Boeing 727-233
Service difficulty reports · 3,034
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 = '727233' 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.
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 = '727233' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR 97FDEA00024Chord · corrodedNR 0574 15 WHILE WORKING NR 0479, FOUND CORROSION ON NOSE CHORD AT NUTPLATE HOLES BS 347 TO BS 351, RBL 17, WL 151. *S/D* REPAIRED NOSE CHORD BS 347 TO 351, RBL 17, WL 151 PER FED-EX E75310-32122.SDR 97FDEA00023Bracket · corrodedNR 0478 14 CORROSION (C53-100-01-1) ON DRAG BRACE SHELF BRACKET BS 337, LBL 16, WL 147. *S/D* FOUND TO BE OUT OF LIMITS. REPLACED BRACKET AT BS 337, LBL 16, WL 147 PER FED-EX SRM 53-10-1.SDR 97FDEA00022Intercostal · corrodedNR 0525 CORROSION (C53-221-01) ON INTERCOSTAL BS 259 TO 277 LBL 9, WL 208. *S/D* REMOVED CORRODED INTERCOSTAL AND INSTALLED NEW PART PER FED-EX SRM 51-30-2.SDR 97FDEA00021Chord · corrodedNR 0524 CORROSION (C53-221-01) ON 25 G-BEAM BS 266 BL 0 TO LBL 7, WL 208. *S/D* REMOVED DAMAGED 25 G-BEAM, INSTALLED NEW PART PER FED-EX SRM 51-30-2.SDR 97FDEA00013Beam · corrodedNR 0489 LBL 45 LONGITUDINAL BEAM BENT TRACK HAS CORROSION EMANATING FROM BETWEEN TRACK AND BEAM BS 760 TO 790 WL 208. *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM SET TRACK AT LBL 45, WL 208 FROM BS 744 TO 848.5 IAW FED EX SRM 53-10-1 SRM 51-10-2 SRM 51-30-2SDR 97FDEA00008Frame · dentedNR 253 FRAME DENTED AT BS 700 RBL 32 TO 40 FWD BAY. *S/D* REMOVED DAMAGE AT BS 700, RBL 32 TO 40, FABRICATED REPAIR PART, ALODINED, PRIMED AND INSTALLED REPAIR PART PER FED-EX SRM 51-40-3.SDR 97FDEA00005Frame · dentedNR 244 FRAME DENTED AT BS 680 RBL 45 FWD BAY. *S/D* REMOVED DAMAGE AT BS 680, RBL 45, FABRICATED REPAIR PART, ALODINED, PRIMED AND INSTALLED REPAIR PART PER FED-EX SRM 51-40-3.SDR 97FDEA00015Frame · dentedFRAME DENTED AT BS 660, LBL 37 FWD BAY. *S/D* REMOVED DAMAGED AREA OF FRAME 660, FABRICATED, DRILLED, ALODINED AND PRIMED REPAIR PART PER FED EX SRM 51-40-3. SEALED MATING SURFACES AND INSTALLED PART AND FASTENERS.SDR 97FDEA00014Long Beam · corrodedRBL 25 LONGITUDINAL BEAM BENT TRACK HAS CORROSION EMANATING FROM IN BETWEEN TRACK AND BEAM BS 760 TO 848.95 WL 208. *S/D* MECHANICALLY REMOVED CORROSION ON SET TRACK AND BEAM. FOUND SEAT TRACK AND BEAM TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1. REMOVED ANSDR 97FDEA00012Beam · corrodedNR 0488 RBL 45 LONGITUDINAL BEAM BENT TRACK HAS CORROSION EMANATING FROM IN BETWEEN TRACK AND BEAM BS 760 TO 847.95 WL 208. *S/D* MECHANICALLY REMOVED CORROSION ON SEAT TRACK AND BEAM. FOUND SEAT TRACK AND BEAM TO BE OUT OF LIMITS PER FED EX SRM 53-10-1. RSDR 97FDEA00006Floorbeam · corrosionNR 0434 CORROSION (53-224-01,1) ON BS 580 BEAM, LBL 35, WL 208.1. *S/D* REMOVED AND REPLACED TOP CHORD OF BS 580, WL 208, FROM LBL 18 TO LBL 60 IAW FED-EX SRM 53-10-8, SRM 51-30-2, SRM 51-10-2.SDR 97FDEA00001Control Valve · failedAT FLIGHT LEVEL 250, LEFT PACK COOLING DOOR WAS CLOSED AND PACK TEMPERATURE REACHED 150 CELSIUS ACCOMPLANIED BY ACRID SMELL AND SMOKE IN COCKPIT. REMOVED AND REPLACED 35 DEGREE CONTROL VALVE LEFT SIDE. CHECKED LEFT COOLING AND EXHAUST DOORS. ALL CHECK NORMASDR 97FDEA00019Frame · dentedNR 0256 FRAME DENTED AT BS 500 RBL 34, 40, 46 WL 159 TO 167. *S/D* REPAIRED DENTED FRAME BS 500 RBL 30 TO 50, WL 155 TO 170 PER FED-EX SRM 51-40-3 FIG 1.SDR 97FDEA00007Chord · corrodedNR 0431 CORROSION (53-224-01,1) BARE METAL ON 344 BEAM FROM LBL 25 TO 10 TO RBL 25 WL 208.1 AND DOUBLE HOLE AT LBL 59 WL 208. *S/D* FABRICATED NEW UPPER CHORD, BACK DRILLED ALL HOLES, FABRICATED SPLICE ANGLES AND BACKDRILLED EXISTING HOLES AND DRILLED ALL NESDR 97FDEA00004Floorbeam · corrodedNR 0437 CORROSION (C53-224-01,3) ON TOP CHORD OF FLOORBEAM AT BS 1070, RBL 27 TO 56, WL 208. *S/D* DAMAGE TO TOP CHORD OF FLOORBEAM AT BS 1070, RBL 27 TO 56, WL 208 WAS FOUND TO BE OUT OF LIMITS PER FED-EX SRM 53-10-1 FIG 4. REPAIRED TOP CHORD PER FED-EX SRSDR 97FDEA00020Floorbeam · corrodedNR 0435 CORROSION (C53-224-01,1) ON BS 620 BEAM, LBL 45 TO RBL 25, WL 208.1. *S/D* REMOVED AND REPLACED TOP CHORD OF FLOORBEAM AT BS 620, RBL 35 TO LBL 35, WL 208 PER FED-EX SRM 53-10-8, FIG 3.SDR 96FDEA01697Actuator · failedA SYSTEM HYDRAULIC PRESSURE WENT TO ZERO IN FLIGHT. A SYSTEM LOW PRESSURE LIGHT ILLUMINATED. PERFORMED EMERGENCY PROCEDURES, HAND CRANKED GEAR DOWN. CLOSED HYDRAULIC FLUID SHUTOFF VALVES, USED ALTERNATE FLAPS AND SHUT OFF ALL A-SYSTEM COMPONENTS. TOWED BACSDR 96FDEA01692Switch · malfunctionedAT FLIGHT LEVEL 290 CLIMBING TO FLIGHT LEVEL 310, PRESSURIZATION NORMAL, MAIN CARGO DOOR LIGHT ILLUMINATED. PRECAUTIONARY DESCENT TO 10,000 FT, SLOWED TO 250 KNOTS PER RED TAB PROCEDURES. ALSO, DEPRESSURIZED THE AIRCRAFT, HAD BULKHEAD CARGO DOOR UNLOCKED LIGSDR 96FDEA01688Position Switch · out of adjustON FINAL, GEAR HANDLE DOWN NO GREEN NOSE GEAR LIGHTS ILLUMINATED. RECYCLED GEAR UP AND DOWN AGAIN GREEN GEAR LIGHT ILLUMINATED NORMALLY. ACCOMPLISHED NOSE GEAR LOCK AND POSITION SWITCHES ADJUSTMENT AND TEST PER MAINTENANCE MANUAL 32-61-71 PAGE 501 TO 502. NSDR 96FDEA01685Mechanism · out of adjustAFTER LANDING GEAR RETRACTION DOORS LIGHT ON FORWARD PANEL AND NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANEL REMAINS ILLUMINATED WHILE GEAR HANDLE WAS IN UP POSITION. LANDING GEAR WAS RECYCLED WITH NO EFFECT. INCREASED NOISE IN COCKPIT SUGGEST THAT THE NOSESDR 96FDEA01664Bonding Jumper · corrodedNR 398 036, CORROSION (C57-562-01-1) NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT. *S/D* REPAIRED NR 1 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER END LOWER ATTACH POINT IAW FEDEX EA 7-5750-31262.SDR 96FDEA01663Angle · corrodedNR 640, 035, CORROSION (C53-224-01, 1) ON MOP SILL AT BS 312 TO 360, LBL 62, WL 208.1. *S/D* REMOVED AND REPLACED MOP SILL FROM BS 259 TO 360, LBL 65 WL 208.1 IAW FEDEX SRM 53-10-1, 51-30-2.SDR 96FDEA01666Bullnose · wornNR 0137 038, LOWER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOVAL AND INSTALL REQUIRED). *S/D* REMOVED LOWER RUDDER, INSTALLED DOUBLERS OVER WORN AREAS IAW FEDEX SRM 55-40-3 FIG 1, REINSTALLED RUDDER ISDR 96FDEA01665Bullnose · wornNR 0136 037, UPPER RUDDER BULLNOSE WORN AT CONTACT POINT OF RUDDER TO VERTICAL FIN FAIRING, BEYOND LIMITS. RUDDER REMOVAL AND INSTALL REQUIRED. *S/D* REMOVED UPPER RUDDER, INSTALLED DOUBLER OVER WORN AREA IAW FEDEX SRM 55-40-3 FIG NR 1. REINSTALLED UPPER RSDR 96FDEA01660Smoke Detector · malfunctionedON DESCENT INTO CLE, MAIN CARGO SMOKE DETECTOR NR 2 INDICATOR FLASHED MOMENTARILY AND RANG THE BELL. OPERATIONAL CHECK OF SMOKE DETECTION SYSTEM FOUND NO DEFECTS.SDR 96FDEA01658Window Frame · corrodedNR 0128 034. MAIN CABIN RIGHT HAND WINDOW PLUG BS 640-660 HAS EVIDENCE OF CORROSION BETWEEN PLUG AND WINDOW FRAME LOWER AFT CORNER. *** S/D *** COMING.SDR 96FDEA01657Clip · crackedNR 0806. FOUND STRINGER CLIP AT BS 950C STRINGER 7 RT TO BE CRACKED. *** S/D *** COMING.SDR 96FDEA01655Shear Tie · corrodedNR 0214 31. CORROSION (C53-111-01) ON SHEAR TIE (FWD AND AFT SIDE) AT BS 520 RBL 24 WL 150. REMOVED AND REPLACED SHEAR TIE AT BS 520, RBL 24, WL 150 PER FEDEX SRM 51-10-1.SDR 96FDEA01654Floorbeam · corrodedNR 0816 32. WHILE WORKING NR 0636 FOUND CORROSION ON BS 328 FLOORBEAM WL 208 LBL 27, 29 AND 45. REPAIRED BS 328 FLOOR BEAM PER FEDEX SR 27-53-017.SDR 96FDEA01648Bullnose · corrodedNR 0407 029, CORROSION ON NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER AND LOWER ATTACH POINT. *S/D* REMOVED CORROSION AND REPAIRED NR 2 K-FLAP BULLNOSE O/B BONDING JUMPER ATTACHMENT POINTS IAW FEDEX SRM 57-50-3 AND FEDEX SR 27-57-010.SDR 96FDEA01646Floorbeam · corrosionNR 0635 026. CORROSION (C53-224-01(1) ON 344 BEAM FROM LBL 60 TO RBL 20 WL 208.1. REMOVED CORROSION ON 344 FLOOR BEAM, TOP CHORD FROM LBL 60 TO RBL 20, W/L 208.1. FOUND TO BE OUT OF LIMITS IAW 727 FEDEX SRM 53-10-01. REMOVED AND REPLACED FLOOR BEAM TOP CHOSDR 96FDEA01639Beam · corrodedNR 0712 027. CORROSION (C53-224-01(2)) ON LONGITUDINAL BEAM AT BS 784 TO BS 810 LBL 25 WL 208 P/N 65-16279-10. REMOVED AND REPLACED LONGITUDINAL BEAM BS 784-810 LBL 25, WL 208 PER FEDEX SRM 51-10-1.SDR 96FDEA01638Skin · corrodedNR 0450 028. CORROSION (C53-111-01(1) ON STR 26 LT AND SPLICE STA 676-679 WL 152 STR 26 LT (FWD BAY). UPON REMOVAL OF STRINGER, FOUND CORROSION ON SKIN AT BS 662. REPAIRED STRINGER AND SKIN BETWEEN BS 650-680, WL 152, STR 26 LT. PER FEDEX SRM 53-30-3, 53-SDR 96FDEA01636Stringer · crackedNR 0153 024. CRACKED STRINGER AT STA 720 B PLUS 3 STRINGER 15 RT. REPAIRED STRINGER AT BS 720B PLUS 3 STR 15 RT PER FED EX SRM 53-10-03.SDR 96FDEA01633Beam · corrodedNR 0711 020. CORROSION (C53-224-01(2) ON LONGITUDINAL BEAM AT BS 740 TO BS 812 AND BS 825- TO BS 840 RBL 25 WL 208 P/N 65-16279-10. REMOVED AND REPLACED LONGITUDINAL BEAM AT BS 740-850, RBL 25, WL 208.SDR 96FDEA01631Web · corrodedNR 742 122, CORROSION ON AFT SIDE OF WEB STA 219.8 LBL 42 WL 210 TO 232. *S/D* REPAIRED WEB DOUBLER BS 219.8 LBL 42 WL 210 TO 232 PER FEDEX SRM 51-40-2.SDR 96FDEA01630Floorbeam · corrodedNR 0648 023, CORROSION (C53-224-01) ON FLOORBEAM AT BS 1030 RBL 48 TO RBL 55. *S/D* REMOVED CORROSION FROM FLOORBEAM AT BS 1030 RBL 48 TO RBL 55. BEAM OUT OF LIMITS IAW FEDEX 727 SRM 53-10-1, REPAIRED BEAM IAW FEDEX 727 SRM 53-10-8.SDR 96FDEA01632Intercostal · corrodedNR 0119 021, CORROSION (C53-111-01-1) NOSE E-BAY INTERCOSTAL BS 219.8 TO 227 LBL 20 WL 163 TO 167. *S/D* REPLACED INTERCOSTAL NOSE E-BAY BS 219.8 TO 227 LBL 20 WL 163 TO 167 PER FEDEX SRM 51-10-1.SDR 96FDEA01627Frame · corrodedNR 0747 019, CORROSION (C53-221-01) ON WEB FORWARD SIDE OF FRAME STA 243, RBL 48, WL 211 TO 233. *S/D* REPAIRED WEB AT STA 243 FRAME RBL 48 WL 211 TO 233 PER FEDEX SRM 51-40-2.SDR 96FDEA01626Hinge Lug · corrosionNR 0399 018, CORROSION NR 1 K-FLAP CENTER HINGE LUG AT LOWER BOLT. *S/D* REMOVED CORROSION ON NR 1 K-FLAP CENTER HINGE LUG. REPAIRED IAW FEDEX EA 7-5750-31276A. FUNCTIONAL TESTED NR 1 K-FLAP OK IAW FEDEX M/M 27-81-1.SDR 96FDEA01625Web · corrodedNR 0739 017. CORROSION (C53-22-01) UNDER HORIZONTAL WEB AND OUTBOARD CHORD STA 225-251 RBL 45 WL 231 (NR 2 WINDOW LOWER TRACK SITS ON IT). REMOVED AND REPLACED HORIZONTAL WEB STA 225 TO 251, RBL 45, WL 231. IAW FEDEX SRM 53-10-1. REMOVED CORROSION ON O/BSDR 96FDEA01624Skin · gougedNR 0043 016, BS 480, STRINGER 22 RT TO 23 RT THERE ARE GOUGES ON THE OUTER SKIN. *S/D* REPAIRED GOUGES ON OUTER SKIN BS 480 STRINGER 22 RT TO 23 RT PER FEDEX SRM 53-30-3.SDR 96FDEA01623Bonding Jumper · corrodedNR 0403 015, CORROSION ON NR 3 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER AND LOWER ATTACH POINTS. *S/D* REPAIRED NR 3 K-FLAP BULLNOSE O/B BONDING JUMPER UPPER ATTACH POINT PER FEDEX SRM 57-50-3 AND THE LOWER ATTACH POINT WAS FOUND TO BE WITHIN LIMITS PER FEDESDR 96FDEA01622Chord · corrosionNR 0255 014. CRACKED LEVELING COMPOUND AT BS 552, RBL 25, WL 152. UPON FURTHER INVESTIGATION, FOUND CORROSION UNDER LEVELING COMPOUND ON CHORD WHICH IS OUT OF LIMITS. FOUND CORROSION FROM CHORD. CORROSION REMOVAL FOUND TO BE OUT OF LIMITS. FABRICATED ANDSDR 96FDEA01621Web · corrodedNR 745 013. CORROSION (C53-221-01) ON AFT SIDE OF WEB AND OUTBD CHORD STA 227 RBL 48 WL 190 - 232. REPAIRED CORROSION ON WEB AND OUTBD CHORD STA 227, RBL 48, WL 190-232 PER FEDEX EA 7-5310-31245; SRM 51-30-2, 51-40-2.SDR 96FDEA01616Skin · delaminationNR 0699 006, RT I/B AFT FLAP HAS LARGE AREA OF DENTS AND DELAMINATIONS ON LOWER SURFACE I/B END *S/D* REPAIRED RT I/B AFT FLAP ON LOWER SURFACE IAW FEDEX SRM 51-40-6.SDR 96FDEA01619Floorbeam · corrodedNR 0652, CORROSION (C53-224-01) ON TOP CHORD OF FLOORBEAM BS 720D RBL 23, LBL 3, 15, 20. *S/D* REPAIRED PER FEDEX SRM 53-10-8.SDR 96FDEA01618Beam · corrodedNR 0710, CORROSION (53-224-01,2) ON LONGITUDINAL BEAM AT BS 779 TO BS 793 RBL 45, WL 208 (P/N 65-16279-10). *S/D* REMOVED AND REPLACED LONGITUDINAL BEAM AT BS 740 TO 850 RBL 45 WL 208.SDR 96FDEA01617G-Beam · corrodedNR 0751 009, CORROSION (C53-221-01) ON TOP OF 25 G-BEAM AND 3 SUPPORTING INTERCOSTALS STA 267 LBL 8 STA 267 LBL 9 STA 267 LBL 11 AND STA 277 TO 259 LBL 13 WL 208. *S/D* REMOVED AND REPLACED 25 G-BEAM AND 3 SUPPORTING INTERCOSTAL FLOOR SUPPORTS AT STA 277 TO SDR 96FDEA01613Skin · delaminationNR 0697, RT I/B FOREFLAP HAS TWO LARGE AREAS OF DENTS AND DELAMINATIONS ON LOWER SURFACE. *S/D* RT I/B FOREFLAP WAS REPAIRED PER FEDEX SRM 51-40-6.
Back to Boeing 727-233