellaneous Structure
  > AFT AIRSTAIRS ANGLE CRACKED AT FORWARD SIDE OF BS 1203 FRAME LT AT S13L. STOP DRILLED CRACK IAW 51-10-1. HFEC CARRIED OUT IAW NDTM PT6 51-00 -00, CRACK CONTAINED BY STOP DRILLED HOLE. REFER TO UPS FILE NUMBER 727-53-20182.
- [SDR UPS05243878](https://openairdocs.org/sdr/UPS05243878.md): Casting · cracked · Feb 1, 2005 · N935UP · Boeing 7271A7C · Spoilers
  > NR 8 SPOILER I/B END HINGE CASTING IS CRACKED AT FASTENER HOLE. HINGE CASTING REPLACED IAW SRM 51-30-2.

Next page: https://openairdocs.org/model/boeing-727-1a7c/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 = '7271A7C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-1a7c/reports

---
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