Boeing 727-185C

Service difficulty reports · 425

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "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"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS07250488Slide · out of positionINSPECTION 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.Aug 17, 2007 · N940UP · Boeing 727185C · Escape SlideSDR UPS07250476Slide · out of positionINSPECTION 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.Aug 17, 2007 · N940UP · Boeing 727185C · Escape SlideSDR UPS07248848Battery · inoperativeCONTROL 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.Jan 10, 2007 · N940UP · Boeing 727185C · Emergency LightingSDR UPS06247337Receptacle · dirtyUPON 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 GEAR WAS RETRACTED AND THE 3 RED GEAR WARNING.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 MODJul 16, 2006 · N940UP · Boeing 727185C · Landing Gear Position and WarningSDR UPS06247313Extinguisher · unserviceableMAIN PORTABLE FIRE EXTINGUISHER NEEDLE IS OUT OF GRN BAND. REMOVED AND REPLACED PORTABLE FIRE EXTINGUISHER BY LAV DOOR. OK FOR SERVICE.Jul 12, 2006 · N954UP · Boeing 727185C · Fire Bottle, PortableSDR UPS06247282Seat Track · corrodedDURING 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 AJun 20, 2006 · N940UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06247273Rib · crackedNR 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 IJun 18, 2006 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS06247210Rib · crackedINSPECTION 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 SRJun 18, 2006 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS06247207Rib · crackedINSPECTION 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 DRILLJun 18, 2006 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS06247277Bracket · crackedRIGHT 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.Jun 17, 2006 · N940UP · Boeing 727185C · SpoilersSDR UPS06247283Skin · corrodedINSPECTION 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 Jun 16, 2006 · N940UP · Boeing 727185C · Wing, Plate/SkinSDR UPS06247285Intercostal · crackedINSPECTION 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 57-5Jun 15, 2006 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS06247278Intercostal · crackedNR 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. FJun 15, 2006 · N940UP · Boeing 727185C · Leading Edge DevicesSDR UPS06247275Flange · crackedFOUND EVIDENCE OF CRACK ON LEFT BS 940 LOWER FWD FLANGE. FLANGE REPAIRED IAW AAAE EO 2006-037-007.Jun 13, 2006 · N940UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS06247276Bearing · failedNOSE 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.Jun 6, 2006 · N940UP · Boeing 727185C · Landing Gear Retraction/Extension SystemSDR UPS06247006Slide · deployedINSPECTION 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.May 31, 2006 · N940UP · Boeing 727185C · Escape SlideSDR UPS06246828Rod · brokenF/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.May 9, 2006 · N940UP · Boeing 727185C · Flight Compartment WindowsSDR UPS06246858Stringer · corrodedFOUND 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 SMay 6, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS06246868Intercostal · crackedINSPECTION 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 May 5, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS06246867Skin · crackedINSPECTION 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 SRMay 5, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS06246797Intercostal · crackedFOUND 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.May 2, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS06246795Seat Track · crackedFOUND 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.May 2, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06246878Door Frame · crackedINSPECTION 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 REApr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS06246796Stringer · corrodedFOUND 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.Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS06246794Seat Track · corrodedFOUND 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.Apr 28, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06246838Skin · corrodedINSPECTION 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.Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS06246837Skin · corrodedINSPECTION 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.Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS06246836Skin · corrodedINSPECTION 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.Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/SkinSDR UPS06246829Stringer · corrodedDURING 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.Apr 25, 2006 · N954UP · Boeing 727185C · Fuselage Main, Longeron/StringerSDR UPS06246883Rib · crackedINSPECTION 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. Apr 24, 2006 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS06246880Floor Panel · corrodedINSPECTION 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.Apr 24, 2006 · N954UP · Boeing 727185C · Fuselage Floor PanelSDR UPS06246879Rib · crackedINSPECTION 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 REPAIRApr 24, 2006 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS06246874Angle · crackedINSPECTION 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 DOApr 24, 2006 · N954UP · Boeing 727185C · Leading Edge DevicesSDR UPS06246889Structure · corrodedINSPECTION 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 Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS06246885Support Beam · corrodedINSPECTION 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.Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach FittingsSDR UPS06246884Support Beam · corrodedINSPECTION 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.Apr 20, 2006 · N954UP · Boeing 727185C · Wing, Landing Gear Attach FittingsSDR UPS06246882Carriage · corrodedINSPECTION TYPE:C T/E FLAP CARRIAGE NR 4 PITTING CORROSION IN BORE OF SPINDLE CARRIAGE ASSY REPLACED IAW OHM 27-58-02.Apr 20, 2006 · N954UP · Boeing 727185C · Trailing Edge FlapsSDR UPS06246881Floor Panel · corrodedINSPECTION 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.Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage Floor PanelSDR UPS06246839Seat Track · corrodedINSPECTION 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.Apr 20, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06246871Pressure Panel · crackedINSPECTION 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 Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS06246851Pin · corrodedINSPECTION TYPE:C BS 740 LT BOTTLE PIN FOUND CORRODED. REPLACED BS 740 LT SIDE IN CONJUNCTION WITH MM 57-41-01.Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, StructureSDR UPS06246835Seat Track · crackedINSPECTION 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.Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06246834Seat Track · corrodedINSPECTION 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.Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage, Seat/Cargo Attach FittingsSDR UPS06246831Pressure Panel · crackedINSPECTION 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-Apr 19, 2006 · N954UP · Boeing 727185C · Fuselage Main, BulkheadSDR UPS06246830Door · corrodedINSPECTION 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.Apr 19, 2006 · N954UP · Boeing 727185C · Emergency ExitsSDR UPS06246887Support · crackedINSPECTION 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-Apr 18, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS06246888Plate · corrodedINSPECTION 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.Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Miscellaneous StructureSDR UPS06246833Floorbeam · corrodedINSPECTION 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.Apr 15, 2006 · N954UP · Boeing 727185C · Fuselage Main, Floor BeamSDR UPS06246877Fitting · crackedINSPECTION 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 FASTENERApr 14, 2006 · N954UP · Boeing 727185C · Fuselage Main, Attach FittingsSDR UPS06246832Skin · crackedINSPECTION 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 FASTEApr 13, 2006 · N954UP · Boeing 727185C · Fuselage Main, Plate/Skin
Back to Boeing 727-185C