# Service difficulty reports: Boeing 727-27C

A list on [Boeing 727-27C](https://openairdocs.org/model/boeing-727-27c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 22 · 1,078 reports

- [SDR CA110817010](https://openairdocs.org/sdr/CA110817010.md): Actuator · sheared · Aug 16, 2011 · Boeing 72727C · Leading Edge Slat Actuator
  > (CAN) UPON DEPARTURE THE NR 2 SLAT FAILED TO RETRACT. THE FLAPS WERE CYCLED AND SHORTLY AFTER "A" SYS HYD QTY WENT TO ZERO. AN EMERGANCY WAS DECLARED AFTER THE CHECK LISTS WERE RUN, AND LANDED WITHOUT PROBLEM. DUE TO HYD LOSS THE ACFT WAS TOWED OFF THE RUNW
- [SDR UPS03240006](https://openairdocs.org/sdr/UPS03240006.md): Battery · discharged · Jan 9, 2003 · N909UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE: PFLT. EMERGENCY EXIT LIGHT ASSEMBLIES AT CABIN ENTRY AND CREW ENTRY DOOR BATTERIES DEAD. RECHARGED BATTERIES, OPS CHECKS OKAY.
- [SDR UPS02239857](https://openairdocs.org/sdr/UPS02239857.md): Cover · loose · Nov 4, 2002 · N908UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A MAIN ENTRY DOOR EMERGENCY LIGHT FELL OUT OF BRACKET DURING T/O. R&R MAIN ENTRY DOOR EMERGENCY LIGHT COVER OK FOR CONTINUED SERVICE.
- [SDR UPS02238614](https://openairdocs.org/sdr/UPS02238614.md): Slat · cracked · Jun 12, 2002 · N910UP · Boeing 72727C · Leading Edge Devices
  > INSPECTION TYPE:AS NR 5 SLAT CRACKED OUTBOARD OF FENCE JUST OUTBOARD OF UPSTOP. REMOVED AND REPLACED NR 5 SLAT PER MM 27-81-11, RIG AND OPS CHECK GOOD.
- [SDR UPS02237507](https://openairdocs.org/sdr/UPS02237507.md): Battery · discharged · Jan 23, 2002 · N910UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT BATTERIES NOT CHARGED OVER MAIN ENTRY DOOR, PARTS ON F/E'S DESK LIGHT ASSY 10-0067-9. INSTALLED NEW BATTERIES.
- [SDR UPS02237399](https://openairdocs.org/sdr/UPS02237399.md): Light · inoperative · Jan 7, 2002 · N909UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:PFLT L1 DOOR EMERGENCY EXIT LIGHT INOP. REMOVED AND REPLACED LIGHT ASSEMBLY PER MM 33-50-01, OPS CHECK NORMAL.
- [SDR UPS01237314](https://openairdocs.org/sdr/UPS01237314.md): Smoke Detector · inoperative · Nov 17, 2001 · N914UP · Boeing 72727C · Smoke Detection
  > INSPECTION TYPE:N/A TARGET ALERT H20824 LOWER CARGO SMOKE DETECTION. LOWER CARGO SMOKE DETECTOR MX LT ILLUM. TECH RECOMMENDS: SUSPECT A-CHANNEL OF CCU FAILED. REPLACE CCU. PERFORMED ADJUSTMENT TEST PER MM 26-18-01, VERIFIED SN OF SMOKE DETECTORS. NO FURT
- [SDR UPS01237194](https://openairdocs.org/sdr/UPS01237194.md): Battery · discharged · Oct 29, 2001 · N909UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:IN CREW ENTRANCE DOOR EMERGENCY EXIT LIGHT WENT DIM SHORTLY AFTER TESTING LIGHTS. REPLACED BATTERIES WITH CHARGED UNITS. OPS CHECKED GOOD IAW MM 33-51-01 PG 104. P/N S106
- [SDR UPS01237094](https://openairdocs.org/sdr/UPS01237094.md): Battery · discharged · Oct 18, 2001 · N909UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:N/A, OVERHEAD LIGHTS ABOVE CREW ENTRY DOOR INOP. REPLACED BATTERIES IAW 33-50-00. OPS CHECKS GOOD.
- [SDR UPS01236825](https://openairdocs.org/sdr/UPS01236825.md): Control Cable · corroded · Sep 16, 2001 · N911UP · Boeing 72727C · Landing Gear Door Retract Section
  > INSPECTION TYPE:IN REF SEG CHECK NR 7 NWW DOOR ACTUATION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED & LUBRICATED AS REQUIRED PER MM 12-20-01.
- [SDR UPS01236824](https://openairdocs.org/sdr/UPS01236824.md): Control Cable · corroded · Sep 16, 2001 · N911UP · Boeing 72727C · Landing Gear Retraction/Extension System
  > REF SEG CHECK NR 7 NOSE GEAR MANUAL EXTENSION CABLES DRY WITH EVIDENCE OF SURFACE CORROSION. CLEANED AND LUBRICATED AS REQUIRED. OK FOR SERVICE PER MM 12-20-01.
- [SDR UPS01236683](https://openairdocs.org/sdr/UPS01236683.md): Hydraulic Line · leaking · Aug 23, 2001 · N907UP · Boeing 72727C · Hydraulic System, Auxiliary
  > INSPECTION TYPE:N/A SHORTLY AFTER TAKEOFF SYSTEM B ELECTRIC SYSTEM LOW PRESSURE LIGHT ILLUMINATED. SYSTEM B QTY INDICATED 0. EMERGENCY CHECKLISTS ACCOMPLISHED AND LANDING WAS UNEVENTFUL. FOUND OUTLET LINE OF NR 2 B PUMP LEAKING. PERFORMED AN INTERIM HOSE REPAI
- [SDR UPS01236690](https://openairdocs.org/sdr/UPS01236690.md): Stringer · cracked · Aug 16, 2001 · N908UP · Boeing 72727C · Wing Main, Frame Structure
  > INSPECTION TYPE:C SUSPECT CRACK IN CENTRE SECTION UPPER STRINGER S1 IN THE WING CENTRE TANK STRINGER REPAIRED IAW SRM 57-10-04 FIG 2
- [SDR UPS01236664](https://openairdocs.org/sdr/UPS01236664.md): Stringer · cracked · Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, S18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIR CARRIED IAW SRM PROCEDURES
- [SDR UPS01236658](https://openairdocs.org/sdr/UPS01236658.md): Stringer · cracked · Aug 15, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON INSPECTION OF FUSELAGE STRINGERS AT BS 400 WHERE ACCESSABLE, STRI NGER 18R AT BS 400 FOUND TO BE CRACKED. STRINGER REPAIRED IAW SRM.
- [SDR UPS01236689](https://openairdocs.org/sdr/UPS01236689.md): Stiffener · corroded · Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C WING CENTRE SECTION UPPER SKIN STIFFENER LWR CHORD IS CORRODED AT BS 870 RBL0. ***CPCP*** DAMAGED SECTION REMOVED AND NEW SECTION SPLICED IAW SRM
- [SDR UPS01236686](https://openairdocs.org/sdr/UPS01236686.md): Intercostal · cracked · Aug 13, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C SUSPECT CRACK AT R/H BS 1183 WL 230 OUTBD LWR CORNER OF INTERCOSTAL AT RBL 62.5 INTERCOSTAL REPLACED IAW DWG 65-16350
- [SDR UPS01236688](https://openairdocs.org/sdr/UPS01236688.md): Terminal · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Auxiliary Gear (Tail Skid)
  > INSPECTION TYPE:C L/H UPPER TENSION TIE CRACKED IN TAIL SKID BAY FABRICATED TERMINAL IAW DWG 65-85208, REMOVED / INSTALLED PER SRM
- [SDR UPS01236679](https://openairdocs.org/sdr/UPS01236679.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S6L AT BS 400 FOUND TO BE CRACKED. DAMAGED STRINGER REPAIRED IAW SRM 53-10-3
- [SDR UPS01236678](https://openairdocs.org/sdr/UPS01236678.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S3R FOUND CRACKED AT BS 400 REPAIRED PER SRM.
- [SDR UPS01236677](https://openairdocs.org/sdr/UPS01236677.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION S9R FOUND CRACKED AT BS 400 STRINGER REPAIRED IAW SRM.
- [SDR UPS01236676](https://openairdocs.org/sdr/UPS01236676.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSP FOR ACCESS S15R AT BS 400 FOUND TO BE CRACKED REPAIRED IAW SRM
- [SDR UPS01236675](https://openairdocs.org/sdr/UPS01236675.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S16R FOUND CRACKED AT BS 400 REPAIRED IAW SRM.
- [SDR UPS01236661](https://openairdocs.org/sdr/UPS01236661.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS S15L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
- [SDR UPS01236660](https://openairdocs.org/sdr/UPS01236660.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION FOR ACCESS, S16L FOUND CRACKED AT BS 400 REPAIRED IAW SRM
- [SDR UPS01236657](https://openairdocs.org/sdr/UPS01236657.md): Stringer · cracked · Aug 11, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C ON FURTHER INSPECTION STRINGER S6R FOUND CRACKED AT BS 400 REPAIRED PER SRM
- [SDR UPS01236687](https://openairdocs.org/sdr/UPS01236687.md): Strap · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON NDT INSP, CRACK INDICATION FOUND IN REINFORCING STRAP OF MID GALLEY DOOR CUTOUT FWD UPPER CORNER. REPAIR CARRIED OUT PER UPS EO B727-5330-2695 APPENDIX 8.2
- [SDR UPS01236685](https://openairdocs.org/sdr/UPS01236685.md): Intercostal · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Standard Practices/Structures
  > INSPECTION TYPE:C INTERCOSTAL CRACKED ABOVE DRAG BRACE FITTING SUPPORT INTERCOSTAL REPLACED IAW DRWG 65-18417
- [SDR UPS01236666](https://openairdocs.org/sdr/UPS01236666.md): Frame · cracked · Aug 10, 2001 · N908UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C CRACK BS 930 R/H FLANGE I/B LOWER CORNER RADIUS REPAIRED PER SRM ADDENDUM B727-5310-2611B
- [SDR UPS01236684](https://openairdocs.org/sdr/UPS01236684.md): Skin · corroded · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C AREA OF LIGHT SURFACE CORROSION ON SKIN AT BS660 S19R ***CPCP*** AREA REPAIRED IAW APPENDIX 8.3 OF EO B727-5330-0509
- [SDR UPS01236681](https://openairdocs.org/sdr/UPS01236681.md): Skin · cracked · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16R 15R REPAIRED IAW SRM
- [SDR UPS01236680](https://openairdocs.org/sdr/UPS01236680.md): Frame · corroded · Aug 9, 2001 · N908UP · Boeing 72727C · Aerodynamic Fairings
  > INSPECTION TYPE:C BODY FAIRING #3430 HAS CORRODED FRAME AT R/H GND FAN LOUVRE DOOR AFT CUTOUT. FRAME FABRICATED AND INSTALLED PER SRM
- [SDR UPS01236673](https://openairdocs.org/sdr/UPS01236673.md): Skin · cracked · Aug 9, 2001 · N908UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SKIN CRACKS BS 400 BETWEEN S16L AND 15L CRACKS REPAIRED IAW SRM
- [SDR UPS01236530](https://openairdocs.org/sdr/UPS01236530.md): Battery · discharged · Aug 3, 2001 · N914UP · Boeing 72727C · Emergency Lighting
  > INSPECTION TYPE:IN ILLEGIBLE EXIT LIGHT AT MAIN ENTRY DOOR INOP. REPLACED ILLEGIBLE EXIT LIGHT BATTERY AND OPS CHECK AS PER B727 M/M 33-50-00.
- [SDR UPS01236437](https://openairdocs.org/sdr/UPS01236437.md): Pressure Panel · cracked · Jul 31, 2001 · N909UP · Boeing 72727C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:C CRACK IN MLG WEB BS 938 O/B AFT CORNER ADJACENT TO STR 18A LWR FASTENER ROW IN RT MLG WW CRACK DRESSED OUT AND NDT CONFIRMED REMOVAL SRM51-10-1 WEB REPAIRED IAW SRM 51-20-02.
- [SDR UPS01236444](https://openairdocs.org/sdr/UPS01236444.md): Fitting · corroded · Jul 30, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:IN FRAME FOOT ANGLE AT FS 351 BETWEEN STRINGERS 24R AND 25R IS SEVERELY CORRODED. THIS IS UNDER FLOOR PANEL ON RT SIDE OF NLG WW ENCLOSURE ON THE INSIDE. R&R FRAME FOOT ASSY PER SRM 51-30-02.
- [SDR UPS01236434](https://openairdocs.org/sdr/UPS01236434.md): Angle · cracked · Jul 27, 2001 · N915UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A FRAME ANGLE CRACKED STA 351 JUST AFT OF O/B AFT CORNER OF ACCESS PANEL BEHIND NLG RT SIDE CUTOUT DAMAGED ANGLE PER SRM 51-10-01 PERFORMED HFEC INSPECTION OF CUTOUT AREA NO CRACKS NOTED REPAIRED PER B727 5330 15208.
- [SDR UPS01236476](https://openairdocs.org/sdr/UPS01236476.md): Fitting · cracked · Jul 22, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C TAIL SKID LT LWR TENSION TIE REAR TERMINAL FITTING CRACKED. LT LWR TENSION TIE AFT FITTING REMOVED AND NEW ONE INSTALLED IAW DRAWING 65-25992.
- [SDR UPS01236400](https://openairdocs.org/sdr/UPS01236400.md): Skin · corroded · Jul 20, 2001 · N915UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:N/A CORROSION AFT OF NLG WW, BELLY SKIN. REMOVED CORROSION AT BS 340 TO BS 360 BETWEEN STR 26 AND 27 RT PER SRM 51-10-01. INSTALLED LT AND RT INTERNAL DOUBLER SPLICES AND T ANGLES, INSTALLED NEW FUSELAGE SKIN IAW 727 SRM 51-30.
- [SDR UPS01236438](https://openairdocs.org/sdr/UPS01236438.md): Frame · damaged · Jul 20, 2001 · N909UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C FRAME DAMAGED AT BS 320 STR22R STR27R (HOLES DAMAGED) FRAME REPLACED IAW SRM 51-30-02 AND DRWG 65-18420
- [SDR UPS01236439](https://openairdocs.org/sdr/UPS01236439.md): Bracket · cracked · Jul 18, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C CRACK ON EDGE OF FLOOR PANEL SUPPORT BRACKET AT STA 755 LBL 50. NEW BRACKET FITTED IAW SRM 51-30-02.
- [SDR UPS01236440](https://openairdocs.org/sdr/UPS01236440.md): Skin · corroded · Jul 17, 2001 · N909UP · Boeing 72727C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CORROSION ON LAP S24R BS 295 CPCP NEAR REPAIR REQUIRED SKIN REPLACEMENT WHICH ENCOMPASSED THIS DAMAGE, SKIN REPLACED.
- [SDR UPS01236436](https://openairdocs.org/sdr/UPS01236436.md): Fitting · cracked · Jul 17, 2001 · N909UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C SUSPECT CRACK AT TAIL SKID COMPT, RT UPPER TENSION TIE END FITTING CRACK CONFIRMED BY NDT, FITTING REPLACED IAW DRAWING.
- [SDR UPS01236460](https://openairdocs.org/sdr/UPS01236460.md): Hinge · cracked · Jul 16, 2001 · N909UP · Boeing 72727C · Cargo/Baggage Doors
  > INSPECTION TYPE:C MAIN CARGO DOOR FWD AND AFT HINGES CRACKED. ON INVESTIGATION HINGES FOUND CORRODED BEYOND LIMITS, HINGES REPLACED IAW OHM 20-50-01
- [SDR UPS01236413](https://openairdocs.org/sdr/UPS01236413.md): Floor Support · corroded · Jul 11, 2001 · N914UP · Boeing 72727C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:N/A LAV FLOOR SUPPORT CORRODED RBL 40 BS290 TP BS 312 REMOVED CORROSION AT LAV FLOOR SUPPORT RBL 40 BS290 TO BS 312 MATERI AL LOSS.050 FOUND OUT OF LIMITS AS PER B727 SRM 51-30-02 REPLACED F LOOR MATERIAL USE 60-8265 T ANGLE 8" TREAT AND P
- [SDR UPS01236411](https://openairdocs.org/sdr/UPS01236411.md): Beam · cracked · Jul 10, 2001 · N914UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:N/A AFT PRESSURE BULKHEAD VERTICAL BEAM LBL 17.8 WL 264.5 SHOW CRACK RUNNING FROM STOP DOOR CUT OUT TO O/B CHORD. CUT OUT DAMAGED SECTION OF VERTICAL BEAM AT W/L 249 IAW UPS EO B727-53 10-11743 APPENDIX E INSTALLED NEW SECTION AND REMOVED PARTS
- [SDR UPS01236414](https://openairdocs.org/sdr/UPS01236414.md): Pressure Panel · cracked · Jul 9, 2001 · N914UP · Boeing 72727C · Fuselage Main, Bulkhead
  > INSPECTION TYPE:N/A NLG WW LT SIDE WALL CRACK INDICATION BETWEEN FASTENERS BS 235 AND LOWER OF FWD ACCESS. REMOVE ACCESS NR 3122 FOR ACCESS REPAIR AS PER B727SRM 51-30-02 CUT OUT DAMAGED AREA AS PER B727 SRM 51-30-02, SIZE OF CUT 2X1 INCH ACCOMPLISHED NDT ON C
- [SDR UPS01236392](https://openairdocs.org/sdr/UPS01236392.md): Stringer · cracked · Jul 9, 2001 · N910UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED. REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3
- [SDR UPS01236314](https://openairdocs.org/sdr/UPS01236314.md): Stringer · cracked · Jul 9, 2001 · N909UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C END OF STRINGER 15 @ BS 676 LH IS CRACKED REPAIR CARRIED OUT IAW 51-30-2 & 53-10-3
- [SDR UPS01236412](https://openairdocs.org/sdr/UPS01236412.md): Frame · cracked · Jul 6, 2001 · N914UP · Boeing 72727C · Fuselage Main, Structure
  > INSPECTION TYPE:C LH WHEEL WELL TOP OB EXPOSED PORTION OF BS 930 FRAME IS CRACKED IB S IDE TOP INSTALL REPAIR AS PER REPAIR ORDER AVHM 233RO-1. ENGINEERING FILE NO 727-53-20023. MAT USED 310 1/2 HD.080 BOTTOM DOUBLER 15X8" TOP DOU BLER 6X6", TOP STRAP 20

Next page: https://openairdocs.org/model/boeing-727-27c/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 = '72727C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-27c/reports

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