Boeing 727-200
Service difficulty reports · 2,835
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 = '727200' 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 = '727200' 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 03FDEA00440Warning Light · illuminatedON CLIMBOUT OF HARLINGEN ,THE FIRE BELL AND GLARESHIELD LIGHT CAME ON INTERMTTENTLY. NO OTHER INDICATION (MOMENTARY/ INSTANTANEOUS THEN OUT). PERFORM ENGINES FIRE TEST NORMAL, NO DEFECT NOTED. CAN'T DUPLICATE PROBLEM. NO HISTORY. OK FOR SERVICE.SDR 03FDEA00443Control Unit · false indicationAT FL 190 AND CLIMBING (310 KIAS) THE FIRE WARNING BELL & MASTER FIRE LIGHT WENT OFF CONTINUOUSLY WITH NO OTHER INDICATIONS. THE BELL WOULD ONLY SILENCE WHEN ANY SILENCING BUTTON WAS HELD IN. BELL AND LIGHT WENT OUT ON DESCENT, CAME BACK ON AS AIRCRAFT BLOCKSDR 03FDEA00439Skin · canningEXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RT FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6 X 4.4 INCH, FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR SDR 03FDEA00438Skin · canningEXTERIOR SKIN OIL CANNED BS 1139 BETWEEN STR 23 AND 24 RT. OIL CANNED EXTERIOR SKIN BS 1139 BETWEEN STR 23 AND 24 RH FOUND TO BE OUT OF LIMITS PER SRM 53-30-1. REMOVED DAMAGE IN AN AREA OF 3.6" X 4.4 FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLSDR 03FDEA00429Indicator · illuminatedRETRACTED GEAR, L AN R MAIN GEAR UNSAFE-RED, NOSE GEAR GREEN. EXTENDED GEAR - ALL 3 LANDING GEAR SAFE -GREEN PER CREW CONVERSATION : NOSE GEAR RETRACTED NORMAL AND NO GREEN LIGHT ON (VARIES FROM ACTUAL WRITE UP). ADDITIONAL INFO, GEAR WAS DROPPED TO SLOSDR 03FDEA00413Frame · corrodedCORROSION (C53-111-01, 3) ON FRAME BS 950F LBL 8-11 WL 148. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69652.SDR 03FDEA00414Frame · corrodedCORROSION (C53-111-01, 3) ON FRAME BS 950E LBL 7 WL 148. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69652.SDR 03FDEA00415Frame · corrodedCORROSION (C53-111-01, 3) ON FRAME BS 950D WL 148 LBL 8-10. REPAIRED FRAME IAW SRM 53-10-4 FIG 15 AND EA 7-5310-69653.SDR DHL2003741530Frame · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, IN AFT PIT BS 1050 FRAME HAS 3 EACH DENTS IN THE RADIUS BETWEEN STRINGERS 25L-27L. REMOVED FRAME SPLICES IAW B-727 SRM 51-30-2. CUT OUT DAMAGE AREA APPROX 3 INCHES IAW B-727 SRM 51-40-3. FABRICATED NEW SPLICE DOUBLER FSDR 03FDEA00408Fan · inoperativeSHORTLY AFTER LVL OFF AT FLT LEVEL 280 THE NO EQUIP COOLING LIGHT ILLUM. QRH DIRECTED TO CHK / RESET EQUIP COOLING C/B. PULLED AND RESET THE C/B AND LIGHT REMAINED ON. QRH THEN DIRECTED TO SHUT OFF RADIO ALT, VHF, & DME - COMPLIED WITH CHK LIST AND LIGHT SDR 03FDEA00395Stringer · corrodedN00566 CORROSION TASK NR C53-111-01(3) CORROSION ON STR 29 LT (KEELBEAM)SDR 03FDEA00396Stringer · crackedN01236 CRACKED STRINGER AT BS 560+17 STR 23 LT.SDR 03FDEA00397Skin · damagedCOMPLY WITH E.A. NR 7-5330-68760 FUSELAGE SKIN- PRE-EXISTING ELONGATED HOLE AT STA. FACT 07APR03 11:48 BFM R COMPLIED WITH E.A. NR 7-5330-68760 FUSELAGE - SKIN PRE-EXISTING ELONGATED HOLE AT STA.508 UNDER MCD HINGE.SDR DHL2003741528Skin · bulgedDURING C-CHECK, FUSELAGE SKIN BULGED AROUND FASTENERS AT BS 1050 STR 27L. REMOVED FASTENERS SRM 51-30-2 WITH CORE FOUND TO BE OUT OF LIMITS SRM 53-30-1 FIG 1. CUT OUT DAMAGED AREA 5 X 5 INCH. FABRICATED DOUBLER 2024 T-3 .063 PO 9912495 DIM 13.5 X 11.5 INCH SDR 03FDEA00386Warning Light · failedEQUIPMENT COOLING LIGHT CAME ON IN FLIGHT. PULLED RADIO ALT CB VIA THE QRH AND LIGHT WENT OUT FOR A FEW MINUTES. LIGHT THEN CAME BACK ON STEADY. QHR SAID LAND, ASAP. ON RETURN TO MEMPHIS, LIGHT WENT OUT A COUPLE OF TIMES IN THE DESCENT BUT WAS ON MOST OF SDR 03FDEA00383Frame · corrodedN00557 CORROSION ON FRAME 950E WL148 LBL18. REMOVED CORROSION ON FRAME BS 950E WL 148 LBL 18 IAW SRM 51-10-1. REMOVED .75 W X 3 L X .012 D. ORIGINAL THICKNESS IS .071. OUT OF LIMITS IAW SRM 53-10-1 FIG 1. FABRICATED, ALODINED, PRIMED, PAINTED ANDSDR DHL2003741538Frame · corrodedDURING C-CHECK DISCREPANCY AS FOLLOWS, A/C BAY AT BS 720 HAS CORROSION AT BOTH LT AND RT SIDE OF RAM AIR DOOR ATTACH FRAME. CORROSION FOUND OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 1. REMOVED SKIN FOR ACCESS IAW B-727 SRM 51-30-2 AND CUT OUT 2 EACH DAMAGED ARSDR DHL2003741535Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT FUSELAGE SKIN AT BS 208 HAS A SHARP DENT ABOVE LT PITOT TUBE. LT FUSELAGE SKIN AT BS 208 HAS A SHARP DENT OUT OF LIMITS IAW B-727 SRM 53-30-1 FIG 1. CUT OUT DAMAGE AREA DIM 1 INCH IAW B-727 SRM 53-30-3 FIG 13. FABRISDR 03FDEA00372Bushing · missingTEST FLIGHT. UPON RAISING LANDING GEAR, NOSE GEAR RED LIGHT AND RED DOOR LIGHT STAYED ON. AIR CREW COULD HEAR SOMETHING STILL IN AIRSTREAM. LOG BOOK ENTRY REQ. UPON FURTHER INVESTIGATION, FOUND BUSHING FROM LOCK & POSITION SWITCH CONTROL ARM TO BE MISSINSDR 03FDEA00371Uplock Switch · inoperativeFLIGHT TEST. AIR BORNE WITH GEAR UP AND LDG GEAR HANDLE IN OFF POSITION, RED NOSE GEAR LIGHT COMES ON BRIGHT, AND GREEN NOSE GEAR LT COMES ON DIM. NO OTHER GEAR OR DOOR LIGHTS ON. NO LIGHTS ON S/O PANEL. LOG BOOK ENTRY REQ. UPON TROUBLESHOOTING NLG FOUND SDR DHL2003741548Fitting · corrodedDURING C-CHECK, BS 1050 STR 27R END FITTING CORRODED. REMOVED FITTING BS 1050 STR 26R FOR REPAIR. REMOVED FASTENERS FOR ACCESS ON STR 27R KEEL BEAM EXTENSION ANGLE. UPON REMOVAL OF STR FITTING FOUND KEELBEAM T-ANGLE CORRODED AND CRACKED. REMOVED PREVIOUS KSDR 03FDEA00364Floorbeam · corrodedCORROSION ON BS 344 FLOORBEAM LBL 55 - RBL 15 WL 208. REMOVED CORROSION ON UPPER CHORD OF FLOORBEAM BS 344 LBL 55 - RBL 15, WL 208 MAX REMOVAL 1 X 1 X 0.030 INCH ORIGINAL THICKNESS 0.090 OUT OF LIMITS IAW SRM 51-10-6 &7 SRM 53-10-1. ACCOMPLSDR 03FDEA00365Floorbeam · corrodedCORROSION ON BS 680 FLOORBEAM, LBL 5 TO LBL 43, WL 208. REMOVED CORROSION, BS 680 FLOORBEAM UPPER CHORD AT NUTPLATE LOCATIONS LBL 5 TO LBL 43. ORIGINAL THICKNESS OF .130 MAX DEPTH OF REMOVAL LBL 27-29 FOUND TO BE .032. OUT OF LIMITS PER B727 SRM 53-SDR 03FDEA00367Skin · dentedCONVEX DENT IN SKIN AT BS 1020, JUST ABOVE STR 26L CONVEX DENT IN SKIN AT BS 1020 JUST ABOVE STRINGER 26L, FOUND TO BE OUT OF LIMITS PER SRM 53-10-1 PG 2A, DETAIL II. REMOVED DENT 1 INCH DIAMETER X .063. FABRICATED REPAIR AND INSTALLED IAW SRM 53-30-3 SDR DHL2003741522Skin · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT FUSELAGE SKIN BS 1270 IS DENTED ABOVE STR 21L. REMOVED 2 EACH PNEUMATIC DUCTS FOR ACCESS MM 36-00-01. CHEMICALLY REMOVED PAINT MM 51-20-01. REMOVED FASTENER AS REQUIRED SRM 51-30-2. CUT OUT DAMAGE AREA 1.25 X 1 INCSDR 03FDEA00368Frame · dentedB/S 600 FRAME DENT STR 23L. DENT IN FRAME AT BS 600 STR 23L FOUND TO BE OUT OF LIMITS. REPAIRED PER FED-EX EA 7-5310-54458.SDR 03FDEA00366Frame · dentedFRAME DENTED BS 990 STR 26L. FRAME DENTED AT BS 990 STR 26L WAS OUT OF LIMITS. COMPLIED WITH FED EX EA 7-5310-69458.SDR 03FDEA00360Skin · dentedN00175 EXTERIOR SKIN IS DENTED AT STA. 702F STR-4R. DENT AT 702F+15 STR 4R WAS FOUND TO BE OUT OF LIMITS IAW SRM 53-30-1, PG 2A, DETAIL II. CUT OUT DAMAGED SKIN 1 INCH DIAMETER AND REPAIRED IAW SRM 53-30-3.SDR 03FDEA00361Floorbeam · corrodedCORROSION ON FLOORBEAM BS 1070 RBL 1 RBL 44, WL 201 AT FASTENER HOLES. REMOVED CORROSION ON LOWER FLOORBEAM BS 1070 RBL 1-44 AT FASTENER HOLES. ORIGINAL THICKNESS .130 REMOVED .010 MAX MATERIAL IN A 1 X 1 AREA RBL 1-RBL 26 & RBL 31-44 IN LIMITSSDR 03FDEA00362Floorbeam · corrodedCORROSION ON FLOORBEAM, STA 620, RBL 11, WL 208 (FASTENER HOLE). REMOVED CORROSION ON FLOORBEAM BS 620 RBL 11 WL 208 IN AN AREA OF 1 X 1 X .019 FOUND TO BE OUT OF LIMITS CUT OUT DAMAGE FABRICATED REPAIR PARTS DRILLED, ALODINED, PRIMED AND INSSDR 03FDEA00363Beam · corrodedCORROSION ON LONGITUDINAL BEAM UPPER FLANGE AT NUT PLATE HOLES BS 758-850 R25 WL 208. CORROSION ON LONGITUDINAL BEAM UPPER FLANGE BS 758-850 RBL 25 WL 208 FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1. REMOVED AND REPLACED BEAM IAW SRM 51-30-5 AND 51SDR 03FDEA00369Frame · damagedMECHANICAL DAMAGE TO FRAME BS 420 BETWEEN STR 6 RT AND 7 RT. INSTALLED REPAIR CHANNEL ON FRAME PER SRM 53-10-4.SDR 03FDEA00373Warning Light · illuminatedDURING INITIAL CLIMB PASSING 800-1000 FT WE EXPERIENCED A RED WINDSHEAR WARNING AND AURAL WARNING. WE PERF THE EMERGENGY ESCAPE MANUVER AND IMMEDIATELY FIREWALL ALL THRUST LEVERS. WARNING LASTED 5 SECONDS. THRUST LEVERS WERE THEN RETARDED TO MAX POWER. SDR 03FDEA00370Floorbeam · corrodedCORROSION ON UPR FLANGE OF FLOORBEAM BS 910 RBL 55 WL 208 LWR SURFACE AT NUT PLATE HOLE.SDR DHL2003749004Wire · brokenGLARESHIELD BELL CUTOUT SWITCH DOES NOT WORK. REPAIRED BROKEN WIRE ON CUTOUT SWITCH IAW M/M 20-11-0. CUTOUT SWITCH OPS CHECKED GOOD.SDR DHL2003741500Skin · canningDURING C CHECK, FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT, REMOVED FASTENER AT FUSELAGE SKIN OIL CANNING AFT BS 1050 BELOW STR 23 LT IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA DIM. APPROX. 2 X 1 INCH IAW B-727 SRM 53-30-2.SDR DHL2003741512Frame · dentedDURING C-CHECK DISCREPANCY AS FOLLOWS, BS 440 FRAME DENTED LT ABOVE FLOOR LEVEL. REMOVED FASTENERS BS 440 FRAME LT ABOVE FLOOR LEVEL IAW B-727 SRM 51-30-2. CUT OUT DAMAGED AREA AND FABRICATED DOUBLER REPAIR IAW B-727 SRM 53-10-4 FIG 2. INSTALL DOUBLER REPAISDR DHL2003741523Stringer · corrodedDURING C-CHECK, LOWER FWD CARGO COMP AIR CONDITIONING AREA FRAME BS 720F CORRODED BETWEEN STR 26 R/27R. REMOVED FASTENERS FOR ACCESS IAW B-727 SRM 51-30-2. CLEANED CORROSION AND FOUND MATERIAL LOSS OUT OF LIMITS IAW B-727 SRM 53-10-1 FIG 1. CUT OUT DAMAGE SDR DHL2003741511Seat Track · gougedDURING C-CHECK DISCREPANCY AS FOLLOWS, BS 521 - 530 LT BL 45 SEAT TRACK ARE GOUGED AT LOCK EARS. REMOVED DAMAGED SEAT TRACK AT BS 480-540 LBL 45 IAW B-727 SRM 51-30-2. LOCATED AND DRILLED NEW SEAT TRACK AND INSTALLED IAW B-727 SRM 53-10-5 FIG 7.SDR DHL2003741510Seat Track · gougedDURING C-CHECK DISCREPANCY AS FOLLOWS, BS 800 AND 824 LT BL 45 SEAT TRACK EARS ARE WORN WITH GOUGES. REMOVED DAMAGED SEAT TRACK AND INSTALLED NEW SEAT TRACK IAW B-727 SRM 51-30-2 AT BS 760 TO 848 LT BL 45.SDR DHL2003741540Structure · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 8L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC 1517-1367 PO 3SDR DHL2003741536Structure · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, EMPENNAGE INT'R STRUCTURE VERTICAL FIN HAS CRACK AT STR 9L FIN STA 133.8 AT THRU BOLT ATTACH ANGLE TO CHORD ANGLE. CUT OUT DAMAGED AREA DIM 7.75 INCH AND FABRICATED FILLER AND 2 EACH REPAIR ANGLES FROM BAC1517-1367 PO 30SDR DHL2003741549Spar · crackedDURING C-CHECK, LT ELEVATOR NR 3 TAB HINGE LOOSE, INDICATION OF CRACK. REMOVED DAMAGED SPAR AND INSTALLED NEW P/N 65C30825-23 PO 307748 PER S/B 727-55-0089 R1. OP'S CHECK GOOD IAW M/M 27-30-00.SDR DHL2003741526Angle · crackedDURING C-CHECK, RT WING, LWR I/B LEADING EDGE, INSIDE ACCESS PANEL CAVITY 6401 UPPER O/B, L/E WEB TO L/E SKIN ATTACH ANGLE HAS 2 INCH CRACK. REMOVED FASTENERS RT LOWER I/B, L/E INSIDE ACCESS PANEL UPPER O/B L/E WEB TO L/E SKIN ANGLE IAW B-727 SRM 51-30-2. CUSDR DHL2003741553Stringer · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, BS 848 RT SIDE STR 17 BELOW THE FLOOR IS CRACKED AFT AT CIRCUM. CUT OUT AREA OF SKIN FOR ACCESS IAW B-727 SRM 53-30-3 FIG 3 DIM 10 X 3.75 INCH. CUT OUT DAMAGED SECTION OF STRINGER DIM 25 INCHES LONG IAW B-727 SRM 51-40-SDR DHL2003741551Hinge · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, MCD HINGE CRACKED (FWD LWR SECTION AND AFT UPPER SECTION) NDT CONFIRMED. REMOVED DAMAGED HINGES AND INSTALLED NEW P/N MS20001-16, PO 307742 IAW AEI B-727 MM CHAPTER 52 FIGURE 5201C. OPS CHECK GOOD IAW AEI B-727 MM CHAPTSDR DHL2003741543Angle · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING LEADING EDGE AT LEADING EDGE STA 130 IS CRACKED. REMOVED EXISTING FASTENERS TO GAIN ACCESS TO THE REPAIR AS PER B-727 SRM 51-30-2. CUT DAMAGED AREA AS PER B-727 SRM 51-40-3 FIG 1. FABRICATED REPAIR ANGLES MATERSDR DHL2003741534Stiffener · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, LT WING FRONT SPAR VERTICAL STIFFENER HAS TWO CRACKS AT LOWER TWO RIVETS AT LEADING EDGE STA 90. REMOVED FASTENER AT LT WING FRONT SPAR VERTICAL STIFFENER CUT OUT DAMAGE AREA DIM APPROX 2.375 BY 2.4375 INCH IAW B-727 SRMSDR DHL2003741533Beam · crackedDURING C-CHECK DISCREPANCY AS FOLLOWS, RT MLG BEAM OUTBOARD TO REAR SPAR SUPPORT FITTING IS CRACKED UPPER INBOARD CORNER OF THE CUTOUT. ROUND OUT REMOVAL AREA TO A .375 INCH RADIUS AND BLENDED OUT UPPER AND LOWER AREA OF DAMAGE WITH .3888 INCH DEPTH REMOVAL OSDR DHL2003741521Frame · dentedDURING C-CHECK, BS 480 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR. REMOVED FASTENERS AT BS 480 RT CIRCUMFERENTIAL DENTED 4 INCHES ABOVE FLOOR IAW B-727 SRM 51-30-2. CUT OUT DAMAGED IAW B-727 SRM 53-10-4 FIG 2. FABRICATED DOUBLER REPAIR MATERIAL USED 70
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