# Service difficulty reports: Boeing 727-185C A list on [Boeing 727-185C](https://openairdocs.org/model/boeing-727-185c.md). Newest first. General aviation reporting is voluntary. Page 1 of 9 · 425 reports - [SDR UPS07250488](https://openairdocs.org/sdr/UPS07250488.md): Slide · out of position · Aug 17, 2007 · N940UP · Boeing 727185C · Escape Slide > INSPECTION TYPE:N/A CREW ENTRY ESCAPE SLIDE FELL OUT OF CASE. REPLACED ESCAPE SLIDE AS NEEDED, OKAY FOR SERVICE. REF M/M 25-60-14- 2. - [SDR UPS07250476](https://openairdocs.org/sdr/UPS07250476.md): Slide · out of position · Aug 17, 2007 · N940UP · Boeing 727185C · Escape Slide > INSPECTION TYPE:N/A CREW ENTRY ESCAPE SLIDE FELL OUT OF CASE. REPLACED ESCAPE SLIDE AS NEEDED. OKAY FOR SERVICE REF MM 25-60-14-2. - [SDR UPS07248848](https://openairdocs.org/sdr/UPS07248848.md): Battery · inoperative · Jan 10, 2007 · N940UP · Boeing 727185C · Emergency Lighting > CONTROL CABIN EMERGENCY LIGHTS FOUND TO BE INOP. REPLACED EMERGENCY LIGHT BATTERY IAW MM 33-50-01-2 AND 33-50-01-5. OPS CHECKED NORMAL. - [SDR UPS06247337](https://openairdocs.org/sdr/UPS06247337.md): Receptacle · dirty · Jul 16, 2006 · N940UP · Boeing 727185C · Landing Gear Position and Warning > UPON GEAR RETRACTION 3 RED GEAR WARNING LIGHTS ILLUMINATED. GEAR DOORS OPERATED NORMAL. GEAR WAS EXTENDED. THREE GREEN GEAR LIGHTS ILLUMINATED AND THE NOSE GEAR RED LIGHT REMAINED ON. GEAR WAS RETRACTED AND THE 3 RED GEAR WARNING. REMOVED LANDING GEAR MOD - [SDR UPS06247313](https://openairdocs.org/sdr/UPS06247313.md): Extinguisher · unserviceable · Jul 12, 2006 · N954UP · Boeing 727185C · Fire Bottle, Portable > MAIN PORTABLE FIRE EXTINGUISHER NEEDLE IS OUT OF GRN BAND. REMOVED AND REPLACED PORTABLE FIRE EXTINGUISHER BY LAV DOOR. OK FOR SERVICE. - [SDR UPS06247282](https://openairdocs.org/sdr/UPS06247282.md): Seat Track · corroded · Jun 20, 2006 · N940UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > DURING REMOVAL OF FLOORBOARDS TO FACILITATE REPLACEMENT OF SEAT TRACK SECTION CORROSION FOUND ON FLOORBEAM UPPER CHORD AT BS 560 BETWEEN LBL 10 - LBL 50. CORROSION REMOVED IAW SRM 51-10-01. FOUND OUTSIDE LIMITS IAW SRM 51-10-1. HFEC CARRIED OUT ON BLENDED A - [SDR UPS06247273](https://openairdocs.org/sdr/UPS06247273.md): Rib · cracked · Jun 18, 2006 · N940UP · Boeing 727185C · Leading Edge Devices > NR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-01. HFEC CARRIED OUT AROUND CUTOUT IAW B7 27-NDTM 51-00-00 PT 6 FIG 4, NDF. REPAIR DOUBLER FORMED IAW SRM 57-50-3. NR 6 SLAT SUPPORT RIB CAD PLATING CARRIED OUT I - [SDR UPS06247210](https://openairdocs.org/sdr/UPS06247210.md): Rib · cracked · Jun 18, 2006 · N940UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED, ABOUT 9 INCHES FROM THE SLAT O/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. REPAIR DOUBLER FORMED IAW SRM 57-50-3. DRILLED AND SHAPED DOUBLER IAW SR - [SDR UPS06247207](https://openairdocs.org/sdr/UPS06247207.md): Rib · cracked · Jun 18, 2006 · N940UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C NR 6 SLAT SUPPORT RIB CRACKED ABOUT 9 INCHES FROM SLAT I/B END. REMOVED DAMAGE IAW SRM 51-10-1. HFEC CARRIED OUT AROUND CUTOUT IAW B72 7NDTM 51-00-00 PT 6 FIG 4. SUPPORT RIB REPAIR DOUBLER FORMED IAW SRM 57--50-3. DOUBLER SHAPED AND DRILL - [SDR UPS06247277](https://openairdocs.org/sdr/UPS06247277.md): Bracket · cracked · Jun 17, 2006 · N940UP · Boeing 727185C · Spoilers > RIGHT WING T/E CAVITY NR 11 SPOILER I/B HINGE BRACKET ASSY, SUSPECT CRACK ON O/B BRACKET AT UPPER AFT CORNER. HFEC CARRIED OUT IAW B727-NDTM 51-00-00 PT6 FIG 4 CRACK CONFIRMED. REMOVED O/B HINGE BRACKET IAW SRM 51-30-02. FABRICATED BRACKET IAW SRM 51-20-01. - [SDR UPS06247283](https://openairdocs.org/sdr/UPS06247283.md): Skin · corroded · Jun 16, 2006 · N940UP · Boeing 727185C · Wing, Plate/Skin > INSPECTION TYPE:C CORROSION ON RT WING TIP UPPER SURFACE AT O/B TRAILING EDGE STATIC DISCHARGER. STATIC DISCHARGER REMOVED IAW SRM 51-30-02. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND OUT OF LIMITS. HFEC CARRIED OUT ON BLENDED AREA IAW B727-NDTM 51-00-00 - [SDR UPS06247285](https://openairdocs.org/sdr/UPS06247285.md): Intercostal · cracked · Jun 15, 2006 · N940UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C NR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT, CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUTOUT IAW SRM 57-50-03. O/B SLAT TRACK DISPLACED AT FWD ATTACHMENT AREA IAW OHM 57-51-51. REPAIR DOUBLER FABRICATED IAW SRM 57-5 - [SDR UPS06247278](https://openairdocs.org/sdr/UPS06247278.md): Intercostal · cracked · Jun 15, 2006 · N940UP · Boeing 727185C · Leading Edge Devices > NR 3 SLAT AT O/B TRACK ATTACHMENT TO SLAT CRACK ON INTERCOSTAL. FASTENERS REMOVED IAW SRM 51-30-02 AND CRACK CUT OUT IAW SRM 57-50-03. REPAIR DOUBLER FABRICATED IAW SRM 57-50-03. CAD PLATING CARRIED IAW SO PM 20-42-10. REPAIR INSTALLED IAW SRM 57-50-03. F - [SDR UPS06247275](https://openairdocs.org/sdr/UPS06247275.md): Flange · cracked · Jun 13, 2006 · N940UP · Boeing 727185C · Fuselage Main, Attach Fittings > FOUND EVIDENCE OF CRACK ON LEFT BS 940 LOWER FWD FLANGE. FLANGE REPAIRED IAW AAAE EO 2006-037-007. - [SDR UPS06247276](https://openairdocs.org/sdr/UPS06247276.md): Bearing · failed · Jun 6, 2006 · N940UP · Boeing 727185C · Landing Gear Retraction/Extension System > NOSE WHEEL WILL NOT MANUALLY EXTEND. BEARINGS REPLACED IN CABLE DRUM IAW SOPM 20-50-03. DRUM REPLACED IAW MM 32-34-11. MANUAL EXTENSION SYSTEM ADJUSTED IAW MM 32-34-00. SYSTEM TESTED IAW AMM 32-34-00 AND RETURNED TO SERVICE. - [SDR UPS06247006](https://openairdocs.org/sdr/UPS06247006.md): Slide · deployed · May 31, 2006 · N940UP · Boeing 727185C · Escape Slide > INSPECTION TYPE:N/A UPON ARRIVAL TO AIRCRAFT PARKED ON RAMP, FOUND L1 DOOR OPEN AND FOUND ESCAPE SLIDE ON RAMP. REMOVED AND REPLACED SLIDE AND COMPARTMENT WITH SERVICEABLE UNITS IAW MM 25-60-14. - [SDR UPS06246828](https://openairdocs.org/sdr/UPS06246828.md): Rod · broken · May 9, 2006 · N940UP · Boeing 727185C · Flight Compartment Windows > F/O SLIDING WINDOW (NR 2) LOCK RELEASE IS BROKEN. REPLACED OPEN WINDOW, RELEASE/LOCK ROD W/REF M/M 56-12-11-4 O/C GOOD W/REF MM 56-12-11-5. - [SDR UPS06246858](https://openairdocs.org/sdr/UPS06246858.md): Stringer · corroded · May 6, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer > FOUND STRINGER AT FRAME 540 RBL22 HAS CORROSION, PLS. REMOVE CORROSION AND CHECK WITHIN LIMITS. DAMAGED PART OF STR FOUND TO BE OUTSIDE LIMITS IAW SRM 53-10-1. DAMAGED STR REMOVED IAW SRM 51-40-4. NEW SPLICES FABRICATED IAW SRM 51-4 0-4. REPROTECTED NEW S - [SDR UPS06246868](https://openairdocs.org/sdr/UPS06246868.md): Intercostal · cracked · May 5, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure > INSPECTION TYPE:C&SI ON REMOVAL OF FRAME AT BS 540 INTERCOSTAL AT BS 520-540 IS CRACKED PLS. REPAIR/REPLACE AS REQUIRED. REMOVED CRACKED INTERCOSTAL AT BS 520-540 IAW SRM 51-30-2. FABRICATED INTERCOSTAL IAW SRM 51-20-1 FIG 7. INSTALLED INTERCOSTAL IAW SRM - [SDR UPS06246867](https://openairdocs.org/sdr/UPS06246867.md): Skin · cracked · May 5, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin > INSPECTION TYPE:C&SI ON REMOVAL OF FRAME AT BS 540 WEB SKIN AT 500-540 S18R HAS EVIDENCE OF MECHANICAL DAMAGE AND CRACKS. NEW WEB SKIN FABRICATED IAW SRM 51-20-01. NEW SKIN DRILLED OFF EXISTING HOLES IAW SRM 51-30-02 ALSO NUT PLATES INSTALLED AS REQ'D IAW SR - [SDR UPS06246797](https://openairdocs.org/sdr/UPS06246797.md): Intercostal · cracked · May 2, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure > FOUND INTERCOSTAL CRACKED AT BS 272 RHS BELOW STR 23R. INTERCOSTAL REMOVED IAW SRM 51-30-02. FABRICATED INTERCOSTAL IAW SRM 51-20-01. INSTALLED INTERCOSTAL IAW SRM 51-30-02. - [SDR UPS06246795](https://openairdocs.org/sdr/UPS06246795.md): Seat Track · cracked · May 2, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > FOUND CABIN UPPER FLANGE AFT END CRACKED AT BS 850 LBL51 HAS SURFACE CORROSION SEAT TRACK REMOVED IAW SRM 51-30-02. NEW SEAT TRACK FABRICATED IAW SRM 53-10-02. INSTALLED NEW SEAT TRACK IAW SRM 51-30-02. - [SDR UPS06246878](https://openairdocs.org/sdr/UPS06246878.md): Door Frame · cracked · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, Structure > INSPECTION TYPE:C NDT CONFIRMED TWO CRACKS ON THE FWD FRAME OF THE FWD CARGO DOOR CUTOUT. REMOVED EXISTING REPAIR AND DOOR STOP IAW SRM 51-30-02. ANGLES BETWEEN STR 19R AND STR 24R REMOVED IAW SRM 51-30-02. FRAME WEB SKIN REMOVED IAW SRM 51-30-02. FRAME RE - [SDR UPS06246796](https://openairdocs.org/sdr/UPS06246796.md): Stringer · corroded · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer > FOUND CORROSION ON STR 22R AT BS 460. CORROSION FOUND OUT OF LIMITS IAW SRM 51-10-01. REMOVED CORRODED STRINGER IAW SRM 53-10-3 REPAIRED STRINGER IAW SRM 53-10-03. - [SDR UPS06246794](https://openairdocs.org/sdr/UPS06246794.md): Seat Track · corroded · Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > FOUND CABIN SEAT TRACK I/B FLANGE CORRODED BETWEEN BS 760- BS 779 LBL 75 CORROSION FOUND TO BE OUT OF LIMITS IAW SRM 53-10-02. NEW SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-10-02 AND SRM 51-30-02. - [SDR UPS06246838](https://openairdocs.org/sdr/UPS06246838.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin > INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BS 800 TO 840 STR 10 LT. CORROSION REMOVED AS REQUIRED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01. - [SDR UPS06246837](https://openairdocs.org/sdr/UPS06246837.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin > INSPECTION TYPE:C AREA OF LITE SURFACE CORROSION ON SKIN BELOW STR 10L BS 465. CORROSION REMOVED IAW SRM 51-10-06. FOUND WITHIN LIMITS IAW SRM 53-30-01. - [SDR UPS06246836](https://openairdocs.org/sdr/UPS06246836.md): Skin · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin > INSPECTION TYPE:C AREAS OF CORROSION ON SKIN BS 640-700 AT VARIOUS LOCATIONS. AREAS OF CORROSION CLEANED UP AND FOUND WITHIN LIMITS IAW SRM 53-30-01 AND SRM 51-10-02. - [SDR UPS06246829](https://openairdocs.org/sdr/UPS06246829.md): Stringer · corroded · Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/Stringer > DURING C-CHECK, AREA OF CORROSION ON SKIN BS 358 BELOW STR 10 LT. CORRROSION REMOVED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01 AREA REPROTECTED IAW SRM 51-10-02. - [SDR UPS06246883](https://openairdocs.org/sdr/UPS06246883.md): Rib · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C LT 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END, NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACK FOUND ON BOTH ENDS OF NUT PLATE AND RIB END CRACKED. REPAIR DOUBLER FABRICATED IAW SRM 51-40-3. NUT PLATE RIVETED IAW SRM 51-40-02. - [SDR UPS06246880](https://openairdocs.org/sdr/UPS06246880.md): Floor Panel · corroded · Apr 24, 2006 · N954UP · Boeing 727185C · Fuselage Floor Panel > INSPECTION TYPE:C SECTION OF COCKPIT FLOOR BEHIND CAPTAIN SEAT IS CORRODED AT SCREW HOLES. CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 51-10-06. FLOOR PANEL FABRICATED IAW BOEING DRWG 65-17593. - [SDR UPS06246879](https://openairdocs.org/sdr/UPS06246879.md): Rib · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C LT NR 2 SLAT SUPPORT RIB CRACKED 2ND FROM LEADING EDGE O/B END NUT PLATE DE-RIVETED IAW SRM 51-30-02. CRACKS FOUND ON NUT PLATE, END BROKEN ON RIB. FABRICATED REPAIR DOUBLER IAW SRM 51-40-03. NUT PLATE RIVETED PER SRM 51-30-02. RIB REPAIR - [SDR UPS06246874](https://openairdocs.org/sdr/UPS06246874.md): Angle · cracked · Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge Devices > INSPECTION TYPE:C LEFT NR 4, 2 RIBS CRACKED I/B AND O/B OF SLAT ACTUATOR FWD ATTACH POINT. DISCONNECTED ACTUATOR ROD END IAW MM 27-81-32 AND FOUND RIB ANGLES BROKEN. REMOVED FASTENERS IAW SRM 51-30-02. FABRICATED REPAIR DOUBLERS IAW SRM 51-40-03. REPAIR DO - [SDR UPS06246889](https://openairdocs.org/sdr/UPS06246889.md): Structure · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure > INSPECTION TYPE:C AS PER TC C53-111-01-1B TENSION BOLTS FOUND CORRODED. ALL CORRODED IAW MM 20-80-01. BOLTS TORQUED IAW MM 53-11-01. CORROSION REMOVED OUT OF HOLES IAW SRM 51-10-01, AND AREA REPROTECTED IAW SRM 51-10-02. BOLT HOLES INSPECTED AFTER SURFACE - [SDR UPS06246885](https://openairdocs.org/sdr/UPS06246885.md): Support Beam · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach Fittings > INSPECTION TYPE:C RT MLG SUPPORT BEAM, PITTING IN BORE OF HOLE. CORROSION REMOVED IAW SRM 51-10-01. HFEC CARRIED OUT IAW B727-NDTM-51-00-00, NO CORROSION FOUND. REF AAAE EO 2006-024-005 FOR REPAIR OF HOLE. - [SDR UPS06246884](https://openairdocs.org/sdr/UPS06246884.md): Support Beam · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach Fittings > INSPECTION TYPE:C LT MLG SUPPORT BEAM PITTING CORROSION IN BORE OF HOLE. CORROSION REMOVED IAW SRM 51-40-01. HFEC CARRIED OUT IAW B727-NDTM 51-00-00, NO CORROSION FOUND. REF AAAE EO 2006-024-005 FOR REPAIR OF HOLE. - [SDR UPS06246882](https://openairdocs.org/sdr/UPS06246882.md): Carriage · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Trailing Edge Flaps > INSPECTION TYPE:C T/E FLAP CARRIAGE NR 4 PITTING CORROSION IN BORE OF SPINDLE CARRIAGE ASSY REPLACED IAW OHM 27-58-02. - [SDR UPS06246881](https://openairdocs.org/sdr/UPS06246881.md): Floor Panel · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Floor Panel > INSPECTION TYPE:C SLIGHT SURFACE CORROSION ON FLOOR WEB BS 560 LBL 45.5. CORROSION ON FLOOR PANEL WEB BS 560 LBL 45.5 OUT OF LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-02. - [SDR UPS06246839](https://openairdocs.org/sdr/UPS06246839.md): Seat Track · corroded · Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:C LITE SPOTS OF SURFACE CORROSION BS 380 ON SEAT TRACK FLANGE LBL 45.5. CORROSION REMOVED IAW SRM 51-10-06 AND FOUND WITHIN LIMITS IAW SRM 53-30-01. - [SDR UPS06246871](https://openairdocs.org/sdr/UPS06246871.md): Pressure Panel · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Bulkhead > INSPECTION TYPE:C CRACK ON RT NWW BS 268 AT LOWER EDGE OF AFT PRESSURE PANEL CUTOUT. HFEC INSPECTION CARRIED OUT ON ABOVE AREA IAW B727-NDTM 51-00-00 FIG 6. CRACK CONFIRMED. REMOVED INTERCOSTAL AND WEB IAW SRM 51-30-02. FABRICATED NEW WEB AND DOUBLERS IAW - [SDR UPS06246851](https://openairdocs.org/sdr/UPS06246851.md): Pin · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Structure > INSPECTION TYPE:C BS 740 LT BOTTLE PIN FOUND CORRODED. REPLACED BS 740 LT SIDE IN CONJUNCTION WITH MM 57-41-01. - [SDR UPS06246835](https://openairdocs.org/sdr/UPS06246835.md): Seat Track · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:C SEAT TRACK UPPER FLANGE AFT END CRACKED AT BS 850 LBL 51. SEAT TRACK REMOVED IAW SRM 51-30-02. SEAT TRACK FABRICATED IAW SRM 53-10-02. INSTALLED SEAT TRACK AND REPROTECTED IAW SRM 51-30-02 AND MM 51-20-91. - [SDR UPS06246834](https://openairdocs.org/sdr/UPS06246834.md): Seat Track · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach Fittings > INSPECTION TYPE:C CABIN SEAT TRACK I/B FLANGE CORRODED BETWEEN BS 760 AND 779 LBL 20. CORROSION FOUND OUT OF LIMITS IAW SRM 53-10-01. SEAT TRACK FABRICATED AND INSTALLED IAW SRM 53-10-02 AND SRM 51-30-02. REPROTECTED IAW MM 51-20-91. - [SDR UPS06246831](https://openairdocs.org/sdr/UPS06246831.md): Pressure Panel · cracked · Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, Bulkhead > INSPECTION TYPE:C SUSPECT CRACK ON NWW PRESSURE WEB RT AT BS 330. HFEC CARRIED OUT IAW B727 NDTM 51-00-00 FIG 4 AND CRACK CONFIRMED. DAMAGE REMOVED IAW SRM 51-10-01. REPAIR PARTS FABRICATED IAW SRM 51-40-02. HFEC CARRIED OUT AROUND CUTOUT IAW B727-NDTM 51- - [SDR UPS06246830](https://openairdocs.org/sdr/UPS06246830.md): Door · corroded · Apr 19, 2006 · N954UP · Boeing 727185C · Emergency Exits > INSPECTION TYPE:C LT AFT ESCAPE HATCH HAS LIGHT SURFACE CORROSION ON LOWER EDGE. HATCH CORROSION REMOVED AND FOUND OUT OF LIMITS IAW SRM 52-00-02. HATCH REPLACED IAW MM 52-21-00. - [SDR UPS06246887](https://openairdocs.org/sdr/UPS06246887.md): Support · cracked · Apr 18, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure > INSPECTION TYPE:C CRACKS ON SUPPORT STRUCTURE FOR SYSTEM -B- HYDRAULIC PUMP AT LOWER RADIUS FWD AND AFT CORNERS. HFEC CARRIED OUT ON PREVIOUS LT STOP DRILLED HOLES IAW B727 NDTM 51-00- 00, CRACK CONFIRMED ENDS MARKED. SUPPORT STRUCTURE REMOVED IAW SRM 51-30- - [SDR UPS06246888](https://openairdocs.org/sdr/UPS06246888.md): Plate · corroded · Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous Structure > INSPECTION TYPE:C CORROSION ON TOP PLATE RIVETED TO FLOOR STRUCTURE AT BS 850 LBL 55. CORROSION FOUND OUTSIDE LIMITS IAW SRM 51-10-06. REPAIR CARRIED OUT IAW SRM 51-40-03. - [SDR UPS06246833](https://openairdocs.org/sdr/UPS06246833.md): Floorbeam · corroded · Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Main, Floor Beam > INSPECTION TYPE:C CORROSION AROUND ANCHOR NUT ON FLOORBEAM AFT CARGO STA 1148. CORROSION FOUND OUT OF LIMITS AT ABOVE AREA IAW SRM 51-10-01. CUTOUT MADE IAW SRM 53-10-08. HFEC CARRIED OUT IAW B727-NDTM PT6 51-00-00 FIG 4. REPAIR COMPLETED IAW SRM 53-10-08. - [SDR UPS06246877](https://openairdocs.org/sdr/UPS06246877.md): Fitting · cracked · Apr 14, 2006 · N954UP · Boeing 727185C · Fuselage Main, Attach Fittings > INSPECTION TYPE:C NEW CRACKS FOUND ON BS 740 LT FITTING BETWEEN STR 22L AND 23L. STRINGER STRIPS REMOVED IAW SRM 51-30-03. FASTENERS INSTALLED ON FITTING FROM UPPER SPLICE TO STR 17 IAW DRWG 65C13724. SKIN TRIMMED IAW AAA E EO 2006-024-004. REPAIR FASTENER - [SDR UPS06246832](https://openairdocs.org/sdr/UPS06246832.md): Skin · cracked · Apr 13, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin > INSPECTION TYPE:C SUSPECT SKIN CRACK AT UPPER VHF ANTENNA CUT OUT AFT EDGE. HFEC INSPECTION CARRIED OUT ON THE ABOVE AREA IAW B727-NDTM PT 6 51-1 00-00 FIG 4. REMOVED ANTENNA IAW SRM 51-30-02. CUTOUT CARRIED OUT IAW EQR 2006024-6. HFEC CARRIED OUT ON FASTE Next page: https://openairdocs.org/model/boeing-727-185c/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 = '727185C' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/model/boeing-727-185c/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.