Boeing 727-62C

Service difficulty reports · 136

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 = '72762C'
  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 UPS02239933Battery Pack · dischargedINSPECTION TYPE:IN BOTH EMERGENCY EXITS WILL NOT ARM. R&R BOTH BATTERY PACKS & INSTALLED NEW BATTERIES OPS CHECK GOOD.Nov 25, 2002 · N913UP · Boeing 72762C · Emergency LightingSDR UPS02239250Pressure Panel · crackedINSPECTION TYPE:SEG4 RIGHT WHEEL WELL FWD BULKHEAD, JUST BELOW APU LOAD CONTROL VLV, HAS A 3.5 INCH CRACK TO 4 INCH CRACK CRACKED THROUGH. STOP DRILLED CRACK AS PER B72 7 SRM 51-10-01, ACCOMPLISHED HFEC 51-000-00 FIG 4 NDT INSP CRACK CONTAINMENT CONFIRMED. ISep 2, 2002 · N913UP · Boeing 72762C · Fuselage Main, BulkheadSDR UPS02237405Battery · dischargedINSPECTION TYPE:PFLT ON PREDEPARTURE CHECK, EMERGENCY EXIT LIGHT AT COCKPIT DOOR INOP. INSTALLED NEW BATTERIES AT COCKPIT DOOR EMERGENCY EXIT LIGHT ASSY, OPS CHECK NORMAL AS PER MM 33-50-1010.Jan 2, 2002 · N912UP · Boeing 72762C · Emergency LightingSDR UPS01237341Slide · unsecureINSPECTION TYPE:N/A ESCAPE SLIDE CAME OFF WHEN CREW CLOSED DOOR. SLIDE RE-INSTALLED NOTE: SLIDE DID NOT DEPLOY.Nov 27, 2001 · N912UP · Boeing 72762C · Escape SlideSDR UPS01237191Slide · unsecureINSPECTION TYPE:IN DOOR PARTIALLY OPENED FROM EXTERIOR WITH SLIDE ARMED SLIDE FELL FROM DOOR BUT DID NOT DEPLOY. RESECURED SLIDE ASSY.Oct 26, 2001 · N912UP · Boeing 72762C · Escape SlideSDR UPS01237071Access Panel · delaminatedINSPECTION TYPE:C NR 1 PYLON PANEL LOWER SURFACE ACCESS PANEL 5408 HAS DELAMINATION ON UPPER SURFACE. REPAIRED IAW SRM 51-40-20.Oct 17, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/SkinSDR UPS01237058Panel · crackedINSPECTION TYPE:C RH WING, WHILE BLENDING PAINT FROM A DENT ON PANEL 65-21655-470 IT W AS NOTED THAT THE UPPER SKIN WAS CRACKED REPAIRED IAW SRM 51-40-20Oct 5, 2001 · N913UP · Boeing 72762C · Trailing Edge Flap Control SystemSDR UPS01237051Beam · crackedINSPECTION TYPE:C SUSPECT CRACK IN NLG DRAGBRACE ATTACH FITTING SUPPORT BEAM IN RT AFT CORNER. REPLACEMENT OF NLG DRAGBRACE SUPPORT BEAM CARRIED OUT IAW UPS EO B72 7-5310-0943 & BOEING DRAWING 65C15724.Oct 4, 2001 · N913UP · Boeing 72762C · Nose/Tail Landing Gear Attach SectionSDR UPS01237063Structure · corrodedINSPECTION TYPE:C SUSPECT CORROSION ON AFT RUDDER CONTROL QUADRANT. REPAIR CARRIED OUT IAW MM 27-20-71, 27-20-00 & DRW 65-20879.Oct 2, 2001 · N913UP · Boeing 72762C · Rudder Control SystemSDR UPS01237046Panel · delaminatedINSPECTION TYPE:C NR 3 PYLON PANEL NR 5501 HAS DELAMINATION AT O/B FWD CORNER. REPAIRED IAW SRM.Oct 2, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/SkinSDR UPS01237039Stringer · corrodedINSPECTION TYPE:C ON REMOVAL OF FLOOR PANELS FOR CABLE INSPECTION, CORROSION FOUND ON FLOOR BEAM TOP CAP BS 344 RBL6. CORROSION REMOVED IAW SRM 51-10-06, DAMAGE OUT OF LIMITS, REPAIRED I AW SRM 53-10-08Oct 2, 2001 · N913UP · Boeing 72762C · Fuselage Main, StructureSDR UPS01237070Panel · delaminatedINSPECTION TYPE:C NR 3 PYLON PANEL 5508 ON LOWER SURFACE HAS DELAMINATION ON LOWER SKIN. REPAIRED IAW SRM 51-40-20.Oct 1, 2001 · N913UP · Boeing 72762C · Nacelle/Pylon, Plate/SkinSDR UPS01237069Spoiler Panel · delaminatedINSPECTION TYPE:C L/H WING DELAM ON #1 SPOILER PANEL PANEL REPLACEDOct 1, 2001 · N913UP · Boeing 72762C · Drag Control SystemSDR UPS01237038Stringer · crackedINSPECTION TYPE:C WHILE INVESTIGATING WING SCANNING LIGHT SUSPECT CRACK STRINGER 15L F OUND CRACKED AT BS 680. DAMAGE BLENDED OUT IAW SRM 53-10-3Oct 1, 2001 · N913UP · Boeing 72762C · Fuselage Main, StructureSDR UPS01237037Stringer · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION ON STRINGER NESTING SECTION AT BS 440 STR24L STRINGER REPAIR CARRIED OUT IAW SRM 53-10-03Sep 30, 2001 · N913UP · Boeing 72762C · Fuselage Main, StructureSDR UPS01237055Stringer · corrodedINSPECTION TYPE:C SUSPECT CORROSION AT BS 1120 STR 19R AREA PAINT STRIPPED, AREA OF SUSPECT CORROSION DERIVETED, SURFACE CO RROSION AND SEALANT REMOVED BETWEEN BS1110-1130 STR19R, STRINGER 19R CUT AND REMOVED AT BS1115-1135, INTERCOSTAL BETWEEN 1110-1130 Sep 28, 2001 · N913UP · Boeing 72762C · Fuselage Main, Plate/SkinSDR UPS01236903Bracket · crackedINSPECTION TYPE:C #3 THRUST REVERSER O/B LATCH FAIRING MID ANF AFT BRACKETS ARE CRACKE D. BRACKETS REPLACED IAW MM 78-30-01Sep 17, 2001 · N912UP · Boeing 72762C · Engine Thrust ReverserSDR UPS01236902Strap · crackedINSPECTION TYPE:C NDI INSP OF MID GALLEY DOOR CUTOUT INDICATES REINFORCING STRAP CRACK AT UPPER FWD CUTOUT. REPAIRED IAW UPS EO B727-5330-2685.Sep 17, 2001 · N912UP · Boeing 72762C · Fuselage Main, Plate/SkinSDR UPS01236901Trunnion · corrodedINSPECTION TYPE:C ON REMOVAL OF NLG TRUNNION CAPS CORROSION WAS FOUND IN ALL FOUR BOLT HOLES FOR CLAMPING OF TRUNNION CAPS. REPAIRED IAW SMRO EO 2001-044-001 UPS 727-53-200032.Sep 17, 2001 · N912UP · Boeing 72762C · Nose/Tail Landing Gear Attach SectionSDR UPS01236877Trunnion · corrodedINSPECTION TYPE:C ON REMOVAL OF TRUNNION CAPS ON NLG TRUNNION AREA WHERE BUSHINGS WERE INSTALLED HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 53-40-1, 20-20-02, & SMRO EO 2001-044-001.Sep 17, 2001 · N912UP · Boeing 72762C · Nose/Tail Landing Gear Attach SectionSDR UPS01236876Drum · corrodedINSPECTION TYPE:C NLG MANUAL EXTENSION AFT DRUM CORRODED. DRUM ASSY REPLACED IAW OHM 32-34-03.Sep 17, 2001 · N912UP · Boeing 72762C · Landing Gear Retraction/Extension SystemSDR UPS01236904Pressure Panel · crackedINSPECTION TYPE:C NDT INSPECTION FOUND CRACK INDICATION AT BS 880 LBL18-19. STOP DRILLED AND HFEC, CRACK CONTAINED. REPAIRED IAW EO B727-5310-04 60.Sep 15, 2001 · N912UP · Boeing 72762C · Fuselage Main, BulkheadSDR UPS01236890Support Fitting · crackedINSPECTION TYPE:C SUSPECT CRACKS ON LT AND RT 940 SUPPORT FRAME FITTING AT FLOOR BEAM ATTACH FLANGES. HFEC CARRIED OUT LT NDF RT CRACK CONFIRMED ON FWD I/B UPPER FLANGE. REPAIRED IAW UPS EO B727-5310-2954 A.Sep 14, 2001 · N912UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS01236905Spar · corrodedINSPECTION TYPE:C EVIDENCE OF CORROSION ON CENTER TANK FRONT SPAR UPPER CHORD VERTICAL FLANGE AT BS 740 RBL 25. REPAIRED IAW SRM 51-30-02 RBL 19 TO 31.Sep 13, 2001 · N912UP · Boeing 72762C · Wing SparSDR UPS01236445Bulkhead · crackedINSPECTION TYPE:N/A RT MLG WHEEL WELL FWD BULKHEAD BELOW APU EXHAUST HAS CRACKS AROUND U PPER INBOARD CANNON PLUG RECEPTICLE STA 870 ****MRR FILED AS OPEN*** AIRCRAFT FERRIED TO GSO REPAIR IN PROGRESS FERRY FLIGHT TO GSOJul 30, 2001 · N912UP · Boeing 72762C · Fuselage Main, StructureSDR UPS01236432Skin · crackedINSPECTION TYPE:N/A CRACKS AT RH WHEEL WELL AREA STA 870 ***MRR FILED AS OPEN***Jul 29, 2001 · N912UP · Boeing 72762C · Fuselage Main, StructureSDR UPS01234964Light · failedINSPECTION TYPE:IN COCKPIT EMERGENCY EXIT LIGHT INOP W/OP CHECKED IN FLIGHT. RELAMPED, OPS CHECKS GOOD.Feb 6, 2001 · N912UP · Boeing 72762C · Emergency LightingSDR UPS01234653Pressure Panel · crackedINSPECTION TYPE:PFLT 2 INCH CRACK ALONG RT NLG W/W SIDE WALL FWD OF GEAR TRUNNION AT APPROX STA 228 (MARKED). VERIFIED END OF CRACK WITH HFEC. STOP DRILLED RACK IAW 51-40-02 FIG 1. REPAIRED CRACK AS PER SRM 51-40-02 FIG 1. REF LOG PAGE 589676.Jan 16, 2001 · N912UP · Boeing 72762C · Fuselage Main, BulkheadSDR UPS00232522Fastener · crackedINSPECTION TYPE:C, CRACK IN FWD CARGO DOOR CUTOUT FWD FRAME INNER FAIL-SAFE STRAP 2ND FASTENER ABOVE STR 23R LOCATED CRACKED FAIL-SAFE STRAP AT BS 522 STR 18-28R. FABRICATED FAIL-SAFE STRAP PER SRM 51-10-2 AND INSTALLED FASTENERS PER SRM 51-30-2.Apr 30, 2000 · N913UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS00232469Channel · corrodedINSPECTION TYPE:C, CORROSION (C53-100-01.00-02) ON CHANNEL FROM BS 873 - BS 899 WL 188, LBL 66.5. REMOVED AND REPLACED CHANNEL PER SRM 51-40-3.Apr 25, 2000 · N913UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS00232307Line · burstINSPECTION TYPE:C, PRESSURE LINE IN B SYS HYD SERVICE BAY BURST ON OPERATION. FAILED UNDER P-CLIP AREA. PRESSURE LINE IN B-SYS HYD SERVICE BAY REPLACED IAW MM 20-80-01. LEAK CHECKED OK.Apr 11, 2000 · N912UP · Boeing 72762C · Hydraulic System, MainSDR UPS00232243Web · crackedINSPECTION TYPE:C, WEB BENEATH STAB ACTUATED ELEV TRIM SENSOR CRACKED AT SYS A & SYS B ELEVATOR HYD LINE SUPPORT POINT (PRESS LINES). WEB REPAIRED IAW SRM 51-40-3.Apr 8, 2000 · N912UP · Boeing 72762C · Elevator StructureSDR UPS00232258Frame · corrodedINSPECTION TYPE:C, CORROSION ON VERT STAB ON T-CHORD AFT OF FEEL COMPUTER. REPLACED T-CHORD IAW SRM 51-30-2. REF IPC 55-30-00, FIG 2.Apr 7, 2000 · N912UP · Boeing 72762C · Vertical Stabilizer, Spar/RibSDR UPS00232257Stiffener · corrodedINSPECTION TYPE:C, WING TO BODY FAIRING NR 3334 HAS CORRODED STIFFENER AROUND GROUND FAN DOOR CUTOUT (RT). ALSO, CORROSION ON DOOR CUTOUT CORRODED STIFFENER REPAIRED IAW SRM 51-40-3, FIGURE 1. CORROSION FOUND ON CORNER OF DOOR CUTOUT. CORROSION REMOVED, SKApr 6, 2000 · N912UP · Boeing 72762C · Aerodynamic FairingsSDR UPS00232245Cargo Track · crackedINSPECTION TYPE:C, SUSPECT CRACK FOUND ON TIE DOWN TRACK AT STA 1080, STR 28 RT ADJACENT TO FRAME CUTOUT. REPAIR CARRIED OUT IAW SRM 53-10-5.Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage, Seat/Cargo Attach FittingsSDR UPS00232244Channel · crackedINSPECTION TYPE:C, CRACK ON FLOOR LONGITUDINAL Z SECTION AT BS 1000 AT STR 30 IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-5 FIG 4.Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS00232242Frame · crackedINSPECTION TYPE:C, CRACK ON FRAME AT BS 1070 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Main, FrameSDR UPS00232241Frame · crackedINSPECTION TYPE:C, CRACK ON EDGE OF FRAME AT BS 1000 STR 29L IN LWR AFT CARGO HOLD. REPAIRED IAW SRM 53-10-4.Apr 6, 2000 · N912UP · Boeing 72762C · Fuselage Main, FrameSDR UPS00232256Web · crackedINSPECTION TYPE:C, LEFT AND RIGHT WEBS AT BS 1387 OVER THE ENGINE 2 HORIZONTAL FIREWALL ARE CRACKED. LT WEB AND BODY SKIN ATTACH TEE REPLACED IAW DRAWING 65-17555.Apr 5, 2000 · N912UP · Boeing 72762C · Nacelle/Pylon, Bulkhead/FirewallSDR UPS00232061Battery Pack · dischargedEMERGENCY EXIT LIGHT INOPERATIVE. REPLACED FWD ENTRY DOOR EMERGENCY EXIT LIGHT BATTERY PACK, SECURED OPS CHECKED GOODMar 21, 2000 · N913UP · Boeing 72762C · Emergency LightingSDR UPS99231094Support · corrodedINSPECTION TYPE AD V LEFT SUPPORT ASSY I/B FLAP TRACK FWD CORRODED. LEFT I/B FLAP TRACK FWD SUPPORT ASSY REPLACED IAW MM 27-51-31.Nov 8, 1999 · N912UP · Boeing 72762C · Trailing Edge FlapsSDR UPS99228532Light · inopINSPECTION TYPE-N/A, REPEAT WRITE UP WITH EMERGENCY EXIT SWITCH IN THE ARMED POSITION, THE EMERGENCY EXIT LIGHT IN THE COCKPIT IS ON. EMERGENCY EXIT LIGHT BY FWD ENTRY DOOR IS OFF. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AS PER MM 33-50-01. OPS CJan 26, 1999 · N912UP · Boeing 72762C · Emergency LightingSDR UPS98228204Skin · corrodedINSPECTION TYPE:C SURFACE CORROSION ON LOWER RUDDER SKIN PANEL LEFT SIDE BETWEEN FRONT SPAR AND REAR SPAR BY PCU ATTACH POINT. RUDDER REPLACED IAW MM 27-20-1.Nov 9, 1998 · N912UP · Boeing 72762C · Rudder, Plate/SkinSDR UPS98228169Frame · crackedINSPECTION TYPE-C DURING NDT INSPECTION, CRACK FOUND EMANATING FROM FOURTH FASTENER HOLE ABOVE FLOOR LINE AT BS 825.95 RT. REPAIRED IAW APPENDIX C OF EO B727-5310-5474.Nov 4, 1998 · N912UP · Boeing 72762C · Fuselage Main, FrameSDR UPS98228205Skin · corrodedINSPECTION TYPE:C CORROSION ON LOWER RUDDER SKIN PANEL RT SIDE FRONT SPAR AREA BY PCU ATTACH POIN. RUDDER REMOVED IAW MM 27-20-11.Nov 3, 1998 · N912UP · Boeing 72762C · Rudder, Plate/SkinSDR UPS98228166Frame · corrodedINSPECTION TYPE-C, FUSELAGE SLIDING FAIRING NR 3601 HAS CORRODED FRAME AT LOWER FWD CORNER. REPAIRED IAW SRM 53-10-4 AND TYPICAL WEB REPAIRS IAW SRM 51-40-3.Nov 3, 1998 · N912UP · Boeing 72762C · Aerodynamic FairingsSDR UPS98228161Bulkhead Beam · crackedINSPECTION TYPE-C, CRACK FOUND ON VERTICAL BEAM AT RIGHT BUTTOCK LINE 26.83 AT BS 1183 BULKHEAD CRACK ON VERTICAL BEAM AT RBL 26.85, BS 1183 BULKHEAD REPAIRED IAW APPENDIX D OF B727-5311-0631.Nov 3, 1998 · N912UP · Boeing 72762C · Fuselage Main, BulkheadSDR UPS98228162Support · corrodedINSPECTION TYPE-C, CORROSION ON ANGLE SUPPORT FOR FRONT NET TIE DOWN BS 780 LBL 60.00. ANGLE SUPPORT REPLACED IAW SRM 51-30-2.Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS98228136Intercostal · damagedINSPECTION TYPE-C, INTERCOSTAL DAMAGED BS 760 LBL 45 LBL 62. REPAIR CARRIED OUT IAW SRM 51-20-1.Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Miscellaneous StructureSDR UPS98228131Bulkhead · damagedINSPECTION TYPE-C, FWD PRESSURE BULKHEAD AND STIFFENERS FOUND DAMAGED BS 178 WL 200 RBL 5. REPAIRED IAW UPS EO B727-5310-4290 USING REPAIR KIT 65C36289-1.Nov 2, 1998 · N912UP · Boeing 72762C · Fuselage Main, Bulkhead
Back to Boeing 727-62C