Boeing 727-277

Service difficulty reports · 627

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '727277'
  ORDER BY difficulty_date DESC"

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SDR 07FDEA00541Unknown · noneDOORS, MAIN CARGO LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX1435-2. COMPLIED WITH EA 7-5230-102022 DOORS MAIN CARGO, LWR AFT CORNER EXTERNAL SKIN PERMANENT REPAIR P/N 52FX14 35-2.Feb 22, 2007 · N240FE · Boeing 727277 · Cargo/Baggage DoorsSDR 07FDEA00245Servo · unknownAFTER DEPARTING MIA WHILE CLEANING UP AIRCRAFT STAB CRUISE TRIM CIRCUIT BREAKER POPPED. CLIMBING THROUGH 17500 IT WAS DISCOVERED AIRCRAFT COULD NOT BE TRIMMED DOWN BELOW 0. REVIEWED QRH FOR GUIDANCE AND CONTACTED GOC AND MOCC FOR SUGGESTIONS. DECISION WAS MFeb 2, 2007 · N491FE · Boeing 727277 · Speed-Attitude Correction SystemSDR 07FDEA00102Landing Gear · failedLANDING GEAR FAILED TO RETRACT NORMALLY. FOLLOWED QRH PROCEDURE TEST 1: INTERMITTENT HORN SOUNDED WHEN RETRACTING FLAPS FROM 5' TO 2'. UNABLE TO TEST WING ANTI-ICE DUE TO SYSTEM OPERATING ALREADY. NOSEWHEEL STEERING ALIGNMENT APPEARED NORMAL. QRH STATES STJan 16, 2007 · N244FE · Boeing 727277 · Landing Gear Retraction/Extension SystemSDR 06FDEA04394Skin · misrepairedREPAIR LOCATED JUST AFT OF STA 1070 BETWEEN STR 20L-21L AND BETWEEN STA 1050-1070, BETWEEN STR 20L-21L. FOUND NOT TO BE INSTALLED USING APPROVED DATA. FOUND TO BE WITHIN 3" OF REPAIR AT STA 1050-1070, STR 1050-1070, STR 21L-22L, NO FASTENERS ABOVE REPAIR AT Dec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04393Stringer · damagedSTRINGER BETWEEN STA 265-285, STR 21L HAS SEVERAL NR 40 HOLES DRILLED IN STRINGER (FROM PREVIOUSLY INSTALLED REPAIR, REF N00918 & N01098). REMOVED STRINGER AND SPLICED IN NEW SECTION REF SRM 53-10-3 DETAIL 1, FIGURE 1, PAGE 4B. CLASSIFIED AS A MAJOR REPAIR.Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 06FDEA04392Frame · crackedFRAME AT ATTACH POINT STA 277 AT STR 21L IS CRACKED AT UPPER ATTACH HOLE TO SKIN. REMOVED DAMAGE AND REPAIRED FRAME REF SRM 53-10-4 FIG 11 PAGE 43. THIS IS CLASSIFIED AS A MAJOR REPAIR.Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04391Skin · misrepairedREPAIR LOCATED AT MED UPPER SKIN FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00910 AND SRM 52-00-3 FIG 3/4 DAMAGE HAS NOT BEEN CUT OUT PER SRM. REMOVED EXISTING DOUBLER, FABRICATED AND INSTALLED NEW DOUBLER REF SRM 52-00-3 FIG 3 PRIMED AND PADec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04390Skin · misrepairedREPAIR LOCATED ON RT WING NR 5 SLAT INBD TRACK FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00930 AND CMM/SRM, THERE IS NO JUSTIFIED DOCUMENT FOR INSTALLATION OF STAINLESS DOUBLER IN THIS LOCATION ACCOMPLISHED REPAIR OF NR 5 SLAT SKIN EXTENSIONDec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04389Skin · misrepairedEXT REPAIR LOCATED JUST AFT OF STA 700, STR 26L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00936 AND SRM 53-30-3 FIG 24, DOUBLER MISSING FASTENERS IN REPAIR AREA, RADIUS FILLER ALSO BENT. REMOVED DOUBLER, FABRICATED NEW DOUBLER AND FILLER. Dec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04388Skin · misrepairedEXTERNAL REPAIR LOCATED AT STA 710, STR 28R FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00937 AND SRM 53-30-3 INCORRECT BLIND FASTENERS ARE INSTALLED ON REPAIR. REMOVED BLIND FASTENERS BS 710 STR 28R AND REINSTALLED SOLID FASTENERS REF SRM 51Dec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04387Skin · misrepairedEXT REPAIR LOCATED AT APPROX STA STA 470-490 BETWEEN STR 21R-22R FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM # N00923 AND SRM 53-30-3 FIG 1 UPPER AND LOWER FASTENER ROWS DO NOT EXTEND BEYOND INTERNAL STRUCTURE. REMOVED DOUBLER, FABRICATED DOUBLEDec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04386Skin · misrepairedEXT REPAIR LOCATED AT APPROX STA 39-410 BETWEEN STA 21R- 22R FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM NR N00922 AND SRM 53-30-3 FIG 3 REPAIR HAS INSUFFICIENT FASTENER ROWS PAST INTERNAL STRUCTURE. REMOVED EXISTING SKIN REPAIR, INSTALLED NEW REDec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04385Skin · misrepairedREPAIR LOCATED AT STA 360 BETWEEN STR 15L-16L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM# N00920 AND SRM 53-30-3 FIG 2, REPAIR DOES NOT HAVE REQUIRED NUMBER OF FASTENER ROWS. REMOVED DOUBLER, EVALUATED REPAIR AND FOUND IT TO BE IAW WITH BACO DRADec 29, 2006 · N243FE · Boeing 727277 · Standard Practices/StructuresSDR 06FDEA04384Flange · corrodedAPU AIR INLET SOUND SUPPRESSOR AND MOUNTING FLANGE IN WHEEL WELL HAVE CORROSION ON MATING SURFACE. BLENDED FORWARD, AFT AND INTERCOSTAL HFEC FOR MATERIAL LOSS, FORWARD STIFFENER AND INTERCOSTAL BEYOND LIMITS, AFT STIFFENER, REPAIRED PER EA NR 7-5310-99309. RDec 29, 2006 · N243FE · Boeing 727277 · Fuselage Structure (General)SDR 06FDEA04383Skin · misrepairedREPAIR LOCATED AT STA 265-285, BETWEEN STR 20L-21L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00918 AND SRM 53-30-3 FIG 3. INSUFFICIENT AMOUNT OF FASTENERS AT FRONT ROW (NEEDS 4 ROWS). REMOVED REPAIR AND REPLACED WITH A DOUBLER AND TRIPLER Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04382Skin · misrepairedEXT REPAIR LOCATED AT STA 970-990, STR 18L FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM# N00957 AND SRM 53-30-3 PG 13-14. FASTENER ROWS ARE INSUFFICIENT AT AFT LOWER CORNER. REMOVED EXISTING DOUBLER, FABRICATED NEW DOUBLER AND INSTALLED REF SRM 53Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04381Skin · misrepairedFLUSH REPAIR LOCATED AT STA 188, BL 0 FOUND NOT TO BE INSTALLED USING APPROVED DATA. REF SNRM NR N00917 REF SRM 53-30-3 FIG 2 DAMAGE CUTOUT NOT PARALLEL TO STRINGER CENTERLINE AND AMOUNT OF FASTENERS INCORRECT. REMOVED EXISTING REPAIR, REF SRM 51-30-02 ENLARDec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04380Skin · misrepairedEXT REPAIR LOCATED BETWEEN STA 1148-1166 STR 30 AT BL 0. FOUND NOT TO BE INSTALLED USING APPROVED DATA, REF SNRM# N00949, REF SRM 53-30-3 FIG 3 ROWS OF FASTENERS. INSUFFICIENT AND SPACING INCORRECT REMOVED PREVIOUS REPAIR AND INTERCOSTALS FOR ACCESS. FABRICDec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04379Skin · damagedREPAIR LOCATED AFT OF STA 1070 BETWEEN STR 17L - 18L, FOUND NOT TO BE INSTALLED USING APPROVED DATA, SNRM# N00956 REF. SRM 53-30-3 FIG 3. THERE IS NO ALLOWANCE FOR TRIPLER INSTALLATION. INSTALLED REPAIR REF FED EX EA NR 7-5530-99315 AND AAR EA I060473 REV IRDec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04375Door Frame · crackedLT AFT SERVICE DOOR FWD FRAME IS CRACKED AT CUTOUT FOR GUIDE ARM, AT INBD LOWER CORNER. INSTALLED REPAIR DOUBLER REF EA NR I060464, FED EX EA NR 7-5210-105271. CLASSIFIED AS A MAJOR REPAIR.Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, StructureSDR 06FDEA04374Nut Plate · damagedNUT PLATE HOLE UNDER FLOORBOARD AT STA 1130 - 1183 LBL 15 IS DOUBLE DRILLED. REMOVED PNL NR 1148 FOR ACCESS. REMOVED DAMAGED AREA, FABRICATED REPAIR ANGLES FROM 7075-T6-.090. FABRICATED FILLER FROM 7075-T6-.125, TREATED PRIMED AND PAINTED REPAIR ANGLES AND Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 06FDEA04373Skin · damagedUPPER AFT FUSELAGE BS 1130 EXTERIOR SKIN BETWEEN STRINGER 4L AND 5L HAS A 2" LONG GOUGE WITH ADJACENT SCRATCH. BLENDED DAMAGE OUT OF LIMITS REF SRM 53-30-1 FIG 1. REMOVED DAMAGE AREA. FABRICATED REPAIR DOUBLER ALODINED, AND PRIMED DOUBLER BEVELED EDGES OF DDec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04371Skin · dentedEXT FUSELAGE HAS DENT AT STA 630 STR 23R REMOVED DAMAGE AND REPAIRED USING A SINGLE DOUBLER REPAIR, REF SRM 53-30-3 FIGURE 13A PGS 74C THROUGH 74F. CLASSIFIED AS A MAJOR REPAIR.Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04370Angle · corrodedFORWARD CARGO PIT DOOR SECOND FROM AFT FRAME ANGLE CORRODED 6" FROM BOTTOM EDGE OF DOOR REMOVED AND REPLACED TEE ANGLE REF SRM 51-30-2 PG 2. CLASSIFIED AS A MAJOR REPAIR.Dec 29, 2006 · N243FE · Boeing 727277 · Fuselage Miscellaneous StructureSDR 07FDEA00627Receptacle · crackedTHREE RECEPTACLES DEFECTIVE ON NR 3 PYLON STRUCTURE WHERE PANEL 5402 MOUNTS TO PYLON. REPLACED THE DEFECTIVE RECEPTACLES AT PYLON PANEL 5502 MOUNT AREA. IAW 727-200 SRM 51-30-2. REINSTALLED PANEL 5502.Dec 22, 2006 · N246FE · Boeing 727277 · Nacelle/Pylon, Main FrameSDR 06FDEA04253Floorbeam · corrodedMCD STA 950 FLOORBEAM BETWEEN RBL0 -24 THE 4 NUT PLATES HAVE CORROSION BETWEEN THEM AND THE FLOORBEAM. CORROSION FOUND OUT OF LIMITS. REMOVED DAMAGED AREAS AND REPAIRED IAW SRZ27-53-033.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04252Stringer · corrodedFOUND STRINGER CORRODED EXT FUSELAGE STA 1071-1080 RBL10 STR 29 R 8 RIVETS DISHED IN EXT SKIN. PERFORMED STR REPAIR IAW SRM 53-10-3 FIG 1.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Longeron/StringerSDR 06FDEA04251Skin · corrodedFOUND SKIN CORRODED EXT FUSELAGE STA 1067 TO 1070 RBL 12, SKIN BULGE AT 3 FASTENERS STR 27R. REPAIRED FUSELAGE SKIN IAW SRM 53-30-3 FIG 3 STA 1067 - 1070 STR 29R.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04250Floorbeam · corrodedFOUND CORROSION BETWEEN RBL 9 AND RBL 2 STA 540 FLOORBEAM, UNDERSIDE FWD PIT. REMOVED CORROSION, INSTALLED NEW FLOORBEAM AND SPLICES IAW SRM 51-40-4.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04249Floorbeam · corrodedSTA 540 LBL 9 FLOOR SUPPORT CORRODED FWD PIT REMOVED CORROSION FOUND OUT OF LIMITS. INSTALLED FLOOR SUPPORT AND REPAIR SPLICES IAW SRM 51-30-2 AND 53-10-5 FIG 4.Dec 16, 2006 · N245FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04233Skin · corrodedEXTERNAL FUSELAGE STA 1067 TO 1070 RBL 12 SKIN BULGE AT (3) FASTENERS. REPAIRED FUSELAGE SKIN IAW SRM 53 -30-3 FIG3 STA 1067 - 1070 STR 29R.Dec 13, 2006 · N245FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04232Fitting · damagedFUSELAGE MAIN FRAME TAIL JACK FITTING DRILL START REPAIR, P/N 25FX990-45 COMPLY WITH EA 7-5310-101994. COMPLIED WITH EA 7-5310-101994 FUSELAGE MAINFRAME TALL JACK FITTING DRILL START REPAIR.Dec 13, 2006 · N245FE · Boeing 727277 · Fuselage Main, Attach FittingsSDR 06FDEA04231Frame · corrodedDURING ACCOMPLISHMENT OF C CHECK MX, AAR AIRCRAFT SERVICES, IND CORROSION WAS FOUND COMMON TO THE FORWARD SIDE OF THE AFT FRAME AT THE NR 3 CARGO DOORWAY AT STA 1142.7 BETWEEN STRINGERS 25R AND 27R (RBL 26). THE DAMAGE WAS BLENDED TO A 20:1 RATIO AND VERIFIEDDec 13, 2006 · N244FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04217Skin · misrepairedREPAIR LOCATED AT 680-700 STR 27L-28L FOUND NOT TO BE INSTALLED USING APPROVED DATA. FILLER DOES NOT PICK UP 2 ADDITIONAL ROWS BEFORE BUTT SPLICE. REMOVED AND REPLACED DOUBLER FILLER ADDED ADDITIONAL ROWS. INSTALLED REPAIR BETWEEN STA 680-710, STR 27L-25R RDec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04216Skin · damagedPREVIOUSLY INSTALLED REPAIR INSTALLED ON THE LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER, WITH DEPTH OF DAMAGE AT .040". REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG 1 PG 2. THIS IS A MAJOR REPAIR ON WO NR 34160 SNRM NRDec 12, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04210Skin · misrepairedLT PASSENGER DOOR, LOWER HINGE CUTOUT DOUBLER, HAS INCORRECT FASTENER SIZE, ACCORDING TO SB 727-53A-0198 FIG 5 COMPLIED WITH FED EX EO NR 7-5330-7-2345 PT3. INSTALLED EXTERNAL DOUBLER REPAIR REF SB727-53AO0198 R3.Dec 11, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04199Skin · gougedPREVIOUSLY INSTALLED REPAIR ON LT OTBD FORE FLAP 10" FROM INBD END HAS GOUGE ON DOUBLER REMOVED DAMAGED DOUBLER AND INSTALLED NEW DOUBLER REF SRM 57-50-4 FIG PG 1. THIS REPAIR CLASSIFIED AS MAJOR ON WO NR 34610, SNRM NR N01238.Dec 8, 2006 · N244FE · Boeing 727277 · Trailing Edge FlapsSDR 06FDEA04198Floorbeam · corrodedCABIN FLOOR STRUCTURE CORROSION ON UPPER SURFACE OF BEAM STA 950, LBL 38-46 STR 17L. REMOVED CORRODED SECTION OF BS 950 AND REPAIRED REF EA NR 7-5310-109942 CLASSIFIED AS A MAJOR REPAIR ON WO NR 34610, SNRM # N00520.Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04197Depressor · wornAFT PIT NR 2 DOOR LWR SEAL DEPRESSOR HAS LIGHT WEAR. REMOVED AND REPLACED SEAL DEPRESSOR REF SRM 51-30-02.Dec 8, 2006 · N244FE · Boeing 727277 · Cargo/Baggage DoorsSDR 06FDEA04196Frame · damagedLT FOWARD CABIN, FRAME WEB BETWEEN STR 3L AND 4L HAS (7 EA.) UNPLUGGED HOLES. REMOVED DAMAGED AND REPAIRED WITH A FORMED SECTION REPAIR REF. SRM 51-40-03 PG 1-6.Dec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, FrameSDR 06FDEA04194Floorbeam · corrodedLT FWD CABIN FLOORBEAM UPPER CAP IS CORRODED AT STA 480, LBL 27-LBL32. CLASSIFIED AS A MAJOR REPAIR ON WO 34610, SNRM # N00525. REMOVED CORROSION, MATERIAL LOSS OUT OF LIMITS REF SRM 51-10-1. CUT OUT DAMAGED SECTION OF BEAM, FABRICATED REPAIR PARTS, TREAT ADec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Floor BeamSDR 06FDEA04195Skin · unknownREPAIR LOCATED AT STA 720D-720E AT STR 18L-19L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REMOVED EXISTING DOUBLER, FABRICATED NEW DOUBLER, ADDING ADITIONAL FASTENERS TO THE REPAIR. REF SRM 53-30-03 PG 76-82 AND DETAIL 3. THIS IS CLASSIFIED AS A MAJOR RDec 8, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04190Seat Track · corrodedLT FWD CABIN SEAT TRACK BEAM IS CORRODED FROM STA 580 - STA 620 LBL 45 REMOVED CORRODED SECTION OF SEAT TRACK AND REPLACED, REF SRM 53-10-1 FIGURE 3, SRM 53-10-2 FIGURE 7A.Dec 7, 2006 · N244FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04188Stringer · crackedLT VERTICAL STAB INTERIOR STRINGER 9L IS CRACKED AT INSPAR RIB CHORDS AT FIN STA 157.2. REMOVED DAMAGE AND REPAIRED REF SRM 51-40-4 FIGURE 3, PAGES 14-17. CLASSIFIED AS A MAJOR REPAIR ON WO 34160, SNRM NR N00685.Dec 7, 2006 · N244FE · Boeing 727277 · Vertical Stabilizer, Plate/SkinSDR 06FDEA04187Repair · misinstalledFOUND FLUSH REPAIR LOCATED AT APPROX STA 227.8, LBL 12, UPPER FUSELAGE ABOVE CAPT'S WINDOW. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPROVED DATA. REMOVED EXISTING NON-CONFORMING DOUBLER AND INSTALLEDDec 7, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04182Seat Track · corrodedMCD SEAT TRACK AT LBL 25, STA 948 - 958 HAS CORROSION. REMOVED AND REPLACED SEAT TRACK IAW 51-30-5. SEAT TRACK FABBED ON TRAVELER, T6/647796.Dec 7, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04181Seat Track · corrodedMCD - SEAT TRACK SPLICE AT LBL 25, STA 950-950 PLUS 20" HAS CORRODED FASTENERS, EXFOLIATION BETWEEN PARTS REMOVED SPLICE ANGLES. REMOVED CORROSION, SPLICE ANGLES OUT OF LIMITS. FABBED NEW ANGLES BATCH NR 9R000776001. TREATED AND PRIMED NEW ANGLES, INSTALLEDDec 7, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04175Seat Track · corrodedMCD, BL 0 SEAT TRACK BETWEEN STA 870 - 880 HAS CORRODED NUT PLATE HOLES, TOP AND BOTTOM SIDES OF TRACK. BLENDED SEAT TRACK, FOUND TO BE OUT OF LIMITS IAW SRM 53-10-1,FIG 3. REMOVED SEAT TRACK IAW SRM 51-10-5, FABRICATED NEW SEAT TRACK ON TRAVELER T6/647662, Dec 5, 2006 · N245FE · Boeing 727277 · Fuselage, Seat/Cargo Attach FittingsSDR 06FDEA04165Skin · misrepairedREPAIR LOCATED AT APPROX STA 294-312, STR 10L-11L FOUND NOT TO BE INSTALLED USING APPROVED DATA. REFERENCE BOEING SB 727-53A0198 AND SNRM NR N00375, THERE ARE INSUFFICIENT FASTENERS IN REPAIR. FABRICATED REPAIR DOUBLER, CAD PLATED, PRIME AND PAINTED REF BOEIDec 2, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/SkinSDR 06FDEA04163Skin · misrepairedREPAIR LOCATED AT STA 1030-1039 BETWEEN S26R-27R INSIDE AFT PIT FOUND NOT TO BE INSTALLED USING FAA APPROVED DATA. REF SNRM # 00574 AND SRM 53-30-3 FIG 2 DOES NOT HAVE REQUIRED NUMBER OF FASTENERS. REMOVED REPAIR DOUBLER STA 1030-1039 BETWEEN STR 26R AND S27Dec 2, 2006 · N244FE · Boeing 727277 · Fuselage Main, Plate/Skin
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