JASC 5522

Service difficulty reports · 3,272

Reports filed under 5522 · Elevator, Plate/Skin, newest first.

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  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE jasc_code = '5522'
  ORDER BY difficulty_date DESC"

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SDR 05FDEA03854Skin · crackedIN THE RIGHT DETACHABLE ELEVATOR UPPER SURFACE AT STA XE 75 FOUND 1 EA CRACK 4 INCHES LONG. REMOVED EXISTING DOUBLER NEAR CRACK, CUT OUT DAMAGE, FABRICATED AND INSTALLED DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. TOUCH UP WHITE TOP COAT ON REPAIR DOUBLER IAW TF11Nov 17, 2005 · N302FE · Doug DC1030SDR MWEA050121Skin · temporaryLEFT ELEVATOR HAS A TEMPORARY SKIN INSTALLED AT STATION XE182 TO TIP WATCH ITEM NUMBER W000403. REMOVED AND REPLACED NEW SKIN SECTION.Nov 9, 2005 · N601ME · Doug MD88SDR DHL2005749004Skin · dentedFOUND LEFT ELEVATOR LOWER SURFACE DENTED 40" I/B FROM O/B TIP. REMOVED LT ELEVATOR LOWER SKIN PANEL AT ELEV STA 173.21 IAW B727 SRM 51-30-2 FIG 9 LOCATED AND DRILLED FASTENERS HOLES IN NEW PANEL ASSY P/N 65-25639-75 PO NR 540027 IAW B727 SRM 51-30-2 FIG 1. TOct 30, 2005 · N749DH · Boeing 7272J0SDR IXXA05SMN266SSkin · crackedDURING C CHECK INSPECT, LT HORIZ STAB ELEVATOR UPPER SKIN CRACKED ½, XE 200.2379. PERFORMED MAJOR REPAIR IAW FAA FORM 8110-3. REMOVED FASTENERS IAW DC8 SRM 51-1-21. REMOVED DAMAGED SECTION IAW SEMAN DWG # ED-4085. NDT INSPECTED REWORKED AREA IAW DC8 NDT SPOct 26, 2005 · N829BX · Doug DC871FSDR UPS05845766Skin · corrodedINSPECTION TYPE:CI 2AE POPPED RIVET HEADS AT I/B LOWER SKIN OF RT ELEVATOR AND OBVIOUS INTERNAL CORROSION. REMOVED AND REPLACED SKIN IAW SRM 55-2-1 PAGE 23 & 24, 51-01-22, 55-2-1 FIG 8, 51-1-21, 51-1-21D AND 51-3-0.Oct 25, 2005 · N813UP · Doug DC873FSDR 2005UALA01131Skin · damagedLT ELEVATOR UPPER SURFACE HAS A ONE SQUARE INCH AREA OF CORE DAMAGE AT 88 INCHES OUTBOARD OF INBD EDGE. REMOVED DAMAGE. ACP. LAYUP AND COOK PER SRM 51-70-05 & SRM 55-20-01.Oct 12, 2005 · N919UA · Boeing 737522SDR ASAA0580527Skin · deterioratedOKC - DURING HV-CHECK, RIGHT ELEVATOR GEARED TAB INBOARD TRAILING EDGE SKIN IS DETERIORATED. SMOOTHED DETERIORATED AREA AND INSTALLED REPAIR DOUBLER. (M)Oct 3, 2005 · N982AS · Doug DC983SDR IXXA05RNG108SSkin · corrodedDURING INSPECTION CHECK, FOUND A CORROSION ON RT ELEVATOR UPPER SURFACE, STA XE 246.875-XE 272. SKIN WAS REPLACED IAW DOUGLAS DRAWING 5654970 AND RIVETS WERE INSTALLED IAW DC8 SRM 51-1-21 PAGE 1-7.Sep 17, 2005 · N721CX · Doug DC872SDR AWXA200600250Skin · damagedPHX - DURING INSPECTION DISCOVERED RT ELEVATOR HAD TRAILING EDGE DAMAGED. MAINTENANCE REMOVED DAMAGED SECTION ON THE TRAILING EDGE OF THE RT ELEVATOR. FABRICATED REPAIR PARTS FROM 2024T3 IAW AMERICA WEST AIRLINES ENGINEERING REPAIR NR 26-5520-05256-HF1. INSSep 13, 2005 · N659AW · Airbus A320232SDR CA050922005Skin · damaged(CAN) DURING INSPECTION OF THE ELEVATOR IAW AD 2005-18-21 AND COMMUNIQUE NO. 261, SMOKING RIVETS WERE DISCOVERED IN THE LOWER SKIN OF BOTH ELEVATORS (2 IN THE LT, 4 IN THE RT). REQUIRED REPAIRS WERE CARRIED OUT.Sep 12, 2005 · Beech 1900CSDR 05FDEA02683Skin · nickedRT I/B ELEVATOR UPPER SURFACE FOUND NICK BETWEEN STA XE 225 AND XE 238. ACCOMPLISH EXTERNAL DOUBLER REPAIR IAW SRM 55-10-00 FIG 8 VOL I.Aug 26, 2005 · N556FE · Doug DC1010SDR ASAA0540381Skin · damagedYXX: DURING C-CHECK FOUND LT ELEVATOR UPPER IB SURFACE DAMAGED AT STA 24.00. REPAIRED IAW SRM. (K)Aug 10, 2005 · N778AS · Boeing 7374Q8SDR 05FDEA02347Skin · damagedRIGHT STAB I/B ELEV XE 61.875 EXISTING 1EA EXT REPAIR DOUBLER ON UPPER DETACHABLE SKIN. REPLACED REPAIR PER SRM 55-00-01 VOL 1 FIG 3 SHT 2 AND SRM 55-00-01 PG 2A, 2B VOL 1.Aug 9, 2005 · N564FE · Doug MD1010FSDR AWXA200501027Skin · delaminatedDURING C15 CHECK DISCOVERED LT ELEVATOR LEADING EDGE DELAMINATED 12 INCHES INBOARD FROM OUTBOARD HINGE. MAINTENANCE REMOVED DELAMINATED PLIES ON THE LEADING EDGE, 12 INCHES FROM OUTBOARD HINGE IAW BOEING 737-300 SRM 55-20-01-2 FIG 201. BONDED REPAIR PLIES TOAug 8, 2005 · N311AW · Boeing 7373G7SDR MALA050614Skin · damagedWARRANTY, 4Y/2Y RT ELEVATOR UPPER SURFACE HAS COMPOSITE DAMAGE 68 INCHES FROM I/B END. REPAIRED IAW MESABA EO NR S51031. REMOVED AND REINSTALLED ELEVATOR.Jul 27, 2005 · N370PX · Saab 340BSDR SWIA200515855Skin · damagedLT ELEVATOR EXTERNAL LWR SKIN 2 PLACES TRANSVERSE SMOOTH CREASES 6" LENGTH BY 0.011" D - APPROX 28" AND 39" FROM ELEV O/B TIP AND 6" FROM T/E (AREA FLAGGED, ITEM FOUND AT C-CHECK INSPECTION. REPAIRED IAW CRJ SRM 55-20-00 FIG 203.Jul 22, 2005 · N406SW · Cndair CL6002B19SDR DHL2005764003Skin · dentedRT. ELEVATOR LOWER SURFACE IS DENTED AT ELEVATOR STA 121. FOUND DENT OUT OF LIMITS. CUT OUT DAMAGE AREA IAW B727 SRM 55-20-1. FABRICATED DOUBLER REPAIR IAW B727 SRM 55-20-3. ALODINED AND PRIMED IAW B727 SRM 51-10-2. INSTALLED DOUBLER IAW B727 SRM 55-20-3 FIG.5Jul 15, 2005 · N764AT · Boeing 727264SDR USAA050846Skin · delaminatedCLT - FOUND ELEVATOR TOP SKIN CRACKED 3 INCHES TOP SURFACE. MAJOR, COMPOSITE REPAIR IAW EA 96681. (M)Jul 7, 2005 · N526AU · Boeing 7373B7SDR COMA0570081Skin · lightning strikeLIGHTNING STRIKE EXIT DAMAGE ON LT ELEVATOR TRAILING EDGE. REPAIRED ELEVATOR UPPER SKIN TRAILING EDGE IAW BOMBARDIER EO 601R-55-6779.Jul 5, 2005 · N317CA · Cndair CL6002C10SDR ASAA0540324Skin · delaminatedYXX - FOUND LT ELEVATOR LOWER SURFACE DELAMINATED. REMOVED DAMAGE AND REPAIRED IAW B737-40 SRM 51-70-04. (M)Jun 26, 2005 · N774AS · Boeing 7374Q8SDR RYNA200500024Skin · separatedTRAILING EDGE OF LEFT ELEVATOR AT STATION 76.547 IS SEPARATED APPROXIMATELY 1 INCH. ELEVATOR REPAIRED PER B757 SRM 51-70-04.Jun 24, 2005 · N526NA · Boeing 757236SDR IXXA05SMN90SSkin · delaminatedDURING ROUTINE C-CHECK INSPECTION, RT ELEVATOR. REMOVE AND REINSTALL GEARED TAB (EXTERNAL SKIN DELAMINATED). REMOVED GEARED TAB FROM RT ELEVATOR IAW MM 27-30-3. INSTALLED GEARED TAB (OVERHAULED CONDITION) IAW MM 27-30-3. FOR OPS CHECK SEE NR 0818.Jun 23, 2005 · N822BX · Doug DC871FSDR CA050623002Skin · crackedTHE ELEVATOR WAS REMOVED TO REPLACE THE TRAILING EDGE SPLINE AND REPAIR CRACKS IN THE LE SKIN NEAR THE OUTBOARD HINGE POINT. THE HORN AREA WAS DISMANTLED TO INSPECT THE INNER STRUCTURE. A TOTAL OF TWENTY CRACKS WERE FOUND IN THE VARIOUS PARTS OF THE STRUCTURJun 22, 2005 · Beech B100SDR UPS05844765Skin · crackedINSPECTION TYPE:C-2. LT ELEVATOR CONTROL TAB SKIN AND DOUBLER CRACKED AT INBD EYEBOLT ACCESS HOLE LWR SKIN. REMOVED AND REPLACED LT ELEVATOR CONTROL TAB ASSY PER TASK CARD 3016 STEP 13.Jun 5, 2005 · N705UP · Doug DC871FSDR USAA050668Skin · debondedCLT - FOUND ELEVATOR SKIN DISBOND 1 INCH, LEFT ELEVATOR LOWER SURFACE 6.2 INCHES FROM THE OUTBOARD EDGE. COMPOSITE REPAIR IAW SRM 51-70-17. (M)May 20, 2005 · N373US · Boeing 7373B7SDR SWAA051494Skin · crackedDURING SCHEDULED RON CHECK, FOUND LT ELEVATOR OUTBOARD T/E CRACKED APPROX 22 OUTBOARD OF ELEVATOR TAB. REPAIRED LT ELEVATOR PER SRM.May 20, 2005 · N654SW · Boeing 7373H4SDR P5CA0501357Skin · chafedLEFT INBOARD ELEVATOR TOP LEADING EDGE SKIN FOUND CHAFED. ACCOMPLISHED REPAIR PER BOEING INSTRUCTIONS 1-1HR8MP AND FAA FORM 8100-9.May 18, 2005 · N508MC · Boeing 747230BSDR 05FDEA01341Skin · dentedHORIZONTAL STABILIZER, RT, UPPER SIDE, THE ELEVATOR HAVE SEVERAL DENTS, IN ADDED, 2EA REPAIRS WITH CHERRYMAX. REMOVED EXISTING REPAIR AT ELEVATOR, STA XE206, AND INSTALLED BIGGER REPAIR COVERING DENT LOCATED AT STA XE200 IAW SRM 55-10-00, FIG 8.May 17, 2005 · N571FE · Doug DC1010SDR 05FDEA01219Skin · damagedDURING C2 CHECK, AN EXISTING REPAIR WAS FOUND ON LEFT ELEVATOR TOP SURFACE OUTBOARD OF RIB 17. NEW REPAIR ACCOMPLISHED PER SRM 55-20-00.May 6, 2005 · N802FD · Airbus A310324SDR ASAA0580213Skin · dentedFOUND DURING C-CHECK, LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE DENTED. INSTALLED REPAIR DOUBLERS. (M)Apr 20, 2005 · N958AS · Doug DC983SDR DHL2005741521Skin · dentedLEFT ELEV LWR SKIN HAS 3EA DENTS AFT OF NR 4 BALANCE BAY. DAMAGED AREA 3 EA DENTS FOUND TO BE OUT OF LIMITS IAW B727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 3" BY 2" ON LT ELEVATOR LOWER SKIN AND FABBED REPAIR DOUBLER FROM 2024T3 .032 DIM 5 3/4" BY 4" POApr 17, 2005 · N741DH · Boeing 7272Q9SDR C2XAO5SH021Skin · crackedSHV - DURING C-CHECK LT ELEVATOR ACCESS PANEL 335 HB, CUTOUT BENT. MAINTENANCE ON FURTHER EVALUATION FOUND LT ELEVATOR ACCESS PNL (CUTOUT)CRACKED. MAINTENANCE REMOVED THE DAMAGED AREA AND PERFORMED REPAIR IAW EC5520-01070. THE AIRCRAFT WAS APPROVED FOR RETUApr 5, 2005 · N16951 · Emb EMB145LRSDR 05FDEA00849Skin · damagedREPAIR NEEDS EVALUATION FOR FAA APPROVED DATA AND MAJOR OR MINOR CLASSIFICATION. LT ELEVATOR UPPER SURFACE T/E 6' O/B FROM I/B END (ITEM 35 OF LIST). REPAIRED ELEVATOR IAW E NR #6-5520-87201. REPAIR IS CLASSIFIED AS MINOR AS PER EA6-5520-87201 AND FEDEX GApr 5, 2005 · N419FE · Airbus A310SDR TIM2005F00003Skin · corrodedCORROSION FOUND ON LT AND RT ELEVATOR: AFT LOWER SPAR CAP LT SIDE, AFT LOWER SPAR CAP RT SIDE, LT OB HINGE, RT OB HINGE, RT CENTER HINGE, LT ELEVATOR TRIM TAB PUSH ROD, RT ELEVATOR TRIM TAB HORN. (K)Apr 4, 2005 · N127BA · Beech 1900SDR 05FDEA00831Skin · delaminatedLT ELEVATOR TOP SURFACE STA 473/ER19 HAS 3EA AREAS OF CORROSION. COMPLIED WITH FEDEX EA NR 6-5520-87163.Apr 4, 2005 · N419FE · Airbus A310SDR 05FDEA00828Skin · delaminatedLT ELEVATOR TOP SURFACE BETWEEN STA468/ER16 AND STA474/ER20 IS DELAMINATION. COMPLIED WITH EA NR 6-5520-87163.Apr 4, 2005 · N419FE · Airbus A310SDR DHL2005782560Skin · damagedACCOMPLISH IDENTIFICATION OF EXISTING REPAIR ON RT ELEVATOR LOWER SKIN AT STAB STA 106 PER ASTAR J/C NR FCD500001-001B. REPAIR ON RT ELEVATOR LWR SKIN AT STAB STA 106 FOUND TO BE IN NON-COMPLIANCE IAW 727 SRM 55-20-3 FIG 5. REMOVED REPAIRS 2 EA FOR INCORPARAMar 22, 2005 · N782DH · Boeing 727227SDR SIMA200509110Skin · crackedDURING MBV INSPECTION FOUND LT ELEVATOR LWR SKIN SURFACE CRACKED BETWEEN STA 99.9 AND 1280.0. REPLACED LT ELEVATOR IAW AMM. AIRCRAFT WAS RETURNED TO SERVICE. (SW21200504818) (K)Mar 21, 2005 · N641AE · Emb EMB145LRSDR 05FDEA00613Skin · dentedDURING INSPECTION FOUND 1 DENT WITH NICK ON THE LEADING EDGE OF DETACHABLE ELEVATOR OF LEFT HORIZONTAL STABILIZER BETWEEN THE STA XE 88.625 AND THE STA XE 93.975 (UPPER SIDE). REMOVED LEADING EDGE PANEL BETWEEN STA 88.625 TO STA 100.455 IAW MM 20-50-07. REPAMar 21, 2005 · N571FE · Doug DC1010SDR 05FDEA00534Skin · misrepairedCOMPLY WITH AGING 9 - AGING INSPECTION, HORIZONTAL STAB - REPAIR AT RT ELEVATOR INBOARD TRAILING EDGE. REPAIR EVALUATED AND FOUND NOT TO CONFORM TO AN EXISTING SRM REPAIR. NEW REPAIR ACCOMPLISHED PER SRM 55-21-11.Mar 15, 2005 · N451FE · Airbus A310222SDR CA050315011Skin · cracked(CAN) AN APPROX. 4 INCH CRACK WAS FOUND ON THE RT SIDE, UPPER REAR PORTION OF VERTICAL STAB. THE AREA IS JUST BELOW THE AFT LOWER FAIRING. THE AIRFRAME STRUCTURAL MANUAL CONTAINS A REPAIR SCHEME SPECIFIC TO THIS CRACKING. REF CHAP 55-00-00. REPAIRS ARE IN PRMar 14, 2005 · Pilats PC1245SDR DHL2005782528Skin · scratchedLT ELEV INBD BOTTOM SIDE HAS ALONG SCRATCH MARK. BURNISHED AREA ON LT ELEV I/B LOWER SKIN AND FOUND AREA CRACKED AND OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" AND 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" Mar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782527Skin · dentedLT ELEV STA 136 HAS 3 DENTS EACH. EVALUATED DENTS AT LT ELEVATOR STA 136 1ST A/Y=1.25/.017=73, 2ND 2.75/.03=91, WITHIN LIMITS AND 3RD OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2" AND FABBED DOUBLER FROM 2024T3 .032 PO AND 90Mar 11, 2005 · N782DH · Boeing 727227SDR DHL2005782525Skin · dentedLT ELEV IB BOTTOM AFT HAS 2 DENTS. EVALUATED 2 DENTS 1ST A/Y=1/.02=50 AND WITHIN LIMITS, 2ND IS OUT OF LIMITS IAW 727 SRM 55-20-1 FIG 1. CUT OUT DAMAGED AREA DIM 5/8" BY 1/2"AND FABBED DOUBLER FROM 2024T3 .032 PO NR 9002034 DIM 2 1/2" BY 2 1/4" IAW 727 SRM 5Mar 11, 2005 · N782DH · Boeing 727227SDR GTIA050115Fairing · crackedLEFT ELEVATOR FAIRING EDGE CRACKED STATION XE 171. TRIMMED LEFT ELEV FAIRING EDGE AT STATION XE 171. MATERIAL LOSS WITHIN LIMITS. TREAT AND PRIMED IAW SRM 51-10-3. (M)Mar 10, 2005 · N821NK · Doug DC982SDR 05FDEA00440Doubler · damagedREPAIR ON RT ELEVATOR I/B T/E LOWER SURFACE REQUIRES EVALUATION REF N00817. REMOVED EXISTING REPAIR AND INSTALLED CORRECT REPAIR IAW SRM 55-21-11 CONF 1 FIG 203 AND EA 6-5510-86111.Mar 8, 2005 · N446FE · Airbus A310SDR 05FDEA00422Skin · damagedREPAIR FUSELAGE AT LT ELEVATOR T/E AFT FROM OB END HAS NO DATA REF N00806. REMOVED AND INSTALLED CORRECT REPAIR IAW EA 6-5100-87090 REF A310 SRM 55-21-11, REPAIR NR 5 G.Mar 8, 2005 · N446FE · Airbus A310SDR USAA050358Skin · damagedPIT - Q4 - COMP SKIN LT ELEVATOR, 2.5 INCH LENGTH X .125 INCH WIDTH, COMPOSITE DAMAGE, STA 55 AT PANEL CENTER TOP SURFACE LT ELEV. INSTALLED REPAIR PLIES IAW SRM AND EA. (K)Mar 2, 2005 · N438US · Boeing 7374B7SDR UPS05844041Skin · crackedINSPECTION TYPE:C2 RT ELEVATOR UPPER SKIN SURFACE I/B SIDE HAS A LIGHTENING STRIKE WITH .5 INCH CRACK STA XE 50. NDT VERIFIED .5 INCH CRACK PER NDT SPM 06-10-01.001. STOP DRILLED CRACK IAW SRM 55-2-1 FIG 10. NDT VERIFIED CRACK TERMINATES AT STOP DRILL PER NFeb 16, 2005 · N811UP · Doug DC873FSDR ASAA0540129Skin · puncturedOKC - LT ELEVATOR HAS A SMALL PUNCTURE IN THE UPPER SKIN. COMPLIED WITH A GRAPHITE WET LAY-UP REPAIR IAW SRM. (K)Feb 7, 2005 · N709AS · Boeing 737490
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