Boeing 727-200

Service difficulty reports · 2,835

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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"

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SDR 06FDEA0106Floorbeam · corrodedAFT CARGO, FLOORBEAM LOWER FLANGE CORRODED AT BS 1070, LBL 28, WL 201. REPAIRED PER SRM 53-10-8.Jan 9, 2006 · N488FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 06FDEA0105Structure · corrodedAFT CARGO CEILING SUPPORT STRUCTURE CORRODED AT BS 1070 LBL 25 WL 201. REMOVED CORROSION FROM SUPPORT FOUND TO BE OUT OF LIMITS FABRICATED NEW SUPPORT INSTALLED REPAIR PART ALL WORK DONE IAW 53-10-1 51-20-1 53-10-8 51-30-2 & 51- 10-2Jan 9, 2006 · N488FE · Boeing 727200 · Fuselage Main, StructureSDR 06FDEA0101Stringer · misdrilledFOUND MCD STRINGER 4L AT STA 450 HAS TOOLING MARKS AND 2 DRILLED MARKS ON OUTBD SIDE OF STRINGER, AFTER BLENDING AND FOUND OUT OF LIMITS PER SRM 5310-01, FIG 1, REMOVED AND REPLACED ALL DAMAGE PARTS IAW SRM 51-30-3.Jan 9, 2006 · N498FE · Boeing 727200 · Fuselage Main, Longeron/StringerSDR 06FDEA0068Repair · unknownFOUND PREVIOUSLY REPAIR, INSTALLED AT STA 1330 ABOVE AIRSTAIRS CUTOUT RT SIDE WAS ACCOMPLISHED IAW SRM 53-30-3 FIG 3, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBERS AND SPACING, GENERAL WJan 8, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00058Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT FWD OF NR 2 ENGINE LT SIDE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP Jan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00057Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA 1325 ABOVE AIRSTAIRS CUTOUT WAS ACCOMPLISHED IAW SRM 51-40-2 FIG 1, BASED ON AN EXTERNAL VISUAL EVALUATION CONSIST OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSJan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00056Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA.1323 LT SIDE BELOW PYLON TRAILING EDGE WAS ACCOMPLISHED IAW SRM 51-40-2, FIG 1, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, SIZE, SHAPE, MATERIAL TYPE AND THICKNESS, FASTENERS NUMBERS AND SPACING, GENERAL WORKJan 6, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00055Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT RT WING OB OF LANDING LIGHT WAS ACCOMPLISHED IAW SRM 57-30-4, BASED ON AN EXTERNAL VISUAL EVALUATION, CONSISTS OF LOCATION, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENERS NUMBER AND SPACING, GENERAL WORKMANSHIP ANDJan 6, 2006 · N498FE · Boeing 727200 · Wing StructureSDR 06FDEA00045Shear Web · fomNO1461 RT SHEAR WEB STA 1130-1140 NEEDS ACCESSED, CUT AND REPAIRED TO ACCOMIDATE 1130 FLOORBEAM UPPER CHORD REPLACEMENT REMOVED & REPLACED RT SHEAR WEB AT BS 1130-1140 IAW SRM 51-40-2 AND SRM 51-30-2.Jan 5, 2006 · N490FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA00044Shear Web · fomNO1460 LT SHEAR WEB STA 1130-1140 NEEDS ACCESSED, CUT AND REPAIRED TO ACCOMIDATE 1130 FLOORBEAM UPPER CHORD REPLACEMENT. REMOVED & REPLACED LT SHEAR WEB BS 1130-1140 IAW 51-40-2 & 51-30-2.Jan 5, 2006 · N490FE · Boeing 727200 · Fuselage Miscellaneous StructureSDR 06FDEA00039Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT NR 2 KRUGER FLAP WAS ACCOMPLISHED IAW SRM 57- 50-3, FIG. 3, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBER AND SPACING, GENERAL WORKMANSHIP,Jan 5, 2006 · N498FE · Boeing 727200 · Wing StructureSDR 06FDEA00038Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 344, STR 7L WAS ACCOMPLISHED IAW EO 7-5340-7-5002 PT1, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE, MATERIAL THICKNESS AND TYPE, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS Jan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00037Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CLAJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00036Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00035Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 312, STR 13L WAS ACCOMPLISHED IAW EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, TYPE, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER NUMBERS AND SPACING, GENERAL WORKMANSHIP, REPAIR IS CJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00034Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 227, STR20L WAS ACCOMPLISHED WITH SRM 53-30-3 FIG. 13, BASED ON AN EXTERNAL EVALUATION CONSISTS OF LOCATION, TYPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP AND REPAIR IS Jan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00033Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT ST.312, STR.9L WAS ACCOMPLISHED WITH ISSUED EO 7-5330-7-2345, BASED ON AN EXTERNAL EVAULATION CONSISTS OF LOCATION, SHAPE, SIZE, TYPE OF MATERIAL AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR IJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00032Repair · unknownFOUND EXISTING REPAIR AT STA 710, STR 26L WAS ACCOMPLISHED IAW ISSUED EA 7-5330-70412, BASED ON AN EXTERNAL VISUAL EVALUATION CONSISTS WITH LOCATION, SHAPE, TYPE OF MATERIAL AND THICKNESS, FASTENERS SPACING AND NUMBERS, GENERAL WORKMANSHIP, REPAIR CLASSIFIED AJan 5, 2006 · N498FE · Boeing 727200 · Aircraft StructuresSDR 06FDEA00031Skin · crackedLFEC SHOWS CRACK INDICATIONS AT MCD DOUBLER LOWER FASTNER ROW BS 523, 524, 525 BETWEEN STR 27L AND 28L. COMPLIED WITH FED EX EA 7-5330-95979.Jan 5, 2006 · N490FE · Boeing 727200 · Cargo/Baggage DoorsSDR 06FDEA0017Shutoff Valve · faultyA/C WOULD NOT MAINTAIN CABIN ALT ON CLIMBOUT. WOULD NOT MAINTAIN PSI IN AUTO-STANDBY OR MANUAL OR ANY BLEED. WHILE TROUBLSHOOTING ITEM FOUND THAT THE RT PACK WAS NOT OPERATING WHEN SELECTED ON, REMOVED AND REPLACED THE RT AIR SHUTOFF VALVE IN REF TO 727-20Jan 4, 2006 · N479FE · Boeing 727200 · Cabin Pressure Control SystemSDR 05FDEA04411Skin · damagedN00235 GRAVEL DAMAGE BS 620-720 STR 25L -20R. REMOVED GRAVEL DAMAGE BS 620-720 STR 25L-20R COMMON TO SKIN WITHIN LIMITS PER SRM 53-30-1 DETAIL 1 AND FIG 2.Dec 27, 2005 · N485FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04409Skin · corrodedN01499 WHILE PREPPING FOR CLOSE FOUND INTERNAL FUSELAGE SKIN CORRODED AT BS 684 STR 26R. REPAIRED INTERNAL FUSELAGE SKIN AT BS 684 STR 26R IAW SRM 53-30-3.Dec 27, 2005 · N490FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04408Flap Track · corrodedN0108, CORROSION ON UPPER SURFACE OF NR 6 FLAP TRACK AROUND BOTH AFT MOUNT BOLT HOLES AND CNT OB MOUNT BOLT HOLE. COMING REPLACED NR 6 FLAP TRACK IAW WC27X5708-03Dec 22, 2005 · N490FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA04394Stop Fitting · gougedN00757 FORWARD ENTRY DOOR AFT LOWER STOP PIN FITTING GOUGED. COMPLIED WITH FED EX EA 7-5210-91434.Dec 21, 2005 · N490FE · Boeing 727200 · Passenger/Crew DoorsSDR 05FDEA04389Repair · unknownFOUND PREVIOUSLY REPAIR INSTALLED AT STA. 1140, STR 20L WAS ACCOMPLISHED IAW SRM 53-30-3 FIG.1, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND TYPE, GENERAL WORKMANSHIP OF THE INSTALLADec 21, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04388Switch · malfunctionedPASSING FL250 RECEIVED INTERMITTENT LE FLAPS AMBER INDICATOR ON FORWARD PANEL WITH INTERMITTENT NR1 SLAT INDICATOR ON S/O AUX PANEL. RAN RED TABS WITH NORMAL EXTENSION TO FLAPS 30. REPLACED NR 1 SLAT RETRACT SWITCH IAW 27-82-011-4, REPLACED NR1 SLAT ACTUADec 21, 2005 · N465FE · Boeing 727200 · Leading Edge Slat Control SystemSDR 05FDEA04385Shear Tie · corrodedBS 970 STR 29L-30 TIE HAS CORROSION. REMOVED SHEAR TIE AT BS 970 STR 29L-30 AND REPLACED WITH NEW SHEAR TIE PER SRM 53-10-4.Dec 20, 2005 · N485FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04384Shear Tie · corrodedSHEAR TIE REPAIR STRAP BS 970 STR 29 L WL 148 HAS CORROSION. *S/D* REMOVED SHEAR TIE AT BS 970 STR 29L WL 148 AND INSTALLED NEW SHEAR TIE PER SRM 53-10-4.Dec 20, 2005 · N485FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04387Shear Tie · crackedN01277 BS 950F LBL 12 WL 140 SHEAR TIE CRACKED. REMOVED AND REPLACED SHEAR TIE IAW SRM 53-10-4, AND SRM 51-30-09.Dec 20, 2005 · N485FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04386Shear Tie · corrodedN01273 BS 950A S28-29R RBL10-15 SHEAR TIE HAS CORROSION. REMOVED AND REPLACED IAW SRM 51-30-2.Dec 20, 2005 · N485FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04381Repair · misinstalledFOUND PREVIOUSLY REPAIR AT STA 1183, STR 27R IS NOT IN CONFORMANCE WITH APPROVED FAA DATA. REMOVED EXISTING REPAIR, ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 3 AND SRM 51-30-2. REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.Dec 20, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04380Repair · misinstalledFOUND PREVIOUSLY REPAIR AT STA 1140, STR 22L DOES NOT CONFORM TO FAA APPROVED DATA. REMOVED EXISTING REPAIR AND ACCOMPLISHED WITH REPAIR IAW SRM 53-30-3, FIG 1, TABLE 1, REPAIR IS CLASSIFIED AS MAJOR PER FEDEX GMM 6-2-100.Dec 20, 2005 · N274FE · Boeing 727200 · Fuselage Main, Plate/SkinSDR 05FDEA04329Shear Tie · corrodedCORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 LBL 4. *S/D* CUT OUT DAMAGED SECTION OF SHEAR TIE AN AREA 1 X 3 INCH IN AFT CARGO BAY BS 1009 WL 136 LBL 4. FABRICATED NEW REPAIR DOUBLER FROM 7075T6 .080 LOT 655633. INSTALLED NEW REPAIR DOUBLER ALL IAWDec 15, 2005 · N490FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04328Frame · dentedFWD CARGO BAY FRAME I/B FLANGE DENTED AT BS 500, BETWEEN STR 23RT AND 24RT. *S/D* REPAIRED FRAME AT BS 500, STR 23R-24R PER SRM 51-40-3.Dec 15, 2005 · N490FE · Boeing 727200 · Fuselage Main, FrameSDR 05FDEA04344Repair · unknownFOUND PREVIOUS REPAIR ON UPPER LEADING EDGE OF LEFT WING AT NR 3 LEADING EDGE SLAT WAS ACCOMPLISHED IAW SRM 57-30-4, FIG 1. BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, MATERIAL TYPE AND THICKNESS, FASTENER SPACING AND NUMBERS, GENERAL Dec 15, 2005 · N274FE · Boeing 727200 · Wing StructureSDR 05FDEA04341Repair · unknownFOUND PREVIOUS REPAIR ON LOWER SURFACE OF RIGHT INBOARD AFT FLAP WAS ACCOMPLISHED IAW SRM 57-50-4 FIG 5, PAGE 12, BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPADec 15, 2005 · N274FE · Boeing 727200 · Wing StructureSDR 05FDEA04340Repair · unknownFOUND PREVIOUS REPAIR ON RIGHT WING NR 7 L/E SLAT WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 1 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENER SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSIFIED AS MAJOR PEDec 15, 2005 · N274FE · Boeing 727200 · Wing StructureSDR 05FDEA04339Repair · unknownFOUND PREVIOUS REPAIR ON LEFT WING NR 1 KRUEGER FLAP FWD SURFACE WAS ACCOMPLISHED IAW SRM 57-50-3, FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, FASTENERS SPACING AND NUMBERS, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR CLASSDec 15, 2005 · N274FE · Boeing 727200 · Wing StructureSDR 05FDEA04337Repair · unknownFOUND PREVIOUSLY REPAIR AT NR 5 KRUEGER FLAP WS 265.0 WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 3, BASED ON EXTERNAL EVALUATION CONSISTED OF LOCATION, SIZE, SHAPE, NUMBER OF FASTENERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED AS Dec 15, 2005 · N274FE · Boeing 727200 · Wing StructureSDR 05FDEA04336None · noneFOUND PREVIOUSLY REPAIR AT RT WING NR 6 KRUEGER FLAP WAS ACCOMPLISHED IAW SRM 57-50-3 FIG 2 BASED ON AN EXTERNAL EVALUATION CONSISTED OF LOCATION, SHAPE, SIZE, NUMBERS OF FASTENER AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP AND REPAIR IS CLASSIFIEDDec 15, 2005 · N274FE · Boeing 727200 · Standard Practices/StructuresSDR 05FDEA04335Repair · unknownFOUND PREVIOUSLY REPAIR AT STA 950A, STR 29L WAS ACCOMPLISHED IAW SRM 53-30-3, FIG 3 PAGE 13, BASED ON EXTERNAL VISUAL EVALUATION OF LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS AND SPACING, MATERIAL THICKNESS AND GENERAL WORKMANSHIP, REPAIR IS CLASSIFIED Dec 15, 2005 · N274FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA04333Repair · unknownFOUND REPAIR AT STA 950A, STR 29R WAS DETERMINED HAD BEEN ACCOMPLISHED IAW SRM 53-30-3 FIG 3 BASED ON EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED LOCATION, SHAPE, SIZE, FASTENER SPACING, NUMBERS, MATERIAL THICKNESS AND TYPE AND GENERAL WORKMANSDec 15, 2005 · N274FE · Boeing 727200 · Fuselage Main, StructureSDR 05FDEA04331Repair · unknownFOUND REPAIR LOCATED ON RIGHT WING L/E WING ROOT REPAIR REQUIRES EVALUATION FOR COMPLIANCE WITH FAA APPROVED DATA. REPAIR WAS DETERMINED ACCOMPLISHED IAW SRM 57-30-4 FIG 2 BASED ON AN EXTERNAL VISUAL EVALUATION WITH REPAIR INSTALLED, CONSISTED OF LOCATION, SHDec 15, 2005 · N274FE · Boeing 727200 · Wing Main, Frame StructureSDR 05FDEA04330Shear Tie · corrodedCORROSION ON AFT CARGO BAY SHEAR TIE BS 1009 WL 136 RBL 2.Dec 15, 2005 · N490FE · Boeing 727200 · Fuselage Internal Mounting StructureSDR 05FDEA04318Repair · unknownREPAIR LOCATED AT STA 303.9 STRINGER 15-L REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. ITEM NR 4, VISUALLY INSPECTED REPAIR AT STA 303.9 STRINGER 15-L. FOUND TO BE IAW SB 727-53A0198 AND EA 7-5Dec 15, 2005 · N486FE · Boeing 727200 · Aircraft StructuresSDR 05FDEA04290Keelbeam · corrodedREWORK REQUIRED FROM CARD N00363. REPAIR DOUBLER AT BS 980, STR 29R HAS PILLOWING AND CRACKED FASTENER HEADS. SUSPECT CORROSION ON INTERNAL BEAM. PILLOWING SEALANT STILL EXISTS ALONG INTERNAL BEAM. REPAIRED PER FED EX EA 7-5310-96552.Dec 13, 2005 · N490FE · Boeing 727200 · Fuselage Main, KeelSDR 05FDEA04295Repair · damagedEXISTING FLOORBEAM REPAIR UPPER CHORD AT BS 1130, RBL 5.5 - RBL 15.5 (10 X 2 INCH). REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REPAIRED PER FED EX EA 7-5310-91426.Dec 13, 2005 · N466FE · Boeing 727200 · Fuselage Main, Floor BeamSDR 05FDEA04210Stringer Clip · bentSTRINGER CLIP, IN MAIN CABIN, IS BENT AND HAS THREE OPEN HOLES AT STA 950F STR 7R. *S/D* REMOVED AND REPLACED STR CLIP AT BS 950F STR 7R IAW SRM 51-30-2.Dec 9, 2005 · N490FE · Boeing 727200 · Fuselage Main, Attach FittingsSDR 05FDEA04201Flap Track · corrodedLEFT WING I/B FLAP O/B TRACK FWD MOUNT HOLE-D HAS PITTING IN INNER BORE. REMOVED PITTING AND CORROSION IAW BAC OHM 57-40-01. FABRICATED AND INSTALLED IAW BAC OHM 57-40-01 AND FED EX EA 7-5710-91314, LT INBOARD FLAP OUTBOARD TRACK OVERSIZE HOLE-D. MINOR REPADec 9, 2005 · N220FE · Boeing 727200 · Trailing Edge FlapsSDR 05FDEA04173Switch · misinstalledAFT AIRSTAIR AMBER LT ILLUMINATED PRIOR TO BLOCKOUT- ADJUSTED BY MAINTENANCE WHEN AFT AIRSTAIR AMBER LT ILLUMINATED IN FLIGHT- RAN QRH RED TABS. ENT BY: 353958 MEL 08DEC05 10:15 IND ACN RELEASED FOR SERVICE PER MEL/CDL: 52-06-B CAT: C EXP: 16DEC05 C/Dec 8, 2005 · N288FE · Boeing 727200 · Door Warning System
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